N203FR, cancelled Dec 17, 2018

Service difficulty reports · 48

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 = 'N203FR' AND deregistration_id = 'N203FR-2018-12-17'
  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 F3LA2018050100336Doubler · gougedAFT CARGO DOOR LOWER AFT INNER SKIN DOUBLER REPAIR GOUGED. REMOVED AND REPLACED THE AFT CARGO DOOR LOWER INNER SKIN DOUBLER REPAIR IAW AMM 52-32-00-300-016, EA A2-52R-33760, 52-32-14-PB400-COMP-00, NTM 51-10-08M, 52-32-21-000-003-A, SRM 51-21-11, AND SRM 51Apr 23, 2018 · N203FR · Airbus A320214 · Cargo/Baggage DoorsSDR F3LA2018050100335Doubler · gougedFWD CARGO DOOR LOWER AFT INNER SKIN DOUBLER REPAIR GOUGED. REMOVED AND REPLACED THE FWD CARGO DOOR LOWER AFT INNER SKIN DOUBLER IAW SRM 52-41-11, 52-31-13, PB 401, CONF 00, EA A2-52R-34068, SRM 51-21-11, NTM 57-10-08, AND 51-10-01.Apr 23, 2018 · N203FR · Airbus A320214 · Cargo/Baggage DoorsSDR F3LA2018050100334Doubler · gougedFWD CARGO DOOR LOWER FWD INNER SKIN DOUBLER REPAIR GOUGED. REMOVED AND REPLACED THE DOUBLER AT FWD DOOR INNER SKIN IAW SRM 51-42-11, NTM 51-10-08, AMM 52-31-21-000-003-A, EA A2-52R-34068, AND SRM 51-21-11.Apr 23, 2018 · N203FR · Airbus A320214 · Cargo/Baggage DoorsSDR F3LA2017070500184Windshield · failedFOUND THE CAPTAIN'S WINDSHIELD SHATTERED. REPLACED THE WINDSHIELD IAW AMM 56-11-11 PB 401. OPS CHECKED GOOD.Jul 2, 2017 · N203FR · Airbus A320214 · Flight Compartment WindowsSDR F3LA2017051600138Floor Support · corrodedFLOOR SUPPORT Y1292 FROM FRAMES 64 - 66 CORRODED. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11-911-001.May 10, 2017 · N203FR · Airbus A320214 · Fuselage Miscellaneous StructureSDR F3LA2017051600139Floor Support · corrodedFLOOR SUPPORT -Y254 BETWEEN FRAMES 68 - 70 HAS CORROSION ON UPPER SURFACE. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-42-11, AND 51-72-11-911-001.May 9, 2017 · N203FR · Airbus A320214 · Fuselage Miscellaneous StructureSDR F3LA2017051700141Floorbeam · corrodedFLOORBEAM -Y1292 AT FR 66 HAS CORROSION ON UPPER SURFACE. REMOVED AND REPLACED, NEW FLOORBEAM -Y1292 AT FR66 IAW SRM A320-51-42-11 AND 51-72-911-01.May 8, 2017 · N203FR · Airbus A320214 · Fuselage Main, Floor BeamSDR F3LA2017051700140Floorbeam · corrodedFLOORBEAM Y765 AT FR66 HAS CORROSION ON UPPER SURFACE. REMOVED CORROSION ON FLOORBEAM Y765 AT FR66 FOUND TO BE OUT OF LIMITS. REMOVED FLOORBEAM Y765 AT FR66 REPLACE WITH NEW FLOORBEAM Y765 IAW SRM A320-51-72-11.May 8, 2017 · N203FR · Airbus A320214 · Fuselage Main, Floor BeamSDR F3LA2017051600132Floorbeam · corrodedFLOORBEAM Y1292 AT FR68 HAS CORROSION ON UPPER SURFACE. REMOVED AND REPLACED THE FLOORBEAM IAW SRM 51-42-11, AND 51-72-11-911-001.May 8, 2017 · N203FR · Airbus A320214 · Fuselage Main, Floor BeamSDR F3LA2017051500137Floor Support · corrodedFLOOR SUPPORT Y765 BETWEEN FRAMES 67 AND 68 HAS CORROSION ON UPPER SERVICE. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11-911-001.May 8, 2017 · N203FR · Airbus A320214 · Fuselage Miscellaneous StructureSDR F3LA2017051500136Floorbeam · corrodedFLOORBEAM Y254 BETWEEN FR66-FR67 HAS CORROSION ON UPPER SURFACE. REMOVED AND REPLACED NEW FLOORBEAM Y254 BETWEEN FR66-FR67 IAW SRM 51-72-11, 51-42-11 AND 53-41-14.May 8, 2017 · N203FR · Airbus A320214 · Fuselage Main, Floor BeamSDR F3LA2017051500135Floor Support · corrodedFLOOR SUPPORT -Y765, FRAMES 67 - 68 HAS CORROSION ON UPPER SURFACE. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-42-11, AND 51-72-11-911-001.May 8, 2017 · N203FR · Airbus A320214 · Fuselage Miscellaneous StructureSDR F3LA2017051500134Floorbeam · corrodedFLOORBEAM -Y765 AT FRAME 66 HAS CORROSION ON UPPER SURFACE. REMOVED AND REPLACED THE FLOORBEAM IAW 51-42-11, AND 51-72-11-911-001.May 8, 2017 · N203FR · Airbus A320214 · Fuselage Main, Floor BeamSDR F3LA2017051500133Floorbeam · corrodedFLOORBEAM Y1292 AT FRAME 67 HAS CORROSION ON UPPER SURFACE. REMOVED AND REPLACED THE FLOORBEAM IAW SRM 51-72-11-911-001.May 8, 2017 · N203FR · Airbus A320214 · Fuselage Main, Floor BeamSDR F3LA2017051500131Floorbeam · corrodedFLOORBEAM -Y1292 AT FRAME 67 HAS CORROSION ON UPPER SURFACE. REMOVED AND REPLACED THE FLOORBEAM IAW SRM 51-42-11, AND 51-72-11-911-001.May 8, 2017 · N203FR · Airbus A320214 · Fuselage Main, Floor BeamSDR F3LA2017051500130Floorbeam · corrodedFLOORBEAM -Y1292 AT FRAME 68 HAS CORROSION ON UPPER SURFACE. REMOVED AND REPLACED THE FLOORBEAM IAW SRM 51-42-11, AND 51-72-11-911-001.May 8, 2017 · N203FR · Airbus A320214 · Fuselage Main, Floor BeamSDR F3LA2016081700001Coffeemaker · odorF/A SMELLED ODOR COMING FROM AFT CABIN DESCRIBED AS POSSIBLY POPCORN, BURNING RUBBER, OF BURNED COFFEE. POSSIBLY COMING FROM HIGHER IN THE CABIN PERFORMED TROUBLESHOOTING IAW TSM 05-50-00-810-831A. IDENTIFIED THE MOST PROBABLE CAUSE OF THE ODOR TO BE COMING May 19, 2016 · N203FR · Airbus A320214 · Buffet/GalleysSDR F3LA2016052000048Coffeemaker · dirtyREFERENCE LOG PAGE 989574, DURING CRUISE THE CREW NOTED AN ODOR COMING FROM THE AFT CABIN & THE ACFT DIVERTED. MX IDENTIFIED THE CAUSE OF THE ODOR TO BE THE AFT GALLEY COFFEE MAKER & FOUND BURNT DRIED COFFEE RESIDUE ON AFT GALLEY COFFEE MAKER. MX CLEANED & IMay 19, 2016 · N203FR · Airbus A320214 · Buffet/GalleysSDR F3LA2015112001153Safety Valve · inoperativeDISCREPANCY ITEM 1, SPOILERS 1 & 2 FAULT INFLIGHT. DISCREPANCY ITEM NR 2 NOSE WHEEL STEERING FAULT INFLIGHT. RESET SEC 1 & 2. OPERATIONS CHECKED OK IAW AMM 27-94-00-710-001 & -002. NR 2 R & R NLG ELECTRONIC BOX 5GC IAW AMM 32-51-12-000-001 & 32-51-12-400-0Nov 15, 2015 · N203FR · Airbus A320214 · Landing Gear Door Retract SectionSDR F3LA2015111201152Line · chafedHYD RESERVOIR LOW LEVLE, DURING CRUISE FLIGHT. DECLARED AN EMERGENCY. MX FOUND A HOLE IN THE RETURN LINE FOR THE NR 2 ENG THRUST