# N316DL: 1984 Boeing 737-232, registration cancelled 2007-08-06 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: August 6, 2007 - Exported to: Philippines - 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: 23088 - Year built: 1984 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-jet - Airworthiness: Standard, transport - Airworthiness date: April 5, 1984 - Certificate issued: October 6, 2005 - Last registry action: October 6, 2005 - Mode S code: A35D71 - Owner when cancelled: [Jetglobal LLC](https://openairdocs.org/faa-owner/JETGLOBAL%20LLC) - Location: [Chicago, IL](https://openairdocs.org/faa-place/IL/Chicago) - Owner type: Corporation - Owner's area on the map: 41.8947° N, 87.6151° W: Placed by OpenAirDocs at the center of ZIP code 60611, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N316DL - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=316DL - Page: https://openairdocs.org/deregistered/N316DL-2007-08-06 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 (46) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR DL73S050276](https://openairdocs.org/sdr/DL73S050276), May 17, 2005: ACTUATOR. STICKING. NR 2 ENGINE THRUST REVERSER UNLOCKED LIGHT ON DURING TAKEOFF ROLL. CLEANED LOWER ACTUATOR FOR STICKING. - [SDR DL73S041053](https://openairdocs.org/sdr/DL73S041053), Nov 20, 2004: SKIN. CRACKED. THE FUSELAGE SKIN AND UNDERLYING BEARSTRAP WERE FOUND CRACKED AT THE LOWER FWD CORNER OF THE R2 DOOR CUTOUT. THE CRACK WAS REMOVED WITH A 2.5 INCH CUTOUT IN THE - [SDR DL73S040503](https://openairdocs.org/sdr/DL73S040503), Jun 2, 2004: FRAME. CORRODED. FOUND ON W-2 LETTER CHECK CORROSION LOWER FRAME INBOARD OF STR 27L AT STA 1006. REPAIRED PER SRM 53-10-4 FIG 10. - [SDR DL73S040500](https://openairdocs.org/sdr/DL73S040500), Jun 2, 2004: STRINGER. CORRODED. FOUND ON W-2 LETTER CHECK STRINGER 27 LEFT CORRODED STA 967-1006. REPAIRED PER SRM 53-10-3 FIG 1. - [SDR DL73S040349](https://openairdocs.org/sdr/DL73S040349), Apr 17, 2004: POWER SUPPLY. FAILED. EMERGENCY INSEAT LIGHTING SEATS 21-24 INOP. REPLACED FUSE IN PWR SUPPLY M9013. CHECKS OK. - [SDR DL73S040197](https://openairdocs.org/sdr/DL73S040197), Feb 27, 2004: POWER SUPPLY. INOPERATIVE. EMERGENCY PATH LIGHTS AT ROWS 22-25D INOP. REMOVED AND REPLACED POWER SUPPLY. - [SDR DL73S030883](https://openairdocs.org/sdr/DL73S030883), Sep 28, 2003: CONTROL PANEL. SMOKE. PRIOR TO PUSHBACK FLT 1111 CREW SMELLED ELEC BURNING ODOR IN COCKPIT THEN NOTICED SMOKE COMING FRM F/O EYEBROW WINDOW AREA. FOUND SMOKE TO COMING FROM ENG/WING - [SDR DL73S030747](https://openairdocs.org/sdr/DL73S030747), Aug 12, 2003: WIRE. INOPERATIVE. SEAT MOUNTED EMERGENCY LIGHTS INOPERATIVE AT ROWS 18-21. REPAIRED WIRING NOW OPS, NORMAL. - [SDR DL73K011465](https://openairdocs.org/sdr/DL73K011465), Sep 1, 2001: WARNING SYSTEM. MALFUNCTIONED. UPON INITIAL T/O ROLL EWR, AUTOBRAKE DISARM LIGHT ILLUMINATED. CYCLED RTO SWITCH AND THE AUTOBRAKE LIGHT ILLUMINATED AGAIN. PERFORMED AUTOBRAKE TEST PER M/M. UN - [SDR DL73K011458](https://openairdocs.org/sdr/DL73K011458), Sep 1, 2001: AUTOTHRUST SYS. MALFUNCTIONED. T/O ROLL NOTICED ENGINE PARAMETERS FLUCTUATING. T/O ABORTED AUTOTHROTTLES WERE ENGAGED. MAINT OPERATED ENGS AT T/O PWR PER PFHB WITH OUT AUTOTHROTTLES ALL PARAM - [SDR DL73K011184](https://openairdocs.org/sdr/DL73K011184), Jul 17, 2001: AIR DUCT. LEAKING. FUMES IN CABIN AND COCKPIT. STRONGEST SMELL IN FIRST 5 ROWS OR SO. SMELLED LIKE RUBBER BURNING. NOTICED AT 2500 FT ABOUT 2 MINUTES AFTER DEPARTURE. FOUND GASPER - [SDR DL73K010678](https://openairdocs.org/sdr/DL73K010678), Apr 26, 2001: HEATER. FAULTY. A/C DIVERTED TO CHS.SMOKE /ELECTRICAL SMELL IN AFT LAV/GALLEY FOLLOWED POM. PULLED C/B SMELL DISIPATED. FOUND SOURCE TO BE AFT LAV WATER HEATER - [SDR DL73K010587](https://openairdocs.org/sdr/DL73K010587), Apr 10, 2001: STRINGER. CORRODED. CORROSION WAS FOUND ON STR 26 RT AT APPROXIMATLEY FS 500+12. THE AFTMOST END OF THE STRINGER WAS CUT OFF AND A NEW SECTION WAS SPLICED IN. THE CORROSION WAS FOU - [SDR DL73K010584](https://openairdocs.org/sdr/DL73K010584), Apr 9, 2001: FRAME. CORRODED. LOWER LOBE FRAME AT FS 500 WAS FOUND CORRODED AT THE INBD FLANGE BETWEEN STR 25R/26R. THE FLANGE WAS CUT OUT AND A REPAIR ANGLE INSTALLED. THE DAMAGE WAS FOUND - [SDR DL73K010583](https://openairdocs.org/sdr/DL73K010583), Apr 9, 2001: BULKHEAD. CORRODED. CORROSION WAS FOUND ON THE BS 1016 PRESSURE BULKHEAD WEB AT BL 0. REPAIR WAS ACCOMPLISHED PER S/B 737-53A1075. THE DAMAGE WAS FOUND DURING HMV. - [SDR DL73K010582](https://openairdocs.org/sdr/DL73K010582), Apr 9, 2001: SKIN. CORRODED. CORROSION WAS FOUND IN THE FUSELAGE SKIN AND BEAR STRAP AT FS 490 BETWEEN STR 27R/28R. THE DAMAGE WAS CUT OUT AND A REPAIR DOUBLER INSTALLED. THE DAMAGE WAS FOU - [SDR DL73K010556](https://openairdocs.org/sdr/DL73K010556), Apr 4, 2001: FRAME. CRACKED. A CRACK WAS FOUND IN THE FS 492 FRAME AT STR 24 RT IN THE FLANGE. THE LENGTH OF THE CRACK IS 2.05 INCHES. THE CRACK WAS CUTOUT AND A REPAIR WAS INSTALLED PER SR - [SDR DL73K010535](https://openairdocs.org/sdr/DL73K010535), Apr 2, 2001: STRAP. CRACKED. CRACKS WERE FOUND AT THE CUTOUT IN THE FUSELAGE FOR THE HORIZONTAL STABILIZER SIMILIAR TO THE TYPICAL CRACKS OF S/B 737-53-1134. CRACKS WERE FOUND IN THE LT & R - [SDR DL73K010534](https://openairdocs.org/sdr/DL73K010534), Apr 2, 2001: FITTING. CORRODED. CORROSION WAS FOUND ON THE LT AND RT HORIZONTAL STABILIZER ATTACH FITTINGS ON BOTH THE BORES AND FACES. THE CORROSION WAS REMOVED AND NEW BUSHINGS INSTALLED PER - [SDR DL73K010533](https://openairdocs.org/sdr/DL73K010533), Apr 2, 2001: FITTING. CORRODED. CORROSION WAS FOUND IN THE BORE AND FACES OF THE LT AND RT FUSELAGE CLEVIS LUGS FOR THE HORIZONTAL STABILIZER. THE CORROSION WAS REMOVED AND NEW BUSHINGS WERE I - [SDR DL73K010532](https://openairdocs.org/sdr/DL73K010532), Apr 2, 2001: FITTING. CORRODED. THE LT MLG STRUT SUPPORT FITTING FRAME INSTALLATION HAD CORROSION LOCATED IN THE BORE. THE FITTING IS LOCATED AT FS 695, LBL 68.5 AND WL 188.5. THE CORROSION WA - [SDR DL73K010519](https://openairdocs.org/sdr/DL73K010519), Mar 30, 2001: ATTACH FITTING. CORRODED. THE LT