# Mitsubishi MU-2B-30 - Type: Aircraft model (FAA registry) - Registry code: 5780410 - Manufacturer (registry): MITSUBISHI - Model: MU-2B-30 - 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: 0 - Page: https://openairdocs.org/model/mitsubishi-mu-2b-30 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 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 97-04-13](https://openairdocs.org/ad/97-04-13): Vent Check Valve Assembly · Mitsubishi Heavy Industries MU-2B, MU-2B-10, MU-2B-15 and 2 more. Effective Apr 16, 1997 - [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 91-23-08](https://openairdocs.org/ad/91-23-08): Rudder Trim Tab · Mitsubishi Heavy Industries MU-2B-10, MU-2B-15, MU-2B-20 and 2 more. Effective Dec 18, 1991 - [AD 88-21-01 R1](https://openairdocs.org/ad/88-21-01-R1): Control Yoke · Mitsubishi Heavy Industries MU-2B, MU-2B-10, MU-2B-15 and 10 more. Effective Jan 28, 1989 - [AD 88-23-01](https://openairdocs.org/ad/88-23-01): Torque Tube Joints · Mitsubishi Heavy Industries MU-2B, MU-2B-10, MU-2B-15 and 10 more. Effective Dec 4, 1988 - [AD 88-13-01](https://openairdocs.org/ad/88-13-01): Autopilots · Mitsubishi Heavy Industries MU-2B, MU-2B-10, MU-2B-15 and 10 more. Effective Jul 11, 1988 - [AD 87-04-03](https://openairdocs.org/ad/87-04-03): Flap Flexible Shafts · Mitsubishi Heavy Industries MU-2B, MU-2B-10, MU-2B-15 and 10 more. Effective Mar 7, 1987 - [AD 86-26-02](https://openairdocs.org/ad/86-26-02): POH/AFM Appendix - Icing · Mitsubishi Heavy Industries MU-2B-10, MU-2B-15, MU-2B-20 and 9 more. Effective Dec 31, 1986 - [AD 86-20-01](https://openairdocs.org/ad/86-20-01): Pitot System Modification · Mitsubishi Heavy Industries MU-2B, MU-2B-10, MU-2B-15 and 10 more. Effective Oct 6, 1986 - [AD 86-15-03](https://openairdocs.org/ad/86-15-03): NLG Strut Assembly · Mitsubishi Heavy Industries MU-2B, MU-2B-10, MU-2B-15 and 6 more. Effective Aug 13, 1986 - [AD 84-25-02](https://openairdocs.org/ad/84-25-02): Trim Tab Brackets · Mitsubishi Heavy Industries MU-2B, MU-2B-10, MU-2B-15 and 10 more. Effective Dec 18, 1984 - [AD 84-12-04](https://openairdocs.org/ad/84-12-04): Mitsubishi Heavy Industries MU-2B, MU-2B-10, MU-2B-15 and 10 more. Effective Jun 28, 1984 - [AD 83-09-02](https://openairdocs.org/ad/83-09-02): Strobe Light Assemblies · Mitsubishi Heavy Industries MU-2B-25, MU-2B-26, MU-2B-30 and 2 more. Effective May 17, 1983 - [AD 82-21-03](https://openairdocs.org/ad/82-21-03): Fire Detection · Mitsubishi Heavy Industries MU-2B, MU-2B-10, MU-2B-15 and 4 more. Effective Oct 14, 1982 - [AD 82-08-02](https://openairdocs.org/ad/82-08-02): Electrical Wiring Inspection · Mitsubishi Heavy Industries MU-2B, MU-2B-10, MU-2B-15 and 6 more. Effective Apr 15, 1982 - [AD 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 - [AD 71-14-01](https://openairdocs.org/ad/71-14-01): Fuel Tank Fungus Coating Peeling · Mitsubishi Heavy Industries MU-2B-10, MU-2B-15, MU-2B-20 and 1 more. Effective May 1, 1972 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 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 None registered with this model now. ## NTSB investigations (14) 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 CHI98FA074](https://openairdocs.org/ntsb/CHI98FA074), Dec 30, 1997: Mitsubishi MU-2B-30 (N999WB), Wayne, IL, destroyed, 2 