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 FDEA201205021707Skin · misrepairedSKIN AT FWD OF DOOR FOUND MISREPAIRED. CARRIED OUT REPAIR IAW SRM 53-00-15, FIG 202, REPAIR 8 REV 49. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 114.SDR FDEA201205021705Hinge Bracket · corrodedDURING FLOURESCENT PARTICLE INSPECTION, FOUND CORROSION ON LT WING INBD FLAP OTBD AFT HINGE BRACKET PIVOT INBD LUG HOLE. REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-52-03, REV 72. REPAIR ACCOMPLISHED IAW EA 1-5750-157194. REPAIR CLASSIFIED AS MAJOR IAW GMM 6SDR FDEA201205021704Hinge Bracket · corrodedDURING FLOURESCENT PARTICLE INSPECTION, FOUND CORROSION ON LT WING INBD FLAP OTBD AFT HINGE BRACKET PIVOT OTBD LUG HOLE. REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-52-03, REV 72. REPAIR ACCOMPLISHED IAW EA 1-5750-157194 PART 1. REPAIR CLASSIFIED AS MAJOR IASDR FDEA201205021703Bushing · wornLEFT WING INBD FLAP, OTBD AFT HINGE BRACKET PIVOT INBD LUG BUSHING FOUND WORN. BUSHING REMOVED CMM 20-20-07, REV 72, EXISTING HOLE DIAMETER 1.328" , MAX ALLOWABLE DIAMETER 1.220" FOUND EXCEED LIMIT IAW CMM 51-52-03, REV 72. BUSHING FABRICATED AND INSTALLED RSDR FDEA201205021702Bushing · wornLEFT WING INBD FLAP, OTBD AFT HINGE BRACKET PIVOT OTBD LUG BUSHING FOUND WORN. BUSHING REMOVED IAW CMM 20-20-07 REV 72. HOLE MEASURED AND FOUND EXCEED LIMIT IAW CMM 57-52-03, REV 72. BUSHING FABRICATED AND INSTALLED REF EA 1-5750-157194. REPAIR CLASSIFIEDSDR FDEA201205021701Hinge Bracket · corrodedLEFT WING OTBD FLAP, INBD AFT HINGE BRACKET PIVOT INBD LUG BORE, FOUND CORRODED. REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-52-04, REV 72. EXISTING BORE DIAMETER: 1.147", FINAL BORE DIAMETER: 1.1605", MAXIMUM ALLOWABLE DIAMETER: 1.150". REPAIR ACCOMPLISHEDSDR FDEA201205021700Hinge Bracket · corrodedLT WING OTBD FLAP, OTBD FORWARD HINGE BRACKET ACTUATOR ATTACH INBD LUG BORE SPOT FACE FOUND CORRODED. REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-44-09 REV 72. EXISITING THICKNESS 0.321", REMAINING THICKNESS 0.318", MATERIAL REMOVED 0.003", MINIMUM ALLOWABLSDR FDEA201204301673Skin · misrepairedAGING AIRCRAFT INSPECTION - CENTER CARGO DOOR FWD LOWER CORNER EDGE FOUND MISREPAIRED. CARRIED OUT REPAIR IAW SRM 52-30-16, FIG 201 REPAIR 3, REV 49. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 114.SDR FDEA201204301678Seat Track · corrodedMAIN DECK CARGO, ON REMOVAL OF FLOOR PANEL 283BF, SEAT TRACK AT STA 1569 X= -8.5 RT FOUND CORRODED ALONG FLANGE AREA. REPAIRED IAW SRM 53-00-52, FIG 201, REPAIR 5, REV 49. SEAT TRACK REWORKED IAW DWG AFA7795, REV F. REPAIR CLASSIFIED AS MAJOR IAW GMM 6- 2-SDR FDEA201204301677Seat Track · corrodedMAIN DECK CARGO, ON REMOVAL OF FLOOR PANEL 282GF SEAT TRACK BS 1581 X= -76 RT FOUND CORRODED ALONG FLANGE AREA. REPAIRED IAW SRM 53-00-52, FIG 201, REPAIR 5, REV 49. