# Mitsubishi MU-300 - Type: Aircraft model (FAA registry) - Registry code: 5780602 - Manufacturer (registry): MITSUBISHI - Model: MU-300 - Aircraft type: Fixed wing multi engine - Category: Airplane - Engines: 2 · Turbo-jet - Seats: 11 - Weight class: 12,500 to 19,999 lb - Certification: Type certificated - Data sheet: [TCDS A14SW](https://openairdocs.org/tcds/A14SW) (OpenAirDocs) - Holder: Textron Aviation Inc. - Registered aircraft: 17 - Page: https://openairdocs.org/model/mitsubishi-mu-300 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 2026-13-02](https://openairdocs.org/ad/2026-13-02): Navigation · Airbus Canada Limited Partnership 18, 49-46, 80-A and 555 more. Effective Jul 1, 2026 - [AD 2023-10-02](https://openairdocs.org/ad/2023-10-02): Indicating/Recording System, Navigation · Boeing 18, 23, 35 and 1,060 more. Effective May 26, 2023 - [AD 2014-21-06](https://openairdocs.org/ad/2014-21-06): Flight Controls · Textron 400, 400A, 400T and 1 more. Effective Nov 28, 2014 - [AD 2014-15-15](https://openairdocs.org/ad/2014-15-15): Stabilizers · Textron 400, 400A, 400T and 1 more. Effective Sep 5, 2014 - [AD 2011-01-09](https://openairdocs.org/ad/2011-01-09): Oxygen · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 290 more. Effective Feb 9, 2011 - [AD 2009-07-02](https://openairdocs.org/ad/2009-07-02): Flightcrew seats · Textron 400, 400A, MU-300 and 1 more. Effective Apr 30, 2009 - [AD 2006-21-02](https://openairdocs.org/ad/2006-21-02): Operating Limitations, Abnormal Procedures, and Normal Procedures · Textron 400, 400A, 400T and 1 more. Effective Oct 25, 2006 - [AD 2004-22-02](https://openairdocs.org/ad/2004-22-02): Spoiler mixer bay · Textron 400, 400A, 400T and 2 more. Effective Dec 1, 2004 - [AD 2002-01-23](https://openairdocs.org/ad/2002-01-23): Left Engine Forward Carry-Through Mount Bracket · Textron 400, 400A, 400T and 2 more. Effective Feb 14, 2002 - [AD 2001-24-11](https://openairdocs.org/ad/2001-24-11): AFM - Emergency Procedures Section - Loss of Airspeed · Textron 400, 400A, 400T and 2 more. Effective Dec 11, 2001 - [AD 2001-03-06](https://openairdocs.org/ad/2001-03-06): Bleed Air Supply Tube Assembly · Textron 400, 400A, MU-300 and 1 more. Effective Mar 22, 2001 - [AD 2000-25-04](https://openairdocs.org/ad/2000-25-04): Anti-Skid Valve Assembly · Textron 400, 400A, 400T and 2 more. Effective Jan 17, 2001 - [AD 99-21-30](https://openairdocs.org/ad/99-21-30): AFM - Icing Conditions · Textron MU-300 and MU-300-10. Effective Nov 30, 1999 - [AD 98-06-30](https://openairdocs.org/ad/98-06-30): Outflow/Safety Valves · Textron 400, 400A, 400T and 2 more. Effective Apr 24, 1998 - [AD 92-15-02](https://openairdocs.org/ad/92-15-02): Engine Mounting System · Textron 400, MU-300 and MU-300-10. Effective Aug 18, 1992 - [AD 90-17-05](https://openairdocs.org/ad/90-17-05): Airplane Flight Manual (AFM) Changes - Fuel · Textron 400, MU-300 and MU-300-10 with STC SA1596NM or 2 others. Effective Sep 17, 1990 - [AD 86-10-03](https://openairdocs.org/ad/86-10-03): Placard - Fire Prevention · Textron MU-300 and MU-300-10. Effective Jun 2, 1986 Historical (superseded or no longer in force): - [AD 94-25-10](https://openairdocs.org/ad/94-25-10) (historical): AFM - Icing Conditions · Hawker Beechcraft 400, 400A, 400T and 2 more. Effective Dec 28, 1994 ## Registered aircraft (17) - [N103HC](https://openairdocs.org/aircraft/N103HC): [Estar Aerospace Corp](https://openairdocs.org/faa-owner/ESTAR%20AEROSPACE%20CORP), [Columbus, OH](https://openairdocs.org/faa-place/OH/Columbus), S/N A068 S.A. - [N250GP](https://openairdocs.org/aircraft/N250GP): [Csds Aircraft Sales & Leasing Inc](https://openairdocs.org/faa-owner/CSDS%20AIRCRAFT%20SALES%20%26%20LEASING%20INC), [Rllng Hls Est, CA](https://openairdocs.org/faa-place/CA/Rllng%20Hls%20Est), built 1984, S/N A069 S.A. - [N2WC](https://openairdocs.org/aircraft/N2WC): [Estar Aerospace Corp](https://openairdocs.org/faa-owner/ESTAR%20AEROSPACE%20CORP), [Columbus, OH](https://openairdocs.org/faa-place/OH/Columbus), S/N A047 S.A. - [N301AE](https://openairdocs.org/aircraft/N301AE): [Unlimited Boat Sales Inc](https://openairdocs.org/faa-owner/UNLIMITED%20BOAT%20SALES%20INC), [Page, AZ](https://openairdocs.org/faa-place/AZ/Page), S/N A091 S.A. - [N37CB](https://openairdocs.org/aircraft/N37CB): [Chexair LLC](https://openairdocs.org/faa-owner/CHEXAIR%20LLC), [Miami, FL](https://openairdocs.org/faa-place/FL/Miami), S/N A035 S.A. - [N399DM](https://openairdocs.org/aircraft/N399DM): [Solomon Mark Trustee](https://openairdocs.org/faa-owner/SOLOMON%20MARK%20TRUSTEE), [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington), built 1980, S/N A008 S.A. - [N400GK](https://openairdocs.org/aircraft/N400GK): [Central Virginia Aviation Inc](https://openairdocs.org/faa-owner/CENTRAL%20VIRGINIA%20AVIATION%20INC), [Petersburg, VA](https://openairdocs.org/faa-place/VA/Petersburg), built 1982, S/N A019 S.A. - [N400HH](https://openairdocs.org/aircraft/N400HH): [400hh Inc](https://openairdocs.org/faa-owner/400HH%20INC), [Oldwick, NJ](https://openairdocs.org/faa-place/NJ/Oldwick), S/N A025 S.A. - [N400UF](https://openairdocs.org/aircraft/N400UF): [Nova Jets USA Corp](https://openairdocs.org/faa-owner/NOVA%20JETS%20USA%20CORP), [Orlando, FL](https://openairdocs.org/faa-place/FL/Orlando), S/N A022 S.A. - [N405MG](https://openairdocs.org/aircraft/N405MG): [Km Operations LLC](https://openairdocs.org/faa-owner/KM%20OPERATIONS%20LLC), [Alpharetta, GA](https://openairdocs.org/faa-place/GA/Alpharetta), built 