# N236WA: 1984 Boeing 737-247, registration cancelled 2007-11-21 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: November 21, 2007 - Exported to: Mexico - Status when cancelled: Triennial form not returned - Airframe: [Boeing 737-247](https://openairdocs.org/model/boeing-737-247) (registry code 138448D) - Engine: [Pratt & Whitney JT8D series](https://openairdocs.org/engine/pratt-whitney-jt8d-series) (registry code 52053) - Data sheets: [TCDS A16WE](https://openairdocs.org/tcds/A16WE) (OpenAirDocs) - Serial number: 23184 - Year built: 1984 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-jet - Airworthiness: Standard, transport - Airworthiness date: November 19, 1984 - Certificate issued: August 5, 2003 - Last registry action: July 18, 2006 - Mode S code: A220BF - Owner when cancelled: [Delta Air Lines Inc](https://openairdocs.org/faa-owner/DELTA%20AIR%20LINES%20INC) - Location: [Atlanta, GA](https://openairdocs.org/faa-place/GA/Atlanta) - Owner type: Corporation - Owner's area on the map: 33.7490° N, 84.3880° W: Placed by OpenAirDocs: center of Atlanta, GA, within about 7 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N236WA - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=236WA - Page: https://openairdocs.org/deregistered/N236WA-2007-11-21 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 737-247: https://openairdocs.org/model/boeing-737-247.md ## Service difficulty reports (20) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR DL73S040046](https://openairdocs.org/sdr/DL73S040046), Jan 16, 2004: FLOORBEAM. CRACKED. DURING ACCOMPLISHMENT OF 03-062982-03AD THE UPPER CHORD OF THE BL 0.07 FLOORBEAM WAS FOUND SEVERED AT A TYPICAL LOCATION (BS 661) AND A CRACK INDICATION AT BS 6 - [SDR DL73S040043](https://openairdocs.org/sdr/DL73S040043), Jan 15, 2004: SKIN. CRACKED. DURING ACCOMPLISHMENT OF INSPECTIONS PER AD 2003-08-15, 3 CRACKS WERE FOUND IN LOWER ROW FASTENER LOCATIONS OF THE STRINGER 4L SKIN LAP JOINT BETWEEN FS 559 & 5 - [SDR DL73S040040](https://openairdocs.org/sdr/DL73S040040), Jan 15, 2004: SKIN. DAMAGED. DENTING NOTED IN THE FUSELAGE SKIN AT APPROXIMATELY BS 862, BETWEEN S13L AND S14L. DAMAGE WAS REMOVED AND REPAIRED PER ERA 385998-14. - [SDR DL73S040039](https://openairdocs.org/sdr/DL73S040039), Jan 15, 2004: FRAME. DAMAGED. A DAMAGED HOLE WAS CREATED IN THE BS 440 FRAME NEAR S26R. HOLE WAS OVERSIZED TO 0.3670 TO REMOVE DAMAGE. FRAME WAS REPAIRED PER ERA 386004-14. - [SDR DL73S040038](https://openairdocs.org/sdr/DL73S040038), Jan 15, 2004: FLOORBEAM. CRACKED. DURING INSPECTION OF THE BS 520 FLOORBEAM, CRACKS WERE NOTED IN THE RADIUS OF THE UPPER CHORD AT LBL 24.75, 45.5 AND RBL 45.5. EACH CRACK WAS APPROXIMATELY 2 IN - [SDR DL73S040022](https://openairdocs.org/sdr/DL73S040022), Jan 9, 2004: FRAME. CRACKED. CRACKS WERE NOTED IN THE BS 663 FRAME AT S3L, S2L, S1 AND S2R WHICH REQUIRED THE FUSELAGE SKIN TO BE TRIMMED AWAY. CRACKS INDICATIONS WERE REMOVED AND REPAIR IN - [SDR DL73S040021](https://openairdocs.org/sdr/DL73S040021), Jan 9, 2004: SKIN. DENTED. THE FUSELAGE SKIN WAS FOUND DENTED FROM BS 328 TO BS 344, BETWEEN S20R AND S21R. DENT WAS REPAIRED PER ERA 386008-14. - [SDR DL73K001960](https://openairdocs.org/sdr/DL73K001960), Oct 6, 2000: SUPPORT FITTING. CORRODED. THE LOWER MAIN LUGS ON THE LT AND RT MAIN LANDING GEAR SIDE STRUT SUPPORT FITTINGS AT FS 685 WERE FOUND CORRODED. THE EXISTING BUSHINGS WERE REMOVED AND LUG BOR - [SDR DL73K001405](https://openairdocs.org/sdr/DL73K001405), Jul 23, 2000: BULKHEAD. CRACKED. WHILE ACCOMPLISHING