# N302DL: 1983 Boeing 737-232, registration cancelled 2008-05-08 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: May 8, 2008 - Exported to: Canada - Status when cancelled: Valid registration - Airframe: [Boeing 737-232](https://openairdocs.org/model/boeing-737-232) (registry code 1384475) - Engine: [Pratt & Whitney JT8D-15](https://openairdocs.org/engine/pratt-whitney-jt8d-15) (registry code 52051) - Data sheets: [TCDS A16WE](https://openairdocs.org/tcds/A16WE), [TCDS E2EA](https://openairdocs.org/tcds/E2EA) (OpenAirDocs) - Serial number: 23074 - Year built: 1983 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: November 8, 1983 - Certificate issued: July 13, 2007 - Last registry action: July 13, 2007 - Mode S code: A32716 - Owner when cancelled: [Global Aircraft Solutions Inc](https://openairdocs.org/faa-owner/GLOBAL%20AIRCRAFT%20SOLUTIONS%20INC) - Location: [Tucson, AZ](https://openairdocs.org/faa-place/AZ/Tucson) - Owner type: Corporation - Owner's area on the map: 32.1478° N, 110.9354° W: Placed by OpenAirDocs at the center of ZIP code 85706, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N302DL - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=302DL - Page: https://openairdocs.org/deregistered/N302DL-2008-05-08 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 737-232: https://openairdocs.org/model/boeing-737-232.md ## Service difficulty reports (44) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR DL73S060309](https://openairdocs.org/sdr/DL73S060309), Apr 18, 2006: SKIN. CRACKED. THE FUSELAGE SKIN AT THE FWD ENTRY DOOR UPPER HINGE CUTOUT IS CRACKED AT THE UPPER CORNER. THE DAMAGED SKIN WAS REMOVED AND A REPAIR DOUBLER WAS INSTALLED. - [SDR DL73S060246](https://openairdocs.org/sdr/DL73S060246), Apr 3, 2006: FLOOR SUPPORT. CRACKED. THE LONGITUDINAL OVERWING FLOOR SUPPORT HAS CRACKS IN THE WEB AND LOWER CHORD. A DOUBLER WAS INSTALLED TO REPAIR THE WEB AND A STRAP WAS INSTALLED TO REPAIR FLO - [SDR DL73S060199](https://openairdocs.org/sdr/DL73S060199), Mar 15, 2006: SKIN. CRACKED. INSPECTIONS OF THE STRINGER 4L SKIN LAP REVEALED A SINGLE CRACKED FASTENER HOLE NEAR FS 490. THE CRACKED AREA OF SKIN WAS CUTOUT. THE CUTOUT WAS REPAIRED WITH A - [SDR DL73S060192](https://openairdocs.org/sdr/DL73S060192), Mar 15, 2006: SKIN. CRACKED. FATIGE CRACK IN SKIN IN LOWER ROW OF S-4R LAP JOINT AT FS 410. CUT OUT SKIN AND INSTALLED REPAIR PARTS PER ER/A. - [SDR DL73S060191](https://openairdocs.org/sdr/DL73S060191), Mar 15, 2006: SKIN. CRACKED. FATIGUE CRACK IN LOWER ROW OF S-14L LAP JOINT, FS 380. CUT OUT CRACK AND REPAIRED PER ER/A. - [SDR DL73S060190](https://openairdocs.org/sdr/DL73S060190), Mar 15, 2006: SKIN. CRACKED. FATIGUE CRACK AT FASTENER IN LOWER ROW OF S-4L LAP JOINT, APPROX FS 490. CUT OUT DAMAGE AND INSTALLED REPAIR DOUBLER PER ER/A. - [SDR DL73S060187](https://openairdocs.org/sdr/DL73S060187), Mar 11, 2006: SKIN. CRACKED. CRACK INDICATIONS WERE FOUND AT STA 385 IN THE S-4 L LAP SPLICE, FUSELAGE SKIN. ACCOMPLISHED BOLT HOLE EDDY CURRENT INSPECTION TO CONFIRM CRACK. INSPECTION FOUN - [SDR