# Service difficulty reports: N949FR

A list on [N949FR](https://openairdocs.org/aircraft/N949FR.md).

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

- [SDR F3LA20200203005](https://openairdocs.org/sdr/F3LA20200203005.md): Line · cracked · Jan 30, 2020 · N949FR · Airbus A319112 · Hydraulic System, Main
  > HYD GREEN RSVR LOW LEVEL. R&R #1 ENGINE HYDRAULIC LINE PER AMM 20-33-11-911-001A, IPC 29-11-06 FIGURE 02E ITEM 220. OPS AND LEAK CHECK OK ON ALL SYSTEMS, NO LEAKS NOTED. SEE LP 1182557 ITEM 3 FOR ADDITIONAL INFORMATION. PERFORMED OPS TASK 32-00-00-481-003A DU
- [SDR F3LA201911060137](https://openairdocs.org/sdr/F3LA201911060137.md): Hinge Fitting · worn · Oct 23, 2019 · N949FR · Airbus A319112 · Fuselage, Door Hinge
  > DISCREPANCY: REFERENCE PEMCO N/R: 2650N343 LH MLG DOOR AFT KEEL BEAM HINGE FITTING FWD LUG WORN CORRECTIVE ACTION: REPAIRED L/H MLG DOOR AFT KEEL BEAM, HINGE FITTING LUG PER AIRBUS REPAIR R533 70508 ISSUE B, AREA REQ RE-INSPECTION WITH A THRESHOLD OF 8500FC
- [SDR F3LA201911060136](https://openairdocs.org/sdr/F3LA201911060136.md): Fitting · cracked · Oct 23, 2019 · N949FR · Airbus A319112 · Fuselage Main, Structure
  > DISCREPANCY: REFERENCE PEMCO N/R: 2650N341 RH FR16 UPPER DOUBLE JOGGLE AREA AFT LOWER HOLE (BL SHOWS CRACK INDICATION IN THE INBD LAYER AT 9 OCLOCK POS. VIEWED FROM THE EXTERIOR CORRECTIVE ACTION: REPAIRED R/H FR16 DOUBLE JOGGLE UPPER CORNER HOLE "B" IAW AIR
- [SDR F3LA201911060135](https://openairdocs.org/sdr/F3LA201911060135.md): Fitting · worn · Oct 23, 2019 · N949FR · Airbus A319112 · Landing Gear Doors
  > DISCREPANCY: REFERENCE PEMCO N/R: 2650N344 RH MLG DOOR AFT KEEL BEAM HINGE FITTING FWD LUG WORN TOTAL CYCLES 122,213 CORRECTIVE ACTION: REPAIRED R/H MLG DOOR AFT KEEL BEAM, HINGE FITTING LUG PER AIRBUS REPAIR R533 70508 ISSUE B, AREA REQ RE-INSPECTION WITH
- [SDR F3LA201911060132](https://openairdocs.org/sdr/F3LA201911060132.md): Fitting · cracked · Oct 23, 2019 · N949FR · Airbus A319112 · Fuselage Main, Attach Fittings
  > DISCREPANCY: REFERENCE PEMCO N/R: 2650N340 RH FR16 UPPER DOUBLE JOGGLE AREA FWD LOWER HOLE (C) SHOWS CRACK INDICATION IN THE MIDDLE LAYER AT 9 OCLOCK POS. VIEWED FROM THE EXTERIOR CORRECTIVE ACTION: REPAIRED R/H FR16 UPPER DOUBLE JOGGLE FASTENER HOLE "C" PER
- [SDR F3LA201911060134](https://openairdocs.org/sdr/F3LA201911060134.md): Structure · cracked · Oct 22, 2019 · N949FR · Airbus A319112 · Emergency Exits
  > DISCREPANCY: REFERENCE PEMCO N/R# 2650N261 R/H EMERG EXIT DOOR, FWD, INNER SEGMENT (SEGMENT #1 FWD) HAS CRACK INDICATIONS. CORRECTIVE ACTION: FAVRICATED & INSTALLED CRACK REPAIR ANGLE ON R/H EMERG. EXIT DOOR, FWD, INNER SEGMENT I.A.W. A319 FRONTIER EA# A9-52
- [SDR F3LA201911060133](https://openairdocs.org/sdr/F3LA201911060133.md): Structure · cracked · Oct 22, 2019 · N949FR · Airbus A319112 · Emergency Exits
  > DISCREPANCY: REFERENCE PEMCO N/R# 2650N260 L/H EMERG EXIT DOOR, FWD, INNER SEGMENT (SEGMENT #1 FWD) HAS CRACK INDICATIONS. CORRECTIVE ACTION: FAVRICATED & INSTALLED CRACK REPAIR ANGLE ON L/H EM ERG. EXIT DOOR, FWD, INNER SEGMENT I.A.W. A319 FRONTIER EA# A9-5
