# N1117H: Piper PA-15

- Status: Valid registration
- Airframe: [Piper PA-15](https://openairdocs.org/model/piper-pa-15) (registry code 7101502, 2 seats)
- Engine: [Lycoming 0-145A series](https://openairdocs.org/engine/lycoming-0-145a-series) (registry code 41501)
- Data sheets: [TCDS A-800](https://openairdocs.org/tcds/A-800) (Piper Aircraft Inc.), [TCDS TC 199](https://openairdocs.org/tcds/TC%20199) (Textron Lycoming AVCO Corporation) (OpenAirDocs)
- Serial number: 15-332
- Type: Fixed wing single engine
- Engine type: Reciprocating
- Certificate issued: August 15, 2018
- Expires: August 31, 2028
- Mode S code: A0333F
- Registered owner: [Senf Raymond L](https://openairdocs.org/faa-owner/SENF%20RAYMOND%20L)
- Location: [Central Square, NY](https://openairdocs.org/faa-place/NY/Central%20Square)
- Owner type: Individual
- Owner's area on the map: 43.3235° N, 76.1890° W: Placed by OpenAirDocs at the center of ZIP code 13036, within about 4 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=1117H
- Page: https://openairdocs.org/aircraft/N1117H

From the FAA registry file of October 24, 2026. ADs below are matched by the registry's airframe and engine model codes. They may apply; each AD's applicability can narrow it by serial number, part number or installed equipment. This is not a compliance determination. The registry lists only the engine series, so ADs for every Lycoming 0-145A model are included.

## ADs that may apply (OpenAirDocs): 11 in force

### Matched by airframe (Piper PA-15)

- [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 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 58-12-02](https://openairdocs.org/ad/58-12-02): Aileron Hinge Brackets · Piper J-3, J3C-40, J3C-50 and 20 more
- [AD 50-23-01](https://openairdocs.org/ad/50-23-01): Shock Strut Fittings · Piper PA-15 and PA-17

### Matched by engine (Lycoming 0-145A series)

- [AD 2012-03-07](https://openairdocs.org/ad/2012-03-07): Carburetor · Lycoming Engines GO-435, GO-435-C2 (O-435-17), GO-435-C2A and 389 more. Effective Mar 27, 2012
- [AD 90-04-06 R1](https://openairdocs.org/ad/90-04-06-R1): Propeller Governor External Oil Line · Lycoming Engines AEIO-320-D1B, AEIO-320-D2B, AEIO-320-E1A and 427 more. Effective May 28, 1991
- [AD 66-06-03](https://openairdocs.org/ad/66-06-03): Connecting Rod Assemblies · Lycoming Engines GO-435-C2 (O-435-17), GO-435-C2A, GO-435-C2A2 and 317 more. Effective Jan 16, 1969

### Historical (superseded or no longer in force)

- [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

## Information bulletins (advisory) (1 in force)

- [SAIB ACE-99-01](https://openairdocs.org/saib/ACE-99-01): . Issued Oct 21, 1998

## NTSB investigations

None matched to N1117H.

## FAA accident and incident reports

None matched to N1117H.

## Service difficulty reports

None filed for this aircraft. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

