N239TA, cancelled Feb 16, 2005

Service difficulty reports · 39

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE n_number = 'N239TA' AND deregistration_id = 'N239TA-2005-02-16'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR P2EA2002M040Acoustic Panel · gougedON 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 MM 78-38-43.Jun 12, 2002 · N239TA · Boeing 73725A · Engine Collector/Tailpipe/NozzleSDR P2EA2002V0032Link · looseDURING 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 GALS. PRESSURE LINK TIGHTENED AT OIL FILTER BYPASS SW IAW MM 20-50-11 PAGE 211, ENGINE OIL SERVICED Apr 6, 2002 · N239TA · Boeing 73725A · Engine Oil Storage (Airframe Furnished)SDR P2EA2002V0020Skin-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 FAA 8110-3 form submited by P.C.LeBar.Note: See Aeroman W/O No. 2002-90/1, VAM100 No.0715, SDA No. 2Mar 9, 2002 · N239TA · Boeing 73725A · Fuselage Main, Plate/SkinSDR P2EA2002V0026Service difficulty-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-SW)-NOTE: SEE AEROMAN W/O No. 2002-90/1, VAM100 0579, SDA 239SDA030Mar 3, 2002 · N239TA · Boeing 73725A · Vertical Stabilizer, Plate/SkinSDR P2EA2002V0021Skin-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 FAA 8110-3 form submited by B.R.Frakes.Note: See Aeroman W/O No. 2002-90/1, VAM100 No.0714, SDA No. 2Feb 21, 2002 · N239TA · Boeing 73725A · Fuselage Main, Plate/SkinSDR P2EA2002V0029Beam · corrodedDURING 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 AREA T/E BEAM REPAIRED IAW SRM 55-107 FIG 1.Feb 20, 2002 · N239TA · Boeing 73725A · Horizontal Stabilizer Miscellaneous StructureSDR P2EA2002V0028Stringer · corrodedDURING Q1 AND Q2 INSPECTION, BETWEEN BS 967 AND BS 986.5 STR 23L WITH CORROSION. STRINGER REPAIRED IAW SRM 53-10-3 FIG 1.Feb 20, 2002 · N239TA · Boeing 73725A · Fuselage Main, Longeron/StringerSDR P2EA2002V0027Spar · delaminatedDURING 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 APPROVED BY 8110-3 FORM BY FAA.Feb 20, 2002 · N239TA · Boeing 73725A · AileronsSDR P2EA2002V0025Aileron · delaminatedRIGHT WING AILERON DELAMINATED BETWEEN WBL 417 AND WBL 446. REPAIRED IAW EO B737HC57-007/02 APPROVED 8110-3 FORM BY FAA.Feb 20, 2002 · N239TA · Boeing 73725A · AileronsSDR P2EA2002V0024Service difficulty-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 8110-3 form, submited by Robert Manashi, (DERT-710167-SW).Note: See Aeroman W/O No. 2002-90/1, VAM100 No.Feb 20, 2002 · N239TA · Boeing 73725A · Trailing Edge FlapsSDR P2EA2002V0023Service difficulty-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, 2002 approved with FAA 8110-3 form, submited by Robert Manashi, (DERT-710167-SW).Note: See Aeroman W/OFeb 20, 2002 · N239TA · Boeing 73725A · Aileron TabsSDR P2EA2002V0022Fitting-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. B737HC55-007/02, DATED Feb 15, 2002 approved with FAA 8110-3 form, submited by Robert Manashi, (DERT-710167-Feb 20, 2002 · N239TA · Boeing 73725A · Ventral StructureSDR P2EA2002V0014Frame-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, VAM100 No.314, SDA No. 239SDA017.Feb 19, 2002 · N239TA · Boeing 73725A · Fuselage Main, FrameSDR P2EA2002V0013Frame · bentDURING Q1+ Q2 INSPECTION, FWD CARGO COMPARTMENT BS 420 STR 24L FRAME BENT. FRAME REPAIRED IAW SRM 51-40-3 FIG 1.Feb 19, 2002 · N239TA · Boeing 73725A · Fuselage Main, FrameSDR P2EA2002V0030Seat 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. 2002-90/1, VAM100 0583, SDA 239SDA097Feb 19, 2002 · N239TA · Boeing 73725A · Fuselage Main, StructureSDR P2EA2002V018Angle · crackedDURING 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.Feb 19, 2002 · N239TA · Boeing 73725A · Fuselage Miscellaneous StructureSDR P2EA2002V0009Floorbeam · corrodedDURING Q1+Q2 INSPECTION, PAX CABIN RBL 12 BS 360 FLOORBEAM WITH CORROSION. FLOORBEAM REPAIRED IAW SRM 53-10-9 FIG 1.Feb 19, 2002 · N239TA · Boeing 73725A · Fuselage Main, Floor BeamSDR P2EA2000V0008Floorbeam · corrodedDURING 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 65C37528, 65C37472.Feb 19, 2002 · N239TA · Boeing 73725A · Fuselage Main, Floor BeamSDR P2EA2002V0007Floorbeam · corrodedDURING 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.Feb 19, 2002 · N239TA · Boeing 73725A · Fuselage Main, Floor BeamSDR P2EA2000V0003Floorbeam · corrodedDURING 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.Feb 19, 2002 · N239TA · Boeing 73725A · Fuselage Main, Floor BeamSDR P2EA2002V0002Floorbeam · corrodedDURING 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.Feb 19, 2002 · N239TA · Boeing 73725A · Fuselage Main, Floor BeamSDR P2EA2002V0001Floorbeam · scratchedDURING 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.Feb 19, 2002 · N239TA · Boeing 73725A · Fuselage Main, Floor BeamSDR P2EA2002V0016Stringer-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. B737MC53-18/02 & S/B 737-53-1145.Note: See Aeroman W/O No. 2002-90/1, VAM100 No.0322, SDA No. 239SDA019.Feb 18, 2002 · N239TA · Boeing 73725A · Fuselage Main, Longeron/StringerSDR P2EA2002V0015Stringer-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. B737MC53-18/02 & S/B 737-53-1145.Note: See Aeroman W/O No. 2002-90/1, VAM100 No.0321, SDA No. 239SDA018.Feb 18, 2002 · N239TA · Boeing 73725A · Fuselage Main, FrameSDR P2EA2002V0012Frame-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.076, SDA No. 239SDA005.Feb 18, 2002 · N239TA · Boeing 73725A · Fuselage Main, FrameSDR P2EA2002V0011Frame-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. 239SDA004.Feb 18, 2002 · N239TA · Boeing 73725A · Fuselage Main, FrameSDR 2PEA2002V0017Service difficulty-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, between WBL250 to WBL254, repair accomplished IAW SRM 57-50-4, Fig 1.Note: See Aeroman W/O No. 2002-Feb 18, 2002 · N239TA · Boeing 73725A · Trailing Edge FlapsSDR P2EA2002V0006Floorbeam · corrodedDURING Q1+Q2 INSPECTION, PASSENGER CABIN FLOORBEAM WITH CORROSION AT BS 294.5 BL 0. FLOORBEAM REPAIRED IAW SRM 53-10-9 FIG 5.Feb 18, 2002 · N239TA · Boeing 73725A · Fuselage Main, Floor BeamSDR P2EA2002V0005Floorbeam · corrodedDURING Q1+Q2 INSPECTION, PASSENGER CABIN FLOORBEAM WITH CORROSION AT BS 312 AND LBL 8. FLOORBEAM REPAIRED IAW SRM 53-10-9 FIG 5.Feb 18, 2002 · N239TA · Boeing 73725A · Fuselage Main, Floor BeamSDR P2EA2002V0004Floorbeam · corrodedDURING Q1+Q2 INSPECTION, PASSENGER CABIN FLOORBEAM WITH CORROSION AT BS 328 AND LBL 28. FLOORBEAM REPAIRED IAW SRM 53-10-9 FIG 6.Feb 18, 2002 · N239TA · Boeing 73725A · Fuselage Main, Floor BeamSDR P2EA2002V0010Floorbeam · crackedDURING 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.Feb 17, 2002 · N239TA · Boeing 73725A · Fuselage Main, Floor BeamSDR P2EA2002V0019Service difficulty-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/O No. 2002-90/1, VAM100 No.0160, SDA No. 239SDA009.Feb 15, 2002 · N239TA · Boeing 73725A · Trailing Edge FlapsSDR P2EA2002V0031SkinDURING 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. 2002-90/1, VAM100 0012, SDA 239SDA112Feb 14, 2002 · N239TA · Boeing 73725A · Electrical/Electronic Compartment DoorsSDR P2EA2002M006Clamp · looseAPU 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 THAT WAS BLOWING ON THE FIRE DETECTION LOOP. TIGHTENED CLAMP, OPS CHECKS NORMAL.Feb 10, 2002 · N239TA · Boeing 73725A · APU Bleed Air SystemSDR P2EA2002M004Fire Detector · malfunctionedPRIOR TO PUSH BACK, APU SHUT DOWN, LATER THE APU FIRE WARNING AND BELL ILLUMINATED. PERFORMED APU FIRE CHECK LIST PROCEDURES PULLED AND ROTATED HANDLE. PERFORMED AN APU FIRE INSPECTION AND FOUND NO EVIDENCE OF FIRE. PLACED THE APU, APU FIRE DETECTION AND THFeb 3, 2002 · N239TA · Boeing 73725A · Fire DetectionSDR P2EA2001M0017Controller · faultyNR 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. OPERATIONAL CHECKS NORMAL.Dec 21, 2001 · N239TA · Boeing 73725A · Compressor Bleed ControlSDR P2EA2001M0014Csd · malfunctionedNR 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. OPERATIONAL CHECK NORMAL IAW MM 24-11-11.Dec 5, 2001 · N239TA · Boeing 73725A · Alternator-Generator DriveSDR P2EA2001M0010Start Valve · failedNR 1 ENGINE START VALVE WOULD NOT OPEN. AIRCRAFT RETURNED TO GATE. REMOVED AND REPLACED START VALVE IAW MM 80-11-21. OPERATIONAL CHECK NORMAL.Nov 10, 2001 · N239TA · Boeing 73725A · Engine Start Valves/ControlsSDR P2EA2001M0001Connector · dirtyAIR-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 BLEED LIGHTS WITH APU BLEED SHUT OFF, PSI HELD, DUAL BLEED LIGHTS STAYED ON. BLEED VALVE OP'S NORSep 23, 2001 · N239TA · Boeing 73725A · APU Bleed Air System
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