fatal. Probable cause: the pilot in command failed to maintain control of the aircraft. A factor was the lack of experience of the pilot and copilot in the type and model of aircraft. An additional factor was the pilot did… - [NTSB NYC96LA188](https://openairdocs.org/ntsb/NYC96LA188), Sep 28, 1996: Mitsubishi MU-2B-30 (N618BB), Chillicothe, OH, substantial damage. Probable cause: failure of the pilot to follow the published emergency procedures after loss of power in the left engine. Factors relating to the accident were: fatigue failure of the left torque sensor and gear… - [NTSB MIA96IA114](https://openairdocs.org/ntsb/MIA96IA114), Apr 12, 1996: Mitsubishi MU-2G-30 (N920S), Columbia, SC, incident, minor damage. Probable cause: failure of the nose landing gear bearing due to improper assembly and staking (inadequate quality control) by the manufacturer; which prevented the nose gear from retracting and the main gear from… - [NTSB DEN92FA064](https://openairdocs.org/ntsb/DEN92FA064), Jun 25, 1992: Mitsubishi MU-2B-30 (N108SC), Alamagordo, NM, destroyed, 6 fatal. Probable cause: THE FAILURE OF THE PILOT TO EXERCISE ADEQUATE VFR DEPARTURE TERRAIN AVOIDANCE PROCEDURES, AND THE FAILURE OF THE CONTROLLER TO ISSUE A SAFETY ALERT TO THE PILOT. FACTORS WHICH CONTRIBUTED TO THE… - [NTSB MIA88WA074](https://openairdocs.org/ntsb/MIA88WA074), Dec 23, 1987: Mitsubishi MU-2B-30 (N255C), San Salvador, El Salvador, substantial damage - [NTSB FTW83LA096](https://openairdocs.org/ntsb/FTW83LA096), Jan 21, 1983: Mitsubishi MU-2B-30 (N555CH), Lubbock, TX, substantial damage - [NTSB ATL82FA110](https://openairdocs.org/ntsb/ATL82FA110), Apr 20, 1982: Mitsubishi MU-2B-30 (N165MA), Lafayette, GA, destroyed, 6 fatal - [NTSB CHI81FEG03](https://openairdocs.org/ntsb/CHI81FEG03), Dec 15, 1980: Mitsubishi MU-2B (N93UM), Cambellstown, OH, substantial damage - [NTSB IAD78DLQ08](https://openairdocs.org/ntsb/IAD78DLQ08), Jan 19, 1978: Mitsubishi MU-2 (N115S), Hawesville, KY, destroyed - [NTSB NYC77FA046](https://openairdocs.org/ntsb/NYC77FA046), Apr 5, 1977: Mitsubishi MU-2 (N888RJ), Bronx, NY, destroyed, 7 fatal - [NTSB MIA77FA049](https://openairdocs.org/ntsb/MIA77FA049), Apr 1, 1977: Mitsubishi MU-2B (N100SW), Augusta, GA, destroyed - [NTSB HAY76AL042](https://openairdocs.org/ntsb/HAY76AL042), Dec 26, 1975: Mitsubishi MU-2B (N133MA), Rollinsville, CO, destroyed, 9 fatal - [NTSB DEN74AD041](https://openairdocs.org/ntsb/DEN74AD041), Mar 2, 1974: Mitsubishi MU-2B (N711AH), Glenwood Spg, CO, destroyed, 5 fatal - [NTSB NYC72AN129](https://openairdocs.org/ntsb/NYC72AN129), Apr 16, 1972: Mitsubishi MU-2G (N132MA), Atlantic City, NJ, destroyed, 3 fatal ## FAA accident and incident reports (21) 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. - [Accident 19971230039729A](https://openairdocs.org/incident/19971230039729A), Dec 30, 1997: Mtsbsi MU2B30 (N999WB), Chicago/West Ch, IL, Destroyed, 2 fatal. Practice engine out on climbout. Stalled. Spun into ground. Right yoke found upside down may be contributing factor - [Accident 19960929030249A](https://openairdocs.org/incident/19960929030249A), Sep 29, 1996: Mtsbsi MU2B30 (N618BB), Chillicothe, OH, Substantial damage. Left engine quit on climbout. Feathered circled. Veered off runway landing into ditch. Torque sensor case failed. (-23) pilot