N903FX
Service difficulty reports · 97
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 = 'N903FX' 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.
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 = 'N903FX' AND registry_match = 'registration' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR COEA2013051704903Stringer Splice · corrodedHEAVY CHECK COE/MINOR REPAIR: LEVEL 2 CORROSION FOUND ON STRINGER SPLICE 11L FWD OF FR 42. REPLACE STRINGER SPLICE PER ATR 42 SRM 53-81-23.SDR COEA2013050801903Intercostal · crackedHEAVY CHECK COE/MINOR REPAIR: INTERCOSTAL CRACKED AT AFT SIDE OF FRAME 24 BETWEEN STRINGER RT 2A-3. REPLACED WITH OEM PART.SDR COEA2013051706903Stringer · corrodedHEAVY CHECK COE/MAJOR REPAIR: CORROSION ON STR 15R BETWEEN FR 35-36. REPAIR STR 15R BETWEEN FR 35-36 REF ATR 42 SRM 53-00-00.SDR COEA2013051705903Seat Track · corrodedHEAVY CHECK COE/MAJOR REPAIR: CORROSION AND MISSING SURFACE PROTECTION ON LEFT I/B SEAT TRACK BETWEEN FR14-16. MAJOR REPAIR PER ATR 42 SRM 53-00-00.SDR COEA2013051703903Stringer · corrodedDURING HEAVY CHECK, CORROSION FOUND ON STRINGER 18R BETWEEN FR 28-29. STRINGER FABRICATED AND REPLACED PER SRM 51-25-01.SDR COEA2013050802903Floor Support · crackedHEAVY CHECK COE/MAJOR REPAIR: CRACKED CARGO MOD LONGITUDINAL FLOORBEAM ON BOTH SIDES OF FLOORBEAM 17, LOCATED BETWEEN LEFT INBD AND OUTBD SEAT TRACKS. REPAIR IAW EA EO5315-01 REV D.SDR COEA2011041521903Stiffener · corrodedSUPPLEMENT: HEAVY CK / COE / MINOR REPAIR / LEVEL 2 CORROSION: FORWARD PRESSURE BULKHEAD, RIGHT O/B VERTICAL STIFFENER TOP HAS AREA OF CORROSION. REMOVED CORROSION, REMOVED AND REPLACED CLIP.SDR COEA2011041420903Floorbeam · crackedHEAVY CHECK/COE/DAMAGED FLOOR BEAM: DISCOVERED CRACKED RIGHT LONGITUDINAL FLOORBEAM AFT OF FRAME 26. FABRICATED NEW SECTION AND SPLICES. DRILLED NEW FLOORBEAM AND SPLICES. ALODINED, PRIMED, AND TOPCOATED FLOORBEAM AND SPLICES. INSTALLED LONGITUDINAL FLOORSDR COEA2011040618903Skin · damagedHEAVY CK COE / MAJOR REPAIR: DENT OUT OF LIMITS 2.0 INCHES AFT OF FRAME 11, NEAR STR 15L. REMOVED DAMAGED SKIN, FABRICATED AND INSTALLED REPAIR DOUBLER IAW ATR72 SRM.SDR COEA2011040617903Floorbeam · crackedHEAVY CK COE / MAJOR REPAIR: FLOORBEAM 22 UPPER FLANGE IS CRACKED OUTBOARD OF THE RT OUTBOARD SEAT TRACK. REPAIRED FLOORBEAM 22 IAW ATR72 SRM.SDR COEA2011040516903Skin · damagedNR 4 HEAVY CK COE / MAJOR REPAIR: SKIN DAMAGED BY DROPPED TOOL BETWEEN FRAMES 8-9 AND STR 20-21R. REMOVED DAMAGE, FABRICATED AND INSTALLED DOUBLER IAW ATR42 SRM.SDR COEA2011040515903Floorbeam · corrodedHEAVY CK COE / MAJOR REPAIR / LEVEL 2 CORROSION: FLOORBEAM 17 IS CORRODED ON THE UPPER AND LOWER SURFACE OF THE UPPER FLANGE BETWEEN LT INBOARD AND LT OUTBOARD SEAT TRACKS.