# Service difficulty reports: N934FR, cancelled Sep 12, 2016

A list on [N934FR, cancelled Sep 12, 2016](https://openairdocs.org/deregistered/N934FR-2016-09-12.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 · 60 reports

- [SDR F3LA2015041501129](https://openairdocs.org/sdr/F3LA2015041501129.md): Hydraulic Line · chafed · Apr 12, 2015 · N934FR · Airbus A319111 · Hydraulic System, Main
  > REFERENCE LOG PAGE 802478 ITEM NR 1. AIR TURN BACK AT 14:55 Z HYD RESERVOIR LOW LEVEL. YELLOW HYD QTY WENT TO ZERO JUST AFTER TAKEOFF. R & R HYD PRESS LINE, PN D2901005100740 & AFT CLAMP BLOCK PN D2901013500000.
- [SDR F3LA2014022401019](https://openairdocs.org/sdr/F3LA2014022401019.md): Battery · discharged · Feb 24, 2014 · N934FR · Airbus A319111 · Emergency Lighting
  > EMERGENCY POWER SUPPLY UNIT LT 11WL FAILED BATTERY DURING HEAVY SERVICE CHECK. R & R EPSU LT 11WL BATTERY ASSEMBLY IAW AMM 33-51-39-000-005A & AMM 33-51-39-400-005A.
- [SDR F3LA2014022401018](https://openairdocs.org/sdr/F3LA2014022401018.md): Battery · discharged · Feb 24, 2014 · N934FR · Airbus A319111 · Emergency Lighting
  > EMERGENCY POWER SUPPLY UNIT FWD LT BATTERY FAULT DURING HEAVY SERVICE CHECK. R & R EPSU FWD LT 10WL BATTERY ASSEMBLY, IAW AMM 33-51-39-000-005A & AMM 33-51-39-400-005A.
- [SDR F3LA2013032000838](https://openairdocs.org/sdr/F3LA2013032000838.md): Power Supply · inoperative · Mar 18, 2013 · N934FR · Airbus A319111 · Emergency Lighting
  > EMERGENCY LIGHT FAILED TEST, R & R POWER SUPPLY IAW AMM 33-51-00-710-001. OPS CHECKED NORMAL.
- [SDR F3LA2012061200768](https://openairdocs.org/sdr/F3LA2012061200768.md): Power Unit · overheated · Jun 7, 2012 · N934FR · Airbus A319111 · Hydraulic System, Main
  > GREEN SERVICE, ENG 1 OVERHEAT, TROUBLE SHOT GREEN HYD SYS IAW TSM 29-11-00-810-800-A. REPLACED PTU IAW AMM 29-23-41 PB401. LEAK AND OPS CHECKED NORMAL.
- [SDR F3LA2012060800766](https://openairdocs.org/sdr/F3LA2012060800766.md): Hose · failed · Jun 4, 2012 · N934FR · Airbus A319111 · Landing Gear Door Actuator
  > AFTER GEAR RETRACTION ECAM - "HYD G ENG 1 PUMP LO PR". THIS WAS FOLLOWED BY "HYD GR RSVR LO LVL". AIR TURN BACK. PERFORMED ECAM ACTIONS AND RETURNED TO DEPARTURE. R & R RT MLG DOOR ACTUATOR FLEXIBLE HOSE ASSY IAW AMM 32-31-39 PB 401. OPS AND LEAK CHECKS GOOD.