MLG STRUT SUPPORT FITTING FRAME AT FS 685 HAD CORROSION AT THE SIDE STRUT ATTACH LUG LOCATED AT LBL 68.5 AND WL 188.5. CORROSION WAS FOUND IN THE BORE AN - [SDR DL73K010500](https://openairdocs.org/sdr/DL73K010500), Mar 27, 2001: FITTING. CORRODED. CORROSION WAS FOUND IN A FASTENER HOLE OF THE UPPER ROW COMMON TO THE REAR SPAR UPPER CAP OF THE MLG SUPPORT BEAM O/B AFT FITTING. ANOTHER FASTENER HOLE WAS MIS - [SDR DL73K010460](https://openairdocs.org/sdr/DL73K010460), Mar 17, 2001: BEARING. WORN. WHILE PERFORMING JIC5957 FOUND PIVOT BEARING PLAY TO BE OUT OF LIMITS. IN THE PROCCESS OF REMOVING BEARING HOUSING FOUND SAFETY WIRE BROKEN AND KEEPER BACKED OF - [SDR DL73K002529](https://openairdocs.org/sdr/DL73K002529), Dec 25, 2000: ACCESSORY UNIT. FAILED. AT TOP OF DESCENT - ISOLATION VALVE LIGHT ILLUMINATED - THEN AFTER PLACING GEAR DOWN HAD NO GEAR LIGHTS RED OR GREEN. VISUALY CHECKED GEAR DOWN AND FOUND GEAR L - [SDR DL73K001144](https://openairdocs.org/sdr/DL73K001144), Jun 13, 2000: BEAM. CRACKED. A CRACK WAS FOUND IN THE RT S18A SHEAR BEAM WEB AT BS 727. SUBJECT CRACK IS TYPICAL OF THOSE DEPICTED IN S/B 737-53-1066. THE CRACK IS LOCATED AT THE AFT, I/B M - [SDR DL73K000586](https://openairdocs.org/sdr/DL73K000586), Mar 27, 2000: WIRE. PINCHED. ON L/O, FOUND AISLE EMERGENCY EXIT LIGHTS INOP FWD OF WING. REPAIRED WIRING. - [SDR DL73K991508](https://openairdocs.org/sdr/DL73K991508), Jul 3, 1999: BATTERY PACK. DISCHARGED. EMERGENCY LIGHTS AT ROWS 4, 6, 8 ABC OVERHEAD FAILED TO LIGHT ON TEST. REPLACED BATTERY PACK. - [SDR DL73K991445](https://openairdocs.org/sdr/DL73K991445), Jun 27, 1999: COFFEEMAKER. FAILED. AFT GALLEY NR 2 COFFEEMAKER WHEN TURNED ON CAUSES SMELL OF HOT ELEC WIRES. INSPECTED CANNON PLUG, CKS OK. REPLACED COFFEEMAKER. - [SDR DL73K990514](https://openairdocs.org/sdr/DL73K990514), Mar 11, 1999: LIGHTS. ODOR. 2L AFT GALLEY HAS ELECTRIC SMELL WHEN GALLEY LIGHTS ON. INSP AFT GALLEY FLUORESCENT LIGHTS AND WIRING, NO SIGNS OF BURNED WIRING. DEACTIVATED THRESHOLD AND WORK - [SDR DL73K990504](https://openairdocs.org/sdr/DL73K990504), Mar 10, 1999: COFFEEMAKER. MALFUNCTIONED. DISCONTINUED TAKEOFF DUE TO ELECTRICAL ODOR IN AFT GALLEY. F/A REPORTED C/B PANEL WARM TO TOUCH. TURNED OFF GALLEY PWR AND RETURNED TO GATE. INSPECTED AFT GALLE - [SDR DL73K982593](https://openairdocs.org/sdr/DL73K982593), Dec 16, 1998: FLOORBEAM. CRACKED. FUSELAGE OVERWING FLOORBEAM, UPPER CAP BL 0 FS 66, REPAIR FOR CRACKED CAP. THE OVERWING FLOORBEAM AT BL 0 WAS FOUND WITH A SEVERED UPPER CAP AT FS 662 WITH AN A - [SDR DL73K982268](https://openairdocs.org/sdr/DL73K982268), Nov 3, 1998: HINGE. CRACKED. THE LOWER GATE HINGE ON THE R1 DOOR WAS FOUND CRACKED. THE CRACKED HINGE WAS REMOVED AND REPLACED PER THE REQUIREMENTS OF BAC S/B 737-52A1124. THE REPAIR WAS DO - [SDR DL73K982264](https://openairdocs.org/sdr/DL73K982264), Nov 2, 1998: SKIN. CRACKED. THE FUSELAGE SKIN AT FS 740 WAS FOUND WITH A 1.25 INCH LONG CRACK BELOW STRINGER 18R. THE CRACK WAS REPAIRED PER THE B737-200 SRM 53-30-3 FIG 1. THE REPAIR DOUB - [SDR