# Sabreliner NA-265-80

- Type: Aircraft model (FAA registry)
- Registry code: 6403001
- Manufacturer (registry): SABRELINER CORP
- Model: NA-265-80
- Aircraft type: Fixed wing multi engine
- Category: Airplane
- Engines: 2 · Turbo-fan
- Seats: 12
- Weight class: 20,000 lb and over
- Certification: Type certificated
- Data sheet: [TCDS A2WE](https://openairdocs.org/tcds/A2WE) (OpenAirDocs)
- Holder: Sabreliner Aviation LLC
- Registered aircraft: 0
- Page: https://openairdocs.org/model/sabreliner-na-265-80

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 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 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 94-01-05](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 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 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 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 80-03-05 R1](https://openairdocs.org/ad/80-03-05-R1): Elevator Trailing Edge · Sabreliner NA-265-70 and NA-265-80. Effective May 29, 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 77-25-02](https://openairdocs.org/ad/77-25-02): Engine Fire Detection System · Sabreliner NA-265-70 and NA-265-80. Effective Dec 12, 1977
- [AD 77-10-10](https://openairdocs.org/ad/77-10-10): Electrical System · Sabreliner NA-265-80. Effective May 23, 1977
- [AD 76-12-09](https://openairdocs.org/ad/76-12-09): Inflight Flutter · Sabreliner NA-265-70 and NA-265-80. Effective Jun 23, 1976
- [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 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 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

## Registered aircraft

None registered with this model now.

## NTSB investigations

None matched to aircraft with this model.

## FAA accident and incident reports

None matched to aircraft with this model.

