# Mitsubishi MU-2B-36

- Type: Aircraft model (FAA registry)
- Registry code: 5780412
- Manufacturer (registry): MITSUBISHI
- Model: MU-2B-36
- Aircraft type: Fixed wing multi engine
- Category: Airplane
- Engines: 2 · Turbo-prop
- Seats: 10
- Weight class: Up to 12,499 lb
- Cruise speed: 255 mph
- Certification: Type certificated
- Data sheet: [TCDS A2PC](https://openairdocs.org/tcds/A2PC) (OpenAirDocs)
- Holder: Mitsubishi Heavy Industries Ltd. 203
- Registered aircraft: 7
- Page: https://openairdocs.org/model/mitsubishi-mu-2b-36

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 2020-26-14](https://openairdocs.org/ad/2020-26-14): Propellers · Mitsubishi Heavy Industries MU-2B, MU-2B-10, MU-2B-15 and 10 more. Effective Feb 2, 2021
- [AD 2016-08-19](https://openairdocs.org/ad/2016-08-19): Landing Gear · Mitsubishi Heavy Industries MU-2B-30, MU-2B-35, MU-2B-36 and 2 more. Effective Jun 6, 2016
- [AD 2015-01-02](https://openairdocs.org/ad/2015-01-02): Fuselage · Mitsubishi Heavy Industries MU-2B-30, MU-2B-35, MU-2B-36 and 2 more. Effective Feb 26, 2015
- [AD 2010-10-17](https://openairdocs.org/ad/2010-10-17): Airplane flight manual · Mitsubishi Heavy Industries MU-2B, MU-2B-10, MU-2B-15 and 10 more. Effective Jul 22, 2010
- [AD 2007-17-09](https://openairdocs.org/ad/2007-17-09): Elevator nose-down trim · Mitsubishi Heavy Industries MU-2B, MU-2B-10, MU-2B-15 and 10 more. Effective Sep 25, 2007
- [AD 2006-17-05](https://openairdocs.org/ad/2006-17-05): Flight checks of the rigging of the engine and propeller systems · Mitsubishi Heavy Industries MU-2B, MU-2B-10, MU-2B-15 and 10 more. Effective Sep 22, 2006
- [AD 2006-13-15](https://openairdocs.org/ad/2006-13-15): Wing attach barrel nuts, bolts · Mitsubishi Heavy Industries MU-2B-10, MU-2B-15, MU-2B-20 and 9 more. Effective Aug 11, 2006
- [AD 2005-18-20](https://openairdocs.org/ad/2005-18-20): "FASTprop" propeller de-icers · Hartzell PHC-C3YF-1RF/F8468A(B,K)-8R constant speed propeller (STC SA00718LA or 17 others). Effective Oct 14, 2005
- [AD 2005-01-19](https://openairdocs.org/ad/2005-01-19): Mode S transponders · GARMIN International GTX 330D, GTX 330, GTX 33D and 830 more. Effective Feb 23, 2005
- [AD 2003-22-07 R1](https://openairdocs.org/ad/2003-22-07-R1): AFM- forecast icing conditions · Mitsubishi Heavy Industries MU-2B, MU-2B-10, MU-2B-15 and 10 more. Effective Apr 16, 2004
- [AD 2003-17-04](https://openairdocs.org/ad/2003-17-04): Cockpit Windshield and Cabin Window · Mitsubishi Heavy Industries MU-2B-10, MU-2B-15, MU-2B-20 and 9 more. Effective Oct 3, 2003
- [AD 2000-09-15 R1](https://openairdocs.org/ad/2000-09-15-R1): Icing Conditions · Mitsubishi Heavy Industries MU-2B, MU-2B-10, MU-2B-15 and 10 more. Effective Jul 24, 2000
- [AD 98-25-02](https://openairdocs.org/ad/98-25-02): Top-mounted Antenna · Bell Helicopter Textron Canada 407, 172, 172A and 243 more. Effective Dec 22, 1998
- [AD 98-20-39](https://openairdocs.org/ad/98-20-39): Forward Attachment Fitting Bolt · Mitsubishi Heavy Industries MU-2B, MU-2B-10, MU-2B-15 and 10 more. Effective Nov 20, 1998
- [AD 96-25-02](https://openairdocs.org/ad/96-25-02): Airplane Flight Manual (AFM) - Icing Limitations · Mitsubishi Heavy Industries MU-2B-10, MU-2B-15, MU-2B-20 and 9 more. Effective Dec 27, 1996
- [AD 94-11-04](https://openairdocs.org/ad/94-11-04): Hub Arm Assembly · AiResearch TPE330-5-252M engines and Hartzell Propeller… (Mitsubishi Heavy Industries America STC SA2413SW). Effective Jun 10, 1994
- [AD 91-23-08](https://openairdocs.org/ad/91-23-08): Rudder Trim Tab · Mitsubishi Heavy Industries MU-2B-10, MU-2B-15, MU-2B-20 and 2 more. Effective Dec 18, 1991
- [AD 88-21-01 R1](https://openairdocs.org/ad/88-21-01-R1): Control Yoke · Mitsubishi Heavy Industries MU-2B, MU-2B-10, MU-2B-15 and 10 more. Effective Jan 28, 1989
- [AD 88-23-01](https://openairdocs.org/ad/88-23-01): Torque Tube Joints · Mitsubishi Heavy Industries MU-2B, MU-2B-10, MU-2B-15 and 10 more. Effective Dec 4, 1988
- [AD 88-13-01](https://openairdocs.org/ad/88-13-01): Autopilots · Mitsubishi Heavy Industries MU-2B, MU-2B-10, MU-2B-15 and 10 more. Effective Jul 11, 1988
- [AD 87-04-03](https://openairdocs.org/ad/87-04-03): Flap Flexible Shafts · Mitsubishi Heavy Industries MU-2B, MU-2B-10, MU-2B-15 and 10 more. Effective Mar 7, 1987
- [AD 86-26-02](https://openairdocs.org/ad/86-26-02): POH/AFM Appendix - Icing · Mitsubishi Heavy Industries MU-2B-10, MU-2B-15, MU-2B-20 and 9 more. Effective Dec 31, 1986
- [AD 86-20-01](https://openairdocs.org/ad/86-20-01): Pitot System Modification · Mitsubishi Heavy Industries MU-2B, MU-2B-10, MU-2B-15 and 10 more. Effective Oct 6, 1986
- [AD 86-15-03](https://openairdocs.org/ad/86-15-03): NLG Strut Assembly · Mitsubishi Heavy Industries MU-2B, MU-2B-10, MU-2B-15 and 6 more. Effective Aug 13, 1986
- [AD 84-25-02](https://openairdocs.org/ad/84-25-02): Trim Tab Brackets · Mitsubishi Heavy Industries MU-2B, MU-2B-10, MU-2B-15 and 10 more. Effective Dec 18, 1984
- [AD 84-12-04](https://openairdocs.org/ad/84-12-04): Mitsubishi Heavy Industries MU-2B, MU-2B-10, MU-2B-15 and 10 more. Effective Jun 28, 1984
- [AD 83-09-02](https://openairdocs.org/ad/83-09-02): Strobe Light Assemblies · Mitsubishi Heavy Industries MU-2B-25, MU-2B-26, MU-2B-30 and 2 more. Effective May 17, 1983
- [AD 82-21-03](https://openairdocs.org/ad/82-21-03): Fire Detection · Mitsubishi Heavy Industries MU-2B, MU-2B-10, MU-2B-15 and 4 more. Effective Oct 14, 1982
- [AD 82-08-02](https://openairdocs.org/ad/82-08-02): Electrical Wiring Inspection · Mitsubishi Heavy Industries MU-2B, MU-2B-10, MU-2B-15 and 6 more. Effective Apr 15, 1982
- [AD 80-04-01](https://openairdocs.org/ad/80-04-01): Avionic Equipment Mounting Shelf · Mitsubishi Heavy Industries MU-2B-36, MU-2B-36A and MU-2B-60. Effective Feb 14, 1980
- [AD 79-24-02](https://openairdocs.org/ad/79-24-02): Outer Fuel Tank Wiring · Mitsubishi Heavy Industries MU-2B, MU-2B-10, MU-2B-15 and 10 more. Effective Nov 21, 1979
- [AD 78-03-05](https://openairdocs.org/ad/78-03-05): Cowling Latches · Mitsubishi Heavy Industries MU-2B, MU-2B-10, MU-2B-15 and 6 more. Effective Feb 23, 1978
- [AD 75-03-06](https://openairdocs.org/ad/75-03-06): Cracks and Optical Distortion · Mitsubishi Heavy Industries MU-2B-26 and MU-2B-36. Effective Nov 13, 1974

