N604FE
Service difficulty reports · 447
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 = 'N604FE' 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 = 'N604FE' 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 04FDEA00104Hinge · corrodedLT OUTBOARD FLAP INBOARD HINGE (FLAP SIDE); INBOARD PIVOT HOLE FOUND CORRODED AT BORE AREA. LT OUTBD FLAP INBD HINGE (FLAP SIDE) INBD PIVOT HOLE BORE CORROSION REMOVED AND REPAIRED AS PER EA 1-5750-74280, WINGS - LT AND RT OUTBOARD FLAP - INBOARD HINGE BRACKESDR 04FDEA00103Hinge · corrodedRIGHT OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), INBOARD PIVOT HOLE FOUND CORRODED AT BORE AREA. COMPLIED WITH FEDEX EA 1-5750-74275, WINGS - RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED.SDR 04FDEA00102Hinge · corrodedLT OUTBOARD FLAP INBOARD HINGE (FLAP SIDE); INBOARD PIVOT HOLE FOUND CORRODED AT SPOT FACES. LT OUTBD FLAP INBD HINGE (FLAP SIDE) INBD PIVOT HOLE SPOT FACES CORROSION REMOVED AND REPAIRED AS PER EA 1-5750-74280, WINGS - LT AND RT OUTBOARD FLAP - INBOARD HINGESDR 04FDEA00101Hinge · corrodedRT OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), INBOARD PIVOT HOLE FOUND CORRODED AT SPOT FACES. COMPLIED WITH FEDEX EA 1-5750-74275, WINGS - RT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED.SDR 04FDEA00100Hinge · corrodedRIGHT OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), PIVOT ATTACH PIN LOCK PLATE BOLT HOLE FOUND CORRODED ON BORE AND SPOT FACES. RT OTBD FLAP INBD HINGE (FLAP SIDE), PIVOT ATTACH PIN LOCK PLATE BOLT HOLE BORE AND SPOT FACES CORROSION REMOVED AND REPAIRED AS PER EASDR 04FDEA00098Hinge · corrodedRIGHT OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), INBOARD PIVOT HOLE CORRODED AT BORE AREA. RT OUTBD FLAP INBD HINGE (FLAP SIDE) INBD PIVOT HOLE BORE CORROSION REMOVED AND REPAIRED AS PER EA 1-5750-74280, WINGS - LT AND RT OUTBOARD FLAP - INBOARD HINGE BRACKET SDR 04FDEA00097Hinge · corrodedRIGHT OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), INBOARD PIVOT HOLE CORRODED ON SPOT FACES AREA. RT OUTBD FLAP INBD HINGE (FLAP SIDE) INBD PIVOT HOLE SPOT FACES CORROSION REMOVED AND REPAIRED AS PER EA 1-5750-74280, WINGS - LT AND RT OUTBOARD FLAP - INBOARD SDR 04FDEA00096Support · crackedRIGHT OUTBOARD FLAP, UP STOP RIB SUPPORT ISLAND FOUND 01 CRACK APPROX 0.25 INCH LONG AT OUTBOARD SIDE. RT OTBD FLAP, UP STOP RIB SUPPORT ISLAND REPAIRED AS PER EA 1-5750-74278, OUTBOARD TRAILING EDGE FLAPS - SECONDARY UP STOP - REPAIR.SDR 04FDEA00088Splice · crackedLEFT CENTER CARGO NR 49 LONGERON SPLICE FOUND CRACKED BETWEEN STA 5- 113 TO STA 1541. CRACKED NR 49 LONGERON SPLICE AT LT CENTER CARGO BETWEEN STA 5-113 TO STA 1541 REMOVED AND REPLACED WITH NEW FABRICATED PART AS PER DRAWING A5A7114 AND INSTALLED AS PER SRM SDR 04FDEA00087Splice · crackedRIGHT CENTER CARGO NR 47 LONGERON SPLICE FOUND CRACKED BETWEEN STA 5- 113 TO STA 1541. CRACKED LONGERON SPLICE AT RT CTR CARGO NR 447, STA 5-113 TO STA 1541, REMOVED AND REPALCED WITH NEW SPLICE AS PER SRM 51-33-01 VOL II.SDR 04FDEA00086Splice · crackedRT CENTER CARGO NR 45 LONGERON SPLICE FOUND CRACKED BETWEEN STA 1661 TO 1681. CRACKED NR 45 LONGERON SPLICE AT RT CENTER CARGO BETWEEN STA 1661 TO 1681 REMOVED AND REPLACED WITH NEW FABRICATED PART AS PER DRAWING AFA7113 AND INSTALLED AS PER SRM 51-33-01, SDR 04FDEA00069Slat Track · crackedLEFT WING LEADING EDGE - NR 16 SLAT TRACK INTERNAL STRUCTURE CRACKED AT INBOARD TRACK BRACKET. LT WING LEADING EDGE NR 16 SLAT TRACK INTERNAL STRUCTURE I/B RIB REMOVED AND REPLACED AS PER SRM 51-33-01 VOL II AND EA 1-5750-74279, WINGS - LEFT HAND SLAT - FABRISDR 04FDEA00070Floor Support · crackedCABIN - FLOOR TRACKS CRACKED AT STA 5-78 RIGHT X=8.5. FLOOR TRACKS CRACKED AT STA 5-78 RT X=8.5 CARRIED OUT REPAIR IAW SRM 53-70-00 FIG 1 V1.SDR 04FDEA00071Floor Support · corrodedCABIN - FLOOR TRACKS CRACKED AT STA 635 RIGHT X=8.5. CRACKED FLOOR TRACKS AT STA 635 RT X=8.5 CARRIED OUT REPAIR IAW SRM 53-70-00 FIG 1 VOL. ISDR 04FDEA00072Floor Support · crackedCABIN - FLOOR TRACKS CRACKED AT STA 635 RIGHT X=47.5. FLOOR TRACKS CRACKED AT STA 635 RT X=47.5 CARRIED OUT REPAIR IAW SRM 53-70-00 FIG. 1 VOL. I.SDR 04FDEA00073Floor Support · crackedCABIN - FLOOR TRACKS CRACKED AT STA 635 LEFT X=47.5. CABIN, CRACKED FLOOR TRACKS AT STA 635 LT X=47.5 CARRIED OUT REPAIR IAW SRM 53-70-00 FIG. 1 VOL. ISDR 04FDEA00074Skin · crackedLEFT WING - ON LEADING EDGE SKIN PANEL INTERIOR FOUND SEVERAL CRACKS, STA XOS 510 UNDER REFUEL ACCESS PANEL. LEADING EDGE SKIN PANEL STA XOS 510 UNDER REFUEL ACCESS PANEL INTERIOR, CRACKED AREA REPAIRED AS PER SRM 57-10-00, FIG. 25, VOL. I.SDR 04FDEA00075Hinge Bracket · crackedLEFT INBOARD FLAP OUTBOARD HINGE (FLAP SIDE) MOST AFT UPPER BRACKET FOUND CRACKED. LT INBD FLAP OUTBD HINGE (FLAP SIDE) MOST AFT UPPER BRACKET REMOVED AND REPLACED AS PER SRM 51-33-01 VOL. II.SDR 04FDEA00076Hinge Bracket · crackedRT INBOARD FLAP OUTBOARD HINGE (FLAP SIDE) MOST AFT UPPER BRACKET FOUND CRACKED. RT INBD FLAP OUTBD HINGE (FLAP SIDE) MOST AFT UPPER BRACKET REMOVED & REPLACED AS PER SRM 51-33-01 V2.SDR 04FDEA00077Hinge Bracket · crackedLEFT INBOARD FLAP OUTBOARD HINGE (FLAP SIDE) FOUND 01 EA BRACKET CRACKED AT OUTBOARD SIDE APPROX 12 INCHES FROM FLAP LOWER SURFACE, 24 INCHES FROM FWD EDGE OF HINGE. LT INBD FLAP OTBD HINGE (FLAP SIDE) OTBD SIDE LOWER AREA 01 BRACKET EDGE CRACK TRIMMED OUT FSDR 04FDEA00078Slat Track · crackedRIGHT WING - NR 16 SLAT TRACK LEADING EDGE INBOARD BRACKET CRACKED. RT WING NR 16 SLAT TRACK LEADING EDGE INBD BRACKET REMOVED AND REPLACED AS PER SRM 51-33-01 VOL IISDR 04FDEA00079Hinge Bracket · crackedRIGHT WING - OUTBOARD FLAP INBOARD HINGE BRACKET (WING SIDE) SIDE LINK CRACKED. OUTBOARD FLAP INBOARD HINGE BRACKET (WING SIDE) SIDE LINK TENSION STRAP SUPPORT REMOVED AND REPLACED AS PER DAC SB57-10.SDR 04FDEA00080Splice · crackedRT CENTER CARGO NR 49 LONGERON SPLICE FOUND CRACKED BETWEEN STA 5-113 TO STA 1541. CRACKED NR 49 LONGERON SPLICE AT RT CENTER CARGO BETWEEN STA 5-113 TO STA 1541 REMOVED AND REPLACED WITH NEW FABRICATED PART AS PER DRAWING A5A 7114 AND INSTALLED AS PER SRM 51SDR 04FDEA00081Vane · corrodedLEFT OUTBOARD FLAP VANE NR 2, 3, 4 AND 5 T-FITTING (COUNTING FROM INBOARD) FOUND FWD HOLE CORRODED AT BORES. LT OUTBOARD FLAP VANE NR 2 TEE FITTING REPAIRED AS PER EA 1-5750-74288, LT & RT OUTBD FLAP - NR 2 FITTING SUPPORT VANE TO TRACK CORROSION.SDR 03FDEA01394Transmitter · failedON TAKEOFF RECEIVED LEVEL 2 "FLAP DISAGREE" ALERT. RIGHT INBOARD FLAP WENT TO 30 DEG., OTHER FLAPS WERE 25 DEG. RAN CHECKLIST AND RETURNED TO RPLB. ACN RELEASED FOR SERVICE PER MEL/CDL: 27-54-01CATEGORY: C EXPIRATION: 05SEP03 "MEL 27-54-01: FLAP POSITIOSDR 02FDEA00553Hinge Fitting · corrodedLT WING OUTBOARD FLAP OUTBOARD HINGE FITTING LWR MOUNTING SIDE CORRODED AFTER SEALANT REMOVAL. REMOVED AND REPLACED BRACKET ASSY PER MM 57-53-01-4.SDR 02FDEA00552Hinge Fitting · corrodedLT WING OUTBOARD FLAP INBOARD HINGE FITTING LOWER MOUNTING SIDE CORRODED AFTER SEALANT REMOVAL. REMOVED AND REPLACED BRACKET ASSY PER MM 57-53-01-4.SDR 02FDEA00551Bracket · corrodedRT WING OUTBOARD FLAP HINGE FITTING LWR MOUNTING SIDE CORRODED AFTER SEALANT REMOVAL. REMOVED AND REPLACED BRACKET ASSY PER MM 57-53-01.SDR 02FDEA00550Bracket · corrodedRIGHT WING OUTBOARD FLAP INBOARD HINGE FITTING LWR MOUNTING SIDE, FOUND HINGE FITTING & WASHERS CORRODED AFTER SEALANT REMOVAL. R&R BRACKET ASSY PER MM 57-53-01.SDR 02FDEA00331Actuator · failedON TAKEOFF AFTER SLATS RETRACTED LVL 2 AIL DEFLECT DISAGREE ALERT ILLUM'D. REMOVED AND REPLACED LT & RT INBOARD DEFLECT AILERON ACTUATORS PER MM 27-16-01-4. RIGGED, ADJUSTED AND TESTED OK.SDR 01FDEA00759Control Unit · failedLEFT ANTI SKID FAIL ALERT ON SHORT FINAL TO SFS HEAVY RAIN AND WET RUNWAY. EXERCISED GO-AROUND AND DIVERTED TO RPLL. GOT SAME A/S ALERT. RAN RED TAB AND LANDED AT RPLL. REMOVED AND REPLACED A/S CONTROL UNIT PER MM 32-45-01-4 & PERF'D R-T-S TEST PER MM 32-4SDR 01FDEA00591Seat Track · damagedNR 2 SEAT TRACK DAMAGED AT BS 1421 MAIN DECK COMPT. *S/D* SMOOTHED AND FOUND WITHIN LIMITS PER SRM 53-70-00 FIG 3.SDR 01FDEA00590Seat Track · damagedDAMAGED SEAT TRACK NR 8 BS 1361 TO 1401 8 IN AT MAIN CARGO DECK. *S/D* REMOVED AND REPLACED PER SRM 53-70-00 FIG 1 VOL 1.SDR 01FDEA00589Seat Track · damagedDAMAGED NR 3 SEAT TRACK BS 1059 MAIN CARGO COMPT. *S/D* REMOVED AND REPLACED PER SRM 53-70-00 FIG 1 VOL 1.SDR 01FDEA00586Doubler · crackedCENTER