# Rockwell International NA-265-65

- Type: Aircraft model (FAA registry)
- Registry code: 7630107
- Manufacturer (registry): ROCKWELL INTERNATIONAL CORP
- Model: NA-265-65
- 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: 26
- Page: https://openairdocs.org/model/rockwell-international-na-265-65

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 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 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 95-26-15 R1](https://openairdocs.org/ad/95-26-15-R1): Traffic Alert and Collision Avoidance Systems · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 159 more. Effective Dec 26, 1996
- [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 82-27-10](https://openairdocs.org/ad/82-27-10): Horizontal Stabilizer Trim Actuator · Sabreliner NA-265-65. Effective Jan 19, 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 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 75-04-05](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 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 (26)

- [N173A](https://openairdocs.org/aircraft/N173A): [Bae Systems Technology Solutions & Services Inc](https://openairdocs.org/faa-owner/BAE%20SYSTEMS%20TECHNOLOGY%20SOLUTIONS%20%26%20SERVICES%20INC), [Mojave, CA](https://openairdocs.org/faa-place/CA/Mojave), built 1980, S/N 465-20
- [N247CS](https://openairdocs.org/aircraft/N247CS): [Team Aero LLC](https://openairdocs.org/faa-owner/TEAM%20AERO%20LLC), [Shawnee, KS](https://openairdocs.org/faa-place/KS/Shawnee), built 1994, S/N 465-27
- [N265FT](https://openairdocs.org/aircraft/N265FT): [Sunshine Aero Industries Inc](https://openairdocs.org/faa-owner/SUNSHINE%20AERO%20INDUSTRIES%20INC), [Crestview, FL](https://openairdocs.org/faa-place/FL/Crestview), built 1980, S/N 465-46
- [N265WS](https://openairdocs.org/aircraft/N265WS): [Portside Aero LLC](https://openairdocs.org/faa-owner/PORTSIDE%20AERO%20LLC), [Edgewater, NJ](https://openairdocs.org/faa-place/NJ/Edgewater), built 1981, S/N 465-62
- [N33TR](https://openairdocs.org/aircraft/N33TR): [Airborne Holdings Inc](https://openairdocs.org/faa-owner/AIRBORNE%20HOLDINGS%20INC), [Midlothian, TX](https://openairdocs.org/faa-place/TX/Midlothian), built 1980, S/N 465-47
- [N376D](https://openairdocs.org/aircraft/N376D): [Bae Systems Tss Inc](https://openairdocs.org/faa-owner/BAE%20SYSTEMS%20TSS%20INC), [Mojave, CA](https://openairdocs.org/faa-place/CA/Mojave), built 1981, S/N 465-76
- [N47SE](https://openairdocs.org/aircraft/N47SE): [Highlands Group LLC](https://openairdocs.org/faa-owner/HIGHLANDS%20GROUP%20LLC), [Lahaina, HI](https://openairdocs.org/faa-place/HI/Lahaina), S/N 465-34
- [N499NH](https://openairdocs.org/aircraft/N499NH): [Haws Aviation LLC](https://openairdocs.org/faa-owner/HAWS%20AVIATION%20LLC), [Huntsville, AL](https://openairdocs.org/faa-place/AL/Huntsville), built 1981, S/N 465-56
- [N58HT](https://openairdocs.org/aircraft/N58HT): [American Air Charter Inc](https://openairdocs.org/faa-owner/AMERICAN%20AIR%20CHARTER%20INC), [Chesterfield, MO](https://openairdocs.org/faa-place/MO/Chesterfield), built 1981, S/N 465-70
- [N603AW](https://openairdocs.org/aircraft/N603AW): [National Test Pilot School](https://openairdocs.org/faa-owner/NATIONAL%20TEST%20PILOT%20SCHOOL), [Mojave, CA](https://openairdocs.org/faa-place/CA/Mojave), built 1981, S/N 46572
- [N651MK](https://openairdocs.org/aircraft/N651MK): [Maxfly Aviation Inc](https://openairdocs.org/faa-owner/MAXFLY%20AVIATION%20INC), [Fort Lauderdale, FL](https://openairdocs.org/faa-place/FL/Fort%20Lauderdale), built 1981, S/N 465-73
- [N654YS](https://openairdocs.org/aircraft/N654YS): built 1981, S/N 465-60
- [N65BT](https://openairdocs.org/aircraft/N65BT): [Dodson International Parts Inc](https://openairdocs.org/faa-owner/DODSON%20INTERNATIONAL%20PARTS%20INC), [Rantoul, KS](https://openairdocs.org/faa-place/KS/Rantoul), built 1979, S/N 465-3
- [N65ML](https://openairdocs.org/aircraft/N65ML): [Bae Systems Technology Solutions & Services Inc](https://openairdocs.org/faa-owner/BAE%20SYSTEMS%20TECHNOLOGY%20SOLUTIONS%20%26%20SERVICES%20INC), [Mojave, CA](https://openairdocs.org/faa-place/CA/Mojave), built 1981, S/N 465-69
- [N66GE](https://openairdocs.org/aircraft/N66GE): [Sunshine Aero Industries Inc](https://openairdocs.org/faa-owner/SUNSHINE%20AERO%20INDUSTRIES%20INC), [Crestview, FL](https://openairdocs.org/faa-place/FL/Crestview), built 1980, S/N 465-28
- [N697US](https://openairdocs.org/aircraft/N697US): [Alanis Armando Jr](https://openairdocs.org/faa-owner/ALANIS%20ARMANDO%20JR), [Mcallen, TX](https://openairdocs.org/faa-place/TX/Mcallen), built 1980, S/N 465-49
- [N700JC](https://openairdocs.org/aircraft/N700JC): [Salameh Aviation LLC](https://openairdocs.org/faa-owner/SALAMEH%20AVIATION%20LLC), [Bethlehem, PA](https://openairdocs.org/faa-place/PA/Bethlehem), built 1981, S/N 465-74
- [N701FW](https://openairdocs.org/aircraft/N701FW): [Dodson International Parts Inc](https://openairdocs.org/faa-owner/DODSON%20INTERNATIONAL%20PARTS%20INC), [Rantoul, KS](https://openairdocs.org/faa-place/KS/Rantoul), S/N 465-21, First renewal notice
- [N70SK](https://openairdocs.org/aircraft/N70SK): [Dylan Dublin Air LLC](https://openairdocs.org/faa-owner/DYLAN%20DUBLIN%20AIR%20LLC), [Hobe Sound, FL](https://openairdocs.org/faa-place/FL/Hobe%20Sound), built 1980, S/N 465-33
- [N75VC](https://openairdocs.org/aircraft/N75VC): [Sunshine Aero Industries Inc](https://openairdocs.org/faa-owner/SUNSHINE%20AERO%20INDUSTRIES%20INC), [Crestview, FL](https://openairdocs.org/faa-place/FL/Crestview), built 1981, S/N 465-71
- [N77GU](https://openairdocs.org/aircraft/N77GU): [Flying Colors Airparts Inc](https://openairdocs.org/faa-owner/FLYING%20COLORS%20AIRPARTS%20INC), [Leesburg, FL](https://openairdocs.org/faa-place/FL/Leesburg), built 1979, S/N 46512
- [N799MW](https://openairdocs.org/aircraft/N799MW): [Sabre 42 Inc](https://openairdocs.org/faa-owner/SABRE%2042%20INC), [Lewes, DE](https://openairdocs.org/faa-place/DE/Lewes), built 1980, S/N 465-42
- [N850CC](https://openairdocs.org/aircraft/N850CC): [Sunshine Aero Industries Inc](https://openairdocs.org/faa-owner/SUNSHINE%20AERO%20INDUSTRIES%20INC), [Crestview, FL](https://openairdocs.org/faa-place/FL/Crestview), built 1980, S/N 465-38
- [N888UP](https://openairdocs.org/aircraft/N888UP): [Team Aero LLC](https://openairdocs.org/faa-owner/TEAM%20AERO%20LLC), [Shawnee, KS](https://openairdocs.org/faa-place/KS/Shawnee), built 1981, S/N 465-68
- [N936JL](https://openairdocs.org/aircraft/N936JL): [Concrete Structures LLC](https://openairdocs.org/faa-owner/CONCRETE%20STRUCTURES%20LLC), [Jupiter, FL](https://openairdocs.org/faa-place/FL/Jupiter), built 1980, S/N 465-43
- [N964C](https://openairdocs.org/aircraft/N964C): [National Test Pilot School](https://openairdocs.org/faa-owner/NATIONAL%20TEST%20PILOT%20SCHOOL), [Mojave, CA](https://openairdocs.org/faa-place/CA/Mojave), built 1981, S/N 465-66

