N912FX
Service difficulty reports · 98
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 = 'N912FX' 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 = 'N912FX' 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 COEA2013052903912Skin · dentedHEAVY CHECK COE/MAJOR REPAIR: FOUND DENT DAMAGE TO SKIN BETWEEN FRAMES 11-12 AND STRINGER 13R-14R. REPAIR PER ATR42 SRM 53-00-00 FIG 403.SDR COEA2013051701912Skin · dentedHEAVY CHECK COE/MAJOR REPAIR: DENT DAMAGE TO SKIN BETWEEN FR 12-13 AND STRINGER 18L-19L. MAJOR REPAIR PER ATR 42 SRM 53-00-00.SDR COEA2013061110912Floor Support · corrodedDURING HEAVY CHECK, CORROSION FOUND ON LONGITUDINAL FLOOR SUPPORT TEE ANGLE UNDER RT SIDE OF COCKPIT PEDESTAL FRAMES 5 & 7. BLENDED OUT CORROSION.SDR COEA2013062819912Stiffener · corrodedDURING HEAVY CHECK, RT HORIZONTAL STAB REAR SPAR STIFFENERS HAVE CORROSION. FABRICATED AND REPLACED PARTS WITH NEW IAW SRM 55-11-10, FIG 102, REV 99.SDR COEA2013061217912Fitting · corrodedDURING HEAVY CHECK, FOUND CORROSION ON THE RT ELEVATOR HORN FITTING. REPLACED RT ELEVATOR.SDR COEA2013061113912Stiffener · corrodedDURING HEAVY CHECK, RT HORIZONTAL STABILIZER REAR SPAR STIFFENERS HAVE CORROSION. REPLACED PART WITH NEW IAW SRM 55-11-10, FIG 102, REV 99. MAJOR REPAIR.SDR COEA2013053104912Bulkhead · scratchedHEAVY CHECK COE/MAJOR REPAIR: FWD SIDE OF FWD PRESSURE BULKHEAD IS SCRATCHED AT UPPER LEFT AREA NEAR UPPER LEFT RADOME. REPAIRED PER IAW SRAS DT/S-2705/13.SDR COEA2013061115912Skin · corrodedDURING HEAVY CHECK, AFT AVIONICS COMPARTMENT DOOR 835 HAS PEELING PAINT & CORROSION ON FWD & AFT INTERNAL SURFACES. INSTALLED DOUBLER REPAIR IAW SRAS DT/S-2711/13. MAJOR REPAIRSDR COEA2013061216912Skin · damagedDURING HEAVY CHECK, LT SIDE HORIZONTAL STABILIZER UPPER SURFACE HAS THREE SMALL DENTS WITH CORE DAMAGE/DISBONDS. MAJOR REPAIR.SDR COEA2013061112912Skin · debondedDURING HEAVY CHECK, RT SIDE HORIZONTAL STABILIZER INBD UPPER SURFACE HAS POSSIBLE AREA OF SKIN DISBOND. MAJOR REPAIR OF DOUBLER IAW SRAS. MAJOR REPAIR.SDR COEA2013060606912Floor Support · crackedHEAVY CHECK COE/MAJOR REPAIR: LEFT LONGITUDINAL FLOORBEAM IS CRACKED AT FWD SIDE OF FRAME 40. REPAIR PER EO 5315-01 REV D.SDR COEA2013060605912Floor Support · crackedHEAVY CHECK COE/MAJOR REPAIR: LEFT LONGITUDINAL FLOORBEAM IS CRACKED AT FWD SIDE OF FRAME 28. REPAIR PER EO 5315-01 REV D.SDR COEA2013052302912Floor Support · crackedHEAVY CHECK COE/MAJOR REPAIR: RIGHT LONGITUDINAL FLOORBEAM IS CRACKED AT AFT SIDE OF FRAME 19. REPAIR PER EO 5315-01.SDR COEA2013061111912Doubler · corrodedDURING HEAVY CHECK, CORROSION ON LOWER BEACON SUPPORT PLATE, UPPER SIDE OF PANEL 193AL. FABRICATE AND REPLACE PART WITH NEW IAW SRM.SDR COEA2011062120912Skin Panel · dentedHEAVY CHECK COE / MAJOR REPAIR / DAMAGE: DENT OUT OF LIMITS WITH CREASE 4.4 INCHES FORWARD OF FRAME 45 AT LEFT STRINGER 9. STRINGER SPLICE FROM 5.5 INCHES AFT OF FRAME 44 TO 12.5 INCHES