- [SDR F3LA2018082100393](https://openairdocs.org/sdr/F3LA2018082100393.md): Unknown · odor · Aug 16, 2018 · N949FR · Airbus A319112 · Air Distribution System
  > NOTICED A FOUL ODOR COMING FROM AFT GALLEY AND LAST ROWS.THE ODOR WENT AWAY AND CAME BACK. PERFORMED TROUBLESHOOTING IAW TSM 05-50-00-810-831-A. RAN PACKS NR 1 AND 2 COULD NOT DUPLICATE THE ODOR ON THE GROUND. PERFORMED BORESCOPE ON THE NR 1 ENGINE HPC STA
- [SDR F3LA2018073000376](https://openairdocs.org/sdr/F3LA2018073000376.md): Door · misaligned · Jul 28, 2018 · N949FR · Airbus A319112 · Landing Gear Door Retract Section
  > MOVED LANDING GEAR LEVER TO UP POSITION AFTER TAKEOFF. GEAR DID NOT RETRACT. LANDING GEAR NOT UPLOCKED FAULT. PERFORMED QRH PROCEDURE. FAULT CLEARED. BOTH LGCIUS AGREE LANDING GEAR IS UP AND LOCKED. LG SYSTEM DISAGREE ECAM ON TAXI IN AT DEN. PERFORMED EXTENSIO
- [SDR F3LA2017121200266](https://openairdocs.org/sdr/F3LA2017121200266.md): Floorbeam · corroded · Dec 3, 2017 · N949FR · Airbus A319112 · Fuselage Main, Floor Beam
  > CABIN FLOORBEAM Y+1292 HAS CORROSION AT FR16-20. FLOORBEAM REMOVED AT FR16-20 FOUND TO BE OUT OF LIMITS IAW SRM 53-11-14-283-004 AND LOCATE AND DRILL IT IAW SRM 51-72-11 AND INSTALLED IAW SRM 51-72-11-911-00.
- [SDR F3LA2017121200265](https://openairdocs.org/sdr/F3LA2017121200265.md): Floorbeam · corroded · Dec 3, 2017 · N949FR · Airbus A319112 · Fuselage Main, Floor Beam
  > CABIN FLOOR BEAM Y+254 HAS CORROSION AT FR20. REMOVED AND REPLACED FLOOR BEAM Y+254 FR12 TO FR23 P/N D5311281820401 IAW SRM 51-42-11, 51-72-11-911-001 AND 53-11-14-283-004.
- [SDR F3LA2017121200267](https://openairdocs.org/sdr/F3LA2017121200267.md): Floorbeam · corroded · Dec 3, 2017 · N949FR · Airbus A319112 · Fuselage Main, Floor Beam
  > CABIN FLOORBEAM Y-1292 HAS CORROSION AT FR 20. REMOVED AND REPLACED FLOORBEAM Y-1292 AT FR 20 IAW SRM 51-42-11, 51-72-11-911-001 AND 53-11-14-283-004.
- [SDR F3LA2017121400268](https://openairdocs.org/sdr/F3LA2017121400268.md): Door Sill · corroded · Dec 2, 2017 · N949FR · Airbus A319112 · Fuselage Miscellaneous Structure
  > DISCREPANCY: L2 DOOR SILL CORRODED AT FR66. CORRECTIVE ACTION: REFERENCE PEMCO NR 177N259. REMOVED AND REPLACED L2 DOOR SILL IAW A319 SRM 51-72-11, 51-42-11 AND 51-44-11./END/
- [SDR F3LA2017121400269](https://openairdocs.org/sdr/F3LA2017121400269.md): Door Sill · corroded · Dec 2, 2017 · N949FR · Airbus A319112 · Fuselage Miscellaneous Structure
  > DISCREPANCY: R2 DOOR SILL CORRODED AT FR68. CORRECTIVE ACTION: REFERENCE PEMCO NR 1777N258. REMOVED AND REPLACED R2 DOOR SILL IAW A319 SRM 51-72-11, 53-41-14, 51-42-11, 51-44-11 AND 20-21-11-911-001-A./END/
- [SDR F3LA2017121200264](https://openairdocs.org/sdr/F3LA2017121200264.md): Floorbeam · corroded · Dec 2, 2017 · N949FR · Airbus A319112 · Fuselage Main, Floor Beam
  > FLOORBEAM +512 CORRODED AT FR66-67. REMOVED AND REPLACED FLOORBEAM +512 LT SIDE IAW SRM 51-44-11, 51-72-11-911-001 AND 53-00-14-283-002.
