# North American NA-265-60

- Type: Aircraft model (FAA registry)
- Registry code: 6402612
- Manufacturer (registry): NORTH AMERICAN
- Model: NA-265-60
- Aircraft type: Fixed wing multi engine
- Category: Airplane
- Engines: 2 · Turbo-jet
- Seats: 12
- Weight class: 20,000 lb and over
- Cruise speed: 376 mph
- Certification: Type certificated
- Data sheet: [TCDS A2WE](https://openairdocs.org/tcds/A2WE) (OpenAirDocs)
- Holder: Sabreliner Aviation LLC
- Registered aircraft: 3
- Page: https://openairdocs.org/model/north-american-na-265-60

Model codes come from the FAA registry's reference file. ADs are matched to them by model name and maker.

## ADs that may apply (OpenAirDocs)

Matched to this model by model name and maker. Each AD's applicability may narrow it by serial number, part number or equipment.

- [AD 2006-16-18 R1](https://openairdocs.org/ad/2006-16-18-R1): Installing a warning placard on the TAWS/RMI · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 100 more. Effective Jul 18, 2008
- [AD 2005-25-18](https://openairdocs.org/ad/2005-25-18): Wing center section · Sabreliner NA-265, NA-265-20, NA-265-30 and 5 more. Effective Jan 18, 2006
- [AD 2002-15-02](https://openairdocs.org/ad/2002-15-02): Compressor Wheels · British Aerospace Regional Jetstream Series 3101, 234, Mystere-Falcon 20 - C5 and 22 more. Effective Aug 28, 2002
- [AD 2001-22-14](https://openairdocs.org/ad/2001-22-14): Fire Extinguishing System Bottle Cartridges · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 105 more. Effective Dec 10, 2001
- [AD 99-19-03](https://openairdocs.org/ad/99-19-03): AFM - Limitations Section - Ice Protection System · Sabreliner NA-265-40, NA-265-60, NA-265-70 and 1 more. Effective Dec 27, 1999
- [AD 97-05-03 R1](https://openairdocs.org/ad/97-05-03-R1): Global Positioning Systems · BAE Systems Avro 146-RJ100A, BAe 146-200A, Jetstream Model 4101 and 27 more. Effective Apr 20, 1999
- [AD 98-04-37](https://openairdocs.org/ad/98-04-37): AFM - Limitations Section - Icing · Sabreliner NA-265-40, NA-265-60, NA-265-70 and 1 more. Effective Mar 25, 1998
- [AD 97-04-15](https://openairdocs.org/ad/97-04-15): Fire Extinguisher Bottle Cartridges · Bombardier DHC-8-101, DHC-8-102, DHC-8-103 and 24 more. Effective Mar 7, 1997
- [AD 96-25-12](https://openairdocs.org/ad/96-25-12): Auxiliary Power Units · BAE Systems HS 748 Series 2A, HS 748 Series 2B, 707-100 Long Body and 74 more. Effective Jan 13, 1997
- [AD 94-01-06](https://openairdocs.org/ad/94-01-06): Traffic Alert and Collision Avoidance System II Processors · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 176 more. Effective Feb 4, 1994
- [AD 94-01-05](https://openairdocs.org/ad/94-01-05): Traffic Alert and Collision Avoidance System II Processors · Airbus A340-211, A340-212, A340-213 and 85 more. Effective Feb 4, 1994
- [AD 92-27-16](https://openairdocs.org/ad/92-27-16): Hydraulic Pump · Sabreliner NA-265, NA-265-20, NA-265-30 and 5 more. Effective Jan 13, 1993
- [AD 82-26-02](https://openairdocs.org/ad/82-26-02): Vertical Floor Panel Inspection · Sabreliner NA-265-60 and NA-265-65. Effective Apr 13, 1983
- [AD 80-04-11 R2](https://openairdocs.org/ad/80-04-11-R2): Wing Leading Edge · Sabreliner NA-265-60 and NA-265-80 with STC SA687NW or SA847NW. Effective Apr 13, 1983
- [AD 82-10-02 R1](https://openairdocs.org/ad/82-10-02-R1): Flap Screwjack Inspection · Sabreliner NA-265-60 and NA-265-65 with STC SA687NW. Effective Sep 13, 1982
- [AD 81-15-51 R1](https://openairdocs.org/ad/81-15-51-R1): Flap Actuation System · Sabreliner NA-265-60 and NA-265-80 with STC SA687NW or SA847NW. Effective May 18, 1982
- [AD 81-13-04](https://openairdocs.org/ad/81-13-04): MLG Shock Strut Trunnion · Sabreliner NA-265-60, NA-265-70 and NA-265-80. Effective Jul 30, 1981
- [AD 81-14-09](https://openairdocs.org/ad/81-14-09): Cabin Depressurization · Sabreliner NA-265-40 and NA-265-60. Effective Jul 13, 1981
- [AD 80-26-01](https://openairdocs.org/ad/80-26-01): Fuselage Structure Inspection · Sabreliner NA-265-40 and NA-265-60. Effective Jan 19, 1981
- [AD 80-22-54](https://openairdocs.org/ad/80-22-54): Aileron Control System · Sabreliner NA-265-60 and NA-265-80 with STC SA687NW or SA847NW. Effective Dec 24, 1980
- [AD 80-01-07 R1](https://openairdocs.org/ad/80-01-07-R1): Raisbeck Modification · Sabreliner NA-265-60 and NA-265-80 with STC SA687NW or SA847NW. Effective Jun 3, 1980
- [AD 80-08-07](https://openairdocs.org/ad/80-08-07): Elevator Trailing Edge · Sabreliner NA-265-40, NA-265-60 and NA-265-70. Effective Apr 21, 1980
- [AD 80-05-02](https://openairdocs.org/ad/80-05-02): Safety Belt Assemblies · Gulfstream Aerospace G-1159, G-1159A, G-1159B and 17 more. Effective Feb 27, 1980
- [AD 79-13-02](https://openairdocs.org/ad/79-13-02): Aileron System · Sabreliner NA-265-60 with STC SA687NW. Effective Sep 4, 1979
- [AD 79-17-01](https://openairdocs.org/ad/79-17-01): Elevators · Sabreliner NA-265-60 with STC SA687NW. Effective Aug 15, 1979
- [AD 75-08-11](https://openairdocs.org/ad/75-08-11): Electrical Power in Flight · Sabreliner NA-265, NA-265-20, NA-265-30 and 3 more. Effective Aug 5, 1976
- [AD 73-12-09](https://openairdocs.org/ad/73-12-09): Thrust Reverser Deployment · Sabreliner NA-265-40, NA-265-60 and NA-265-70. Effective Jul 29, 1975
- [AD 75-12-04](https://openairdocs.org/ad/75-12-04): Engine Supports · Sabreliner NA-265-40 and NA-265-60. Effective Jun 9, 1975
- [AD 75-04-05](https://openairdocs.org/ad/75-04-05): Engine Fuel Pressure Switches · Sabreliner NA-265, NA-265-20, NA-265-30 and 5 more. Effective Feb 18, 1975
- [AD 75-01-03](https://openairdocs.org/ad/75-01-03): Landing Gear Warning System · Sabreliner NA-265, NA-265-20, NA-265-30 and 4 more. Effective Jan 6, 1975
- [AD 74-26-08](https://openairdocs.org/ad/74-26-08): Engine Oil Low Pressure Switch · Sabreliner NA-265-40, NA-265-60 and NA-265-70. Effective Dec 24, 1974
- [AD 72-23-04](https://openairdocs.org/ad/72-23-04): Main Gear Strut Cylinder · Sabreliner NA-265-40 and NA-265-60. Effective Nov 11, 1972
- [AD 72-19-03](https://openairdocs.org/ad/72-19-03): Landing Gear Side Brace · Sabreliner NA-265, NA-265-20, NA-265-30 and 2 more. Effective Sep 15, 1972
- [AD 72-14-04](https://openairdocs.org/ad/72-14-04): Main Gear Door Torque Tube · Sabreliner NA-265, NA-265-20, NA-265-30 and 2 more. Effective Jul 7, 1972
- [AD 71-25-04](https://openairdocs.org/ad/71-25-04): Aileron Control Cables · Sabreliner NA-265, NA-265-20, NA-265-30 and 3 more. Effective Dec 4, 1971
- [AD 71-03-03](https://openairdocs.org/ad/71-03-03): Flap Track Attachment Lug · Sabreliner NA-265, NA-265-20, NA-265-30 and 2 more. Effective Feb 6, 1971
- [AD 70-24-03](https://openairdocs.org/ad/70-24-03): Engine Fire Control Handle · Sabreliner NA-265, NA-265-20, NA-265-30 and 5 more. Effective Nov 28, 1970
- [AD 70-12-06](https://openairdocs.org/ad/70-12-06): Nose Gear Shimmy · Sabreliner NA-265, NA-265-20, NA-265-30 and 2 more. Effective Jun 16, 1970
- [AD 70-02-09](https://openairdocs.org/ad/70-02-09): Engine Thrust Reverser · Sabreliner NA-265-40 and NA-265-60. Effective Dec 19, 1969
- [AD 69-10-01](https://openairdocs.org/ad/69-10-01): Main Landing Gear Pistons · Sabreliner NA-265, NA-265-20, NA-265-30 and 5 more. Effective May 9, 1969
- [AD 68-20-01](https://openairdocs.org/ad/68-20-01): Horizontal Stabilizer Support · Sabreliner NA-265, NA-265-20, NA-265-30 and 2 more. Effective Oct 28, 1968

