# N319DL: 1984 Boeing 737-232, registration cancelled 2009-05-13 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: May 13, 2009 - 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-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: 23091 - Year built: 1984 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Experimental, research and development, showing compliance - Airworthiness date: October 22, 1984 - Certificate issued: December 5, 1984 - Last registry action: May 16, 2006 - Mode S code: A36896 - Owner when cancelled: [Wilmington Trust Co Trustee](https://openairdocs.org/faa-owner/WILMINGTON%20TRUST%20CO%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/N319DL - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=319DL - Page: https://openairdocs.org/deregistered/N319DL-2009-05-13 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 (38) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR DL73S060132](https://openairdocs.org/sdr/DL73S060132), Feb 15, 2006: GASPER FAN. FAILED. BURNT ELECT SMELL WITH GASPER FAN ON. REPLACED FAN. - [SDR DL73S060092](https://openairdocs.org/sdr/DL73S060092), Jan 30, 2006: STIFFENER. CORRODED. CORROSION FOUND ON THE BS 1016 AFT PRESSURE BULKHEAD Z-STIFFENER AT STR 26R. REMOVED CORROSION, DAMAGE WITHIN ALLOWABLE LIMITS WITHOUT REINFORCEMENT. REF AD 200 - [SDR DL73S060090](https://openairdocs.org/sdr/DL73S060090), Jan 29, 2006: FLOORBEAM. CRACKED. THE LBL & RBL 24 LONGITUDINAL OVERWING FLOORBEAMS WERE PREVIOUSLY MODIFIED PER REV B OF 3-56673-12AD, HOWEVER THIS INSTALLATION DOES NOT MEET THE REQUIREMENTS O - [SDR DL73S050226](https://openairdocs.org/sdr/DL73S050226), Apr 20, 2005: INDICATOR. FAILED. DURING PUSHBACK A ELECTRICAL SPARKING ARCING LIKE SOUND A VERY SLIGHT SMELL OF ELECTRICAL FUMES WHICH STOPPED VERY QUICKLY F/O`S VSI WENT INOP. REPLACED VSI. - [SDR DL73S050091](https://openairdocs.org/sdr/DL73S050091), Feb 8, 2005: ENGINE. MALFUNCTIONED. FLT 7000 FT CLIMB EPR 250 - CLIMBING CLEAN HEARD LOUD BOOM WITH A/C SHUDDER ONCE. ALL ENG IND NORM AND STEADY. PNEU NORM. NO VISIBLE DAMAGE FROM CABIN F/A'S. AT - [SDR DL73S050026](https://openairdocs.org/sdr/DL73S050026), Jan 13, 2005: BALLAST. INOPERATIVE. CREW REPORTED ACRID SMELL THROUGHTOUT CABIN. INSP E/E COMP, CARGO BAYS, CABIN BALLAST. FOUND BALLAST OF SEAT 2CD BAD. REPLACED BALLAST. A/C OK FOR SERVICE. - [SDR DL73S040999](https://openairdocs.org/sdr/DL73S040999), Oct 28, 2004: SKIN. CRACKED. THE FUSELAGE SKIN WAS FOUND WITH A 4 INCH CRACK RUNNING ALONG THE BONDED DOUBLER EDGE JUST BELOW STRINGER 23R BETWEEN FS 927 & 947. AN EXISTING SKIN DOUBLER WAS - [SDR DL73S040193](https://openairdocs.org/sdr/DL73S040193), Feb 26, 2004: ACCESSORY UNIT. FAILED. ON T/O WHEN GEAR HANDLE RAISED LEFT MAIN GEAR RED UNSAFE LIGHT REMAINED ON. NO OTHER ABNORMAL INDICATIONS. REPLACED LANDING GEAR ACCESSORY UNIT. - [SDR DL73S040172](https://openairdocs.org/sdr/DL73S040172), Feb 18, 2004: CLEVIS. CORRODED. CORROSION DAMAGE WAS NOTED ON THE NR 5, NR 6 AND NR 11 BODY CLEVIS LUGS. CORROSION WAS REMOVED AND FITTINGS REWORKED IAW 386170-14. - [SDR DL73S040170](https://openairdocs.org/sdr/DL73S040170), Feb 18, 2004: SKIN. DENTED. THE UPPER SKIN OF THE S19R WAS FOUND DENTED. DENTED WAS REMOVED AND REPAIR INSTALLED IAW 386089-14. - [SDR DL73S040169](https://openairdocs.org/sdr/DL73S040169), Feb 18, 2004: SUPPORT FITTING. CORRODED. CORROSION WAS NOTED ON BOTH THE LT AND RT BS 685 MLG SUPPORT FITTINGS IN THE LUG BORES AND FACES. CORROSION WAS REMOVED AND FITTINGS REWORKED IAW ERA 386114-14. - [SDR DL73S040152](https://openairdocs.org/sdr/DL73S040152), Feb 12, 2004: BULKHEAD. CORRODED. CORROSION WAS NOTED AT BS 1016 PRESSURE BLKHD, AT BL 0 AND AFFECTED THE WEB/GORE AND CHANNEL STIFFENERS. REPAIRED PER ERA 386069-14AD. - [SDR DL73S040149](https://openairdocs.org/sdr/DL73S040149), Feb 11, 2004: FRAME. CRACKED. DURING INSPECTION OF THE BS 663 FRAME CRACKS WERE NOTED IN THE FRAME AT S3L, S2L AND S1. DURING INSTALLATION OF THE SRM FRAME REPAIR IT WAS NECESSARY TO CUT THE - [SDR DL73S040144](https://openairdocs.org/sdr/DL73S040144), Feb 9, 2004: FLAP TRACK. CORRODED. THE REAR ENGINE MOUNT ATTACH HOLES, LOCATED AT THE NR 2 AND NR 3 T/E FLAPS, OUTBOARD TRACKS WERE NOTED WITH CORROSION IN THE BORES. CORROSION WAS REMOVED AND TR - [SDR DL73S040115](https://openairdocs.org/sdr/DL73S040115), Jan 28, 2004: ATTACH FITTING. CORRODED. THE STABILZER ATTACHMENT LUGS WERE FOUND WITH DAMAGE EXCEEDING THE LIMITS OF SB 737-55-1033. DAMAGE WAS REMOVED BY BLENDING AND OVERSIZING BORES PER ER/A 386108 - [SDR DL73S040104](https://openairdocs.org/sdr/DL73S040104), Jan 28, 2004: ATTACH FITTING. CORRODED. NUMEROUS ATTACHMENT FITTING LUGS ON THE HORIZ STAB TO FUSELAGE JOINT REQUIRED MACHINING BEYOND PUBLISHED LIMITS IN ORDER TO REMOVE CORROSION. CORROSION WAS REMO - [SDR DL73S040102](https://openairdocs.org/sdr/DL73S040102), Jan 28, 2004: FLOORBEAM. CRACKED. DURING INSPECTION THE BS 520 FLOORBEAM WAS NOTED WITH CRACKS IN THE RADIUS, ALONG THE UPPER CHORD TO WEB RADIUS AT LBL 24.75, LBL 45.5 AND RBL 24.75. UPPER CAP - [SDR DL73K002017](https://openairdocs.org/sdr/DL73K002017), Oct 15, 2000: ACTUATOR. INTERMITTENT. AFTER STARTING NR 1ENG (NORMAL START) DURING TAXI OUT NR 1 