# N753MA: 1997 Boeing 737-48E, registration cancelled 2018-11-07 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: November 7, 2018 - Exported to: Brazil - Status when cancelled: Valid registration - Airframe: [Boeing 737-48E](https://openairdocs.org/model/boeing-737-48e) (registry code 13844BV) - Engine: [CFM International CFM56-3C series](https://openairdocs.org/engine/cfm-international-cfm56-3c-series) (registry code 13064) - Serial number: 28053 - Year built: 1997 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: November 17, 2006 - Certificate issued: March 5, 2018 - Last registry action: March 5, 2018 - Mode S code: AA2642 - Owner when cancelled: [V79a-734 LLC](https://openairdocs.org/faa-owner/V79A-734%20LLC) - Location: [San Francisco, CA](https://openairdocs.org/faa-place/CA/San%20Francisco) - Owner type: Corporation - Owner's area on the map: 37.7984° N, 122.3992° W: Placed by OpenAirDocs at the center of ZIP code 94111, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N753MA - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=753MA - Page: https://openairdocs.org/deregistered/N753MA-2018-11-07 From the FAA registry file of October 29, 2026, cancelled registrations. Owners' street addresses are left out. The Mode S code belongs to the N-number, not the airframe. ADs and bulletins for the Boeing 737-48E: https://openairdocs.org/model/boeing-737-48e.md ## Service difficulty reports (37) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR MYWA2017031400070](https://openairdocs.org/sdr/MYWA2017031400070), Mar 11, 2017: BATTERY PACK. INOPERATIVE. DURING PRE FLIGHT CHECK, RIGHT SIDE AFT EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. TROUBLESHOOTING REVEALED A FAULTY BATTERY PACK, WHICH WAS REMOVED AND REP - [SDR MYWA201703080036](https://openairdocs.org/sdr/MYWA201703080036), Mar 7, 2017: MEGAPHONE. INOPERATIVE. DURING THE PRE-FLIGHT TRANSIT CHECK, THE MEGAPHONE FAILED THE OPERATIONAL CHECK. THE UNIT WAS REMOVED AND REPLACED. - [SDR MYW2016F00007](https://openairdocs.org/sdr/MYW2016F00007), Feb 26, 2016: ANGLE. CORRODED. FWD LOWER CARGO COMPARTMENT, BS 520, STR 28.ANGLE REPLACED FABRICATED IAW SAMPLE. WET AREA- CAUSE. - [SDR MYW20160518006](https://openairdocs.org/sdr/MYW20160518006), Feb 26, 2016: INTERCOSTAL. CRACKED. INTERCOSTAL CRACKED, BS 312-328 LBL 45, SECTION 41. REPLACED, MADE ISE SAMPLE 1. DOUBLER INSTALLED, NDT STOP DRILLED CRACK. NR 0077, W/O 17007. - [SDR MYW2016051700001](https://openairdocs.org/sdr/MYW2016051700001), Feb 26, 2016: STIFFENER. CORRODED. CORROSION ON STIFFENER IN LAVATORY, & GALLEY AREA. WET AREA. - [SDR MYWA201512140001](https://openairdocs.org/sdr/MYWA201512140001), Dec 12, 2015: LIGHT. INOPERATIVE. EMERGENCY LIGHT AT SEAT 9DF INOPERATIVE. - [SDR MYWA201511240001](https://openairdocs.org/sdr/MYWA201511240001), Nov 21, 2015: BATTERY PACK. FAILED. LT AFT DOOR EMERGENCY LIGHT BATTERY PACK DEFECTIVE. - [SDR MYWA201508190001](https://openairdocs.org/sdr/MYWA201508190001), Aug 19, 2015: LIGHT. INOPERATIVE. R1 DOOR EMERGENCY LIGHT INOPERATIVE. - [SDR