N603FE
Service difficulty reports · 488
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 = 'N603FE' 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 = 'N603FE' 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 03FDEA01523Skin · corrodedLT WING - UPPER SURFACE, STA 118 TO 162, FWD AREA BETWEEN FRONT AND REAR AREA, NUMEROUS PLACES FOUND CORRODED. LT WING UPPER SURFACE, NUMEROUS CORRODED PLACES AT FORWARD AREA BETWEEN FRONT AND REAR AREA STA 118 TO 162 BLENDED OUT AS PER SRM 51-21-01 VOSDR 03FDEA01441Hinge · corrodedO/B FLAP I/B HINGE (FLAP SIDE) LOWER ATTACHMENT BORE FOUND CORRODED. O/B FLAP I/B HINGE (FLAP SIDE) LOWER ATTACHMENT I/B & O/B BORES. CORROSION REMOVED AND REPAIRED AS PER FEDEX EA 1-5750-71894. WINGS - TRAILING EDGE & TRAILING EDGE DEVICES - LT O/B FLAP SDR 03FDEA01442Hinge · corrodedLT WING- O/B FLAP I/B HINGE (FLAP SIDE) UPPER ATTACHMENT BORE FOUND CORRODED. LT WING- O/B FLAP I/B HINGE (FLAP SIDE) UPPER ATTACHMENT BORE CORROSION REMOVED AND REPAIRED AS PER FEDEX EA 1-5750-71894. WINGS - TRAILING EDGE & TRAILING EDGE DEVICES - LT SDR 03FDEA01528Support Bracket · corrodedRT WING OUTBOARD FLAP INBD HINGE (FLAP SIDE) LOWER OUTBOARD ATTACHMENT BORE FOUND CORRODED.SDR 03FDEA01530Support Bracket · corrodedRT WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE) LOWER INBOARD ATTACHMENT BORE FOUND CORRODED.SDR 03FDEA01443Structure · corrodedLT WING O/B FLAP O/B HINGE (FLAP SIDE) LOWER ATTACHMENT BORE FOUND CORRODED.SDR 03FDEA01444Structure · corrodedLT WING O/B FLAP O/B HINGE (FLAP SIDE) UPPER BORE FOUND CORRODED.SDR 03FDEA01413Hinge · corrodedLT WING- I/B FLAP O/B HINGE LOWER BORE FOUND CORRODED. (FLAP SIDE).SDR 03FDEA01524Hinge · crackedLT WING OUTBOARD FLAP HINGE (A/C) SIDE FWD SEAL ATTACHMENT STRIP FOUND CRACKED.SDR 03FDEA01525Bracket · corrodedRT WING OUTBOARD FLAP OUTBOARD HINGE (A/C SIDE) SIDE ATTACHMENT BORE FOUND CORRODED.SDR 03FDEA01440Structure · corrodedLT WING O/B FLAP I/B HINGE (A/C SIDE) PIVOT BEARING ATTACHMENT BORE FOUND CORRODED. LT WING O/B FLAP I/B HINGE (A/C SIDE) PIVOT BEARING ATTACHMENT BORE CORROSION REMOVED AND REPLACED AS PER EA 1-5750-72654 .SDR 03FDEA01431Rib · crackedLT WING L/E CAVITY, NR 16 RIB CRACKED. LT WING- L/E CAVITY, NR 16 RIB REMOVED AND REPLACED AS PER SRM 51-31-01 VOL 2.SDR 02FDEA00789Mfc · malfunctionedAFTER TAKEOFF, RECEIVED A LEVEL 2 AIR MANF 1 FAIL ALERT. DUMPED 62000 LBS FUEL AND MFC FAULT REVIEW LAST LEG SHOWS IN FLIGHT FAULTED MFC PNEU 1 OUT AND ON GROUND FAULTED ALARM (PNEU 1 Z4 OVHT). INSPECT Z4 FOR AIR LEAK NOT FOUND. TROUBLESHOT FIM 36-23-06 R ASDR 