# N732MA: 2001 Boeing 737-81Q

- Status: Valid registration
- Airframe: [Boeing 737-81Q](https://openairdocs.org/model/boeing-737-81q) (registry code 13844GE, 149 seats)
- Engine: [CFM International CFM56-7B26 series](https://openairdocs.org/engine/cfm-international-cfm56-7b26-series) (registry code 13045)
- Serial number: 30618
- Year built: 2001
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: November 10, 2010
- Certificate issued: August 24, 2016
- Expires: August 31, 2029
- Mode S code: A9D38D
- Registered owner: [Wells Fargo Trust Co Na Trustee](https://openairdocs.org/faa-owner/WELLS%20FARGO%20TRUST%20CO%20NA%20TRUSTEE)
- Location: [Columbia, MD](https://openairdocs.org/faa-place/MD/Columbia)
- Owner type: Corporation
- Owner's area on the map: 39.2060° N, 76.8282° W: Placed by OpenAirDocs at the center of ZIP code 21045, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=732MA
- Page: https://openairdocs.org/aircraft/N732MA

From the FAA registry file of October 24, 2026. ADs below are matched by the registry's airframe and engine model codes. They may apply; each AD's applicability can narrow it by serial number, part number or installed equipment. This is not a compliance determination. The registry lists only the engine series, so ADs for every CFM International CFM56-7B26 model are included.

## ADs that may apply (OpenAirDocs): 19 in force

### Matched by airframe (Boeing 737-81Q)

None in force.

### Matched by engine (CFM International CFM56-7B26 series)

- [AD 2023-05-05](https://openairdocs.org/ad/2023-05-05): Turbine Engine Compressor Section · CFM International CFM56-5B1, CFM56-5B1/2P, CFM56-5B1/3 and 98 more. Effective May 10, 2023
- [AD 2022-02-03](https://openairdocs.org/ad/2022-02-03): Turbine Engine Accessory Drive · CFM International CFM56-3, CFM56-3B, CFM56-3C and 34 more. Effective Mar 22, 2022
- [AD 2021-16-08](https://openairdocs.org/ad/2021-16-08): Turbine Section · CFM International CFM56-5B1, CFM56-5B1/2P, CFM56-5B1/P and 55 more. Effective Sep 28, 2021
- [AD 2018-26-01](https://openairdocs.org/ad/2018-26-01): Turbine Engine Compressor Section · CFM International CFM56-7B20, CFM56-7B20/2, CFM56-7B20/3 and 46 more. Effective Jan 10, 2019
- [AD 2018-09-51](https://openairdocs.org/ad/2018-09-51): Engine · CFM International CFM56-7B20, CFM56-7B20/2, CFM56-7B20/3 and 46 more. Effective Jun 7, 2018
- [AD 2015-18-04](https://openairdocs.org/ad/2015-18-04): 73-tooth gearshaft located in the engine accessory gearbox (AGB) · CFM International CFM56-3, CFM56-7B20, CFM56-7B20/2 and 47 more. Effective Oct 20, 2015
- [AD 2015-04-02](https://openairdocs.org/ad/2015-04-02): Dual engine thrust instability event · CFM International CFM56-7B20, CFM56-7B20/2, CFM56-7B20/3 and 46 more. Effective Mar 31, 2015
- [AD 2010-13-09](https://openairdocs.org/ad/2010-13-09): Stage 3 low-pressure turbine (LPT) · CFM International CFM56-5, CFM56-5-A1/F, CFM56-5A4 and 88 more. Effective Jul 26, 2010
- [AD 2010-01-05](https://openairdocs.org/ad/2010-01-05): LP turbine rear frames · CFM International CFM56-7B20, CFM56-7B20/2, CFM56-7B20/3 and 25 more. Effective Feb 18, 2010
- [AD 2009-11-02](https://openairdocs.org/ad/2009-11-02): HPC 4-9 spools · CFM International CFM56-2, CFM56-2A, CFM56-2B and 109 more. Effective Jun 23, 2009
- [AD 2008-03-09](https://openairdocs.org/ad/2008-03-09): Low pressure turbine rear frames (TRFs) · CFM International CFM56-7B18, CFM56-7B20, CFM56-7B22 and 10 more. Effective Mar 10, 2008
- [AD 2006-26-01](https://openairdocs.org/ad/2006-26-01): Fuel filters · CFM International CFM56-2, CFM56-2A, CFM56-2B and 93 more. Effective Jan 3, 2007
- [AD 2002-16-18](https://openairdocs.org/ad/2002-16-18): Low pressure turbine (LPT) nozzle segments · CFM International CFM56-5B1, CFM56-5B1/2P, CFM56-5B1/P and 33 more. Effective Sep 18, 2002
- [AD 2002-13-03](https://openairdocs.org/ad/2002-13-03): Turbofan Engines · CFM International CFM56-2, CFM56-2A, CFM56-2B and 55 more. Effective Aug 1, 2002
- [AD 2001-11-05](https://openairdocs.org/ad/2001-11-05): No. 4 Bearings · CFM International CFM56-2, CFM56-2B, CFM56-3 and 45 more. Effective Jun 11, 2001
- [AD 2001-02-12](https://openairdocs.org/ad/2001-02-12): On-Wing Torque Inspection · CFM International CFM56-7B20, CFM56-7B20/2, CFM56-7B22 and 11 more. Effective Feb 14, 2001
- [AD 98-21-23](https://openairdocs.org/ad/98-21-23): Electronic Engine Control · CFM International CFM56-7B20, CFM56-7B20/2, CFM56-7B22 and 10 more. Effective Nov 2, 1998
- [AD 98-19-20](https://openairdocs.org/ad/98-19-20): Hydromechanical Unit · CFM International CFM56-7B20, CFM56-7B20/2, CFM56-7B22 and 7 more. Effective Oct 7, 1998
- [AD 98-14-51](https://openairdocs.org/ad/98-14-51): Accessory Gearbox · CFM International CFM56-7B20, CFM56-7B20/2, CFM56-7B22 and 10 more. Effective Oct 1, 1998