## Service difficulty reports (33)

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

- [SDR 2021FA0000004](https://openairdocs.org/sdr/2021FA0000004), Nov 4, 2021: PANEL. DAMAGED. CABIN FLOOR PANEL IS DAMAGED.
- [SDR BTA2003F00001](https://openairdocs.org/sdr/BTA2003F00001), Feb 12, 2003: ENGINE. FLAMED OUT. AIRCRAFT IN FLIGHT AT HIGH ALTITUDE (FL410) AIRCRAFT GOT SLOW (APPROXIMATELY 165 KNOTS). RIGHT ENGINE FLAMED OUT. ADVISE ATC THAT WE HAD ENGINE PROBLEM AND REQU
- [SDR BTA2003F00000](https://openairdocs.org/sdr/BTA2003F00000), Feb 12, 2003: ENGINE. FLAMED OUT. AIRCRAFT IN FLIGHT AT HIGH ALTITUDE (FL410) AIRCRAFT GOT SLOW (APPROX. 165 KNTS). RIGHT ENGINE FLAMED OUT. ADVISE ATC THAT WE HAD ENGINE PROBLEM AND REQUEST TO 
- [SDR UVV2002F00000](https://openairdocs.org/sdr/UVV2002F00000), Apr 19, 2002: PANEL. CORRODED. FOUND OVER FLAP PANEL UNDERSIDE CORRODED COMPLETELY THROUGH SKIN TO HONEYCOMB SUBSTRUCTURE. AREA NOT READILY INSPECTABLE DUE TO VELCRO APPLIED OVER AREA TO ACT 
- [SDR 2001FA0000393](https://openairdocs.org/sdr/2001FA0000393), Sep 27, 2001: SUPPORT. BROKEN. DURING SCHEDULED INSPCTION FOUND SMALL PIECE OF A BEARING BOSS IN HELL HOLE. UPON INVESTIGATION FOUND ELEVATOR TORQUE TUBE SUPPORT MISSING PIECE. ALSO FOUND RT 
- [SDR 20010510AP001](https://openairdocs.org/sdr/20010510AP001), Apr 24, 2001: LEVER. MISMANUFACTURED. ON 8/9/99 1EA. P/N232-20258-511 WAS INSTALLED ON LT T/R. 2EA. P/N 232-20258-513 AND 2EA. 232-20258-514 LEVERS WERE INSTALLED ON RT T/R DURING REPAIR OF THESE T/
- [SDR 20010501AP004](https://openairdocs.org/sdr/20010501AP004), Apr 24, 2001: LEVER. MISMANUFACTURED. ON 8/9/99 1EA. P/N232-20258-511 WAS INSTALLED ON L/H T/R. 2EA. P/N 232-20258-513 AND 2EA. 232-20258-514 LEVERS WERE INSTALLED ON R/H T/R DURING REPAIR OF THESE 
- [SDR 20000508SH006](https://openairdocs.org/sdr/20000508SH006), Apr 10, 2000: RIB. CRACKED. WHILE DOING HARD LANDING INSPECTION, THE RIB ASSEMBLY IN THE RT MAIN LANDING GEAR WHEELWELL WAS FOUND CRACKED. THIS POSSIBLE HARD LANDING WAS REPORTED TO MAINTE
- [SDR 20000504SH029](https://openairdocs.org/sdr/20000504SH029), Apr 10, 2000: RIB. CRACKED. DUE TO SUSPECTED HARD LANDING, AIRCRAFT WAS INSPECTED AND MAINTENANCE DISCOVERED A 1.50 INCH CRACK IN THE LOWER RADIUS OF THE RT MAIN LANDING GEAR ACTUATOR ATTA
- [SDR 20000505SH021](https://openairdocs.org/sdr/20000505SH021), Mar 2, 2000: THRUST REVERSER. MALFUNCTIONED. LEFT THRUST REVERSER FAILED TO RETURN TO STOW POSITION AFTER LANDING. CONNECTED EXTERNAL AIR SUPPLY TO THRUST REVERSER AIR SUPPLY MANIFOLD AND CLOSED THRUST REV