- [SDR F3LA2010090100496](https://openairdocs.org/sdr/F3LA2010090100496.md): Roll Pin · broken · Sep 3, 2010 · N934FR · Airbus A319111 · Escape Slide
  > C-CHECK: NON ROUTINE N0785. LT EMERGENCY EXIT SLIDE ARMING MECHANISM WILL NOT STAY IN ARMED POSITION. R & R SLIDE RELEASE MECHANISM SPRING PIN IAW AMM 52-21-11-000-003 AND AMM 52-11-420-051. PERFORMED SLIDE MECHANISM OPS CHECK IAW AMM 52-21-00-720-001. NO DEFE
- [SDR F3LA2010090100495](https://openairdocs.org/sdr/F3LA2010090100495.md): Sill · corroded · Sep 3, 2010 · N934FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > C-CHECK: NON ROUTINE N0590, R2 DOOR SILL TRAY AT FRAME 66 HAS 1 AREA OF CORROSION AROUND NUT PLATE HOLE. REMOVED CORROSION IAW SRM 51-74-00. OPENED HOLE TO.310, BLEND OUT MEASURES 1 INCH X 1.5 INCH X.020 WITHIN LIMITS IAW 53-00-14 FIG 102. REPROTECTED IAW SR
- [SDR F3LA2010090100494](https://openairdocs.org/sdr/F3LA2010090100494.md): Seat Track · corroded · Sep 3, 2010 · N934FR · Airbus A319111 · Fuselage, Seat/Cargo Attach Fittings
  > C-CHECK: NON ROUTINE N0586, AFT MAIN CABIN, RT SEAT TRACK, YR2 DOOR SILL TRAY AT FRAME 66-Y122 AT FRAME 68 HAS 2 AREAS OF CORROSION ON UPPER SURFACE. REMOVED CORROSION IAW SRM 51-74-00. BLEND OUT MEASURES 2.5 INCH X 1.5 INCH X.012 INCH AND 3 INCH X 1.5 INCH
- [SDR F3LA2010090100493](https://openairdocs.org/sdr/F3LA2010090100493.md): Seat Track · corroded · Sep 3, 2010 · N934FR · Airbus A319111 · Fuselage, Seat/Cargo Attach Fittings
  > C-CHECK, NON ROUTINE N0567, AFT MAIN CABIN RT SEAT TRACK YR2 DOOR SILL TRAY AT FRAME 66-Y122 AT FRAME 68 HAS 2 AREAS OF CORROSION ON UPPER SURFACE. REMOVED CORROSION IAW SRN 51-74-00. BLEND OUT MEASURES 2.5 INCH X 1.5 INCH X.012 INCH AND 3 INCH X 1.5 INCH X.
- [SDR F3LA2010083100489](https://openairdocs.org/sdr/F3LA2010083100489.md): Floor Panel · cut · Aug 24, 2010 · N934FR · Airbus A319111 · Fuselage Floor Panel
  > C-CHECK; REF NON-ROUTINE N0681 AFT CARGO FLOOR PANEL 161BF HAS A 2 INCH CUT. REPAIRED 2 INCH CUT BY APPLYING RESIN AND GLASS CLOTH ON PANEL 161BF IAW SRM 53-02-00 PARA 8B. PREPPED AND RESTORED PROTECTIVE COATINGS IAW SRM 51-75-12 PARA 3A.
- [SDR F3LA2010083100488](https://openairdocs.org/sdr/F3LA2010083100488.md): Floor Panel · cut · Aug 24, 2010 · N934FR · Airbus A319111 · Fuselage Floor Panel
  > C-CHECK; REF NON-ROUTINE N680 AFT CARGO FLOOR PANEL 162CF HAS A 7 INCH CUT. REPAIRED 7 INCH CUT BY APPLYING RESIN AND GLASS CLOTH IAW SRM 53-02-00 PARAGRAPH 8B. PREPPED AND RESTORED PROTECTIVE COATINGS IAW SRM 51-75-12 PARAGRAPH 3A ON PANEL 162CF.
- [SDR F3LA2010083100487](https://openairdocs.org/sdr/F3LA2010083100487.md): Transition Panel · punctured · Aug 24, 2010 · N934FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > C-CHECK; REFERENCE NON-ROUTINE N0696 BULK CARGO PIT SIDE TRANSITION PANEL HAS 2 EACH 1 INCH PUNCTURES. FABRICATED REPLACEMENT PANEL 161EF IAW MCG 1RM 9701 REV G.