## NTSB investigations (5)

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 CEN19FA119](https://openairdocs.org/ntsb/CEN19FA119), Apr 13, 2019: Rockwell International NA-265-65 (N265DS), New Albany, MS, destroyed, 3 fatal. Probable cause: An unidentified electrical system malfunction that led to the pilots losing awareness of the airplane's performance in instrument meteorological conditions and resulted in a loss of control of the…
- [NTSB DEN08LA011](https://openairdocs.org/ntsb/DEN08LA011), Oct 15, 2007: North American NA-265-65 (N65BT), New Century, KS, substantial damage. Probable cause: The pilot's failure to maintain directional control. Contributing factors in this accident were the sudden wind shift, from calm to a gusty crosswind, the runway light, and the concrete pad.
- [NTSB LAX00FA191](https://openairdocs.org/ntsb/LAX00FA191), May 11, 2000: Rockwell NA-265-65 (N241H), Kaunakakai, HI, destroyed, 6 fatal. Probable cause: Inadequate crew coordination led to the captain's decision to discontinue the instrument approach procedure and initiate a maneuvering descent solely by visual references at night in an area of…
- [NTSB SEA00LA026](https://openairdocs.org/ntsb/SEA00LA026), Nov 30, 1999: Rockwell NA-265-65 (N920DY), Seattle, WA, substantial damage. Probable cause: Inadequate visual lookout and clearance was not maintained. Diverted attention, dark night conditions and rain were factors.
- [NTSB LAX98IA158](https://openairdocs.org/ntsb/LAX98IA158), May 10, 1998: North American NA265-65 (N651MK), Palm Springs, CA, incident, minor damage. Probable cause: the fatigue failure and uncontained separation of the high pressure impeller in the No. 2 engine during the takeoff roll. While the impeller showed evidence of a subsurface fatigue origin, the…