(LENGTH 1.25, WIDTH .300, DEPTH .015 INCH). REMOVED CORROSION, FABRICATED AND INSTALLESDR COEA2011040414903Crease Beam · corrodedHEAVY CK COE / MAJOR REPAIR / LEVEL 2 CORROSION: RT CREASE BEAM WEB FR 18-19 CORRODED ON UPPER AND LOWER SURFACES WITH A TOOLING MARK ON UPPER SURFACE (LENGTH 1.0', WIDTH .400"). REMOVED CORROSION AND TOOLING MARK, FABRICATED AND INSTALLED RT CREASE BEAM WEBSDR COEA2011040413903Crease Beam · corrodedHEAVY CK COE / LEVEL 2 CORROSION: LT CREASE BEAM INNER CHORD FR 17 - 22 CORRODED (LENGTH 4.00, WIDTH .700, DEPTH .013 INCH). REMOVED CORROSION, REMOVED AND REPLACED LT INNER CHORD IAW ATR42 SRM.SDR COEA2011040412903Crease Beam · corrodedHEAVY CK COE / LEVEL 2 CORROSION: RT CREASE BEAM INNER CHORD HAS THREE SMALL AREAS OF CORROSION FR 18-22. REMOVED CORROSION; REMOVED AND REPLACED CREASE BEAM INNER CHORD IAW ATR SRM.SDR COEA2011040111903Frame · damagedHEAVY CK COE / MAJOR REPAIR: PERFORM CUTOUT AND SRM REPAIR TO FRAME 44 TO ACCESS PRESSURE BULKHEAD TO FOM. (REF: NR 100029) PERFORMED CUTOUT; FABRICATED AND INSTALLED LT AND RT REPAIR SPLICES, LT AND RT UPPER AND LOWER ANGLE SPLICE PER ATR SRM.SDR COEA2011032610903Floorbeam · corrodedHEAVY CK COE / MAJOR REPAIR / LEVEL 2 CORROSION: CORROSION ON UPPER FLANGE OF FLOORBEAM 9 AT PILOTS/COPILOTS SEAT FITTINGS. REPAIR PER STRUCTURAL REPAIR INSTRUCTIONS AND STRUCTURAL REPAIR APPROVAL SHEET FROM ATR.SDR COEA2011032509903Crease Beam · corrodedHEAVY CK COE / MAJOR REPAIR / LEVEL 2 CORROSION: LT CREASE BEAM INNER CHORD SPLICE FR 23 HAS CORROSION (LENGTH 6.5", WIDTH .910 ", DEPTH .025"). REMOVED CORROSION FROM CHORD SPLICE. FABRICATED AND INSTALL NEW REPLACEMENT LT CREASE BEAM CHORD SPLICE IAW ATR7SDR COEA2011032308903Skin · damagedHEAVY CK COE / MAJOR REPAIR: LOWER SKIN MOUNT SURFACE FOR DME 2 ANTENNA HAS TOOLING MARKS BY THE FORWARD LT NUT PLATE. BLENDED TOOLING MARKS BY FWD LT NUT PLATE AT DME 2 ANTENNA; FABRICATED AND INSTALLED REPAIR DOUBLER & MATCHED DRILLED SKIN, INSTALLED DME ASDR COEA2011032307903Crease Beam · corrodedHEAVY CK COE / MAJOR REPAIR / LEVEL 2 CORROSION: RT CREASE BEAM WEB FR 17-18 IS CORRODED ON THE UPPER AND LOWER SURFACES (LENGTH .750", WIDTH .200", DEPTH .020"). REMOVED CORROSION, VERIFIED CRACK FREE; FABRICATED AND INSTALLED REPLACEMENT