REVERSER HYDRAULIC LINE. THE LINE WAS REPLACED IAW AMM 78-31-49 & HYD SYS SERVICED IAW AMM 29-13-00-710003-A.Nov 8, 2015 · N203FR · Airbus A320214 · Hydraulic System, MainSDR F3LA2015101401150Slide · defectiveEMERGENCY SLIDE LIGHT AT DOOR 1 RT INOPERATIVE. PLACED ON MEL CONTROL NR 1116039. REPLACED L1 DOOR SLIDE AMM 25-62-44-000-002-A & 25-62-44-400-006-A. OPERATIONAL CHECKED GOOD, LIGHTS OPERATE NORMAL & PLACARD REMOVED.Oct 10, 2015 · N203FR · Airbus A320214 · Escape SlideSDR F3LA2015030901117Wire · damagedDISCREPANCY, EMER EXIT LIGHTS INOPERATIVE AT L1, L2, R1 & R2. RETERMINATED WIRING AT ALL 4 EPSUS AS REQUIRED, COMPLIED WITH EA A2-33R-33040. EMER LIGHTS OPERATIONS CHECKED GOOD. PN INVOLVED, 10WL 3351-5408, 11WL 3351-1917, 12WL 3351-1779 & 13WL 3351-1927.Mar 7, 2015 · N203FR · Airbus A320214 · Light System WiringSDR F3LA2013111800934Seat Track · corrodedDURING C8/S2 CHECK. SEAT TRACK Y1292 HAS CORROSION AT FRAME 16. SEAT TRACK CORROSION EVALUATED AND FOUND OUT OF LIMITS. REMOVED DAMAGED TRACK AND INSTALLED NEW SEAT TRACK, IAW SRM 51-42-11, SECT 5.A THRU C.6 AND SECT 7.B3 A-D.Oct 30, 2013 · N203FR · Airbus A320214 · Fuselage, Seat/Cargo Attach FittingsSDR F3LA2013111800933Skin · damagedDURING C8/S2 CHECK. THERMOGRAPHIC INSPECTION OF LT ELEVATOR REVEALED INDICATIONS ON UPPER PANEL IRREGULAR IN SHAPE AND BLACK IN COLOR. REPAIRED IAW SRM 55-20-00, PB201, PARA 2.A.-B, PARA. 2.B, 2.B(1)(A)2, SRM 55-21-11, PB201, C1 PARA.5.E.(2)(A)(B), FIGURE 20Oct 23, 2013 · N203FR · Airbus A320214 · Elevator, Plate/SkinSDR F3LA2013111800932Sill · corrodedDURING C8/S2 CHECK. FORWARD CARGO LOWER SILL UPPER SURFACE HAS CORROSION BETWEEN FRAMES 26 AND 27. REPAIRED IAW SRM 51-74-00 PARA 6.A - 6.B(2}(5), SRM 51-75-12, SRM 51-21-11 AND SRM 51-23-11.Oct 22, 2013 · N203FR · Airbus A320214 · Fuselage Miscellaneous StructureSDR F3LA2013111800931Sill · corrodedDURING C8/S2 CHECK. FORWARD CARGO DOOR SILL LOWER SKIN HAS SURFACE CORROSION ON UPPER SURFACE AT FRAMES 24 TO 25. REPAIRED IAW SRM 5L-74-00 PARA 6.A-6.B.Oct 22, 2013 · N203FR · Airbus A320214 · Fuselage Miscellaneous StructureSDR F3LA2013111800930Shear Tie · corrodedDURING C8/S2 CHECK, LT LATERAL SHEAR PLATE HAS CORROSION AT FRAME 70, STRINGER 24. REMOVED AND REPLACED IAW SRM 51-42-11, PARAGRAPH 6.B., 1 THROUGH 8.Oct 20, 2013 · N203FR · Airbus A320214 · Fuselage Internal Mounting StructureSDR F3LA2013111800929Shear Tie · corrodedDURING C8/S2 CHECK. RT LATERAL SHEAR PLATE HAS CORROSION AT FRAME 70, STRINGER 24. R & R IAW SRM 51-42-11, PARA 6.B., 1 THROUGH 8.Oct 20, 2013 · N203FR · Airbus A320214 · Fuselage Internal Mounting StructureSDR F3LA2012050400750Lamp · burned outSEAT ROW 25 EMERGENCY LIGHT INOPERATIVE. R & R BULBS IAW AMM 33-51-18-400-002A. OPS CHECKED OK.May 1, 2012 · N203FR · Airbus A320214 · Emergency LightingSDR F3LA2012050400749Lamp · burned outSEAT ROW 24 EMERGENCY LIGHT