# Service difficulty reports: N940FR, cancelled Dec 3, 2012

A list on [N940FR, cancelled Dec 3, 2012](https://openairdocs.org/deregistered/N940FR-2012-12-03.md).

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

- [SDR F3LA2012083100781](https://openairdocs.org/sdr/F3LA2012083100781.md): Skin · dented · Aug 27, 2012 · N940FR · Airbus A319111 · Nacelle/Pylon, Plate/Skin
  > NR 1 ENGINE NOSE COWL INNER BARREL AT 9:30 POSITION HAS A DENT. REPAIRED IAW SRM 54-10-00, REPAIR 23, PARAGRAPH 2.A,B,C(1-3}, D, E(1 -2), F{1 -2), G AND H( 1-4).
- [SDR F3LA2012083100780](https://openairdocs.org/sdr/F3LA2012083100780.md): Skin · dented · Aug 27, 2012 · N940FR · Airbus A319111 · Nacelle/Pylon, Plate/Skin
  > NR 1 ENGINE NOSE COWL INNER BARREL AT 9:00 POSITION HAS A DENT, REPAIRED IAW SRM 54-10-00, REPAIR 23, PARAGRAPH 2.A,B,C(1 -3), D, E(1 -2), F( 1-2), G AND H( 1-4).
- [SDR F3LA2012041000733](https://openairdocs.org/sdr/F3LA2012041000733.md): Valve · inoperative · Apr 4, 2012 · N940FR · Airbus A319111 · Landing Gear Brake System
  > LEFT BRAKE PRESSURE INDICATION SHOWS ZERO PSI. R & R ALTERNATE BRAKE DIRECT DRIVE VALVE. OPS CHECK NORMAL REF AMM 32-43-35 PAGE BLOCK 401. TORQUE WRENCH F9TAB2197C CALIBRATION DUE 01/13. MEL CLEARED.
- [SDR F3LA2012021400710](https://openairdocs.org/sdr/F3LA2012021400710.md): Epsu · failed · Feb 12, 2012 · N940FR · Airbus A319111 · Emergency Lighting
  > CIDS 1 EPSU SYS TEST FAILS EPSU (10WL) FWD L/ DEU B (300RH1), R & R FAP DUE TO FAP NOT ACCEPTING CAM WRT AMM 23-73-12 PB 401. FAP LAYOUT SELECTION NOT CONFIGURED FOR CURRENT CABIN LAYOUT-CONT T/S. REINSTALLED ORIGINAL FAP IAW AMM 23-73-12 PB401 CLEANED AND T
- [SDR F3LA2011110900688](https://openairdocs.org/sdr/F3LA2011110900688.md): Light · malfunctioned · Nov 4, 2011 · N940FR · Airbus A319111 · Emergency Lighting
  > EMERGENCY EXIT LIGHTS AND ESCAPE PATH LIGHTS REMAINED ON DURING FLIGHT WITH SWITCH IN "NORM" POSITION- AND FAP AMBER NOTE "CHECK PAX RELATED FUNCTIONS" TROUBLESHOT REF TSM 33-51-00-810-881. CHECKED EPSU BATTERIES FOR CONDITION AND SECURITY. OPS TEST NORMAL IAW
- [SDR F3LA2011091300671](https://openairdocs.org/sdr/F3LA2011091300671.md): Relay · inoperative · Sep 13, 2011 · N940FR · Airbus A319111 · Emergency Lighting
  > EMERGENCY EXIT LIGHTS FLICKERING ON TAKEOFF ROLL. R & R RELAY (8WL) REF ASM 33-51-00. OPS TEST OF THE EMERGENCY LIGHTS TEST GOOD REF AMM 33-51-00-710-001.