ENG FLAMED OUT. ON RESTART ATTEMPT AT GATE, NO FUEL FLOW INDICATION AFTER START LEVER RAISED TO IDLE. - [SDR DL73K001081](https://openairdocs.org/sdr/DL73K001081), Jun 2, 2000: ANTENNA. INOPERATIVE. WEATHER RADAR INOP, CON/IND FAULT. REPLACED R/T AND ANT PER MM, PUSHED OUT INTO RAMP AND PAINTED ACTUAL WEATHER, OPS NORMAL IN ALL MODES. - [SDR DL73K000625](https://openairdocs.org/sdr/DL73K000625), Apr 2, 2000: CONTROLLER. MALFUNCTIONED. ON DESCENT INTO TPA PASSING THROUGH 15000 FT, RECEIVED A WHEEL WELL FIRE INDICATION. AFTER PERFORMING APPROPRIATE PROCEDURE WHEEL WELL FIRE LIGHT BECAME INTERMI - [SDR DL73K000529](https://openairdocs.org/sdr/DL73K000529), Mar 17, 2000: VALVE. MALFUNCTIONED. AIRCRAFT FAILED TO PRESSURIZE AFTER T/O FROM PBI. OUTFLOW VLVS INDICATED FULL CLOSED. F/A REPORTED THERE WAS LOUD WIND NOISE AROUND L1 DOOR. DOOR INDICATED CLOS - [SDR DL73K991715](https://openairdocs.org/sdr/DL73K991715), Jul 31, 1999: WIRE. FAILED. STAB TRIM CONTROL WHEEL SWITCHES INOP. POPS ACTUATOR C/B. AUTOPILOT TRIM IS OK. FOUND WIRES SHORTED TO GROUND AT BULKKHEAD 1088. REPAIRED WIRE WITH SPLICES. WIR - [SDR DL73K982229](https://openairdocs.org/sdr/DL73K982229), Oct 29, 1998: O-RING. FAILED. LOSS OF HYD SYS A QTY IN FLT. REPL NO3 FLT SPOILER ACTUATOR. O-RING RUPTURED ON ACTUATOR. ALL LEAK AND OPN TEST NML. - [SDR DL73K980223](https://openairdocs.org/sdr/DL73K980223), Jan 26, 1998: BULKHEAD WEB. CRACKED. SEVERAL CRACKS FOUND IN THE FS 178 BULKHEAD. REPAIRED PER ERA 331261-14. - [SDR DL73K980222](https://openairdocs.org/sdr/DL73K980222), Jan 26, 1998: FITTING. CRACKED. DURING INSPECTION PER SB 737-57-1216 TWO CRACKS WERE FOUND IN THE MLG BEAM AFT SUPPORT FITTING ON THE RS OF THE RT WING. THE INBD CRACK LOCATION IS TYP PER SB. - [SDR DL73K980221](https://openairdocs.org/sdr/DL73K980221), Jan 26, 1998: SPAR CHORD. CORRODED. CORROSION FOUND ON THE UPPER SURFACE OF THE AFT FLANGE OF THE HORIZ STAB REAR SPAR UPPER CHORD. REPAIRED PER ERA 331272-14. - [SDR DL73K980184](https://openairdocs.org/sdr/DL73K980184), Jan 22, 1998: SKIN. CRACKED. SKIN AT THE COOLING DUCT CUTOUT AT BS 379, APPROXIMATELY BL0 WAS FOUND CRACKED AT THE AFT EDGE OF THE CUTOUT. CRACK IS APPROXIMATELY 1.5 IN LENGTH AND IS TYPICA - [SDR DL73K980066](https://openairdocs.org/sdr/DL73K980066), Jan 9, 1998: APU. ODOR. SMOKE ALARM WENT OFF IN FWD LAV CREW COULD SMELL ACRID SMELL. FOUND APU PUTTING OIL INTO PNEUMATIC DUCTS. FWD APU TO MCO REPLD DETECTOR BATTERY, REPLD LT AND RT - [SDR DL73K972197](https://openairdocs.org/sdr/DL73K972197), Oct 17, 1997: SKIN. CRACKED. FUSELAGE SKIN AND BEAR STRAP AFT GALLEY DOOR