N949FR

Service difficulty reports · 46

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

Query with SQL
duckdb -csv -c "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"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR F3LA20200203005Line · crackedHYD 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 DUJan 30, 2020 · N949FR · Airbus A319112 · Hydraulic System, MainSDR F3LA201911060137Hinge Fitting · wornDISCREPANCY: 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 Oct 23, 2019 · N949FR · Airbus A319112 · Fuselage, Door HingeSDR F3LA201911060136Fitting · crackedDISCREPANCY: 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 AIROct 23, 2019 · N949FR · Airbus A319112 · Fuselage Main, StructureSDR F3LA201911060135Fitting · wornDISCREPANCY: 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 WITHOct 23, 2019 · N949FR · Airbus A319112 · Landing Gear DoorsSDR F3LA201911060132Fitting · crackedDISCREPANCY: 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" PEROct 23, 2019 · N949FR · Airbus A319112 · Fuselage Main, Attach FittingsSDR F3LA201911060134Structure · crackedDISCREPANCY: 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# A9-52Oct 22, 2019 · N949FR · Airbus A319112 · Emergency ExitsSDR F3LA201911060133Structure · crackedDISCREPANCY: 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# A9-5Oct 22, 2019 · N949FR · Airbus A319112 · Emergency ExitsSDR F3LA2018082100393Unknown · odorNOTICED 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 STAAug 16, 2018 · N949FR · Airbus A319112 · Air Distribution SystemSDR F3LA2018073000376Door · misalignedMOVED 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 EXTENSIOJul 28, 2018 · N949FR · Airbus A319112 · Landing Gear Door Retract SectionSDR F3LA2017121200266Floorbeam · corrodedCABIN 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.Dec 3, 2017 · N949FR · Airbus A319112 · Fuselage Main, Floor BeamSDR F3LA2017121200265Floorbeam · corrodedCABIN 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.Dec 3, 2017 · N949FR · Airbus A319112 · Fuselage Main, Floor BeamSDR F3LA2017121200267Floorbeam · corrodedCABIN 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.Dec 3, 2017 · N949FR · Airbus A319112 · Fuselage Main, Floor BeamSDR F3LA2017121400268Door Sill · corrodedDISCREPANCY: 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/Dec 2, 2017 · N949FR · Airbus A319112 · Fuselage Miscellaneous StructureSDR F3LA2017121400269Door Sill · corrodedDISCREPANCY: 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/Dec 2, 2017 · N949FR · Airbus A319112 · Fuselage Miscellaneous StructureSDR F3LA2017121200264Floorbeam · corrodedFLOORBEAM +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.Dec 2, 2017 · N949FR · Airbus A319112 · Fuselage Main, Floor BeamSDR F3LA2017122600273Threshold · corrodedFORWARD 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.Dec 1, 2017 · N949FR · Airbus A319112 · Fuselage Miscellaneous StructureSDR F3LA2017052300154Power Supply · inoperativeDURING EMERGENCY LIGHT TEST L1 EPSU INOPERATIVE. REMOVED AND REPLACED EPSU 10WL FWD. OPERATIONAL CHECK OK. REFERENCE AMM 33-51-38 PAGE BLOCK 401.May 22, 2017 · N949FR · Airbus A319112 · Emergency LightingSDR F3LA2017052300153Battery · dischargedEPSU 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.May 22, 2017 · N949FR · Airbus A319112 · Emergency LightingSDR F3LA2016042900043Fitting · out of adjustDEFECT 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 52-13-0Apr 27, 2016 · N949FR · Airbus A319112 · Emergency EquipmentSDR F3LA2016042300038Door Sill · corrodedDURING 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.Apr 18, 2016 · N949FR · Airbus A319112 · Fuselage Miscellaneous StructureSDR F3LA2016042300041Floorbeam · corrodedDURING 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.Apr 17, 2016 · N949FR · Airbus A319112 · Fuselage Main, Floor BeamSDR F3LA2016042300036Shear Plate · crackedDURING 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.Apr 17, 2016 · N949FR · Airbus A319112 · Fuselage Miscellaneous StructureSDR F3LA2016042300037Shear Plate · corrodedDURING 