DL73S060186](https://openairdocs.org/sdr/DL73S060186), Mar 10, 2006: SKIN. CRACKED. CRACK INDICATIONS WERE FOUND BETWEEN STA 827-847 IN THE S-4L LAP SPLICE, FUSELAGE SKIN. ACCOMPLISHED BOLT HOLE EDDY CURRENT INSPECTION TO CONFIRM CRACK. INSPECT - [SDR DL73S060008](https://openairdocs.org/sdr/DL73S060008), Jan 3, 2006: WINDOW. CRACKED. R1 WINDOW CRACKED WITH ARCING - REPLACED SAME. - [SDR DL73S041051](https://openairdocs.org/sdr/DL73S041051), Nov 22, 2004: MODULE. MALFUNCTIONED. ON CLIMBOUT AT 14,000 FEET NR 1 ENG OVERHEAT LIGHT ILLUM. IAW CK LIST THRUST LEVER RETARDED. LIGHT WENT OUT. REPLACED ENG FIRE/OVERHEAT MODULE. RAN ENGS AT T/O - [SDR DL73S040958](https://openairdocs.org/sdr/DL73S040958), Oct 10, 2004: ACTUATOR. FAILED. AFTER LANDING A-SYS HYD QTY DROPPED TO 0. REPLACED NR 1 SPOILER ACTUATOR FOR LEAKING. - [SDR DL73S040402](https://openairdocs.org/sdr/DL73S040402), May 6, 2004: RMI. SMOKE. NR 2 RMI STARTED TO SMOKE. REPLACED SAME - [SDR DL73S040259](https://openairdocs.org/sdr/DL73S040259), Mar 20, 2004: SKIN. CRACKED. INSPECTION OF THE SKIN LAPS PER AD 2003-08-15 REVEALED A CRACKED FASTENER HOLE IN THE STRINGER 10R SKIN LAP SPLICE AT FS 432. A 1 X 6 INCH CUTOUT WAS MADE IN TH - [SDR DL73S040258](https://openairdocs.org/sdr/DL73S040258), Mar 20, 2004: SKIN. CRACKED. INSPECTION OF THE SKIN LAP JOINTS PER AD 2003-08-15 REVEALED A CRACKED FASTENER HOLE IN THE STRINGER 14R SKIN LAP JOINT. A 1 X 6 INCH CUTOUT WAS MADE IN THE SKI - [SDR DL73S040248](https://openairdocs.org/sdr/DL73S040248), Mar 12, 2004: STRINGER. CRACKED. STRINGER 4L DAMAGED IN LWR RADIUS AT STA 797. REPAIRED PER SRM 53-10-3 FIG 4. - [SDR DL73S040045](https://openairdocs.org/sdr/DL73S040045), Jan 15, 2004: CHARGER. INOPERATIVE. MCO OVERHEAD EMERGENCY LIGHT BULLNOSE INOP 19D. FOUND BATTERY CHARGER RACK AT M1134 STA 629L INOP. REPLACED CHARGER RACK. - [SDR DL73S030899](https://openairdocs.org/sdr/DL73S030899), Oct 3, 2003: DUCT. DAMAGED. RT ENGINE OVERHEAT LIGHT CAME ON DURING CLIMB, WENT OUT WITH THROTTLE AT IDLE. FOUND DAMAGED STARTER DUCT. REPLACED SAME. - [SDR DL73K030140](https://openairdocs.org/sdr/DL73K030140), Feb 8, 2003: BULKHEAD. CRACKED. FUSELAGE / BULKHEAD / FS 178 / WEB AND SIDE CHORDS : CRACK REPAIR THE FS 178 BULKHEAD WEB AND SIDE CHORDS WERE FOUND WITH CRACKS TYPICAL OF BAC S/B 737-53-1173 - [SDR DL73K010691](https://openairdocs.org/sdr/DL73K010691), Apr 28, 2001: FLOORBEAM. CRACKED. THE LONGITUDINAL FLOOR BEAM AT RBL 24 WAS FOUND WITH A TYPICAL CRACK IN THE BEAM WEB AND WEB DOUBLER AT FS 678. THE BEAM UPPER CHORD WAS FOUND CRACKED AT FS 674 - [SDR DL73K010617](https://openairdocs.org/sdr/DL73K010617), Apr 14, 2001: POWER SUPPLY. DISCHARGED. RT AFT AISLE EMERGENCY LIGHT INOP. REPLACED BATTERY POWER SUPPLY CKS NORMAL - [SDR DL73K010475](https://openairdocs.org/sdr/DL73K010475), Mar 23, 2001: MOUNT. WORN. FWD ENGINE MOUNT FOUND WITH MIGRATING BEARING RESULTING IN OVERSIZED MOUNT HOLES. REPAIR PER ER/A 401250-14AD. - [SDR DL73K002050](https://openairdocs.org/sdr/DL73K002050), Oct 18, 2000: PCU. MALFUNCTIONED. ON T/O ROLL 125 KNOTS FELT A UNCOMMANDED YAW TO THE RIGHT, FELT LIKE SOMEONE KICKED