N803FR, cancelled Jan 22, 2014

Service difficulty reports · 38

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 = 'N803FR' AND deregistration_id = 'N803FR-2014-01-22'
  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 F3LA2013071700885Unknown · vibrationAIR TURN BACK DUE TO SEVERE AIRFRAME VIBRATION. BEGAN AT 25,500 FT AND AROUND 330 KIAS. DID NOT STOP UNTIL SPEED MANUALLY FLOWN LESS THAN 300 KIAS. EMERGENY DECLARED. R & R LT AND RT ELEVATOR ATTACH HARDWARE AND BEARINGS REF AMM 27-34-41, PAGE BLOCK 401. Jul 9, 2013 · N803FR · Airbus A318111 · Flight Control SystemSDR F3LA2012041000740Plate · corrodedLATERAL SHEAR PLATE FRAME 69 TO FRAME 70, STRINGER 23 RT TO STRINGER 24 RT HAS CORROSION. R & R SHEAR PLATE IAW SRM 51 -42-11, PARA 6 B-18, D 1-5 AND EO AO-53EO-31 434.Apr 6, 2012 · N803FR · Airbus A318111 · Fuselage Miscellaneous StructureSDR F3LA2012041000739Plate · corrodedLATERAL SHEAR PLATE FRAME 69 TO FRAME 70, STRINGER 23 LT TO STRINGER 24 LT HAS CORROSION. R & R SHEAR PLATE IAW SRM 51-42-11 PARAGRAPH 6 B-1 B, 0 1-5 AND EO AO-53EO-31434.Apr 6, 2012 · N803FR · Airbus A318111 · Fuselage Miscellaneous StructureSDR F3LA2012041000738Floorbeam · corrodedAFT CABIN FLOORBEAM FRAME 66 Y765 CORROSION. R & R FLOORBEAM IAW SRM 51-42-11, PARA 5.Apr 6, 2012 · N803FR · Airbus A318111 · Fuselage Main, Floor BeamSDR F3LA2012041000737Floor Support · corrodedAFT CABIN FRAME 66 TO FRAME 68, Y1292 FLOOR SUPPORT HAS CORROSION IN 3 AREAS. R & R FLOOR SUPPORT IAW SRM 51-42-11, PARA 5.Apr 6, 2012 · N803FR · Airbus A318111 · Fuselage Miscellaneous StructureSDR F3LA2012041000734Floorbeam · corrodedAFT CABIN FRAME 66 TO FRAME 68, Y1292 FLOORBEAM HAS CORROSION IN 3 AREAS. R & R FLOORBEAM IAW SRM 51-42-11, PARA 5.Apr 6, 2012 · N803FR · Airbus A318111 · Fuselage Main, Floor BeamSDR F3LA2012041000736Floorbeam · corrodedAFT CABIN FRAME 68, Y-1292 FLOORBEAM HAS CORROSION. R & R FLOORBEAM IAW SRM 51-42-11, PARA 5.Apr 6, 2012 · N803FR · Airbus A318111 · Fuselage Main, Floor BeamSDR F3LA2012041000735Tray · crackedSHEAR PLATE TRAY AT FRAME 68 TO FRAME 69. STRINGER 23 RT TO STRINGER 24, RT IS CRACKED. R & R SHEAR PLATE TRAY IAW SRM 51 -42-11, PARAGRAPH 5, 6, 7 AND 13.Apr 6, 2012 · N803FR · Airbus A318111 · Fuselage Miscellaneous StructureSDR F3LA201204100734Plate · crackedC-CHECK, SHEAR PLATE TRAY AT FRAME 68 TO FRAME 69, S23-24L CRACKED. R & R SHEAR PLATE TRAY IAW SRM 51-42-11 PARAGRAPH 5, 6, 7 AND 13.Apr 6, 2012 · N803FR · Airbus A318111 · Fuselage Miscellaneous StructureSDR F3LA2011080900665Battery Pack · failedESPU LLWL (13WL) FAILED SYS TEST IAW A-CHECK CARD A332201-03. REPLACED BATTERY PACK ON ESPU LLWL(13WL) IAW AMM 33-51-38, PB 401.Aug 5, 2011 · N803FR · Airbus A318111 · Emergency LightingSDR F3LA2011051800641Battery · failedACFT LP 598021 I2M: EPSU TEST FAILED 11WL BATTERY. R & R EPSU BATTERY FOR 11WL IAW A318 AMM 33-51-38-000-002 AND 33-51-38-400-002. TEST OK.May 13, 2011 · N803FR · Airbus A318111 · Emergency LightingSDR F3LA2011032100618Windshield · crackedF/O FRONT WINDSHIELD CRACKED, ANTI-ICE RT WINDSHIELD ECAM. R & R THE F/O FRONT WINDSHIELD IAW AMM 56-11-11-400-000-001.Mar 17, 2011 · N803FR · Airbus A318111 · Flight Compartment WindowsSDR F3LA2011022100605Engine · overtempAIR TURN BACK DUE TO BIRDSTRIKE ON NR 1 ENGINE. ENGINE SHUTDOWN, INVESTIGATION FOR ENGINE SHUTDOWN SHOWS THE EGT WAS EXCEEDED AT 1015 DEGREES CELCIUS FOR 21 SECONDS. PERFORMED AN AIRFRAME AND ENG NR 1 BIRDSTRIKE INSP. REF TASK CARDS MP05510-02 AND MP72400-0Feb 16, 2011 · N803FR · Airbus A318111 · Engine (Turbine/Turboprop)SDR F3LA2010100600529Lens · crackedC-CHECK: NON ROUTINE N0616; L-1 ENTRY LOWER EXIT LIGHT, THE LENS IS ILLEGIBLE. R & R LENS ASSY ON L-1 DOOR LOWER EXIT LIGHT IAW AMM 33-51-13-400-001 PAGE 3 STEP A 3 AND AMM 33-51-13-020-050 STEP A(1)(A)(B).Oct 17, 2010 · N803FR · Airbus A318111 · Emergency LightingSDR F3LA2010100600528Floor Panel · delaminatedC-CHECK: NON ROUTINE N0613; AFT CARGO FLOOR PANEL 161DF EDGE DELAMINATED AND EDGE FILLER DAMAGED 10 INCH. FABRICATED REPLACEDMENT FLOOR PANEL IAW MCG IRM 9701, REV G.Oct 17, 2010 · N803FR · Airbus A318111 · Fuselage Floor PanelSDR F3LA2010100600527Lens · crackedC-CHECK: NON ROUTINE N0610; EMERGENCY LIGHT ABOVE L-1 DOOR, THE LENS IS CRACKED. R & R EMERGENCY LIGHT ASSY IAW AMM 33-51-11-020-050B AND AMM 33-51-11-420-050A.Oct 17, 2010 · N803FR · Airbus A318111 · Emergency LightingSDR F3LA2010100600526Power Supply · no testC-CHECK: NON ROUTINE N0607; NUMEROUS EMERGENCY PATH LIGHTS INOP ON SEATS AND CEILING PANELS. PERFORMED OPS TEST OF EMERGENCY LIGHTS IAW AMM 33-51-00-710-059A. EMERGENCY POWER SUPPLY UNIT 10WL FAILED SYS TEST "BATT FAULT' LIGHT ILLUMINATED. R & R EPSU 10WL IAW Oct 17, 2010 · N803FR · Airbus A318111 · Emergency LightingSDR F3LA2010100600525Fitting · gougedC-CHECK: NON ROUTINE N0124; FWD CARGO LOWER FWD CORNER SEALING SECTION FITTING GOUGED .1250 IN X .2500 IN X .040 INCH. R & R FWD LOWER SEALING SECTION FITTING IAW SRM 51-72-11, PAGE 1.Oct 17, 2010 · N803FR · Airbus A318111 · Fuselage Miscellaneous StructureSDR F3LA2010100600524Connector · misinstalledC-CHECK: NON ROUTINE N0033, EMERGENCY EXIT LIGHT AT ROW 13ABC INOP. FOUND CONNECTOR AT LIGHT ASSEMBLY TO BE INPROPERLY CONNECTED. RE-SEATED CONNECTOR IAW AIRBUS A318 AMM 33-51-19-400-003 SUBTASK 33-51-19-420-052 STEP A(1)(A)(B). OPS CHECK GOOD IAW AMM 33-51-00Oct 17, 2010 · N803FR · Airbus A318111 · Light System WiringSDR F3LA200700193Floor Panel · corrodedDURING C-3 CHECK, INSPECTION REPORTED L2 DOOR THRESHOLD CORRODED