# TCDS A-797: FS 2002 Corp. - Type: Type certificate data sheet - Status: Current - Holder: FS 2002 Corp. - Revision: 11 - Revised: March 30, 2001 - Product: Aircraft, Small Airplane - Certification basis: CAR 3 - Registered aircraft: 100, by the registry models matched to it (OpenAirDocs) - Data sheet PDF: https://openairdocs.org/files/sha256/a9/df/a9df3b23d6f1ef8659326891d269ffaaa7fcfd28fe9156a98d80c8c43a91c854 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/FD34B4A887CF0AB786256A61006CAC5C.0001 - Page: https://openairdocs.org/tcds/A-797 ## Models (1) As the data sheet lists them. - PA-14 ## What the data sheet says From the PDF's text layer, line by line; tables lose their columns. The PDF is the record. ```text P a g e N o . 1234 Rev. No. 11 11 9 9 DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION A-797 Revision 11 FS 2002 Corp. PA-14 March 30, 2001 AIRCRAFT SPECIFICATION NO. A-797 Type Certificate Holder FS 2002 Corporation. 709 Dupont Street, P. O. Box 1678 Bellingham, WA 98227-1678 Type Certificate Ownership Record The New Piper Aircraft, Inc. 2926 Piper Drive Vero Beach, Florida 32960 TC 797 transferred 9-25-00, reissued 3-30-01 I - Model PA-14: 4 PCLM (Normal Category), 2 PCLM (Utility Category); Approved August 26, 1948 Engine Lycoming O-235-C1 Fuel 80 minimum octane aviation gasoline Engine Limits Take-off, 2800 r.p.m. (115 hp) Airspeed Limits Maneuvering 97 mph (84 knots) (True Indicated) Max. Structural Cruising 110 mph (96 knots) Never exceed (Normal Category) 138 mph (120 knots) Never Exceed (Utility Category) 148 mph (129 knots) Flaps extended 85 mph (74 knots) C. G. Range Normal Category: (+9.0) to (+21.0) Utility Category: (+9.0) to (+18.6) Empty Weight C. G. Range (+8.6) to (+12.9) for Serial Nos. 14-1 to 14-489 (+8.6) to (+11.7) for Serial Nos. 14-490 and up with adjustable front seats Ranges are valid regardless of category but are not valid for non-standard arrangements. When empty weight C. G. falls within the pertinent range, computation of critical fore and aft C. G. positions is unnecessary. Datum Wing leading edge Leveling Means Plumb bob from hole in upper door frame near center to hole in lower door frame Maximum Weight Normal Category: 1850 lbs. Utility Category: 1550 lbs. Number of Seats 4 (2 at +12 and 2 at +42) Rear seats may not be occupied for operation in Utility Category. On Serial Nos. 14-490 and up, front seats are adjustable from (+12) to (+15). Maximum Baggage 80 lbs. (+60) for Normal Category only Fuel Capacity 35 gallons (Two 17.5 gallon wing tanks) (+23) A-797 2 Oil Capacity 1.5 gallons (-41) Control Surface Stabilizer 1° 15' Up 5° 30' Down Movements Elevator 27° Up 18° Down Aileron 31° Up 25° Down Rudder 20° Left 20° Right Flaps 50° Down Serial Numbers Eligible 14-1 and up Required Equipment In addition to the pertinent required basic equipment specified in CAR 3, the following items of equipment must be installed: Landplane: Items 1, 201(a), 202, 204(a), and 401(a). Skiplane: Items 1, 205, 401(a) and (b). Airplane is eligible for original certification with or without wing flaps. Specifications Pertinent to All Models Certification Basis Type Certificate No. 797 (CAR 3) Production Basis None. Export Eligibility Deleted as of August 14, 1995. Equipment: A plus (+) or minus (-) sign preceding the weight of an item indicates net weight change when that item is installed. Approval for the installation of all items of equipment listed herein has been obtained by the aircraft manufacturer except those items preceded by an asterisk (*). The asterisk denotes that approval has been obtained by someone other than the aircraft manufacturer. Propellers and Propeller Accessories 1. Propeller - Sensenich FP-76RM39, or any other fixed pitch wood propeller which is eligible for the engine speed and power and which meets the following limits: Static r.p.m. at max. permissible throttle settling: Not over 2500, not under 1970. No additional tolerance permitted. Diameter: Not