## 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 20240505004519I](https://openairdocs.org/incident/20240505004519I), May 5, 2024: Rockwell International Corp NA-265-65 (N265FT), Mobile, AL, Minor damage. Enroute to ktus at cruise altitude crew advised ATC of a cracked windshield and requested to return direct to kcew. The aircraft landed safely at kcew.
- [Incident 20210501007969I](https://openairdocs.org/incident/20210501007969I), May 1, 2021: Rockwell International Corp NA-265-65 (N799MW), Fort Lauderdale, FL, Minor damage. Aircraft N799MW saberliner landed runway 9 at approximately 1900 with two pilots onboard from toledo, Ohio to fxe. After landing, the pilot reported a steering…
- [Incident 20190626008099I](https://openairdocs.org/incident/20190626008099I), Jun 26, 2019: Rockwell International Corp NA-265-65 (N65HH), Mcclellan, CA, Minor damage. Right main landing gear safe indicator failed to illuminate when gear handle was selected down. Pilot had visual indication gear was down from ground crew and…
- [Incident 20190424003379I](https://openairdocs.org/incident/20190424003379I), Apr 24, 2019: Rockwell International Corp NA-265-65 (N799MW), Fort Lauderdale, FL, No damage. Flight from fxe to mgbt. Hydraulic system failure at FL 330 while leveling off after departure. Crew reported emergency to ATC and chose to land at fll due to…
- [Accident 20190413002749A](https://openairdocs.org/incident/20190413002749A), Apr 13, 2019: Rockwell International Corp NA-265-65 (N265DS), New Albany, MS, Destroyed, 3 fatal. On April 13, 2019 about 1514 CDT, a Rockwell/sabreliner airplane (NA-265-65), FAA registration N265DS, impacted terrain near New Albany, Mississippi. The two…
- [Incident 20180804010039I](https://openairdocs.org/incident/20180804010039I), Aug 4, 2018: Rockwell International Corp NA-265-65 (N770MD), Eagle, CO, Minor damage. On August 4, 2018 at approximately 1230 mountain daylight time, a Rockwell saberliner N770MD, experienced hydraulic failure during approach. The pilots…
- [Incident 20160206001239I](https://openairdocs.org/incident/20160206001239I), Feb 6, 2016: Rockwell International Corp NA-265-65 (N779CS), West Memphis, AR, Minor damage. On February 6, 2016 at approximately 16:00 CST, N779CS a Rockwell international, model NA-265-65 (sabre liner) aircraft, operated by a ATP rated pilot…
- [Incident 20130805014409I](https://openairdocs.org/incident/20130805014409I), Aug 5, 2013: Rockwell International Corp NA-265-65 (N670H), Spokane, WA, No damage. Pilot observed #2 engine oil pressure was at the low end of the yellow arc. Pilot reduced power and elected to make a precautionary landing at geg. Engine was…
- [Incident 20081024855859I](https://openairdocs.org/incident/20081024855859I), Oct 24, 2008: Rkwell NA26565 (N33TR), Atlanta, GA, Minor damage. (-23) Aircraft registration number N33TR landed on runway 20L Dekalb Peachtree airport (kpdk) at 1345UTC upon slowing the aircraft down after touch down the…
- [Accident 20071014824299A](https://openairdocs.org/incident/20071014824299A), Oct 14, 2007: Rkwell NA26565 (N65BT), Olathe, KS, Substantial damage. (-23) The aircraft landed at ixd, runway 18, touching down on or near the touchdown zone marker. The pilot deployed thrust reversers. During the rollout, the…
- [Incident 20001023038039I](https://openairdocs.org/incident/20001023038039I), Oct 23, 2000: Rkwell NA26565 (N651MK), Albany, NY. (-23) A/c landed alb. Lear jet on ground notified tower and crew of N651MK of left brake smoking. A/c stopped on taxiway where the 7 pax deplaned. After left…
- [Accident 20000510006709A](https://openairdocs.org/incident/20000510006709A), May 10, 2000: Rkwell NA26565 (N241H), Kaunakakai, HI, Destroyed, 6 fatal. (-23) Saberliner on night approach into the Molokai Airport. IFR departure from kahului, maui. Pilots were behind airplane and required ATC vectors to turn at…
- [Accident 19991129045841A](https://openairdocs.org/incident/19991129045841A), Nov 29, 1999: Rkwell NA26565 (N920DY), Seattle, WA, Substantial damage. (-23) Sabreliner N920DY was taxiing to parking after landing. An astrajet requested taxi for takeoff. Sabreline N920DY held its position on the taxiway to…
- [Incident 19990122010619I](https://openairdocs.org/incident/19990122010619I), Jan 22, 1999: Rkwell NA26565 (N91BZ), Little Rock, AR. On January 15,1999, at approximately 1615, on a flight to dallas, TX, a rockwell sabreliner, N91BZ, registered to general foam plastic corp. piloted by david…
- [Incident 19980510013139I](https://openairdocs.org/incident/19980510013139I), May 10, 1998: Rkwell NA26565 (N651MK), Philipsburg, PA, Minor damage. Narrative: on may 5, 1998, at 1220 hours pacific daylight time, a north American sabreliner NA265-65, N651MK, experienced an uncontained engine failure during…
- [Incident 19910920047619I](https://openairdocs.org/incident/19910920047619I), Sep 20, 1991: Rkwell NA26565 (N701FW), South Bend, IN. No safe light for nose gear on approach. Pilot replaced bulb and got safe indication. Landed without incident.
- [Incident 19910315015179I](https://openairdocs.org/incident/19910315015179I), Mar 15, 1991: Rkwell NA26560 (N33TR), Dallas, TX. Unsafe gear indication on approach. Landed safely. Found a burned out gear indication bulb.

