# N239WA: 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: 23187 - Year built: 1984 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-jet - Airworthiness: Standard, transport - Airworthiness date: December 13, 1984 - Certificate issued: August 5, 2003 - Last registry action: July 18, 2006 - Mode S code: A22BE4 - 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/N239WA - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=239WA - Page: https://openairdocs.org/deregistered/N239WA-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 (33) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR DL73S050792](https://openairdocs.org/sdr/DL73S050792), Dec 15, 2005: POWER SUPPLY. INOPERATIVE. DURING LAYOVER, FOUND EMERGENCY ESCAPE PATH LIGHTING INOP FROM 1C TO 14DEF. REPLACED POWER SUPPLY AT FIRST CLASS CENTER AISLE OVERHEAD. - [SDR DL73S050756](https://openairdocs.org/sdr/DL73S050756), Dec 2, 2005: FUSE. BLOWN. APPROX 1/3 OF EMERGENCY LIGHTS ARE INOP. FOUND BATTERY CHARGER FUSES BLOWN AT M9026. T/S FOUND EMERGENCY WIRES IN 3 LOCATION SHORTED TO GROUND. REPAIRED WIRING - [SDR DL73S041144](https://openairdocs.org/sdr/DL73S041144), Dec 27, 2004: FUEL CONTROL. MALFUNCTIONED. AT APPROX 9800 FT DURING MANUAL POWER ADVANCE NR 2 ENGINE COMPRESSOR STALLED. REPLACED FUEL CONTROL. - [SDR DL73S040279](https://openairdocs.org/sdr/DL73S040279), Mar 26, 2004: SKIN. DAMAGED. DAMAGED HOLES FOUND IN STR 20R LAP SPLICE FASTENER ROWS. DURING REPLACEMENT OF UPPER SKIN PANEL BETWEEN STA 916-990. REPAIRED PER ERA 386177-14. - [SDR DL73S040272](https://openairdocs.org/sdr/DL73S040272), Mar 26, 2004: SKIN. FATIGUED. CRACK INDICATIONS WERE NOTED DURING MFEC INSPECTION OF THE S4R LAP. DURING REPAIR ACCOMPLISHMENT PER SRM 53-30-3, FIG 42, 12 MORE ADDITIONAL CRACK INDICATIONS W - [SDR DL73S040268](https://openairdocs.org/sdr/DL73S040268), Mar 25, 2004: FLOOR SUPPORT. FATIGUED. A CRACKED WAS NOTED IN THE BBL 0.07 LONGITUDINAL FLOOR SUPPORT AT BS 715. CRACKED REMOVED AND FLOOR SUPPORT REPAIRED PER ERA 386095-14AD. - [SDR DL73S040267](https://openairdocs.org/sdr/DL73S040267), Mar 25, 2004: ATTACH FITTING. CORRODED. CORROSION WAS NOTED ON THE LUGS OF THE HORIZONTAL STABILIZER CENTER SECTION REAR SPAR HINGE AND HOUSING FITTING. CORROSION REMOVED AND FITTINGS REWORKED IAW ERA - [SDR DL73S040266](https://openairdocs.org/sdr/DL73S040266), Mar 25, 2004: SKIN. CORRODED. CORROSION WAS FOUND ON THE KEEL BEAM LOWER SKIN PANEL. LOWER SKIN PANEL WAS REPLACED PER ERA 386233-14. - [SDR DL73S040205](https://openairdocs.org/sdr/DL73S040205), Mar 1, 2004: SKIN. DAMAGED. SCRIBE MARKS WERE NOTED BETWEEN BS 360 AND BS 540 ALONG S26L LAP JOINT IN THE LOWER SKIN. LAP JOINT WAS REWORKED PER INSTRUCTIONS CONTAINED IN ERA 386161-14. - [SDR DL73S040204](https://openairdocs.org/sdr/DL73S040204), Mar 1, 2004: SKIN. DAMAGED. SCRIBE MARKS WERE NOTED BETWEEN BS 360 TO BS 540 AT THE S26R LAP JOINT. LAP WAS REWORKED PER INSTRUCTIONS CONTAINED IN