# Boeing 737-81Q - Type: Aircraft model (FAA registry) - Registry code: 13844GE - Manufacturer (registry): BOEING - Model: 737-81Q - Aircraft type: Fixed wing multi engine - Category: Airplane - Engines: 2 · Turbo-fan - Seats: 149 - Weight class: 20,000 lb and over - Certification: Type certificated - Registered aircraft: 1 - Page: https://openairdocs.org/model/boeing-737-81q 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. None matched. ## Registered aircraft (1) - [N732MA](https://openairdocs.org/aircraft/N732MA): [Wells Fargo Trust Co Na Trustee](https://openairdocs.org/faa-owner/WELLS%20FARGO%20TRUST%20CO%20NA%20TRUSTEE), [Columbia, MD](https://openairdocs.org/faa-place/MD/Columbia), built 2001, S/N 30618 ## 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 DCA19MA143](https://openairdocs.org/ntsb/DCA19MA143), May 4, 2019: Boeing 737 (N732MA), Jacksonville, FL, substantial damage. Probable cause: An extreme loss of braking friction due to heavy rain and the water depth on the ungrooved runway, which resulted in viscous hydroplaning. Contributing to the accident was the operator’s inadequate… - [NTSB DCA18WA279](https://openairdocs.org/ntsb/DCA18WA279), Aug 20, 2018: Boeing 737 (N520AM), Guadalajara, Mexico, incident, no damage ## FAA accident and incident reports (2) 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 20120927021219I](https://openairdocs.org/incident/20120927021219I), Sep 27, 2012: Boeing 737-81Q (N732MA), Concord, NC, Minor damage. Pilot attempted to make a positioning right turn onto runway 020 from taxiway b at the jqf airport. The aircraft right main tire truck went off of the… - [Incident 20050726031629I](https://openairdocs.org/incident/20050726031629I), Jul 26, 2005: Boeing 73781Q (N732MA), Miami, FL, Minor damage. (-23) While ac was being marshalled into gate E-25, the leading edge of left wing struck an improperly parked catering truck. Air carrier stated that the… ## Service difficulty reports (174, newest 50) As reported by operators and repair stations, by the model named in the report. - [SDR 2025F00254](https://openairdocs.org/sdr/2025F00254), Oct 31, 2025: A/C PACK. TRIPPED. FLIGHT 393 HVN-ATL. OCT. 31, 2025. RIGHT PACK OVERHEAT THEN TRIP OFF AND SMOKE ODOR IN THE FLIGHT DECK AND CABIN. AIR RETURN TO BDL. - [SDR ASMF20200603015](https://openairdocs.org/sdr/ASMF20200603015), Mar 12, 2020: TRIM SYSTEM. OUT OF ADJUST. DURING TRANSIT CHECK, IT WAS DETECTED THAT THE HORIZONTAL STABILIZER TRIM MOVEMENT WAS OUT OF RANGE. MAINTENANCE PERSONNEL PERFORMED REVISION TO STABILIZER DETE - [SDR ASMF20200602001](https://openairdocs.org/sdr/ASMF20200602001), Feb 3, 2020: SENSOR. FAILED. AIRCRAFT RETURNED TO PLATFORM DUE TO DURING PUSH BACK, IT WAS DETECTED SPOILER ASYMMETRY DURING FLIGHT CONTROLS CHECK. MAINTENANCE PERSONNEL PERFORMED FLIGHT CO - [SDR MYWA202001280284](https://openairdocs.org/sdr/MYWA202001280284), Jan 25, 2020: BALLAST. INOPERATIVE. FWD L/H EMERGENCY EXIT WALL LIGHT INOP. REFERENCE LOG PAGE 255569. - [SDR ASMF2019100912](https://openairdocs.org/sdr/ASMF2019100912), Sep 8, 2019: SENSOR. DAMAGED. AIRCRAFT REJECTED TAKE OFF BEFORE AT 70 KNOTS DUE TO AFT CARGO DOOR LIGHT TURNED ON. MAINTENANCE PERSONNEL PERFORMED REVISION TO AFT SERVICE DOOR IAW AMM 52-71- - [SDR MYWA201908010146](https://openairdocs.org/sdr/MYWA201908010146), Jul 30, 2019: BULKHEAD WEB. CRACKED. DURING PHASE CHECK 76, FOUND A 19 INCH CRACK IN THE LEFT WHEEL WELL VAPOR BARRIER BETWEEN LBL 6.15 AND LBL 10.54. THE CRACK IS OUT OF LIMITS IAW SRM 57-10-10 AL - [SDR K8FF2018123100112](https://openairdocs.org/sdr/K8FF2018123100112), Dec 30, 2018: BLADE. SHEARED. MIAMI AIR INTL LOGPAGE 254162-3: "DURING FLIGHT AT 33000 FT IDG DRIVE AMBER LIGHT FOLLOWED BY HIGH VIBRATION #1 ENGINE. UPON LANDING, VISUAL INSPECTION REVEALED - [SDR MYWA201912170104](https://openairdocs.org/sdr/MYWA201912170104), Dec 13, 2018: BATTERY PACK. INOPERATIVE. RH AFT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED M01671 BATTERY PACK ASSEMBLY. OPS CHECK NORMAL IAW AMM 33-51-06. SEE MAI LP 2558920-6 - [SDR MYWA2018110300037](https://openairdocs.org/sdr/MYWA2018110300037), Nov 3, 2018: POWER SUPPLY. INOPERATIVE. BOTH LEFT AND RIGHT FWD EMERGENCY OVERWING EXIT SIDEWALL LIGHT WAS INOPERATIVE. TROUBLESHOT THE SYSTEM, REMOVED AND REPLACED THE LT MID SECTION EMERGENCY POWER - [SDR MYWA2019F00084](https://openairdocs.org/sdr/MYWA2019F00084), Oct 8, 2018: BATTERY PACK. DISCHARGED. FORWARD LEFT CABIN EMERGENCY EXIT LIGHTS INOPERATIVE. BATTERY PACK REPLACED. REF LP 260660-5. - [SDR MYWA2018FA0000400](https://openairdocs.org/sdr/MYWA2018FA0000400), Sep 29, 2018: RING ASSEMBLY. CRACKED. LEFT HAND WHEEL WELL RING SUPPORT ASSEMBLY IS CRACKED AND BROKEN UNDER PANEL 193CL. CORRECTIVE ACTION ACCOMPLISHED PER THE SRM 53-40-71, 51-40-02 AND 51-70-13. - [SDR ASMF2018101509022](https://openairdocs.org/sdr/ASMF2018101509022), Sep 25, 2018: HYDRAULIC LINE. DAMAGED. LOW PRESSURE HYDRAULIC PUMP SYSTEM B. CAPTAIN REPORTED THAT DURING CRUISE THE LOW PRESSURE HYDRAULIC PUMP SYSTEM B LIGHTS TURNED ON, SO FLIGHT CREW ACCOMPLISHED - [SDR ASMF20180918013](https://openairdocs.org/sdr/ASMF20180918013), Aug 23, 2018: VALVE. FAILED. AIRCRAFT PERFORMED AN EMERGENCY DESCENT DUE TO PRESSURIZATION SYSTEM FAILURE. MAINTENANCE PERSONNEL PERFORMED BITE TO CABIN PRESSURE CONTROLLERS IAW AMM 21-31-0 - [SDR ASMF200180918005](https://openairdocs.org/sdr/ASMF200180918005), Jul 22, 2018: STARTER. DAMAGED. AIRCRAFT PERFORMED AN UNSCHEDULED LANDING AT MZT DUE TO DURING CRUISE, THE LEFT ENGINE PRESENTED LOW OIL QUANTITY INDICATION; SO FLIGHT CREW ACCOMPLISHED THE QR - [SDR MYWA2018071100095](https://openairdocs.org/sdr/MYWA2018071100095), Jul 10, 2018: BATTERY PACK. DISCHARGED. FORWARD RIGHT HAND PASSENGER CABIN EMERGENCY LIGHTS INOPERATIVE. THE BATTERY PACK WAS REPLACED. - [SDR