# Service difficulty reports: N904FR, cancelled Apr 14, 2016

A list on [N904FR, cancelled Apr 14, 2016](https://openairdocs.org/deregistered/N904FR-2016-04-14.md).

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

Page 1 of 2 · 58 reports

- [SDR F3LA2013062500869](https://openairdocs.org/sdr/F3LA2013062500869.md): Lamp · burned out · Jun 25, 2013 · N904FR · Airbus A319111 · Emergency Lighting
  > EMERGENCY LIGHT EPSU TEST FAILED DURING A SCHEDULED HEAVY CHECK. R & R LAMPS IAW AMM 33-51-16-400-001A.
- [SDR F3LA2013051700856](https://openairdocs.org/sdr/F3LA2013051700856.md): Skin · contaminated · May 15, 2013 · N904FR · Airbus A319111 · Elevator, Plate/Skin
  > ACCOMPLISHED THERMOGRAPHIC INSPECTION OF LT ELEVATOR. SIX AREAS IN UPPER SKIN INDICATING WATER INGRESS, THREE AREAS ON LOWER SKIN. REPAIRED IAW SRM 55-20-00, PB201.
- [SDR F3LA2012101500806](https://openairdocs.org/sdr/F3LA2012101500806.md): Shear Plate · corroded · Oct 15, 2012 · N904FR · Airbus A319111 · Fuselage Main, Structure
  > FRAME 70 RIGHT SIDE SHEAR PLATE CORROSION. R & R SHEAR PLATE IAW EO AO-53EO-31434.
- [SDR F3LA2012101500805](https://openairdocs.org/sdr/F3LA2012101500805.md): Plate · corroded · Oct 15, 2012 · N904FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > FRAME 70 LT SIDE SHEAR PLATE CORROSION. R & R SHEAR PLATE IAW EO AO-53EO-31434.
- [SDR F3LA2012101500804](https://openairdocs.org/sdr/F3LA2012101500804.md): Sill · corroded · Oct 15, 2012 · N904FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > FRAME 66 RIGHT DOOR SILL BEAM SURFACE CORROSION AROUND FASTENER HOLE. REMOVED CORROSION AND FOUND TO BE WITHIN LIMITS IAW SRM 53-41-14 PB101, PARAGRAPH 4 B, FIG 101, SRM 51-21-11 AND SRM 51-23-11.
- [SDR F3LA2012101500803](https://openairdocs.org/sdr/F3LA2012101500803.md): Floorbeam · corroded · Oct 15, 2012 · N904FR · Airbus A319111 · Fuselage Main, Floor Beam
  > FR66, -Y1292 FLOORBEAM CORROSION. R & R FLOORBEAM REF SRM 51-42 -11, PARAGRAPH 5.
- [SDR F3LA2012101500802](https://openairdocs.org/sdr/F3LA2012101500802.md): Sill · corroded · Oct 15, 2012 · N904FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > L2 DOOR CUT OUT AT DOOR SILL HAS CORROSION 5 PLACES. R & R SHAPE SILL IAW SRM 51-42-11 PARA 6.B AND D.
- [SDR F3LA2012101500801](https://openairdocs.org/sdr/F3LA2012101500801.md): Sill · corroded · Oct 15, 2012 · N904FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > AFT CARGO DOOR SILL HAS CORROSION IN SEVERAL PLACES FROM FRAMES 55A TO 59. R & R DOOR SILL IAW REF SRM 51-42- 11, PARA 6.B. AND 7.B.
