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INTRODUCTION

The Piper Progressive Inspection meets the F.A.A. progressive inspection requirements of F.A.R. 91.407,
for use in the corporation’s transportation and personnel; i.e., air taxi purposes, air freight, air mail, etc.

At least one complete 200 hour cycle must be accomplished within 12 calendar months since the
completion of the last 200 hour cycle. For example: if the 600 hour cycle is completed on March 12, of a
given year, the next 200 hour cycle must be completed by the time 800 hours time-in-service has been
accumulated, or on or before April 1, of the next year, whichever comes first. Should the 800 cycle be
completed by November of the same year, then the next 200 hour cycle must be completed by the time
1000 hours time-in-service has been accumulated, or on or before December 1, of the next year,
whichever comes first, etc.

FACTS YOU SHOULD KNOW

Every two weeks the Federal Aviation Administration (FAA) publishes Airworthiness Directives (ADs) that
apply to specific groups of aircraft.They are mandatory changes and are to be complied with within a time
limit set by the FAA. When an AD is issued, it is sent to the latest registered owner of the affected aircraft
and also to subscribers of the service. The owner should periodically check with his Piper Service Center
or A & P mechanic to see whether he has the latest issued AD against his airplane. The owner is solely
responsible for keeping up with ADs.

Piper Aircraft Corporation takes a continuing interest in having the owner get the most efficient use from
his airplane and keeping it in the best mechanical condition. Consequently, Piper Aircraft from time to time
issues Service Bulletins, Service Letters, and Service Spares Letters relating to the aircraft.

Service Bulletins are of special importance and Piper considers compliance mandatory . These are sent
to the latest registered owners. Piper Service Centers and Corporate Aircraft Centers.

Service Letters deal with product improvements and service hints pertaining to the aircraft. They are sent
to Piper Service Centers and Corporate Aircraft Centers and sometimes directly to owners so they can
properly service the aircraft and keep it up to date with the latest changes. Owners should give careful
attention to the Service Letter information.

Service Spares Letters, which are usually sent to Piper Service Centers and Corporate Aircraft Centers,
offer improved parts, kits and optional equipment which were not available originally and which may be of
interest to the owner.

An owner should periodically check with a Piper Service Center or Corporate Aircraft Centers to find out
the latest information to keep his aircraft up to date.

Piper Aircraft Corporation has a Subscription Service for the Service Bulletins, Service Letters and
Service Spares Letters. This service is offered to interested persons such as owners, pilots and mechan-
ics at a nominal fee, and may be obtained through Piper Service Centers and Corporate Aircraft Centers.
Owners residing outside of the United States are urged to subscribe to this service since Piper can sel-
dom otherwise obtain the addresses of foreign owners. Service Product Support Manuals and revisions
are available through a Piper Service Center.

Interim Revision: October 26, 1994

Page 3

Содержание CHEYENNE PA-31T

Страница 1: ...CHEYENNE PIPER PROGRESSIVE INSPECTION 50 HOUR CYCLE PA 31T PA 31T1 PIPER AIRCRAFT CORPORATION PART NUMBER 761 520 IR OCTOBER 26 1994...

Страница 2: ...shed by PUBLICATIONS DEPARTMENT Piper Aircraft Corporation 761 520 Issucd December 8 1973 Reissued May 1 1981 Reissued February 22 1983 Reissued December 16 1983 Interim Revision April 30 1986 Interim...

Страница 3: ...airplane and keeping it in the best mechanical condition Consequently Piper Aircraft from time to time issues Service Bulletins Service Letters and Service Spares Letters relating to the aircraft Ser...

Страница 4: ...of Canada Ltd 50x 10 Longuevil Que Canada 34K4X9 Hartzell Compact Constant Speed and Feathering Propeller Part No 118 D Hartzell Propeller Inc Piqua Ohio 45356 Gulton Nickel Cadmium Aircraft Battery P...

Страница 5: ...nual 23048 Series Lear Siegler Power Equipment Division Part No 23202 Lear Siegler Inc 17600 Broadway Ave Maple Heights Ohio 44137 Maintenance and Overhaul Manual Auxilec Part No 8013C Auxi let Inc 53...

Страница 6: ...tion Record and Sign Off Sheet Continuous Cycle Inspection Record and Sign Off Sheet Discrepancy Record Service Publication Compliance Record FAA A D Compliance Record Equipment Change Record Access P...

