Page 4
SC-AMM-1-0-00 INTENTIONALLY LEFT BLANK Date of issue: : 2015-05-24 Revision No.: 5...
Page 5
SC-AMM-1-0-00 SportCruiser PiperSport RECORD OF REVISIONS Rev. Date and Revision name Changed pages Issue date signature Supplementation of LiFePo4 i, ii, iii, iv, 0-1, 0-5, 0-7, 2013-05-09 2013-09-05 battery 0-8, 0-9 Konečný Check of nose landing gear leg i, ii, iii, iv, 0-1, 0-5 to...
Page 6
SC-AMM-1-0-00 SportCruiser PiperSport RECORD OF REVISIONS Rev. Date and Revision name Changed pages Issue date signature Revision No.: - Date of issue: 2013-06-30 0 - 2...
Page 7
SC-AMM-1-0-00 SportCruiser PiperSport RECORD OF REVISIONS Rev. Date and Revision name Changed pages Issue date signature Date of issue: 2013-06-30 Revision No.: - 0 - 3...
Page 8
SC-AMM-1-0-00 SportCruiser PiperSport RECORD OF REVISIONS Rev. Date and Revision name Changed pages Issue date signature Revision No.: - Date of issue: 2013-06-30 0 - 4...
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 1 – GENERAL Contents Introduction ......................1-5 Airplane Classification ................... 1-6 1.2.1 Power Unit ....................1-6 1.2.2 Main Technical Data ................. 1-7 Airplane Manufacturer and Type Certificate Holder ..........1-11 Chapter Order ...................... 1-11 1.4.1 Page Numbering..................1-11 Warnings, Cautions and Notes ................
Page 18
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 1 – GENERAL INTENTIONALLY LEFT BLANK Revision No.: - Date of issue: 2013-06-30 1 - 4...
CHAPTER 1 – GENERAL Introduction In accordance with requirements of the ASTM LSA regulations, the Czech Sport Aircraft a.s., as manufacturer of SportCruiser / PiperSport airplane, provides information on maintaining airworthiness of the SportCruiser / PiperSport airplane. Information is also contained in the...
PiperSport CHAPTER 1 – GENERAL Airplane Classification SportCruiser / PiperSport airplane is two-seat, single engine, low-wing, all-metal airplane with fixed three-wheel landing gear. The airplane is designed for basic and advanced training and for leisure time flying. 1.2.1 Power Unit Power unit consists of: •...
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 1 – GENERAL Airplane Manufacturer and Type Certificate Holder Czech Sport Aircraft a.s. Na Záhonech 1177/212, 686 04 Kunovice Czech Republic www.czechsportaircraft.com; office@czechsportaircraft.com Fax: +420 576 519 394, Phone: +420 576 514 034 (Sales Dept.) Chapter Order Chapters in this manual are ordered in ascending sequence from No.
Refer to the SportCruiser / PiperSport Pilot′s Operating Handbook, Section 9 for actual Equipment list. Sources to Purchase Parts Spare parts can be ordered from CSA through the PS-28 Cruiser / SportCruiser / PiperSport Illustrated Parts Catalogue (Doc. No. CR-IPC-1-0-00). List of Disposable Replacement Parts...
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 1 – GENERAL 1.14 General Safety Information Safety must be considered the first priority when performing maintenance or service on an aircraft or part. To minimize the risk to both yourself and others, begin by thinking through each task that is to be performed before starting any work.
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 1 – GENERAL 1.15 Definitions and abbreviations ACCU Accumulator ADAHRS Air Data Attitude and Heading Reference System Annual condition inspection detailed inspection accomplished once a year on a LSA in accordance with instructions provided in the maintenance manual supplied with the aircraft. The purpose of the inspection is to look for any wear, corrosion, or damage that would cause an aircraft to not be in a condition for safe operation.
Page 29
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 1 – GENERAL Power unit (1 kW = 1.341 hp) liter (1 l = 0.22 UK gal = 0.264 US gal) pounds (1 lb = 0.4536 kg) force unit (1 lbf = 4.45 N) Line maintenance...
Page 30
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 1 – GENERAL Nautical Mile (1 NM = 1,852 m) Outside Air Temperature System is switched off or control element is in off-position System is switched on or control element is in on- position Overhaul maintenance, inspection, repair, or alterations that are only to be accomplished...
Page 31
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 2 – TIME LIMITS / MAINTENANCE CHECKS Contents General ........................2-3 Airframe life limitation .................... 2-3 Aircraft parts life limitation..................2-3 Ordering spare parts ....................2-4 Terms and list of aircraft regular maintenance works..........2-4 2.5.1 General .....................
Page 32
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 2 – TIME LIMITS / MAINTENANCE CHECKS INTENTIONALLY LEFT BLANK Revision No.: - Date of issue: 2013-06-30 2 - 2...
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 2 – TIME LIMITS / MAINTENANCE CHECKS General This chapter contains information about: • airframe life limitations • aircraft parts life limitations • terms and list of aircraft regular maintenance works • lubrication chart Airframe life limitation Initial airframe life is 5,000 FH.
2.5.1 General Authorization to perform Time Limits/Maintenance Checks and Inspections: Repairman (LS-M) or Mechanic (A&P) Maintenance system serves to maintain flight airworthiness of the SportCruiser / PiperSport airplane. Maintenance system is composed of special and scheduled inspections, which must be...
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 2 – TIME LIMITS / MAINTENANCE CHECKS INTERVAL, MUST INCLUDED TIME FLOWN DETERMINATION OF THE NEXT 100-FH INSPECTION. (g) Scheduled annual inspection contains works of 100-FH inspection and other specified works (inspections of airframe, engine and propeller).
Page 36
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 2 – TIME LIMITS / MAINTENANCE CHECKS SPECIAL INSPECTION AFTER FIRST 25 FH Aircraft S/N: ………………… TSN (FH): ………… Registration mark: ………………… TSN (cycles): ………… Page: 1 of 1 Chpt. Prescribed works Made by Checked by...
Page 37
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 2 – TIME LIMITS / MAINTENANCE CHECKS SCHEDULED SPECIAL INSPECTION Aircraft S/N: ………………… TSN (FH): ………… Registration mark: ………………… TSN (cycles): ………… Page: 1 of 1 Chpt. Prescribed works Made by Checked by Klassic 170 /3/R propeller 50 FH inspection Remove the propeller spinner.
Page 38
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 2 – TIME LIMITS / MAINTENANCE CHECKS SCHEDULED INSPECTION AFTER 25 FH or 50 cycles whatever occurs first Aircraft S/N: ………………… TSN (FH): ………… Registration mark: ………………… TSN (cycles): ………… Page: 1 of 1 Chpt. Prescribed works...
Page 39
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 2 – TIME LIMITS / MAINTENANCE CHECKS SCHEDULED INSPECTION AFTER 50 FH Aircraft S/N: ………………… TSN (FH): ………… Registration mark: ………………… TSN (cycles): ………… Page: 1 of 1 Chpt. Prescribed works Made by Checked by Landing Gear...
Page 40
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 2 – TIME LIMITS / MAINTENANCE CHECKS SCHEDULED ANNUAL PERIODICAL INSPECTION OR INSPECTION AFTER 100 FH Aircraft S/N: ………………… ………… TSN (FH): Registration mark: ………………… TSN (cycles): ………… Type of inspection: ………………… Page: 1 of 7 Chpt.
Page 41
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 2 – TIME LIMITS / MAINTENANCE CHECKS SCHEDULED ANNUAL PERIODICAL INSPECTION OR INSPECTION AFTER 100 FH Page: 2 of 7 Chpt. Prescribed works Made by Checked by Wing Visually check surface condition - loosened rivets, deformation, cracks and some other damage.
Page 42
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 2 – TIME LIMITS / MAINTENANCE CHECKS SCHEDULED ANNUAL PERIODICAL INSPECTION OR INSPECTION AFTER 100 FH Page: 3 of 7 Chpt. Prescribed works Made by Checked by Tail Unit (continued) Check for free travel of the rudder.
Page 43
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 2 – TIME LIMITS / MAINTENANCE CHECKS SCHEDULED ANNUAL PERIODICAL INSPECTION OR INSPECTION AFTER 100 FH Page: 4 of 7 Chpt. Prescribed works Made by Checked by Equipment (continued) Check attachment, security and routing of BRS activating handle.
Page 44
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 2 – TIME LIMITS / MAINTENANCE CHECKS SCHEDULED ANNUAL PERIODICAL INSPECTION OR INSPECTION AFTER 100 FH Page: 5 of 7 Chpt. Prescribed works Made by Checked by Fuel System Drain fuel tanks and gascolator (see 9.5.2).
Page 45
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 2 – TIME LIMITS / MAINTENANCE CHECKS SCHEDULED ANNUAL PERIODICAL INSPECTION OR INSPECTION AFTER 100 FH Page: 6 of 7 Chpt. Prescribed works Made by Checked by Electrical System Check attachment and condition of battery. Check level of battery charge.
Page 46
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 2 – TIME LIMITS / MAINTENANCE CHECKS SCHEDULED ANNUAL PERIODICAL INSPECTION OR INSPECTION AFTER 100 FH Page: 7 of 7 Chpt. Prescribed works Made by Checked by Operational and Functional Tests Check the function of the interior and exterior lighting.
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 2 – TIME LIMITS / MAINTENANCE CHECKS Lubrication chart After first Every Every Unit Area of lubrication Lubricant 25 FH 100 FH 500 FH Throttle control cable on the inlet into LPS1 terminal (in the engine compartment).
Page 48
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 2 – TIME LIMITS / MAINTENANCE CHECKS After first Every Every Unit Area of lubrication Lubricant 25 FH 100 FH 500 FH AeroShell Hinges. Grease 22 AeroShell Rod end bearings of the control tubes. Grease 22...
Page 49
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 2 – TIME LIMITS / MAINTENANCE CHECKS After first Every Every Unit Area of lubrication Lubricant 25 FH 100 FH 500 FH AeroShell Rudder hinges. Grease 22 Cable shackles on the rudder control AeroShell cables. Grease 22 Trim Tabs hinges.
Page 50
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 2 – TIME LIMITS / MAINTENANCE CHECKS After first Every Every Unit Area of lubrication Lubricant 25 FH 100 FH 500 FH Aileron, AeroShell elevator All movable links in the cockpit. Grease 22 control AeroShell All movable links in the cockpit.
Page 51
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 3 – FUSELAGE Contents General ........................3-3 Description and operation..................3-3 3.2.1 Front part of the fuselage ..............3-3 3.2.2 Rear part of the fuselage ............... 3-3 3.2.3 Cockpit....................3-4 3.2.4 Baggage compartment ................3-5 3.2.5 Crew canopy..................
Page 52
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 3 – FUSELAGE INTENTIONALLY LEFT BLANK Revision No.: - Date of issue: 2013-06-30 3 - 2...
CHAPTER 3 – FUSELAGE General SportCruiser / PiperSport fuselage is a semi-monocoque structure formed by stiffeners and aluminum sheet. The fuselage consists of the front part with the cockpit and the rear part, the integral part of which is the fin.
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 3 – FUSELAGE 3.2.4 Baggage compartment Baggage compartment (8, Fig. 3-3) is located between the seats and the bulkhead No. 7. Max. baggage weight transported in the baggage compartment is 18 kg (40 lbs). 3.2.5 Crew canopy The crew canopy is produced of organic glass and consists of opening canopy and rear fixed canopy windows.
(9, Fig. 3-3) and sliding ventilation windows located on both sides of the canopy. For newer models of the SportCruiser airplane closing and securing of the canopy is sensed by one terminal switch, located at the inside opening lever between the seats (see Wiring Manual).
