# Sabreliner NA-265-40 - Type: Aircraft model (FAA registry) - Registry code: 6403000 - Manufacturer (registry): SABRELINER CORP - Model: NA-265-40 - Aircraft type: Fixed wing multi engine - Category: Airplane - Engines: 2 · Turbo-jet - Seats: 9 - Weight class: 12,500 to 19,999 lb - 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-265-40 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 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 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 80-08-07](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 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 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 (55, newest 50) As reported by operators and repair stations, by the model named in the report. - [SDR C2XA06TY067](https://openairdocs.org/sdr/C2XA06TY067), Oct 12, 2006: BULKHEAD. CORRODED. TYS - DURING A CURRENT 2C INSPECTION THE VENTRAL TANK FWD BULKHEAD WAS FOUND CORRODED AT THE FUEL LINE SUPPORT BRACKET. MAINTENANCE CUT OUT THE EFFECTED AREA, F - [SDR 2003FA0000661](https://openairdocs.org/sdr/2003FA0000661), Jun 23, 2003: SELECTOR VALVE. FAILED. MAIN LANDING GEAR DOOR SELECTOR VALVE FAILED CAUSING MAIN GEAR FAIRING DOORS TO REMAIN OPEN. THE LANDING GEAR UN-SAFE LIGHT REMAINED ON WITH GEAR UP. WITH MAIN - [SDR 98ZZZX3632](https://openairdocs.org/sdr/98ZZZX3632), Aug 17, 1998: TRUNNION. CRACKED. DURING SCHEDULED INSPECTION, THE NOSE LANDING GEAR UPPER BARREL ASSY WAS FOUND WITH A CRACK COMPLETELY THROUGH THE RT TRUNNION PIN HOLE. THE TRUNNION/BEARING PI - [SDR 98ZZZX2725](https://openairdocs.org/sdr/98ZZZX2725), Jul 9, 1998: PIN. FAILED. THE CLIP THAT RETAINS THE DRAG CHUTE RETAINING PIN VIBRATES LOOSE WHEN CHUTE WAS DEPLOYED, IT DETACHED FROM THE AIRCRAFT. THE YOKE AND RETAINING PIN CAUGHT ON T - [SDR 98ZZZX481](https://openairdocs.org/sdr/98ZZZX481), Jan 19, 1998: LINE. LEAK. LINE INSTALLED AT NOSE STEERING ACTUATOR TO SWIVEL JOINT IN NOSE WHEELWELL. LINE STARTED TO LEAK AT POINT IN LINE WHERE LINE BENDS WHEN NLG ACTIVATED. - [SDR 97ZZZX3779](https://openairdocs.org/sdr/97ZZZX3779), Jul 28, 1997: REGULATOR. CORRODED. PART RECEIVED FROM SUPPLY WITH CORROSION ON TERMINAL ENDS. THESE ARE NEWLY OVERHAULED UNITS. SUBMITTER STATED THIS IS AN ONGOING PROBLEM, APPARENTLY, THIS AREA - [SDR 97ZZZX3778](https://openairdocs.org/sdr/97ZZZX3778), Jul 28, 1997: REGULATOR. CORRODED. PART RECEIVED FROM SUPPLY WITH CORROSION ON TERMINAL ENDS. THESE ARE NEWLY OVERHAULED UNITS. SUBMITTER STATED THIS IS AN ONGOING PROBLEM, APPARENTLY, THIS AREA - [SDR 97ZZZX3783](https://openairdocs.org/sdr/97ZZZX3783), Jul 17, 1997: PUMP. SEAL DAMAGED. HYDRAULIC PUMP WAS REMOVED AFTER 7.9 HOURS TIME