# Mitsubishi MU-2B-36A

- Type: Aircraft model (FAA registry)
- Registry code: 5780413
- Manufacturer (registry): MITSUBISHI
- Model: MU-2B-36A
- Aircraft type: Fixed wing multi engine
- Category: Airplane
- Engines: 2 · Turbo-prop
- Seats: 10
- Weight class: Up to 12,499 lb
- Certification: Type certificated
- Data sheet: [TCDS A10SW](https://openairdocs.org/tcds/A10SW) (OpenAirDocs)
- Holder: Mitsubishi Heavy Industries Ltd.
- Registered aircraft: 10
- Page: https://openairdocs.org/model/mitsubishi-mu-2b-36a

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 2006-14-08](https://openairdocs.org/ad/2006-14-08): Flight idle blade angles · Mitsubishi Heavy Industries MU-2B-26A, MU-2B-36A, MU-2B-40 and 1 more. Effective Aug 21, 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 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 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 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 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

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 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

## 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 (10)

- [N222FA](https://openairdocs.org/aircraft/N222FA): [Express Aviation Management LLC](https://openairdocs.org/faa-owner/EXPRESS%20AVIATION%20MANAGEMENT%20LLC), [Dover, DE](https://openairdocs.org/faa-place/DE/Dover), S/N 714SA
- [N24WC](https://openairdocs.org/aircraft/N24WC): [Dach Capital Holdings Inc](https://openairdocs.org/faa-owner/DACH%20CAPITAL%20HOLDINGS%20INC), [Newark, DE](https://openairdocs.org/faa-place/DE/Newark), S/N 705SA
- [N32EC](https://openairdocs.org/aircraft/N32EC): [Alan H Brodine Dmd Pc](https://openairdocs.org/faa-owner/ALAN%20H%20BRODINE%20DMD%20PC), [Rochester, NY](https://openairdocs.org/faa-place/NY/Rochester), built 1977, S/N 699SA
- [N61BA](https://openairdocs.org/aircraft/N61BA): [Unlimited Boat Sales Inc](https://openairdocs.org/faa-owner/UNLIMITED%20BOAT%20SALES%20INC), [Page, AZ](https://openairdocs.org/faa-place/AZ/Page), built 1978, S/N 729SA
- [N718EE](https://openairdocs.org/aircraft/N718EE): [N718ee LLC](https://openairdocs.org/faa-owner/N718EE%20LLC), [Missoula, MT](https://openairdocs.org/faa-place/MT/Missoula), built 1978, S/N 718SA
- [N7601L](https://openairdocs.org/aircraft/N7601L): [Jci Aviation Inc](https://openairdocs.org/faa-owner/JCI%20AVIATION%20INC), [Canadian, TX](https://openairdocs.org/faa-place/TX/Canadian), S/N 697SA
- [N777LP](https://openairdocs.org/aircraft/N777LP): [Grace On Wings Inc](https://openairdocs.org/faa-owner/GRACE%20ON%20WINGS%20INC), [Indianapolis, IN](https://openairdocs.org/faa-place/IN/Indianapolis), S/N 719SA
- [N895MA](https://openairdocs.org/aircraft/N895MA): [Top Tier Truck And Trailer LLC](https://openairdocs.org/faa-owner/TOP%20TIER%20TRUCK%20AND%20TRAILER%20LLC), [Dalhart, TX](https://openairdocs.org/faa-place/TX/Dalhart), S/N 723SA
- [N89DR](https://openairdocs.org/aircraft/N89DR): [N89dr LLC](https://openairdocs.org/faa-owner/N89DR%20LLC), [Lowell, AR](https://openairdocs.org/faa-place/AR/Lowell), built 1978, S/N 713SA
- [N9NB](https://openairdocs.org/aircraft/N9NB): [Siebette Aviation LLC](https://openairdocs.org/faa-owner/SIEBETTE%20AVIATION%20LLC), [Hendersonville, TN](https://openairdocs.org/faa-place/TN/Hendersonville), built 1978, S/N 728SA