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 3 – FUSELAGE Removal / Installation 3.3.1 Canopy removal Type of maintenance: line Authorization to perform: Sport pilot, Repairman (LS-M) or Mechanic (A&P) Tools needed: socket wrench 7/16” screwdriver pliers CAUTION: DURING CANOPY REMOVAL BE CAREFULLY TO AVOID SCRATCHING THE GLASS.
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 3 – FUSELAGE (b) Remove the lock (1). 1 Lock 2 Screw Fig 3-6: Canopy lock removal / installation 3.3.6 Cabin lock installation Type of maintenance: line Authorization to perform: Sport pilot, Repairman (LS-M) or Mechanic (A&P)
Page 61
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 3 – FUSELAGE CAUTION: USE ONLY ONE BALANCE BALLAST, NOT THEIR COMBINATION. MAX. WEIGHT OF BALLAST IS 0.8 KG. (a) By weighing or computation determine the mass of required ballast (mass of ballast: 0.25 kg or 0.5 kg or 0.8 kg; arm of ballast: 4,545 mm). Weighing process is given in the POH, Section 6.
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 3 – FUSELAGE Check / Adjustment 3.4.1 Canopy lock adjustment Adjust the locks so that the canopy could be locked freely. Set the length of the rod. 3.4.2 Towing gear control cable adjustment Adjust the length of towing gear control cable so that the control lever and hook lever in the open position touched the stops.
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 4 - WING General SportCruiser / PiperSport wing is an aluminum structure and is equipped with flaps, ailerons and fuel tanks. This chapter describes the structure of: • wings • wing flaps • ailerons • fuel tanks Fig.
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 4 - WING 1 Flap skin 2 Flap rib 3 Guiding plate 4 Flap hinge Fig. 4-3: Wing flap, left 4.2.3 Ailerons Ailerons (Fig. 4-4) are of aluminum structure consisting of the skin (1) aluminum sheet metal, spar and ribs (2) which are connected by means of riveting.
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 4 - WING 4.2.4 Fuel tanks Fuel tanks are of welded all-metal structure consisting of aluminum sheet metal skin (1, Fig. 4- 5) and two ribs (2). There are on each tank filler neck (3), fuel quantity sensor (4), venting tube (5), finger screen (6) and drain valve (7).
CHAPTER 4 - WING (d) Remove bushes (24, Fig. 4-6) (if installed) from the aileron control push rod (valid for SportCruiser airplanes from S/N C0416). (e) Remove cover (11, Fig. 4-7) on the bottom wing root. (f) Disconnect rear attachment bolts on rear spar.
Page 70
(l) Install bushes (24, Fig. 4-6) (if installed) to the aileron control push rod (valid for SportCruiser airplanes from S/N C0416). (m) Perform check the trim tab operation, flaps and ailerons deflections (see 6.4.3), possibly adjusting of theirs deflections (see 6.4.4).
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 4 - WING 4.3.3 Wing flap removal Type of maintenance: line Authorization to perform: Repairman (LS-M) or Mechanic (A&P) Tools needed: wrench size 7/16 in (a) Open the flap (1, Fig, 4-7) in full position. (b) Unscrew the nuts (5), remove the washers (6), bolts (4) and disconnect both flap hinges;...
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 4 - WING 4.3.4 Wing flap installation Type of maintenance: line Authorization to perform: Repairman (LS-M) or Mechanic (A&P) Tools needed: wrench size 7/16 in (a) Clean all attachments and apply lubricant on it (see 2.6). Do the same for the hinges on the wing.
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 4 - WING 4.3.6 Aileron installation Type of maintenance: heavy Authorization to perform: Repairman (LS-M) or Mechanic (A&P) Tools needed: wrench size 7/16 in pliers (a) Clean all attachments and apply lubricant on it (see 2.6). Do the same for the hinges on the wing.
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 4 - WING Check / Adjustment No procedures included. Exchanges / Service information No procedures included. Revision No.: - Date of issue: 2013-06-30 4 - 12...
Page 75
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 5 – TAIL UNIT Contents General ........................5-3 Description and operation..................5-3 5.2.1 Horizontal stabilizer ................5-3 5.2.2 Elevator with tabs .................. 5-4 5.2.3 Fin......................5-5 5.2.4 Rudder ....................5-6 Removal / Installation .................... 5-7 5.3.1 Horizontal stabilizer removal ..............
Page 76
SC-AMM-1-0-00 PS-28 Cruiser SportCruiser CHAPTER 5 – TAIL UNIT INTENTIONALLY LEFT BLANK Revision No.: - Date of issue: 2013-06-30 5 - 2...
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 5 – TAIL UNIT General Tail unit of SportCruiser / PiperSport airplane is of all-metal structure and is composed of: • stabilizer • elevator with tabs • • rudder. Description and operation 5.2.1 Stabilizer Stabilizer (1, Fig. 5-1) is of the all-metal structure consisting of the two spars, ribs and aluminum skin.
Mass balances (6) are riveted at the both elevator ends and covered composite tips (7). The elevator is equipped with the trim tab (2); newer SportCruiser airplanes also have balance tab (3). Both tabs are hinged by means of the piano hinge on the rear spar close to the trailing edge of the elevator.
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 5 – TAIL UNIT 5.2.3 Fin The vertical fin (1, Fig. 5-3) is of an aluminum structure and is an integral part with the rear part of the fuselage. The fin consists of stiffeners, spar, ribs and aluminum skin. Individual parts are assembled by riveting.
Individual parts are assembled by riveting. On the spar are two attachments lower one (3) and upper one (2) for the rudder suspension on the fin. Control lever (4) is riveted on root rib. On the trailing edge is riveted fixed trim tab (6) – only newer SportCruiser airplanes. 1 Rudder...
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 5 – TAIL UNIT Removal / Installation 5.3.1 Horizontal stabilizer removal Type of maintenance: heavy Authorization to perform: Repairman (LS-M) or Mechanic (A&P) Tools needed: wrench size 7/16 in screwdriver cutting pliers NOTE: For stabilizer removal three persons are requested.
Page 82
SC-AMM-1-0-00 PS-28 Cruiser SportCruiser CHAPTER 5 – TAIL UNIT (i) Perform check the trim tab operation and elevator deflections (see 6.4.3), possibly adjusting of elevator deflections (see 6.4.4). Fig. 5-5: Stabilizer, elevator removal / installation (page 1 of 2) Revision No.: -...
SC-AMM-1-0-00 PS-28 Cruiser SportCruiser CHAPTER 5 – TAIL UNIT NOTE: For elevator installation two persons are requested. (a) Inspect the hinges on the elevator, clean them and apply lubricant on them (see 2.6). Do the same for the hinges on the stabilizer.
Page 85
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 5 – TAIL UNIT 1 Trim tab Piano hinge 2 Control lever Rivet 3 Pin Balance tab 4 Washer 10 Control lever 5 Cotter pin 11 Control rod 6 Control rod Fig. 5-6: Elevator tabs removal / installation Date of issue: 2013-06-30 Revision No.: -...
SC-AMM-1-0-00 PS-28 Cruiser SportCruiser CHAPTER 5 – TAIL UNIT 5.3.7 Balance tab removal Type of maintenance: heavy Authorization to perform: Repairman (LS-M) or Mechanic (A&P) Tools needed: pliers, cutting pliers electric drill, drill diam. 3.2 mm (1/8 in) (a) Remove cotter pin (5, Fig. 5-6), washers (4), pin (3) and disconnect control rod (11) from the tab control lever (10).
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 5 – TAIL UNIT 5.3.10 Rudder installation Type of maintenance: heavy Authorization to perform: Repairman (LS-M) or Mechanic (A&P) Tools needed: wrench size 3/8 in, 7/16 in NOTE: For rudder installation two persons are requested. (a) Inspect the hinges on the rudder, clean them and apply lubricant on them (see 2.6). Do the same for the hinges on the fin.
Page 89
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 6 – CONTROL SYSTEM Contents General ........................6-3 Description and operation..................6-3 6.2.1 Lateral control..................6-3 6.2.2 Longitudinal control ................6-4 6.2.3 Directional control.................. 6-4 6.2.4 Elevator and aileron trim tab control............6-5 6.2.5 Wing flap control..................6-6 6.2.6...
Page 90
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 6 – CONTROL SYSTEM Check / Adjustment....................6-27 6.4.1 Check of play in control ............... 6-27 6.4.2 Check for friction in control system ............. 6-28 6.4.3 Checking control surface deflections........... 6-29 6.4.4 Adjustment of control surface deflections ........... 6-32 6.4.5...
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 6 – CONTROL SYSTEM 6.1 General SportCruiser / PiperSport airplane is equipped with dual controls which enables pilot training. Airplane control includes: • lateral control (aileron control) • longitudinal control (elevator control) • directional control (rudder control) •...
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 6 – CONTROL SYSTEM 6.2.2 Longitudinal control The elevator is controlled by control sticks. Movement of control sticks is transferred by system of transmission levers and push rods to the elevator. Forward and backward movement of the control stick is transferred by the push rod lead through the central channel between seats to the two-arm lever which is located under the baggage floor.
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 6 – CONTROL SYSTEM Fig. 6-3: Directional control scheme 6.2.4 Elevator and aileron trim tab control The elevator and aileron trim tabs are controlled by the electrical actuators installed in elevator/right aileron and connected per threaded rod with trim tab. Control switches are integrated part of grips.
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 6 – CONTROL SYSTEM 6.2.5 Wing flap control Wing flaps are controlled by electric flaps actuator connected with flaps per torque tube with control pins on each end. The flaps actuator located in fuselage under floor of baggage space and is controlled by a rocker switch located in cockpit.
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 6 – CONTROL SYSTEM 6.2.6 Autopilot system The EFIS D100 autopilot system is a digital flight control system that provides roll and pitch control. The system has the following components: - EFIS D100 - AP74 autopilot interface module...
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 6 – CONTROL SYSTEM 6.3 Removal / Installation 6.3.1 General principles for work on control system Push rod assembly Type of maintenance: heavy Authorization to perform: Repairman (LS-M) or Mechanic (A&P) Tools needed: wrench size 7/16 in Set the push rods to the prescribed length before assembling, tighten the nuts slightly, and do not secure them for the time being.
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 6 – CONTROL SYSTEM (b) Unscrew the nuts (17), remove the washers (18) and disconnect the aileron control rods (4) from sticks (2); remove the cases (19). (c) Remove the grips (3) and disconnect wires (24) for trim tab switches and PTT on the grips.
Page 98
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 6 – CONTROL SYSTEM 1 Transmission tube 14 Washer 2 Control stick 15 Nylon washer 3 Grip 16 Cotter pin 4 Aileron control rod 17 Nut 5 Bolt 18 Washer 6 Nut 19 Case 7 Washer...
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 6 – CONTROL SYSTEM 6.3.4 Flap control actuator removal Type of maintenance: line Authorization to perform: Repairman (LS-M) or Mechanic (A&P) Tools needed: wrench size 7/16 in, 1/2 in, screwdriver (a) Set the flap to the landing position; switch off electrical power of the airplane.
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 6 – CONTROL SYSTEM 6.3.5 Flap control actuator installation Type of maintenance: line Authorization to perform: Repairman (LS-M) or Mechanic (A&P) Tools needed: wrench size 7/16 in, 1/2 in, screwdriver (a) Fit the flap actuator (1, Fig. 6-8) to the actuator hinge (10), insert the bolt (3) to the hole, install the washer (5), screw and tighten the nut (4).