IN SERVICE DUE TO SHAFT SEAL FAILURE AND EXCESSIVE FLUID LEAKAGE. PUMP, SN MX193803A, REJECTED FOR INSTALLATION - [SDR 97ZZZX3782](https://openairdocs.org/sdr/97ZZZX3782), Jul 17, 1997: PUMP. SEAL DAMAGED. HYDRAULIC PUMP WAS REMOVED AFTER 7.9 HOURS TIME IN SERVICE DUE TO SHAFT SEAL FAILURE AND EXCESSIVE FLUID LEAKAGE. PUMP, SN MX193803A, REJECTED FOR INSTALLATION - [SDR 97ZZZX2939](https://openairdocs.org/sdr/97ZZZX2939), Jun 5, 1997: LINE ASSY. CHAFED. DURING PYLON MATCHING ANGLES AND FUSELAGE SKIN INSPECTION, NOTED AN ADEL CLAMP, PN MS21919DG6, WAS BROKEN ON THE RIGHT HAND SIDE FS 367. FURTHER INSPECTION REVE - [SDR 96ZZZX5327](https://openairdocs.org/sdr/96ZZZX5327), Oct 4, 1996: BELLCRANK. CORRODED. SEVERELY CORRODED MAGNESIUM BELLCRANK PN 265-522130-3 WHICH OPERATES THE BIAS BUNGEE ELEVATOR TO STABILIZER LONGITUDINAL CONTROL. THIS UNIT IS LOCATED IN THE AF - [SDR 96ZZZX5326](https://openairdocs.org/sdr/96ZZZX5326), Oct 4, 1996: BELLCRANK. CORRODED. SEVERELY CORRODED MAGNESIUM BELLCRANK, PN 265-522130-3, WHICH OPERATES THE BIAS BUNGEE FOR ELEVATOR TO STABILIZER LONGITUDINAL CONTROL. THIS UNIT IS LCOATED IN - [SDR 96ZZZX5270](https://openairdocs.org/sdr/96ZZZX5270), Sep 30, 1996: BELLCRANK. CORRODED. SEVERELY CORRODED MAGNESIUM BELLCRANK WHICH OPERATES THE BIAS BUNGEE FOR ELEVATOR TO STABILIZER LONGITUDINAL CONTROL. THIS UNIT IS LOCATED IN THE AFT LOWER LEFT - [SDR 96ZZZX5272](https://openairdocs.org/sdr/96ZZZX5272), Sep 27, 1996: CONTROL CABLE. CORRODED. LOWER AFT ELEV CONTROL CABLE FS 388 TO FS 457 SHOWED SIGNS OF CORROSION ON UPPER SURFACE 'ONLY' JUST AFT OF THE FIBERGLASS PROTECTIVE CABLE SHROUD PN 265-540425 - [SDR 96ZZZX5274](https://openairdocs.org/sdr/96ZZZX5274), Sep 26, 1996: CONTROL CABLE. CORRODED. LOWER AFT ELEV CONTROL CABLE FS 388 TO FS 457 SHOWED SIGNS OF CORROSION ON UPPER SURFACE 'ONLY' JUST AFT OF FIBERGLASS PROTECTIVE CABLE SHROUD PN 265-540425-37, - [SDR 96ZZZX5273](https://openairdocs.org/sdr/96ZZZX5273), Sep 25, 1996: BELLCRANK. CORRODED. SEVERELY CORRODED MAGNESIUM BELLCRANK WHICH OPERATES THE BIAS BUNGEE FOR ELEVATOR TO STABILIZER LOCATED IN AFT LOWER LEFT SIDE OF FS 457. VISUAL INSPECTION IS V - [SDR 96ZZZX5271](https://openairdocs.org/sdr/96ZZZX5271), Sep 24, 1996: CONTROL CABLE. CORRODED. LOWER AFT ELEV CONTROL CABLE FS 388 TO FS 457 SHOWED SIGNS OF CORROSION ON UPPER SURFACE 'ONLY' JUST AFT OF FIBERGLASS PROTECTIVE CABLE SHROUD PN 265-540425-37 - [SDR 96ZZZX5144](https://openairdocs.org/sdr/96ZZZX5144), Sep 24, 1996: CONTROL CABLE. BROKEN. LOWER AFT ELEVATOR CONTROL CABLE FS 388 TO FS 457, SHOWED SIGNS OF CORROSION ON UPPER SURFACE 'ONLY' JUST AFT OF FIBERGLASS PROTECTIVE CABLE SHROUD PN 265-54042 - [SDR 96ZZZX5145](https://openairdocs.org/sdr/96ZZZX5145), Sep 23, 1996: CONTROL CABLE. FRAYED. LOWER AFT ELEVATOR CONTROL CABLE FS 388 TO FS 457, SHOWED SIGNS OF CORROSION ON UPPER SURFACE 'ONLY' JUST AFT OF FIBERGLASS PROTECTIVE CABLE SHROUD PN 265-54042 - [SDR 96ZZZX5142](https://openairdocs.org/sdr/96ZZZX5142), Sep 23, 1996: CONTROL CABLE. FRAYED. LOWER AFT ELEVATOR CONTROL CABLE, FS 388 TO FS 457, SHOWED SIGNS OF CORROSION ON UPPER SURFACE 'ONLY' JUST AFT OF THE FIBERGLASS PROTECTIVE CABLE SHROUD PN 265- - [SDR 96ZZZX4331](https://openairdocs.org/sdr/96ZZZX4331), Aug 8, 1996: COMPRESSOR. BINDING. COMPRESSOR VERY DIFFICULT TO ROTATE, IINTERNAL BINDING COULD BE FELT WHEN ROTATING BY HAND WITH SHORT SPOOL DOWN TIME. NO FOD NOTED, NO DAMAGE OR VISUAL DEFECTS - [SDR 96ZZZX4332](https://openairdocs.org/sdr/96ZZZX4332), Aug 7, 1996: ACTUATOR. LEAK. ACTUATOR WAS INSTALLED ON THE AIRCRAFT, OPERATIONALLY CHECKED, AND REMOVED DUE TO LEAKAGE THROUGH A HOLE (OR CRACK) IN THE ACTUATOR CYLINDER (BARREL) WALL. THE - [SDR 96ZZZX4385](https://openairdocs.org/sdr/96ZZZX4385), Aug 6, 1996: POWER SUPPLY. FAILED. STROBE POWER SUPPLY WAS INSTALLED IN THE AIRCRAFT, OPERATED FOR 25 HOURS, AND WAS REMOVED FOR INTERNAL FAILURE WITH NO POWER OUTPUT. UNIT WAS OVERHAULED ON 10-1 - [SDR 96ZZZX3905](https://openairdocs.org/sdr/96ZZZX3905), Jul 25, 1996: PUMP. SEAL FAILED. HYDRAULIC PUMP SHAFT SEAL FAILURE IN-FLIGHT 'WITHOUT INCIDENT', BUT ELECTRIC DRIVE MOTOR AND SURROUNDING AFT FUSELAGE AREA TO TAIL WAS SATURATED WITH APPROXIMAT - [SDR 96ZZZX4135](https://openairdocs.org/sdr/96ZZZX4135), Jul 22, 1996: VALVE. FAILED. AIRCRAFT WAS INITIALLY EXPERIENCING LANDING GEAR OPERATION PROBLEMS. PROBLEM WAS TROUBLESHOT TO A BAD LANDING GEAR HYDRAULIC CONTROL VALVE. REQUIRED A REPAIRED - [SDR 96ZZZX4033](https://openairdocs.org/sdr/96ZZZX4033), Jul 17, 1996: TRANSDUCER. FAILED. UNIT WAS INSTALLED IN THE AIRCRAFT, TESTED, AND FOUND TO BE INOPERATIVE. UNIT WAS TESTED AGAIN (IN OPPOSITE POSITION ON SAME AIRCRAFT) AND WAS STILL INOPERABLE. - [SDR 96ZZZX3906](https://openairdocs.org/sdr/96ZZZX3906), Jul 10, 1996: COMPRESSOR. BINDING. COMPRESSOR VERY DIFFICULT TO ROTATE AND SPOOL DOWN VERY SHORT. INTERNAL BINDING COULD BE FELT WHEN ROTATING BY HAND. THIS IS A MULTI-STAGE UNIT, SO VISUAL INSPE - [SDR 96ZZZX4166](https://openairdocs.org/sdr/96ZZZX4166), Jun 28, 1996: SENSOR. INOPERATIVE. RECEIVING INSPECTION CONDUCTED BY RAYTHON AEROSPACE. THERE IS 'NO WAY' THAT THIS NR 7 FUEL QUANTITY TANK UNIT COULD HAVE BEEN BENCH CHECKED/FUNCTIONAL TESTED. R - [SDR 96ZZZX4034](https://openairdocs.org/sdr/96ZZZX4034), Jun 21, 1996: COMPRESSOR. BINDING. COMPRESSOR VERY DIFFICULT TO ROTATE AND SPOOL