# Mitsubishi MU-2B-35

- Type: Aircraft model (FAA registry)
- Registry code: 5780411
- Manufacturer (registry): MITSUBISHI
- Model: MU-2B-35
- Aircraft type: Fixed wing multi engine
- Category: Airplane
- Engines: 2 · Turbo-prop
- Seats: 10
- Weight class: Up to 12,499 lb
- Cruise speed: 147 mph
- Certification: Type certificated
- Data sheet: [TCDS A2PC](https://openairdocs.org/tcds/A2PC) (OpenAirDocs)
- Holder: Mitsubishi Heavy Industries Ltd. 203
- Registered aircraft: 4
- Page: https://openairdocs.org/model/mitsubishi-mu-2b-35

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 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 87-12-02](https://openairdocs.org/ad/87-12-02): Generator Shield Jumper Wires · Mitsubishi Heavy Industries MU-2B-25, MU-2B-26 and MU-2B-35. Effective Jul 3, 1987
- [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 82-08-02](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 81-25-04 R1](https://openairdocs.org/ad/81-25-04-R1): Electrical Wiring Inspection · Mitsubishi Heavy Industries MU-2B-25, MU-2B-26, MU-2B-26A and 4 more. Effective Jan 21, 1982
- [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 74-11-01](https://openairdocs.org/ad/74-11-01): Windshield Outer Panes · Mitsubishi Heavy Industries MU-2B, MU-2B-10, MU-2B-15 and 4 more. Effective Jan 30, 1978
- [AD 76-22-04](https://openairdocs.org/ad/76-22-04): Main Landing Gear · Mitsubishi Heavy Industries MU-2B-30 and MU-2B-35. Effective Nov 15, 1976
- [AD 75-16-13](https://openairdocs.org/ad/75-16-13): Main Wing Flap · Mitsubishi Heavy Industries MU-2B-20, MU-2B-25, MU-2B-30 and 1 more. Effective Aug 5, 1975

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 (4)

- [N129DW](https://openairdocs.org/aircraft/N129DW): [Delta Whiskey Ltd](https://openairdocs.org/faa-owner/DELTA%20WHISKEY%20LTD), [Staten Island, NY](https://openairdocs.org/faa-place/NY/Staten%20Island), built 1974, S/N 653
- [N601SD](https://openairdocs.org/aircraft/N601SD): [Northern Jet Sales LLC](https://openairdocs.org/faa-owner/NORTHERN%20JET%20SALES%20LLC), [Port Saint Lucie, FL](https://openairdocs.org/faa-place/FL/Port%20Saint%20Lucie), built 1973, S/N 610
- [N621TA](https://openairdocs.org/aircraft/N621TA): [Austin Bill DBA](https://openairdocs.org/faa-owner/AUSTIN%20BILL%20DBA), [Sparta, TN](https://openairdocs.org/faa-place/TN/Sparta), S/N 605
- [N910NF](https://openairdocs.org/aircraft/N910NF): [Air 1st Aviation Companies Of Oklahoma Inc](https://openairdocs.org/faa-owner/AIR%201ST%20AVIATION%20COMPANIES%20OF%20OKLAHOMA%20INC), [Tulsa, OK](https://openairdocs.org/faa-place/OK/Tulsa), built 1973, S/N 623

