# Service difficulty reports: N941FR

A list on [N941FR](https://openairdocs.org/aircraft/N941FR.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 · 56 reports

- [SDR F3LA2021040200028](https://openairdocs.org/sdr/F3LA2021040200028.md): Power Supply · faulted · Apr 2, 2021 · N941FR · Airbus A319112 · Emergency Lighting
  > DISCREPANCY: LP1264105 ITEM 1- EPSU 10WL FAILED EPSU SYS TEST. FOUND 10WL BATTERY EXPIRED, CORRECTIVE ACTION: R&R BATTERY & FAULT CONTINUED, R&R EPSU UNIT FAULT CLEARED, TEST OK AT THIS TIME REF AMM 33-51-38-04- CONF 00.
- [SDR F3LA201912120153](https://openairdocs.org/sdr/F3LA201912120153.md): Ecu · defective · Dec 11, 2019 · N941FR · Airbus A319112 · Fuel Controlling System
  > DISCREPANCY: LP1229399 ITEM, ENGINE 2 CTL VALVE FAULT OCCURRED ON T/O. ABORTED T/O @ 80 KTS, 137,000LB, TEMP 2 C. CORRECTIVE ACTION: REPLACED ENGINE #2 ECU. OPS TEST GOOD, OK TO CONTINUE. PERFORMED LAND TEST. OPS NORMAL. AIRCRAFT RETAINED CATIIIB STATUS. REF.
- [SDR F3LA201910090123](https://openairdocs.org/sdr/F3LA201910090123.md): Door Frame · cracked · Sep 23, 2019 · N941FR · Airbus A319112 · Fuselage Main, Structure
  > L1 DOOR CUTOUT, UPPER FWD CORNER, AFT FASTENER ROW, LWR 1 /4" HOLE, CRACK INDICATION, BOTTOM OF OUTER LAYER, 2:30 OCLOCK ORIENTATION. REPAIRED L1 DOOR FR 16 HOLE# 1 PER AIRBUS RDAS REF: 80686917 /003/2019 REPAIR INSPECTION THRESHOLD =6800FC WITH INTERVALS OF
- [SDR F3LA2018091400431](https://openairdocs.org/sdr/F3LA2018091400431.md): Strut · out of adjust · Sep 10, 2018 · N941FR · Airbus A319112 · Trailing Edge Flap Control System
  > FLIGHT CONTROL FLAPS LOCKED AFTER SELECTING FLAPS 2. ADJUSTED RIGHT FLAP INTERCONNECTING STRUT. RIG AND OPS CHECK GOOD. REFERENCE AMM 27-51-44-820-001A.
- [SDR F3LA2018091000428](https://openairdocs.org/sdr/F3LA2018091000428.md): Fastener · missing · Sep 7, 2018 · N941FR · Airbus A319112 · Trailing Edge Flap Control System
  > OPERATIONAL CHECK FLIGHT UNSATISFACTORY. AFTER 3RD TIME OF EXTENDING FLAPS (12000FT 170KTS) ECAM, F/CTL FLAPS LOCK-ALIGNMENT FAULT. SLATS AT GREEN 2, FLAPS AMBER 0. VISUAL INSPECTION SHOWS FLAPS 1. PERFORMED POST FLIGHT WALK AROUND, NO DEFECTS NOTED. FOUND MIS
- [SDR F3LA2018090600425](https://openairdocs.org/sdr/F3LA2018090600425.md): Warning System · false activation · Sep 4, 2018 · N941FR · Airbus A319112 · Trailing Edge Flap Control System
  > F/CTL FLAPS LOCKED - ALIGNMENT FAULT. PERFORMED BITE TEST OF SFCC 1 AND 2 NO FAULTS NOTED. OPS CHECK GOOD AMM 27-51-00-740-002-A.
- [SDR F3LA2018090600423](https://openairdocs.org/sdr/F3LA2018090600423.md): Computer · malfunctioned · Sep 3, 2018 · N941FR · Airbus A319112 · Trailing Edge Flap Control System
  > F/CTR FLAPS LOCKED. PERFORMED BITE TEST OF SFCC 1 AND 2 MESSAGE CLEARED. PERFORMED OPS CHECK OF FLAPS. OPS CHECK GOOD AT THIS TIME. AMM 27-51-00-740-002-A AND 27-51-00-710-001.