## Service difficulty reports (76, newest 50)

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

- [SDR 2020F00358](https://openairdocs.org/sdr/2020F00358), Aug 9, 2020: GROUND WIRE. FAILED. LIGHT SMOKE IN THE BACK OF PASSENGERS CABIN. DECLARED AN EMERGENCY AND LANDED. INVESTIGATING AFTER LANDING FOUND FAULTY GROUND CONNECTOR GENERATING EXCESSIVE HE
- [SDR UVVR2020020300049](https://openairdocs.org/sdr/UVVR2020020300049), Jan 6, 2020: STRUT. OVERSERVICED. DURING LANDING ROLLOUT THE AIRCRAFT DEPARTED THE RIGHT SIDE OF THE RUNWAY AND STOPPED IN THE GRASS. THE FLIGHT CREW REPORTED LOSS OF NOSE STEERING AND BRAKES. A
- [SDR UVVR2018060600048](https://openairdocs.org/sdr/UVVR2018060600048), Jun 6, 2018: SKIN. CRACKED. FUSELAGE SKIN WAS FOUND CRACK AT LOWER AFT CORNER OF THE RT OVERWING ESCAPE HATCH OPENING.
- [SDR UVVR2017060900046](https://openairdocs.org/sdr/UVVR2017060900046), Jun 9, 2017: UNKNOWN. UNKNOWN. DURING LANDING ROLL, THE ACFT WAS TRACKING TO THE RIGHT. THE PILOT TRIED TO CORRECT IT BY APPLYING MORE LEFT RUDDER AND LEFT BRAKE, THE ACFT STILL CONTINUING TO
- [SDR UVVR2017031500044](https://openairdocs.org/sdr/UVVR2017031500044), Jan 12, 2017: SKIN. CORRODED. CORROSION WAS DISCOVERED AT LT UPPER WING PLANK BETWEEN WING STATION 146.4 TO 159.0.
- [SDR UVVR2016031500043](https://openairdocs.org/sdr/UVVR2016031500043), Jul 15, 2016: FLEX LINE. LEAKING. DURING OPS CHECK OF CREW OXYGEN MASK, FOUND OXYGEN SYSTEM LEAKS BEYOND ALLOWABLE LIMIT WITH A 1 HOUR PERIOD. UPON INVESTIGATION FOUND O2 FLEX TO PILOT SYS OUTLE
- [SDR UVVR2016020900036](https://openairdocs.org/sdr/UVVR2016020900036), Feb 7, 2016: PUMP. FAILED. AFTER LANDING AND DURING ROLLOUT THE PILOT REPORTED THAT THE BRAKES HAD FAILED. EMERGENCY BRAKING WAS SELECTED AND BRAKING POWER WAS RESTORED. POST LANDING OPS 
- [SDR UVVR2016020900035](https://openairdocs.org/sdr/UVVR2016020900035), Feb 7, 2016: CLEVIS. FRACTURED. ON LANDING ROLLOUT THE LT MLG COLLAPSED AND THE LT WINGTIP CONTACTED THE RUNWAY. LANDING GEAR INDICATED DOWN AND LOCKED BEFORE AND AFTER THE GEAR COLLAPSED.
- [SDR UVVR2015091500033](https://openairdocs.org/sdr/UVVR2015091500033), Sep 11, 2015: SKIN. CORRODED. LEFT WING AT WING 159-171, TOP SKIN BULGING. REMOVED TOP SKIN AND DISCOVERED SIGNIFICANT AREA OF CORROSION MEASURING APPROXIMATELY 3" X 4".
- [SDR 1HYR20141103001](https://openairdocs.org/sdr/1HYR20141103001), Nov 3, 2014: SKIN. CRACKED. A SKIN CRACK WAS IDENTIFIED IN THE AFT UNPRESSURIZED AREA OF THE FUSELAGE, RT ABOVE, LT PYLON. THE CRACK IS ABOUT 1.375" LONG LOCATED AT APPROXIMATELY FS 390.5 
- [SDR UVVR2013101500027](https://openairdocs.org/sdr/UVVR2013101500027), Nov 14, 2013: BOLT. FRACTURED. BOLT HEAD MISSING FROM UPPER FWD WING SPLICE PLATE. BOLT SHANK AND NUT WERE FOUND INTACT.
- [SDR UVVR2011072500018](https://openairdocs.org/sdr/UVVR2011072500018), Jul 25, 2011: ATTACH FITTING. CRACKED. DURING COMPLIANCE OF CAMP CARD 52.006 (521040) INSPECT MAIN ENTRANCE DOOR FOR CORROSION. THE MAIN ENTRANCE DOOR FORWARD HANDRAIL ATTACH FITTING (L-ANGLE) WAS FO
- [SDR UVVR2011072200017](https://openairdocs.org/sdr/UVVR2011072200017), Jul 22, 2011: SKIN. CORRODED. DURING COMPLIANCE OF SB 99-2 INSPECT LT & RT WING TIPS, LT TOP AND BOTTOM AFT WING PLANK CORRODED AROUND NUT PLATE AREAS AT REAR SPAR (RS) 258.371 TO 270.371.
- [SDR DGCA10844](https://openairdocs.org/sdr/DGCA10844), Dec 3, 2010: HYDRAULIC SYSTEM. LOW PRESSURE. LOST MAIN HYD SYS PRESSURE INDICATION. DECLARED AN EMERGENCY LANDING.
- [SDR UVVR2010042800007](https://openairdocs.org/sdr/UVVR2010042800007), Apr 28, 2010: SKIN. CORRODED. (UVVR) WHILE AIRCRAFT WAS STRIPPED FOR A PAINT JOB, VISUAL INSPECTION OF LT WING OVERWING FAIRING WAS DELAMANATED. AFTER FUTHER PANEL REMOVAL, FOUND CORROSION E
