# N317DL: 1984 Boeing 737-232, registration cancelled 2007-12-21 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: December 21, 2007 - Exported to: Venezuela - Status when cancelled: Valid registration - Airframe: [Boeing 737-232](https://openairdocs.org/model/boeing-737-232) (registry code 1384475) - 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: 23089 - Year built: 1984 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-jet - Airworthiness: Standard, transport - Airworthiness date: May 3, 1984 - Certificate issued: November 19, 2007 - Last registry action: November 19, 2007 - Mode S code: A36128 - Owner when cancelled: [Wells Fargo Bank Northwest Na Trustee](https://openairdocs.org/faa-owner/WELLS%20FARGO%20BANK%20NORTHWEST%20NA%20TRUSTEE) - Location: [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City) - Owner type: Corporation - Owner's area on the map: 40.7558° N, 111.8843° W: Placed by OpenAirDocs at the center of ZIP code 84111, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N317DL - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=317DL - Page: https://openairdocs.org/deregistered/N317DL-2007-12-21 From the FAA registry file of October 31, 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 (24) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR DL73S040915](https://openairdocs.org/sdr/DL73S040915), Sep 23, 2004: SKIN. CRACKED. A 1.5 INCH CRACK WAS FOUND IN THE FUSELAGE SKIN RUNNING ALONG THE BONDED DOUBLER MILL LINE AT STRINGER 20L AND FS 765. THE CRACK WAS REMOVED WITH A SKIN CUTOUT - [SDR DL73S040908](https://openairdocs.org/sdr/DL73S040908), Sep 22, 2004: SKIN. CRACKED. TWO INCH CRACK IN FUSELAGE SKIN STA 930 STR 24 RIGHT. REPAIRED PER SRM. - [SDR DL73S030918](https://openairdocs.org/sdr/DL73S030918), Oct 11, 2003: GASPER FAN. FAILED. GASPER FAN C/B POPPED IN CLIMB WITH A BURNED METAL ODOR. REPLACED FAN. - [SDR DL73S030778](https://openairdocs.org/sdr/DL73S030778), Aug 23, 2003: COFFEEMAKER. BURNED. BURNING ODOR IN AFT GALLEY, TURNED GALLEY POWER OFF, ODOR WENT AWAY. REPLACED AFT GALLEY NR 2 COFFEE DISPENSER. - [SDR DL73S030594](https://openairdocs.org/sdr/DL73S030594), Jun 26, 2003: CHARGER. INOPERATIVE. AFTER LANDING FWD EMERGENCY LIGHT COVER FELL ON FLOOR. REINSTALLED COVER AND LIGHT DOES NOT OPS OK. CHANGED EMERGENCY LIGHT BATTERY PACK, NO HELP. CHANGED BATTE - [SDR DL73S030497](https://openairdocs.org/sdr/DL73S030497), May 29, 2003: FRAME. CUT. FRAME AND REINFORCEMENT ANGLE CUT AT STA 380 TO REPLACE SECTION OF STR 17L. REPAIRED FORMER PER SRM 53-10-4 FIG 9. REPAIRED REINFORCEMENT ANGLE PER SRM 51-40-3, - [SDR DL73S030466](https://openairdocs.org/sdr/DL73S030466), May 14, 2003: ACTUATOR. CRACKED. AFTER LANDING ROLL OUT, LOSS OF SYSTEM -A- QUANTITY PRESSURE FOUND NR 1 SPOILER ACTUATOR CRACKED. REPLACED ACTUATOR - [SDR DL73K011265](https://openairdocs.org/sdr/DL73K011265), Jul 30, 2001: WEB. CORRODED. CORROSION WAS FOUND ON THE AFT PRESSURE DOME WEB AT BL 0. THE CORROSION WAS CUT OUT AND A REPAIR DOUBLER INSTALLED. THE DAMAGE WAS FOUND AT HMV. - [SDR DL73K011196](https://openairdocs.org/sdr/DL73K011196), Jul 19, 2001: SKIN. CRACKED. THE FUSELAGE SKIN SKIN JUST FWD OF FS 767 AT STR 19R UNDER THE WING-TO-BODY FAIRING WAS FOUND CRACKED. THE CRACK WAS LIMITED TO THE SKIN ONLY AND WAS CUT OUT. T - [SDR DL73K011194](https://openairdocs.org/sdr/DL73K011194), Jul 19, 2001: FITTING. CORRODED. CORROSION WAS FOUND ON THE LUG BORES AND FACES OF THE RH ANDLH HORIZONTAL STABILIZER CLEVIS ATTACH FITTINGS. THE CORROSION WAS REMOVED AND OVERSIZED BUSHINGS IN - [SDR DL73K011193](https://openairdocs.org/sdr/DL73K011193), Jul 19, 2001: FITTING. CORRODED. CORROSION WAS FOUND RH AND LH HORIZONTAL STABILIZER ATTACH FITTINGS ON THE FACES AND BORES. THE CORROSION WAS