# N314DA: Boeing 737-232, registration cancelled 2022-03-05 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: March 5, 2022 - Status when cancelled: Registration expired, pending cancellation - 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: 23086 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-jet - Airworthiness: Standard, transport - Airworthiness date: March 15, 1984 - Certificate issued: November 27, 2018 - Last registry action: November 27, 2018 - Mode S code: A355F9 - Owner when cancelled: [First Class Air Support Inc](https://openairdocs.org/faa-owner/FIRST%20CLASS%20AIR%20SUPPORT%20INC) - Location: [Louisville, KY](https://openairdocs.org/faa-place/KY/Louisville) - Owner type: Corporation - Owner's area on the map: 38.1517° N, 85.5172° W: Placed by OpenAirDocs at the center of ZIP code 40299, within about 4 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N314DA - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=314DA - Page: https://openairdocs.org/deregistered/N314DA-2022-03-05 From the FAA registry file of November 5, 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 (30) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR DL73S060261](https://openairdocs.org/sdr/DL73S060261), Apr 6, 2006: LAP JOINT. CRACKED. THE FUSELAGE SKIN HAS 3 CRACKS IN THE LAP JOINT AT S-10R, BS 500-500A. THE CRACKED SKIN WAS REMOVED AND A REPAIR DOUBLER WAS INSTALLED. - [SDR DL73S060259](https://openairdocs.org/sdr/DL73S060259), Apr 6, 2006: LAP JOINT. CRACKED. FIVE CRACKS WERE FOUND IN THE FUSELAGE LAP JOINT AT S14L BETWEEN BS 480-500A. THE DAMAGED SKIN WAS REMOVED AND A REPAIR DOUBLER WAS INSTALLED. - [SDR DL73S050527](https://openairdocs.org/sdr/DL73S050527), Sep 8, 2005: SKIN. CRACKED. THE FUSELAGE SKIN WAS FOUND WITH A CRACK JUST ABOVE THE BONDED DOUBLER MILL LINE OF STRINGER 16R AT FS 525. THE CRACK WAS 1 INCH LONG AND TYPICAL OF THOSE DOCUM - [SDR DL73S050032](https://openairdocs.org/sdr/DL73S050032), Jan 14, 2005: PROXIMITY SWITCH. OUT OF ADJUST. SELECTED FLAPS AND L/E TRANSIT AMBER LIGHT ILLUMINATED. CONFIRMED BY L/E AMBER LIGHTT ON OVERHEAD PNL. FOLLOWED QRH PROCEDURES AND PLANNED FLAP 15 LANDING. ON S - [SDR DL73S040932](https://openairdocs.org/sdr/DL73S040932), Sep 27, 2004: SKIN. CRACKED. THE FUSELAGE SKIN AT THE L1 DOOR OPENING WAS FOUND CRACKED AT THE CUTOUT EDGE JUST ABOVE THE LOWER AFT CORNER. THE CRACKS WERE SMALL AND TYPICAL OF BAC S/B 737- - [SDR DL73S040931](https://openairdocs.org/sdr/DL73S040931), Sep 27, 2004: DOOR FRAME. CRACKED. INSPECTION OF THE C2 DOOR OPENING FRAME AT FS 794 PER AD 93-14-10 REVEALED CRACK IN THE DOOR FRAME WEB AND FLANGE JUST BELOW THE NR 5 DOOR STOP FITTING. THE CRA - [SDR DL73S040883](https://openairdocs.org/sdr/DL73S040883), Sep 15, 2004: SKIN. CRACKED. INSPECTION OF THE STRINGER 4L SKIN LAP JOINT PER AD 2003- 08-15 REVEALED A CRACK INDICATION IN A FASTENER HOLE AT FS 690. THE CRACKED AREA WAS REMOVED WITH A SK - [SDR DL73S030530](https://openairdocs.org/sdr/DL73S030530), Jun 6, 2003: FITTING. GOUGED. THE