040-999
51-20-00PAGE
Jan 7
10/90
PIPERAIRCRAFT
PA-42-720(AdvancedTrainer)
MAINTENANCEMANUAL
A. Processes(continued)
FayingSealBetweenSkinsat Skin Lap Skin Skin
an 10/90
PIPERAIRCRAFT
PA-42-720 (Advanced Trainer)
MAINTENANCEMANUAL
A. Processes(continued)
1.
Bulkhead
2.
Fayingseal
Pressure Side
3.
Stringer
4.
Skin
5.
Stringer seal plate
6.
Brush coat with ClassA-1/2sealant
7.
Filletseal
8.
Bulkhead cutout
14
SEALING HOLES
9.
Fuselageskin
10.Faying seal at forward bulkheads between skin and stringer
11.Bulkhead flange
12.Screw
13.Seal plane (skin, bulkhead, etc.)
14.Large hole (greater than .125")
15.Nut
SEALINGSTRINGERS 16. Washer
Stringers, Holes and Voids Seals
Figure 205
Apply Sealantwith Flow Gun
D
View A
Applicationof Fillet Seal
ViewC
Dimensions
Press Sealant into Place
with Fairing Tool
D = 0.10" Min.
W = 0.20" Min.
A + B = W, Except A = 0 when
B = 0.20" or More
View B
Forming of Fillet Seal
Fillet Seal
Figure 206
EFFECTIVITY:
040-999
51-20-00an10/90
PIPER AIRCRAFT
PA-42-720(AdvancedTrainer)
MAINTENANCE MANUAL
A. Processes(continued)
1. SealingProcedures(continued)
(b) FuselageSealing (continued)
(10.)SealingSeamsandJoints (Figure 206)
Fillet seals must be used along edges of all structures rivettedtothe skin in the pressurizedarea,such as frames, stringers,doublers, laps, seams, and joints. Apply sealant with a pressure gun and be sure to avoid getting gaps or bridges along the seam joint. Final dimensions of a cross section of bead must conform to those shown in Figure
206.
CAUTION: ENSURE PRESSURE GUN CONTAINSENOUGHSEALANTTO COMPLETEA SEAL AT ONE INJECTION WITHOUT ANY BREAK. STOPPINGAND STARTING CAUSES AIR BUBBLES IN SEALS AND WILL PRODUCE A POOR SEAL.
(11.) Sealing Fasteners (Figure207)
Seal all fasteners installed in a seal plane by filleting around fasteners,after installation, with a coat of B-2 class sealant.
NOTE: If a bolt or nut is being sealed, it must be torqued before sealants set. Tightening after sealant sets is not recommended.
(12.)Sealing"AN"StandardBulkheadFittings
SealAN fittings passing through pressure plain of the bulkhead by cleaning aroundseal area. Apply sealant to inside surface around the hole and install the fitting before the sealantsets.
0.06"
Bolthead
.005 to .015'
Bolts and Rivets Seals
Figure 207
EFFECTIVITY:
PIPER AIRCRAFT PA-42-720(AdvancedTrainer)
MAINTENANCEMANUAL
A Processes(continued)
1. Sealing Procedures (continued)
(b) FuselageSealing (continued)
(13.)SealingElectricalHarnesseswith sealing compound (Figure 208)
Thesesteps pertain to the main fuselageand wing harnessonly. The wire harnesses are
sealedat the point where they pass through the pressure bulkhead.
(a.) Clean area of bulkhead where seal fittings will seal.
(b.) Pass wire bundle through hole provided in bulkhead.
(c.) Place sealfitting halves aroundwire harness, on pressure sideof bulkhead.
(d.) Fill groove in mounting flange of the fitting halves with sealant. (Refer to view A of
Figure 208.)
NOTE: Use enough sealant to assure it extrudes around the mounting flange after securingthemto the bulkhead.
(e.) Secure fitting to bulkhead with fasteners. (f.) Fillet seal extrudedsealant around sides of mountingflange (shown in view B of Figure 208). (g.) Put nozzle of sealant gun in center of wire harness and work sealant throughout wires inside seal fitting (shown in view C of Figure 208). (h.) Place a strong piece of string against the seal assembly,parellel with the wires. (Refer to view D of Figure 208.) (i.) Wrap fittinghalves with threeturns of 1.50 inch wide maskingtape. (Refer to view D
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址:夏延飞机维护手册 Cheyenne IIIA PA-42-720 AMM 2(99)