### Historical (superseded or no longer in force)

- [AD 2021-10-09](https://openairdocs.org/ad/2021-10-09) (historical): Turbine Engine Compressor Section · CFM International CFM56-5B1, CFM56-5B1/2P, CFM56-5B1/3 and 82 more. Effective Jun 24, 2021
- [AD 2019-12-05](https://openairdocs.org/ad/2019-12-05) (historical): Turbine Section · CFM International CFM56-5B1, CFM56-5B1/2P, CFM56-5B1/P and 39 more. Effective Jul 5, 2019
- [AD 2018-18-01](https://openairdocs.org/ad/2018-18-01) (historical): Turbine Engine Compressor Section · CFM International CFM56-7B20, CFM56-7B20/2, CFM56-7B20/3 and 46 more. Effective Oct 16, 2018
- [AD 2018-10-11](https://openairdocs.org/ad/2018-10-11) (historical): Turbine Engine Compressor Section · CFM International CFM56-7B20, CFM56-7B20/2, CFM56-7B20/3 and 46 more. Effective Jun 1, 2018
- [AD 2018-09-10](https://openairdocs.org/ad/2018-09-10) (historical): Turbine Engine Compressor Section · CFM International CFM56-7B20, CFM56-7B20/2, CFM56-7B20/3 and 46 more. Effective May 14, 2018
- [AD 2013-26-01](https://openairdocs.org/ad/2013-26-01) (historical): Oil dynamic seal assembly · CFM International CFM56-3, CFM56-3B, CFM56-3C and 52 more. Effective Feb 3, 2014
- [AD 2000-12-01](https://openairdocs.org/ad/2000-12-01) (historical): Critical Life-Limited Parts · CFM International CFM56-2, CFM56-2A, CFM56-2B and 54 more. Effective Dec 11, 2000

## Information bulletins (advisory) (1 in force)

- [SAIB NE-08-17R3](https://openairdocs.org/saib/NE-08-17R3): Turbine Section - Propulsion Technology LLC Unapproved Repair. Issued May 28, 2014
- [SAIB NE-08-17R2](https://openairdocs.org/saib/NE-08-17R2) (historical): Turbine Section - Propulsion Technology LLC Unapproved Repair. Issued Mar 7, 2011
- [SAIB NE-08-17R1](https://openairdocs.org/saib/NE-08-17R1) (historical): Propulsion Technology LLC Unapproved Repair. Issued May 22, 2008
- [SAIB NE-08-17](https://openairdocs.org/saib/NE-08-17) (historical): Propulsion Technologies International Unapproved Repair. Issued May 14, 2008