- [SDR F3LA2010031400365](https://openairdocs.org/sdr/F3LA2010031400365.md): Epsu · inoperative · Mar 14, 2010 · N934FR · Airbus A319111 · Emergency Lighting
  > DURING HEAVY SERVICE CHECK, MX NOTED EMERGENCY ISLE LIGHTS ON SEATS ABC ROWS 23, 22, 19, 18, 15, AND 14 ARE INOPERATIVE. MX R & R EMERGENCY POWER SUPPLY UNIT 13WL IAW AMM 33-51-38-000-001 AND 33-51-38-400-001. TEST OK.
- [SDR F3LA2009122900273](https://openairdocs.org/sdr/F3LA2009122900273.md): Adiru · faulty · Dec 26, 2009 · N934FR · Airbus A319111 · Airspeed/Mach Indicator
  > DURING CLIMB OUT, THE FLIGHT CREW RECEIVED AN IR1 FAULT. THE ACFT RETURNED TO DEPARTURE AND MX TROUBLESHOT AND REPLACED ADIRU 1 AT 1FP1 IAW AMM 34-12-34, AMM 34-14-00-740-001 AND AMM 34-13-00-740-002.
- [SDR F3LA2009071400099](https://openairdocs.org/sdr/F3LA2009071400099.md): Heat Exchanger · leaking · Jul 11, 2009 · N934FR · Airbus A319111 · Pneumatic Distribution System
  > REF LOG PAGE 446358, DURING CLIMB OUT, PILOT REPORTED AN ELECTRONIC CENTRALIZED ACFT MONITORING MESSAGE FOR "AIR ENGINE BLEED LEAK" AND MADE AN AIR RETURN TO DEPARTURE. MX REMOVED AND REPLACED THE NR 1 ENGINE PRECOOLER HEAT EXCHANGER ALONG WITH ASSOCIATED SEA
- [SDR F3LA2009032700068](https://openairdocs.org/sdr/F3LA2009032700068.md): Skin · damaged · Mar 13, 2009 · N934FR · Airbus A319111 · Fuselage Main, Plate/Skin
  > DURING OPERATIONS IN DEN, THE AIRCRAFT SUSTAINED BIRD STRIKE DAMAGE LOCATED ON THE RIGHT FORWARD FUSELAGE AT FRAME 5. 6.50 INCHES ABOVE Z508. MAINTENANCE CUT OUT AFFECTED SKIN, FABRICATED REPAIR DOUBLER, AND INSTALLED IAW ENGINEERING AUTHORIZATION A9-53R-3100
- [SDR F3LA2009032700067](https://openairdocs.org/sdr/F3LA2009032700067.md): Skin · damaged · Mar 13, 2009 · N934FR · Airbus A319111 · Fuselage Main, Plate/Skin
  > DURING OPERATIONS IN DEN, THE AIRCRAFT SUSTAINED BIRD STRIKE DAMAGE LOCATED ON THE RIGHT FORWARD FUSELAGE AT FRAME 4, 6.675 INCHES ABOVE Z508. MAINTENANCE CUT OUT AFFECTED SKIN, FABRICATED REPAIR DOUBLER AND INSTALLED IAW ENGINEERING AUTHORIZATION A9-53R-3100
- [SDR F3LA2009012900017](https://openairdocs.org/sdr/F3LA2009012900017.md): Plate · corroded · Jan 28, 2009 · N934FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > INSPECTION NOTED THE R2 DOOR AFT GIRT BAR BLANKING PLATE HAS CORROSION. MAINTENANCE REMOVED AND REPLACED BLANKING PLATE IAW AMM 52-13-31-400-003.
