The cells to be repaired should be placed on a well-lighted table. Maintain natural contours, if possible, while
repairing. Prevent contact with sharp edges, corners, dirty floors or other surfaces. Repair area must be well-
ventilated. Do not stack cells. Inspect cavities and insure cleanliness prior to installing any cell.
2. When storing cells, observe the following rules:
A.
Fold cells smoothly and lightly as possible with a minimum number of folds. Place protective
wadding between folds.
B.
Wrap cell in moisture-proof paper and place it in a suitable container. Do not crowd cell in container,
use wadding to prevent movement.
C.
Stack boxed cells to allow access to oldest cells first. Do not allow stacks to crush bottom boxes.
Leave cells in boxes until used.
D.
Storage area must be dry, 70° F, and free of exposure to sunlight, dirt and damage.
E.
Used cells must be cleaned with soap and warm water prior to storage. Dry, and box as outlined
above.
REPAIR OF FUEL CELLS.
— WARNING —
WHEN SERVICING OR INSPECTING VENDOR EQUIPMENT INSTA L L E D
IN PIPER AIRCRAFT, IT IS THE USER’S RESPONSIBILITY TO REFER TO
THE APPLICABLE VENDOR PUBLICATION.
Procedures for the maintenance, repair and “quick cure” repair of fuel cells constructed of LORAL or
GOODYEAR VITHANE
material, should be referenced to the applicable vendor publication (see VENDOR
P U B L I C ATIONS page, introduction section). There are two methods by which these repairs may be
accomplished. One method is by heat cure, the other is air cure. The end result of either repair is a neat,
permanent repair. The heat repair allows the cell to be cured and ready for reinstallation in two hours while the
air cure method requires that the cell not be moved for 72 hours during the air cure period.
— Note —
Air cure repairs to be made at room temperature at approximately 75°F. For each 10°
drop in temperature add 20 hours cure time. For instance if room temperature reads
65°F, air cure for 92 hours instead of 72 hours.
PA - 4 4 - 1 8 0 / 1 8 0 T
AIRPLANE MAINTENANCE MANUAL
2 8 - 11 - 0 8
Page 28-08
Revised: May 15, 1989
2B4
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...