# Service difficulty reports: N912FR, cancelled Feb 5, 2016

A list on [N912FR, cancelled Feb 5, 2016](https://openairdocs.org/deregistered/N912FR-2016-02-05.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 · 62 reports

- [SDR F3LA2015031101118](https://openairdocs.org/sdr/F3LA2015031101118.md): Battery Pack · failed · Mar 9, 2015 · N912FR · Airbus A319111 · Emergency Lighting
  > EPSU EMER LIGHT BATTERY 12WL, MIDDLE RT FAILED CAPACITY TEST ON A6 CHECK. R & R EPSU BATTERY 12WL IAW AMM 33-51-38-000-002A & 33-51-38-400-002A. OPERATIONS CHECKED GOOD. OK FOR SERVICE.
- [SDR F3LA2014100101073](https://openairdocs.org/sdr/F3LA2014100101073.md): Battery · discharged · Sep 28, 2014 · N912FR · Airbus A319111 · Emergency Lighting
  > AFT EPSU BATTERY FAILED A CHECK TASK CARD FFT-335100-03-1, CAPACITY CHECK. R & R BATTERY ASSEMBLY IAW AMM 33-51-39-000-005A & AMM 33-51-39-400-005-A.
- [SDR F3LA2014013001004](https://openairdocs.org/sdr/F3LA2014013001004.md): Skin · saturated · Jan 16, 2014 · N912FR · Airbus A319111 · Elevator, Plate/Skin
  > AIRCRAFT OUT OF SERVICE DUE TO C8 52 CHECK. RT ELEVATOR SN CC2574 THERMO GRAPHIC INSPECTION REVEALED INDICATIONS ON UPPER PANEL IRREGULAR IN SHAPE & BLACK IN COLOR. REPAIRED RT ELEVATOR UPPER PANEL AT 13 EACH AREAS OF LIQUID INGRESS IAW A319 SRM 55-20-00, PB
- [SDR F3LA2014013001003](https://openairdocs.org/sdr/F3LA2014013001003.md): Shear Plate · cracked · Jan 11, 2014 · N912FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > AIRCRAFT OUT OF SERVICE DUE TO C8 S2 CHECK. MAIN CABIN RT SIDE SHEAR PLATE FR 69 TO FR 70 IS CRACKED. REMOVED RT SHEAR PLATE FROM FR 69 - FR 70, REPLACED WITH NEW SHEAR PLATE IAW AIRBUS A319 SRM 51-42-11 PG 6 & 7.
- [SDR F3LA2014013001002](https://openairdocs.org/sdr/F3LA2014013001002.md): Floorbeam · corroded · Jan 11, 2014 · N912FR · Airbus A319111 · Fuselage Main, Floor Beam
  > AIRCRAFT OUT OF SERVICE DUE TO C8 S2 CHECK. MAIN CABIN AFT FLOOR SUPPORT BEAM AFT OF SEAT TRACK BEAM Y 1732 HAS CORROSION AT FR 68. REMOVED CORROSION ON AFT CABIN FLOOR SUPPORT BEAM IAW SRM 51-74-00 & FOUND TO BE OUT OF LIMITS IAW SRM 53-00-14 PB 101 FIG 102
- [SDR F3LA2014013001001](https://openairdocs.org/sdr/F3LA2014013001001.md): Floorbeam · corroded · Jan 11, 2014 · N912FR · Airbus A319111 · Fuselage Main, Floor Beam
  > AIRCRAFT OUT OF SERVICE DUE TO C8 S2 CHECK. MAIN CABIN FLOOR BEAM Y 1292 HAS CORROSION AT FR 16. R & R MAIN CABIN FLOOR BEAM LAW A319 SRM 51-72-11 PARA 5 & 6.