UPPER ATTACH LUG OF THE HORIZONTAL STABILIZER CENTER SECTION WAS FOUND WITH A GOUGE FROM INTERFERENCED WITH AN IMPROPERLY INSTALLED FASTENER ON ADJACENT STR - [SDR DL73S030520](https://openairdocs.org/sdr/DL73S030520), Jun 6, 2003: SKIN. CRACKED. THE FUSELAGE SKIN AT FS 750 WAS FOUND WITH A 2 INCH CRACK RUNNING ALONG THE EDGE OF THE BONDED DOUBLER AT STRINGER 18R. THE CRACK WAS CUTOUT OF THE SKIN AND REP - [SDR DL73S030113](https://openairdocs.org/sdr/DL73S030113), Jan 29, 2003: BULKHEAD. CANNING. INSPECTION OF THE AFT P-DOME REVEALED A 10 X 8 X .25 INCH OIL CAN IN THE LOWER WEB AREA OF NEAR BL 0. THE OIL CAN WAS REMOVED WITH A CUTOUT AND REPAIRED WITH AN - [SDR DL73K020573](https://openairdocs.org/sdr/DL73K020573), May 20, 2002: TEE FITTING. CRACKED. IRREG/ LOSS OF A SYSTEM HYDRAULIC QUANTITY FOLLOWED BY A LOSS OF PRESSURE AFTER LOWERING THE LANDING GEAR CA/ FOUND TEE FITTING IN THE NOSE WHEEL WELL CRACKED _ - [SDR DL73K011885](https://openairdocs.org/sdr/DL73K011885), Dec 2, 2001: COMPRESSOR. STALLED. IR - COMPRESSOR STALL NR 1 ENG ON TAKE TAKE OFF. INITIATED ABORT BETWEEN 70-80 KTS. DEAD HEATING CAPT REPORTED BRIGHT FLASH FROM NR 1 ENG SHORTLY AFTER T/O PWR - [SDR DL73K011673](https://openairdocs.org/sdr/DL73K011673), Oct 16, 2001: FRAME. CRACKED. 1" CRACK IN R-2 DOOR CUTOUT FRAME, JUST BELOW UPPER FWD. ROLLER CASTING REMOVE & REPLACE FRAME SECTION PER DRAWING - [SDR DL73K010311](https://openairdocs.org/sdr/DL73K010311), Feb 21, 2001: LIGHT. INTERMITTENT. ON LANDING GEAR EXTENSION, RT MAIN LANDING GEAR GREEN LIGHT DID NOT ILLUMINATE. BULB CK WAS GOOD. CYCLED GEAR WITH SAME INDICATION. PUSHED LIGHT ASSY SEVERAL TI - [SDR DL73K010292](https://openairdocs.org/sdr/DL73K010292), Feb 18, 2001: FAN. FAULTY. SMOKE AND FUMES IN COCKPIT DURING PREFLIGHT. FOUND CONTROL CABIN AUGMENTATION FAN PUTTING FUMES INTO COCKPIT. FWD TO MCO AND PLACARD. - [SDR DL73K002498](https://openairdocs.org/sdr/DL73K002498), Dec 22, 2000: SKIN. CORRODED. CORROSION WAS FOUND ON THE FUSELAGE SKIN AT STATION 887 AND 907 IN THE UPPER SKIN WHERE THE VERTICAL STABILIZER FAIRING ATTACHES AT ABOUT RBL 4 AND 5. THE MAXIM - [SDR DL73K002488](https://openairdocs.org/sdr/DL73K002488), Dec 21, 2000: FITTING. CORRODED. THE RT FUSELAGE CLEVIS LUGS ATTACHING THE HORIZONTAL STABILIZER WERE FOUND CORRODED ON THE FACES AND BORES. THE CORROSION WAS REMOVED AND NEW BUSHINGS WERE INST - [SDR DL73K002455](https://openairdocs.org/sdr/DL73K002455), Dec 15, 2000: FLOOR SUPPORT. CRACKED. CRACKS WERE FOUND IN THE WEB, DOUBLER AND UPPER CHORD OF THE LBL 24 LONGITUDINAL FLOOR SUPPORT AT FS 675. THE CRACKS WERE REMOVED AND THE DAMAGE REPAIRED PER ER - [SDR DL73K002218](https://openairdocs.org/sdr/DL73K002218), Nov 11, 2000: SKIN. CRACKED. THE FUSELAGE SKIN WAS FOUND WITH A 1 INCH CRACK NEAR FS 520 AND STRINGER 16L. THE CRACK WAS ROUTED OUT AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER B737 S - [SDR DL73K001485](https://openairdocs.org/sdr/DL73K001485), Aug 4, 2000: POWER SUPPLY. FAILED. EMERGENCY POWER