# Service difficulty reports: N914FR, cancelled Jul 31, 2013

A list on [N914FR, cancelled Jul 31, 2013](https://openairdocs.org/deregistered/N914FR-2013-07-31.md).

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

- [SDR F3LA2013031100836](https://openairdocs.org/sdr/F3LA2013031100836.md): Floor Support · corroded · Feb 12, 2013 · N914FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > MAIN CABIN FLOOR SUPPORT CORROSION AT FR16, Y1292. R & R FLOORBEAM IAW SRM 51-42-11, PARA 5 AND 7.
- [SDR F3LA2013031100835](https://openairdocs.org/sdr/F3LA2013031100835.md): Shear Plate · cracked · Feb 12, 2013 · N914FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > CABIN UNDER FLOOR LT SIDE BETWEEN STATION 69-70 LT SHEAR PLATE CRACKED. R & R LT SHEAR PLATE IAW SRM 51-42-11, PAR 6.B. 1-8.
- [SDR F3LA2011040500631](https://openairdocs.org/sdr/F3LA2011040500631.md): Floor Support · corroded · Mar 31, 2011 · N914FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > C-CHECK: NON ROTINE 36933; CABIN FR66, Y-765 FWD OF SPLICE, FLOOR SUPPORT HAS CORROSION AT FLOOR PANEL. REPLACED CABIN FLOOR SUPPORT FR66, Y-765 IAW SRM 51-42-11 PARA 5, PARA 6.D, PARA 5.A. AND B.
- [SDR F3LA2011040500630](https://openairdocs.org/sdr/F3LA2011040500630.md): Floor Support · corroded · Mar 31, 2011 · N914FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > C-CHECK: NON ROUTINE NR 36931; CABIN FR66 Y-1292 FWD OF SPLICE FLOOR SUPPORT HAS CORROSION. REPLACED FWD FLOOR SUPPORT IN MAIN CABIN AT FR66 Y-1292 IAW SRM 51-42-11 PARA 5, PARA 6A.(3), PARA 7.A.(6)(7).
- [SDR F3LA2011040500629](https://openairdocs.org/sdr/F3LA2011040500629.md): Floorbeam · corroded · Mar 31, 2011 · N914FR · Airbus A319111 · Fuselage Main, Floor Beam
  > C-CHECK: NON ROUTINE NR 36930; CABIN FR66, Y-765 FWD OF SPLICE HAS CORROSION AT FLOOR PANEL ON FLOOR SUPPORT. REPLACED CABIN FLOOR SUPPORT FR66, Y-765 IAW A319 SRM 51-42-11, PARA 5 AND 6.D AND PARA 5A. AND B.
- [SDR F3LA2011040500628](https://openairdocs.org/sdr/F3LA2011040500628.md): Floor Support · corroded · Mar 31, 2011 · N914FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > C-CHECK: NON ROUTINE 36929; CABIN FRAME 68 Y-765, FLOOR SUPPORT HAS SURFACE CORROSION. R & R FLOOR IAW SRM 51-42-11, PARA 5 AND 6.B, PARA 7.B, SRM 51-44-11, PARA 2.A. AND B.
- [SDR F3LA2011040500627](https://openairdocs.org/sdr/F3LA2011040500627.md): Floor Support · corroded · Mar 31, 2011 · N914FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > C-CHECK: NON ROUTINE NR 36907; CABIN FR66, Y-1292 AFT OF SPLICE FLOOR SUPPORT HAS CORROSION. REPLACED AFT FLOOR SUPPORT IAW SRM 51-42-11, PARA 5, PARA 6.A.(3) AND PARA 7A.(6)(7).
- [SDR F3LA2011040500626](https://openairdocs.org/sdr/F3LA2011040500626.md): Floor Support · corroded · Mar 31, 2011 · N914FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > C-CHECK: NON ROUTINE 36906; CABIN FR68 - FR66 Y-1292 FLOOR SUPPORT HAS CORROSION IN NUMEROUS AREAS. REPLACED FLOOR SUPPORT, MAIN CABIN AT FR68 - FR66 Y-1292 IAW SRM 51-42-11, PARA 5, PARA 6.A.(3), PARA 7.A(6)(7).