## NTSB investigations (26)

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 DEN06MA119](https://openairdocs.org/ntsb/DEN06MA119), Sep 1, 2006: Mitsubishi MU-2B-35 (N6569L), Argyle, FL, destroyed, 1 fatal. Probable cause: the pilot's inadvertent flight into thunderstorm activity that resulted in the loss of control, design limits of the airplane being exceeded and subsequent in-flight breakup. A contributing factor…
- [NTSB MIA04WA027](https://openairdocs.org/ntsb/MIA04WA027), Nov 3, 2003: Mitsubishi MU-2B-35 (N630HA), Bonaire, NT, substantial damage
- [NTSB MIA02FA084](https://openairdocs.org/ntsb/MIA02FA084), Apr 15, 2002: Mitsubishi MU-2B-35 (N45BS), Carolina, PR, destroyed, 2 fatal. Probable cause: The failure of the pilot to maintain airspeed (Vs) while maneuvering following inadvertent encounter with clouds resulting in an inadvertent stall and uncontrolled descent and subsequent in-flight…
- [NTSB MIA01FA206](https://openairdocs.org/ntsb/MIA01FA206), Aug 1, 2001: Mitsubishi MU-2B-35 (N1VY), Hilton Head, SC, destroyed, 1 fatal. Probable cause: Improper maintenance/installation and and inadequate inspection of the airplane's flap torque tube joints during routine maintenance by company maintenance personnel, which resulted in the right flap…
- [NTSB FTW00LA242](https://openairdocs.org/ntsb/FTW00LA242), Aug 24, 2000: Mitsubishi MU-2B-35 (N770MA), Corsicana, TX, substantial damage. Probable cause: the in-flight separation of the propeller blade, which resulted from intergranular corrosion and fatigue cracking.
- [NTSB MIA95FA226](https://openairdocs.org/ntsb/MIA95FA226), Sep 21, 1995: Mitsubishi MU-2B-35 (N309MA), Smyrna, TN, destroyed. Probable cause: FAILURE OF THE PILOT TO MAINTAIN A PROPER CLIMB RATE AFTER TAKEOFF, AND HIS INADVERTENT ENTRY IN A DESCENDING SPIRAL, WHICH HE FAILED TO CORRECT. FACTORS RELATING TO THE ACCIDENT WERE: DARKNESS, AND…
- [NTSB SEA93FA088](https://openairdocs.org/ntsb/SEA93FA088), Apr 6, 1993: Mitsubishi MU-2B-35 (N96JP), Casper, WY, destroyed, 4 fatal. Probable cause: FAILURE OF THE PILOT TO MAINTAIN PROPER ALTITUDE DURING THE NIGHT IFR APPROACH IN INSTRUMENT METEOROLOGICAL CONDITIONS (IMC).
- [NTSB ANC93LA025](https://openairdocs.org/ntsb/ANC93LA025), Jan 6, 1993: Mitsubishi MU-2B-35 (N900YH), Nome, AK, substantial damage. Probable cause: FUEL STARVATION DUE TO IMPROPER REFUELING PROCEDURES BY THE FBO PERSONNEL, INADEQUATE PREFLIGHT BY THE PILOT, AND RESULTANT ICE IN THE FUEL, WHICH BLOCKED FUEL FLOW TO THE ENGINES. A FACTOR WAS THE…
- [NTSB NYC90LA066](https://openairdocs.org/ntsb/NYC90LA066), Feb 9, 1990: Mitsubishi MU-2B-35 (N533DM), Teterboro, NJ, substantial damage. Probable cause: THE PILOT OF N349MA FAILED TO SEE AND AVOID ANOTHER AIRPLANE TAXIING IN THE SAME DIRECTION.
- [NTSB NYC89FA111](https://openairdocs.org/ntsb/NYC89FA111), Mar 31, 1989: Mitsubishi MU-2B-35 (N638MA), Syracuse, NY, substantial damage. Probable cause: FAILURE OF THE CREW OF BROCKWAY FLIGHT 993 TO SEE-AND-AVOID THE OTHER AIRCRAFT DUE TO THE FIRST OFFICER'S INADEQUATE VISUAL LOOKOUT & THE CAPTAIN'S INADEQUATE SUPERVISION. FACTORS RELATED TO THE…
- [NTSB DCA89LA012](https://openairdocs.org/ntsb/DCA89LA012), Dec 9, 1988: Mitsubishi MU-2J (N296MA), Missing (Pacific Ocean), destroyed, 1 fatal
- [NTSB NYC88LA085](https://openairdocs.org/ntsb/NYC88LA085), Feb 12, 1988: Mitsubishi MU-2B-35 (N339MA), Philadelphia, PA, substantial damage
- [NTSB FTW86MA097](https://openairdocs.org/ntsb/FTW86MA097), Jun 3, 1986: Mitsubishi MU-2B-35 (N8CC), Bartlett, TX, destroyed, 1 fatal
- [NTSB FTW85LA183](https://openairdocs.org/ntsb/FTW85LA183), Apr 15, 1985: Mitsubishi MU2J (N808W), Patterson, LA, substantial damage
- [NTSB FTW85LA067](https://openairdocs.org/ntsb/FTW85LA067), Dec 2, 1984: Mitsubishi MU-2B-35 (N112SK), Robert Lee, TX, substantial damage
- [NTSB DEN82FA008](https://openairdocs.org/ntsb/DEN82FA008), Nov 18, 1981: Mitsubishi MU-2B (N444AR), Eagle, CO, destroyed, 7 fatal
- [NTSB FTW81FA075](https://openairdocs.org/ntsb/FTW81FA075), Apr 19, 1981: Mitsubishi MU-2B (N500GL), Lajitas, TX, destroyed, 2 fatal
- [NTSB CHI81FET04](https://openairdocs.org/ntsb/CHI81FET04), Jan 21, 1981: Mitsubishi MU-2B (N770MA), Wabash, IN, substantial damage
- [NTSB FTW80FA042](https://openairdocs.org/ntsb/FTW80FA042), Feb 14, 1980: Mitsubishi MU-2B (N346MA), Houston, TX, destroyed, 4 fatal
- [NTSB FTW79FPG15](https://openairdocs.org/ntsb/FTW79FPG15), Jan 23, 1979: Mitsubishi MU-2B (N5NW), Searcy, AR, substantial damage
- [NTSB DEN78FA065](https://openairdocs.org/ntsb/DEN78FA065), Aug 25, 1978: Mitsubishi MU-2J (N178MA), Raton, NM, substantial damage, 6 fatal
- [NTSB UNK78X0128](https://openairdocs.org/ntsb/UNK78X0128), Jul 12, 1978: Mitsubishi MU-2 (N19GU), Savnt Lake, Canada, substantial damage
- [NTSB UNK78X0106](https://openairdocs.org/ntsb/UNK78X0106), Feb 12, 1978: Mitsubishi MU2 (N888MA), Neiva, Colombia, destroyed, 5 fatal
- [NTSB FTW78FPA10](https://openairdocs.org/ntsb/FTW78FPA10), Dec 28, 1977: Mitsubishi MU-2J (N245MA), Addison, TX, substantial damage
- [NTSB FTW77FA045](https://openairdocs.org/ntsb/FTW77FA045), Mar 18, 1977: Mitsubishi MU-2B (N777MA), Austin, TX, destroyed, 1 fatal
- [NTSB IAD76AI054](https://openairdocs.org/ntsb/IAD76AI054), Feb 8, 1976: Mitsubishi MU-2B (N300MA), Easton, MD, destroyed, 3 fatal