- [SDR F3LA2011083100666](https://openairdocs.org/sdr/F3LA2011083100666.md): Power Supply · failed · Aug 30, 2011 · N940FR · Airbus A319111 · Emergency Lighting
  > PATHWAY EMERGENCY LIGHTS ON & OFF INTERMITTENTLY, EMERGENCY EXIT LIGHT ACFT LT OVERWING EXIT ON THROUGHOUT NIGHT. R & R EPSU EMERGENCY POWER SUPPLY UNIT 11WL WITH SERVICEABLE PART IAW AMM 33-51-38 PB 401, OPS CHECK GOOD.
- [SDR F3LA2010010500287](https://openairdocs.org/sdr/F3LA2010010500287.md): Blanking Plate · corroded · Jan 3, 2010 · N940FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > DURING C3 C-CHECK INSP NOTED L2 DOOR AFT GIRT BAR BLANKING PLATE CORRODED. MX INSTALLED NEW L2 DOOR AFT GIRT BAR BLANKING PLATE IAW AMM 52-13-31-400-007.
- [SDR F3LA2010010500286](https://openairdocs.org/sdr/F3LA2010010500286.md): Blanking Plate · corroded · Jan 3, 2010 · N940FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > DURING C3 C-CHECK INSP NOTED L2 DOOR FWD GIRT BAR BLANKING PLATE CORRODED. MX INSTALLED NEW L2 DOOR FWD GIRT BAR BLANKING PLATE IAW AMM 52-13-31-400-007.
- [SDR F3LA2010010500285](https://openairdocs.org/sdr/F3LA2010010500285.md): Blanking Plate · corroded · Jan 3, 2010 · N940FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > DURING C3 C-CHECK INSP NOTED R2 DOOR AFT GIRT BAR BLANKING PLATE CORRODED. MX INSTALLED NEW R2 DOOR AFT GIRT BAR BLANKING PLATE IAW AMM 52-13-31-400-007.
- [SDR F3LA2010010500284](https://openairdocs.org/sdr/F3LA2010010500284.md): Blanking Plate · corroded · Jan 3, 2010 · N940FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > DURING C3 C-CHECK INSP NOTED R2 DOOR FWD GIRT BAR BLANKING PLATE CORRODED. MX INSTALLED NEW R2 DOOR FWD GIRT BAR BLANKING PLATE IAW AMM 52-13-31-400-007.
- [SDR F3LA2010010500283](https://openairdocs.org/sdr/F3LA2010010500283.md): Floor Panel · delaminated · Jan 2, 2010 · N940FR · Airbus A319111 · Fuselage Floor Panel
  > DURING C3 C-CHECK INSP NOTED FLOOR PANEL 261EF TOP GLASS LAYER IS DELAMINATED AFT LT SIDE. MX REPAIRED FLOOR PANEL IAW EA A9-53R-31605.
- [SDR F3LA2010010500282](https://openairdocs.org/sdr/F3LA2010010500282.md): Floor Panel · corroded · Dec 28, 2009 · N940FR · Airbus A319111 · Fuselage Floor Panel
  > DURING C3 C CHECK INSP NOTED AFT R2 DOOR THRESHOLD AREA FLOOR PANEL 262FF HAS CORROSION AROUND ATTACHMENT HOLES AND TOP SURFACE. MX REPLACED PANEL 262FF IAW ROUTINE TASK CARD C534103-2.
- [SDR F3LA2010010500281](https://openairdocs.org/sdr/F3LA2010010500281.md): Skin · gouged · Dec 28, 2009 · N940FR · Airbus A319111 · Fuselage Main, Plate/Skin
  > DURING C3 C-CHECK INSP, NOTED SKIN GOUGED IN 3 SPOTS BETWEEN FRAME 52 AND FRAME 51 BETWEEN STRINGER 1 RT AND STRINGER 2 RT. MX REPAIRED FUSELAGE SKIN IAW SRM 53-00-11, FIG 204.