DOWN VERY SHORT. INTERNAL BINDING COULD BE FELT WHEN ROTATING BY HAND. THIS IS A MULTI 9-STAGE UNIT, SO VISUAL INS - [SDR 96ZZZX4035](https://openairdocs.org/sdr/96ZZZX4035), Jun 14, 1996: COMPRESSOR. BINDING. COMPRESSOR VERY DIFFICULT TO ROTATE AND SPOOL DOWN VERY SHORT. INTERNAL BINDING COULD BE FELT WHEN ROATING BY HAND. THIS IS A MULTI 9-STAGE UNIT, SO VISUAL INSP - [SDR 96ZZZX3523](https://openairdocs.org/sdr/96ZZZX3523), Jun 11, 1996: COMPRESSOR. BINDING. COMPRESSOR VERY DIFFICULT TO ROTATE AND SPOOL DOWN VERY SHORT. INTERNAL BINDING COULD BE FELT WHEN ROTATING BY HAND. THIS IS A MULTI-STAGE UNIT, SO VISUAL INSPE - [SDR 96ZZZX3016](https://openairdocs.org/sdr/96ZZZX3016), May 14, 1996: TRANSDUCER. FAILED. TRANSDUCER WAS INSTALLED IN THE AIRCRAFT, TESTED, AND REMOVED WITH ZERO HOURS SINCE OVERHAUL. UNIT WAS REMOVED DUE TO EPR INDICATION WOULD STICK AT 2.0 AND WOUL - [SDR 96ZZZX3051](https://openairdocs.org/sdr/96ZZZX3051), May 13, 1996: BLADE. BROKEN. SECOND STAGE TURBINE ROTOR BLADE FAILURE IN-FLIGHT, WITHOUT INCIDENT. ENGINE TT, 11,164.7 HRS, CYCLES, 8,081, TSO, 330.9 HRS, TTHSI, 330.9 HRS, TOTAL PART TIME - [SDR 96ZZZX3050](https://openairdocs.org/sdr/96ZZZX3050), May 13, 1996: PUMP. FAILED. UNIT FAILED IN-FLIGHT WITHOUT INCIDENT, SUSPECT INTERNAL MOTOR BRUSH OR COMMUTATOR FAILURE. UNIT OVERHAULED. - [SDR 96ZZZX2638](https://openairdocs.org/sdr/96ZZZX2638), May 7, 1996: PUMP. SEAL FAILED. PUMP WAS INSTALLED, TEST RUN FOR 30 SECONDS, AND REMOVED WITH ZERO HOURS TIME IN SERVICE SINCE OVERHAUL. PUMP WAS REMOVED DUE TO SHAFT SEAL FAILED WHICH PUMPED - [SDR 96ZZZX3052](https://openairdocs.org/sdr/96ZZZX3052), May 6, 1996: O-RING. MISSING. WHEEL ASSY OVERHAULED 4-11-96. UNITS FUSIBLE PLUG O-RING, PN 9524796, NOT REPLACED DURING OVERHAUL. - [SDR 96ZZZX3049](https://openairdocs.org/sdr/96ZZZX3049), May 6, 1996: O-RING. MISSING. WHEEL ASSY OVERHAULED 4-5-96. UNITS FUSIBLE PLUG O-RING NOT REPLACED DURING OVERHAUL. - [SDR 96ZZZX3017](https://openairdocs.org/sdr/96ZZZX3017), May 3, 1996: BEACON ASSY. FAILED. BEACON WAS REMOVED FROM SERVICE WITH 27.0 HRS SINCE OVERHAUL DUE TO WOULD NOT ROTATE. UNIT WAS OVERHAULED BY REPAIR STATION. SUBMITTER STATED RELIABILITY OF REP - [SDR 96ZZZX3823](https://openairdocs.org/sdr/96ZZZX3823), Apr 8, 1996: TURBINE. FAILED. CLIMBING THROUGH 5,000 FEET, THE CREW HEARD AND FELT A LOUD REPORT FOLLOWED IMMEDIATELY BY THE LT ENGINE FIRE WARNING LIGHT. THE LT ENGINE SPEED ROLLED BACK TO - [SDR 96ZZZX1962](https://openairdocs.org/sdr/96ZZZX1962), Apr 1, 1996: TRANSDUCERS. ERRATIC. TRANSDUCER WAS INSTALLED IN AIRCRAFT, TESTED DURING GROUND RUN, AND REMOVED WITH ZERO HOURS TIME IN SERVICE SINCE OVERHAUL. E.P.R. READINGS