N919FX
Service difficulty reports · 156
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 = 'N919FX' 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 = 'N919FX' 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 COEA2013073108919Skin · corrodedDURING HEAVY CHECK, LT WING SKIN LOWER SURFACE HAS CORROSION BY THE WATER DRAIN VALVE OTBD OF THE NACELLE. REPAIRED IAW SRAS DT/S-4114/13.7909.SDR COEA2013073107919Frame · gougedDURING HEAVY CHECKK, FRAME 20 UPPER FLANGE IS GOUGED AND BENT JUST OTBD OF STRINGER 21L. REPAIR IAW SRAS DT/S-4112/13.7905.SDR COEA2013072404919Shear Tie · damagedDURING HEAVY CHECK, LT FRAME 26 SHEAR TIE HAS TOOL DAMAGE S12-13L. REPLACED WITH OEM PART IAW SRM 51-25-01 AND 53-51-40, FIG 103, ITEM 85B.SDR COEA2013071903919Frame · crackedDURING HEAVY CHECK, RT FRAME 26 IS CRACKED AT THE STRINGER 13 CUTOUT. REPLACED IAW SRM 53-25-01 AND 53-51-40, FIG 103.SDR COEA2013071902919Frame · crackedDURING HEAVY CHECK, LT FRAME 26 IS CRACKED AT STRINGER 13L CUTOUT. REPLACED IAW SRM 53-25-01 AND 53-51-40, FIG 103.SDR COEA2013071701919Floor Support · crackedDURING HEAVY CHECK, RT LONGITUDINAL FLOOR SUPPORT JUST FWD OF FRAME 33 IS CRACKED. REMOVED DAMAGED SECTION AND SPLICED IN A NEW SECTION IAW E.O. 5315-01.SDR COEA2013073114919Spar · corrodedDURING HEAVY CHECK, RT HORIZONTAL STABILIZER REAR SPAR, LOWER FLANGE HAS SEVERAL AREAS OF CORROSION. REPAIR IAW SRAS.SDR COEA2013073113919Spar · corrodedDURING HEAVY CHECK, RT HORIZONTAL STABILIZER REAR SPAR, UPPER FLANGE HAS SEVERAL AREAS OF CORROSION. REPAIR IAW SRAS.SDR COEA2013073112919Spar · corrodedDURING HEAVY CHECK, LT HORIZONTAL STABILIZER REAR SPAR, LOWER FLANGE HAS CORROSION BETWEEN THE 3RD & 4TH VERTICAL STIFFENER FROM INBD HINGE POINT. REPAIR IAW SRAS.SDR COEA2013073111919Spar · corrodedDURING HEAVY CHECK, LT HORIZONTAL STABILIZER REAR SPAR, UPPER FLANGE HAS SEVERAL AREAS OF LEVEL 2 CORROSION. REPAIR IAW SRAS.SDR COEA2013073110919Strap · corrodedDURING HEAVY CHECK, RT HORIZONTAL STABILIZER T/E STRAP HAS SEVERAL AREAS OF CORROSION. REPLACED.SDR COEA2012010301919Seal · wornAIR TURNBACK: FLIGHT 8216: ON CLIMB RECEIVED A MASTER CAUTION AND "ENG" LIGHT ILLUMINATED ON THE CAP. PILOT ELECTED TO RETURN. AIRCRAFT LANDED AT AIRPORT VFR WITHOUT INCIDENT. MAINTENANCE RE-INDEXED PROP TRANSFER TUBE TO PCU, REPLACED SEALS ON TRANSFER TUBSDR COEA2011111729919Skin · corrodedHEAVY CK COE / MAJOR REPAIR / LEVEL 2 CORROSION: EXTERIOR FUSELAGE SKIN AT MAIN CARGO DOOR CUT OUT FORWARD LOWER CORNER HAS AREAS OF CORROSION (LENGTH 18", WIDTH 8", DEPTH .020"). REPAIR PER SRAS DT/S-485/11...6792, SEE ALSO M7 DRAWING FOR DTI 42-25000 AND 8SDR COEA2011111628919Tab · damagedHEAVY CK COE / MAJOR REPAIR: RT AILERON TAB, INBOARD TRAILING EDGE OF TAB IS DAMAGED. REMOVED DAMAGE, FABRICATED U-CHANNEL SPLICE REPAIR TO RT AILERON FIXED TAB TRAILING EDGE PER SRM.SDR COEA2011101205919Structure · corrodedHEAVY CK COE / MAJOR REPAIR / LEVEL 2 CORROSION: RT AFT DOOR THRESHOLD OUTBOARD CHORD HAS CORROSION AROUND THE FASTENERS ON UNDERSIDE. ALSO FOUND LEVEL 2 CORROSION ON WEBS P/N S53671318212 (LENGTH 4", WIDTH 4", DEPTH .028") AT STRINGER 14R, FRAME 37 - 39 ANDSDR COEA2011110727919Stiffener · corrodedHEAVY CK COE / MAJOR REPAIR / LEVEL 2 CORROSION: RT HORIZONTAL ELEVATOR COVE HAS 4 STIFFENERS WITH CORROSION BETWEEN RIB 2 AND 4. (ALL 4 LENGTH 4", WIDTH 2"). 2 STIFFENERS FABRICATED AND INSTALLED; PN S55171200204 AND PN S55171200206; 2 STIFFENERS REPLACEDSDR COEA2011110726919Stiffener · corrodedHEAVY CK COE / MAJOR REPAIR / LEVEL 2 CORROSION: LT HORIZONTAL ELEVATOR COVE HAS 6 STIFFENERS WITH CORROSION BETWEEN RIB 2 AND 3. (ALL 6 LENGTH 4", WIDTH 1"). 4 STIFFENERS FABRICATED AND INSTALLED; PN S55171200202, PN S55171200204, PN S55171200206, PN S55171SDR COEA2011110425919Stiffener · corrodedHEAVY CK COE / LEVEL 2 CORROSION. LT HORIZONTAL ELEVATOR COVE HAS 4 STIFFENERS WITH CORROSION BETWEEN RIBS 3 AND 4 (ALL 4:LENGTH 4", WIDTH 1"). REMOVED AND REPLACED ALL 4 STIFFENERS (P/N S5517120022801, S5517120021801, S5517120022001 AND S5517120023001).SDR COEA2011110324919Frame · damagedHEAVY CK COE / MAJOR REPAIR. ACCESS FWD SIDE OF AFT PRESSURE BULKHEAD TO REPAIR SPLICE TO FRAME 44. REPAIR FRAME 44-21 INCHES TO THE RIGHT AND TO THE LEFT OF BL 0 PER STRUCTURAL REPAIR INSTRUCTIONS.SDR COEA2011110123919Stiffener · corrodedSTIFFENER AT LT HORIZONTAL CENTER ELEVATOR HAS LEVEL 2 CORROSION. (LENGTH 1", WIDTH .75", DEPTH .027"). MOVED AND REPLACED STIFFENER IAW SRM.SDR COEA2011102621919Shear Web · corrodedHEAVY CK COE / MAJOR REPAIR / LEVEL 2 CORROSION. RT AFT SHEAR WEB AT FR 27 SUPPORT ANGLE HAS CORROSION. (LENGTH .5", WIDTH .5", DEPTH .019"). REPAIR PER STRUCTURAL REPAIR INSTRUCTIONS FROM ATR.SDR COEA2011102622919Rib · chafedHEAVY CK COE / MAJOR REPAIR. RT WING