# N12715: Robinson Helicopter R22

- Status: Valid registration
- Airframe: [Robinson Helicopter R22](https://openairdocs.org/model/robinson-helicopter-r22) (registry code 7640102, 2 seats)
- Data sheets: [TCDS H10WE](https://openairdocs.org/tcds/H10WE) (Robinson Helicopter Company) (OpenAirDocs)
- Serial number: 0103
- Type: Rotorcraft
- Engine type: Reciprocating
- Certificate issued: August 1, 2011
- Expires: August 31, 2027
- Mode S code: A0704C
- Registered owner: [Helicopteracademy.Com LLC](https://openairdocs.org/faa-owner/HELICOPTERACADEMY.COM%20LLC)
- Location: [Rehoboth Beach, DE](https://openairdocs.org/faa-place/DE/Rehoboth%20Beach)
- Owner type: LLC
- Owner's area on the map: 38.6945° N, 75.0997° W: Placed by OpenAirDocs at the center of ZIP code 19971, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=12715
- Page: https://openairdocs.org/aircraft/N12715

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.

## ADs that may apply (OpenAirDocs): 37 in force

### Matched by airframe (Robinson Helicopter R22)

- [AD 2024-04-02](https://openairdocs.org/ad/2024-04-02): Tail Rotor Blades · Robinson Helicopter R22, R22 ALPHA, R22 BETA and 4 more. Effective Apr 2, 2024
- [AD 2023-11-07](https://openairdocs.org/ad/2023-11-07): Ground Proximity System · Airbus Helicopters 47, 206, 210 and 237 more. Effective Jun 22, 2023
- [AD 2014-23-16](https://openairdocs.org/ad/2014-23-16): Main Rotor Blades · Robinson Helicopter R22, R22 ALPHA, R22 BETA and 3 more. Effective Jan 9, 2015
- [AD 2013-19-06](https://openairdocs.org/ad/2013-19-06): JASC Code: 2823: Fuel Selector/Shut-Off Valve · Robinson Helicopter R22, R22 ALPHA, R22 BETA and 1 more. Effective Nov 5, 2013
- [AD 2010-24-03](https://openairdocs.org/ad/2010-24-03): Tail rotor · Robinson Helicopter R22, R22 ALPHA, R22 BETA and 3 more. Effective Dec 29, 2010
- [AD 2006-12-07](https://openairdocs.org/ad/2006-12-07): ECi cylinder assemblies · Aerostar AEIO-320-D1B, AEIO-320-D2B, AEIO-320-E1A and 386 more. Effective Jul 11, 2006
- [AD 2005-16-05](https://openairdocs.org/ad/2005-16-05): Door assembly . · Modified door and window (Tech-Tool Plastics STC SR09189RC). Effective Aug 26, 2005
- [AD 2004-19-09](https://openairdocs.org/ad/2004-19-09): Main rotor blades (blades) · Robinson Helicopter R22, R22 ALPHA, R22 BETA and 1 more. Effective Oct 7, 2004
- [AD 2003-04-04](https://openairdocs.org/ad/2003-04-04): Pitch control bearing housing (housing) · Robinson Helicopter R22, R22 ALPHA, R22 BETA and 1 more. Effective Mar 26, 2003
- [AD 2000-20-51](https://openairdocs.org/ad/2000-20-51): Yoke Inspection · Robinson Helicopter R22, R22 ALPHA, R22 BETA and 1 more. Effective Nov 22, 2000
- [AD 2000-08-09](https://openairdocs.org/ad/2000-08-09): Sprag Clutches · Robinson Helicopter R22, R22 ALPHA, R22 BETA and 1 more. Effective May 5, 2000
- [AD 99-07-17](https://openairdocs.org/ad/99-07-17): Sprag Clutch · Robinson Helicopter R22, R22 ALPHA, R22 BETA and 1 more. Effective Apr 28, 1999
- [AD 99-02-02](https://openairdocs.org/ad/99-02-02): Flexplates · Robinson Helicopter R22, R22 ALPHA, R22 BETA and 1 more. Effective Feb 1, 1999
- [AD 98-21-09](https://openairdocs.org/ad/98-21-09): Fuel Tank Vent Tube(s) In Mast Fairing · Robinson Helicopter R22, R22 ALPHA, R22 BETA and 1 more. Effective Dec 9, 1998
- [AD 97-25-05](https://openairdocs.org/ad/97-25-05): Carburetor and Carburetor Air Temperature Gage · Robinson Helicopter R22, R22 ALPHA, R22 BETA and 1 more. Effective Jan 12, 1998
- [AD 97-02-14](https://openairdocs.org/ad/97-02-14): Main Rotor RPM Sensor Resetting · Robinson Helicopter R22, R22 ALPHA, R22 BETA and 1 more. Effective Mar 4, 1997
- [AD 96-09-29](https://openairdocs.org/ad/96-09-29): Replace V-Belt Sheave · Robinson Helicopter R22, R22 ALPHA, R22 BETA and 1 more. Effective Jun 7, 1996
- [AD 95-26-04](https://openairdocs.org/ad/95-26-04): Rotorcraft Flight Manual - Limitation Section · Robinson Helicopter R22, R22 ALPHA, R22 BETA and 1 more. Effective Jan 26, 1996
- [AD 95-23-05](https://openairdocs.org/ad/95-23-05): Tail Rotor Gearboxes · Robinson Helicopter R22, R22 ALPHA, R22 BETA and 1 more. Effective Dec 27, 1995
- [AD 95-11-09](https://openairdocs.org/ad/95-11-09): FAA FM - Limitations - Low-G Pushovers · Robinson Helicopter R22, R22 ALPHA, R22 BETA and 1 more. Effective Jul 14, 1995
- [AD 95-06-03](https://openairdocs.org/ad/95-06-03): Main Rotor Gearbox · Robinson Helicopter R22, R22 ALPHA, R22 BETA and 1 more. Effective Jun 29, 1995
- [AD 94-15-08](https://openairdocs.org/ad/94-15-08): Main Rotor Blade Inspection · Robinson Helicopter R22, R22 ALPHA, R22 BETA and 1 more. Effective Aug 9, 1994
- [AD 92-06-17](https://openairdocs.org/ad/92-06-17): NAS1304-16 AF Bolt Inspection · Robinson Helicopter R22, R22 ALPHA, R22 BETA and 1 more. Effective Jul 24, 1992
- [AD 90-17-01](https://openairdocs.org/ad/90-17-01): Carburetor Air Box Latches · Robinson Helicopter R22, R22 ALPHA, R22 BETA and 1 more. Effective Sep 10, 1990
- [AD 88-26-01 R2](https://openairdocs.org/ad/88-26-01-R2): Main Rotor Spindle · Robinson Helicopter R22, R22 ALPHA, R22 BETA and 1 more. Effective Aug 7, 1990
- [AD 87-18-03](https://openairdocs.org/ad/87-18-03): Main Rotor Pitch Link Assembly · Robinson Helicopter R22, R22 ALPHA, R22 BETA and 1 more. Effective Apr 25, 1988
- [AD 84-18-04](https://openairdocs.org/ad/84-18-04): Main Rotor Gearbox · Robinson Helicopter R22 and R22 ALPHA. Effective Nov 8, 1986
- [AD 83-15-07 R1](https://openairdocs.org/ad/83-15-07-R1): Main Rotor Blade Inspection · Robinson Helicopter R22. Effective Nov 21, 1983
- [AD 82-15-07](https://openairdocs.org/ad/82-15-07): Tail Rotor Drive Shaft · Robinson Helicopter R22. Effective Nov 21, 1983
- [AD 82-11-01](https://openairdocs.org/ad/82-11-01): Steel Tube Frame · Robinson Helicopter R22. Effective May 21, 1982
- [AD 82-03-07](https://openairdocs.org/ad/82-03-07): Main Rotor Blades · Robinson Helicopter R22. Effective Mar 4, 1982
- [AD 81-17-01](https://openairdocs.org/ad/81-17-01): Starting Vibrator Assemblies · Bendix Starting Vibrator Assemblies, B-2, B-2A and 49 more. Effective Aug 13, 1981
- [AD 81-05-52 R1](https://openairdocs.org/ad/81-05-52-R1): Main Gear Box · Robinson Helicopter R22. Effective Apr 13, 1981
- [AD 80-26-06](https://openairdocs.org/ad/80-26-06): Tail Rotor Plate · Robinson Helicopter R22. Effective Dec 29, 1980
- [AD 80-21-53](https://openairdocs.org/ad/80-21-53): Main Transmission Gears · Robinson Helicopter R22. Effective Dec 18, 1980
- [AD 80-24-01](https://openairdocs.org/ad/80-24-01): Tailcone · Robinson Helicopter R22. Effective Nov 24, 1980
- [AD 80-11-07](https://openairdocs.org/ad/80-11-07): Main Rotor Blades · Robinson Helicopter R22. Effective Jul 14, 1980