Historical (superseded or no longer in force):

- [AD 2006-17-01](https://openairdocs.org/ad/2006-17-01) (historical): Airplane Flight Manual (AFM) · Mitsubishi Heavy Industries MU-2B, MU-2B-10, MU-2B-15 and 10 more. Effective Sep 22, 2006
- [AD 2006-15-07](https://openairdocs.org/ad/2006-15-07) (historical): Airplane Flight Manual (AFM) · Mitsubishi Heavy Industries MU-2B, MU-2B-10, MU-2B-15 and 10 more. Effective Aug 24, 2006
- [AD 2003-22-07](https://openairdocs.org/ad/2003-22-07) (historical): Airplane Flight Manual (AFM) - icing conditions · Mitsubishi Heavy Industries MU-2B, MU-2B-10, MU-2B-15 and 10 more. Effective Dec 15, 2003
- [AD 2000-09-15](https://openairdocs.org/ad/2000-09-15) (historical): Icing · Mitsubishi Heavy Industries MU-2B, MU-2B-10, MU-2B-15 and 10 more. Effective Jul 24, 2000
- [AD 2000-02-25](https://openairdocs.org/ad/2000-02-25) (historical): Airframe Pneumatic Deicing Boots · Mitsubishi Heavy Industries MU-2B-10, MU-2B-15, MU-2B-20 and 9 more. Effective Mar 24, 2000
- [AD 97-25-02](https://openairdocs.org/ad/97-25-02) (historical): Airplane Flight Manual (AFM) - Power Levers · Mitsubishi Heavy Industries MU-2B, MU-2B-10, MU-2B-15 and 9 more. Effective Jan 21, 1998
- [AD 97-20-14](https://openairdocs.org/ad/97-20-14) (historical): Airplane Flight Manual (AFM) - Icing Limitations · Mitsubishi Heavy Industries MU-2B, MU-2B-10, MU-2B-15 and 10 more. Effective Oct 17, 1997
- [AD 94-04-16](https://openairdocs.org/ad/94-04-16) (historical): Elevator Nose-Down Trim · Mitsubishi Heavy Industries MU-2B-10, MU-2B-15, MU-2B-20 and 5 more. Effective Apr 11, 1994
- [AD 93-07-11](https://openairdocs.org/ad/93-07-11) (historical): Elevator Nose-Down Trim · Mitsubishi Heavy Industries MU-2B-25, MU-2B-26, MU-2B-26A and 5 more. Effective Jun 1, 1993
- [AD 75-16-20](https://openairdocs.org/ad/75-16-20) (historical): Propeller Pitch Control Lever · Mitsubishi Heavy Industries MU-2B, MU-2B-10, MU-2B-15 and 6 more. Effective Aug 12, 1975

## Information bulletins (advisory) (2)

- [SAIB CE-19-09](https://openairdocs.org/saib/CE-19-09): Wing Miscellaneous Structure. Issued Jun 10, 2019
- [SAIB CE-12-33](https://openairdocs.org/saib/CE-12-33): Landing Gear Retraction/Extension System, Nose Landing Gear. Issued Jun 12, 2012

## Registered aircraft (7)

- [N13YS](https://openairdocs.org/aircraft/N13YS): [Air 1st Aviation Companies Inc](https://openairdocs.org/faa-owner/AIR%201ST%20AVIATION%20COMPANIES%20INC), [Aiken, SC](https://openairdocs.org/faa-place/SC/Aiken), built 1976, S/N 694
- [N15TC](https://openairdocs.org/aircraft/N15TC): [Stax Holdings LLC](https://openairdocs.org/faa-owner/STAX%20HOLDINGS%20LLC), [Hot Springs, AR](https://openairdocs.org/faa-place/AR/Hot%20Springs), built 1976, S/N 692
- [N500PJ](https://openairdocs.org/aircraft/N500PJ): [Fly2mellc](https://openairdocs.org/faa-owner/FLY2MELLC), [Ooltewah, TN](https://openairdocs.org/faa-place/TN/Ooltewah), built 1974, S/N 668
- [N59KS](https://openairdocs.org/aircraft/N59KS): [Oconnell Meares Investments Ltd](https://openairdocs.org/faa-owner/OCONNELL%20MEARES%20INVESTMENTS%20LTD), [Tampa, FL](https://openairdocs.org/faa-place/FL/Tampa), built 1974, S/N 664
- [N687HB](https://openairdocs.org/aircraft/N687HB): [Southern Jets Inc](https://openairdocs.org/faa-owner/SOUTHERN%20JETS%20INC), [Naples, FL](https://openairdocs.org/faa-place/FL/Naples), S/N 687
- [N741FN](https://openairdocs.org/aircraft/N741FN): [Air 1st Aviation Co Of Ok](https://openairdocs.org/faa-owner/AIR%201ST%20AVIATION%20CO%20OF%20OK), [Tulsa, OK](https://openairdocs.org/faa-place/OK/Tulsa), built 1975, S/N 658
- [N866D](https://openairdocs.org/aircraft/N866D): [Air 1st Aviation Companies Inc](https://openairdocs.org/faa-owner/AIR%201ST%20AVIATION%20COMPANIES%20INC), [Aiken, SC](https://openairdocs.org/faa-place/SC/Aiken), built 1974, S/N 656

## NTSB investigations (9)

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 DFW07CA189](https://openairdocs.org/ntsb/DFW07CA189), Aug 22, 2007: Mitsubishi MU-2B-36 (N6KF), Hobby Airport, TX, no damage. Probable cause: The failure of the ramp employee to maintain clearance from the rotating propeller. A contributing factor was the prevailing night conditions.
- [NTSB ENG07IA009](https://openairdocs.org/ntsb/ENG07IA009), Jan 12, 2007: Mitsubishi MU-2B-36 (N950MA), Chicago, IL, incident, minor damage. Probable cause: Complete loss of No. 2 engine power due to a partial rim failure of the 2nd stage turbine wheel, resulting in No. 2 engine shutdown and turbine debris exiting the side of the engine. The wheel…
- [NTSB CHI05FA272](https://openairdocs.org/ntsb/CHI05FA272), Sep 23, 2005: Mitsubishi MU-2B-36 (N103RC), West Memphis, AR, destroyed, 1 fatal. Probable cause: The pilot's improper in-flight decision not to land at the departure runway or other available airports during the emergency descent, and his failure to maintain clearance from a vehicle and terrain.…
- [NTSB NYC04FA093](https://openairdocs.org/ntsb/NYC04FA093), Mar 25, 2004: Mitsubishi MU-2B-36 (N201UV), Pittsfield, MA, substantial damage, 1 fatal. Probable cause: The pilot's loss of aircraft control for undetermined reasons, which resulted in an inadvertent stall/spin and subsequent impact with the ground.
- [NTSB LAX96LA280](https://openairdocs.org/ntsb/LAX96LA280), Jul 20, 1996: Mitsubishi MU-2B (N999FA), Scottsdale, AZ, destroyed. Probable cause: an uncontained failure of the second stage turbine wheel due to fatigue. Factors were: obstructions in the forced landing area and the inability of the airplane to climb after the turbine wheel…
- [NTSB LAX92TL#06](https://openairdocs.org/ntsb/LAX92TL%2306), May 18, 1992: Mitsubishi MU2B-36 (N742FN), Edwards Afb, CA, substantial damage
- [NTSB ATL90FA163](https://openairdocs.org/ntsb/ATL90FA163), Sep 6, 1990: Mitsubishi MU-2B-36 (N82MA), Nashville, TN, destroyed, 1 fatal. Probable cause: THE COMPANY/OPERATOR MANAGEMENT'S DECISION TO OPERATE THE AIRCRAFT WITH A KNOWN DEFICIENCY WITHOUT FURTHER MAINTENANCE, THE PILOT'S IMPROPER PLANNING/DECISION AND THE PILOT'S FAILURE TO ABORT THE…
- [NTSB FTW84LA267](https://openairdocs.org/ntsb/FTW84LA267), Jun 9, 1984: Mitsubishi MU-2N (N850MA), Sugarland, TX, substantial damage
- [NTSB MKC83IA063](https://openairdocs.org/ntsb/MKC83IA063), Feb 5, 1983: Mitsubishi MU-2B-36 (N709US), Salina, KS, incident, minor damage