WERE ERRATIC IN ALL - [SDR 96ZZZX1964](https://openairdocs.org/sdr/96ZZZX1964), Mar 25, 1996: PUMP. FAILED. PUMP WAS REMOVED AND REPLACED DUE TO AFTER SEVERAL MINUTES OF OPERATION, PUMP BECAME EXTREMELY NOISY AND ROUGH INDICATING A POSSIBLE IMPENDING FAILURE. TIME IN - [SDR 96ZZZX831](https://openairdocs.org/sdr/96ZZZX831), Jan 5, 1996: SEAT ASSY. WELD BROKEN. PILOT'S SEAT WOULD NOT ADJUST FORWARD AND AFT OR VERTICALLY, AND SEAT WOULD NOT SIT LEVEL. INSPECTION FOUND SEAT STRUCTURAL MEMBERS (WELD ASSYS) BROKEN AT WELDE - [SDR 96ZZZX830](https://openairdocs.org/sdr/96ZZZX830), Jan 5, 1996: SEAT ASSY. WELD BROKEN. PILOT'S SEAT WOULD NOT ADJUST FORWARD AND AFT OR VERTICALLY, AND SEAT WOULD NOT SIT LEVEL. INSPECTION FOUND SEAT STRUCTURAL MEMBERS (WELD ASSYS) BROKEN AT WELDE - [SDR 96ZZZX763](https://openairdocs.org/sdr/96ZZZX763), Dec 14, 1995: VANE. DEBONDED. UNDER NORMAL OPERATING CONDITIONS, THE PROTECTIVE COATING IS DEBONDING FROM THE SURFACE OF NEW VANES. DEFECT WAS FOUND BY BORESCOPING THE ENGINE. - [SDR 96ZZZX750](https://openairdocs.org/sdr/96ZZZX750), Dec 14, 1995: VANE. DEBONDING. UNDER NORMAL OPERATING CONDITIONS, THE PROTECTIVE COATING IS DEBONDING FROM THE SURFACE (LEADING EDGE) OF NEW VANES. DEFECT WAS FOUND BY BORESCOPING THE ENGINE. - [SDR 95ZZZX6606](https://openairdocs.org/sdr/95ZZZX6606), Nov 6, 1995: PUMP. DEFECTIVE. THIS BOOST PUMP WAS RECEIVED FROM THE VENDOR WITH A FRESH OVERHAUL. ON OPS CHECK, THE PUMP HAD A RUBBING NOISE. THE SCREEN WAS REMOVED AND THE IMPELLER WAS FOUN - [SDR 95ZZZX6605](https://openairdocs.org/sdr/95ZZZX6605), Nov 6, 1995: PUMP. FAILED. BOOST PUMP CAUSES CIRCUIT BREAKER TO TRIP IN-FLIGHT. SUSPECT CAUSE, INTERNAL SHORT OR BAD BEARINGS. - [SDR 95ZZZX6604](https://openairdocs.org/sdr/95ZZZX6604), Nov 6, 1995: PUMP. SHORTED. BOOST PUMP CAUSES CIRCUIT BREAKER TO TRIP IN-FLIGHT. SUSPECT INTERNAL SHORT OR BAD BEARINGS. - [SDR 95ZZZX5545](https://openairdocs.org/sdr/95ZZZX5545), Sep 14, 1995: PUMP. FAILURE. PUMP WAS REMOVED FROM AIRCRAFT WITH 5.6 HOURS TIME IN SERVICE SINCE OVERHAUL DUE TO PUMP CAUSED CIRCUIT BREAKER TO TRIP AND WOULD NOT RESET. UNIT WAS OVERHAULED - [SDR 95ZZZX5546](https://openairdocs.org/sdr/95ZZZX5546), Sep 13, 1995: PUMP. FAILED. PUMP WAS REMOVED FROM AIRCRAFT WITH 52.0 HOURS TIME IN SERVICE SINCE OVERHAUL DUE TO INTERNAL FAILURE CAUSING BOOST PUMP CIRCUIT BREAKER TO TRIP AND WOULD NOT R All 55: https://openairdocs.org/model/sabreliner-na-265-40/reports.md ## STCs that may be installed (OpenAirDocs) (168, 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 SA1963SW](https://openairdocs.org/stc/SA1963SW): Installation of Monogram Toilet. 