- [SDR F3LA2010010500280](https://openairdocs.org/sdr/F3LA2010010500280.md): Floor Support · corroded · Dec 28, 2009 · N940FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > DURING C3 C-CHECK INSP NOTED FLOOR SUPPORT Y1292 FRAME 68 TO FRAME 69 OTBD FASTENER HOLE AT FRAME 68 CORRODED. MX REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 51-74-00, SRM 53-00-14, SRM 51-42-11, SRM 51-44-11 AND SRM 51-75-12.
- [SDR F3LA2010010500279](https://openairdocs.org/sdr/F3LA2010010500279.md): Plate · corroded · Dec 28, 2009 · N940FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > DURING C3 C-CHECK INSP NOTED R2 DOOR SILL PLATE INBD FASTENER HOLE FWD OF FRAME 68 IS CORRODED. MX REPAIRED FASTENER HOLE IAW SRM 53-41-14 FIGURE 201 REPAIR PRINCIPLE NR 5.
- [SDR F3LA2009123100276](https://openairdocs.org/sdr/F3LA2009123100276.md): Plate · corroded · Dec 28, 2009 · N940FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > DURING C-3 C-CHECK INSP NOTED LT AFT SHEAR PLATE IS CORRODED ON NUT PLATE HOLES. MX REMOVED AND REPLACED SHEAR PLATE IAW SRM 51-42-11, SRM 51-21-11, SRM 51-44-11, SRM 51-75-12 AND EO A0-53EO-31434.
- [SDR F3LA2010010500278](https://openairdocs.org/sdr/F3LA2010010500278.md): Floorbeam · corroded · Dec 27, 2009 · N940FR · Airbus A319111 · Fuselage Main, Floor Beam
  > DURING C3 C-CHECK INSP, NOTED FLOORBEAM CORRODED AFT CABIN AT FRAME 67 Y1295. MX REMOVED AND REPLACED FLOORBEAM IAW SRM 51-74-00, SRM 53-00-14, SRM 51-42-11, SRM 51-44-11 AND SRM 51-75-12.
- [SDR F3LA2010010200277](https://openairdocs.org/sdr/F3LA2010010200277.md): Floorbeam · corroded · Dec 27, 2009 · N940FR · Airbus A319111 · Fuselage Main, Floor Beam
  > DURING C3 C-CHECK INSP NOTED FLOORBEAM CORRODED AFT CABIN AT FRAME 67 Y1295. MX REMOVED AND REPLACED FLOORBEAM IAW SRM 51-74-00, SRM 53-00-14, SRM 51-42-11, SRM 51-44-11 AND SRM 51-75-12.
- [SDR F3LA2009123100275](https://openairdocs.org/sdr/F3LA2009123100275.md): Plate · corroded · Dec 27, 2009 · N940FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > DURING C-3 C-CHECK INSP, NOTED THE SHEAR PLATE CORRODED RT SIDE AFT CABIN UNDER GALLEY AT FRAME 70 Y1162. MX REMOVED AND REPLACED SHEAR PLATE IAW SRM 51-42-11 AND EO A0-53EO-31434.
- [SDR F3LA2009090800164](https://openairdocs.org/sdr/F3LA2009090800164.md): Line · chafed · Sep 5, 2009 · N940FR · Airbus A319111 · Hydraulic System, Main
  > REFERENCE LOG PAGE 472314. CREW MADE AN AIR TURN BACK TO DEN DUE TO AN INDICATION FOR THE GREEN HYDRAULIC RESERVOIR LEVEL LOW. MAINTENANCE INSPECTED AND FOUND A GREEN HYDRAULIC SYSTEM PRESSURE PIPE WITH CHAFING DAMAGE AND A PIN HOLE. MAINTENANCE REMOVED AND RE
- [SDR F3LA2009082500137](https://openairdocs.org/sdr/F3LA2009082500137.md): Seal · displaced · Aug 21, 2009 · N940FR · Airbus A319111 · Aircraft Fuel Distribution System
  > FUEL TRANSFERRED TO RT WING TANK DURING CTR PUMP OPERATION. MX FOUND SEAL FROM AFT FUEL SURGE ACCESS PANEL HAD MIGRATED INTO THE RT WING FUEL PUMP SUCTION VALVE. MX REPLACED THE PUMP SUCTION VALVE (PN D2825006400200)AND FUEL SURGE VALVE SEAL (PN 5725054220000)
- [SDR F3LA2009072200108](https://openairdocs.org/sdr/F3LA2009072200108.md): Hose · leaking · Jul 19, 2009 · N940FR · Airbus A319111 · Pneumatic Distribution System
  > REF LOG PAGES 475705 AND 475708. DURING CLIMB OUT, PILOTS RECEIVED A WARNING FOR "AIR ENGINE 1 AND 2 BLEED FAULT" AND MADE AN AIR RETURN TO DEPARTURE. MX REMOVED AND REPLACED THE PRESSURE SENSE LINE AND PERFORMED OPS CHECK.
