N606FE
Service difficulty reports · 403
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 = 'N606FE' 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 = 'N606FE' 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 07FDEA01734Web · corrodedFOUND UPPER CARGO DOOR CUTOUT, LOWER SILL'S WEB CORRODED AT STA 660. [SUP 05-22-07] REPAIR CARRIED OUT AT UPPER CARGO DOOR CUTOUT, LOWER SILL'S WEB, STA 660 AS PER FEDEX EA 1-5310-111100.SDR 07FDEA01717Seat Track · corrodedFOUND UPPER CARGO COMPARTMENT, SEAT TRACK AT LBL 8.5 CORRODED AT STA 1299. [SUP 05-21-07] REPAIR CARRIED OUT AS PER SRM 53-70-00 FIG. 1 VOL.I. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100.SDR 07FDEA01710Spar Cap · corrodedRIGHT WING, TRAILING EDGE REAR SPAR UPPER CAP FOUND CORROSION AT XORS 1042. [SUP 05-22-07] REPAIRED AS PER FEDEX EA 1-5710-111099.SDR 07FDEA01692Skin · crackedRIGHT WING, LEADING EDGE LOWER SURFACE 619CB PANEL FWD I/B SIDE CORNER FOUND 5/8 INCH CRACK AT XOS 607. [SUP 05-22-07] REPAIR CARRIED OUT AT RIGHT WING - LEADING EDGE LOWER SURFACE 619CB PANEL FWD I/B SIDE CORNER, XOS 607 AS PER SRM 57-10-00 FIGURE 21 VOSDR 07FDEA00522Duct · disconnectedINTMT LVL 3 APU FIRE ALERT AFTER 1 50, EN ROUTE-SUSPECTED BLEED/DUCT LEAK COMPLIED W/QRH, BOTTLE BLOWN INSTALLED SERVICEABLE FIREX CONTAINER AND CARTRIDGE IN THE NR 1 POSITION AND REINSTALLED FIREX CONTAINER IN THE NR 2 POSITION IN REF FOUND FLEX DUCT AT EXHAUSDR 07FDEA00518Duct · disconnectedINTERMITTENT LEVEL 3 APU FIRE ALERT AFTER 150 EN ROUTE-SUSPECTED BLEED/DUCT LEAK-COMPLIED W/QRH, BOTTLE BLOWN. FOUND FLEX DUCT AT EXHAUST DISCONNECTED AND CLAMP MISSING, DUCT COMES FROM THE GEN COOLING SHROUD. RAN APU FOUND AIR LEAKING AT PRESS REG VALVE CLASDR 05FDEA03951Flap · corrodedSNRM N0963: LH OUTBD FLAP AFT INBD HINGE BRACKET ATTACH FITTING INBD CENTER BORE FOUND CORRODED. CORRECTIVE ACTION: SNRM N0963: LEFT HAND WING OUTBOARD FLAP ASSEMBLY REMOVED AND REPLACED AS PER AMM 27-50-30-4. ADJUSTMENT AND OPERATION TEST CARRIED OUT SDR 05FDEA03950Support Fitting · corrodedCRACK FOUND AT LT WING OUTBD FLAP LOWER FASTENER HOLE COMMON TO ARC 4009 SUPPORT FITTING LOCATED AT THE MOST OUTBD HOLE DURING HFEC INSPECTION. LT WING OUTBOARD FLAP ASSEMBLY REMOVED AND REPLACED AS PER AMM 27-50-30-4. ADJUSTMENT AND OPERATION TEST CARRIESDR 05FDEA03949Hinge Bracket · corrodedLT WING OUTBD FLAP INBOARD HINGE BRACKET OUTBD CENTER ATTACH HOLE FOUND CORRODED. LT WING OUTBOARD FLAP ASSEMBLY REMOVED AND REPLACED AS PER AMM 27-50-30-4. ADJUSTMENT AND OPERATION TEST CARRIED OUT AS PER AMM 27-50-00-5, SATIS.SDR 05FDEA03948Skin · corrodedSNRM N1008: CRACK FOUND AT RH WING OUTBD FLAP LOWER FASTENER HOLE COMMON TO ARC 4009 SUPPORT FITTING LOCATED AT THE #2 HOLE FROM INBD DURING HFEC INSPECTION. CORRECTIVE ACTION: SNRM N1008: RIGH HAND OUTBOARD FLAP ASSEMBLY REMOVED AND REPLACED AS PER AMSDR 05FDEA03947Skin · corrodedSNRM N0596: RH WING OUTBD FLAP AFT INBD HINGE BRACKET FWD OUTBD AFT ATTACH HOLE FOUND WITH CORROSION. CORRECTIVE ACTION: SNRM N0596: RIGHT HAND OUTBOARD FLAP ASSEMBLY REMOVED AND REPLACED AS PER AMM 27-50-30-4. ADJUSTMENT AND OPERATION TEST CARRIED OSDR 05FDEA03829Hinge · wornRIGHT MAIN LANDING GEAR WHEEL WELL DOOR AFT HINGE FOUND WORN. REMOVED AND REPLACED AS PER SRM 51-31-01 VOL. II. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.SDR 05FDEA03828Hinge · wornLEFT MAIN LANDING GEAR WHEEL WELL DOOR AFT HINGE FOUND WORN. REMOVED AND REPLACED AS PER SRM 51-31-01 VOL. II. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.SDR 05FDEA03762Hinge Fitting · corrodedFOUND RIGHT WING OUTBOARD FLAP INBOARD HINGE FITTING OUTBOARD NR 3 BOLT HOLE FOUND CORROSION. CORROSION REMOVED & REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-90057.SDR 05FDEA03760Hinge Fitting · corrodedFOUND LEFT WING OUTBOARD FLAP INBOARD HINGE FITTING OUTBOARD NR 3 BOLT HOLE FOUND CORROSION. CORROSION REMOVED & REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-90056.SDR 05FDEA03759Hinge Fitting · corrodedFOUND LEFT WING OUTBOARD FLAP INBOARD HINGE FITTING MOST AFT BOLT HOLE FOUND CORROSION. CORROSION REMOVED & REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-90059.SDR 05FDEA03761Hinge Fitting · corrodedFOUND RIGHT WING OUTBOARD FLAP INBOARD HINGE FITTING MOST AFT BOLT HOLE FOUND CORROSION. CORROSION REMOVED & REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-90058.SDR 05FDEA03698Doubler · crackedRIGHT FIXED LEADING EDGE INTERIOR BEADED DOUBLER FOUND CRACKED AT XORS663. REPAIRED AS PER FEDEX EA 1-5730-90044SDR 05FDEA03647Seat Track · damagedFOUND MAIN DECK COMPARTMENT, SEAT TRACK FOUND EDGE DAMAGED AT STA 5/23, X= -47.5. REPAIR CARRIED OUT AS PER SRM 53-70-00 VOL. I FIG. 1 AND SRM 51-33-01 VOL. II. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.SDR 05FDEA03646Seat Track · corrodedFOUND MAIN DECK COMPARTMENT, SEAT TRACK FOUND CORROSION AT STA 1521, X=8.5. REPAIR CARRIED OUT IAW SRM 53-70-00 FIG. 3 VOL. I AND SRM 51-33-01 VOL. II. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.SDR 05FDEA03645Seat Track · corrodedFOUND MAIN DECK COMPARTMENT, SEAT TRACK FOUND CORROSION AT STA 5/0 - 5/73, X=8.5. REPAIR CARRIED OUT IAW SRM 53-70-00 VOL. I FIG. 1 AND SRM 51-33-01 VOL. II. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.SDR 05FDEA03632Stringer · crackedDURING HFEC INSPECTION, FOUND CRACK AT LEFT WING, END OF STRINGER 43. REPAIR CARRIED OUT IAW SRM 57-20- 00 FIG. 10 VOL I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.SDR 05FDEA03631Stringer · crackedDURING HFEC INSPECTION, FOUND CRACK AT LEFT WING, END OF STRINGER 44 APPROXIMATELY 1/2 INCH. REPAIR CARRIED OUT IAW SRM 57-20- 00 FIG. 10 VOL I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.SDR 05FDEA03630Stringer · crackedDURING HFEC INSPECTION, FOUND CRACK AT LEFT WING, END OF STRINGER 14 APPROXIMATELY 13 INCHES. REPAIRED AS PER SRM 57-20-00 FIG. 10 VOL. I. CLIP FABRICATION CARRIED OUT AS PER FEDEX E.A. 1-5720-90050 (TITLE: WINGS - STRINGER 14L REPAIR PER SRM VOL. I 57-2SDR 05FDEA03629Stringer · crackedDURING HFEC INSPECTION, FOUND