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

- [AD 2021-23-13](https://openairdocs.org/ad/2021-23-13) (historical): Ground Proximity System · Airbus Helicopters K-225, K-190A, K-240 and 237 more. Effective Dec 9, 2021
- [AD 2011-12-10](https://openairdocs.org/ad/2011-12-10) (historical): Main rotor blade · Robinson Helicopter R22, R22 ALPHA, R22 BETA and 3 more. Effective Jul 5, 2011
- [AD 2007-26-12](https://openairdocs.org/ad/2007-26-12) (historical): Blade skin debond · Robinson Helicopter R22, R22 ALPHA, R22 BETA and 3 more. Effective Jan 18, 2008
- [AD 2004-06-52](https://openairdocs.org/ad/2004-06-52) (historical): Main rotor blade (blade) · Robinson Helicopter R22, R22 ALPHA, R22 BETA and 1 more
- [AD 98-14-08](https://openairdocs.org/ad/98-14-08) (historical): Flexplate · Robinson Helicopter R22, R22 ALPHA, R22 BETA and 1 more
- [AD 96-11-08](https://openairdocs.org/ad/96-11-08) (historical): Main Rotor RPM Sensor Resetting · Robinson Helicopter R22, R22 ALPHA, R22 BETA and 1 more. Effective Jul 2, 1996
- [AD 95-06-07](https://openairdocs.org/ad/95-06-07) (historical): Flexplate · Robinson Helicopter R22, R22 ALPHA, R22 BETA and 1 more. Effective Apr 4, 1995
- [AD 95-04-14](https://openairdocs.org/ad/95-04-14) (historical): RFM - Limitation Section · Robinson Helicopter R22, R22 ALPHA, R22 BETA and 1 more. Effective Mar 17, 1995
- [AD 94-11-01](https://openairdocs.org/ad/94-11-01) (historical): Flexplate · Robinson Helicopter R22, R22 ALPHA, R22 BETA and 1 more