## FAA accident and incident reports (20)

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 20070112007749I](https://openairdocs.org/incident/20070112007749I), Jan 12, 2007: Mtsbsi MU2B36 (N950MA), Chicago, IL, Minor damage. (-23) Pilot stated that during the circle to 22L, he selected gear down and was reaching for the flap selector when he heard a large bang and saw a flash…
- [Accident 20050922025139A](https://openairdocs.org/incident/20050922025139A), Sep 22, 2005: Mtsbsi MU2B36 (N103RC), West Memphis, AR, Destroyed, 1 fatal. (-23) On September 22, 2005, at 1958 central daylight time, a mitsubishi MU2B-36, N103RC, operated by mcneely charter services, was destroyed when it impacted…
- [Incident 20050524013439I](https://openairdocs.org/incident/20050524013439I), May 24, 2005: Mtsbsi MU2B36 (N6KF), Milwaukee, WI, Minor damage. (-23) Pilot stated he used 20 degrees flap and an approach speed between 120 and 135 kt and overshot the touch down spot while landing rwy 7L. The tire skid…
- [Incident 20040827025619I](https://openairdocs.org/incident/20040827025619I), Aug 27, 2004: Mtsbsi MU2B36 (N740PB), Chicago, IL. (-23) After shutdown and the pilot departing the aircraft the right engine started on fire. The fire department was called and the fire extinguished.
- [Accident 20040325003729A](https://openairdocs.org/incident/20040325003729A), Mar 25, 2004: Mtsbsi MU2B36 (N201UV), Pittsfield, MA, Destroyed, 1 fatal. (-23) On March 25, 2004, at approximately 0535 EST, N201UV, royal air cargo flight number 747, operating as a part 135 air cargo flight, departed level flight…
- [Incident 20000714034859I](https://openairdocs.org/incident/20000714034859I), Jul 14, 2000: Mtsbsi MU2B36 (N823MA), Savannah, GA, Minor damage. (-23) Gear up landing go around normal landing made.
- [Incident 19970807027239I](https://openairdocs.org/incident/19970807027239I), Aug 7, 1997: Mtsbsi MU2B36 (N305CW), Rockford, IL, Minor damage. Narrative: at rotation speed, on departure from rfd rwy 19, a loud bang was heard and vibration felt. Acft was rotated into air and seemed normal. Assumed tire…
- [Accident 19960720019079A](https://openairdocs.org/incident/19960720019079A), Jul 20, 1996: Mtsbsi MU2B36 (N999FA), Scottsdale, AZ, Destroyed. Right engine blew on climbout. Landed on street. Hit rock wall. Turbine rotor disk failed.
- [Incident 19960229007699I](https://openairdocs.org/incident/19960229007699I), Feb 29, 1996: Mtsbsi MU2B36 (N717PS), Pontiac, MI, Minor damage. Narrative: aircraft was inbound into Oakland-Pontiac Airport (ptk). At 0008 local, the pilot reported rapid depressurization and that he lost a window in the…
- [Incident 19951212045669I](https://openairdocs.org/incident/19951212045669I), Dec 12, 1995: Mtsbsi MU2B36 (N915RF), Tulsa, OK, Minor damage. Narrative: aircraft departed on 135 cargo only flight when at 6 to 7,000 feet, the pilot door blew off. Pilot declared emergency, returned to airport, and…
- [Incident 19920921040859I](https://openairdocs.org/incident/19920921040859I), Sep 21, 1992: Mtsbsi MU2B35 (N535WM), Albuquerque, NM, Minor damage. Right engine failed on takeoff roll. Aborted. Secured engine. Returned to ramp.
- [Incident 19910929047519I](https://openairdocs.org/incident/19910929047519I), Sep 29, 1991: Mtsbsi MU2B36 (N13RR), Morgantown, WV. Loss of power on left engine en route. Shut engine down. Landed at destination safely.
- [Accident 19900906038359A](https://openairdocs.org/incident/19900906038359A), Sep 6, 1990: Mtsbsi MU2B36 (N82MA), Nashville, TN, Destroyed, 1 fatal. Slow takeoff. Hot day. Stalled, crashed and burned. No engine defects found.
- [Incident 19900126004169I](https://openairdocs.org/incident/19900126004169I), Jan 26, 1990: Mtsbsi MU2B36 (N13RR), Parkersburg, WV. Left engine fire warning. Shut engine down. Landed safely. Cause was a false fire warning signal.
- [Incident 19890713041249I](https://openairdocs.org/incident/19890713041249I), Jul 13, 1989: Mtsbsi MU2B36 (N740PB), Springfield, MO, Minor damage. Left cockpit side window blew out en route. Forced landing. Window had been altered when escape door installed.
- [Incident 19871214076489I](https://openairdocs.org/incident/19871214076489I), Dec 14, 1987: Mtsbsi MU2B36 (N201UV), Mcalester, OK, Minor damage. Windshear on three VOR approaches. Touchdown with gear up on second with go around and normal landing on third.
- [Accident 19840609023479A](https://openairdocs.org/incident/19840609023479A), Jun 9, 1984: Mtsbsi MU2B36A (N850MA), Sugarland, TX, Substantial damage. Damaged occurred when pilot allowed the aircraft to land short of the runway.
- [Incident 19830204030709I](https://openairdocs.org/incident/19830204030709I), Feb 4, 1983: Mtsbsi MU2B36 (N709US), Salina, KS, Minor damage. Landed in 18 inch deep snow on a portion of closed runway. Collapsed nose gear. Given NOTAM at weather briefing.
- [Incident 19801211088949I](https://openairdocs.org/incident/19801211088949I), Dec 11, 1980: Mtsbsi MU2* (N305CW), Midland, TX, Minor damage. Pilot moved gear selector switch to down position but failed to visually check position.
- [Incident 19790523027679I](https://openairdocs.org/incident/19790523027679I), May 23, 1979: Mtsbsi MU2B36 (N68TN), Abilene, TX. Landed with engine shut down, ran off end of runway. Found failed gear shaft.