ON SURFACE OF PANEL 261FF. REPLACED FLOOR PANEL 261FF IAW AMM 53-42-12-400-002.Aug 3, 2007 · N803FR · Airbus A318111 · Fuselage Floor PanelSDR F3LA200700190Floor Support · corrodedDURING C-3 CHECK, INSPECTION REPORTED CORROSION ON FLOOR SUPPORT AT FR 66 TO FR 70 AT Y1292, FWD INBD FASTENER LOCATIONS. REPLACED FLOOR SUPPORT BETWEEN FR 66 AND FR 68 PER SRM 51-42-11. REPAIRED OTHER DAMAGE TO FLOOR SUPPORT IAW EA A8-53R-12042.Aug 3, 2007 · N803FR · Airbus A318111 · Fuselage Miscellaneous StructureSDR F3LA200700192Plate · corrodedDURING C-3 CHECK, INSPECTION REPORTED L2 DOOR FWD AND AFT GIRT BAR FITTING BLANKING PLATES CORRODED. REPLACED L2 DOOR FWD AND AFT GIRT BAR FITTING BLANKING PLATES IAW AMM 52-11-31-991-011/012.Aug 1, 2007 · N803FR · Airbus A318111 · Fuselage Miscellaneous StructureSDR F3LA200700191Girt Bar · corrodedDURING C-3 CHECK, INSPECTION REPORTED CORROSION ON L2 DOOR SEAL NUT PLATE HOLE AFT OF AFT GIRT BAR FITTING PLATE. REPAIRED PER EA A8-53R-12044.Jul 31, 2007 · N803FR · Airbus A318111 · Escape SlideSDR F3LA200700188Plate · corrodedDURING C-3 CHECK, INSPECTION REPORTED L2 DOOR FWD AND AFT GIRT BAR FITTING BLANKING PLATES CORRODED. REPLACED BLANKING PLATES IAW A318 SRM 51-42-11 AND AMM 52-13-31-400-007.Jul 30, 2007 · N803FR · Airbus A318111 · Escape SlideSDR F3LA200700187Floor Panel · corrodedDURING C-3 CHECK, INSPECTION REPORTED L1 DOOR THRESHOLD FLOOR PANEL 221FF CORRODED. REPLACED FLOOR PANEL 221FF IAW AIRBUS AMM 53-12-12-400-001.Jul 28, 2007 · N803FR · Airbus A318111 · Fuselage Floor PanelSDR F3LA200700185Torque Link · corrodedDURING C-3 CHECK, INSPECTION REPORTED PITTING AND CORROSION ON NLG UPPER TORQUE LINK ATTACH POINT. REMOVED PITS AND CORROSION AND CADMIUM PLATED INNER BORE IAW EA A8-23R-12046.Jul 24, 2007 · N803FR · Airbus A318111 · Main Landing GearSDR F3LA200700184Plate · damagedDURING C-3 CHECK, INSPECTION REPORTED HOLES ON JOINT PLATE COMMON TO FLOORBEAM AT -Y1292 BETWEEN FR68 AND FR69 DAMAGED. FABRICATED AND INSTALLED REPLACEMENT JOINT PLATE IAW A318 SRM 53-41-14, FIG 17, AND 51-42-11, STEP 7B.Jul 24, 2007 · N803FR · Airbus A318111 · Fuselage Main, StructureSDR F3LA200700183Skate Angle · corrodedDURING C-3 CHECK, INSPECTION REPORTED MODERATE CORROSION IN NUT PLATE MOUNT HOLES OF SKATE ANGLE AFT OF R2 DOOR GIRT BAR CUTOUTS. REMOVED AND REPLACED SKATE ANGLE IAW A318 SRM 51-42-11, STEPS B AND D.Jul 24, 2007 · N803FR · Airbus A318111 · Fuselage Main, Attach FittingsSDR F3LA200700182Skate Angle · corrodedDURING C-3 CHECK, INSPECTION REPORTED MODERATE CORROSION IN NUT PLATE MOUNT HOLES OF SKATE ANGLE AFT OF L2 DOOR GIRT BAR CUT OUTS. REMOVED AND REPLACED SKATE ANGLE IAW A318 SRM 51-42-11, PARA. 5, 6 AND 13.Jul 24, 2007 · N803FR · Airbus A318111 · Fuselage Main, Attach