LOWER STRIP SLAT RIB 19-21 IN REFUEL AREA IS CHAFED. REPAIR PER STRUCTURAL REPAIR INSTRUCTIONS FROM ATR.SDR COEA2011102620919Skin · damagedHEAVY CK COE / MAJOR REPAIR. FOUND CORROSION ON PREVIOUS TOOLING DAMAGE FRAME 13 LT INNER SKIN 2 INCHES AFT OF FRAME 12 BELOW CREASE BEAM WEB. REPAIR PER STRUCTURAL REPAIR INSTRUCTIONS FROM ATR.SDR COEA2011102619919Bulkhead · corrodedHEAVY CK COE / MAJOR REPAIR: FWD PRESSURE BULKHEAD HAS A PIT AT BL-10 RT, BELOW THE WEATHER RADAR. REPAIR PER ATR42 STRUCTURAL REPAIR MANUAL, FABRICATED AND INSTALLED PLUG, SHIM AND DOUBLER.SDR COEA2011102618919Structure · corrodedHEAVY CK COE / MAJOR REPAIR / LEVEL 2 CORROSION. CORROSION ON SURFACE OF INTERIOR RT LOWER SIDE BOX BETWEEN FR 25-27. (LENGTH 13", WIDTH 2.5", DEPTH .021"). REPAIR PER STRUCTURAL REPAIR INSTRUCTIONS FROM ATR.SDR COEA2011102417919Skin · corrodedFOUND LEVEL 2 CORROSION ON SURFACE OF LT WING LEADING EDGE PANEL 514. REMOVE CORROSION AND REPAIRED PER SRM AND SRAS.SDR COEA2011102116919Mount · corrodedHEAVY CK COE / LEVEL 2 CORROSION. LT CONTROL CABLE POST FWD "T" EXTRUSION MOUNT CORRODED AROUND NUT PLATE FWD I/B BOTTOM SIDE BETWEEN FR 12-13. (LENGTH 2", WIDTH 3", DEPTH .03"). REMOVE AND REPLACE WITH OEM PART PER ATR42 SRM.SDR COEA2011102115919Skin · corrodedHEAVY CK COE / MAJOR REPAIR / LEVEL 2 CORROSION. EXTERNAL SKIN, FWD AND CENTER PANEL AT FRAME 23, BL 0, STR 20L - 18R HAS CORROSION. (LENGTH 36", WIDTH 3", DEPTH .009"). REMOVE CORROSION AND REPAIR CENTER PANEL SKIN AND FWD PANEL SKIN PER STRUCTURAL REPAIR ISDR COEA2011102014919Attach Fitting · corrodedHEAVY CK COE / LEVEL 2 CORROSION / RT WING RIB 6 LOWER REAR SPAR ATTACH FITTING FOR UPPER TRAILING EDGE SUPPORT BRACE EXFOLIATEING. (LENGTH 1.5", WIDTH 1.5", DEPTH EXFOLIATED). REMOVE AND REPLACE FITTING.SDR COEA2011102013919Doubler · gougedHEAVY CK COE / MAJOR REPAIR / EXTERIOR WINDSHIELD CENTER LOWER JOINT (NODE 5) HAS A GOUGE ON LT SIDE. REPAIR PER STRUCTURAL REPAIR INSTRUCTIONS FROM ATR.SDR COEA2011102012919Longeron · corrodedHEAVY CK COE / LEVEL 2 CORROSION: LONGERON AT 80VU RACK INBOARD AFT MOUNT HAS CORROSION (LENGTH 2", WIDTH 2", DEPTH .012"). REMVOED AND REPLACED LONGERON WITH OEM PART.SDR COEA2011102011919Support · corrodedHEAVY CK COE / LEVEL 2 CORROSION. BELLY FAIRINGS SUPPORT STRUCTURE - INTERCOSTAL 19R CORRODING BETWEEN FR 22A- 23A. REMOVE AND REPLACE WITH OEM PART PER SRM.SDR