departed runway 5 for a flight to… - [Accident 19960412045149A](https://openairdocs.org/incident/19960412045149A), Apr 12, 1996: Mtsbsi MU2B30 (N920S), Columbia, SC, Minor damage. Nose gear failed retract departing atl. Diverted cae. Landed mains up. Wheel bearing failed jammed in housing. - [Incident 19950627024409I](https://openairdocs.org/incident/19950627024409I), Jun 27, 1995: Mtsbsi MU2B30 (N60KG), Omaha, NE. Right engine surging on climbout. Shutdown and returned. Replaced sensor and returned to service. - [Accident 19920624031079A](https://openairdocs.org/incident/19920624031079A), Jun 24, 1992: Mtsbsi MU2B30 (N108SC), Alamogordo, NM, Destroyed, 6 fatal. Departed VFR night. Talking to ATC, circling to go above mountains but hit mountain just below ridgeline. - [Incident 19900816054159I](https://openairdocs.org/incident/19900816054159I), Aug 16, 1990: Mtsbsi MU2B30 (N134MA), Santa Ana, CA. Smoke in cockpit. Returned and landed safely. Main seal in air cycle machine cooling turbo failed. - [Accident 19871223074879A](https://openairdocs.org/incident/19871223074879A), Dec 23, 1987: Mtsbsi MU2B30 (N255C), San Salvador Is, Bahamas, Substantial damage. Aircraft crashed on landing on san Salvador Island. - [Incident 19860721041099I](https://openairdocs.org/incident/19860721041099I), Jul 21, 1986: Mtsbsi MU2B30 (N300BD), Houston, TX, Minor damage. Selected gear handle down. Landed with gear retracted and circuit breaker popped. Failed to check gear position. - [Incident 19850714043099I](https://openairdocs.org/incident/19850714043099I), Jul 14, 1985: Mtsbsi MU2B30 (N40PP), Lampasas, TX, Minor damage. Low fuel light came on and engines quit. Landed long and ran off runway. Fuel exhaustion due to gauge malfunction. - [Incident 19840817051849I](https://openairdocs.org/incident/19840817051849I), Aug 17, 1984: Mtsbsi MU2B30 (N555CH), Philadelphia, PA, Minor damage. Flight instructor allowed a gear up landing. Blamed distraction of heavy traffic. Needed to use checklist. - [Incident 19840203010049I](https://openairdocs.org/incident/19840203010049I), Feb 3, 1984: Mtsbsi MU2B30 (N134MA), Chesterfield, SC, Minor damage. Unable to retract gear. Lost control of aircraft. Actuators not properly rigged. Loss of control from drag possible - [Accident 19830120002169A](https://openairdocs.org/incident/19830120002169A), Jan 20, 1983: Mtsbsi MU2B30 (N555CH), Lubbock, TX, Substantial damage. During roll out on landing aircraft skidded into snowbank on side of runway separating left tip tank. - [Incident 19820517023909I](https://openairdocs.org/incident/19820517023909I), May 17, 1982: Mtsbsi MU2B30 (N555CH), Ft Stockton, TX, Minor damage. Landing gear would not extend. Landed gear up. "J" hook would not release, possible rigging problem. - [Accident 19820420010329A](https://openairdocs.org/incident/19820420010329A), Apr 20, 1982: Mtsbsi MU2B30 (N165MA), Lafayette, GA, Destroyed, 4 fatal. Aircraft impacted ridgeline at 2020 foot elevation. Pilot was attempting en route below low ceiling. - [Accident 19801215072759A](https://openairdocs.org/incident/19801215072759A), Dec 15, 1980: Mtsbsi MU2B30 (N93UM), Campbellstown, OH, Substantial damage. Descended below mda, struck ground 3 miles short of runway. Possible pilot ingestion of toxic fumes & fatigue. - [Incident 