# N239TA: 1987 Boeing 737-25A, registration cancelled 2005-02-16 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: February 16, 2005 - Exported to: Peru - Status when cancelled: Valid registration - Airframe: [Boeing 737-25A](https://openairdocs.org/model/boeing-737-25a) (registry code 1384481) - Engine: [Pratt & Whitney JT8D-17 series](https://openairdocs.org/engine/pratt-whitney-jt8d-17-series) (registry code 52049) - Data sheets: [TCDS E2EA](https://openairdocs.org/tcds/E2EA) (OpenAirDocs) - Serial number: 23789 - Year built: 1987 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-jet - Airworthiness: Standard, transport - Airworthiness date: June 8, 1987 - Certificate issued: November 21, 2002 - Last registry action: November 21, 2002 - Mode S code: A22B99 - Owner when cancelled: [Art 23789 LLC](https://openairdocs.org/faa-owner/ART%2023789%20LLC) - Location: [San Francisco, CA](https://openairdocs.org/faa-place/CA/San%20Francisco) - Owner type: Corporation - Owner's area on the map: 37.7984° N, 122.3992° W: Placed by OpenAirDocs at the center of ZIP code 94111, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N239TA - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=239TA - Page: https://openairdocs.org/deregistered/N239TA-2005-02-16 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 737-25A: https://openairdocs.org/model/boeing-737-25a.md ## Service difficulty reports (39) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR P2EA2002M040](https://openairdocs.org/sdr/P2EA2002M040), Jun 12, 2002: ACOUSTIC PANEL. GOUGED. ON WALKAROUND, FOUND THE NR 2 ENGINE TAIL PIPE EXTENSION WITH GOUGE IN ACOUSTIC PANEL 4 INCHES LONG, .0625 INCH WIDE AND .5 INCH DEEP. WELD GOUGE ACCORDING TO M - [SDR P2EA2002V0032](https://openairdocs.org/sdr/P2EA2002V0032), Apr 6, 2002: LINK. LOOSE. DURING EVALUATION FLIGHT AFTER Q1 AND Q2 INSPECTION, NR 1 ENGINE OIL QUANTITY STARTED DECREASING AFTER TAKEOFF, ENGINE NR 1 SHUTDOWN UPON TOUCHDOWN WITH 0.750 G - [SDR P2EA2002V0020](https://openairdocs.org/sdr/P2EA2002V0020), Mar 9, 2002: SKIN. -During Q1+Q2 inspection.-IMPROPER REPAIR LOCATED AT BS 1000 STR 14L.-Existing repair replaced IAW E.O. No.B737HC53-022/02, Dated March 15, 2002, approved with - [SDR P2EA2002V0026](https://openairdocs.org/sdr/P2EA2002V0026), Mar 3, 2002: -DURING Q1 AND Q2 INSPECTION:-RUDDER STA 85 SKIN WITH DENT-REPAIRED IAW EO B737HC57-051/02. APPROVED 8110-3 DTD 03-06-02 BY FAA DER ROBERT MANASHI (DERT-71067-S - [SDR P2EA2002V0021](https://openairdocs.org/sdr/P2EA2002V0021), Feb 21, 2002: SKIN. -During Q1+Q2 inspection.-IMPROPER REPAIR LOCATED AT BS 259 STR 19L.