## FAA accident and incident reports (42)

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 20220327004379I](https://openairdocs.org/incident/20220327004379I), Mar 27, 2022: Mitsubishi MU-2B-35 (N770RW), Hastings, NE, Minor damage. PIC was receiving flight instruction from the SIC during the March 27,2022, flight. Aircraft departed VFR from the lawrence regional airport lawrence, KS,…
- [Incident 20091023051079I](https://openairdocs.org/incident/20091023051079I), Oct 23, 2009: Mitsubishi MU-2B-35 (N400RX), Sioux Falls, SD, Minor damage. Night VFR departure from kfsd to kane. Flaps 5 and gear up. Aircraft struck unseen bird during initial climb out shortly after departure. Auto pilot was…
- [Incident 20080527835119I](https://openairdocs.org/incident/20080527835119I), May 27, 2008: Mtsbsi MU2B35 (N450MA), San Antonio, TX, Minor damage. (-23) Pilot was cleared to land on runway 12L. The pilot was distracted during the items on the checklist and forgot to lower the landing gear. He landed with…
- [Accident 20060901020189A](https://openairdocs.org/incident/20060901020189A), Sep 1, 2006: Mtsbsi MU2B35 (N6569L), Argyle, FL, Destroyed, 1 fatal. (-23) This was an IFR flight from tulsa, ok to panama city, FL. While on descent near Argyle, FL the aircraft entered a level 5 thunderstorm which caused an…
- [Incident 20060628018009I](https://openairdocs.org/incident/20060628018009I), Jun 28, 2006: Mtsbsi MU2B35 (N118P), Newport, AR, Minor damage. (-23) On June 28, 2006, at 1600 central daylight time, a mitsubishi MU23-35 airplane N118P, received minor damage during an emergency landing when the main…
- [Incident 20050321004679I](https://openairdocs.org/incident/20050321004679I), Mar 21, 2005: Mtsbsi MU2B35 (N110MA), Naples, FL, Minor damage. (-23) Pilot inadvertently scratched a fuel truck back with his left wing tip while parking in close quarters area. The wing tip outboard side paint was…
- [Accident 20031103036149A](https://openairdocs.org/incident/20031103036149A), Nov 3, 2003: Mtsbsi MU2B35 (N630HA), Kralendijk, NT, Destroyed. (-23) Pilot supposedly topped off all tanks at Bonaire, netherlan antilles (tncb) for a flight that took him from tncb to aruba (tnca), then to barranquilla,…
- [Accident 20020415014239A](https://openairdocs.org/incident/20020415014239A), Apr 15, 2002: Mtsbsi MU2B35 (N45BS), Caroline, Puerto Rico, No damage, 2 fatal. (-23) On 04/15/02 at 1503 ast inbound from st. croix, usvi to luis munoz marin int'l airport N45BS, s/n 558 a mitsubishi MU-2B-35 aircraft operated by crucian…
- [Accident 20010801023399A](https://openairdocs.org/incident/20010801023399A), Aug 1, 2001: Mtsbsi MU2B35 (N1VY), Hiltonhead, SC, No damage, 1 fatal. (-23) This investigation disclosed that the center wing flap torque tube assembly was installed improperly which resulted in a split flap configuration that…
- [Accident 20000824015709A](https://openairdocs.org/incident/20000824015709A), Aug 24, 2000: Mtsbsi MU2B35 (N770MA), Corsicana, TX, No damage. (-23) On August 24, 2000, at 02:15 CDT, mitsubishi MU-2B-35 airplane N770MA, was on a flight from dallas, TX. To houston, TX., when one of the propeller blades…
- [Incident 20000127000719I](https://openairdocs.org/incident/20000127000719I), Jan 27, 2000: Mtsbsi MU2B35 (N5AP), Covington/Cinci, KY, Minor damage. (-23) On January 27, 2000 at approximately 0805 utl, gail force flt #404 was taxiing onto the ramp for parking when the aircraft encountered a patch of ice.…
- [Incident 19990610027089I](https://openairdocs.org/incident/19990610027089I), Jun 10, 1999: Mtsbsi MU2B35 (N755MA), Seminole, OK, Minor damage. The crew failed to lower landing gear. The PIC thought he saw green lights during final check.
- [Incident 19960503013809I](https://openairdocs.org/incident/19960503013809I), May 3, 1996: Mtsbsi MU2B35 (N637WG), Memphis, TN, Minor damage. Narrative: pilot stated that after landing on runway 270 and was taxiing on to the ramp area between a row of parked aircraft's he taxied into an APU that was…
- [Accident 19950921029709A](https://openairdocs.org/incident/19950921029709A), Sep 21, 1995: Mtsbsi MU2B35 (N309MA), Smyrna, TN, Destroyed. Lost control on night VFR climb into foggy dark night. Departed VFR. No clearance. Spatial disorientation indicated
- [Accident 19930406007999A](https://openairdocs.org/incident/19930406007999A), Apr 6, 1993: Mtsbsi MU2B35 (N96JP), Casper, WY, Destroyed, 4 fatal. Descended below glide slope interception altitude. Struck top ridgeline and broke up. Had minimal recent IFR time.
- [Accident 19930105002509A](https://openairdocs.org/incident/19930105002509A), Jan 5, 1993: Mtsbsi MU2B35 (N900YH), Nome, AK, Substantial damage. Lost power both engines. Landed on sea ice. Hit pressure ridge. Water ice in fuel. No prist added or sumps drained.
- [Incident 19911203057779I](https://openairdocs.org/incident/19911203057779I), Dec 3, 1991: Mtsbsi MU2B35 (N339MA), Providence, RI. Landed with gear up. Main landing gear doors were frozen closed.
- [Incident 19900209001789I](https://openairdocs.org/incident/19900209001789I), Feb 9, 1990: Mtsbsi MU2B35 (N533DM), Teterboro, NJ, Minor damage. Aircraft was struck from behind by N349MA while taxiing on taxiway.
- [Accident 19890331010281A](https://openairdocs.org/incident/19890331010281A), Mar 31, 1989: Mtsbsi MU2B35 (N638MA), Syracuse, NY, Substantial damage. On taxi for takeoff failed to see and avoid N7254R that was entering taxiway without clearance.