19800222027779I](https://openairdocs.org/incident/19800222027779I), Feb 22, 1980: Mtsbsi MU2B30 (N313BB), Crossville, TN, Minor damage. Instructor and student on training flight. Forgot to extend landing gear. - [Accident 19780119000539A](https://openairdocs.org/incident/19780119000539A), Jan 19, 1978: Mtsbsi MU2B30 (N115S), Hawesville, KY, Substantial damage - [Accident 19770405021789A](https://openairdocs.org/incident/19770405021789A), Apr 5, 1977: Mtsbsi MU2B30 (N888RJ), Bronx, NY, Destroyed, 6 fatal - [Accident 19770401017369A](https://openairdocs.org/incident/19770401017369A), Apr 1, 1977: Mtsbsi MU2B30 (N100SW), Augusta, GA, Destroyed - [Accident 19751226040869A](https://openairdocs.org/incident/19751226040869A), Dec 26, 1975: Mtsbsi MU2B30 (N133MA), CO, Destroyed, 8 fatal - [Accident 19740302016469A](https://openairdocs.org/incident/19740302016469A), Mar 2, 1974: Mtsbsi MU2B30 (N711AH), Glenwood Spg, CO, Destroyed, 4 fatal. Below clouds,nr mtn peaks.l turn to locate arpt. Hit mtn. Rcvrd 3/4/74. ## Service difficulty reports (16) As reported by operators and repair stations, by the model named in the report. - [SDR CA000824028](https://openairdocs.org/sdr/CA000824028), Aug 9, 2000: BRACKET. BROKEN. (CAN) PIREP VIBRATION ON INITIAL START-UP, AFTER ENGINE START AND OFF PITCH LOCKS VIBRATION WENT AWAY.UPON INVESTIGATION MAINTENANCE FOUND 2 OUT OF 3 PITCH STOP - [SDR 20000623SH015](https://openairdocs.org/sdr/20000623SH015), May 20, 2000: FITTING. DETERIORATED. OIL SUPPLY LINE FOR OIL COOLER, FITTING THREADS IN CASE DETERIORATED ALLOWING FITTING TO BLOW OUT. THIS ALLOWED ENGINE OIL TO PUMP OUT. PILOT SHUT ENGINE DOWN W - [SDR AU981132](https://openairdocs.org/sdr/AU981132), Aug 28, 1998: ROD FORK. FAILED. (AUS) RUDDER CONTROL ROD FORK END ROTATED AND CAUSED RESTRICTED MOVEMENT WHICH EVENTUALLY SNAPPED THE FORK. INVESTIGATION FOUND THAT THE LOCKNUT HAD WORKED LOOS - [SDR AU980524](https://openairdocs.org/sdr/AU980524), May 14, 1998: CONTROL ROD. BROKEN. (AUS) RUDDER TRIM TAB CONTROL ROD BROKEN. AD/MU-2/48 HAD NOT BEEN COMPLIED WITH. - [SDR AU980250](https://openairdocs.org/sdr/AU980250), Mar 11, 1998: CONTROL CABLE. FAILED. (AUS) ELEVATOR TRIM CABLE FRAYED WITH ONLY ONE STRAND REMAINING . CABLE FAILED DURING REMOVAL. AIRCRAFT WAS PREVIOUSLY REGISTERED ASVH-UZN. - [SDR AU980181](https://openairdocs.org/sdr/AU980181), Jan 21, 1998: LANDING GEAR. FAILED. (AUS) LANDING GEAR FAILED TO RETRACT. SYSTEM WORKED NORMALLY DURING GROUND CHECKS WHEN FOLLOWING RESETTING OF THE EMERGENCY EXTENSION SYSTEM. SUSPECT CAUSED BY - [SDR AU971630](https://openairdocs.org/sdr/AU971630), Dec 16, 1997: SKIN. CRACKED. (AUS) HORIZONTAL STABILISER LEADING EDGE SKINS CRACKED. CRACKS ORIGINATE FROM RIB RIVETS FOR THE OUTBOARD ELEVATOR HINGE. CRACK LENGTH 50.8MM (2IN). FOUND DURIN - [SDR AU970727](https://openairdocs.org/sdr/AU970727), Jun 20, 1997: BLADE. SEPARATED. (AUS) RH PROPELLER NO3 BLADE SEPARATED AT BLADE ROOT. EXTENSIVE DAMAGE CAUSED TO REDUCTION GEARBOX, ENGINE, ENGINE MOUNTS, COWLING AND NACELLE. - [SDR 97ZZZX526](https://openairdocs.org/sdr/97ZZZX526), Sep 28, 1996: SENSOR BODY. BROKEN. DURING THE AFTER TAKEOFF CLIMB, AND IMMEDIATELY AFTER GEAR RETRACTION THE ENGINE FLAMED OUT. THE TORQUE SENSOR BODY FAILED AROUND THE DRIVE GEAR FOR THE FUEL CO - [SDR