INOPERATIVE. R & R BULBS, IAW AMM 33-41-11-400-002A, 33--41-11-000-002A. OPS CHECKED OK.May 1, 2012 · N203FR · Airbus A320214 · Emergency LightingSDR F3LA2012011300699Electrical Box · failedODOR OF ELETRICITY BETWEEN ROW 3 AND 4. NO VISIBLE SMOKE. TURNED OFF LIVE TV AND ODOR CLEARED. PERFORMED ELETRICAL ODOR SYS INTEGRITY CHECK IAW LTV AMM 44-25-00. NO DISCREPANCIES NOTED. CHANGED SEB IAW LTV AMM 44-25-00. OPS CHECKED GOOD.Jan 12, 2012 · N203FR · Airbus A320214 · Entertainment SystemSDR F3LA2011080400663Feel Unit · bindingREFERENCE PILOT REPORT LOG PAGE 615630 ITEM 1, UPON TOUCHDOWN PILOT NEEDED RIGHT RUDDER TO STRAIGHTEN NOSE BUT RUDDER FELT LOCKED IN CENTERED POSITION. AFTER APPLYING MORE PRESSURE PEDAL UNLOCKED AND APPEARED TO WORK NORMALLY. REMOVED AND REPLACED ARTIFICIAL FJul 29, 2011 · N203FR · Airbus A320214 · Rudder Control SystemSDR F3LA2010111400548Module · looseC-CHECK: NON ROUTINE N0694; EMERGENCY EXIT LIGHTS ON SEAT ROWS 16 AND 24 ARE INOP. RETERMINATED PINS ON EMERGENCY EXIT LIGHT CONNECTORS AT SEATS 16 LT AND 24 LT IAW AMM 33-51-19-020-051, STEP 4A1C AND AMM 33-51-19-420-051 STEP 4B1B. OPS CHECK GOOD IAW AMM 33-Nov 14, 2010 · N203FR · Airbus A320214 · Emergency LightingSDR F3LA2010111400547Floorbeam · corrodedC-CHECK: NON ROUTINE N0566; MAIN CABIN FLOORBEAM RT SIDE NR4 BETWEEN FRAME 67-69, CORROSION ON BOTTOM SIDE OF FLOORBEAM AT FASTENER HOLE. R & R FLOORBEAM IAW SRM 51-72-11, PAGE 1 AND 2.Nov 14, 2010 · N203FR · Airbus A320214 · Fuselage Main, Floor BeamSDR F3LA2010111400546Plate · corrodedC-CHECK: NON ROUTINE N0561; AFT GALLEY UNDERFLOOR STRUCTURE RT LATERAL SHEAR PLATE BETWEEN FRAME 69 AND 70, HAS CORROSION AT 8 IN AFT OF FRAME 69 (ABOUT 2 SQUARE INCHES). R & R SHEARPLATE IAW SRM 51-42-11.Nov 14, 2010 · N203FR · Airbus A320214 · Fuselage Miscellaneous StructureSDR F3LA2010111400545Sill · corrodedC-CHECK: NON ROUTINE N0558; MAIN CABIN FLOOR AT FRAME 68L FLOOR SUPPORT HAS CORROSION APPROX 25 SQ IN AT THE FASTENER HOLES. CORROSION ON FLOOR SILL. REMOVED CORROSION ON L-2 DOOR SILL AT FRAME 68 IAW SRM 51-74-00 BLEND OUT FOUND TO BE OUT OF LIMITS, REPAIREDNov 14, 2010 · N203FR · Airbus A320214 · Fuselage Miscellaneous StructureSDR F3LA2010111400544Floorbeam · corrodedC-CHECK: NON ROUTINE N0557; MAIN CABIN FLOORBEAM, NR 4 LT BETWEEN FRAME 67-68 HAS APPROX 2 SQ IN OF CORROSION AT THE FASTENER HOLES. R & R FLOORBEAM IAW SRM 51-44-11, SRM 51-42-11.Nov 14, 2010 · N203FR · Airbus A320214 · Fuselage Main, Floor BeamSDR F3LA2010111400543Floor Panel · delaminatedC-CHECK: NON ROUTINE N0401; FLOORBOARD UNDER LAV E IS DELAMINATED. FABRICATED REPLACEMENT PANEL IAW MCG IRM 9701 REV G.Nov 14, 2010 · N203FR · Airbus A320214 · Fuselage Floor PanelSDR F3LA2010111400542Transition Panel · debondedC-CHECK: NON ROUTINE N0291; FWD CARGO TRANSITION PANEL 132FF UPPER SURFACE DEBONDED 6 SQ IN. FABRICATED REPLACEMENT PANEL