# Boeing 737-7BC - Type: Aircraft model (FAA registry) - Registry code: 1384509 - Manufacturer (registry): BOEING - Model: 737-7BC - 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: 9 - Page: https://openairdocs.org/model/boeing-737-7bc 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 (9) - [N108MS](https://openairdocs.org/aircraft/N108MS): [Yona Aviation II LLC](https://openairdocs.org/faa-owner/YONA%20AVIATION%20II%20LLC), [Las Vegas, NV](https://openairdocs.org/faa-place/NV/Las%20Vegas), built 2002, S/N 33102 - [N162WC](https://openairdocs.org/aircraft/N162WC): [Wca Holdings III LLC](https://openairdocs.org/faa-owner/WCA%20HOLDINGS%20III%20LLC), [Missoula, MT](https://openairdocs.org/faa-place/MT/Missoula), built 1999, S/N 30329 - [N707J](https://openairdocs.org/aircraft/N707J): [Spectre Air Capital LLC](https://openairdocs.org/faa-owner/SPECTRE%20AIR%20CAPITAL%20LLC), [Horseshoe Bay, TX](https://openairdocs.org/faa-place/TX/Horseshoe%20Bay), built 2001, S/N 30884 - [N737CM](https://openairdocs.org/aircraft/N737CM): [Wren Acquisitions LLC](https://openairdocs.org/faa-owner/WREN%20ACQUISITIONS%20LLC), [Birmingham, MI](https://openairdocs.org/faa-place/MI/Birmingham), built 1999, S/N 30327 - [N737JB](https://openairdocs.org/aircraft/N737JB): [Wi Bbj LLC](https://openairdocs.org/faa-owner/WI%20BBJ%20LLC), [Mequon, WI](https://openairdocs.org/faa-place/WI/Mequon), built 2000, S/N 30572 - [N7600K](https://openairdocs.org/aircraft/N7600K): [Sas Institute Inc](https://openairdocs.org/faa-owner/SAS%20INSTITUTE%20INC), [Cary, NC](https://openairdocs.org/faa-place/NC/Cary), built 2001, S/N 32628 - [N7777Q](https://openairdocs.org/aircraft/N7777Q): [Cobra Aviation Services LLC](https://openairdocs.org/faa-owner/COBRA%20AVIATION%20SERVICES%20LLC), [Oklahoma City, OK](https://openairdocs.org/faa-place/OK/Oklahoma%20City), built 2002, S/N 33036 - [N800KS](https://openairdocs.org/aircraft/N800KS): [Aej Services LLC](https://openairdocs.org/faa-owner/AEJ%20SERVICES%20LLC), [Los Angeles, CA](https://openairdocs.org/faa-place/CA/Los%20Angeles), built 2000, S/N 30782 - [N836BA](https://openairdocs.org/aircraft/N836BA): [Boeing Co](https://openairdocs.org/faa-owner/BOEING%20CO), [Gary, IN](https://openairdocs.org/faa-place/IN/Gary), built 2000, S/N 30756 ## NTSB investigations None matched to aircraft with this model. ## FAA accident and incident reports (1) 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 20150107000431I](https://openairdocs.org/incident/20150107000431I), Jan 7, 2015: Boeing 737-7BC (N836BA), Dulles, VA, Minor damage. Arrived at scene approximately 20:15 looked at both aircraft decided it was minor damage talked to crew was not familiar with area they were being parked the… ## Service difficulty reports (22) As reported by operators and repair stations, by the model named in the report. - [SDR 