# Service difficulty reports: N510TA, cancelled Jul 25, 2012

A list on [N510TA, cancelled Jul 25, 2012](https://openairdocs.org/deregistered/N510TA-2012-07-25.md).

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

- [SDR WRN2009F00000](https://openairdocs.org/sdr/WRN2009F00000.md): Fire Loop · defective · Dec 19, 2008 · N510TA · Airbus A300B4203 · Fire Detection
  > ENGINE NR 1 SHUT DOWN IN FLIGHT DUE TO A FIRE INDICATION DURING FLIGHT FROM BDL TO BQN. BOTH FIRE BOTTLES WERE DISCHARGED. WARNING LIGHT EXTINGUISHED. ACFT LANDED NORMALLY. NO FUEL DUMPED. MX REPLACED 3 FIRE LOOPS AND AN AMPLIFIER. RUN UP CHECK OK. ACFT
- [SDR WRN2008F00004](https://openairdocs.org/sdr/WRN2008F00004.md): Sill · fod · Jun 23, 2008 · N510TA · Airbus A300B4203 · Fuselage Miscellaneous Structure
  > AC AFTER TAKEOFF, LOUD WHISTLING NOISE HEARD AND AC HAD PROBLEMS PRESSURIZING. AC MADE UNSCHEDULED STOP, WITH NORMAL LANDING. FOUND F.O.D. AND DEBRIS IN MAIN CARGO DOOR SILL AREA. REMOVED F.O.D. AND DEBRIS FROM CARGO DOOR SEAL AREA IAW 52-70-00. SEAL FOR MAIN
- [SDR WRN2008F00002](https://openairdocs.org/sdr/WRN2008F00002.md): Valve · stuck · Jun 16, 2008 · N510TA · Airbus A300B4203 · Cabin Pressure Control System
  > AFTER TAKEOFF, PRESSURIZATION MALFUNCTION OCCURRED. ACCOMPLISHED ABNORMAL PROCEDURES. AC RETURNED TO FIELD. LANDING NORMAL. MX FOUND GROUND VENT VALVE STUCK CLOSED. MX CLEANED AND RESET GROUND VENTING VALVE IAW 21-31-17, PG 501. OPS CHECKED SATISFACTORY
- [SDR WRNA200800037](https://openairdocs.org/sdr/WRNA200800037.md): Csd · malfunctioned · Apr 29, 2008 · N510TA · Airbus A300B4203 · AC Generator-Alternator
  > DURING FLIGHT, NR 1 CONSTANT SPEED DRIVE LOW OIL PRESSURE LIGHT ILLUMINATED FOLLOWED BY RISING OIL TEMPERATURE. DISCONNECTED CSD AND RETURNED TO MFM FOR A SAFE LANDING. REPLACED CSD IAW MM 24-11-11 PG 401 AND CSD OIL COOLER IAW 24-11-21 PAGE 401. AIRCRAFT R
- [SDR WRNA200700064](https://openairdocs.org/sdr/WRNA200700064.md): Damper · malfunctioned · Dec 28, 2007 · N510TA · Airbus A300B4203 · Landing Gear Retraction/Extension System
  > AFTER DEPARTURE WHEN RAISING GEAR, LEVER WOULD NOT GO PAST THE MID POSITION, GEAR POSITION LIGHTS REMAINED 'GREEN'. RETURNED TO FIELD AND MADE A SAFE LANDING. AIRCRAFT MAINTENANCE FERRIED TO CTS IN JAPAN FOR CORRECT ACTION. REPLACED LT GEAR PITCH DAMPER, AI
- [SDR WRNA200700058](https://openairdocs.org/sdr/WRNA200700058.md): Line · obstructed · Oct 23, 2007 · N510TA · Airbus A300B4203 · Airspeed/Mach Indicator
  > DURING TAKEOFF ROLL, FIRST OFFICERS AIR SPEED LAGGED BEHIND CAPTAINS BY 40-60 KNOTS, ABORTED TAKEOFF. FLUSHED DEBRIS FROM PITOT PRESSURE LINES, ACCOMPLISHED PITOT/STATIC TEST IAW 34-11-10 PAGE 501. TEST NORMAL. AIRCRAFT RELEASED FOR SERVICE.
- [SDR WRNA200700057](https://openairdocs.org/sdr/WRNA200700057.md): Pitot Tube · leaking · Oct 23, 2007 · N510TA · Airbus A300B4203 · Airspeed/Mach Indicator
  > DURING TAKEOFF THE FIRST OFFICERS AIRSPEED INDICATOR LAGGED 40-60 KNOTS BEHIND CAPTAINS AIRSPEED INDICATOR. FOUND RT PITOT PROBE LEAKING, REPLACED RT PITOT PROBE IAW A300 MM 34-11-15 PAGE 401. ACCOMPLISHED LEAK CHECK IAW A300 MM 34-11-10 PAGE 501. AIRCRAFT
- [SDR WRNA200700051](https://openairdocs.org/sdr/WRNA200700051.md): Circuit Breaker · weak · Oct 18, 2007 · N510TA · Airbus A300B4203 · Electrical Power System Wiring