-Existing repair replaced IAW E.O. No.B737HC53-023/02, Dated March 15, 2002, approved with F - [SDR P2EA2002V0029](https://openairdocs.org/sdr/P2EA2002V0029), Feb 20, 2002: BEAM. CORRODED. DURING Q1 AND Q2 INSPECTION, RT HORIZONTAL STABILIZER LWR AREA T/E BEAM WITH CORROSION BETWEEN ELEV STA 94.07 AND ELEV STA 100. RT HORIZONTAL STABILIZER LWR ARE - [SDR P2EA2002V0028](https://openairdocs.org/sdr/P2EA2002V0028), Feb 20, 2002: STRINGER. CORRODED. DURING Q1 AND Q2 INSPECTION, BETWEEN BS 967 AND BS 986.5 STR 23L WITH CORROSION. STRINGER REPAIRED IAW SRM 53-10-3 FIG 1. - [SDR P2EA2002V0027](https://openairdocs.org/sdr/P2EA2002V0027), Feb 20, 2002: SPAR. DELAMINATED. DURING Q1 AND Q2 INSPECTION, LT WING AILERON FRONT SPAR LOWER CHORD WITH DELAMINATION SPOTS BETWEEN WBL 417.250 AND WBL 251.8. REPAIRED IAW EO B737HC57-008/02 A - [SDR P2EA2002V0025](https://openairdocs.org/sdr/P2EA2002V0025), Feb 20, 2002: AILERON. DELAMINATED. RIGHT WING AILERON DELAMINATED BETWEEN WBL 417 AND WBL 446. REPAIRED IAW EO B737HC57-007/02 APPROVED 8110-3 FORM BY FAA. - [SDR P2EA2002V0024](https://openairdocs.org/sdr/P2EA2002V0024), Feb 20, 2002: -During Q1+Q2 inspection.-L-H WING IMB. FORE FLAP WITH UPPER SKIN DELAMINATED.-Repaired IAW E.O. No. B737HC57-006/02, DATED Feb 27, 2002 approved with FAA 8110- - [SDR P2EA2002V0023](https://openairdocs.org/sdr/P2EA2002V0023), Feb 20, 2002: -During Q1+Q2 inspection.-RH WING AILERON TAB BROKEN NEAR INBD AND OUTBD CENTER HINGE ASSEMBLY.-Repaired cracks IAW E.O. No. B737HC57-012/02, DATED March 08, 20 - [SDR P2EA2002V0022](https://openairdocs.org/sdr/P2EA2002V0022), Feb 20, 2002: FITTING. -During Q1+Q2 inspection.-VERTICAL STABILIZER SUPPORT FITTING WITH CRACK AT REAR SPAR CAVITY FIN STA 90.3.-Rudder support fitting repaired IAW E.O. No. B737HC55 - [SDR P2EA2002V0014](https://openairdocs.org/sdr/P2EA2002V0014), Feb 19, 2002: FRAME. -During Q1+Q2 inspection.-FWD CARGO COMPARTMENT AT BS 492.4 ATR 24R FRAME WITH CRACK.-Frame repaired IAW SRM 51-40-3, Fig 1.Note: See Aeroman W/O No. 2002-90/1, - [SDR P2EA2002V0013](https://openairdocs.org/sdr/P2EA2002V0013), Feb 19, 2002: FRAME. BENT. DURING Q1+ Q2 INSPECTION, FWD CARGO COMPARTMENT BS 420 STR 24L FRAME BENT. FRAME REPAIRED IAW SRM 51-40-3 FIG 1. - [SDR P2EA2002V0030](https://openairdocs.org/sdr/P2EA2002V0030), Feb 19, 2002: SEAT TRACK. -DURING Q1 AND Q2 INSPECTION:-PAX CABIN BS 380 AND RBL 45.5 SEAT TRACK WITH CORROSION -SEAT TRACK REPAIRED IAW SRM 53-10-5 FIG. 2-NOTE: SEE AEROMAN W/O No. 2002 - [SDR P2EA2002V018](https://openairdocs.org/sdr/P2EA2002V018), Feb 19, 2002: ANGLE. CRACKED. DURING Q1+Q2 INSPECTION, MAIN PASSENGER CABIN FLOOR AREA AT STA 520 FLOOR ANGLE CRACKED. FLOOR ANGLE REPAIRED IAW SRM 51-40-4 FIG 1 DETAIL 5. - [SDR P2EA2002V0009](https://openairdocs.org/sdr/P2EA2002V0009), Feb 19, 2002: FLOORBEAM. CORRODED. DURING Q1+Q2 INSPECTION, PAX CABIN RBL 12 BS 360 FLOORBEAM WITH CORROSION. FLOORBEAM REPAIRED IAW SRM 53-10-9 FIG 1. - [SDR P2EA2000V0008](https://openairdocs.org/sdr/P2EA2000V0008), Feb 19, 2002: FLOORBEAM. CORRODED. DURING Q1+Q2 INSPECTION, AFT GALLEY AREA BS 1016 LBL 