# Service difficulty reports: N931FR, cancelled Jan 14, 2016

A list on [N931FR, cancelled Jan 14, 2016](https://openairdocs.org/deregistered/N931FR-2016-01-14.md).

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

- [SDR F3LA2014081401051](https://openairdocs.org/sdr/F3LA2014081401051.md): Battery · failed · Aug 13, 2014 · N931FR · Airbus A319111 · Emergency Lighting
  > EMERGENCY LIGHT BATTERY AFT LT FIN 13WL FAILED TEST ON OVERNIGHT MX CHECK. R & R BATTERY 13WL IAW AMM 33-51-39-000-005A & 33-51-39-400-005A.
- [SDR F3LA2013051600854](https://openairdocs.org/sdr/F3LA2013051600854.md): Structure · contaminated · May 10, 2013 · N931FR · Airbus A319111 · Elevator Structure
  > RT ELEVATOR, THERMOGRAPHY INSPECTION SHOWS FOUR INDICATIONS OF WATER INGRESS, LOCATED ON UPPER SKIN PANEL. INDICATIONS ARE IRREGULAR IN SHAPE AND BLACK IN COLOR. SEE NDT REPORT FOR SPECIFIC LOCATIONS. REMOVED SKIN AT AREAS OF LIQUID INGRESS. COMBINED AREAS 1
- [SDR F3LA2013051600855](https://openairdocs.org/sdr/F3LA2013051600855.md): Structure · contaminated · May 9, 2013 · N931FR · Airbus A319111 · Elevator Structure
  > LT ELEVATOR, THERMOGRAPHY INSPECTION SHOWS ONE INDICATIONS OF WATER INGRESS, LOCATED ON UPPER SKIN PANEL, INDICATION IS IRREGULAR IN SHAPE AND BLACK IN COLOR. SEE NDT REPORT FOR SPECIFIC LOCATION. REMOVED SKIN AT AREA OF LIQUID INGRESS, PREPARED SURFACE FOR RE
- [SDR F3LA2010052500434](https://openairdocs.org/sdr/F3LA2010052500434.md): Epsu · inoperative · May 19, 2010 · N931FR · Airbus A319111 · Emergency Lighting
  > REFERENCE HEAVY MAINTENANCE NON ROUTINE N0772. EMERGENCY EXIT MARKER INOPERATIVE LOWER FWD AT L-1 DOOR. R & R EPSU 10WL IAW AMM 33-51-38-000-001 AND 33-51-38-400-001.
- [SDR F3LA2010052200431](https://openairdocs.org/sdr/F3LA2010052200431.md): Connector · not seated · May 19, 2010 · N931FR · Airbus A319111 · Light System Wiring
  > REF HEAVY MX NON ROUTINE N0771. EMERGENCY EXIT SIGN OVER LT AFT ENTRY DOOR DOES NOT ILLUMINATE. FOUND CONNECTOR IMPROPERLY SEATED. PROPERLY SEATED CONNECTOR IAW AWM 33-51-04 P005 FIG 3.
- [SDR F3LA2010052200422](https://openairdocs.org/sdr/F3LA2010052200422.md): Sign · inoperative · May 19, 2010 · N931FR · Airbus A319111 · Emergency Lighting
  > REF HEAVY MX NON ROUTINE N0773. RT FWD LOWER EMERGENCY EXIT IDENTIFIER DOES NOT ILLUMINATE. R & R IDENTIFIER IAW AMM 33-51-13-000-001.
- [SDR F3LA2010052200432](https://openairdocs.org/sdr/F3LA2010052200432.md): Wire Harness · damaged · May 17, 2010 · N931FR · Airbus A319111 · Light System Wiring
  > REF HEAVY MX NON ROUTINE N0757. LT ROW 7 EMERGENCY ESCAPE PATH LIGHTING HARNESS HAS 1 EACH WIRE PULLED LOOSE. R & R WIRING HARNESS IAW ASM 33-51-00 SCH 04 P106.
- [SDR F3LA2010052200426](https://openairdocs.org/sdr/F3LA2010052200426.md): Floor Panel · debonded · May 13, 2010 · N931FR · Airbus A319111 · Fuselage Floor Panel
  > REF HEAVY MX NON ROUTINE N0733. FWD CARGO FLOOR PANEL 131AF DISBONDED AT CORNERS. REPAIRED IAW SRM 53-02-00, PAGE 208, FIG 203.