- [SDR F3LA2009012900016](https://openairdocs.org/sdr/F3LA2009012900016.md): Plate · corroded · Jan 28, 2009 · N934FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > INSPECTION NOTED THE R2 DOOR FORWARD GIRT BAR FITTING BLANKING PLATE HAS CORROSION. MAINTENANCE REMOVED AND REPLACED BLANKING PLATE IAW AMM 52-13-31-400-007.
- [SDR F3LA2009012900015](https://openairdocs.org/sdr/F3LA2009012900015.md): Floor Panel · corroded · Jan 28, 2009 · N934FR · Airbus A319111 · Fuselage Floor Panel
  > INSPECTION NOTED THE L2 DOOR FLOOR PANEL 261FF HAS CORROSION. MAINTENANCE REMOVED AND REPLACED PANEL 261FF WITH NEW PER WORK CARD C534103-2 AND AMM 53-42-12-400-002.
- [SDR F3LA2009012700014](https://openairdocs.org/sdr/F3LA2009012700014.md): Plate · corroded · Jan 27, 2009 · N934FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > INSPECTION NOTED THAT THE L2 AFT DOOR GIRT BAR FITTING BLANKING PLATE HAS CORROSION. MAINTENANCE REMOVED AND REPLACED THE BLANKING PLATE IAW SRM 51-42-00, AMM 52-13-31-400-003 AND AMM 53-13-00-820-001.
- [SDR F3LA2009012700013](https://openairdocs.org/sdr/F3LA2009012700013.md): Plate · corroded · Jan 27, 2009 · N934FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > INSPECTION NOTED THAT THE L2 FORWARD DOOR GIRT BAR FITTING BLANKING PLATE HAS CORROSION. MAINTENANCE REMOVED AND REPLACED THE BLANKING PLATE IAW SRM 51-42-00, AMM 52-13-31-400-003 AND AMM 52-13-00-820-001.
- [SDR F3LA2009012600012](https://openairdocs.org/sdr/F3LA2009012600012.md): Beam · corroded · Jan 25, 2009 · N934FR · Airbus A319111 · Fuselage Main, Frame
  > INSPECTION NOTED THE AFT GALLEY, RT BEAM AT FRAME 68 AND -1292, OUTBOARD ATTACHMENT HOLE HAS CORROSION AROUND IT. MAINTENANCE REPAIRED AREA IAW ENGINEERING AUTHORIZATION A9-53R-30890.
- [SDR F3LA2009012600011](https://openairdocs.org/sdr/F3LA2009012600011.md): Floorbeam · corroded · Jan 25, 2009 · N934FR · Airbus A319111 · Fuselage Main, Floor Beam
  > INSPECTION NOTED CORROSION AT NUTPLATES ON TOP OF FLOORBEAM LOCATED BETWEEN FRAME 66 AND FRAME 67 AT Y1292 LEFT. MAINTENANCE REMOVED AND REPLACED BEAM IAW SRM 51-42-11, 51-40-00, 51-49-00, 51-21-11 AND ENGINEERING AUTHORIZATION A9-53T-30392.
- [SDR F3LA2009012600010](https://openairdocs.org/sdr/F3LA2009012600010.md): Stringer · cracked · Jan 25, 2009 · N934FR · Airbus A319111 · Nacelle/Pylon, Frame/Spar/Rib
  > INSPECTION NOTED NR 2 ENGINE UPPER PYLON RIB 06 FORWARD INBOARD STRINGER WAS CRACKED AT CORNER HOLE. MAINTENANCE PERFORMED REPAIR BY FABRICATING SUPPORT ANGLE AND INSTALLING PER SRM 51-42-11 AND 54-52-12.
- [SDR F3LA2009012600009](https://openairdocs.org/sdr/F3LA2009012600009.md): Shear Plate · corroded · Jan 24, 2009 · N934FR · Airbus A319111 · Fuselage Main, Structure
  > INSPECTION NOTED SHEAR PLATE CORROSION IN THE AFT GALLEY, RT FROM FRAME 69 TO FRAME 70. MAINTENANCE REMOVED AND REPLACED SHEAR PLATE IAW SRM 51-42-00, 51-72-11 AND 53-41-14.