- [SDR 20000504SH028](https://openairdocs.org/sdr/20000504SH028), Dec 27, 1999: SWITCH. FAILED. THE AIRCRAFT RETURNED TO THE USMS RAMP WITH A LOG ENTRY STATING THE GEAR WILL NOT LOCK NORMAL, FREE FELL GEAR ALL GREEN. THE AIRCRAFT WAS PLACED ON JACKS AND TH
- [SDR 20000503SH008](https://openairdocs.org/sdr/20000503SH008), Aug 24, 1999: WHEEL. FAILED. THE AIRCRAFT RETURNED TO THE USMS RAMP WITH A DISCREPANCY ON THE NR 3 TIRE BEING FLAT. THE NR 3 WHEEL ASSY WAS REMOVED AND THE RIM HAD A 6-10 INCH SECTION OF TH
- [SDR RU3A99004](https://openairdocs.org/sdr/RU3A99004), May 24, 1999: VALVE. MALFUNCTIONED. OK - STRONG ODOR OF BURNING RUBBER COCKPIT IMMEDIATELY AFTER TAKEOFF. RIGHT ENGINE FIRE WARNING LIGHT ILLUMINATED IMMEDIATELY AFTER TAKEOFF. ENGINE SHUT DOWN AN
- [SDR 99ZZZX1969](https://openairdocs.org/sdr/99ZZZX1969), Mar 12, 1999: SUPPORT. CRACKED. DURING THE COURSE OF A ROUTINE ELEVATOR BALANCE INSPECTION, BOTH LEFT AND RIGHT ELEVATOR INBOARD HINGE BEARING SUPPORTS WERE FOUND CRACKED THROUGH THE BEARING S
- [SDR RU3A9805](https://openairdocs.org/sdr/RU3A9805), Oct 6, 1998: FIRE LOOP. MALFUNCTIONED. RIGHT ENGINE FIRE LIGHT ILLUMINATED IN FLIGHT. ENGINE POWER LEVER WAS BROUGHT BACK TO IDLE AND LIGHT EXTINGUISHED. RETURN TO STATION WITHOUT FURTHER INCIDENT. (
- [SDR 98ZZZX3333](https://openairdocs.org/sdr/98ZZZX3333), Aug 26, 1998: WHEEL RIM. DAMAGED. AFTER AIRCRAFT TAXIED TO PARKING, THE TIRE WAS FOUND FLAT. INSPECTION DISCOVERED THE INBOARD SIDE OF RIM BROKEN. THE MISSING PART WAS FOUND ON THE TAXIWAY. THE 
- [SDR 98ZZZX3594](https://openairdocs.org/sdr/98ZZZX3594), Aug 12, 1998: WEB. CRACKED. WHILE PERFORMING A VISUAL INSPECTION OF THE NOSE GEAR WHEEL WELL DURING A SCHEDULED 150 HOUR INSPECTION, CRACKS WERE DISCOVERED INSIDE THE NOSE GEAR WELL AT THE
- [SDR 98ZZZX3593](https://openairdocs.org/sdr/98ZZZX3593), Aug 12, 1998: WEB. CRACKED. WHILE PERFORMING A VISUAL INSPECTION OF THE NOSE GEAR WHEEL WELL DURING A SCHEDULED 150 HOUR INSPECTION, CRACKS WERE DISCOVERED INSIDE THE NOSE GEAR WELL AT THE
- [SDR 98ZZZX3592](https://openairdocs.org/sdr/98ZZZX3592), Aug 12, 1998: WEB. CRACKED. WHILE PERFORMING A VISUAL INSPECTION OF THE NOSE GEAR WHEEL WELL DURING A SCHEDULED 150 HOUR INSPECTION, CRACKS WERE DISCOVERED INSIDE THE NOSE GEAR WELL AT THE
- [SDR 98ZZZX3591](https://openairdocs.org/sdr/98ZZZX3591), Aug 12, 1998: WEB. CRACKED. WHILE PERFORMING A VISUAL INSPECTION OF THE NOSE GEAR WHEEL WELL DURING A SCHEDULED 150 HOUR INSPECTION, CRACKS WERE DISCOVERED INSIDE THE NOSE GEAR WELL AT THE
- [SDR 98ZZZX3341](https://openairdocs.org/sdr/98ZZZX3341), Aug 5, 1998: SLAT. SEPARATED. ON POST-FLIGHT INSPECTION, LT INBD SLAT WAS DISCOVERED MISSING (38) RIVETS ON THE UNDERSIDE AND BOTH INBD RIBS CRACKED AND BROKEN, HOLES VERY ELONGATED. ALSO, W