  > AFTER TAKEOFF, FUEL PUMP NR 1; 1A; 2 CIRCUIT BREAKERS POPPED, AND AFCS AND FLIGHT ENGINEER PANEL LIGHTS WENT OFF. RETURNED TO FIELD AND MADE A SAFE LANDIBG. REPLACED FAULTY BREAKER IN 101VU PANEL.
- [SDR WRNA200700065](https://openairdocs.org/sdr/WRNA200700065.md): Bulkhead · cracked · Oct 11, 2007 · N510TA · Airbus A300B4203 · Fuselage Main, Bulkhead
  > DURING ACCOMPLISHMENT OF CPCP TASK C53-310-02-00 AT M96 CHECK, LEVEL II CORROSION WAS FOUND ON AFT PRESSURE BULKHEAD AT STR TIE END ANGLE FITTING AT 35R. FABRICATED FITTING FROM 7076 T6511 EXTRUSION IAW SRM 51-10-40. APPLIED PROTECTIVE COATINGS IAW SRM 51-40
- [SDR WRNA200700070](https://openairdocs.org/sdr/WRNA200700070.md): Fitting · corroded · Oct 11, 2007 · N510TA · Airbus A300B4203 · Fuselage Miscellaneous Structure
  > DURING ACCOMPLISHMENT OF CPCP TASK C53-310-02-00 AT M96 CHECK, LEVEL II CORROSION WAS FOUND ON AFT PRESSURE BULKHEAD STR TIE END ANGLE FITTING AT 38R. FABRICATED FITTING FROM 7076 T6511 EXTRUSION IAW SRM 51-10-40, APPLIED PROTECTIVE COATINGS IAW SRM 51-40-12,
- [SDR WRNA200700069](https://openairdocs.org/sdr/WRNA200700069.md): Fitting · corroded · Oct 11, 2007 · N510TA · Airbus A300B4203 · Fuselage Miscellaneous Structure
  > DURING ACCOMPLISHMENT OF CPCP TASK C53-310-02-00 AT M96 CHECK, LEVEL II CORROSION WAS FOUND ON AFT PRESSURE BULKHEAD STR TIE END ANGLE FITTING AT 37R. FABRICATED FITTING FROM 7076 T6511 EXTRUSION IAW SRM 51-10-40, APPLIED PROTECTIVE COATINGS IAW SRM 51-40-12,
- [SDR WRNA200700068](https://openairdocs.org/sdr/WRNA200700068.md): Fitting · corroded · Oct 11, 2007 · N510TA · Airbus A300B4203 · Fuselage Miscellaneous Structure
  > DURING ACCOMPLISHMENT OF CPCP TASK C53-310-02-00 AT M96 CHECK, LEVEL II CORROSION WAS FOUND ON AFT PRESSURE BULKHEAD STR TIE END ANGLE FITTING AT 36R. FABRICATED FITTING FROM 7076 T6511 EXTRUSION IAW SRM 51-10-40, APPLIED PROTECTIVE COATINGS IAW SRM 51-40-12,
- [SDR WRNA200700067](https://openairdocs.org/sdr/WRNA200700067.md): Fitting · corroded · Oct 11, 2007 · N510TA · Airbus A300B4203 · Fuselage Main, Attach Fittings
  > DURING ACCOMPLISHMENT OF CPCP TASK C53-310-02-00 AT M96 CHECK, LEVEL II CORROSION WAS FOUND ON AFT PRESSURE BULKHEAD STR TIE END ANGLE FITTING AT 35R. FABRICATED FITTING FROM 7076 T6511 EXTRUSION IAW SRM 51-10-40, APPLIED PROTECTIVE COATINGS IAW SRM 51-40-12,
- [SDR WRNA200700066](https://openairdocs.org/sdr/WRNA200700066.md): Bolt · corroded · Oct 11, 2007 · N510TA · Airbus A300B4203 · Engine Mount Section
  > DURING ACCOMPLISHMENT OF CPCP C54-400-03-00 AT M96 CHECK LEVEL II CORROSION WAS FOUND ON 4 HORIZONTAL BOLTS OF NR 2 ENGINE AFT MOUNT. REMOVED AND REPLACED 4 HORIZONTAL MOUNT BOLTS IAW MM 20-21-17 AND MM 70-00-00.
- [SDR WRNA200700049](https://openairdocs.org/sdr/WRNA200700049.md): Indication Sys · malfunctioned · Aug 18, 2007 · N510TA · Airbus A300B4203 · Leading Edge Slat Position Indicating System
  > DURING TAKEOFF FOR TEST FLIGHT AFTER HEAVY MAINTENANCE VISIT, CONFIGURATION LIGHT AND WARNING HORN CAME ON, TAKEOFF ABORTED. REPLACED LEADING EDGE INSTRUMENTATION UNIT IAW MM 27-84-11. AIRCRAFT RELEASED, TEST FLIGHT COMPLETED SATISFACTORY.
- [SDR WRNA200700053](https://openairdocs.org/sdr/WRNA200700053.md): Support · cracked · Jul 23, 2007 · N510TA · Airbus A300B4203 · Nacelle/Pylon, Main Frame