1982, S/N A021 S.A. - [N442EA](https://openairdocs.org/aircraft/N442EA): [Aziz Walid George Haddad](https://openairdocs.org/faa-owner/AZIZ%20WALID%20GEORGE%20HADDAD), [San Antonio, TX](https://openairdocs.org/faa-place/TX/San%20Antonio), built 1983, S/N A058SA - [N44MM](https://openairdocs.org/aircraft/N44MM): [Mike Moser Inc](https://openairdocs.org/faa-owner/MIKE%20MOSER%20INC), [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington), built 1984, S/N A080 S.A. - [N600GW](https://openairdocs.org/aircraft/N600GW): [G3x Aerospace Inc](https://openairdocs.org/faa-owner/G3X%20AEROSPACE%20INC), [Dover, DE](https://openairdocs.org/faa-place/DE/Dover), S/N A044S.A. - [N60EF](https://openairdocs.org/aircraft/N60EF): [Tvpx Aircraft Solutions Inc Trustee](https://openairdocs.org/faa-owner/TVPX%20AIRCRAFT%20SOLUTIONS%20INC%20TRUSTEE), [North Salt Lake, UT](https://openairdocs.org/faa-place/UT/North%20Salt%20Lake), built 1984, S/N A070SA - [N765KC](https://openairdocs.org/aircraft/N765KC): [Jetset LLC](https://openairdocs.org/faa-owner/JETSET%20LLC), [Denison, TX](https://openairdocs.org/faa-place/TX/Denison), built 1984, S/N A079 S.A. - [N907MX](https://openairdocs.org/aircraft/N907MX): [Tvpx Aircraft Solutions Inc Trustee](https://openairdocs.org/faa-owner/TVPX%20AIRCRAFT%20SOLUTIONS%20INC%20TRUSTEE), [North Salt Lake, UT](https://openairdocs.org/faa-place/UT/North%20Salt%20Lake), built 1983, S/N A036 S.A. - [N94LD](https://openairdocs.org/aircraft/N94LD): [Sky Aviation Holdings LLC](https://openairdocs.org/faa-owner/SKY%20AVIATION%20HOLDINGS%20LLC), [Pompano Beach, FL](https://openairdocs.org/faa-place/FL/Pompano%20Beach), built 1984, S/N A073 S.A. ## NTSB investigations (7) 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 CEN16IA091](https://openairdocs.org/ntsb/CEN16IA091), Jan 12, 2016: Mitsubishi MU 300 (N200LP), Little Rock, AR, incident, minor damage. Probable cause: The flight crew's inadequate preflight inspection of the airplane, during which they failed to see a fueling mat that had been placed on the inboard trailing edge of the right wing, which the right… - [NTSB CHI02FA097](https://openairdocs.org/ntsb/CHI02FA097), Mar 25, 2002: Mitsubishi MU-300 (N617BG), Anderson, IN, substantial damage. Probable cause: Missed approach not executed and flight to a destination alternate not performed by the flight crew. The tail wind and snow/ice covered runway were contributing factors. - [NTSB NYC02FA059](https://openairdocs.org/ntsb/NYC02FA059), Feb 11, 2002: Mitsubishi MU-300 (N541CW), Cleveland, OH, substantial damage. Probable cause: The pilot's failure to obtain the proper touch down point on the runway, and the pilot-in-commands failure to initiate a go-round. Factors in the accident were the tailwind condition, the… - [NTSB FTW00LA084](https://openairdocs.org/ntsb/FTW00LA084), Jan 27, 2000: Mitsubishi MU-300 (N900WJ), Dallas, TX, substantial damage. Probable cause: The diminished effectiveness of the anti-skid brake system due to the slush contaminated runway. Factors were the freezing rain encountered during the approach, coupled with a failure of the… - [NTSB CHI99LA093](https://openairdocs.org/ntsb/CHI99LA093), Feb 18, 1999: Mitsubishi 300 (N110DS), Columbus, NE, substantial damage. Probable cause: the pilot-in-command failed to attain the proper touchdown point during the landing. Factors associated with the accident were the rough, snow covered terrain encountered off the end of the runway,… - [NTSB CHI94FA050](https://openairdocs.org/ntsb/CHI94FA050), Dec 15, 1993: Mitsubishi MU-300 (N710MB), Goodland, KS, destroyed, 3 fatal. Probable cause: THE PILOT-IN-COMMAND'S INADVERTENT STALL OF THE AIRPLANE. A FACTOR ASSOCIATED WITH THE ACCIDENT IS THE PILOT-IN-COMMAND'S POOR IFR PROCEDURES. - [NTSB CHI86IA231](https://openairdocs.org/ntsb/CHI86IA231), Sep 25, 1986: Mitsubishi MU-300IA (N19R), Chicago, IL, incident, minor damage ## FAA accident and incident reports (23) 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 20221027011189I](https://openairdocs.org/incident/20221027011189I), Oct 27, 2022: Mitsubishi MU-300 (N44MM), Orlando, FL, Minor damage. On October 27, 2022 approximately 2 pm, [privacy data omitted] turning a 5 mile final to runway 07 the aircraft took a bird strike to the left side cockpit and… - [Incident 20210108004769I](https://openairdocs.org/incident/20210108004769I), Jan 8, 2021: Mitsubishi MU-300 (N442EA), Henderson, NV, Minor damage. The aircraft was inbound to the airport and was given instructions from the tower to make left traffic. After maneuvering the aircraft landed and the left wing… - [Incident 20200901021519I](https://openairdocs.org/incident/20200901021519I), Sep 1, 2020: Mitsubishi MU-300 (N214PG), Upland, CA, Minor damage. Beechjet (MU-300) N214PG departed chino airport (kcno) at 1539 local time on sep. 1, 2020 headed for Upland Cable Airport (kccb). During the landing on runway… - [Incident 20160112000659I](https://openairdocs.org/incident/20160112000659I), Jan 12, 2016: Mitsubishi MU-300 (N200LP), Little Rock, AR, Minor damage. On 01/12/2016 N200LP was taking off from lit located in Little Rock, Arkansas. Aircraft was being operated by an ATP rated pilot with a valid 1st class medical… - [Incident 20120310003699I](https://openairdocs.org/incident/20120310003699I), Mar 10, 2012: Mitsubishi MU-300 (N8LE), Ruston, LA, Minor damage. Aircraft dual generator failure and diversion to 5000 foot runway. The aircraft flaps could not be extented and the primary braking system