## NTSB investigations (2)

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 SEA96MA043](https://openairdocs.org/ntsb/SEA96MA043), Jan 15, 1996: Mitsubishi MU-2B-36 (N693PA), Malad City, ID, destroyed, 8 fatal. Probable cause: continued flight by the flightcrew into icing conditions with known faulty deice equipment; structural (airframe) ice; and failure of the flight crew to maintain adequate airspeed, which resulted in…
- [NTSB LAX91FA280](https://openairdocs.org/ntsb/LAX91FA280), Jun 29, 1991: Mitsubishi MU-2B-36A (N2CJ), Goleta, CA, destroyed, 4 fatal. Probable cause: THE PILOT'S FAILURE TO MAINTAIN DIRECTIONAL CONTROL OF THE AIRPLANE AFTER BECOMING SPATIALLY DISORIENTED. FACTORS RELATED TO THE ACCIDENT WERE: DARKNESS, LOW OVERCAST CLOUD CONDITION, THE PILOT'S…

## FAA accident and incident reports (6)

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 20200227001289I](https://openairdocs.org/incident/20200227001289I), Feb 27, 2020: Mitsubishi MU-2B-36A (N9NB), New Bern, NC, Minor damage. While on an instrument flight plan from ewn to opf with 2 souls aboard, during climb phase at approximately 12,000?, approximately 60 miles sw of ewn, a bird…
- [Accident 19960115000389A](https://openairdocs.org/incident/19960115000389A), Jan 15, 1996: Mtsbsi MU2B36A (N693PA), Malad City, ID, Destroyed, 8 fatal. Declared emergency. ATC lost contact. Dived in, crashed and burned. Icy conditions. Poor maintained.
- [Incident 19930205003589I](https://openairdocs.org/incident/19930205003589I), Feb 5, 1993: Mtsbsi MU2B36A (N338CM), Gary, IN, Minor damage. Lost pressurization at level off. Rapid descent and returned. Cabin window on . Left side had failed.
- [Accident 19910628025069A](https://openairdocs.org/incident/19910628025069A), Jun 28, 1991: Mtsbsi MU2B36A (N2CJ), Santa Barbara, CA, Destroyed, 4 fatal. On VOR approach,no clearance,came through clouds close to airliner on IFR clearance. Stalled. Dived into ocean.
- [Incident 19870505022839I](https://openairdocs.org/incident/19870505022839I), May 5, 1987: Mtsbsi MU2B36A (N892MA), Tivoli, TX. The pilot made a precautionary landing due to suspected fire. Cargo was found to be loaded near main heating outlet
- [Incident 19870224025129I](https://openairdocs.org/incident/19870224025129I), Feb 24, 1987: Mtsbsi MU2B36A (N892MA), Mc Allen, TX, Minor damage. The aircraft landed with the wheels retracted. Pilot was directed to circle to another runway and became distracted