SUPPLY WOULD NOT TEST AT ROWS 14, 15 DEF. REPLACED POWER SUPPLY. - [SDR DL73K992023](https://openairdocs.org/sdr/DL73K992023), Sep 11, 1999: FUSE. BLOWN. E-PATH LIGHTS INOP ROW 10 TO 18. REPLACED FUSE IN PWR SUPPLY. - [SDR DL73K990909](https://openairdocs.org/sdr/DL73K990909), Apr 23, 1999: SKIN. CRACKED. FUSELAGE AFT GALLEY DOOR CUTOUT SKIN UPPER HINGE CUTOUT, CRACK REPAIR. THE UPPER HINGE CUTOUT OF THE AFT GALLEY DOOR CUTOUT SKIN WAS FOUND WITH A .25 LONG TYPIC - [SDR DL73K990358](https://openairdocs.org/sdr/DL73K990358), Feb 23, 1999: BLADES. DAMAGED. AT CRUISE, CREW NOTE COMPRESSOR SURGING. DIVERTED TO BOS. FOUND NOSE BULLET LOOSE. DAMAGE INCURRED TO FIRST AND SECOND STAGE FAN BLADES, NOSE COWL ACCOUSTIC LIN - [SDR DL73K990345](https://openairdocs.org/sdr/DL73K990345), Feb 21, 1999: GCU. MALFUNCTIONED. ON CLIMBOUT, APU OFF BOTH GEN ON, RECEIVED A SPIKE. LOST ALL ELECTRICAL PWR IN COCKPIT AND CABIN FOR A SPLIT SECOND. NO C/B POPPED, NO EQUIP LOSS. INSPECTED LT - [SDR DL73K981505](https://openairdocs.org/sdr/DL73K981505), Jul 20, 1998: LINE. RUPTURED. LOSS OF A/B HYDRAULICS RESULTED IN DIVERSION BACK TO MCO. FOUND 01 ENG PRESS LINE RUPTURED. REPLACED SAME, LEAK CKS OK. REPLACED ALL CASE DRAIN FILTERS. - [SDR DL73K970080](https://openairdocs.org/sdr/DL73K970080), Jan 10, 1997: BULKHEAD WEB. CRACKED. DURING ACCOMPLISHMENT OF SI 3-69482-12, SEVEN CRACKS WERE DISCOVERED ON THE FORWARD FACE OF THE FS 178 BULKHEAD WEB. SEVEN INDEPENDENT CUTOUTS WERE REQUIRED TO - [SDR DL73K970041](https://openairdocs.org/sdr/DL73K970041), Jan 7, 1997: SKIN. CRACKED. A CRACK WAS FOUND IN THE FUSELAGE SKIN AT THE L2 DOOR CUTOUT IN THE UPPER AFT CORNER. THE CRACK WAS IN THE INNER LAYER OF THE BONDED SKIN ASSEMBLY AND WAS APPRO - [SDR DL73S961819](https://openairdocs.org/sdr/DL73S961819), Jul 23, 1996: SKIN. CRACKED. FOUND A 2.25 INCH CRACK IN THE R-2 DOORWAY. REPAIRED PER B737-200 SRM 53-30-3, FIG 24. - [SDR DL73S951630](https://openairdocs.org/sdr/DL73S951630), Mar 17, 1995: NOSE COWL. DAMAGED. DURING SHOP INSPECTION, A DEEP NICK WAS FOUND IN THE LEADING EDGE LIP OF NR 2 ENGINE NOSE COWL. REPAIRED PER SRM 54-30-3 FIG. 4. - [SDR DL73S951629](https://openairdocs.org/sdr/DL73S951629), Mar 17, 1995: NOSE COWL. CRACKED. DURING SHOP INSPECTION, A .5 INCH CRACK WAS FOUND IN THE LEADING EDGE LIP OF NR 2 NOSE COWL. REPAIRED PER SRM 54-30-3 FIG. 4. ## 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 20040509019759I](https://openairdocs.org/incident/20040509019759I), May 9, 2004: Boeing 737232 (N314DA), Albany, NY, Substantial damage. (-23) On 05/09/04, delta flight 650, N314DA aborted takeoff due to #2 engine failure. At approximately 1248 aircraft was cleared for t/o, during t/o roll crew… - [Incident 19930202003579I](https://openairdocs.org/incident/19930202003579I), Feb 2, 1993: Boeing 737232 (N314DA), Raleigh-Durham, NC. NR1 engine flamed out on descent. Unable to restart. Landed safely. Replaced pressurization seal on inlet line. --- 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.