- [SDR UVVR2010022600006](https://openairdocs.org/sdr/UVVR2010022600006), Feb 23, 2010: FLOORBEAM. CORRODED. ANGLE CORRODED (EXFOLIATED) ON LOWER FS 166.3 FUSELAGE FLOOR SUPPORT WEB RT BP 8-10, ATTACHED TO LOWER FUSELAGE SKIN AND WEB.
- [SDR UVVR2010021500005](https://openairdocs.org/sdr/UVVR2010021500005), Feb 12, 2010: SKIN. CRACKED. FUSELAGE SKIN CRACKED AT LOWER AFT CORNER OF LEFT OVERWING ESCAPE HATCH OPENING.
- [SDR UVVR2010021500004](https://openairdocs.org/sdr/UVVR2010021500004), Feb 12, 2010: SKIN. CRACKED. FUSELAGE SKIN CRACKED AT LOWER FWD CORNER OF RT OVERWING ESCAPE HATCH OPENING.
- [SDR UVVR2010021100001](https://openairdocs.org/sdr/UVVR2010021100001), Feb 10, 2010: FRAME. CRACKED. 3 INCH CRACK IN LEFT FUSELAGE SIDE FRAME AT FUSELAGE STATION 257.65 APPROXIMATELY 2 INCHES ABOVE CABIN FLOOR.
- [SDR DGCA10523](https://openairdocs.org/sdr/DGCA10523), Feb 6, 2010: CIRCUIT BREAKER. BROKEN. AIRCRAFT LOST ALL EMERGENCY POWER.
- [SDR DGCA10501](https://openairdocs.org/sdr/DGCA10501), Jan 28, 2010: PUMP. FAILED. HYDRAULIC PUMP FAILURE.
- [SDR DGCA09327](https://openairdocs.org/sdr/DGCA09327), Nov 17, 2009: EXCITER. INOPERATIVE. RT ENGINE WOULD NOT START. EXCITER INOPERATIVE.
- [SDR DGCA 09104 11](https://openairdocs.org/sdr/DGCA%2009104%2011), Apr 29, 2009: PROXIMITY SWITCH. DEFECTIVE. RT MAIN GEAR, DOWN AND LOCKED GREEN INDICATOR LIGHT, WOULD NOT EXTINGUISH.
- [SDR DGC2008F00001](https://openairdocs.org/sdr/DGC2008F00001), Aug 18, 2008: PUMP. INOPERATIVE. ON AUGUST 16, 2008, AT APPROXIMATELY 8:30 AM, AFTER LANDING, THE CREW HEARD AUDIBLE WARNING OF HYDRAULIC SYSTEM LOW PRESSURE. THE AC TAXIED TO THE RAMP OF DESTI
- [SDR DGCA175D081867](https://openairdocs.org/sdr/DGCA175D081867), Aug 18, 2008: PUMP. INOPERATIVE. ON AUGUST 16, 2008, AT APPROXIMATELY 8:30 AM, ACFT N570R S/N 485-075, AFTER LANDING AT YIP, THE CREW HEARD AUDIBLE WARNING OF HYDRAULIC SYSTEM LOW PRESSURE. THE
- [SDR DGC2008F00000](https://openairdocs.org/sdr/DGC2008F00000), Aug 16, 2008: PUMP. INOPERATIVE. HYDRAULIC PRESSURE SYSTEM FAILURE, DISCOVERED PUMP INOPERATIVE. (S)
- [SDR 0805714](https://openairdocs.org/sdr/0805714), Mar 27, 2008: PROXIMITY SWITCH. UNKNOWN. RED LIGHT IN MLG HANDLE.
- [SDR 07060](https://openairdocs.org/sdr/07060), Apr 26, 2007: HOUSING. CRACKED. NOSE LANDING GEAR STEERING ACTUATOR HOUSING DEVELOPED A CRACK AND LEAKED HYDRAULIC FLUID ON THE RAMP.
- [SDR DGCA06233](https://openairdocs.org/sdr/DGCA06233), Nov 2, 2006: PIN. CRACKED. RT EMERGENCY EXIT, LOWER AFT ALIGNMENT PIN CRACKED.
- [SDR DGCA06009](https://openairdocs.org/sdr/DGCA06009), Jan 2, 2006: CARBON SEAL. FAILED. AFTER DEPARTURE, PLTS NOTICED RT ENG OIL PRESSURE WAS ABOVE THE GREEN ARC INTO THE YELLOW. PULLED BACK ON THE THROTTLE AND THE OIL PRESSURE FOLLOWED THE THROTTL
- [SDR DGCA06002](https://openairdocs.org/sdr/DGCA06002), Jan 2, 2006: PROXIMITY SWITCH. BROKEN. WHEN DEPARTING FROM SPIRIT OF ST. LOUIS AIRPORT S.U.S., THE CREW RETRACTED THE MAIN GEAR, UPON COMPLETION OF THE UP CYCLE THE CREW HEARD A KNOCKING NOISE FROM T
- [SDR DGCA05020](https://openairdocs.org/sdr/DGCA05020), Feb 10, 2005: CONTROL BOX. MALFUNCTIONED. DC VOLTAGE "SPIKE", CAUSING MULTIPLE COMPONENT/SYSTEM FAILURES, CIRCUIT BREAKERS POPPING.
- [SDR JV2R200400003](https://openairdocs.org/sdr/JV2R200400003), Dec 9, 2004: EEC. DEFECTIVE. OPERATOR REPORTED LEFT DIGITAL ELECTRONIC ENGINE CONTROL COMPUTER FAIL LIGHT ILLUMINATED DURING CLIMB PUTTING THE SYSTEM IN MANUAL. THE OPERATOR REPORTED ATTEMP
- [SDR JV2R200400001](https://openairdocs.org/sdr/JV2R200400001), Dec 9, 2004: COMPUTER. FAILED. DURING MAINTENANCE ENGINE RUN, THE LT COMPUTER FAIL LIGHT ILLUMINATED AT 92 PERCENT AND THE SYSTEM WENT TO MANUAL. THE ENGINE OPERATOR RESET THE SYSTEM PER MANU