- [Accident 19880212002659A](https://openairdocs.org/incident/19880212002659A), Feb 12, 1988: Mtsbsi MU2B35 (N339MA), Philadelphia, PA, Substantial damage. Left wing wrinkled by stress. Had cracked spur from prior hard landings.
- [Incident 19871027065829I](https://openairdocs.org/incident/19871027065829I), Oct 27, 1987: Mtsbsi MU2B35 (N375CA), Fresno, CA. The gear failed to lower for landing emergency extension used. A broken wire was found at the gear down solenoid.
- [Incident 19870516033879I](https://openairdocs.org/incident/19870516033879I), May 16, 1987: Mtsbsi MU2B35 (N503AA), Shreveport, LA, Minor damage. Loud pop heard with gear extension. Unsafe gear indication. Nose gear partially extended. Found a broken bracket.
- [Incident 19860913046459I](https://openairdocs.org/incident/19860913046459I), Sep 13, 1986: Mtsbsi MU2B35 (N96JP), Valentine, NE. Air recycling machine failed causing smoke in cabin. Pilot made precautionary landing.
- [Accident 19860602024669A](https://openairdocs.org/incident/19860602024669A), Jun 2, 1986: Mtsbsi MU2B35 (N8CC), Bartlett, TX, Destroyed. The pilot reported an autopilot problem before ground impact. Suspect elevator trim servo malfunction.
- [Incident 19860529030349I](https://openairdocs.org/incident/19860529030349I), May 29, 1986: Mtsbsi MU2B35 (N503AA), Aurora, IL. Power lever split during climb. During descent, engine was shut down and a diversion made. Faulty fuel controller.
- [Incident 19860321014479I](https://openairdocs.org/incident/19860321014479I), Mar 21, 1986: Mtsbsi MU2B35 (N96JP), Omaha, NE, Minor damage. Both nose tires blew out following vibration on rollout. Nose gear torque arm was improperly connected after tow.
- [Incident 19851225069189I](https://openairdocs.org/incident/19851225069189I), Dec 25, 1985: Mtsbsi MU2B35 (N490MA), Portland, ME. Aircraft veered into snowbank during rollout. No discrepancies found in nose wheel steering.
- [Incident 19851011064349I](https://openairdocs.org/incident/19851011064349I), Oct 11, 1985: Mtsbsi MU2B35 (N289MA), Kansas City, MO. Unsafe gear indication. Made manual extension. Both generators had failed. Landed normally.
- [Accident 19850414014549A](https://openairdocs.org/incident/19850414014549A), Apr 14, 1985: Mtsbsi MU2B35 (N808W), Patterson, LA, Substantial damage. Aircraft landed on waterway at night. Pilot mistook brighter lights for paved runway. Ground fog a factor.
- [Accident 19841201065369A](https://openairdocs.org/incident/19841201065369A), Dec 1, 1984: Mtsbsi MU2B35 (N112SK), Robert Lee, TX, Substantial damage. Landed beside runway to avoid deer. Nose gear collapsed. Deer warning on chart for the unlighted field.
- [Incident 19831127073089I](https://openairdocs.org/incident/19831127073089I), Nov 27, 1983: Mtsbsi MU2B35 (N298MA), Tulsa, OK, Substantial damage. Both engines flamed out on final. Restarted and landed. Nose cowl anti ice system disconnected. Bad circuit breaker
- [Accident 19811118089809A](https://openairdocs.org/incident/19811118089809A), Nov 18, 1981: Mtsbsi MU2B35 (N444AR), Eagle, CO, Destroyed, 5 fatal. Struck trees on mountain in premature IFR descent possibly began due to aircrafts low fuel status and IMC weather.
- [Accident 19810419017619A](https://openairdocs.org/incident/19810419017619A), Apr 19, 1981: Mtsbsi MU2B35 (N500GL), Lajitas, TX, Destroyed, 1 fatal. Failed to climb on downwind. Flaps up takeoff. Struck wires off end of runway. Insufficient runway for conditions.
- [Accident 19810121001189A](https://openairdocs.org/incident/19810121001189A), Jan 21, 1981: Mtsbsi MU2B26A (N770MA), Wabash, IN, Substantial damage. Right wing stalled on level-off on landing. Side load impact failed right main wheel. Plane veered into snowbank.
- [Incident 19800305029479I](https://openairdocs.org/incident/19800305029479I), Mar 5, 1980: Mtsbsi MU2B35 (N113SD), Kerrville, TX, Minor damage. As aircraft reached 90 knots, a deer ran onto the runway in front of the aircraft. Landing gear struck deer.
- [Accident 19800214002929A](https://openairdocs.org/incident/19800214002929A), Feb 14, 1980: Mtsbsi MU2B35 (N346MA), Houston, TX, Destroyed, 3 fatal. Too low on final IFR approach. Struck trees short of runway.
- [Accident 19790123001399A](https://openairdocs.org/incident/19790123001399A), Jan 23, 1979: Mtsbsi MU2B35 (N5NW), Searcy, AK, Substantial damage. Pilot witness stated the acft overshot the rwy during an attempt at runway realignment.
- [Accident 19780825042449A](https://openairdocs.org/incident/19780825042449A), Aug 25, 1978: Mtsbsi MU2B35 (N178MA), Raton, NM, Destroyed, 5 fatal. Recovery date 08/27/78.alcohol 64 mg from lungtissue,54 mg frastric contents.
- [Incident 19780110002429I](https://openairdocs.org/incident/19780110002429I), Jan 10, 1978: Mtsbsi MU2/ (N776CC), Jackson, MS, Minor damage. Nose gear collapsed on roll out. Actuator bracket had failed.
- [Accident 19771228043149A](https://openairdocs.org/incident/19771228043149A), Dec 28, 1977: Mtsbsi MU2B35 (N245MA), Addison, TX, Substantial damage. Aircraft struck approach light stanchion.
- [Accident 19770318007649A](https://openairdocs.org/incident/19770318007649A), Mar 18, 1977: Mtsbsi MU2B35 (N777MA), Austin, TX, Destroyed
- [Accident 19760208009639A](https://openairdocs.org/incident/19760208009639A), Feb 8, 1976: Mtsbsi MU2B35 (N300MA), Easton, MD, Destroyed, 2 fatal. Black smoke obsvd followed by a stall departure to the l.acft abt 150 ft AGL aprx 200 ft l of rwy.

