# N329DL: 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-1](https://openairdocs.org/engine/pratt-whitney-jt8d-1) (registry code 52044) - Data sheets: [TCDS A16WE](https://openairdocs.org/tcds/A16WE), [TCDS E2EA](https://openairdocs.org/tcds/E2EA) (OpenAirDocs) - Serial number: 23101 - Year built: 1984 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-jet - Airworthiness: Standard, transport - Airworthiness date: October 26, 1984 - Certificate issued: November 19, 2007 - Last registry action: November 19, 2007 - Mode S code: A39015 - 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/N329DL - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=329DL - Page: https://openairdocs.org/deregistered/N329DL-2007-12-21 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 737-232: https://openairdocs.org/model/boeing-737-232.md ## Service difficulty reports (40) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR DL73S060242](https://openairdocs.org/sdr/DL73S060242), Apr 3, 2006: BEAR STRAP. CRACKED. THE UPPER AFT CORNER OF THE L2 DOOR OPENING HAS A FATIGUE CRACK IN THE BEAR STRAP AND ONE IN THE FUSELAGE OUTER SKIN AND DOUBLER. CUTOUT IS 3.5 X 1.5 INCH. INST - [SDR DL73S050615](https://openairdocs.org/sdr/DL73S050615), Oct 13, 2005: FLOORBEAM. CRACKED. THE RBL 24 LONGITUDINAL OVERWING FLOORBEAM HAS BEEN PREVIOUSLY MODIFIED PER 3-056673-3AD. THE C-CHANNEL INSTALLED PER THIS EO DOES NOT MEET EXISTING AD REQUIREM - [SDR DL73S050614](https://openairdocs.org/sdr/DL73S050614), Oct 13, 2005: FLOORBEAM. CRACKED. THE LBL 24 LONGITUDINAL OVERWING FLOORBEAM WAS MODIFIED USING A PREVIOUSLY ACCEPTALBE C-CHANNEL THAT IS NOT ACCEPTABLE PER AD 2001-17-18. CRACKS WERE FOUND IN T - [SDR DL73S041012](https://openairdocs.org/sdr/DL73S041012), Nov 2, 2004: SHEAR BEAM. CRACKED. A 1 INCH CRACK WAS FOUND EMANATING FROM A FASTENER HOLE AT THE AFT END OF THE STRINGER 18A SHEAR BEAM WEB AT FS 727 ON THE LT SIDE OF THE AIRCRAFT. THE CRACK EX - [SDR DL73S040229](https://openairdocs.org/sdr/DL73S040229), Mar 11, 2004: RELIEF VALVE. FAILED. DURING APPROACH PHASE AFTER PLACING THE FLAP LEVER TO 5 SYSTEM A PRESSURE WENT TO ZERO WITH ASSOCIATED SYSTEM A LOW PRESSURE LIGHTS ILLUMINATED. REPLACED SEVERA - [SDR DL73S040191](https://openairdocs.org/sdr/DL73S040191), Feb 25, 2004: REGULATOR. LEAKING. LOSS OF A-SYSTEM HYDRAULIC PRESSURE. FOUND NO RESERVOIR HEAD PRESSURE. REPLACED RESERVOIR PRESSURE REGULATOR AND BOTH CHECK VALVES. - [SDR DL73S030630](https://openairdocs.org/sdr/DL73S030630), Jul 12, 2003: INSULATION. OUT OF POSITION. SMOKE SMELL IN AFT CABIN. FOUND INSULATION TOUCHING APU BLEED DUCT CAUSING SMELL. REPOSITIONED INSUL. FWD APU AIR TO MCO AND PLAC AS PRECAUTION. - [SDR