# N330DL: 1984 Boeing 737-232, registration cancelled 2007-03-13 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: March 13, 2007 - Exported to: Brazil - Status when cancelled: Triennial form not returned - 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: 23102 - Year built: 1984 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-jet - Airworthiness: Standard, transport - Airworthiness date: September 27, 1984 - Certificate issued: October 24, 1984 - Last registry action: May 16, 2006 - Mode S code: A39625 - Owner when cancelled: [Wilmington Trust Company Trustee](https://openairdocs.org/faa-owner/WILMINGTON%20TRUST%20COMPANY%20TRUSTEE) - Location: [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington) - Owner type: Corporation - Owner's area on the map: 39.7357° N, 75.5321° W: Placed by OpenAirDocs: center of Wilmington, DE, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N330DL - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=330DL - Page: https://openairdocs.org/deregistered/N330DL-2007-03-13 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 (23) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR DL73S060013](https://openairdocs.org/sdr/DL73S060013), Dec 13, 2005: SKIN. CRACKED. A CRACK WAS FOUND IN THE FUSELAGE SKIN. CRACK IS 3 INCH LONG LOCATED JUST AFT OF BS 727B, JUST BELOW S-18L. INSTALLED A DOUBLER IAW ER/A 452077-14AD. - [SDR DL73S050097](https://openairdocs.org/sdr/DL73S050097), Feb 8, 2005: FRAME. CRACKED. A FASTENER HOLE COMMON TO THE OUTER CHORD OF THE AFT FRAME OF THE L2 DOOR CUTOUT (FS 992, BETWEEN STRINGERS 7L & 8L) WAS FOUND CRACKED. THE HOLE WAS OVERSIZED A - [SDR DL73S031040](https://openairdocs.org/sdr/DL73S031040), Nov 21, 2003: SKIN PANEL. CRACKED. DURING ACCOMPLISHMENT OF 03-058543-03, ME-01 EXISTING REPAIRS AND NEW CRACK DAMAGE WERE NOTED ON THE KEEL BEAM LOWER SKIN PANEL. THE SUBJECT SKIN PANEL WAS REPL - [SDR DL73S031039](https://openairdocs.org/sdr/DL73S031039), Nov 21, 2003: ATTACH FITTING. CORRODED. DURING ACCOMPLISHMENT OF 03-069697-03 NUMEROUS ATTACHMENT LUGS REQUIRED MACHINING BEYOND THE LIMITS PROVIDED, IN ORDER TO REMOVE ALL CORROSION DAMAGE FOUND. LUG - [SDR DL73S031033](https://openairdocs.org/sdr/DL73S031033), Nov 20, 2003: FLOORBEAM. CORRODED. DURING MODIFICATION OF THE BL 24 FLOORBEAMS PER EO 03-056673-03AD ADDITIONAL WORK WAS REQUIRED DUE TO ADDITIONAL DAMAGE INCURRED. ERA 385831-14AD IMPLEMENTS THE - [SDR DL73S031028](https://openairdocs.org/sdr/DL73S031028), Nov 19, 2003: FITTING. CORRODED. CORROSION DAMAGE WAS FOUND ON THE VERTICAL STAB NR 2 FIN LUG AND THE NR 11 BODY CLEVIS LUG. CORROSION WAS REMOVED AND REWORKED PER ERA 385810-14. - [SDR DL73S031036](https://openairdocs.org/sdr/DL73S031036), Nov 17, 2003: SKIN. DAMAGED. THE FUSELAGE SKIN WAS FOUND DAMAGED AROUND 2 NUT PLATE HOLES USED FOR ATTACHMENT OF A WING TO FUSELAGE FAIRING PANEL AT FS 760 BETWEEN STRINGERS 19R & 20R. THE - [SDR DL73S031035](https://openairdocs.org/sdr/DL73S031035), Nov 17, 2003: SKIN. GOUGED. THE FUSELAGE SKIN WAS FOUND DENTED AND GOUGED NEAR FS 178 AND STRINGER 24R. THE DAMAGED SECTION OF SKIN WAS CUT OUT AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBL - [SDR DL73S031025](https://openairdocs.org/sdr/DL73S031025), Nov 17, 2003: SKIN. DENTED. A DENT WAS NOTED IN THE FUSELAGE SKIN AT BS 380, BETWEEN S17L AND S18-L. THE DENT WAS CUT OUT AND REPAIRED PER ERA 385827-14. - [SDR DL73S031010](https://openairdocs.org/sdr/DL73S031010), Nov 12, 2003: FLOORBEAM. CRACKED. THE FS 520 FLOORBEAM WAS FOUND WITH 1 INCH TO 2 INCH CRACKS NEAR THE UPPER CAP FLANGE AT RBL & LBL 24 & 45. THE CRACKS WERE TYPICAL OF BAC S/B 737-53-1120. THE - [SDR DL73S030975](https://openairdocs.org/sdr/DL73S030975), Oct 29, 2003: STOP FITTING. DAMAGED. DURING ACCOMPLISHMENT OF EO 3-059252-3AD, OPN 0301, (S/B 737-52A1100), A 65-46861-0) FITTING WAS FOUND. EO INSTRUCTIONS REQUIRE ENGINEERING EVALUATION. EVALUATI - [SDR DL73K030896](https://openairdocs.org/sdr/DL73K030896), Oct 2, 2003: FRAME. CRACKED. THE LOWER FORWARD FRAME OF THE C1 DOOR HAD A TIME-LIMITED REPAIR PREVIOUSLY INSTALLED AND NEEDED PERMANENT REPAIR INSTRUCTIONS. PERMANENT REPAIR ISSUED VIA ERA - [SDR DL73K011340](https://openairdocs.org/sdr/DL73K011340), Aug 14, 2001: KEELBEAM. CRACKED. THE LT STRINGER 18A SHEAR BEAM AT FS 727 WAS FOUND WITH A 1 INCH CRACK EMANATING FROM THE EDGE OF THE WEB. THE CRACK IS TYPICAL OF THOSE SHOWN IN BAC S/B 737-53 - [SDR DL73K010377](https://openairdocs.org/sdr/DL73K010377), Mar 6, 2001: KEELBEAM. CRACKED. THE RT STRINGER 18A SHEAR BEAM WAS FOUND WITH A WEB CRACK AT FS 727. THE CRACK IS TYPICAL OF THOSE FOUND IN BAC S/B 737-53-1066, HOWEVER THE S/B IS NOT EFFECTIV - [SDR DL73K002530](https://openairdocs.org/sdr/DL73K002530), Dec 29, 2000: RELAY. FAILED. DURING CLIMB RIGHT CENTER LOW PRESSURE LIGHT ILLUMINATED. CB POPPED RETURNED TO EWR. - REPLACED CONTROL RELAY FOR RT CENTER FUEL BOOST PUMP - [SDR DL73K001620](https://openairdocs.org/sdr/DL73K001620), Aug 21, 2000: LIGHT. INOPERATIVE. ON LAYOVER, EMERGENCY LIGHT INOP AT ROW 10 DEF. REPLACED LIGHT ASSY, CKS GOOD. - [SDR DL73K000674](https://openairdocs.org/sdr/DL73K000674), Apr 8, 2000: SEAT. CRACKED. SEAT ROW 3 DEF LOOSE ON MOUNTS LIKE A ROCKING CHAIR. FOUND SEAT FRAME CRACKED. REPLACED SEAT ASSEMBLY. - [SDR DL73K990542](https://openairdocs.org/sdr/DL73K990542), Mar 11, 1999: FRAME. CRACKED. THE AFT DOOR JAMB FRAME OF THE R1 DOOR OPENING WAS FOUND WITH A 3 INCH LONG CRACK UNDER UPPER DOOR STOP FITTING. THE CRACKED FRAME WAS REPAIRED PER THE REQUIREM - [SDR DL73S981794](https://openairdocs.org/sdr/DL73S981794), Aug 30, 1998: ACTUATOR. FAILED. RUNAWAY STAB TRIM ON SHORT FINAL. GO-AROUND MADE. REPLACED STAB TRIM ACTUATOR. - [SDR DL73S980538](https://openairdocs.org/sdr/DL73S980538), Mar 9, 1998: SKIN. GOUGED. SEVERAL GOUGES AND NICKS WERE FOUND IN THE EDGE OF THE SKIN O THE AFT SIDE OF THE C1 DOOR CUTOUT AT APPROX FS 489, BETWEEN S21R AND S23R. REPAIRED PER ERA 33146 - [SDR DL73S980537](https://openairdocs.org/sdr/DL73S980537), Mar 9, 1998: INTERCOSTAL. CRACKED. DURING INSPECTION PER SI 3-55852-12, THE R1 DOOR AFT FRAME INTERCOSTALS BETWEEN FS 332 AND 344 WERE FOUND CRACKED AT 3 LOCATIONS S8A, 10A, AND 11A. REPAIRED PER - [SDR DL73S960651](https://openairdocs.org/sdr/DL73S960651), Mar 14, 1996: BLKHD WEB. CRACKED. THE BS 178 BULKHEAD WEB WAS FOUND CRACKED BENEATH THE VERTICAL STIFFENERS AT LBL 5.7 AND RBL 5.7. DAMAGE REMOVAL RESULTED IN A 1.45 INCH LEFT AND RIGHT BY 1.2 I - [SDR DL73S953838](https://openairdocs.org/sdr/DL73S953838), Sep 8, 1995: COWL. DENTED. DURING SHOP VISIT, ENGINE NOSE COWL ASSEMBLY WAS RESTORED PER CMM 65-85378. OUTER SKIN DENTED AT 5:30 POSITION. REPAIRED PER SRM 51-40-2. ## 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 19970609016489I](https://openairdocs.org/incident/19970609016489I), Jun 9, 1997: Boeing 737232 (N330DL), Buffalo, NY. Narrative: on Thursday, June 5, 1997, at 2038 EST, a Boeing 737, N330DL, registered to wilmington trust company, trustee and operated by delta airlines, a… - [Incident 19861217079539I](https://openairdocs.org/incident/19861217079539I), Dec 17, 1986: Boeing 737232 (N330DL), Memphis, TN. Engine start valve light came on en route. Diverted and found warning system to be faulty. --- 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.