# Service difficulty reports: N909FR, cancelled Jul 22, 2008

A list on [N909FR, cancelled Jul 22, 2008](https://openairdocs.org/deregistered/N909FR-2008-07-22.md).

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

- [SDR F3LA200700232](https://openairdocs.org/sdr/F3LA200700232.md): Light · miswired · Sep 15, 2007 · N909FR · Airbus A319112 · Light System Wiring
  > BLOCK TURN BACK, FLIGHT CREW REPORTED L2 DOOR EMERGENCY EXIT LIGHT 'ON' DURING TAXI, EMERGENCY EXIT SIGN 'OFF' DURING TAXI. MAINTENANCE FOUND 45WL, EXIT MARKING SIGN, AND 33WL, EMERGENCY CABIN LIGHT, WIRED INCORRECTLY. REWIRED 45WL AND 33WL IAW AMM 33-51-00,
- [SDR F3LA200700227](https://openairdocs.org/sdr/F3LA200700227.md): Slide · faulted · Sep 9, 2007 · N909FR · Airbus A319112 · Escape Slide
  > DURING C4/S1 CHECK, INSPECTION REPORTED EMERGENCY LIGHT TEST SHOWED LEFT EPSU EXTERNAL FAULT. REPLACED R1 DOOR SLIDE IAW AMM 25-62-44-400-007.
- [SDR F3LA200700221](https://openairdocs.org/sdr/F3LA200700221.md): Battery · failed · Sep 9, 2007 · N909FR · Airbus A319112 · Emergency Lighting
  > DURING C4/S1 CHECK, INSPECTION REPORTED "TEST EMERG LIGHT BAT" BATTERY CAPACITY CHECK FAILED. REMOVED AND REPLACED EMERGENCY EXIT BATTERIES IAW AMM 33-51-38-PB401. OPERATIONAL CHECK GOOD IAW 33-51-00-710-001, (S/N'S 26827, 24286, 26936, 042015).
- [SDR F3LA200700229](https://openairdocs.org/sdr/F3LA200700229.md): Access Panel · corroded · Sep 8, 2007 · N909FR · Airbus A319112 · Wing, Plate/Skin
  > DURING C4/S1 CHECK, INSPECTION REPORTED CORROSION ON FUEL PANEL 640JB ATTACHMENT HOLES. REMOVED AND REPLACED FUEL PANEL 640JB ON RT WING IAW AMM 57-27-11-400-002. PERFORMED LEAK CHECK IAW 57-27-11-400-002, NO LEAKS FOUND.
- [SDR F3LA200700228](https://openairdocs.org/sdr/F3LA200700228.md): Attach Fitting · corroded · Sep 8, 2007 · N909FR · Airbus A319112 · Landing Gear Doors
  > DURING C4/S1 CHECK, INSPECTION REPORTED LWR FWD ATTACH FITTING ON RT MLG STRUT DOOR RUSTED. REMOVED AFFECTED PARTS AND INSTALLED LWR FWD ATTACH FITTING IAW MM 32-12-14-400-002.
- [SDR F3LA200700222](https://openairdocs.org/sdr/F3LA200700222.md): Plate · gouged · Sep 6, 2007 · N909FR · Airbus A319112 · Horizontal Stabilizer Structure
  > DURING C4/S1 CHECK, INSPECTION REPORTED THE TRIMMABLE HORIZONTAL STAB MECHANICAL LINKAGE INBD OF UPPER CHAIN SPROCKET DAMAGED. SWIVEL PLATE AND LINK PLATE GOUGED. REPLACED SWIVEL PLATE AND LINK PLATE IAW AMM 27-41-45-400-001. PERFORMED OPERATIONAL CHECK IAW
- [SDR F3LA200700220](https://openairdocs.org/sdr/F3LA200700220.md): Bolt · corroded · Sep 6, 2007 · N909FR · Airbus A319112 · Fuselage Floor Panel
  > DURING C4/S1 CHECK, INSPECTION REPORTED THE FLOOR MOUNT BOLT ON THE AFT INBD CORNER OF THE AFT WALL OF LAV A WAS CORRODED AND COULD NOT BE REMOVED WITH STANDARD WRENCHES. THE HEAD WAS CUT OFF FROM BELOW TO REMOVE THE LAV WALL. REMOVED AND REPLACED BOLT IAW A
- [SDR F3LA200700218](https://openairdocs.org/sdr/F3LA200700218.md): Floor Panel · corroded · Sep 5, 2007 · N909FR · Airbus A319112 · Fuselage Floor Panel
  > DURING C4/S1 CHECK, INSPECTION REPORTED FLOOR THRESHOLD PANEL 221FF CORRODED TO EDGE. REMOVED AND REPLACED THRESHOLD PANEL 221FF IAW AMM 53-12-12 AND WORK CARD CP753-12.