## Information bulletins (advisory) (11 in force)

- [SAIB 2023-01](https://openairdocs.org/saib/2023-01): MAIN ROTOR BLADES; Brinelled Main Rotor Blade Spindle Bearing. Issued Feb 14, 2023
- [SAIB AIR-22-08](https://openairdocs.org/saib/AIR-22-08): MAIN ROTOR DRIVE SYSTEM,TAIL ROTOR DRIVE SYSTEM. Issued Apr 11, 2022
- [SAIB AIR-22-03](https://openairdocs.org/saib/AIR-22-03): Robinson Helicopter Company Model R22, R44, and R66 Helicopters; Emergency Locator Transmitter Retention. Issued Mar 3, 2022
- [SAIB SW-12-45](https://openairdocs.org/saib/SW-12-45): Garmin Model 400W/500W Series GPS-WAAS Navigation System. Issued Oct 3, 2012
- [SAIB SW-11-15](https://openairdocs.org/saib/SW-11-15): Carbon Monoxide Detectors. Issued Jan 6, 2011
- [SAIB SW-09-07](https://openairdocs.org/saib/SW-09-07): JASC Code 2410 Alternator-Generator Drive, Robinson Helicopter Company Alternator Belts. Issued Jan 30, 2009
- [SAIB SW-07-16](https://openairdocs.org/saib/SW-07-16): Rotor blade skin debonding. Issued Feb 9, 2007
- [SAIB SW-06-55](https://openairdocs.org/saib/SW-06-55): . Issued Jul 13, 2006
- [SAIB SW-04-36](https://openairdocs.org/saib/SW-04-36): . Issued Dec 17, 2003
- [SAIB SW-01-07](https://openairdocs.org/saib/SW-01-07): . Issued Dec 19, 2000
- [SAIB ASW-95-01](https://openairdocs.org/saib/ASW-95-01): . Issued Jan 10, 1995

## NTSB investigations

None matched to N12715.

## FAA accident and incident reports

None matched to N12715.

## Reports on N12715 not matched to an aircraft (1)

They name N12715, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [Incident 19910630032439I](https://openairdocs.org/incident/19910630032439I), Jun 30, 1991: Emb EMB120RT (N12715), Rochester, NY. Left propeller problems on takeoff roll. Aborted. Returned to gate. Propeller control unit replaced.