over 76 inches, not under 72.5 inches +11 lbs. (-62) *2. Propeller - Koppers Aeromatic F200 with 00-74E blades Parts List Assembly No 4292-A, dated April 9, 1948. Low pitch 11° at 24" station. Static r.p.m. at max. permissible throttle setting: Not over 2750, not under 2650. No additional tolerance permitted. Diameter: Not over 74 inches, not under 72.5 inches The following note must be inserted in the Airplane Flight Manual: "Aeromatic Propeller F200/00-74E - Installation and Operation, must be accomplished in accordance with Koppers 'Installation Procedure and Operation Limitation' dated March 10, 1948." Item 401(c) required with this propeller. +21 lbs. (-62) *3. Propeller - 2 position controllable, Sensenich Hub C-2FM-4, Blades PC-276A6 Pitch settings at 28.5" sta.: Low 11.5°, high 14.5° Diameter: Not more than 74 inches, not less than 72.5 inches Item 401(c) required with this propeller. +15 lbs. (-62) *4. Propeller - fixed pitch metal, McCauley 1C90-LM/7254 or any other model 1C90-LM propeller which meets the following limits: Static r.p.m. at max. permissible throttle setting: No over 2310, not under 2180. No additional tolerance permitted. Diameter: Not over 72 inches, not under 70.5 inches Item 401(c) required with this propeller. +23 lbs. (-62) 3 A-797 *5. Propeller - fixed pitch metal, Sensenich model M76AM-2-47, M76AM-2-54 or any other M76AM propeller which meets the following limits: Static r.p.m. at max. permissible throttle setting: Not over 2500, not under 2150. No additional tolerance permitted. Diameter: Not over 74 inches, not under 72.5 inches Item 401(c) required with this propeller. +24 lbs. (-62) Engines and Engine Accessories - Fuel and Oil Systems *101. Oil filter, Fram PB5, Kit No. K-520, Fram Dwg. 62704 and Instruction Sheet 62703 (weight includes 1 quart oil) +5 lbs. (-28) Landing Gear and Floats 201. Two main wheel-brake assemblies, 8.00-4, Type III (a) Goodrich Model 841A Wheel Assembly #D-3-13-A-1 Brake Assembly #D-2-113 +10 lbs. (+1) 202. Two main wheel 4 ply-rating tires, 8.00-4, Type III with reg. tubes +21 lbs. (+1) 204. Tail wheel assembly (a) Scott Model 3-24B, Steerable, full swiveling +5 lbs. (+200) 205. Two skis (a) Federal A-1850 (b) Federal A-2000 or A-2000A per Federal Dwg. 11R262 *(c) Wesco per Western Aircraft Equipment Company Dwg. Nos. 12 and 148: (1) AS-2, (2) AS-2A, (3) AS-2B, (4) A-20, (5) A-25 Use Actual Weight Change *210. Consolidair Model 17 wheel fenders (installed in accordance with Consolidair Dwg. No. 0039) +9 lbs. (+1) *211. Tandem gear Model GW-100 installed in accordance with A. W. Whitaker, 5001 N.E. Union Avenue, Portland, Oregon, Dwg. T-10 and Installation Instructions dated June 8, 1949. +46 lbs. (+1) Electrical Equipment 301. Battery (12 volt) and box +25 lbs. (+7) 302. Position lights +3 lbs. (+65) 303. Landing lights in wing leading edge per Piper Dwg. 12534 +4 lbs. (+5) Interior Equipment 401. (a) CAA (FAA) Approved Airplane Flight Manual, Piper Model PA-14, dated March 10, 1948, for Serial Nos. 14-1 to 14-489 and dated D ecember 16, 1948, for Serial Nos. 14-490 and up. (b) Skiplane Supplement to Manual as follows: Performance Information with Ski Installation. Climb: Skiplane climb performance is essentially equal to that of the landplane. Take-off and landing: Under the most favorable conditions of smooth packed snow at temperature approximating 30°F, skiplane take-off distance is essentially equal to the landplane distance. Landing distance is approximately 20% greater than the landplane distance. In applying the performance data, caution should be exercised in that lower temperatures or other snow conditions will increase the ski friction and hence increase the take-off run and decrease the landing run. (c) When the Item 2, 3, 4 or 5 propeller is installed, the Airplane Flight Manual should be revised to reflect this installation under "Limitations" section and under "Performance" section, the following statement shall be added following Item 