## Service difficulty reports (20)

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

- [SDR 2009FA0000713](https://openairdocs.org/sdr/2009FA0000713), Aug 14, 2009: WINDOW. CRACKED. PILOT COMPLAINED OF LOSS OF PRESSURIZATION IN FLIGHT AND UNABLE TO MAINTAIN SUFFICIENT CABIN PRESSURE TO SUSTAIN FLIGHT AT HIGHER ALTITUDES. RT CABIN WINDOW FWD
- [SDR 2008FA0000571](https://openairdocs.org/sdr/2008FA0000571), Jul 22, 2008: CONTROL CABLE. BROKEN. PILOT COMPLAINED OF POOR ELEVATOR TRIM OPS. UPON INSP, FOUND ELEVATOR TRIM CABLE 311AS-14-7245 BROKEN (RT CABLE). 311AS-14-7362 (LT CABLE), 010A-61179-81 (RT AF
- [SDR 2007FA0000100](https://openairdocs.org/sdr/2007FA0000100), Dec 4, 2006: ROD END. BROKEN. DURING GEAR EXTENSION FOR LANDING, A LOUD BANG WAS NOTICED BY THE PIVOT AND UNSAFE LIGHT STAYED ON. AIRCRAFT WAS ROUTED TO MAINTENANCE AFTER LANDING. MAINTENANC
- [SDR CA060523005](https://openairdocs.org/sdr/CA060523005), May 16, 2006: NUT. CRACKED. WHILE CARRYING OUT A WINGS OFF INSPECTION AND COMPLYING WITH SERVICE BULLETIN 103/57-004 WING ATTACHMENT HARDWARE. INSPECTION, THE RT LOWER FORWARD WING ATTACH 
- [SDR 2006FA0000476](https://openairdocs.org/sdr/2006FA0000476), Apr 26, 2006: GEAR. CRACKED. PILOT REPORTED DURING CRUISE LEVEL FLIGHT FEELING A SUDDEN VIBRATION AND HEARING A SCREAMING NOISE FROM THE LT ENGINE. PILOT THEN NOTICED TORQUE INDICATION ON L
- [SDR IZ22003F00004](https://openairdocs.org/sdr/IZ22003F00004), Jul 11, 2003: SOLENOID VALVE. LEAKING. SOLENOID VALVE LEAKING EXCESSIVE OIL BETWEEN SOLENOID AND VALVE BODY.
- [SDR IZ22003F00003](https://openairdocs.org/sdr/IZ22003F00003), Jan 6, 2003: NUT. CRACKED. DURING INSPECTION, FOUND UPPER WING INBOARD/OUTBOARD ATTACH BOLT WOULD NOT PROPERLY TIGHTEN TO TORQUE VALUE. INVESTIGATION REVEALED RIGHT UPPER FORWARD BARREL N
- [SDR IZ22001F00004](https://openairdocs.org/sdr/IZ22001F00004), Nov 7, 2001: SOLENOID VALVE. LEAKING. PILOT REPORTED FUEL LEAKING FROM COWLING. INVESTIGATION FOUND FUEL LEAK FROM MATING SURFACES OF PRIMARIES ONLY SOLENOID VALVE. REPLACED VALVE WITH SN 3894.
- [SDR IZ22001F00002](https://openairdocs.org/sdr/IZ22001F00002), Oct 15, 2001: VALVE. LEAKING. VALVE REPLACED DUE TO OIL LEAK BETWEEN SOLENOID AND VALVE BODY.
- [SDR CA010813024](https://openairdocs.org/sdr/CA010813024), Aug 9, 2001: BOLT. CRACKED. (CAN) THE NOSE LANDING GEAR DRAG STRUT ATTACH BOLT WAS FOUND CRACKED AT SCHEDULED NDT INSPECTION OF BOLT. THIS BOLT HAD BEEN MAGNETIC PARTICAL INSPECTED EVERY 2
- [SDR 20000609SH022](https://openairdocs.org/sdr/20000609SH022), May 24, 2000: TIRE. SEPARATED. THE SUBMITTER STATED, TIRE REPAIRED AND RECAPPED BY AERO WHEEL & BRAKE SERVICE CORP., NR U8SR971J. TIRE WAS INSTALLED ON THIS AIRCRAFT ON 4-15-00 AND HAD 13.2 H
- [SDR CA000110044](https://openairdocs.org/sdr/CA000110044), Dec 19, 1999: BRACKET. CRACKED. (CAN) DURING 100 HOUR INSPECTION THE SUBJECT LANDING GEAR FORWARD DOOR RETRACTION MECHANISM SUPPORT BRACKET WAS FOUND CRACKED AT THE OUTER MOST AFT HOLE.
- [SDR 99ZZZX3982](https://openairdocs.org/sdr/99ZZZX3982), Sep 1, 1999: CASE. FAILED. THE COMBUSTION CASE ASSY FAILED ALONG THE ENTIRE LENGTH OF THE MFG WELD. AIRCRAFT WAS ON TAKEOFF ROLL RESULTING IN AN ABORTED TAKEOFF AND FIRE IN THE NACELLE. N
- [SDR 99ZZZX2966](https://openairdocs.org/sdr/99ZZZX2966), Jul 6, 1999: TIRE. FAILED. AT ROTATION (110 KNOTS), PILOT FELT BAD VIBRATION. PILOT RETURNED TO AIRPORT, FOUND THAT RIGHT HAND RECAP CAME OFF. RECAP DONE BY HAWKINS AIRCRAFT TIRE COMPANY.
- [SDR 99ZZZX2946](https://openairdocs.org/sdr/99ZZZX2946), Jul 6, 1999: GEAR BOX. BROKEN. DURING MAINTENANCE INSPECTION, FOUND TOP AFT HOUSING FLANGE BROKEN ON RIGHT HAND MAIN LANDING GEAR THRUST GEAR BOX. FAA INSP NOTE: THIS PART HAS A S/B FOR LOOSE
- [SDR 98ZZZX1371](https://openairdocs.org/sdr/98ZZZX1371), Mar 9, 1998: RELAY. FAILED. PILOT SELECTED FLAPS DOWN 20 DEGREES FOR TAKEOFF. FLAPS WENT PAST 20 DEGREE POSITION, PAST 40 DEGREE DOWN POSITION, AND STOPPED AT THE MECHANICAL STOP. INVESTIG
- [SDR CA971027006](https://openairdocs.org/sdr/CA971027006), Sep 30, 1997: SWITCH. FROZEN. (CAN) AFTER TAKEOFF, RT MAIN LANDING GEAR DOWN LIGHT (GREEN) REMAINED ON WITH NO UNSAFE LIGHTS ON. LIGHT EXTINGUISHED AFTER 2O MINUTES. MAINTENANCE ACTION FOUND
- [SDR CA970918006](https://openairdocs.org/sdr/CA970918006), Sep 10, 1997: IMPELLER. CRACKED. (CAN) DURING HSI GBI, THE COMPRESSOR SECTION WAS DISMANTLED DUE TO COMPRESSOR RUB. 1ST STAGE IMPELLER HAS A CRACK IN IT. THIS PN IS REFERENCED IN SB TPE331A72-0
- [SDR 97ZZZX2709](https://openairdocs.org/sdr/97ZZZX2709), May 22, 1997: HOSE. WRONG PART. FOUND, CLEVELAND BRAKE KIT 199-101 STC SA648GL BRAKE HOSES U/A HOSE LISTED SAE DOAS SAE DOT 3000 PSI AIR BRAKE HOSE, FITTING CONNECTORS WERE 45 DEGREE ANGLE AND
- [SDR 97ZZZX619](https://openairdocs.org/sdr/97ZZZX619), Jan 1, 1996: SKIN. CRACKED. PERFORMING 100 HR INSPECTION, DEFORMATION OF FUSELAGE SKIN WAS NOTED ABOVE BOTH MAIN GEAR ATTACH POINTS. FURTHER INSP WAS REQUIRED AND THE INTERIOR WALLS OF THE