- [SDR F3LA2012003200728](https://openairdocs.org/sdr/F3LA2012003200728.md): Blade · lack of lube · Mar 20, 2012 · N904FR · Airbus A319111 · Turbine Engine Compressor Section
  > NR 1 ENGINE VIBRATION IN CLIMB OVER 4.0. VIBRATION WOULD FOLLOW THRUST. AIR TURN BACK. PERFORMED TSM TASKS 77-00-00-81 0-863-A AND 77-00-00-81 O-B64-A INCLUDING FAN BLADE LUBE REF AMM 72-21-00-210-004 AND COLD TRIM BALANCE REF AMM 71-00-00-750-001. MAXIMUM
- [SDR F3LA2011122100696](https://openairdocs.org/sdr/F3LA2011122100696.md): Electrical Box · odor · Dec 21, 2011 · N904FR · Airbus A319112 · Electrical Power System Wiring
  > PAX & F/A'S REPORTED THE STRONG BURNING ELECTRICAL ODOR IN ROW 20-22 A/C LEFT. FOUND SEB ROW 21ABC EMITTING ELECTRICAL ODOR, PERFORMED INSPECTIONS OF AFT GALLEYS & LAVS. INSPECTED LIVE TV SYS RACK IN AFT CARGO PIT, NO PROBLEMS NOTED REF AMM TSM 24-00-00-810
- [SDR F3LA2011121100692](https://openairdocs.org/sdr/F3LA2011121100692.md): Switch · failed · Dec 7, 2011 · N904FR · Airbus A319111 · Emergency Lighting
  > EMERGENCY EXIT LIGHT SWITCH NOT INDICATING OFF WHEN PLACED IN THE OFF POSITION. REPLACED TOGGLE SWITCH 4WL (ON/OFF/ARM) REF ESPM 20-45-21, TEST OK REF AMM 33-51 -11-710-050.
- [SDR F3LA2011052300653](https://openairdocs.org/sdr/F3LA2011052300653.md): Support Fitting · corroded · May 20, 2011 · N904FR · Airbus A319111 · Wing, Landing Gear Attach Fittings
  > C-CHECK: RT WING MLG SUPPORT RIB 5 FWD LUG INNER BORE HAS CORROSION. IAW EO A0-57EO-20243. REMOVED CORROSION BY OVER SIZING BORE TO 3.8772" AND INSTALLING NEW BUSHINGS. IAW SRM 57-26-13, PAR 5C AND FIG 203 AND 204.
- [SDR F3LA2011022100606](https://openairdocs.org/sdr/F3LA2011022100606.md): Stop · seized · Feb 17, 2011 · N904FR · Airbus A319111 · Turbine Engine Compressor Section
  > ACFT LOG PAGE 590497: AIR TURN BACK AT 01302. ECAM WARNING NR 2 ENGINE COMPRESSOR VANE (AIR RETURN. REPLACED NR 2 ENGINE MASTER BALLSCREW ACTUATOR STOP. REF AMM 75-31-50 PB 401, OPS CHECK NORMAL.
- [SDR F3LA2010043000392](https://openairdocs.org/sdr/F3LA2010043000392.md): Warning Light · illuminated · Apr 27, 2010 · N904FR · Airbus A319111 · Trailing Flap Position Indicating System
  > PILOT REPORT REF LOG PAGE 508494 ITEM(S) 1 FCTL FLAP FAULT (FLIGHT CONTROL FLAP FAULT)AND ITEM 2 FCTL SLAT FAULT (FLIGHT CONTROL SLAT FAULT) EMERGENCY DECLARED. OPS TEST OF THE FLAP AND SLAT SYS OK IAW AMM 27-54-00-710-002.
- [SDR F3LA2010022300353](https://openairdocs.org/sdr/F3LA2010022300353.md): Bulb · burned out · Feb 20, 2010 · N904FR · Airbus A319111 · Emergency Lighting
  > DURING VISUAL INSPECTION IT WAS NOTED THE EXIT SIGN BULB WAS BURNED OUT OVER FORWARD ENTRY. MAINTENANCE REMOVED AND REPLACED EMERGENCY EXIT SIGN BULB IAW AMM 33-51-16 PB 401.