- [SDR F3LA2014013001000](https://openairdocs.org/sdr/F3LA2014013001000.md): Floorbeam · corroded · Jan 10, 2014 · N912FR · Airbus A319111 · Fuselage Main, Floor Beam
  > AIRCRAFT OUT OF SERVICE FOR C8 S2 CHECK. AFT CABIN FLOOR SUPPORT BEAM INBD OF SEAT TRACK BEAM Y 765 6 INCHES FWD OF FR 66 HAS CORROSION. R & R FLOOR BEAM AT AFT CABIN INBD OF SEAT TRACK Y 765 6 INCHES FWD OF FR 66 IAW A319 SRM 51-42-11.
- [SDR F3LA2014013000959](https://openairdocs.org/sdr/F3LA2014013000959.md): Shear Plate · corroded · Jan 4, 2014 · N912FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > AIRCRAFT OUT OF SERVICE DUE TO C8 S2 CHECK. AFT CABIN LT LATERAL SHEAR PLATE CRACKED AT FRAME 69. R & R LT LATERAL SHEAR PLATE WITH NEW PART IAW SRM 51-42-11, PAR 6, 7 & 13.
- [SDR F3LA2014013000958](https://openairdocs.org/sdr/F3LA2014013000958.md): Floorbeam · corroded · Jan 4, 2014 · N912FR · Airbus A319111 · Fuselage Main, Floor Beam
  > AIRCRAFT OUT OF SERVICE FOR C8 S2 CHECK. MAIN CABIN FLOOR BEAM Y 254 HAS CORROSION AT FR 18. REMOVED CORROSION AT MAIN CABIN FLOOR BEAM Y 254, FR L8 IAW SRM 51-74-00, 6 B ORIGINAL THICKNESS.079 INCHES, REMOVED.022 INCHES FOUND TO BE WITHIN LIMITS IAW SRM 5
- [SDR F3LA2014013000957](https://openairdocs.org/sdr/F3LA2014013000957.md): Floorbeam · corroded · Jan 2, 2014 · N912FR · Airbus A319111 · Fuselage Main, Floor Beam
  > AIRCRAFT OUT OF SERVICE DUE TO C8 S2 CHECK. FLOOR SUPPORT BEAM AFT OF SEAT TRACK Y 1292 HAS CORROSION AT FR 68. REMOVED FLOOR SUPPORT BEAM Y 1292 AT FR 68. REPLACED WITH NEW FLOOR SUPPORT BEAM PN D5347218920400 IAW A319 SRM 51-42-11 PG 7.
- [SDR F3LA2012083100782](https://openairdocs.org/sdr/F3LA2012083100782.md): Actuator · intermittent · Aug 28, 2012 · N912FR · Airbus A319111 · Landing Gear Actuator
  > ACFT LEFT C-CHECK AFTER COMPLETE SET LANDING GEAR TIME, DEPARTED. NLG DID NOT LOCK UP, GEAR DOORS DID NOT CLOSE. ACFT WAS PREPPED FOR GEAR DOWN FERRY FLIGHT. FERRY FLIGHT DID NOT OCCUR. DISCREPANCY WAS WORKED AT AIRPORT, ADJUSTMENTS MADE, REF NR 43936. OCF U
- [SDR F3LA2011022200609](https://openairdocs.org/sdr/F3LA2011022200609.md): Support · corroded · Feb 19, 2011 · N912FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > C-CHECK: NON ROUTINE 2994; LATERAL SHEAR PLATE, FRAME 69 - 70 RIGHT, HAS OUT OF LIMITS CORROSION AT FASTENER HOLES. REMOVED AND REPLACED SHEAR PLATE IAW AO-53EO-31434.
- [SDR F3LA2011022200608](https://openairdocs.org/sdr/F3LA2011022200608.md): Support · corroded · Feb 19, 2011 · N912FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > C-CHECK: NON ROUTINE # 29844; LATERAL SHEAR PLATE, FRAME 69 - 70 LEFT, HAS OUT OF LIMITS CORROSION AT FASTENER HOLES. REMOVED AND REPLACED SHEAR PLATE IAW AO-53EO-31434.
