# N311DL: 1984 Boeing 737-232, registration cancelled 2007-01-26 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: January 26, 2007 - Exported to: Lebanon - 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: 23083 - Year built: 1984 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-jet - Airworthiness: Standard, transport - Airworthiness date: February 9, 1984 - Certificate issued: December 5, 2006 - Last registry action: December 5, 2006 - Mode S code: A34ADE - Owner when cancelled: [Aventura Aviation LLC](https://openairdocs.org/faa-owner/AVENTURA%20AVIATION%20LLC) - Location: [New York, NY](https://openairdocs.org/faa-place/NY/New%20York) - Owner type: Corporation - Owner's area on the map: 40.7524° N, 73.9727° W: Placed by OpenAirDocs at the center of ZIP code 10017, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N311DL - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=311DL - Page: https://openairdocs.org/deregistered/N311DL-2007-01-26 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 (74, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR DL73S060308](https://openairdocs.org/sdr/DL73S060308), Apr 19, 2006: SKIN. CRACKED. THE FUSELAGE SKIN WAS FOUND CRACKED AT THE LAP JOINT AT S-14L BETWEEN BS 380 AND 500A. THE DAMAGED SKIN WAS REMOVED AND A REPAIR DOUBLER WAS INSTALLED. - [SDR DL73S060307](https://openairdocs.org/sdr/DL73S060307), Apr 19, 2006: SKIN. CRACKED. THE FUSELAGE SKIN WAS FOUND WITH CRACKS IN THE LAP JOINT AT S-4L BETWEEN BS 727A+19 TO 762. THE DAMAGED SKIN WAS REMOVED AND A REPAIR DOUBLER WAS INSTALLED. - [SDR DL73S060306](https://openairdocs.org/sdr/DL73S060306), Apr 19, 2006: SKIN. CRACKED. THE FUSELAGE SKIN WAS FOUND WITH CRACKS IN THE LAP JOINT AT BS 400-410. THE DAMAGED SKIN WAS REMOVED AND A REPAIR DOUBLER WAS INSTALLED. - [SDR DL73S060305](https://openairdocs.org/sdr/DL73S060305), Apr 19, 2006: SKIN. CRACKED. THE FUSELAGE SKIN WAS FOUND WITH CRACKS IN THE LAP JOINT AT S-4L BETWEEN BS 380 AND 500. THE DAMAGED SKIN WAS REMOVED AND A REPAIR DOUBLER WAS INSTALLED. - [SDR DL73S060304](https://openairdocs.org/sdr/DL73S060304), Apr 19, 2006: SKIN. CRACKED. THE FUSELAGE SKIN WAS FOUND WITH CRACKS IN THE LAP JOINT AT S-4R BETWEEN BS 727A+1 AND 752. THE DAMAGED SKIN WAS REMOVED AND A REPAIR DOUBLER WAS INSTALLED. - [SDR DL73S050574](https://openairdocs.org/sdr/DL73S050574), Sep 29, 2005: ENGINE. BIRD INGESTION. ON T/O AT 1000 FT, HEARD LOUD BANG AND AIRCRAFT YAWED MOMENTARLLY LT AND RT. PASSENGER REPORTED BLUE FLAME FROM FWD OF LT ENGINE. FOWL SMELL IN CABIN. ENGINE PA - [SDR DL73S050202](https://openairdocs.org/sdr/DL73S050202), Apr 5, 2005: FIRE LOOP. FAILED. CLIMBING THRU 18,000 FT WHEEL WELL FIRE INDICATION. LOWERED GEAR AND INDICATION REMAINED ON. REPLACED DETECTOR LOOP. - [SDR DL73S050029](https://openairdocs.org/sdr/DL73S050029), Jan 13, 2005: SHAFT. FAILED. FUEL PUMP SHAFT SHEARED AT ROTATION. RUNWAY EXCURSION ON RETURN IN BAD WEATHER. REPLACING NR 2 ENGINE FUEL PUMP AND CONTROL. - [SDR