- [SDR F3LA2011040500625](https://openairdocs.org/sdr/F3LA2011040500625.md): Floor Support · corroded · Mar 31, 2011 · N914FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > NON-ROUTINE 36905; CABIN FR68 Y-1292 AFT OF SPLICE FLOOR SUPPORT HAS CORROSION. REPLACED AFT FLOOR SUPPORT IN MAIN CABIN AT FR68 Y-1292 IAW SRM 51-42-11 PARA 5, PARA 6.A.(3), PARA 7 A.(6)(7).
- [SDR F3LA2011040500624](https://openairdocs.org/sdr/F3LA2011040500624.md): Sill · corroded · Mar 31, 2011 · N914FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > NON ROUTINE NR 36903; CABIN FR68 AT RT AT DOOR SILL BEAM HAS CORROSION. REPAIRED SILL BEAM IAW SRM 53-41-14. REPAIR PRINCIPLE K.
- [SDR F3LA2011040500623](https://openairdocs.org/sdr/F3LA2011040500623.md): Plate · corroded · Mar 31, 2011 · N914FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > C-CHECK: NON ROUTINE NR 36902; FRAME 70 RT INTERNAL SHEAR PLATE HAS CORROSION. R & R SHEAR PLATE IAW SRM 51-42-11, FIG 8, 51-44-11 PARA 6A (1), 7A(1) AND PARA 7, FIG 12, 51-21-11 PARA 4 (A)-(D), 51-75-12 AND 51-23-11.
- [SDR F3LA2011040500622](https://openairdocs.org/sdr/F3LA2011040500622.md): Floor Support · corroded · Mar 31, 2011 · N914FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > C-CHECK: NON ROUTINE NR 36890; CABIN FR68 AT L2 DOOR OTBD FLOOR SUPPORT HAS CORROSION. REPAIRED SILL BEAM IAW SRM 53-41-14, FIG 201, REPAIR PRINCIPLE K.
- [SDR F3LA2011040500621](https://openairdocs.org/sdr/F3LA2011040500621.md): Floor Support · corroded · Mar 31, 2011 · N914FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > C-CHECK: NON ROUTINE NR 36889; CABIN FR68-FR66, Y1292 FWD OF SPLICE FLOOR SUPPORT HAS CORROSION. REPLACED FWD FLOOR SUPPORT IN MAIN CABIN AT FR68-FR666, Y1292 IAW SRM 51-42-11, PARA 5, PARA 6.A.(3), PARA 7. A.(6)(7).
- [SDR F3LA2011040500620](https://openairdocs.org/sdr/F3LA2011040500620.md): Skin · dented · Mar 31, 2011 · N914FR · Airbus A319111 · Fuselage Main, Plate/Skin
  > C-CHECK: NON ROUTINE NR 36804; FUSELAGE UNDER FWD CARGO DOOR FRAME 26, BETWEEN STR 43 RT AND 43 LT HAS A DENT. REPAIR SKIN DENT REF SRM 53-21-11, PARA 5.K, FIG 214 REPAIR CATEGORY B.
- [SDR F3LA2009091700182](https://openairdocs.org/sdr/F3LA2009091700182.md): Profile · corroded · Sep 16, 2009 · N914FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > DURING C5 C-CHECK, INSPECTION NOTED THE PROFILE LOCATED BETWEEN THE FORWARD AND AFT FLOOR PANELS AT FRAME 28 HAD CORRODED ATTACH HOLES. MAINTENANCE REMOVED AND REPLACED THE PROFILE IAW SRM 51-72-11.
- [SDR F3LA2009091700180](https://openairdocs.org/sdr/F3LA2009091700180.md): Profile · corroded · Sep 16, 2009 · N914FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > DURING C5 C-CHECK, INSPECTION NOTED THAT THE PROFILE LOCATED BETWEEN FRAME 24.5 AND FRAME 28, HAD CORROSION AROUND THE FLOOR PANEL ATTACH HOLES. MAINTENANCE REMOVED AND REPLACED THE PROFILE IAW SRM 51-72-11.
- [SDR F3LA2009091700179](https://openairdocs.org/sdr/F3LA2009091700179.md): Profile · corroded · Sep 16, 2009 · N914FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > DURING C5 C-CHECK, INSPECTION NOTED THAT THE PROFILE AT FRAME 28 IN THE FORWARD CARGO PIT HAD CORRODED FLOOR PANEL ATTACH HOLES. MAINTENANCE REMOVED AND REPLACED THE PROFILE IAW SRM 51-72-11 AND 51-42-11.