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 6 – CONTROL SYSTEM 6.3.7 Trim tab control actuator installation Type of maintenance: heavy Authorization to perform: Repairman (LS-M) or Mechanic (A&P) Tools needed: wrench size No.5 screwdriver pliers pliers for riveting (a) Fit the rod (6, Fig. 6-9) to the actuator rod, insert pin (7) with washer (8) into the hole, insert the washer (5) and secure with the new cotter pin (9).
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 6 – CONTROL SYSTEM 6.3.9 Installation of aileron control lever behind the seats Type of maintenance: heavy Authorization to perform: Repairman (LS-M) or Mechanic (A&P) Tools needed: wrench size 7/16 in (a) Check condition of the control lever and lubrication of the friction surfaces. If the friction surfaces are contaminated, then carefully remove contamination and grease them with lubricant (see 2.6).
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 6 – CONTROL SYSTEM 1 Two-arm lever 2 Bolt 10 Washer 3 Nut 11 Nylon washer 4 Washer 12 Cotter pin 5 Bolt 13 Control rod I 6 Nut 14 Control rod II 7 Washer For information:...
Page 105
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 6 – CONTROL SYSTEM NOTE: The bell cranks located on the bracket in the position of the rear rib No. 7 between the spars. Removal is identical for the left and the right aileron bell crank.
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 6 – CONTROL SYSTEM 6.3.11 Installation of aileron control bell crank in the wing Type of maintenance: heavy Authorization to perform: Repairman (LS-M) or Mechanic (A&P) Tools needed: wrench size 7/16 in screwdriver NOTE: Installation is identical for the left and the right aileron bell crank.
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 6 – CONTROL SYSTEM 6.3.12.2 Removal of middle two-arm lever (a) Remove the front cover (between bulkheads No. 8 and 9) at the bottom of the fuselage rear part. (b) Unscrew the nuts (5, Fig. 6-12), remove washers (6) and bolts (4) and disconnect rods (13;...
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 6 – CONTROL SYSTEM 6.3.13.2 Installation of middle two-arm lever (a) Check condition of the control lever and lubrication of the friction surfaces. If the friction surfaces are contaminated, then carefully remove contamination and grease them with lubricant (see 2.6).
Page 109
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 6 – CONTROL SYSTEM 1 Front two-arm lever 11 Cotter pin 2 Middle two-arm lever 12 Front control rod I 3 Rear two-arm lever 13 Front control rod II 4 Bolt 14 Middle control rod 5 Nut...
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 6 – CONTROL SYSTEM 6.3.14 Autopilot servos removal Type of maintenance: heavy Authorization to perform: Repairman (LS-M) or Mechanic (A&P) Tools needed: wrench size 7/16 in screwdriver pliers drill diam. 3.2 mm (1/8 in) electric drill...
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 6 – CONTROL SYSTEM 6.3.15.1 Installation of roll servo (a) Rivet the new bracket (3, Fig. 6-14) on the rear seat stiffener angle and lower fuselage skin. (b) Insert the servo (1) to the servo base (9), insert the bolts (4) with the washers (5; 6) to the holes and tighten the bolts;...
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 6 – CONTROL SYSTEM 6.4 Check / Adjustment 6.4.1 Check of play in control Admissible plays in control are mentioned in the following table: Control Admissible play Area to measure play longitudinal max 4 mm (5/32 in) at the end of the control stick in longitudinal axis of the airplane...
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 6 – CONTROL SYSTEM Lateral control Measure play at the end of the control stick by the measuring instrument from the fuselage side at blocked ailerons in the neutral position. First block the right aileron and measure play on the control stick, then measure play at the blocked left aileron.
CHAPTER 6 – CONTROL SYSTEM Fig 6-17: Friction in directional control system 6.4.3 Checking control surface deflections Control surface deflections of SportCruiser / PiperSport are shown in the following table: Valid for S/N P1102012, Valid for S/N 06SC001 P1102014, P1102015,...
Page 118
(d) Calculate angle and compare it with the value mentioned in the Tab. 6-1. Measuring trim tab deflections (PiperSport / early SportCruiser) (a) Set the gauge to the trailing edge of the trim tab (see Fig. 6-18).
Page 119
(e) Check values of deflections according to the Tab. 6-1. Fig 6-18: Measuring trim tab deflections Measuring trim tab deflections (SportCruiser) (a) Set the protractor with the deflecting pointer to the trailing edge of the trim tab by means of the clamp.
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 6 – CONTROL SYSTEM 6.4.4 Adjustment of control surface deflections Adjustment of control surface deflections to be made to the values showed in the Tab. 6-1. At adjusting the airplane control, neutral position of the control surfaces is taken as the starting point.
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 6 – CONTROL SYSTEM 6.4.5 Checking condition of rudder control cables. (a) Carefully inspect the control cable especially on the following areas: • in the area of cable attachment on the rudder control pedals • in the area of cable attachment on rudder lever •...
Page 122
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 6 – CONTROL SYSTEM (m) Check (see 6.4.3) and adjust (see 6.4.4) rudder deflections. (n) Secure the turnbuckle (4; 5; 6) with the lockwire. 1 Control cable 10 Cotter pin 2 Cable thimble 11 Cable shackle...
Description and operation 7.2.1 Seats Seats (1, Fig. 7-1) of the PS-28 Cruiser / SportCruiser airplane are fixed and are equipped with upholstered cushions attached on Velcro. The seat backs (2) are attached to the bulkhead No. 4 per piano hinge.
NOTE: For detailed information refer to Owner's Manual for BRS-6 Emergency Parachute Recovery Systems (Doc. No. 020000-03) and Parachute Installation Manual for the BRS-1350 onto the Czech Sport Aircraft PS-28 Cruiser & SportCruiser (Doc. No. 020016-PM), latest revision. 1 Parachute...
PiperSport CHAPTER 7 – EQUIPMENT The ELT main unit is mounted in baggage compartment; some SportCruiser airplanes from S/N C0416 have ELT main unit mounted below the right instrument panel (see Fig. 7-6). The remote switch unit with the buzzer is mounted on the right instrument panel; the ELT antenna is installed on the upper part of the fuselage.
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 7 – EQUIPMENT 1 Attachment bracket 4 Nut 2 Bushing 5 Washer 3 Bolt Fig. 7-3: Safety harnesses removal / installation 7.3.4 BRS parachute removal Type of maintenance: heavy Authorization to perform: Repairman (LS-M) or Mechanic (A&P)
Page 129
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 7 – EQUIPMENT WARNING: UNAUTHORIZED PERSONNEL SHOULD NOT ATTEMPT TO MODIFY, REPAIR, OR DISASSEMBLE BRS SYSTEM AT ANY TIME. DURING ALL SERVICE WORK BEWARE OF ACTIVATING THE BRS ROCKET! NOTE: BRS parachute must be removed from the aircraft for repacking. This service date is printed on placards located on the side of centre panel and on the parachute.
ALL SERVICE WORK BEWARE OF ACTIVATING THE BRS ROCKET! (a) Install the parachute – see Parachute Installation Manual for the BRS-1350 onto the Czech Sport Aircraft PS-28 Cruiser & SportCruiser (Doc. No. 020016-PM), points 2.8 to 2-17, and 3-5 to 3.11.
Page 131
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 7 – EQUIPMENT WARNING: NEVER POINT ROCKET AT ANYONE. ACCIDENTAL ACTIVATION MAY CAUSE DEATH OR SERIOUS INJURY! ASSEMBLY MUST BE DONE IN THIS SEQUENCE. IF DONE INCORRECTLY, ACCIDENTAL DISCHARGE OF ROCKET MAY OCCUR AND MAY CAUSE DEATH OR SERIOUS INJURY! (c) Remove plastic cap (6).
3-11. (e) Connect the activation housing to the rocket - see Parachute Installation Manual for the BRS-1350 onto the Czech Sport Aircraft PS-28 Cruiser & SportCruiser (Doc. No. 020016-PM), points 5.1 to 5-7. (f) Glue (by means of the Emfimastic PU 50 sealant) the cover over parachute on the canopy fixed frame.
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 7 – EQUIPMENT 7.3.8 ELT antenna installation Type of maintenance: line Authorization to perform: Repairman (LS-M) or Mechanic (A&P) Tools needed: wrench No. 3/4 in (a) Remove the protective cover from the antenna connector. (b) Insert the antenna (4, Fig. 7-6) to the hole in the fuselage upper part (7).
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 7 – EQUIPMENT 7.4 Check / Adjustment 7.4.1 Checking of safety harnesses Check harnesses surface for any damages. Check the lock system function. Check the attachment points of shoulder and side harnesses for any damages or corrosion.
Page 136
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 7 – EQUIPMENT INTENTIONALLY LEFT BLANK Revision No.: - Date of issue: 2013-06-30 7 - 14...
Page 137
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 8 – LANDING GEAR Contents General ........................8-3 Description and operation..................8-3 8.2.1 Main landing gear .................. 8-3 8.2.1.1 Main landing gear wheel ............ 8-4 8.2.2 Nose landing gear ................. 8-5 8.2.2.1 Nose landing gear wheel ........... 8-6 8.2.3...
Page 138
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 8 – LANDING GEAR INTENTIONALLY LEFT BLANK Revision No.: - Date of issue: 2013-06-30 8 - 2...
CHAPTER 8 – LANDING GEAR General SportCruiser / PiperSport airplane landing gear is of three-wheel fixed design and consists of the main landing gear and the nose landing gear. The nose landing gear is freely rotatable. The main landing gear wheels are equipped with hydraulic disc brakes.
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 8 – LANDING GEAR 8.2.1.1 Main landing gear wheel Main landing gear wheel rim (2; 3, Fig. 8-2) is pressed of aluminum. Wheel rim is split in order to facilitate assembly and disassembly of tire. Both halves are joined by bolts (9). Main landing gear wheels are equipped with the brake discs (7) which are attached to the inner half of the wheel rims (3).
CHAPTER 8 – LANDING GEAR 8.2.2 Nose landing gear The nose landing gear of SportCruiser / PiperSport airplane is not steerable and consists of steel welded landing gear leg (1, Fig. 8-3), aluminum fork (1, Fig. 8-4), shock absorber (2, Fig.
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 8 – LANDING GEAR 8.2.2.1 Nose landing gear wheel The nose landing gear wheel rim (2; 3, Fig. 8-4) is pressed of aluminum. Wheel rim is split in order to facilitate assembly and disassembly of tire. Both halves are connected by bolts (9).
CHAPTER 8 – LANDING GEAR 8.2.3 Brake system SportCruiser / PiperSport airplane is equipped with hydraulic disc brakes on the main landing gear wheels. Brake system consists of the brake pedals (part of rudder control pedals, see Fig. 8-9), brake pumps, parking brake valve, hoses for brake fluid supply, brake calipers and brake pads.
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 8 – LANDING GEAR Removal / Installation 8.3.1 Removal of main wheel fairing Type of maintenance: line Authorization to perform: Sport pilot, Repairman (LS-M) or Mechanic (A&P) Tools needed: Phillips PH2 screwdriver (a) Unscrew the bolts (4, Fig. 8-6) with the washers (5) (if used) attaching the wheel fairing (1) on the brackets (2;...
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 8 – LANDING GEAR 8.3.3 Removal of main landing gear wheel Type of maintenance: line Authorization to perform: Sport pilot, Repairman (LS-M) or Mechanic (A&P) Tools needed: socket wrench size 1 1/2 in Allen wrench size 3/16 in...
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 8 – LANDING GEAR 8.3.4 Installation of main landing gear wheel Type of maintenance: line Authorization to perform: Sport pilot, Repairman (LS-M) or Mechanic (A&P) Tools needed: socket wrench size 1 1/2 in Allen wrench size 3/16 in pliers (a) Clear the wheel axle (2, Fig.