## NTSB investigations (1)

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…

## 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 (52, newest 50)

As reported by operators and repair stations. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [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 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 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 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 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 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 UAL2013F00006](https://openairdocs.org/sdr/UAL2013F00006), May 8, 2013: CARGO TRACK. CORRODED. DURING PHASE 48 INSPECTION, FOUND CORROSION IN FWD CARGO BIN FLOOR TRACK AT LBL 18 AT BODY STA 500H+15. REPLACED FLOOR TRACK FROM BODY STATION 500G+12 TO 520 IA
- [SDR UAL2013F00005](https://openairdocs.org/sdr/UAL2013F00005), May 8, 2013: FLOORBEAM. CORRODED. DURING PHASE 48 INSPECTION, FOUND CORROSION ON 986 FLOORBEAM, LBL20 TO RBL 20. REPLACED T-CHORD ON FLOORBEAM FROM LBL 50 TO RBL 50 IAW SRM 53-70-51.
- [SDR UAL2013F00004](https://openairdocs.org/sdr/UAL2013F00004), May 8, 2013: FITTING. CORRODED. DURING PHASE 48 INSP FOUND CORROSION IN AFT OUTER MOUNT FITTING FOR A LAVATORY. REPLACED MOUNT FITTING IAW 25-46-99 SPM.
- [SDR MYW2013F00002](https://openairdocs.org/sdr/MYW2013F00002), May 8, 2013: FLOORBEAM. CORRODED. DURING PHASE 48 INSPECTION FOUND CORROSION ON 986 FLOORBEAM, LBL 20. REPLACED T CHORD ON FLOORBEAM FROM LBL 50 TO RBL 50 IAW SRM 53-70-51.
- [SDR MYW2013F00001](https://openairdocs.org/sdr/MYW2013F00001), May 8, 2013: CARGO TRACK. CORRODED. DURING PHASE 48 INSPECTION, FOUND CORROSION IN FWD CARGO BIN FLOOR TRACK AT LBL 18 AT BODY STATION 500H+15. REPLACED FLOOR TRACK FROM BODY STATION 500G+12 TO 52
- [SDR MYW2013F00000](https://openairdocs.org/sdr/MYW2013F00000), May 8, 2013: MOUNT FITTING. CORRODED. DURING PHASE 48 INSPECTION, FOUND CORROSION IN AFT OUTER MOUNT FITTING FOR A LAVATORY. REPLACED MOUNT FITTING IAW 25-46-99 AND SPM.
- [SDR 2013F00001](https://openairdocs.org/sdr/2013F00001), Dec 30, 2012: LAMP. INOPERATIVE. DURING A PREFLIGHT TRANSIT CHECK, MX NOTED AN EMERGENCY ISLE LIGHT AT ROW 14 ABC WAS DIM. LAMPED EMERGENCY ISLE LIGHT AT ROW 14 ABC. OPS CHECKED NORMAL.
- [SDR MYWA07232012732](https://openairdocs.org/sdr/MYWA07232012732), Jul 23, 2012: WARNING LIGHT. ILLUMINATED. AFTER ENGINE START "TR UNIT" LIGHT ILLUMINATED.
- [SDR MYWA05212012732](https://openairdocs.org/sdr/MYWA05212012732), May 21, 2012: TIRE. SEPARATED. DURING GEAR RETRACTION NOSE GEAR NOISE WAS LOUDER THAN NORMAL ALL OTHER INDICATIONS NORMAL. FOUND LEFT FWD TIRE ASSEMBLY HAS A SPLIT ON INNER SIDEWALL AND AN AR
- [SDR MYWA120037](https://openairdocs.org/sdr/MYWA120037), Mar 25, 2012: UNKNOWN. MALFUNCTIONED. ETOPS SIGNIFICANT SYSTEM: RIGHT PACK TRIP ILLUMINATED AFTER ENG START. PERFORMED CABIN CONTROLLER BITE IAW FIM TASK 21-31 TASK 822 CLEARED FAULT PACK TRIP EXT.
- [SDR MYWA120005](https://openairdocs.org/sdr/MYWA120005), Jan 16, 2012: UNKNOWN. MALFUNCTIONED. ETOPS SIGNIFICANT SYSTEM: APU FAULT LIGHT ON START. MAINT MESSAGE 49-31016, OVERTEMP SHUT DOWN. PERFORMED BITE TEST OF APU IAW 737-800 FIM 49-60 TASK 801. FOUND
- [SDR MYWA110123](https://openairdocs.org/sdr/MYWA110123), Dec 1, 2011: UNKNOWN. LEAKING. ETOPS SIGNIFICANT SYSTEM: DURING WALKAROUND FOUND FUEL DRIPPING FROM HPTCC DRAIN. ACCOMPLISHED ACTUATOR TEST IAW 737-800 AMM (TEST 12) ACTUATOR TEST PASSED, NO 