- [SDR F3LA2009091700178](https://openairdocs.org/sdr/F3LA2009091700178.md): Profile · corroded · Sep 16, 2009 · N914FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > DURING C5 C-CHECK, INSPECTION NOTED THE PROFILE AT FRAME 34 IN THE FORWARD CARGO PIT HAD CORRODED FLOOR PANEL ATTACH HOLES. MAINTENANCE REMOVED AND REPLACED THE PROFILE IAW SRM 51-72-11 AND 51-42-11.
- [SDR F3LA2009091700181](https://openairdocs.org/sdr/F3LA2009091700181.md): Control Cable · lack of lube · Sep 15, 2009 · N914FR · Airbus A319111 · Emergency Exits
  > DURING C5 C-CHECK, INSPECTION NOTED THAT THE RT OVERWING EXIT FLEX CONTROL CABLE FOR THE INFLATION RESERVOIR FAILED THE FUNCTIONAL TEST. MAINTENANCE LUBRICATED THE OVERWING EXIT CONTROL CABLE IAW AMM 52-21-00-720-001 AND AMM 25-62-00-640-001.
- [SDR F3LA2009091700177](https://openairdocs.org/sdr/F3LA2009091700177.md): Roll Pin · sheared · Sep 15, 2009 · N914FR · Airbus A319111 · Emergency Exits
  > DURING DEN C5 C-CHECK, INSPECTION NOTED THAT THE LT EMERGENCY EXIT DOOR LOCKING PIN WILL NOT LOCK IN THE ARMED POSITION. MAINTENANCE REMOVED AND REPLACED THE ROLL PIN THAT HOLDS THE LOCKING PIN IN PLACE PER AMM 52-21-11-400-003.
- [SDR F3LA2009091700176](https://openairdocs.org/sdr/F3LA2009091700176.md): Profile · corroded · Sep 14, 2009 · N914FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > DURING DEN C5 C-CHECK, INSPECTION NOTED CORROSION BETWEEN FRAME 28 AND FRAME 30 ON THE AFT RIGHT HAND FLOOR PROFILE ATTACH HOLES. MAINTENANCE REMOVED AND REPLACED THE PROFILE IAW SRM 51-42-11 AND 51-72-11 PARAGRAPH 6.
- [SDR F3LA200800192](https://openairdocs.org/sdr/F3LA200800192.md): Plate · corroded · Apr 20, 2008 · N914FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > DURING C4 S1 C CHECK INSPECTION NOTED MAIN DECK WEB AT FRAME 70 RBL 52 WAS CORRODED. MAINTENANCE REMOVED AND REPLACED MAIN DECK WEB AT FRAME 70 RBL 52 IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 51-72-11. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOU
- [SDR F3LA200800193](https://openairdocs.org/sdr/F3LA200800193.md): Fitting · failed · Apr 17, 2008 · N914FR · Airbus A319111 · Passenger/Crew Doors
  > DURING C4 S1 C CHECK INSPECTION NOTED THE FORWARD ENTRY DOOR FAILED RIG CHECK AT THE TORSION BAR BELL CRANK AND REDUCER SHAFT. MAINTENANCE REMOVED AND REPLACED THE LEFT FITTING FOR RIG PIN AND ADJUSTED DOOR RODS IN ACCORDANCE WITH THE REQUIREMENTS OF AMM 52-1
- [SDR F3LA200800180](https://openairdocs.org/sdr/F3LA200800180.md): Fitting · failed · Apr 17, 2008 · N914FR · Airbus A319111 · Passenger/Crew Doors
  > DURING C4 S1 C CHECK INSPECTION REPORTED THE FORWARD ENTRY DOOR FAILED RIG CHECK AT TORSION BAR BELL CRANK AND REDUCER SHAFT BELLCRANK. MAINTENANCE REMOVED AND REPLACED LEFT FITTING FOR RIG PIN AND ADJUSTED DOOR RODS IN ACCORDANCE WITH THE REQUIREMENTS OF AMM
- [SDR F3LA200800181](https://openairdocs.org/sdr/F3LA200800181.md): Floor Panel · corroded · Apr 15, 2008 · N914FR · Airbus A319111 · Fuselage Floor Panel
  > DURING C4 S1 C CHECK INSPECTION REPORTED CORROSION ON MAIN CABIN R1 DOOR ENTRY FLOOR PANEL LOWER SURFACE AND AT VARIOUS FASTENER HOLES. MAINTENANCE REMOVED AND REPLACED R1 DOOR ENTRY PANEL 222FF. INSTALLATION WILL BE ACCOMPLISHED ON WORK CARD CP753-12.