Page 147
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 8 – LANDING GEAR 1 Front part of the nose wheel fairing 4 Bolt (10 pcs.) 2 Rear part of the nose wheel fairing 5 Wheel bracket 3 Bolt (8 pcs.) 6 Tow bracket Fig. 8-8: Nose wheel fairing removal / installation Date of issue: 2013-06-30 Revision No.: -...
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 8 – LANDING GEAR 8.3.7 Removal of nose landing gear wheel Type of maintenance: line Authorization to perform: Sport pilot, Repairman (LS-M) or Mechanic (A&P) Tools needed: wrench size 1 1/8 in pliers (a) Jack and support the airplane (see 14.2).
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 8 – LANDING GEAR 8.3.8 Installation of nose landing gear wheel Type of maintenance: line Authorization to perform: Sport pilot, Repairman (LS-M) or Mechanic (A&P) Tools needed: wrench size 1 1/8 in pliers (a) Clear the wheel axle (2, Fig. 8-9) of impurities and grease it slightly.
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 8 – LANDING GEAR 8.3.14 Installation of brake pumps Type of maintenance: line Authorization to perform: Sport pilot, Repairman (LS-M) or Mechanic (A&P) Tools needed: wrench size 1/2 in, 3/8 in (a) Insert the brake pump (1; 2, Fig. 8-12) according to the figure to the floor bracket (14) and install the bolt (4) with the nut (5) and washer (6);...
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 8 – LANDING GEAR 8.4 Check / Adjustment 8.4.1 Check of nose landing gear shock absorber a) Several times hoist and lower the nose landing gear of the airplane. (b) Measure value of absorber and nose landing gear compression according to Fig. 8-13.
Page 155
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 8 – LANDING GEAR (h) Torque castellated nut (3) so a constant force of 4-6 kg is required to rotate nose wheel fork. Take attention that nut does not spin against spindle (1) because there is a risk of cotter pin shear.
Page 156
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 8 – LANDING GEAR (e) Check tire worn and specified inflation (1.2 + 0.1 bar (17.4 + 1.5 psi)). CAUTION: DO NOT EXCESS SPECIFIED TIRE PRESSURE OVERPRESSURED TIRE CAUSED SHIMMY. Check condition of spring washers (3). Keep washers free of lubricants. Remove cotter pin (6), loose nut (5) and clean washers (2;...
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 8 – LANDING GEAR 8.4.3 Check of nose landing gear leg for cracks Tools needed: Flashlight 10x magnifier (a) Remove key from ignition switch and disconnect battery. (b) Remove the nose wheel fairing (see 8.3.5). (c) Visually inspect the bottom side of the nose landing gear leg lower section, in the place of the weld of the tube and the bracket (see Fig.
Page 158
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 8 – LANDING GEAR Fig. 8-16: Inspected area of the nose landing gear leg Revision No.: 2 Date of issue: 2013-10-11 8 - 22...
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 8 – LANDING GEAR Changes / Service infor mation 8.5.1 Tire change Type of maintenance: line Authorization to perform: Sport pilot, Repairman (LS-M) or Mechanic (A&P) Tools needed: wrench size 1/2 in Allen wrench size 1/4 in (a) Jack and support the airplane (see 14.2).
Page 161
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 8 – LANDING GEAR (h) Gradually install on the tube end (1) washers (5; 7; 6; 8), screw and tighten the nut (9); secure it with new cotter pin (10). (i) Put the lower end of the tube (1) to the bracket (16); install the bolt (11) with the nut (13) and washers (12), secure nut with the new cotter pin (10).
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 8 – LANDING GEAR 8.5.3 Change of brake lining Type of maintenance: line Authorization to perform: Sport pilot or higher Tools needed: wrench size 7/16 in drill # 25 electric drill brake relining tool, pneumatic press...
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 8 – LANDING GEAR NOTE: The lining requires replacement when the wear indicator is no longer visible. Fig. 8-19: Change of brake lining 8.5.4 Lubrication of axis of rotation of nose landing gear Type of maintenance: line...
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 8 – LANDING GEAR 8.5.5 Refilling / exchanging brake fluid Draining brake fluid from brake system Type of maintenance: line Authorization to perform: Sport pilot or higher Tools needed: wrench size 7/16” (a) Disconnect the brake hose from the brake cylinder and let brake fluid drain into the previously prepared can.
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 8 – LANDING GEAR 8.5.6 Bleeding the brake system Type of maintenance: line Authorization to perform: Sport pilot or higher Tools needed: wrench size 7/16” brake bleeder unit (a) Open the brake bleeder valve (6, Fig. 8-19) slightly on the brake caliper to facilitate bleeding of air from the system.
Page 166
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 8 – LANDING GEAR (d) If properly conditioned, the pads will have a uniform shiny appearance (glaze) on the surface. Repeat steps (a) – (c) if necessary to produce glaze. NOTE: Forward movement of the airplane during runup could be caused by the wheels skidding and not brake malfunction.
Page 167
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 9 – FUEL SYSTEM Contents General ........................9-2 Description and operation..................9-6 9.2.1 Fuel storage................... 9-6 9.2.2 Fuel distribution ..................9-6 9.2.3 Indication of fuel quantity and pressure..........9-7 Removal / Installation .................... 9-8 9.3.1 Fuel tank removal .................. 9-8 9.3.2...
Page 168
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 9 – FUEL SYSTEM INTENTIONALLY LEFT BLANK Revision No.: - Date of issue: 2013-06-30 9 - 2...
The fuel system (see Fig. 9.1) is used for storing fuel in the airplane and it’s delivering to the engine. The fuel system of SportCruiser / PiperSport airplane consists of the following parts: two fuel tanks, fuel tubing, selector valve, gascolator, mechanical fuel pump (located on the engine), electrical fuel pump, fuel quantity sensor, fuel flow-meter, fuel pressure sensor and drain valves of the fuel tanks.
Page 170
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 9 – FUEL SYSTEM Fig. 9-1: Fuel system layout (page 2 of 4) Revision No.: - Date of issue: 2013-06-30 9 - 4...
Page 171
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 9 – FUEL SYSTEM Fig. 9-1: Fuel system layout (page 3 of 4) Date of issue: 2013-06-30 Revision No.: - 9 - 5...
Page 172
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 9 – FUEL SYSTEM Fig. 9-1: Fuel system layout (page 4 of 4) Revision No.: - Date of issue: 2013-06-30 9 - 6...
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 9 – FUEL SYSTEM Description and operation 9.2.1 Fuel storage Fuel is stored in airplane in the fuel tanks. The fuel tanks are welded from Al-alloy sheet and their volume is 57 liters (15 US gallons) each. The tanks are located in the outer wings between ribs No.4 and 6a in front of the main spar.
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 9 – FUEL SYSTEM fuel system and eliminates all mechanical impurities. The electrical fuel pump (6) is located on the firewall above the gascolator. 1 Fuel tank, left 5 Gascolator 2 Fuel tank, right 6 Electrical fuel pump...
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 9 – FUEL SYSTEM 9.3.2 Fuel tank installation Type of maintenance: heavy Authorization to perform: Repairman (LS-M) or Mechanic (A&P) Tools needed: wrench size No. 8, 1/2 in, screwdriver riveting pliers cutting pliers, pliers (a) Remove any hole seals from the tank.
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 9 – FUEL SYSTEM 9.3.4 Installation of the finger screen Type of maintenance: line Authorization to perform: Repairman (LS-M) or Mechanic (A&P) Tools needed: Screwdriver Socket wrench 11/16 inch (a) Screw the finger screen (2, Fig. 9-5) into the root tank rib – use LOCTITE 565 or equivalent sealant on finger screen thread.
Page 178
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 9 – FUEL SYSTEM 1 Fuel quantity sensor 5 Wire 2 Gasket 6 Cover plate 3 Bolt 7 Rivet 4 Washer Fig. 9-6: Fuel quantity sensor removal / installation 9.3.6 Fuel quantity sensor installation Type of maintenance: line Authorization to perform: Sport pilot, Repairman (LS-M) or Mechanic (A&P)
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 9 – FUEL SYSTEM (a) Set the gasket (2, Fig. 9-6) on the fuel tank flange. (b) Set position and length of the fuel quantity sensor lever according to the Fig. 9-4. (c) Carefully put the fuel quantity sensor (1) into the tank and attach it using bolts (3) with washers (4) –...
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 9 – FUEL SYSTEM 9.3.8 Fuel drain valve installation Type of maintenance: line Authorization to perform: Sport pilot, Repairman (LS-M) or Mechanic (A&P) Tools needed: wrench size 1/2 in (a) Screw the drain valve (1, Fig. 9-7) in the tank (2) or gascolator – use LOCTITE 565 or equivalent sealant on the drain valve thread.
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 9 – FUEL SYSTEM Exchanges / Service information 9.5.1 Fuel tank filling CAUTION: WHEN FILLING FUEL IN THE AIRPLANE, USE ONLY APPROVED KINDS OF FUEL MENTIONED IN THIS MANUAL IN 10.2.1, IN THE POH SECTION 2.4, IN THE ROTAX OPERATOR’S MANUAL SECTION 10.2.2 FUEL, IN THE ROTAX SERVICE INSTRUCTIONS SI-912-016.
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 9 – FUEL SYSTEM 9.5.3 Fuel filter cleaning Perform fuel filter cleaning at each scheduled maintenance or signs of irregular engine running Cleaning procedure (a) Move the fuel selector valve to the OFF position. (b) Use the drain valve to drain the existing fuel from the gascolator bowl.
Page 183
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 10 – POWERPLANT Contents 10.1 General ........................ 10-3 10.2 Description and operation..................10-3 10.2.1 Engine ....................10-3 10.2.1.1 Engine mount..............10-4 10.2.1.2 Engine cowling..............10-4 10.2.1.3 Engine control ..............10-5 10.2.1.4 Engine instruments ............10-5 10.2.1.5 Engine cooling system .............
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 10 – POWERPLANT Fuel type: MOGAS (EN228 Super or EN228 Super plus with max. 5 % ethanol blend, min RON 95; ASTM D4814, min. AKI 91); AVGAS (100LL; ASTM D910; ASTM D7547). Refer to the Rotax Operator’s Manual, Section Section 2.4 Operating media - Fuel, Rotax Service Instructions SI-912-016, latest revision.
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 10 – POWERPLANT The lower cowling (2) is attached by means of quick fasteners (4) to the firewall and to the upper cowling (1). In the front part of the lower cowling (2), there is an oval hole (3) for air inlet to the radiator.
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 10 – POWERPLANT Fig. 10-3: EMS D-120 10.2.1.5 Engine cooling system Engine cooling is combined, cylinder heads are liquid cooled, and cylinders are air cooled. Cooling circuit of cylinder heads is made as a closed system containing the pump (5, Fig.
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 10 – POWERPLANT 10.2.1.6 Engine lubrication system Engine lubrication system is made with the dry sump. Engine lubrication system is equipped with the mechanically driven oil pump (3, Fig. 10-5) with oil filter (6) which ensures oil supply from the oil tank (4) located on the firewall through the thermostatic valve (9) (if used) and the oil cooler (5) to the lubricated points on the engine.
10.2.1.8 Exhaust system Exhaust system of SportCruiser / PiperSport airplane consist of four exhaust tubes (1, Fig. 10-7) which lead exhaust gases from individual cylinders to the muffler (2). The muffler serves at the same time as a silencer. Exhaust gases are led from there by the exhaust tube (3) down the airplane.