- [SDR F3LA2009012600008](https://openairdocs.org/sdr/F3LA2009012600008.md): Shear Plate · corroded · Jan 24, 2009 · N934FR · Airbus A319111 · Fuselage Main, Structure
  > INSPECTION NOTED SHEAR PLATE CORROSION IN THE AFT GALLEY, LT FROM FRAME 69 TO FRAME 70. MAINTENANCE REMOVED AND REPLACED THE SHEAR PLATE IAW SRM 51-42-00, 51-72-11 AND 53-41-14.
- [SDR F3LA2009012600007](https://openairdocs.org/sdr/F3LA2009012600007.md): Support Frame · corroded · Jan 24, 2009 · N934FR · Airbus A319111 · Fuselage Main, Structure
  > INSPECTION NOTED CORROSION ON THE SHEAR PLATE SUPPORT FRAME, LOCATED IN THE AFT GALLEY, LT FROM FRAME 69 TO FRAME 70. MAINTENANCE REMOVED AND REPLACED SUPPORT FRAME IAW SRM 51-42-00, 51-72-11 AND 53-41-14.
- [SDR F3LA2009012600006](https://openairdocs.org/sdr/F3LA2009012600006.md): Support Frame · corroded · Jan 24, 2009 · N934FR · Airbus A319111 · Fuselage Main, Structure
  > INSPECTION NOTED CORROSION ON THE SHEAR PLATE SUPPORT FRAME, LOCATED IN THE AFT GALLEY, RT FROM FRAME 69 TO FRAME 70. MAINTENANCE REMOVED AND REPLACED SUPPORT FRAME IAW SRM 51-42-00.
- [SDR F3LA2008123000729](https://openairdocs.org/sdr/F3LA2008123000729.md): Manifold · leaking · Dec 25, 2008 · N934FR · Airbus A319111 · Hydraulic System, Auxiliary
  > PILOT RETURNED TO BLOCK DUE TO LOSS OF GREEN SYSTEM HYDRAULIC FLUID. MAINTENANCE REMOVED AND REPLACED LANDING GEAR SAFETY VALVE MANIFOLD IAW A319 AMM 32-32-17 PB 401. OPERATION AND LEAK CHECK NORMAL.
- [SDR F3LA200700169](https://openairdocs.org/sdr/F3LA200700169.md): Slide · loose · Jul 2, 2007 · N934FR · Airbus A319111 · Escape Slide
  > DURING C-2 CHECK, INSPECTION REPORTED L1 DOOR SLIDE CAME UNPACKED. REPLACED L1 DOOR SLIDE IAW AMM 25-62-44-000-002. OPERATIONAL CHECK GOOD.
- [SDR F3LA200700168](https://openairdocs.org/sdr/F3LA200700168.md): Floor Panel · delaminated · Jun 28, 2007 · N934FR · Airbus A319111 · Fuselage Floor Panel
  > DURING C-2 CHECK, INSPECTION REPORTED AFT CARGO COMPARTMENT FLOOR PANEL 151ZG DELAMINATED AT RT SIDE OF PANEL AT CARGO DOOR OPENING. REPLACED FLOOR PANEL 151ZG IAW AMM 53-42-14-000-001.
- [SDR F3LA200700162](https://openairdocs.org/sdr/F3LA200700162.md): Transition Panel · punctured · Jun 28, 2007 · N934FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > DURING C-2 CHECK, INSPECTION REPORTED AFT CARGO COMPARTMENT TRANSITION PANEL 161CF DAMAGED. REPAIRED PUNCTURES IN TRANSITION PANEL 161CF IAW SRM 53-02-00, PB 201, PARA 8 C., FIG 204.