4 of the section: "5. Performance with the model _______ propeller has been demonstrated to equal or exceed that presented herein over the altitude and temperature range shown." Miscellaneous (not listed above) *601. Fuselage metal plating when installed in accordance with Met-Co-Aire's Dwg. No. 12108, 13108, and Installation Instructions dated June 17, 1954, issued by Met-Co-Aire Co., Municipal Airport, Fullerton, California. Use Actual Weight Change and Moment Arm A-797 4 NOTE 1. Current weight and balance report including list of equipment included in certificated weight empty, and loading instructions when necessary, must be in each aircraft at the time of original certification and at all times thereafter (except in the case of air carrier operators having an approved weight control system). NOTE 2. The following placards must be displayed on the instrument panel in full view of the pilot: (a) "This airplane must be operated as a Normal or Utility Category airplane in accordance with the Limitations in the CAA Approved Airplane Flight Manual. Airplane marked and placarded for Normal Category. No acrobatics including spins approved in Normal Category. No acrobatics approved for Utility Category except those listed in Airplane Flight Manual." (b) "No Smoking." (c) "Right tank should be used in level flight only." ....END.... ``` ## ADs (12, in force first) - [AD 2025-02-11](https://openairdocs.org/ad/2025-02-11): Rudder Structure · FS 2001 J5A (Army L-4F), J5A-80, J5B (Army L-4G) and 67 more. Effective Mar 20, 2025 - [AD 2015-08-04](https://openairdocs.org/ad/2015-08-04): Wings · FS 2000 L-14, AE-1, HE-1 and 77 more. Effective Jun 3, 2015 - [AD 2001-23-17](https://openairdocs.org/ad/2001-23-17): GNS 430 units · Cessna 172, 182, 206 and 209 more. Effective Dec 28, 2001 - [AD 85-06-04](https://openairdocs.org/ad/85-06-04): Fuel Tank · FS 2001 AE-1, HE-1, J5A-80 and 60 more. Effective May 4, 1985 - [AD 78-10-03](https://openairdocs.org/ad/78-10-03): Fuel Venting · FS 2001 AE-1, HE-1, J5A-80 and 66 more. Effective May 23, 1978 - [AD 74-17-04](https://openairdocs.org/ad/74-17-04): Fabric Reinforcement · FS 2002 PA-14, PA-12, PA-12S and 18 more. Effective Apr 11, 1977 - [AD 68-05-01](https://openairdocs.org/ad/68-05-01): Exhaust Mufflers · FS 2001 J5A-80, J5A (Army L-4F), J5B (Army L-4G) and 67 more. Effective Mar 31, 1968 - [AD 60-01-07](https://openairdocs.org/ad/60-01-07): Tail Brace Wires · FS 2002 PA-14, PA-12, PA-12S and 5 more - [AD 49-27-02](https://openairdocs.org/ad/49-27-02): Aileron Bellcrank Castings · FS 2002 PA-14 and PA-12 - [AD 99-01-05 R1](https://openairdocs.org/ad/99-01-05-R1) (historical): Wings · FS 2000 L-14, AE-1, HE-1 and 73 more. Effective Jan 14, 2014 - [AD 99-01-05](https://openairdocs.org/ad/99-01-05) (historical): Wing Lift Struts or Forks · FS 2000 L-14, AE-1, HE-1 and 73 more. Effective Feb 8, 1999 - [AD 93-10-06](https://openairdocs.org/ad/93-10-06) (historical): Corroded Wing Lift Struts or Cracked Forks · Piper Aircraft, Inc., The New J-2, J-3, J4 and 28 more. Effective Jul 9, 1993 ## Registered aircraft by registry model (OpenAirDocs) - [Piper PA-14](https://openairdocs.org/model/piper-pa-14): 100 aircraft (registry code 7101402) ## STCs approved under this data sheet (219, first 50) - [STC SA01233SE](https://openairdocs.org/stc/SA01233SE): Fabrication and installation of Alaskan Bushwheel LLC tail wheel and fork assembly. ABI, LLC - [STC SA12428CH](https://openairdocs.org/stc/SA12428CH): Installation of the Lycoming Engines Electronic Ignition System (EIS). Lycoming Engines, An Operating Division of AVCO Corporation - [STC SA04837NY](https://openairdocs.org/stc/SA04837NY): Installation of AeroLED's Holdings, LLC., position lights, navigation lights, strobe lights and beacon lights. AeroLED's Holdings, LLC - [STC SA12406WI](https://openairdocs.org/stc/SA12406WI): Installation of a Garmin AXIS Flight Display System. Garmin International Inc. - [STC SA04652CH](https://openairdocs.org/stc/SA04652CH): To