# Service difficulty reports: N945FR, cancelled Jul 2, 2013

A list on [N945FR, cancelled Jul 2, 2013](https://openairdocs.org/deregistered/N945FR-2013-07-02.md).

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

- [SDR F3LA2013031100837](https://openairdocs.org/sdr/F3LA2013031100837.md): Lamp · burned out · Feb 24, 2013 · N945FR · Airbus A319112 · Emergency Lighting
  > EMERGENCY EXIT SIGN AT L1 DOOR HAS BURNED OUT LAMP. R & R L1 EMERGENCY SIGN IAW AMM 33-51-13-020-050-C AND AMM 33-51-13-420-050-C. OPS CHECKED GOOD IAW AMM 33-51-13-710-050-A D(1).
- [SDR F3LA2013012400824](https://openairdocs.org/sdr/F3LA2013012400824.md): Line · failed · Jan 18, 2013 · N945FR · Airbus A319112 · Hydraulic System, Main
  > DURING CRUISE FLIGHT LOST GREEN SYSTEMS HYD; GREEN SYS HYD INOPERATIVE. FOUND BROKEN HYD LINE AT RT MLG DOOR ACTUATOR. R & R AFT HYD LINE ON RT MLG DOOR ACTUATOR. SERVICED GREEN HYD SYSTEM. LEAK AND OPS CHECKS NORMAL. REF 32-31-35 PB 401.
- [SDR F3LA2012122800822](https://openairdocs.org/sdr/F3LA2012122800822.md): Control Unit · inoperative · Dec 23, 2012 · N945FR · Airbus A319112 · AC Power Distribution System
  > AIRCRAFT BEING POWERED BY APU. ALL DROPPED OFF WITH APU STILL INDICATING AVAILABLE - STRONG ODOR OF ELECTRICAL SMOKE IN COCKPIT. R & R GAPCU-(GROUND AUX POWER CTRL UNIT) IAW AMM 24-41-34-400-001-B. CHECKED GOOD IAW AMM 24-41-00-740-002-B.
- [SDR F3LA2012042300747](https://openairdocs.org/sdr/F3LA2012042300747.md): Sill · corroded · Apr 23, 2012 · N945FR · Airbus A319112 · Fuselage Miscellaneous Structure
  > C-CHECK: FWD CARGO EIGHT INCHES AFT OF FRAME 27 DOOR SILL WEB HAS LIGHT SURFACE CORROSION. BLENDED AREA AND FOUND TO BE WITHIN LIMITS IAW SRM 51-73-00, PAR 5.F AND FIG 001.
- [SDR F3LA2012041800745](https://openairdocs.org/sdr/F3LA2012041800745.md): Sill · corroded · Apr 16, 2012 · N945FR · Airbus A319112 · Fuselage Miscellaneous Structure
  > C-CHECK: MAIN CABIN FRAME 66 AT L2 DOOR, DOOR SILL BEAM HAS CORROSION AT FASTENER HOLE. REPAIRED IAW SRM 53-41 -14 PB201.
- [SDR F3LA2012041800744](https://openairdocs.org/sdr/F3LA2012041800744.md): Floorbeam · corroded · Apr 16, 2012 · N945FR · Airbus A319112 · Fuselage Main, Floor Beam
  > C-CHECK: MAIN CABIN FLOORBEAM AT FRAME 68 Y765 HAS CORROSION. R & R FLOORBEAM IAW SRM 51-42-11 PARA 5.
- [SDR F3LA2012041800743](https://openairdocs.org/sdr/F3LA2012041800743.md): Floorbeam · corroded · Apr 16, 2012 · N945FR · Airbus A319112 · Fuselage Main, Floor Beam
  > C-CHECK: MAIN CABIN FLOORBEAM AT FRAME 68 -Y1292 AFT OF SPLICE HAS LIGHT SURFACE CORROSION. R & R FLOORBEAM IAW SRM 51-42-11, PARA 5.