- [SDR HAIHEEA9853](https://openairdocs.org/sdr/HAIHEEA9853), May 13, 1997: ACTUATOR. LEAKS. ACTUATOR LEAKS.
- [SDR HAIHEEA9287](https://openairdocs.org/sdr/HAIHEEA9287), Mar 31, 1997: TRANSPONDER. INOPERATIVE. TRANSPONDER COMPLETELY DEAD.
- [SDR 97ZZZX1077](https://openairdocs.org/sdr/97ZZZX1077), Feb 5, 1997: BRAKE VALVE. MALFUNCTIONED. AIRCRAFT LANDED AT PTK AND DURING BRAKING, WENT OFF THE RIGHT SIDE OF RUNWAY. PILOTS STATED ACFT WAS PULLING TO THE RIGHT AND WAS NOT SLOWING DOWN FAST ENOUGH T
- [SDR HEEA978878](https://openairdocs.org/sdr/HEEA978878), Jan 14, 1997: ENGINE. OIL LEAK. LEAKING OIL FROM FAN SPLIT LINE.
- [SDR 96ZZZX4696](https://openairdocs.org/sdr/96ZZZX4696), Aug 20, 1996: SKIN. CRACKED. WHILE PERFORMING PRE-FLIGHT INSP, MECH NOTICED PAINT CRACKED AND CHIPPED ON L/E OF WING ABOUT SS 236.9. UPON FURTHER INSP FOUND A CRACK, ABOUT 8.5 INCHES, THROU
- [SDR 96ZZZX1345](https://openairdocs.org/sdr/96ZZZX1345), Jan 30, 1996: SKIN. CORRODED. DURING REPAINT OF AIRCRAFT WITH SUPER CRITICAL WING, FOUND EXISTING SEALANT CRACKED AND DETERIORATED. AT CUSTOMER REQUEST, REMOVED SEALANT AND FOUND ALUMINUM SK
- [SDR 96ZZZX1344](https://openairdocs.org/sdr/96ZZZX1344), Jan 30, 1996: SKIN. CORRODED. DURING REPAINT OF AIRCRAFT WITH SUPER CRITICAL WING, FOUND EXISTING SEALANT CRACKED AND DETERIORATED. AT CUSTOMER REQUEST, REMOVED SEALANT AND FOUND ALUMINUM SK
- [SDR 95ZZZX6840](https://openairdocs.org/sdr/95ZZZX6840), Oct 16, 1995: SUPPORT. CRACKED. SUPPORT CRACKED AT END WHERE ELEVATOR ATTACHES. THIS CAUSES HINGE BEARINGS, PN BR4, TO BE LOOSE. THIS PART CAN ONLY BE SEEN BY REMOVING HINGE SUPPORT, PN 285-22
- [SDR 95ZZZX5705](https://openairdocs.org/sdr/95ZZZX5705), Aug 23, 1995: SUPPORT ASSY. CRACKED. DEFECTS WERE FOUND DURING ROUTINE MAINTENANCE INSPECTION PER CAMP CARD NR 27013, ATA 274006, LT, AND ATA 274007, RT. THE LT INBD HORIZ SUPPORT WAS FOUND BROKEN 
- [SDR 95ZZZX5704](https://openairdocs.org/sdr/95ZZZX5704), Aug 23, 1995: SUPPORT ASSY. CRACKED. DEFECTS WERE FOUND DURING ROUTINE MAINTENANCE INSPECTION PER CAMP CARD NR 27013, ATA 274006, LT, AND ATA 274007, RT. THE LT INBD HORIZ SUPPORT WAS FOUND BROKEN 
- [SDR 95ZZZX1488](https://openairdocs.org/sdr/95ZZZX1488), Mar 6, 1995: INNER ARM. MISMANUFACTURED. ARMS ARE MANUFACTURED BY LEARJET UNDER PMA. BIZJET RECEIVED AND PUT IN STOCK 1 EACH DASH 511 ARM AND 6 EACH DASH 512 ARMS. ONE EACH DASH 511 ARM AND 2 EACH DASH
- [SDR 95ZZZX1487](https://openairdocs.org/sdr/95ZZZX1487), Mar 6, 1995: INNER ARM. MISMANUFACTURED. ARMS ARE MANUFACTURED BY LEARJET UNDER PMA. BIZJET RECEIVED AND PUT IN STOCK 1 EACH DASH 511 ARM AND 6 EACH DASH 512 ARMS. ONE EACH DASH 511 ARM AND 2 EACH DASH

