# Service difficulty reports: N942FR, cancelled Oct 17, 2012

A list on [N942FR, cancelled Oct 17, 2012](https://openairdocs.org/deregistered/N942FR-2012-10-17.md).

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

- [SDR F3LA2012051600756](https://openairdocs.org/sdr/F3LA2012051600756.md): Battery · discharged · May 15, 2012 · N942FR · Airbus A319111 · Emergency Lighting
  > WHILE ACCOMPLISHING CARD A332204-02 ON THE A6 CHECK THE POWER SUPPLY UNIT, 10 WL BATTERY FAILED THE CAPACITY TEST. ACFT OUT OF SERVICE. POWER SUPPLY UNIT BATTERY REPLACED IAW AMM 33-S1-38-000-002A AND 33-S1-38-400-002A. TESTED GOOD. ACFT RETURNED TO SERVICE.
- [SDR F3LA2012041800741](https://openairdocs.org/sdr/F3LA2012041800741.md): Switch · intermittent · Apr 13, 2012 · N942FR · Airbus A319111 · Emergency Lighting
  > PATH LIGHTING AND EMERGENCY EXIT LGHTS COMING ON INTERMITTENTLY. REPLACED TOGGLE SWITCH, SIGNS & EMERGENCY EXIT LIGHT IAW ESPM 20-45-21. TEST OK REF AMM 33-51-00-710-004.
- [SDR F3LA2011092600680](https://openairdocs.org/sdr/F3LA2011092600680.md): Hose · ruptured · Sep 25, 2011 · N942FR · Airbus A319111 · Hydraulic System, Main
  > ON DEPARTURE, GREEN SYS FAILURE (FLUID LOSS) R & R LT MLG SWIVEL JOINT REF AMM 32-31-38-000, PB401. R & R FLEX HOSE ASSY REF AMM 32-31-39-000, PB 401. OPS LEAK CHECKED NORMAL, SERVICED GREEN HYD SYS 12-12-29-611-001, OK.
- [SDR F3LA2011080300662](https://openairdocs.org/sdr/F3LA2011080300662.md): Connector · misinstalled · Aug 3, 2011 · N942FR · Airbus A319111 · Light System Wiring
  > EXTERIOR OVERWING EMERGENCY LIGHTS INOP". "FOUND BOTH EXTERNAL OVERWING EMERGENCY LIGHTS ON THE RT SIDE WERE NOT CONNECTED TO ACFT WIRING. RECONNECTED CONNECTORS TO LIGHT ASSY. SYS OPS CHECKS NORMAL REF AMM 33-S1-1 S PB401. NOTE: THERE WERE NO DEFECTIVE PAR
- [SDR F3LA2011063000658](https://openairdocs.org/sdr/F3LA2011063000658.md): Sill · corroded · Jun 25, 2011 · N942FR · Airbus A319112 · Fuselage Miscellaneous Structure
  > C-CHECK: L-2 DOOR SILL AT FR66 HAS CORROSION. REPAIRED L-2 DOOR SILL AT FR66 IAW 53-41-14, FIG 201, REPAIR PRINCIPLE 6.
- [SDR F3LA2011063000657](https://openairdocs.org/sdr/F3LA2011063000657.md): Sill · corroded · Jun 25, 2011 · N942FR · Airbus A319112 · Fuselage Miscellaneous Structure
  > C-CHECK: NON ROUTINE NR 38830; R-2 DOOR SILL AT FR66 Y-1500 HAS CORROSION OUT OF LIMITS. REPAIRED R-2 DOOR SILL AT FR66 IAW SRM 53-41-14, FIG 201, REPAIR PRINCIPLE 6.