INSPECTIONS OF THE FS 178 BULKHEAD PER AD 2000-05-29, A TYPICAL CRACK WAS FOUND IN THE BULKHEAD WEB AT WL 234 AND RBL 7. THE CRACK WAS ROUTE - [SDR DL73K001404](https://openairdocs.org/sdr/DL73K001404), Jul 23, 2000: BULKHEAD. CRACKED. WHILE ACCOMPLISHING INSPECTIONS OF THE FS 178 BULKHEAD PER AD 2000-05-29, TYPICAL CRACKS WERE FOUND IN THE ADJACENT FLOOR WEBS AT WL 207 AND RBL & LBL 25. THE C - [SDR DL73K000682](https://openairdocs.org/sdr/DL73K000682), Apr 9, 2000: BULLET. DENTED. EN ROUTE FROM BDL TO FLL, NR 1 ENGINE HAD COMPRESSOR STALLS. CREW PULLED THROTTLE TO IDLE. DIVERTED TO BOS. BOS MTC FOUND NR 1 ENGINE NOSE BULLET DETACHED AND F - [SDR DL73E992274](https://openairdocs.org/sdr/DL73E992274), Oct 15, 1999: DUCT. FAILED. AIRCRAFT WOULD NOT PRESSURIZE AFTER T/O CONFIGURED FOR RIGHT BLEED AND RIGHT PACK OPERATION. AUTO/STBY/AND MANUAL MODES ATTEMPED. OUTFLOW VALVE FULL CLOSED FWD - [SDR DL73E982039](https://openairdocs.org/sdr/DL73E982039), Oct 3, 1998: FAN. FAILED. GASPER FAN C/B FOUND OPEN, WHEN CLOSED IT RETRIPPED ACCOMPANIED BY A LOUD POP HEARD UNDER FLOOR IN MID CABIN AND STRONG ELECTRICAL SMELL. INSP GASPER FAN NO PRO - [SDR DL73E981375](https://openairdocs.org/sdr/DL73E981375), Jun 30, 1998: LINE. CHAFFED. A/C RETURN ATL, DUE TO RT HYD PUMP LOW PRESS LIGHT AND HYD QTY ZERO ON CLIMB-OUT. FOUND HYD RTN LINE CHAFFED. REPLACED LINE AND FILTER AND EDP PER M/M. LEAK CK - [SDR DL73E981270](https://openairdocs.org/sdr/DL73E981270), Jun 16, 1998: DUCT. CRACKED. WITH APU BLEED OPEN POWERING RIGHT PACK LEFT WING BODY OVERHEAT LIGHT ILLUMINATED APU BLEED PLACED OFF AFTER DELAY LIGHT WENT OUT LATER F/A NOTICED BURNING SMEL - [SDR DL73E980933](https://openairdocs.org/sdr/DL73E980933), Apr 28, 1998: SKIN. CRACKED. THE R2 DOOR OPENING SURROUND SKIN WAS FOUND WITH A .75 INCH LONG CRACK AT THE CUTOUT FOR THE LOWER HINGE. THE SKIN AND BONDED DOUBLERS WERE CUTOUT TO REMOVE THE - [SDR DL73E971675](https://openairdocs.org/sdr/DL73E971675), Aug 9, 1997: SKIN. CORROSION. A BULGE WAS FOUND IN THE FUSELAGE SKIN AT STA 927 BETWEEN STR 14R AND 15R. MX REMOVED THE AFFECTED AREA OF THE CHEM-MILLED LOWER SKIN (65-45778-82), JUST BELOW - [SDR DL73E961724](https://openairdocs.org/sdr/DL73E961724), Jul 9, 1996: BULKHEAD WEB. CRACKED. THREE CRACKS WERE DISCOVERED ON THE FWD FACE OF THE FS 178 BULKHEAD WEB. THE FIRST CRACK IS LOCATED NEAR THE RBL 5.7 VERTICAL STRAP AT APPROX WL 198. THE SECOND - [SDR DL73E954574](https://openairdocs.org/sdr/DL73E954574), Nov 29, 1995: FAIRING. CAME LOOSE. LEFT INBD FLAP FAIRING CANOE BROKE LOOSE IN FLT AND WAS FOUND PARTLY DETACHED FROM WING DURING POST FLT. REMOVED LEFT WING MIDFLAP CANOE, REPLACED BELL CRANK AS - [SDR DL73E960091](https://openairdocs.org/sdr/DL73E960091), Jan 15, 1995: BULB. FAILED. AFT LOWER BODY EMERGENCY LIGHT INOP. RELAMPED SAME, OPS CHECK GOOD. ## 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 19900624040429I](https://openairdocs.org/incident/19900624040429I), Jun 24, 1990: Boeing 737247 (N236WA), Rapid City, SD. Crew smelled odor of burning wire. Pilot made unscheduled landing at Rapid City. - [Incident 19860129012759I](https://openairdocs.org/incident/19860129012759I), Jan 29, 1986: Boeing 737247 (N236WA), Phoenix, AZ, Minor damage. While pulling off to side of taxiway to await IFR clearance, wingtip struck a blast fence. Navigation lens broken. ## Other aircraft with N236WA - [Registered now](https://openairdocs.org/aircraft/N236WA): DJI AGRAS T40, S/N 1581F574B235D001001W --- 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.