Historical (superseded or no longer in force):

- [AD 73-18-03](https://openairdocs.org/ad/73-18-03) (historical): Front and Rear Wing Spars · Sabreliner NA-265-40, NA-265-60 and NA-265-70. Effective May 5, 1978

## Registered aircraft (3)

- [N11LX](https://openairdocs.org/aircraft/N11LX): [N492a LLC](https://openairdocs.org/faa-owner/N492A%20LLC), [Goodyear, AZ](https://openairdocs.org/faa-place/AZ/Goodyear), built 1974, S/N 306-75
- [N33JW](https://openairdocs.org/aircraft/N33JW): [Bj Aviation LLC](https://openairdocs.org/faa-owner/BJ%20AVIATION%20LLC), [Beaver Meadows, PA](https://openairdocs.org/faa-place/PA/Beaver%20Meadows), built 1974, S/N 306-92
- [N378D](https://openairdocs.org/aircraft/N378D): [National Test Pilot School](https://openairdocs.org/faa-owner/NATIONAL%20TEST%20PILOT%20SCHOOL), [Mojave, CA](https://openairdocs.org/faa-place/CA/Mojave), built 1975, S/N 306-101

## NTSB investigations (2)

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [NTSB LAX93FA033](https://openairdocs.org/ntsb/LAX93FA033), Nov 8, 1992: Sabreliner N-265-60 (N169RF), Phoenix, AZ, destroyed. Probable cause: THE DELAY OF THE PIC TO APPLY NORMAL BRAKING AND HIS FAILURE TO EXECUTE THE APPROPRIATE EMERGENCY PROCEDURES. CONTRIBUTING TO THIS ACCIDENT WAS AN UNDETERMINED ANTISKID MALFUNCTION; THE COPILOT'S…
- [NTSB DEN73AD047](https://openairdocs.org/ntsb/DEN73AD047), Apr 13, 1973: N.American NA-265 (N743R), Montrose, CO, destroyed, 2 fatal