## 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 N12715 not matched to an aircraft (84, newest 50)

They name N12715, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR C2XA02IA011](https://openairdocs.org/sdr/C2XA02IA011), Jan 12, 2002: CONTROL PANEL. FAULTY. IAH- DURING FLIGHT 4375, A TEST FLIGHT, THE CREW NOTED THAT THE FLAP ASYMMETRY LIGHT GLOWS THEN THE FLAPS FAIL. MAINTENANCE REMOVED AND REPLACED THE FLAP ANNUNC
- [SDR C2XA02IA010](https://openairdocs.org/sdr/C2XA02IA010), Jan 12, 2002: ACTUATOR. FAILED. IAH- DURING FLIGHT 4375, A TEST FLIGHT, THE CREW NOTED THAT THE FLAPS FAIL INFLIGHT, CONTROL FAULT WITH FLAPS AT ZERO DEGREES. MAINTENANCE REMOVED AND REPLACED 
- [SDR C2XA02IA009](https://openairdocs.org/sdr/C2XA02IA009), Jan 11, 2002: ROLLER. DAMAGED. IAH- FLIGHT 3664DURING TAKEOFF THE CREW NOTED A FLAP CONTROL FAULT,AND, ABORTED THE TAKEOFF. IAH-MAINTENANCE INSPECTEDTHE FLAPS,AND, FOUND THE BEARING ON THE RI
- [SDR C2XA01IA286](https://openairdocs.org/sdr/C2XA01IA286), Jul 1, 2001: VALVE. INOPERATIVE. IAH - FLIGHT 2963, THE CREW REPORTED SMOKE IN THE COCKPIT AFTER THE NUMBER ONE PACK WAS TURNED ON. MAINTENANCE REMOVED AND REPLACED THE NUMBER ONE PRESSURIZATIO
- [SDR C2XA01IA197](https://openairdocs.org/sdr/C2XA01IA197), Apr 5, 2001: LATCH. BROKEN. CLL - FLIGHT 3532, DURING PRE-FLIGHT INSPECTION, THE CREW REPORTED THAT THE LAFT MAIN LANDING GEAR OUTBOARD FORWARD DOOR WOULD NOT LATCH. MAINTENANCE REMOVED AN
- [SDR C2XA01IA087](https://openairdocs.org/sdr/C2XA01IA087), Feb 14, 2001: LIGHT. INOPERATIVE. IAH - FLIGHT 3408, DURING POST-FLIGHT INSPECTION, THE CREW REPORTED THAT THE FORWARD OVERHEAD EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED 
- [SDR C2XA01IA088](https://openairdocs.org/sdr/C2XA01IA088), Feb 10, 2001: CONNECTOR. LOOSE. IAH- DURING PRE-FLIGHT INSPECTION, THE CREW REPORTED THAT THE AISLE PATH EMERGENCY EXIT LIGHT AT SEAT 2A WAS FOUND TO BE INOPERATIVE. MAINTENANCE PLACED THE LIG
- [SDR C2XA01IA079](https://openairdocs.org/sdr/C2XA01IA079), Feb 10, 2001: BULB. INOPERATIVE. IAH - FLIGHT 3534, DURING PRE-FLIGHT INSPECTION, ONE AISLE PATH EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE PLACED THE LIGHT ON MEL, AND THE AIRCRA
- [SDR C2XA01IA099](https://openairdocs.org/sdr/C2XA01IA099), Jan 19, 2001: FLOORBEAM. CRACKED. MYR - DURING CONTINENTAL EXPRESS C-CHECK INSPECTION, THE RIGHT HAND FLOORBEAM WAS FOUND TO BE CRACKED AT FRAME 38. MAINTENANCE PERFORMED A DOUBLER REPAIR IN ACC
- [SDR C2XA01IA098](https://openairdocs.org/sdr/C2XA01IA098), Jan 12, 2001: BEAM. CORRODED. MYR - DURING CONTINENTAL EXPRESS C-CHECK INSPECTION, THE RIGHT HAND OMEGA BEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 38 AND 40. MAINTENANCE PERFORMED A SPLICE
- [SDR C2XA01IA097](https://openairdocs.org/sdr/C2XA01IA097), Jan 12, 2001: BEAM. CORRODED. MYR - DURING CONTINENTAL EXPRESS C-CHECK INSPECTION, THE LEFT HAND OMEGA BEAM WAS FOUND TO BE CORRODED FROM FRAME 38 TO FRAME 40. MAINTENANCE PERFORMED A SPLICE
- [SDR C2XA01IA095](https://openairdocs.org/sdr/C2XA01IA095), Jan 9, 2001: INTERCOSTAL. CORRODED. MYR - DURING CONTINENTAL EXPRESS C-CHECK, THE RIGHT HAND T-SECTION AT FRAME 40 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED T-SECTION
- [SDR C2XA01IA113](https://openairdocs.org/sdr/C2XA01IA113), Jan 9, 2001: STRAP. CORRODED. MYR - DURING CONTINENTAL EXPRESS C-CHECK INSPECTION, THE LEFT HAND BUTT STRAP WAS FOUND TO BE CORRODED AT STATION 13255. MAINTENANCE REMOVED AND REPLACED THE AF
- [SDR C2XA01IA111](https://openairdocs.org/sdr/C2XA01IA111), Jan 9, 2001: STRAP. CORRODED. MYR - DURING CONTINENTAL EXPRESS C-CHECK INSPECTION, THE CENTER BUTT STRAP WAS FOUND TO BE CORRODED FROM STATION 13255 TO STATION 15050. MAINTENANCE REMOVED AND
- [SDR C2XA01IA096](https://openairdocs.org/sdr/C2XA01IA096), Jan 9, 2001: STRAP. CORRODED. MYR - DURING CONTINENTAL EXPRESS C-CHECK INSPECTION, THE CENTER BUTT STRAP WAS FOUND TO BE CORRODED FROM STATION 11430 TO 13255. MAINTENANCE REMOVED AND REPLACE
- [SDR C2XA01IA1095](https://openairdocs.org/sdr/C2XA01IA1095), Jan 9, 2001: INTERCOSTAL. CORRODED. MYR - DURING CONTINENTAL EXPRESS C-CHECK, THE RIGHT HAND T-SECTION AT FRAME 40 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED T-SECTION