## Service difficulty reports (53, newest 50)

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

- [SDR OXKA856K](https://openairdocs.org/sdr/OXKA856K), Jan 15, 2010: FUEL CONTROL. MALFUNCTIONED. RT ENGINE FUEL CONTROL MALFUNCTION. NO POWER LEVER RESPONSE ON THE RT ENGINE. COULD NOT REDUCE BELOW 900 DEG C. DIVERTED. ON APPROACH , SHUTDOWN ENGINE AND LAND
- [SDR BKAA200710004](https://openairdocs.org/sdr/BKAA200710004), Nov 15, 2007: OIL TANK. CRACKED. OIL TANK CRACKED.
- [SDR BKAA200710001](https://openairdocs.org/sdr/BKAA200710001), Aug 27, 2007: ACM. SEIZED. AIR CYCLE MACHINE TURBINE SEIZED UP CAUSING SMOKE IN THE COCKPIT. THE AIR CYCLE MACHINE REQUIRED REPLACEMENT.
- [SDR 2007F00006](https://openairdocs.org/sdr/2007F00006), Dec 26, 2006: CLAMP. CRACKED. CRACK WAS FOUNDING STARTING AT THE DOWL PIN HOLE OF THE BLADE CUFF.
- [SDR OXK2006F00000](https://openairdocs.org/sdr/OXK2006F00000), Feb 15, 2006: GEARSHAFT. FAILED. ENGINE, SN P20186, EXPERIENCED AN UN-COMMANDED INFLIGHT SHUTDOWN, ON SITE INSPECTION REVEALED THAT THE FUEL PUMP DRIVE TRAIN HAD BECOME UNCOUPLED. TEARDOWN INSP
- [SDR AALA20031479](https://openairdocs.org/sdr/AALA20031479), Dec 28, 2003: BATTERY PACK. DISCHARGED. ATL DURING OVERNIGHT MAINTENANCE FOUND EXIT SIGN ABOVER EMERGENCY EXIT DOOR ROW 21 INOPERATIVE. REPLACED BATTERY PACK FOR EXIT SIGN. SYSTEM GROUND CHECKED NORMA
- [SDR HMN2002F00003](https://openairdocs.org/sdr/HMN2002F00003), Jun 10, 2002: CONTROL CABLE. FRAYED. FRAYED LT ENGINE POWER LEVER CABLE FOUND DURING ROUTINE 100 HOUR INSPECTION. FRAYED PORTION UNDER CENTER PEDESTAL IN COCKPIT. (SW15200210206)
- [SDR HMN2002F00002](https://openairdocs.org/sdr/HMN2002F00002), May 30, 2002: CONTROL CABLE. FRAYED. FRAYED THROTTLE CABLE FOUND DURING ROUTINE 100 HOUR INSPECTION. FRAYED PORTION IN AFT FUSELAGE ON A 90 DEGREE TURN PULLEY. FOUND AND REPLACED.
- [SDR HMN2002F00001](https://openairdocs.org/sdr/HMN2002F00001), May 30, 2002: CONTROL CABLE. FRAYED. FRAYED CABLE FOUND DURING ROUTINE 100 HOUR INSPECTION. FRAYED PORTION IN AFT FUSELAGE ON A 90 DEGREE TURN PULLEY. FOUND AND REPLACED. (SW15200209702)
- [SDR HMN2002F00000](https://openairdocs.org/sdr/HMN2002F00000), May 30, 2002: CONTROL CABLE. BROKEN. ON ENGINE SHUTDOWN, PILOT COULD NOT BRING LEFT PROP BACK ON LOCKS. INSPECTION FOUND LEFT ENGINE POWER LEVER CONTROL CABLE BROKEN BELOW CENTER PEDISTAL IN COCKPI
- [SDR 2002FA0000750](https://openairdocs.org/sdr/2002FA0000750), May 21, 2002: CONTROL CABLE. FRAYED. DURING INSPECTION IN THE AFT FUSELAGE FOUND ONE OF THE ENGINE CONTROL CABLES FRAYED WHERE THE CABLE GOES OVER A PULLEY AND TURNS 90 DEGREES. THIS IS THE 2ND OF 
- [SDR 2002FA0000749](https://openairdocs.org/sdr/2002FA0000749), Mar 26, 2002: CONTROL CABLE. FRAYED. DURING ROUTINE MAINTENANCE FOUND A FRAYED ENGINE CONTROL CABLE. THE FRAYED PORTION WAS LOCATED IN THE AFT FUSELAGE WHERE THE CABE GOES OVER A 90DEGREE TURN PULL
- [SDR KBMA88674](https://openairdocs.org/sdr/KBMA88674), Jul 16, 2001: IGNITER. INTERMITTENT. IGNITER - REPORTED TO BE INTERMITTENT. REMOVED AND REPLACED WITH NEW IGNITER.
- [SDR 20010409CW019](https://openairdocs.org/sdr/20010409CW019), Mar 1, 2001: CONTROL CABLE. SEPARATED. CABLE SEPARATED AT A 90 DEGREE TURN OVER PULLEY IN AFT TAIL CONE AREA
- [SDR CA001103006](https://openairdocs.org/sdr/CA001103006), Oct 26, 2000: LIMIT SWITCH. FAILED. (CAN) DURING APPROACH FOR LDG AT PRINCE GEORGE, BC, CREW SELECTED GEAR DOWN & FWD GEAR DOORS OPENED ABOUT 1/2 WAY THEN STOPPED. CREW OPENED LDG GEAR CONTOL CCT 
- [SDR 20001101SH003](https://openairdocs.org/sdr/20001101SH003), Sep 6, 2000: BLADE. BROKEN. AIRCRAFT AT CRUISE, ALT 11,000 FEET, NR 1 PROPELLER BLADE BROKE APPROXIMATELY 10 INCHES FROM HUB ON NR 2 ENGINE. BLADE DID NOT CONTACT AIRCRAFT. DAMAGE TO COWLI