ERA 386165-14. - [SDR DL73S040203](https://openairdocs.org/sdr/DL73S040203), Mar 1, 2004: SKIN. DENTED. A TIME LIMITED REPAIR WAS REMOVED FROM BS 1025 NEAR S25R, NEARBY ADDITIONAL DAMAGE WAS NOTED (EG, DENTS AND GOUGES). DENTS AND GOUGES WERE CUTOUT AND A PERMANEN - [SDR DL73S040175](https://openairdocs.org/sdr/DL73S040175), Feb 19, 2004: ATTACH FITTING. CORRODED. CORROSION WAS NOTED ON THE VERT STAB ATTACH LUGS, ON THE AFT FACE OF THE NR 6 FIN LUG. CORROSION REMOVED AND LUG REWORKED PER ERA 386225-14. - [SDR DL73K011510](https://openairdocs.org/sdr/DL73K011510), Sep 8, 2001: WIRE. BROKEN. EMERGENCY LIGHT INOP AT 16D. REPAIRED BROKEN WIRE. - [SDR DL73K010814](https://openairdocs.org/sdr/DL73K010814), May 21, 2001: ACM. SEIZED. A/C DIVERTED INTO JAX WITH SMOKE/FUMES IN THE CABIN AND COCKPIT. PASSENGERS IN SEAT 10ABC FELT AND HEARD RUMBLING UNDER FLOOR INDICATING A PACK PROBLEM. UPON FU - [SDR DL73K002217](https://openairdocs.org/sdr/DL73K002217), Nov 11, 2000: FITTING. CORRODED. THE LT MAIN LANDING GEAR SIDE STRUT SUPPORT FITTING AT FS 685 WAS FOUND WITH CORROSION IN THE MAIN LUG BORE. THE BORE WAS OVERSIZED TO REMOVE ALL CORROSION AND - [SDR DL73K002216](https://openairdocs.org/sdr/DL73K002216), Nov 11, 2000: FITTING. CORRODED. THE RT MAIN LANDING GEAR SIDE STRUT SUPPORT FITTING AT FS 685 WAS FOUND WITH CORROSION IN THE MAIN LUG BORE. THE BORE WAS OVERSIZED TO REMOVE ALL CORROSION AND - [SDR DL73K002035](https://openairdocs.org/sdr/DL73K002035), Oct 16, 2000: HYDRAULIC LINE. RUPTURED. SHIP 363 FLIGHT 2131 ARRIVED EWR AT 2353E. DURING TAXI TO TERMINAL CREW NOTICED A SYSTEM HYDRAULIC QUANTITY DEPLETED. FOUND BRAIDED HYDRAULIC LINE WITH PINHOLE - [SDR DL73K002014](https://openairdocs.org/sdr/DL73K002014), Oct 15, 2000: TIRE. FAILED. NR 1 TIRE BLEW ON LANDING. SPEED 142 KTS, AUTOBRAKES MEDIUM. AUTOBRAKE DISARM LIGHT W/OUT CREW INTERVENTION. REPLACED NR 1 AND NR 2 WHEEL ASSYS PER M/M. INSPECT - [SDR DL73K001000](https://openairdocs.org/sdr/DL73K001000), May 19, 2000: FRAME. CORRODED. THE FWD FRAME OF THE C2 DOOR OPENING (FS 794) WAS FOUND WITH AN AREA OF CORROSION IN THE FRAME WEB UNDER THE LOWER LATCH FITTING. THE CORROSION WAS REMOVED WITH - [SDR DL73K991964](https://openairdocs.org/sdr/DL73K991964), Sep 4, 1999: O RING. DEFORMED. AT 30 KTS ON TAKEOFF ROLL HAD NR 1 ENG GENERATOR LOW OIL PRESS LIGHT FLICKER FOLLOWED BY GENERATOR KICKING OFF-LINE. AN ABORT WAS ACCOMPLISHED AND TAXI BACK TO - [SDR DL73K991917](https://openairdocs.org/sdr/DL73K991917), Aug 27, 1999: MASK. FAILED. OBSERVERS 02 MASK FAILED. REPLACED OBSERVERS 02 MASK. - [SDR DL73K990481](https://openairdocs.org/sdr/DL73K990481), Mar 8, 1999: PUMP. MALFUNCTIONED. ON DESCENT INTO MCO, LOST BOTH A SYSTEM ENGINE DRIVEN HYDRAULIC PUMPS, LOW PRESSURE LIGHT ILLUMINATED. CHECKED AND REPLACED ALL CASE DRAIN AND RETURN FILTERS, N - [SDR DL73K982635](https://openairdocs.org/sdr/DL73K982635), Dec 26, 1998: TIRE. FAILED. AFTER TAKEOFF FROM