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 SA244CE](https://openairdocs.org/stc/SA244CE): Electronics components package version F. Sabreliner Aviation LLC - [STC SA1057CE](https://openairdocs.org/stc/SA1057CE): Installation of electronic components package, version Z. Sabreliner Aviation LLC - [STC SA1162CE](https://openairdocs.org/stc/SA1162CE): Installation of P & D valve fuel reservoir drain. Sabreliner Aviation LLC - [STC SA1338CE](https://openairdocs.org/stc/SA1338CE): Installation of Global GNS-500A VLF/Omega navigation system. Sabreliner Aviation LLC - [STC SA1365CE](https://openairdocs.org/stc/SA1365CE): Installation of Compensated Pitot Static Heads (Rosemount Engineering). Sabreliner Aviation LLC - [STC SA1374SW](https://openairdocs.org/stc/SA1374SW): Installation of avionics system. Sabreliner Aviation LLC - [STC SA1375SW](https://openairdocs.org/stc/SA1375SW): Installation of 8-place cabin interior arrangement, Version No. 9. Sabreliner Aviation LLC - [STC SA139CE](https://openairdocs.org/stc/SA139CE): General interior configuration, 7 place. Sabreliner Aviation LLC - [STC SA140CE](https://openairdocs.org/stc/SA140CE): Reclining passenger seat installation (Tpy). Sabreliner Aviation LLC - [STC SA141CE](https://openairdocs.org/stc/SA141CE): Swivel reclining passenger seat installation (Typ). Sabreliner Aviation LLC - [STC SA1429CE](https://openairdocs.org/stc/SA1429CE): Removal of fuel jettisoning provisions. Sabreliner Aviation LLC - [STC SA142CE](https://openairdocs.org/stc/SA142CE): passenger couch installation, Two place. Sabreliner Aviation LLC - [STC SA143CE](https://openairdocs.org/stc/SA143CE): Crew and passenger oxygen system installation. Sabreliner Aviation LLC - [STC SA1492SW](https://openairdocs.org/stc/SA1492SW): Interior installation. Sabreliner Aviation LLC - [STC SA1671CE](https://openairdocs.org/stc/SA1671CE): Interior installation. Sabreliner Aviation LLC - [STC SA1674CE](https://openairdocs.org/stc/SA1674CE): Installation of modernized avionics. Sabreliner Aviation LLC - [STC SA1679CE](https://openairdocs.org/stc/SA1679CE): Installation of modernized avionics. Sabreliner Aviation LLC - [STC SA1680CE](https://openairdocs.org/stc/SA1680CE): FAA airways checker interior installation. Sabreliner Aviation LLC - [STC SA171CE](https://openairdocs.org/stc/SA171CE): General Interior Configuration, Eight-Place, Version #2. Sabreliner Aviation LLC - [STC SA172CE](https://openairdocs.org/stc/SA172CE): Two-Place Passenger Seat Installation (Typ). Sabreliner Aviation LLC - [STC SA1730CE](https://openairdocs.org/stc/SA1730CE): Installation of Collins FMS-90 Flight Management System, Dual Collins DME-40 System and Second Collins 590A-301 Air Data System. Sabreliner Aviation LLC - [STC SA173CE](https://openairdocs.org/stc/SA173CE): Electronics Component Package, Version A. Sabreliner Aviation LLC - [STC SA181CE](https://openairdocs.org/stc/SA181CE): Two place passenger/baggage seat. Sabreliner Aviation LLC - [STC SA1910CE](https://openairdocs.org/stc/SA1910CE): Increase maximum zero fuel weight to 13,300 lbs. 