## STCs that may be installed (OpenAirDocs) (91, 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 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 ST11216DS](https://openairdocs.org/stc/ST11216DS): Installation of automatic dependent surveillance-broadcast (ADS-B) out on Part 25 aircraft. BHE & Associates Ltd
- [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 ST03424CH](https://openairdocs.org/stc/ST03424CH): Certification of Automatic Dependent Surveillance - Broadcast (ADS-B) Out System with Rockwell Collins TDR-94/-94D Transponders. CMD Flight Solutions LLC
- [STC ST01930LA](https://openairdocs.org/stc/ST01930LA): Installation of Sandel Avionics SN4500 Electronic Horizontal Situation Indicator (EHSI). Sandel Avionics 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 ST00304WI](https://openairdocs.org/stc/ST00304WI): Installation of Keddeg Company 21BC113 coaleser assembly. Purolator Facet, Inc
- [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 ST02300NY](https://openairdocs.org/stc/ST02300NY): Certification of Sabreliner Model NA-265-80 to Stage 3 Noise Levels Utilizing Reduced Landing Weight. Flight Test Aerospace, Inc
- [STC SA00120WI](https://openairdocs.org/stc/SA00120WI): Modification of existing Sabreliner Model 80 thrust reverser 232-20262-503 flexure plate to provide improved fatigue life. Sabreliner Aviation LLC
- [STC SA1015CE](https://openairdocs.org/stc/SA1015CE): Installation of electronic components package Version C. Sabreliner Aviation LLC
- [STC SA1026CE](https://openairdocs.org/stc/SA1026CE): Install interior, version No. 3. Sabreliner Aviation LLC
- [STC SA1028CE](https://openairdocs.org/stc/SA1028CE): Installation of electronic components package, version B. Sabreliner Aviation LLC
- [STC SA1043CE](https://openairdocs.org/stc/SA1043CE): Installation of electronic components package, version D. Sabreliner Aviation LLC
- [STC SA1065CE](https://openairdocs.org/stc/SA1065CE): Installation of electronic components package, version E. Sabreliner Aviation LLC
- [STC SA1066CE](https://openairdocs.org/stc/SA1066CE): Installation of Teledyne angle of attack indicating system SL112B1400. Sabreliner Aviation LLC
- [STC SA1067CE](https://openairdocs.org/stc/SA1067CE): Auxiliary seat installation - aft lavatory. Sabreliner Aviation LLC
- [STC SA1074CE](https://openairdocs.org/stc/SA1074CE): Auxiliary seat installation. Sabreliner Aviation LLC
- [STC SA1100CE](https://openairdocs.org/stc/SA1100CE): Interior installation No. 4. Sabreliner Aviation LLC
- [STC SA1101CE](https://openairdocs.org/stc/SA1101CE): Installation of cockpit voice recorder and flight data recorder. Sabreliner Aviation LLC
- [STC SA1129CE](https://openairdocs.org/stc/SA1129CE): Installation of IFR delivery package. Sabreliner Aviation LLC
- [STC SA1132CE](https://openairdocs.org/stc/SA1132CE): Install aft lavatory auxiliary seat. Sabreliner Aviation LLC
- [STC SA1133CE](https://openairdocs.org/stc/SA1133CE): Interior installation, FAA Airways Checker. Sabreliner Aviation LLC
- [STC SA1142CE](https://openairdocs.org/stc/SA1142CE): Interior installation, version No. 5. Sabreliner Aviation LLC
- [STC SA1272CE](https://openairdocs.org/stc/SA1272CE): Interior installation, version No. 7. Sabreliner Aviation LLC
- [STC SA1274CE](https://openairdocs.org/stc/SA1274CE): Installation of electronic components package, Version F. Sabreliner Aviation LLC
- [STC SA1275CE](https://openairdocs.org/stc/SA1275CE): Interior installation, version No. 8 (wide body). Sabreliner Aviation LLC