BDL, TOWER NOTIFIED US OF RUBBER DEBRIS ON THE RUNWAY. ON APPROACH TO MCO, AT GEAR EXTENTION HAD A RIGHT MAIN GEAR UNSAFE LIGHT ON AND GREEN - [SDR DL73K982628](https://openairdocs.org/sdr/DL73K982628), Dec 25, 1998: SIGN. INOP. EXIT SIGN AT DOOR 2L WILL NOT TEST. - [SDR DL73E981768](https://openairdocs.org/sdr/DL73E981768), Aug 26, 1998: SKIN. GOUGED. THE UPPER AFT PORTION OF THE C1 DOOR CUTOUT WAS FOUND TO HAVE A GOUGE APPROX 10.5 BY 2.5. REPAIRED PER ERA 332098-14. - [SDR DL73E981767](https://openairdocs.org/sdr/DL73E981767), Aug 26, 1998: SKIN. DAMAGED. DURING INSP OF THE C1 DOOR CUTOUT PER RTN OPN 8706, AN EXISTING DOUBLER WAS REMOVED TO ACCOMMODATE THE INSPECTION. UPON REMOVING THE DOUBLER, ADDITIONAL SKIN DA - [SDR DL73E981758](https://openairdocs.org/sdr/DL73E981758), Aug 25, 1998: DOUBLER. CRACKED. DURING RTN INSP PER SI3-56673-12 OF THE LH AND RH LONGITUDINAL OVERWING FLOORBEAMS, CRACKS WERE FOUND IN THE WEB DOUBLERS. THE CRACKS ARE LOCATED IN THE DOUBLER - [SDR DL73E980648](https://openairdocs.org/sdr/DL73E980648), Mar 24, 1998: GENERATOR. TRIPPED. ON CLIMB-OUT OF 23,000 FEET, CTR FUEL PUMPS WERE TURNED ON AND WE LOST THE NR 1 GEN IN ABOUT 2-3 SECONDS, THE NR 1 BUS OFF AND GEN OFF BUS LIGHTS ILLUM FOLLOWIN - [SDR DL73E980226](https://openairdocs.org/sdr/DL73E980226), Jan 26, 1998: SEAL. TORN. CLIMBING THROUGH FL242 CABIN ALT WARN HORN. CABIN ALT OBSERV CLIMB THROUGH 10000 AND AIRCRAFT LEVELED. DESCENT BEGAN AND CABIN ALT CLIMBED TO 13500, NO HELP IN - [SDR DL73E962788](https://openairdocs.org/sdr/DL73E962788), Dec 30, 1996: DUCT. COLLAPSED. ON TAKEOFF AFTER RETRACTING L/GEAR, LOUD BANG FOLLOWED BY SMOKE IN CABIN. A/C RETURNED TO GATE. FOUND DUCT FROM RT PACK HOT AIR SIDE OF MIX VALVE DISCONNECTED A - [SDR DL73E961922](https://openairdocs.org/sdr/DL73E961922), Aug 9, 1996: BULKHEAD WEB. CRACKED. DURING INSPECTION, 2 CRACKS WERE DISCOVERED ON THE FWD FACE OF BS 178 BULKHEAD WEB. CRACKS WERE LOCATED UNDER THE LBL 5.7 AND RBL 5.7 VERTICAL STRAPS. IN ACCORD - [SDR DL73E962045](https://openairdocs.org/sdr/DL73E962045), Aug 7, 1996: SKIN. CRACKED. SKIN AT THE COOLING DUCT CUTOUT BS 379 BL 2 WAS FOUND CRACKED AT THE AFT EDGE OF THE CUTOUT INTO A FASTENER HOLE. THE CRACK IS APPROXIMATELY .6 IN LENGTH AND IS - [SDR DL73E953899](https://openairdocs.org/sdr/DL73E953899), Oct 3, 1995: AOA SENSOR. BROKEN. ON LIFT-OFF, THE STICK SHAKER ACTIVATED AND DID NOT STOP UNTIL TOUCHDOWN. FOUND LEFT AOA SENSOR BROKEN OFF FROM A/C. REPLACED LEFT AOA, OPS CKS GOOD. ## 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 19931213048659I](https://openairdocs.org/incident/19931213048659I), Dec 13, 1993: Boeing 737247 (N239WA), Wichita, KS. Cargo compartment door warning light on. Returned. Found faulty door light switch. ## Other aircraft with N239WA - [Registered now](https://openairdocs.org/aircraft/N239WA): Cirrus Design SR22T, S/N 1146, built 2015 --- 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.