## Service difficulty reports (49)

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

- [SDR NM5R201308191](https://openairdocs.org/sdr/NM5R201308191), Aug 13, 2013: DOOR. UNSECURE. CUSTOMER REPORTED, LT CREW DOOR BLEW OPEN DURING FLIGHT CAUSING EXTENSIVE DAMAGE TO THE OUTER WINDOW, DOOR FRAME AND OUTER SKIN. DOOR WAS SENT TO US FOR REPAIR.
- [SDR MCCA2013FA0000430](https://openairdocs.org/sdr/MCCA2013FA0000430), Aug 5, 2013: DOOR. FAILED. DURING CRUISE, CREW DOOR BLEW OPEN CAUSING THE ACFT TO DEPRESSURIZE. DECLARED AN EMERGENCY, DESCENDED, AND RETURNED TO POINT OF TAKEOFF. A SAFE LANDING WAS MADE
- [SDR VOX2009F00002](https://openairdocs.org/sdr/VOX2009F00002), May 11, 2009: TORQUE SENSOR. FAILED. PILOT REPROTED AFTER TAKEOFF, EXPERIENCED RT ENGINE SPOOLED DOWN. SECURED ENGINE AND RETURNED TO DEPARTURE. FOLLOW UP: TORQUE SENSOR FAILED IN RT ENGINE. (K)
- [SDR VOX2009F00001](https://openairdocs.org/sdr/VOX2009F00001), May 11, 2009: POWERPLANT. SHUTDOWN. PILOT REPORTED AFTER TAKEOFF, EXPERIENCED RT ENGINE SPOOLED DOWN. SECURED ENGINE AND RETURNED TO DEPARTURE. CAUSE OF ENGINE PROBLEM UNDETERMINED AT THIS TIME. (
- [SDR MCC2009F00000](https://openairdocs.org/sdr/MCC2009F00000), Feb 20, 2009: LATCH. FAILED. ACFT ON FINAL APPROACH, WHEN PILOT HEARD A THUD. STATED HE THOUGHT HE HAD HIT A BIRD. UNEVENTFUL LANDING WAS MADE. PILOT DEPARTED AC AND FOUND LT ENGINE TOP COW
- [SDR CA081027001](https://openairdocs.org/sdr/CA081027001), Oct 23, 2008: SHAFT. BINDING. (CAN) PROP OVERSEED DURING DESCENT. FOUND ENGINE INNER CONCENTRIC SHAFT TO BE BINDING ON OUTER CONCENTRIC SHAFT. AS POWER LEVER IS RETARDED, INNER CONCENTRIC SH
- [SDR BKAA200710003](https://openairdocs.org/sdr/BKAA200710003), Oct 16, 2007: TERMINAL BLOCK. DAMAGED. PITCH CONTROL JAMMED IN FLIGHT. SLIGHT MOVEMENT UP ABOUT 1 INCH CONTROL TRAVEL. A/C TRIED A FEW TIMES TO PITCH DOWN. A/P AND AVIONICS SWITCH OFF. LANDED WITH PO
- [SDR CA070718004](https://openairdocs.org/sdr/CA070718004), Jul 14, 2007: LEVER. LOOSE. (CAN) THE PPC LEVER WAS FOUND SEPARATED FROM THE PPC INPUT SHAFT. THE BOLT WAS OF THE CORRECT P/N, YET WAS THREAD BOUND WITHOUT PRODUCING ENOUGH TENSION TO HOLD
- [SDR CA070503004](https://openairdocs.org/sdr/CA070503004), Apr 26, 2007: FUEL CONTROL. WORN. (CAN) ENGINE WAS SHUTDOWN DUE TO ABNORMAL INDICATIONS. ENGINE REMOVED AND SENT TO OVERHAUL FACILITY, FCU AND FUEL PUMP REMOVED, DAMAGE FOUND TO THE FUEL CONTROL
- [SDR VOX2007F00000](https://openairdocs.org/sdr/VOX2007F00000), Apr 4, 2007: COWLING. DAMAGED. UPPER RT COWLING CAME OPEN IN FLIGHT. RECOMMEND INSTALLING 2 SCREWS AT LEADING EDGE OF COWLING TO PREVENT THIS HAPPENING. (K)
- [SDR CA060503006](https://openairdocs.org/sdr/CA060503006), Dec 20, 2005: PLENUM. CRACKED. (CAN) AIRCRAFT TOOK OFF FROM AIRPORT RUNWAY 15 OR A COURIER FLIGHT. THE AIRCRAFT CRASHED ABOUT 500 METERS EAST OF, AND APPROXIMATELY ABEAM, THE SOUTH END OF RUN
- [SDR CA060503005](https://openairdocs.org/sdr/CA060503005), Dec 20, 2005: PLENUM. CRACKED. (CAN) AC TOOK OFF, AC CRASHED, POST-CRASH FIRE OCCURRED. AC WAS DESTROYED. BOTH PILOTS FATALLY INJURED. DURING TEAR-DOWN OF RT ENG (WHICH WAS FOUND TO BE OPERAT
- [SDR MCC2005F00000](https://openairdocs.org/sdr/MCC2005F00000), Sep 23, 2005: FIRE WARNING. INTERMITTENT. RT ENGINE FINE WARNING FLICKERED ONE TIME IN FLIGHT. PILOT SECURED ENGINE AND FEATHERED PROP. UNEVENTFUL LANDING MADE AT MAINTENANCE INSPECTED ENGINE AND FOUND 
- [SDR 2003FA0000840](https://openairdocs.org/sdr/2003FA0000840), Aug 1, 2003: TIRE. FAILED. UPON LANDING, THE TIRE DISINTEGRATED. ASSURE THE TIRE WAS FLAT ON LANDING, DUE TO RUNWAY FOD ON TAKEOFF.
- [SDR IZ22003F00001](https://openairdocs.org/sdr/IZ22003F00001), Dec 20, 2002: SOLENOID VALVE. LEAKING. VALVE LEAKING FUEL BETWEEN THE SOLENOID AND VALVE BODY DUE TO BLOWN O-RING. THE FUEL WAS LEAKING INTO THE COWLING AND DRIPPING OUT.
- [SDR CA020307012](https://openairdocs.org/sdr/CA020307012), Mar 5, 2002: SWITCH. INTERMITTENT. (CAN) DURING APPROACH, CREW SELECTED GEAR DOWN & NOTHING HAPPENED. THEY BROKE OFF APPROACH & FLEW LOCALLY MAKING SEVERAL ATTEMPTS. EMERGENCY EXTENSION PERFORMED