MYWA2019052300021](https://openairdocs.org/sdr/MYWA2019052300021), May 20, 2018: BALLAST. FAILED. RIGHT AFT EMERGENCY EXIT LIGHTS WERE INOPERATIVE. THE BALLAST WAS REPLACED. - [SDR MYWA201905230020](https://openairdocs.org/sdr/MYWA201905230020), May 20, 2018: BALLAST. FAILED. DURING THE PRE FLIGHT TRANSIT CHECK, THE RIGHT AFT EMERGENCY EXIT LIGHTS WERE INOPERATIVE. THE BALLAST WAS REPLACED. - [SDR ASMF201802003](https://openairdocs.org/sdr/ASMF201802003), Feb 12, 2018: SENSOR. MALFUNCTIONED. CAPTAIN REPORTED THAT AFTER LANDING, FLAPS AND SLATS LEADING EDGE DID NOT RETRACT, MAINTENANCE PERFORMED A BITE TEST IAW FIM 27-51 DETECTING FAULT 27-53252, THE - [SDR ASMF201801017](https://openairdocs.org/sdr/ASMF201801017), Jan 5, 2018: SLAT SYSTEM. MALFUNCTIONED. CAPTAIN REPORTED THAT AFTER LANDING THE FLAPS AND SLATS DO NOT RETRACT. MAINTENANCE PERSONNEL PERFORMED BITE TO FSEU IAW FIM 27-53 TASK 803 PROCEDURE, NO CONFIR - [SDR ASMF201708008](https://openairdocs.org/sdr/ASMF201708008), Aug 23, 2017: SPOILER SYS. MALFUNCTIONED. AIRCRAFT RETURNS TO PLATFORM DUE TO DURING FLIGHT CONTROLS TESTS CAPTAIN REPORTED THAT SPOILERS DID NOT REACH THE MAXIMUM EXTENSION. AIRCRAFT WAS SENT TO HANGAR - [SDR ASMF201708003](https://openairdocs.org/sdr/ASMF201708003), Aug 6, 2017: CONTROL PANEL. MALFUNCTIONED. CAPTAIN REPORTED THAT DURING APPROACH AUTOTHROTTLE DISENGAGES CONTINUOUSLY, LEFT COURSE CAN NOT BE ADJUSTED DURING DESCENT PROCEDURE AND FLIGHT DIRECTOR CAPTAIN - [SDR ASMF20170717008](https://openairdocs.org/sdr/ASMF20170717008), Jun 29, 2017: COAX. DAMAGED. DURING TRANSIT CHECK CAPTAIN REPORTED IAS/MACH STAYS IN 100 OF ALTITUDE BUT SHOWS 50000 FT OF ALTITUDE AND NO NAV INDICATION, MAINTENANCE PERFORMED FIM PROCEDUR - [SDR ASMF201704017](https://openairdocs.org/sdr/ASMF201704017), Apr 28, 2017: SKIN. DAMAGED. DURING TRANSIT CHECK, IT WAS DETECTED A FOREIGN OBJECT DAMAGE IN THE LEFT INBOARD FLAP OF 4.843 LENGTH, 0.062 DEPTH, 2.718 WIDE. MAINTENANCE PERSONNEL PERFORMED - [SDR ASMF201703006](https://openairdocs.org/sdr/ASMF201703006), Mar 10, 2017: SENSOR. DAMAGED. AIRCRAFT PERFORMED AN EMERGENCY DESCENT AT GDL DUE TO DURING CLIMB, THE LEFT BLEED TRIP OFF LIGHT TURNED ON AND CONTROL PRESS AUTO, SEMI AUTO AND MANUAL WITH NO - [SDR ASMF201702003](https://openairdocs.org/sdr/ASMF201702003), Jan 6, 2017: SENSOR. FAILED. AIRCRAFT RETURNED TO GATE DUE TO A LE FLAP TRANSIT LIGHT ILLUMINATED AND LE DEVICE SLAT 1 LIGHT DID NOT ILLUMINATE. PERFORMED A BITE OF THE FSEU IAW FIM 27-51 T - [SDR ASMF2016072600016](https://openairdocs.org/sdr/ASMF2016072600016), Jun 8, 2016: AXLE. DAMAGED. DURING TRANSIT CHECK, IT WAS DETECTED A HIGH TEMPERATURE LOW PRESSURE AT MAIN WHEEL ASSY NUMBER 4. MAINTENANCE PERSONNEL PERFORMED THE FLAT SPOTTED TIRES CONDIT - [SDR ASMF201605007](https://openairdocs.org/sdr/ASMF201605007), Mar 17, 2016: OVEN. DEFECTIVE. AIRCRAFT RETURNED TO PLATFORM DUE TO AFTER ENGS START, SMOKE