not operable during… - [Incident 20041214034639I](https://openairdocs.org/incident/20041214034639I), Dec 14, 2004: Mtsbsi MU300 (N110DS), Cleveland, OH. (-23) Aircraft slid off the FAR end of runway 23 at Cuyahoga County Airport (cgf), Cleveland, Ohio. The runway was snow and ice covered. After leaving the… - [Accident 20020325006019A](https://openairdocs.org/incident/20020325006019A), Mar 25, 2002: Mtsbsi MU300 (N617BG), Anderson, IN, No damage. (-23) On 03/25/02, aircraft mitsubish MU-300-300, registration N617BG, slid off end of runway 30 during landing roll out at Anderson, IN (aid) airport due to… - [Accident 20020210005959A](https://openairdocs.org/incident/20020210005959A), Feb 10, 2002: Mtsbsi MU300 (N541CW), Cleveland, OH, No damage. (-23) Aircraft, an MU300 not equipped with thurst reversers was cleared for ILS to runway 23 at cgf. Winds were reported to crew as 310-360 at 12 knots. Type… - [Incident 20020119000849I](https://openairdocs.org/incident/20020119000849I), Jan 19, 2002: Mtsbsi MU300 (N617BG), Atlanta, GA, Minor damage. (-23) Mr. Solomon stated that they flew the ILS 20L into pdk and were visual last 1000 ft of the approach. They flew the calculated vref speed and landed as… - [Incident 20011228038739I](https://openairdocs.org/incident/20011228038739I), Dec 28, 2001: Mtsbsi MU300 (N417KT), Omaha, NE. (-23) Aircraft departed Omaha, NE, 50 miles south of Omaha. The crew reported smoke in the cockpit. Aircraft returned to Omaha and landed without incident.… - [Incident 20011119036959I](https://openairdocs.org/incident/20011119036959I), Nov 19, 2001: Mtsbsi MU300 (N399MM), Sarnia Ont, CN, Minor damage. (-23) The pilots stated that the approach was flown with a slight tailwind approximately 10 knots above vref. The second-in-command was the pilot flying. The… - [Incident 20011009032769I](https://openairdocs.org/incident/20011009032769I), Oct 9, 2001: Mtsbsi MU300 (N417KT), Omaha, NE. (-23) On October 10, 2001 at approximately 20:00 CDT a mitsubishi MU-300, N417KT experienced a loss of oil pressure on the right engine during descent through… - [Accident 20000127043969A](https://openairdocs.org/incident/20000127043969A), Jan 27, 2000: Mtsbsi MU300 (N900WJ), Dallas, TX, Substantial damage. (-23) During ILS approach to rwy 31R at dal, a warning light for ice accumulation on the horizontal stabilizer illuminated. The aircraft was landed at 120K in… - [Accident 19990218001539A](https://openairdocs.org/incident/19990218001539A), Feb 18, 1999: Mtsbsi MU300 (N110DS), Columbus, NE, Substantial damage. Acft landed on ice and snow, slid off the end of the rwy, and struck a piece of concrete under the snow. Other circumstances are unknown. (-23) pilot was… - [Incident 19980907028489I](https://openairdocs.org/incident/19980907028489I), Sep 7, 1998: Mtsbsi MU300 (N399MM), Greenville, NC, Minor damage. On landing, pilot noticed small deer run toward aircraft. Deer struck aircraft at nose gear. Aircraft taxied to hanger. Aircrafta was inspected the following… - [Incident 19980819031209I](https://openairdocs.org/incident/19980819031209I), Aug 19, 1998: Mtsbsi MU300 (N160H), Southbend, IN, Minor damage. While aircraft was in cruise flight, the pilot stated he felt the aircraft shudder. No abnormal operations or indications were observed, the pilot decided to… - [Incident 19970506012709I](https://openairdocs.org/incident/19970506012709I), May 6, 1997: Mtsbsi MU300 (N88ME), Rochester, NY. Narrative: on may 6, 1997, at approximately 1020 EDT, a MU-300, N88ME, operated by aerodynamics, inc., had an unsafe landing gear warning on approach to… - [Incident 19951209046749I](https://openairdocs.org/incident/19951209046749I), Dec 9, 1995: Mtsbsi MU300 (N300TS), Jackson, WY. Narrative: aircraft landed jac and slid off end of runway. Pilots state vref was 105 KTS. Computed landing distance 3350' at 26 degree f, .6 degrees downslope… - [Accident 19931215046889A](https://openairdocs.org/incident/19931215046889A), Dec 15, 1993: Mtsbsi MU300 (N710MB), Goodland, KS, Destroyed, 3 fatal. Stalled, impacted ground near airport on ILS approach. Recorder shows trouble with speed and intercept of localizer - [Incident 19920517025119I](https://openairdocs.org/incident/19920517025119I), May 17, 1992: Mtsbsi MU300 (N100RS), Chicago, IL, Minor damage. Crew failed to lower landing gear and landed gear up. - [Incident 19910312011999I](https://openairdocs.org/incident/19910312011999I), Mar 12, 1991: Mtsbsi MU300 (N134RG), Alexandria, MN, Minor damage. Unable to stop on a snow packed and ice covered runway. Departed end of runway stopping in a field. - [Incident 19861030064299I](https://openairdocs.org/incident/19861030064299I), Oct 30, 1986: Mtsbsi MU300 (N399MJ), Reno, NV. Left engine failed during cruise flight. Pilot secured engine and diverted to nearest suitable field. - [Incident 19860925083099I](https://openairdocs.org/incident/19860925083099I), Sep 25, 1986: Mtsbsi MU300 (N19R), Chicago, IL, Minor damage. Wing collided with truck on cargo taxiway. Driver not aware of taxiing aircraft. ATC had cleared driver to proceed. ## Service difficulty reports (35) As reported by operators and repair stations, by the model named in the report. - [SDR 2009FA0000054](https://openairdocs.org/sdr/2009FA0000054), Jan 14, 2009: RADOME. DAMAGED. WHILE PARKED, FBO PERSONNEL BACKED EQUIPMENT INTO NOSE OF AIRCRAFT FWD OF PRESSURE BULKHEAD. DAMAGE TO RADOME, PITOT TUBE, AND SKIN. AIRCRAFT WAS AUTHORIZED FOR - [SDR JX6A200800001](https://openairdocs.org/sdr/JX6A200800001), Jan 16, 2008: CABLE ASSY. KINKED. DURING LANDING IN FAY THE LT MLG DOOR CONTACTED THE RUNWAY. 