allow use of 100R grade aviation fuel meeting Swift Fuel, LLC specification. Swift Fuels LLC - [STC SA800EA](https://openairdocs.org/stc/SA800EA): Installation of Whelen Anti-Collision, Position, or Anti-Collision/Position Light System, and applicable associated power supplies. Whelen Aerospace Technologies - [STC SA02525LA](https://openairdocs.org/stc/SA02525LA): Installation of Wheel and Brake Assemblies. Game Aerospace LLC - [STC SA01704LA](https://openairdocs.org/stc/SA01704LA): Installation of the Grove Disk Brake System. Grove Aircraft Landing Gear Systems Inc. - [STC SA00081NY](https://openairdocs.org/stc/SA00081NY): Installation of Iceman Aviation Supplies, Inc. Carburetor Ice Detector.. Alcor LLC - [STC SA7965SW](https://openairdocs.org/stc/SA7965SW): Application of fabric and polyurethane finishing system.. Shady Aviation LLC - [STC SA11854CH](https://openairdocs.org/stc/SA11854CH): Installation of modified exhaust system in lieu of original components. Dakota Cub Aircraft Inc. - [STC SA02764SE](https://openairdocs.org/stc/SA02764SE): Installation of Acme Aero Shock landing gear shock absorbers. Acme Suspensions LLC - [STC SA02765SE](https://openairdocs.org/stc/SA02765SE): Installation of Acme Stinger tailwheel landing gear shock absorber. Acme Suspensions LLC - [STC SA00805CH](https://openairdocs.org/stc/SA00805CH): Installation of Air-Energy Service Inc. (AESI) P/N AESI-12-1900 (-1) wing fuel tanks.. Crown MN Aviation LLC - [STC SA01333CH](https://openairdocs.org/stc/SA01333CH): Installation of a 24-gallon wing fuel tanks.. Crown MN Aviation LLC - [STC SA01757WI](https://openairdocs.org/stc/SA01757WI): To allow the use of UL91 or UL94 (minimum) grade aviation fuel. Swift Fuels LLC - [STC SA01343WI](https://openairdocs.org/stc/SA01343WI): Installation of B&C Specialty Products BC400 alternator. B & C Specialty Products Inc. - [STC SA4503NM](https://openairdocs.org/stc/SA4503NM): Remove original cloth covering and install Ceconite covering. Ceconite Division of Poly-Fiber Inc. - [STC SA02582AK](https://openairdocs.org/stc/SA02582AK): Installation of Airframes Alaska Brake Pedal and Master Cylinder Assembly. Airframes Alaska LLC - [STC SA02581AK](https://openairdocs.org/stc/SA02581AK): Installation of Ground Adjustable Sensenich Composite 2G0M(X)/C82BGF Propeller. Sensenich Propeller Company - [STC SA02576AK](https://openairdocs.org/stc/SA02576AK): Installation of Cleveland and ABI, LLC Wheel and Brake Kits. ABI LLC - [STC SA02233AK](https://openairdocs.org/stc/SA02233AK): Installation of high visibility fuel sight gauge.. Dakota Cub Aircraft Inc. - [STC SA02987CH](https://openairdocs.org/stc/SA02987CH): Installation of the Electroair Electronic Ignition System. Electroair Acquisition Corporation - [STC SA5-33](https://openairdocs.org/stc/SA5-33): Removed unbalanced tail surfaces and installed balanced tail surfaces. Install elevators, Piper P/N 12789-00 and 12789-01 and stabilizers, Piper P/N 12790-00 and 12790-01. Wilbur Repair Service Marguerite Benson or Anne Wilbur - [STC SA02534AK](https://openairdocs.org/stc/SA02534AK): Installation of Airframes Alaska Aluminum Lift Struts. Airframes Alaska LLC - [STC SA01967WI](https://openairdocs.org/stc/SA01967WI): Use of GAMI G100UL High Octane Unleaded Avgas. General Aviation Modifications Inc. - [STC SA02203AK](https://openairdocs.org/stc/SA02203AK): Installation of FlightLogic Synthetic Vision Electronic Flight Information System (EFIS-SV).. Genesys Aerosystems Inc. - [STC SA02123AK](https://openairdocs.org/stc/SA02123AK): Installation of Baumann Model BF-2100 floats.. Baumann Floats LLC - [STC SA04776NY](https://openairdocs.org/stc/SA04776NY): The HIPEC Covering and Finishing System must be performed and maintained. HIPEC Aircraft Coatings Inc. - [STC SA02153AK](https://openairdocs.org/stc/SA02153AK): Installation of Burl's Aircraft Rebuild Magnum I tail wheel Penetration ski. Burl's Aircraft Rebuild LLC - [STC