## FAA accident and incident reports (17)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Incident 20110409005899I](https://openairdocs.org/incident/20110409005899I), Apr 9, 2011: North American NA-265-60 (N71CC), Ft. Lauderdale, FL, Minor damage. Aircraft repositioning from kfxe to kpbi for passenger pick-up. On approach to kpbi gear left gear light did not illuminate on landing gear actuation. Captain…
- [Incident 20070928023269I](https://openairdocs.org/incident/20070928023269I), Sep 28, 2007: Rkwell NA26560 (N59K), Cedar Rapids, IA, No damage. (-23) Due to loss of cabin pressurization, the pilot initiated an emergency descent resulting in a loss of standard separation from an aircraft traveling in…
- [Incident 20000201002909I](https://openairdocs.org/incident/20000201002909I), Feb 1, 2000: Rkwell NA26560 (N642RP), Long Beach, CA. Submitted a malfunction and defect report about the parking brake valve, p/n HP681100-5, s/n 1485 and the accumulator, p/n 1356-583328, s/n 63471. It was…
- [Incident 19960820028789I](https://openairdocs.org/incident/19960820028789I), Aug 20, 1996: Rkwell NA26560 (N1JX), Monroe, NC, Minor damage. Narrative: aircraft N1JX, a north American sabreliner, made a normal approach and landing at the Monroe Airport, north carolina. During the landing roll the…
- [Incident 19941020039159I](https://openairdocs.org/incident/19941020039159I), Oct 20, 1994: Rkwell NA26560 (N15HF), Dyersburg, TN, Minor damage. Ground looped into mud trying tturn off on taxiwaty. Wet runway. Thrust reversers not deployed. Landed long and fas
- [Accident 19921107049419A](https://openairdocs.org/incident/19921107049419A), Nov 7, 1992: Rkwell NA26560 (N169RF), Phoenix, AZ, Destroyed. Reported throttle jammed open and no brakes. Overran runway. Collided with objects. Cause of problem not determined
- [Incident 19920421018079I](https://openairdocs.org/incident/19920421018079I), Apr 21, 1992: Rkwell NA26560 (N90EC), Washington, DC, Minor damage. Hydraulic pump off. Hydraulic pressure depleted by brake check. Lost steering and hit parked aircraft while taxiing
- [Incident 19901204063889I](https://openairdocs.org/incident/19901204063889I), Dec 4, 1990: Rkwell NA26560 (N401MS), Ft Lauderdale, FL, Minor damage. Lost directional control of aircraft while taxiing for takeoff. Veered off taxiway. Left main sank in dirt.
- [Incident 19900207049079I](https://openairdocs.org/incident/19900207049079I), Feb 7, 1990: Rkwell NA26560 (N90EC), Fort Wayne, IN, Minor damage. Left engine fire after landing. Inspection found no mechanical problem.
- [Incident 19900120003919I](https://openairdocs.org/incident/19900120003919I), Jan 20, 1990: Rkwell NA26560 (N33JW), Syracuse, NY. Hydraulic problem on climb. Returned. Up limit switch out of adjustment due to worn linkage.
- [Incident 19890302011779I](https://openairdocs.org/incident/19890302011779I), Mar 2, 1989: Rkwell NA26560 (N71CC), Rifle, CO. Landed and slid off wet slippery runway.
- [Incident 19890212013609I](https://openairdocs.org/incident/19890212013609I), Feb 12, 1989: Rkwell NA26560 (N401MS), Ft Lauderdale, FL. While attempting to start second engine while taxiing, lost hydraulics. Ran off taxiway. Procedure not recommended.
- [Incident 19880822058299I](https://openairdocs.org/incident/19880822058299I), Aug 22, 1988: Rkwell NA26560 (N743UP), Dallas, TX, Minor damage. Lost nose gear steering control during turn while taxiing. Nose gear struck concrete curb shearing strut.
- [Incident 19871127074339I](https://openairdocs.org/incident/19871127074339I), Nov 27, 1987: Rkwell NA26560 (N401MS), Ft Lauderdale, FL. Made a go around due failure to find runway at night VFR. A second go around due inability to verify gear lights.
- [Incident 19810518044989I](https://openairdocs.org/incident/19810518044989I), May 18, 1981: Rkwell NA26560 (N155EC), Ft Worth, TX, Minor damage. During taxi aircraft had no steering or brakes. Hydraulic switch found in off position.
- [Incident 19790315009379I](https://openairdocs.org/incident/19790315009379I), Mar 15, 1979: Rkwell NA26560 (N3278), Quincy, IL, Minor damage. Pilot failed to extend gear before landing
- [Accident 19730413010249A](https://openairdocs.org/incident/19730413010249A), Apr 13, 1973: Rkwell NA26530 (N743R), Montrose, CO, Destroyed. Contd opn of l eng at climb pwr after unwanted in-flt deployment of l eng thrust reverser.

## Service difficulty reports (24)

As reported by operators and repair stations, by the model named in the report.