- [SDR F3LA200700217](https://openairdocs.org/sdr/F3LA200700217.md): Floor Panel · corroded · Sep 5, 2007 · N909FR · Airbus A319112 · Fuselage Floor Panel
  > DURING C4/S1 CHECK, INSPECTION REPORTED FLOOR PANEL THRESHOLD PANEL 222FF CORRODED TO EDGE. REMOVED AND REPLACED FLOOR THRESHOLD PANEL 222FF IAW AMM 53-12-12 AND WORK CARD CP753-12.
- [SDR F3LA200700223](https://openairdocs.org/sdr/F3LA200700223.md): Floorbeam · corroded · Sep 3, 2007 · N909FR · Airbus A319112 · Fuselage Main, Floor Beam
  > DURING C4/S1 CHECK, INSPECTION REPORTED LT FLOORBEAM Y1292 CORRODED ON BOTTOM OF NUTPLATE HOLE AT FR66. FLOORBEAM FOUND TO BE OUT OF LIMITS IAW A319 SRM 53-00-14, PAGE 106. REMOVED AND REPLACED DAMAGED FLOORBEAM Y1292 SECTION FROM FR64 TO FR66 IAW 51-42-11.
- [SDR F3LA200700216](https://openairdocs.org/sdr/F3LA200700216.md): Floor Panel · corroded · Sep 2, 2007 · N909FR · Airbus A319112 · Fuselage Floor Panel
  > DURING C4/S1 CHECK, INSPECTION REPORTED CORROSION ON LOWER SURFACE OF FLOOR PANEL 261FF. REMOVED REPLACED FLOOR PANEL IAW SRM 51-24-00 AND AMM 53-42-12-400-002.
- [SDR F3LA200700215](https://openairdocs.org/sdr/F3LA200700215.md): Floorbeam · corroded · Sep 2, 2007 · N909FR · Airbus A319112 · Fuselage Main, Floor Beam
  > DURING C4/S1 CHECK, INSPECTION REPORTED CABIN FLOOR CENTER SUPPORT AT Y254, FR16, CORRODED. REMOVED DAMAGED AREA OF FLOORBEAM Y254 IAW SRM 53-00-14, FIG 204. REMOVED AND REPLACED FLOORBEAM AND ANGLES IAW SRM 51-42-11, EA NR A9-53R-12100 AND EA NR AO-51T-1197
- [SDR F3LA200700214](https://openairdocs.org/sdr/F3LA200700214.md): Floor Panel · corroded · Sep 2, 2007 · N909FR · Airbus A319112 · Fuselage Floor Panel
  > DURING C4/S1 CHECK, INSPECTION REPORTED CORROSION ON TOP SURFACE OF FLOOR PLANEL 221EF AFT OTBD CONNECTING PLATE. REMOVED AND REPLACED CONNECTING PLATE IAW AMM 53-12-12-400-001.
- [SDR F3LA200700213](https://openairdocs.org/sdr/F3LA200700213.md): Floor Panel · corroded · Sep 2, 2007 · N909FR · Airbus A319112 · Fuselage Floor Panel
  > DURING C4/S1 CHECK, INSPECTION REPORTED CORROSION ON LOWER SURFACE OF FLOOR PANEL 262FF. REMOVED AND REPLACED FLOOR PANEL 262FF IAW AMM 53-42-12-400-002.