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.Apr 16, 2016 · N949FR · Airbus A319112 · Fuselage Miscellaneous StructureSDR F3LA2016042300039Floorbeam · corrodedDURING 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.Apr 15, 2016 · N949FR · Airbus A319112 · Fuselage Main, Floor BeamSDR F3LA2016042300040Floorbeam · corrodedDURING 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.Apr 14, 2016 · N949FR · Airbus A319112 · Fuselage Main, Floor BeamSDR F3LA2016042300035Floorbeam · corrodedDURING 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.Apr 10, 2016 · N949FR · Airbus A319112 · Fuselage Main, Floor BeamSDR F3LA2014021001006Light · inoperativeSEAT 4C EMERGENCY PATH LIGHT INOPERATIVE. R & R SEAT 4C EMERGENCY PATH LIGHT IAW AMM 33-51-19 PB401, OPERATIONS CHECKED GOOD.Feb 8, 2014 · N949FR · Airbus A319112 · Emergency LightingSDR F3LA2012091700793Lamp · burned outC-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.Sep 17, 2012 · N949FR · Airbus A319112 · Emergency LightingSDR F3LA2012091700792Sill · corrodedC-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.Sep 17, 2012 · N949FR · Airbus A319112 · Fuselage Miscellaneous StructureSDR F3LA2012091700790Light · burned outC-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.Sep 17, 2012 · N949FR · Airbus A319112 · Escape SlideSDR F3LA2012091300789Floorbeam · corrodedC-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.Sep 10, 2012 · N949FR · Airbus A319112 · Fuselage Main, Floor BeamSDR F3LA2012091300788Sill · corrodedC-CHECK: LT SIDE DOOR SILL BEAM CORROSION AROUND FASTENER HOLE. REPAIRED IAW REF SRM 53-41-14 PB 201, NOTE 1.Sep 10, 2012 · N949FR · Airbus A319112 · Fuselage Miscellaneous StructureSDR F3LA2012091300787Floorbeam · corrodedC-CHECK: FLOORBEAM CORRODED IN TWO AREAS. R & R FLOORBEAM IAW SRM 51-42-11, PARA 5 AND SRM 53-00-14, PB 101 B.Sep 10, 2012 · N949FR · Airbus A319112 · Fuselage Main, Floor BeamSDR F3LA2012091300786Frame · corrodedC-CHECK: FRAME 68-1292, RM 51-42-11, PARA 5 AND SRN 53-00-14 PB 101B.Sep 10, 2012 · N949FR · Airbus A319112 · Fuselage Main, FrameSDR F3LA2012091300785Shear Plate · corrodedC-CHECK: FRAME 69 LT SIDE SHEAR PLATE CORROSION. R & R SHEAR PLATE EO A0-53EO-31434.Sep 10, 2012 · N949FR · Airbus A319112 · Fuselage Miscellaneous StructureSDR F3LA2012091300784Shear Plate · corrodedC-CHECK; FRAME 69 RT SIDE SHEAR PLATE CORROSION. R & R SHEAR PLATE IAW EO A0-53EO-31434.Sep 10, 2012 · N949FR · Airbus A319112 · Fuselage Miscellaneous StructureSDR F3LA2011051900642Floorboard · damagedC-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.May 13, 2011 · N949FR · Airbus A319111 · Fuselage Floor PanelSDR F3LA2011041300634Spar · dentedC-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.Apr 11, 2011 · N949FR · Airbus A319112 · Wing SparSDR F3LA2011041300633Floorbeam · corrodedC-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-Apr 11, 2011 · N949FR · Airbus A319112 · Fuselage Main, Floor BeamSDR F3LA2011041300632Floorbeam · corrodedC-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 Apr 11, 2011 · N949FR · Airbus A319112 · Fuselage Main, Floor BeamSDR F3LA2010061500442Oil System · leakingREF 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.Jun 14, 2010 · N949FR · Airbus A319112 · APU Oil SystemSDR F3LA2009122200264Control Panel · deactivatedREFERENCE 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.Dec 21, 2009 · N949FR · Airbus A319112 · Emergency LightingSDR F3LA2009081100126Grommet · unsecureDURING 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 AAug 4, 2009 · N949FR · Airbus A319112 · Passenger/Crew DoorsSDR F3LA200800073Epsu · inoperativeDURING 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 33-51-3Feb 25, 2008 · N949FR · Airbus A319111 · Emergency LightingSDR F3LA200800074Floor Panel · damagedDURING 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 Feb 23, 2008 · N949FR · Airbus A319111 · Fuselage Floor PanelSDR F3LA200800075Floor Panel · damagedDURING 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 WIFeb 23, 2008 · N949FR · Airbus A319111 · Fuselage Floor Panel
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