CREASE BEAM WEB FRSDR COEA2011032206903Frame · corrodedHEAVY CK COE / LEVEL 2 CORROSION / MAJOR REPAIR: RT FR 25 HAS A SMALL AREA OF CORROSION ON THE AFT SIDE AT FLOOR LEVEL (LENGTH: .4", WIDTH .4", DEPTH .040"). CORROSION DAMAGE ON FRAME 25 RT FLOOR LEVEL BLENDED AND MAPPED. REPAIRED PER STRUCTURAL REPAIR INSTSDR COEA2011032205903Crease Beam · corrodedHEAVY CK COE / LEVEL 2 CORROSION: RT CREASE BEAM INNER CHORD FR 22-23 CORRODED. REMOVED CORROSION PER SRM. INSTALLED OEM RT CREASE BEAM INNER CHORD FR 13-FR 23 PER ATR42 SRM.SDR COEA2011032204903Crease Beam · corrodedHEAVY CK COE / LEVEL 2 CORROSION: LT CREASE BEAM WEB FR 17-18 CORRODED ON UPPER SURFACE. REMOVED CORROSION PER SRM; REPLACED CREASE BEAM WEB WITH OEM COMPONENT.SDR COEA2011031103903Plate · corrodedHEAVY CK COE / MAJOR REPAIR / LEVEL 2 CORROSION: FLOOR PLATE RT SEAT HAS SEVERAL AREAS OF PITTING CORROSION TOP SURFACE COMMON TO SEAT MOUNT LOCATIONS. REMOVED CORROSION, REMOVED AND REPLACED SEAT FITTINGS.SDR COEA2011031102903Plate · corrodedHEAVY CK COE / MAJOR REPAIR / LEVEL 2 CORROSION: FLOOR PLATE FOR PILOTS SEAT HAS PITTING CORROSION TOP SURFACE COMMON TO SEAT MOUNT LOCATIONS. REMOVED CORROSION, REMOVED AND REPLACED SEAT FITTINGS.SDR COEA2011041419903Crease Beam · corrodedHEAVY CHECK / COE / CORROSION LEVEL 2: REMOVED CORROSION IAW ATR 42 SRM. REMAINING MATERIAL THICKNESS FOUND TO BE OUT OF LIMITS. REMOVED WEB, LOCATED, MATCH-DRILLED AND DEBURRED NEW WEB. INSTALLED WEB, LT CREASE BEAM WEB 17 - 18.SDR COEA2011030301903Floorbeam · damagedHEAVY CHECK / COE / MAJOR REPAIR: WHILE WORKING REPAIR ON LONGITUDINAL FLOORBEAM AT FR 26 & 25.5 RBL FOUND INTERSECTING FASTENER HOLES IN TOP FLANGE OF FLOORBEAM 26. REPAIRED PER SRM / COMPLEX BUT CONSIDERED MINOR REPAIR.SDR COEA2009051203903Actuator · defectiveTRAINING FLIGHT 100: NOSE GEAR DID NOT RETRACT AFTER TAKEOFF AND MAIN RETRACTED SLOWLY AND ONE AT A TIME. MX REMOVED AND REPLACED NLG ACTUATOR. OPS TEST FLIGHT WAS PERFORMED AND REVEALED EXCESSIVE RETRACTION TIME. MX REMOVED AND REPLACED RT MLG ACTUATOR. PESDR COEA2009031702903Skin Panel · corrodedFOUND IN COE. MAJOR REPAIR, LEVEL 2 CORROSION. CORROSION FOUND ON INNER FUSELAGE SKIN, UNDER STRINGER 19L BETWEEN FRAMES 33L & 34L. BLEND OUT OF CORROSION ON SKIN BEYOND ALLOWABLE LIMIT. CUT OUT DAMAGED SECTION OF SKIN. INSTALLED DOUBLER AND FILLER UNDER SDR COEA2009031301903Stringer · corrodedMAJOR REPAIR, LEVEL 2 CORROSION. CORROSION FOUND UNDER STRINGER 19L BETWEEN FRAMES 33L AND 34L. CUT STRINGER 6 