- [SDR F3LA200700226](https://openairdocs.org/sdr/F3LA200700226.md): Floorbeam · corroded · Sep 1, 2007 · N909FR · Airbus A319112 · Fuselage Main, Floor Beam
  > DURING C4/S1 CHECK, INSPECTION REPORTED FWD CARGO COMPARTMENT FLOORBEAM FROM STR 38R TO STR 38L CORRODED AROUND FASTENER HOLES. REMOVED AND REPLACED TRANSITION PLATE AT FR28 BETWEEN STR 38R THRU STR 38L IAW SRM 51-42-11.
- [SDR F3LA200700212](https://openairdocs.org/sdr/F3LA200700212.md): Support Angle · cracked · Sep 1, 2007 · N909FR · Airbus A319112 · Nacelle/Pylon, Frame/Spar/Rib
  > DURING C4/S1 CHECK, INSPECTION REPORTED RT ENGINE PYLON SUPPORT ANGLE THAT ATTACHES PYLON PANELS 423DL AND 424CR AT RIB 5 CRACKED (AREA AROUND AFT SCREW HOLE). REMOVED AND FABRICATED REPLACEMENT SUPPORT ANGLE IAW SRM'S 54-52-12, P28, 51-31-00, P44,51-44-11, 5
- [SDR F3LA200700225](https://openairdocs.org/sdr/F3LA200700225.md): Floorbeam · corroded · Aug 31, 2007 · N909FR · Airbus A319112 · Fuselage Main, Floor Beam
  > DURING C4/S1 CHECK, INSPECTION REPORTED CORROSION ON UNDERNEATH SIDE OF NUTPLATE HOLE AT FR66. REPLACED COUPLING IAW 51-42-11.
- [SDR F3LA200700224](https://openairdocs.org/sdr/F3LA200700224.md): Shear Plate · corroded · Aug 30, 2007 · N909FR · Airbus A319112 · Fuselage Miscellaneous Structure
  > DURING C4/S1 CHECK, INSPECTION REPORTED SURFACE CORROSION AT AFT END OF LT SHEAR PLATE BETWEEN FR69 AND FR70. REMOVED AND REPLACED SHEAR PLATE BETWEEN FR69 AND FR70 IAW SRM 51-72-11 AND 51-42-11.
- [SDR F3LA200700211](https://openairdocs.org/sdr/F3LA200700211.md): Seal · corroded · Aug 30, 2007 · N909FR · Airbus A319112 · Passenger/Crew Doors
  > DURING C4/S1 CHECK, INSPECTION REPORTED LT DOOR SEAL CORRODED AT NUT PLATE HOLE AT FR66. FABRICATED REPAIR ANGLE, FILLERS AND DOUBLER IAW SRM 53-41-14. INSTALLED SPLICE ANGLE, DOUBLERS AND FILLER IAW SRM 53-41-11.
- [SDR F3LA200700210](https://openairdocs.org/sdr/F3LA200700210.md): Shim · corroded · Aug 30, 2007 · N909FR · Airbus A319112 · Fuselage Miscellaneous Structure
  > DURING C4/S1 CHECK, INSPECTION REPORTED FWD FLOOR PROFILER IN FWD CARGO COMPARTMENT HAD CORROSION AROUND FASTENER HOLE. REMOVED CORROSION ON SHIM FROM AROUND FASTENER HOLE IAW SRM 51-73-00. BLENDED AREA WAS APPROX.5" BY.5" WITH MAX DEPTH OF.012". REMOVED
- [SDR F3LA200700208](https://openairdocs.org/sdr/F3LA200700208.md): Bracket · corroded · Aug 30, 2007 · N909FR · Airbus A319112 · Fuselage Main, Attach Fittings
  > DURING C4/S1 CHECK, INSPECTION REPORTED FWD CARGO DOOR BOTTOM FRAME ALONG STR 38, JUST FWD OF FR26 FITTING BETWEEN 2ND AND 3RD LOCKING ROLLERS, CORRODED AT OTBD DOME NUT HOLE. REMOVED AND REPLACED FITTING AT FWD CARGO DOOR BOTTOM FRAME 26, STR 38, IAW A319 SR
- [SDR F3LA200700207](https://openairdocs.org/sdr/F3LA200700207.md): Frame · corroded · Aug 30, 2007 · N909FR · Airbus A319112 · Fuselage Main, Frame
  > DURING C4/S1 CHECK, INSPECTION REPORTED RT SUPPORT FRAME BETWEEN FR69 AND FR70 CORRODED. REMOVED AND REPLACED SUPPORT FRAME IAW A319 SRM 51-42-11.