- [SDR CA000905002](https://openairdocs.org/sdr/CA000905002), Aug 22, 2000: TUBE. CRACKED. (CAN) THE ENGINE WAS SHUTDOWN IN FLIGHT AS A PRECAUTION DUE TO AN OIL LEAK AND LOW OIL PRESSURE. ONCE ON THE GROUND, THE SOURCE OF THE OIL LEAK COULD NOT POSITI
- [SDR CA000614005](https://openairdocs.org/sdr/CA000614005), Jun 7, 2000: NUT. LOOSE. (CAN) INVESTIGATION REVEALED THE P/N 016A-43298 LT-RT THREADED ADJUSTMENT ROD ON THE POWER LEVER ATTACHMENT TO THE ENGINE, HAD COME LOOSE AND HAD MOVED, CAUSING
- [SDR CA000120008](https://openairdocs.org/sdr/CA000120008), Jan 18, 2000: SWITCH. BROKEN. (CAN) DURING APPROACH, THE CREW SELECTED GEAR DOWN AND FAILED TO GET A GREEN LIGHT FOR THE NOSE GEAR, THE UNSAFE LIGHT WAS NOT ILLUMINATED. AFTER A TOWER FLYBY 
- [SDR 2000ZZZX25](https://openairdocs.org/sdr/2000ZZZX25), Jan 4, 2000: FITTING. BROKEN. FOUND BROKEN PART ON RAMP. INSPECTED AIRCRAFT ON RAMP AND NO PROBLEM FOUND. CALLED OUT STATION AND FOUND THE AIRCRAFT IN DALLAS HAD THE BROKEN FITTING ASSY. GRO
- [SDR 99ZZZX3911](https://openairdocs.org/sdr/99ZZZX3911), Sep 24, 1999: LOCK. WORN. PROPELLER HAS NEW STYLE BLADE LOCKS. COTTERPIN THAT HOLDS SPRING AND LOCK IN ASSEMBLY IS FAILING OR WEARING OUT THE HOLES IN HOUSING.
- [SDR 99ZZZX939](https://openairdocs.org/sdr/99ZZZX939), Feb 12, 1999: BOLT. DAMAGED. DURING 150-HOUR INSPECTION ON BOTH PROPELLERS, THE PROPELLER STOP LOCK BOLTS ON ALL PROP BLADES WERE FOUND CHAFING ON THE BLADE STOP PLATES. REMOVED ALL 6 BOLTS
- [SDR 99ZZZX924](https://openairdocs.org/sdr/99ZZZX924), Jan 13, 1999: HARNESS. DAMAGED. FOUND FIRE DETECT CABLE GROUNDED DUE TO CONDITION OF CABLE, CHANGE CABLE BEFORE REACHING SAME CONDITON. THE RIGHT ENGINE'S, P-20199, FIRE LIGHT CAME ON IN-FLIGH
- [SDR 98ZZZX4689](https://openairdocs.org/sdr/98ZZZX4689), Nov 20, 1998: WINDOW. CRACKED. DURING FLIGHT, MAIN CABIN DOOR WIDOW CRACKED. CRACK STARTED ALONG EDGE OF PAIN PARALLEL TO OPENING JUST UNDER SEAL.
- [SDR 99ZZZX176](https://openairdocs.org/sdr/99ZZZX176), Sep 23, 1998: SWITCH. MALFUNCTIONED. WITH AIR CONDITIONER ON AUTO, PILOT GOT COOL AND TURNED MANUAL HOT SWITCH ON AND LEFT IT THERE. THIS CAUSED EXCESS HEAT IN AIR DUCTS AND HIGH CONDENSATION. PILO
- [SDR 98ZZZX3623](https://openairdocs.org/sdr/98ZZZX3623), Sep 1, 1998: PUMP. FAILED. AT LANDING PILOT NOTICED OIL PRESSURE LOW. DURING TAXI, PILOT SHUT ENGINE DOWN. MAINTENANCE FOUND ENGINE WOULD NOT TURN BY PROP MOVEMENT. ENGINE WAS REMOVED AND
- [SDR CA980602013](https://openairdocs.org/sdr/CA980602013), May 12, 1998: LINE. CRACKED. (CAN) ON SHORT FINAL, WHILE DOING PRE-LANDING CHECK, THE CREW NOTICED OIL ON THE RIGHT ENGINE COWL. NORMAL LANDING CARRIED OUT. INVESTIGATION REVEALED A CRACKED
- [SDR CA980317020](https://openairdocs.org/sdr/CA980317020), Mar 13, 1998: ACTUATOR. FAILED. (CAN) OVERHAULED GEAR DOOR ACTUATOR INSTALLED TO RECTIFY A PREVIOUS PROBLEM. GROUND TEST OK. TEST FLIGHT FORWARD GEAR DOORS FAILED TO OPEN AND GEAR MANUALLYLOWE
- [SDR CA980317019](https://openairdocs.org/sdr/CA980317019), Mar 12, 1998: ACTUATOR. FAILED. (CAN) DURING DEPARTURE THE FORWARD GEAR DOORS WOULD NOT OPEN, PREVENTING GEAR RETRACTION. INVESTIGATION FOUND THE FORWARD GEAR DOOR ACTUATOR WAS DEVELOPING INSU
- [SDR 99ZZZX267](https://openairdocs.org/sdr/99ZZZX267), Jan 11, 1998: CREW DOOR. SEPARATED. CREW HATCH/EMERGENCY ESCAPE DOOR DEPARTED THE AIRCRAFT DURING CLIMB.
- [SDR CA970702001](https://openairdocs.org/sdr/CA970702001), Jun 25, 1997: INSULATOR. MISSING. (CAN) ON LANDING, THE LEFT ENGINE FIRE WARNING LIGHT ILLUMINATED. INVESTGATION FOUND NO FIRE, BUT REVEALED A MISSING INSULATOR INSIDE THE BULKHEAD CONNECTOR. SU
- [SDR CA970401005](https://openairdocs.org/sdr/CA970401005), Mar 27, 1997: ACTUATOR. FROZEN. (CAN) ON APPROACH, CREW SELECTED GEAR DOWN, FOLLOWING A MINUS 35 DEGREE TEMPERATURE CRUISE, AND NOTHING HAPPENED. GEAR SELECTED DOWN BY EMERGENCY EXTENSION. THE