- [SDR F3LA2009112400237](https://openairdocs.org/sdr/F3LA2009112400237.md): Coffeemaker · odor · Nov 23, 2009 · N904FR · Airbus A319111 · Buffet/Galleys
  > REFERENCE LOG PAGES 492755 AND 492756. FLIGHT CREW MADE AN AIR RETURN DUE TO A BURNING ODOR IN THE AFT GALLEY. MX PERFORMED TROUBLESHOOTING IAW TSM 21-00-00-810-802, TSM 24-00-00-810-823 AND SIL 21-135. MX DETERMINED THE AFT GALLEY COFFEEMAKERS WERE CAUSING T
- [SDR F3LA2009100500194](https://openairdocs.org/sdr/F3LA2009100500194.md): Hook · broken · Sep 30, 2009 · N904FR · Airbus A319111 · Passenger/Crew Doors
  > DURING C6 C-CHECK, INSP NOTED THAT THE L1 DOOR HANDLE WAS ABLE TO CLOSE WITHOUT THE DOOR BEING IN THE CLOSED POSITION. MX REMOVED AND REPLACED THE L1 DOOR HOOK ASSY IAW AMM 52-11-21-400-001.
- [SDR F3LA2009100500195](https://openairdocs.org/sdr/F3LA2009100500195.md): Floor Panel · corroded · Sep 27, 2009 · N904FR · Airbus A319111 · Fuselage Floor Panel
  > DURING C6 C-CHECK, INSP NOTED THE L2 ENTRY DOOR FLOOR PANEL HAS SEVERAL SPOTS OF CORROSION AROUND FASTENER HOLES. MX REMOVED AND REPLACED THE FLOOR PANEL AT POSITION 261FF, IAW TASK CARD C534103-02.
- [SDR F3LA2009100100189](https://openairdocs.org/sdr/F3LA2009100100189.md): Stringer · corroded · Sep 26, 2009 · N904FR · Airbus A319111 · Fuselage Main, Longeron/Stringer
  > DURING C6 C-CHECK, INSP NOTED CORROSION ON STR 44, SIX INCHES AFT OF FRAME 65 NEAR POTABLE WATER SERVICE PANEL. MX CUT OUT DAMAGED AREA, FABRICATED REPAIR STR AND INSTALLED IAW SRM 53-00-13, 51-42-11, 53-41-13 AND 51-21-11.
- [SDR F3LA2009100100188](https://openairdocs.org/sdr/F3LA2009100100188.md): Hook · broken · Sep 26, 2009 · N904FR · Airbus A319111 · Passenger/Crew Doors
  > DURING C6 C-CHECK, INSP NOTED THE R2 DOOR CLOSING BEFORE DOOR WAS IN DOOR JAM. MX REMOVED AND REPLACED THE HOOK AT THE R2 DOOR HANDLE IAW AMM 52-13-21-400-001.
- [SDR F3LA2009100100187](https://openairdocs.org/sdr/F3LA2009100100187.md): Shear Plate · corroded · Sep 26, 2009 · N904FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > DURING C6 C-CHECK, INSP NOTED THE LT HAND SHEAR PLATE AT Y1292 BETWEEN FRAME 69 AND FRAME 70 WAS CORRODED AT THE AFT SCREW HOLE. MX REMOVED AND REPLACED THE SHEAR PLATE IAW SRM 51-42-11, 51-72-11, 51-44-11 AND 51-23-11.
- [SDR F3LA2009100100186](https://openairdocs.org/sdr/F3LA2009100100186.md): Floorbeam · corroded · Sep 26, 2009 · N904FR · Airbus A319111 · Fuselage Main, Floor Beam
  > DURING C6 C-CHECK, INSP NOTED CORRODED FASTENER HOLES AT STATION -Y1292 AND FRAME 66. MX REMOVED AND REPLACED THE FLOORBEAM IAW SRM 51-42-11 AND 51-44-11.
- [SDR F3LA2009100100193](https://openairdocs.org/sdr/F3LA2009100100193.md): Shear Plate · corroded · Sep 25, 2009 · N904FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > DURING C6 C-CHECK, INSPECTION NOTED THE RT SHEAR PLATE AT Y1732 BETWEEN FRAME 69 AND FRAME 70 HAS CORROSION. MX REMOVED AND REPLACED THE SHEAR PLATE IAW SRM 51-44-11 AND 51-42-11.