- [SDR CA011221008](https://openairdocs.org/sdr/CA011221008), Dec 20, 2001: LINE. CHAFED. (CAN) THE OIL LINE RUNNING FROM THE OIL COOLER WAS FOUND CHAFED BY A SCREW THAT WAS TOO LONG IN A PANEL ON THE SIDE OF THE NACELLE. THE LINE WAS REPLACED AND TH
- [SDR CA011221007](https://openairdocs.org/sdr/CA011221007), Dec 5, 2001: BOLT. CRACKED. (CAN) THE NOSE LANDING GEAR DRAG STRUT ATTACH BOLT WAS FOUND CRACKED. THIS BOLT HAD BEEN MAGNETIC PARTICAL INSPECTED EVERY 2000 HOURS.
- [SDR CA000606003](https://openairdocs.org/sdr/CA000606003), Jun 1, 2000: VALVE. MALFUNCTIONED. (CAN) DURING CRUISE, THE CREW STARTED TO TRANSFER TIP FUEL WITH NO PROBLEM. WHEN THE CREW SELECTED TIP TRANSFER OFF, THE RT TIP TANK CONTINUED TO FLOW UNTIL TIP
- [SDR CA000215006](https://openairdocs.org/sdr/CA000215006), Feb 9, 2000: SWITCH. FROZEN. (CAN) THE CREW SELECTED GEAR DOWN ON APPROACH AND THE GEAR FAILED TO EXTEND. THE CREW ELECTED TO OVERSHOOT AND RETURN TO THEIR MAIN BASE. ON APPROACH TO THE MAI
- [SDR CA000209006](https://openairdocs.org/sdr/CA000209006), Feb 8, 2000: ACTUATOR. FROZEN. (CAN) THE LANDING GEAR FAILED TO EXTEND WHEN SELECTED DUE TO A FROZEN DOOR ACTUATOR CLUTCH. THE CREW THEN INITIATED AN EMERGENCY EXTENSION WHICH WAS UNSUCCESSFU
- [SDR CA000120006](https://openairdocs.org/sdr/CA000120006), Jan 17, 2000: ROLLER. MISSING. (CAN) THE CREW TRIED TO EXTEND THE LANDING GEAR USING THE EMERGENCY EXTENSION SYSTEM, AFTER A LANDING GEAR MALFUNCTION. THE LANDING GEAR COULD NOT BE EXTENDED A
- [SDR CA990728017](https://openairdocs.org/sdr/CA990728017), Jul 14, 1999: TORQUE SENSOR. FAILED. (CAN) THE FAILURE WAS LIMITED TO THE DIRECT DRIVE GEAR STACK ON THE TORQUE SENSOR. THIS GEAR DRIVES THE FUEL PUMP AND FUEL CONTROL THE FAILURE OF WHICH SHUT DOW
- [SDR 99ZZZX2364](https://openairdocs.org/sdr/99ZZZX2364), May 25, 1999: VALVE. DAMAGED. HIGH PRESSURE RELIEF VALVE BODY, P/N 867927-1, WAS STILL IN FUEL PUMP HOUSING, BUT THE WRENCHING FLATS AND CAP OF RELIEF VALVE WERE FOUND HANGING FROM SAFETY WI
- [SDR 99ZZZX1417](https://openairdocs.org/sdr/99ZZZX1417), Mar 1, 1999: HOUSING. DAMAGED. THREADS FOR FITTING OF AFT OIL SCAVENGE PUMP LINE, IN ACCESSORY/GEAR HOUSING, STRIP OUT CAUSING OIL LEAK.
- [SDR CA980928019](https://openairdocs.org/sdr/CA980928019), Sep 11, 1998: CARBON SEAL. FAILED. (CAN) THE PILOT OBSERVED FLUCTUATIONS IN TORQUE AND OIL PRESSURE, AS WELL AS VISIBLE OIL VENTING FROM THE ENGINE. THE ENGINE WAS SHUT DOWN AND THE AIRCRAFT LAND
- [SDR 98ZZZX2640](https://openairdocs.org/sdr/98ZZZX2640), Jun 26, 1998: WHEEL. FAILED. INNER WHEEL HALF EXPERIENCED A BEARING FAILURE. FAILURE RESULTED IN BRAKE DISC RUBBING INTO BRAKE ASSEMBLY REQUIRING BRAKE ASSEMBLY REPLACEMENT. INNER WHEEL HAL
- [SDR CA971113013](https://openairdocs.org/sdr/CA971113013), Oct 24, 1997: GASKET. FAILED. (CAN) DURING CRUISE, CREW NOTICED FLUCTUATING OIL PRESSURE ON LT ENGINE. OIL PRESSURE MONITORED AND AIRCRAFT LANDED. FRETTED AND DETERIORATED TURBINE SCAVANGE P
- [SDR 97ZZZM1086](https://openairdocs.org/sdr/97ZZZM1086), Sep 25, 1997: KNOB. LOOSE. AILERON CONTROL KNOW FALLS OFF POTENTIALLY CAUSING A CONTROL PROBLEM IF PILOT EXPERIENCES ENGINE FAILURE ON TAKEOFF. A POTENTIAL LOSS OF CONTROL AND OR AIRCRAFT
- [SDR CA970909006](https://openairdocs.org/sdr/CA970909006), Aug 21, 1997: LINE. CRACKED. (CAN) RIGHT HAND OIL PRESSURE LINE TO TORQUE TRANSDUCER CHAFED THROUGH DUE TO B-NUT COMING LOOSE AND SUBSEQUENT LOSS OF OIL PRESSURE. NEW LINE INSTALLED AND GRO
- [SDR 97ZZZM885](https://openairdocs.org/sdr/97ZZZM885), Aug 7, 1997: TIRE. FAILED. UPON ROTATION, TREAD SEPARATED FROM CARCASS ON THE NR 1 TIRE ASSEMBLY. AT SEPARATION TIRE TREAD DAMAGED AFT GEAR DOOR AND DOOR CONNECTING ROD. TREAD THEN FLEW F
- [SDR 97ZZZX4686](https://openairdocs.org/sdr/97ZZZX4686), Apr 30, 1997: TIRE. SEPARATED. LEFT HAND MAIN GEAR TIRE TREAD SEPARATED FROM CASING ALONG INBOARD EDGE FOR APPROXIMATELY 10 INCHES. OCCURRED ON LANDING. TIRE REMAINED INFLATED. THIS WAS ONE O
- [SDR 97ZZZX2637](https://openairdocs.org/sdr/97ZZZX2637), Apr 30, 1997: TIRE. SEPARATION. LEFT HAND MAIN GEAR TIRE TREAD SEPARATED FROM CASING ALONG INBOARD EDGE FOR APPROXIMATELY 10 INCHES. OCCURRED ON LANDING. TIRE REMAINED INFLATED. THIS WAS ONE O