- [SDR F3LA2017122600273](https://openairdocs.org/sdr/F3LA2017122600273.md): Threshold · corroded · Dec 1, 2017 · N949FR · Airbus A319112 · Fuselage Miscellaneous Structure
  > FORWARD CARGO BAY DOOR CUT OUT LOWER SILL UPPER SIDE HAS CORROSION AROUND FASTENERS AND FASTENER HOLES, SEVERAL AREAS. REMOVED AND INSTALLED A NEW WEB IAW SRM 51-72-11-911-001, 51-74-00, 51-73-11, 51-42-11, AND 51-44-11.
- [SDR F3LA2017052300154](https://openairdocs.org/sdr/F3LA2017052300154.md): Power Supply · inoperative · May 22, 2017 · N949FR · Airbus A319112 · Emergency Lighting
  > DURING EMERGENCY LIGHT TEST L1 EPSU INOPERATIVE. REMOVED AND REPLACED EPSU 10WL FWD. OPERATIONAL CHECK OK. REFERENCE AMM 33-51-38 PAGE BLOCK 401.
- [SDR F3LA2017052300153](https://openairdocs.org/sdr/F3LA2017052300153.md): Battery · discharged · May 22, 2017 · N949FR · Airbus A319112 · Emergency Lighting
  > EPSU BATTERY 12WL RIGHT FAULT. FAILS TEST. REMOVED AND REPLACED BATTERY ASSEMBLY 12WL RIGHT. REFERENCE AMM 33-51-38-000-002A AND AMM 22-51-38-400-002A. EPSU UNIT P/N 3214-62-10 S/N 007451. OPERATIONAL CHECK GOOD.
- [SDR F3LA2016042900043](https://openairdocs.org/sdr/F3LA2016042900043.md): Fitting · out of adjust · Apr 27, 2016 · N949FR · Airbus A319112 · Emergency Equipment
  > DEFECT 1047578, DURING CRUISE THE R2 DOOR PRESS LIGHT WARNING INDICATION CAME ON & SLIDE INDICATION WENT OUT ON ECAM DOOR PAGE. ADJUSTED THE R2 DOOR GIRT BAR FITTINGS & PERFORMED LOAD ADJUSTMENT OF THE CONTROL HANDLE & OPERATIONAL CHECKED GOOD IAW AMM 52-13-0
- [SDR F3LA2016042300038](https://openairdocs.org/sdr/F3LA2016042300038.md): Door Sill · corroded · Apr 18, 2016 · N949FR · Airbus A319112 · Fuselage Miscellaneous Structure
  > DURING C6 C CHECK NON ROUTINE INSPECTION NOTED THE R2 DOOR SILL HAS AREAS OF CORROSION BETWEEN FRAME 67 & 68. REPAIRED R2 DOOR SILL PLATE BETWEEN FRAME 67 & 68 IAW SRM 53-41-14.
- [SDR F3LA2016042300041](https://openairdocs.org/sdr/F3LA2016042300041.md): Floorbeam · corroded · Apr 17, 2016 · N949FR · Airbus A319112 · Fuselage Main, Floor Beam
  > DURING C6 C CHECK NON ROUTINE INSPECTION NOTED CORROSION ON FLOORBEAM Y512 ON FRAME 66 ON HARD POINT. R & R FLOORBEAM Y512 ON FRAME 66 IAW SRM AT FRAME 64 & 67 IAW 51-21-11.
- [SDR F3LA2016042300036](https://openairdocs.org/sdr/F3LA2016042300036.md): Shear Plate · cracked · Apr 17, 2016 · N949FR · Airbus A319112 · Fuselage Miscellaneous Structure
  > DURING C6 C CHECK NON ROUTINE INSPECTION NOTED LT LATERAL SHEAR PLATE, BETWEEN FRAME 69 & 70 CRACKED. R & R NEW SHEAR PLATE & SHEAR PLATE SUPPORT ON LT SIDE IAW SRM 51-42-11.