## STCs that may be installed (OpenAirDocs) (111, 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 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 SA648GL](https://openairdocs.org/stc/SA648GL): Install Parker Hannifin wheels and brakes 199-101 conversion kit dated9/28/82. Kaman Corporation Aircraft Wheel and Brake LLC
- [STC SA684GL](https://openairdocs.org/stc/SA684GL): 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 SA00490WI](https://openairdocs.org/stc/SA00490WI): Installation of Test Instrumentation, Inc. (TII) Over-Torque Warning System. Mitsubishi Heavy Industries America Inc
- [STC SA00492WI](https://openairdocs.org/stc/SA00492WI): Installation of Test Instrumentation, Inc., (TII) Pneumatic De-Ice Monitoring System on Mitsubishi MU-2B airplanes. Mitsubishi Heavy Industries America Inc
- [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 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)
- [STC SA11174SC PAGE 1](https://openairdocs.org/stc/SA11174SC%20PAGE%201): Installation of BendixKing by Honeywell KSN 770 and KSN 765 WAAS LPV approach capable nav/comm systems. Honeywell International Inc (Bendix King)
- [STC SA02265SE](https://openairdocs.org/stc/SA02265SE): Installation of a camera housing. Airborne Sensor LLC
- [STC ST01930LA](https://openairdocs.org/stc/ST01930LA): Installation of Sandel Avionics SN4500 Electronic Horizontal Situation Indicator (EHSI). Sandel Avionics LLC
- [STC SA09916AC](https://openairdocs.org/stc/SA09916AC): Installation of Hartzell 4-Bladed Propellers Model HC-E4N-5KFL/JE9782SB. Intercontinental Jet Service Corporation
- [STC SA04514NY](https://openairdocs.org/stc/SA04514NY): Single/Dual Transponder System ADS-B Upgrade. Scandinavian Avionics Design ApS
- [STC SA01452CH](https://openairdocs.org/stc/SA01452CH): Installation of an air ambulance conversion kit. Med-Pac Inc
- [STC SA01714WI](https://openairdocs.org/stc/SA01714WI): Installation of a Garmin transponders: (a) GTX 330/330D/33/33D with ADS-B Out functionality; (b) GTX 335/335R/345/345R with ADS-B Out and In functionality; or (c) GTX 335R/345R with ADS-B Out functionality in select airplanes installed with G950/G1000 systems. Garmin International Inc
- [STC SA85CH](https://openairdocs.org/stc/SA85CH): Replace cabin door seal with door seal. Mitsubishi Heavy Industries America Inc
- [STC SA00765DE](https://openairdocs.org/stc/SA00765DE): Installation of Automatic Dependent Surveillance Broadcast (ADS-B) Out functionality using the BendixKing KT74 Transponder and qualified position sensor. Peregrine
- [STC SA04165NY](https://openairdocs.org/stc/SA04165NY): Installation of Latitude Technologies Skynode S200 Satcom system must be performed. Latitude Technologies Corporation
- [STC SA02153LA-D PAGE 1](https://openairdocs.org/stc/SA02153LA-D%20PAGE%201): Installation of Garmin G600 Primary Flight Display (PFD) and Multifunction Display (MFD) System. Garmin International Inc
- [STC SA02503AK](https://openairdocs.org/stc/SA02503AK): Installation of AMSAFE State of the Art Restraint System (SOARS) inflatable restraints. AMSAFE Inc
- [STC SA02013CH](https://openairdocs.org/stc/SA02013CH): Installation of Avidyne Corporation Traffic Advisory System (TAS). Avidyne Corporation
- [STC SA1182GL](https://openairdocs.org/stc/SA1182GL): Replace cabin door with cargo door. Intercontinental Jet Service Corporation
- [STC SA1183GL](https://openairdocs.org/stc/SA1183GL): Replace left side cockpit window with crew door. Intercontinental Jet Service Corporation
- [STC SA1341GL](https://openairdocs.org/stc/SA1341GL): Replace right side cockpit Window with Crew Door. Intercontinental Jet Service Corporation