- [SDR MYWA110116](https://openairdocs.org/sdr/MYWA110116), Nov 28, 2011: SMOKE DETECTOR. INOPERATIVE. ETOPS SIGNIFICANT SYSTEM: AFT CARGO FIRE DETECTION "B" LOOP WILL NOT TEST. ACCOMPLISHED BITE TEST ON AFT CARGO ELECTRONICS UNIT. FOUND B1 DETECTOR AT FAULT. REM
- [SDR MYWA110101](https://openairdocs.org/sdr/MYWA110101), Sep 28, 2011: LOCK. POPPED. POWER ADVANCED FOR T/O, WARN LTS RIGHT FWD & AFT OVERWING EXIT LTS ON, T/O ABORTED APPROX 20 KTS. DURING T/S FOUND R OVERWING FLT LOCK POPPED. RESET C/B LIGHTS 
- [SDR MYWA110097](https://openairdocs.org/sdr/MYWA110097), Sep 14, 2011: FIRE WARNING. MALFUNCTIONED. ETOPS SIGNIFICANT SYSTEM: CARGO FIRE TEST FAILED AFT CARGO FIRE LIGHT DOES NOT COME ON DETECTOR FAULT LIGHT COMES ON DET SELECT SWITCH AT "B". PERFORMED FIM 26-
- [SDR MYWA110091](https://openairdocs.org/sdr/MYWA110091), Aug 24, 2011: DISPLAY. INOPERATIVE. ETOPS SIGNIFICANT SYSTEM: WEATHER RADAR RETURNS WEAK CAPTAIN'S SIDE. ADDITIONAL INFO, WEATHER RADAR (CAPTAIN'S SIDE) DISPLAY INTERMITTENT. T/S IAW FIM 31-62 TAS
- [SDR MYWA110073](https://openairdocs.org/sdr/MYWA110073), Jul 12, 2011: WARNING SYSTEM. INTERMITTENT. ETOPS SIGNIFICANT SYSTEM: APU FAULT LIGHT 492-020-00. PERFORMED APU BITE TEST IAW FIM 49-60 TASK 801 FOUND FAULT TO BE INTERMITTENT LIGHT EXTINGUISHED OK TO CON
- [SDR MYWA110070](https://openairdocs.org/sdr/MYWA110070), Jul 9, 2011: SHUTOFF VALVE. MALFUNCTIONED. ETOPS SIGNIFICANT SYSTEM: APU FAULT LIGHT. REMOVED AND REPLACED S/O VALVE ASSY, OPS CHECK GOOD IAW AMM 28-25-02.
- [SDR MYWA110062](https://openairdocs.org/sdr/MYWA110062), Jun 25, 2011: RELAY. FAILED. ETOPS SIGNIFICANT SYSTEM: WITH 5000K LEFT IN CENTER TANK LT FUEL BOOST PUMP LIGHT CAME ON AND STAYED ON, PUMP TURNED OFF, LIGHT WENT OFF. PERFORMED FIM 28-22-80
- [SDR MYWA110061](https://openairdocs.org/sdr/MYWA110061), Jun 22, 2011: INDICATION SYS. ACTIVATED. ETOPS SIGNIFICANT SYSTEM: AFTER NR 2 REVERSER DEPLOYED NR 2 ENGINE CONTROL LIGHT CAME ON. PERFORMED NR 2 ENGINE BITE TEST NO FAULTS FOUND DURING BITE TEST. GROU
- [SDR MYWA110060](https://openairdocs.org/sdr/MYWA110060), Jun 21, 2011: WARNING SYSTEM. INTERMITTENT. ETOPS SIGNIFICANT SYSTEM: LEFT CENTER FUEL TANK LOW PRESSURE LIGHT ILLUMINATES INTERMITTENTLY. PERFORMED OPS TEST OF LEFT CENTER FUEL TANK BOOST PUMP NO PROBLEM
- [SDR MYWA110053](https://openairdocs.org/sdr/MYWA110053), Jun 16, 2011: HMU. MALFUNCTIONED. ETOPS SIGNIFICANT SYSTEM: NR 2 ENG CONTROL LIGHT CAME ON DURING LANDING. REMOVED AND INSTALLED HMU PER AMM 73-21-10 RAN ENGINE & TESTED PER AMM 71-00-00, ALL CH
- [SDR MYWA110052](https://openairdocs.org/sdr/MYWA110052), Jun 15, 2011: INDICATION SYS. FALSE ACTIVATION. ETOPS SIGNIFICANT SYSTEM: NR 2 ENGINE CONTROL LIGHT CAME ON DURING LANDING ROLL OUT. PERFORMED FIM 73-06 TASK 801 FAULTS CLEARED RAN ENG AND PERFORMED FMC/EEC B
- [SDR MYWA110049](https://openairdocs.org/sdr/MYWA110049), Jun 11, 2011: SWITCH. MALFUNCTIONED. ETOPS SIGNIFICANT SYSTEM: START VALVE OPEN ALERT ON ENGINE NR 2. REMOVED AND REPLACED NR 2 ENGINE START SWITCH IAW B737-800 MM 80-11-00. STARTED NR 2 ENGINE TWI
- [SDR MYWA110044](https://openairdocs.org/sdr/MYWA110044), May 28, 2011: SMOKE DETECTOR. MALFUNCTIONED. ETOPS SIGNIFICANT SYSTEM: AFT CARGO COMPARTMENT LOOP "A" FAILED CARGO FIRE TEST. REMOVED AND REPLACED AFT CARGO COMPT POSITION "A3" SMOKE DETECTOR IAW AMM. OPS 