- [SDR F3LA2009100100192](https://openairdocs.org/sdr/F3LA2009100100192.md): Sill · corroded · Sep 25, 2009 · N904FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > DURING C6 C-CHECK, INSPECTION NOTED THE L2 DOOR SILL HAS SEVERAL AREAS OF CORROSION. MX REMOVED AND REPLACED THE DOOR SILL IAW SRM 51-42-11 AND D53408505.
- [SDR F3LA2009100100184](https://openairdocs.org/sdr/F3LA2009100100184.md): Floorbeam · corroded · Sep 24, 2009 · N904FR · Airbus A319111 · Fuselage, Seat/Cargo Attach Fittings
  > SUPPLEMENTAL INFORMATION: REFERENCE NON ROUTINE C070051. DURING DEN C6 C-CHECK, INSPECTION NOTED CORROSION AROUND THE NUT PLATES LOCATED AT R2, Y1292 BETWEEN FRAME 66 AND FRAME 68. MAINTENANCE REMOVED AND REPLACED THE FLOORBEAM IAW SRM 51-44-11 AND 51-42-11.
- [SDR F3LA2009100100191](https://openairdocs.org/sdr/F3LA2009100100191.md): Floorbeam · corroded · Sep 24, 2009 · N904FR · Airbus A319111 · Fuselage Main, Floor Beam
  > DURING C6 C-CHECK, INSP NOTED THE COUPLING ATTCH POINT AT L2, STATION Y1292 AND FRAME 68 HAS CORROSION. MX REMOVED AND REPLACED THE FLOORBEAM IAW SRM 51-42-11 AND DWG SD53472815 AND D53472780.
- [SDR F3LA2009100100190](https://openairdocs.org/sdr/F3LA2009100100190.md): Floorbeam · corroded · Sep 24, 2009 · N904FR · Airbus A319111 · Fuselage Main, Floor Beam
  > DURING C6 C-CHECK, INSP NOTED CORROSION AROUND THE NUT PLATES AT L2, STATION Y1292 BETWEEN FRAME 66 AND FRAME 68. MX REMOVED AND REPLACED THE FLOORBEAM IAW SRM 51-42-11 AND DWG SD53472815.
- [SDR F3LA2009100100185](https://openairdocs.org/sdr/F3LA2009100100185.md): Floorbeam · corroded · Sep 24, 2009 · N904FR · Airbus A319111 · Fuselage Main, Floor Beam
  > DURING C6 C-CHECK, INSP NOTED THE COUPLING ATTACH POINT AT STATION Y1292 AND FRAME 68 HAS CORROSION. MX REMOVED AND REPLACED THE FLOORBEAM IAW SRM 53-41-14, 51-42-11 AND 51-44-11.
- [SDR F3LA2009020300019](https://openairdocs.org/sdr/F3LA2009020300019.md): Bulb · inoperative · Feb 2, 2009 · N904FR · Airbus A319111 · Emergency Lighting
  > DURING HEAVY CHECK, MAINTENANCE NOTED THE EMERGENCY PATH LIGHTS WERE INOPERATIVE AT SEATS 3, 6, 7, 18 AND 22. MAINTENANCE REMOVED AND REPLACED ALL INOPERATIVE EMERGENCY PATH LIGHT BULBS AND PERFORMED OPERATIONAL CHECK IAW AMM 33-51-19 PB401.