- [SDR F3LA2011022200610](https://openairdocs.org/sdr/F3LA2011022200610.md): Frame · corroded · Feb 19, 2011 · N912FR · Airbus A319111 · Fuselage Main, Frame
  > C-CHECK: NON ROUTINE 29941; FRAME 69 -Y765 HAS OUT OF LIMITS CORRORION AT FASTER HOLES, PER SRM 53-00-14 FIG 102. REMOVED AND REPLACE BEAM IAW A319 SRM 51-42-1.
- [SDR F3LA2010033000377](https://openairdocs.org/sdr/F3LA2010033000377.md): Thermostat · inoperative · Mar 29, 2010 · N912FR · Airbus A319111 · Pneumatic Distribution System
  > CAPTAIN REPORTED BLEED 2 FAULT AND LOSS OF CABIN PRESSURISATION. MAXIMUM CABIN ALTITUDE 10,500. FLIGHT NR 963 DIVERTED FOR AN UNSCHEDULED LANDING. MX TROUBLESHOOT NR 2 ENGINE BLEED AIR SYS IAW AMM 36-11-00-720-005 AND R & R THE NR 2 ENGINE FAN AIR VALVE THERM
- [SDR F3LA2009121600258](https://openairdocs.org/sdr/F3LA2009121600258.md): Epsu · malfunctioned · Dec 16, 2009 · N912FR · Airbus A319111 · Emergency Lighting
  > THE FLIGHT CREW NOTED THAT THE EMERGENCY EXIT LIGHTS AND ESCAPE PATH LIGHTS IN CABIN ARE CONTINUOUSLY ON WITH THE EMERGENCY EXIT LIGHT SWITCH IN THE ARM POSITION. MX PERFORMED AN OPS TEST OF THE EMERGENCY LIGHTING SYS AND THE OPS CHECK WAS GOOD IAW AMM 33-51-
- [SDR F3LA2009040100070](https://openairdocs.org/sdr/F3LA2009040100070.md): Window · cracked · Mar 30, 2009 · N912FR · Airbus A319111 · Flight Compartment Windows
  > AT FL 390, PILOT REPORTED THE RIGHT SLIDING WINDOW CRACKED IN BOTH PANES. MAINTENANCE REMOVED AND REPLACED THE RIGHT SLIDING WINDOW AND PERFORMED LEAK CHECK IAW AMM 56-12-11 PB 401.
- [SDR F3LA200800010](https://openairdocs.org/sdr/F3LA200800010.md): Cabin Pressure · fluctuates · Jan 16, 2008 · N912FR · Airbus A319111 · Cabin Pressure Control System
  > THE FLIGHT CREW REPORTED, DURING CLIMB-OUT, PRESSURIZATION FLUCTUATED 200 FEET PER MINUTE BETWEEN FLIGHT LEVEL 350 UP TO AND LEVELING AT FLIGHT LEVEL 380. AT THE SAME TIME, THE R2 DOOR PRESSURE LIGHT FLASHED AND THE SLIDE "DISARM" ILLUMINATED, ON THE LOWER EC
- [SDR F3LA200700404](https://openairdocs.org/sdr/F3LA200700404.md): Floor Panel · corroded · Dec 23, 2007 · N912FR · Airbus A319111 · Fuselage Floor Panel
  > DURING C4/S1 CHECK, INSPECTION REPORTED FLOOR PANEL 262FF CORRODED ON LOWER SURFACE. REMOVED AND REPLACED FLOOR PANEL 262FF IAW EO A0-53T-11996.
- [SDR F3LA200700393](https://openairdocs.org/sdr/F3LA200700393.md): Fastener · corroded · Dec 20, 2007 · N912FR · Airbus A319111 · Aerodynamic Fairings
  > DURING C4/S1 CHECK, INSPECTION REPORTED CORRODED FASTENERS THAT SECURE LIGHT TO RT WING-TO-BODY FAIRING 192DT. REMOVED AND REPLACED RT UPPER WING LIGHT COVER MOUNTING SCREWS ON PANEL NR 192DT.