- [SDR F3LA2017101700240](https://openairdocs.org/sdr/F3LA2017101700240.md): Shear Web · cracked · Oct 7, 2017 · N941FR · Airbus A319112 · Fuselage Miscellaneous Structure
  > CABIN AFT WET AREA, LT SHEAR WEB CRACKED AT FRAMES 68 - 70. REMOVED AND REPLACED THE SHEAR WEB IAW SRM 51-42-11, 51-72-11-911-001, AND 51-44-11.
- [SDR F3LA2017101100235](https://openairdocs.org/sdr/F3LA2017101100235.md): Floor Support · corroded · Oct 7, 2017 · N941FR · Airbus A319112 · Fuselage Miscellaneous Structure
  > CABIN AFT WET AREA, Y765 AT FRAMES 66 - 70 FLOOR SUPPORT CORRODED. FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 53-00-14, SRM 51-72-11-911-001, AND 51-44-00.
- [SDR F3LA2017101100234](https://openairdocs.org/sdr/F3LA2017101100234.md): Floorbeam · corroded · Oct 7, 2017 · N941FR · Airbus A319112 · Fuselage Main, Floor Beam
  > CABIN AFT WET AREA FLOORBEAM Y1292 CORRODED AT FRAME 66. REMOVED AND REPLACED THE FLOORBEAM IAW SRM 51-42-11, AND 51-72-11-911-001.
- [SDR F3LA2017101000232](https://openairdocs.org/sdr/F3LA2017101000232.md): Floor Support · corroded · Oct 7, 2017 · N941FR · Airbus A319112 · Fuselage Miscellaneous Structure
  > CABIN AFT FLOOR SUPPORT Y512 CORRODED AT BOLT HOLES FRAME 66. REMOVED AND REPLACED THE FLOOR SUPPORT FROM FRAMES 64 -66 IAW SRM 51-42-11, AND 51-72-11-911-001.
- [SDR F3LA2017101000231](https://openairdocs.org/sdr/F3LA2017101000231.md): Floor Support · corroded · Oct 7, 2017 · N941FR · Airbus A319112 · Fuselage Miscellaneous Structure
  > CORROSION FOUND ON THE FLOOR SUPPORT, Y 765, FRAMES 65-66. REMOVED AND REPLACED THE FLOOR SUPPORT IAW 51-72-11-911-001, AND 51-44-11.
- [SDR F3LA2017101600239](https://openairdocs.org/sdr/F3LA2017101600239.md): Floorbeam · corroded · Oct 5, 2017 · N941FR · Airbus A319112 · Fuselage Main, Floor Beam
  > RIGHT FLOORBEAM -Y1162, FRAME 68. REMOVED AND REPLACED THE FLOORBEAM IAW SRM 51-42-11, AND 51-72-11-911-001.
- [SDR F3LA2017101600238](https://openairdocs.org/sdr/F3LA2017101600238.md): Floorbeam · corroded · Oct 5, 2017 · N941FR · Airbus A319112 · Fuselage Main, Floor Beam
  > RIGHT FLOORBEAM -Y1292 CORRODED ON THE TOP SURFACE AT FRAME 66. REMOVED AND REPLACED THE FLOORBEAM IAW SRM 51-42-11, 51-72-11-911-001, AND 51-44-71.
- [SDR F3LA2017101600237](https://openairdocs.org/sdr/F3LA2017101600237.md): Door Sill · corroded · Oct 5, 2017 · N941FR · Airbus A319112 · Fuselage Miscellaneous Structure
  > R2 DOOR SILL CORRODED ON THE TOP SURFACE AT FRAME 68. REMOVED AND REPLACED THE DOOR SILL, FRAMES 66 - 68 IAW SRM 51-42-11, AND 51-72-11-911-001.
- [SDR F3LA2017101600236](https://openairdocs.org/sdr/F3LA2017101600236.md): Floor Support · corroded · Oct 5, 2017 · N941FR · Airbus A319112 · Fuselage Miscellaneous Structure
  > RIGHT FLOOR SUPPORT -Y1292 CORRODED ON THE TOP SURFACE FRAMES 66 - 68. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-42-11 AND 51-72-11-911-001.
- [SDR F3LA2017101000233](https://openairdocs.org/sdr/F3LA2017101000233.md): Floorbeam · corroded · Oct 5, 2017 · N941FR · Airbus A319112 · Fuselage Main, Floor Beam
  > FLOORBEAM -Y765 CORRODED ON TOP SURFACE AT FRAME 68. REMOVED AND REPLACED THE FLOORBEAM IAW SRM 51-72-11-911-001, 51-42-11, AND 51-44-11.