- [STC SA1288CE](https://openairdocs.org/stc/SA1288CE): Interior installation, version No. 9. Sabreliner Aviation LLC
- [STC SA1293CE](https://openairdocs.org/stc/SA1293CE): Commode installation - aft lavatory. Sabreliner Aviation LLC
- [STC SA1323CE](https://openairdocs.org/stc/SA1323CE): Interior installation, Version No. 10. Sabreliner Aviation LLC
- [STC SA1329CE](https://openairdocs.org/stc/SA1329CE): Installation of Collins NCS-31A Navigation Control System with Dual Control Heads, HI-350 Remote Compass and Collins 718U-5 HF Transceiver System. Sabreliner Aviation LLC
- [STC SA1337CE](https://openairdocs.org/stc/SA1337CE): Installation of Intercontinental Dynamics Corp vertical navigation system. Sabreliner Aviation LLC
- [STC SA1338CE](https://openairdocs.org/stc/SA1338CE): Installation of Global GNS-500A VLF/Omega navigation system. Sabreliner Aviation LLC
- [STC SA1342CE](https://openairdocs.org/stc/SA1342CE): Install electronics components package, version 'G'. Sabreliner Aviation LLC
- [STC SA1374CE](https://openairdocs.org/stc/SA1374CE): Installation of 800 VA and2500 VA static inverters. Sabreliner Aviation LLC
- [STC SA1387CE](https://openairdocs.org/stc/SA1387CE): Passenger compartment wiring provisions installation. Sabreliner Aviation LLC
- [STC SA1479CE](https://openairdocs.org/stc/SA1479CE): Installation of forward auxiliary fuel cell (56 gallons). 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 SA2199CE](https://openairdocs.org/stc/SA2199CE): Installation of Universal Navigation Corporation UNS-1 Jr. Navigation Management System. Sabreliner Aviation LLC
- [STC SA2545CE](https://openairdocs.org/stc/SA2545CE): Installation of Fairchild Model GA-100 cockpit voice recorder system. Sabreliner Aviation LLC
- [STC SA2585CE](https://openairdocs.org/stc/SA2585CE): Installation of Global-Wulfsberg GNS-X Navigation Management System (NMS), Flightfone VI system, and Bendix/King RDS-82VP Vertical Profile Weather Radar system. Sabreliner Aviation LLC
- [STC SA995CE](https://openairdocs.org/stc/SA995CE): Installation of electronic components package, version A. Sabreliner Aviation LLC
- [STC SA997CE](https://openairdocs.org/stc/SA997CE): Install interior, version No. 2. Sabreliner Aviation LLC
- [STC ST00969WI](https://openairdocs.org/stc/ST00969WI): Installation of Honeywell Mark VIII Enhanced Ground Proximity Warning System. Sabreliner Aviation LLC
- [STC ST00995WI](https://openairdocs.org/stc/ST00995WI): Installation of ARTEX 110-406 MHz Emergency Locator Transmitter. Sabreliner Aviation LLC
- [STC ST01054WI](https://openairdocs.org/stc/ST01054WI): Installation of a Universal Corp Terrain Awareness Warning System (TAWS). Sabreliner Aviation LLC
- [STC ST01239WI](https://openairdocs.org/stc/ST01239WI): Installation of Dual Innovative Solutions and Support Inc. (IS&S) Air Data Display Units (ADDU), IS&S Air Data Sensor (ADS) and an Aerosonic Corporation Standby Altimeter. Sabreliner Aviation LLC
- [STC SA1663SW](https://openairdocs.org/stc/SA1663SW): Installation of Teledyne Avionic's normalized angle of attack indicating system, P/N 112B600. Aerosonic Corporation
- [STC SA30GL](https://openairdocs.org/stc/SA30GL): Installation of electronic engine synchronizer system. Ontic Engineering and Manufacturing Inc
- [STC ST01246WI](https://openairdocs.org/stc/ST01246WI): Reduced Vertical Separation Minimum (RVSM) Group airworthiness approval. Kohlman Systems Research Inc