- [SDR F3LA200800463](https://openairdocs.org/sdr/F3LA200800463.md): Floor Panel · damaged · Jul 11, 2008 · N940FR · Airbus A319111 · Fuselage Floor Panel
  > DURING C-CHECK INSP NOTED FWD PIT FLOOR PANEL 131CG DAMAGED. MAINT REPAIRED DAMAGE IAW SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B)
- [SDR F3LA200800462](https://openairdocs.org/sdr/F3LA200800462.md): Floor Panel · damaged · Jul 11, 2008 · N940FR · Airbus A319111 · Fuselage Floor Panel
  > DURING C-CHECK INSP NOTED AFT PIT TRANSITION PANEL 151HE DAMAGED. MAINT REPAIRED DAMAGE IAW SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B)
- [SDR F3LA200800461](https://openairdocs.org/sdr/F3LA200800461.md): Panel · damaged · Jul 11, 2008 · N940FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > DURING C-CHECK INSP NOTED AFT PIT TRANSITION PANEL 151GE DAMAGED. MAINT REPAIRED DAMAGE IAW SRM 53-02-00, FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B)
- [SDR F3LA200800460](https://openairdocs.org/sdr/F3LA200800460.md): Floor Panel · damaged · Jul 11, 2008 · N940FR · Airbus A319111 · Fuselage Floor Panel
  > DURING C-CHECK INSP NOTED AFT PIT FLOOR PANEL 151CE DAMAGED. MAINT REPAIRED DAMAGE IAW SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B)
- [SDR F3LA200800459](https://openairdocs.org/sdr/F3LA200800459.md): Floor Panel · damaged · Jul 11, 2008 · N940FR · Airbus A319111 · Fuselage Floor Panel
  > DURING C-CHECK INSP NOTED AFT PIT PANEL 152UG DAMAGED. MAINT REMOVED DAMAGED AREA, FILLED DAMAGED AREA IAW SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B)
- [SDR F3LA200800458](https://openairdocs.org/sdr/F3LA200800458.md): Floor Panel · damaged · Jul 11, 2008 · N940FR · Airbus A319111 · Fuselage Floor Panel
  > DURING C-CHECK INSP NOTED AFT PIT PANEL 152WG DAMAGED. MAINT REMOVED DAMAGED AREA, FILLED DAMAGED AREA IAW SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B)
- [SDR F3LA200800457](https://openairdocs.org/sdr/F3LA200800457.md): Floor Panel · damaged · Jul 11, 2008 · N940FR · Airbus A319111 · Fuselage Floor Panel
  > DURING C-CHECK INSP NOTED AFT PIT PANEL 151FE DAMAGED. MAINT REMOVED DAMAGED AREA, FILLED DAMAGED AREA IAW SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B)
- [SDR F3LA200800456](https://openairdocs.org/sdr/F3LA200800456.md): Panel · damaged · Jul 11, 2008 · N940FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > DURING C-CHECK INSP NOTED AFT PIT PANEL 151DE DAMAGED. MAINT REMOVED DAMAGED AREA, FILLED DAMAGED AREA IAW SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B)
- [SDR F3LA200800455](https://openairdocs.org/sdr/F3LA200800455.md): Floor Panel · damaged · Jul 11, 2008 · N940FR · Airbus A319111 · Fuselage Floor Panel