THE RUDDER PEDAL. REPLACED RUDDER PCU PER M/M. - [SDR DL73K001174](https://openairdocs.org/sdr/DL73K001174), Jun 18, 2000: COFFEEMAKER. BURNED. ON T/O, STRONG SMELL OF SMOKE/ELECTRICAL/SULFUR. RETURN TO LAND MCO OVERWEIGHT LANDING AT 200 FPM, LANDING WEIGHT 112.8. REPLACED BOTH COALESCER BAGS. BOTH CLEA - [SDR DL73K001089](https://openairdocs.org/sdr/DL73K001089), Jun 3, 2000: SMOKE DETECTOR. WILL NOT TEST. AFT LAV SMOKE DETECTOR WOULD NOT TEST. REPLACED SMOKE DETECTOR. - [SDR DL73K000595](https://openairdocs.org/sdr/DL73K000595), Mar 29, 2000: UNKNOWN. ODOR. FLT 2452 MCO-EWR, HAD ELECTRICAL ODOR AROUND THE FWD F/A JUMPSEAT. CREW DIVERTED TO RIC. TROUBLESHOOTING WITH CONTRACT MTC AND NOTHING FOUND. SENT MECH FROM CVG - [SDR DL73K000557](https://openairdocs.org/sdr/DL73K000557), Mar 22, 2000: DOUBLER. WORN. AN EXISTING DOUBLER WAS WORN ALONG IT'S AFT EDGE LOCATED AT THE FORWARD EDGE OF THE C1 DOOR. THE DOUBLER WAS REMOVED AND REPLACED PER ERA 334214-14. THE DAMAGE - [SDR DL73K000539](https://openairdocs.org/sdr/DL73K000539), Mar 20, 2000: SPAR. CORRODED. CORROSION WAS FOUND ON THE FRONT AND REAR SPAR OF THE HORIZONTAL STABILIZER CENTER SECTION ATTACH FITTING. CORROSION WAS FOUND ON THE FORWARD AND AFT FACES AND - [SDR DL73K000538](https://openairdocs.org/sdr/DL73K000538), Mar 20, 2000: FITTING. CORRODED. CORROSION WAS FOUND ON THE REAR SPAR ATTACH LUGS OF THE HORIZONTAL STABILIZER. THE CORROSION WAS TO THE FORWARD AND AFT FACES OF THE FITTING AND INSIDE THE LOWE - [SDR DL73K000526](https://openairdocs.org/sdr/DL73K000526), Mar 17, 2000: FITTING. CORRODED. CORROSION WAS FOUND ON THE FORWARD AND AFT FACE OF BOTH THE INNER LUGS OF THE VERTICAL STABILIZER ATTACH FITTING. THE CORROSION WAS REMOVED AND THE AREA WAS TRE - [SDR DL73K000525](https://openairdocs.org/sdr/DL73K000525), Mar 17, 2000: FITTING. CORRODED. CORROSION WAS FOUND ON ALL EIGHT OF THE AFT SPAR ATTACH LUGS ON THE BODY ATTACHMENT POINT FOR THE VERTICAL STABILIZER AT APPROXIMATELY FS 1080. CORROSION WAS RE - [SDR DL73K000518](https://openairdocs.org/sdr/DL73K000518), Mar 16, 2000: DOUBLER. WORN. WEAR WAS FOUND ON THE LAP JOINT LOWER INTERNAL BONDED DOUBLER AT APPROXIMATELY FS 310 AND STR 10L JUST BELOW THE L1 DOOR UPPER HINGE CUTOUT. THE WEAR WAS .25 IN - [SDR DL73K992800](https://openairdocs.org/sdr/DL73K992800), Dec 20, 1999: SEAL. SEPARATED. NR 1 ENG HAD MULTIPLE COMPRESSOR STALLS AT FL310 AS THROTTLES RETARDED FROM CLIMB EPR TO CRUISE EPR OF 1.96. COMPRESSOR STALLS STOPPED AS THROTTLES WERE PULLED - [SDR DL73K992651](https://openairdocs.org/sdr/DL73K992651), Dec 4, 1999: LIGHT. INOPERATIVE. EMERGENCY EXIT LIGHTING INOP ROWS 1 THRU 3. REPLACED PWR SUPPLY AND FOUND WIRES SHORTED AT ROW 4 D, E, F. REPAIRED SAME, OPS CKS NORMAL. - [SDR DL73K991413](https://openairdocs.org/sdr/DL73K991413), Jun 22, 1999: LIGHT. INOPERATIVE. ON MTC INSPECTION, FOUND FWD CABIN EMERGENCY LIGHTS WOULD NOT EXTINGUISH AFTER TEST. REPLACED POWER SUPPLY AND TEST GOOD. - [SDR DL73K991221](https://openairdocs.org/sdr/DL73K991221), May 28, 1999: FITTING. CORRODED. THE LT AND RT FS 685 MLG SIDE STRUT SUPPORT FITTINGS