- [SDR F3LA2011052300652](https://openairdocs.org/sdr/F3LA2011052300652.md): Pump · leaking · May 19, 2011 · N942FR · Airbus A319111 · Hydraulic Pump (Electric/Engine), Main
  > PILOT REPORT YELLOW HYDRAULIC LOW RESERVOIR LEVEL. REMOVED AND REPLACED ENGINED NR2 HYDRAULIC PUMP DRIVER IAW AMM 29-13-51, PB 401, OPS CHECKS GOOD. FOUND SEVERAL LEAK YELLOW SYSTEM LINE TO PRESSURE SWITCH. REMOVED AND REPLACED LINE IAW AMM 28-23-11 LEAKED CH
- [SDR F3LA2011031500615](https://openairdocs.org/sdr/F3LA2011031500615.md): Battery Pack · failed · Mar 11, 2011 · N942FR · Airbus A319111 · Emergency Lighting
  > EPSU BATTERY 13WL FAILED OPS TEST IAW REPLACED BATTERY PACK 13WL IAW AMM 33-51-38-400-002.
- [SDR F3LA2011011800586](https://openairdocs.org/sdr/F3LA2011011800586.md): Hose · leaking · Jan 13, 2011 · N942FR · Airbus A319111 · Hydraulic System, Main
  > DURING CLIM, AFTER RETRACTING THE LANDING GEAR, VISUAL GREEN HYD LOW PRESSURE MESSAGE. MANUAL GEAR EXTENTION PERFORMED. AIR TURN BACK, REPLACED RT MLG AFT HYD HOSE ASSY IAW AMM 32-31-39, PB 401. SERVICED GREEN HYD SYS IAW AMM 12-12-29-611-001. STOWED GRAVITY
- [SDR F3LA2010012900322](https://openairdocs.org/sdr/F3LA2010012900322.md): Proximity Switch · malfunctioned · Jan 28, 2010 · N942FR · Airbus A319111 · Door Warning System
  > DURING C3 C CHECK INSP NOTED EXIT OVERWING EMERGENCY EXTERIOR LIGHTS ON THE RT SIDE DO NOT COME ON WHEN DISARMING OVER WING EXIT DOOR. MX REMOVED AND REPLACED PROXIMITY SWITCH IAW AMM 52-73-11-400-004A AND AMM 52-73-00-710-002.
- [SDR F3LA2010012900323](https://openairdocs.org/sdr/F3LA2010012900323.md): Connector · inoperative · Jan 26, 2010 · N942FR · Airbus A319111 · Light System Wiring
  > REFERENCE NON ROUTINE C078794. DURING C3 C CHECK INSP NOTED THE OPS TEST OF THE EMERGENCY LIGHTS WITH THE MCDU FAULTING. MX REPAIRED IAW AMM 33-51-38-000-001, AMM 33-51-38-400-001, AMM 25-62-44-000-002 AND AMM 33-51-00-710-001.
- [SDR F3LA2010012600320](https://openairdocs.org/sdr/F3LA2010012600320.md): Blanking Plate · corroded · Jan 20, 2010 · N942FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > DURING C3 C CHECK INSPECTION NOTED BLANKING PLATE CORRODED ON AFT PLATE R2 DOOR. MX REMOVED AND REPLACED PLATE IAW AMM 52-13-31-400-007.
- [SDR F3LA2010012600319](https://openairdocs.org/sdr/F3LA2010012600319.md): Blanking Plate · corroded · Jan 20, 2010 · N942FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > DURING C3 C CHECK INSPECTION NOTED BLANKING PLATE CORRODED FORWARD R2 DOOR. MX REMOVED AND REPLACED PLATE IAW AMM 52-13-31-400-007.
- [SDR F3LA2010012600318](https://openairdocs.org/sdr/F3LA2010012600318.md): Blanking Plate · corroded · Jan 20, 2010 · N942FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > DURING C3 C CHECK INSPECTION NOTED BLANKING PLATE CORRODED AFT PLATE L2 DOOR. MX REMOVED AND REPLACED PLATE IAW AMM 52-13-31-400-007.
- [SDR F3LA2010012600317](https://openairdocs.org/sdr/F3LA2010012600317.md): Blanking Plate · corroded · Jan 20, 2010 · N942FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > DURING C3 C CHECK INSPECTION NOTED BLANKING PLATE CORRODED FORWARD PLATE L2 DOOR. MX REMOVED AND REPLACED PLATE IAW AMM 52-13-400-007.