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 10 – POWERPLANT 1 Exhaust tube 4 Spring 2 Muffler 5 Heat exchanger 3 Outlet exhaust tube 6 Spring Fig. 10-7: Exhaust system 10.2.1.9 Ignition system The engine is equipped with the double contactless ignition system. Every ignition circuit has its source of energy, control unit, 2-ignition coils and 4-spark plugs.
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 10 – POWERPLANT 10.2.2 Propeller The Woodcomp Klassic is a three-blade ground adjustable composite propeller designed for the airplanes with piston engines with power up to 75 kW (100 hp) and max. propeller speed up to 2,600 rpm.
Page 193
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 10 – POWERPLANT Propeller type: 3B0R5R68C Max. speed: 5,800 rpm engine Diameter: 1.73 m (68 in) Pitch setting: No. 4 Fig. 10-9: SR 3000 propeller control scheme NOTE: For detailed information refer to: - Operator´s Manual Electrical Adjustable Aircraft Propeller SR 3000;...
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 10 – POWERPLANT 10.3 Removal / Installation 10.3.1 Removal of the engine from the airplane Type of maintenance: heavy Authorization to perform: Repairman (LS-M) or Mechanic (A&P) Tools needed: wrench size No.8, No.9, 3/8”, 7/16”, 9/16”...
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 10 – POWERPLANT 1 Engine 3 Washer 2 Bolt 4 Engine mount Fig. 10-10: Engine removal / installation 10.3.2 Installation of the engine on the airplane Type of maintenance: heavy Authorization to perform: Repairman (LS-M) or Mechanic (A&P) Tools needed: wrench size No.8, No.9, 3/8”, 7/16”, 9/16”...
Page 196
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 10 – POWERPLANT (c) Install the exhaust system (see 10.3.14). (d) Connect wiring according the wiring diagrams (see Chapter 16). (e) Install the oil cooler (see 10.3.16). (f) Install the water cooler (see 10.3.18). (g) Connect and secure oil system hoses.
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 10 – POWERPLANT 10.3.3 Klassic 170/3/R propeller removal Type of maintenance: line Authorization to perform: Repairman (LS-M) or Mechanic (A&P) Tools needed: wrench size No.13, No. 16 (5/8”) Allen wrench size No.6 screwdriver cutting pliers, pliers WARNING: ENGINE IGNITION MUST BE SWITCHED OFF! (a) Disconnect the battery and remove upper line of spark plugs from the engine.
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 10 – POWERPLANT 10.3.4 Klassic 170/3/R propeller installation Type of maintenance: line Authorization to perform: Repairman (LS-M) or Mechanic (A&P) Tools needed: wrench size No.13, No. 16 (5/8”) Allen wrench size No.6 screwdriver cutting pliers, pliers WARNING: ENGINE IGNITION MUST BE SWITCHED OFF! (a) Disconnect the battery and remove upper line of spark plugs from the engine.
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 10 – POWERPLANT (h) The difference can be max. 1.5 mm (0.06 in). Possible bigger differences can be corrected by repetition the procedure from point (d) or (f). Fig. 10-14: Check of axial propeller running-out (i) Secure bolt heads (7, Fig. 10-12) by lockwire (see 15.8.2).
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 10 – POWERPLANT (c) Unscrew and remove the nuts (8) and take out the propeller from the propeller flange (9). (d) Put the protective covers on the propeller blades and store the propeller on a safe place so that no damage can occur.
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 10 – POWERPLANT (c) Remove protective covers from the propeller blades and carry out visual check of the propeller integrity and condition. (d) Loose the screws of the carbon brush housing flange and shift the carbon brush housing (6) to its rear position.
Page 202
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 10 – POWERPLANT WARNING: ENGINE IGNITION MUST BE SWITCHED OFF! NOTE: For propeller removal two persons are requested. (a) Disconnect the battery and remove upper line of spark plugs from the engine. (b) Unscrew the screws (13, Fig. 10-17) and remove the propeller spinner (6).
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 10 – POWERPLANT CAUTION: THE HUB MUST SIT FLUSH AGAINST THE MOUNTING FLANGE. BOLT BREAKAGE WILL OCCUR IF NOT FLUSH. (g) Insert the pitch cylinder (3, Fig. 10-17) into the hub mount half (1), aligning the blade pin slots with the hub barrels.
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 10 – POWERPLANT (b) Unscrew the screws (10, Fig. 10-19) with the washers (11) and remove the propeller spinner (2). (c) Unscrew and remove the nuts (6), the washers (7) and take out the propeller (1) along with the spinner flange (9) and spacer (3) from the propeller flange (12).
Page 206
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 10 – POWERPLANT WARNING: ENGINE IGNITION MUST BE SWITCHED OFF! (a) Disconnect the battery and remove upper line of spark plugs from the engine. (b) Check the contacting areas of the propeller flange (12, Fig. 10-19), propeller (1) and spacer (3).
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 10 – POWERPLANT 10.3.11 Air intake system removal Type of maintenance: line Authorization to perform: Sport pilot, Repairman (LS-M) or Mechanic (A&P) Tools needed: wrench size No.8, No.10 screwdriver WARNING: ENGINE IGNITION MUST BE SWITCHED OFF! (a) Remove the upper engine cowling.
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 10 – POWERPLANT 10.3.14 Exhaust system installation Type of maintenance: line Authorization to perform: Repairman (LS-M) or Mechanic (A&P) Tools needed: wrench size No.13 pliers small wire hook (spring removal/assembly jig) WARNING: ENGINE IGNITION MUST BE SWITCHED OFF! (a) Install the exhaust tubes (2;...
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 10 – POWERPLANT (c) Install hoses (8) on the banjo fittings (5) and secure them with hose clamps (9). (d) Fill the oil system with oil (see 10.5.1) and check oil system tightness. (e) Install the lower and upper engine cowling.
Page 214
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 10 – POWERPLANT screwdriver cutting pliers WARNING: ENGINE IGNITION MUST BE SWITCHED OFF! (a) Remove the cover (11, Fig. 10-24) from the middle channel. (b) Remove the upper engine cowling. (c) Disconnect the throttle (7) and choke (9) cables from carburetor levers (12; 3) and from the throttle and choke control levers (1).
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 10 – POWERPLANT 10.3.20 Throttle and choke control levers installation Type of maintenance: line Authorization to perform: Repairman (LS-M) or Mechanic (A&P) Tools needed: wrench size No.14 Allen wrench size No. 2 screwdriver cutting pliers WARNING: ENGINE IGNITION MUST BE SWITCHED OFF! (a) Set the throttle control lever witch choke (1, Fig, 10-24) into the middle channel.
ROTAX 912 ULS. IN THE COURSE OF THE WHOLE TEST AN AIRCRAFT MECHANIC WHO IS FAMILIARIZED WITH THE AIRCRAFT TYPE SPORTCRUISER / PIPERSPORT MUST BE PRESENT. (a) Perform the test out of the buildings at the place assigned for performing engine tests in broad daylight.
Page 218
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 10 – POWERPLANT ENGINE TEST REPORT Aircraft Registration Serial No. Engine ROTAX Type 912 ULS2 Serial No. Propeller Type Serial No. Activity Set down values Measured values Starting up the engine Min. oil pressure up to 10 sec.
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 10 – POWERPLANT 10.4.2 Klassic 170/3/R propeller inspections 10.4.2.1 Summary of propeller periodical inspection: • Inspection of propeller after 50 hours of operation. • Inspection of propeller on 500 hours of operation or 2 years, depending what occurs first and following after each next 500 hours of operation or 2 years, depending what occurs first.
Page 220
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 10 – POWERPLANT (b) Disassembly of the propeller and check the grip. Grip of the composite shank in propeller hub must be with interference 0.25 mm (diameter of shank of propeller blade must be by 0.25 mm higher than diameter of the hole in the hub.
Page 221
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 10 – POWERPLANT (c) Check the surface of propeller blade. The blades must not exhibit traces of damage, cracks and deformations. As a damage it is not mentioned the usual operational wear (by friction, operation, washing etc.). In case of necessity can be exchanged the protection of leading edges –...
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 10 – POWERPLANT 10.4.3 Klassic 170/3/R propeller blades pitch setting (a) Pull out each blade to it´s outer limit-away from the hub as there is an 1.5 mm (1/16″) movement range in its lock for expansion.
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 10 – POWERPLANT (b) Prepare a small amount of resin in a clean mixing cup. It is possible to use polyester or vinyl ester, but epoxy resin is the best choice. Always use a strong and stable resin based on high strength adhesives.
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 10 – POWERPLANT 10.4.5 SR3000 propeller inspections 10.4.5.1 Summary of propeller periodical inspection: • Inspection of propeller after 25 hours of operation. • Inspection of propeller on 150 hours of operation and following after each next 150 hours of operation.
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 10 – POWERPLANT (f) Check by means of laser or electronic (digital) protractor the mechanical radial clearance on the individual blades. This clearance must not exceed 2 degrees. (g) According to the data of protocol for given propeller check the function of: •...
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 10 – POWERPLANT (b) Release the bolt on the lever of choke control (6), slightly loosen the cable and tighten up the bolt. (c) Check again if the choke lever and the lever on the carburetor are on the stops. If not, carry out adjustment by adjustable bowden terminals.
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 10 – POWERPLANT 10.5 Exchanges / Service information 10.5.1 Exchange / Refilling oil Refer to the Rotax Maintenance Manual, Chapter 12-20-00, Section 11 Lubrication. NOTE: Recommended kinds of oil are mentioned in the Rotax Operator's Manual, Section 2.5 Operating media –...
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 10 – POWERPLANT and better flows both from the engine and from the tank. Clean the tank before filing it with new oil - see the Rotax Maintenance Manual. Refilling oil Refill oil in the oil tank that is located on the firewall.
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 10 – POWERPLANT (e) Pull the cooler (1) so that you obtain access to the oil filter (see Fig. 10-31); hold the cooler. (f) Remove used oil filter (7) with oil filter wrench. (g) Clean the contact surface of the oil pump housing with a clean cloth.
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 10 – POWERPLANT 10.5.5 Exchange / Check of air filter (a) Remove the hose fastener and the bracket attaching the air filter to the left side lower engine cowling and remove the air filter. (b) Inspect the air filter and if contaminated, clean it according to instructions in the Rotax Maintenance Manual, Chapter Chapter 12-20-00, Section 2.
Page 231
11.3.3 Battery installation ................11-12 11.3.4 Position / strobe light removal ............11-14 11.3.4.1 SportCruiser / PiperSport airplanes up to S/N C0416 ... 11-14 11.3.4.2 SportCruiser airplanes from S/N C0416 ......11-14 11.3.5 Position / strobe light installation ............11-14 11.3.5.1...
Page 232
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 11 – ELECTRICAL SYSTEM INTENTIONALLY LEFT BLANK Revision No.: - Date of issue: 2013-06-30 11 - 2...
PiperSport CHAPTER 11 – ELECTRICAL SYSTEM 11.1 General Electrical system of the SportCruiser / PiperSport airplane serves for supplying electrical current to the instruments. 11.2 Description and operation The airplane is equipped with 14 VDC electrical installations with grounded negative pole (see Fig.
Page 234
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 11 – ELECTRICAL SYSTEM Fig. 11-1: Electrical system scheme (from S/N C0416) Revision No.: - Date of issue: 2013-06-30 11 - 4...
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 11 – ELECTRICAL SYSTEM 11.2.1 Switches The switches serve for switching (ON/OFF) individual electrical circuits. Every switch is marked with a placard with designation of the circuit. The switches are located on the left instrument panel and on the middle channel. The buttons for ailerons and elevator trim are on the grip of the control stick.