- [SDR F3LA2012041800742](https://openairdocs.org/sdr/F3LA2012041800742.md): Floorbeam · corroded · Apr 16, 2012 · N945FR · Airbus A319112 · Fuselage Main, Floor Beam
  > C-CHECK: MAIN CABIN FLOORBEAM AT FRAME 68 -Y1292 FWD OF SPLICE HAS LIGHT SURFACE CORROSION. R & R FLOORBEAM IAW SRM 51-42-11, PARAGRAPH 5.
- [SDR F3LA2010122000570](https://openairdocs.org/sdr/F3LA2010122000570.md): Plate · corroded · Dec 17, 2010 · N945FR · Airbus A319112 · Fuselage Miscellaneous Structure
  > C-CHECK: NON ROUTINE N0596; FR69-70 SHEAR WEB PLATE HAS CORROSION AROUND FASTNER HOLES AND IS OLD CONFIGURATION. FOUND TO BE OUT OF LIMITS. REPLACED SHEAR WEB PLATE WITH NEW CONFIGURATION IAW EO AO-53EO-31434.
- [SDR F3LA2010122000569](https://openairdocs.org/sdr/F3LA2010122000569.md): Shear Tie · corroded · Dec 17, 2010 · N945FR · Airbus A319112 · Fuselage Internal Mounting Structure
  > C-CHECK: NON ROUTINE N0595; LT MAIN CABIN SHEAR PLATE HAS CORRORION AROUND FASTENER HOLES. SHEAR PLATE IS UNMODIFIELD TYPE ACFT IS IN C-CHECK. REPLACED THE SHEAR, FRAME FR69L TO FR70L IAW SRM 51-42-11 AND FRONTIER E) 53EO-31434.
- [SDR F3LA2010122000568](https://openairdocs.org/sdr/F3LA2010122000568.md): Sill · corroded · Dec 17, 2010 · N945FR · Airbus A319112 · Fuselage Miscellaneous Structure
  > C-CHECK: NON ROUTINE N0484; R2 DOOR SILL HAS 3 SQ INCHES OF CORROSION AROUND AFT GIRT BAR FITTING. FOUND TO BE OUT OF LIMITS. REPLACED THE R2 DOOR SILL IAW SRM 51-74-00 & CHECK LIMITS IAW SRM 53-41-14.
- [SDR F3LA2010122000567](https://openairdocs.org/sdr/F3LA2010122000567.md): Splice · corroded · Dec 17, 2010 · N945FR · Airbus A319112 · Fuselage Main, Floor Beam
  > C-CHECK: NON ROUTINE N0438; LT FLOORBEAM, Y1292 SPLICE COUPLING AT FRAME 66L HAS 2 INCHES OF CORROSION. CORROSION IS OUT OF LIMITS. REPLACED SPLICE COUPLING AT FRAME 66L IAW SRM 53-72-11, PARA 6.
- [SDR F3LA2010122000565](https://openairdocs.org/sdr/F3LA2010122000565.md): Floorbeam · corroded · Dec 17, 2010 · N945FR · Airbus A319112 · Fuselage Main, Floor Beam
  > C-CHECK: NON ROUTINE N0436; LT FLOORBEAM, Y1292 AT FRAME 68L HAS A 2 SQ. INCHES OF CORROSION ON THE UPPER AND LOWER SIDERS. CORROSION IS OUT OF LIMITS. REPLACED FLOORBEAM, Y1292 BETWEEN FRAMES 68LT AND 69LT IAW SRM 51-72-11, PARA 6.
- [SDR F3LA2010122000563](https://openairdocs.org/sdr/F3LA2010122000563.md): Floor Panel · chafed · Dec 17, 2010 · N945FR · Airbus A319112 · Fuselage Floor Panel
  > C-CHECK: NON ROUTINE N0399; AFT CARGO PANEL 151VG AFT EDGE IS WORN THROUGH TOP PLY. AREA IS 10 SQ INCHES. DAMAGE IS OUT OF LIMITS. FABRICATED REPLACEMENT PANEL 151VG IAW MCG IRM 9701 REV G.