- [SDR CA970421001](https://openairdocs.org/sdr/CA970421001), Feb 28, 1997: MOTOR. INTERMITTENT. (CAN) CREW NOTED THE GEAR WOULD NOT FULLY RETRACT. GEAR SWINGS BY MAINTENANCE FOUND THE MOTOR RAN SLOWLY. INSPECTION OF THE MOTOR FOUND ONE OF THE BRUSHES STUCK
- [SDR CA970226002](https://openairdocs.org/sdr/CA970226002), Feb 21, 1997: BULL GEAR. FAILED. (CAN) DURING CRUISE, THE RIGHT HAND ENGINE SUDDENLY FEATHERED. ENGINE SECURED. INSPECTION FOUND THAT THE BULL GEAR HAD FAILED EITHER IN THE GEAR TOOTH BASE AND/
- [SDR 97ZZZX495](https://openairdocs.org/sdr/97ZZZX495), Jan 8, 1997: CASTING. EAR BROKEN. AT 100 HR INSP, LANDING GEAR THRUST GEAR BOX CASTING MOUNT EAR WAS FOUND BROKEN AND MOUNT BOLTS LOOSE. SUSPECT CAUSE TO BE SHIM SPACERS USED BETWEEN BOX AND AIR
- [SDR CA961205011](https://openairdocs.org/sdr/CA961205011), Nov 28, 1996: GEAR DOOR. FROZEN. (CAN) ICE CONTAMINATION IN THE GEAR DOOR ACTUATOR CAUSED THE PILOT ABORT THE APPROACH. SUBSEQUENT CYCLING OF THE GEAR PRODUCED A GEAR DOWN AND LOCKED CONDITION 
- [SDR CA961128010](https://openairdocs.org/sdr/CA961128010), Nov 26, 1996: SWITCH. FROZEN. (CAN) ON APPROACH WHEN GEAR SELECTED DOWN, NO RESPONSE. GEAR LOWERED MANUALLY. IT IS ASSUMED THAT THE NOSE GEAR DOWN LOCK SWITCH HAD PICKED UP WATER CONTAMINATI
- [SDR CA961203001](https://openairdocs.org/sdr/CA961203001), Nov 6, 1996: SWITCH. BROKEN WIRE. (CAN) DURING APPROACH THE PILOT COULD NOT GET AN INDICATION OF THE NOSE GEAR DOWN AND LOCKED. EMERGENCY EXTENSION PERFORMED AND THE AIRCRAFT LANDED SAFELY. MAIN
- [SDR CA970130004](https://openairdocs.org/sdr/CA970130004), Nov 5, 1996: SWITCH. WIRE BROKEN. (CAN) ON APPROACH THE CREW WERE UNABLE TO GET A GREEN LIGHT ON THE NOSE GEAR. THE SYSTEM WAS CYCLED AND A SUCCESSFUL LANDING WAS MADE. INVESTIGATION REVEALED A 
- [SDR CA961113002](https://openairdocs.org/sdr/CA961113002), Nov 5, 1996: WIRE. BROKEN. (CAN) ON APPROACH WHEN GEAR SELECTED DOWN, DID NOT GET A GREEN LIGHT ON THE NOSE GEAR. GEAR CYCLED WITH NO CHANGE. EMERGENCY EXTENSION USED. INVESTIGATION REVEA
- [SDR 96ZZZX5619](https://openairdocs.org/sdr/96ZZZX5619), Oct 15, 1996: CONTROL CABLE. FAILED. DURING ROUTINE 500-HOUR INSPECTION, FLAPS WERE OPERATED TO VERIFY PROPER FUNCTION. DURING OPERATION, A 'POP' WAS HEARD AND THE LEFT OUTBOARD FLAP WAS NO LONGER 
- [SDR CA960924009](https://openairdocs.org/sdr/CA960924009), Sep 18, 1996: UNFEATHER SWITCH. STUCK ON. (CAN) DURING TAKEOFF ROLL, CREW NOTED THE LEFT ENGINE BETA LIGHT DID NOT EXTINGUISH WHEN THE RIGHT WENT OUT. WHEN THE ENGINES ENTERED PROPELLER GOVERNING MODE I
- [SDR CA960909001](https://openairdocs.org/sdr/CA960909001), Sep 5, 1996: RELAY. BURNT CONTACTS. (CAN) THE CREW SELECTED 20 DEGREES FOR FLAPS AND NOTED THE SETTING GOING TO 40 DEGREES. A CIRCUIT WAS CARRIED OUT AND THE AIRCRAFT LANDED WITHOUT FURTHER INCIDE
- [SDR 96ZZZX2112](https://openairdocs.org/sdr/96ZZZX2112), Mar 7, 1996: PILOT TUBE. CRACKED. LONGITUDINAL CRACKS FOUND IN PILOT TUBE OF NR 3 SPIDER ARM.
- [SDR 96ZZZX2111](https://openairdocs.org/sdr/96ZZZX2111), Mar 7, 1996: PILOT TUBE. CRACKED. LONGITUDINAL CRACKS FOUND IN PILOT TUBE OF NR 2 SPIDER ARM.
- [SDR 96ZZZX2110](https://openairdocs.org/sdr/96ZZZX2110), Mar 7, 1996: LINK ARM. CRACKED. PROPELLER LINK ARM IS CRACKED BETWEEN HOLES IN LINK ARM.
- [SDR 96ZZZX2109](https://openairdocs.org/sdr/96ZZZX2109), Mar 7, 1996: BRACKET. CRACKED. PROPELLER INSPECTION FOUND 2 EACH START LOCK BRACKETS CRACKED.
- [SDR 96ZZZX2108](https://openairdocs.org/sdr/96ZZZX2108), Mar 7, 1996: COUNTERWEIGHT. CRACKED. PROPELLER COUNTERWEIGHT DOWEL PIN HOLE IS CRACKED.
- [SDR AU960125](https://openairdocs.org/sdr/AU960125), Feb 1, 1996: OIL SYSTEM. CONTAM-METAL. (AUS) RH ENGINE OIL SYSTEM METAL CONTAMINATION
- [SDR CA951122001](https://openairdocs.org/sdr/CA951122001), Nov 15, 1995: FCU. FAILED. (CAN) DURING TAXI FOR TAKEOFF, THE RIGHT HAND ENGINE EXPERIENCED AN UNCOMMANDED INCREASE IN POWER OUTPUT TOWARD MAXIMUM. THE CREW SHUTDOWN THE ENGINE WITH EMERG

