N601FE
Service difficulty reports · 546
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 = 'N601FE' 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 = 'N601FE' 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 04FDEA00833Panel · corrodedRIGHT WING UPPER SURFACE FIXED T/E PANELS FWD OF OUTBOARD AILERON FOUND WITH SEVERAL BULGES. COMPLIED WITH FEDEX EA 1-5710-76644 - WINGS - LEFT AND RIGHT HAND WING AFT UPPER SPAR CAP AFT TANG CORROSION REMOVAL AND REPAIR.SDR 04FDEA00832Panel · corrodedLEFT WING UPPER SURFACE FIXED T/E PANELS FWD OF OUTBOARD AILERON FOUND WITH BULGE. COMPLIED WITH FEDEX EA 1-5710-76644. LEFT AND RIGHT HAND WING - AFT UPPER SPAR CAP AFT TANG CORROSION REMOVAL AND REPAIR.SDR 04FDEA00834Skin · crackedFUSELAGE PAX DOOR 3 OFF CRACK ON INTERNAL PRIMARY DOUBLER OF LOWER FWD CORNER APPROXIMATELY .1875 INCH. CLEANED UP IAW SRM 53-00-01 FIG 1A VOL I. AND CARRIED OUT AS PER DAC NDT SPM PART 06-10-01-001 REV 11 AND FOUND NO CRACK EVIDENT.SDR 04FDEA00820Slat Track · crackedRT WING LEADING EDGE SLAT TRACK 16, I/B SUPPORT RIB FOUND CRACK. RT WING LEADING EDGE SLAT TRACK 16, I/B SUPPORT RIB REMOVED AND REPLACED AS PER SRM 51-31-01 VOL II.SDR 04FDEA00819Slat Track · crackedLEFT WING LEADING EDGE SLAT TRACK 16, I/B SUPPORT RIB FOUND CRACK. LT WING LEADING EDGE SLAT TRACK 16, I/B SUPPORT RIB REMOVED AND REPLACED AS PER SRM 51-31-01 VOL II.SDR 04FDEA00818Track · crackedNR 3 ENG RIGHT REVERSER COWL OF TRANSLATING COWL MOST UPPER TRACK END FOUND WITH CRACK. NR 3 ENG RT REVERSER TRANSLATING COWL REMOVED AS PER AMM 78-31-16-4. REPAIRED AS PER FAA 8130-3/FA2004/0118, & REINSTALLED AS PER AMM 78-31-16-4.SDR 03FDEA01598Pump · failedHYDRAULIC 3 FAILURE DURING FLIGHT. REMOVED AND REPLACED UPPER AND LOWER ENG DRIVEN HYD PUMP ASSY AS PER MM 29- 11-20-4, FOR LEAK CHK AND OPS CHK. REMOVED AND REPLACED PER MOCC REQUEST FOR PRECAUTIONARY.SDR 03FDEA01088Display · inoperativeCLIMBING THRU 18,000 FT BOTH "TIP LOW" (1 AND 3) LEVEL ONE ALERTS CAME ON SHORTLY AFTER FUEL SYSTEM SELF CORRECTED. UPON REACHING CRUISE FL 370 NOTICED FUEL DECREASING AT AN ABNORMAL RATE. ONE MINUTE LATER "FUEL QTY/USED CHK" LEVEL 2 ALERT CAME ON. AT THASDR 02FDEA00746Structure · corrodedHORIZ STAB INTERIOR , FOUND BARREL 27TH NUT HOLE AFTER CORROSION BLEND OUT, EXCEEDED SB LIMIT. R&R HORIZ STABILIZER PER EA 1-5510-66415.SDR 02FDEA00748Structure · corrodedHORIZ STAB INTERIOR, NR 16 RT BARREL NUT HOLE CORRODED. R&R HORIZ STABILIZER PER EA 1-5510-66415.SDR 02FDEA00743Structure · corrodedHORIZ STAB INTERIOR, FOUND BARREL