Страница 7: ...Right Wing Detailed 31 Right Propeller Routine 31 Right Engine Routine 31 Left Wing Routine 32 Left Propeller Detai fed 32 Left Engine Detailed 33 Fuselage Forward Routine 34 Fuselage Main Routine 34...

Страница 8: ...t 43 Right and Left Wing 43 Cabin Pressurization Check 43 Starter Generator 43 Engine Fuel Pump 43 800 HOUR 44 Oil Drain Period 44 1000 HOUR 44 Right and Left Engines 45 Right and Left Wings 45 LANDIN...

Страница 9: ...OPERATIONAL INSPECTION 47 Pre Run Up 47 Engine Start 47 Run Up and Operational Checks 48 Engine Shutdown 50 Emergency Check List Engine Fire Ground 51 EVENT INSPECTION RECORD AND SIGN OFF SHEET 52 CO...

Страница 10: ...cy used in the Piper Continuous Inspection is based on previous PA 31 T 31 Tl Operating experience However adjustments to the inspection intervals can be made only by Piper Aircraft Corporation Discre...

Страница 11: ...50flying hour interval for the next event inspection will be maintained The Event Inspections are arranged so that the 200 flying hour cycle results in a complete inspection When the Four Events are...

Страница 12: ...ion 5 Event Inspection Record and Sign Off Sheet is a permanent record and contains the following 1 Event Inspection Number 2 Aircraft Hours Tach 3 Date Accomplished 4 Work Order Number FAA approved r...

Страница 13: ...Aircraft Hours 6 Work Order Number FAA approved repair stations only 7 Signature and Certificate Number of person accomplishing the compliance 9 FAA Airworthiness Directives Compliance Record is used...

Страница 14: ...be deducted from the next inspection This ten 10 percent shall only be used to return the aircraft back to the maintenance base when inspection intervals fall due and the aircraft is away from home ba...

Страница 15: ...ioning properly This person will log the bench test and operational test in the permanent aircraft records Serviceable parts that were issued to the component will be filed in the aircraft permanent r...

Страница 16: ...orm to their local FAA GADO office Aduplicate copy should be maintained in this manual Address Street City State Zip Telephone Number Any change in personnel responsible for scheduling the inspection...

Страница 17: ...hanges can be made to this inspection program unless prior notice is given to the responsible FAA dis trict office who in turn must approve of the change prior to its enactment A record of all revisio...

Страница 18: ...ately rated certified mechanic qualified on this type aircraft The results of the inspection will be noted on the proper Sign Off Sheets which are then brought back to the home base The pilot will be...

Страница 19: ...tion of ignition plugs per P W Maintenance Manual 8 Inspect ignition harness and insulators for high tension leakage and continuity Piper Service Manual Section Vlll 9 Inspect electrical connections o...

Страница 20: ...nspect rubber engine mount for deterioration refer to Special Inspection 40 hours 34 Inspect firewall for cracks and stress 35 Inspect firewall seals 36 Inspect condition of starter generator refer to...

Страница 21: ...light for operation if applicable 22 Inspect wing tip navigation and strobe lights for broken lenses and operation replace bulb or flash tube as required 23 Lubricate as per Piper Service Manual Sect...

Страница 22: ...place bulb or flash tube as required 9 Lubricate as per Piper Service Manual Section II 1 Remove inspection plates and panels and open Radome 2 Inspect baggage door latch hinges door ajar switch and c...

Страница 23: ...ernal skins for condition damage and corrosion 23 Lubricate as per Piper Service Manual Section 11 24 Reinstall inspection plates and panels and close Radome 1 Remove inspection plates panels and floo...

Страница 24: ...knobs Inspect circuit breakers for condition and security of installation Check cabin pressure controller filter change as required Refer to 200 and 500 hour Special Inspection With master switch on...

Страница 25: ...able Check isobaric and safety valve cover screen for obstruction rear baggage compartment See latest Garrett Airesearch Service Bulletin No 5 2243 and 5 2294 Inspect isobaric valve filter change as r...

Страница 26: ...er Service Manual section VII 0 7 Inspect actuating cylinder for leaks and security 0 8 Inspect condition of up and downlock springs 0 9 Lubricate as per Piper Service Manual section II I NOSE GEAR RO...