- [SDR F3LA200700392](https://openairdocs.org/sdr/F3LA200700392.md): Fastener · corroded · Dec 20, 2007 · N912FR · Airbus A319111 · Aerodynamic Fairings
  > DURING C4/S1 CHECK, INSPECTION REPORTED RT WING-TO-BODY FAIRING 192DT HAD CORRODED FASTENERS AT LOWER SEAL. REMOVED AND REPLACED RT WING UPPER WING-TOO-BODY FAIRING PANEL NR 192DT LOWER SEAL MOUNTING SCREWS IAW 51-42-11.
- [SDR F3LA200700403](https://openairdocs.org/sdr/F3LA200700403.md): Plate · damaged · Dec 16, 2007 · N912FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > DURING C4/S1 CHECK, INSPECTION REPORTED AFT CARGO COMPARTMENT AFT BULKHEAD CROSSOVER BEAM HAD FASTENERS PULLING THROUGH THE CENTER PLATE. REMOVED AND REPLACED AFT CARGO COMPARTMENT AFT BULKHEAD CROSSOVER BEAM CENTER PLATE IAW SRM 51-42-11.
- [SDR F3LA200700391](https://openairdocs.org/sdr/F3LA200700391.md): Plate · corroded · Dec 16, 2007 · N912FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > DURING C4/S1 CHECK, INSPECTION REPORTED L2 DOOR FWD GIRT BAR LATCH FLOOR FILLER HAD A SMALL SPOT OF CORROSION. REMOVED AND REPLACED L2 DOOR FWD GIRT BAR LATCH FILLER PANEL IAW AMM 53-42-12-PB401.
- [SDR F3LA200700390](https://openairdocs.org/sdr/F3LA200700390.md): Plate · corroded · Dec 16, 2007 · N912FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > DURING C4/S1 CHECK, INSPECTION REPORTED R2 DOOR AFT GIRT BAR LATCH FILLER CORRODED. REMOVED AND REPLACED R2 DOOR AFT GIRT BAR LATCH FILLER PANEL IAW AMM 53-42-12-PB401.
- [SDR F3LA200700389](https://openairdocs.org/sdr/F3LA200700389.md): Plate · corroded · Dec 16, 2007 · N912FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > DURING C4/S1 CHECK, INSPECTION REPORTED L2 DOOR AFT GIRT BAR LATCH FILLER CORRODED. REMOVED AND REPLACED L2 DOOR AFT GIRT BAR LATCH FILLER IAW AMM 53-42-12-PB401.
- [SDR F3LA200700402](https://openairdocs.org/sdr/F3LA200700402.md): Blanking Plate · corroded · Dec 15, 2007 · N912FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > DURING C4/S1 CHECK, INSPECTION REPORTED F1 DOOR AFT GIRT BAR STOP LEVER FITTING BLANKING PLATE CORRODED ON BOTTOM SIDE. REMOVED AND REPLACED R1 DOOR AFT GIRT BAR STOP LEVER FITTING BLANKING PLATE IAW AMM 53-12-12-PB401.
- [SDR F3LA200700397](https://openairdocs.org/sdr/F3LA200700397.md): Floorbeam · corroded · Dec 15, 2007 · N912FR · Airbus A319111 · Fuselage Main, Floor Beam
  > DURING C4/S1 CHECK, INSPECTION REPORTED FLOORBEAM AT FR16, STA Y254, CORRODED ON THE TOP CAP. DETERMINED CORROSION TO BE OUT OF LIMITS IAW SRM 53-11-14. REMOVED AND REPLACED FLOORBEAM FROM FR12 THRU FR24, STA 254, IAW SRM 52-42-11 AND 51-72-11.
- [SDR F3LA200700388](https://openairdocs.org/sdr/F3LA200700388.md): Floor Panel · corroded · Dec 15, 2007 · N912FR · Airbus A319111 · Fuselage Floor Panel
  > DURING C4/S1 CHECK, INSPECTION REPORTED FLOOR PANEL 221FF (L1 DOOR) CORRODED ON BOTTOM SIDE. REMOVED AND REPLACED FLOOR PANEL 221FF IAW AMM 53-12-12-PB401.