- [SDR F3LA2016042300037](https://openairdocs.org/sdr/F3LA2016042300037.md): Shear Plate · corroded · Apr 16, 2016 · N949FR · Airbus A319112 · Fuselage Miscellaneous Structure
  > DURING C6 C CHECK NON ROUTINE INSPECTION NOTED RT LATERAL SHEAR PLATE BETWEEN FRAME 69 & 70 CORRODED. R & R RT LATERAL SHEAR PLATE IAW SRM 51-42-11.
- [SDR F3LA2016042300039](https://openairdocs.org/sdr/F3LA2016042300039.md): Floorbeam · corroded · Apr 15, 2016 · N949FR · Airbus A319112 · Fuselage Main, Floor Beam
  > DURING C6 C CHECK NON ROUTINE INSPECTION NOTED AREAS OF CORROSION FOUND ON Y1292, BETWEEN FRAME 66 & 68. R & R NEW Y1292 IAW SRM 52-42-11.
- [SDR F3LA2016042300040](https://openairdocs.org/sdr/F3LA2016042300040.md): Floorbeam · corroded · Apr 14, 2016 · N949FR · Airbus A319112 · Fuselage Main, Floor Beam
  > DURING C6 C CHECK NON ROUTINE INSPECTION, NOTED CORROSION AT FLOORBEAM Y765M, AT FRAME 66 & 68. R & R FLOORBEAM BETWEEN FRAME 66 & 77 IAW SRM 51-42-11.
- [SDR F3LA2016042300035](https://openairdocs.org/sdr/F3LA2016042300035.md): Floorbeam · corroded · Apr 10, 2016 · N949FR · Airbus A319112 · Fuselage Main, Floor Beam
  > DURING C6 CHECK NON ROUTINE NR 779N175 INSPECTION NOTED SEVERAL AREAS OF CORROSION FOUND ON Y765 FLOORBEAM, BETWEEN FRAME 66 & 68. R & R FLOORBEAM IAW SRM 51-42-11.
- [SDR F3LA2014021001006](https://openairdocs.org/sdr/F3LA2014021001006.md): Light · inoperative · Feb 8, 2014 · N949FR · Airbus A319112 · Emergency Lighting
  > SEAT 4C EMERGENCY PATH LIGHT INOPERATIVE. R & R SEAT 4C EMERGENCY PATH LIGHT IAW AMM 33-51-19 PB401, OPERATIONS CHECKED GOOD.
- [SDR F3LA2012091700793](https://openairdocs.org/sdr/F3LA2012091700793.md): Lamp · burned out · Sep 17, 2012 · N949FR · Airbus A319112 · Emergency Lighting
  > C-CHECK: MAIN CABIN LT SEATS, ROW 13 HAS BURNED OUT LAMP FOR EMERGENCY EXIT LIGHT. R & R LAMP IAW AMM 33-51-19-420-052D. OPS CHECKED GOOD LAW AMM 33-51-00-71 0-00L-A.
- [SDR F3LA2012091700792](https://openairdocs.org/sdr/F3LA2012091700792.md): Sill · corroded · Sep 17, 2012 · N949FR · Airbus A319112 · Fuselage Miscellaneous Structure
  > C-CHECK: R2 DOOR SILL BEAM CORRODED AROUND FASTENER HOLE AT FRAME 66. REPAIRED DOOR SILL BEAM WITH CUTOUT, FILLER AND SPLICE IAW SRM 53-41-14 PB201, PARA 5.A, FIG 201.
- [SDR F3LA2012091700790](https://openairdocs.org/sdr/F3LA2012091700790.md): Light · burned out · Sep 17, 2012 · N949FR · Airbus A319112 · Escape Slide
  > C-CHECK: R2 DOOR "SLIDE ARMED" LIGHT DOES NOT ILLUMINATED DURING TEST. REMOVED SLIDE ARMED INDICATOR LIGHT ASSY IAW AMM 52-76-000-002-A. INSTALLED SERVICEABLE SLIDE ARMED LIGHT ASSY IAW AMM 52-73-21-400-002A. OPS CHECK GOOD IAW AMM 52-73-00-710-001-A.