2025FA0000288](https://openairdocs.org/sdr/2025FA0000288), Apr 22, 2025: FUEL CELL. DAMAGED. NO 5, 7 & 8 AUXILIARY FUEL TANKS FOUND TO HAVE DAMAGE INCLUDING DENTS AND SCRATCHES. AFT AUXILIARY FUEL SYSTEM HAS MISSING HARDWARE & PARTS. BOLT MISSING FROM 9 - [SDR QV1Y2023062224283](https://openairdocs.org/sdr/QV1Y2023062224283), Jun 22, 2023: UNKNOWN. UNKNOWN. THIS REPORT IS SUBMITTED ON BEHALF OF JET AVIATION AG BASEL - FAA APPROVAL NUMBER QV1Y440K. DURING THE CURRENT MAINTENANCE INPUT AT JET AVIATION BASEL, REF. PRO - [SDR 2GYR2020060400001](https://openairdocs.org/sdr/2GYR2020060400001), Jun 4, 2020: LOCK WIRE. MISSING. WHILE COMPLYING WITH SERVICE LETTER 737-SL-27-286-A, IT WAS FOUND THAT THE LOCK WIRE FOR THE GROUND SPOILER INTERLOCK VALVE PUSH/PULL CABLE WAS MISSING FOR THE - [SDR YGJR201703010001](https://openairdocs.org/sdr/YGJR201703010001), Feb 1, 2017: FLEX HOSE. BROKEN. A REPLACEMENT FLEXIBLE OXYGEN HOSE WAS PURCHASED FROM A VENDOR. THE PART WAS IN NEW CONDITION IN ORIGINAL PACKAGING WITH TRACEABILITY AS NEW SURPLUS CONDITION W - [SDR QV1Y20160608002](https://openairdocs.org/sdr/QV1Y20160608002), Jun 7, 2016: SLIDE. NO TEST. OPERATIONAL TEST OF FWD ENTRY ESCAPE SLIDE: SLIDE DEPLOYED NORMALLY, WHEN DISCONNECTING IT FROM THE AIRCRAFT THE SLIDE OPENED, THE LEFT SIDE SEEM AND DEFLATED. - [SDR YGJR2016020300001](https://openairdocs.org/sdr/YGJR2016020300001), Oct 15, 2015: SATCOM. FAULTED. CREW REPORTED THEY WERE UNABLE TO ESTABLISH A CPDLC CONNECTION. THE CREW NOTED THAT AFTER SENDING A WINDS REQUEST THEY SAW THE MESSAGE, SENDING AND THE DATA LIN - [SDR BJ6A2009090812901](https://openairdocs.org/sdr/BJ6A2009090812901), Sep 6, 2009: COVER. DISLODGED. ON 9/6/2009 DURING THE TAKEOFF ROLL, CREW NOTICED THE MASTER WARNING LIGHT ILLUMINATED. CREW ABORTED THE TAKEOFF BELOW 80 KTS. ONCE CLEAR OF THE RUNWAY THE CREW - [SDR BJ6A2009082612701](https://openairdocs.org/sdr/BJ6A2009082612701), Aug 25, 2009: WINDOW. FAILED. NR3 RT WINDOW SHATTERED IN FLIGHT. FOUND THAT THE FRACTURE OF WINDOW INITIATED IN THE STRUCTURAL GLASS PANE AT THE EDGE OF THE SOLDER TAB. THERE WAS NO EVIDENCE - [SDR BJ6A200712901](https://openairdocs.org/sdr/BJ6A200712901), Sep 14, 2007: CHARGER. FAILED. DURING GROUND OPERATIONAL TEST OF THE EMERGENCY LIGHTING SYSTEM, SEVERAL EMERGENCY LIGHTS AT THE AFT LAVATORY AREA AND L2 DOOR FAILED TO ILLUMINATE. REPLACED EM - [SDR BJ6A200612903](https://openairdocs.org/sdr/BJ6A200612903), Nov 10, 2006: FLOORBEAM. CORRODED. GALLEY FLOOR STRUCTURE FOUND CORRODED WHEN GALLEY WAS REMOVED FOR OTHER MAINTENANCE. REPAIRED FLOORBEAM IAW DRAWING 4182527-01 AND SRM 51-10-51. NEW MOISTURE PR - [SDR SBJ6A12906001](https://openairdocs.org/sdr/SBJ6A12906001), Jul 26, 2006: MANIFOLD. CRACKED. WHILE PERFORMING RAYTHEON SB 737IGW-35A1 REV 1 AN O2 LEAK WAS DETECTED. FURTHER INSPECTION REVEALED A CRACKED WELD ON THE RT PASSENGER OXYGEN