33 FLOORBEAM WITH CORROSION. FLOORBEAM REPAIRED IAW EO B737MC53-019/02, BOEING SL 737-SL-53-036 AND DWG NR - [SDR P2EA2002V0007](https://openairdocs.org/sdr/P2EA2002V0007), Feb 19, 2002: FLOORBEAM. CORRODED. DURING Q1+Q2 INSPECTION, PAX CABIN BS 294.5 FLOORBEAM UPPER CHORD LWR SURFACE WITH CORROSION RBL 24. FLOORBEAM REPAIRED IAW SRM 53-10-9 FIG 6. - [SDR P2EA2000V0003](https://openairdocs.org/sdr/P2EA2000V0003), Feb 19, 2002: FLOORBEAM. CORRODED. DURING Q1+Q2 INSPECTION, PASSENGER CABIN FLOORBEAM WITH CORROSION AT BS 344 BTW LBL 14 AND LBL 21. FLOORBEAM REPAIRED IAW SRM 53-10-9, FIG 5. - [SDR P2EA2002V0002](https://openairdocs.org/sdr/P2EA2002V0002), Feb 19, 2002: FLOORBEAM. CORRODED. DURING Q1+Q2 INSPECTION, PAX CABIN FLOORBEAM UPPER CHORD WITH CORROSION AT BS 947.5 BETWEEN LBL 5 AND RBL 5. FLOORBEAM REPAIRED IAW SRM 53-10-9 FIG 2. - [SDR P2EA2002V0001](https://openairdocs.org/sdr/P2EA2002V0001), Feb 19, 2002: FLOORBEAM. SCRATCHED. DURING Q1+Q2 INSPECTION, PAX CABIN AT BS 380 BETWEEN RBL 24.5 AND RBL 45.5 FLOORBEAM UPPER CHORD WITH SCRATCH. SCRATCH REPAIRED IAW SRM 53-10-9 FIG 1. - [SDR P2EA2002V0016](https://openairdocs.org/sdr/P2EA2002V0016), Feb 18, 2002: STRINGER. -During Q1+Q2 inspection.-INTERNAL FUSELAGE STR 16L WITH CRACK BTW BS 520 AND SCANNING LIGHT BASE.-Scaqnning ligth base at Str 16L-H repaired IAW E.O. No. B737M - [SDR P2EA2002V0015](https://openairdocs.org/sdr/P2EA2002V0015), Feb 18, 2002: STRINGER. -During Q1+Q2 inspection.-INTERNAL FUSELAGE STR 16R WITH CRACK BTW BS 520 AND SCANNING LIGHT BASE.-Scaqnning ligth base at Str 16R-H repaired IAW E.O. No. B737M - [SDR P2EA2002V0012](https://openairdocs.org/sdr/P2EA2002V0012), Feb 18, 2002: FRAME. -During Q1+Q2 inspection.-BS 420 AT STR 26LH FRAME WITH CRACK.-Frame upper flange repaired IAW SRM 51-40-3, Fig1.Note: See Aeroman W/O No. 2002-90/1, VAM100 No. - [SDR P2EA2002V0011](https://openairdocs.org/sdr/P2EA2002V0011), Feb 18, 2002: FRAME. -During Q1+Q2 inspection.-BS 460 AT STR 26LH FRAME WITH CRACK.-Frame repaired IAW SRM 51-40-3, Fig 1.Note: See Aeroman W/O No. 2002-90/1, VAM100 No.073, SDA No. - [SDR 2PEA2002V0017](https://openairdocs.org/sdr/2PEA2002V0017), Feb 18, 2002: -During Q1+Q2 inspection.-RIGHT WING FORE FLAP EXISTING REPAIR FROM WBL227 TO 254 FOUND WITH GOUGE.-Doubler of existing repair replaced IAW SRM 51-10-1, Fig 1, - [SDR P2EA2002V0006](https://openairdocs.org/sdr/P2EA2002V0006), Feb 18, 2002: FLOORBEAM. CORRODED. DURING Q1+Q2 INSPECTION, PASSENGER CABIN FLOORBEAM WITH CORROSION AT BS 294.5 BL 0. FLOORBEAM REPAIRED IAW SRM 53-10-9 FIG 5. - [SDR P2EA2002V0005](https://openairdocs.org/sdr/P2EA2002V0005), Feb 18, 2002: FLOORBEAM. CORRODED. DURING Q1+Q2 INSPECTION, PASSENGER CABIN FLOORBEAM WITH CORROSION AT BS 312 AND LBL 8. FLOORBEAM REPAIRED IAW SRM 53-10-9 FIG 5. - [SDR P2EA2002V0004](https://openairdocs.org/sdr/P2EA2002V0004), Feb 