02FDEA00282Fitting · corrodedLT MLG RETRACT ACTUATOR FITTING FOUND PITTING CORROSION ON UPPER FWD BOLT HOLE. REMOVED AND REPLACED ACTUATOR FITTING PER SRM 51-31-01 VOL 11.SDR 02FDEA00281Fitting · corrodedRT MLG RETRACT ACTUATOR FITTING FOUND CORRODED ON LOWER BOLT HOLES. REMOVED AND REPLACED ACTUATOR FITTING PER SRM 51-31-01 VOL 11.SDR 02FDEA00283Fitting · corrodedLT MLG RETRACT ACTUATOR FITTING FOUND BOTH LOWER MOUNTING BOLT HOLES CORRODED (PITTING CORROSION). REMOVED AND REPLACED ACTUATOR FITTING PER SRM 51-31-01 VOL 11.SDR 02FDEA00255Stanchion · corrodedEXFOLIATION CORROSION ON FWD CARGO COMP AFT BULKHEAD VERT BEAM SUPPORT (U-CHANNEL) AT X =+ 56 IN. REMOVED AND REPLACED STANCHION PER DWG A6A7094.SDR 02FDEA00253Stanchion · corrodedEXFOLIATION CORROSION ON FWD CARGO COMPT AFT BULKHEAD VERT BEAM SUPPORT (U-CHANNEL) AT X=+ 8 IN. REMOVED AND REPLACED STANCHION PER DWG A6A7094.SDR 02FDEA00254Stanchion · corrodedINTERGRANULAR CORROSION ON FWD CARGO COMPT AFT BULKHEAD VERT BEAM SUPPORT (U-CHANNEL) AT X=+ 29 IN. REMOVED AND REPLACED STANCHION PER DWG A6A7094.SDR 02FDEA00252Stanchion · corrodedEXFOLIATION CORROSION ON FWD CARGO COMPT VERTICAL BEAM SUPPORT (U-CHANNEL) AT X=-8 IN. REMOVED AND REPLACED STANCHION PER DWG A6A7094.SDR 01FDEA00758Aileron · malfunctionedAILERON DEFLECT DISAGREE LIGHT ILLUM'D LEVEL 2 ALERT ON FLAP RETRACTION. COMPLETED QRH PROCEDURES, LIGHT REMAINED ILLUM'D. CONFIG PAGE SHOWED RIGHT OUTBOARD AILERON EXTENDED. HARD RIGHT AILERON CONTROL REQ'D THIS INPUT ALL THE WAY TO TOUCHDOWN.SDR 01FDEA00205Support Fitting · crackedRT WING L/E STA XFS 1004, NR 16 SLAT TRACK SUPPORT FITTING CRACKED. *S/D* REMOVED AND REPLACED PER DWG ARB2850.SDR 01FDEA00204Stop Fitting · crackedCABIN R3 DOOR PLUG AFT LWR STOP FITTING FOUND CRACKED. *S/D* REMOVED AND REPLACED PER SRM 51-31-01, VOL II, IAW DWG NO ADA 3462. HOLES TRANSFERRED TO NEW STOP FITTING AS PER SRM 51-35-01, VOL II.SDR 00FDEA00720Transmitter · malfunctionedDURING CLIMBOUT RECEIVED ALERT FLAP DISAGREE. REMOVED AND REPLACED LEFT INBD FLAP POSITION TRANSMITTER PER MM 27-54-04. BOTH FCC FLAP SYS RTS PASSED, WORKS NORMAL.SDR 00FDEA00135Control Cable · twistedAILERON LOCKOUT SLAT INPUT CABLE 85B. REMOVED AND REPLACED AS PER MM 20-20-06. ADJ AND OPER CK CARRIED OUT PER MM 27-10-00, FOUND SATISFACTORY.SDR 00FDEA00115Seat Track · crackedMAIN DECK SEAT TRACK CRACKED AT 635 X= 47.5 LEFT 557. MAIN DECK SEAT TRACK CRACK AT 755 X= 8.5 RIGHT 640. REMOVED AND REPLACED PER SRM 51-31-01 VOL II, SRM 53-70-00 FIG I VOL I.SDR 00FDEA00136Cargo Track · corrodedUPPER CARGO COMP FLOOR TRACK HOLE