- [SDR F3LA200700387](https://openairdocs.org/sdr/F3LA200700387.md): Floor Panel · corroded · Dec 15, 2007 · N912FR · Airbus A319111 · Fuselage Floor Panel
  > DURING C4/S1 CHECK, INSPECTION REPORTED FLOOR PANEL 222FF (R1 DOOR) CORRODED ON BOTTOM SIDE. REMOVED AND REPLACED FLOOR PANEL 222FF IAW AMM 53-12-12-PB401.
- [SDR F3LA200700386](https://openairdocs.org/sdr/F3LA200700386.md): Dummy Rail · corroded · Dec 15, 2007 · N912FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > DURING C4/S1 CHECK, INSPECTION REPORTED DUMMY RAIL AT Y503.2, FR 12 TO FR 16, CORRODED ON TOP. CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 53-11-14. REMOVED AND REPLACED DUMMY RAIL IAW SRM 51-42-11 AND 51-44-11.
- [SDR F3LA200700384](https://openairdocs.org/sdr/F3LA200700384.md): Floorbeam · corroded · Dec 15, 2007 · N912FR · Airbus A319111 · Fuselage Main, Floor Beam
  > DURING C4/S1 CHECK, INSPECTION REPORTED CORROSION ON FLOORBEAM AT Y1292 AND FR16, AT ATTACH POINT. REMOVED AND REPLACED FLOORBEAM AT Y1292 IAW SRM 51-42-11.
- [SDR F3LA200700401](https://openairdocs.org/sdr/F3LA200700401.md): Support Beam · bent · Dec 14, 2007 · N912FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > DURING C4/S1 CHECK, INSPECTION REPORTED AFT CARGO FWD BULKHEAD PANEL SUPPORT BEAM AT APPROX STR 42L, FR47 TO FR51, BENT. REMOVED, FABRICATED AND INSTALLED REPLACEMENT SUPPORT BEAM IAW SRM 51-42-11, SRM 51-44-11, 51-75-12 AND DRAWING D53974679.
- [SDR F3LA200700400](https://openairdocs.org/sdr/F3LA200700400.md): Lock Fastener · corroded · Dec 14, 2007 · N912FR · Airbus A319111 · Emergency Equipment
  > DURING C4/S1 CHECK, INSPECTION REPORTED L2 DOOR SILL AFT GIRT BAR FITTING CORRODED AT LOCK FASTENER. REMOVED AND REPLACED FASTENER IAW SRM 51-42-11.
- [SDR F3LA200700399](https://openairdocs.org/sdr/F3LA200700399.md): Shear Plate · corroded · Dec 14, 2007 · N912FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > DURING C4/S1 CHECK, INSPECTION REPORTED SHEAR PLATE AT Y1292, BETWEEN FR69 AND FR70, CORRODED. REMOVED AND REPLACED SHEAR PLATE AND FLOORBEAM IAW SRM 51-42-11 AND EA A9-53R-12329.
- [SDR F3LA200700398](https://openairdocs.org/sdr/F3LA200700398.md): Floorbeam · corroded · Dec 14, 2007 · N912FR · Airbus A319111 · Fuselage Main, Floor Beam
  > DURING C4/S1 CHECK, INSPECTION REPORTED FLOORBEAM AT Y765, FR68, CORRODED. DETERMINED CORROSION TO BE OUT OF LIMITS IAW 53-00-14. REMOVED AND REPLACED FLOOR BEAM AT Y768 IAW SRM 51-42-11.
- [SDR F3LA200700396](https://openairdocs.org/sdr/F3LA200700396.md): Floorbeam · corroded · Dec 14, 2007 · N912FR · Airbus A319111 · Fuselage Main, Floor Beam
  > DURING C4/S1 CHECK, INSPECTION REPORTED FLOORBEAM AT Y1292, FR68, CORRODED. DETERMINED CORROSION TO BE OUT OF LIMITS IAW SRM 53-00-14, PAR 4 B. REMOVED AND REPLACED FLOORBEAM Y1292 AT FR 68-69 IAW SRM 51-42-11 AND 51-44-11.