- [SDR F3LA2010052200429](https://openairdocs.org/sdr/F3LA2010052200429.md): Floor Panel · debonded · May 11, 2010 · N931FR · Airbus A319111 · Fuselage Floor Panel
  > REF HEAVY MX NON ROUTINE N0601. AFT CARGO FLOOR PANEL 152UG DISBONDED. FABRICATED NEW PANEL IAW MCG IRM 9701 REV G.
- [SDR F3LA2010052200428](https://openairdocs.org/sdr/F3LA2010052200428.md): Floor Panel · debonded · May 11, 2010 · N931FR · Airbus A319111 · Fuselage Floor Panel
  > REFERENCE HEAVY MX NON ROUTINE N0639. AFT CARGO PANEL 151UG DISBONDED. FABRICATED NEW PANEL IAW NCG IRM 9701 REV G.
- [SDR F3LA2010052200427](https://openairdocs.org/sdr/F3LA2010052200427.md): Floor Panel · debonded · May 11, 2010 · N931FR · Airbus A319111 · Fuselage Floor Panel
  > REF HEAVY MX NON ROUTINE N0654 AFT CARGO FLOOR PANEL 151FE DISBONDED. FABRICATED REPLACEMENT PANEL IAW MCG IRM 9701 REV G.
- [SDR F3LA2010052200430](https://openairdocs.org/sdr/F3LA2010052200430.md): Strut · corroded · May 10, 2010 · N931FR · Airbus A319111 · Main Landing Gear Strut/Axle/Truck
  > REF HEAVY MX NON ROUTINE N0538. RT MLG INNER BARREL (CYL) HAS CORROSION. REMOVED CORROSION AND REPAIRED IAW EA 3 AC-32R-31779.
- [SDR F3LA2010052500433](https://openairdocs.org/sdr/F3LA2010052500433.md): Sill · corroded · May 9, 2010 · N931FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > REFERENCE HEAVY MX NON ROUTINE N0432. AFT CARGO COMPARTMENT DOOR CUTOUT LOWER SILL HAS 6 AREAS OF CORROSION TOTALING 10 SQ INCHES. REPAIRED DOOR SEAL IAW EA A9-53R-31778.
- [SDR F3LA2010052200424](https://openairdocs.org/sdr/F3LA2010052200424.md): Floor Panel · delaminated · May 9, 2010 · N931FR · Airbus A319111 · Fuselage Floor Panel
  > REFERENCE HEAVY MAINTENANCE NON ROUTINE N0366. COCKPIT FLOOR PANEL 211GF IS DELAMINATED. REPAIRED PANEL IAW SRM 5302-00.
- [SDR F3LA2010052200425](https://openairdocs.org/sdr/F3LA2010052200425.md): Floorbeam · corroded · May 8, 2010 · N931FR · Airbus A319111 · Fuselage Main, Floor Beam
  > REF HEAVY MX NON ROUTINE N0281. FLOORBEAM AT FRAME 68 BEAM +4765 CORRODED. CUT OUT DAMAGED AREA.FABRICATED REPAIR SECTION AND INSTALLED IAW SRM 53-00-14 FIG 204.
- [SDR F3LA2010052200423](https://openairdocs.org/sdr/F3LA2010052200423.md): Shear Plate · corroded · May 8, 2010 · N931FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > REF HEAVY MX NON-ROUTINE N0280. AFTER FINDING MINOR CORROSION ON SHEAR PLATE FOUND PART TO BE WRONG CONFIGURATION. R & R SHEAR PLATE IAW EO- A0-53EO-31434.
- [SDR F3LA2010052200421](https://openairdocs.org/sdr/F3LA2010052200421.md): Floorbeam · corroded · May 8, 2010 · N931FR · Airbus A319111 · Fuselage Main, Floor Beam
  > HEAVY MX NON-ROUTINE N0283. REAR FUSELAGE FLOORBEAM AT FRAME 66 HAS CORROSION AROUND FASTENER HOLE. REPAIRED AREA IAW SRM 53-41-14, PAGE 201, FIGURE 201 PRINCIPLE NR 6.
- [SDR F3LA2010052200420](https://openairdocs.org/sdr/F3LA2010052200420.md): Sill · corroded · May 8, 2010 · N931FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > REF HEAVY MX NON ROUTINE N0295. LT AFT DOOR SILL AREA FWD OF FRAME 66 ATTACH SUPPORT HAS (6) SQUARE INCHES OF CORROSION ON UPPER SURFACE. R & R DOOR SILL IAW SRM 51-42-11, PAGE 5.