## Service difficulty reports on N1117H not matched to an aircraft (55, newest 50)

They name N1117H, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR SWIA200210769](https://openairdocs.org/sdr/SWIA200210769), Apr 2, 2002: PROXIMITY SENSOR. FAULTY. THE TAKEOFF TRIM AURAL WARNING SOUNDED ON TAKEOFF ROLL, TRIM WAS SET WELL WITHIN THE GREEN BAND. ABORTED TAKEOFF. REPLACED LEFT HORIZONTAL TRIM PROXIMITY SENSOR
- [SDR SWIA200210692](https://openairdocs.org/sdr/SWIA200210692), Feb 28, 2002: SPLICE. FAULTY. ON TAKEOFF WITH TRIM SET IN THE GREEN BAND, RECEIVED A TAKEOFF TRIM AURAL WARNING. ABORTED THE TAKEOFF PER THE SOP AND TAXIED CLEAR. TESTED THE SYSTEM TWICE AND
- [SDR SWIA200210665](https://openairdocs.org/sdr/SWIA200210665), Feb 25, 2002: WIRE. BROKEN. ROW 2BC EXIT SIGN INOP. REPAIRED BROKEN WIRE AT EXIT SIGN SEAT 2BC.
- [SDR SWIA200210664](https://openairdocs.org/sdr/SWIA200210664), Feb 25, 2002: FUSE. BLOWN. RIGHT FORWARD EXTERIOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED FUSE AT FUSE HOLDER XF0016 IAW WM 20-00-00. OPS CHECK GOOD.
- [SDR SWIA200210505](https://openairdocs.org/sdr/SWIA200210505), Jan 1, 2002: WINDSHIELD. CRACKED. DURING TAXI FOR TAKEOFF, CO-PILOT'S WINDSHIELD CRACKED. REPLACED CO-PILOT'S WINDSHIELD WITH SERVICEABLE UNIT IAW MM 56-10-01 AND RII 56-301.
- [SDR SWIA200110274](https://openairdocs.org/sdr/SWIA200110274), Oct 25, 2001: COMPUTER. FAULTY. ON TAKEOFF ROLL SYSTEM NR 1 STALL WARNING LIGHTS ILLUMINATED. ABORTED TAKEOFF. REPLACED NR 1 STALL WARNING COMPUTER. OPS CHECK GOOD.
- [SDR SWIA200110137](https://openairdocs.org/sdr/SWIA200110137), Aug 20, 2001: CONNECTOR. MALFUNCTIONED. ON DESCENT WITH A/P SELECTED TO FIRST OFFICER AND ENGAGED, AIRCRAFT PITCHED OVER. NO AURAL WARNING, NO LIGHTS ON MAP. NOTED CAPTAIN'S RMI FLAGGED AT THE TIME OF
- [SDR SWIA200110119](https://openairdocs.org/sdr/SWIA200110119), Aug 20, 2001: SEAL. LEAKING. ON DEPARTURE FA REPORTED A LOUD SQUEAL COMING FROM FLOOR LEVEL EXIT AT ROW 9.REPAIRED EMERGENCY EXIT DOOR SEAL AS REQUIRED. PRESSURIZATION CHECK TO 4 PSI. ALL C
- [SDR SWIA200110108](https://openairdocs.org/sdr/SWIA200110108), Aug 17, 2001: COMPUTER. MALFUNCTIONED. UNCOMMANDED PITCH UP WITH AP ENGAGED, AP DISCONNECTED. PERFORMED QRH, RE-ENGAGED AP, AND EXPERIENCED UNCOMMANDED PTICH ROLL. AP DEFERRED ON FO SIDE. MEL 22-11-1
- [SDR SWIA200110025](https://openairdocs.org/sdr/SWIA200110025), Jun 8, 2001: FRAME. CRACKED. CARGO FLOOR, BEAM AND FRAME AND SECTION CRACKED AT STATION 16080.0 LEFT SIDE LOWER PER SRM 53-30-04. REMOVED DAMAGED AREA OF FRAME FABRICATED DOUBLER AND FILLER
- [SDR SWIA200110024](https://openairdocs.org/sdr/SWIA200110024), Jun 8, 2001: SUPPORT. CRACKED. LEFT FRAME 9 SUPPORT UNDER FORWARD DIRECT VISION WINDOW CRACKED. REPAIRED IAW EMB 120 SERVICE BULLETIN 120-53-0045 DATED AUG 6, 92. REWORK TO INNER REINFORCING 