INCHES FWD OF FRAME 33 AND 6 INCHES AFT OF FRAME 34. SPLICED IN A NEW SECTION OF STRINGER FROM FWD OF FRAME 33 TO AFT OF FRAME 34.SDR COEA0804903Skin · corrodedMAJOR REPAIR & LEVEL 2 CORROSION. LT LOWER BELLY SKIN INNER SURFACE IS CORRODED BELOW RECIRCULATION DUCT SUPPORT ON FRAME 24. S/D ATR SRAS (STRUCTURAL REPAIR APPROVAL SHEET) WITH REPAIR INSTRUCTION DO/TS-4977/08-10961 ISSUED FOR DAMAGE REMOVAL & REPAIR. CSDR COEA0803903Frame · corrodedMAJOR REPAIR & LEVEL 2 CORROSION. LT LOWER FRAME 24 SEGMENT IS CORRODED BELOW RECIRCULATION DUCT SUPPORT. S/D CUT THE FRAME ASSY WITH A STEPPED CUT FROM STRINGER 16L TO 16R AND FROM STRINGER 17L TO 17R. SPLICED IN NEW FRAME ASSEMBLY WITH SPLICES AT STRINGSDR COEA0802903Oil Cap · unsecureAIR TURNBACK, & ENG SHUTDOWN: FLT 8813 CPR TO JAC: ON CLIMBOUT FROM CPR AT APPROXIMATELY 500 FT AGL. THE CREW NOTICED FLUCTUATING OIL PRESSURE ON THE NR 1 ENG FOLLOWED BY AN AUDIO MASTER WARNING AND LOW OIL PRESSURE LIGHT. A PRECAUTIONARY ENG SHUTDOWN OF NSDR COEA0801903Windshield · crackedAIR TURNBACK, FLT NR 100. ON CLIMB OUT, THE FO WINDSHIELD CRACKED. CABIN PRESSURE WAS REDUCED AND THE WINDSHIELD HEAT WAS TURNED OFF. THE CREW ELECTED TO RETURN TO DEPARTURE. THE AC MADE A SAFE AND NORMAL FLIGHT AND LANDING. REPLACED RT WINDSHIELD. (K)SDR COEA0703903Stringer · corrodedDURING HEAVY CHECK, MAINTENANCE FOUND CORROSION ALONG STRINGER 16R BETWEEN FRAME 22 AND FRAME 23. THE STRINGER WILL NEED TO BE INSTALLED IN SECTIONS WITH REPAIR SLICES. THIS WILL RESULT IN A MAJOR REPAIR. REMOVED STRINGER 16R FROM FRAME 22 TO FRAME 23. INSSDR COEA0702903Stringer · corrodedDURING HEAVY CHECK MAINTENANCE, FOUND AREAS OF LEVEL 2 CORROSION ALONG STRINGER 17R FROM FRAME 15 TO 23 WITH A MAXIMUM DEPTH OF .010 INCH. THE STRINGER WILL NEED TO BE INSTALLED IN SECTIONS WITH REPAIR SLICES. THIS WILL RESULT IN A MAJOR REPAIR. (M)SDR COEA0701903Fitting · corrodedAREAS OF LEVEL 2 CORROSION ON FORWARD OUTBOARD CORNER OF RIGHT MAIN LANDING GEAR BULKHEAD FRONT SPAR ON FRAME 25. BLENDED OUT CORROSION AND REINFORCED FITTING AND STRAP. COMPLIED WITH SB ATAR42-53-0155 ON RT SIDE AND FOUND SB ATR42-53-0155 PCW ON LT SIDE. RSDR COEA0708903Skin · corrodedDURING HEAVY CHECK, FOUND CORROSION ON FUSELAGE SKIN COMMON TO VHF 1 LOWER ANTENNA MATING SURFACE. LEVEL 2 CORROSION REQUIRED REPLACEMENT OF ANTENNA DOUBLER. REMOVED LOWER VHF 1 ANTENNA DOUBLER AND FABRICATED AND INSTALLED NEW DOUBLER IAW ATR42 SRM. (M)SDR COEA0707903Keelbeam · corrodedFOUND EXFOLIATING CORROSION ON