TOWING.
— CAUTION —
WHEN TOWING WITH POWER EQUIPMENT, DO NOT TURN THE NOSE
GEAR IN EITHER DIRECTION BEYOND ITS STEERING RADIUS LIMITS
AS THIS WILL RESULT IN DAMAGE TO THE NOSE GEAR AND
STEERING MECHANISM. WHEN MOVING THE AIRCRAFT FORWA R D
BY HAND, AVOID PUSHING ON THE TRAILING EDGE OF THE
AILERONS AS THIS WILL CAUSE THE AILERON CONTOUR TO
CHANGE RESULTING IN AN OUT-OF-TRIM CONDITION.
The airplane may be moved by using the nose wheel steering bar that is stowed below the forward ledge of
the rear baggage compartment or power equipment that will not damage or cause excess strain to the nose gear
steering assembly. Tow bar engages front axle inside fork.
In the event towing lines are necessary, lines (rope) should be attached to both main gear struts as high up on
the tubes as possible. Lines should be long enough to clear the nose and / or tail by not less than 15 feet, and a
qualified person to ride in the pilot's seat to maintain control by use of the brakes.
TAXIING.
Before attempting to taxi the airplane, ground personnel should be checked out by a qualified pilot or other
responsible person. Engine starting and shutdown procedures should be covered as well. When it is ascertained
that the propeller back blast and taxi areas are clear, apply power to start the taxi roll and perform the following
checks:
1. Taxi forward a few feet and apply brakes to determine their effectiveness.
2. Taxi with propellers set in low pitch, high RPM setting.
3. While taxiing, make slight turns to ascertain the effectiveness of steering.
4. Observe wing clearances when taxiing near buildings or other stationary objects. If possible, station a
guide outside the airplane to observe.
5. When taxiing on uneven ground, look for and avoid holes and ruts.
6. Do not operate the engines at high RPM when running up or taxiing over ground containing loose stones,
gravel, or any loose material that may cause damage to the propeller blades.
— END —
PA - 4 4 - 1 8 0 / 1 8 0 T
AIRPLANE MAINTENANCE MANUAL
9 - 2 0 - 0 0
Page 9-01
Revised: May 15, 1989
1C13
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...