- [STC SA01933LA-D](https://openairdocs.org/stc/SA01933LA-D): Installation of Garmin Model 400W / 500W Series GPS-WAAS Navigation System. Garmin International Inc
- [STC ST00366WI](https://openairdocs.org/stc/ST00366WI): Installation of Keddeg Company P/N 21BC115 Coalescer Assembly. Purolator Facet, Inc
- [STC SA00343BO](https://openairdocs.org/stc/SA00343BO): Installation of a single configuration or a dual configuration Avidyne Corporation Integrated Flight Display, Model IFD540 loaded with Release 10.0 software (or later FAA approved release). Avidyne Corporation
- [STC SA00352BO PAGE 1](https://openairdocs.org/stc/SA00352BO%20PAGE%201): Installation of an Avidyne Corporation Mode A/C/S Transponder with ADS-B Out capability, Model AXP340 loaded with Version 3.13 software (or later FAA approved version),. Avidyne Corporation
- [STC SA1205GL](https://openairdocs.org/stc/SA1205GL): Install Egan Aviation air ambulance stretcher P/N 126 using Installation Kit P/N 806. Paul/ Lanna Egan LLC
- [STC SA03533NY](https://openairdocs.org/stc/SA03533NY): Installation of Hawker 9750W0538 (24V40Ah) Sealed Lead Acid-Batteries. Securaplane Technologies Inc
- [STC SA03686NY](https://openairdocs.org/stc/SA03686NY): Replacement of certain Goodrich pneumatic deicer boots. BE Aerospace Inc. DBA SMR Technologies, Inc
- [STC SA02547AT](https://openairdocs.org/stc/SA02547AT): Installation of a Voice Alert System. Aircraft Components Inc
- [STC SA01594SE](https://openairdocs.org/stc/SA01594SE): Fabrication of Stretched Acrylic Cabin windows. Mitsubishi Heavy Industries America Inc
- [STC SA01969SE](https://openairdocs.org/stc/SA01969SE): Installation of a Mid-Continent MD302 Standby Attitude Module. Mid-Continent Instruments and Avionics
- [STC SA01229SE PAGE 1](https://openairdocs.org/stc/SA01229SE%20PAGE%201): Installation of GNS 480 (CNX80) GPS WAAS Navigator with integrated VHF Navigation and Communication radios. Garmin International Inc
- [STC SA01933LA-D PAGE 1](https://openairdocs.org/stc/SA01933LA-D%20PAGE%201): Installation of Garmin Model 400W / 500W Series GPS-WAAS Navigation System. Garmin International Inc
- [STC SA02121SE](https://openairdocs.org/stc/SA02121SE): Installation of Garmin GTS 825 (TAS) or GTS 855 (TCAS I) Traffic System. Garmin International Inc
- [STC SA00269BO](https://openairdocs.org/stc/SA00269BO): Installation of Avidyne Corporation TWX 670 Tactical Weather Detection System P/N 850-00026-000-( ) consisting of Avidyne Processor P/N 700-00033-000-( ), Sensor Systems Inc. Antenna P/N S72-1715-1 with doubler plate P/N S72-171530-1, and Avidyne Mounting Tray P/N 700-00034-000. Avidyne Corporation
- [STC SA03315NY](https://openairdocs.org/stc/SA03315NY): Installation of Model MTV-27-1-E-C-F-R(G)/CFR210-58d 5-bladed, full feathering composite propellers. MT- Propeller Entwicklung GmbH
- [STC SA00816SE](https://openairdocs.org/stc/SA00816SE): Installation of emergency exit placards. Mitsubishi Heavy Industries America Inc
- [STC SA01434SE](https://openairdocs.org/stc/SA01434SE): Fabrication and Installation of a Tip Tank Sniffle Valve Decal. Mitsubishi Heavy Industries America Inc
- [STC SA02064SE](https://openairdocs.org/stc/SA02064SE): Fabrication and installation of a Test Instrumentation, Inc., Tip Fuel Tank Pressure-Vacuum Relief Valve. Mitsubishi Heavy Industries America Inc
- [STC SA01300WI](https://openairdocs.org/stc/SA01300WI): Installation of the MU-2B Voice Alerting System. Mitsubishi Heavy Industries America Inc
- [STC SA01692SE](https://openairdocs.org/stc/SA01692SE): Installation of a Garmin GMX 200 Multi-Function Display. Garmin International Inc
- [STC SA03148NY](https://openairdocs.org/stc/SA03148NY): The installation of the Latitude Technologies Corporation S100 Tracking System. Latitude Technologies Corporation