Страница 27: ...ace bearing if ball is frozen or hard to move 20 Check elevator trim mechanisms for operation and full travel 21 Inspect rudder elevator and trim cables turnbuckles guides and pulleys for safety cable...

Страница 28: ...ervice Manual Section Vlll See Note 2 6 Clean exterior of engine P W Maintenance Manual 7 Inspect condition of ignition plugs per P W Maintenance Manual 8 Inspect ignition harness and insulators for h...

Страница 29: ...for security 31 Inspect engine mounts for cracks and loose mount bolts Piper Service Manual Section Vlll 32 Inspect P3 air filter for foreign material clean as required P W Maintenance Manual Refer t...

Страница 30: ...s 15 Inspect rubber engine mounts for deterioration refer to Special Inspection 400 hour 16 Inspect fire extinguisher pressure Piper Service Manual Section XIV 17 Inspect condition of starter generato...

Страница 31: ...on IX 16 Check fuel tanks for proper placards fuel cap7s for proper seal and quick drains for proper operation 17 Check fuel tanks marked for correct operating fuel 18 Inspect fuel vents for blockage...

Страница 32: ...owl LEFT WING ROUTINE 13 1 Check surfaces skins and tip for damage loose rivets and corrosion Cl 2 Inspect aileron and attachments for security and corrosion El 3 Inspect aileron balance weight and ar...

Страница 33: ...nd replace on condition Refer to Piper Service Manual Section Ill Inspect gas generator case drain valves for security and leaks to be checked during engine run P W Maintenance Manual Inspect conditio...

Страница 34: ...ion and security check at least every thirty 30 days and clean as required per Piper Service Manual Section XI l 4 Lubricate as per Piper Service Manual Section II r 5 Inspect hydraulic power pack flu...

Страница 35: ...n c 6 Inspect cabin entrance door for damage and operation q 7 Lubricate as per Piper Service Manual Section II tf 8 Check isobaric and safety valve cover screen for obstructions rear baggage compartm...

Страница 36: ...o 682 18 Inspect warning horn and light for operation 19 Retract gear check operation 20 Retract gear check doors for clearance and operation 21 Inspect anti retraction system 22 Inspect actuating cyl...

Страница 37: ...r strut attachments torque link retraction links and bolts for condition security and corrosion 11 Inspect down lock and up lock for operation and adjustment 12 Clean and inspect up and down lock actu...

Страница 38: ...r cracks security and corrosion 0 5 Inspect propeller mounting bolts and safety check torque if safety is broken Piper Service Manual Section VIII a 6 Inspect hub parts for cracks and corrosion fl 7 R...

Страница 39: ...oil leaks Inspect all flexible fines fuel hydraulic and oil replace on condition Refer to Piper Service Manual Section 111 Lnspect fuel system for leaks Check electric fuel pumps for operation Replace...

Страница 40: ...on lever and propeller governor for travel and operating conditions Piper Service Manual Section VIII I 13 Inspect breather tube for obstructions and security Cl 14 Inspect propeller shaft for oil lea...

Страница 41: ...dow per section IV of the service manual HEATER INSPECTION 0 1 Conduct 190 hour inspection of affected heaters per AD 82 07 03 and in accordance with Janitrol s Maintenance and Overhaul Manual P N 24E...

Страница 42: ......

Страница 43: ...and Overhaul Manual P N 24E25 1 dated October 1981 and AD 82 07 03 2 Operational check or replace heater fuel pump 3 Replace heater fuel filter 4 Operational check and or replace heater fuel solenoid...

Страница 44: ...igh utilization commuter airline type operation a basic oil drain period of 800 hours for 7 1 2 centistoke or 1200 hours for a 5 centistoke oil or 9 months whichever occurs first Extensions beyond bas...

Страница 45: ...tion Xl PA 31 T only 1 Inspect fuel cells every two years or 2000 hours whichever comes first Refer to Piper Service Manual Section IX 2 For aircraft equipped with Calco Flap Control System remove ser...

Страница 46: ...al 1 Refer to UACL Maintenance Manual 1 Check with the appropriate manufacturer for the necessary corrective action 1 Consult P W Agtoil 7 for frequency and instructions Observe starter limitations Pa...

Страница 47: ...Off Checked Checked 3 green Checked ENGINE START When APU is used turn battery master switch off and monitor airplane voltmeter until reading stabilizes 27V min 30V max then turn the battery master sw...

