# Service difficulty reports: N239TA, cancelled Feb 16, 2005

A list on [N239TA, cancelled Feb 16, 2005](https://openairdocs.org/deregistered/N239TA-2005-02-16.md).

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

- [SDR P2EA2002M040](https://openairdocs.org/sdr/P2EA2002M040.md): Acoustic Panel · gouged · Jun 12, 2002 · N239TA · Boeing 73725A · Engine Collector/Tailpipe/Nozzle
  > 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 MM 78-38-43.
- [SDR P2EA2002V0032](https://openairdocs.org/sdr/P2EA2002V0032.md): Link · loose · Apr 6, 2002 · N239TA · Boeing 73725A · Engine Oil Storage (Airframe Furnished)
  > 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 GALS. PRESSURE LINK TIGHTENED AT OIL FILTER BYPASS SW IAW MM 20-50-11 PAGE 211, ENGINE OIL SERVICED
- [SDR P2EA2002V0020](https://openairdocs.org/sdr/P2EA2002V0020.md): Skin · Mar 9, 2002 · N239TA · Boeing 73725A · Fuselage Main, Plate/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 FAA 8110-3 form submited by P.C.LeBar.Note: See Aeroman W/O No. 2002-90/1, VAM100 No.0715, SDA No. 2
- [SDR P2EA2002V0026](https://openairdocs.org/sdr/P2EA2002V0026.md): Service difficulty · Mar 3, 2002 · N239TA · Boeing 73725A · Vertical Stabilizer, Plate/Skin
  > -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 239SDA030
- [SDR P2EA2002V0021](https://openairdocs.org/sdr/P2EA2002V0021.md): Skin · Feb 21, 2002 · N239TA · Boeing 73725A · Fuselage Main, Plate/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 FAA 8110-3 form submited by B.R.Frakes.Note: See Aeroman W/O No. 2002-90/1, VAM100 No.0714, SDA No. 2
- [SDR P2EA2002V0029](https://openairdocs.org/sdr/P2EA2002V0029.md): Beam · corroded · Feb 20, 2002 · N239TA · Boeing 73725A · Horizontal Stabilizer Miscellaneous Structure
  > 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 AREA T/E BEAM REPAIRED IAW SRM 55-107 FIG 1.
- [SDR P2EA2002V0028](https://openairdocs.org/sdr/P2EA2002V0028.md): Stringer · corroded · Feb 20, 2002 · N239TA · Boeing 73725A · Fuselage Main, Longeron/Stringer
  > 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.md): Spar · delaminated · Feb 20, 2002 · N239TA · Boeing 73725A · Ailerons
  > 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 APPROVED BY 8110-3 FORM BY FAA.
- [SDR P2EA2002V0025](https://openairdocs.org/sdr/P2EA2002V0025.md): Aileron · delaminated · Feb 20, 2002 · N239TA · Boeing 73725A · Ailerons
  > 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.md): Service difficulty · Feb 20, 2002 · N239TA · Boeing 73725A · Trailing Edge Flaps
  > -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.
- [SDR P2EA2002V0023](https://openairdocs.org/sdr/P2EA2002V0023.md): Service difficulty · Feb 20, 2002 · N239TA · Boeing 73725A · Aileron Tabs
  > -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/O
- [SDR P2EA2002V0022](https://openairdocs.org/sdr/P2EA2002V0022.md): Fitting · Feb 20, 2002 · N239TA · Boeing 73725A · Ventral Structure
  > -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-
- [SDR P2EA2002V0014](https://openairdocs.org/sdr/P2EA2002V0014.md): Frame · Feb 19, 2002 · N239TA · Boeing 73725A · Fuselage Main, 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, VAM100 No.314, SDA No. 239SDA017.
- [SDR P2EA2002V0013](https://openairdocs.org/sdr/P2EA2002V0013.md): Frame · bent · Feb 19, 2002 · N239TA · Boeing 73725A · Fuselage Main, Frame
  > 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.md): Seat Track · Feb 19, 2002 · N239TA · Boeing 73725A · Fuselage Main, Structure
  > -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 239SDA097
- [SDR P2EA2002V018](https://openairdocs.org/sdr/P2EA2002V018.md): Angle · cracked · Feb 19, 2002 · N239TA · Boeing 73725A · Fuselage Miscellaneous Structure
  > 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.md): Floorbeam · corroded · Feb 19, 2002 · N239TA · Boeing 73725A · Fuselage Main, Floor Beam
  > 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.md): Floorbeam · corroded · Feb 19, 2002 · N239TA · Boeing 73725A · Fuselage Main, Floor Beam
  > 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 65C37528, 65C37472.
- [SDR P2EA2002V0007](https://openairdocs.org/sdr/P2EA2002V0007.md): Floorbeam · corroded · Feb 19, 2002 · N239TA · Boeing 73725A · Fuselage Main, Floor Beam
  > 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.md): Floorbeam · corroded · Feb 19, 2002 · N239TA · Boeing 73725A · Fuselage Main, Floor Beam