- [SDR C2XA01IA094](https://openairdocs.org/sdr/C2XA01IA094), Jan 9, 2001: BEAM. CORRODED. MYR - DURING CONTINENTAL EXPRESS C-CHECK, THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED BEYOND LIMITS BETWEEN FRAMES 37 AND 39. MAINTENANCE REMOVED AND REPLACE
- [SDR C2XA01IA110](https://openairdocs.org/sdr/C2XA01IA110), Jan 8, 2001: DUCT. CRACKED. MYR - DURING CONTINENTAL EXPRESS C-CHECK INSPECTION, RIGHT HAND EXHAUST DUCT WAS FOUND TO BE CRACKED ON THE OUTBOARD SIDE. MAINTENANCE PERFORMED A WELD REPAIR I
- [SDR C2XA01IA109](https://openairdocs.org/sdr/C2XA01IA109), Jan 8, 2001: CROSSBEAM. CORRODED. MYR - DURING CONTINENTAL EXPRESS C-CHECK INSPECTION, THE AFT CROSSBEAM AT STATION 13509.0 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTE
- [SDR C2XA01IA108](https://openairdocs.org/sdr/C2XA01IA108), Jan 8, 2001: CROSSBEAM. CORRODED. MYR - DURING CONTINENTAL EXPRESS C-CHECK INSPECTION, THE AFT CROSSBEAM AT STATION 12445.0 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTE
- [SDR C2XA01IA107](https://openairdocs.org/sdr/C2XA01IA107), Jan 8, 2001: STRAP. CORRODED. MYR - DURING CONTINENTAL EXPRESS C-CHECK INSPECTION, THE LEFT HAND AFT BUTT STRAP WAS FOUND TO BE CORRODED FROM STATION 12130.0 TO STATION 13255.0. MAINTENANCE 
- [SDR C2XA01IA106](https://openairdocs.org/sdr/C2XA01IA106), Jan 8, 2001: STRAP. CORRODED. MYR - DURING CONTINENTAL EXPRESS C-CHECK INSPECTION, THE RIGHT HAND AFT BUTT STRAP WAS FOUND TO BE CORRODED FROM STATION 12130.0 TO 13509.0. MAINTENANCE REMOVED
- [SDR C2XA01IA105](https://openairdocs.org/sdr/C2XA01IA105), Jan 8, 2001: STRAP. CORRODED. MYR - DURING CONTINENTAL EXPRESS C-CHECK INSPECTION, THE RIGHT HAND AFT BUTT STRAP WAS FOUND TO BE CORRODED FROM STATION 11715.0 TO STATION 13509.0. MAINTENANCE
- [SDR C2XA01IA104](https://openairdocs.org/sdr/C2XA01IA104), Jan 8, 2001: SEAT TRACK. CORRODED. MYR - DURING CONTINENTAL EXPRESS C-CHECK INSPECTION, THE LEFT HAND INBOARD SEAT TRACK WAS FOUND TO BE CORRODED FROM STATION 11715.0 TO 13509.0. MAINTENANCE REMO
- [SDR C2XA01IA103](https://openairdocs.org/sdr/C2XA01IA103), Jan 8, 2001: CROSSBEAM. CORRODED. MYR - DURING CONTINENTAL EXPRESS C-CHECK INSPECTION, THE CROSSBEAM AT STATION 5118.0 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED CRO
- [SDR C2XA01IA102](https://openairdocs.org/sdr/C2XA01IA102), Jan 8, 2001: RETAINER. CRACKED. MYR - DURING CONTINENTAL EXPRESS C-CHECK INSPECTION, THE RIGHT HAND NACELL FIRE SEAL RETAINER WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFE
- [SDR C2XA01IA101](https://openairdocs.org/sdr/C2XA01IA101), Jan 8, 2001: RETAINER. CRACKED. MYR - DURING CONTINENTAL EXPRESS C-CHECK INSPECTION THE LEFT HAND NACELLE FIRE SEAL RETAINER WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFEC
- [SDR C2XA01IA114](https://openairdocs.org/sdr/C2XA01IA114), Jan 7, 2001: STOP. WORN. MYR - DURING CONTINENTAL EXPRESS C-CHECK INSPECTION, THE CARGO DOOR LATERAL STOPS WERE FOUND TO BE WORN OUT OF LIMITS. MAINTENANCE REMOVED AND REPLACED THE AFFE
- [SDR C2XA01IA112](https://openairdocs.org/sdr/C2XA01IA112), Jan 7, 2001: STOP. WORN. MYR - DURING CONTINENTAL EXPRESS C-CHECK INSPECTION ,THE CARGO DOOR LATERAL STOPS WERE FOUND TO BE WORN OUT OF LIMITS. MAINTENANCE REMOVED AND REPLACED THE AFFE
- [SDR C2XA01IA100](https://openairdocs.org/sdr/C2XA01IA100), Jan 7, 2001: PAD. WORN. MYR - DURING CONTINENTAL EXPRESS C-CHECK INSPECTION, THE EMERGENCY EXIT CUTOUT CHAFE PADS ON THE FUSELAGE WERE FOUND TO BE WORN BEYOND LIMITS. MAINTENANCE REMOV
- [SDR C2XA00IA222](https://openairdocs.org/sdr/C2XA00IA222), Jul 25, 2000: SIGN. MISSING. IAH - DURING POST FLIGHT INSPECTION, THE CABIN EMERGENCY EXIT SIGN BY PASSENGER DOOR WAS FOUND TO BE MISSING. MAINTENANCE REPLACED THE MISSING SIGN, AND THE AIR
- [SDR C2XA00CL040](https://openairdocs.org/sdr/C2XA00CL040), May 24, 2000: CONNECTOR. CORRODED. CLE - FLT 3138 - AFTER TAKEOFF, THE CREW REPORTED SMOKE IN THE COCKPIT. THE AIRCRAFT RETURNED TO CLEVELAND WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REP
- [SDR C2XA00CL037](https://openairdocs.org/sdr/C2XA00CL037), May 7, 2000: FAN. ODOR. BUF - FLT 3206 - CREW REPORTED THAT COCKPIT AND CABIN FILLED WITH SMOKE WITH BOTH PACKS ON, APU ON, AND BOTH ENGINES OFF. MAINTENANCE INSPECTED APU, PACK COOLIN