- [SDR F3LA2010011800304](https://openairdocs.org/sdr/F3LA2010011800304.md): Strut · discharged · Jan 15, 2010 · N931FR · Airbus A319111 · Main Landing Gear Strut/Axle/Truck
  > DURING CLIMB OUT THE FLIGHT CREW RECEIVED A WARNING THAT THE NLG WOULD NOT FULLY RETRACT. MX COMPLIED WITH BORESCOPE INSP OF THE ANTI ROTATION LUG IAW AMM 32-21-00-200-008 AND NO DAMAGE WAS NOTED. MX REPLACED CHARGING VALVE, SERVICED NLG STRUT AND PERFORMED
- [SDR F3LA2009120900255](https://openairdocs.org/sdr/F3LA2009120900255.md): Selector Valve · unserviceable · Dec 8, 2009 · N931FR · Airbus A319111 · Landing Gear Retraction/Extension System
  > THE FLIGHT CREW MADE AN AIR RETURN TO DEPARTURE DUE TO AN ELECTRONIC CENTRALIZED ACFT MONITORING MESSAGE FOR NLG DOORS NOT CLOSED AND LANDING GEAR SYS DISAGREE. MX REMOVED AND REPLACED THE LANDING GEAR SELECTOR VALVE AT POSITION 41GA AND PERFORMED A FUNCTIONA
- [SDR F3LA2008100600667](https://openairdocs.org/sdr/F3LA2008100600667.md): Control Panel · failed · Oct 4, 2008 · N931FR · Airbus A319111 · Fire Detection
  > DURING C3 C-CHECK, INSPECTION NOTED THE FIRE PANEL DISCHARGE LIGHT FOR THE NR 1 FIRE BOTTLE OF THE NR 2 ENGINE FAILS TO ILLUMINATE DURING THE OPERATIONAL CHECK OF THE BOTTLE LOW PRESSURE INDICATING CIRCUIT TEST. MAINTENANCE REMOVED AND REPLACED FIRE PANEL IN
- [SDR F3LA2008100600666](https://openairdocs.org/sdr/F3LA2008100600666.md): Floor Panel · punctured · Oct 4, 2008 · N931FR · Airbus A319111 · Fuselage Floor Panel
  > DURING C3 C-CHECK, INSPECTION NOTED SEVERAL PUNCTURES AND EDGE DELAMINATION TO AFT CARGO TRANSITION PANEL 151AE. MAINTENANCE REMOVED AND REPLACED CARGO PANEL IN ACCORDANCE WITH THE REQUIREMENTS OF A319 AMM 53-42-14-400-001.
- [SDR F3LA2008100600665](https://openairdocs.org/sdr/F3LA2008100600665.md): Floor Panel · delaminated · Oct 4, 2008 · N931FR · Airbus A319111 · Fuselage Floor Panel
  > DURING C3 C-CHECK, INSPECTION NOTED PASSENGER FLOOR PANEL 261DF HAS AREAS OF DELAMINATION. MAINTENANCE REPAIRED FLOOR PANEL IN ACCORDANCE WITH THE REQUIREMENTS OF A319 SRM 53-02-00 FIGURE 212.
- [SDR F3LA2008100600664](https://openairdocs.org/sdr/F3LA2008100600664.md): Floor Panel · delaminated · Oct 4, 2008 · N931FR · Airbus A319111 · Fuselage Floor Panel
  > DURING C3 C-CHECK, INSPECTION NOTED PASSENGER FLOOR PANEL 262EF HAS AREAS OF DELAMINATION. MAINTENANCE REPAIRED FLOOR PANEL IN ACCORDANCE WITH THE REQUIREMENTS OF A319 SRM 53-02-00, FIGURE 212.
- [SDR F3LA2008100600659](https://openairdocs.org/sdr/F3LA2008100600659.md): Floor Panel · corroded · Oct 4, 2008 · N931FR · Airbus A319111 · Fuselage Floor Panel
  > DURING C3 C-CHECK, INSPECTION NOTED FLOOR PANEL 262FF IS CORRODED ON UPPER AND LOWER SURFACE. MAINTENANCE REMOVED FLOOR PANEL AND INSTALLED SERVICEABLE PANEL IN ACCORDANCE WITH THE REQUIREMENTS OF A319 AMM 53-42-12-400-002.