FLAPS UP/DOWN Switch of flaps control AUTOPILOT Quick disconnects of autopilot (momentary switch, optional) DISCONNECT Switches – PiperSport / SportCruiser up to S/N C0416 Designation Description INSTR Switch of engine monitoring instruments (toggle switch) Switch of radio, intercom, transponder, GPS and other optional...
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 11 – ELECTRICAL SYSTEM Switches – circuit breakers – PiperSport / SportCruiser up to S/N C0416 Designation Value Description MASTER Main switch STROBE Switch - circuit breaker of strobe lights NAV L. Switch - circuit breaker of position lights...
Page 238
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 11 – ELECTRICAL SYSTEM Circuit breakers – instrument panel with the analog instruments COMM Circuit breaker of VHF transceiver Circuit breaker of intercom ENG INSTR Circuit breaker of engine instruments Circuit breaker of optional navigation device...
11.2.4 Fuses Fuses serve for protecting individual electrical circuits from overloading. The box with the fuses is located on the firewall in the engine compartment (valid for SportCruiser airplanes from S/N C0416). Fuses – instrument panel with the EFIS/EMS Designation Description 1A SIGN.
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 11 – ELECTRICAL SYSTEM Generator 11.2.5 The generator is a part of the engine which supplies electric current through the rectifier. Regulator supplies electric current of 14 V voltage to onboard network. Technical parameters of generator:...
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 11 – ELECTRICAL SYSTEM CCA Current 400 A Continuous discharge current 280A¨ Nominal charging current 12 A @ 25 ° C Max charging current 20 A @ 25 ° C Duration 1000 cycles @ 100% Dod / 10C...
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 11 – ELECTRICAL SYSTEM 11.3 Removal / Installation 11.3.1 Electrical Safety The aircraft has a low-voltage DC electrical system. When correctly maintained it is safe to work on. But the battery can supply heavy current through low-resistance circuits (for example, if you ground the positive output with a wrench by accident).
PiperSport CHAPTER 11 – ELECTRICAL SYSTEM 11.3.4 Position / strobe light removal 11.3.4.1 SportCruiser / PiperSport airplanes up to S/N C0416 Type of maintenance: line Authorization to perform: - Sports pilot, Repairman (LS-M) or Mechanic (A&P) Tools needed: - screwdriver (a) Set the MASTER, NAV L, and STROBE switches to OFF.
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 11 – ELECTRICAL SYSTEM 11.3.5.2 SportCruiser airplanes from S/N C0416 Type of maintenance: line Authorization to perform: - Sports pilot, Repairman (LS-M) or Mechanic (A&P) Tools needed: - screwdriver (a) Pass the wires (3, Fig. 11-3) through the appropriate hole in the gasket (2).
Page 246
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 11 – ELECTRICAL SYSTEM (d) After charging grease the battery contacts with lubricating grease and reconnect the battery to the onboard electrical network. LiFePo4 battery CAUTION: FOR BATTERY CHARGING USE ONLY ALIANT CB1210 OR CB1213 CHARGER.
Page 247
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 11 – ELECTRICAL SYSTEM Fig. 11-4: Lead-acid battery characteristics Date of issue: 2013-09-05 Revision No.: 1 11 - 17...
Fig. 11-5: Setting the optional wing landing light 11.4.3 Exchange of the strobe light discharge tube NOTE: Valid for SportCruiser / PiperSport airplanes up to S/N C0416. Type of maintenance: line Authorization to perform: - Sports pilot, Repairman (LS-M) or Mechanic (A&P)
Page 249
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 11 – ELECTRICAL SYSTEM (c) Carefully remove the discharge tube (2), disconnect wires (3). (d) Exchange the discharge tube for the same type; connect wires. (e) Set the cover glass (4) to the light housing (1) and fasten it with screws (6).
Page 250
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 11 – ELECTRICAL SYSTEM INTENTIONALLY LEFT BLANK Revision No.: 1 Date of issue: 2013-09-05 11 - 20...
Page 251
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 12 –INSTRUMENTS AND AVIONICS Contents 12.1 General ........................ 12-3 12.2 Description and operation.................. 12-10 12.2.1 Pitot-static system ................12-10 12.2.2 Stall warning system................12-10 12.2.3 Flight instruments ................12-12 12.2.4 Engine instruments................12-13 12.2.5 Avionics ..................... 12-13 12.2.6...
Page 252
12.3.42 Installation of drain sump ..............12-51 12.3.43 Draining of drain sumps ..............12-52 12.3.43.1 SportCruiser airplanes manufactured up to April 2013.. 12-52 12.3.43.2 SportCruiser airplanes manufactured fromr April 2013 . 12-52 12.3.44 Removal of SV-ADSB-470 module ........... 12-53 12.3.34 Installation of SV-ADSB-470 module ..........
38 EMS ALARM yellow warning light 19 LDG L switch 39 CABIN OPENED red warning light 20 Keyed ignition switch Fig. 12-1: SportCruiser typical instrument panel with EFIS / EMS Date of issue: 2013-06-30 Revision No.: - 12 - 3...
Page 254
46 GEN red warning light 23 AVIONICS switch 47 FUEL PUMP green signaling light 24 FUEL P switch 48 CABIN OPENED red warning light Fig. 12-2: SportCruiser typical instrument panel with analog instruments Revision No.: - Date of issue: 2013-06-30 12 - 4...
Page 255
14 LDG L switch 30 COCKPIT L dimmer 15 Keyed ignition switch 31 EMS ALARM yellow warning light 16 SL30 NAV/COMM Fig. 12-3: SportCruiser typical instrument panel with Skyview system Date of issue: 2013-06-30 Revision No.: - 12 - 5...
Page 256
29 EMS ALARM yellow warning light 14 EFIS 2 circuit breaker 15 AVIONICS switch 16 FUEL P circuit breaker Fig. 12-4: SportCruiser typical instrument panel with Skyview system (from S/N C0416) Revision No.: - Date of issue: 2013-06-30 12 - 6...
Page 257
30 BRS activation handle cover 15 FUEL P circuit breaker 31 BRS activation handle 16 NAV L circuit breaker Fig. 12-5: SportCruiser typical instrument panel with Skyview system(from S/N C0416) Date of issue: 2013-06-30 Revision No.: - 12 - 7...
Page 258
29 EMS ALARM yellow warning light 14 AVIONICS switch 15 FUEL P circuit breaker 16 NAV L circuit breaker Fig. 12-6: SportCruiser typical instrument panel with Skyview system(from S/N C0416) Revision No.: - Date of issue: 2013-06-30 12 - 8...
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 12 – INSTRUMENTS AND AVIONICS 12.2 Description and operation 12.2.1 Pitot-static system The pitot-static tube for sensing static and total pressure is located under the left half of the wing close to the rib No. 4. Total pressure is sensed through the hole in the pitot-tube face and static pressure is sensed through the holes on the tube circumference.
Page 261
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 12 –INSTRUMENTS AND AVIONICS Fig. 12-9: Pitot-static system scheme Date of issue: 2013-06-30 Revision No.: - 12 - 11...
Normal Operating Range. Yellow Maneuvers must be conducted with 108-138 200-255 124-158 caution and only in smooth air. Red line Maximum speed for all operations. SportCruiser from S/N C0416 White 31-75 57-139 36-86 Flap Operating Range. Green 37-108 69-200 43-124 Normal Operating Range.
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 12 –INSTRUMENTS AND AVIONICS NOTE: For detailed information refer to EFIS D100 Installation Guide (P/N 100487-000, latest edition). 12.2.4 Engine instruments Engine parameters (RPM, CHT, EGT, oil pressure and temperature, fuel pressure, manifold pressure) are displayed either on the EMS D120 or on the classical analog instruments. A typical example of the EMS display is shown in the Figure 10-3.
Page 264
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 12 – INSTRUMENTS AND AVIONICS The Apollo SL-40 is a 760-channel VHF Comm transceiver. NOTE: For detailed information refer to SL-40 Installation Manual (P/N 560-0956- 02a, latest edition) and Pilot′s Guide (P/N 560-0954-02, latest edition). Fig. 12-11: SL-40 VHF transceiver GNC 255A includes a 760-channel (w/ 25 kHz spacing) and 2280-channel (w/ 8.33 kHz...
Page 265
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 12 –INSTRUMENTS AND AVIONICS The PM3000 is a panel mounted, 4-place high-fidelity stereo intercom system that allows the pilot and copilot/passenger to communicate and listen to music. NOTE: For detailed information refer to PM3000 Installation Manual (P/N 200-193- 0005, latest edition) and Pilot′s Guide (P/N 202-193-0001, latest edition).
Page 266
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 12 – INSTRUMENTS AND AVIONICS The panel-mounted GTX 330 is a TSO-certified Mode S digital transponder. In addition to displaying the code, reply symbol and mode of operation, the GTX 330 screen displays pressure altitude, density altitude, temperature, and timer functions, depending on equipment connections and configuration selection.
Page 267
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 12 –INSTRUMENTS AND AVIONICS The Aera 510 presents GPS-derived analog flight instrumentation, position, navigation, and hazard avoidance information to the pilot using a bright 4.3-inch diagonal high-definition sunlight readable color display with touch screen. NOTE: For detailed information refer to Aera Models 500, 510, 550, 560 Owner′s Manual (P/N 190-01117-00, latest edition).
Page 268
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 12 – INSTRUMENTS AND AVIONICS The GTN 750 unit is a panel mounted GPS / NAV / COM navigator. The GTN 750 unit is 6.25 in wide and 6.00 in tall. It features a 600 by 708 pixel color LCD touchscreen which provides a rich and intuitive user interface.
Page 269
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 12 –INSTRUMENTS AND AVIONICS The Aera 795/796 GPS is the ultimate MFD and incorporates the features of the Garmin GPSMAP 695/696, while adding new capabilities such as a touchscreen interface, selectable screen orientation (landscape or portrait), and 3-D Vision. The Aera 795/796 also takes the pilot one step closer to a paperless cockpit with a digital document viewer, scratch pad and pre-loaded geo-referenced AeroNav IFR and VFR enroute charts.
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 12 – INSTRUMENTS AND AVIONICS Antennas Fig. 12-23 shows the antenna locations. The COMM antenna (1) is installed on the upper part of the fuselage behind the canopy. The ELT antenna (3) is installed directly in the rear of the COMM antenna.
Page 271
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 12 –INSTRUMENTS AND AVIONICS Two SV-BAT-320 Backup Batteries provides over an hour of backup power to displays and modules. SV-EMS-220 engine module measures engine parameters - engine speed, manifold pressure, oil temperature and pressure, exhaust gas temperature, cylinder head temperature, fuel quantity, voltage, current, fuel pressure, fuel flow, flap and trim position.
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 12 – INSTRUMENTS AND AVIONICS 12.3 Removal / Installation 12.3.1 Removal of the pitot-static tube Type of maintenance: line Authorization to perform: Repairman (LS-M) or Mechanic (A&P) Tools needed: Phillips PH1 screwdriver pliers, cutting pliers (a) Loose securing bolt (4, Fig. 12-25) in the pitot-static tube bracket (2) and pull out a bit the pitot-static tube (1) with hoses from the bracket.
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 12 –INSTRUMENTS AND AVIONICS Tools needed: Phillips PH1 screwdriver pliers, cutting pliers (a) Connect the hoses (3, Fig. 12-25) to the ports on the pitot-static tube (1) and secure them with cable ties. WARNING: WHEN CONNECTING THE PITOT-STATIC SYSTEM HOSES PAY INCREASED ATTENTION.
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 12 – INSTRUMENTS AND AVIONICS NOTE: The hose for static pressure line mark by S letter and for total pressure mark by T letter. (c) Connect the wires (10) to the illuminator (3). (d) Put the instrument (1; 2) and illuminator (3) in position in the panel (11).