- [SDR C2XA00CL036](https://openairdocs.org/sdr/C2XA00CL036), May 5, 2000: SMOKE. DETECTED. AXO - FLT 3032 - CREW REPORTED THE COCKPIT AND CABIN FILLED WITH SMOKE IN-FLIGHT. AIRCRAFT RETURNED TO AZO WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED THE B
- [SDR C2XA00CL032](https://openairdocs.org/sdr/C2XA00CL032), Apr 5, 2000: A/C PACK. MALFUNCTIONED. CLE - FLT 3285 - THE CREW REPORTED THE COCKPIT FILLED WITH SMOKE WHILE AT THE GATE. MAINTENANCE INSPECTED AND PLACED LEFT PACK ON MEL 21-50-02. THE AIRCRAFT WAS
- [SDR C2XA99CL067](https://openairdocs.org/sdr/C2XA99CL067), Aug 2, 1999: PACK. ODOR. CLE - FLT 3179 - THE CREW REPORTED A BURNING SMELL IN FLIGHT FROM THE LEFT PACK. THE AIRCRAFT LANDED IN CLEVELAND WITHOUT FURTHER INCIDENT. MAINTENANCE RELEASED
- [SDR C2XA99CL033](https://openairdocs.org/sdr/C2XA99CL033), Apr 17, 1999: RETRACT MECH. MALFUNCTIONED. CLE - FLT 3052 - CREW REPORTED THAT AFTER TAKEOFF THEY WERE UNABLE TO RETRACT THE LANDING, QRH ITEMS WERE PERFORMED BUT THE LANDING GEAR STILL FAILED TO RETRACT
- [SDR C2XA99IA153](https://openairdocs.org/sdr/C2XA99IA153), Feb 13, 1999: UNKNOWN. SMOKE. VCT - DURING FLT 3612, THE CREW REPORTED THE APPEARANCE AND SMELL OF SMOKE IN THE CABIN. THE AIRCRAFT RETURNED TO VCT WHERE IT LANDED WITHOUT INCIDENT. THE AIRC
- [SDR C2XA98CL061](https://openairdocs.org/sdr/C2XA98CL061), Aug 9, 1998: CONNECTOR. CORRODED. CLE - FLT 3344 - CREW REPORTED THAT UPON SELECTION OF GEAR UP, NO GEAR RETRACTION OCCURRED. THE CREW RECEIVED ALL RED AND ALL GREEN INDICATION LIGHTS WITH THE G
- [SDR C2XA97IA289](https://openairdocs.org/sdr/C2XA97IA289), Sep 18, 1997: FRAME. CRACKED. IAH - DURING C-CHECK INSPECTION, FOUND LEFT NACELLE INBOARD AFT LOWER HALF FRAME AT STATION 3346 TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE HALF FRAME 
- [SDR C2XA97IA288](https://openairdocs.org/sdr/C2XA97IA288), Sep 18, 1997: FRAME. CRACKED. IAH - DURING C-CHECK INSPECTION, FOUND RIGHT NACELLE INBOARD FORWARD LOWER HALF FRAME AT STATION 3346 TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE HALF F
- [SDR C2XA97IA287](https://openairdocs.org/sdr/C2XA97IA287), Sep 18, 1997: FRAME. CRACKED. IAH - DURING C-CHECK INSPECTION, FOUND LEFT NACELLE INBOARD FORWARD LOWER HALF FRAME AT STATION 3346 CRACKED. MAINTENANCE STOP DRILLED CRACK AND INSTALLED REPAI
- [SDR C2XA97IA286](https://openairdocs.org/sdr/C2XA97IA286), Sep 18, 1997: FRAME. CRACKED. IAH - DURING C-CHECK INSPECTION, FOUND RIGHT NACELLE INBOARD AFT LOWER HALF FRAME AT STATION 3346.0 TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE HALF FRA
- [SDR C2XA97IA285](https://openairdocs.org/sdr/C2XA97IA285), Sep 18, 1997: BRACKET. CRACKED. IAH - DURING C-CHECK INSPECTION, FOUND SKIN SUPPORT BRACKET CRACKED AT FRAME NR 46 AND STRINGER 16 RIGHT. MAINTENANCE REMOVED AND REPLACED THE BRACKET IAW EMB12
- [SDR C2XA97IA284](https://openairdocs.org/sdr/C2XA97IA284), Sep 18, 1997: SUPPORT. CRACKED. IAH - DURING C-CHECK INSPECTION, FOUND RIGHT VERTICAL FLOOR SUPPORT AT FRAME NR 13 CRACKED. MAINTENANCE STOP DRILLED CRACK AND INSTALLED REPAIR DOUBLER IAW EMB1
- [SDR C2XA97IA283](https://openairdocs.org/sdr/C2XA97IA283), Sep 18, 1997: SUPPORT. CRACKED. IAH - DURING C-CHECK INSPECTION, FOUND LEFT VERTICAL FLOOR SUPPORT AT FRAME NR 13 CRACKED. MAINTENANCE STOP DRILLED CRACK AND INSTALLED REPAIR DOUBLER IAW EMB12
- [SDR C2XA97IA282](https://openairdocs.org/sdr/C2XA97IA282), Sep 18, 1997: STRINGER. CORRODED. IAH - DURING C-CHECK INSPECTION, FOUND LEFT STRINGER 21 CORRODED FROM FRAME NR 41 TO 42. MAINTENANCE REMOVED AND REPLACED THE STRINGER SECTION IAW EMB120 SRM 53
- [SDR C2XA97IA281](https://openairdocs.org/sdr/C2XA97IA281), Sep 18, 1997: OMEGA BEAM. CORROSION. IAH - DURING C-CHECK INSPECTION, FOUND FLOOR SUPPORT OMEGA BEAM ON LEFT SIDE BETWEEN FRAMES NR 38 AND 39 CORRODED. MAINTENANCE REMOVED CORROSION AND INSTALLED R
- [SDR C2XA97IA280](https://openairdocs.org/sdr/C2XA97IA280), Sep 18, 1997: SEAT TRACK. CORRODED. IAH - DURING C-CHECK INSPECTION, FOUND LEFT AFT FLOOR SEAT TRACK TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK IAW EMB120 MM 53-01-05. THE AIR
- [SDR C2XA97IA279](https://openairdocs.org/sdr/C2XA97IA279), Sep 18, 1997: STRINGER. CORRODED. IAH - DURING C-CHECK INSPECTION, FOUND LEFT STRINGER 21 BETWEEN FRAMES NR 41 TO 42 CORRODED. MAINTENANCE REMOVED AND REPLACED THE CORRODED SECTION OF STRINGER 2