MYWA201507280001](https://openairdocs.org/sdr/MYWA201507280001), Jul 28, 2015: BATTERY PACK. FAILED. EMERGENCY EXIT LIGHT AT REAR OVERWING WINDOW INOPERATIVE. - [SDR MYWA201200052](https://openairdocs.org/sdr/MYWA201200052), Jul 23, 2012: INDICATION SYS. MALFUNCTIONED. LEFT PNUEMATIC PRESSURE INDICATOR DROPPED TO ZERO. NO CHANGE IN AIRCRAFT PRESSURIZATION FOR THE REMAINDER OF FLIGHT. - [SDR MYWA201200053](https://openairdocs.org/sdr/MYWA201200053), Jul 21, 2012: WARNING LIGHT. ILLUMINATED. ON PUSHBACK LEFT BODY WING OVERHEAT LIGHT ILLUMINATED ISOLATED PER QRH. LIGHT WENT OUT BUT CAME BACK ON WHEN APU BLEED OPENED FOR NR 1 ENG START. - [SDR MYWA201200054](https://openairdocs.org/sdr/MYWA201200054), Jul 20, 2012: INDICATOR. FAILED. NUMBER TWO OIL QTY INDICATIONS FAILED IN FLIGHT. PRESSURE AND TEMP REMAINED WITHIN LIMITS. - [SDR MYWA120033](https://openairdocs.org/sdr/MYWA120033), Mar 10, 2012: BATTERY PACK. DISCHARGED. ON P/T FOUND RT AFT SERVICE DOOR EMERGENCY EXIT LIGHT 3E INOP. T/S FOUND BAD BATTERY PACK, REMOVED & REPLACED POWER SUPPLY ASSY FOR RT AFT SERVICE DOOR POS AS P - [SDR MYWA110072](https://openairdocs.org/sdr/MYWA110072), Jul 9, 2011: CIRCUIT BREAKER. TRIPPED. ETOPS SIGNIFICANT SYSTEM: GEN PWR CONT CB POPPED AND APU SHUTDOWN AT GATE. FOUND GEN PWR CONT C/B INADVERTENTLY POPPED RESET C/B AND ACCOMPLISHED OPERATIONAL CH - [SDR MYWA110039](https://openairdocs.org/sdr/MYWA110039), Mar 30, 2011: INDICATOR. FLUCTUATES. ETOPS SIGNIFICANT SYSTEM: ENGINE NR 2 VIBRATION INDICATOR FLUCTUATES OCCASIONALLY FROM 0 TO 4.5 AND BACK. REPLACED VIB COMPUTER IAW AMM 77-31-03 ENG RUN UP ACCO - [SDR MYWA110036](https://openairdocs.org/sdr/MYWA110036), Mar 12, 2011: STARTER. MALFUNCTIONED. ETOPS SIGNIFICANT SYSTEM: NR 2 ENGINE STARTER IS NOT AUTOMATICALLY CUTTING OUT AT 46 PERCENT OCCASIONALLY. REMOVED AND REPLACED NR 2 ENG START SWITCH IAW AMM 80 - [SDR MYWA110009](https://openairdocs.org/sdr/MYWA110009), Jan 21, 2011: CONNECTOR. DIRTY. ETOPS SIGNIFICANT SYSTEM: ON DESCENT NR 2 ENGINE VIBRATION MONITOR FLUCTUATES BETWEEN .5 AND MAX OF 5. PERFORMED BITE CHECK OF AVMS, CHECKED SENSORS, WIRING, CL - [SDR MYWA110003](https://openairdocs.org/sdr/MYWA110003), Jan 11, 2011: CONTROL VALVE. INOPERATIVE. ETOPS SIGNIFICANT SYSTEM: RIGHT PACK LIGHT ILLUMINATED ON RECALL. REPLACED RIGHT PACK TEMP CONTROL VALVE. - [SDR MYWA110001](https://openairdocs.org/sdr/MYWA110001), Jan 4, 2011: VALVE. OUT OF ADJUST. ETOPS SIGNIFICANT SYSTEM: APU EGT GAUGE INTERMITTENT. FOUND THE CIRCUIT RESISTANCE VALVE TOO HIGH. ADJUSTED VALVE. SYSTEM OPERATION NORMAL. - [SDR MYWA100124](https://openairdocs.org/sdr/MYWA100124), Dec 2, 2010: INDICATOR. FAULTY. ETOPS SIGNIFICANT SYS: ON APPROACH CREW HAD A FLAP ASSEMETRY BETWEEN 2 AND 5. ACCOMPLISHED NON-NORMAL CHECKLIST. AFTER LANDING, REPLACED FLAP POSITION INDICATOR - [SDR MYWA100119](https://openairdocs.org/sdr/MYWA100119), Nov 16, 2010: GAUGE. ERRATIC. ETOPS SIGNIFICANT SYSTEM: DURING FLIGHT NR 2 ENGINE VIBRATION BECAME ERRATIC AND UNRELIABLE. - [SDR MYWA100108](https://openairdocs.org/sdr/MYWA100108), Aug 31, 2010: BATTERY PACK. DISCHARGED. DURING PT INSP FOUND SEVERAL LIGHTS INOPERATIVE ON EMERGENCY LIGHTING SYSTEM. - [SDR MYWA100103](https://openairdocs.org/sdr/MYWA100103), Aug 29, 2010: KNOB. BROKEN. ETOPS SIGNIFICANT SYSTEM: NR 2 HF RADIO INNER KNOB BROKEN. - [SDR MYWA100093](https://openairdocs.org/sdr/MYWA100093), Jun 24, 2010: WARNING LIGHT. ILLUMINATED. ETOPS SIGNIFICANT SYSTEM - LT WINDOW OVERHEAT ILLUMINATED. - [SDR MYWA100070](https://openairdocs.org/sdr/MYWA100070), Apr 15, 2010: INDICATION SYS. ACTIVATED. ETOPS SIGNIFICANT ITEM - NR 2 ENGINE VIBRATION INDICATION. TRANSFERRED FROM DMI 7265. - [SDR MYWA100069](https://openairdocs.org/sdr/MYWA100069), Apr 14, 2010: INDICATION SYS. ACTIVATED. ETOPS SIGNIFICANT ITEM - NR 2 ENGINE VIBRATION INDICATION. NO AIRFRAME VIBRATION. - [SDR MYWA100068](https://openairdocs.org/sdr/MYWA100068), Apr 13, 2010: ACTUATOR. LEAKING. ETOPS SIGNIFICANT ITEM - UPPER AILERON POWER CONTROL UNIT IS LEAKING FROM ACTUATOR PISTON. - [SDR MYWA100042](https://openairdocs.org/sdr/MYWA100042), Feb 22, 2010: SOLENOID VALVE. INOPERATIVE. ETOPS SIGNIFICANT SYSTEM - APU GENERATOR KICKED OFF LINE DURING ENGINE START. - [SDR MYWA100041](https://openairdocs.org/sdr/MYWA100041), Feb 17, 2010: GENERATOR. SHUTDOWN. ETOPS SIGNIFICANT SYSTEM - APU GENERATOR KICKED OFF LINE DURING ENGINE START. - [SDR MYWA100040](https://openairdocs.org/sdr/MYWA100040), Feb 16, 2010: FUEL CONTROL. MALFUNCTIONED. ETOPS SIGNIFICANT SYSTEM - APU DROPPED OFF LINE WHILE STARTING ENGINES. - [SDR MYWA100039](https://openairdocs.org/sdr/MYWA100039), Feb 14, 2010: APU. MALFUNCTIONED. ETOPS SIGNIFICANT SYSTEM - APU DROPPED OFF LINE WHEN STARTING ENGINES. - [SDR MYWA100017](https://openairdocs.org/sdr/MYWA100017), Jan 25, 2010: WARNING SYSTEM. FALSE ACTIVATION. ETOPS SIGNIFICANT SYSTEM - L/E SLAT IN TRANSIT LIGHT REMAINS ON. - [SDR MYWA09083](https://openairdocs.org/sdr/MYWA09083), Dec 24, 2009: WARNING LIGHT. ILLUMINATED. ETOPS SIGNIFICANT SYSTEM -TRANSCRIBED FROM DMI 6985 AUTO FAIL LIGHT GOES OFF WHEN PRESSURIZATION MODE SELECTOR IS IN ALTN. - [SDR MYWA09080](https://openairdocs.org/sdr/MYWA09080), Dec 12, 2009: WARNING LIGHT. ILLUMINATED. ETOPS SIGNIFICANT SYSTEM - REFERENCE DEFERRED DMI CTL 6943 ALL 3 ZONE TEMP LIGHT CAME ON DURING MASTER CAUTION RECALL. - [SDR MYWA09079](https://openairdocs.org/sdr/MYWA09079), Dec 12, 2009: WARNING LIGHT. ILLUMINATED. ETOPS SIGNIFICANT SYSTEM - ALL THREE ZONE TEMP LIGHTS ILLUMINATED ON RECALL. - [SDR MYWA09077](https://openairdocs.org/sdr/MYWA09077), Dec 8, 2009: WARNING LIGHT. ILLUMINATED. ETOPS SIGNIFICANT SYSTEM - TRANSCRIBED FROM DMI 6931 "AUTO FAIL LIGHT ILLUMINATED AGAIN INFLIGHT PRESSURIZATION NORMAL, SELECTED ALTN MODE - PRESSURIZATION NORM - [SDR MYWA09063](https://openairdocs.org/sdr/MYWA09063), Nov 17, 2009: APU. OUT OF TOLERANCE. ETOPS SIGNIFICANT SYSTEM - APU SPEED DECREASES WHEN LOAD IS APPLIED. ## Other aircraft with N753MA - [Registered now](https://openairdocs.org/aircraft/N753MA): Compagnie Daher TBM 700, S/N 1544, built 2024 --- 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.