- [SDR F3LA2008121600724](https://openairdocs.org/sdr/F3LA2008121600724.md): Fire Detector · no test · Dec 13, 2008 · N904FR · Airbus A319111 · Smoke Detection
  > PILOT REPORTED THE NR 2 ENGINE FIRE PUSHBUTTON SWITCH LIGHT, CONTINUOUS REPETITIVE CHIME, BOTH MASTER WARNINGS AND ENGINE CONTROL PANEL FIRE LIGHT FAIL TO TEST. MAINTENANCE REMOVED AND REPLACED THE NR 2 ENGINE FIRE DETECTION UNIT IN ACCORDANCE WITH AMM 26-12-
- [SDR F3LA200800520](https://openairdocs.org/sdr/F3LA200800520.md): Switch · faulty · Jul 27, 2008 · N904FR · Airbus A319111 · Emergency Lighting
  > DURING PRE-FLIGHT INSP, CREW NOTED THE EMERGENCY EXIT AND AISLE LIGHTS WERE ILLUMINATED IN THE ARMED POSITION. MAINT REMOVED AND REPLACED THE TOGGLE SWITCH AND PERFORMED AN OPS CHECK IAW AMM 33-51-00. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND
- [SDR F3LA200800135](https://openairdocs.org/sdr/F3LA200800135.md): Skin · gouged · Apr 6, 2008 · N904FR · Airbus A319111 · Fuselage Main, Plate/Skin
  > DURING PRE FLIGHT INSPECTION, THE FLIGHT CREW REPORTED AFT LEFT FUSELAGE SKIN GOUGE AND DENT AT FRAME 61 AND STRINGER 38 LEFT. BLENDED THE GOUGE IN ACCORDANCE WITH EA A9-53R-30192. INTERIM REPAIR WAS INSPECTED AND FOUND ACCEPTABLE, TDI 1061199 ISSUED FOR FOL
- [SDR F3LA200800133](https://openairdocs.org/sdr/F3LA200800133.md): Stringer · damaged · Mar 29, 2008 · N904FR · Airbus A319111 · Wing, Longeron/Stringer
  > DURING C5 C CHECK INSPECTION REPORTED DURING PERFORMANCE OF REPAIR STRINGER WAS DAMAGED. MAINTENANCE REPAIRED THE STRINGER IN ACCORDANCE WITH THE REQUIREMENTS OF SRM A319 51-27-00 PAGE 1 AND SRM 51-42-11 PAGE 7. FOLLOWING COMPLETION OF THE REPAIR, THE STRIN
- [SDR F3LA200800132](https://openairdocs.org/sdr/F3LA200800132.md): Hinge Fitting · corroded · Mar 29, 2008 · N904FR · Airbus A319111 · Fuselage, Landing Gear Attach Fittings
  > DURING C5 C CHECK INSPECTION REPORTED CORROSION WAS FOUND IN THE MOUNTING HOLES OF THE RIGHT MAIN LANDING GEAR FORWARD HINGE BEARING SUPPORT BRACKET. MAINTENANCE REAMED FITTING ONE SIZE OVER AND INSTALLED NEW BUSHING IN ACCORDANCE WITH THE REQUIREMENTS OF EA
- [SDR F3LA200700123](https://openairdocs.org/sdr/F3LA200700123.md): Engine · malfunctioned · May 31, 2007 · N904FR · Airbus A319111 · Engine (Turbine/Turboprop)
  > AIR TURN BACK AT 1710Z, FLIGHT CREW REPORTED NR 2 ENGINE ROLLBACK TO BETWEEN 45 PERCENT AND 55 PERCENT N1 DURING CLIMB-OUT OF 10,000 FT. ENGINE WAS ALSO MAKING VERY LOUD BANGS EVERY 3 SECONDS ACCOMPANIED BY LARGE VIBRATIONS FELT THROUGHOUT THE AIRCRAFT. ALL
- [SDR F3LA200700110](https://openairdocs.org/sdr/F3LA200700110.md): Skin · gouged · Apr 23, 2007 · N904FR · Airbus A319111 · Wing, Plate/Skin
  > DURING TAKEOFF, NR 2 ENGINE FAN COWL DEPARTED AIRCRAFT HITTING INBD UNDER WING AREA. SEVERAL GOUGES AND SCRATCHES WERE FOUND BETWEEN RIBS 4 AND 6 AND STRINGERS 2 THRU 7.