DL73S030508](https://openairdocs.org/sdr/DL73S030508), May 30, 2003: FRAME. CRACKED. MTC FOUND CRACKS IN THE FRAME AT S6L, 3L, 2L, 1, 2R, AND 3R EXTENDING FROM THE STRINGER PASS THRU CUTOUTS. THE CRACKS WERE CUTOUT AND A REPAIR SIMILAR TO B737-2 - [SDR DL73S030505](https://openairdocs.org/sdr/DL73S030505), May 30, 2003: FRAME. CRACKED. THE SUBJECT DOOR FRAME WAS FOUND CRACKED AT THE INTERSECTION OF FS 440 AND STR 24R. THE FRAME WAS ORIGINALLY 0.071 INCH 7075-T6 CLAD. THE CRACK WAS TRIMMED OUT, - [SDR DL73S030495](https://openairdocs.org/sdr/DL73S030495), May 28, 2003: ATTACH FITTING. CORRODED. STABILIZERS / HORIZONTAL / ATTACH FITTINGS / LT, RT AND CENTER SECTION - CORROSION: WHILE ACCOMPLISHING AN INSPECTION OF THE HORIZONTAL STABILIZER ATTACH LUGS P - [SDR DL73S030485](https://openairdocs.org/sdr/DL73S030485), May 22, 2003: SKIN. DENTED. FUSELAGE SKIN FS 344, S-19R TO S-20R - DENT: A DENT WAS REPORTED APPROXIMATELY 2 INCHES BELOW THE LOWER EDGE OF THE UPPER SKIN OF THE LAP SPLICE AT S-19R. THE D - [SDR DL73S030479](https://openairdocs.org/sdr/DL73S030479), May 19, 2003: ATTACH FITTING. CORRODED. FUSELAGE ATTACH FITTINGS: VERTICAL STABILIZER CLEVIS LUGS - CORROSION. THE NR 11 CLEVIS LUG FWD FACE WAS FOUND GOUGED. THE DAMAGE WAS CLEANED UP USING A SPOTFAC - [SDR DL73K010986](https://openairdocs.org/sdr/DL73K010986), Jun 16, 2001: BLEED VALVE. MALFUNCTIONED. SHORTLY AFTER T/O NR 2 ENGINE EGT REACHED 640 FOR 3 TO 4 SECONDS. INSPECTED INLET AND EXHAUST, NO DEFECTS. CHECKED EPR SYSTEM WITH P/S TEST BOX INDICATION GOOD. - [SDR DL73K010840](https://openairdocs.org/sdr/DL73K010840), May 25, 2001: SKIN. CRACKED. A 1 INCH LONG CRACK WAS FOUND IN THE FUSELAGE SKIN AT FS 750 JUST ABOVE STRINGER 18R. THE CRACK WAS REMOVED WITH A CUTOUT IN THE SKIN. THE CUTOUT WAS REPAIRED W - [SDR DL73K010004](https://openairdocs.org/sdr/DL73K010004), Dec 30, 2000: SKIN. CRACKED. THE LOWER HINGE CUTOUT OF THE FWD ENTRY DOOR CUTOUT WAS FOUND WITH A 1 INCH CRACK. THE CRACK WAS ROUTED OUT AND REPAIRED WITH AN EXTERNAL STEEL DOUBLER PER B737 - [SDR DL73K002113](https://openairdocs.org/sdr/DL73K002113), Oct 25, 2000: POWER SUPPLY. INOPERATIVE. ON MTC CK FOUND R2 OVER DOOR EMERGENCY LIGHT AND AFT EXIT LOCATOR EMERGENCY LIGHT NOT ILLUMINATING ON TEST. REPLACED POWER SUPPLY. - [SDR DL73K001234](https://openairdocs.org/sdr/DL73K001234), Jun 29, 2000: BULKHEAD. DAMAGED. INSPECTIONS OF THE FS 178 BULKHEAD STRUCTURE PER AD 2000-05-19, REVEALED CRACKS IN THE BULKHEAD STRUCTURE COMMON TO THE COCKPIT FLOOR (REF. DAL ER/A 377636-14AD - [SDR DL73K001221](https://openairdocs.org/sdr/DL73K001221), Jun 28, 2000: WEB. CRACKED. WHILE ACCOMPLISHING AD 2000-05-29 INSPECTIONS OF THE FS 178 BULKHEAD AND ADJACENT STRUCTURE, A 1 INCH CRACK