- [SDR F3LA200700209](https://openairdocs.org/sdr/F3LA200700209.md): Panel · corroded · Aug 29, 2007 · N909FR · Airbus A319112 · Wing, Plate/Skin
  > DURING C4/S1 CHECK, INSPECTION REPORTED CORROSION ON ATTACHMENT HOLES ON PANEL 540JB. REPLACED PANEL IAW A319 WORKCARD CP757-2
- [SDR F3LA200700206](https://openairdocs.org/sdr/F3LA200700206.md): Shear Plate · corroded · Aug 27, 2007 · N909FR · Airbus A319112 · Fuselage Miscellaneous Structure
  > DURING C4/S1 CHECK, INSPECTION REPORTED RT SHEAR PLATE BETWEEN FR 69 AND FR 70 CORRODED. REMOVED AND REPLACED SHEAR PLATE IAW A319 SRM 51-42-11, PARA 6.B.
- [SDR F3LA200700205](https://openairdocs.org/sdr/F3LA200700205.md): Dummy Rail · corroded · Aug 27, 2007 · N909FR · Airbus A319112 · Fuselage Miscellaneous Structure
  > DURING C4/S1 CHECK, INSPECTION REPORTED CABIN FLOOR LT DUMMY RAIL AT FR12 TO FR16 CORRODED. REMOVED AND REPLACED DUMMY RAIL IAW A319 SRM 51-42-11.
- [SDR F3LA200700204](https://openairdocs.org/sdr/F3LA200700204.md): Profile · corroded · Aug 27, 2007 · N909FR · Airbus A319112 · Fuselage Miscellaneous Structure
  > DURING C4/S1 CHECK, INSPECTION REPORTED CORROSION AROUND FWD CARGO COMPARTMENT AFT FLOOR PROFILE FASTENER HOLES. REMOVED AND REPLACED PROFILE IAW A319 SRM 51-42-11 AND 53-21-14.
- [SDR F3LA200700203](https://openairdocs.org/sdr/F3LA200700203.md): Floorbeam · corroded · Aug 27, 2007 · N909FR · Airbus A319112 · Fuselage Main, Floor Beam
  > DURING C4/S1 CHECK, INSPECTION REPORTED CORROSION ON UPPER SURFACE OF LT FLOORBEAM Y765 AT FR68. FLOORBEAM FOUND TO BE OUT OF LIMITS IAW A319 SRM 53-00-14, PG 106. REMOVED AND REPLACED FLOORBEAM AT FRAME 68-70 IAW A318 SRM 53-00-14, SRM 51-42-11, DRAWING D53
- [SDR F3LA200700186](https://openairdocs.org/sdr/F3LA200700186.md): Window · unknown · Jul 26, 2007 · N909FR · Airbus A319112 · Flight Compartment Windows
  > DIVERSION AT FL 370, FLIGHT CREW HEARD A LOUD POP AND HISSING SOUND FROM THE CAPTAIN'S AFT SIDE WINDOW. AIRCRAFT DESCENDED TO 14000 RA AND LANDED AT KMCI. REPLACED CAPTAIN'S FIXED WINDOW AS A PRECAUTIONARY MEASURE IAW AMM 56-11-12. PERFORMED OPS TEST OF ANT
- [SDR F3LA200700036](https://openairdocs.org/sdr/F3LA200700036.md): Windshield · cracked · Feb 16, 2007 · N909FR · Airbus A319112 · Flight Compartment Windows
  > UPON ARRIVAL AT GATE, CAPTAIN'S WINDSHIELD CRACKED. REPLACED NR 1 WINDSHIELD IAW AMM 56-11-11, PB 401, P/N STA320-2-7-1A, S/N 5910 (MFG SULLY). ON PUSHBACK, FIRST OFFICER'S WINDSHIELD CRACKED. REPLACED NR 2 WINDSHIELD IAW AMM 56-11-11, PB 401, P/N STA320-2-