COEA2011101310919Crease Beam · corrodedHEAVY CK COE / LEVEL 2 CORROSION: LT CREASE BEAM WEB FR 12-13 CORRODED. (LENGTH .75", WIDTH .25", DEPTH .016"). REMOVED AND REPLACED CREASE BEAM WEB.SDR COEA2011101309919Intercostal · corrodedHEAVY CK COE / LEVEL 2 CORROSION: BELLY FAIRING REMOVABLE INTERCOSTAL AND ATTACH ANGLES AT OUTBOARD EDGE OF PANEL 192FR, FR 23A-24A ARE CORRODED. (LENGTH 8", WIDTH 2", DEPTH .024"). REMOVED AND REPLACED INTERCOSTAL CHANNEL WITH OEM PART.SDR COEA2011101308919Intercostal · corrodedHEAVY CK COE / LEVEL 2 CORROSION: BELLY FAIRING REMOVABLE INTERCOSTAL AND ATTACH ANGLES OUTBOARD EDGE OF PANEL 192FR, FR 22A-23A ARE CORRODED. (LENGHT 6", WIDTH 1.5", DEPTH .024") REMOVED AND REPLACED INTERCOSTAL CHANNEL WITH OEM PART.SDR COEA2011101307919Intercostal · corrodedHEAVY CK COE / LEVEL 2 CORROSION: BELLY FAIRING REMOVABLE INTERCOSTAL AND ATTACH ANGLES AT OUTBOARD EDGE OF PANEL 191FL, FR 23A-24A ARE CORRODED. (LENGTH 5", WIDTH 3", DEPTH .071") REMOVED AND REPLACED CHANNEL WITH OEM PART.SDR COEA2011101306919Intercostal · corrodedHEAVY CK COE / LEVEL 2 CORROSION: BELLY FAIRINIG REMOVABLE INTERCOSTAL AND ATTACH ANGLES AT OUTBOARD EDGE OF PANEL 191FL, FR 22A-23A ARE CORRODED. (LENGTH 8", WIDTH 2", DEPTH .028") REMOVED AND REPLACED INTERCOSTAL CHANNEL WITH OEM PART.SDR COEA2011101305919Structure · corrodedHEAVY CK COE / LEVEL 2 CORROSION: DISCREPANCY: RT AFT DOOR THRESHOLD OUTBOARD CHORD HAS CORROSION AROUND THE FASTENERS ON UNDERSIDE. (LENGTH 52", WIDTH 4", DEPTH .024"). REMOVE AND REPLACE CHORD WITH OEM PART.SDR COEA2011101204919Angle · corrodedHEAVY CK COE / LEVEL 2 CORROSION. BOTH BELLY FAIRING INTERCOSTALS ANGLES WHERE PANAL 191FL MOUNT HAVE CORROSION BEYOND LIMITS. (LENGTH 18", WIDTH 2.5", DEPTH .010"). REMOVED AND REPLACED 2 ANGLES WITH OEM PARTS.SDR COEA2011101203919Support Angle · corrodedHEAVY CK COE / LEVEL 2 CORROSION: DISCREPANCY: BELLY FAIRINGS SUPPORT STRUCTURE INTERCOSTAL 19R BETWEEN FR 23A - 24A CORREDED BEYOND LIMITS (LENGTH 12", WIDTH 2.5", DEPTH .006"). REMOVE AND REPLACE SUPPORT ANGLE WITH OEM.SDR COEA2011100702919Frame · corrodedDURING HEAVY CHECK FOUND LEVEL 2 CORROSION FRAME 13 AT LT CREASE BEAM. REPAIRED IAW SRM.SDR COEA2011100701919Stringer · corrodedHEAVY CK COE / MAJOR REPAIR / LEVEL 2 CORROSION: DISCREPANCY: STRINGER 20R HAS LEVEL 2 CORROSION BETWEEN FR 19-20 (LENGTH 2", WIDTH 1", DEPTH .040"). REPAIRED