- [SDR F3LA2008100600663](https://openairdocs.org/sdr/F3LA2008100600663.md): Floor Panel · damaged · Oct 3, 2008 · N931FR · Airbus A319111 · Fuselage Floor Panel
  > REFERENCE NON-ROUTINE C052153. DURING C3 C-CHECK, INSPECTION NOTED PASSENGER FLOOR PANEL 261EF HAS A CUT ON THE SURFACE. MAINTENANCE REPAIRED FLOOR PANEL IN ACCORDANCE WITH THE REQUIREMENTS OF A319 SRM 53-02-00, FIGURE 212.
- [SDR F3LA2008100600662](https://openairdocs.org/sdr/F3LA2008100600662.md): Floorbeam · corroded · Oct 3, 2008 · N931FR · Airbus A319111 · Fuselage Main, Floor Beam
  > DURING C3 C-CHECK, INSPECTION NOTED FLOORBEAM Y1292 AT FRAME 68, FORWARD AND AFT HOLES HAVE CORROSION. MAINTENANCE BLENDED CORROSION AND OVERSIZED HOLES IN ACCORDANCE WITH THE REQUIREMENTS OF A319 SRM 53-00-14, FIGURE 102. MAINTENANCE PERFORMED ROTO-PROBE IN
- [SDR F3LA2008100600661](https://openairdocs.org/sdr/F3LA2008100600661.md): Floorbeam · corroded · Oct 3, 2008 · N931FR · Airbus A319111 · Fuselage Main, Floor Beam
  > DURING C3 C-CHECK, INSPECTION NOTED FLOORBEAM Y1292 BETWEEN FRAME 66 AND FRAME 68, HAS CORROSION IN SEVERAL HOLES. MAINTENANCE BLENDED CORROSION AND OVERSIZED HOLES, HOLES OUT OF LIMITS PER SRM 53-00-14. MAINTENANCE REMOVED CORRODED FLOORBEAM AND UPPER COUPL
- [SDR F3LA2008100600660](https://openairdocs.org/sdr/F3LA2008100600660.md): Floorbeam · corroded · Oct 3, 2008 · N931FR · Airbus A319111 · Fuselage Main, Floor Beam
  > DURING C3 C-CHECK, INSPECTION NOTED FLOORBEAM Y1292 BETWEEN FRAME 66 AND FRAME 68, HAS CORROSION IN SEVERAL HOLES. MAINTENANCE BLENDED CORROSION AND OVERSIZED HOLES, HOLES OUT OF LIMITS PER SRM 53-00-14. MAINTENANCE REMOVED CORRODED FLOORBEAM AND UPPER COUPL
- [SDR F3LA2008100600658](https://openairdocs.org/sdr/F3LA2008100600658.md): Floorbeam · corroded · Oct 3, 2008 · N931FR · Airbus A319111 · Fuselage Main, Floor Beam
  > DURING C3 C-CHECK, INSPECTION NOTED FLOORBEAM Y1292 AT FRAME 66, FORWARD HOLE HAS CORROSION. MAINTENANCE BLENDED CORROSION, OVERSIZED HOLE, ROTO-PROBED, TREATED, PRIMED AND PAINTED IN ACCORDANCE WITH THE REQUIREMENTS OF A319 SRM 53-00-14, NONDESTRUCTIVE TESTI
- [SDR F3LA200800656](https://openairdocs.org/sdr/F3LA200800656.md): Floorbeam · corroded · Oct 2, 2008 · N931FR · Airbus A319111 · Fuselage Main, Floor Beam
  > REFERENCE NON ROUTINE C051966. DURING C3 C CHECK, INSPECTION NOTED FLOOR BEAM Y-1292 BETWEEN FRAME 66 AND FRAME 68 HAS CORROSION IN SEVERAL HOLES. MX R&R FLOOR BEAM IAW THE REQUIREMENTS OF A319 SRM 51-42-11 AND DRAWING D53472780. UPON COMPLETION OF THE REPA
- [SDR F3LA200800655](https://openairdocs.org/sdr/F3LA200800655.md): Light · inoperative · Oct 2, 2008 · N931FR · Airbus A319111 · Emergency Lighting
  > REFERENCE NON ROUTINE C051883. DURING C3 C CHECK INSPECTION NOTED THE RED EMERGENCY FLOOR PATH INDICATOR ON ROW 11ABC IS NOT ILLUMINATING. MX R&R LIGHT ASSEMBLY IAW THE REQUIREMENTS OF A319 AWM 33-51-07, PAGE 003. UPON COMPLETION OF THE REPAIR, IT WAS INSPE
- [SDR F3LA200800654](https://openairdocs.org/sdr/F3LA200800654.md): Battery · failed · Oct 2, 2008 · N931FR · Airbus A319111 · Emergency Lighting
  > REFERENCE NON ROUTINE CO51711. DURING C3 C-CHECK, INSPECTION NOTED AFT EMERGENCY POWER SUPPLY UNIT BATTERY FAILED CAPACITY CHECK. MX R&R BATTERY IN ACCORDANCE WITH THE REQUIREMENTS OF A319 AMM 33-51-38-000-001 AND 33-51-38-400-001. UPON COMPLETION OF THE RE
- [SDR F3LA2008100600670](https://openairdocs.org/sdr/F3LA2008100600670.md): Plate · corroded · Oct 2, 2008 · N931FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > DURING C3 C-CHECK, INSPECTION NOTED L-2 GIRT BAR FITTINGS ATTACH PLATE HOLES HAVE CORROSION. MAINTENANCE FABRICATED REPAIR DOUBLER AND FILLER, TREATED, PRIMED, PAINTED AND INSTALLED IN ACCORDANCE WITH THE REQUIREMENTS OF ENGINEERING AUTHORIZATION A9-53R-30662.