LG RT BULKHEAD DOUBLER BETWEEN BS 1360 - 1380 FOUND CRACKED. *S/D* REMOVED AND REPLACED DOUBLER PER DWG AEA0526.SDR 01FDEA00573Doubler · crackedCENTER LG LT BULKHEAD DOUBLER BETWEEN BS 1360 - 1380 FOUND CRACKED. *S/D* REMOVED AND REPLACED DOUBLER PER SRM 51-31-01, 51-21-02 VOL 2.SDR 01FDEA00588Bulkhead · crackedAFT FX INTERNAL FOUND CREW REST FWD BULKHEAD AT BS 2014.982 WITH FITTING QTY 1 CRACKED AT RBL 20. *S/D* REMOVED AND REPLACED BULKHEAD AND FITTING PER SRM 51-33-01, DWG AJL7140.SDR 01FDEA00587Seat Track · corrodedCABIN CORROSION FOUND ON SEAT TRACK CAVITY AROUND BS 540 & X=-8. *S/D* REMOVED AND REPLACED PER SRM 53-70-00 FIG 1 VOL 1.SDR 01FDEA00138Fuel Tank · flamed out01-051 #2 ENG FLAMED OUT ABOUT 1 PLUS 15 MIN OUT OF LAX. #2 TANK WAS FUELED TO KNOW QTY DUE TO INOP FUEL IND THE ENG WAS RESTART WITH FUEL CROSSFEED. FUEL SLIP RECK AND SHOW RELEASE FUEL HOWEVER #2 WAS UNDERFUELED BY 20,000 #. THE FUEL CREW DEBRIEF- #2 TANKSDR 00FDEA00793Warning System · activatedDURING R/O CHECK GOT A DEFLECTED AILERON DISAGREE LEVEL 2 ALERT.SDR 00FDEA00169Cylinder · corrodedRT MLG RETRACT ACTUATOR ROD END, INTERNAL BORE THREADS HAS CORROSION WITH PITTING NOTED. *S/D* REMOVED AND REPLACED PER MM 32-33-20-4. REFER TO WORK CARD 32 X 1701 PG 14 OF 42 FOR INSTALL.SDR 00FDEA00168Cylinder · corrodedLT MAIN GEAR RETRACT CYLINDER, UPON REMOVAL OF ACTUATOR ROD END, FOUND INTERNAL BORE THREADS CORRODED AND PITTED. *S/D* REMOVED AND REPLACED PER MM 32-33-20-4. WORK CARD 32 X 1702 14 OF 42 FOR INSTALL LT MAIN GEAR.SDR 99FDEA00161Access Door · damagedRT WING LEAD EDGE, SLAT DRIVE MECH ACCESS DOOR OPEN DURING AC TEST FLT CAUSING DAMAGE TO THE DOOR, SLAT NR 3 RT AND THE WING LEAD EDGE ADJACENT TO SLAT NR 3. REMOVED AND REPLACED SLAT DRIVE MECH PER MM 20-50-02-2. SKIN REPAIRED PER 57-10-00, RIB REPAIR STA 5SDR 97FDEA00035Pseu · malfunctionedAFTER TAKEOFF, RT MLG UNSAFE LIGHT ON BOTH PRIMARY AND SECONDARY GEAR INDICATION. CHECKED DOOR CYLINDER PISTON LENGTH IS WITHIN M/M LIMITS. REMOVED AND REPLACED PROX SWITCH ELECTRONICS UNIT. REMOVED AND REPLACED BOTH PRIMARY AND SECONDARY GEAR UP AND LATCHESDR 95FDEA01099Cowl Web · crackedNR 2 ENG INTERNAL NOSE COWL FWD BULKHEAD WEB AND LOWER CHORD IS CRACKED AT 4 O'CLOCK POS APPROX 1, PANEL 362GR. REMOVED AND REPLACED LOWER CHORD WEB PER SRM 51-00-00 (P/N AJC7564-45).SDR 95FDEA01098Blkhd Skin · damagedEA 1-5330-24396 SPLICE REPAIRED SKIN AT STA 62 LONGERON 36 TO 48 LT AND RT. PERMANENT REPAIR EA 1-5310-25112 REPAIRED PRESSURE BULKHEAD AT BS 595.SDR 95FDEA01097Frame · crackedRT/CENTER GEAR DOOR, 1B FWD CORNER ON INSIDE FRAME CRACKED APPROX 2. VERIFIED CRACK W/EDDY CURRENT, REMOVED DAMAGED SECTION OF DOOR FRAME, INSTALLED NEW SECTION OF FRAME (P/N AW87376-2) PER 53-00-7.
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