WAS DETECTED IN AFT GALLEY. PERFORMED SMOKE OR FUMES IN CABIN CONDITIONAL INSPECTION IAW MM 05-51-5 - [SDR ASMF201602010](https://openairdocs.org/sdr/ASMF201602010), Feb 10, 2016: DOOR. OUT OF ADJUST. CAPTAIN REPORTED THAT DURING CLIMB, THE FWD ENTRY DOOR LIGHT TURNED ON. ACFT WAS SENT TO THE HANGAR & MX PERFORMED FWD ENTRY DOOR ADJUSTMENT IAW AMM 52-11-00 TA - [SDR MYWA201510130001](https://openairdocs.org/sdr/MYWA201510130001), Oct 13, 2015: BATTERY PACK. FAILED. R1 DOOR EMERGENCY LIGHT BATTERY PACK FAILED. - [SDR ASMF201510024](https://openairdocs.org/sdr/ASMF201510024), Sep 29, 2015: PITOT TUBE. BLOCKED. AIRCRAFT REJECTED TAKEOFF AT 80 KNOTS DUE TO EICAS MSG IAS DISAGREE & A DIFFERENCE OF 10 KNOTS BETWEEN SPEEDOMETERS BEING BIGGEST LT SIDE. PERFORMED FIM 31-62 T - [SDR ASMF201510019](https://openairdocs.org/sdr/ASMF201510019), Sep 14, 2015: WARNING SYSTEM. FALSE ACTIVATION. AIRCRAFT RETURNED TO PLATFORM DUE TO DURING BOTH ENGINE START, THE EEC ALT MODE LIGHTS TURNED ON. PERFORMED BITE TO BOTH EEC’S IAW AMM 73-21-00, CONTINUING THE - [SDR MYWA201506180001](https://openairdocs.org/sdr/MYWA201506180001), Jun 18, 2015: BULB. FAILED. L1 EMERGENCY EGRESS LIGHT INOPERATIVE. - [SDR MYWA201506020001](https://openairdocs.org/sdr/MYWA201506020001), Jun 2, 2015: LIGHT. INOPERATIVE. L1 DOOR EMERGENCY EXIT LIGHT INOPERATIVE. - [SDR MYWA201505300001](https://openairdocs.org/sdr/MYWA201505300001), May 28, 2015: BATTERY PACK. INOPERATIVE. EMERGENCY LIGHT BATTERY PACK AT FS 500C RT, FOUND INOPERATIVE DURING MAINTENANCE CHECK. - [SDR ASMF201507004](https://openairdocs.org/sdr/ASMF201507004), May 20, 2015: FLAP SYSTEM. MALFUNCTIONED. CAPTAIN REPORTED THAT DURING APPROACH, TE FLAP DISAGREE WITH FLAPS INDICATOR STAYING IN 2 UNITS & DECLARED AN EMERGENCY. ACCOMPLISHED WITH THE PROCEDURE TO EXTE - [SDR ASMF201503023](https://openairdocs.org/sdr/ASMF201503023), Mar 9, 2015: WARNING SYSTEM. FALSE ACTIVATION. AIRCRAFT PERFORMED AN UNSCHEDULED LANDING, DUE TO DURING CRUISE, THE FUEL QTY PRESENTED LOW FUEL QTY INDICATION. PERFORMED REVISION OF FUEL LEAKS & CABIN FUEL I - [SDR ASMF201503010](https://openairdocs.org/sdr/ASMF201503010), Feb 24, 2015: SHUTOFF VALVE. MALFUNCTIONED. DURING FUELING, A FUEL SPILLAGE IN THE LT TANK OCCURRED DUE TO THE SOV DID NOT CLOSE. THE PLATFORM WAS CLEANED BY FIREMEN & MX PERSONNEL CLEANED THE SELECTOR & - [SDR ASMF201503009](https://openairdocs.org/sdr/ASMF201503009), Jan 31, 2015: DRIVE UNIT. FAILED. AIRCRAFT RETURNED TO PLATFORM DUE TO DURING TAXING, THE EICAS MSG WXR FAIL WAS SHOWN. DURING MX REVISION, THE TRANSCEIVER & RADAR WERE DETECTED FAILED IAW AMM 3 - [SDR ASMF201408002](https://openairdocs.org/sdr/ASMF201408002), Jul 20, 2014: PITOT LINE. LOOSE. AIRCRAFT REJECTED TAKEOFF AT 100 KNOTS DUE TO EICAS MSG IAS DISAGREE. PERFORMED PITOT SYS REVISION BY CONDITION, DETECTING A LT ADM LINE LOOSEN, SO THE ADM LINE - [SDR