- [SDR 97ZZZX4685](https://openairdocs.org/sdr/97ZZZX4685), Apr 17, 1997: TIRE. SEPARATED. RIGHT HAND MAIN GEAR TIRE TREAD SEPARATED FROM CASING ALONG INBOARD EDGE FOR APPROXIMATELY 1 INCH. SEPARATION WAS NOTICED DURING A POST-FLIGHT WALK AROUND INSPE
- [SDR 97ZZZX2643](https://openairdocs.org/sdr/97ZZZX2643), Apr 17, 1997: TIRE. SEPARATION. RIGHT HAND MAIN GEAR TIRE TREAD SEPARATED FROM CASING ALONG INBOARD EDGE FOR APPROXIMATELY 1 INCH. SEPARATION NOTICED DURING A POST-FLIGHT WALK AROUND INSPECTIO
- [SDR 97ZZZX4687](https://openairdocs.org/sdr/97ZZZX4687), Apr 2, 1997: TIRE. SEPARATED. RIGHT HAND MAIN GEAR TIRE TREAD SEPARATED FROM CASING ALONG INBOARD EDGE COMPLETELY AROUND CIRCUMFERENCE. OCCURRED ON LANDING. TIRE REMAINED INFLATED. TREAD STA
- [SDR 97ZZZX2636](https://openairdocs.org/sdr/97ZZZX2636), Apr 2, 1997: TIRE. SEPARATION. RIGHT HAND MAIN GEAR TIRE TREAD SEPARATED FROM CASING ALONG INBOARD EDGE COMPLETELY AROUND CIRCUMFERENCE. OCCURRED ON LANDING. TIRE REMAINED INFLATED. TREAD STA
- [SDR CA961007013](https://openairdocs.org/sdr/CA961007013), Aug 5, 1996: SUN GEAR. FRACTURED. (CAN) PILOT NOTED SEVERE VIBRATION WITH NO WARNING. PRIOR TO SHUTDOWN, THE TORQUE WENT TO ZERO. AIRCRAFT RETURNED OK. INSPECTION REVEALED THE PLANETARY PIN P/N 
- [SDR CA960619002](https://openairdocs.org/sdr/CA960619002), Jun 13, 1996: SWITCH. SHORTED. (CAN) ON GEAR EXTENSION, 3 GREEN LIGHTS SHOWED MOMENTARILY THEN WENT OUT AS THE GEAR DOORS CLOSED. FORWARD LEFT GEAR DOOR SWITCH FAILED AND SHORTED TO GROUND IN
- [SDR CA960126004](https://openairdocs.org/sdr/CA960126004), Jan 16, 1996: MLG SOLENOID. BURNT CONTACTS. (CAN)THE CREW SELECTED GEAR DOWN ON APPROACH AND THE GEAR DOORS OPENED BUT NOTHING FURTHER HAPPENED. THEY THEN NOTICED THAT THE GEAR MOTOR CIRCUIT MOTOR HAD TRI
- [SDR 96ZZZM20](https://openairdocs.org/sdr/96ZZZM20), Dec 9, 1995: BRAKE. BURNED. ON LANDING AT YIP, AIRCRAFTS RIGHT MAIN BRAKE WAS DRAGGING. RESUTLED IN FLAT SPOT ON TIRE AND OVERHEATED BRAKE ASSEMBLY. WHEEL AND BRAKE REPLACED WITH SERVICEAB
- [SDR CA951211003](https://openairdocs.org/sdr/CA951211003), Dec 7, 1995: O-RING. CHAFED. (CAN)THE CREW MADE AN UNEVENTFUL SHORT TURN AROUND AT DAWSON CREEK (-35C),THEN PROCEEDED TO FT. ST. JOHN (-41C). DURING THE APP A LOUD BANG WAS HEARD DURING GEA
- [SDR 95ZZZX6838](https://openairdocs.org/sdr/95ZZZX6838), Nov 27, 1995: FRAME. CRACKED. FRAME 4610, LEFT, CRACKED THROUGH SCREW HOLES APPROXMATELY 31MM BELOW LOWER HOLE. ALL 6 STATIONS HAD TO BE SHIMMED PER SB 209A.
- [SDR 95ZZZM702](https://openairdocs.org/sdr/95ZZZM702), Nov 11, 1995: TIRE. FAILED. ON LANDING AT DET, BOTH NOSE TIRES FAILED (BLEW OUT). THIS FAILURE CAUSED BOTH NOSE WHEEL RIMS TO CONTACT THE RUNWAY SURFACE AT HIGH SPEED DESTROYING BOTH NOSE 
- [SDR BUHA95002](https://openairdocs.org/sdr/BUHA95002), Nov 1, 1995: DOWNLOCK SWITCH. FAILED. INTERNAL FAILURE OF NOSE GEAR DOWNLOCK SWITCH ALLOWED INDICATOR LIGHT VOLTAGE TO BLEED OVER TO THE LANDING GEAR CONTROL SECTION OF THE SWITCH. (X)
- [SDR 95ZZZX6049](https://openairdocs.org/sdr/95ZZZX6049), Oct 12, 1995: GEARBOX FITTING. DEFECT. IN CRUISE FLIGHT, LEFT ENGINE OIL PRESSURE STARTED TO FLUCTUATE. A PRECAUTIONARY SHUT DOWN WAS MADE AND THE AIRCRAFT HAD AN UNEVENTFUL LANDING. TROUBLESHOOTING 
- [SDR 95ZZZM692](https://openairdocs.org/sdr/95ZZZM692), Oct 4, 1995: TQ SENSOR BRG. FAILED. AT FL 150 IN LEVEL CRUISE CONDITIONS, THE NR 2 ENGINE FLAMED OUT. AN UNEVENTFUL LANDING WAS ACCOMPLISHED AT IPT . TROUBLESHOOTING OF THE ENGINE REVEALED THE MAI
- [SDR 95ZZZX3583](https://openairdocs.org/sdr/95ZZZX3583), Jul 13, 1995: FUEL CONTROL. FAILED. ENGINE LOST FUEL FLOW IN CRUISE FLIGHT. ENGINE SHUT-DOWN AND FEATHERED. TROUBLESHOOTING DETERMINED FUEL CONTROL FAILED. THE FUEL CONTROL UNIT HAD APPROXIMATELY 
- [SDR 95ZZZX2304](https://openairdocs.org/sdr/95ZZZX2304), Apr 11, 1995: WINDOW. CRACKED. DURING A POST-INSPECTION WALK-AROUND, A CRACK WAS NOTED EXTENDING APPROXIMATELY 1 INCH INTO THE VISIBLE AREA OF THE OUTER WINDOW IN THE CREW EMERGENCY ESCAPE DO