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 SA204CE](https://openairdocs.org/stc/SA204CE): General Interior Configuration, Nine-Place - Version #4. Sabreliner Aviation LLC - [STC SA205CE](https://openairdocs.org/stc/SA205CE): Hand Baggage Rack Installation - STA 147-206. Sabreliner Aviation LLC - [STC SA206CE](https://openairdocs.org/stc/SA206CE): Auxiliary Passenger Seat Installation - STA 194. 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 SA2155CE](https://openairdocs.org/stc/SA2155CE): Installation of single Sperry Corp. electronic flight instrument system (EFIS) EDZ-601. Sabreliner Aviation LLC - [STC SA2160CE](https://openairdocs.org/stc/SA2160CE): Installation of Teledyne angle of attack system. 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 SA219CE](https://openairdocs.org/stc/SA219CE): Electronics Component Package, Version E. Sabreliner Aviation LLC All 168: https://openairdocs.org/model/sabreliner-na-265-40/stcs.md ## PMA parts (OpenAirDocs) (272, 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 - [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 - [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 - [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 - [7000-911521](https://drs.faa.gov/browse/excelExternalWindow/74F1F5A1D072E9C886257BC70056A769.0001): Check Valve. Aero Fluid Products · PMA PQ2093CE · Replaces Saberliner P/N 370-870008-3 · Jul 23, 2013 - [26S-7D5017-01](https://drs.faa.gov/browse/excelExternalWindow/F9412885C73FC85786257B48006FBEF3.0001): 1st Slat De-icer, LH. Goodrich Sensors and Integrated Systems · PMA PQ0822NE · Replaces Goodrich P/N 26S-7D5017-01 · Apr 8, 2013 - [26S-7D5017-03](https://drs.faa.gov/browse/excelExternalWindow/F9028AC181514F1F86257B48006FBEFA.0001): 2nd Slat De-icer, LH. Goodrich Sensors and Integrated Systems · PMA PQ0822NE · Replaces Goodrich P/N 26S-7D5017-03 · Apr 8, 2013 - [26S-7D5017-11](https://drs.faa.gov/browse/excelExternalWindow/EAF3BE9A6159B9DF86257B48006FBF0C.0001): Fuselage-to-Slat De-icer, LH. Goodrich Sensors and Integrated Systems · PMA PQ0822NE · Replaces Goodrich P/N 26S-7D5017-11 · Apr 8, 2013 - [26S-7D5017-16](https://drs.faa.gov/browse/excelExternalWindow/E2B7CBBF9B17C03886257B48006FBF15.0001): Outboard Underwing De-icer, RH. Goodrich Sensors and Integrated Systems · PMA PQ0822NE · Replaces Goodrich P/N 26S-7D5017-16 · Apr 8, 2013 - [26S-7D5017-12](https://drs.faa.gov/browse/excelExternalWindow/E1489390CC63BF4986257B48006FBF0D.0001): Fuselage-to-Slat De-icer, RH. Goodrich Sensors and Integrated Systems · PMA PQ0822NE · Replaces Goodrich P/N 26S-7D5017-12 · Apr 8, 2013 - [26S-7D5017-04](https://drs.faa.gov/browse/excelExternalWindow/D7F0644A8B256C0286257B48006FBEFC.0001): 2nd Slat De-icer, RH. Goodrich Sensors and Integrated Systems · PMA PQ0822NE · Replaces Goodrich P/N 26S-7D5017-04 · Apr 8, 2013 - [25S-7D5017-18](https://drs.faa.gov/browse/excelExternalWindow/D16B1895F4AFA71B86257B48006FBF18.0001): Horizontal Stabilizer De-icer, RH. Goodrich Sensors and Integrated Systems · PMA PQ0822NE · Replaces Goodrich P/N 25S-7D5017-18 · Apr 8, 2013 - [25S-7D5017-20](https://drs.faa.gov/browse/excelExternalWindow/CD2356C9770CC9A986257B48006FBF1B.0001): Upper Vertical Fin Stabilizer De-icer. Goodrich Sensors and Integrated Systems · PMA PQ0822NE · Replaces Goodrich P/N 25S-7D5017-20 · Apr 8, 2013 - [25S-7D5017-17](https://drs.faa.gov/browse/excelExternalWindow/BC251A576191430886257B48006FBF17.0001): Horizontal Stabilizer De-icer, LH. Goodrich Sensors and Integrated Systems · PMA PQ0822NE · Replaces Goodrich P/N 25S-7D5017-17 · Apr 8, 2013 - [26S-7D5017-14](https://drs.faa.gov/browse/excelExternalWindow/B3D0D120C27A51A086257B48006FBF12.0001): Inboard Underwing De-icer, RH. Goodrich Sensors and Integrated Systems · PMA PQ0822NE · Replaces Goodrich P/N 26S-7D5017-14 · Apr 8, 2013 - [26S-7D5017-10](https://drs.faa.gov/browse/excelExternalWindow/9643F0173C929DA486257B48006FBF09.0001): 5th Slat De-icer, RH. Goodrich Sensors and Integrated Systems · PMA PQ0822NE · Replaces Goodrich P/N 26S-7D5017-10 · Apr 8, 2013 - [25S-7D5017-19](https://drs.faa.gov/browse/excelExternalWindow/5E3FE3FE5D39D35A86257B48006FBF1A.0001): Lower Vertical Fin Stabilizer De-icer. Goodrich Sensors and Integrated Systems · PMA PQ0822NE · Replaces Goodrich P/N 25S-7D5017-19 · Apr 8, 2013 All of them: https://openairdocs.org/model/sabreliner-na-265-40/pma.md ## The same model under other registry codes Amateur-built copies and renamed makers get their own codes. - [North American NA-265-40](https://openairdocs.org/model/north-american-na-265-40): 6 registered aircraft, registry code 6402608 - [Rockwell International NA-265-40](https://openairdocs.org/model/rockwell-international-na-265-40): 1 registered aircraft, registry code 7630104 - [North American Rockwell NA-265-40](https://openairdocs.org/model/north-american-rockwell-na-265-40): 0 registered aircraft, registry code 6402609 --- 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.