  > 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.md): Floorbeam · corroded · Feb 19, 2002 · N239TA · Boeing 73725A · Fuselage Main, Floor Beam
  > 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.md): Floorbeam · scratched · Feb 19, 2002 · N239TA · Boeing 73725A · Fuselage Main, Floor Beam
  > 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.md): Stringer · Feb 18, 2002 · N239TA · Boeing 73725A · Fuselage Main, Longeron/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. B737MC53-18/02 & S/B 737-53-1145.Note: See Aeroman W/O No. 2002-90/1, VAM100 No.0322, SDA No. 239SDA019.
- [SDR P2EA2002V0015](https://openairdocs.org/sdr/P2EA2002V0015.md): Stringer · Feb 18, 2002 · N239TA · Boeing 73725A · Fuselage Main, Frame
  > -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.
- [SDR P2EA2002V0012](https://openairdocs.org/sdr/P2EA2002V0012.md): Frame · Feb 18, 2002 · N239TA · Boeing 73725A · Fuselage Main, 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.076, SDA No. 239SDA005.
- [SDR P2EA2002V0011](https://openairdocs.org/sdr/P2EA2002V0011.md): Frame · Feb 18, 2002 · N239TA · Boeing 73725A · Fuselage Main, 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. 239SDA004.
- [SDR 2PEA2002V0017](https://openairdocs.org/sdr/2PEA2002V0017.md): Service difficulty · Feb 18, 2002 · N239TA · Boeing 73725A · Trailing Edge Flaps
  > -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-
- [SDR P2EA2002V0006](https://openairdocs.org/sdr/P2EA2002V0006.md): Floorbeam · corroded · Feb 18, 2002 · N239TA · Boeing 73725A · Fuselage Main, Floor Beam
  > 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.md): Floorbeam · corroded · Feb 18, 2002 · N239TA · Boeing 73725A · Fuselage Main, Floor Beam
  > 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.md): Floorbeam · corroded · Feb 18, 2002 · N239TA · Boeing 73725A · Fuselage Main, Floor Beam
  > 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.md): Floorbeam · cracked · Feb 17, 2002 · N239TA · Boeing 73725A · Fuselage Main, Floor Beam
  > 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.md): Service difficulty · Feb 15, 2002 · N239TA · Boeing 73725A · Trailing Edge Flaps
  > -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.
- [SDR P2EA2002V0031](https://openairdocs.org/sdr/P2EA2002V0031.md): Skin · Feb 14, 2002 · N239TA · Boeing 73725A · Electrical/Electronic Compartment Doors
  > 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. 2002-90/1, VAM100 0012, SDA 239SDA112
- [SDR P2EA2002M006](https://openairdocs.org/sdr/P2EA2002M006.md): Clamp · loose · Feb 10, 2002 · N239TA · Boeing 73725A · APU Bleed Air System
  > 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 THAT WAS BLOWING ON THE FIRE DETECTION LOOP. TIGHTENED CLAMP, OPS CHECKS NORMAL.
- [SDR P2EA2002M004](https://openairdocs.org/sdr/P2EA2002M004.md): Fire Detector · malfunctioned · Feb 3, 2002 · N239TA · Boeing 73725A · Fire Detection
  > 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. PERFORMED AN APU FIRE INSPECTION AND FOUND NO EVIDENCE OF FIRE. PLACED THE APU, APU FIRE DETECTION AND TH
- [SDR P2EA2001M0017](https://openairdocs.org/sdr/P2EA2001M0017.md): Controller · faulty · Dec 21, 2001 · N239TA · Boeing 73725A · Compressor Bleed Control
  > 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. OPERATIONAL CHECKS NORMAL.
- [SDR P2EA2001M0014](https://openairdocs.org/sdr/P2EA2001M0014.md): Csd · malfunctioned · Dec 5, 2001 · N239TA · Boeing 73725A · Alternator-Generator Drive
  > 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. OPERATIONAL CHECK NORMAL IAW MM 24-11-11.
- [SDR P2EA2001M0010](https://openairdocs.org/sdr/P2EA2001M0010.md): Start Valve · failed · Nov 10, 2001 · N239TA · Boeing 73725A · Engine Start Valves/Controls
  > 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.md): Connector · dirty · Sep 23, 2001 · N239TA · Boeing 73725A · APU Bleed Air System
  > 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 BLEED LIGHTS WITH APU BLEED SHUT OFF, PSI HELD, DUAL BLEED LIGHTS STAYED ON. BLEED VALVE OP'S NOR

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
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
```

This list as a web page: https://openairdocs.org/deregistered/N239TA-2005-02-16/reports

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