## STCs that may be installed (OpenAirDocs) (187, 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 SA01800SE](https://openairdocs.org/stc/SA01800SE): Fabrication and installation of new or replacement of existing instrument panel lights dimmer control. TCW Technologies, LLC
- [STC SA01861SE](https://openairdocs.org/stc/SA01861SE): Fabrication and installation of Landing Light Controller. TCW Technologies, LLC
- [STC SA02019SE-D](https://openairdocs.org/stc/SA02019SE-D): Installation of Garmin Model GTN 625/635/650; 725/750 Navigation System. Garmin International Inc
- [STC SA02658SE](https://openairdocs.org/stc/SA02658SE): Installation of Garmin GI 275 Multi-Function Display System. Garmin International Inc
- [STC SA02532AT](https://openairdocs.org/stc/SA02532AT): Installation of subject Michelin tires on appropriate aircraft. For Michelin 5, 6, 8, and 10-inch rim diameter tires on General Aviation Aircraft. Michelin North America Inc
- [STC SA02010WI](https://openairdocs.org/stc/SA02010WI): Installation of the Mid-Continent Instruments & Avionics MD23 FLEX Custom Function Display (CFD). Mid-Continent Instruments and Avionics
- [STC SA652GL](https://openairdocs.org/stc/SA652GL): Install Parker Hannifin wheel and brakes conversion kit, 199-101 dated 9/28/82. Kaman Corporation Aircraft Wheel and Brake LLC
- [STC SA685GL](https://openairdocs.org/stc/SA685GL): To convert a Cleveland nose wheel from Model 40-87 to Model 40-87F, install Parker Hannifin 199-121 conversion kit. Kaman Corporation Aircraft Wheel and Brake LLC
- [STC SA02203AK](https://openairdocs.org/stc/SA02203AK): Installation of FlightLogic Synthetic Vision Electronic Flight Information System (EFIS-SV). Genesys Aerosystems Inc
- [STC SA00491WI](https://openairdocs.org/stc/SA00491WI): Installation of Test Instrumentation, Inc., (TII) Trim-in-Motion Alert System on Mitsubishi MU-2B airplanes. Mitsubishi Heavy Industries America Inc
- [STC SA00489WI](https://openairdocs.org/stc/SA00489WI): Installation of Test Instrumentation, Inc automatic autopilot disconnect system on airplanes equipped with Sperry SPZ-500 or Bendix M-4C or M-4D autopilot. Mitsubishi Heavy Industries America Inc. Lists MU-2B Series
- [STC SA00601WI](https://openairdocs.org/stc/SA00601WI): Installation of Test Instrumentation, Inc. (TII) Icing Alert (Rosemount 0871HL1/HL2 or 0871CT1 Ice Detector) System. Mitsubishi Heavy Industries America Inc
- [STC SA1352SW](https://openairdocs.org/stc/SA1352SW): Installation of interior. Mitsubishi Heavy Industries America Inc
- [STC SA1411SW](https://openairdocs.org/stc/SA1411SW): Installation of emergency locator transmitter. Mitsubishi Heavy Industries America Inc
- [STC SA1419SW](https://openairdocs.org/stc/SA1419SW): Replacement of Gulton GB40A or CA5 Sonotone batteries with type 4076 Saft batteries. Mitsubishi Heavy Industries America Inc
- [STC SA1456SW](https://openairdocs.org/stc/SA1456SW): Installation of antennas. Mitsubishi Heavy Industries America Inc
- [STC SA1470SW](https://openairdocs.org/stc/SA1470SW): Installation of avionics support shelving. Mitsubishi Heavy Industries America Inc
- [STC SA1489SW](https://openairdocs.org/stc/SA1489SW): Installation of antennas. Mitsubishi Heavy Industries America Inc
- [STC SA1511SW](https://openairdocs.org/stc/SA1511SW): Installation of PC-17 600 VA main inverter and PC-17 standby inverter; or installation of Flitetronics 250VA PC-15B main and standby inverters. Mitsubishi Heavy Industries America Inc
- [STC SA1541SW](https://openairdocs.org/stc/SA1541SW): Installation of King basic avionic package. Mitsubishi Heavy Industries America Inc
- [STC SA1542SW](https://openairdocs.org/stc/SA1542SW): Installation of King KNC 610 area navigation computer. Mitsubishi Heavy Industries America Inc
- [STC SA1545SW](https://openairdocs.org/stc/SA1545SW): Installation of Sperry Stars IVB flight director. Mitsubishi Heavy Industries America Inc
- [STC SA1557SW](https://openairdocs.org/stc/SA1557SW): Installation of autopilot transfer system. Mitsubishi Heavy Industries America Inc
- [STC SA1560SW](https://openairdocs.org/stc/SA1560SW): Installation of Avionics basic Collins package. Mitsubishi Heavy Industries America Inc
- [STC SA1561SW](https://openairdocs.org/stc/SA1561SW): Installation of AVQ-21 weather radar. Mitsubishi Heavy Industries America Inc
- [STC SA1563SW](https://openairdocs.org/stc/SA1563SW): Installation of Bonzer Radar Altimeter TRN-71. Mitsubishi Heavy Industries America Inc
- [STC SA1586SW](https://openairdocs.org/stc/SA1586SW): Installation of alternate oil pressure transmitter. Mitsubishi Heavy Industries America Inc
- [STC SA1587SW](https://openairdocs.org/stc/SA1587SW): Installation of Aerosonic altimeter P/N A35-MA-10L1 to replace McCleod altimeter. Mitsubishi Heavy Industries America Inc
- [STC SA1614SW](https://openairdocs.org/stc/SA1614SW): Installation of IDC 570-24929-002 encoding altimeter or Smith's WL-1350 AM/MS-1(-2) encoding altimeter. Mitsubishi Heavy Industries America Inc
- [STC SA1615SW](https://openairdocs.org/stc/SA1615SW): Installation of encoding altimeter/alerting system. Mitsubishi Heavy Industries America Inc
- [STC SA1641SW](https://openairdocs.org/stc/SA1641SW): Installation of Sperry SPZ-200 autopilot and Stars IVC flight director system. Mitsubishi Heavy Industries America Inc
- [STC SA1674SW](https://openairdocs.org/stc/SA1674SW): Installation of Smith's encoding altimeter and alerting system. Mitsubishi Heavy Industries America Inc
- [STC SA1693SW](https://openairdocs.org/stc/SA1693SW): Installation of Bendix M-4D autopilot system. Mitsubishi Heavy Industries America Inc
- [STC SA1703SW](https://openairdocs.org/stc/SA1703SW): Installation of 5V light source. Mitsubishi Heavy Industries America Inc
- [STC SA1708SW](https://openairdocs.org/stc/SA1708SW): Installation of ASB 125P/SAC-69 HF Comm. Mitsubishi Heavy Industries America Inc
- [STC SA1804SW](https://openairdocs.org/stc/SA1804SW): Installation of 110 V outlet and wiring. Mitsubishi Heavy Industries America Inc
- [STC SA1814SW](https://openairdocs.org/stc/SA1814SW): Installation of a dual baro scale altimeter. Mitsubishi Heavy Industries America Inc
- [STC SA1816SW](https://openairdocs.org/stc/SA1816SW): Installation of King flight phone. Mitsubishi Heavy Industries America Inc
- [STC SA1849SW](https://openairdocs.org/stc/SA1849SW): Installation of dual ASB 100A high frequency radios. Mitsubishi Heavy Industries America Inc
- [STC SA1851SW](https://openairdocs.org/stc/SA1851SW): Installation of -501 single encoding altimeter and alerter system. Mitsubishi Heavy Industries America Inc
- [STC SA1872SW](https://openairdocs.org/stc/SA1872SW): Modification of Hamilton Standard temperature control system. Mitsubishi Heavy Industries America Inc
- [STC SA1941SW](https://openairdocs.org/stc/SA1941SW): Modification of the basic King Gold Crown avionics. Mitsubishi Heavy Industries America Inc
- [STC SA2247SW](https://openairdocs.org/stc/SA2247SW): Installation of oxygen cylinder, P/N 6350 A20 00B. Mitsubishi Heavy Industries America Inc
- [STC SA2263SW](https://openairdocs.org/stc/SA2263SW): Modification of ECS mixing chamber. Mitsubishi Heavy Industries America Inc
- [STC SA2266SW](https://openairdocs.org/stc/SA2266SW): Fabrication and installation of wing panel flap actuator access. Mitsubishi Heavy Industries America Inc
- [STC SA2269SW](https://openairdocs.org/stc/SA2269SW): Installation of King KRA 405 radar altimeter. Mitsubishi Heavy Industries America Inc
- [STC SA2274SW](https://openairdocs.org/stc/SA2274SW): Installation of heated windshield. Mitsubishi Heavy Industries America Inc
- [STC SA2295SW](https://openairdocs.org/stc/SA2295SW): Installation of alternate interstage turbine temperature indicator. P/N 935A-6012. Mitsubishi Heavy Industries America Inc
- [STC SA2309SW](https://openairdocs.org/stc/SA2309SW): Installation of Sperry TP114B transponder. Mitsubishi Heavy Industries America Inc
- [STC SA09856AC](https://openairdocs.org/stc/SA09856AC): Installation of BendixKing Aerowave 100 In-flight Data Link System for non-essential, non-required aircraft Cabin Systems & Equipments. Honeywell International Inc (Bendix King)