- [SDR F3LA200800176](https://openairdocs.org/sdr/F3LA200800176.md): Floor Panel · punctured · Apr 15, 2008 · N914FR · Airbus A319111 · Fuselage Floor Panel
  > DURING C4 S1 C CHECK INSPECTION NOTED PANEL 251RF HAS TWO PUNCTURES. MAINTENANCE CLEANED AREA OF DAMAGE, PREPPED AND APPLIED REPAIR IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 53-02-00. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE.
- [SDR F3LA200800175](https://openairdocs.org/sdr/F3LA200800175.md): Strap · corroded · Apr 15, 2008 · N914FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > DURING C4 S1 C CHECK INSPECTION REPORTED SURFACE CORROSION ON AFT CARGO BAY FLOOR STRAP FROM FLOOR STRAP 2350-2030 STRINGER 38 LEFT. MAINTENANCE FABRICATED NEW STRAP OUT OF 2024-T3.040 IN ACCORDANCE WITH THE REQUIREMENTS OF AIRBUS A319 DRAWING D53470477. PAR
- [SDR F3LA200800169](https://openairdocs.org/sdr/F3LA200800169.md): Wire Harness · missing · Apr 8, 2008 · N914FR · Airbus A319111 · Equipment/Furnishings Wiring
  > DURING C4 S1 C CHECK INSPECTION REPORTED EMERGENCY LIGHT CONNECTOR MISSING MATE LOCK CAP SEAT ROW 1 HARNESS 350WLI. MAINTENANCE REPLACED CONNECTOR HARNESS, HARNESS TO BE INSTALLED ON AIRCRAFT IN CONJUNCTION WITH INSTALLATION OF CARPET, SEATS IN ACCORDANCE WIT
- [SDR F3LA200800149](https://openairdocs.org/sdr/F3LA200800149.md): Floor Panel · damaged · Apr 6, 2008 · N914FR · Airbus A319111 · Fuselage Floor Panel
  > DURING C4 S1 C CHECK, INSPECTION REPORTED DELAMINATION, AT THE EDGES, AND A LARGE GOUGE, IN FLOOR PANEL 221DF. MAINTENANCE REPAIRED THE FLOOR PANEL IN ACCORDANCE WITH THE REQUIREMENTS OF A319 SRM 51-77-12. UPON COMPLETION OF THE REPAIR, THE PANEL WAS INSPECT
- [SDR F3LA200800170](https://openairdocs.org/sdr/F3LA200800170.md): Panel · damaged · Apr 5, 2008 · N914FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > DURING C4 S1 C CHECK INSPECTION REPORTED PANEL 151TG AFT CARGO SLANT PANEL HAS HOLE. MAINTENANCE FABRICATED DOUBLER AND APPLIED REPAIR IN ACCORDANCE WITH SRM 53-02-00 AND AMM 25-00-00. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE.
- [SDR F3LA200800146](https://openairdocs.org/sdr/F3LA200800146.md): Floor Panel · damaged · Apr 4, 2008 · N914FR · Airbus A319111 · Fuselage Floor Panel
  > DURING C4 S1 C CHECK, INSPECTION REPORTED FLOOR PANEL 221EF HAD PUNCTURE DAMAGE. MAINTENANCE REPAIRED THE PUNCTURE IN THE PANEL IN ACCORDANCE WITH THE REQUIREMENTS OF A319 SRM 53-12-00. UPON COMPLETION OF THE REPAIR, THE PANEL WAS INSPECTED AND FOUND ACCEPTA
- [SDR F3LA200800168](https://openairdocs.org/sdr/F3LA200800168.md): Strap · corroded · Apr 3, 2008 · N914FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > DURING C4 S1 C CHECK INSPECTION REPORTED SURFACE CORROSION ON AFT CARGO BAY FLOOR STRAP FROM FLOOR STRAP 2216 TO 2030 STRINGER 38 RIGHT. MAINTENANCE REMOVED AND REPLACED DAMAGED FLOOR STRAP IN ACCORDANCE WITH SRM 53-41-14 FIGURE 2 AND SRM 51-42-11. UPON COMP
- [SDR F3LA200800167](https://openairdocs.org/sdr/F3LA200800167.md): Seat Track · corroded · Apr 3, 2008 · N914FR · Airbus A319111 · Fuselage, Seat/Cargo Attach Fittings