DL73K981793](https://openairdocs.org/sdr/DL73K981793), Aug 29, 1998: POWER SUPPLY. INOPERATIVE. MID PATH LIGHTS INOP. REPLACED POWER SUPPLY. - [SDR DL73K981358](https://openairdocs.org/sdr/DL73K981358), Jun 27, 1998: SKIN. CRACKED. THE SKIN ASSY AT THE LOWER FWD CORNER OF THE AFT ENTRY DOOR WAS FOUND WITH A TYPICAL CRACK THROUGH THE SKIN, DOUBLER, AND BEAR STRAP. THE CRACK WAS REPAIRED PER - [SDR DL73K980843](https://openairdocs.org/sdr/DL73K980843), Apr 18, 1998: FUSE. BLOWN. ON SERVICE CK DURING TEST OF EMERGENCY LIGHT SYTEM, FOUND AFT SECTION OF SEAT LIGHTS INOP. FOUND BLOWN FUSE ON PWR SUPPLY CKD FOR SHORTS, NONE FOUND. REPLACED P - [SDR DL73K970929](https://openairdocs.org/sdr/DL73K970929), May 15, 1997: FLOORBEAM. CORRODED. FLOORBEAM T-CAP FS 328 CORRODED AT LBL 27 AND FROM RBL12 TO RT SIDE OF FUSELAGE, C53-107-02. REMOVED ALL HARDWARE FROM DAMAGED BEAM SECTION. COMPLETED REMOVING - [SDR DL73K970902](https://openairdocs.org/sdr/DL73K970902), May 5, 1997: FLOORBEAM. CORRODED. AT MIDVISIT, THE FLOORBEAM T-CAP WAS FOUND TO BE CORRODED SEVERAL PLACES, LBL 7 TO RBL O/B END. THE CORROSION WAS REMOVED PER SRM 51-10-6, ALL OUT OF LIMITS EXC - [SDR DL73K970231](https://openairdocs.org/sdr/DL73K970231), Feb 6, 1997: SOLENOID. FAILED. ON OXYGEN SYSTEM TEST ROW 14ABC OXYGEN DOOR DID NOT OPEN. REPLACED DOOR LATCH ACTUATOR SOLENOID. - [SDR DL73K962459](https://openairdocs.org/sdr/DL73K962459), Oct 16, 1996: BULKHEAD. CRACKED. STATION 178 BULKHEAD WAS FOUND CRACKED IN SEVERAL LOCATIONS. DAMAGE CUTOUTS ARE 1 INCH X 2 INCH AT RBL 4, WL 200 AND WL 203, AND LBL 4, WL 200, AND A 1 INCH BY - [SDR DL73S961054](https://openairdocs.org/sdr/DL73S961054), May 2, 1996: WATER SEPARATOR. CONTAMINATED. AFTER TAKEOFF, CVG UNABLE TO PRESSURIZE. OUTFLOW VALVE WAS FULL, CLOSED BOTH BLEEDS, AND LT PACK WERE ON AS WAS ISOLATION VALVE. OPEN CBS WERE ALL IN CABIN CLIM - [SDR DL73S954724](https://openairdocs.org/sdr/DL73S954724), Dec 16, 1995: SKIN. CRACKED. THE R-2 DOOR HAS A 1.3 INCH CRACK AT THE LOWER AFT CORNER. IT WILL BE REPAIRED PER THE SRM WITH THE EXCEPTION OF BLIND FASTENER SUBSTITUTION TO FACILITATE MAINT - [SDR DL73S953871](https://openairdocs.org/sdr/DL73S953871), Oct 1, 1995: EEL BULB. FAILED. FOUND EMERGENCY AISLE LIGHT INOP AT 21ABC. RELAMPED, CKS GOOD. - [SDR DL73S953870](https://openairdocs.org/sdr/DL73S953870), Oct 1, 1995: EEL BATTERY PACK. DISCHARGED. EMERGENCY LIGHTS ON LEFT HAND AFT DOOR ARE INOP. REPLACED BATTERY PACK, CKS GOOD. - [SDR DL73S951971](https://openairdocs.org/sdr/DL73S951971), May 1, 1995: LE SKIN. DENTED. DURING SHOP INSPECTION, VERTICAL STABILIZER LEADING EDGE PANEL WAS REPAIRED FOR A DENT AT 51 INCHES FROM THE LOWER END OF PANEL. DAMAGE WAS REPAIRED PER SRM 55- ## 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 19930219020279I](https://openairdocs.org/incident/19930219020279I), Feb 19, 1993: Boeing 737232 (N316DL), San Jose, CA, Minor damage. Applied heavy brakes on rollout. Blew four main tires. Had departed with anti-skid and auto speedbrake inoperative. --- 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.