  > DURING M-96 CHECK, A 3 INCH CRACK WAS FOUND IN THE NR 2 ENGINE OUTBOARD CORE COWL SUPPORT. ACCOMPLISHED WELD REPAIR IAW ENGINEERING ORDER 2-54907-800 FROM EMTEQ.
- [SDR WRNA200700052](https://openairdocs.org/sdr/WRNA200700052.md): Trunnion · corroded · Jul 6, 2007 · N510TA · Airbus A300B4203 · Fuselage, Landing Gear Attach Fittings
  > DURING M-96 CHECK, CORROSION WAS FOUND IN LT MAIN LANDING GEAR AFT TRUNNION FORWARD LUG FITTING BORE AND FACE. REMOVED CORROSION BY OVERSIZING BORE AND SPOT FACING THE LUG FACE AND INSTALLED NEW BUSHING IAW REPAIR DESIGN APPROVAL SHEET RAS/BAE/1005347/2007.
- [SDR WRNA200700055](https://openairdocs.org/sdr/WRNA200700055.md): Rib · unserviceable · Jun 29, 2007 · N510TA · Airbus A300B4203 · Trailing Edge Flaps
  > DURING M96 COMPLY WITH S/B A300-57-0245, REPLACEMENT OF LT INBOARD FLAP RIB NR 7. REMOVED LEFT WING INBOARD FLAP, RIB NR 7, PERFORMED HFEC INSPECTION IAW A300-57-0245, NO DEFECTS NOTED. INSTALLED NEW NR 7 RIB P/N A5796005000400 IAW S/B A300-57-0245.
- [SDR WRNA200700056](https://openairdocs.org/sdr/WRNA200700056.md): Floorbeam · cracked · Jun 25, 2007 · N510TA · Airbus A300B4203 · Fuselage Main, Floor Beam
  > DURING M-96 CHECK, FOUND LOWER CROSS BEAM OF FLOORBEAM AT FRAME 57 BL 0 CRACKED. STOP DRILLED CRACK AND INSTALLED REPAIR DOUBLER IAW SRM 51-40-30.
- [SDR RNA200700054](https://openairdocs.org/sdr/RNA200700054.md): Floorbeam · corroded · Jun 24, 2007 · N510TA · Airbus A300B4203 · Fuselage Main, Floor Beam
  > DURING M-96 CHECK, FLOOR SUPPORT BEAM IN AFT CARGO AT FRAME 63 WAS FOUND CORRODED AND HAD A 5 INCH CRACK BETWEEN STR 41L AND 43L. CUT OUT DAMAGED SECTION OF FLOORBEAM CAP ANGLE AND INSTALLED 12 INCH LENGTH OF FLOORBEAM AND REPAIR DOUBLER IAW SRM 51-41-40.
- [SDR WRNA200700054](https://openairdocs.org/sdr/WRNA200700054.md): Floorbeam · corroded · Jun 24, 2007 · N510TA · Airbus A300B4203 · Fuselage Main, Floor Beam
  > DURING M-96 CHECK, FLOOR SUPPORT BEAM IN AFT CARGO A7 FRAME 63 WAS FOUND CORRODED AND HAD A 5 INCH CRACK BETWEEN STR 41L AND 43L. CUT OUT DAMAGED SECTION OF FLOORBEAM CAP ANGLE AND INSTALLED 12 INCH LENGTH OF FLOORBEAM AND REPAIR DOUBLER IAW SRM 51-41-40.
- [SDR WRNA200700028](https://openairdocs.org/sdr/WRNA200700028.md): Slide · deployed · Jun 5, 2007 · N510TA · Airbus A300B4203 · Escape Slide
  > ON GROUND, CREW OPENED LEFT HAND DOOR WITH DOOR ARMED, SLIDE WAS DEPLOYED. SLIDE WAS PLACED ON MEL 52-61-01 AND AIRCRAFT RELEASED FOR SERVICE. SLIDE WAS REPLACED ON 6-6-07 PER MM 25-61-00 PAGE 401.
- [SDR WRNA200600026](https://openairdocs.org/sdr/WRNA200600026.md): Slide · will not arm · Jun 20, 2006 · N510TA · Airbus A300B4203 · Escape Slide
  > R2 DOOR SLIDE WILL NOT ARM. REPLACED DOOR SLIDE IAW A300 25-61-11. RETURNED TO SERVICE.
- [SDR WRNA200500007](https://openairdocs.org/sdr/WRNA200500007.md): Adc · unserviceable · Mar 24, 2005 · N510TA · Airbus A300B4203 · Air Data Computer
  > AFTER TAKEOFF, CAPTAINS AIRSPEED INDICATOR DECREASED TO ZERO (0). CAPTIANS ALTIMETER REMAINED AT 300 FT. DURING CLIMB OUT. AIRCRAFT RETURNED TO AIRPORT, LANDING NORMAL. REMOVED AND REPLACED AIR DATA COMPUTER IAW 34-12-34. OPS AND FUNCTIONAL CHECK SATISFACTO

## 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 = 'N510TA' AND deregistration_id = 'N510TA-2012-07-25'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N510TA-2012-07-25/reports

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