3 DOWN & LOCKED LIGHTS WERE ILLUMINATED IN THE COCKPIT. MAINTENANCE DISCOVERED THE LT MLG EMERGENCY - [SDR 2007F00036](https://openairdocs.org/sdr/2007F00036), Apr 27, 2007: DOOR. CRACKED. DURING SCHEDULED A, B, & C INSPECTION FOUND CABIN ENTRANCE DOOR CASE ASSEMBLY P/N: 45A30096 CRACKED AT DOOR BUSHING HOLES. CASE ASSEMBLY IS NONE REPAIRABLE AND - [SDR 148J020807](https://openairdocs.org/sdr/148J020807), Feb 8, 2007: GCU. SHORTED. RT ENGINE WOULD NOT START. STARTER WOULD NOT ROTATE ENGINE AND TRIP CIRCUIT BREAKER. FOUND GCU BAD. - [SDR DIXA200600002](https://openairdocs.org/sdr/DIXA200600002), Nov 23, 2006: FUEL CONTROL. FAILED. DURING CLIMBOUT, FLIGHT CREW REPORTED THE RT ENGINE N1 (FAN) OVERSPED TO 116.8 PERCENT. ITT DID NOT EXCEED LIMITS. N2 WAS RT AT RED LINE LIMIT OF 97.0 PERCENT. - [SDR YP62006F00000](https://openairdocs.org/sdr/YP62006F00000), Oct 16, 2006: O-RING. LEAKING. DURING THE DESCENT, PILOTS NOTICE OIL PRESSURE LOW ON LT ENGINE AND CONTINUE SLOWLY DROPPING. PILOT TOOK IMMEDIATE ACTION CHECKING THE EMERGENCY PROCEDURE FOLLO - [SDR 148J063006](https://openairdocs.org/sdr/148J063006), Jun 30, 2006: BRAKE. FAILED. LEFT MAIN BRAKE FAILURE. - [SDR 2006FA0000696](https://openairdocs.org/sdr/2006FA0000696), Feb 10, 2006: WIRE. BURNED. SHORT CIRCUIT, WIRES BURNED ON LT CNTRL JUNCT BOX AREA. DURING SCHEDULED B INSP IAW MM, FOUND WIRES BURNED, DAMAGED ON CABLE LOOM CONNECTOR P AND J 230. DUE TO - [SDR DJFA2005074](https://openairdocs.org/sdr/DJFA2005074), Mar 13, 2005: LANDING GEAR. MALFUNCTIONED. KDAL - KBGM TRIP ID NR 797353 CREW REPORTED THAT AFTER GEAR RETRACTION FOLLOWING A FUEL STOP AT KLEX THE NOSE LANDING GEAR DROPPED AND LOCKED. GEAR WAS CYCLED T - [SDR JX62004F00001](https://openairdocs.org/sdr/JX62004F00001), Nov 10, 2004: ENGINE. FAILED. DURING DESCENT, THE FLIGHT CREW REDUCED THE POWER LEVERS TO IDLE. NOTICED THAT THE ENGINE PITCH NOISE CHANGED CONSIDERABLY. THE MASTER CAUTION LIGHT CAME ON WIT - [SDR A075SA2](https://openairdocs.org/sdr/A075SA2), Jan 25, 2004: UPLOCK ROLLER. OUT OF RIG. RT MAIN LANDING GEAR INBOARD DOOR DID NOT LOCK IN UP POSITION DURING GEAR EXTENSION. VERIFIED GEAR DOWN AND LOCKED, CONTINUED APPROACH, LANDED WITHOUT EVENT. IN - [SDR A063SA](https://openairdocs.org/sdr/A063SA), May 9, 2003: SQUAT SWITCH. MISRIGGED. UPON LANDING, THRUST REVERSERS FAILED TO DEPLOY AND SPEED BRAKES FAILED TO EXTEND. WHEEL BRAKES INITIALLY WORKED, BUT FAILED DURING ROLLOUT. THE USE OF EMERGENC - [SDR MGO2003F00001](https://openairdocs.org/sdr/MGO2003F00001), Jan 20, 2003: CONTROL CABLE. BROKEN. WHILE INVESTIGATING PILOT REPORT OF SPEED BRAKES. FAILURE TO DEPLOY IN FLIGHT. FOUND LT HAND FORWARD FLAP CABLE CORRODED INTO TWO PIECES INSIDE SWAGED TERMINAL. - [SDR JOU2002F00001](https://openairdocs.org/sdr/JOU2002F00001), Sep 26, 2002: VENTURI. CRACKED. PILOT REPORTED DURING A ROUTINE MAINTENANCE CHECK FLIGHT AT 10,000 FT., WHEN RIGHT OR LEFT (ONLY) BLEED AIR SUPPLY WAS SELECTED, CABIN PRESSURIZATION COULD NOT - [SDR S8A2002F00002](https://openairdocs.org/sdr/S8A2002F00002), Jun 1, 2002: LINE. RUPTURED. CREW REPORTED REAR DUCT OVERHEAT WARNING WHILE ON THE GROUND AWAITING DEPARTURE. TROUBLESHOOTING REVEALED RIGHT ENGINE BLEED AIR DUCT PN 45A63517-31 (SUPERCEDED - [SDR JG0201741](https://openairdocs.org/sdr/JG0201741), May 21, 2002: BRAKE ASSY. DISINTEGRATED. WHILE TAXIING AFTER LANDING FELT AIRCRAFT SHUTTER. STOPPED AIRCRAFT ON TAXIWAY AND VISUALY INSPECTED OUTSIDE OF AIRCRAFT NO DEFECTS NOTED. CONTINUED TAXI TO PAR - [SDR 482DM40802](https://openairdocs.org/sdr/482DM40802), Apr 8, 2002: TRANSCEIVER. FAULTY. RADAR INDICATOR COMES ON THE GOES OUT WITHIN 10 MINUTES. REMOVE AND REPLACE RADAR R/T. - [SDR 482DM40102](https://openairdocs.org/sdr/482DM40102), Apr 1, 2002: INDICATOR. MALFUNCTIONED. RADAR INDICATOR HAS A GOOD TEST PATTERN BUT WILL NOT PAINT WEATHER AND/OR GROUND. - [SDR 482DM32702](https://openairdocs.org/sdr/482DM32702), Mar 29, 2002: RECEIVER. UNRELIABLE. ADF INDICATOR INTERMITTENTLY WILL NOT LOCK ON SIGNAL, NEEDLE WOULD WANDER OFF STATION, THEN LOCK ON TO STATION. PILOT REPORTED THAT IT WAS UNRELIABLE. - [SDR 482DM32002](https://openairdocs.org/sdr/482DM32002), Mar 29, 2002: ANTENNA. DEBONDED. NR 1 COMMUNICATION RADIO DIFFICULT TO UNDERSTAND WHEN IN VISUAL MOISTURE. FOUND LEFT SIDE OF LEADING EDGE OF ANTENNA DEBONDED. - [SDR 2002FA0000182](https://openairdocs.org/sdr/2002FA0000182), Feb 8, 2002: PUSHROD. CHAFED. UPON INSPECTION, PILOT AND COPILOT RUDDER PEDAL PUSH RODS WERE FOUND SEVERELY CHAFED ON THE TOP SIDE, EVIDENTLY BY MAKING CONTACT WITH THE FLOOR SKIN. THIS COND - [SDR JEM2002F00000](https://openairdocs.org/sdr/JEM2002F00000), Dec 17, 2001: MOUNT. CRACKED. CONCERNING A VISUAL INSPECTION OF THE LT ENGINE CARRY THROUGH MOUNT BACKET FOR CRACKS ON MFG 400 NAD 400A. IT DOES NOT COVER THE MU-300 SERIES AIRCRAFT. WE IN S - [SDR A027SA](https://openairdocs.org/sdr/A027SA), Oct 9, 2001: UPLOCK. FAILED. RIGHT MAIN INBOARD GEAR DOOR (UPON LANDING) DID NOT LATCH IN UP POSITION, ALLOWING DOOR TO LOWER ITSELF TO PAVEMENT, CAUSING SKIN DAMAGE TO DOOR. - [SDR A083SA](https://openairdocs.org/sdr/A083SA), Oct 9, 2001: O-RING. DAMAGED. CREW OBSERVED OIL PRESSURE ON RIGHT ENGINE DROPPING FOLLOWED BY A MASTER WARNING. VERIFIED LOSS OF OIL PRESSURE OCCURRING. FLIGHT CREW SHUT RIGHT ENGINE DOWN PR - [SDR FJT01031261](https://openairdocs.org/sdr/FJT01031261), Mar 1, 2001: DOOR SEAL. WORN. BNA - CREW REPORTED DURING CLIMB TO 27,000 FT GOING THROUGH APPROXIMATELY 26,000 FT JUST PRIOR TO CABIN ATTAINING MAXIMUM DIFFERENTIAL A LOUD HOWL WAS HEARD FRO - [SDR DJFA200100011](https://openairdocs.org/sdr/DJFA200100011), Mar 5, 2000: LIGHT. INOPERATIVE. INSPECTION FOUND TAIL NAVIGATION LIGHT INOPERATIVE. BULB DISCOVERED TO BE BLOWN. REPLACED LAMP, OPS CHECK GOOD. MANY SIMILAR OCCURRENCES. - [SDR DJFA200100010](https://openairdocs.org/sdr/DJFA200100010), Feb 29, 2000: LIGHT. INOPERATIVE. INSPECTION FOUND TAIL NAVIGATION LIGHT INOPERATIVE. BULB DISCOVERED TO BE BLOWN. REPLACED LAMP, OPS CHECK GOOD. MANY SIMILAR OCCURRENCES. - [SDR 99ZZZX4679](https://openairdocs.org/sdr/99ZZZX4679), Dec 7, 1999: FILTER ASSY. MISINSTALLED. DURING A NORMAL INSPECTION, BOTH FUEL STRAINERS WERE FOUND INSTALLED BACKWARDS. WITH FUEL FLOW IN THE WRONG DIRECTION, THE BYPASS ANNUNCIATOR WOULD BE INOPERATI - [SDR 99ZZZX823](https://openairdocs.org/sdr/99ZZZX823), Feb 3, 1999: DUCT. CRACKED. AN INVESTIGATION WAS CONDUCTED TO DETERMINE THE CAUSE OF A VERY SUBSTANTIAL BLEED AIR LEAK IN THE TAIL COMPARTMENT. THE LEAK WAS TRACED TO A DRILLED HOLE IN THE - [SDR 98ZZZX478](https://openairdocs.org/sdr/98ZZZX478), Jan 21, 1998: TORQUE TUBE. MISALIGNED. DURING A AND B CHECK, AIRCRAFT TECHNICIANS FOUND AIRCRAFT RUDDER DISPLACED TO THE RIGHT APPROXIMATELY 3 INCHES. THIS CONDITION WAS FOUND WITH RUDDER CONTROL SYS - [SDR 97ZZZX2545](https://openairdocs.org/sdr/97ZZZX2545), May 14, 1997: CONTROL CABLE. BROKE. ON APPROACH, CREW SELECTED LANDING GEAR DOWN, BUT RECEIVED NO GEAR INDICATION. CREW CYCLED GEAR, RECEIVED NO INDICATION. PERFORMED EMERG EXT PROCEDURE IAW FLT M - [SDR 97ZZZX1089](https://openairdocs.org/sdr/97ZZZX1089), Jan 27, 1997: RELEASE CABLE. BROKEN. DURING A POST-FLIGHT INSP DAMAGE WAS NOTICED ON THE LT FUSELAGE MLG DOOR, THE AFT SIDE COVER ASSEMBLY, AND THE MIDDLE FUSELAGE SKIN ASSY. AFTER FURTHER INSP THE - [SDR 96ZZZX5601](https://openairdocs.org/sdr/96ZZZX5601), Oct 8, 1996: CONTROL CABLE. FAILED. DURING ROUTINE A-CHECK INSPECTION WHILE PERFORMING EMERGENCY GEAR EXTENSION CHECK, RIGHT HAND GEAR DOOR WOULD NOT OPEN. INVESTIGATED DISCREPANCY AND FOUND SWAGE - [SDR 96ZZZX4336](https://openairdocs.org/sdr/96ZZZX4336), Jul 19, 1996: BYPASS DUCT. FAILED. A CRACK DEVELOPED AT THE FORWARD FLANGE OF THE AFT INNER BYPASS DUCT AT THE 6 O'CLOCK POSITION ALLOWING IT TO COME OUT OF THE MATING FLANGE AND ENTER THE AIR FL - [SDR 96ZZZX834](https://openairdocs.org/sdr/96ZZZX834), Feb 2, 1996: BUSHINGS. SEIZED. UPPER TORQUE KNEE PIVOT BUSHINGS WOULD NOT ACCEPT GREASE. DISASSEMBLED TORQUE KNEE FROM AIRCRAFT AND FOUND GREASE HOLE IN BUSHING NOT ALIGNED WITH GALLERY IN CA ## STCs that may be installed (OpenAirDocs) (73, first 50) Approved for this model: the STC's model list names it on its data sheet, or a series that includes it. In force first, then newest. The registry doesn't record which STCs an aircraft has. - [STC ST01305WI-D](https://openairdocs.org/stc/ST01305WI-D): Modification of a Collins ALT-50A or ALT-55B Radio Altimeter system installation to a Collins ALT-1000 or ALT-4000 Radio Altimeter system installation in accordance with Collins Drawing Index as listed on AML No. ST01305WI-D, Revision -, or later FAA approved revision. Rockwell Collins Inc - [STC ST12461IB](https://openairdocs.org/stc/ST12461IB): Installation of Cockpit Voice Recorder with optional RIPS Upgrade. Mid- Canada Mod Center - [STC SA2622NM](https://openairdocs.org/stc/SA2622NM): Installation of Precise Flight Pulselite Control Unit in landing/taxi system. (767-200 B17) (DHC-8 101). Precise Flight Inc - [STC ST04740NY](https://openairdocs.org/stc/ST04740NY): Installation of LAI Windshields. Lee Aerospace Inc - [STC ST03424CH](https://openairdocs.org/stc/ST03424CH): Certification of Automatic Dependent Surveillance - Broadcast (ADS-B) Out System with Rockwell Collins TDR-94/-94D Transponders. CMD Flight Solutions LLC - [STC ST04723NY](https://openairdocs.org/stc/ST04723NY): Installation of LAI Windshields. Lee Aerospace Inc - [STC ST01930LA](https://openairdocs.org/stc/ST01930LA): Installation of Sandel Avionics SN4500 Electronic Horizontal Situation Indicator (EHSI). Sandel Avionics LLC - [STC SA3891NM](https://openairdocs.org/stc/SA3891NM): Modification for increased ramp, takeoff, landing, and maximum zero fuel weights. New Flight Corporation - [STC ST01935WI](https://openairdocs.org/stc/ST01935WI): Installation of windshield. Lee Aerospace - [STC ST01805WI](https://openairdocs.org/stc/ST01805WI): Modification of Rockwell Collins TCAS II System Installation with DC powered TCAS Transmitter Receiver Processor. Rockwell Collins Inc - [STC SA5933SW](https://openairdocs.org/stc/SA5933SW): Installation of a freon air conditioning system for use up to 18,000 feet. Air Comm Corporation - [STC SA00526SE](https://openairdocs.org/stc/SA00526SE): Installation of emergency medical stretcher and base, oxygen, and electrical systems. LifePort LLC - [STC ST04340NY](https://openairdocs.org/stc/ST04340NY): Installation of TCAS 7.1 (ACAS II) upgrade of Prior Existing TCAS 7.0. Scandinavian Avionics Design ApS - [STC ST00347BO](https://openairdocs.org/stc/ST00347BO): Modification to upgrade a BendixKing CAS 67A TCAS II system to CAS 67B TCAS II Change 7.1. Pro Star Aviation, LLC - [STC ST00276WI](https://openairdocs.org/stc/ST00276WI): Installation of Kedeg Company 21BC11e Coaleser Assemly. Purolator Facet, Inc - [STC SA1596NM](https://openairdocs.org/stc/SA1596NM): Installation of extended