- [SDR F3LA200700105](https://openairdocs.org/sdr/F3LA200700105.md): Skin · delaminated · Apr 23, 2007 · N904FR · Airbus A319111 · Elevator, Plate/Skin
  > DURING TAKEOFF, NR 2 ENGINE FAN COWL DEPARTED AIRCRAFT HITTING ELEVATOR ABOUT MID-SPAN. OUTER SKIN WAS DELAMINATED AND SHOWED LOSS OF INNER CORE MATERIAL. ALSO, THE END OF A COWL HOLD OPEN ROD WAS IMBEDDED IN THE ELEVATOR. [SUP 05-10-07] REPLACED RT ELEVAT
- [SDR F3LA200700104](https://openairdocs.org/sdr/F3LA200700104.md): Skin · punctured · Apr 23, 2007 · N904FR · Airbus A319111 · Horizontal Stabilizer, Plate/Skin
  > DURING TAKEOFF, NR 2 ENGINE FAN COWL DEPARTED AIRCRAFT HITTING OTBD HORIZONTAL STABILIZER LEADING EDGE. PUNCTURE WAS FOUND ABOUT MID SPAN OF LEADING EDGE. REPLACED RT OTBD HORIZONTAL STAB L/E IAW AMM 55-12-11-400-001, REFERENCE SDR F3LA200700083.
- [SDR F3LA200700103](https://openairdocs.org/sdr/F3LA200700103.md): Skin · dented · Apr 23, 2007 · N904FR · Airbus A319111 · Leading Edge Devices
  > DURING TAKEOFF, NR 2 ENGINE FAN COWL DEPARTED AIRCRAFT HITTING NR 1 SLAT. SLAT HAD SEVERE DENT DAMAGE TO LEADING EDGE OF STRUCTURE. REPLACED NR 1 SLAT IAW AMM 27-84-63-400-002, REFERENCE SDR F3LA200700083.
- [SDR F3LA200700102](https://openairdocs.org/sdr/F3LA200700102.md): Skin · dented · Apr 23, 2007 · N904FR · Airbus A319111 · Leading Edge Devices
  > DURING TAKEOFF, NR 2 ENGINE FAN COWL DEPARTED AIRCRAFT HITTING NR 2 SLAT. SLAT HAD SEVERE DENT AND GOUGE TO LEADING EDGE OF STRUCTURE. REPLACED NR 2 SLAT IAW AMM 27-84-64-400-002, REFERENCE SDR F3LA200700083.
- [SDR F3LA200700083](https://openairdocs.org/sdr/F3LA200700083.md): Structure · failed · Apr 22, 2007 · N904FR · Airbus A319111 · Nacelle/Pylon, Main Frame
  > NR 2 ENGINE COWLING DEPARTED AIRCRAFT. CAUSE UNKNOWN AT THIS TIME AND IS UNDER INVESTIGATION BY THE FAA. [SUP 05-15-07] THE NR 2 ENGINE FWD CANTILEVER ASSY SUSTAINED SIGNIFICANT DAMAGE. REMOVED AND REPLACED NR 2 ENGINE CANTILEVER ASSY. PER EA A9-57R-1187
- [SDR F3LA200600157](https://openairdocs.org/sdr/F3LA200600157.md): Battery · inoperative · Nov 8, 2006 · N904FR · Airbus A319111 · Emergency Lighting
  > FLIGHT CREW REPORTED FRONT EMERGENCY EXIT LIGHTS INOP. IN AUTOMATIC. OPERATES OK IN (ON) POSITION. REPLACED EPSU AND BATTERY AT 10WL IAW AMM 33-51-38, PB401. OPS CHECK GOOD. THE PN AND SN FOR THE UNITS REMOVED ARE AS FOLLOWS: EPSU, P/N 3214-54-10, S/N 41
- [SDR F3LA200600120](https://openairdocs.org/sdr/F3LA200600120.md): Floorbeam · corroded · Sep 13, 2006 · N904FR · Airbus A319111 · Fuselage Main, Floor Beam
  > DURING C-4 CHECK, INSPECTION REPORTED L2 DOOR THRESHOLD FLOORBEAM AT Y1732 AND FRAME 68 CORRODED ABOVE NUT PLATE. CORROSION DAMAGE ON DOOR SILL BEAM WAS FOUND TO EXCEED 50 PERCENT OF THE DEPTH OF THE BEAM AT THE NUT PLATE LOCATION. DAMAGE WAS FOUND TO BE OUT
- [SDR F3LA200600118](https://openairdocs.org/sdr/F3LA200600118.md): Plate · corroded · Sep 7, 2006 · N904FR · Airbus A319111 · Escape Slide
  > DURING C-4 CHECK, INSPECTION REPORTED R1 DOOR FWD GIRT BAR FITTING ATTACH PLATE CORRODED. REPLACED FWD GIRT BAR PLATE ASSY. IAW SRM 51-42-11 AND AMM 20-21-11.