- [SDR SWIA972610](https://openairdocs.org/sdr/SWIA972610), May 27, 2001: CONNECTOR. FAULTY. AFTER GEAR RETRACTION, LEFT MAIN GEAR SYSTEM-A RED LIGHT STILL ILLUMINATED. LOUD VIBRATION IN AIRCRAFT. TROUBLESHOOT SYSTEM. FOUND PUSHED BACK PIN ON A-UPLOCK C
- [SDR SWIA972512](https://openairdocs.org/sdr/SWIA972512), Apr 17, 2001: SWITCH. OUT OF ADJ. ON TAKEOFF ROLL, PRIOR TO V1 TRIPLE CHIME, DOORS AURAL WARNING SOUNDED. TAKEOFF WAS ABORTED. AIRCRAFT RETURNED TO GATE. (FORWARD DOOR LIGHT ILLUMINATED). DEFERR
- [SDR SWIA972487](https://openairdocs.org/sdr/SWIA972487), Apr 2, 2001: HARNESS. FAULTY. AFTER TAKEOFF, RIGHT MAIN GEAR SYSTEM-A RED LIGHT REMAINED ILLUMINATED. GEAR RETRACTED, BUT GEAR DOORS REMAINED OPEN. RECYCLED GEAR, BUT RIGHT MAIN GEAR SYSTEM-
- [SDR SWIA972473](https://openairdocs.org/sdr/SWIA972473), Mar 31, 2001: PROXIMITY SENSOR. FAILED. ON TAKEOFF, RIGHT MAIN GEAR RED ''A'' LIGHT REMAINED ON AND ALL GEAR CAME UP BUT ALL DOORS STAYED OPEN. NO CHANGE WHEN GEAR HANDLE WAS CYCLED. REMOVED AND REPLA
- [SDR SWIA972166](https://openairdocs.org/sdr/SWIA972166), Dec 12, 2000: LIGHT. INOPERATIVE. MOST FORWARD PORTION OF EMERGENCY LIGHTS INOP. REPLACED FORWARD ELBP IAW MM 33-50-02. OPS CHECK GOOD. PN ON D366-04-001 SN ON 1161 SN OFF 1277
- [SDR SWIA971863](https://openairdocs.org/sdr/SWIA971863), Jul 2, 2000: FLAP TRACK. ROUGH. FLAP DISAGREEMENT INVOLVING OUTBOARD FLAP PAIRS. QRH FOLLOWED WITH NO SUCCESS, RETURNED TO FIELD. FLAP EXTENDED NORMALLY ON APPROACH. RETRACTED NORMALLY ON GROU
- [SDR SWIA971347](https://openairdocs.org/sdr/SWIA971347), Dec 25, 1998: SWITCH. LOOSE. AFTER GEAR RETRACTION, LEFT LOOP A GREEN LIGHT REMAINED ILLUMINATED. ATTEMPTED TO CYCLE GEAR AND GEAR WOULD NOT EXTEND. USED QRH GEAR ELECTRICAL OVERRIDE PROCED
- [SDR SWIA971328](https://openairdocs.org/sdr/SWIA971328), Dec 2, 1998: CLAMP. LOOSE. LEFT FIRE DETECTION ENGINE/WHEEL WELL LIGHT CAME ON IN FLIGHT INTERMITTENTLY. STAYED ON FOR A MINUTE OR TWO, THEN INTERMITTENT AGAIN. VISUALLY INSPECTED LEFT WH
- [SDR SWIA971321](https://openairdocs.org/sdr/SWIA971321), Nov 25, 1998: LINE. FAILED. UPON FLAP RETRACTION AFTER TAKEOFF, LOST ALL GREEN SYSTEM HYDRAULICS. PERFORMED QRH PROCEDURES FOLLOWING LOSS OF GREEN SYSTEM HYDRAULICS. RETURNED TO GATE. REMO
- [SDR SWIA971291](https://openairdocs.org/sdr/SWIA971291), Oct 16, 1998: SELECTOR. FAILED. FLAP WOULD NOT EXTEND. MADE A FLAPS UP LANDING. REPLACED FLAP SELECTOR HANDLE, OPS CHECK GOOD.
- [SDR SWIA971217](https://openairdocs.org/sdr/SWIA971217), Jul 9, 1998: FCU. TRIPPED. CONTROL FAULT WARNING CAME ON IN FLIGHT. TRIED RESET, NOT SUCCESSFUL. RETURNED TO PDX. RERACKED FCU AND CONTROL FAULT WENT AWAY, OPS CHECKS NORMAL.