- [SDR F3LA200700161](https://openairdocs.org/sdr/F3LA200700161.md): Transition Panel · punctured · Jun 28, 2007 · N934FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > DURING C-2 CHECK, INSPECTION REPORTED AFT CARGO COMPARTMENT TRANSITION PANEL 151HE DAMAGED. REPAIRED PUNCTURES IN TRANSITION PANEL 151HE IAW SRM 53-02-00, PB 201, PARA 8 C., FIG 204.
- [SDR F3LA200700160](https://openairdocs.org/sdr/F3LA200700160.md): Transition Panel · punctured · Jun 28, 2007 · N934FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > DURING C-2 CHECK, INSPECTION REPORTED AFT CARGO COMPARTMENT TRANSITION PANEL 151DE DAMAGED. REPAIRED PUNCTURES IN TRANSITION PANEL 151DE IAW SRM 53-02-00, PB 201, PARA 8 C., FIG 204.
- [SDR F3LA200700167](https://openairdocs.org/sdr/F3LA200700167.md): Floor Panel · damaged · Jun 27, 2007 · N934FR · Airbus A319111 · Fuselage Floor Panel
  > DURING C-2 CHECK, INSPECTION REPORTED AFT CARGO COMPARTMENT FLOOR PANEL 151CE DAMAGED. REPLACED FLOOR PANEL 151CE IAW AMM 53-42-11-400-001.
- [SDR F3LA200700166](https://openairdocs.org/sdr/F3LA200700166.md): Transition Panel · punctured · Jun 27, 2007 · N934FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > DURING C-2 CHECK, INSPECTION REPORTED AFT CARGO COMPARTMENT TRANSITION PANEL 161BF PUNCTURED ON TOP SKIN. REPLACED TRANSITION PANEL 161BF IAW AMM 53-42-14-400-001.
- [SDR F3LA200700165](https://openairdocs.org/sdr/F3LA200700165.md): Release Cable · out of adjust · Jun 27, 2007 · N934FR · Airbus A319111 · Escape Slide
  > DURING C-2 CHECK, INSPECTION REPORTED OPERATIONAL TESTS OF BOTH OVERWING RELEASE SLIDE CABLES FAILED. ADJUSTED LT AND RT EMERGENCY SLIDE EXIT RELEASE CABLES IAW AMM 25-62-43-820-050 AND CHECKED GOOD.
- [SDR F3LA200700164](https://openairdocs.org/sdr/F3LA200700164.md): Transition Panel · punctured · Jun 27, 2007 · N934FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > DURING C-2 CHECK, INSPECTION REPORTED HOLES IN AFT CARGO COMPARTMENT FWD RT LOWER TRANSITION PANEL 152WG. REPLACED TRANSITION PANEL 152WG IAW AMM 53-42-14-400-001.
- [SDR F3LA200700163](https://openairdocs.org/sdr/F3LA200700163.md): Transition Panel · punctured · Jun 27, 2007 · N934FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > DURING C-2 CHECK, INSPECTION REPORTED HOLES IN AFT CARGO COMPARTMENT LT UPPER TRANSITION PANEL 151UG. REPLACED TRANSITION PANEL 151UG IAW AMM 53-42-14-000-001.
- [SDR F3LA200700159](https://openairdocs.org/sdr/F3LA200700159.md): Transition Panel · punctured · Jun 27, 2007 · N934FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > DURING C-2 CHECK, INSPECTION REPORTED AFT CARGO COMPARTMENT TRANSITION PANEL 151AE DAMAGED. REPAIRED PUNCTURES IN TRANSITION PANEL 151AE IAW SRM 53-02-00, PB 201, PARA 8 C., FIG 204.