FORWARD OF FRAME 46. COMPLETE SPLICE MEASURES 25.5 INCHES. REFERENCE: SDR COEA2011060819912Skin · corrodedWO 101935 NR 600012 HEAVY CK COE / MAJOR REPAIR / LEVEL 2 CORROSION: WING TANK LOWER SURFACE HAS EXFOLIATON I NJET PUME CUTOUT (LENGTH 1.5", WIDTH 1.7", DEPTH .030"). REMOVED CORROSION AND REPAIRED PER ATR42 STRUCTURAL REPAIR INSTRUCTIONS AND SRAS, MAJOR REPSDR COEA2011060818912Skin Panel · dentedWO 101935 NR 200015 HEAVY CK COE / MAJOR REPAIR: DENT OUT OF LIMITS WITH GOUGE 3 INCHES FWD OF FRAME 16, 4.8 INCHES ABOVE RT STR 14 (.060" WIDE X 105" LENGTH). REPAIRED PER ATR42 STRUCTURAL REPAIR MANUAL.SDR COEA2011060317912Skin · corrodedWO 101935 NR 100061: HEAVY CK COE / MAJOR REPAIR / LEVEL 2 CORROSION: FUSELAGE BELLY SKIN INNER SURFACE CORRODED AT DME NR 2 CUTOUT BETWEEN FRAMES 8 & 9, BL 0 (LENGTH 2.0", WIDTH 1.5", DEPTH .030"). REPAIR PER ATR42 STRUCTURAL REPAIR MANUAL.SDR COEA2011060316912Skin · corrodedWO 101935 NR 100049 HEAVY CK COE / MAJOR REPAIR / LEVEL 2 CORROSION: LOWER EXTERNAL FUSELAGE SKIN HAS CORROSION UNDER DME 1 ANTENNA (LENGTH 2.2", WIDTH 1.5", DEPTH .030"). REMOVED CORROSION AND DAMAGED SKIN COMMON TO DME 1 ANTENNA. FABRICATED REPAIR DOUBLERSDR COEA2011053115912Skin Panel · damagedWO 103546 N4 4 HEAVY CK COE / MAJOR REPAIR: FOUND DISTORTION TO FUSELAGE SKIN FROM FR 19 TO FR 20, BETWEEN STR 1L & 1R. REPAIR PER STRUCTRUAL REPAIR INSTRUCTIONS FROM ATR.SDR COEA2011052514912Floor Support · corrodedWO 101935 NR 100046 HEAVY CK COE / LEVEL 2 CORROSION : FLOOR SUPPORT BEAM AT FLOORBEAM 39 LT SIDE JUST INBOARD OF THRESHOLD IS CORRODED (LENGTH 1.7", WIDTH 2.0", DEPTH .050"). REMOVED CORRODED FLOOR SUPPORT BEAM AND CLIP AND INSTALLED NEW PER ATR42 SRM.SDR COEA2011052013912Angle · nickedWO 101935 NR 300001 HEAVY CK COE / MAJOR REPAIR: AFT PRESSURE BULKHEAD CHORD AFT SURFACE, PERIPHERAL ANGLE HAS 3 NICKS AT APPROXIMATELY THE 8 O'CLOCK POSITION. REPAIR PER STRUCTURAL REPAIR INSTRUCTIONS FROM ATR.SDR COEA2011051912912Skin · corrodedWO 101935 NR 500010 HEAVY CK COE / MAJOR REPAIR / LEVEL 2 CORROSION: LT WING AT RIB 5 INTERNAL HAS CORROSION ON THE LOWER SURFACE UNDER THE ENGINE FEED JET PUMP (LENGTH 1.5", WIDTH 1.5", DEPTH .047"). REMOVE CORROSION AND REPAIR PER STRUCTURAL REPAIR INSTRUCSDR COEA2011051811912Crease Beam · corrodedWO 101935 NR 100008 HEAVY CK COE / MAJOR REPAIR / LEVEL 2 CORROSION: LT CREASE BEAM WEB DOUBLER AFT OF FR 17 IS CORRODED (LENGTH 1.5", WIDTH 1.4", DEPTH .012"). REMOVED CORROSION, FABRICATED AND INSTALLED NEW CREASE BEAM WEB DOUBLER.SDR COEA2011051710912Crease Beam · corrodedWO 101935 NR 100042 HEAVY CK COE / MAJOR REPAIR / LEVEL 2 CORROSION: LT CREASE BEAM WEB BETWEEN FRAMES 13 & 14 HAS CORROSION ON TOP SURFACE (LENGTH .5", WIDTH .6", DEPTH .010"). REMOVED CORROSION, FABRICATED AND INSTALLED CREASE BEAM WEB.SDR COEA2011051709912Crease Beam · corrodedWO 101935 NR 100002 HEAVY CK COE / MAJOR REPAIR / LEVEL 2 CORROSION: LT CREASE BEAM INNER CHORD FR 17-18 HAS AREAS OF CORROSION (LENGTH 1.5", WIDTH 1.0", DEPTH .011"). REMOVED CORROSION AND REPAIR PER STRUCTURAL REPAIR MANUAL.SDR COEA2011051608912Crease Beam · corrodedWO 101935 NR 100053 HEAVY CK COE / MAJOR REPAIR / LEVEL 2 CORROSION: FOUND CORROSION ON FR 17 ON FWD SURFACE AND I/B FLANGE COMMMON TO CREASE BEAM INNER CHORD (DEPTH .01'). REPAIR PER STRUCTURAL REPAIR INSTRUCTIONS AND SRAS FROM ATR.SDR COEA2011051607912Crease Beam · corrodedWO 101935 NR 100014 HEAVY CK COE / MAJOR REPAIR / LEVEL 2 CORROSION: RT CREASE BEAM WEB FR 17-18 HAS CORROSION ON THE UPPER AND LOWER SURFACES (LENGTH .75", WIDTH .5", DEPTH .009"). REMOVED CORROSION, FABRICATED AND INSTALLED RT CREASE BEAM WEB.SDR COEA2011051606912Crease Beam · corrodedWO 101935 NR 100013 HEAVY CK COE / MAJOR REPAIR / LEVEL 2 CORROSION: RT CREASE BEAM WEB FR 18-19 HAS CORROSION ON UPPER AND LOWER SURFACES (LENGTH .5", WIDTH .5", DEPTH .009"). REMOVED CORROSION, FABRICATED AND INSTALLED NEW CREASE BEAM WEB.SDR COEA2011051605912Crease Beam · corrodedWO 101935 NR 100009 HEAVY CK COE / LEVEL 2 CORROSION: RT CREASE BEAM INNER CHORD IS CORRODED FR 17-23 (LENGTH 2.5", WIDTH 1.0", DEPTH 0.10"). REMOVED CORROSION, REMOVED AND REPLACED INNER CHORD WITH OEM PART.SDR COEA2011051104912Floorbeam · corrodedWO 101935 NR 100043 HEAVY CK COE / MAJOR REPAIR / LEVEL 2 CORROSION: FLOORBEAM 13 HAS AREAS OF BARE METAL & CORROSION BETWEEN STRINGERS 14L & 14R. (DEPTH .012"). REPAIR PER STRUCTURAL REPAIR INSTRUCTIONS & SRAS FROM ATR.SDR COEA2011051103912Crease Beam · corrodedWO 101935 NR 100006: HEAVY CK COE / MAJOR REPAIR / LEVEL 2 CORROSION: LT CREASE BEAM WEB FR 21-22 HAS CORROSION ON THE UPPER SURFACE (LENGTH .800", WIDTH .800", DEPTH .011"). REPAIR PER STRUCTURAL REPAIR INSTRUCTIONS FROM ATR.SDR COEA2011051002912Crease Beam · corrodedWO 101935 NR 100009 HEAVY CK COE / LEVEL 2 CORROSION: RT CREASE BEAM INNER CHORD IS CORRODED FR 17 - 23. REMOVED AND REPLACED CHORD WITH OEM PART.SDR COEA2011051001912Floorbeam · crackedWO 101935 NR 100044 HEAVY CK COE / MAJOR REPAIR: RT LONGITUDINAL FLOORBEAM AT FWD SIDE OF FLOORBEAM 18 IS CRACKED. CUT OUT CRACKED SECTION OF LONGITUDINAL FLOORBEAM BETWEEN FR 17 & 18. FABRICATED AND INSTALLED FLOORBEAM PER EO.SDR COEA2009101405912Vent · openAIR TURN BACK SEA FLT 7202, CARGO DOOR VENT OPENED AFTER TAKEOFF. PILOT RETURNED TO SEA. MAINTENANCE ACCOMPLISHED INSPECTION AND OPERATIONAL CHECK OF CARGO DOOR LATCHING AND LOCKING MECHANISM. REINSTALLED ACCESS PANEL. PERFORMED HARD LANDING INSPECTION DUESDR COEA2009040604912Skin · canningEXTERNAL FUSELAGE JUST AFT OF LT NOSE JACKING POINT IS OIL CANNED. APPLIED SRM REPAIR CONSISTING OF THE FABRICATION AND INSTALLATION OF AN INTERCOSTAL ACROSS THE AFFECTED SKIN AREA.SDR COEA2009033003912Floorbeam · corrodedIN HEAVY CHECK MAJOR REPAIR: FOUND LEVEL 2 CORROSION ON TOP SIDE OF FLOORBEAM 17 AT FRAME 17. CORROSION REMOVED