FittingsSDR F3LA200700181Floorbeam · corrodedDURING C-3 CHECK, INSPECTION REPORTED AFT GALLEY RT FLOORBEAM -Y1292, FR 68 TO FR69 CORRODED AT NUT PLATE FASTENER LOCATIONS.Jul 24, 2007 · N803FR · Airbus A318111 · Fuselage Main, Floor BeamSDR F3LA200700180Floorbeam · corrodedDURING C-3 CHECK, INSPECTION REPORTED FLOORBEAM INBD OF R2 DOOR GIRT BAR CUTOUTS HAD LIGHT TO MODERATE CORROSION AT ALL NUT PLATE ATTACH POINTS. REPLACED FLOORBEAM IAW A318 SRM 51-42-11, STEP 7B.Jul 24, 2007 · N803FR · Airbus A318111 · Fuselage Main, Floor BeamSDR F3LA200700179Floorbeam · corrodedDURING C-3 CHECK, INSPECTION REPORTED FLOORBEAM INBD OF L2 DOOR GIRT BAR CUTOUTS HAD LIGHT TO MODERATE CORROSION AT ALL NUT PLATE ATTACH POINTS. REPLACED FLOORBEAM IAW A318 SRM 51-42-11, PARA 5-7.Jul 24, 2007 · N803FR · Airbus A318111 · Fuselage Main, Floor BeamSDR UPS07449033Floorbeam · corrodedDURING C-3 CHECK, INSPECTION REPORTED AFT GALLEY RT FLOORBEAM -Y1292, FR 68 TO FR69 CORRODED AT NUT PLATE FASTENER LOCATIONS.Jul 24, 2007 · N803FR · Airbus A318111 · Fuselage Main, Floor BeamSDR F3LA200700084Contactor · damagedAIR RETURN AT 0130Z FOR MULTIPLE ECAMS ASSOCIATED W/AC ESS BUSS. DEPARTURE OUT OF KDEN, LEVELING AT 35,000 FT, RECEIVED ECAM ENG 1 IGN A AND ENG 2 IGN A, C/B TRIPPED L ELEC BAY, YAW DAMPER 1, RUD TRIM 1, AND TRV LIM 1. CAPTAINS PFD ND FWD DISPLAYS ALL WENT BApr 27, 2007 · N803FR · Airbus A318111 · Electrical Power System WiringSDR F3LA200600063Line · leakingDURING CRUISE, FLIGHT CREW REPORTED -Y- HYDRAULIC SYSTEM LEVEL LOW. AS A PRECAUTIONARY MEASURE, AN EMERGENCY WAS DECLARED UPON LANDING AT PDX. REPLACED NR 2 ENGINE YELLOW SYSTEM CASE DRAIN RETURN LINE FOR LEAKING. RAN NR 2 ENGINE. OPS AND LEAK CHECKED NORMJun 30, 2006 · N803FR · Airbus A318111 · Hydraulic System, MainSDR F3LA200500032Controller · unserviceableFLT CREW REPORTED CABIN PRESSURIZATION FLUCTUATING FOLLOWED BY NR 2 CONTROLLER FAILURE. ECAM EXCESS CABIN ALT. AT APPROX 30,000 FT & CLIMBING. NOTICED CABIN ALT SHOWING IN EXCESS OF 29,000 FT, CABIN MODE NR 1 CONTROLLER LATER ASSUMED CONTROL & CABIN PRESSUREJul 15, 2005 · N803FR · Airbus A318111 · Cabin Pressure ControllerSDR F3LA200400065Control Unit · odorIN CRUISE CREW REPORTED SMOKE COMING FROM FLIGHT CONTROL UNIT. NO ECAMS NOTED, SMOKE/AVNCS SMOKE. QRH PROCEDURE APPLIED, EMERGENCY DECLARED. DIVERTED TO OKC & LANDED WITHOUT INCIDENT. PERFORMED INSPECTION OF FWD E&E BAY, MID & AFT E&E BAY, MID LT E&E BAY AJun 6, 2004 · N803FR · Airbus A318111 · Auto Flight SystemSDR F3LA200300136Power Supply · inoperativeFLIGHT CREW REPORTED SEAT BELT/NO SMOKING LIGHTS AND FWD GALLEY EXIT SIGNS INOPERATIVE. REPLACED EPSU IAW MM 33-51-13-04.Sep 15, 2003 · N803FR · Airbus A318111 · Emergency Lighting
Back to N803FR, cancelled Jan 22, 2014