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TASK 27-51-51-400-802
6. Flap Power Drive Unit (PDU) Seal Installation
(Figure 402)
A. General
(1) This procedure is applicable to the seals on the power drive unit (PDU) at the attachment of the
hydraulic motor, and the electric motor.
B. References
Reference Title
12-22-51-610-801 Trailing Edge Flap Power Drive Unit Servicing (P/B 301)
27-51-00-440-801 Trailing Edge Flap System Reactivation (P/B 201)
27-51-00-860-801 Trailing Edge Flap System Operation With Primary Control (P/B 201)
27-51-52-400-801 Flap Hydraulic Motor Installation (P/B 401)
27-51-53-400-801 Flap Electric Motor Installation (P/B 401)
C. Tools/Equipment
NOTE: When more than one tool part number is listed under the same "Reference" number, the
tools shown are alternates to each other within the same airplane series. Tool part numbers
that are replaced or non-procurable are preceded by "Opt:", which stands for Optional.
Reference Description
SPL-1755 Sleeve - Tool Set, Seal Installation (-17 is Part of -1 Set)
(Part #: J27058-17, Supplier: 81205, A/P Effectivity: 737-600, -700,
-700C, -700ER, -700QC, -800, -900, -900ER, -BBJ)
D. Consumable Materials
Reference Description Specification
C00913 Compound - Nondrying Resin Mix Corrosion
Inhibiting Material
BMS3-27
D00070 Fluid - Hydraulic, Petroleum Base MIL-PRF-5606
(Replaces
MIL-H-5606)
D00467 Fluid - Landing Gear Shock Strut BMS3-32, Type
II
D50011 Grease - Perfluoropolyether - Christo-lube MCG111
G50136 Paste - Corrosion Inhibiting, Non-drying BMS3-38
E. Expendables/Parts
AMM Item Description AIPC Reference AIPC Effectivity
52 Packing 27-51-55-02-440 GUN 001-028, 101-121,
155-157, 201-999
53 Seal 27-51-55-02-095 GUN 001-028, 101-121,
155-157, 201-999
27-51-55-02-295 GUN 001-028, 101-121,
155-157, 201-999
54 Retainer 27-51-55-02-085 GUN 001-028, 101-121,
155-157, 201-999
27-51-55-02-285 GUN 001-028, 101-121,
155-157, 201-999
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-51-51
Page 418
Oct 10/2007
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
F. Location Zones
Zone Area
133 Main Landing Gear Wheel Well, Body Station 663.75 to Body Station
727.00 - Left
134 Main Landing Gear Wheel Well, Body Station 663.75 to Body Station
727.00 - Right
G. Seal Installation
SUBTASK 27-51-51-020-010
(1) Install the seal [53] on the power drive unit [21]:
(a) Make sure the seal [53], and the mating surfaces on the power drive unit [21] are clean.
(b) Lubricate the new seal [53], and the mating surfaces on the power drive unit [21] with fluid,
D00070.
CAUTION: MAKE SURE YOU PROTECT THE SEAL LIP DURING THE INSTALLATION. THE
SPLINES ON THE SHAFT [56] CAN CAUSE DAMAGE TO THE SEAL.
(c) Use a seal installation sleeve, SPL-1755 to install the seal [53] in the power drive unit [21].
NOTE: If the sleeve is not available, you can use hand pressure to install the seal [53].
You can use the retainer [54] to protect the seal lip, and to get the correct seal
depth.
1) Insert the seal [53] to a depth of 0.32 to 0.33 inch (8.13 to 8.38 mm).
NOTE: There are two types of seal retainers used on the PDU. They are only
interchangeable at the hydraulic motor input shaft location.
(d) To install the plain retainer [54], do the following steps:
1) Apply a layer of compound, C00913 to the flange of the retainer [54], and to the shank
and threads of the screws [55].
2) Install the retainer [54] and the screws [55] on the power drive unit [21].
(e) To install the retainer [54], with the excluder seal (and O-ring), do the following steps:
1) Apply a layer of corrosion inhibiting non-drying paste, G50136 to the flange of the
retainer [54], and to the shank and threads of the screws [55].
2) Make sure the seal bore in the power drive unit [21] is clean.
3) Lubricate the seal bore in power drive unit [21] the with the Christo-lube MCG111
grease, D50011.
4) Lubricate the excluder seal lips (and O-ring) on the retainer [54] with the Christo-lube
MCG111 grease, D50011.
(f) Install the retainer [54] and the screws [55] on the power drive unit [21].
SUBTASK 27-51-51-410-004
(2) If you removed the electric motor [19], then, do this task: Flap Electric Motor Installation,
TASK 27-51-53-400-801
SUBTASK 27-51-51-410-005
(3) If you removed the hydraulic motor [22], then, do this task: Flap Hydraulic Motor Installation,
TASK 27-51-52-400-801
SUBTASK 27-51-51-680-002
(4) Install the plug [51] in the power drive unit [5]:
(a) Lubricate the new packing [52] with fluid, D00467.
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737-600-700-800-900 飞机维护手册5 AIRCRAFT MAINTENANCE MANUA(78)