- [SDR F3LA200700158](https://openairdocs.org/sdr/F3LA200700158.md): Floor Panel · punctured · Jun 27, 2007 · N934FR · Airbus A319111 · Fuselage Floor Panel
  > DURING C-2 CHECK, INSPECTION REPORTED TOP SKIN PUNCTURED ON AFT CARGO COMPARTMENT FLOOR PANEL 161NF. REPAIRED PUNCTURES ON FLOOR PANEL 161NF IAW SRM 53-02-00, PB 201, PARA 8 C., FIG 204.
- [SDR F3LA200700157](https://openairdocs.org/sdr/F3LA200700157.md): Floor Panel · damaged · Jun 27, 2007 · N934FR · Airbus A319111 · Fuselage Floor Panel
  > DURING C-2 CHECK, INSPECTION REPORTED HOLES IN TOP SURFACE OF AFT CARGO COMPARTMENT FLOOR PANEL 151PE. REPAIRED HOLES IN FLOOR PANEL 151PE IAW SRM 53-02-00, PB201, PARA 8 C., FIG 204.
- [SDR F3LA200700156](https://openairdocs.org/sdr/F3LA200700156.md): Floor Panel · damaged · Jun 27, 2007 · N934FR · Airbus A319111 · Fuselage Floor Panel
  > DURING C-2 CHECK, INSPECTION REPORTED HOLES IN TOP SURFACE OF AFT CARGO COMPARTMENT FLOOR PANEL 151VG. REPAIRED HOLES IN FLOOR PANEL 151VG IAW SRM 53-02-00, PB 201, PARA 8 C., FIG 204.
- [SDR F3LA200700155](https://openairdocs.org/sdr/F3LA200700155.md): Floor Panel · damaged · Jun 27, 2007 · N934FR · Airbus A319111 · Fuselage Floor Panel
  > DURING C-2 CHECK, INSPECTION REPORTED HOLES IN TOP SURFACE OF AFT CARGO COMPARTMENT FLOOR PANEL 161NF. REPAIRED HOLES IAW SRM 53-02-00, FIG 204.
- [SDR F3LA200700154](https://openairdocs.org/sdr/F3LA200700154.md): Floor Panel · damaged · Jun 27, 2007 · N934FR · Airbus A319111 · Fuselage Floor Panel
  > DURING C-2 CHECK, INSPECTION REPORTED HOLES IN TOP SURFACE OF AFT CARGO COMPARTMENT FLOOR PANEL 161PF. REPAIRED HOLES IN FLOOR PANEL 161PF IAW SRM 53-02-00, FIG. 204.
- [SDR F3LA200700153](https://openairdocs.org/sdr/F3LA200700153.md): Transition Panel · damaged · Jun 27, 2007 · N934FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > DURING C-2 CHECK, INSPECTION REPORTED HOLES IN AFT CARGO COMPARTMENT TRANSITION PANEL 152BF. REPAIRED HOLES IN TRANSITION PANEL 152BF IAW SRM 53-02-00, FIG 204.
- [SDR F3LA200700152](https://openairdocs.org/sdr/F3LA200700152.md): Transition Panel · damaged · Jun 27, 2007 · N934FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > DURING C-2 CHECK, INSPECTION REPORTED HOLES IN AFT CARGO COMPARTMENT TRANSITION PANEL 162CF. REPAIRED TRANSITION PANEL 162CF IAW SRM 53-02-00, FIG. 204.
- [SDR F3LA200700151](https://openairdocs.org/sdr/F3LA200700151.md): Floor Panel · damaged · Jun 27, 2007 · N934FR · Airbus A319111 · Fuselage Floor Panel
  > DURING C-2 CHECK, INSPECTION REPORTED FWD CARGO COMPARTMENT FLOOR PANEL 131AF DAMAGED. REPAIRED FLOOR PANEL 131AF IAW SRM 53-02-00, FIG 204.

Next page: https://openairdocs.org/deregistered/N934FR-2016-09-12/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 = 'N934FR' AND deregistration_id = 'N934FR-2016-09-12'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N934FR-2016-09-12/reports

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.