All 91: https://openairdocs.org/model/sabreliner-na-265-80/stcs.md

## PMA parts (OpenAirDocs) (288, 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.

- [D6-4HP](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID173898989120250807175623.0001): Spring Washer. Central Texas Aircraft Parts (CTAP) · PMA PQ0880SW · Replaces D6-4 · Aug 4, 2025
- [3233190-2HP](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID116750333120250807175624.0001): Vespel Bearing. Central Texas Aircraft Parts (CTAP) · PMA PQ0880SW · Replaces 3233190-2 · Aug 4, 2025
- [D6-1HP](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID106601338320250807175622.0001): Spring Washer. Central Texas Aircraft Parts (CTAP) · PMA PQ0880SW · Replaces D6-1 · Aug 4, 2025
- [RFS9536729](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID122082803820250401174125.0001): Wear Pad. Rapco Fleet Support Inc · PMA PQ2386CE · Replaces 9536729 · Mar 31, 2025
- [N1235XXXX](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID149447132020240819142524.0001): Fluorescent Lamp. Aircraft Lighting International · PMA PQ2043NE · Replaces AL1235XXXX · Aug 6, 2024
- [232-20426-1HP](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID193733723020240703182621.0001): Bushing. Central Texas Aircraft Parts (CTAP) · PMA PQ0880SW · Replaces 232-20426-1 · Jun 24, 2024
- [232-20260-1HP](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID195545626220240703182603.0001): Bearing. Central Texas Aircraft Parts (CTAP) · PMA PQ0880SW · Replaces 232-20260-1 · May 17, 2024
- [232-20268-503HP](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID124664868220240703182602.0001): Bolt. Central Texas Aircraft Parts (CTAP) · PMA PQ0880SW · Replaces 232-20268-503 · May 17, 2024
- [GYR8A20AB](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID171129164020250128190839.0001): Rivet, Semi-Tubular. Aero Brake & Spares Inc · PMA PQ0694SW · Replaces GYR8A20 · Apr 3, 2024
- [232-20260-1HP](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID151555150120231024184828.0001): Bearing. Central Texas Aircraft Parts (CTAP) · PMA PQ0880SW · Replaces 232-20260-1 · Dec 22, 2022
- [232-20426-1HP](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID115863883220231024184809.0001): Bushing. Central Texas Aircraft Parts (CTAP) · PMA PQ0880SW · Replaces 232-20426-1 · Dec 22, 2022
- [232-20268-503HP](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID102760286420231024184823.0001): Bolt. Central Texas Aircraft Parts (CTAP) · PMA PQ0880SW · Replaces 232-20268-503 · Dec 22, 2022
- [121460-2-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID195005801520230907125102.0001): Shaft Assembly, Flexible. Honeywell International Inc. · PMA PQ1222NM · Replaces 121460-2-1 · Dec 7, 2022
- [121878-2](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID156304585120230907125106.0001): Rack Assembly, Gear. Honeywell International Inc. · PMA PQ1222NM · Replaces 121878-2 · Dec 7, 2022
- [121878-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID137840231220230907125105.0001): Rack Assembly, Gear. Honeywell International Inc. · PMA PQ1222NM · Replaces 121878-1 · Dec 7, 2022
- [52-2848-004](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID107059029420230907125111.0001): Fuel Filter. Honeywell International Inc. · PMA PQ1222NM · Replaces 52-2848-004 · Dec 7, 2022
- [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
- [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
- [443613-00](https://drs.faa.gov/browse/excelExternalWindow/FE732206F3742AAA86258560003BDD25.0001): Harness, 833613-00. Shadin Avionics · PMA PQ2088CE · Replaces 443613-00 · Jun 6, 2019
- [613603-00](https://drs.faa.gov/browse/excelExternalWindow/F474BD51883E678086258560003BDD89.0001): Bracket, AFID RA Mount. Shadin Avionics · PMA PQ2088CE · Replaces 613603-00 · Jun 6, 2019
- [833613-00](https://drs.faa.gov/browse/excelExternalWindow/E9293882A965D1D286258560003BDC47.0001): ADS-B Flight ID Adapter. Shadin Avionics · PMA PQ2088CE · Replaces 833613-00 · Jun 6, 2019