Page 277
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 12 –INSTRUMENTS AND AVIONICS 1 EFIS D100 Hose 2 Access hole of the locking screw Cable tie 3 Static port Connector 4 Pitot port For information: 5 Hose Mounting rack Fig. 12-28: EFIS D100 removal / installation Date of issue: 2013-06-30 Revision No.: -...
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 12 – INSTRUMENTS AND AVIONICS 12.3.8 Installation of the EFIS D100 Type of maintenance: line Authorization to perform: Repairman (LS-M) or Mechanic (A&P) Tools needed: 7/64 Allen wrench (a) Remove the protective covers from the rear ports on the unit.
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 12 –INSTRUMENTS AND AVIONICS 1 Remote compass module 2 Connector 3 Screw (4 pcs.) 4 Washer (2 pcs.) For information: 5 Bracket Fig. 12-29: NAV antenna removal / installation 12.3.10 Installation of EDC-10A remote compass module...
Page 280
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 12 – INSTRUMENTS AND AVIONICS (a) Set the MASTER BAT / MASTER, EMS / INSTR switches to OFF. (b) Put a 7/64 Allen wrench into the access hole (2, Fig. 12-30 for the locking screw; engage the screw.
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 12 –INSTRUMENTS AND AVIONICS 12.3.12 Installation of the EMS D120 Type of maintenance: line Authorization to perform: Repairman (LS-M) or Mechanic (A&P) Tools needed: 7/64 Allen wrench (a) Connect the connectors (3; 4, Fig. 12-30) to the unit (1).
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 12 – INSTRUMENTS AND AVIONICS (b) Looking at the bottom of the unit, make sure the front lobe of the locking mechanism is in a vertical positron. (c) Slide the transponder (1, Fig. 12-31) into the rack (3). Engage the locking screw so that the latch front lobe touches the rack.
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 12 –INSTRUMENTS AND AVIONICS (b) Put a 3/32 Allen wrench into the access hole (2, Fig. 12-32) for the locking screw; engage the screw. (c) Turn the screw counter-clockwise until the unit (1) disengages from the mounting rack.
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 12 – INSTRUMENTS AND AVIONICS (c) Slide the unit (1, Fig. 12-32) into the rack (3). Engage the locking screw so that the latch front lobe touches the rack. (d) Turn the locking screw clockwise so that the rear lobe engages the mounting rack.
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 12 –INSTRUMENTS AND AVIONICS 1 Intercom 5 Connector 2 Knob For information: 3 Faceplate Instrument panel 4 Screw Fig. 12-33: Intercom removal / installation 12.3.19 Removal of GPS / NAV COM Type of maintenance: line Authorization to perform: Repairman (LS-M) or Mechanic (A&P)
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 12 – INSTRUMENTS AND AVIONICS 1 GPS / NAV / COM unit 2 Access hole of the locking screw For information: 3 Mounting rack Fig. 12-34: GPS / NAV / COM unit removal / installation 12.3.20 Installation of GPS / NAV COM...
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 12 –INSTRUMENTS AND AVIONICS (f) Set the MASTER BAT / MASTER, GPS switches to ON and do a post installation (see 17.6) and operational test. 12.3.21 Removal of COMM antenna Type of maintenance: line Authorization to perform: Repairman (LS-M) or Mechanic (A&P)
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 12 – INSTRUMENTS AND AVIONICS 12.3.22 Installation of COMM antenna Type of maintenance: line Authorization to perform: Repairman (LS-M) or Mechanic (A&P) Tools needed: screwdriver wrench No. 7 (a) Remove the protective cover from the antenna connector.
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 12 – INSTRUMENTS AND AVIONICS 12.3.25 Removal of transponder antenna Type of maintenance: line Authorization to perform: Repairman (LS-M) or Mechanic (A&P) Tools needed: wrench No. 3/4 in (a) Tilt forward the right seat back. (b) Set the MASTER BAT / MASTER, AVIONICS switches to OFF.
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 12 –INSTRUMENTS AND AVIONICS (e) Place the fin tip (6) on the fin (8) and fasten it by means of the screws (7). (f) Tilt backward the right seat back. (g) Set the MASTER BAT / MASTER, AVIONICS switches to ON and do an operational test.
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 12 – INSTRUMENTS AND AVIONICS 12.3.28 Installation of GPS antenna NOTE: This type of antenna is used when GPS / NAV / COM unit is installed. Type of maintenance: line Authorization to perform: Repairman (LS-M) or Mechanic (A&P)
Page 293
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 12 –INSTRUMENTS AND AVIONICS 1 SV-D1000 display 5 Ethernet connector 2 DB37 display connector Screw (6 pcs.) 3 SkyView network connector For information: 4 USB connector Instrument panel Fig. 12-39: SV-D1000 display removal / installation 12.3.30 Installation of SV-D1000 display NOTE: Installation is the same for both displays.
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 12 – INSTRUMENTS AND AVIONICS 12.3.31 Removal of SV-BAT-320 backup battery / batteries Type of maintenance: line Authorization to perform: Repairman (LS-M) or Mechanic (A&P) Tools needed: Phillips PH2 screwdriver (a) Set the MASTER BAT, EFIS1 / EFIS 2 switches to OFF.
Page 295
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 12 –INSTRUMENTS AND AVIONICS Fig. 12-36: SV-EMS-220 engine module and SV-BAT-320 backup battery removal / installation (page 1 of 2) Date of issue: 2013-06-30 Revision No.: - 12 - 45...
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 12 –INSTRUMENTS AND AVIONICS (g) Install the protective cover on the ports (4; 5) of the module. 12.3.36 Installation of SV-ADAHRS-200 / 201 module NOTE: Removal the same for both ADAHRS modules. Type of maintenance: heavy Authorization to perform: Repairman (LS-M) or Mechanic (A&P)
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 12 –INSTRUMENTS AND AVIONICS 12.3.38 Installation of SV-OAT-340 probe Type of maintenance: line Authorization to perform: Repairman (LS-M) or Mechanic (A&P) Tools needed: wrench No. 9/16 in NOTE: Do not insert the pins on the ends of the OAT probe wires into the connector until you are done running probe wires through the aircraft.
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 12 –INSTRUMENTS AND AVIONICS 12.3.40 Installation of SV-XPDR-261 transponder Type of maintenance: line Authorization to perform: Repairman (LS-M) or Mechanic (A&P) Tools needed: screwdriver (a) Remove the protective cover from the antenna connector (b) Put the transponder (1, Fig. 12-38) into the mounting tray (4) by hooking the connector end under the lip on the tray.
NOTE: If you find impurities or water in pitot-static system drain sumps, these sumps must be drain. 12.3.43.1 SportCruiser airplanes manufactured before April 2013 Tools needed: Cobra hose clip pliers (a) Tilt forward the left seat back. (b) Remove the hose clips (8, Fig. 12-38) from hoses (9).
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 12 –INSTRUMENTS AND AVIONICS (f) Tilt backward the left seat back and carry out check of pitot-static system tightness test (see 12.4.1). 12.3.44 Removal of SV-ADSB-470 module Type of maintenance: line Authorization to perform: Repairman (LS-M) or Mechanic (A&P)
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 12 – INSTRUMENTS AND AVIONICS (c) Set the MASTER BAT, EFIS1 switches to ON and do operational test of the system. 12.4 Check / Adjustment 12.4.1 Check of pitot-static system tightness (a) In the static pressure system create the under pressure by means of an appropriate instrument corresponding to altitude of 1,000 ft.
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 12 –INSTRUMENTS AND AVIONICS (e) Turn on EFIS (external or internal battery power is acceptable). Keep airplane still while EFIS is powered on. Do not adjust the pitot or static pressures being applied to the EFIS / ADAHRS while it is powered on.
Page 306
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 12 – INSTRUMENTS AND AVIONICS REPORT OF MAGNETIC COMPASS SWING Aircraft Aircraft S/N Compass type Compass S/N Check 1. All electrical equipment ON and operating The engine running, idle Fuselage placed in flying attitude XPDR ON, XCVR receiving Check 2.
Page 307
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 12 –INSTRUMENTS AND AVIONICS REPORT OF EFIS COMPASS SWING Aircraft Aircraft S/N Compass type EDC-D10A Compass S/N EFIS type DYNON D100 EFIS S/N Check 1. All electrical equipment ON and operating The engine running, idle Fuselage placed in flying attitude XPDR ON, XCVR receiving Check 2.
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 12 – INSTRUMENTS AND AVIONICS 12.4.6 EFIS D100 internal emergency battery check EFIS-D100 has a rechargeable internal emergency battery, it is necessary to ensure that the battery capacity is such that it will last at least 2 hours on a full charge. Once per year, perform the battery capacity test.
Page 309
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 12 –INSTRUMENTS AND AVIONICS 12.4.8 Flight test for the verification of the stall warning system Fly the airplane at a safe altitude in a heavy / forward CG configuration, since this configuration has the narrowest stall margin. The airplane should have flaps retracted.
Page 310
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 12 – INSTRUMENTS AND AVIONICS INTENTIONALLY LEFT BLANK Revision No.: - Date of issue: 2013-06-30 12 - 60...
Page 311
Heating control knob removal.............. 13-6 13.3.2 Heating control knob installation ............13-7 13.3.3 Air vents....................13-7 13.3.3.1 Early SportCruiser / PiperSport airplane air vents removal.............. 13-7 13.3.3.2 Early SportCruiser / PiperSport airplane air vents installation ............13-7 13.3.3.3 SportCruiser airplane air vents removal (from S/N C0416).............
Page 312
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 13 – VENTING / HEATING INTENTIONALLY LEFT BLANK Revision No.: - Date of issue: 2013-06-30 13 - 2...
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 13 – VENTING / HEATING 13.1 General This chapter contains information on crew compartment heating and ventilation system. 13.2 Description and operation 13.2.1 Venting system Cockpit ventilation is ensured by two regulated air vents located on the cockpit sides under the instrument panel (see Fig.13-5) or on the instrument panel (see Fig.13-6).
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 13 – VENTING / HEATING 13.2.2.2 Efficient heating system Cockpit heating is ensured by hot air from the heat exchanger (1, Fig. 13-2). This heat exchanger has a larger area compared with standard heat exchanger. The heat exchanger is located on the muffler (2).
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 13 – VENTING / HEATING 13.2.3 Carbon monoxide detector The airplane is equipped with Quantum Eye carbon monoxide (CO) detector, if the efficient heating system is installed. The Quantum Eye is a multi-level carbon monoxide detector. It provides a visual indication of carbon monoxide contamination.
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 13 – VENTING / HEATING 13.3 Removal / Installation 13.3.1 Heating control knob removal Type of maintenance: line Authorization to perform: Sport pilot, Repairman (LS-M) or Mechanic (A&P) Tools needed: wrench size No. 14, 9/16” pliers, cutting pliers (a) Disconnect the control cable on the control flap lever (3, Fig.
CHAPTER 13 – VENTING / HEATING 13.3.3 Air vents 13.3.3.1 Early SportCruiser / PiperSport airplane air vents removal (a) Open the control flap (1, Fig. 13-5) 90 degree and pull the vent (2) out from the housing (3). 1 Control flap...
5 Instrument panel Fig. 13-6: Air vents removal / installation 13.3.3.4 SportCruiser airplane air vents installation (from S/N C0416) (a) Put the hose (3, Fig. 13-6) to the tube (2) and secure with the cable tie (4). (b) Insert the tube (2) to the hole in the instrument panel (5), screw and tighten the vent (1).