- [SDR F3LA200600146](https://openairdocs.org/sdr/F3LA200600146.md): Fan · failed · Oct 19, 2006 · N909FR · Airbus A319112 · Air Distribution Fan
  > DIVERSION, DURING CRUISE EN ROUTE TO MCO, FLIGHT CREW REPORTED BLOWER FAULT WITH ASSOCIATED ODOR. FLIGHT CREW DECLARED AN EMERGENCY AND DIVERTED TO BIRMINGHAM, AL. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE DISCOVERED THE VENT BLOWER FAN BAD. PLACED ON
- [SDR F3LA200600009](https://openairdocs.org/sdr/F3LA200600009.md): Support Beam · corroded · Mar 22, 2006 · N909FR · Airbus A319112 · Fuselage Main, Structure
  > DURING C-3 CHECK, INSPECTION REPORTED CORROSION AT SCREW HOLES IN FLOOR SUPPORT BEAM BL50L, BETWEEN FS 66 AND FS 68, L2 DOOR THRESHOLD. REMOVED AND REPLACED DAMAGED SECTION OF FLOOR SUPPORT BEAM PER SRM 53-00-14 AND 53-41-14.
- [SDR F3LA200500035](https://openairdocs.org/sdr/F3LA200500035.md): Control Unit · unserviceable · Jul 20, 2005 · N909FR · Airbus A319112 · Landing Gear Retraction/Extension System
  > AIR TURNBACK. ON TAKEOFF, FLIGHT CREW REPORTED LGCIU NR 1 FAULT ON WHEEL PAGE. HAD X'S ON WHEEL PAGE. REVERSER 1 FAULT ON STATUS PAGE. REPLACED NO. 1 LGCIU PER AMM 32-31-71, PB 401. PERFORMED BITE TEST PER AMM 32-69-00-740-001. PERFORMED SIMULATION OF FL
- [SDR F3LA200500012](https://openairdocs.org/sdr/F3LA200500012.md): Computer · faulty · Mar 10, 2005 · N909FR · Airbus A319112 · Autopilot System
  > FLIGHT CREW REPORTED ECAM FLIGHT CONTROL ELAC 2 PITCH FAULT (PASSING THROUGH FL180). AIRCRAFT RETURNED TO DEN AND LANDED WITHOUT INCIDENT. REPLACED NR 2 ELAC COMPUTER PER AMM 27-93-PB401; REPLACED THS ACTUATOR POSITION TRANSDUCER PER AMM 27-44-PB401; AND REP
- [SDR F3LA200400075](https://openairdocs.org/sdr/F3LA200400075.md): Computer · failed · Jul 27, 2004 · N909FR · Airbus A319111 · Central Warning
  > AIR TURN BACK. FLIGHT CREW REPORTED NUMEROUS SYSTEM FAILURES (GPS, GPWS, NR 1 RA, NR 1 ILS, NR 1 ENGINE REVERSER, NR 1 FADEC). CHECKED LAST LEG ECAM REPORT AND WAS UNABLE TO VERIFY FAULTS WITH CREW OR AIRCRAFT. CREW STATED ALL (FAULTED) SYSTEMS OPERATED 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 = 'N909FR' AND deregistration_id = 'N909FR-2008-07-22'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N909FR-2008-07-22/reports

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