- [SDR MYWA110006](https://openairdocs.org/sdr/MYWA110006), Jan 20, 2011: IDG. INOPERATIVE. ETOPS SIGNIFICANT SYSTEM: AFTER ENGINE START, NR 1 DRIVE LIGHT ILLUMINATED AND GENERATOR WOULD NOT GO ON LINE. REMOVED AND REPLACED NR 1 IDG IAW MM 24-11-11. DM
- [SDR MYWA110002](https://openairdocs.org/sdr/MYWA110002), Jan 5, 2011: CONNECTOR. DIRTY. ETOPS SIGNIFICANT SYSTEM: NR 2 ENGINE FIRE DETECTION LOOP "B" WOULD NOT TEST. CLEANED CONNECTOR DP1620 ON NR 2 ENGINE FIRE WALL IAW WDM 26-11-21 OPS CHECK NORMA
- [SDR MYWA100136](https://openairdocs.org/sdr/MYWA100136), Dec 26, 2010: A/C PACK. INOPERATIVE. ETOPS SIGNIFICANT SYSTEM: PACK LIGHT COMES ON UNEXPECTEDLY DURING MASTER CAUTION RECALL. RIGHT PACK INOP.
- [SDR MYWA100133](https://openairdocs.org/sdr/MYWA100133), Dec 19, 2010: CONNECTOR. LOOSE. ETOPS SIGNIFICANT SYSTEM: NR 2 ENGINE FIRE DETECTION "B" LOOP HAS FAULT LIGHT. FOUND CONNECTOR LOOSE ON PYLON. RE-SECURED AND OPS CHECKED OK.
- [SDR MYWA100132](https://openairdocs.org/sdr/MYWA100132), Dec 19, 2010: UNKNOWN. MALFUNCTIONED. ETOPS SIGNIFICANT SYSTEM: PACK LIGHT ILLUMINATED ON RECALL ONLY. SYSTEM BITE AND OPS CHECK PERFORMED. NO DEFECTS NOTED.
- [SDR MYWA100018](https://openairdocs.org/sdr/MYWA100018), Feb 6, 2010: FMC. FAULTED. ETOPS SIGNIFICANT SYSTEM - FMC FAIL LIGHT ILLUMINATED ON CDU. FMC DISAGREE.
- [SDR MYWA09058](https://openairdocs.org/sdr/MYWA09058), Dec 4, 2009: FLAP. MALFUNCTIONED. ETOPS SIGNIFICANT SYSTEM - FLAPS STUCK AT FLAPS 2 DURING APPROACH WITH FLAP HANDLE AT 30 SETTING. FLAPS REMAINED AT 2 AFTER FLAP HANDLE WAS RETRACTED FOR GO ARO
- [SDR MYWA09057](https://openairdocs.org/sdr/MYWA09057), Nov 6, 2009: EEC. FAULTED. ETOPS SIGNIFICANT SYSTEM - NR 1 ENGINE EEC FAULT FOUND DURING BITE CHECK WHILE C/W PREFLIGHT/TRANSIT CHECK.
- [SDR MYWA2010F00038](https://openairdocs.org/sdr/MYWA2010F00038), Nov 6, 2009: EEC. MALFUNCTIONED. FOUND FAULT ON NR 1 ENGINE EEC DURING BITE CHECK WHILE C/W PREFLIGHT/TRANSIT CHECK.
- [SDR MYW2006F00002](https://openairdocs.org/sdr/MYW2006F00002), Jan 15, 2006: VALVE. STUCK. DURING DEPARTURE, APU BLEED VALVE CLOSED WITH APU BLEED SWITCH OPEN. TROUBLESHOT SYSTEM. REMOVED AND REPLACED APU BLEED AIR VALVE IAW AMM. OPERATIONAL CHECKED S
- [SDR SDR040015](https://openairdocs.org/sdr/SDR040015), Jun 14, 2004: WARNING LIGHT. ILLUMINATED. DURING TAKEOFF ROLL, ENGINE LIGHT CAME ON AT F/O ANNUNCIATOR PANEL AND EEC ALTERNATE LIGHT CAME ON AT OVERHEAD PANEL. ABORTED TAKEOFF AND RETURNED TO GATE WITHO
- [SDR 2003F00602](https://openairdocs.org/sdr/2003F00602), Sep 17, 2003: ROLLER. DISLODGED. AFTER TAKEOFF FROM PHX AND DURING CLIMB THE COCKPIT WAS INFORMED THE L1 DOOR WAS NOT SEALED. THE AIRCRAFT WOULD NOT PRESSURIZE. FOLLOWED ABNORMAL PROCEDURES AND
- [SDR 2003F00607](https://openairdocs.org/sdr/2003F00607), Aug 7, 2003: IDG. INOPERATIVE. DURNG CRUISE INBOUND TO SNN, NR 1 IDG LIGHT ILLUMINATED IN FILGHT. ALSO,NR 1 GENERATOR OFF BUS AND SOURCE OFF LIGHTS ILLUMINATED. AIRCRAFT LANDED WITHOUT INCIDE
- [SDR 2003F00514](https://openairdocs.org/sdr/2003F00514), Jul 17, 2003: ACTUATOR. INOPERATIVE. LEFT PACK LIGHT ILLUMINATED IN FLIGHT. PREVIOUS DMI NR 3104 ON LEFT RAM AIR DOOR FULL OPEN LIGHT REMAINS ON AFTER FLAPS ARE RETRACTED. RETURNED TO MIAMI. REMOVE
- [SDR 2003F00145](https://openairdocs.org/sdr/2003F00145), Jan 31, 2003: WARNING LIGHT. ILLUMINATED. DURING CRUISE DESCENT TO BGR, ENGINE DRIVEN HYDRAULIC PUMPS AMBER LIGHTS CAME ON. WHEN FLAPS SELECTED, 'A' SYSTEM SHOWED '0' QTY AND '0' PRESSURE. DECLARED AN E