All 84: https://openairdocs.org/aircraft/N12715/unmatched-reports.md

## STCs that may be installed (OpenAirDocs) (73, 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 (Robinson Helicopter R22)

- [STC SR12177IB](https://openairdocs.org/stc/SR12177IB): Installation of Floor Protector. Delastek Inc
- [STC SR01980WI](https://openairdocs.org/stc/SR01980WI): Installation of Garmin GI 275 Multi-Function Instrument. Garmin International Inc
- [STC SH760NE](https://openairdocs.org/stc/SH760NE): Operation of rotorcraft on unleaded and leaded automotive gasoline, 91 minimum anti-knock index(RON + MON)/2. Intermixing with aviation gasoline is also approved. Petersen Aviation Inc
- [STC SA11137SC](https://openairdocs.org/stc/SA11137SC): Installation of Plane-Power ALT-FLX alternator. Hartzell Engine Technologies, LLC
- [STC SR03512AT](https://openairdocs.org/stc/SR03512AT): Installation of HID Landing and Taxi Lights. Whelen Aerospace Technologies
- [STC SR00557SE](https://openairdocs.org/stc/SR00557SE): Fabrication of Onboard Systems Model 200-225-00 (without load weight) or 200-226-00 (with load weight) cargo hook suspension system. Onboard Systems International
- [STC SR00920SE](https://openairdocs.org/stc/SR00920SE): Fabrication of Onboard Systems Model 200-262-00 cargo hook suspension system. Onboard Systems International
- [STC SR00102AT](https://openairdocs.org/stc/SR00102AT): Installation of Skysign Model H-47C electronic billboard. Sky Sign Inc
- [STC SR02704SE](https://openairdocs.org/stc/SR02704SE): Installation and maintenance of the Sunspot 36 and 46 series lights. AeroLED's Holdings LLC
- [STC SR02124SE](https://openairdocs.org/stc/SR02124SE): Installation functionality. of Data Garmin Required: transponders: (1) Garmin GTX Master 345/345R Drawing with List ADS-B (MDL), Out and In 005-00734-A4, functionality;. Garmin International Inc
- [STC SR00359BO](https://openairdocs.org/stc/SR00359BO): Installation of Parmetheus Plus LED PAR36 and PAR46 taxi and landing lights. Whelen Aerospace Technologies
- [STC SR00821DE](https://openairdocs.org/stc/SR00821DE): Installation of Automatic Dependent Surveillance - Broadcast (ADS-B) Out and in functionality using the BendixKing KT74 Transponder and qualified position sensor and ADS-B In Receiver. Peregrine
- [STC SR00387BO](https://openairdocs.org/stc/SR00387BO): Installation of Avidyne 700-00182-XXX IFD5XX and 700-00179-XXX IFD4XX Series Integrated Flight Displays (IFD). Avidyne Corporation
- [STC SH1052NE](https://openairdocs.org/stc/SH1052NE): Installation of Airwolf Model AFC-500 full flow engine oil filter P/N AFC-500. Airwolf Filter Corporation
- [STC SR02506SE](https://openairdocs.org/stc/SR02506SE): Installation of the Collective Pull Down System, installed and maintained. HeliTrak Inc
- [STC SA2586NM](https://openairdocs.org/stc/SA2586NM): Installation of J.P. Instruments temperature monitoring systems. J P Instruments
- [STC SR02487AK](https://openairdocs.org/stc/SR02487AK): Installation of L-3 Communications Avionics Systems ESI-500 Standby Instrument System. ADS-B Technologies, LLC
- [STC SR00840DE](https://openairdocs.org/stc/SR00840DE): Installation of the Rosen Sunvisor System into the Robinson R22. R44 and R66. Rosen Sunvisor Systems LLC
- [STC SR02470AK](https://openairdocs.org/stc/SR02470AK): Installation of the L-3 Communications NGT -1000/2000/2500 ADS-B System. ADS-B Technologies, LLC
- [STC SR02471AK](https://openairdocs.org/stc/SR02471AK): Installation of the L-3 Communications NGT -9000/9000R ADS-B System. ADS-B Technologies, LLC
- [STC SR00197SE](https://openairdocs.org/stc/SR00197SE): Addition of strug leg fairings to landing gear. Cascade STC LLC
- [STC SR02394AK](https://openairdocs.org/stc/SR02394AK): Replacement of existing landing and/or hover light bulbs with Light Emitting Diode (LED) lighting system. Seaplanes North LLC
- [STC SA01669CH](https://openairdocs.org/stc/SA01669CH): Installation of Challenger Reusable Air Filter. Challenger Aviation Products Inc
- [STC SA00432SE](https://openairdocs.org/stc/SA00432SE): Installation of EGT 701 series fuel flow instrument. J P Instruments
- [STC SA00861SE](https://openairdocs.org/stc/SA00861SE): Installation of J.P. Instruments (JPI) fuel flow indicating system. J P Instruments
- [STC SA01026SE](https://openairdocs.org/stc/SA01026SE): Improved fuel gascolator assembly. Steve's Aircraft