  > DURING C4 S1 C CHECK INSPECTION REPORTED DEEP CORROSION CABIN FLOOR STRUCTURE SEAT TRACK AT FRAME 21, Y1292 FLOOR STRAP 810. MAINTENANCE REMOVED AND REPLACED NEW SEAT TRACK AND ONE SPLICE IN ACCORDANCE WITH SRM 51-72-11. UPON COMPLETION OF THE REPAIR IT WAS
- [SDR F3LA200800166](https://openairdocs.org/sdr/F3LA200800166.md): Strap · corroded · Apr 3, 2008 · N914FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > DURING C4 S1 C CHECK INSPECTION REPORTED CORROSION ON AFT CARGO BAY FLOOR FRAME STRAP UPPER SURFACE FLOOR STRAP 2350 FRAME 58. MAINTENANCE REMOVED AND REPLACED FLOOR STRAP 2350 AT FRAME 58 IN ACCORDANCE WITH SRM 51-72-11. UPON COMPLETION OF THE REPAIR IT WAS
- [SDR F3LA200800165](https://openairdocs.org/sdr/F3LA200800165.md): Strap · corroded · Apr 3, 2008 · N914FR · Airbus A319111 · Fuselage Floor Panel
  > DURING C4 S1 C CHECK INSPECTION REPORTED SURFACE CORROSION ON AFT CARGO BAY FLOOR FRAME STRAP UPPER SURFACE AT FLOOR STRAP 2243 FRAME 56. MAINTENANCE REMOVED AND REPLACED FLOOR STRAP IN ACCORDANCE WITH SRM 51-72-11. UPON COMPLETION OF THE REPAIR IT WAS INSPE
- [SDR F3LA200800164](https://openairdocs.org/sdr/F3LA200800164.md): Strap · corroded · Apr 3, 2008 · N914FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > DURING C4 S1 CHECK INSPECTION REPORTED SURFACE CORROSION ON CARGO BAY FLOOR STRAP 2403 TO 2456 STRINGER 38R. MAINTENANCE REMOVED AND REPLACED FLOOR STRAP IN ACCORDANCE WITH SRM 51-72-11. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE.
- [SDR F3LA200800145](https://openairdocs.org/sdr/F3LA200800145.md): Web · corroded · Apr 3, 2008 · N914FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > DURING C4 S1 C CHECK, INSPECTION REPORTED CORROSION WAS FOUND UNDER THE WEB AT FRAME 70 AND RIGHT BUTT LINE 52. MAINTENANCE REMOVED AND REPLACED THE WEB AT FRAME 70 IN ACCORDANCE WITH THE REQUIREMENTS OF A319 SRM 51-72-11. UPON COMPLETION OF THE INSTALLATION
- [SDR F3LA200800144](https://openairdocs.org/sdr/F3LA200800144.md): Seat Track · corroded · Apr 3, 2008 · N914FR · Airbus A319111 · Fuselage, Seat/Cargo Attach Fittings
  > DURING C4 S1 C CHECK, INSPECTION REPORTED CORROSION WAS FOUND ON SEAT TRACK Y-1292, AT FUSELAGE STATION 810, ON THE RIGHT SIDE, EXTENDING FORWARD TOWARD FRAME 20. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK IN ACCORDANCE WITH THE REQUIREMENTS OF A319 SRM
- [SDR F3LA2008OO144](https://openairdocs.org/sdr/F3LA2008OO144.md): Seat Track · corroded · Apr 3, 2008 · N914FR · Airbus A319111 · Fuselage, Seat/Cargo Attach Fittings
  > DURING C4 S1 C CHECK, INSPECTION REPORTED CORROSION WAS FOUND ON SEAT TRACK Y-1292, AT FUSELAGE STATION 810, ON THE RIGHT SIDE, EXTENDING FORWARD TOWARD FRAME 20. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK IN ACCORDANCE WITH THE REQUIREMENTS OF A319 SRM
- [SDR F3LA200800148](https://openairdocs.org/sdr/F3LA200800148.md): Floor Panel · corroded · Apr 2, 2008 · N914FR · Airbus A319111 · Fuselage Floor Panel
  > DURING C4 S1 C CHECK, INSPECTION REPORTED CORROSION AND DAMAGE WAS FOUND ON FLOOR PANEL 261PF, UNDER THE RIGHT CORNER OF THE AFT GALLEY. MAINTENANCE REPAIRED THE CORROSION AND DAMAGE IN ACCORDANCE WITH THE REQUIREMENTS OF A319 SRM 53-12-00. UPON COMPLETION O