- [SDR SWIA971227](https://openairdocs.org/sdr/SWIA971227), Jul 7, 1998: CONTROL PANEL. TRIPPED. UPON FLAP RETRACTION WE GOT FLAP DISAGREEMENT AND THE OUTBOARD PAIR APPEARED MORE EXTENDED THAN THE REST ON THE FLAP PANEL. RETURNED TO SEA. RESET FLAP PANEL. F
- [SDR COMA9710492](https://openairdocs.org/sdr/COMA9710492), Dec 8, 1997: WIRE. LOOSE. FLOOR EMERGENCY LIGHT AT ROW 9 IS INOP. RECONNECTED LOOSE WIRE AT LIGHT.
- [SDR COMA9710334](https://openairdocs.org/sdr/COMA9710334), Jul 20, 1997: CIRCUIY BREAKERS. TRIPPED. THE FLIGHT IDLE STOP SOLENOID CIRCUIT BREAKERS WERE TRIPPED. RESET BREAKERS, SYSTEM TEST NORMAL.
- [SDR COMA9710303](https://openairdocs.org/sdr/COMA9710303), May 28, 1997: FUEL PRESS WARN. ACTIVATED. LOW FUEL PRESSURE WARNING CAME ON DURING TAKEOFF ROLL. DEFERRED THE RT ENGINE LOW FUEL PRESSURE WARNING.
- [SDR COMA9710190](https://openairdocs.org/sdr/COMA9710190), Mar 28, 1997: DOOR. NOT LATCHED. SERVICE DOOR WARNING CAME ON AFTER TAKEOFF. FOUND FUEL SERVICE DOOR UNLATCHED. SECURED LATCHES AND AIRCRAFT RETURNED TO SERVICE.
- [SDR COMA9710019](https://openairdocs.org/sdr/COMA9710019), Jan 5, 1997: FILTER. CLOGGED. LEFT ENGINE FUEL FILTER BYPASS INDICATION DURING TAKEOFF. REPLACED THE ENGINE HIGH PRESSURE FUEL FILTER.
- [SDR COMA9710018](https://openairdocs.org/sdr/COMA9710018), Jan 3, 1997: EEC. MALFUNCTIONED. RT ENGINE SURGING DURING TAKEOFF. TORQUE AND NP FLUCTUATING 10 TO 20 PERCENT. DEACTIVATED AND DEFERRED THE ENGINE ELECTRONIC CONTROL SYSTEM.
- [SDR COMA9610322](https://openairdocs.org/sdr/COMA9610322), Nov 2, 1996: RETRACT MECH. MALFUNCTIONED. LT MLG DID NOT EXTEND ON FIRST ATTEMPT. LANDING GEAR CYCLED 4 TIMES BEFORE A DOWNLOCK INDICATION WAS RECEIVED. COULD NOT DUPLICATE DISCREPANCY. LANDING GEAR WAS
- [SDR COMA9610321](https://openairdocs.org/sdr/COMA9610321), Nov 1, 1996: FUEL DOOR. NOT LATCHED. SERVICE DOOR WARNING ACTIVATED AFTER TAKEOFF. FOUND FUEL SERVICE DOOR UNLATCHED. SECURED DOOR CLOSED AND AIRCRAFT RETURNED TO SERVICE.
- [SDR COMA9610270](https://openairdocs.org/sdr/COMA9610270), Aug 31, 1996: ACTUATOR. MALFUNCTION. FLAP CONTROL FAULT WARNING DURING FLIGHT WITH FLAPS AT ZERO. REPLACED THE LT OUTBD FLAP ACTUATOR.
- [SDR COMA9660136](https://openairdocs.org/sdr/COMA9660136), Aug 21, 1996: SEAL. LOOSE. CABIN PRESSURIZATION, DUMPED AT 18,000 FEET. REPAIRED LOOSE CARGO DOOR SEAL.
- [SDR COMA9610236](https://openairdocs.org/sdr/COMA9610236), Jul 31, 1996: PACK. SMOKING. CABIN FILLED WITH SMOKE WITH RT COOLING PACK ON. COULD NOT DUPLICATE. OPERATIONAL CHECK OF COOLING SYSTEM NORMAL.
- [SDR COMA9610231](https://openairdocs.org/sdr/COMA9610231), Jul 25, 1996: PACK. SMOKING. RIGHT COOLING PACK FAIL WARNING - SMOKE IN CABIN. COULD NOT DUPLICATE DISCREPANCY. INSPECTION AND OPERATION OF SYSTEM NORMAL. NO DEFECTS FOUND.
- [SDR COMA9610220](https://openairdocs.org/sdr/COMA9610220), Jul 7, 1996: FUEL HEATER. LEAKING. STRONG FUEL SMELL IN AIRCRAFT DURING TAXI. REPLACED THE LEFT ENGINE FUEL/OIL HEAT EXCHANGER.