- [STC SH5863NM](https://openairdocs.org/stc/SH5863NM): Installation of skid shoe assembly kit. Bell Helicopter Textron Inc
- [STC SR02232LA](https://openairdocs.org/stc/SR02232LA): Installation of Garmin Model 400W / 500W Series GPS-WAAS Navigation System. Garmin AT Inc
- [STC SR03863AT](https://openairdocs.org/stc/SR03863AT): Installation of Power Flow Systems, Inc. (PFS) tuned exhaust system. Power Flow Systems Inc
- [STC SA2693NM](https://openairdocs.org/stc/SA2693NM): Installation of Electronics International digital volt/amp gauges and accessories. Electronics International Inc
- [STC SR00038BO](https://openairdocs.org/stc/SR00038BO): Installation of Helipod cargo containers. Simplex Manufacturing Company
- [STC SA4172NM](https://openairdocs.org/stc/SA4172NM): Installation of Aviation Development oil filter. Aviation Development Corporation
- [STC SA593CH](https://openairdocs.org/stc/SA593CH): Install Champion SlickSTART magneto booster system. Champion Aerospace LLC
- [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 SR01821SE](https://openairdocs.org/stc/SR01821SE): Installation of High Intensity Discharge (HID) aviation lighting system manufactured. Precise Flight Inc
- [STC SR02491CH](https://openairdocs.org/stc/SR02491CH): Installation of Airwolf Aerospace, LLC Protective Rotor Blade Tape. Airwolf Aerospace LLC
- [STC ST00049BO](https://openairdocs.org/stc/ST00049BO): Installation of a Pratt & Whitney Engine Services, Inc. Health Usage Monitoring System (HUMS) Model 1022, P/N HUMS-A-030-1. Pratt & Whitney Engine Services Inc
- [STC SA00402SE](https://openairdocs.org/stc/SA00402SE): Installation of a remote spin-on oil filter adapter. (GC-1B w/Lycoming or Cont 360 engine installed). Aviation Development 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 SR01430LA](https://openairdocs.org/stc/SR01430LA): Installation of Stainless Steel Skid shoes. Papas Gary Los Angeles Laboratories Inc
- [STC SH2011CE](https://openairdocs.org/stc/SH2011CE): Operation of rotorcraft on unleaded automotive gasoline, 87 minimum antiknock index and leaded automotive gasoline, 88 minimum antiknock index (RON + MON)/2. Intermixing with aviation gasoline also approved. Fuller Howard J Jr
- [STC SH407NE](https://openairdocs.org/stc/SH407NE): Installation of Robinson R-22 Beta model muffler P/N A169-6L. Fuller Howard J Jr
- [STC SR18BO](https://openairdocs.org/stc/SR18BO): Installation of a low rotor RPM voice warning system. Fuller Howard J Jr
- [STC SR01362SE](https://openairdocs.org/stc/SR01362SE): Installation of the support assembly for the ground handling wheel on the skid tube of the above model rotorcraft. Micro AeroDynamics Inc
- [STC SA00701SE](https://openairdocs.org/stc/SA00701SE): Installation of Precise Flight Pulselite System. Precise Flight Inc
- [STC SH3298NM](https://openairdocs.org/stc/SH3298NM): Installation of Classic Aircraft Products CH-400 Cargo Hook System. Test Instrumentation Inc
- [STC SR01624AT](https://openairdocs.org/stc/SR01624AT): Permit replacing of existing 25 amp battery in original factory battery box with Concord Battery Corp, Model RG25XC. Concorde Battery Corporation
- [STC SH288NE](https://openairdocs.org/stc/SH288NE): Installation of Model 2201 bubble doors. Fuller Howard J Jr
- [STC SA02520AT](https://openairdocs.org/stc/SA02520AT): Installation of M-20 Oil Separator, model 600-WP. M-20 Oil Separators LLC
- [STC SA2687NM](https://openairdocs.org/stc/SA2687NM): Installation of Truboplus/ Electronics Int'l gauges and switches. Aero Manufacturing Inc

All 73: https://openairdocs.org/aircraft/N12715/stcs.md

## Earlier aircraft with N12715

The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N12715 before.

- [Cancelled 1973-10-24](https://openairdocs.org/deregistered/N12715-1973-10-24): Cessna 172M, S/N 17262200. Exported to Canada
- [Cancelled 1934-05-16](https://openairdocs.org/deregistered/N12715-1934-05-16): Karlberg Jack KARLBERG GLIDER, S/N 100, built 1932. Owner: [Karlberg Jack](https://openairdocs.org/faa-owner/KARLBERG%20JACK), [Seattle, WA](https://openairdocs.org/faa-place/WA/Seattle)
- [Cancelled (date not recorded)](https://openairdocs.org/deregistered/N12715-undated): Cessna S550, S/N S5500062

## Related

- Other Robinson Helicopter R22 aircraft: https://openairdocs.org/model/robinson-helicopter-r22/aircraft.md

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