All 111: https://openairdocs.org/model/mitsubishi-mu-2b-36a/stcs.md

## PMA parts (OpenAirDocs) (278, 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.

- [RAP164-07200](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID126779200920260722154728.0001): Brake Disc. Rapco Inc. · PMA PQ2101CE · Replaces 164-07200 · Jun 3, 2026
- [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
- [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
- [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
- [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
- [APM016A-13472](https://drs.faa.gov/browse/excelExternalWindow/10A911A72674965586258591005E85A5.0001): Roller. Aero Parts Mart Inc · PMA PQ0982SW · Replaces 016A-13472 · Jan 5, 2020
- [9100-001-C](https://drs.faa.gov/browse/excelExternalWindow/DD343890DCD8BFDB86258569004013FB.0001): MaxDim Lamp Intensity Controller. Seaton Engineering Corporation · PMA PQ2574NM · Modification part · Sep 3, 2019
- [9100-001-D](https://drs.faa.gov/browse/excelExternalWindow/C7B6725B325949E98625856900401478.0001): MaxDim Lamp Intensity Controller. Seaton Engineering Corporation · PMA PQ2574NM · Modification part · Sep 3, 2019
- [9200-000-B](https://drs.faa.gov/browse/excelExternalWindow/BD58B0712CA0C6AA86258569004016AD.0001): MaxPulse Landing Light Controller. Seaton Engineering Corporation · PMA PQ2574NM · Modification part · Sep 3, 2019
- [9100-001-G](https://drs.faa.gov/browse/excelExternalWindow/ADE62C91D97E8B788625856900401557.0001): MaxDim Lamp Intensity Controller. Seaton Engineering Corporation · PMA PQ2574NM · Modification part · Sep 3, 2019
- [9100-001-E](https://drs.faa.gov/browse/excelExternalWindow/A37F050253EE808A86258569004014BA.0001): MaxDim Lamp Intensity Controller. Seaton Engineering Corporation · PMA PQ2574NM · Modification part · Sep 3, 2019
- [9200-000-A](https://drs.faa.gov/browse/excelExternalWindow/8E10EF4D973C1D6D8625856900401662.0001): MaxPulse Landing Light Controller. Seaton Engineering Corporation · PMA PQ2574NM · Modification part · Sep 3, 2019
- [9100-001-A](https://drs.faa.gov/browse/excelExternalWindow/62DC748A2B9B1D9386258569004012FD.0001): MaxDim Lamp Intensity Controller. Seaton Engineering Corporation · PMA PQ2574NM · Modification part · Sep 3, 2019
- [9100-001-F](https://drs.faa.gov/browse/excelExternalWindow/3746AAB4CC0D6883862585690040151B.0001): MaxDim Lamp Intensity Controller. Seaton Engineering Corporation · PMA PQ2574NM · Modification part · Sep 3, 2019
- [9100-001-B](https://drs.faa.gov/browse/excelExternalWindow/32446D71EB78157686258569004013B2.0001): MaxDim Lamp Intensity Controller. Seaton Engineering Corporation · PMA PQ2574NM · Modification part · Sep 3, 2019

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