- [SDR COMA9610168](https://openairdocs.org/sdr/COMA9610168), Jun 5, 1996: CIRCUIT BREAKER. TRIPPED. RIGHT POWER LEVER FLIGHT IDLE STOP SOLENOID CIRCUIT BREAKER TRIPPED. RESET BREAKER - SYSTEM TEST NORMAL.
- [SDR COMA9610085](https://openairdocs.org/sdr/COMA9610085), Feb 16, 1996: OIL PRESS TRANS. DEFECTIVE. RT ENGINE OIL PRESSURE INDICATES 80 PSI AT CRUISE POWER SETTING. WHEN POWER WAS REDUCED, OIL PRESSURE DECREASED TO NORMAL. REPLACED THE OIL PRESSURE TRANSDUCER.
- [SDR COMA9610049](https://openairdocs.org/sdr/COMA9610049), Jan 31, 1996: SKIN. DELAMINATED. RIGHT INBOARD WING FLAP IS DELAMINATING ON THE TRAILING EDGE. REPAIRED FLAP. PART TOTAL CYCLES, 20,031.
- [SDR COMA9512043](https://openairdocs.org/sdr/COMA9512043), Dec 26, 1995: ACTUATOR. DEFECTIVE. FLAP DISAGREEMENT WARNING AFTER TAKEOFF. INBD FLAPS STUCK AT 15 DEGREES. REPLACED THE LT INBD FLAP ACTUATOR.
- [SDR COMA9511980](https://openairdocs.org/sdr/COMA9511980), Oct 3, 1995: FCU. DEFECTIVE. FLAP DISAGREEMENT WARNING SOUNDED WHEN FLAPS SELECTED TO 15 DEGREES. AIRCRAFT DIVERTED, DUE TO RUNWAY LENGTH. REPLACED THE FLAP CONTROL UNIT.
- [SDR COMA9511972](https://openairdocs.org/sdr/COMA9511972), Sep 21, 1995: ACTUATOR. DEFECTIVE. DURING LANDING, FLAP CONTROL FAULT WARNING. REPLACED THE NACELLE FLAP ACTUATOR.
- [SDR COMA9511970](https://openairdocs.org/sdr/COMA9511970), Sep 20, 1995: ACTUATOR. DEFECTIVE. FLAP CONTROL FAULT. REPLACED THE LEFT NACELLE FLAP ACTUATOR.
- [SDR COM11935](https://openairdocs.org/sdr/COM11935), Jul 25, 1995: SWIVEL. LEAKING. HYDRAULIC LEAK, LT MLG REPLACED LEAKING BRAKE SWIVEL FITTING.
- [SDR COM11933](https://openairdocs.org/sdr/COM11933), Jul 24, 1995: SERVO. DEFECTIVE. THERE IS NO STICK PUSHER WHEN TESTING STALL WARNING SYSTEM. REPLACED THE STICK PUSHER SERVO MOTORS.
- [SDR COM11860](https://openairdocs.org/sdr/COM11860), Apr 16, 1995: DOOR. NOT LATCHED. CARGO DOOR WARNING ACTIVATED DURING TAKEOFF. CLOSED AND LATCHED DOOR, PROBLEM DID NOT DUPLICATE. AIRCRAFT RETURNED TO SERVICE.
- [SDR COM11828](https://openairdocs.org/sdr/COM11828), Mar 20, 1995: ACTUATOR. DEFECTIVE. DISAGREEMENT WARNING WHEN ATTEMPTING TO RETRACT FLAPS DURING CLIMB. REPLACED RT OUTBD FLAP ACTUATOR.
- [SDR COM11794](https://openairdocs.org/sdr/COM11794), Feb 21, 1995: CIRCUIT BREAKER. TRIPPED. FLIGHT IDLE STOP SOLENOID CIRCUIT BREAKERS ARE TRIPPED. RESET CIRCUIT BREAKERS AND SYSTEM TEST NORMAL.
- [SDR COM11796](https://openairdocs.org/sdr/COM11796), Feb 17, 1995: SKIN. CORRODED. DURING MAINTENANCE SERVICE CHECK, RIVETS WERE FOUND TO HAVE BROKEN OR MISSING HEADS AT LOWER FUSELAGE CENTER LINE, FRAME 21 STA FS 6842.6. FURTHER INSPECTION RE
- [SDR COM11784](https://openairdocs.org/sdr/COM11784), Feb 15, 1995: SWIVEL. DEFECTIVE. LEFT BRAKE TEST FUNCTION IS INOP. REPLACED LT MLG BRAKE SWIVEL.