All 52: https://openairdocs.org/aircraft/N732MA/reports.md

## STCs that may be installed (OpenAirDocs) (2)

Approved for this aircraft's airframe or engine model, in force first, then newest. The registry doesn't record which STCs an aircraft has; its records do.

### Approved for the engine (CFM International CFM56-7B26 series)

- [STC SE04840NY](https://openairdocs.org/stc/SE04840NY): Installation of HarcoSemco Exhaust Gas Temperature (EGT) Electrical Harnesses in CFM56-7 engine. Kilroy Aviation LLC
- [STC SE03036CH](https://openairdocs.org/stc/SE03036CH): Application of a deep compressive stress layer using a Low Plasticity Burnishing (LPB) process on CFM56-7 Series Engines Stage 1 High Pressure Compressor (HPC) Blade Dovetails in accordance with Delta Air Lines Inc. Drawing No. 72-0396, Revision B, dated November 3, 2011, or later FAA Approved revision. Delta Air Lines Inc

## Earlier aircraft with N732MA

The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N732MA before.

- [Cancelled 1976-09-24](https://openairdocs.org/deregistered/N732MA-1976-09-24): Mitsubishi MU-2B-26, S/N 347. Exported to Venezuela. Owner: [Mu2 Corp](https://openairdocs.org/faa-owner/MU2%20CORP), [San Angelo, TX](https://openairdocs.org/faa-place/TX/San%20Angelo)

## Related

- Other Boeing 737-81Q aircraft: https://openairdocs.org/model/boeing-737-81q/aircraft.md
- The CFM International CFM56-7B26 series engine: https://openairdocs.org/engine/cfm-international-cfm56-7b26-series.md

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