AU961167](https://openairdocs.org/sdr/AU961167), Aug 8, 1996: LANDING GEAR. FAULTY. (AUS) LANDING GEAR WOULD NOT EXTEND IN NORMAL OR EMERGENCY MODES - [SDR EY2R9600819](https://openairdocs.org/sdr/EY2R9600819), Jun 1, 1996: BEARING. CORRODED. BEARING CORRODED. - [SDR AU960376](https://openairdocs.org/sdr/AU960376), Mar 26, 1996: HEATER. STRIPPED. (AUS) RH ENGINE OIL/FUEL HEATER OIL OUTLET FITTING PNO AN815-8J LOOSE AND LEAKING DUE TO STRIPPED THREADS IN THE HEATER HOUSING -PERSONNEL/MAINTENANCE ERROR - [SDR AU960327](https://openairdocs.org/sdr/AU960327), Mar 11, 1996: PLENUM. CRACKED. (AUS) RH ENGINE PLENUM CHAMBER CRACKED AROUND DRAIN FITTING TAKEOFF FLANGE - CRACK LENGTH 50.8MM (2IN) - RH ENGINE BLEED AIR TUBECHAFED AND LEAKING - PERSONNEL/ - [SDR 96ZZZX756](https://openairdocs.org/sdr/96ZZZX756), Jan 19, 1996: LIMIT SWITCH. MISWIRED. DURING TROUBLESHOOTING THE GEAR EXTENSION SYSTEM, AN ERROR WAS FOUND IN THE WIRING DIAGRAM ON PAGE 10-2 OF MITSUBISHI MM, YET 69016. WIRE LABELED 'G125D20' ON N - [SDR 95ZZZX736](https://openairdocs.org/sdr/95ZZZX736), Jan 20, 1995: BRACKET. FAILED. FORWARD MLG DOOR ACTUATOR SUPPORT BRACKET TORN OUT. SB NR 172 WAS PREVIOSULY COMPLIED WITH, BUT SB 197A HAD NOT BEEN DONE. IF SB NR 197A IS COMPLIED WITH, THIS - [SDR 95ZZZX749](https://openairdocs.org/sdr/95ZZZX749), Jan 9, 1995: CHAIN. SEPARATED. AFTER A NORMAL LIFT OFF AND CLIMB OUT, FLYING PILOT NOTED HE WAS GETTING NO ROLL RESPONSE TO RT CONTROL (ROLL COLUMN INPUT AND LITTLE RESPONSE TO LT WHILE IT SE ## STCs that may be installed (OpenAirDocs) (156, 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 SA800EA](https://openairdocs.org/stc/SA800EA): Installation of Whelen Anti-Collision, Position, or Anti-Collision/Position Light System, and applicable associated power supplies. Whelen Aerospace Technologies - [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 SA1069SW](https://openairdocs.org/stc/SA1069SW): Installation of Mooney AB1001, TSO C-39 seats. Mitsubishi Heavy Industries America Inc - [STC SA1085SW](https://openairdocs.org/stc/SA1085SW): Installation of air conditioning system. Mitsubishi Heavy Industries America Inc - [STC SA1140SW](https://openairdocs.org/stc/SA1140SW): Installation of Hartzell HC-B3TN-5/T1078HB-11R propeller. Mitsubishi Heavy Industries America Inc - [STC SA1146SW](https://openairdocs.org/stc/SA1146SW): Interior installation. Mitsubishi Heavy Industries America Inc - [STC SA1198SW](https://openairdocs.org/stc/SA1198SW): Installation of eleven piece interior. Mitsubishi Heavy Industries America Inc - [STC SA1257SW](https://openairdocs.org/stc/SA1257SW): Seat arrangement and other interior installations. Mitsubishi Heavy Industries America Inc - [STC SA1266SW](https://openairdocs.org/stc/SA1266SW): Installation of a drawer type toilet and across the back baggage shelf. Mitsubishi Heavy Industries America Inc - [STC SA1275SW](https://openairdocs.org/stc/SA1275SW): Modification of air-conditioning system. Mitsubishi Heavy Industries America Inc - [STC SA1295SW](https://openairdocs.org/stc/SA1295SW): Installation of stretch headliner. Mitsubishi Heavy Industries America Inc - [STC SA1316SW](https://openairdocs.org/stc/SA1316SW): Installation of a series/parallel selector switch for battery start selection. 