DL73S040842](https://openairdocs.org/sdr/DL73S040842), Sep 3, 2004: SKIN. CRACKED. INSPECTION OF THE STRINGER 4L SKIN LAP JOINT PER AD 2003-08-15 REVEALED A CRACKED FASTENER LOCATION AT FS 700. THE CRACK WAS REMOVED WITH A CUTOUT AND REPAIRED - [SDR DL73S040841](https://openairdocs.org/sdr/DL73S040841), Sep 2, 2004: SKIN. CRACKED. INSPECTION OF THE STRINGER 4R SKIN LAP JOINT PER AD 2003-08-15 REVEALED A CRACKED FASTENER HOLE AT FS 631. THE CRACK WAS REMOVED WITH A CUTOUT AND REPAIRED WITH - [SDR DL73S040839](https://openairdocs.org/sdr/DL73S040839), Sep 1, 2004: SKIN. CRACKED. INSPECTION OF THE STRINGER 4R SKIN LAP JOINT PER AD 2003-08-15 REVEALED A CRACKED FASTENER HOLE AT FS 848. THE CRACK WAS REMOVED WITH A CUTOUT AND REPAIRED WITH - [SDR DL73S040838](https://openairdocs.org/sdr/DL73S040838), Sep 1, 2004: SKIN. CRACKED. INSPECTION OF THE STRINGER 4L SKIN LAP JOINT PER AD 2003-08-15 REVEALED A CRACKED FASTENER LOCATION AT FS 500. THE CRACK WAS REMOVED WITH A CUTOUT IN THE SKIN. - [SDR DL73S040498](https://openairdocs.org/sdr/DL73S040498), May 31, 2004: PIN. BROKEN. FOUND ON SERVICE CHECK, AISLE LIGHTS AT SEAT 22L AND 24L INOP. FOUND PIN BROKE ON M1136 AT STATION L753. REPLACED AND TESTED PER M/M. - [SDR DL73S040412](https://openairdocs.org/sdr/DL73S040412), May 7, 2004: BATTERY. INOPERATIVE. FWD BULLNOSE EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY. CHECKS OK. - [SDR DL73S040411](https://openairdocs.org/sdr/DL73S040411), May 7, 2004: FUSE. FAILED. AFT LT BULLNOSE EMERGENCY LIGHTS INOPERATIVE, REPLACED BATTERY. NO HELP. REPLACED FUSES ON CHARGER. CHECKS GOOD. - [SDR DL73S031097](https://openairdocs.org/sdr/DL73S031097), Dec 16, 2003: DOUBLER. DAMAGED. FOUND ON W-2 LETTER CK, STRINGER 22RT CUT AT STA 957, 977, 996 FOR OUTFLOW VALVE DOUBLER REPLACEMENT. REPAIR PER SRM 53-10-3 FIG 1. - [SDR DL73S031096](https://openairdocs.org/sdr/DL73S031096), Dec 16, 2003: FRAME. CORRODED. FOUND ON W2 LETTER CK, CORROSION ON FORMER STA 967 O/B OF STR 27 RIGHT. REPAIRED PER SRM 53-10-4 FIG 11. - [SDR DL73S031095](https://openairdocs.org/sdr/DL73S031095), Dec 16, 2003: FRAME. CORRODED. FOUND ON W-2 LETTER CK, CORROSION ON FORMER STA 967 AT SKIN ATTACH ANGLE BETWEEN STR 27 LEFT AND 27 RIGHT. REPAIRED PER SRM 53-10-4 FIG 11. - [SDR DL73S031094](https://openairdocs.org/sdr/DL73S031094), Dec 16, 2003: FRAME. CORRODED. FOUND ON W-2 LETTER CK, SKIN BULGED/ RIVETS SHEARED AT FRAME STA 847 BETWEEN STR 27 LEFT AND 27 RIGHT. FOUND FORMER CORRODED AT THIS LOCATION. REPAIRED PER SRM - [SDR DL73S031024](https://openairdocs.org/sdr/DL73S031024), Nov 16, 2003: WIRE. SHORTED. ON L/O FOUND EMERGENCY LIGHTS AT SEAT ROWS 22-25 INOP AND L2 EXIT IDENTIFIER INOP. REPAIRED DAMAGED WIRE. - [SDR DL73K030507](https://openairdocs.org/sdr/DL73K030507), Jun 3, 2003: SKIN. CRACKED. A 3 INCH CRACK WAS FOUND IN THE FUSELAGE SKIN AT FS 525 JUST ABOVE STRINGER 16L RUNNING ALONG THE EDGE OF THE INTERNAL BONDED WAFFLE DOUBLER. THE CRACK WAS REMO - [SDR DL73K030504](https://openairdocs.org/sdr/DL73K030504), Jun 2, 