MANIFOLD P/N 97108 - [SDR BJ6A200612902](https://openairdocs.org/sdr/BJ6A200612902), Mar 30, 2006: CHECK VALVE. LEAKING. FLIGHT CREW REPORTED AFTER A FLIGHT FROM EGGW TO KEWR THAT THE A SYSTEM HYDRAULIC QUANTITY DECREASED FROM 92% TO 63%. THERE IS EVIDENCE OF FLUID IN THE RIGHT MA - [SDR BJ6A12906001](https://openairdocs.org/sdr/BJ6A12906001), Feb 6, 2006: MANIFOLD. CRACKED. PASSENGER OXYGEN SYSTEM DISTRIBUTION MANIFOLD FOUND TO HAVE A CRACK IN THE LINE WHERE A FITTING ATTACHES TO THE MANIFOLD P/N 97108928-013. THE FITTING SEPARATED - [SDR 1270601](https://openairdocs.org/sdr/1270601), Jan 27, 2006: OVERHEAT SENSOR. OUT OF TOLERANCE. RIGHT WING BODY OVERHEAT LIGHT ILLUMINATED DURING CLIMB THROUGH 10,000 FT CHECKLIST PERFORMED AND LIGHT EXTINGUISHED. AIRPLANE RETURNED TO WSSL AIRPORT. PRELIMI - [SDR 12706001](https://openairdocs.org/sdr/12706001), Jan 27, 2006: OVERHEAT SENSOR. OUT OF TOLERANCE. RIGHT WING BODY OVERHEAT LIGHT ILLUMINATED DURING CLIMB THROUGH 10,000 FT. CHECKLIST PERFORMED AND LIGHT EXTINGUISHED. AIRPLANE RETURNED TO WSSL AIRPORT. PRELIM - [SDR 1290503](https://openairdocs.org/sdr/1290503), Jul 26, 2005: TRANSMITTER. INTERMITTENT. FLAP POSITION DISAGREE WITH FLAP HANDLE. RT FLAP 0 DEGREES, LT FLAP 5 DEGREES. BECAUSE OF SKEW INDICATION THE FLAP SYSTEM WOULD NOT EXTEND. CREW MADE AN UNEVENT - [SDR 1290502](https://openairdocs.org/sdr/1290502), Jun 20, 2005: AMPLIFIER. FAILED. ELECTRICAL ODOR IN DINING/CONFERENCE AREA. SHUT OFF CABIN ENTERTAINMENT & GALLEY POWER. ODOR DID NOT FULLY GO AWAY. ACFT DIVERTED & LANDED. MX DISPATCHED. FOUND - [SDR 1290501](https://openairdocs.org/sdr/1290501), Jun 20, 2005: O-RING. CUT. COMPLETE A-SYSTEM HYDRAULIC FLUID LOSS IN FLIGHT. REPLACED O-RING P/N NAS 1612-4 ON "A" SYSTEM ELECTRIC MOTOR DRIVEN HYDRAULIC PUMP BLANKING PLUG. RESERVOIR "A" - [SDR N129QS0401](https://openairdocs.org/sdr/N129QS0401), Aug 16, 2004: ROD. DISCONNECTED. DURING TAXI, CAPTAIN REPORTED HIS RT BRAKE PEDAL INOPERATIVE. PEDAL REPORTED AS (HARD). AC RETURNED TO BLOCKS, MECHANIC FOUND CAPTAINS RT BRAKE PEDAL INTERCONNE - [SDR N171QS04001](https://openairdocs.org/sdr/N171QS04001), Mar 29, 2004: CONNECTOR. ARCED. NR 2 IDG DROPPED OF LINE. APU USED TO SUPPLY POWER TO BUS. CREW ELECTED TO DIVERT TO PBI FOR REPAIRS. AIRCRAFT ON FAR 91 POSITIONING FLIGHT. REPLACED AFFECTED N - [SDR BJ6A](https://openairdocs.org/sdr/BJ6A), Nov 11, 2003: BUSHING. BROKEN. HOT WATER TANK ATTACHMENT FAILURE DISCOVERED. REVIEW OF FAILED PARTS SHOWED CLEVIS PIN PULLED THROUGH WEB, BUSHING DISLODGED. BUSHING FOUND INTACT ON PIN IN CLE - [SDR 2003F00611](https://openairdocs.org/sdr/2003F00611), Oct 2, 2003: MOUNT. CRACKED. DURING MAINTENANCE IT WAS NOTED THAT THE FORWARD AND AFT MOUNT STRUCTURES FOR THE AFT WATER HEATER WERE FOUND DAMAGED. WATER HEATER IS SUSPENDED AT 6 POINTS. TH --- 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.