- [SDR F3LA2010012600316](https://openairdocs.org/sdr/F3LA2010012600316.md): Floorboard · corroded · Jan 20, 2010 · N942FR · Airbus A319111 · Fuselage Floor Panel
  > DURING C3 C CHECK INSPECTION NOTED FLOOR PANEL 261FF WAS CORRODED. MX REMOVED AND REPLACED FLOOR PANEL 261FF IAW AMM 53-42-12-400-002.
- [SDR F3LA2010012600312](https://openairdocs.org/sdr/F3LA2010012600312.md): Floor Panel · corroded · Jan 20, 2010 · N942FR · Airbus A319111 · Fuselage Floor Panel
  > DURING C3 C CHECK INSP NOTED FLOOR PANEL 262FF WAS CORRODED. MX REMOVED AND REPLACED FLOOR PANEL 262FF IAW TASK CARD C534103-02.
- [SDR F3LA2010012100308](https://openairdocs.org/sdr/F3LA2010012100308.md): Support · corroded · Jan 19, 2010 · N942FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > DURING C3 C-CHECK INSP NOTED THE LT FRAME SUPPORT AT FRAME 70 HAS CORROSION ON THE BOTTOM SIDE AT NUTPLATE HOLES. MX REMOVED AND REPLACED SUPPORT FRAME IAW SRM 51-42-11.
- [SDR F3LA2010012600315](https://openairdocs.org/sdr/F3LA2010012600315.md): Floorbeam · corroded · Jan 18, 2010 · N942FR · Airbus A319111 · Fuselage Main, Floor Beam
  > DURING C3 C CHECK INSP NOTED Y1292 FROM FRAME 60 TO FRAME 68 ALL SCREW HOLES ARE CORRODED ON UPPER AND LOWER AREAS. MX REMOVED AND REPLACED FLOORBEAM IAW SRM 51-42-11 PAGE 6.
- [SDR F3LA2010012600314](https://openairdocs.org/sdr/F3LA2010012600314.md): Plate · corroded · Jan 18, 2010 · N942FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > DURING C3 C CHECK INSP NOTED PLATE BETWEEN Y1292 AND L2 THRESHOLD AT FRAME 66 IS CORRODED. MX REMOVED AND REPLACED PLATE IAW SRM 51-74-00, SRM 51-75-12 AND DWG D53670670.
- [SDR F3LA2010012600313](https://openairdocs.org/sdr/F3LA2010012600313.md): Floorbeam · corroded · Jan 18, 2010 · N942FR · Airbus A319111 · Fuselage Main, Floor Beam
  > DURING C3 C CHECK INSP NOTED Y1292 JUST AFT OF FRAME 68 HAS A LARGE AREA OF CORROSION ON TOP SIDE WHICH EXTENDS UNDER GALLEY FLOORBOARD. MX REMOVED AND REPLACED FLOORBEAM IAW SRM 51-42-11 PAGE 6.
- [SDR F3LA2010012200311](https://openairdocs.org/sdr/F3LA2010012200311.md): Plate · corroded · Jan 18, 2010 · N942FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > DURING C3 C CHECK INSP NOTED LT SHEAR PLATE AT FRAME 70 HAS SURFACE CORROSION AND APPEARS TO BE COMING FROM UNDER GALLEY FLOORBOARD. MX REMOVED AND REPLACED SHEAR PLATED IAW SRM 51-57-12.
- [SDR F3LA2010012200310](https://openairdocs.org/sdr/F3LA2010012200310.md): Sill · corroded · Jan 18, 2010 · N942FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > DURING C3 C-CHECK INSP NOTED L2 DOOR SILL FASTENER HOLE AFT OF AFT GIRT BAR MOUNT FITTING HAS CORROSION. MX REPAIRED IAW EA A9-53R-31638, SRM 51-74-00, SRM 53-41-14, NTM 51-10-01-250-802-A-01, NTM 51-10-04-270-801-A-01 AND NTM 51-10-08-250-803-A-01.
- [SDR F3LA2010012200309](https://openairdocs.org/sdr/F3LA2010012200309.md): Sill · corroded · Jan 18, 2010 · N942FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > DURING C3 C CHECK INSPECTION NOTED L2 DOOR FASTENER HOLES INBD OF AFT GIRT BAR MOUNT FITTING HAS CORROSION. MX REPAIRED IAW EA A9-53R-31638, SRM 53-41-14, NTM 51-10-01, NTM 51-10-01-250-802-A-01 AND NTM 51-10-08-250-803-A-01.