2003: ENGINE. MALFUNCTIONED. ENG FUEL FLOWS WERE 1500 SPLIT AFTER TAKEOFF. TRIED ENG ANTIICE ON AND MISMATCH ON THROTTLES REVERSED. EPR ON LEFT ENG 1.40 AND ON RIGHT ENG WAS 1.77. AFTER CON - [SDR DL73K021318](https://openairdocs.org/sdr/DL73K021318), Nov 13, 2002: SKIN. CORRODED. FUSELAGE / SKIN / AFT LAV SERVICE CUTOUT / FS 986.5 / STRG. 27R : CORROSION CUTOUT REPAIR AN AREA OF CORROSION WAS FOUND IN THE SKIN AT THE FWD INBD CORNER OF T - [SDR DL73K021215](https://openairdocs.org/sdr/DL73K021215), Oct 20, 2002: SPAR. CORRODED. THE CENTER SECTION OF THE HORIZONTAL STAB WAS PREVIOUSLY REWORKED FOR CORROSION IN SEVERAL LUGS. THE REWORK WAS APPROVED FOR A 24 MONTH LIMIT WHICH HAS BEEN REA - [SDR DL73K020047](https://openairdocs.org/sdr/DL73K020047), Jan 13, 2002: WARNING SYSTEM. MALFUNCTIONED. LEFT WING BODY OVERHEAT LIGHT ON IN FLT. DIVERTED TO MCO. REPAIRING OVERHEAT SYSTEM. TRIED CONTROLLER AND OVERHEAD PANEL, NO HELP. RE-INSTALLED ORIGINAL. INSPEC - [SDR DL73K011994](https://openairdocs.org/sdr/DL73K011994), Dec 28, 2001: SKIN. CRACKED. THE FWD LOWER CORNER OF THE AFT GALLEY DOOR OPENING WAS FOUND WITH A CRACK IN THE SKIN AND UNDERLYING BEAR STRAP. THE CRACK WAS REMOVED WITH A 1.5 INCH X 1.5 IN - [SDR DL73K011993](https://openairdocs.org/sdr/DL73K011993), Dec 28, 2001: SKIN. CRACKED. THE UPPER HINGE CUTOUT OF THE AFT ENTRY DOOR OPENING WAS FOUND WITH A SMALL CRACK IN THE BONDED SKIN ASSY. THE CRACK WAS REMOVED WITH A TRIM-OUT. THE DAMAGE WAS - [SDR DL73K011290](https://openairdocs.org/sdr/DL73K011290), Aug 6, 2001: FAN. UNSERVICEABLE. ON LANDING, COCKPIT FILLED WITH SMOKE, TURNED GASPER AND PACKS OFF. AT GATE DETERMINED SMOKE WAS COMING IN WHEN RT PACK WAS TURNED ON. CA FOUND CONTROL CABIN AI - [SDR DL73K011157](https://openairdocs.org/sdr/DL73K011157), Jul 12, 2001: PUMP. DEFECTIVE. HYD SYSTEM A PUMP 2/ LOW PRESSURE. REMOVED AND REPLACED RT EDP, REPLACED CASE DRAIN AND A SYS FILTERS SERV HYD, LEAK CKS GOOD. - [SDR DL73K011051](https://openairdocs.org/sdr/DL73K011051), Jun 24, 2001: CIRCUIT BREAKER. BURNED. SMOKE IN COCKPIT FOUND LEFT SIDE WINDOW ANTI-ICE C/B C392 AND C848 STANBY HYD PUMP ALTERNATE C/B BURNED - [SDR DL73K010667](https://openairdocs.org/sdr/DL73K010667), Apr 23, 2001: LIGHT. INOPERATIVE. 3 BULLNOSE EMERGENCY EXIT LIGHTS INOP C/A RELAMPED - [SDR DL73K002088](https://openairdocs.org/sdr/DL73K002088), Oct 23, 2000: FRAME. WORN. THE FS 440 FRAME HAS A WORN AREA AT THE FORWARD LOWER CORNER OF THE C1 DOORWAY. THE WEAR IS LOCATED ON THE VERTICAL WEB OF THE Z-FRAME. THE DAMAGE WAS BLENDED S - [SDR DL73K002066](https://openairdocs.org/sdr/DL73K002066), Oct 19, 2000: FLOORBEAM. CRACKED. CRACK INDICATIONS WERE FOUND ON THE BL 0.07 LONGITUDINAL FLOORBEAM BETWEEN FS 700 AND FS 717. THE CRACKS WERE REMOVED AND REPAIRED SIMILIAR TO THAT OF B737 S/B - [SDR DL73K002065](https://openairdocs.org/sdr/DL73K002065), Oct 19, 2000: FLOORBEAM. CORRODED. THE FS 294 FLOORBEAM WAS CORRODED ON THE UPPER CAP AT LBL 10 AND RBL 49. REPAIRED PER ERA 396233-14AD AT HMV. - [SDR