All 187: https://openairdocs.org/model/mitsubishi-mu-2b-36/stcs.md

## PMA parts (OpenAirDocs) (402, 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.

- [W/T-2802](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID197103814720240426151106.0001): Cabin Pane – Inner (Green). Great Lakes Aero Products Inc · PMA PQ2056CE · Replaces 010A-31785-3 · Feb 23, 2024
- [W-2802](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID193306555220240426151105.0001): Cabin Pane – Inner (Clear). Great Lakes Aero Products Inc · PMA PQ2056CE · Replaces 010A-31785-3 · Feb 23, 2024
- [SC-W/G-2802](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID171850049420240426151106.0001): Cabin Pane – Inner (Solar Control Gray). Great Lakes Aero Products Inc · PMA PQ2056CE · Replaces 010A-31785-3 · Feb 23, 2024
- [SC-W/T-2802](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID139563343220240426151106.0001): Cabin Pane – Inner (Solar Control Green). Great Lakes Aero Products Inc · PMA PQ2056CE · Replaces 010A-31785-3 · Feb 23, 2024
- [W/XT-2802](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID127473430720240426151107.0001): Cabin Pane – Inner (Any Tint). Great Lakes Aero Products Inc · PMA PQ2056CE · Replaces 010A-31785-3 · Feb 23, 2024
- [SC-W/XT-2802](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID116640686220240426151107.0001): Cabin Pane – Inner (Solar Control Any Tint). Great Lakes Aero Products Inc · PMA PQ2056CE · Replaces 010A-31785-3 · Feb 23, 2024
- [W/G-2802](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID104304759320240426151106.0001): Cabin Pane – Inner (Gray). Great Lakes Aero Products Inc · PMA PQ2056CE · Replaces 010A-31785-3 · Feb 23, 2024
- [W/BL-2801-RH](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID191678417920240307183046.0001): Crew Side Pane – Inner (Right Blue). Great Lakes Aero Products Inc · PMA PQ2056CE · Replaces 010A-31780-4 · Feb 21, 2024
- [W-2801-RH](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID191354825820240307183045.0001): Crew Side Pane – Inner (Right Clear). Great Lakes Aero Products Inc · PMA PQ2056CE · Replaces 010A-31780-4 · Feb 21, 2024
- [W/G-2801-RH](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID169421191120240307183046.0001): Crew Side Pane – Inner (Right Gray). Great Lakes Aero Products Inc · PMA PQ2056CE · Replaces 010A-31780-4 · Feb 21, 2024
- [SC-W/T-2801-RH](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID168261223620240307183046.0001): Crew Side Pane – Inner (Right Solar Control Green). Great Lakes Aero Products Inc · PMA PQ2056CE · Replaces 010A-31780-4 · Feb 21, 2024
- [SC-W/BL-2801-LH](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID161332577520240307183045.0001): Crew Side Pane – Inner (Left Solar Control Blue). Great Lakes Aero Products Inc · PMA PQ2056CE · Replaces 010A-31780-3 · Feb 21, 2024
- [SC-W/BL-2801-RH](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID161264228420240307183047.0001): Crew Side Pane – Inner (Right Solar Control Blue). Great Lakes Aero Products Inc · PMA PQ2056CE · Replaces 010A-31780-4 · Feb 21, 2024
- [SC-W/T-2801-LH](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID145749906720240307183045.0001): Crew Side Pane – Inner (Left Solar Control Green). Great Lakes Aero Products Inc · PMA PQ2056CE · Replaces 010A-31780-3 · Feb 21, 2024
- [SC-W/G-2801-RH](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID144432166720240307183046.0001): Crew Side Pane – Inner (Right Solar Control Gray). Great Lakes Aero Products Inc · PMA PQ2056CE · Replaces 010A-31780-4 · Feb 21, 2024
- [W/G-2801-LH](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID131491862220240307183044.0001): Crew Side Pane – Inner (Left Gray). Great Lakes Aero Products Inc · PMA PQ2056CE · Replaces 010A-31780-3 · Feb 21, 2024
- [W/T-2801-RH](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID120806853720240307183046.0001): Crew Side Pane – Inner (Right Green). Great Lakes Aero Products Inc · PMA PQ2056CE · Replaces 010A-31780-4 · Feb 21, 2024
- [SC-W/G-2801-LH](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID120278807020240307183045.0001): Crew Side Pane – Inner (Left Solar Control Gray). Great Lakes Aero Products Inc · PMA PQ2056CE · Replaces 010A-31780-3 · Feb 21, 2024
- [W-2801-LH](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID115865056920240307183044.0001): Crew Side Pane – Inner (Left Clear). Great Lakes Aero Products Inc · PMA PQ2056CE · Replaces 010A-31780-3 · Feb 21, 2024
- [W/BL-2801-LH](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID108774606920240307183045.0001): Crew Side Pane – Inner (Left Blue). Great Lakes Aero Products Inc · PMA PQ2056CE · Replaces 010A-31780-3 · Feb 21, 2024
- [W/T-2801-LH](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID106953107920240307183044.0001): Crew Side Pane – Inner (Left Green). Great Lakes Aero Products Inc · PMA PQ2056CE · Replaces 010A-31780-3 · Feb 21, 2024
- [TII-34120-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID117338001920240213214508.0001): Ventral Fin Assy, Aft Fuselage. Test Instrumentation Inc · PMA PQ05428NM · Replaces 030A-34120-1030A-34120-2 · Feb 8, 2024
- [AAI- 150SG1070](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID127161186920240320173349.0001): Friction Disc. Augusta Aero Innovations LLC · PMA PQ04441CE · Replaces 150SG1070 · Jan 31, 2024
- [01-7079-24](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID172881902320231108124805.0001): LIGHT-ASSY, StarLight. AeroLEDs LLC · PMA PQ5259NM · Replaces WA7079B-24NLI7079-24CMA-7079B-24A7079B… · Nov 3, 2023
- [APS68-03300](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID174431311220231102131432.0001): Shim, Brake. Aviation Products Systems Inc · PMA PQ3830CE · Replaces 068-03300 · Sep 25, 2023
- [102464-37](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID189499656720230727204622.0001): Control. Honeywell International Inc. · PMA PQ1222NM · Replaces 102464-37 · May 2, 2023
- [102464-36](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID175594177520230727204612.0001): Control. Honeywell International Inc. · PMA PQ1222NM · Replaces 102464-36 · May 2, 2023
- [103570-14](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID154897424620230727204617.0001): Outflow/Safety Valve. Honeywell International Inc. · PMA PQ1222NM · Replaces 103570-14 · May 2, 2023
- [103310-10](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID146021214020230727204613.0001): Outflow. Honeywell International Inc. · PMA PQ1222NM · Replaces 103310-10 · May 2, 2023
- [103310-16](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID135550008820230727204619.0001): Outflow Flow. Honeywell International Inc. · PMA PQ1222NM · Replaces 103310-16 · May 2, 2023
- [102464-2](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID132052189020230727204618.0001): Control. Honeywell International Inc. · PMA PQ1222NM · Replaces 102464-2 · May 2, 2023
- [107312-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID130442373420230727204620.0001): Pneumatic Relay. Honeywell International Inc. · PMA PQ1222NM · Replaces 107312-1 · May 2, 2023
- [103570-24](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID128769111220230727204623.0001): Outflow/Safety Valve. Honeywell International Inc. · PMA PQ1222NM · Replaces 103570-24 · May 2, 2023
- [135157-4](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID124645580620230727204616.0001): Filter. Honeywell International Inc. · PMA PQ1222NM · Replaces 135157-4 · May 2, 2023
- [135157-5](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID118741636720230727204621.0001): Filter. Honeywell International Inc. · PMA PQ1222NM · Replaces 135157-5 · May 2, 2023
- [107312-2](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID112610372320230727204614.0001): Pneumatic Relay. Honeywell International Inc. · PMA PQ1222NM · Replaces 107312-2 · May 2, 2023
- [102464-30](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID108748994220230727204611.0001): Control. Honeywell International Inc. · PMA PQ1222NM · Replaces 102464-30 · May 2, 2023
- [035A-42401HP](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID134728256720230504143240.0001): Exhaust Duct. Central Texas Aircraft Parts (CTAP) · PMA PQ0880SW · Replaces 035A-42401 · Dec 22, 2022
- [035A-42401HP](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID102771921420230825114322.0001): Exhaust Duct. Central Texas Aircraft Parts (CTAP) · PMA PQ0880SW · Replaces 035A-42401 · Dec 22, 2022
- [MG94A-902-1M](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID197932883820220808113548.0001): Brush, Electrical Contact. Miraj Corporation · PMA PQ0870NE · Replaces 23093-1307 · Jul 28, 2022
- [131004-2](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID153531390320230727204658.0001): Manual. Honeywell International Inc. · PMA PQ1222NM · Replaces 131004-2 · Mar 31, 2022
- [RA068-03300](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID436454334120220208125017.0001): Shim - Insulator. Rapco Inc · PMA PQ2101CE · Replaces 068-03300 · Jan 20, 2022
- [APS68-03300](https://drs.faa.gov/browse/excelExternalWindow/59A6A96FB4AE250A862586290049F16B.0001): Shim, Brake. Aviation Products Systems Inc · PMA PQ3830CE · Replaces 068-03300 · Nov 4, 2020
- [744238-1WE](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID251701465220210611172357.0001): Shaft, Drive. Wencor LLC · PMA PQ1370NM · Replaces 744238-1 · Oct 15, 2020
- [NOHIPOT](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID198024333720240320173406.0001): Decal. Augusta Aero Innovations LLC · PMA PQ04441CE · Replaces 06-201020 · Oct 6, 2020
- [APS068-03300](https://drs.faa.gov/browse/excelExternalWindow/A32F8EBA841374C6862585EC00452418.0001): Shim, Brake. Aviation Products Systems Inc · PMA PQ3830CE · Replaces 068-03300 · Aug 26, 2020
- [TII-24025](https://drs.faa.gov/browse/excelExternalWindow/8BA0C7802BFCDD97862585C200606DDF.0001): Cover - Tab Rod, Rudder Assy.. Test Instrumentation Inc · PMA PQ05428NM · Replaces 010A-24025 · Jun 30, 2020
- [MB6202ZZ](https://drs.faa.gov/browse/excelExternalWindow/D9F727C56198553286258593004DF0BA.0001): Ball Bearing. Miraj Corporation · PMA PQ0870NE · Replaces 6202ZZCEB325 · Jan 26, 2020
- [MB466054](https://drs.faa.gov/browse/excelExternalWindow/C50464F45D19EE1186258593004DF16E.0001): Brush, Electrical Contact. Miraj Corporation · PMA PQ0870NE · Replaces B466054G51 · Jan 26, 2020
- [MB6201ZZ](https://drs.faa.gov/browse/excelExternalWindow/A781BC76CB6636D786258593004DF071.0001): Ball Bearing. Miraj Corporation · PMA PQ0870NE · Replaces 6201ZZCEB325 · Jan 26, 2020

All of them: https://openairdocs.org/model/mitsubishi-mu-2b-36/pma.md

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