- [SDR F3LA2017092500229](https://openairdocs.org/sdr/F3LA2017092500229.md): Battery · failed · Sep 25, 2017 · N941FR · Airbus A319112 · Emergency Lighting
  > EPSU TEST FAULT 11WL.. REMOVED AND REPLACED EPSU 11WL BATTERY IAW AMM 33-51-38-PB401. OPS CHECKED GOOD.
- [SDR F3LA2017062000180](https://openairdocs.org/sdr/F3LA2017062000180.md): Power Supply · no test · Jun 18, 2017 · N941FR · Airbus A319112 · Emergency Lighting
  > EPSU 10WL, 12WL AND 13WL FAILED BATTERY CAPACITY TESTS IAW 33-51-00-710-003-A. REMOVED AND REPLACED EPSU. OPS TESTED GOOD IAW AMM 33-51-38 PB 401.
- [SDR F3LA2015050701131](https://openairdocs.org/sdr/F3LA2015050701131.md): Windshield · cracked · May 4, 2015 · N941FR · Airbus A319112 · Flight Compartment Windows
  > RIGHT WINDSHIELD CRACKED AT 34,000 FEET. REPLACED FIRST OFFICERS WINDSHIELD IAW AMM 56-11-11-401.
- [SDR F3LA2015030401112](https://openairdocs.org/sdr/F3LA2015030401112.md): Battery · failed · Mar 4, 2015 · N941FR · Airbus A319112 · Emergency Lighting
  > EPSU BATTERY 13WL, AFT LT, FAILED CAPACITY TEST ON TASK CARD FFT-335100-03-1 ON SCHEDULED A8 CHECK. R & R BATTERY ASSEMBLY IAW AMM 33-51-38-000-002A & AMM 33-51-38-400-002A.
- [SDR F3LA2015030401111](https://openairdocs.org/sdr/F3LA2015030401111.md): Battery · failed · Mar 4, 2015 · N941FR · Airbus A319112 · Emergency Lighting
  > EPSU EMER LIGHTS BATTERY 12WL RT FAILED THE CAPACITY CHECK DURING A SCHEDULED A8 CHECK, TASK CARD FFT-335100-03-1. R & R EPSU EMER BATTERY 12WL RT IAW AMM 33-51-38 PB 401. OPERATIONS CHECK IS GOOD.
- [SDR F3LA2015030401110](https://openairdocs.org/sdr/F3LA2015030401110.md): Battery · failed · Mar 4, 2015 · N941FR · Airbus A319112 · Emergency Lighting
  > EPSU EMER LIGHTS, BATTERY 11WL LT FAILED THE CAPACITY CHECK DURING A SCHEDULED A8 CHECK. TASK CARD FFT-335100-03-1, R & R EPSU EMER BATTERY 11WL LT IAW AMM 33-51-38 PB 401. OPERATIONS CHECK IS GOOD.
- [SDR F3LA2015030401109](https://openairdocs.org/sdr/F3LA2015030401109.md): Battery · failed · Mar 4, 2015 · N941FR · Airbus A319112 · Emergency Lighting
  > EPSU BATTERY 10WL, FWD LT FAILED CAPACITY TEST ON TASK CARD FFT-335100-03-1 ON SCHEDULED A8 CHECK. R & R BATTERY ASSEMBLY IAW AMM 33-51-38-000-002A & AMM 33-51-38-400-002A.
- [SDR F3LA2014072401049](https://openairdocs.org/sdr/F3LA2014072401049.md): Hydraulic Line · leaking · Jul 22, 2014 · N941FR · Airbus A319112 · Hydraulic System, Main
  > AFTER TAKEOFF GREEN HYD SYS FAILURE LOW RES & LOW HYD PRESS MESSAGES. EMER DECLARED. REPLACED FLEXIBLE HOSE FOR RT GEAR DOOR ACTUATOR, AFT HOSE IAW AMM 32-31-39 PAGE BLOCK 401.
- [SDR F3LA2014052301039](https://openairdocs.org/sdr/F3LA2014052301039.md): Slide · failed · May 21, 2014 · N941FR · Airbus A319112 · Escape Slide
  > EMERGENCY LIGHTING SYS FAILED FUNCTIONAL CHECK DURING ROUTINE MX CHECK HEAVY SERVICE. R & R LT FWD EMER ESCAPE SLIDE LAW AMM 25-62-44 PB 401. OPERATIONAL CHECK GOOD.