- [613604-00](https://drs.faa.gov/browse/excelExternalWindow/C99B32ED23A9740F86258560003BDDC9.0001): Bracket, AFID Side Mount. Shadin Avionics · PMA PQ2088CE · Replaces 613604-00 · Jun 6, 2019
- [833613-10](https://drs.faa.gov/browse/excelExternalWindow/99326314CB6EBE8F86258560003BDCEA.0001): Digital Discrete Adapter (DDA). Shadin Avionics · PMA PQ2088CE · Replaces 833613-10 · Jun 6, 2019
- [613606-00](https://drs.faa.gov/browse/excelExternalWindow/501E105EA0BF714E86258560003BDE36.0001): Bracket, AFID Under Mount. Shadin Avionics · PMA PQ2088CE · Replaces 613606-00 · Jun 6, 2019
- [443613-10](https://drs.faa.gov/browse/excelExternalWindow/313ABE429C4C505186258560003BDD5A.0001): Harness, DDA. Shadin Avionics · PMA PQ2088CE · Replaces 443613-10 · Jun 6, 2019
- [613605-00](https://drs.faa.gov/browse/excelExternalWindow/078709A82EB7C91386258560003BDDF9.0001): Bracket, AFID Top Mount. Shadin Avionics · PMA PQ2088CE · Replaces 613605-00 · Jun 6, 2019
- [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
- [833613-00](https://drs.faa.gov/browse/excelExternalWindow/B58F1D94BA606C32862580F4006A88EF.0001): ADS-B Flight ID Adapter. Shadin Avionics · PMA PQ2088CE · Replaces 833613-00 · Mar 13, 2017
- [613606-00](https://drs.faa.gov/browse/excelExternalWindow/A6441B538423DE94862580F4006A88FA.0001): Bracket, AFID Under Mount. Shadin Avionics · PMA PQ2088CE · Replaces 613606-00 · Mar 13, 2017
- [833613-10](https://drs.faa.gov/browse/excelExternalWindow/9CAB585FE78A04A7862580F4006A88F2.0001): Digital Discrete Adapter (DAA). Shadin Avionics · PMA PQ2088CE · Replaces 833613-10 · Mar 13, 2017
- [443613-00](https://drs.faa.gov/browse/excelExternalWindow/9460FF77F2A69542862580F4006A88F5.0001): Harness, 833613-00. Shadin Avionics · PMA PQ2088CE · Replaces 443613-00 · Mar 13, 2017
- [613605-00](https://drs.faa.gov/browse/excelExternalWindow/827B265784FF139D862580F4006A88F9.0001): Bracket, AFID Top Mount. Shadin Avionics · PMA PQ2088CE · Replaces 613605-00 · Mar 13, 2017
- [613603-00](https://drs.faa.gov/browse/excelExternalWindow/43E03A8C504EAD02862580F4006A88F7.0001): Bracket, AFID RA Mount. Shadin Avionics · PMA PQ2088CE · Replaces 613603-00 · Mar 13, 2017
- [613604-00](https://drs.faa.gov/browse/excelExternalWindow/3B805E8C35F6F339862580F4006A88F8.0001): Bracket, AFID Side Mount. Shadin Avionics · PMA PQ2088CE · Replaces 613604-00 · Mar 13, 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
- [DB1602009](https://drs.faa.gov/browse/excelExternalWindow/B4DE301424EF562A862580CE00749BFB.0001): DR Bracket DDA Mount Assembly. Nextant Aerospace LLC · PMA PQ04311CE · Modification part · Oct 4, 2016
- [DB1602009](https://drs.faa.gov/browse/excelExternalWindow/78DF8E71275000108625805E006A7289.0001): DR Bracket DDA Mount Assembly. Nextant Aerospace LLC · PMA PQ04311CE · Modification part · Oct 4, 2016
- [DB1602007](https://drs.faa.gov/browse/excelExternalWindow/50C9D29CF4D757928625805E006A735F.0001): Harness - ADS-B Out Wire Diagram. Nextant Aerospace LLC · PMA PQ04311CE · Modification part · Oct 4, 2016
- [DB1602007](https://drs.faa.gov/browse/excelExternalWindow/4E5A8D7E52324A07862580CE00749C01.0001): Harness - ADS-B Out Wire Diagram. Nextant Aerospace LLC · PMA PQ04311CE · Modification part · Oct 4, 2016
- [DB1602008](https://drs.faa.gov/browse/excelExternalWindow/3A0E9A6453136D27862580CE00749BFE.0001): L Bracket DDA Mount. Nextant Aerospace LLC · PMA PQ04311CE · Modification part · Oct 4, 2016
- [DB1602008](https://drs.faa.gov/browse/excelExternalWindow/2ABC1E9D44871DA38625805E006A730E.0001): L Bracket DDA Mount. Nextant Aerospace LLC · PMA PQ04311CE · Modification part · Oct 4, 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

All of them: https://openairdocs.org/model/sabreliner-na-265-80/pma.md

## The same model under other registry codes

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

- [North American NA-265-80](https://openairdocs.org/model/north-american-na-265-80): 1 registered aircraft, registry code 6402618
- [Rockwell International NA-265-80](https://openairdocs.org/model/rockwell-international-na-265-80): 1 registered aircraft, registry code 7630108

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