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1.
Planning Data (TASK 33-30-15-99C-808-A01)
A.
Reason for the Job (Subtask 33-30-15-99C-016-A01)
(1)
This section gives the fits and clearances used when the door mounted cargo loading light
was made.
B.
Job Setup Data (Subtask 33-30-15-99C-017-A01)
(1)
The list that follows identifies Honeywell publications that are related to this section:
• ATA No. 20-00-03 (Pub. No. A09-1100-004), Standard Repair Procedures for Honeywell
Avionics Equipment Instruction Manual.
2.
Fits and Clearances (TASK 33-30-15-220-801-A01)
A.
Fits and Clearances of the Door Mounted Cargo Loading Light (Subtask 33-30-15-220-001-A01)
(1)
Refer to Table 8001 when you do the procedures in REPAIR (PGBLK 33-30-15-6000) and
ASSEMBLY (PGBLK 33-30-15-7000).
Nomenclature/Description
Figure - Item
Lens lanyard - 50, IPL Figure 1
B.
Torque Values (Subtask 33-30-15-220-002-A01)
(1)
Tighten nuts, bolts, screws, and tube fittings to standard torque values unless specified
differently in this manual. Refer to ATA No. 20-00-03 (Pub. No. A09-1100-004), Standard
Repair Procedures for Honeywell Avionics Equipment Instruction Manual, for standard torque
values.
EFFECTIVITY
ALL
© Honeywell International Inc. Do not copy without express permission of Honeywell.
COMPONENT MAINTENANCE MANUAL
15-0705
FITS AND CLEARANCES
Table 8001. Fits and Clearances
Requirement/Dimension
2.0 ± 0.10 inches (51 ± 2.5 mm) final length of lens lanyard, measured
between centers of terminal (62) eyelets
33-30-15
Page 8001
30 Mar 2017
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