- [SDR F3LA2014051401038](https://openairdocs.org/sdr/F3LA2014051401038.md): Shear Plate · corroded · May 4, 2014 · N941FR · Airbus A319112 · Fuselage Miscellaneous Structure
  > AFT CABIN RT LATERAL SHEAR PLATE HAS CORROSION. R & R RT LATERAL SHEAR PLATE IAW 51-42-11 PAR 6, 7 & 13 EO A0-53EO-31434.
- [SDR F3LA2014051401037](https://openairdocs.org/sdr/F3LA2014051401037.md): Shear Plate · corroded · May 4, 2014 · N941FR · Airbus A319112 · Fuselage Miscellaneous Structure
  > AFT CABIN LT LATERAL SHEAR HAS CORROSION. R & R LT LATERAL SHEAR PLATE IAW 51-42-11 PAR 6, 7 & 13 EO A0-53EO-31434.
- [SDR F3LA2014051401036](https://openairdocs.org/sdr/F3LA2014051401036.md): Floorbeam · corroded · Apr 30, 2014 · N941FR · Airbus A319112 · Fuselage Main, Floor Beam
  > FLOOR BEAM AT FRAME 67 L2 DOOR HAS CORROSION. CORROSION BEYOND LIMITS, R & R FLOOR BEAM IAW SRM 51-42-11 PAR 5 A-C.
- [SDR F3LA2014051401035](https://openairdocs.org/sdr/F3LA2014051401035.md): Angle · corroded · Apr 30, 2014 · N941FR · Airbus A319112 · Fuselage Miscellaneous Structure
  > RT SERVICE DOOR HAS CORROSION AFT INBD END AT FRAME 68. REMOVED CORROSION & REPAIRED THRESHOLD IAW SRM 53-41-14 PB 201 FIG 201.
- [SDR F3LA2012052300758](https://openairdocs.org/sdr/F3LA2012052300758.md): Bulb · burned out · May 18, 2012 · N941FR · Airbus A319112 · Emergency Lighting
  > SEAT ROW 4ABC EMERGENCY EXIT LIGHT INOPERATIVE. R & R BULB EMERGENCY EXIT LIGHT IAW AMM 33-51-18, PB 401.
- [SDR F3LA2011072100661](https://openairdocs.org/sdr/F3LA2011072100661.md): A/C Pack · smoke · Jul 16, 2011 · N941FR · Airbus A319112 · Cabin Cooling System
  > DURING APPROACH 8,000 MSL, WHISTLE AND SMOKE COMING FROM LONG A/C VENT. NO ECAM CHECKED AIR COND PAGE LOWER SCREEN AIR WAS 100+ FROM PACK ONE. LANDED AND MECHANIC HAD TURNED PACK 1 ON AND OFF AND SMELLED SMOKE. PERFORMED TROUBLESHOOTING OF PACK 1 OVERHEAT ME
- [SDR F3LA2011050300638](https://openairdocs.org/sdr/F3LA2011050300638.md): Shear Plate · corroded · Apr 29, 2011 · N941FR · Airbus A319112 · Fuselage Miscellaneous Structure
  > C-CHECK: NON ROUTINE NR 35292; RT SIDE LATERAL SHEAR PLATE HAS CORROSION AT FASTENER HOLES. R & R SHEAR PLATE WITH NEW CONFIGURATION IAW EO AO-53EO-31 AND SRM 51-42-11, PARA 6B 1-8, PARA 7B 2A-C AND PARA 13D 1-6, SRM 51-21-11 PARA 2C, 3C.
- [SDR F3LA2010090100492](https://openairdocs.org/sdr/F3LA2010090100492.md): Line · leaking · Aug 30, 2010 · N941FR · Airbus A319112 · Hydraulic System, Main
  > AIR TURN BACK, HYD GREEN RESERVOIR LOW LEVEL ECAM IN FLIGHT. 54COMPLETED ECAM, VOL II PROCEDURES AND GRAVITY LANDING GEAR EXTENSION PROCEDURE. PILOT REPORT EMERGENCY DECLARED. R & R LT MLG GEAR DOOR ACTUATOR FLEXIBLE HYD LINE. REF AMM 32-12-00-991-015. PER
- [SDR F3LA2009110500224](https://openairdocs.org/sdr/F3LA2009110500224.md): Threshold · corroded · Nov 3, 2009 · N941FR · Airbus A319112 · Fuselage Miscellaneous Structure
  > REF NON ROUTINE C073471. DURING DEN C3 C-CHECK, INSP NOTED CORROSION ON THE L2 THRESHOLD PANEL 261FF. MX REMOVED AND REPLACED THE PANEL IAW AMM 53-42-12-400-002.