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.SDR FDEA201204301676Seat Track · corrodedMAIN DECK CARGO, ON REMOVAL OF FLOOR PANEL 282FF SEAT TRACK BS 1801 X= -49 RT FOUND CORRODED ALONG FLANGE AREA. REPAIRED IAW SRM 53-00-52, FIG 201, REPAIR 5, REV 49. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 114.SDR FDEA201204301675Seat Track · corrodedMAIN DECK CARGO, ON REMOVAL OF FLOOR PANEL 282JF SEAT TRACK BETWEEN BS 1781 AND 1801 X= -70 RT FOUND CORRODED ALONG FLANGE AREA. REPAIRED IAW SRM 53-00-52, FIG 201, REV 49. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.SDR FDEA201204301674Rib · crackedUPON REMOVAL OF LT NR 3 L/E SLAT FOUND INBD RIB CRACKED. RIB REMOVED IAW SRM 51-31-01, REV 49 AND REPLACED WITH FABRICATED RIB IAW SRM 51-31-01, REV 49. RIB FABRICATED IAW DWG ARB1680, REV H. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.SDR FDEA201204271644Longeron · crackedMAIN DECK CARGO, ON REMOVAL OF CRACK SPLICE 6L AT STA 5-123 FOUND LONGERON CRACKED. REPAIRED IAW SRM 53-00-05 REPAIR 1, FIG 202, REV 49 AND SRM 51-31-01, REV 49. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.SDR FDEA201204271643Longeron Splice · crackedCENTER CARGO COMPARTMENT APPROX BETWEEN STA 5-93 AND STA 5-113, LONGERON 45 RT SPLICE CRACK. R & R IAW SRM 51-31-01, REV 49. SPLICE FABRICATED IAW DWG A5A7116, REV D. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.SDR FDEA201204271642Longeron Splice · crackedCENTER CARGO COMPARTMENT APPROX BETWEEN STA 5-93 AND STA 5-113, LONGERON 44 RT SPLICE CRACK. R & R IAW SRM 51-33-01, REV 49. SPLICE FABRICATED IAW DWG A5A7114, REV E. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.SDR FDEA201204271641Longeron Splice · crackedCENTER CARGO COMPARTMENT APPROX BETWEEN STA 5-93 AND STA 5-113, LONGERON 37LT SPLICE CRACK. R & R IAW SRM 51-33-01, REV 49. SPLICE FABRICATED IAW DWG A5A7114, REV E. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.SDR FDEA201204271640Longeron Splice · crackedCENTER CARGO COMPARTMENT APPROX BETWEEN STA 5-93 AND STA 5-113 LONGERON, 47LT SPLICE CRACK. R & R IAW SRM 51-33-01, REV 49. SPLICE FABRICATED IAW DWG A5A7114, REV E. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.SDR FDEA201204271639Bushing · wornRIGHT WING INBD FLAP, OTBD AFT HINGE BRACKET PIVOT INBD LUG BUSHING, FOUND WORN. BUSHING REMOVED IAW CMM 20-20-07, REV 72 . HOLE MEASURED AND FOUND EXCEEDED LIMIT IAW CMM 57-52-03, REV 72 EXISTING HOLE DIA 1.253" MAX ALLOWABLE DIA 1.220" . REPAIR ACCOMPLISSDR FDEA201204271638Bushing · wornRIGHT WING INBD FLAP OTBD AFT HINGE BRACKET PIVOT OTBD LUG BUSHING, FOUND WORN. BUSHING REMOVED IAW CMM 20-20-07, REV 72. HOLE