- [SDR UVVR2012101700028](https://openairdocs.org/sdr/UVVR2012101700028), Dec 24, 2013: LONGERON. CORRODED. DURING VISUAL INSPECTION OF COCKPIT FLOORS LOWER LONGERONS. FOUND CORROSION LT LOWER LONGERON CORRODED & SIGN OF EXFOLIATION FROM FS 108-134.
- [SDR 2012FA0000643](https://openairdocs.org/sdr/2012FA0000643), Sep 17, 2012: STIFFENER. CRACKED. WHILE PERFORMING A ROUTINE INSPECTION, FOUND A CRACK IN THE LT STIFFENER. CRACK PROPAGATED FROM A CORROSION PIT IN THE HAT SECTION STIFFENER. REPLACED IAW SRM A
- [SDR 2009FA0000877](https://openairdocs.org/sdr/2009FA0000877), Mar 17, 2009: VALVE. FAILED. ACFT EXPERIENCED AN UNCOMMANDED GEAR UP DURING TROUBLE SHOOTING FOR FREQUENT HYD CYCLING, WHILE IN HANGAR. MX WAS ATTEMPTING TO LOCATE THE SOURCE OF HYDARULIC F
- [SDR 2008FA0000663](https://openairdocs.org/sdr/2008FA0000663), Aug 26, 2008: PUMP. WORN. AFTER TAKEOFF THE PILOT COULD NOT ADJUST THE LT ENGINE POWER OUTPUT. ENGINE REMAINED AT TAKEOFF POWER WHILE POWER LEVER WAS RETARDED TO IDLE. PILOT RETURNED TO 
- [SDR 2007FA0001032](https://openairdocs.org/sdr/2007FA0001032), Oct 22, 2007: DUCT. DEFORMED. ATTACHING SLEEVE SLID OFF OF DUCT CAUSING LOSS OF PRESSURIZATION. EMERGENCY PRESSURIZATION FUNCTIONED NORMALLY. CLAMPS TIGHTENED TOO TIGHT AND DEFORMED FIBERGLA
- [SDR UVVR200600001](https://openairdocs.org/sdr/UVVR200600001), Feb 21, 2006: NUT. CRACKED. WHILE PERFORMING MAINTENANCE ON AIRCRAFT, IT WAS DISCOVERED THAT APPROXIMATELY 10 NUTS ON EACH WING THAT SECURES UPPER WING PLANK TO REAR SPAR UPPER FLANGE, FRO
- [SDR CAR110](https://openairdocs.org/sdr/CAR110), Jun 4, 2005: MIXING VALVE. NOT BONDED. HOT AIR MIXING VALVE WAS OVERHAULED BY ROCKER, 1-25-05, REF WO 56559. INSTALLED IN AIRCRAFT FROM STOCK ON 6-4-05. DURING FUNCTIONAL TEST FLIGHT FOR PRESSURIZATI
- [SDR WK42004F00003](https://openairdocs.org/sdr/WK42004F00003), Feb 10, 2004: TIRE. DAMAGED. CENTER TREAD CHUNKED AFTER 23 LANDINGS ON RT TIRE. THE REVISION IS TO THE SN OF THE TIRE WHICH HAS THE DAMAGE TO IT. THE PREVIOUS SN WAS TO THE WHEEL ASSY ITSEL
- [SDR WK42004F00001](https://openairdocs.org/sdr/WK42004F00001), Feb 10, 2004: TIRE. DAMAGED. CENTER TREAD CHUNKED AFTER 23 LANDINGS ON RT HAND TIRE.
- [SDR T2C2004F00000](https://openairdocs.org/sdr/T2C2004F00000), Feb 4, 2004: CASTING. CRACKED. DURING RUDDER RIGGING CHECK, FOUND CRACKED CASTING AT RUDDER PEDAL TORQUE TUBE SUPPORT, BELOW CO-PILOTS FLOOR. SUSPECT WIND GUST DAMAGE AS POSSIBLE CAUSE. ALSO 
- [SDR 20000516SH026](https://openairdocs.org/sdr/20000516SH026), Apr 25, 2000: FAIRING. CORRODED. DURING ROUTINE MAINTENANCE TO REPAIR FUEL LEAK FROM OVERWING FAIRING ASSY, REMOVED LEFT OVERWING FAIRING AND DISCOVERED EXTREME CASE OF EXFOLIATION CORROSION TH
- [SDR 20000516SH025](https://openairdocs.org/sdr/20000516SH025), Apr 25, 2000: FAIRING. CORRODED. DURING ROUTINE MAINTENANCE TO REPAIR FUEL LEAK FROM OVERWING FAIRING ASSY, REMOVED LEFT OVERWING FAIRING AND DISCOVERED EXTREME CASE OF EXFOLIATION CORROSION TH
- [SDR 20000516SH024](https://openairdocs.org/sdr/20000516SH024), Apr 25, 2000: FAIRING. CORRODED. DURING ROUTINE MAINTENANCE TO REPAIR FUEL LEAK FROM OVERWING FAIRING ASSY, REMOVED LEFT OVERWING FAIRING AND DISCOVERED EXTREME CASE OF EXFOLIATION CORROSION TH
- [SDR 20000516SH023](https://openairdocs.org/sdr/20000516SH023), Apr 25, 2000: FAIRING. CORRODED. DURING ROUTINE MAINTENANCE TO REPAIR FUEL LEAK FROM OVERWING FAIRING ASSY, REMOVED LEFT OVERWING FAIRING AND DISCOVERED EXTREME CASE OF EXFOLIATION CORROSION TH
- [SDR 2000ZZZX27](https://openairdocs.org/sdr/2000ZZZX27), Dec 7, 1999: SWITCH. OUT OF RIG. CREW EXTENDED LANDING GEAR ON APPROACH TO SUS. NO GREEN DOWN AND LOCKED LIGHT ON LT SIDE. LANDING GEAR WAS CYCLED WITH SAME RESULTS. CREW PERFORMED EMERGENCY EX
- [SDR 99ZZZX3469](https://openairdocs.org/sdr/99ZZZX3469), Aug 6, 1999: THERMOSTAT. FAILED. THERMOSTAT INSTALLED ON A FRESHLY OVERHAULED ENGINE. ENGINE WAS OVERHAULED BY FAA CRS OTUR438L. PART DID NOT FAIL UNTIL ONE HOUR INTO FIRST FLIGHT.
- [SDR 96ZZZX1360](https://openairdocs.org/sdr/96ZZZX1360), Feb 9, 1996: BLADE. OVERLAP. DUE TO CORROSION DMG DISCOVERED ON RT ENG, CUSTOMER ELECTED TO DISASSEMBLE LT ENG FOR CORROSION INSP, & SUBSEQUENT COMPR OVERHAUL PER P&WA. UPON DISASSEMBLY OF 
- [SDR 96ZZZX1359](https://openairdocs.org/sdr/96ZZZX1359), Feb 9, 1996: BLADE. RUB. DURING INSPECTION OF ENGINE, SN P673149NB, A CRACKED INLET GUIDE VANE PROMPTED REMOVAL OF INLET CASE FOR REPAIRS. WITH CASE REMOVED, A COMPRESSOR BLADE RUB, WHI
- [SDR 95ZZZX5865](https://openairdocs.org/sdr/95ZZZX5865), Oct 4, 1995: ACTUATOR. LEAKING. REMOVED THRUST REVERSER ACTUATOR DUE TO LEAKING AT SHAFT. PARKER HANNIFIN CALLS OUT MINOR LEAKING AFTER SO MANY CYCLES. ACTUATOR REMOVED HAS 12.8 HOURS TSO AND 
- [SDR 95ZZZX5864](https://openairdocs.org/sdr/95ZZZX5864), Oct 4, 1995: ACTUATOR. LEAKING. REMOVED THRUST REVERSER ACTUATOR DUE TO LEAKING AT SHAFT. PARKER HANNIFIN CALLS OUT MINOR LEAKING AFTER SO MANY CYCLES. ACTUATOR REMOVED, HAS 18 HOURS TSO AND I
- [SDR 95ZZZX5863](https://openairdocs.org/sdr/95ZZZX5863), Oct 4, 1995: ACTUATOR. LEAKING. REMOVED TRUST REVERSER ACTUATOR DUE TO LEAKING AT SHAFT. PARKER HANNIFIN CALLS OUT MINOR LEAKING AFTER SO MANY CYCLES. ACTUATOR REMOVED HAS 18 HOURS TSO AND IS 
- [SDR 95ZZZX6460](https://openairdocs.org/sdr/95ZZZX6460), Sep 4, 1995: WHEEL ASSY. RIM BOLTS LOOSE. NOSE WHEEL ASSY VIBRATED DURING ROUTINE TAKEOFF. WHILE ON GROUND, NOSE WHEEL ASSY WAS INSPECTED AND 2 RIM RETAINING BOLTS WERE FOUND LOOSE. TIRE WAS DEFLATED AN
- [SDR 95ZZZX5314](https://openairdocs.org/sdr/95ZZZX5314), Aug 28, 1995: GUIDE VANE. BURNED. ENGINE RECEIVED FOR CORR & HOT SECT INSP PER SB 1508. ENG OPERATED TO 1,227 HRS TIME SINCE LAST HOT SECT INSP. ENG SUFFERED LOSS OF 3 EA NOZZLE GUIDE VANES COMP
- [SDR 95ZZZX906](https://openairdocs.org/sdr/95ZZZX906), Jan 31, 1995: PROBE. CRACKED. PILOTS REPORTED THAT FUEL QUANTITY INDICATION BECAME ERRATIC IN-FLIGHT. AFTER TROUBLESHOOTING AND PINPOINTING PROBLEM TO BE AUXILIARY FUEL TANK PROBE, REMOVAL O