- [SDR F3LA2009110500225](https://openairdocs.org/sdr/F3LA2009110500225.md): Threshold · corroded · Nov 2, 2009 · N941FR · Airbus A319112 · Fuselage Miscellaneous Structure
  > REF NON ROUTINE C073470. DURING DEN C3 C-CHECK, INSP NOTED CORROSION ON THE R3 THRESHOLD PANEL 262FF. MX REMOVED AND REPLACED THE FLOOR PANEL IAW AMM 53-42-12-400-002.
- [SDR F3LA2009110200223](https://openairdocs.org/sdr/F3LA2009110200223.md): Floor Support · corroded · Oct 30, 2009 · N941FR · Airbus A319112 · Fuselage Miscellaneous Structure
  > REFERENCE NON ROUTINE C073394. DURING DEN C3 C-CHECK, INSPECTION NOTED CORROSION ON THE FLOOR SUPPORT NUT CLIP HOLES LOCATED AT STATION -Y1292 BETWEEN FRAMES 68 AND 69. MX REMOVED AND REPLACED THE FLOORBEAM IAW SRM 51-44-11, 51-42-11 AND 51-75-11.
- [SDR F3LA2009110200222](https://openairdocs.org/sdr/F3LA2009110200222.md): Floor Support · corroded · Oct 29, 2009 · N941FR · Airbus A319112 · Fuselage Miscellaneous Structure
  > REFERENCE NON ROUTINE C073186. DURING DEN C3 C-CHECK, INSP NOTED CORROSION ON THE FLOOR SUPPORT NUT CLIP HOLES LOCATED AT STATION Y1292 BETWEEN FRAMES 66 AND 68. MX REMOVED AND REPLACED THE FLOORBEAM IAW SRM 51-44-11, 51-42-11 AND 51-72-11.
- [SDR F3LA2009110200221](https://openairdocs.org/sdr/F3LA2009110200221.md): Floor Support · corroded · Oct 29, 2009 · N941FR · Airbus A319112 · Fuselage Miscellaneous Structure
  > REFERENCE NON ROUTINE C073187. DURING DEN C3 C-CHECK, INSP NOTED CORROSION ON THE FLOOR SUPPORT NUTCLIP HOLES LOCATED AT STA -Y1292 BETWEEN FRAMES 66 AND 68. MX REMOVED AND REPLACED THE FLOOR BEAM ASSY IAW SRM 51-44-11 AND 51-42-11.
- [SDR F3LA200800498](https://openairdocs.org/sdr/F3LA200800498.md): Floor Panel · punctured · Jul 15, 2008 · N941FR · Airbus A319112 · Fuselage Floor Panel
  > DURING C2 C-CHECK, INSPECTION NOTED THE AFT PIT TRANSITION PANEL 161BF WAS PUNCTURED. MAINTENANCE REPAIRED DAMAGE IAW THE REQUIREMENTS OF A319 SRM 53-02-00, PARAGRAPH 8C FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (S)
- [SDR F3LA200800440](https://openairdocs.org/sdr/F3LA200800440.md): Unknown · odor · Jul 9, 2008 · N941FR · Airbus A319112 · Air Distribution System
  > DURING TAXI THE F/A NOTICED A FAINT ODOR FOR A DURATION LESS THAN FIVE SECONDS. DURING TAKEOFF ROLL THE F/A NOTICE THAT SAME DOOR AGAIN. THE ODOR WAS LOCATED IN THE AFT GALLEY ON THE LT SIDE OF THE ACFT. NO OTHER OCCURANCES WERE NOTED FOR THE DURATION OF THE F
- [SDR F3LA200800381](https://openairdocs.org/sdr/F3LA200800381.md): Relay · damaged · Jun 20, 2008 · N941FR · Airbus A319112 · Overheat Detection
  > DURING C-CHECK INSP NOTED OPS TEST OF APU AUTO FIRE EXTINGUISHING EXITING CIRCUIT AND THE APU LOW PRESSURE VALVE OPERATION USING EACH INDIVIDUAL MOTOR IN TURN AND TEST APU EMERGENCY SHUTDOWN CIRCUIT FAILS. MAINT REMOVED AND REPLACED RELAY 39WF AND OPS CHECKED
- [SDR F3LA200800375](https://openairdocs.org/sdr/F3LA200800375.md): Sleeve · damaged · Jun 19, 2008 · N941FR · Airbus A319112 · Spoilers