MEASURED AND FOUND EXCEED LIMIT IAW CMM 57-52-03, REV 72 EXISTING HOLE DIA 1.221" MAX ALLOWABLE DIA. 1.220". REPAIR ACCOMPLISHED ISDR FDEA201204271637Bushing · wornRIGHT WING OTBD FLAP, OTBD FORWARD HINGE BRACKET ACTUATOR ATTACH INBD LUG BUSHING FOUND WORN. BUSHING REMOVED IAW CMM 20-20-07, REV 72. BORE MEASURED DIAMETER 1.221" AND MAXIMUM ALLOWABLE DIAMETER 1.220" FOUND EXCEED LIMIT IAW CMM 57-44-09, REV 72. REPAISDR FDEA201204271636Bushing · wornRIGHT WING OTBD FLAP, OTBD FORWARD HINGE BRACKET ACTUATOR ATTACH OTBD LUG BUSHING FOUND WORN. BUSHING REMOVED IAW CMM 20-20-07, REV 72. BORE MEASURED DIAMETER 1.222" AND MAXIMUM ALLOWABLE DIAMETER 1.220" FOUND EXCEED LIMIT IAW CMM 57-44-09, REV 72. REPAIR ASDR FDEA201204271635Bushing · wornRIGHT WING OTBD FLAP, INBD FORWARD HINGE BRACKET ACTUATOR ATTACH, OTBD LUG BUSHING FOUND WORN. BUSHING REMOVED IAW CMM 20-20-07, REV 72. BORE MEASURED DIAMETER 1.225" AND MAXIMUM ALLOWABLE DIAMETER 1.220" FOUND EXCEED LIMIT IAW CMM 57-44-08, REV 72. REPAIR ASDR FDEA201204271634Bushing · wornRIGHT WING OTBD FLAP, INBD FORWARD HINGE BRACKET ACTUATOR ATTACH INBD LUG BUSHING FOUND WORN. HINGE BRACKET ACTUATOR ATTACH REMOVED IAW CMM 20-20-07, REV 72. BORE MEASURED DIAMETER 1.223" AND MAXIMUM ALLOWABLE DIAMETER 1.220" FOUND EXCEED LIMIT IAW CMM 57-4SDR FDEA201204271633Bushing · wornLEFT WING OTBD FLAP, INBD FORWARD HINGE BRACKET ACTUATOR ATTACH OTBD LUG BUSHING FOUND WORN. BUSHING REMOVED IAW CMM 20-20-07, REV 72. HOLE MEASURED FOUND EXCEED LIMIT IAW CMM 57-44-08, REV 72 EXISTING HOLE DIAMETER 1.221" AND MAXIMUM ALLOWABLE DIAMETER 1.220SDR FDEA201204271632Bushing · wornLEFT WING OTBD FLAP, INBD FWD HINGE BRACKET ACTUATOR ATTACH INBD LUG BUSHING FOUND WORN. BUSHING REMOVED IAW CMM 20-20-07, REV 72. HOLE MEASURED FOUND EXCEED LIMIT IAW CMM 57-44-08, REV 72. EXISTING HOLE DIAMETER 1.222" AND MAXIMUM ALLOWABLE DIAMETER 1.220".SDR FDEA201204271631Hinge Bracket · corrodedLEFT WING OTBD FLAP, OTBD FORWARD HINGE BRACKET, ACTUATOR ATTACH OTBD LUG BORE FOUND CORRODED. REWORKED AND FOUND EXCEED LIMIT IAW CMM 57- 44-09 REV 72. EXISTING DIAMETER 1.223", FINAL DIAMETER 1.228", MAXIMUM ALLOWABLE DIAMETER 1.220". REPAIR CARRIED OUSDR FDEA201204271630Hinge Bracket · corrodedLEFT WING OTBD FLAP, OTBD FORWARD HINGE BRACKET ACTUATOR ATTACH, INBD LUG BORE FOUND CORRODED. REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-44-09 REV 72. EXISTING DIAMETER 1.248", FINAL DIAMETER 1.257", MAXIMUM ALLOWABLE DIAMETER 1.220". REPAIR CARRIED OUT SDR FDEA201204271629Hinge Bracket · corrodedLEFT WING OTBD FLAP OTBD FORWARD HINGE BRACKET SIDE ATTACH SURFACE, FOUND CORRODED. REWORKED IAW CMM 20-11-02, REV 72. EXISTING THICKNESS UPPER: 0.468", LOWER: 0.479". MATERIAL REMOVED UPPER: 