PER ATR42 STRUCTURAL REPAIR MANUAL.SDR COEA2010041301919Warning System · activatedAIR TURNBACK FLIGHT 7757 AT MAF: WHEN CREW SELECTED GEAR UP, THE MAIN GEAR WOULD NOT RETRACT AND RECEIVED A LOW PRESSURE LIGHT ON THE GREEN HYDRAULIC SYSTEM. THE NR 2 ACW SYSTEM FAILED. CREW ELECTED TO RETURN TO MAF. INSPECTED C/B AND FOUND THE GREEN SYSTESDR COEA2009102104919Connector · looseENGINE SHUTDOWN: WHEN CLIMBING TO CRUISE PWR NR 2 ENG TORQUE BECAME ERRATIC WITH PWR CHANGES. CREW NOTICED THE RT ENGINE APPEARED TO BE SURGING OUT OF CONTROL. PILOT ELECTED SHUTDOWN NR 2 ENG. NO EMERGENCY WAS DECLARED. T/S FOUND CONNECTOR FOR TSC, ECU, SDR COEA2009080202919Doubler · corrodedFOUND IN COE HEAVY CHECK: LEVEL 2 CORROSION / MINOR REPAIR. EXTERIOR FUSELAGE UPPER GPS ANTENNA MOUNTING DOUBLER BETWEEN FRAMES 17 - 18 HAS LEVEL 2 CORROSION. REMOVED DOUBLER AND INSTALLED NEW FABRICATED DOUBLER.SDR COEA2009080103919Doubler · corrodedFOUND IN COE HEAVY CHECK: LEVEL 2 CORROSION / MINOR REPAIR. EXTERIOR FUSELAGE T2CAS ANTENNA DOUBLER BETWEEN FRAMES 19 & 20 (FORE & AFT) AND STRINGER 19 & 20 (RIGHT TO LEFT) HAS LEVEL 2 PITTING CORROSION. REMOVED DOUBLER AND INSTALLED NEW FABRICATED DOUBLER.SDR COEA2009073001919Floorbeam · crackedFOUND IN COE HEAVY CHECK: MAJOR REPAIR: CARGO COMPARTMENT, LONGITUDINAL FLOORBEAM AFT OF FRAME 20 UNDERSIDE IN RADIUS IS CRACKED. NOTE: .25 INCH CRACK IN RADIUS .5 INCH AFT OF FLOORBEAM 22, 25.5 INCHES RIGHT OF BL 0. REMOVED AND REPLACED DAMAGED SECTION OSDR COEA0804919Skin · crackedDAMAGE TO AFT LT PASSENGER. DOOR SKIN DENTED AND CRACKED BEYOND SRM LIMITS. ATR SRAS DO/TS-3648.08, 4803 ISSUED TO REPAIR DOOR. DOOR SKIN DAMAGED AREA CUT OUT AND A DOUBLER INSTALLED. DOUBLER INSTALLED USING SRAS DO/TS-3648/08-10619 INSTRUCTIONS. (K)SDR COEA0803919Skin · damagedMAJOR REPAIR: DAMAGE TO AFT LT DOOR AND FUSELAGE. IMPACT DAMAGE TO LT AFT FUSELAGE SKIN DOUBLER PLATE AFT OF AFT PASSENGER DOOR. FUSELAGE SKIN DENTED WITH CRACKING FOUND AT ONE FASTENER. FUSELAGE SKIN DAMAGED AREA CUT OUT AROUND CRACKED FASTENER HOLE AND DOUBSDR COE2008F00001Indicator · failedABORTED TAKEOFF, FLT NR 8202: DURING TAKEOFF ROLL THE CREW NOTICED THAT ANALOG PORTION ON THE NR 2 ENGINE TORQUE GAGE WAS INOPERATIVE. TAKEOFF WAS ABORTED AND THE AC WAS SAFELY TAXIED BACK TO THE BLOCKS. REMOVED AND REPLACED THE TORQUE GAUGE. (K)
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