18, 2002: FLOORBEAM. CORRODED. DURING Q1+Q2 INSPECTION, PASSENGER CABIN FLOORBEAM WITH CORROSION AT BS 328 AND LBL 28. FLOORBEAM REPAIRED IAW SRM 53-10-9 FIG 6. - [SDR P2EA2002V0010](https://openairdocs.org/sdr/P2EA2002V0010), Feb 17, 2002: FLOORBEAM. CRACKED. DURING Q1+Q2 INSPECTION, LONGITUDINAL FLOORBEAM AT BL 0, BS 663 UPPER CHORD CRACKED. LONGITUDINAL FLOORBEAM REPAIRED IAW EO B737MC57-010/02, S/B 737-57-1210. - [SDR P2EA2002V0019](https://openairdocs.org/sdr/P2EA2002V0019), Feb 15, 2002: -During Q1+Q2 inspection.-RH WING FORE FLAP AT WSL 479 LOWER SURFACE WITH SEVERAL GOUGES.-R-H wing Fore flap repaired IAW SRM 57-40-4, Fig 1.Note: See Aeroman W - [SDR P2EA2002V0031](https://openairdocs.org/sdr/P2EA2002V0031), Feb 14, 2002: SKIN. DURING Q1 AND Q2 INSPECTION:-E/E COMPARTMENT DOOR WITH NICK ON SKIN EDGES STA 325.18-NICK REPAIRED IAW SRM 737-200 52-00-3 FIG.5-NOTE: SEE AEROMAN W/O No. 2002- - [SDR P2EA2002M006](https://openairdocs.org/sdr/P2EA2002M006), Feb 10, 2002: CLAMP. LOOSE. APU FIRE LIGHT CAME ON IN FLIGHT. FIRE HANDLE PULLED AND FIRE BOTTLE DISCHARGED. LIGHT WENT OUT AFTER 10 MINUTES. FOUND AN APU BLEED AIR DUCT WITH LOOSE CLAMP T - [SDR P2EA2002M004](https://openairdocs.org/sdr/P2EA2002M004), Feb 3, 2002: FIRE DETECTOR. MALFUNCTIONED. PRIOR TO PUSH BACK, APU SHUT DOWN, LATER THE APU FIRE WARNING AND BELL ILLUMINATED. PERFORMED APU FIRE CHECK LIST PROCEDURES PULLED AND ROTATED HANDLE. PERFORME - [SDR P2EA2001M0017](https://openairdocs.org/sdr/P2EA2001M0017), Dec 21, 2001: CONTROLLER. FAULTY. NR 2 ENGINE STALLED THREE TIMES DURING TAXI, ALSO NR 2 EPR STICKING. REMOVED AND REPLACED PRBC IAW MM 75-31-11. REMOVED AND REPLACED EPR TRANSMITTER IAW 77-11-0 - [SDR P2EA2001M0014](https://openairdocs.org/sdr/P2EA2001M0014), Dec 5, 2001: CSD. MALFUNCTIONED. NR 1 ENGINE CSD LOW OIL PRESSURE LIGHT WOULD NOT EXTINGUISH AFTER ENGINE START. AIRCRAFT RETURNED TO BLOCKS WITH NO INCIDENT. RESET NR 1 ENGINE CSD T-HANDLE. OP - [SDR P2EA2001M0010](https://openairdocs.org/sdr/P2EA2001M0010), Nov 10, 2001: START VALVE. FAILED. NR 1 ENGINE START VALVE WOULD NOT OPEN. AIRCRAFT RETURNED TO GATE. REMOVED AND REPLACED START VALVE IAW MM 80-11-21. OPERATIONAL CHECK NORMAL. - [SDR P2EA2001M0001](https://openairdocs.org/sdr/P2EA2001M0001), Sep 23, 2001: CONNECTOR. DIRTY. AIR-CONDITION AND MASTER CAUTION ON PRE-TAKEOFF RECALL WITH NO ASSOCIATED PANEL INDICATION. RETURNED TO GATE. SUSPECTED APU BLEED VALVE. OP'S CHECKED, GOT DUAL ## Other aircraft with N239TA - [Registered now](https://openairdocs.org/aircraft/N239TA): Textron 172S, S/N 172S13613 - [Cancelled 2020-07-22](https://openairdocs.org/deregistered/N239TA-2020-07-22): Costruzioni Aeronautiche Tecna P92 EAGLET, S/N 1429. Sale reported, canceled. Owner: [Farmingdale, NY](https://openairdocs.org/faa-place/NY/Farmingdale) --- 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.