- [SDR F3LA200700395](https://openairdocs.org/sdr/F3LA200700395.md): Sill · corroded · Dec 14, 2007 · N912FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > DURING C4/S1 CHECK, INSPECTION REPORTED L2 DOOR SILL CORRODED AT VARIOUS LOCATIONS BETWEEN FR 66 AND FR 68. REMOVED AND REPLACED L2 DOOR SILL PLATE IAW SRM 51-42-11, 51-44-11, DRAWING D53480505 AND EA A9-53R-12330.
- [SDR F3LA200700394](https://openairdocs.org/sdr/F3LA200700394.md): Floorbeam · corroded · Dec 14, 2007 · N912FR · Airbus A319111 · Fuselage Main, Floor Beam
  > DURING C4/S1 CHECK, INSPECTION REPORTED FLOORBEAM AT Y1292, FR66, CORRODED AT NUTPLATE HOLES. REMOVED AND REPLACED FLOORBEAM AT Y1292, FR66, IAW SRM 51-42-11.
- [SDR F3LA200700383](https://openairdocs.org/sdr/F3LA200700383.md): Attach Bolt · corroded · Dec 14, 2007 · N912FR · Airbus A319111 · Lavatories
  > DURING C4/S1 CHECK, INSPECTION REPORTED LWR ATTACHMENT BOLT ON INBD AFT CORNER OF LAV "A" SEVERELY CORRODED. REMOVED AND REPLACED BOLT IAW AMM 25-41-41-PB401.
- [SDR F3LA200700381](https://openairdocs.org/sdr/F3LA200700381.md): Shear Plate · corroded · Dec 14, 2007 · N912FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > DURING C4/S1 CHECK, INSPECTION REPORTED SHEAR PLATE AT BS -Y1292 BETWEEN FR 69 AND FR 70 CORRODED. CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 53-41-14-101. REMOVED AND INSTALLED REPLACEMENT SHEAR PLATE IAW SRM 51-42-11, SRM 51-44-11 AND EA A9-53R-12329.
- [SDR F3LA200700380](https://openairdocs.org/sdr/F3LA200700380.md): Floorbeam · corroded · Dec 14, 2007 · N912FR · Airbus A319111 · Fuselage Main, Floor Beam
  > DURING C4/S1 CHECK, INSPECTION REPORTED FLOORBEAM AT BS -Y1292 HAD CORROSION AT NUT PLATE HOLES BETWEEN FR 68 AND FR 69. FOUND CORROSION TO BE OUT OF LIMITS IAW SRM 53-00-14, FIG. 102. REMOVED AND REPLACED FLOORBEAM IAW SRM 51-42-11.
- [SDR F3LA200700378](https://openairdocs.org/sdr/F3LA200700378.md): Rivet · sheared · Dec 14, 2007 · N912FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > DURING C4/S1 CHECK, INSPECTION REPORTED SHEARED RIVETS ON WEB AT STA. -Y1292 BETWEEN FR68 AND FR69. REMOVED AND REPLACED RIVETS IAW A319 SRM 51-44-11, 51-46-11 AND EA A9-53R-12329.
- [SDR F3LA200700405](https://openairdocs.org/sdr/F3LA200700405.md): Mount Bolt · corroded · Dec 13, 2007 · N912FR · Airbus A319111 · Lavatories
  > DURING C4/S1 CHECK, INSPECTION REPORTED LAV E LOWER FLOOR MOUNT BOLTS CORRODED. REMOVED AND REPLACED CORRODED FLOOR MOUNT BOLTS IN LAV E IAW AMM 25-43-42-PB401.
- [SDR F3LA200700382](https://openairdocs.org/sdr/F3LA200700382.md): Bolt · corroded · Dec 13, 2007 · N912FR · Airbus A319111 · Lavatories
  > DURING C4/S1 CHECK, INSPECTION REPORTED LAV "D" MOUNT BOLTS CORRODED. REMOVED AND REPLACED CORRODED MOUNT BOLTS IAW AMM 25-43-41-PB401.
