2. Preswaged swageloc fittings are fabricated and installed as follows:
A. Assemble the nut and ferrules finger tight on the pre-swaging tool and insert the tube until it firmly
bottoms on the shoulder in the tool. The pre-swaging tool can be attained from Crawford Fitting
Company, refer to List of Consumable Materials in Chapter 91.
B. Tighten the nut on the fitting just enough that the tube within the fitting will not turn by hand.
C. With a wrench tighten the nut as follows:
(1) On tubing with diameters over 3/16 inch, tighten 1-1/4 turns.
(2) On tubing with 1/16, 1/8 or 3/16 inch diameter tighten 3/4 of a turn.
D. Unscrew the nut to release the ferrule tube assembly from the tool.
E. The assembly is installed on the fitting as follows:
(1) Slide tube in fitting until it bottoms, turn nut to finger tight position, and tighten one quarter
turn with wrench.
(2) Snug slightly with wrench.
APPLICATION OF TEFLON TAPE THREAD SEALANT.
All male pipe (tapered) threads of the oxygen system should be sealed with 3M No. 48 teflon tape. Teflon
tape should not be used on straight threads. Do not use any other lubricants in place of the teflon or on any
other threads.
1. Wrap tape on the threads, starting with those farthest from the opening, in the direction of the thread
spiral. Circle the threads, making sure that each side of the tape has a slight overlap.
2. Wrap the tape such that is does not extend beyond the last thread on the fitting at the opening. The tape
should then be pulled till it separates. Do not cut the tape, it will not stick properly.
CHART 3502. OXYGEN SYSTEM LIMITS
PARTS
INSPECTION
OVERHAUL
Regulator
300 Flight Hrs.
5 Years
Pressure Gauge
300 Flight Hrs.
Replace on Condition
High Pressure Lines
300 Flight Hrs.
Replace on Condition
Low Pressure Lines
300 Flight Hrs.
Replace on Condition
Outlets
300 Flight Hrs.
External Recharge Valve
Each Use
Masks
Each Use
Replace as Necessary
NOTES:
1 On condition replace the rubber components in the assembly or replace assembly.
2 If the screen in front of valve is dirty, replace valve. Valve replacement is recommended for every 5 years.
35-10-05
Page 35-11
Added: November 6, 1979
2H9
PIPER AIRCRAFT
PA-28RT-201 / 201T
MAINTENANCE MANUAL
Summary of Contents for Arrow IV
Page 18: ...CHAPTER AIRWORTHINESS LIMITATIONS 1A18...
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Page 22: ...CHAPTER TIME LIMITS MAINT CHECKS 1A22...
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Page 40: ...CHAPTER DIMENSIONS AND AREAS 1B16...
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Page 53: ...CHAPTER LIFTING AND SHORING 1C5...
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Page 57: ...CHAPTER LEVELING AND WEIGHING 1C9...
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Page 62: ...CHAPTER TOWING AND TAXIING 1C14...
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Page 66: ...CHAPTER PARKING AND MOORING 1C18...
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Page 70: ...CHAPTER REQUIRED PLACARDS 1C22...
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Page 77: ...CHAPTER SERVICING 1D5...
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Page 110: ...CHAPTER STANDARD PRACTICES AIRFRAME 1E14...
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Page 117: ...CHAPTER ENVIRONMENTAL SYSTEM 1E21...
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Page 169: ...CHAPTER AUTO FLIGHT 1H1...
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Page 176: ...CHAPTER COMMUNICATIONS 1H8...
Page 185: ...CHAPTER ELECTRICAL POWER 1H17...
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Page 233: ...CHAPTER FLIGHT CONTROLS 1J17...
Page 297: ...CHAPTER FUEL 2A18...
Page 320: ...CHAPTER HYDRAULIC POWER 2B17...
Page 355: ...CHAPTER LANDING GEAR 2D4...
Page 418: ...CHAPTER LIGHTS 2F19...
Page 430: ...CHAPTER NAVIGATION AND PITOT STATIC 2G7...
Page 444: ...CHAPTER OXYGEN SYSTEM 2G21...
Page 464: ...CHAPTER VACUUM SYSTEM 2H17...
Page 473: ...CHAPTER ELECTRICAL ELECTRONIC PANELS AND MULTI PURPOSE PARTS 2I2...
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Page 477: ...CHAPTER STRUCTURES 2I6...
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Page 496: ...CHAPTER DOORS 2J1...
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Page 505: ...CHAPTER STABILIZERS 2J10...
Page 514: ...CHAPTER WINDOWS 2J19...
Page 519: ...CHAPTER WINGS 2J24...
Page 550: ...CHAPTER PROPELLER 3A18...
Page 565: ...CHAPTER STANDARD PRACTICES ENGINE 3B9...
Page 568: ...CHAPTER POWER PLANT 3B12...
Page 592: ...CHAPTER ENGINE FUEL AND CONTROL 3C12...
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Page 611: ...CHAPTER IGNITION 3D7...
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Page 655: ...CHAPTER ENGINE INDICATING 3F16...
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Page 664: ...CHAPTER EXHAUST 3G1...
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Page 669: ...CHAPTER OIL SYSTEM 3G6...
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Page 673: ...CHAPTER STARTING 3G10...
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Page 688: ...CHAPTER TURBINES 3H1...
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Page 694: ...CHAPTER 91 CHARTS AND WIRING DIAGRAMS 3H7...
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