NUT HOLE NR 35 AFTER CORROSION BLEND OUT, EXCEEDED SB LIMIT. R&R HORIZ STABILIZER PER EA 1-5510-66415.SDR 02FDEA00710Structure · corrodedHORIZ STAB INT, BARREL NUT HOLE 32R AFTER CORROSION BLEND OUT, EXCEEDED SB LIMIT. R&R HORIZ STAB PER EA 1-5510-66415.SDR 02FDEA00711Structure · corrodedHORIZ STAB INT, BARREL NUT HOLE NR 26R AFTER CORROSION BLEND OUT, EXCEEDED SB LIMIT. R&R HORIZ STABILIZER PER EA 1-5510-66415.SDR 02FDEA00713Structure · corrodedHORIZ STAB INT, BARREL NUT HOLE NR 23L AFTER CORROSION BLEND OUT, OUT OF SB LIMIT. R&R HORIZ STABILIZER PER EA 1-5510-66415.SDR 02FDEA00714Structure · corrodedHORIZ STAB INT BARREL NUT HOLE NR 24R AFTER CORROSION BLEND OUT, EXCEEDED SB LIMIT. R&R HORIZ STABILIZER PER EA 1-5510-66415.SDR 02FDEA00712Structure · corrodedHORIZ STAB INT, BARREL NUT HOLE NR 20R EXCEEDED SB LIMIT. R&R HORIZ STABILIZER PER 1-5510-66415.SDR 02FDEA00704Structure · damagedHORIZ STAB INTERIOR, FOUND BARREL NUT HOLE NR 19R BOTTOM SURFACE EXCEEDED LIMIT AS PER SB. R&R HORIZ STAB PER EA 1-5510-66415.SDR 02FDEA00705Structure · damagedHORIZ STAB INTERIOR, FOUND BARREL NUT HOLE NR 9R BOTTOM SURFACE EXCEEDED LIMIT AS PER SB. R&R HORIZ STAB PER EA 1-5510-66415.SDR 02FDEA00706Structure · damagedHORIZ STAB EXTERIOR, FOUND BARREL NUT HOLE NR 14R ELONGATED. R&R STAB HORIZ PER EA 1-5510-66415.SDR 02FDEA00707Structure · damagedHORIZ STAB INTERIOR, FOUND BARREL NUT HOLE NR 14L OUT OF SB LIMIT. R&R HORIZ STAB PER EA 1-5510-66415.SDR 02FDEA00708Structure · corrodedHORIZ STAB INTERIOR FOUND BARREL NUT HOLE NR 21 L BOTTOM SURFACE LOCAL BLENDOUT CORROSION EXCEEDED LIMIT AS PER SB. R&R HORIZ STAB PER EA 1-5510-66415.SDR 02FDEA00672Structure · corrodedAFTER CORROSION REMOVAL ON BARREL NUT HOLE NR 36 RT, BOTTOM SURFACE AND SIDEWALL BLEND OUT EXCEEDED LIMIT AS PER SB MD11-55-023. R&R HORIZ STAB PER EA 1-5510-66415.SDR 02FDEA00671Structure · corrodedAFTER CORROSION REMOVAL ON BARREL NUT HOLE NR 36 LT, BOTTOM SURFACE BLENDOUT EXCEEDED LIMIT AS PER SB MD11-55-023. R&R HORIZ STABILIZER PER EA 1-5510-66415.SDR 02FDEA00769Structure · corrodedCORROSION ON HORIZONTAL STABILIZER. R&R HORIZONTAL STABILIZER PER ME 11-55-023.SDR 02FDEA00609Structure · scratchedFUSELAGE RIGHT SIDE LWR SURFACE OF WING ROOT AT WING TO BODY FILLET (154AB) SCRATCHED. REMOVED & REPLACED SKIN PER EA. 1-5330-66000.SDR 01FDEA00783Wire · damagedWIRE BUNDLES IN RT WING ROOT LEADING EDGE BURNT.SDR 01FDEA00490Pump · burnedBOTH NR 1 & 2 HYD AUXILIARY PUMPS FOUND BURNT/DAMAGED DURING RT MLG WHEEL WELL CLEANING. REMOVED AND REPLACED