  > DURING C-CHECK INSP NOTED AFT PIT PANEL 151PE DAMAGED. MAINT REMOVED DAMAGED AREA, FILLED DAMAGED AREA IAW SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B)
- [SDR F3LA200800454](https://openairdocs.org/sdr/F3LA200800454.md): Panel · damaged · Jul 11, 2008 · N940FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > DURING C-CHECK INSP, NOTED AFT PIT PANEL 161NF DAMAGED. MAINT REMOVED DAMAGED AREA, FILLED DAMAGED AREA IAW SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B)
- [SDR F3LA200800453](https://openairdocs.org/sdr/F3LA200800453.md): Floor Panel · damaged · Jul 11, 2008 · N940FR · Airbus A319111 · Fuselage Floor Panel
  > DURING C-CHECK INSP AFT PIT PANEL 161BF DAMAGED. MIANT REMOVED DAMAGED AREA, FILLED DAMAGED AREA IAW SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B)
- [SDR F3LA200800452](https://openairdocs.org/sdr/F3LA200800452.md): Floor Panel · damaged · Jul 11, 2008 · N940FR · Airbus A319111 · Fuselage Floor Panel
  > DURING C-CHECK INSP, NOTED AFT PIT PANEL 162EF DAMAGED. MAINT REMOVED DAMAGED AREA, FILLED DAMAGED AREA IAW SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B)
- [SDR F3LA200800451](https://openairdocs.org/sdr/F3LA200800451.md): Floor Panel · damaged · Jul 11, 2008 · N940FR · Airbus A319111 · Fuselage Floor Panel
  > DURING C-CHECK INSP, NOTED AFT PIT PANEL 161CF DAMAGED. MAINT REMOVED DAMAGE AREA, FILLED DAMAGED AREA IAW SRM 53-02-00 FIGURE 204. UPON COMPETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B)
- [SDR F3LA200800464](https://openairdocs.org/sdr/F3LA200800464.md): Floor Panel · damaged · Jul 11, 2008 · N940FR · Airbus A319111 · Fuselage Floor Panel
  > DURING C-CHECK INSP NOTED FWD PIT PANEL 131EG DAMAGED. MAINT REPAIRED DAMAGE IAW SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B)
- [SDR F3LA200800003](https://openairdocs.org/sdr/F3LA200800003.md): Epsu · inoperative · Jan 10, 2008 · N940FR · Airbus A319111 · Emergency Lighting
  > DURING PERFORMANCE OF EPSU (12WL) FUNCTIONAL TEST, THE MECHANIC NOTED A POWER SUPPLY FAULT ON THE MDCU. THE EPSU WAS REPLACED, IAW AMM 33-51-38 PB 401 AND OPERATIONS CHECKED OKAY. PART TOTAL TIMES AND TOTAL CYCLES WILL BE PROVIDED AT A LATER DATE. REFERENCE
- [SDR F3LA200600163](https://openairdocs.org/sdr/F3LA200600163.md): Rib · failed · Dec 10, 2006 · N940FR · Airbus A319111 · Nacelle/Pylon, Frame/Spar/Rib
  > DURING C-1 CHECK, INSPECTION REPORTED RT PYLON RIB 9 FAILED HEAT TREATMENT TEST. READINGS BELOW 200. ACCOMPLISHED MODIFICATION (INSTALLATION OF RIB REINFORCEMENT KIT) PER EA A9-54R-11704.

## 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 = 'N940FR' AND deregistration_id = 'N940FR-2012-12-03'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N940FR-2012-12-03/reports

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