DL73K002062](https://openairdocs.org/sdr/DL73K002062), Oct 19, 2000: FRAME. CRACKED. THE FS 400 RT SIDE FRAME WAS FOUND CRACKED IN THE SKIN ATTACH FLANGE IN THE BEND RADIUS ADJACENT TO THE FIRST FASTENER ABOVE STR 14R. THE DAMAGE WAS TRIMMED OUT - [SDR DL73K002057](https://openairdocs.org/sdr/DL73K002057), Oct 19, 2000: ATTACH FITTING. CORRODED. THE RT AND LT HORIZONTAL STABILIZER ATTACH FITTINGS WERE FOUND CORRODED. MATERIAL WAS REMOVED FROM THE FACES AND THE BORES WERE OVERSIZED TO REMOVE CORROSION. T - [SDR DL73K002056](https://openairdocs.org/sdr/DL73K002056), Oct 19, 2000: FITTING. CORRODED. THE RT HORIZONTAL STABILIZER CLEVIS LUG WAS FOUND CORRODED THE BORES WERE OVERSIZED AND SOME LOCAL BLENDED WAS APPLIED TO THE FACES PER ERA 396224-14 AT HMV. - [SDR DL73K002055](https://openairdocs.org/sdr/DL73K002055), Oct 19, 2000: FITTING. CORRODED. CORROSION WAS FOUND ON MULTIPLE LUGS ON THE VERTICAL STABILIZER ATTACHMENT LUGS AND FUSELAGE ATTACH LUGS. ALL CORROSION WAS REMOVED AND REPAIRED PER ERA 396259- - [SDR DL73K002053](https://openairdocs.org/sdr/DL73K002053), Oct 19, 2000: FRAME. CORRODED. CORROSION WAS FOUND ON THE INBOARD CHORD OF THE FS 500B FRAME AT STR 25R. THE DAMAGE WAS REMOVED AND A FACTORY SPLICE EXTENDED TO REPAIR THE DAMAGE. THE DAMAGE - [SDR DL73K001895](https://openairdocs.org/sdr/DL73K001895), Sep 26, 2000: SKIN. DAMAGED. SKIN AT AFT GALLEY DOOR LWR HINGE CUTOUT CRACKED. DAMAGE IS TRIMMED OUT AND REPAIRED. ER/A 300224-14 REV.A - [SDR DL73K001865](https://openairdocs.org/sdr/DL73K001865), Sep 25, 2000: FLOORBEAM. CORRODED. STA 328 FLOORBEAM - PREVIOUS REPAIR CORROSION ON SURFACE TASK NR C53-107-02 OPN 58101AD NRC 416. FLOORBEAM REPAIRED PER SRM 53-10-9 FIG 9. - [SDR DL73K001917](https://openairdocs.org/sdr/DL73K001917), Sep 20, 2000: FLOORBEAM. CORRODED. STA 328 FLOORBEAM PREVIOUS REPAIR CORROSION ON SURFACE, TASK NR C53-107-02. REMOVED FASTENERS. TRIMMED BEAM AND PICKED UP HOLES. TREATED AND PAINTED PER SRM 53- - [SDR DL73K000705](https://openairdocs.org/sdr/DL73K000705), Apr 13, 2000: SKIN. CRACKED. THE FUSELAGE SKIN ASSY BELOW THE L1 DOOR CUTOUT LOWER SILL NEAR THE AFT CORNER WAS FOUND WITH A 1 INCH CRACK. THE CRACK IS TYPICAL OF BAC S/B 737-53-1083. THE C - [SDR DL73K000255](https://openairdocs.org/sdr/DL73K000255), Feb 3, 2000: FITTING. CORRODED. THE LT & RT MAIN LANDING GEARS SIDE STRUT SUPPORT FITTING LUGS AT FS 685 WERE FOUND WITH CORROSION IN THE LUG BORES AND ON THE LUG FACES. THE CORROSION WAS REMO - [SDR DL73K992329](https://openairdocs.org/sdr/DL73K992329), Oct 22, 1999: POWER SUPPLY. INOP. AT DEPARTURE TIME, EMERGENCY LIGHTS ROWS 1 THRU 16 WOULD NOT TURN OFF. REPLACED POWER SUPPLY AND BATTERY LIGHTS OPERATION NORMAL. - [SDR DL73K991589](https://openairdocs.org/sdr/DL73K991589), Jul 15, 1999: VALVE. FAILED. ENGINE OIL TEMP WAS IN THE YELLOW ZONE AROUND 150 DEG C FOR 15 MINUTES. WHEN THE ENGINE WAS IN IDLE THE TEMP WENT UP TO THE RED LINE. REPLACED NR 1 ENGINE FUEL - [SDR DL73K991432](https://openairdocs.org/sdr/DL73K991432), Jun 