## STCs that may be installed (OpenAirDocs) (155, first 50)

Approved for this model: the STC's model list names it on its data sheet, or a series that includes it. In force first, then newest. The registry doesn't record which STCs an aircraft has.

- [STC ST01305WI-D](https://openairdocs.org/stc/ST01305WI-D): Modification of a Collins ALT-50A or ALT-55B Radio Altimeter system installation to a Collins ALT-1000 or ALT-4000 Radio Altimeter system installation in accordance with Collins Drawing Index as listed on AML No. ST01305WI-D, Revision -, or later FAA approved revision. Rockwell Collins Inc
- [STC SA2622NM](https://openairdocs.org/stc/SA2622NM): Installation of Precise Flight Pulselite Control Unit in landing/taxi system. (767-200 B17) (DHC-8 101). Precise Flight Inc
- [STC ST00106WI](https://openairdocs.org/stc/ST00106WI): Installation of a BFGoodrich model TCAS791 traffic alert and collision avoidance system (TCAS) I. Acron Aviation Inc
- [STC ST01930LA](https://openairdocs.org/stc/ST01930LA): Installation of Sandel Avionics SN4500 Electronic Horizontal Situation Indicator (EHSI). Sandel Avionics LLC
- [STC ST02635LA](https://openairdocs.org/stc/ST02635LA): Modification to replace the existing Mode S Transponder system with the ACSS NXT-600 Mode S Transponder with ADS-B Out. Aviation Communication and Surveillance Systems (ACSS) LLC
- [STC SA4991SW](https://openairdocs.org/stc/SA4991SW): Installation of freon air conditioning. Air Comm Corporation
- [STC ST00790DE](https://openairdocs.org/stc/ST00790DE): Installation of BendixKing CAS 67B Traffic Alert and Collision Avoidance System (TCAS) II Version 7.1. Peregrine
- [STC ST02636LA](https://openairdocs.org/stc/ST02636LA): Modification to upgrade the existing XS-950 Mode S Transponder system to add ADS-B Out. Aviation Communication and Surveillance Systems (ACSS) LLC
- [STC ST00347BO](https://openairdocs.org/stc/ST00347BO): Modification to upgrade a BendixKing CAS 67A TCAS II system to CAS 67B TCAS II Change 7.1. Pro Star Aviation, LLC
- [STC ST00373BO](https://openairdocs.org/stc/ST00373BO): Installation of Rockwell Collins TDR-94D Transponders with ADS-B Out. Pro Star Aviation, LLC
- [STC SA2901SW](https://openairdocs.org/stc/SA2901SW): Installation of Global GNS-500A Omega/VLF Navigation System. Associated Air Center, Inc. - c/o CT Corporation System
- [STC ST00304WI](https://openairdocs.org/stc/ST00304WI): Installation of Keddeg Company 21BC113 coaleser assembly. Purolator Facet, Inc
- [STC ST02632LA](https://openairdocs.org/stc/ST02632LA): Modification to replace the existing Mode S Transponder system with ACSS NXT-700 Mode S Transponder with ADS-B Out and optionally install ACSS NXG-900 GPS as a position source for ADS-B Out. Aviation Communications and Surveillance Systems
- [STC ST02609LA](https://openairdocs.org/stc/ST02609LA): Modification to replace the existing Mode S Transponder system with ACSS NXT-700 Mode S Transponder with ADS-B Out. Aviation Communication and Surveillance Systems (ACSS) LLC
- [STC SA1357GL](https://openairdocs.org/stc/SA1357GL): Install air ambulance stretcher P/N 125 using installation kit P/N 805. Paul/ Lanna Egan LLC
- [STC ST00881WI-D](https://openairdocs.org/stc/ST00881WI-D): Modification of a TCAS II system installation to Change 7.0 or Change 7.1. Rockwell Collins Inc
- [STC SA1725SW](https://openairdocs.org/stc/SA1725SW): Installation of Foxtronics/TRAMM BTI-600 nickel cadmium battery temperature indicator and optional TRAMM R-600 voltage control. FoxCart GSE, LLC
- [STC SA1012CE](https://openairdocs.org/stc/SA1012CE): Install interior, version No. 8. Sabreliner Aviation LLC
- [STC SA1014CE](https://openairdocs.org/stc/SA1014CE): Cockpit voice and flight data recorder, altitude alerting system, encoding, and radio altimeters and weather radar installation. Sabreliner Aviation LLC
- [STC SA1075CE](https://openairdocs.org/stc/SA1075CE): Aft lavatory auxiliary seat installation. Sabreliner Aviation LLC
- [STC SA1078CE](https://openairdocs.org/stc/SA1078CE): Aft lavatory and auxiliary L.H. seat installation. Sabreliner Aviation LLC
- [STC SA1092CE](https://openairdocs.org/stc/SA1092CE): Installation of electronic components package, version H. Sabreliner Aviation LLC
- [STC SA1129CE](https://openairdocs.org/stc/SA1129CE): Installation of IFR delivery package. Sabreliner Aviation LLC