Страница 48: ...ontrols 10 Flaps 11 Pneumatic boots check a Pneumatic pressure b Deicer switch 12 Power levers 13 Hydraulic topping governor HTG test a Propeller control b HTG test switches Off To red line Right fuel...

Страница 49: ...ch g Observe regain of original torque h Repeat Steps a through g above for Right Engine 1800 RPM Np ON ON LEFT PRESS AND HOLD OFF CAUTION Engine Inlet Lip Deicers can be damaged if heated without the...

Страница 50: ...th more than 60 Ng in reverse e Prop feathering ENGINE SHUTDOWN 1 Parking brake 2 Avionics master switch 3 Electrical equipment 4 Battery check charge condition a Battery master switch OFF observe amm...

Страница 51: ...MERGENCY CHECK LIST ENGINE FIRE GROUND Affected Engine 1 Condition lever Stop 2 Emergency fuel shutoff valve Off 3 Starter switch On 4 Fuel pump Off 5 Ignition switch Off NOTE Do not attempt to restar...

Страница 52: ...cedures are the responsibility of the individual performing the inspection and must be made in accordance with all applicablecurrent Federal Aviation Regulations Always check for and use only current...

Страница 53: ...53 REISSUED 12 16 83...

Страница 54: ...NTINUOUS INSPECTION 50 HOUR CYCLE SERIAL NUMBER REGISTRATION NUMBER ENGINE SERIAL NO PROPELLER SERIAL NO Left Left Right Right EVENT INSP A C TIME DATE W O 4 2800 1 2850 2 2900 I 4 3000 I I SIGNATURE...

Страница 55: ...FICATE IN AIRCRAFT AND PROPERLY DISPLAYED 5 RADIO STATION F C C LICENSES IN AIRCRAFT AND PROPERLY DISPLAYED 6 AIRCRAFT EQUIPMENT LIST WEIGHT AND BALANCE F A A FORM 337 IF APPLICABLE ARE IN AIRCRAFT AN...

Страница 56: ...56...

Страница 57: ...I I I I i I...

Страница 58: ...REISSUED 12 16 83 58...

Страница 59: ...I I q q I REISSUED 12 16 83...

Страница 60: ...I I i i i t z P E i z 3 i i REISSUED 12 16 83 60...

Страница 61: ...61 REISSUED 12 16 83...

Страница 62: ...REISSUED 12 16 83 62...

Страница 63: ......

Страница 64: ...13 14 GENERATOR SUPPLY CABLE RIGHT GENERATOR SUPPLY CABLE LEFT BATTERY CABLE ELECTRICAL LEADS NOSE WHEEL STEERING ENGINE INSTRUMENT LINES ENGINE INSTRUMENT LINES AND CONTROL CABLES TRIM GABLES CABIN P...

Страница 65: ...RADAR HYDRAULIC RESERVOIR BRAKE SYSTEM ENVIRONMENTAL CONTROL UNITS HYDRAULIC SERVlCE HOOKUP LANDING GEAR EMERGENCY EXIT WINDOW VERTICAL FIN DEICER BOOT CONNECTION ELT TRANSMITTER RUDDER TRIM DRUM ANTI...

Страница 66: ...PECTION 50 HOUR CYCLE SERIAL NUMBER REGISTRATION NUMBER ENGINE SERIAL NO PROPELLER SERlAL NO Left Left Right Right vh PRESSURE VESSEL STATION 274 15 13 II II 25 581 14 3l Access Plates and Panels Fuse...

Страница 67: ...ELLE RIGHT NACELLE 5 9 6 6 9 3 I 1 ICE DEFLECTOR DOOR ROD 2 FUEL FlLTER 3 HEAT EXCHANGER AND PLUMBING 4 OIL FILLER QUANTlTY DIPSTICK 5 OIL COOLER DOOR TRANSMISSION RIGHT NACELLE ONLY AIR CONDITIONING...

Страница 68: ...ANSFORMER STROBE LIGHT 9 ELECTRONIC GEAR 10 AILERON BELLCRANK 11 ELECTRIC FUEL PUMP 12 AILERON CABLE AND FUEL LINE 13 AILERON CONTROL CABLE 14 FLAP TRANSMISSION lb FLAP TIME DELAY SWITCH 16 PNEUMATIC...

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