- [SDR WK42004F00002](https://openairdocs.org/sdr/WK42004F00002), Mar 15, 2004: TIRE. DAMAGED. CENTER TREAD CHUNKED AFTER 54 LANDINGS ON LT TIRE.
- [SDR JV2R20040001](https://openairdocs.org/sdr/JV2R20040001), Mar 8, 2004: TIRE. SEPARATED. TIRE TREAD SEPARATION FROM TIRE CASING. EACH TIRE REPORTED HAS LESS THAN TWENTY LANDINGS ON IT. THIS PROBLEM REPORTED TO TIRE MFG. SAMPLES OF DISCREPANT UNITS F
- [SDR WK42004F00000](https://openairdocs.org/sdr/WK42004F00000), Feb 10, 2004: TIRE. DAMAGED. CENTER TREAD CHUNKED AFTER 19 LANDINGS ON LEFT LAND TIRE.
- [SDR JV2R200300001](https://openairdocs.org/sdr/JV2R200300001), Sep 19, 2003: FRAME. CRACKED. CRACK FOUND UPON ROUTINE INSPECTION. CRACK IS APPOXIMATLY FOURTEEN INCHES INTO FRAME. APPOXIMATE LOCATION OF FRAME IS FS 264.
- [SDR 2003F00513](https://openairdocs.org/sdr/2003F00513), Jun 27, 2003: BELLCRANK. CRACKED. AFTER FINDING THE LT AFT ELEVATOR BELLCRANK PN 265-5221313 FS457 CRACKED AT LOWER BEARING BOSS AREA ON A DIFFERENT NA 265-65 AIRCRAFT WE PERFORMED INSPECTIONS O
- [SDR 032031A](https://openairdocs.org/sdr/032031A), Mar 20, 2003: RESTRICTOR VALVE. BYPASSING. DURING PREFLT INSP, MAINT CREW NOTED THAT SPOILERS FULLY DEPLOYED IN LESS THAN 1 SECOND WITH SPOILER SWITCHES SET TO "IN-FLT" MODE. NORMAL DEPLOY TIME IN THIS M
- [SDR 032031](https://openairdocs.org/sdr/032031), Mar 20, 2003: RESTRICTOR VALVE. BYPASSING. MAIN ACCOMPLISHED PREFLT INSP AND THEN PILOTS PROCEEDED TO DO THEIR PREFLT INSP. UPON NORMAL EXTENSION OF SPEED BRAKE PANELS, THEY RETRACTED WITH HIGH SPEED AS 
- [SDR ROCK012303](https://openairdocs.org/sdr/ROCK012303), Jan 23, 2003: SWITCH. INOPERATIVE. PILOT'S TRIM SWITCH BECAME INTERMITTENT AND THEN FAILED TO OPERATE COMPLETELY IN FLIGHT. CO-PILOT AND ALTERNATE TRIM SYSTEMS BOTH REMAINED FUNCTIONAL. TESTED AN
- [SDR JV2R200200004](https://openairdocs.org/sdr/JV2R200200004), Nov 6, 2002: LINE. NICKED. WHEN COMPLYING WITH CAMP CARDS, A VISUAL INSPECTION OF THE ENGINE WAS PERFORMED AND FOUND THE OIL LINE HAD NICKS IN THE LINE CAUSE BY THE CLAMPS, THAT HAD THE T
- [SDR JV2R200200003](https://openairdocs.org/sdr/JV2R200200003), Nov 6, 2002: LINE. NICKED. WHEN COMPLYING WITH CAMP CARDS, A VISUAL INSPECTION OF THE ENGINE WAS PERFORMED AND FOUND THE OIL LINE HAD NICKS IN IT CAUSE BY THE CLAMPS THAT HAD THE TEFLON W
- [SDR 02341](https://openairdocs.org/sdr/02341), Oct 22, 2002: BEARING. FAILED. PILOT BEGAN FEELING VIBRATION FROM LEFT ENGINE, LEFT GENERATOR HOT LIGHT CAME ON, FOLLOWED BY GENERATOR FAILURE.
- [SDR 2002FA0001066](https://openairdocs.org/sdr/2002FA0001066), Sep 16, 2002: BRACKET. BROKEN. DURING GEAR RETRACTION TEST, LT MLG DOOR ACTUATOR ATTACH BRACKET BROKE AT GEAR DOOR.
- [SDR UVVR200200001](https://openairdocs.org/sdr/UVVR200200001), Aug 5, 2002: GASKET. FAILED. "AFT FUSELAGE HOT" LIGHT CAME ON IN FLIGHT. CREW MADE LANDING AT SUS. AVMATS TROUBLESHOT PROBLEM, FOUND APU START BYPASS VALVE GASKET BLOWN - CAUSING HOT BLEED 
- [SDR I5W2002F00000](https://openairdocs.org/sdr/I5W2002F00000), Jun 20, 2002: FITTING. BROKEN. LANDING GEAR WOULD NOT RETRACT AFTER TAKE-OFF. THE MAIN GEAR INNER DOOR ACTUATOR SUPPORT FITTING PN 2823330511 BROKE AT THE ACTUATOR ATTACH POINT. MANUALLY RETR
- [SDR 029041702](https://openairdocs.org/sdr/029041702), Apr 17, 2002: LINE. CRACKED. PILOTS STARTED TAXI OUT TO TAKEOFF. IN PROCESS CONDUCTED THE LANDING SPOILER EXTENSION OPERATIONAL TEST WHICH SURGES AND SLAMS THE HYDRAULIC SYSTEM FAIRLY HARD.
- [SDR 2001112329](https://openairdocs.org/sdr/2001112329), Nov 26, 2001: LINE. CRACKED. MAINTENANCE PERSONNEL NOTICED FLUID LEAKAGE FROM BELLY PANEL AFT OF LANDING GEAR FOLLOWING PILOT'S COMPLETION OF "SPOILER AUTO EXTEND" PREFLIGHT CHECK BY FLIGHT