SA02214AK](https://openairdocs.org/stc/SA02214AK): Installation of Alpha Omega Suspension System in place of original bungees or bungees and hydasorbs.. Burl's Aircraft Rebuild LLC - [STC SA01015SE](https://openairdocs.org/stc/SA01015SE): Installation of eligible Alaska Bushwheel, Inc. wheels and TSO-C62d tires. ABI LLC - [STC SA02553AK](https://openairdocs.org/stc/SA02553AK): Fabrication and installation of a Tail Wheel Anti-Shimmy Dampener. Keller Engineering Group LLC - [STC SA04474CH](https://openairdocs.org/stc/SA04474CH): Installation of Rubbert Exhaust Assembly RR-1210, RR-1210-HR, RR-1212 and RR-1212-HR on Piper Aircraft models PA-12, PA- 14, PA-16, PA-18, PA-19, PA-20 and PA-22, in accordance with Installation Instructions, document number RR-120, revision Org., dated 04/24/2020 and Instruct 1201, revision Org., dated July 27, 2020 or later FAA approved revision.. Rubbert Aircraft Services - [STC SA01831WI](https://openairdocs.org/stc/SA01831WI): To allow the use of UL91 (minimum) grade aviation fuel. Petersen Aviation Inc - [STC SA03328CH](https://openairdocs.org/stc/SA03328CH): Installation of Lycoming O-320 or O-360 engine. Svenn's Aviation LLC - [STC SA04032CH](https://openairdocs.org/stc/SA04032CH): Install rocker switch assemblies. Electroair Acquisition Corporation - [STC SA00344BO PAGE 1](https://openairdocs.org/stc/SA00344BO%20PAGE%201): Installation of Parmetheus Plus LED PAR36 and PAR46 taxi and landing lights.. Whelen Aerospace Technologies - [STC SA615EA](https://openairdocs.org/stc/SA615EA): Installation of a Whelen Anti-Collision Strobe Light System as replacement for originally installed anti-collision lights.. Whelen Aerospace Technologies - [STC SA1629WE](https://openairdocs.org/stc/SA1629WE): Installation of left-hand door and associated fuel line routing and stabilizer trim cable changes. (PA-14 S/N 14-66, N4262H). Kenmore Air Harbor LLC - [STC SA4-78](https://openairdocs.org/stc/SA4-78): Installation of a Lycoming O-320 engine and Sensenich M74DM59 propeller. Installation of Piper PA-18A-150 engine cooling baffles, modified to fit cowling. Installation of oil cooler (Harrison AP13SJ03-01) in accordance with Piper Drawing 14368. Installation of pressure type gas tank caps.. John P. Warren - [STC SA04165NY](https://openairdocs.org/stc/SA04165NY): Installation of Latitude Technologies Skynode S200 Satcom system must be performed. Latitude Technologies Corporation - [STC SA00024NY](https://openairdocs.org/stc/SA00024NY): Installation of Airwolf remote mounted engine oil filter kit AFC-K007 on single or multi-engine fixed wing light aircraft incorporating Lycoming reciprocating engines of 450 horsepower or less.. Airwolf Filter Corporation - [STC SA02212AK](https://openairdocs.org/stc/SA02212AK): Replacement of existing landing and/or taxi light reflector and bulbs with high intensity discharge (HID) lighting systems. Seaplanes North LLC - [STC SA3606NM](https://openairdocs.org/stc/SA3606NM): Installation of landing gear fueling step.. F. Atlee Dodge Aircraft Services, LLC - [STC SA01734SE](https://openairdocs.org/stc/SA01734SE): Application of Stewart Systems synthetic fabric covering system to aircraft fuselage, wings, tail surfaces, control surfaces and related parts.. Andrew D. Humphrey - [STC SA00780SE](https://openairdocs.org/stc/SA00780SE): Installation of the True Lock Safety Retention Axle Lock Nut System. True Lock LLC - [STC SA02734CH](https://openairdocs.org/stc/SA02734CH): Installation of Lightweight Battery and Circuit Breaker Master Switch in lieu of original components. Svenn s Aviation LLC - [STC SA02452AK](https://openairdocs.org/stc/SA02452AK): Installation of F. Atlee Dodge Aircraft Services, LLC, Pilot s Safety Barrier Net. F. Atlee Dodge Aircraft Services, LLC - [STC SA00478CH](https://openairdocs.org/stc/SA00478CH): Installation of Cooper Superflite 102 Fabric.. Aviation Products Systems Inc. All 219: https://openairdocs.org/tcds/A-797/stcs.md --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.