- [SDR F3LA2010110800535](https://openairdocs.org/sdr/F3LA2010110800535.md): Thermostat · defective · Nov 3, 2010 · N945FR · Airbus A319112 · Cabin Temperature Control System
  > LOST BLEED NR1 AT 36,000 CAUSING CABIN PRESSURE EXCESS CABIN ALTITUDE. EMERGENCY WAS DECLARE AND DECENTED TO 10,000. FOUND THERMOSTAT DEFECTIVE, R & R THE THERMOSTAT IAW AMM 36-11-43-PB401. OPS CHECK GOOD.
- [SDR F3LA2010063000444](https://openairdocs.org/sdr/F3LA2010063000444.md): Unknown · arced · Jun 27, 2010 · N945FR · Airbus A319112 · Electrical Power System
  > UPON ENGINE SHUTDOWN BRIGHT ARCHING FROM AFT CIRCUIT BREAKER PANEL WITH LOUD BANG FROM WITHIN CIRCUIT BREAKER PANEL. ALSO PUFF OF SMOKE. PERFORMED TSM PROCESS REFERENCE TSM 24-00-00-810-823. NO CIRCUIT BREAKERS TRIPPED. NO ECAM WARNINGS. INSPECTED CIRCUIT
- [SDR F3LA2009051300086](https://openairdocs.org/sdr/F3LA2009051300086.md): Servo Control · faulted · May 9, 2009 · N945FR · Airbus A319111 · Elevator Control System
  > IN DEN, AIRCRAFT RETURNED TO BLOCK DUE TO NR 1 ELEVATOR AILERON COMPUTER PITCH FAULT DURING FLIGHT CONTROL CHECK. MAINTENANCE REMOVED AND REPLACED THE LEFT OUTBOARD ELEVATOR SERVO (BLUE SYSTEM, POSITION 34CE3) AND MADE ADJUSTMENTS PER AMM 27-34-51-000-001, 27
- [SDR F3LA200700283](https://openairdocs.org/sdr/F3LA200700283.md): Lanyard · missing · Oct 12, 2007 · N945FR · Airbus A319111 · Escape Slide
  > DURING C-1 CHECK, INSPECTION REPORTED RT OVERWING EMERGENCY ESCAPE SLIDE RELEASE CABLE FAILED TO RETRACT DURING MANUAL RELEASE TEST. REMOVED AND REPLACED PULL CABLE AND OPS CHECKED RT OVERWING EXIT SLIDE RELEASE CABLE IAW AMM 52-21-00, PB501, AND TASK CARD C5
- [SDR F3LA200700282](https://openairdocs.org/sdr/F3LA200700282.md): Lanyard · missing · Oct 12, 2007 · N945FR · Airbus A319111 · Escape Slide
  > DURING C-1 CHECK, INSPECTION REPORTED LT OVERWING EMERGENCY ESCAPE SLIDE LOWER ACTUATING CABLE WAS MISSING THE LOWER END PIECE TO ATTACH TO THE SLIDE RELEASE BOTTLE/TEST FIXTURE. REMOVED, REPLACED AND OPS CHECKED LT OVERWING EMERGENCY ESCAPE SLIDE LOWER ACTUA
- [SDR F3LA200700010](https://openairdocs.org/sdr/F3LA200700010.md): Bushing · out of adjust · Jan 22, 2007 · N945FR · Airbus A319111 · Passenger/Crew Doors
  > R1 DOOR WOULD NOT LATCH IN OPEN POSITION. RESEATED BUSHING UNDER PUSHBUTTON. PERFORMED OPS CHECK IAW AMM 52-10-00, PAGE 201. CHECKED GOOD. INSPECTED R1 DOOR GUST LOCK. OPERATED PROPERLY.

## 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 = 'N945FR' AND deregistration_id = 'N945FR-2013-07-02'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N945FR-2013-07-02/reports

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