23, 1999: SKIN. CRACKED. THE FUSELAGE SKIN WAS FOUND WITH A 2 INCH CRACK AT FS 750 AND STRINGER 19R. THE CRACK WAS ROUTED OUT OF THE SKIN AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER. - [SDR DL73K990795](https://openairdocs.org/sdr/DL73K990795), Apr 11, 1999: VALVE. STUCK. NR 1 ENG OIL TEMP IN YELLOW BAND. ENG FUEL HEAT VLV STUCK IN THE OPEN POSITION. SHUT DOWN ENG AS PRECAUTIONARY. FLIGHT DIVERTED INTO CAE. VLV DEFERRED PER MEL. - [SDR DL73K990233](https://openairdocs.org/sdr/DL73K990233), Feb 1, 1999: SKIN. CRACKED. THE FUSELAGE SKIN WAS FOUND WITH A 1 INCH LONG CRACK JUST ABOVE STRINGER 16R AT FS 522. THE CRACK WAS ROUTED OUT AND A REPAIR DOUBLER INSTALLED PER B737 SRM 53- - [SDR DL73K982285](https://openairdocs.org/sdr/DL73K982285), Nov 6, 1998: MODULE. FAILED. COCKPIT FIRE CONTROL PANEL SHORTED. POPPING NOISE COMING FROM PEDESTAL AREA. REMOVED AND REPLACED ENG/APU FIRE CONTROL MODULE. All 74: https://openairdocs.org/deregistered/N311DL-2007-01-26/reports.md ## FAA accident and incident reports (7) 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 20041019027399I](https://openairdocs.org/incident/20041019027399I), Oct 19, 2004: Boeing 737232 (N311DL), Kansas City, MO. (-23) On takeoff out of mci at rotation the flight crew heard a loud bang - epr rolled back, EGT entered yellow, then the engine indications returned to normal… - [Incident 19960713026839I](https://openairdocs.org/incident/19960713026839I), Jul 13, 1996: Boeing 737232 (N311DL), Salt Lake City, UT. Narrative: on July 13, 1996, aircraft N311DL, delta flight #977, departed slc enroute to oma. During climb out, the APU master fire warning illuminated. Crew… - [Incident 19951019037259I](https://openairdocs.org/incident/19951019037259I), Oct 19, 1995: Boeing 737200 (N311DL), Houston, TX, Minor damage. Narrative: seat back on passenger seat 24 b&c fell into seat row 25 during climbout from Houston inter Continental airport, causing minor knee injuries to 41… - [Incident 19930515017509I](https://openairdocs.org/incident/19930515017509I), May 15, 1993: Boeing 737232 (N311DL), Great Falls, MT, Minor damage. Experienced several bird strikes on descent. Landed safely. - [Incident 19920409012039I](https://openairdocs.org/incident/19920409012039I), Apr 9, 1992: Boeing 737232 (N311DL), Covington - Cin, OH. Stabilizer up warning horn sounded on takeoff. Aborted. Replaced stabilizer up takeoff warning limit switch. - [Incident 19911230062559I](https://openairdocs.org/incident/19911230062559I), Dec 30, 1991: Boeing 737232 (N311DL), Los Angeles, CA, Minor damage. Aircraft struck a runway advisory sign during a maintenance taxi test. Mechanics failed to control the aircraft. - [Incident 19910210005309I](https://openairdocs.org/incident/19910210005309I), Feb 10, 1991: Boeing 737232 (N311DL), Reno, NV, Minor damage. Nose steering and rudder inoperative when turn was attempted. A failed recapped tire had damaged hydraulic system. --- 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.