range fuselage auxiliary fuel tank. Sierra Industries Ltd - [STC SA1597NM](https://openairdocs.org/stc/SA1597NM): Installation of aft fuselage fuel tank fill system. Sierra Industries Ltd - [STC SA1598NM](https://openairdocs.org/stc/SA1598NM): Installation of tailcone baggage compartment modification,including access door modification. Sierra Industries Ltd - [STC SA2714NM](https://openairdocs.org/stc/SA2714NM): Installation of extended range fuselage auxiliary fuel tank. Sierra Industries Ltd - [STC SA2736NM](https://openairdocs.org/stc/SA2736NM): Installation of two-zone temperature control system MU-300 (S/N A023SA only). Sierra Industries Ltd - [STC SA2737NM](https://openairdocs.org/stc/SA2737NM): Installation of aft fuselage maintenance access doors. Sierra Industries Ltd - [STC ST00965AT](https://openairdocs.org/stc/ST00965AT): Installation of pilot and co-pilot seat crotch belt. Textron Aviation Inc - [STC SA2499SO](https://openairdocs.org/stc/SA2499SO): Installation of Whelen flashing anticollision light, P/N 90033. Textron Aviation Inc - [STC ST00804AT](https://openairdocs.org/stc/ST00804AT): Installation of external power overvoltage protection system. Textron Aviation Inc - [STC ST00345AT](https://openairdocs.org/stc/ST00345AT): Installation of emergency lighting system improvement modification. Textron Aviation Inc - [STC ST00769AT](https://openairdocs.org/stc/ST00769AT): Installation of replacement emergency power supply. Textron Aviation Inc - [STC ST01326AT](https://openairdocs.org/stc/ST01326AT): Installation of replacement cabin door step and assist handle. Textron Aviation Inc - [STC ST02625AT](https://openairdocs.org/stc/ST02625AT): Installation of a LED Tail Position Navigation Light Replacement. Textron Aviation Inc - [STC ST02774AT](https://openairdocs.org/stc/ST02774AT): Installation of Dual Innovative Solutions and Support (IS&S) Air Data Display Units (ADDU) and a Single Analog Interface Unit (AIU). Textron Aviation Inc - [STC ST02850AT](https://openairdocs.org/stc/ST02850AT): Certification of Reduced Vertical Separation Minimum (RVSM) Operational capability. Textron Aviation Inc - [STC SA2202SO](https://openairdocs.org/stc/SA2202SO): Installation of environmental control system per Hangar One. Textron Aviation Inc - [STC ST00383WI](https://openairdocs.org/stc/ST00383WI): Installation of the Rosemount Model0871CT1 Ice Detector System. Textron Aviation Inc - [STC ST00780WI-D](https://openairdocs.org/stc/ST00780WI-D): Modification of Collins VHF-22A/VHF-22B VHF COMM Receiver Transmitter with CTL-22 Control Pro Line II System Installation to a Collins VHF-22C/VHF-22D VHF COMM Receiver Transmitter with CTL-22C Control 8.33 kHz Pro Line II System Installation. Textron Aviation Inc - [STC ST00781WI-D](https://openairdocs.org/stc/ST00781WI-D): Modification of Collins VHF-20/VHF-20A/VHF-20B VHF COMM Receiver Transmitter with CTL-20 Control Pro Line I System Installation to a Collins VHF-22C/VHF-22D VHF COMM Receiver Transmitter with CTL-22C Control 8.33 kHz Pro Line II System Installation. Textron Aviation Inc - [STC SA1903CE](https://openairdocs.org/stc/SA1903CE): Installation of Sperry EDZ-600 electronic flight instrument system (pilot's position). Textron Aviation Inc - [STC SA1905CE](https://openairdocs.org/stc/SA1905CE): Relocation of No. 1 and No. 2 static inverters from nose to aft section of the airplane. Textron Aviation Inc - [STC SA5539SW](https://openairdocs.org/stc/SA5539SW): Installation of equipment shelf in aft fuselage. Textron Aviation Inc - [STC SA5564SW](https://openairdocs.org/stc/SA5564SW): Installation of Sundstrand Model AV557C cockpit voice recorder system. Textron Aviation Inc - [STC SA5630SW](https://openairdocs.org/stc/SA5630SW): Installation of Lockheed Model 310 flight data recorder. Textron Aviation Inc - [STC ST03776NY](https://openairdocs.org/stc/ST03776NY): Modification to upgrade existing Rockwell Collins TCAS (Model: TTR-920, TTR-921, and TTR-4000) at VERSION 7.0 to Rockwell Collins TCAS (Model: TTR-921, TTR-4000, and TTR-4100) at VERSION 7.1 (ACAS II). Scandinavian Avionics Design ApS - [STC SA1902CE](https://openairdocs.org/stc/SA1902CE): Installation of Sperry Primus 800 weather radar system. Textron Aviation Inc - [STC ST04238AT](https://openairdocs.org/stc/ST04238AT): Upgrade of Honeywell Traffic Collision Avoidance Systems II (TCAS II) Processor Software from TCAS II Version 7.0 to TCAS II Version 7.1. Aviation Partners Group Inc - [STC SA3894NM](https://openairdocs.org/stc/SA3894NM): Installation of medical stretcher left or right side. Aviation Fabricators Inc - [STC ST00673WI-D](https://openairdocs.org/stc/ST00673WI-D): Modification of Collins VHF-22A/VHF-22B VHF COMM Receiver Transmitter with CTL-22 Control Pro Line II System Installation to a Collins VHF-22C/VHF-22D VHF COMM Receiver Transmitter with CTL-22C Control 8.33 kHz Pro Line II System installation. Rockwell Collins Inc - [STC ST00682WI-D](https://openairdocs.org/stc/ST00682WI-D): Modification of Collins VHF-20/VHF-20A/VHF-20B VHF COMM Receiver Transmitter with CTL-20 Control Pro Line I System Installation to a Collins VHF-22C/VHF-22D VHF COMM Receiver Transmitter with CTL-22C Control 8.33 kHz Pro Line II System Installation in accordance with Collins Installation Instructions as listed on AML No. ST00682WI-D, Revision -, or later FAA approved revisions. Rockwell Collins Inc - [STC ST09579SC](https://openairdocs.org/stc/ST09579SC): Installation of a Traffic Alert and Collision Avoidance System (TCAS) 2000. Hawker Beechcraft Services Inc - [STC ST09589SC](https://openairdocs.org/stc/ST09589SC): Installation of an AlliedSignal Enhanced Ground Proximity Warning System (EGPWS). Hawker Beechcraft Services Inc - [STC SA3646SW](https://openairdocs.org/stc/SA3646SW): Establish 264 KIAS Vmo at 8,000 feet or below and 264 KIAS linear variation to 320 KIAS at 11,000 feet. Install IDC P/N 37277-2139//3139 maximum allowable airspeed/ mach indicator. Intercontinental Jet Service Corporation - [STC ST00562DE](https://openairdocs.org/stc/ST00562DE): Installation of a pilot's and co-pilot's digital air data display unit. AeroMech Incorporated - [STC ST00091AT](https://openairdocs.org/stc/ST00091AT): Installation of an aircraft security system. Raytheon Aircraft Services Inc All 73: https://openairdocs.org/model/mitsubishi-mu-300/stcs.md ## PMA parts (OpenAirDocs) (217, 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. - [TR-46056-3](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID142308714120250908153055.0001): Bushing – Torque Knee. Aerospace Turbine Rotables · PMA PQ3736CE · Replaces Beech Aircraft Corp. (Raytheon… · Aug 27, 2025 - [RFS5004743](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID118122882420250424175705.0001): Swage, Adjusting. Rapco Fleet Support Inc · PMA PQ2386CE · Replaces 5004743 · Apr 22, 2025 - [RFS8B7](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID128303272320250401174123.0001): Rivet. Rapco Fleet Support Inc · PMA PQ2386CE · Replaces GYR8B7 · Mar 31, 2025 - [APS-GYR8B7](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID182680532420250131173803.0001): Rivet. Aviation Products Systems Inc · PMA PQ3830CE · Replaces GYR8B7 · Jan 21, 2025 - [APS-GY18B11](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID137309194820250131173801.0001): Rivet. Aviation Products Systems Inc · PMA PQ3830CE · Replaces GY18B11 · Jan 21, 2025 - [APS5007921](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID112792459020250131173805.0001): Wear Pad. Aviation Products Systems Inc · PMA PQ3830CE · Replaces 5007921 · Jan 21, 2025 - [APS-GY18A14](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID106456890920250131173759.0001): Rivet. Aviation Products Systems Inc · PMA PQ3830CE · Replaces GY18A14 · Jan 21, 2025 - [LAC45AS31001-024-70](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID173973362620241106135459.0001): Windshield Assy Heated, RH (CoolView). Lee Aerospace, Inc. · PMA PQ3766CE · Modification part · Nov 1, 2024 - [LAC45AS31001-024](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID148574595520241106135458.0001): Windshield Assy Heated, RH. Lee Aerospace, Inc. · PMA PQ3766CE · Modification part · Nov 1, 2024 - [LAC45AS31001-023-70](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID119274227820241106135458.0001): Windshield Assy Heated, LH (CoolView). Lee Aerospace, Inc. · PMA PQ3766CE · Modification part · Nov 1, 2024 - [LAC45AS31001-023](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID114629887820241106135457.0001): Windshield Assy Heated, LH. Lee Aerospace, Inc. · PMA PQ3766CE · Modification part · Nov 1, 2024 - [HWP7072-4](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID124854259820250304194238.0001): Performed Packing. Hemico Inc. · PMA PQ2145NE · Replaces 9524796 · Oct 16, 2024 - [LA45AS31001T-023A](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID197070637020241001211806.0001): Windshield Assy Heated, LH. Lee Aerospace, Inc. · PMA PQ3766CE · Modification part · Aug 28, 2024 - [LA45AS31001T-024](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID193701058120241001211807.0001): Windshield Assy Heated, RH. Lee Aerospace, Inc. · PMA PQ3766CE · Modification part · Aug 28, 2024 - [LA45AS31001T-023](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID182323362220241001211806.0001): Windshield Assy Heated, LH. Lee Aerospace, Inc. · PMA PQ3766CE · Modification part · Aug 28, 2024 - [LA45AS31001T-023-70](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID175459904120241001211807.0001): Windshield Assy Heated, LH (CoolView). Lee Aerospace, Inc. · PMA PQ3766CE · Modification part · Aug 28, 2024 - [LA45AS31001T-023A-70](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID171932292020241001211807.0001): Windshield Assy Heated, LH (CoolView). Lee Aerospace, Inc. · PMA PQ3766CE · Modification part · Aug 28, 2024 - [LA45AS31001T-024A-70](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID162717679720241001211808.0001): Windshield Assy Heated, RH (CoolView). Lee Aerospace, Inc. · PMA PQ3766CE · Modification part · Aug 28, 2024 - [LA45AS31001T-024-70](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID135623083120241001211808.0001): Windshield Assy Heated, RH (CoolView). Lee Aerospace, Inc. · PMA PQ3766CE · Modification part · Aug 28, 2024 - [LA45AS31001T-024A](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID116286460520241001211807.0001): Windshield Assy Heated, RH. Lee Aerospace, Inc. · PMA PQ3766CE · Modification part · Aug 28, 2024 - [M23065-1341](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID136309153020240328193745.0001): Air Inlet. Miraj Corporation · PMA PQ0870NE · Replaces 23065-1341 · Mar 20, 2024 - [M06-200001](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID150992302220240223153731.0001): Label. Miraj Corporation · PMA PQ0870NE · Replaces Safran 06-200001 · Feb 15, 2024 - [5004743AB](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID143070927820230824130828.0001): Swage, Adjuster. Aero