IAW MCG IRM 9701, REV G.Nov 14, 2010 · N203FR · Airbus A320214 · Fuselage Miscellaneous StructureSDR F3LA2010111400541Transition Panel · delaminatedC-CHECK: NON ROUTINE N0289; FWD CARGO TRANSITION PANEL 132GF UPPER SURFACE IS DELAMINATED IN 2 PLACES, 2 SQUARE IN, 4 SQUARE IN. FABRICATED REPLACEMENT PANEL IAW MCG IRM 9701, REV G.Nov 14, 2010 · N203FR · Airbus A320214 · Fuselage Miscellaneous StructureSDR F3LA2010111400540Floor Panel · corrodedC-CHECK: FWD CARGO PIT TRANSITION FLOOR PANEL 131BF UPPER SURFACE AFT END DISBOUNDED 8 SQUARE INCHES. FABRICATED TRANSITION PANEL IAW MCW IRM 9701 REV G.Nov 14, 2010 · N203FR · Airbus A320214 · Fuselage Floor PanelSDR F3LA2010111400539Floor Panel · puncturedC-CHECK: NON ROUTINE N0286; FWD CARGO TRANSITION FLOOR PANEL 131BF HAS A 1 SQUARE IN PUNCTURE. FABRICATED REPLACEMENT PANEL IAW MCG 9701, REV G.Nov 14, 2010 · N203FR · Airbus A320214 · Fuselage Floor PanelSDR F3LA2010111400538Cover · gougedC-CHECK: NON ROUTINE N0138; FWD CARGO DOOR INTERNAL SIDE HAS 2.5 INCHES ABOVE THE LOWER DOOR SEAL AND 26.5 INCHES FWD AFT DOOR SEAL IS GOUGED, THAT MEASURES 1/8 INCH WIDE BY 3/4 INCH LONG BY .008 INCH DEEP. REPAIRED IAW A320SRM 52-31-00 PARAGRAPH (O).Nov 14, 2010 · N203FR · Airbus A320214 · Cargo/Baggage DoorsSDR F3LA2010111400537Seal · gougedC-CHECK: NON ROUTINE N0134; AFT CARGO DOOR INTERNAL SIDE HAS 2 IN ABOVE THE LOWER SEAL AND 25 INCHES OF FWD SEAL IS GOUGED THAT MEASURES .3750 IN WIDE X .7500 IN LONG X 0018 INCH DEEP. REPAIRED IAW SRM 52-31-00, PARAGRAPH (O)Nov 14, 2010 · N203FR · Airbus A320214 · Cargo/Baggage DoorsSDR F3LA2010111400536Panel · gougedC-CHECK: NON ROUTINE N0132; AFT CARGO DOOR INTERNAL SIDE HAS A 2.5 INCHES ABOVE THE LOWER DOOR SEAL AND 27 INCHES FWD OF AFT SEAL IS A GOUGE THAT MEASURES .7500 IN WIDE BY 1 IN LONG BY .090 IN DEEP. REPAIRED IAW SRM 52-30-00, PARAGRAPH (O).Nov 14, 2010 · N203FR · Airbus A320214 · Cargo/Baggage DoorsSDR F3LA2010071400466Bleed Valve · faultedAIR TURNBACK DUE TO ENGINE NUMBER 1 CONTROL VALVE FAULT. REMOVED AND REPLACED TRANSIENT BLEED VALVE REFERENCE AMM 75-26-10-000-001 AND AMM 75-26-10-400-001. OPERATIONAL CHECK GOOD.Jul 13, 2010 · N203FR · Airbus A320214 · Compressor Bleed ValveSDR F3LA2009120400241Relay · inoperativeREF LOG PAGE 492624. FLIGHT CREW MAD A BLOCK TURN BACK DUE TO THE F/A CIDS PANEL EMERGENCY LIGHTS ON AND COULD NOT BE RESTORED AND TURNED OFF. MX REMOVED AND REPLACED RELAY 8WL IAW AMM 33-31-00-710-004.Dec 4, 2009 · N203FR · Airbus A320214 · Emergency LightingSDR F3LA2009042700081Oxygen Mask · no testDURING AIRCRAFT INDUCTION CHECK, THE FORWARD LAVATORY OXYGEN MASK WOULD NOT DROP DURING THE MANUAL MASK DROP TEST. MAINTENANCE REPACKED THE OXYGEN MASK AND PERFORMED SATISFACTORY DROP TEST, REFERENCE AMM 35-23-00-550-053.Apr 24, 2009 · N203FR · Airbus A320214 · Passenger Oxygen System
Back to N203FR, cancelled Dec 17, 2018