All 53: https://openairdocs.org/model/mitsubishi-mu-2b-35/reports.md

## STCs that may be installed (OpenAirDocs) (198, 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 SA1257SW](https://openairdocs.org/stc/SA1257SW): Seat arrangement and other interior installations. 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 SA1443SW](https://openairdocs.org/stc/SA1443SW): Modification of pilot and copilot seats. 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 SA1544SW](https://openairdocs.org/stc/SA1544SW): Installation of AVQ-55 weather radar. 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 SA1616SW](https://openairdocs.org/stc/SA1616SW): Installation of Sperry AA-210 radar altimeter 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 SA1805SW](https://openairdocs.org/stc/SA1805SW): Installation of Foxboro fuel flow signal conditioning unit PC-260. 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 SA1857SW](https://openairdocs.org/stc/SA1857SW): Installation of B.F. Goodrich type 25S de-ice boot. 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 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

All 198: https://openairdocs.org/model/mitsubishi-mu-2b-35/stcs.md

## PMA parts (OpenAirDocs) (429, 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
- [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
- [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
- [MB922162](https://drs.faa.gov/browse/excelExternalWindow/5CF0254992554F6C86258593004DF121.0001): Brush, Electrical Contact. Miraj Corporation · PMA PQ0870NE · Replaces 922162 · Jan 26, 2020
- [MBR4AZZ](https://drs.faa.gov/browse/excelExternalWindow/5BE9530A5163532786258593004DF0F1.0001): Ball Bearing. Miraj Corporation · PMA PQ0870NE · Replaces R4AAZZMC3B32S · Jan 26, 2020

All of them: https://openairdocs.org/model/mitsubishi-mu-2b-35/pma.md

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OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.