E.
Dry with air as described in previous caution or by heating at a temperature of 250° to 300° F for one
half hour.
— Note —
Solvents can be reused provided they do not become excessively contaminated with
oil. This condition can be determined by thoroughly evaporating 100 milligrams of the
liquid in a glass dish of a determined weight. Evaporation may be accomplished by
heating the dish at 20°F for one hay hour. If after evaporation and cooldown, the
residue exceeds 100 milligrams in weight, the solvent shall not be reused
3. Method 111.
A.
Flush with hot inhibited alkaline cleaner until free from oil and grease.
B.
Rinse thoroughly with fresh water.
C.
Dry thoroughly with a stream of clean air as described in the previous caution, or by heating 250° to
300° F for one half hour minimum.
4.
After cleaning. all tubing must be protected by caps, plugs, and/or plastic bags.
— CAUTION —
DO NOT USE ADHESIVE TAPE ON OXYGEN COMPONENTS FOR
AT TACHING OR SECURING PROTECTIVE COVERINGS. USE LUDLOW
NO. 6 WAXED LACING TWINE OR TIE WRAPS
5. Before reinstallation make sure fitting, tube, and fixture threads are in good condition and that the cones do
not exhibit pitting or disfigurement.
SWAGELOC FITTING INSTALLATIONS. (Refer to Figure 35-5.)
— Note —
The high pressure line fitting at the regulator should be tightened until it bottoms
Make sure to use teflon tape on all male pipe threads.
1. For swageloc fittings not preswaged or for in-aircraft installation, proceed as follows:
A.
Turn the fitting nut onto the fitting finger tight, and insert the tube until it bottoms firmly on the
shoulder in the fitting.
B.
Tighten the nut with a wrench until the tube will not turn by hand.
C.
Mark the nut at the six o'clock position.
D.
Hold the fitting body steady with a backup wrench and tighten as follows:
(1). On tubing with a diameter bigger then 3/16 inch, tighten 11/4 turns (to the nine o'clock position).
(2). On tubing of 1/16, 1/8, and 3/16 inch diameter tighten only 3/4 turn.
E.
If nut and tube must be disconnected from the fitting reconnect by seating the tube on the shoulder of
the fitting and tightening the nut finger tight. Follow up by tightening the nut with a wrench, one-
quarter turn (if absolutely necessary the original 11/4 or 3/4 tight position) and then snug with wrench.
PA - 4 4 - 1 8 0 / 1 8 0 T
AIRPLANE MAINTENANCE MANUAL
3 5 - 11 - 0 3
Page 35-09
Revised: May 15, 1989
2J17
PIPER AIRCRAFT
Содержание SEMINOLE PA-44-180
Страница 18: ...CHAPTER AIRWORTHINESS LIMITATIONS PA 44 180 180T AIRPLANE MAINTENANCE MANUAL 1A18 PIPER AIRCRAFT...
Страница 21: ...CHAPTER TIME LIMITS MAINTENANCE CHECKS PA 44 180 180T AIRPLANE MAINTENANCE MANUAL 1A21 PIPER AIRCRAFT...
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Страница 38: ...CHAPTER DIMENSIONS AND AREAS 1B14...
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Страница 49: ...CHAPTER LIFTING AND SHORING 1C1...
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Страница 53: ...CHAPTER LEVELING AND WEIGHING 1C5...
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Страница 58: ...CHAPTER TOWING AND TAXIING 1C10...
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Страница 62: ...CHAPTER PARKING AND MOORING 1C14...
Страница 65: ...CHAPTER REQUIRED PLACARDS 1C17...
Страница 70: ...CHAPTER SERVICING 1C22...
Страница 98: ...CHAPTER STANDARD PRACTICES AIRFRAME 1E2...
Страница 108: ...CHAPTER ENVIRONMENTAL SYSTEM 1E12...
Страница 189: ...CHAPTER AUTOFLIGHT 1H21...
Страница 192: ...CHAPTER COMMUNICATIONS 1H24...
Страница 202: ...CHAPTER ELECTRICAL POWER 1I10...
Страница 228: ...CHAPTER EQUIPMENT FURNISHINGS 1J12...
Страница 233: ...CHAPTER FIRE PROTECTION 1J17...
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Страница 238: ...CHAPTER FLIGHT CONTROLS 1J24...
Страница 304: ...2A18 CHAPTER FUEL...
Страница 325: ...2B17 CHAPTER HYDRAULIC POWER...
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Страница 357: ...2D1 CHAPTER ICE AND RAIN PROTECTION...
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Страница 414: ...CHAPTER LANDING GEAR 2F13...
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Страница 479: ...2I6 CHAPTER LIGHTS...
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Страница 488: ...2I16 CHAPTER NAVIGATION AND PITOT STATIC...
Страница 503: ...2J7 CHAPTER OXYGEN...
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Страница 524: ...2K6 CHAPTER VACUUM...
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Страница 535: ...2K19 CHAPTER ELECTRICAL ELECTRONIC PANELS AND MULTIPURPOSE PARTS...
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Страница 547: ...2L7 CHAPTER STRUCTURES...
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Страница 582: ...CHAPTER DOORS 3A18...
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Страница 593: ...CHAPTER STABILIZERS 3B8...
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Страница 604: ...CHAPTER WINDOWS 3B22...
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Страница 611: ...CHAPTER WINGS 3C10...
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Страница 624: ...CHAPTER PROPELLER 3D1...
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Страница 643: ...CHAPTER POWER PLANT 3D21...
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Страница 667: ...CHAPTER ENGINE FUEL SYSTEM 3F1...
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Страница 681: ...CHAPTER IGNITION 3F16...
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Страница 712: ...CHAPTER ENGINE INDICATING 3H1...
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Страница 730: ...CHAPTER EXHAUST 3H19...
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Страница 734: ...CHAPTER OIL 3I1...
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Страница 743: ...CHAPTER STARTING 3I11...
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Страница 755: ...CHAPTER TURBINES 3J1...
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Страница 787: ...CHAPTER CHARTS AND WIRING DIAGRAMS 4A18...
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