BOTH PUMPS.SDR 01FDEA00445Fire Detector · intermittentON ARRIVAL INTERMITTENT ENG 1 FIRE (AURAL ALSO) WARN. SHOW AS LEVEL 1 ALERT. REMOVED AND REPLACED UPPER RIGHT FIRE DETECTOR ASSY PER MM 26-11-03-4. OPS CK OK. CLOSED COWLING.SDR 00FDEA00321Fitting · crackedSNRM 587 CRACK AT LT SIDE FWD RADIUS. SNRM 588 RT SIDE FWD RADIUS. *S/D* REMOVED AND REPLACED PER SRM 55-20-00 FIG 3 VOL 1 AND EA 1-5530-49647.SDR 00FDEA00322Seat Track · crackedSNRM 456 & 590 MAIN DECK, SEAT TRACK CRACKED AT BS 635 X = 27.5 RT. *S/D* REWORKED SEAT TRACK PER SRM 53-70-00 FIG 1 VOL 1.SDR 99FDEA00505Throttle · failed99-288 - ON T/O FROM LFPG, MISC DISPLAY IND NO AUTOLAND AND AUTOPILOT 1 AND 2 WOULD NOT ENGAGE. GOT AILERON DISAGREE ALERT. PERF FCC NR 1 AND 2 RTS PER MM 22-00-00-5, (TASK 22-00-00-701-801). ALL RTS PASSED DUE TO PREVIOUS HISTORY. CAT 2 PRECAUTIONARY AND SDR 99FDEA00231Pillow Block · corrodedPILLOW BLOCK ASSY ON RT CENTER LANDING GEAR HAS CORROSION ON A/C STRUCTURE PAD, BOLT HOLES AND ALIGNMENT PIN HOLE. *S/D* REMOVED CORROSION FROM CENTER LANDING GEAR, SHEAR PIN AND ATTACH BOLT HOLES PER SRM 53-40-00. DIMENSIONS ARE WITHIN SRM 53-40-00 REPAIR SDR 99FDEA00230Pillow Block · corrodedPILLOW BLOCK ASSY ON LT CTR LAND GEAR HAS CORROSION ON A/C STRUCTURE PAD, BOLT HOLES AND ALIGNMENT PIN HOLE. *S/D* REPAIRED LT PILLOW BLOCK MOUNTING PAD SURFACE AND BORES PER SRM 53-40-00 ON CTR GEAR ASSY.SDR 99FDEA00044Skin · corrodedCENTER WING UPPER SKIN ROUND WITH EXFOLIATION CORROSION AT BS 1229 STR 13, BS 1256 STR 14 AND BETWEEN BS XCW 118 AND XCW 100 RT SIDE AT BS 1273 STR 10 AND BS 1289 STR 5-SNRM 0358. RBL 18 AT BS 1160 AND BS 1219-SNRM 0455. RT AREA OF BS 1293 AND BS 1315-SNRM 0SDR 98FDEA00576Duct · blownNR 1 ENG FIRE WARN AND IND. SHUT ENGINE DOWN IAW CKLIST. DISCHARGED NR 1 FIRE BOTTLE. FOUND HIGH PRESSURE TURBINE COOL DUCT BLOWN. REMOVED AND REPLACED DUCT, NR 1 FIRE BOTTLE AND SQUIB. RAN ENGINE, LEAK CHECK GOOD.SDR 98FDEA00569Circuit Breaker · trippedDURING FUEL SYS STATUS CK WORKCARD 28B1301, L/TAIL TANK TRANSFER PUMP C/B TRIPPED. FIRE STARTED IN AFT ACCESSORY SECTION DURING FUEL TRANSFER TEST. C/W REPAIR IAW EA 1-2800-38210 AND WDM 28-22-05.SDR 97FDEA00763Bolt · shearedNR 1 PYLON INSIDE ACCESS PANEL 438HL STA YN 342, BULKHEAD TO UPPER SPAR WEB FWD END 1 ATTACH BOLT HAS SHEARED AND SEVERAL OTHER BOLTS ARE LOOSE. *S/D* HFEC INSPECTED AREA OF SHEARED AND LOOSE FASTNERS, NO CRACK INDICATIONS NOTED. INSTALLED NEW BOLT PER M/SDR 97FDEA00762Bolt · shearedNR 3 PYLON INSIDE ACCESS PANEL 488HL BS YN 342, BULKHEAD