All 55: https://openairdocs.org/aircraft/N1117H/unmatched-reports.md

## STCs that may be installed (OpenAirDocs) (98, first 50)

Approved for this aircraft's airframe or engine model, in force first, then newest. The registry doesn't record which STCs an aircraft has; its records do.

### Approved for the airframe (Piper PA-15)

- [STC SA01233SE](https://openairdocs.org/stc/SA01233SE): Fabrication and installation of Alaskan Bushwheel LLC tail wheel and fork assembly. ABI, LLC
- [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 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 SA02738CH](https://openairdocs.org/stc/SA02738CH): Installation of L-3 Communications Avionics Systems. Acron Aviation Inc
- [STC SA7965SW](https://openairdocs.org/stc/SA7965SW): Application of fabric and polyurethane finishing system. Shady Aviation LLC
- [STC SA02386AK](https://openairdocs.org/stc/SA02386AK): Replacement of existing landing and/or taxi light reflector and bulbs with Light Emitting Diode (LED) lighting systems. AeroLED's Holding LLC
- [STC SA01757WI](https://openairdocs.org/stc/SA01757WI): To allow the use of UL91 or UL94 (minimum) grade aviation fuel. Swift Fuels LLC
- [STC SA03898NY](https://openairdocs.org/stc/SA03898NY): Installation and maintenance of ORATEX covering and coating material. Aircraft Design & Certification Ltd
- [STC SA02576AK](https://openairdocs.org/stc/SA02576AK): Installation of Cleveland and ABI, LLC Wheel and Brake Kits. ABI LLC
- [STC SA3-424](https://openairdocs.org/stc/SA3-424): Installation of Wiparie Skis Model CTF-2200 (Acft Skis) (FluiDyne) (Federal) tail ski on airplanes equipped with Scott Model 3000 tail wheel. F.Atlee Dodge Aircraft Services
- [STC SA01967WI](https://openairdocs.org/stc/SA01967WI): Use of GAMI G100UL High Octane Unleaded Avgas. General Aviation Modifications Inc
- [STC SA04776NY](https://openairdocs.org/stc/SA04776NY): The HIPEC Covering and Finishing System must be performed and maintained. HIPEC Aircraft Coatings Inc
- [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 SA01831WI](https://openairdocs.org/stc/SA01831WI): To allow the use of UL91 (minimum) grade aviation fuel. Petersen Aviation Inc
- [STC SA02268CH](https://openairdocs.org/stc/SA02268CH): Installation of Airwolf Filter Corp. Air Oil Separator. Airwolf Filter 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 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 SA00478CH](https://openairdocs.org/stc/SA00478CH): Installation of Cooper Superflite 102 Fabric. Aviation Products Systems Inc
- [STC SA4305WE](https://openairdocs.org/stc/SA4305WE): Installation of GAR-AERO wheel adapters and tundra type tires on the main landing gear. Seaplanes North LLC
- [STC SA02283SE PAGE 1](https://openairdocs.org/stc/SA02283SE%20PAGE%201): Installation of Electronics International Inc. Glass Panel Engine Monitor (with In Flight Data) CGR-30P. Electronics International Inc
- [STC SA02402SE PAGE 2](https://openairdocs.org/stc/SA02402SE%20PAGE%202): Installation of Electronics International Inc. Glass Panel Engine Monitor (with In-Flight Data) CGR-30C. Electronics International Inc
- [STC SA02428AK](https://openairdocs.org/stc/SA02428AK): Installation of a hydraulically actuated ski drag assembly. Northern Airframes LLC
- [STC SA02128LA](https://openairdocs.org/stc/SA02128LA): Installation of aileron and flap hinge repair bushings. Univair Aircraft Corporation
- [STC SA01765SE](https://openairdocs.org/stc/SA01765SE): Installation of Alaskan Bushwheel TSO-C26d wheels, Part Number (P/N) ABI-1010. ABI, LLC
- [STC SA01026SE](https://openairdocs.org/stc/SA01026SE): Improved fuel gascolator assembly. Steve's Aircraft
- [STC SA02825NY PAGE 1](https://openairdocs.org/stc/SA02825NY%20PAGE%201): Installation of Aerospace Logic Aircraft Instruments. Aerospace Logic Inc
- [STC SA02825NY PAGE 2](https://openairdocs.org/stc/SA02825NY%20PAGE%202): Installation of Aerospace Logic Aircraft Instruments. Aerospace Logic Inc