- [SDR F3LA200600122](https://openairdocs.org/sdr/F3LA200600122.md): Cover · corroded · Sep 1, 2006 · N904FR · Airbus A319111 · Passenger/Crew Doors
  > DURING C-4 CHECK, INSPECTION REPORTED L2 DOOR FLOORBOARD ACCESS COVER PLATE CORRODED ON LWR SIDE. COVER PLATE WAS FOUND TO BE OUT OF LIMITS PER SRM 53-41-14. FABRICATED AND INSTALLED NEW COVER PLATE PER SRM 51-44-11, AIRBUS DRAWING 10D53670092, AND SRM 51-75
- [SDR F3LA200600117](https://openairdocs.org/sdr/F3LA200600117.md): Plate · corroded · Sep 1, 2006 · N904FR · Airbus A319111 · Escape Slide
  > DURING C-4 CHECK, INSPECTION REPORTED R2 DOOR FWD GIRT BAR PLATE CORRODED. REPLACED FWD GIRT BAR PLATE IAW AMM 52-13-31-400-003. SEALED AREA AROUND FWD PLATE AT R2 DOOR IAW AMM 52-13-31-400-007.
- [SDR F3LA200600121](https://openairdocs.org/sdr/F3LA200600121.md): Web · corroded · Aug 31, 2006 · N904FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON FLOOR WEB OB AND AFT OF BEAM AT FR69 AND Y1292. REMOVED FLOOR WEBS IAW SRM 51-42-11. FOUND UPPER WEB TO BE OUT OF LIMITS AND LOWER WEB TO BE WITHIN LIMITS IAW SRM 53-00-14. PERFORMED PANAMETRIC ULTRASONIC T
- [SDR F3LA200600116](https://openairdocs.org/sdr/F3LA200600116.md): Floorbeam · corroded · Aug 31, 2006 · N904FR · Airbus A319111 · Fuselage Main, Floor Beam
  > DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON FLOORBEAM (LONGERON) FWD OF FR68 AT Y1292. BLENDED OUT CORRODED AREA ON FLOORBEAM AND FOUND AREA TO BE OUT OF LIMITS IAW SRM 53-00-14, FIG. 102. REMOVED AND REPLACED FLOORBEAM FROM FR66 TO FR68 IAW SRM 51-42
- [SDR F3LA200600113](https://openairdocs.org/sdr/F3LA200600113.md): Floor Support · corroded · Aug 30, 2006 · N904FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON FLOOR SUPPORT IB OF L2 AT Y1292 FROM FR66 TO FR68 AT HOLES. FLOORBEAM WAS FOUND TO BE OUT OF LIMITS IAW SRM 51-00-14. REMOVED AND REPLACED FLOORBEAM FROM C64 TO C69 IAW SRM'S 51-42-11 AND 51-44-11.
- [SDR F3LA200600108](https://openairdocs.org/sdr/F3LA200600108.md): Floorbeam · corroded · Aug 30, 2006 · N904FR · Airbus A319111 · Fuselage Main, Floor Beam
  > DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON FLOORBEAM AFT OF L2 DOOR CUTOUT AT FR68 TO FR69, Y1292. FLOORBEAM WAS FOUND TO BE OUT OF LIMITS PER 53-00-14. REMOVED AND REPLACED FLOORBEAM FROM C64 TO C69 PER SRM'S 51-42-11 AND 51-44-11.

Next page: https://openairdocs.org/deregistered/N904FR-2016-04-14/reports.md?page=2

## 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 = 'N904FR' AND deregistration_id = 'N904FR-2016-04-14'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N904FR-2016-04-14/reports

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