CRACK AT LEFT WING, END OF STRINGER 12. REPAIR CARRIED OUT IAW SRM 57-20- 00 FIG. 10 VOL I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.SDR 05FDEA03628Stringer · crackedDURING HFEC INSPECTION, FOUND CRACK AT RIGHT WING, END OF STRINGER 44 APPROXIMATELY 2 INCHES.SDR 05FDEA03627Stringer · crackedDURING HFEC INSPECTION, FOUND CRACK INDICATION AT LEFT WING, END OF STRINGER 11.SDR 05FDEA03626Stringer · crackedDURING HFEC INSPECTION FOUND CRACK AT RIGHT WING, END OF STRINGER 14 APPROXIMATELY 14 INCHES. REPAIR CARRIED OUT IAW SRM 57-20 -00 FIG. 10 VOL I. CLIP FABRICATED AS PER FEDEX EA 1-5720-90053SDR 05FDEA03625Stringer · crackedDURING HFEC INSPECTION, FOUND CRACK INDICATION AT LEFT WING, END OF STRINGER 10.SDR 05FDEA03624Stringer · crackedDURING HFEC INSPECTION, FOUND CRACK INDICATION AT LEFT WING, END OF STRINGER 9.SDR 05FDEA03623Stringer · crackedDURING HFEC INSPECTION, FOUND CRACK AT RIGHT WING, END OF STRINGER 12 APPROXIMATELY 13.25 INCHES. REPAIR CARRIED OUT IAW SRM 57-20-00 FIG. 10 VOL I. CLIP FABRICATED AS PER FEDEX EA 1-5720-90052.SDR 05FDEA03622Stringer · crackedDURING HFEC INSPECTION, FOUND CRACK INDICATION AT RIGHT WING, END OF STRINGER 11. REPAIR CARRIED OUT IAW SRM 57-20 -00 FIG. 10 VOL I. CLIP FABRICATED AS PER FEDEX EA 1-5720-90051.SDR 05FDEA03621Stringer · crackedDURING HFEC INSPECTION, FOUND CRACK INDICATION AT RIGHT WING, END OF STRINGER 10. REPAIR CARRIED OUT IAW SRM 57-20 -00 FIG. 10 VOL I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.SDR 05FDEA03620Stringer · crackedDURING HFEC INSPECTION, FOUND CRACK INDICATION AT LEFT HAND WING, END OF STRINGER 41. REPAIR CARRIED OUT IAW SRM 57-20- 00 FIG. 10 VOL I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.SDR 05FDEA03619Stringer · crackedDURING HFEC INSPECTION, FOUND CRACK INDICATION AT RIGHT WING, END OF STRINGER 9.SDR 05FDEA03618Seat Track · corrodedMAIN DECK COMPARTMENT, SEAT TRACK FOUND CORROSION AT STATION 5/0- 5/73, X=8.5. REPAIR CARRIED OUT IAW SRM 53-70-00 VOL. I FIG. 1 AND SRM 51-33-01 VOL. II. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.SDR 05FDEA03616Seat Track · wornMAIN DECK COMPARTMENT, SEAT TRACK EDGE FOUND WORN AT STATION 755, X=-8.5. CARRIED OUT REPAIR IAW SRM 53-70-00 FIG. 1 VOL. I AND SRM 51-33-01 VOL.II. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.SDR 05FDEA02451Warning Light · illuminatedON FINAL APPROACH GOT FLAP DISAG ALERT WHILE EXTENDING FLAPS FROM 35 TO 50. RETURNED FLAPS TO 35 AND ALERT CLEARED MOMENTARILY THEN CAME BACK ON, MISSED APPROACH ACCOMPLISHED AND RAN QRH PROCEDURES. ABLE TO RETURN FLAPS TO 35/EXT WITH NO ALERTS. NORMAL APPSDR 04FDEA02056Seat Track · corrodedFORWARD CABIN SEAT TRACK AT STA 495 APRROXIMATELY 27.5 CORRODED. REMOVED PER SRM 53-70-00 FIGURE 1 VOLUME I. NEW SET TRACK TRIMMED, REWORKED AND REPAIR PARTS INSTALLED PER SRM 53-70-00 FIGURE 1 VOLUME 1 AND SRM 51-31-01 VOLUME II.SDR 04FDEA02055Hinge · corrodedRIGHT OUTBOARD FLAP, OUTBOARD HINGE (FLAP SIDE) AFT MOUNTING AREA FORWARD HOLE FOUND CORRODED. CORROSION REMOVED