TESTING FUEL CELLS.
Either of the following test procedures may be used to detect leaks in the bladder cells:
1. Soap Suds Test.
A.
Attach test plates to all fittings.
B.
Inflate the cell with air to a pressure of 1/4 psi MAXIMUM.
C.
Apply a soap and water solution to all repaired areas and any areas suspected of leakage. Bubbles will
appear at any point where leakage occurs.
D.
After test. remove all plates and wipe soap residue from the exterior of the cell.
2. Chemical Test.
A.
Attach test plates to all fitting openings except one.
B.
Make up a phenolphthalein solution as follows: Add 40 grams phenolphthalein crystals in 1/2 gallon
of ethyl alcohol. mix, then add 1/2 gallon of water.
C.
Pour ammonia on an absorbent cloth in the ratio of 3ml per cubic foot of cell capacity. Place the
saturated cloth inside the cell and install remaining test plate.
D.
Innate the cell with air to a pressure of 1/4 psi MAXIMUM, and maintain pressure for fifteen minutes.
E.
Soak a large white cloth in the phenolphthalein solution, wring it out thoroughly, and spread it
smoothly on the outer surface of the cell. Press the cloth down to insure detection of minute leaks.
F.
Check the cloth for red spots which will indicate a leak. Mark any leaks found and move the cloth to a
new location. Repeat this procedure until the entire exterior surface of the cell has been covered. If
red spots appear on the cloth. they may be removed by re-soaking the cloth in the solution.
G.
The solution and test cloth are .satisfactory only as long as they remain clean. Indicator solution that is
not in immediate use should be stored in a closed rustproof container to prevent evaporation and
deterioration.
After the test. remove all plates and test equipment. Allow the cell to air out.
In conducting either text outlined above, the cell need not be confined by a cage or jig, providing the 1/4 psi
pressure is not exceeded.
— Note —
The chemical test is the more sensitive and preferred test.
PA - 4 4 - 1 8 0 / 1 8 0 T
AIRPLANE MAINTENANCE MANUAL
2 8 - 11 - 1 6
Page 28-10
Revised: May 15, 1989
2B8
PIPER AIRCRAFT
Summary of Contents for SEMINOLE PA-44-180
Page 38: ...CHAPTER DIMENSIONS AND AREAS 1B14...
Page 49: ...CHAPTER LIFTING AND SHORING 1C1...
Page 53: ...CHAPTER LEVELING AND WEIGHING 1C5...
Page 58: ...CHAPTER TOWING AND TAXIING 1C10...
Page 62: ...CHAPTER PARKING AND MOORING 1C14...
Page 65: ...CHAPTER REQUIRED PLACARDS 1C17...
Page 70: ...CHAPTER SERVICING 1C22...
Page 98: ...CHAPTER STANDARD PRACTICES AIRFRAME 1E2...
Page 108: ...CHAPTER ENVIRONMENTAL SYSTEM 1E12...
Page 189: ...CHAPTER AUTOFLIGHT 1H21...
Page 192: ...CHAPTER COMMUNICATIONS 1H24...
Page 202: ...CHAPTER ELECTRICAL POWER 1I10...
Page 228: ...CHAPTER EQUIPMENT FURNISHINGS 1J12...
Page 233: ...CHAPTER FIRE PROTECTION 1J17...
Page 238: ...CHAPTER FLIGHT CONTROLS 1J24...
Page 304: ...2A18 CHAPTER FUEL...
Page 325: ...2B17 CHAPTER HYDRAULIC POWER...
Page 357: ...2D1 CHAPTER ICE AND RAIN PROTECTION...
Page 414: ...CHAPTER LANDING GEAR 2F13...
Page 479: ...2I6 CHAPTER LIGHTS...
Page 488: ...2I16 CHAPTER NAVIGATION AND PITOT STATIC...
Page 503: ...2J7 CHAPTER OXYGEN...
Page 524: ...2K6 CHAPTER VACUUM...
Page 535: ...2K19 CHAPTER ELECTRICAL ELECTRONIC PANELS AND MULTIPURPOSE PARTS...
Page 546: ...INTENTIONALLY LEFT BLANK PA 44 180 180T AIRPLANE MAINTENANCE MANUAL 2L6 PIPER AIRCRAFT...
Page 547: ...2L7 CHAPTER STRUCTURES...
Page 582: ...CHAPTER DOORS 3A18...
Page 593: ...CHAPTER STABILIZERS 3B8...
Page 604: ...CHAPTER WINDOWS 3B22...
Page 611: ...CHAPTER WINGS 3C10...
Page 624: ...CHAPTER PROPELLER 3D1...
Page 643: ...CHAPTER POWER PLANT 3D21...
Page 667: ...CHAPTER ENGINE FUEL SYSTEM 3F1...
Page 681: ...CHAPTER IGNITION 3F16...
Page 712: ...CHAPTER ENGINE INDICATING 3H1...
Page 730: ...CHAPTER EXHAUST 3H19...
Page 734: ...CHAPTER OIL 3I1...
Page 743: ...CHAPTER STARTING 3I11...
Page 755: ...CHAPTER TURBINES 3J1...