- [SDR F3LA2010012100307](https://openairdocs.org/sdr/F3LA2010012100307.md): Plate · corroded · Jan 18, 2010 · N942FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > DURING C3 C-CHECK INSP NOTED THE RT SHEAR PLATE AT FRAME 70 HAS SURFACE CORROSION AND APPEARS TO BE COMING FROM UNDER GALLEY FLOORBOARD. MX REMOVED AND REPLACED SHEAR PLATE IAW SRM 51-42-11 AND SRM 51-44-11.
- [SDR F3LA2010012100306](https://openairdocs.org/sdr/F3LA2010012100306.md): Sill · corroded · Jan 18, 2010 · N942FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > DURING C3 C-CHECK INSP NOTED THE L2 DOOR SILL INBD FLANGE FASTENER HOLE CORRODED. MX REPAIRED IAW SRM 53-41-14, SRM 51-23-11 AND SRM 51-42-11.
- [SDR F3LA2010012000305](https://openairdocs.org/sdr/F3LA2010012000305.md): Plate · corroded · Jan 18, 2010 · N942FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > DURING C3 C-CHECK INSP NOTED THE RT SHEAR PLATE AT FRAME 70 HAS SURFACE CORROSION AND APPEARS TO BE COMING FROM UNDER GALLEY FLOORBOARD. MX REMOVED AND REPLACED SHEAR PLATE IAW SRM 51-42-11 AND SRM 51-44-11.
- [SDR F3LA2009063000095](https://openairdocs.org/sdr/F3LA2009063000095.md): Sensor · failed · Jun 25, 2009 · N942FR · Airbus A319111 · Pitot/Static System
  > FLIGHT CREW DIVERTED. PILOT REPORTED LOST TOTAL AIR TEMPERATURE AND STATIC AIR TEMPERATURE INDICATIONS. MX REMOVED AND REPLACED THE NR 1 TOTAL AIR TEMPERATURE SENSOR AT POSITION 11FP1 AND PERFORMED OPERATIONAL TEST, REF AMM 34-11-18 PB 401. DURING THE SAME
- [SDR F3LA200800518](https://openairdocs.org/sdr/F3LA200800518.md): Floor Panel · gouged · Jul 22, 2008 · N942FR · Airbus A319111 · Fuselage Floor Panel
  > DURING C-CHECK, INSP NOTED THE AFT CARGO PIT AFT RT LOWER TRANSITION PANEL 162BF WAS GOUGED AND A PREVIOUS REPAIR WAS PEELING UP. MAINT REPAIRED TRANSITION PANEL 162BF IAW SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEP
- [SDR F3LA200800509](https://openairdocs.org/sdr/F3LA200800509.md): Floor Panel · peeling · Jul 22, 2008 · N942FR · Airbus A319111 · Fuselage Floor Panel
  > DURING C-CHECK, INSP NOTED THE PREVIOUS REPAIRS PEELING LOOSE ON THE AFT CARGO PIT FWD LT UPPER TRANSITION PANEL 151UG. MAINT REPAIRED TRANSITION PANEL 151UG IAW SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A
- [SDR F3LA200800510](https://openairdocs.org/sdr/F3LA200800510.md): Floor Panel · punctured · Jul 22, 2008 · N942FR · Airbus A319111 · Fuselage Floor Panel
  > DURING C2 C-CHECK, INSP NOTED THE AFT CARGO PIT FWD RT LOWER TRANSITION PANEL 152WG WAS PUNCTURED. MAINT REPAIRED TRANSITION PANEL 152WG IAW SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)
- [SDR F3LA200800511](https://openairdocs.org/sdr/F3LA200800511.md): Floor Panel · punctured · Jul 22, 2008 · N942FR · Airbus A319111 · Fuselage Floor Panel
  > DURING C2 C-CHECK, INSP NOTED THE AFT CARGO PIT FWD LT UPPER TRANSITION PANEL 151BE WAS PUNCTURED. MAINT REPAIRED TRANSITION PANEL 151BE IAW SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)
- [SDR F3LA200800512](https://openairdocs.org/sdr/F3LA200800512.md): Floor Panel · gouged · Jul 22, 2008 · N942FR · Airbus A319111 · Fuselage Floor Panel