- [STC SA1139CE](https://openairdocs.org/stc/SA1139CE): aft facing forward L.H. seat installation. Sabreliner Aviation LLC
- [STC SA1146CE](https://openairdocs.org/stc/SA1146CE): Interior installation, version No. 9. Sabreliner Aviation LLC
- [STC SA1148CE](https://openairdocs.org/stc/SA1148CE): Installation of electronic components package, version N. Sabreliner Aviation LLC
- [STC SA1149CE](https://openairdocs.org/stc/SA1149CE): Installation of electronic components package, version P. Sabreliner Aviation LLC
- [STC SA1162CE](https://openairdocs.org/stc/SA1162CE): Installation of P & D valve fuel reservoir drain. Sabreliner Aviation LLC
- [STC SA1182CE](https://openairdocs.org/stc/SA1182CE): Auxiliary seat and baggage area installation. Sabreliner Aviation LLC
- [STC SA1191CE](https://openairdocs.org/stc/SA1191CE): Aisle facing seat and baggage area installation. Sabreliner Aviation LLC
- [STC SA1221CE](https://openairdocs.org/stc/SA1221CE): Install interior, version No. 10. Sabreliner Aviation LLC
- [STC SA1242CE](https://openairdocs.org/stc/SA1242CE): Installation of Collins ADF-60A Automatic Direction Finding and Intercontinental Dynamics Corp. RAD/BAR with Voice Terrain Advisory Systems. Sabreliner Aviation LLC
- [STC SA1247CE](https://openairdocs.org/stc/SA1247CE): Forward lavatory L.H. installation. Sabreliner Aviation LLC
- [STC SA1249CE](https://openairdocs.org/stc/SA1249CE): Interior installation, version No. 6 (wide body). Sabreliner Aviation LLC
- [STC SA1285SW](https://openairdocs.org/stc/SA1285SW): Installation of Collins 937R-1 weather radar antenna and WXR-80 weather radar system. Sabreliner Aviation LLC
- [STC SA1338CE](https://openairdocs.org/stc/SA1338CE): Installation of Global GNS-500A VLF/Omega navigation system. Sabreliner Aviation LLC
- [STC SA1339CE](https://openairdocs.org/stc/SA1339CE): Aft lavatory installation. Sabreliner Aviation LLC
- [STC SA1365CE](https://openairdocs.org/stc/SA1365CE): Installation of Compensated Pitot Static Heads (Rosemount Engineering). Sabreliner Aviation LLC
- [STC SA1367CE](https://openairdocs.org/stc/SA1367CE): Interior installation, Version No. 11. Sabreliner Aviation LLC
- [STC SA1379CE](https://openairdocs.org/stc/SA1379CE): Installation of Collins FPC-75 GPWS, IDC SAT/TAS Collins ALT-558 Radio Altimeter and Wulfsberg Flitefone III Provisions. Sabreliner Aviation LLC
- [STC SA1385CE](https://openairdocs.org/stc/SA1385CE): Installation of Electronic Components Package, Version R. Sabreliner Aviation LLC
- [STC SA1386CE](https://openairdocs.org/stc/SA1386CE): Installation of Electronic Components Package, Version Q. Sabreliner Aviation LLC
- [STC SA1429CE](https://openairdocs.org/stc/SA1429CE): Removal of fuel jettisoning provisions. Sabreliner Aviation LLC
- [STC SA1434CE](https://openairdocs.org/stc/SA1434CE): Interior installation Version No. 12. Sabreliner Aviation LLC
- [STC SA1479CE](https://openairdocs.org/stc/SA1479CE): Installation of forward auxiliary fuel cell (56 gallons). Sabreliner Aviation LLC
- [STC SA1768CE](https://openairdocs.org/stc/SA1768CE): Install wing rib fuel baffles and clips. Sabreliner Aviation LLC
- [STC SA1811WE](https://openairdocs.org/stc/SA1811WE): Installation of Reinforced Structure and Certain Components in Partial Provision for the University Corporation for Atmospheric Research (UCAR) Configuration. Sabreliner Aviation LLC
- [STC SA1917CE](https://openairdocs.org/stc/SA1917CE): Installation of Puritan-Bennett "sweep on, low profile" quick donning crew mask and regulator assembly. Sabreliner Aviation LLC
- [STC SA2143CE](https://openairdocs.org/stc/SA2143CE): Installation of a modified entry step system for the entrance door. Sabreliner Aviation LLC
- [STC SA2160CE](https://openairdocs.org/stc/SA2160CE): Installation of Teledyne angle of attack system. Sabreliner Aviation LLC

All 155: https://openairdocs.org/model/north-american-na-265-60/stcs.md

## PMA parts (OpenAirDocs) (321, first 50)

Current parts manufacturer approvals (PMA): parts the FAA has approved companies to make as replacements or modifications. Each record lists its models as free text; OpenAirDocs matched them to this model on its data sheet, so check the FAA record before relying on it. Newest first.