REMOVED AND OVERSIZED BUSHINGS WERE INSTALLED PER - [SDR DL73K011181](https://openairdocs.org/sdr/DL73K011181), Jul 17, 2001: SKIN. CRACKED. A CRACK WAS FOUND IN THE FUSELAGE SKIN FORWARD OF THE LOWER AFT CORNER. THE DAMAGE WAS REPAIRED PER BOEING S/B 737-53- 1083. THE DAMAGE WAS FOUND AT HMV. - [SDR DL73K011180](https://openairdocs.org/sdr/DL73K011180), Jul 17, 2001: ATTACH FITTING. CORRODED. THE FUSELAGE CLEVIS LUGS AND THE VERTICAL FIN ATTACHMENT LUGS WERE FOUND CORRODED IN THE BORES AND THE FACES. THE CORROSION WAS REMOVED AND OVERSIZED BUSHINGS I - [SDR DL73K011179](https://openairdocs.org/sdr/DL73K011179), Jul 17, 2001: SPAR CAP. CRACKED. A CRACK WAS FOUND IN THE REAR SPAR UPPER CAP AT RSS 224.14. A REPAIR WAS INSTALLED PER BOEING REWORK DRAWING 65C30105. THE DAMAGE WAS FOUND DURING AN INSPECTION - [SDR DL73K011146](https://openairdocs.org/sdr/DL73K011146), Jul 11, 2001: SKIN. CRACKED. THE FUSELAGE SKIN AT FS 727B AND STR 18L UNDER THE WING-TO- BODY FAIRING WAS FOUND CRACKED. THE DAMAGE WAS CUT OUT AND REPAIRED WITH AN EXTERNAL DOUBLER SIMILIA - [SDR DL73K011100](https://openairdocs.org/sdr/DL73K011100), Jul 2, 2001: SKIN. DENTED. LEADING EDGE OF LT HORIZONTAL STAB HAD SKIN DENTED OUT OF LIMITS. - [SDR DL73K011088](https://openairdocs.org/sdr/DL73K011088), Jun 29, 2001: FRAME. CRACKED. CRACKS WERE FOUND AT THE BOTTOM TWO FASTENERS ON THE INNER CCHORD OF THE LEFT FS 616 FRAME AT THE OVERWING FRAME TO STUB BEAM JOINT. THE CRACKS ARE TYPICAL OF T - [SDR DL73K991660](https://openairdocs.org/sdr/DL73K991660), Jul 23, 1999: LIGHT. INOP. EMER TRACK LTS INOP SEATS ROW 10-16. REPLACED EMER TRACK LT PACK BATTERY AND CHARGER OPS NML. - [SDR DL73K971606](https://openairdocs.org/sdr/DL73K971606), Aug 1, 1997: BULKHEAD WEB. CRACKED. DURING REPETITIVE INSPECTIONS PER SI 3-69482-12, THE STA 178 BULKHEAD WAS FOUND CRACKED AT LBL 5.7, WL 200. A REPAIR HAD PREVIOUSLY BEEN INSTALLED ON THE RIGHT - [SDR DL73K971503](https://openairdocs.org/sdr/DL73K971503), Jul 29, 1997: FITTING. CRACKED. THE LEFT WING OUTBOARD AFT SUPPORT FITTING FOR THE MAIN LANDING GEAR BEAM WAS FOUND CRACKED. THE CRACKING IS TYPICAL TO THAT DESCRIBED IN S/B 737-57-1216, REV 1 - [SDR DL73K971498](https://openairdocs.org/sdr/DL73K971498), Jul 22, 1997: ANGLE. CORRODED. SUPPORT ANGLE CORRODED LT SIDEWALL CABIN FLOOR SUPPORT ANGLE IS CORRODED FS 300 TO 360. STARTED REMOVAL OF CORR PER SRM 51-10-6, REMOVED SECTION OF ANGLE FOR RE - [SDR DL73K970604](https://openairdocs.org/sdr/DL73K970604), Apr 3, 1997: ENGINE. TAILPIPE FIRE. DURING NR 1 ENG START HAD POSSIBLE TAIL PIPE FIRE AFTER ABORTED START. FIRED LEFT ENG FIRE BOTTLE. REPLACED LEFT ENG FIRE BOTTLE. PERFORMED VISUAL INSP OF NR 1 - [SDR DL73K970501](https://openairdocs.org/sdr/DL73K970501), Mar 18, 1997: FIRE WARNING. MALFUNCTIONED. APU FIRE WARNING ON SHORT FINAL. BOTTLE DISCHARGED PER POM. EGT INDICATED 600 DEGREES ON SHUT DOWN. INSPECTED APU, NO EVIDENCE OF FIRE. FWD APU TO MCO AND PLACA - [SDR DL73K970069](https://openairdocs.org/sdr/DL73K970069), Jan 15, 1997: BATTERY. DISCHARGED. AFT CABIN UPPER EMERGENCY FLASHLIGHT INOP. REPLACED BATTERIES, CHECKS NORMAL. ## 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 19960811043099I](https://openairdocs.org/incident/19960811043099I), Aug 11, 1996: Boeing 737232 (N317DL), El Paso, TX. Narrative: on August 11, 1996 at 1820 MST, in El Paso, TX delta flight 446, a Boeing 737-232, tail number N317DL, aborted takeoff approaching 100 knots due to… - [Incident 19870116003589I](https://openairdocs.org/incident/19870116003589I), Jan 16, 1987: Boeing 737232 (N317DL), Memphis, TN. Engine shutdown after start. Valve open light illuminated in flight. Pressure switch replaced, after safe landing. --- 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.