TO UPPER SPAR WEB FWD END 3 ATTACH BOLTS HAVE SHEARED AND THE OTHERS ARE LOOSE. * S/D* HFEC BOLT HOLES NO CRACK INDICATIONS NOTED. INSTALLED AND TORQUED NEW BOLTS PER M/M 20-50-02. RETORQUED REMAISDR 97FDEA00754Washer · brokenRT WING TRAILING EDGE FLAP, INBOARD HINGE SUPPORT FITTING TO FWD CLEVIS BRACKET, INBOARD UPPER ATTACH BOLT CONICAL WASHER IS BROKEN. * S/D* REMOVED FITTING, INSPECTED AND CLEANED BOLT HOLES, NO CORROSION NOTED. INSTALLED SERVICEABLE CLEVIS FITTING WITH NESDR 97FDEA00753Bolt · brokenLT WING TRAILING EDGE FLAP, INBOARD HINGE SUPPORT FITTING TO FWD CLEVIS BRACKET, INBOARD LOWER ATTACH BOLT IS SHEARED OFF AND INBOARD UPPER ATTACH BOLT CONICAL WASHER MISSING. OUTBOARD UPPER BOLT CONICAL WASHER IS BROKEN. *S/D* REPLACED BOLT WITH NEW SERVICSDR 97FDEA00479Duct · failureNRT: AFTER T/O SMOKE OF UNKNOWN ORIGIN APPEARED IN COCKPIT; DID AIR TURNBACK AND RETURNED TO NRT. SMOKE APPEARED TO BE COMING FROM AIR CONDITIONING. FOUND DIRTY OIL IN COALESER OF WATER SEPARATOR IN THE NR 1 PACK AND WET OIL IN NR 1 ENG STATER PNEU DUCT IN TSDR 96FDEA01297Casting · brokenSNRM 5020 THE L/H WING, O/B FLAP, I/B HINGE FITTING SUPPORT CASTING IS BROKEN OUT AT THE WING REAR SPAR, LOWER TANG, WING STA XORS 560 APPROX. ******S/D ******* REPLACED L/FLAP TENSION STRAP SUPPORT WITH NEW ONE, PER MDC SB 57-0-10 CONDITION II DSDR 96FDEA01351Strap · crackedRIGHT WING OUTBOARD FLAP, INBOARD HINGE TENSION STRAP SUPPORT CRACKED AT LOWER ATTACH BOLT HOLE, LOWER SURFACE (EXTERNAL) STA X ODRSX562390. REPLACED RIGHT FLAP TENSION STRAP SUPPORT WITH NEW PART PER MDC SB 57-0-10 CONDITION II AND C/W EA 1-5710-29039.SDR 96FDEA00731Retract Mech · malfunctionedAFTER TAKEOFF, THE LANDING GEAR HANDLE WOULD NOT MOVE TO THE UP POSITION. ACCOMPLISHED CHECKLIST AND LANDED. WE HAD NOSE WHEEL STEERING AVAILIABLE IN FLT AND THE AUTOPILOT AND THE FCP WORKED NORMALLY. RESET AND SAFTIED MLG TRIM CYLINDER INTERLOCK CYL FUSE PSDR 95FDEA01838Actuator · malfunctionedUPON FLAP/SLAT RETRACTION FOLLOWING T/O, AILERON DEFLECT DISAGREE LEVEL 2 LIGHT ILLUMINATED. PERFORMED ABNORMAL CHECKLIST IN RED BOOK PAGE 2-5-13 AND IAW CHECKLIST DUMPED FUEL AND RETURNED FOR LANDING. FOUND RT O/B AILERON FULLY DEFLECTED AND LT O/B AILERON SDR 95FDEA00205Door Frame · crackedTHE LEFT HAND CENTERLINE LANDING GEAR DOOR FRAME IS CRACKED ALONG THE FWD, INBOARD CORNER, CRACK IS APPOX 3.5 INCHES LONG C-CK N/R 7004. REMOVED LT FWD CENTERLINE DOOR AND INSTALLED NEW FRAME. P/N ANB 7387-1 PER SRM 53-00-01.
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