WAS FOUND EMANATING FROM A LIGHTNING HOLE IN THE WEB - [SDR DL73K001222](https://openairdocs.org/sdr/DL73K001222), Jun 27, 2000: BULKHEAD. CRACKED. A TYPICAL CRACK WAS FOUND IN THE FS 178 BULKHEAD WEB AT WL 233.5, RBL 7 DURING INSPECTIONS MANDATED PER AD 2000-05-29. THE CRACK WAS REPAIRED PER B737-200 SRM 5 - [SDR DL73K000791](https://openairdocs.org/sdr/DL73K000791), Apr 23, 2000: WARNING LIGHT. FALSE INDICATION. LEFT, RIGHT AND APU FAULT DET ILLUMINATED. REPLACED COCKPIT FIRE CONTROL PANEL. GROUND CHECKS NORMAL. REPLACED FIRE DETECTOR MODULE PRECAUTIONARY OPS NORMAL. RA - [SDR DL73K992655](https://openairdocs.org/sdr/DL73K992655), Dec 6, 1999: TURBINE WHEEL. DAMAGED. AT APPROX 400 FT AGL, LOUD BANG, NR 1 ENGINE FAILED 700 DEGREES EGT, WINDMILLING N1 AND N2 WAS BLOF T/O DUE TO GROSS WT. FOUND 3RD STAGE OF LPT DAMAGED. REPLACE - [SDR DL73K991837](https://openairdocs.org/sdr/DL73K991837), Aug 14, 1999: BULKHEAD WEB. CRACKED. WHILE ACCOMPLISHING LFEC INSPECTIONS OF THE AFT PRESSURE BULKHEAD WEB, A CRACK INDICATION WAS NOTED NEAR STRINGER 6R. INTERNAL HFEC INSPECTION CONFIRMED TWO CRA - [SDR DL73K991563](https://openairdocs.org/sdr/DL73K991563), Jul 12, 1999: SUPPORT. WORN. DURING INSP PER OPN 5264, FOUND BUSHING MIGRATED RT FWD ENG MOUNT SUPPORT FITTING. REPLACED SUPPORT FITTING PER EO 03-073535-12AD ME-04. FWD MOUNT SUPPORT ASSY - [SDR DL73K991330](https://openairdocs.org/sdr/DL73K991330), Jun 12, 1999: TIRE. FAILED. EXPERIENCE NOSE WHEEL TIRE FAILURE AT ROTATION. CONTINUED TAKEOFF. INSPECTED AIRCRAFT AND FOUND RT NOSE TIRE TREAD CAP MISSING. REPLACED LEFT AND RIGHT NOSE WHE - [SDR DL73K990925](https://openairdocs.org/sdr/DL73K990925), Apr 26, 1999: TIRE. FAILED. A/C BLEW NR 2 TIRE ON T/O FROM EWR. UPON LANDING IN MCO, LOST ALL 'A' SYSTEM HYDS AND HAD TO BE TOWED IN AFTER TIRE REPLACEMENT. REPLACED NR 1 AND 2 TIRES AND B - [SDR DL73K990453](https://openairdocs.org/sdr/DL73K990453), Mar 3, 1999: COMPRESSOR. DAMAGED. DURING CRUISE AT FL370 FROM MCO-BOS, CREW EXPERIENCED HEAVY COMPRESSOR STALLS ON THE NR 2 ENGINE. CREW REDUCED POWER AND LANDED IN RDU. CONTRACT MTC INSPECTED E - [SDR DL73K982610](https://openairdocs.org/sdr/DL73K982610), Dec 22, 1998: FITTING. CORRODED. FUSELAGE LT AND RT MLG SIDE STRUT SUPPORT FITTING, BS 685. REPAIR FOR OVERSIZE LUG BORES. THE LUG BORES OF THE LT AND RT MLG SIDE STRUT SUPPORT FITTINGS AT BS 6 - [SDR DL73K982498](https://openairdocs.org/sdr/DL73K982498), Dec 5, 1998: ACTUATOR. FAILED. LEADING EDGE AMBER LIGHT ON SLAT NR 5. REPLACED NR 5 SLAT AND ACTUATOR. - [SDR DL73K981632](https://openairdocs.org/sdr/DL73K981632), Aug 8, 1998: BULKHEAD CHORD. CRACKED. A 0.5 INCH CRACK WAS FOUND IN THE MLG WHEEL WELL BLKHD AT STA 727. THE CRACK WAS