SURROUND. REPAIR FOR CRACK AT LWR HINGE CUT OUT. A .25 INCH CRACK WAS FOUND IN THE SKIN AND A 1.0 INCH CRACK IN THE - [SDR DL73K971141](https://openairdocs.org/sdr/DL73K971141), Jun 15, 1997: POWER SUPPLY. INOPERATIVE. FWD CABIN EMERGENCY LIGHTS STUCK ON AFTER TEST. REPLACED POWER SUPPLY. - [SDR DL73K962792](https://openairdocs.org/sdr/DL73K962792), Dec 31, 1996: P6 PANEL. TRIPPED. BOTH GENRATORS WERE LOST AT FL310. ACCOMPLISHED LOSS OF BOTH GENERATORS CHECKLIST PER AOM. DIVERTED TO JFK, STIMATED LANDING WT 103,500 AND LANDING NORMAL. REP - [SDR DL73K962355](https://openairdocs.org/sdr/DL73K962355), Oct 18, 1996: CHARGER. INOPERATIVE. FOUND ON L/O CHECK, EMERGENCY FLOOR TRACK LIGHTING HAS A SECTION INOP. REPLACED CHARGER ASSY, OPS CHECK NORMAL. - [SDR DL73S953413](https://openairdocs.org/sdr/DL73S953413), Aug 15, 1995: SKIN. DAMAGED. RUDDER HAS TEMPORARY REPAIR ON UPPER RT SIDE SKIN. REPAIRED DAMAGE AS PER SRM 55-40-5 WITH REF TO 51-40-15. - [SDR DL73S953409](https://openairdocs.org/sdr/DL73S953409), Aug 14, 1995: SKIN. DAMAGED. FUSELAGE SKIN AT FS 935 BETWEEN STR 21 AND 22, SUSTAINED PUNCTURE DAMAGE FROM GROUND EQUIPMENT. REPAIRED PER DL ERA 302319-14 AND SRM 53-10-3 FIG 1 FOR DAMAGE T - [SDR DL73S953056](https://openairdocs.org/sdr/DL73S953056), Jul 11, 1995: ANTI-ICE DUCT. CRACKED. AFTER TAKEOFF, NR 2 OIL TEMP CLIMBED THROUGH YELLOW ZONE, ENGINE WAS SHUTDOWN WHEN TEMP WENT TO RED. RETURNED TO ATL. FOUND ENGINE ANTI-ICE DUCT CRACKED AND BLO - [SDR DL73S952862](https://openairdocs.org/sdr/DL73S952862), Jun 28, 1995: GCU. FAILED. DURING CRUISE, LOST NR 1 GENERATOR, GCU BREAKER TRIPPED. STARTED APU, UNABLE TO TRANSFER POWER, DIVERTED BOS. REPLACED NR 1 GCU AND NR 1 GEN BREAKER. OP CHECK N - [SDR DL73S952692](https://openairdocs.org/sdr/DL73S952692), Jun 19, 1995: RELAY. FAILED. ON CLIMBOUT, LOST ALL FLT INSTRUMENTS ON LEFT SIDE, RETURNED TO CVG. FOUND NORMAL TRANSFER C/B TRIPPED. REPLACED R3 TRANSFER RELAY, OPERATION NORMAL. - [SDR DL73S950481](https://openairdocs.org/sdr/DL73S950481), Feb 1, 1995: FLOOR BEAM. CRACKED. DURING ROUTINE INSPECTION, THE BL 0.07 FLOORBEAM OF THE WING CENTER SECTION WAS FOUND CRACKED AT STA 657. THE UPPER CAP WAS COMPLETELY CRACKED, BUT NO CRACKS WE ## 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 20000323032269I](https://openairdocs.org/incident/20000323032269I), Mar 23, 2000: Boeing 737232 (N319DL), Allentown, PA. (-23)Pilot reported a/c hydraulic systme "a" quantity loss approximately 7 miles before arrival point (abe). Pilot (capt.) declared an emegency, overflew the… --- 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.