AND BLENDED FOUND TO EXCEED DAMAGE TOLERANCE. CUT OUT AND FABRICATED REPAIR SPLICE FOR FLOORBEAM.SDR COEA2009032502912Crease Beam · damagedIN HEAVY CHECK: FOUND FR27 LT SIDE AT CREASE BEAM DAMAGED. DAMAGED AREAS EXCEED OUT OF DAMAGE TOLERANCE.SDR COEA2009032601912Floorbeam · corrodedCORROSION FOUND ON LT FLOORBEAM AT FRAME 25L UNDER LT OTBD SEAT TRACK. BLEND OUT BEYOND SRM LIMIT. ATR STRUCTURAL REPAIR INSTRUCTION DO/TS-1351/09-11496 ISSUED FOR THIS DISCREPANCY. BLEND OUT CORROSION IAW ATR INSTRUCTIONS AND LEAVE "AS IS".SDR COEA2009010204912Ahrs · failedAIR TURNBACK: FLT NR 8202 JNU-SIT. ENROUTE TO SIT FROM JNU THE CAPT'S EFIS (ELECTRONIC FLIGHT INSTRUMENTS SYSTEM) COMP HEADING, PITCH, AND ATTITUDE FAILED. SINCE COPILOT'S SYSTEM WAS OPERATING NORMALLY. A DECISION TO RETURN TO JNU WAS MADE SINCE PARTS WERE NOSDR COEA0803912Indicator · failedAIR TURN BACK, ENROUTE, THE CAPT`S VSI FLASHED MOMENTARILY CAUSING A TCAS FAIL AND RESOLUTION ALERT, THEN WENT BLANK. SINCE THE COPILOT`S SYSTEM WAS OPERATING NORMALLY. A DECISION TO RETURN TO DEPARTURE WAS MADE SINCE PARTS WERE AVAILABLE THERE AND MAINTENANCESDR COEA0802912Adc · intermittentOVER FLY KTN & SIT: FLT 7202 SEA-KTN-SIT-JNU. EN ROUTE TO KTN FROM SEA THE NR 1 AIR DATA COMPUTER (ADC) STARTED TO INTERMITTENTLY FAIL. SINCE THE NR 2 ADC AND STANDBY SYSTEM WERE OPERATING NORMALLY, A DECISION TO BYPASS KTN AND SIT SO MAINTENANCE COULD BE SDR COEA0801912Wire Harness · wornOVER FLY. FLT NR 7202, ENROUTE, THE NAVIGATION LIGHT CIRCUIT BREAKERS ALL POPPED. THE CREW ATTEMPTED TO RESET THE CIRCUIT BREAKERS BUT THEY WOULD NOT STAY IN. A DECISION WAS MADE TO OVER FLY AND CONTINUE TO OTHER DESTINATION FOR MAINTENANCE. NO EMERGENCY WASDR COEA0704912Switch · failedAIR TURNBACK. FLIGHT NR 7202. DURING CLIMB 12 MILES OUT, THE NR 2 BLEED VALVE WOULD NOT OPEN AND FAULTED. RESET UNSUCCESSFUL CREW ELECTED TO RETURN TO DEPARTURE. AC LANDED NORMALLY. REPLACED NR 2 ENGINE BLEED PUSH BUTTON SWITCH. (K)SDR COEA0703912Frame · damagedIN HEAVY CHECK AT COE, FOUND TOOLING DAMAGE ON FUSELAGE FRAME 42 AFT PRESSURE BULKHEAD RT LWR DOUBLER. DAMAGE DOUBLER CUT AWAY AND SPLICE PERFORMED IAW ATR SRAS DO/TS-2637/07 4169. (K)SDR COEA0702912Intercostal · crackedIN HEAVY CHECK AT COE FOUND CRACKED INTERCOSTAL IN AFT CARGO DOOR UPPER FWD POSITION. REMOVED AND REPLACED INTERCOSTAL. (K)SDR COE2006F00000Adc · failedAIR TURNBACK, F/O INSTRUMENTATION LOST DATA FROM NR2 AIR DATA COMPUTER (ADC) IN FLIGHT. MAINTENANCE REMOVED AND REPLACED NR 2 AIR DATA COMPUTER (ADC). AIRCRAFT WAS RETURNED TO SERVICE. (K)SDR COE2005F00004Bpcu · inoperativeAIR TURNBACK, PILOT REPORTED (CAC SOUNDED, ELEC CAP WARNING ILLUMINATED, ADI (CPL DATA INVALID) ANNUNCIATION ON T/O ROLL. MAINTENANCE REPLACED EMER BATTERY CHARGER RELAY PROTECTION UNIT (BPU). OPS CHECKED GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (K)
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