  > DURING C-CHECK, INSP NOTED THE AFT CARGO PIT FORWARD LT LOWER TRANSITION PANEL 151AE WAS GOUGED IN THE CENTER OF THE PANEL. MAINT REPAIRED TRANSITION PANEL 151AE IAW SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE
- [SDR F3LA200800513](https://openairdocs.org/sdr/F3LA200800513.md): Floor Panel · punctured · Jul 22, 2008 · N942FR · Airbus A319111 · Fuselage Floor Panel
  > DURING C-CHECK, INSP NOTED THE AFT CARGO PIT CENTER LT UPPER TRANSITION PANEL 151FE WAS PUNCTURED. MAINT REPAIRED TRANSITION PANEL 151FE IAW SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)
- [SDR F3LA200800514](https://openairdocs.org/sdr/F3LA200800514.md): Floor Panel · punctured · Jul 22, 2008 · N942FR · Airbus A319111 · Fuselage Floor Panel
  > DURING C-CHECK, INSP NOTED THE AFT CARGO PIT CENTER LT LOWER TRANSITION PANEL 151DE WAS PUNCTURED. MAINT REPAIRED TRANSITION PANEL 151DE IAW SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)
- [SDR F3LA200800515](https://openairdocs.org/sdr/F3LA200800515.md): Floor Panel · punctured · Jul 22, 2008 · N942FR · Airbus A319111 · Fuselage Floor Panel
  > DURING C-CHECK, INSP NOTED THE AFT CARGO PIT FLOOR PANEL 161NF WAS PUNCTURED SEVERAL TIMES. MAINT REPAIRED FLOOR PANEL 161NF IAW SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE.(A)
- [SDR F3LA200800516](https://openairdocs.org/sdr/F3LA200800516.md): Floor Panel · punctured · Jul 22, 2008 · N942FR · Airbus A319111 · Fuselage Floor Panel
  > DURING C-CHECK, INSP NOTED THE AFT CARGO PIT AFT LT UPPER TRANSITION PANEL 161CF WAS PUNCTURED IN THE CENTER, COVERED WITH TAPE. MAINT REPAIRED TRANSITION PANEL 161CF IAW SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEP
- [SDR F3LA200800517](https://openairdocs.org/sdr/F3LA200800517.md): Floor Panel · punctured · Jul 22, 2008 · N942FR · Airbus A319111 · Fuselage Floor Panel
  > DURING C-CHECK, INSP NOTED THE AFT CARGO PIT AFT LT LOWER TRANSITION PANEL 161BF WAS PUNCTURED. MAINT REPAIRED TRANSITION PANEL 161BF IAW SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)
- [SDR F3LA200600124](https://openairdocs.org/sdr/F3LA200600124.md): Gust Lock · inoperative · Sep 21, 2006 · N942FR · Airbus A319111 · Passenger/Crew Doors
  > FOUND GUST LOCK 1L INOP. ADJUSTED BUFFER PER AMM 52-11-12-820. RII INSPECTION ACCOMPLISHED. AIRCRAFT RELEASED FOR SERVICE.
- [SDR F3LA200500045](https://openairdocs.org/sdr/F3LA200500045.md): Odor · detected · Nov 22, 2005 · N942FR · Airbus A319111 · Entertainment System
  > FLIGHT CREW RECEIVED LIVE TV SMOKE INDICATION. FLIGHT ATTENDANT REPORTED AN ELECTRIC ODOR IN AFT GALLEY. DECLARED AM EMERGENCY AND LANDED WITHOUT INCIDENT IN DEN. PERFORMED INSPECTION PER AMM 24-00-00-810-873. VERIFIED LIVE TV EXHAUST COOLING FAN FAILED.

## 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 = 'N942FR' AND deregistration_id = 'N942FR-2012-10-17'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N942FR-2012-10-17/reports

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