- [SDR F3LA2012091300789](https://openairdocs.org/sdr/F3LA2012091300789.md): Floorbeam · corroded · Sep 10, 2012 · N949FR · Airbus A319112 · Fuselage Main, Floor Beam
  > C-CHECK: BS 1292 FLOORBEAM CORROSION. R & R FLOORBEAM IAW SRM 51-42-11 PAR 5 AND SRM 53-00-14, PB 101, B. (2), FIGURE 102.
- [SDR F3LA2012091300788](https://openairdocs.org/sdr/F3LA2012091300788.md): Sill · corroded · Sep 10, 2012 · N949FR · Airbus A319112 · Fuselage Miscellaneous Structure
  > C-CHECK: LT SIDE DOOR SILL BEAM CORROSION AROUND FASTENER HOLE. REPAIRED IAW REF SRM 53-41-14 PB 201, NOTE 1.
- [SDR F3LA2012091300787](https://openairdocs.org/sdr/F3LA2012091300787.md): Floorbeam · corroded · Sep 10, 2012 · N949FR · Airbus A319112 · Fuselage Main, Floor Beam
  > C-CHECK: FLOORBEAM CORRODED IN TWO AREAS. R & R FLOORBEAM IAW SRM 51-42-11, PARA 5 AND SRM 53-00-14, PB 101 B.
- [SDR F3LA2012091300786](https://openairdocs.org/sdr/F3LA2012091300786.md): Frame · corroded · Sep 10, 2012 · N949FR · Airbus A319112 · Fuselage Main, Frame
  > C-CHECK: FRAME 68-1292, RM 51-42-11, PARA 5 AND SRN 53-00-14 PB 101B.
- [SDR F3LA2012091300785](https://openairdocs.org/sdr/F3LA2012091300785.md): Shear Plate · corroded · Sep 10, 2012 · N949FR · Airbus A319112 · Fuselage Miscellaneous Structure
  > C-CHECK: FRAME 69 LT SIDE SHEAR PLATE CORROSION. R & R SHEAR PLATE EO A0-53EO-31434.
- [SDR F3LA2012091300784](https://openairdocs.org/sdr/F3LA2012091300784.md): Shear Plate · corroded · Sep 10, 2012 · N949FR · Airbus A319112 · Fuselage Miscellaneous Structure
  > C-CHECK; FRAME 69 RT SIDE SHEAR PLATE CORROSION. R & R SHEAR PLATE IAW EO A0-53EO-31434.
- [SDR F3LA2011051900642](https://openairdocs.org/sdr/F3LA2011051900642.md): Floorboard · damaged · May 13, 2011 · N949FR · Airbus A319111 · Fuselage Floor Panel
  > C-CHECK: COCKPIT FLOORBOARD, 211GF SURFACE IS DAMAGED. FOUND DAMAGE TO FLOORBOARD, 211GF BEYOND REPAIRABLE LIMITS. REPLACED FLOORBOARD IAW SRM 53-12-00 IAW DIAGRAM 101.
- [SDR F3LA2011041300634](https://openairdocs.org/sdr/F3LA2011041300634.md): Spar · dented · Apr 11, 2011 · N949FR · Airbus A319112 · Wing Spar
  > C-CHECK: NON ROUTINE NR30121; RT WING L/E STA 7792/RIB 14 IS DENTED WITH INTERNAL DAMAGE AT CLOSEOUT WEB. REPAIRED RIGHT WING L/E DAMANGE STATION 7792/RIB 14 REPAIRED IAW EA A9-57R-32036 INSTRUTIONS 1-4 AS WRITTEN. HFEC INSPECTED, NO CRACKS WERE FOUND.