UNDERSIDE OF KEEL BEAM WEB PLATE BETWEEN FRAME 27 AND 27A. REMOVED FAIRING ATTACH BRACKET FROM KEEL BEAM WEB PLATE AT FRAME 26BL0. REMOVED AND INSTALLED NEW FABRICATED WEB PLATE AND FAIRING ATTACH BRACKET AT FRAME 26 BL0 IAW ATSDR COEA0712903Bulkhead · crackedDURING HEAVY CHECK, FOUND CRACK ON FRAME 25 LT AND RT OUTBOARD LOWER SIDE OF HYDRAULIC LINE CUTOUT. MAINTENANCE FOUND SB ATR42-53-0120 HAD BEEN PREVIOUSLY COMPLIED WITH. COMPLIED WITH SB ATR42-53-0121 ON BOTH LT AND RT SIDES FOR FRAME 25 HYDRAULIC LINES CUT SDR COEA0711903Stringer · corrodedDURING HEAVY CHECK, FOUND CORROSION ON LT MLG KEEL BEAM SPECIAL STRINGER FROM FRAME 25 TO FRAME 27. REMOVED CORROSION FROM KEEL BEAM STRINGER 21. REMOVED AND REPLACED SPECIAL STRINGER 21 IAW ATR42 SRM. (M)SDR COEA0706903Sill · corrodedDURING HEAVY CHECK MAINTENANCE, FOUND CORROSION ON LT AND RT UPPER SURFACES OF LOWER SIDEBOX AT STRINGER 14 CREASEBEAM BETWEEN FRAME 26 AND 27. REMOVED CORROSION AND REPAIRED IAW SRI DO/TS-709/07-8327 AND DO/TS-709/07-8327 WITH REFERENCE TO SRAS DOTS-640/07, SDR COEA0705903Frame · damagedDURING HEAVY CHECK MAINTENANCE FOUND DENT AND CRACK IN CARGO COMPARTMENT FRAME 23 BETWEEN STRINGERS 19-20 RT. FABRICATED REPAIR DOUBLER AND INSTALLED TO FRAME 23 BETWEEN STRINGERS 19-20 RIGHT SIDE IAW ATR42 SRM. (M)SDR COEA0704903Window Frame · dentedDURING HEAVY CHECK MAINTENANCE FOUND DENT ON CAPTAIN WINDSHIELD FRAME UPPER POST. REMOVED WINDSHIELD, NO CRACKS FOUND. DENT DRESSED BACK PER DO/TS-386/07-8256. WINDSHIELD INSTALLED. REFERENCE SRAS DO/TS-386/07. 3978 AS A PERMANENT REPAIR. (M)SDR COEA0709903Bulkhead · corrodedCORROSION LEVEL 2, DURING HEAVY CHECK, FOUND CORROSION AT FRAME 27, RIGHT WHEEL WELL REAR SPAR BULKHEAD, BOTTOM SURFACE OF LOWER FLANGE FROM BL 0 TO BL 4R. BLENDED OUT CORROSION AND NO CRACKS NOTED. REPAIRED IAW SRM DO/TS-784/07-8383 WITH REF TO SRAS DO/TS 7SDR COEA0710903Keelbeam · corrodedCORROSION LEVEL 2, DURING HEAVY CHECK, FOUND CORROSION ON BOTTOM SIDE OF KEEL BEAM CHORD FROM AFT EDGE TO 4 INCHES OF AFT EDGE. REMOVED KEEL BEAM CHORD FROM FRAMES 25-27 AND REMOVED CORROSION. FABRICATED AND INSTALLED NEW KEEL BEAM CHORD IAW ATR42 SRM. (M)SDR COE2006F00002Antenna · failedTWO AIR TURNBACKS SAME DAY, SAME AIRCRAFT, FOR RADAR. FIRST TIME, RADAR FAILED AFTER DEPARTURE. SECOND TIME, RADAR WOULD ONLY PAINT PARTIAL SCREEN. FIRST TIME RADAR RT WAS REPLACED. SECOND TIME, RADAR RT AND ANTENNA ASSY WERE REPLACED. NO FURTHER PROBLEMS
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