All 76: https://openairdocs.org/model/rockwell-international-na-265-65/reports.md

## STCs that may be installed (OpenAirDocs) (105, 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 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 ST04183AT](https://openairdocs.org/stc/ST04183AT): Installation of the Honeywell CAS-100 Traffic Alert and Collision Avoidance System (TCAS), Version 7.1, and the ACSS NXT-800 Mode S Transponder with associated hardware. Woven Electronics LLC
- [STC SA2698SO](https://openairdocs.org/stc/SA2698SO): Installation of provisions for a CAS-81 TCAS. Honeywell International Inc
- [STC SA2734SO](https://openairdocs.org/stc/SA2734SO): Installation of a CAS-81 TCAS II. Honeywell International Inc
- [STC ST00445WI-D](https://openairdocs.org/stc/ST00445WI-D): Installation of Honeywell Enhanced Ground Proximity Warning System. Limited to installation on NA-265-65, serial number 465-58 ONLY. Honeywell International Inc
- [STC ST00715WI-D](https://openairdocs.org/stc/ST00715WI-D): Installation of provisions for AlliedSignal AIRSAT 1 IRIDIUM Aeronautical Satelite Communication System. Honeywell International Inc
- [STC ST00093WI-D](https://openairdocs.org/stc/ST00093WI-D): ONE-ONLY STC, S/N 465-58: Installation of hte Bendix/King CAS 66A TCAS I System. Honeywell International Inc
- [STC ST01343CH-D](https://openairdocs.org/stc/ST01343CH-D): Installation of AlliedSignal CAS-67A Traffic Alert and Collision Avoidance System (TCAS II) incorporating MOPS Change 7. Airplane must be previously equipped with STC ST333CH-D. Honeywell International Inc
- [STC ST01344CH-D](https://openairdocs.org/stc/ST01344CH-D): Installation of dual Honeywell enhanced GNS-XLS Flight Management System. Aircraft must have STC ST335CH-D installed. Honeywell International Inc
- [STC SA2073CE-D](https://openairdocs.org/stc/SA2073CE-D): Installation of Bendix/King EFS-10 electronic flight instrument sys (5 tube) dual KFC-400 automatic flight control sys, dual KAD-480 air data sys, dual KNS-660 flight mgmt sys, KHF-950HF Comm System and MLS-21 microwave landing system. Honeywell International Inc
- [STC SA2311CE-D](https://openairdocs.org/stc/SA2311CE-D): ONE-ONLY STC, SN 465-058: Installation of Bendix/King CAS 80A Traffic Alert and Collision Avoidance System. Honeywell International Inc
- [STC ST00791WI](https://openairdocs.org/stc/ST00791WI): Installation of AlliedSignal Avionics, Inc., KAD-481 adaptor module, part number 065-05041-28E1 (software part number 125-00981-00E1). Approved for installation on NA-265-65, serial number 465-58 ONLY. Honeywell International Inc
- [STC ST333CH-D](https://openairdocs.org/stc/ST333CH-D): Installation of a Bendix/King CAS67A TCAS II System with dual MST-67 Mode S Transponders installed per Garrett Aviation Services. Honeywell International Inc
- [STC ST335CH-D](https://openairdocs.org/stc/ST335CH-D): Installation of Dual AlliedSignal Aerospace, Global Wulfsberg GNS-XLS Flight Management. Honeywell International Inc
- [STC ST01553WI](https://openairdocs.org/stc/ST01553WI): Installation of the Honeywell MKV EGPWS with RAAS and Monitor Functions or the Honeywell MKV-A EGPWS with RAAS and Monitor Functions. Honeywell International Inc
- [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 ST00105AT](https://openairdocs.org/stc/ST00105AT): Installation of a replacement coalescer filter. Purolator Facet, Inc
- [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 SA4407SW](https://openairdocs.org/stc/SA4407SW): Installation of emergency brake pressure indication system. Centurion Investments
- [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 ST04238AT](https://openairdocs.org/stc/ST04238AT): Upgrade of Honeywell Traffic Collision Avoidance Systems II (TCAS II) Processor Software from TCAS II Version 7.0 to TCAS II Version 7.1. Aviation Partners Group Inc
- [STC SA1537CE](https://openairdocs.org/stc/SA1537CE): Installation of Solar Model T-62T-40C auxiliary power unit(APU). Sabreliner Aviation LLC
- [STC SA1603CE](https://openairdocs.org/stc/SA1603CE): Installation of Collins FPC-75 ground proximity warning system. Sabreliner Aviation LLC
- [STC SA1604CE](https://openairdocs.org/stc/SA1604CE): Installation of Collins DNS-61B inertial navigation system. 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 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 SA2640CE](https://openairdocs.org/stc/SA2640CE): tallation of Global-Wulfsberg GNS-500A Series 5 Navigation System with VLF, Omega and GPS Sensors. Sabreliner Aviation LLC
- [STC SA2649CE](https://openairdocs.org/stc/SA2649CE): Installation of dual Global-Wulfsberg GNS-500A Series 5 navigation systems with VLF, Omega, GPS and Loran C sensors. Sabreliner Aviation LLC
- [STC SA2759CE](https://openairdocs.org/stc/SA2759CE): Installation of Fairchild Model A100A Cockpit Voice Recorder. Sabreliner Aviation LLC
- [STC ST00007WI](https://openairdocs.org/stc/ST00007WI): Installation of Collins TCAS-94 (TCAS II), TDR-94D (dual) Mode S transponder system, TWR-850 turbulence weather radar, VHF-72 COM's, VIR-32 NAV's, DME-42's, Dual CTL-22, and Dual CTL-32 controls. Sabreliner Aviation LLC
- [STC ST00119WI](https://openairdocs.org/stc/ST00119WI): Installation of a Bendix TCAS I. Sabreliner Aviation LLC
- [STC ST00262WI](https://openairdocs.org/stc/ST00262WI): Installation of a Trimble TNL-2100T (I/O) GPS Navigation System. Sabreliner Aviation LLC
- [STC ST00456WI](https://openairdocs.org/stc/ST00456WI): Installation of an AlliedSignal Avionics Inc., MARK VI Ground Proximity Warning System. Sabreliner Aviation LLC
- [STC ST00535WI](https://openairdocs.org/stc/ST00535WI): Installation of an AlliedSignal Avionics Inc., GNS-XLS Flight Management System (Dual). Sabreliner Aviation LLC
- [STC ST00552WI](https://openairdocs.org/stc/ST00552WI): Installation of a Universal Avionics Systems UNS-1D with GPS and a UNS-1MSP with GPS Navigation Management Systems. Sabreliner Aviation LLC
- [STC ST00603WI](https://openairdocs.org/stc/ST00603WI): Installation of dual Universal Navigation Corp UNS-1 Msp. Navigation Management Systems with dual GPS. Sabreliner Aviation LLC