Brake & Spares Inc · PMA PQ0694SW · Replaces 5004743 · Jun 9, 2023 - [129836-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID170938381020230803185038.0001): Low Limit Sensor. Honeywell International Inc. · PMA PQ1222NM · Replaces 45AS3018-159 · Nov 4, 2022 - [129834-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID116307424620230803185044.0001): Temp Sensor. Honeywell International Inc. · PMA PQ1222NM · Replaces 45AS63018-155 · Nov 4, 2022 - [979580-5](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID105265017420230803185043.0001): Shutoff Valve. Honeywell International Inc. · PMA PQ1222NM · Replaces 45AS63018-079 · Nov 4, 2022 - [M2005-71](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID213842640020211220180012.0001): Brush, Electrical Contact. Miraj Corporation · PMA PQ0870NE · Replaces 23080-1971 · Sep 22, 2021 - [SJ8665 FP-084](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID417180030020211021172553.0001): Radome Boot. 3M Aerospace · PMA PQ04414CE · Modification part · Aug 30, 2021 - [SJ8665 FP-084](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID115176121202110211726020.0001): Radome Boot. 3M Aerospace · PMA PQ04414CE · Modification part · Aug 30, 2021 - [NOHIPOT](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID161452533920240320173407.0001): Decal. Augusta Aero Innovations LLC · PMA PQ04441CE · Replaces 06-201020 · Oct 6, 2020 - [EGR-525-00](https://drs.faa.gov/browse/excelExternalWindow/EA8EA89B05A41BC4862585690051C709.0001): Air Medical System. LifePort, LLC. · PMA PQ0172NM · Modification part · Jul 31, 2019 - [AG247000-04](https://drs.faa.gov/browse/excelExternalWindow/F4D9B388DAECF53586258553004D4A85.0001): Gasket - L-Band Antenna. Aviation Devices & Electronic Components, LLC · PMA PQ03846SW · Modification part · Jun 25, 2019 - [443613-00](https://drs.faa.gov/browse/excelExternalWindow/FE732206F3742AAA86258560003BDD25.0001): Harness, 833613-00. Shadin Avionics · PMA PQ2088CE · Replaces 443613-00 · Jun 6, 2019 - [613603-00](https://drs.faa.gov/browse/excelExternalWindow/F474BD51883E678086258560003BDD89.0001): Bracket, AFID RA Mount. Shadin Avionics · PMA PQ2088CE · Replaces 613603-00 · Jun 6, 2019 - [833613-00](https://drs.faa.gov/browse/excelExternalWindow/E9293882A965D1D286258560003BDC47.0001): ADS-B Flight ID Adapter. Shadin Avionics · PMA PQ2088CE · Replaces 833613-00 · Jun 6, 2019 - [613604-00](https://drs.faa.gov/browse/excelExternalWindow/C99B32ED23A9740F86258560003BDDC9.0001): Bracket, AFID Side Mount. Shadin Avionics · PMA PQ2088CE · Replaces 613604-00 · Jun 6, 2019 - [833613-10](https://drs.faa.gov/browse/excelExternalWindow/99326314CB6EBE8F86258560003BDCEA.0001): Digital Discrete Adapter (DDA). Shadin Avionics · PMA PQ2088CE · Replaces 833613-10 · Jun 6, 2019 - [613606-00](https://drs.faa.gov/browse/excelExternalWindow/501E105EA0BF714E86258560003BDE36.0001): Bracket, AFID Under Mount. Shadin Avionics · PMA PQ2088CE · Replaces 613606-00 · Jun 6, 2019 - [443613-10](https://drs.faa.gov/browse/excelExternalWindow/313ABE429C4C505186258560003BDD5A.0001): Harness, DDA. Shadin Avionics · PMA PQ2088CE · Replaces 443613-10 · Jun 6, 2019 - [613605-00](https://drs.faa.gov/browse/excelExternalWindow/078709A82EB7C91386258560003BDDF9.0001): Bracket, AFID Top Mount. Shadin Avionics · PMA PQ2088CE · Replaces 613605-00 · Jun 6, 2019 - [04320073-0005B](https://drs.faa.gov/browse/excelExternalWindow/8213C712E21826E486258550005032DE.0001): LCD Display Module. Optical Display Engineering · PMA PQ04407CE · Replaces Honeywell P/N 04320073-0005 · May 30, 2019 - [MCG-1900](https://drs.faa.gov/browse/excelExternalWindow/C5FE45C228B3339F86258474006122F8.0001): Dampener Hub. Miraj Corporation · PMA PQ0870NE · Replaces 23032-1900 · Feb 24, 2019 - [9524796WE](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID100946453920240830180816.0001): Packing, Preformed. Wencor, LLC · PMA PQ1370NM · Replaces 9524796 · Oct 17, 2018 - [M23032-2710](https://drs.faa.gov/browse/excelExternalWindow/98EF27A0292FF3CE862582CF006DC090.0001): Dampener Plate. Miraj Corporation · PMA PQ0870NE · Replaces 23032-2710 · Jun 17, 2018 - [21BC112](https://drs.faa.gov/browse/excelExternalWindow/5C2947413AFB692D86258244006F1F88.0001): Coalescer Assembly. Purolator Facet Inc (formerly Facet Filter Products) · PMA PQ1207CE · Modification part · Jan 18, 2018 - [04320073-0005B](https://drs.faa.gov/browse/excelExternalWindow/C7B9A18130E6FB24862581AE0077E6F0.0001): LCD DISPLAY MODULE. Optical Display Engineering · PMA PQ5342NM · Replaces 04320073-0005 · Sep 5, 2017 - [04320073-0005B](https://drs.faa.gov/browse/excelExternalWindow/2691AB4003318B528625818A006F0151.0001): LCD DISPLAY MODULE. Optical Display Engineering · PMA PQ5342NM · Replaces 04320073-0005 · Aug 2, 2017 - [21BC130G](https://drs.faa.gov/browse/excelExternalWindow/7ABBEF1C27001A518625819A00790D89.0001): Coalescer Assembly. Purolator Facet Inc (formerly Facet Filter Products) · PMA PQ1207CE · Replaces 21BC112, Including Attaching Hardware… · Jul 13, 2017 - [833613-00](https://drs.faa.gov/browse/excelExternalWindow/B58F1D94BA606C32862580F4006A88EF.0001): ADS-B Flight ID Adapter. Shadin Avionics · PMA PQ2088CE · Replaces 833613-00 · Mar 13, 2017 - [613606-00](https://drs.faa.gov/browse/excelExternalWindow/A6441B538423DE94862580F4006A88FA.0001): Bracket, AFID Under Mount. Shadin Avionics · PMA PQ2088CE · Replaces 613606-00 · Mar 13, 2017 All of them: https://openairdocs.org/model/mitsubishi-mu-300/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.