- [SDR F3LA200700410](https://openairdocs.org/sdr/F3LA200700410.md): Battery Pack · no test · Dec 12, 2007 · N912FR · Airbus A319111 · Emergency Lighting
  > DURING C4/S1 CHECK, INSPECTION REPORTED AFT EMERGENCY LIGHT BATTERY FAILED CAPACITY CHECK. REMOVED AND INSTALLED SERVICEABLE AFT EMERGENCY LIGHT BATTERY PACK IAW AMM 33-51-38-000-002. PERFORMED BITE TEST OF AFT EMERGENCY LIGHT EPSU/BATTERY PACK IAW AMM 33-51
- [SDR F3LA200700409](https://openairdocs.org/sdr/F3LA200700409.md): Battery Pack · failed · Dec 12, 2007 · N912FR · Airbus A319111 · Emergency Lighting
  > DURING C4/S1 CHECK, INSPECTION REPORTED LT OVERWING EMERGENCY LIGHT BATTERY FAILED CAPACITY CHECK. REMOVED AND INSTALLED SERVICEABLE BATTERY IN LT OVERWING EPSU IAW AMM 33-51-38-420-052. PERFORMED BITE TEST IAW AMM 33-51-38-400-002 AND TESTED GOOD.
- [SDR F3LA200700408](https://openairdocs.org/sdr/F3LA200700408.md): Battery Pack · failed · Dec 12, 2007 · N912FR · Airbus A319111 · Emergency Lighting
  > DURING C4/S1 CHECK, INSPECTION REPORTED RT OVERWING EMERGENCY LIGHT BATTERY FAILED CAPACITY CHECK. REMOVED AND INSTALLED SERVICEABLE BATTERY PACK IN RT OVERWING EPSU IAW AMM 33-51-38-400-002. PERFORMED BITE TEST OF RT OVERWING EMERGENCY LIGHT EPSU/BATTERY PA
- [SDR F3LA200700407](https://openairdocs.org/sdr/F3LA200700407.md): Battery Pack · failed · Dec 12, 2007 · N912FR · Airbus A319111 · Emergency Lighting
  > DURING C4/S1 CHECK, INSPECTION REPORTED FWD EMERGENCY LIGHT BATTERY FAILED CAPACITY CHECK. REMOVED AND INSTALLED SERVICEABLE BATTERY IN FWD EPSU (10WL) IAW AMM 33-51-38-400-002. PERFORMED A BITE TEST OF THE FWD EMERGENCY LIGHT EPSU/BATTERY PACK IAW AMM 33-51
- [SDR F3LA200700406](https://openairdocs.org/sdr/F3LA200700406.md): Release Cable · inoperative · Dec 12, 2007 · N912FR · Airbus A319111 · Escape Slide
  > DURING C4/S1 CHECK, INSPECTION REPORTED RT OVERWING EXIT SLIDE RELEASE CABLE WOULD NOT RETRACT. REMOVED AND REPLACED RT OVERWING SLIDE RELEASE CABLE IAW AMM 25-62-43-PB401.
- [SDR F3LA200700377](https://openairdocs.org/sdr/F3LA200700377.md): Release Cable · inoperative · Dec 12, 2007 · N912FR · Airbus A319111 · Escape Slide
  > DURING C4/S1 CHECK, INSPECTION REPORTED LT OVERWING EMERGENCY EXIT SLIDE RELEASE CABLE WOULD NOT RETRACT. REMOVED AND REPLACED LT OVERWING EXIT SLIDE RELEASE CABLE IAW AMM 25-62-43-000-001. COMPLETED ADJUSTMENT AND OPERATIONAL CHECK OF SLIDE RELEASE CABLE IA

Next page: https://openairdocs.org/deregistered/N912FR-2016-02-05/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 = 'N912FR' AND deregistration_id = 'N912FR-2016-02-05'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N912FR-2016-02-05/reports

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