WERE FOUND WITH CORROSION IN THE STRUT ATTACH LUG BORES. THE LUGS WERE OVERSIZED TO CLEAN UP THE CORROSION, - [SDR DL73K982186](https://openairdocs.org/sdr/DL73K982186), Oct 20, 1998: SKIN. CRACKED. FUSELAGE SKIN, FS 520, S-16L SKIN CRACK REPAIR. THE FUSELAGE SKIN WAS FOUND WITH A CRACK ABOVE STRINGER 16L AT FS 520. THE CRACK WAS CUTOUT AND REPAIRED WITH AN - [SDR DL73K981000](https://openairdocs.org/sdr/DL73K981000), May 6, 1998: SKIN. PUNCTURED. THE FUSELAGE SKIN WAS PUNCTURED DUE TO GROUND EQUIPMENT IMPACT AT FS 920 AND STRINGERS 21L-22L. ALSO, STRINGER 22L WAS DAMAGED. THE SKIN WAS REPAIRED WITH AN EX - [SDR DL73K970606](https://openairdocs.org/sdr/DL73K970606), Apr 3, 1997: FUEL CONTROL. FAILED. PUSHED PWR UP FOR T/O AND ENGAGED, ATS NOTICED NR 2 ENG INST ROLLING BACK AS IF FLAMING OUT. PERFORMED ABORT PROCEDURES AND REALIZED NR 1 ENG WAS STILL OPER AT - [SDR DL73S961474](https://openairdocs.org/sdr/DL73S961474), Jun 11, 1996: BULKHEAD WEB. CRACKED. THREE CRACKS FOUND ON THE FWD FACE OF THE STA 178 BLKHD WEB. THE FIRST CRACK WAS LOCATED NEAR LBL 5.7 VERTICAL STRAP AT APPROX WL 195, THE SECOND CRACK WAS LOCA - [SDR DL73S961353](https://openairdocs.org/sdr/DL73S961353), May 27, 1996: FLOOR BEAM. CRACKED. THE BL .07 FLOOR BEAM OF THE WING CENTER SECTION IS CRACKED AT FS 660. NO CRACKS WERE FOUND IN THE WEB. THE CRACK IS TYPICAL PER BACO SB 737-57-1210. THIS ERA W - [SDR DL73S960840](https://openairdocs.org/sdr/DL73S960840), Apr 11, 1996: TRACK LIGHT. CRACKED. ON LAYOVER, FOUND FLOOR TRACK TOP COVER CRACKED BETWEEN ROWS 15 AND 18. REPLACED TOP TRACK BETWEEN ROWS 15 AND 18. - [SDR DL73S960744](https://openairdocs.org/sdr/DL73S960744), Mar 15, 1996: ACTUATOR FITTING. FAILED. ONE OF THE ACTUATOR FITTINGS HAS FAILED ON THE RT INBOARD GROUND SPOILER. THE FITTING IS THE SUBJECT OF S/B 737-57-1207. ACCOMPLISHED REPAIRS PER DL ERA 357237- - [SDR DL73S952370](https://openairdocs.org/sdr/DL73S952370), May 31, 1995: SKIN. DENTED. FOUND ON LAY OVER-DENT AFT OF AFT B/B DOOR APPROX. .25 INCH IN DIAMETER. REPAIRED PER SRM 53-30-3 FIG. 23. - [SDR DL73S953104](https://openairdocs.org/sdr/DL73S953104), Jan 19, 1995: SKIN. DAMAGED. DURING LAYOVER IN ATLANTA, THE FUSELAGE SKIN WAS DAMAGED JUST AFT OF STATION 360 AND JUST ABOVE STRINGER 19R WHEN STRUCK BY A BAGGAGE CONTAINER. DAMAGE WAS CUT ## 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 20001018016509I](https://openairdocs.org/incident/20001018016509I), Oct 18, 2000: Boeing 737232 (N302DL), Tampa, FL. (-23) On October 18, 2000, at 1405 EDT, a B-737-232, operated by delta airlines, on take-off from Tampa International Airport, FL., at 125 knots the a/c… - [Incident 19961007039889I](https://openairdocs.org/incident/19961007039889I), Oct 7, 1996: Boeing 737232 (N302DL), Atlanta, GA, Minor damage. Narrative: fuel truck o/b half of right engine cowl when positioning to fuel a/c. maintenance replaced cowl. Ship # 302-N302DL. ## Other aircraft with N302DL - [Registered now](https://openairdocs.org/aircraft/N302DL): DJI AGRAS T50, S/N 1581F6BUB24B4001KK68 --- 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.