- [SDR F3LA2008100600669](https://openairdocs.org/sdr/F3LA2008100600669.md): Plate · corroded · Oct 2, 2008 · N931FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > DURING C3 C-CHECK, INSPECTION NOTED THE L-2 FORWARD GIRT BAR FITTING BLANKING PLATE HAS CORROSION ON CORNER. MAINTENANCE REMOVED AND REPLACED L-2 DOOR FORWARD GIRT BAR FITTING BLANKING PLATE IN ACCORDANCE WITH THE REQUIREMENTS OF A319 AMM 52-13-31-400-007.
- [SDR F3LA2008100700672](https://openairdocs.org/sdr/F3LA2008100700672.md): Blanking Plate · corroded · Sep 29, 2008 · N931FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > DURING C3 C-CHECK, INSPECTION NOTED THE R2 DOOR AFT GIRT BAR FITTING BLANKING PLATE IS CORRODED ON LOWER SURFACE. MAINTENANCE REMOVED GIRT BAR BLANKING PLATE AND INSTALLED NEW, REFERENCE WORK CARD C534103-01.
- [SDR F3LA2008100700671](https://openairdocs.org/sdr/F3LA2008100700671.md): Blanking Plate · corroded · Sep 29, 2008 · N931FR · Airbus A319111 · Emergency Equipment
  > DURING C3 C-CHECK, INSPECTION NOTED THE R2 FORWARD DOOR GIRT BAR FITTING BLANKING PLATE IS CORRODED ON UPPER AND LOWER SURFACE. MAINTENANCE REMOVED CORRODED GIRT BAR BLANKING PLATE AND INSTALLED NEW, REFERNCE WORK CARD C534103-01.
- [SDR F3LA200800134](https://openairdocs.org/sdr/F3LA200800134.md): Battery · inoperative · Apr 1, 2008 · N931FR · Airbus A319111 · Emergency Lighting
  > DURING HEAVY SERVICE CHECK INSPECTION REPORTED RIGHT OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT BATTERY IN ACCORDANCE WITH THE REQUIREMENTS OF A319 AMM 33-51-38-420-052. FOLLOWING INSTALLATION THE SYSTEM WAS T
- [SDR F3LA200700040](https://openairdocs.org/sdr/F3LA200700040.md): Latch · stuck · Mar 1, 2007 · N931FR · Airbus A319111 · Escape Slide
  > DURING C-2 CHECK INSPECTION, REPORTED GIRT BAR LATCH STUCK IN THE DOWN POSITION - L1 DOOR AFT LATCH. CLEANED GIRT BAR FITTING IAW AMM 12-21-12-100-006.
- [SDR F3LA200700030](https://openairdocs.org/sdr/F3LA200700030.md): Stowage Box · no test · Mar 1, 2007 · N931FR · Airbus A319111 · Crew Oxygen System
  > DURING C-2 CHECK, INSPECTION REPORTED 3RD CREW O2 STOWAGE BOX DID NOT FUNCTION DURING PUSH-TO-TEST. REPLACED 3RD CREW O2 STOWAGE BOX IAW 35-12-41, PB 401. OPS AND LEAK CHECK GOOD.

## 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 = 'N931FR' AND deregistration_id = 'N931FR-2016-01-14'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N931FR-2016-01-14/reports

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