- [STC SA01251SE](https://openairdocs.org/stc/SA01251SE): The manufacture of a Sunvisor System. Rosen Sunvisor Systems LLC
- [STC SA460SW](https://openairdocs.org/stc/SA460SW): Install wing tips in accordance with Cub Crafters, Inc. Master Drawing List., MDL102400, Revision C, dated May 30, 2001, or later FAA approved revision. Cub Crafters Inc
- [STC SA69AL](https://openairdocs.org/stc/SA69AL): Fabrication and installation of Stoddard Aero Service Model 15 fuel tanks per Stoddard Aero Service Drawing List No. 447, dated February 7, 1975, or later Federal Aviation Administration approved revision. Stoddard Aero Service Airplane Flight Manual Supplement, dated June 10, 1963, is required for this installation. Cub Crafters Inc
- [STC SA00068SE](https://openairdocs.org/stc/SA00068SE): Installation of fuel flow/pressure instruments. (W/TSIO-360-MB1). Electronics International Inc
- [STC SA02110CH](https://openairdocs.org/stc/SA02110CH): Installation of a Time Trac Data Recorder. P2 Incorporated
- [STC SA2693NM](https://openairdocs.org/stc/SA2693NM): Installation of Electronics International digital volt/amp gauges and accessories. Electronics International Inc
- [STC SA02033AT](https://openairdocs.org/stc/SA02033AT): Modification to install an air-oil separator to prevent oil from being aspirated from the engine breather line. M-20 Oil Separators LLC
- [STC SA3518NM](https://openairdocs.org/stc/SA3518NM): Installation of a skylight, in accordance with Steve s Aircraft Drawing No. SP-3200, Sheet 1 through 6, dated June 23, 1986, or later FAA approved revision. Steve's Aircraft
- [STC SA4-977](https://openairdocs.org/stc/SA4-977): Installation of Fiberglass rudder post mount for either Grimes or Whelen WRM rotating beacons. Univair Aircraft Corporation
- [STC SA00680SE](https://openairdocs.org/stc/SA00680SE): Installation of Electronics International model UBG-16 or UBG-16T bar graph engine analyzer. Electronics International
- [STC SA10400SC](https://openairdocs.org/stc/SA10400SC): Installation of Teledyne Continental Motors C-85-8F engine, a Flottorp Manufacturing Co. 72A48 propeller, and an 18 gallon auxiliary fuel tank in the right wing. Smith Casey B
- [STC SA1-619](https://openairdocs.org/stc/SA1-619): Installation of Continental A-65-8F engine and McCauley 1A90CF-7147 propeller. Short Wing Piper Club Library
- [STC SA01293WI](https://openairdocs.org/stc/SA01293WI): Operation of airplane on unleaded automotive gasoline, 87 minimum antiknock index and leaded automotive gasoline, 88 minimum antiknock index (RON+MON)/ 2 per ASTM Specification D-439. Intermixing with aviation gasoline also approved. Data required: 1. Petersen Drawing No. 1521A dated November 15, 1989, or later FAA Approved revision. 2. Airplane Flight Manual Supplement dated November 22, 2004 or later FAA Approved revision. Petersen Aviation Inc

All 98: https://openairdocs.org/aircraft/N1117H/stcs.md

## Earlier aircraft with N1117H

The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N1117H before.

- [Cancelled 2008-05-19](https://openairdocs.org/deregistered/N1117H-2008-05-19): Cessna 172R, S/N 17281442, built 2007. Exported to China. Owner: [Aircraft Packaging And Shipping LLC](https://openairdocs.org/faa-owner/AIRCRAFT%20PACKAGING%20AND%20SHIPPING%20LLC), [Wichita, KS](https://openairdocs.org/faa-place/KS/Wichita)
- [Cancelled 1949-04-21](https://openairdocs.org/deregistered/N1117H-1949-04-21): Aeronca 15AC, S/N 15AC-133, built 1948. Owner: [Rocco Aviation Inc](https://openairdocs.org/faa-owner/ROCCO%20AVIATION%20INC), [Pueblo, CO](https://openairdocs.org/faa-place/CO/Pueblo)

## Related

- Other Piper PA-15 aircraft: https://openairdocs.org/model/piper-pa-15/aircraft.md
- The Lycoming 0-145A series engine: https://openairdocs.org/engine/lycoming-0-145a-series.md

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