FROM BS 1361 TO BS 1481 AT RBL 106 CORRODED. REMOVED AND REPLACED PER SRM 53-70-00 FIG 3 VOL 1.SDR 00FDEA00102Seat Track · crackedMAIN DECK SEAT TRACK CRACKED AT BS 635 X PLUS 27.5 RT. REMOVED AND REPLACED PER SRM 53-70-00 FIG 1 VOL 1.SDR 00FDEA00101Sill · damagedUPPER CARGO DOOR JAMB FORWARD LWR SILL SKIN DAMAGED. REPAIR, FABRICATED PER SRM 53-50-00 FIG 4 VOL 1.SDR 00FDEA00043Bleed Valve · malfunctioned00-24 - AC AIR TURN BACK DUE TO NR 1 BLD LOW ALERT. NR 2 BLD WAS ALREADY DEFERRED. NO LEAKS NOTED, FOR T/S MANUALLY CLOSED AND LOCKED APU LOAD BLD VALVE. REMOVED AND INSTALLED APU LOAD BLEED VALVE REF WRI 49-50/5443. PRESSURE DECAY TEST ALL PASSED. A/C OSDR 99FDEA00445Mfdu · failed99-260 - AT FLT LEVEL 330, ON CLIMB-OUT RECEIVED AIR MANIFOLD 2 FAIL GOT ALERT AIR SYS 1/2 FAIL, NOTE THE NR 2 ENGINE BLD VALVE DID NOT CLOSE. REMOVED AND REPLACED THE MANIFOLD FAILURE CONTROLLER PER MM 36-23-00-5. SYSTEM TEST NORMAL.SDR 98FDEA00766Strut · deformedCENTERLINE LAND GEAR CARRIER AYG 7216-503 CRACK AND RING AYG7217-1 DEFORMED. 1.5 INCH CRACK AT SHOCK STRUT PISTON TOP CHROME AREA. REMOVED AND REPLACED CTR LAND GEAR RING IAW MM 32-15-01-8. REMOVED AND REPLACED LAND GEAR PISTON WITH CLG CARRIER SERVICEABLE FSDR 98FDEA00752Tail Cone · crackedSNRM 413 TAIL CONE STRUCTURE OF RT HINGE FAIL DURING OPER: AREA DAMAGED DURING EXTEND OPER. REMOVED AND REPLACED TAIL CONE RT HINGE STRUCTURE DAMAGE LWR SKIN, INTERCOSTAL, RIBS, FRAME, PNL AND DOUBLERS PER DWG AKC 7504 AND OPER CK MM 53-52-01-2 FND SAT.SDR 97FDEA00254Sensor · dirtySIN - PASSING FL260 IN CLIMB, AIRCRAFT EXPERIENCED BUFFET AND VIBRATION. CHECKED CONFIGURATION PAGE AND IT SHOWED THE NOSE GEAR UNSAFE. RETURNED TO SINGAPORE AT 260KTS .REVIEWED CFDS LRU FAULT - NO FAULT. PER CREW INFO ALERT SHOWN ON PILOT DISPLAY VISUAL ISDR 96FDEA01695Trim Cylinder · malfunctionedAFTER TAKEOFF, GEAR HANDLE WOULD NOT RAISE TO RETRACT THE GEAR. REMOVED AND REPLACED THE BOGIE TRIM CYCLINDER, OPS CHECK GOOD.SDR 96FDEA01572Fan Air Valve · malfunctionedNR 2 ENG BLEED AIR HIGH TEMP, POWER REDUCED, ALERT WENT OUT. REMOVED AND REPLACED NR 2 ENG FAN AIR VALVE SYS OPS CHECK GOOD WITH ENG RUN.SDR 96FDEA01448Spar Chord · corrodedNR 6047. RIGHT WING TOP TE PANEL OUTBOARD OF NR 5 SPOILER BULGING AT AFT SPAR STA XORS 782 - 827. SUBJECT CORROSION HAS BEEN REMOVED, AREA TREATED AND PAINTED PER 51-21-01.SDR 96FDEA01447Spar Chord · corrosionNR 5050 AND 505. LEFT WING REAR SPAR UPPER CHORD ANGLE AFT TANG BETWEEN STA XORS 670 TO 830 HAS NUMEROUS AREAS OF EXFOLIATION CORROSION. REMOVED CORROSION PER SRM 51-21-01.
Back to N603FE