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 SA1448SW](https://openairdocs.org/stc/SA1448SW): Installation of divan and and one-place jump seat. 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 SA1484SW](https://openairdocs.org/stc/SA1484SW): Installation of a Hartman series-parallel battery relay. Mitsubishi Heavy Industries America Inc - [STC SA1489SW](https://openairdocs.org/stc/SA1489SW): Installation of antennas. 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 SA1805SW](https://openairdocs.org/stc/SA1805SW): Installation of Foxboro fuel flow signal conditioning unit PC-260. 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 SA2266SW](https://openairdocs.org/stc/SA2266SW): Fabrication and installation of wing panel flap actuator access. 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 SA01452CH](https://openairdocs.org/stc/SA01452CH): Installation of an air ambulance conversion kit. Med-Pac Inc - [STC SA161GL](https://openairdocs.org/stc/SA161GL): Install Garrett AiResearch TPE331-6-252M engines. Standard Aero Business Aviation Services LLC - [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 SA84CH](https://openairdocs.org/stc/SA84CH): Replace Cabin 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 SA1160GL](https://openairdocs.org/stc/SA1160GL): Replace left side cockpit window with crew door. Intercontinental Jet Service Corporation - [STC SA1161GL](https://openairdocs.org/stc/SA1161GL): Replace cabin door with cargo door. Intercontinental Jet Service Corporation - [STC SA1338GL](https://openairdocs.org/stc/SA1338GL): Replace right side cockpit window with Crew Door conforming to National Aircraft Service Drawing List NA-DL1R, Rev. E. Intercontinental Jet Service Corporation - [STC SA1442GL](https://openairdocs.org/stc/SA1442GL): Replace inside cabin windows with aluminum plates. Intercontinental Jet Service Corporation All 156: https://openairdocs.org/model/mitsubishi-mu-2b-30/stcs.md ## PMA parts (OpenAirDocs) (418, 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 - [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 - [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 - [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 - [9100-001-H](https://drs.faa.gov/browse/excelExternalWindow/1AEB415100FB45D8862585690040159F.0001): MaxDim Lamp Intensity Controller. Seaton Engineering Corporation · PMA PQ2574NM · Modification part · Sep 3, 2019 - [Approved AML dated 12-15-1993](https://drs.faa.gov/browse/excelExternalWindow/A6CDB86429824DF4862585690051CA9D.0001): Air Medical System. LifePort, LLC. · PMA PQ0172NM · Modification part · Jul 31, 2019 - [D4E1188-5](https://drs.faa.gov/browse/excelExternalWindow/B19E161E319F679086258288005E263C.0001): Propeller De-Icer. UTC Aerospace Systems, Goodrich Sensors & Integrated Systems · PMA PQ0822NE · Replaces 4E1188-5 · Apr 3, 2018 - [30010-1026WE](https://drs.faa.gov/browse/excelExternalWindow/35EFA3975F14CD24862582280078876D.0001): Brush. Wencor LLC · PMA PQ1370NM · Replaces 30010-1026 · Nov 19, 2017 - [150SG1052-14EH](https://drs.faa.gov/browse/excelExternalWindow/BC96C120506BDC458625808800591142.0001): Bearing - Ball. Seginus Inc · PMA PQ4083CE · Replaces APC 150SG1052-14 · Dec 6, 2016 All of them: https://openairdocs.org/model/mitsubishi-mu-2b-30/pma.md --- 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.