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 13 – VENTING / HEATING 13.3.5 Heat exchanger installation NOTE: Installation of the standard heat exchanger is shown in Section 10.3.14. Type of maintenance: line Authorization to perform: Sport pilot, Repairman (LS-M) or Mechanic (A&P) Tools needed: Screwdriver, pliers, cutting pliers (a) Carefully install both halves (1;...
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 13 – VENTING / HEATING 13.3.6 Defogging blowers removal Type of maintenance: line Authorization to perform: Sport pilot, Repairman (LS-M) or Mechanic (A&P) Tools needed: Screwdriver, pliers, cutting pliers (a) Set the MASTER BAT, BLOWERS switches to OFF.
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 13 – VENTING / HEATING 13.4 Check / Adjustment 13.4.1 Adjusting the heating control (a) Adjust the control by screwing or unscrewing the control cable terminal from the control flap. (b) After adjustment of the control, mark the mutual position of the control cable terminal and the flap controller with red color.
Page 323
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 14 – AIRPLANE HANDLING Contents 14.1 General ........................ 14-3 14.2 Jacking and supporting the airplane..............14-3 14.3 Airplane towing ....................14-4 14.4 Airplane parking....................14-4 14.5 Airplane anchoring....................14-4 Date of issue: 2013-06-30 Revision No.: -...
Page 324
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 14 – AIRPLANE HANDLING INTENTIONALLY LEFT BLANK Revision No.: - Date of issue: 2013-06-30 14 - 2...
Page 325
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 14 – AIRPLANE HANDLING 14.1 General This chapter contains information on airplane handling - jacking, parking and anchoring. 14.2 Jacking and supporting the airplane Due to the relatively low empty weight, the airplane jacking can be carried out by two persons.
Page 326
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 14 – AIRPLANE HANDLING 14.3 Airplane towing The airplane can be moved by tow bar inserted into the bracket mounted on nose wheel fork, by main gear legs, or pushing on the wing root. WARNING: SWITCH OFF THE IGNITION BEFORE HANDLING THE AIRPLANE ON...
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 15 – AIRPLANE REPAIRS 15.1 General This chapter contains information about standard procedures for performing common repairs of the airplane. These repairs can be made by an authorized organization. Other procedures for repairing individual airplane systems you can find in the appropriate chapter describing the system.
Riveted parts are used in design of SportCruiser / PiperSport airplane for whole fuselage, wings, flaps, ailerons and tail unit. In the following table there is a survey of rivets that are used on SportCruiser / PiperSport airplane structure. Type of rivets...
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 15 – AIRPLANE REPAIRS overruns the area before riveting max. by 0.2 mm (0.008 in), the rivet head must not be under the surface level (sunk). (c) Before applying the bonding sealant carefully clean the connected parts of impurities and degrease contact surfaces by appropriate agent, e.g.
(c) Damage with disturbance of basic structural elements of the aircraft. (Deformation of wing and stabilizer spar, deformation of wing ribs, fuselage bulkheads etc.). These repairs can be made only by Czech Sport Aircraft a.s. as producer or by authorized repair shop - for more detailed information contact Czech Sport Aircraft a.s.
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 15 – AIRPLANE REPAIRS (f) Use at least two rivets on each side from the crack. (g) At riveting follow Section 15.3. Fig. 15-2: Scheme of angle repair 15.4.5 Skin repair 15.4.5.1 Stopping cracks and blinding small holes Enlarging of small cracks can be stopped by drilling a hole with the drill bit of dia 3.2 mm...
Page 336
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 15 – AIRPLANE REPAIRS 1 Correctly located patch Incorrectly located patch Fig. 15-3: Location of patches on the airplane skin Mark the damaged surface area (preferably by spirit felt tip) and cut out the most suitable geometrical shape (circle, square, rectangle).
Page 337
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 15 – AIRPLANE REPAIRS 1 Skin Stiffening frame 2 Patch Fig. 15-4: Repair of the punctured skin in the frame area Date of issue: 2013-06-30 Revision No.: - 15 - 9...
Page 338
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 15 – AIRPLANE REPAIRS A Punctured skin Patch B Cutting out and cleaning the damaged skin Frame C Repair with the unsunk patch Skin D Repair with the sunk patch Fig. 15-5: Repair of the punctured skin Revision No.: -...
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 15 – AIRPLANE REPAIRS 15.5 Repair of fiberglass parts 15.5.1 Damage classification Any damage of parts from reinforced plastics with epoxy matrix leads to increased saturation of the matrix with humidity and subsequently to loss of properties. Therefore we recommend carry out their repair as soon as possible after the damage has occurred.
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 15 – AIRPLANE REPAIRS Manufacturer, Mixing Rate of Time of Type Delay Temperature Fillers name ratio setting setting to be 16 FH 20-35° C 68-95° F processed MGS, (32 FH) (17-20° C) (62-68° F) thickening: within 50...
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 15 – AIRPLANE REPAIRS Stiffener preparation For this kind of repairs we recommend the stiffener G (glass) with plain weave 150 g/m (0.037 lb/ft ), with surface protection for epoxy resins. Number of needed stiffener layers depends on depth of damage.
Structural parts On these parts we do not recommend to do other as small damages repair. In case of the other damage we recommend to contact Czech Sport Aircraft a.s. as manufacturer. CAUTION: WHEN REPAIRING, IT IS NECESSARY TO PAY ATTENTION TO TIMELY REPAIR (SEE THE TEXT ABOUT LOW OF PROPERTIES AT HUMIDITY EFFECT AT THE BEGINNING OF 15.5.1)!
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 15 – AIRPLANE REPAIRS CAUTION: THESE AGENTS MUST NOT BE USED FOR DEGREASING PARTS FROM PLASTICS (PC -LEXAN, PMMA PLEXIGLASS). (b) Water-based agents - emulgation substances, wetting agents • Applied also by spraying onto washed surfaces or by wiping with wet (by pouring and dipping) textile wad.
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 15 – AIRPLANE REPAIRS 15.6.2.3 Application of primer (paint) In order to reach a uniform resistance to corrosion and smooth surface, we recommend carry out application by means of spraying (air standard gun with the upper vessel, air HVLP gun, airless electric gun).
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 15 – AIRPLANE REPAIRS spectrum of colors, but it is difficult to do metallic paint coats (we do not recommend them). Drying (between Color Manufacturer, Other Surface Type Recom. thickness spraying / total) type name items mass 18°...
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 15 – AIRPLANE REPAIRS 15.6.3.2 Sanding For good adhesion of the repair coats it is necessary to carry out sanding of the old paint coat at least up to such depth as the depth of damage. Ground area must be larger from 51 to 102 mm (2 to 4 in) than damaged area.
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 15 – AIRPLANE REPAIRS Drying Manufacturer, Color Other Surface Recomm. (between spray Type type components mass thickness coats / total) name 18° C ( 65° F ) BASF 1-1.6 Glasurit [kg/mm/m 922-36 BASF Glasurit (standard 0.02-0.04 mm single acrylic –...
Page 349
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 15 – AIRPLANE REPAIRS 1. Adjust the correct position of 6. Pull the upper wire through the holes for locking wire. hole in the other bolt. Hold the wire end by pliers and tighten it firm.
General In order to keep the set down values of the transition resistances between some stuctural parts of the SportCruiser / PiperSport airplane structure, the bonding (conductive interconnection) is installed between all important parts of the fuselage structure. Revision No.: -...
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 15 – AIRPLANE REPAIRS 15.9.2 Removal and installation Before installing the bonding remove the paint coat which protects the joint. Principles for repeated installation of the bonding: (a) Carefully clean the whole bonding including the washers, bolts and nuts from all impurities, if necessary degrease the contacting surfaces on the connecting material.
Page 352
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 15 – AIRPLANE REPAIRS 1 Clamp Inspection gauge 2 Eye Gauge No. 3 Squeezing sequence Fig. 15-9: Installation of clamps by Nicopress pliers Revision No.: - Date of issue: 2013-06-30 15 - 24...
Page 353
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 16 – WIRING DIAGRAMS Contents 16.1 General ........................ 16-3 16.2 Wiring diagram of the DC power system ............16-4 16.3 Wiring diagram of the Rotax 912 engine ............. 16-5 16.4 Wiring diagram of the EFIS D100, HS34............. 16-6 16.5 Wiring diagram of the EMS D120 ................
Page 354
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 16 – WIRING DIAGRAMS INTENTIONALLY LEFT BLANK Revision No.: - Date of issue: 2013-06-30 16 - 2...
CHAPTER 16 – WIRING DIAGRAMS 16.1 General This chapter contains typical wiring diagrams of SportCruiser airplane systems, navigation and communication means. Further wiring diagrams, relating to additional equipment of the airplane, are the part of additional equipment description which is mentioned in Chapter 17 - Appendices.
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 16 – WIRING DIAGRAMS 16.2 Wiring diagram of the DC power system Fig. 16-1: Wiring diagram of the DC power system Revision No.: - Date of issue: 2013-06-30 16 - 4...
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 16 – WIRING DIAGRAMS 16.8 Wiring diagram of the aileron and elevator trim Fig. 16-7: Wiring diagram of the aileron and elevator trim Revision No.: - Date of issue: 2013-06-30 16 - 10...
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 16 – WIRING DIAGRAMS 16.11 Wiring diagram of the external lights Kuntzleman Fig. 16-10: Wiring diagram of the external lights Kuntzleman Date of issue: 2013-06-30 Revision No.: - 16 - 13...
Page 366
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 16 – WIRING DIAGRAMS 16.12 Wiring diagram of the XPDR GTX-328/330 Fig. 16-11: Wiring diagram of the XPDR GTX-328/330 Revision No.: - Date of issue: 2013-06-30 16 - 14...
Page 367
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 16 – WIRING DIAGRAMS 16.13 Wiring diagram of the autopilot AP-74 Fig. 16-12: Wiring diagram of the autopilot AP-74 Date of issue: 2013-06-30 Revision No.: - 16 - 15...
Page 368
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 16 – WIRING DIAGRAMS INTENTIONALLY LEFT BLANK Revision No.: - Date of issue: 2013-06-30 16 - 16...
Page 369
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 17 – APPENDICES Contents 17.1 General ......................17-3 17.2 List of appendices..................... 17-3 17.3 List of used material for airframe production ............ 17-4 17.4 Airplane failure card..................17-5 17.5 Operating liquids....................17-6 17.6 GTN 650 / 750 Post-Installation Checkout Log ..........17-7 Date of issue: 2013-06-30 Revision No.: -...
Page 370
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 17 – APPENDICES INTENTIONALLY LEFT BLANK Revision No.: - Date of issue: 2013-06-30 17 - 2...
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 17 – APPENDICES 17.1 General This chapter contains other information necessary to maintain the SportCruiser / PiperSport airplane in the form of appendices. 17.2 List of appendices Title 17.3 List of used materials 17.4 Airplane failure card 17.5...
Page 372
SC-AMM-1-0-00 SportCruiser PiperSport CHAPTER 17 – APPENDICES 17.3 List of used materials for airframe production Prescribed material 2024 T351 Duraluminium 6061 T6 Duraluminium 4130 N Steel 15 130 Steel 11 353 Steel 17 240.4 Stainless steel D 671 Stainless steel Revision No.: -...
PiperSport CHAPTER 17 – APPENDICES 17.4 Airplane failure card CZECH SPORT AIRCRAFT a.s. Na Záhonech 1177/212, 686 04 Kunovice, Czech Republic Airplane Failures Card Dear customer, We would like to ask you for your assistance at obtaining information for continuous increasing reliability of airplanes produced by our company.
Need help?
Do you have a question about the SportCruiser and is the answer not in the manual?
Questions and answers