- [HWP7072-4](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID106803255520250304194239.0001): Performed Packing. Hemico Inc. · PMA PQ2145NE · Replaces 9524796 · Oct 16, 2024
- [N1235XXXX](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID149447132020240819142524.0001): Fluorescent Lamp. Aircraft Lighting International · PMA PQ2043NE · Replaces AL1235XXXX · Aug 6, 2024
- [5002742AB](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID143151553720230824131312.0001): Plate, Instruction. Aero Brake & Spares Inc · PMA PQ0694SW · Replaces 5002742 · May 26, 2023
- [R1235XXXX](https://drs.faa.gov/browse/excelExternalWindow/D509AE89EEB5DFE086258618004BDA08.0001): LED Lamp. Aircraft Lighting International · PMA PQ2043NE · Replaces AL1235XXXX · Oct 29, 2020
- [N1235XXXX](https://drs.faa.gov/browse/excelExternalWindow/C18A1D02C7887EAF86258618004BDA8B.0001): Fluorescent Lamp. Aircraft Lighting International · PMA PQ2043NE · Replaces AL1235XXXX · Oct 29, 2020
- [744238-1WE](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID251701465220210611172357.0001): Shaft, Drive. Wencor LLC · PMA PQ1370NM · Replaces 744238-1 · Oct 15, 2020
- [L1235XXXX KIT](https://drs.faa.gov/browse/excelExternalWindow/BA375A52AAD1423F862585D80046E4EB.0001): LED Lamp and Adapter Kit. Aircraft Lighting International · PMA PQ2043NE · Replaces AL1235XXXX and AL2000 · Aug 22, 2020
- [04320073-0005B](https://drs.faa.gov/browse/excelExternalWindow/8213C712E21826E486258550005032DE.0001): LCD Display Module. Optical Display Engineering · PMA PQ04407CE · Replaces Honeywell P/N 04320073-0005 · May 30, 2019
- [M23032-2710](https://drs.faa.gov/browse/excelExternalWindow/98EF27A0292FF3CE862582CF006DC090.0001): Dampener Plate. Miraj Corporation · PMA PQ0870NE · Replaces 23032-2710 · Jun 17, 2018
- [21BC113](https://drs.faa.gov/browse/excelExternalWindow/01000DB549F4BF1F86258244006F1F8B.0001): Coalescer Assembly. Purolator Facet Inc (formerly Facet Filter Products) · PMA PQ1207CE · Modification part · Jan 18, 2018
- [SK2210](https://drs.faa.gov/browse/excelExternalWindow/F881DD5C26667D96862582D300748009.0001): Radome Boot. Skandia, Inc. · PMA PQ2665CE · Modification part · Dec 18, 2017
- [04320073-0005B](https://drs.faa.gov/browse/excelExternalWindow/C7B9A18130E6FB24862581AE0077E6F0.0001): LCD DISPLAY MODULE. Optical Display Engineering · PMA PQ5342NM · Replaces 04320073-0005 · Sep 5, 2017
- [04320073-0005B](https://drs.faa.gov/browse/excelExternalWindow/2691AB4003318B528625818A006F0151.0001): LCD DISPLAY MODULE. Optical Display Engineering · PMA PQ5342NM · Replaces 04320073-0005 · Aug 2, 2017
- [21BC113G](https://drs.faa.gov/browse/excelExternalWindow/9072C379E89535758625816E00788ED5.0001): Coalescer Assembly. Purolator Facet Inc (formerly Facet Filter Products) · PMA PQ1207CE · Replaces 83237-12 · Jun 28, 2017
- [M05-374094](https://drs.faa.gov/browse/excelExternalWindow/04A248CF6B40096C862580E40064D09B.0001): Washer, Non Metallic. Miraj Corporation · PMA PQ0870NE · Replaces Safran/Goodrich 05-374094 · Mar 6, 2017
- [L610549](https://drs.faa.gov/browse/excelExternalWindow/CDB691EA97580B1C86257FC5006D9EEC.0001): CONE. Timken Corporation · PMA PQ4105CE · Replaces L610549 · May 24, 2016
- [18720](https://drs.faa.gov/browse/excelExternalWindow/A849DA3AAA8855AC86257FC5006D9DC8.0001): CUP. Timken Corporation · PMA PQ4105CE · Replaces 18720 · May 24, 2016
- [L305610](https://drs.faa.gov/browse/excelExternalWindow/852030EE83B1F2D186257FC5006D9ECD.0001): CUP. Timken Corporation · PMA PQ4105CE · Replaces L305610 · May 24, 2016
- [L610510](https://drs.faa.gov/browse/excelExternalWindow/69E25E87552998F386257FC5006D9EE7.0001): CUP. Timken Corporation · PMA PQ4105CE · Replaces L610510 · May 24, 2016
- [L305649](https://drs.faa.gov/browse/excelExternalWindow/389562090106BBC386257FC5006D9ED0.0001): CONE. Timken Corporation · PMA PQ4105CE · Replaces L305649 · May 24, 2016
- [18790](https://drs.faa.gov/browse/excelExternalWindow/34DF4E007D21128286257FC5006D9DCE.0001): CONE. Timken Corporation · PMA PQ4105CE · Replaces 18790 · May 24, 2016
- [P30903819](https://drs.faa.gov/browse/excelExternalWindow/9D71C046EBD7E23F86257BBF0062D22D.0001): Cartridge. HRD Aerosystems Inc · PMA PQ1451NM · Replaces HTL 30903819 · Mar 13, 2016
- [P13083-10](https://drs.faa.gov/browse/excelExternalWindow/968310E0C66A2CEC86257BBF0062D1F3.0001): Cartridge. HRD Aerosystems Inc · PMA PQ1451NM · Replaces HTL 13083-10 · Mar 13, 2016
- [P31840000 or P31840001](https://drs.faa.gov/browse/excelExternalWindow/834FBA1D12D7887786257F8E006C0E2F.0001): Stem, Valve. HRD Aerosystems Inc · PMA PQ1451NM · Replaces HTL 31840000 · Mar 13, 2016
- [P31840000 or P31840001](https://drs.faa.gov/browse/excelExternalWindow/744B99969426B75186257F8E006C0ED6.0001): Stem, Valve. HRD Aerosystems Inc · PMA PQ1451NM · Replaces HTL 31840000 · Mar 13, 2016
- [P13146](https://drs.faa.gov/browse/excelExternalWindow/43776E3B244F95BD86257BBF0062D1E4.0001): House Assy.. HRD Aerosystems Inc · PMA PQ1451NM · Replaces HTL 13146 · Mar 13, 2016