0.003", LOWER 0.003". REPAIR CARRIED OUT IAW EA 1-5750-157176SDR FDEA201204271628Hinge Bracket · corrodedRT WING OTBD FLAP, OTBD FORWARD HINGE BRACKET SIDE ATTACH SURFACE, FOUND CORRODED. REWORKED IAW CMM 20-11-02, REV 72 UPPER: EXISTING THICKNESS 0.451", MATERIAL REMOVED 0.005", REMAINING THICKNESS 0.446". LOWER: EXISTING THICKNESS 0.453", MATERIAL REMOVED SDR FDEA201204261603Skin · misrepairedSKIN FOUND MISREPAIRED. CARRIED OUT IAW SRM 53-00-15, FIG 202, REPAIR 8, REV 49. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 114.SDR FDEA201204261602Skin · misrepairedSKIN MISREPAIRED. CARRIED OUT REPAIR IAW SRM 53-00-15, FIG 202, REPAIR 8 REV 49. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 114.SDR FDEA201204261596Frame · misrepairedFRAME AT STA 535, LONGERON 24 RT MISREPAIRED. CARRIED OUT REPAIR IAW SRM 53-20-07, FIG 201. REPAIR 1, REV 49 EO 1-5100-7-5001B PART 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 114.SDR FDEA201204261595Frame · misrepairedFRAME AT STA 535, LONGERON 24 LEFT MISREPAIRED. CARRIED OUT REPAIR IAW EA 1-5310-157190 . REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 114.SDR FDEA201204261614Longeron Splice · crackedDURING X-RAY INSPECTION, FOUND CRACK AT STATION 5-123 LONGERON SPLICE 4R AT CENTER ROW NR 4 TOWARD NR 5 FASTENER COUNT FROM AFT. R & R IAW SRM 51-31-01, REV 49. SPLICE FABRICATED IAW DWG A5A7111, REV C. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114SDR FDEA201204261613Longeron Splice · crackedDURING X-RAY INSPECTION, FOUND CRACK AT STATION 5-123 LONGERON SPLICE 6L AT CENTER ROW OF CENTER SECTION FASTENER. R & R IAW SRM 51-31-01, REV 49. SPLICE FABRICATED IAW DWG A5A7112, REV D. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.SDR FDEA201204261612Stringer Splice · crackedDURING X-RAY INSPECTION, FOUND CRACK APPROX 0.9 INCH LONG AT STA 5-123, LONGERON 6R, STRINGER SPLICE AT CENTER ROW NR 4 TOWARD NR 5 FASTENER COUNT FROM AFT. REMOVED AND REPLACED IAW SRM 51-31-01, REV 49. SPLICE FABICATED IAW DWG A5A7112, REV D. REPAIR CLASSDR FDEA201204261611Skin · crackedRIGHT WING L/E NR 10 SLAT TRACK CUT-OUT LOWER OTBD CORNER WITH CRACK AT STA XOS 661. TRIMMED AND REPAIR CARRIED OUT IAW SRM 57-40-02, FIGURE 201, REPAIR 7, REV 49. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 114.SDR FDEA201204261610Angle · corrodedLEFT WING T/E ACCESS PANEL 541JB FORWARD SUPPORT TEE ANGLE FOUND WITH CORROSION. R & R IAW SRM 51-31-01, REV 49 AND SRM 51-33-01, REV 49. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 114.SDR FDEA201204261609Skin · crackedLT WING L/E NR 11 SLAT TRACK CUT-OUT LOWER OTBD CORNER CRACK AT STATION XOS 721. TRIMMED AND CARRIED OUT REPAIR IAW SRM 57-40-02, FIG 201, REV 49. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100 REV 114.SDR FDEA201204261601Seat Track · crackedFWD CARGO COMPARTMENT CEILING AREA APPROX BS 635, X= 47.5. FOUND SEAT TRACK CRACKED. R & R IAW SRM 51-31-01, REV 49. SEAT TRACK REWORKED IAW DWG ACA7399, REV E. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 114.SDR FDEA201204261600Seat Track · crackedFWD CARGO COMPARTMENT CEILING AREA APPROX BS 635, X= 27.5 FOUND SEAT TRACK CRACKED. R & R IAW SRM 53-00-52, FIG 201, REV 49. SEAT TRACK REWORKED IAW DWG REV E. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.SDR FDEA201204261599Seat Track · crackedFWD CARGO COMPARTMENT CEILING AREA APPROX BS 635, X= -8.5 FOUND SEAT TRACK CRACKED. R & R IAW SRM 51-31-01, REV 49. SEAT TRACK REWORKED IAW DWG ACA7104, REV T. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 114.SDR FDEA201204261598Seat Track · crackedFWD CARGO COMPARTMENT CEILING AREA APPROX BS 755, X= -30 FOUND SEAT TRACK CRACKED. R & R IAW SRM 51-31-01, REV 49, SEAT TRACK REWORKED IAW DWG ACA7102 REV R. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.SDR FDEA201204261597Seat Track · crackedFORWARD CARGO COMPARTMENT CEILING AREA APPROX STA 939, X= 47.5 FOUND SEAT TRACK CRACKED. REPAIRED IAW SRM 53-00-52, FIG 201 REVISION 49. SEAT TRACK REWORKED IAW DWG ACA7399, REV T. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.SDR FDEA201204251574Longeron Splice · crackedDURING X-RAY INSPECTION, FOUND A CRACK APPROXIMATELY 0.9" LONG AT STA 5-0. LONGERON 4R, LONGERON SPLICE AT CENTER ROW NR 7 TOWARD NR 8 FASTENER COUNT FROM AFT. R & R IAW SRM 51-33-01, REV 49. SPLICE FABRICATED IAW DWG EA 7634, REV B. REPAIR CLASSIFIED AS SDR FDEA201204241554Beam · crackedLOWER FUSELAGE CENTER CARGO DOOR JAMB UPPER BEAM APPROX STA 1721, DOOR ACTUATOR LOCATION FOUND 0.75" CRACKED. CARRIED OUT REPAIR IAW EA 1-5310-157182, PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.SDR FDEA201204241553Keelbeam · damagedCENTER LANDING GEAR WW, RT SIDE KEEL BEAM WEB STATION Y= 1436, X= 31.50 25" ABOVE DOOR HINGE LINE FOUND OIL CANNING EXCEED LIMIT (MAXIMUM ALLOWABLE IS 0.190", MEASURED 0.35".0). CARRIED OUT REPAIR IAW EA 1-5310-157187. REPAIR CLASSIFIED AS MAJOR IAW GMM SDR FDEA201204241552Seat Track · corrodedMAIN DECK CARGO SEAT TRACK AT BS 492, X= -27.5 RT FOUND CORRODED. R & R WITH NEW REWORKED SEAT TRACK IAW SRM 51-31-01, REV 49. NEW SEAT TRACK REWORK CARRIED OUT IAW DWG ACA7102, REV R. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.SDR FDEA201204241550Seat Track · corrodedMAIN DECK CARGO SEAT TRACK AT BS 1851, X= 8.5 LT, FOUND CORRODED. REPAIRED IAW SRM 53-00-52, FIG 201, REV 49. SEAT TRACK REWORKED IAW DWG AFA7795, REV F. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.
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