PER SRM 51-21-01 VOLUME II. ORIGINAL DIAMETER = 0.521, FINAL DIAMETER = 0.610. COMPLIED WITH FEDEX EA 1-5750-76755, WINGS - RIGHT OUTBOARD FLAP - SDR 04FDEA02033Splice · crackedCENTER CARGO BETWEEN BS 5-113 TO 1541, LONGERON SPLICE 48R CRACKED. LONGERON SPLICE 48R REMOVED PER SRM 51-33-01 VOLUME II. NEW LONGERON SPLICE FABRICATED AS PER DWG: A5A7124, INSTALLED PER SRM 51-33-01 VOLUME II AND PART MARKED FX A5A7124-1 PER GMM 7-0-1001.SDR 04FDEA02032Fitting · crackedLEFT WING, OUTBOARD FLAP ATTACHING RIB STOP FITTING FOUND CRACKED. REMOVED AND REPLACED AS PER SRM 51-31-01 VOLUME II.SDR 04FDEA02029Pressure Panel · canningFUSELAGE OIL CANNING FOUND ON CENTER LANDING GEAR WHEEL WELL RT VERTICAL WEBS FROM STA 1394.5 TO STA 1470. FUSELAGE, MAXIMUM DEPTH OF THE OIL CANNING ON CENTER LANDING GEAR WHEEL WELL RT VERTICAL WEBS FROM STA 1394.5 TO STA 1470 FOUND WITHIN LIMITS PER SRM SDR 04FDEA02028Pressure Panel · canningFUSELAGE OIL CANNING FOUND ON CENTER LANDING GEAR WHEEL WELL LEFT VERTICAL WEBS FROM STA 1394.5 TO STA 1470. FUSELAGE, MAXIMUM DEPTH OF THE OIL CANNING ON CENTER LANDING GEAR WHEEL WELL LEFT VERTICAL WEBS FROM STA 1394.5 TO STA 1470 FOUND WITHIN LIMITS PER SRSDR 04FDEA02027Fitting · corrodedRT WING, INBOARD FLAP VANE TEE-FITTING INBOARD MOST AFT ATTACHING HOLE CORRODED. RT WING, INBOARD FLAP VANE TEE-FITTING INBOARD MOST AFT ATTACHING HOLE CORROSION REMOVED AS PER CMM 20-11-02 PAGE 2 - 4. ORIGINAL DIAMETER = 0.8755 INCH, FINAL DIAMETER = 0.882 SDR 04FDEA02004Seat Track · wornMAIN CABIN, SEAT TRACK AT STA 775, APPROXIMATELY LBL 8.5 CROWN WORN. MAIN CABIN, SEAT TRACK AT STA 745 TO STA 785, LBL 8.5. REMOVED PER SRM 51-33-01 VOLUME I. NEW SEAT TRACK SPLICE FABRICATED AND INSTALLED PER SRM 53- 70-00 FIGURE 1 VOLUME I AND SRM 51-33-SDR 04FDEA02002Seat Track · wornMAIN DECK, SEAT TRACK CROWN AT STA 1059 - 1065, LBL 47.5 FOUND DAMAGED. MAIN DECK, SEAT TRACK FROM STA 1049 TO STA 1129 LBL 47.5 REMOVED PER SRM 53-70-00 FIGURE 1 VOLUME I AND SRM 51-31-01 VOLUME II. REPAIR PARTS AND FABRICATED SEAT TRACK INSTALLED AS PER SDR 04FDEA02003Seat Track · corrodedFWD CABIN, SEAT TRACK AT STA 465 - 495, APPROXIMATELY LBL 58 CORRODED. FWD CABIN, SEAT TRACK AT STA 465 TO STA 495, LBL 58 CUT AND REMOVED PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR PARTS FABRICATED AND INSTALLED PER SRM 53-70-00 FIGURE 1 VOLUME 1 AND SRM SDR 04FDEA02013Hinge Bracket · corrodedLT WING OUTBOARD FLAP INBOARD AFT HINGE, INBOARD PIVOT HOLE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGE 2-4. ORIGINAL DIAMETER:1.093; FINAL DIAMETER: 1.096 AND REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-76783, WINGS- LEFT AND RIGHT OUTBOARD FLSDR 04FDEA02012Hinge Bracket · corrodedLT WING OUTBOARD FLAP INBOARD AFT HINGE, OUTBOARD PIVOT HOLE SPOT SURFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGE 2-4. ORIGINAL THICKNESS: 0.504; MATERIAL REMOVED 0.002"; REMAINING THICKNESS: 0.502 AND REPAIR CARRIED OUT AS PER FEDEX EA 1-
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