All 105: https://openairdocs.org/model/rockwell-international-na-265-65/stcs.md

## PMA parts (OpenAirDocs) (237, 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
- [979516-1-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID145204884720230907125107.0001): Valve, Shutoff. Honeywell International Inc. · PMA PQ1222NM · Replaces 979516-1-1 · Dec 7, 2022
- [3214034-1-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID133738282220230907125103.0001): Valve, Butterfly, Shutoff and Regulating, 2.0 In. Dia.. Honeywell International Inc. · PMA PQ1222NM · Replaces 3214034-1-1 · Dec 7, 2022
- [3214200-1-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID132869439720230907125104.0001): Valve, Regulating, Bleed Air Mixing. Honeywell International Inc. · PMA PQ1222NM · Replaces 3214200-1-1 · 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
- [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
- [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
- [M23076-1250](https://drs.faa.gov/browse/excelExternalWindow/0B92DED19BE700E98625841D0057119A.0001): Thermostatic Switch. Miraj Corporation · PMA PQ0870NE · Replaces 23076-1250 · Nov 14, 2018
- [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
- [920055](https://drs.faa.gov/browse/excelExternalWindow/9B31CCF1377D70E5862581F500525F06.0001): Airshow 410 Digital Interface Unit. Rockwell Collins Inc · PMA PQ0390NM · Replaces 920055 · Jun 1, 2016
- [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

All of them: https://openairdocs.org/model/rockwell-international-na-265-65/pma.md

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