APPLICATION OF LIQUID SAFETY WALK COMPOUND
— NOTE —
Apply in an area which is free of moisture for a period of 24
hours minimum after application.
— NOTE —
Do not apply when surface to be coated is below 50°F (10° C).
— NOTE —
Do not walk on coated surface for a minimum of six hours after
final coating.
1. Mix and thin liquid safety walk compound per manufacturer’s instructions on container.
2. Coat surfaces with a smooth, unbroken film of liquid safety walk compound. A nap type roller or a
stiff bristle brush is recommended, using fore and aft strokes.
3. Allow coating to dry for 15 minutes to 1 hour before recoating or touch-up, if required, after the initial
coating.
4 . After coating or touch-up, allow coating to dry for 15 minutes to 1 hour before removing masking.
SURFACE PREPARATION FOR PRESSURE SENSITIVE SAFETY WALK
1. Remove all contaminates and moisture.
2. Mask off area to protect painted surfaces.
3. Apply suitable stripper MEK Federal Spec. TT-M-261, U.S.Rubber No. 3339 to wing walk compound.
As compound softens, remove with putty knife or other suitable tool.
4. Prime and paint area.
— NOTE —
For newly painted surfaces allow 2.5 hours minimum drying
time before application of safety walk.
APPLICATION OF PRESSURE SENSITIVE SAFETY WALK
— NOTE —
Do not apply when surface to be coated is below 50°F.
1. Peel back full width of protective liner approximately 2 inches from leading edge of safety walk.
2. Beginning at leading edge, apply safety walk to wing area. Verify proper alignment and position from
wing flap.
3. Remove remaining protective liner as safety walk is being applied.
4. Roll firmly with a long handled cylindrical brush in both lengthwise directions. Verify all edges
adhere to wing skin.
5. Install and rivet leading edge retainer.
PIPER AIRCRAFT
PA - 4 4 - 1 8 0 / 1 8 0 T
AIRPLANE MAINTENANCE MANUAL
51-14-05
Page 51-15
Revised: June 20, 1995
2L23
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...