LOCATED IN THE UPPER FLANGE OF THE COMPRESSION CHORD AT BL 0.0 AND RUNS THRU A - [SDR DL73S981294](https://openairdocs.org/sdr/DL73S981294), Jun 18, 1998: SKIN. DENTED. FUSELAGE SKIN AND BONDED DOUBLER WERE FOUND DENTED BETWEEN S17L AND 18L AT FS 400. REPAIRED PER ERA 331844-14. - [SDR DL73S981289](https://openairdocs.org/sdr/DL73S981289), Jun 18, 1998: SKIN. CRACKED. UPON HFEC AND LFEC INSPECTIONS OF THE UPPER AFT CORNER OF THE FWD GALLEY DOORWAY PER 3-58715-3AD, A CRACK WAS INDICATED. REPAIRED PER ERA 331849-14AD. - [SDR DL73S972195](https://openairdocs.org/sdr/DL73S972195), Oct 21, 1997: SKIN. DAMAGED. FUSELAGE SKIN FS 460-480 STR 27R - 28L GROUND DAMAGE REPAIR. THE FUSELAGE SKIN BETWEEN FS 460 AND 480 AND BETWEEN STRG 27R AND 28L WAS DAMAGED BY A CARGO LOADER - [SDR DL73S970640](https://openairdocs.org/sdr/DL73S970640), Apr 10, 1997: COALESCER BAG. DIRTY. STRONG ODOR NOTED IN COCKPIT AND CABIN. REPLACED BOTH LT AND RT WATER BAGS, RAN PACKS OFF ENG AND NO SMELLS NOTED. - [SDR DL73S980089](https://openairdocs.org/sdr/DL73S980089), Jan 13, 1997: HYD LINE. RUPTURED. ON CLIMBOUT AT 12000, THE MASTER CAUTION AND HYD LIGHTS ILLUMINATED ON GLARESHIELD PANEL. ENG NR 2 HYD PUMP LOW PRESSURE ILLUMINATED ON OVERHEAD PANEL, QTY WENT - [SDR DL73S961969](https://openairdocs.org/sdr/DL73S961969), Aug 26, 1996: BURNED OUT. EMERGENCY LIGHTS AT 1L DOOR AND ROWS 17 ABC, 21 ABC, AND 25 ABC INOPERATIVE. - [SDR DL73S961461](https://openairdocs.org/sdr/DL73S961461), Jun 3, 1996: BULKHEAD WEB. CRACKED. DURING SPECIAL INSPECTION 3-69482-12, CRACKS WERE DISCOVERED ON THE FWD FACE OF THE FS 178 BULKHEAD WEB. THE FIRST CRACK IS LOCATED NEAR THE LBL 5.7 VERTICAL ST - [SDR DL73S960158](https://openairdocs.org/sdr/DL73S960158), Jan 20, 1996: VALVE. LEAKING. ON CLIMBOUT, LOST A/B HYDRAULIC SYSTEM PRESSURE. FLIGHT RETURNED MSP. FOUND PARKING BRAKE VALVE LEAKING. REPLACED VALVE, SERVICED SYSTEM AND OPERATION NORMAL. - [SDR DL73S952205](https://openairdocs.org/sdr/DL73S952205), May 19, 1995: DOOR. CRACKED. FWD B/B DOOR PAN CRACKED AT FWD AND AFT CORNERS INSIDE RADIUS. REPAIRED PER DL ERA 301812-14. - [SDR DL73S952204](https://openairdocs.org/sdr/DL73S952204), May 19, 1995: SKIN. DELAMINATED. NR 6 SPOILER UPPER SURFACE DELAMINATED. REPAIRED PER SRM 57-50-5 FIG 5. FOUND AT M1 LTR CK. - [SDR DL73S952203](https://openairdocs.org/sdr/DL73S952203), May 19, 1995: SKIN. DELAMINATED. RUDDER DELAMINATED AT TOP LEFT SIDE T/E NEXT TO PREV REPAIR. ACCOMPLISHED REPAIRS PER SRM 51-40-9 FIG 1 AND ERA 301817-14. ## Other aircraft with N329DL - [Registered now](https://openairdocs.org/aircraft/N329DL): Clydesdale Asset Mgmt CCX-2000, S/N CCX-2000-0210, built 2024 --- 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.