- [SDR F3LA200800147](https://openairdocs.org/sdr/F3LA200800147.md): Floor Panel · damaged · Apr 2, 2008 · N914FR · Airbus A319111 · Fuselage Floor Panel
  > DURING C4 S1 C CHECK, INSPECTION REPORTED FLOOR PANEL 222EF HAD PUNCTURE DAMAGE. MAINTENANCE REPAIRED THE PUNCTURE IN THE FLOOR PANEL IN ACCORDANCE WITH THE REQUIREMENTS OF A319 SRM 53-12-00. UPON COMPLETION OF THE REPAIR, THE PANEL WAS INSPECTED AND FOUND A
- [SDR F3LA200800142](https://openairdocs.org/sdr/F3LA200800142.md): Cover · broken · Apr 1, 2008 · N914FR · Airbus A319111 · Emergency Lighting
  > DURING C4 S1 C CHECK, INSPECTION REPORTED A CRACK WAS FOUND IN THE EMERGENCY EXIT LIGHT LENS COVER LOCATED ON THE AFT SIDE OF THE FORWARD RIGHT DOOR FRAME. MAINTENANCE REMOVED AND REPLACED THE LENS COVER IN ACCORDANCE WITH AMM 33-51-13 PB 400-001. THE LIGHT
- [SDR F3LA200800143](https://openairdocs.org/sdr/F3LA200800143.md): Lamp · defective · Mar 30, 2008 · N914FR · Airbus A319111 · Emergency Lighting
  > DURING C4 S1 C CHECK, INSPECTION REPORTED THE EMERGENCY EXIT LIGHT, ABOVE THE L1 DOOR ENTRANCE, FLICKERED. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE EMERGENCY EXIT LIGHT IN ACCORDANCE WITH THE REQUIREMENTS OF AMM 33-21-11-020-50 AND AMM 33-21-11-42-050
- [SDR F3LA200600007](https://openairdocs.org/sdr/F3LA200600007.md): Attach Fitting · corroded · Feb 9, 2006 · N914FR · Airbus A319111 · Fuselage Main, Attach Fittings
  > DURING REMOVAL OF FLOOR PANEL 262EF FOR DISCREPANCY REGARDING AFT LAVATORIES, MAINTENANCE REPORTED L-2 DOORWAY FLOOR PANEL AFT ATTACH PLATE CORRODED. FABRICATED NEW ATTACH PLATE PER AIRBUS DRAWING 10D53670099. TREATED, INSTALLED AND INSTALLED ATTACH PLATE PE
- [SDR F3LA200600006](https://openairdocs.org/sdr/F3LA200600006.md): Floor Panel · corroded · Feb 9, 2006 · N914FR · Airbus A319111 · Fuselage Floor Panel
  > DURING REMOVAL OF FLOOR PANEL 262EF FOR DISCREPANCY REGARDING AFT LAVATORIES, MAINTENANCE REPORTED CORROSION ON AFT GALLEY CONNECTING PLATE MOUNT HOLES FOR FLOOR PANEL. REPLACED CONNECTING PLATE IAW AMM 53-42-12-400-002.
- [SDR F3LA200600005](https://openairdocs.org/sdr/F3LA200600005.md): Support Beam · corroded · Feb 9, 2006 · N914FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > DURING REMOVAL OF FLOOR PANEL 262EF FOR DISCREPANCY REGARDING AFT LAVATORIES, MAINTENANCE REPORTED CORROSION ON AFT GALLEY FLOOR SUPPORT BEAM BETWEEN FRAME 67-69 Y-765. REPLACED FLOOR SUPPORT BEAM IAW SRM 53-00-14 AND 53-41-14.
- [SDR F3LA200600004](https://openairdocs.org/sdr/F3LA200600004.md): Floorbeam · corroded · Feb 9, 2006 · N914FR · Airbus A319111 · Fuselage Main, Floor Beam
  > DURING REMOVAL OF FLOOR PANEL 262EF FOR DISCREPANCY REGARDING AFT LAVATORIES, MAINTENANCE REPORTED AFT GALLEY FLOOR SUPPORT BEAM AT R-2 DOOR CORRODED ON TOP OF FLANGE. REPLACED SUPPORT BEAM IAW SRM 53-00-14, 53-41-14 AND AIRBUS DRAWING 18D53472815.

## 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 = 'N914FR' AND deregistration_id = 'N914FR-2013-07-31'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N914FR-2013-07-31/reports

---
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