ASMF2014061706013](https://openairdocs.org/sdr/ASMF2014061706013), May 7, 2014: WHEEL. DAMAGED. DURING TRANSIT CHECK, DETECTED THE FOUR MLG WHEELS WITH DAMAGES OUT OF LIMITS. THE WHEELS WERE REPLACED IAW AMM 32-45-11, ALL CORRECT. - [SDR CA140318002](https://openairdocs.org/sdr/CA140318002), Mar 13, 2014: LINE. BROKEN. (CAN) ON MARCH 13, 2014, DURING FLIGHT, ACFT EXPERIENCED A DUCT PRESSURE INDICATION, LT AND RT POINTERS WERE NOT THE SAME, SPLIT. THIS OCCUR WHILE THE ENGINE WA - [SDR MYWA20140116001](https://openairdocs.org/sdr/MYWA20140116001), Jan 16, 2014: SMOKE DETECTOR. FALSE ACTIVATION. DURING FLIGHT, FORWARD LAVATORY SMOKE DETECTOR ACTIVATED. THERE WAS NO SMOKE FIRE OR FUMES. MAINTENANCE FOUND SMOKE DETECTOR PROBE NOT SECURED PROPERLY. SWAPPED - [SDR ASMF201312004](https://openairdocs.org/sdr/ASMF201312004), Nov 24, 2013: CONTROL VALVE. FAILED. AIRCRAFT RETURNED TO PLATFORM, DURING TAXING THE RT PACK TEMP REACHED MORE THAN 60 CELSIUS DEGREES & BOTH PACKS REACHED LESS THAN 18 CELSIUS DEGREES IN PAX CABI - [SDR ASMF201310004](https://openairdocs.org/sdr/ASMF201310004), Sep 19, 2013: MECHANISM. OUT OF ADJUST. AIRCRAFT REJECTED TAKEOFF AT 70 KNOTS WITH 54,600 KG WEIGHT, DUE TO CONFIGURATION ALARM. DURING MX REVISION, THE SPEED BRAKE LEVER FAILED; THE HIGH ENERGY STOP - [SDR MYWA20130813001](https://openairdocs.org/sdr/MYWA20130813001), Aug 13, 2013: POWER SUPPLY. INOPERATIVE. EMERGENCY LIGHTS FROM MID CABIN TO AFT LT SIDEWALL WILL NOT TURN OFF. TROUBLESHOT AND FOUND EMERGENCY POWER SUPPLY AT LT AT MID CABIN SIDEWALL AT FAULT. R & R E - [SDR MYWA20130703001](https://openairdocs.org/sdr/MYWA20130703001), Jul 3, 2013: BATTERY PACK. INOPERATIVE. ON P/T FOUND LEFT OVERWINE EMERGENCY EXIT LIGHTS TURNING OFF AFTER 20 SECONDS SWITCH ON. TROUBLESHOT AND FOUND BAD BATTERY PACK AT POWER SUPPLY STA 565 LT SIDE. - [SDR ASMF201306010](https://openairdocs.org/sdr/ASMF201306010), Jun 17, 2013: FIRE WARNING. FALSE ACTIVATION. ACFT RETURNED, DURING CLIMB THE FWD CARGO FIRE WARNING AND MASTER FIRE WARNING LIGHTS TURNED ON AND WITH FIRE WARNING AUDIBLE ALARM. DURING MX REVISION, THE DIS - [SDR MYWA20130612001](https://openairdocs.org/sdr/MYWA20130612001), Jun 12, 2013: POWER SUPPLY. INOPERATIVE. EMERGENCY LIGHTS INOPERATIVE. TROUBLESHOOTING FOUND BAD POWER SUPPLY, R & R POWER SUPPLY FOR R1 DOOR LIGHT IAW AMM 33-51-06. OPS CHECKED GOOD. - [SDR 39NR20130612008](https://openairdocs.org/sdr/39NR20130612008), Jun 11, 2013: FRAME. DAMAGED. DURING PHASE 48, INSPECTION FOUND FUSELAGE FRAME DAMAGED AT BS 727C, ABOVE STRINGER 25 LEFT. INSTALLED REPAIR PER 737-800 SRM 51-70-11. - [SDR 39NR20130612007](https://openairdocs.org/sdr/39NR20130612007), Jun 11, 2013: FRAME. DAMAGED. DURING PHASE 48, INSPECTION FOUND FUSELAGE FRAME DAMAGED AT BS 727I ABOVE STRINGER 25 LEFT. INSTALLED REPAIR IAW SRM 51-70-11. All 174: https://openairdocs.org/model/boeing-737-81q/reports.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.