- [SDR F3LA2011041300633](https://openairdocs.org/sdr/F3LA2011041300633.md): Floorbeam · corroded · Apr 11, 2011 · N949FR · Airbus A319112 · Fuselage Main, Floor Beam
  > C-CHECK: NON ROUTINE 30064; FLOORBEAM ON FRAMES 66-68 HAS CORROSION AT FASTENER HOLES, BLENDED CORROSION, MEASURED OUT OF LIMITS. ORIGINAL THICKNESS.100", REMAINING.078". SRM 53-41-14 4A(1)AND 53-00-14 4B, FIG 102. LOCATED AND DRILLED NEW BEAM. IAW SRM 51-
- [SDR F3LA2011041300632](https://openairdocs.org/sdr/F3LA2011041300632.md): Floorbeam · corroded · Apr 11, 2011 · N949FR · Airbus A319112 · Fuselage Main, Floor Beam
  > C-CHECK: NON ROUTINE NR 30063; FLOORBEAM ON FRAMES 66- 68 HAS CORROSION AT FASTENER HOLES, BLENDED CORROSION, MEASURED OUT OF LIMITS. ORIGINAL THICKNESS.100", REMAINING.080". SRM 53-41-14 4A(1)AND 53-00-14 4B, FIG 102. LOCATED AND DRILLED NEW BEAM. IAW SRM
- [SDR F3LA2010061500442](https://openairdocs.org/sdr/F3LA2010061500442.md): Oil System · leaking · Jun 14, 2010 · N949FR · Airbus A319112 · APU Oil System
  > REF LOG PAGE 522934. ITEM 1. FOUL ODOR EMITS FROM PACKS WITH BOTH APU AND ENGINE BLEEDS. FOUND APU OIL LEAKING INTO BLEED AIR. APU RENDERED INOPERATIVE. APU PLACED ON MEL.
- [SDR F3LA2009122200264](https://openairdocs.org/sdr/F3LA2009122200264.md): Control Panel · deactivated · Dec 21, 2009 · N949FR · Airbus A319112 · Emergency Lighting
  > REFERENCE LOG PAGE 489469. DURING FLIGHT THE CREW NOTED THE AFT F/A PANEL HAD NO POWER AND COULD NOT MANUALLY TURN ON EMERGENCY LIGHTING FROM AFT PANEL. MX RESET THE CIDS SYS IAW AMM 23-73-00-740-005.
- [SDR F3LA2009081100126](https://openairdocs.org/sdr/F3LA2009081100126.md): Grommet · unsecure · Aug 4, 2009 · N949FR · Airbus A319112 · Passenger/Crew Doors
  > DURING C2 C-CHECK, INSP NOTED THE GUSTLOCK ON THE R1 DOOR DOES NOT ENGAGE WITH THE DOOR IN THE FULL OPEN POSITION. MX FOUND THE NYLON GROMMET ON GUSTLOCK RELEASE ROD TO BE UNSEATED CAUSING GUSTLOCK TO STICK IN THE UNLOCKED POSITION. MX RESEATED THE GROMMET A
- [SDR F3LA200800073](https://openairdocs.org/sdr/F3LA200800073.md): Epsu · inoperative · Feb 25, 2008 · N949FR · Airbus A319111 · Emergency Lighting
  > DURING C1 C CHECK, INSPECTION REPORTED THE OPERATIONAL TEST OF THE EMERGENCY LIGHTS FAILED WITH A FAULT MESSAGE OF "EPSU (13WL) AFT L/DEU B." MAINTENANCE REMOVED AND REPLACED THE EPSU IN ACCORDANCE WITH THE REQUIREMENTS OF AMM 33-51-38-000-001 AND AMM 33-51-3
- [SDR F3LA200800074](https://openairdocs.org/sdr/F3LA200800074.md): Floor Panel · damaged · Feb 23, 2008 · N949FR · Airbus A319111 · Fuselage Floor Panel
  > DURING C1 C CHECK, INSPECTION REPORTED AFT CARGO PIT FLOOR PANEL 151ZG WAS DAMAGED BEYOND REPAIRABLE LIMITS. MAINTENANCE REMOVED AND REPLACED THE FLOOR PANEL IN ACCORDANCE WITH THE REQUIREMENTS OF AMM 53-42-14-400-001. FOLLOWING THE REPLACEMENT OF THE FLOOR
- [SDR F3LA200800075](https://openairdocs.org/sdr/F3LA200800075.md): Floor Panel · damaged · Feb 23, 2008 · N949FR · Airbus A319111 · Fuselage Floor Panel
  > DURING C1 C CHECK, INSPECTION REPORTED AFT CARGO PIT FLOOR PANEL 151VG WAS DAMAGED BEYOND REPARABLE LIMITS. MAINTENANCE REMOVED THE FLOOR PANEL IN ACCORDANCE WITH THE REQUIREMENTS OF AMM 53-42-14-000-001 AND REPLACED IT WITH A NEW FLOOR PANEL IN ACCORDANCE WI

## 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 = 'N949FR' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N949FR/reports

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