- [N1235XXXX](https://drs.faa.gov/browse/excelExternalWindow/E957B45B9CF1398086257F55005E97D4.0001): Fluorescent Lamp. Aircraft Lighting International · PMA PQ2043NE · Replaces Aerospace Lighting Corp. P/N AL1235XXXX · Feb 7, 2016
- [R1235XXXX](https://drs.faa.gov/browse/excelExternalWindow/862EA0DC987F710F86257F55005E984B.0001): LED Lamp. Aircraft Lighting International · PMA PQ2043NE · Replaces Aerospace Lighting Corp. P/N AL1235XXXX · Feb 7, 2016
- [L1235XXXXKIT](https://drs.faa.gov/browse/excelExternalWindow/3C11606BBC6DA71886257F55005E98E5.0001): LED Lamp and Adapter Kit. Aircraft Lighting International · PMA PQ2043NE · Replaces Aerospace Lighting Corp. Fluorescent… · Feb 7, 2016
- [RFS2050](https://drs.faa.gov/browse/excelExternalWindow/E8AD6281C4BF526986257F380074250B.0001): Stationary Disc. Rapco Fleet Support Inc · PMA PQ2386CE · Replaces 5002756 Meggitt Aircraft Braking Systems · Jan 6, 2016
- [RFS5125](https://drs.faa.gov/browse/excelExternalWindow/A88D077485C3CC1C86257F3800742585.0001): Stationary Disc Assembly. Rapco Fleet Support Inc · PMA PQ2386CE · Replaces 5003957 Meggitt Aircraft Braking Systems · Jan 6, 2016
- [RFS3090](https://drs.faa.gov/browse/excelExternalWindow/66C6564CD72E35C386257F3800742466.0001): Wear Pad. Rapco Fleet Support Inc · PMA PQ2386CE · Replaces 5003956 Meggitt Aircraft Braking Systems · Jan 6, 2016
- [RFS4150](https://drs.faa.gov/browse/excelExternalWindow/643A4976D81C052186257F38007424D3.0001): Pressure Plate. Rapco Fleet Support Inc · PMA PQ2386CE · Replaces 5002758 Meggitt Aircraft Braking Systems · Jan 6, 2016
- [RFS18B9](https://drs.faa.gov/browse/excelExternalWindow/22828CBEB0436F0686257F38007424A0.0001): Rivet. Rapco Fleet Support Inc · PMA PQ2386CE · Replaces GY18B9 Meggitt Aircraft Braking Systems · Jan 6, 2016
- [RFS5175](https://drs.faa.gov/browse/excelExternalWindow/119180F7E0D26F4386257F3800742548.0001): Pressure Plate Assembly. Rapco Fleet Support Inc · PMA PQ2386CE · Replaces 5003958 Meggitt Aircraft Braking Systems · Jan 6, 2016
- [RFS1055](https://drs.faa.gov/browse/excelExternalWindow/0B966E5DA6071E7F86257F3800742430.0001): Rotating Disc. Rapco Fleet Support Inc · PMA PQ2386CE · Replaces 5002531 Meggitt Aircraft Braking Systems · Jan 6, 2016
- [18790](https://drs.faa.gov/browse/excelExternalWindow/8CD1842E6FAEEF9E86257D2A00574574.0001): CONE. Timken Corporation · PMA PQ4105CE · Replaces 18790 · Jun 29, 2014
- [L305649](https://drs.faa.gov/browse/excelExternalWindow/85E66C8B460A07F486257D2A005745F7.0001): CONE. Timken Corporation · PMA PQ4105CE · Replaces L305649 · Jun 29, 2014
- [L610510](https://drs.faa.gov/browse/excelExternalWindow/722FAD27DF52029B86257D2A00574604.0001): CUP. Timken Corporation · PMA PQ4105CE · Replaces L610510 · Jun 29, 2014
- [L610549](https://drs.faa.gov/browse/excelExternalWindow/6E7DC10A73D1D1B186257D2A00574607.0001): CONE. Timken Corporation · PMA PQ4105CE · Replaces L610549 · Jun 29, 2014
- [18720](https://drs.faa.gov/browse/excelExternalWindow/6B23BA6708AB445286257D2A00574571.0001): CUP. Timken Corporation · PMA PQ4105CE · Replaces 18720 · Jun 29, 2014
- [L305610](https://drs.faa.gov/browse/excelExternalWindow/5209E7E442B5AE1D86257D2A005745F5.0001): CUP. Timken Corporation · PMA PQ4105CE · Replaces L305610 · Jun 29, 2014
- [P13083-10](https://drs.faa.gov/browse/excelExternalWindow/E8F1BC94F7DA565B86257CB70060F34C.0001): Cartridge. HRD Aerosystems Inc · PMA PQ1451NM · Replaces HTL, 13083-10 · May 27, 2014
- [P31840000 or P31840001](https://drs.faa.gov/browse/excelExternalWindow/E3C5010A3C4E138286257C470070FCCE.0001): Stem, Valve. HRD Aerosystems Inc · PMA PQ1451NM · Replaces HTL P31840000 · May 27, 2014
- [P31840000 or P31840001](https://drs.faa.gov/browse/excelExternalWindow/C058F78125CE24AB86257C470070FD9A.0001): Stem, Valve. HRD Aerosystems Inc · PMA PQ1451NM · Replaces HTL P31840000 · May 27, 2014
- [P13146](https://drs.faa.gov/browse/excelExternalWindow/945B2D7B16AC1A2D86257CB70060F33A.0001): House Assy.. HRD Aerosystems Inc · PMA PQ1451NM · Replaces HTL, 13146 · May 27, 2014
- [P30903819](https://drs.faa.gov/browse/excelExternalWindow/41B70991D2A19DC486257CB70060F396.0001): Cartridge. HRD Aerosystems Inc · PMA PQ1451NM · Replaces HTL, 30903819 · May 27, 2014
- [NPFA517-1070-1](https://drs.faa.gov/browse/excelExternalWindow/C6FB72C136D5022D86257C60005CF0BD.0001): Cover Assembly. New POP LLC · PMA PQ4166CE · Replaces 517-1070-1 · Dec 11, 2013
- [P13146](https://drs.faa.gov/browse/excelExternalWindow/FD36B812B10EC52286257C470070F0DB.0001): House Assy.. HRD Aerosystems Inc · PMA PQ1451NM · Replaces HTL 13146 · Nov 21, 2013
- [P30903819](https://drs.faa.gov/browse/excelExternalWindow/F3B166A9085E241086257C470071084F.0001): Cartridge. HRD Aerosystems Inc · PMA PQ1451NM · Replaces HTL 30903819 · Nov 21, 2013

All of them: https://openairdocs.org/model/north-american-na-265-60/pma.md

## The same model under other registry codes

Amateur-built copies and renamed makers get their own codes.

- [Rockwell International NA-265-60](https://openairdocs.org/model/rockwell-international-na-265-60): 4 registered aircraft, registry code 7630106

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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.