  > DURING C-CHECK INSP, NOTED LT WING NR FOUR SPOILER ATTACH BOLT IS ROTATED IN LUG ON SPOILER. MAINT MACHINED.040 OFF ANTI-ROTATION WEB VERIFIED SS MATERIAL FOR REPAIRED PO RT090486 AND BONDED AND THE REINFORCING PLATE TO THE ANTI-ROTATION WEB FOR THE CENTER H
- [SDR F3LA200800374](https://openairdocs.org/sdr/F3LA200800374.md): Floor Panel · damaged · Jun 18, 2008 · N941FR · Airbus A319112 · Fuselage Floor Panel
  > DURING C-CHECK INSP, NOTED AFT PIT SCREW PULLING THROUGH FLOOR PANEL 151CE NEXT TO FORWARD TIE DOWN BY SILL PLATE. MAINT REPAIRED PANEL 151CE IAW EA A0-53T-10131. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)
- [SDR F3LA200800365](https://openairdocs.org/sdr/F3LA200800365.md): Floor Panel · damaged · Jun 16, 2008 · N941FR · Airbus A319112 · Fuselage Floor Panel
  > DURING C2 C-CHECK, INSPECTION NOTED AFT PIT TRANSITION PANEL 151DE HAS SEVERAL PUNCTURES. MAINTENANCE REPAIRED PANEL IN ACCORDANCE WITH A319 SRM 53-02-00, FIGURE 204.
- [SDR F3LA200800360](https://openairdocs.org/sdr/F3LA200800360.md): Latch · no test · Jun 16, 2008 · N941FR · Airbus A319112 · Service Doors
  > DURING C-CHECK INSP NOTED R2 DOOR HOLD OPEN LATCH BUTTON FAILED PRESS TEST. MAINT ADJUSTED R2 DOOR BUFFER IAW AMM 52-11-00-820-001 STEP 4J. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)
- [SDR F3LA200800359](https://openairdocs.org/sdr/F3LA200800359.md): Buffer · no test · Jun 16, 2008 · N941FR · Airbus A319112 · Passenger/Crew Doors
  > DURING C-CHECK INSP, NOTED L1 DOOR HOLD OPEN LATCH BUTTON FAILED PRESS TEST. MAINT ADJUSTED L1 DOOR BUFFER IAW AMM 52-11-00-820-001 STEP 4J. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)
- [SDR F3LA200800358](https://openairdocs.org/sdr/F3LA200800358.md): Latch · no test · Jun 16, 2008 · N941FR · Airbus A319112 · Passenger/Crew Doors
  > DURING C-CHECK INSP, NOTED L2 DOOR HOLD OPEN LATCH BUTTON FAILED PRESS TEST. MAINT ADJUSTED L2 DOOR BUFFER IAW AMM 52-13-00-820-001 STEP 4J. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)
- [SDR F3LA200800361](https://openairdocs.org/sdr/F3LA200800361.md): Latch · no test · Jun 16, 2008 · N941FR · Airbus A319112 · Service Doors
  > DURING C-CHECK INSP, NOTED R1 DOOR HOLD OPEN LATCH BUTTON FAILED PRESS TEST. MAINT ADJUSTED R1 DOOR BUFFER IAW AMM 52-11-00-820-001 STEP 4J. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)
- [SDR F3LA200800367](https://openairdocs.org/sdr/F3LA200800367.md): Floor Panel · damaged · Jun 16, 2008 · N941FR · Airbus A319112 · Fuselage Floor Panel
  > DURING C-CHECK INSP, NOTED AFT PIT FLOOR PANEL 151CE HAS SEVERAL PUNCTURES. MAINT REPAIRED PANEL 151CE IAW SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)

Next page: https://openairdocs.org/aircraft/N941FR/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 = 'N941FR' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N941FR/reports

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