N595FE
Service difficulty reports · 389
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 = 'N595FE' 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 = 'N595FE' 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 FDEA201804171021Seat Track · gougedMAIN DECK SEAT TRACK AT BS 1281, RBL 8.5, CROWN GOUGED. THE SEAT TRACK WAS REPLACED IAW SRM 53-00-52-2R, FIGURE 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201804171020Seat Track · gougedMAIN DECK SEAT TRACK AT BS 1281, LBL 8.5, FOUND CROWN GOUGED. THE SEAT TRACK WAS REPLACEMED IAW SRM 53-00-52-2R, FIGURE 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201804171018Seat Track · gougedMAIN DECK FLOOR SEAT TRACK AT BS 1541, X=47.5, FOUND CROWN DAMAGED. THE SEAT TRACK WAS REPLACED IAW SRM 53-00-52-2R, FIGURE 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201804171015Seat Track · gougedMAIN DECK SEAT TRACK AT BS 5-10, RBL 8.5 FOUND CROWN DAMAGED. OUT OF LIMITS IAW SRM 53-00-52-1A FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPLACED IAW SRM 53-00-52-2R, FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201804171025Seat Track · chafedRT OBSERVER`S SEAT TRACK FOUND CHAFED.SDR FDEA201804171024Frame · crackedNR 1 AIR CONDITIONING COMPARTMENT BS 555 FRAME FOUND CRACKED.SDR FDEA201804171022Seat Track · gougedMAIN DECK SEAT TRACK AT BS 1281, RBL 47.5, CROWN GOUGED.SDR FDEA201804171019Seat Track · gougedMAIN DECK SEAT TRACK AT BS 1541, LBL 8.5, FOUND CROWN DAMAGED.SDR FDEA201804171017Seat Track · damagedMAIN DECK FLOOR SEAT TRACK AT BS 5-10, X-47.5 FOUND CROWN DAMAGED.SDR FDEA201804171016Seat Track · damagedMAIN DECK FLOOR SEAT TRACK AT BS 5-10, X=27.5 FOUND CROWN DAMAGED.SDR FDEA201804161008Seat Track · gougedMAIN DECK SEAT TRACK AT BS 6-50, RBL 27.5, FOUND CROWN DAMAGE. THE SEAT TRACK WAS REPLACED IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201803250781Tire · failedDURING CLIMBOUT, PASSING APPROXIMATELY 15,000 FT, RECEIVED A LVL 1 TIRE PRESSURE LOW ALERT. CALLED UP CONFIG SYNOPTIC AND OBSERVED LEFT CENTER TIRE PRESSURE FALLING RAPIDLY FROM APPROX 100 - 120 TO 0. LVL 2 TIRE FAIL ALERT WITH PRESSURE PASSING APPROXIMATELSDR FDEA201803210749Lamp · inoperativeDURING A POST FLIGHT INSPECTION. FOUND THE L1 DOOR SLIDE PRESSURE, PRESS TO TEST LIGHT INOPERATIVE. REPLACED THE LAMP AND OPS CHECKED GOOD IAW AMM 25-61-03-5SDR FDEA201712183411Handle · obstructedON PREFLT NOTICED THAT THE NR 2 ENGINE FIRE HANDLE WAS OUT THE NORMAL POSITION, SLIGHTLY DOWN. ATTEMPTED TO RETURN TO NORMAL WITHOUT LUCK, 19 MINUTES AFTER TAKEOFF APPROACHED A LEVEL ONE GENERATOR 2 OFF ALERT ACCOMPANIED WITH THE NR 2 FUEL LEVER ENGINE FIRE SDR FDEA201712183407Pushrod · out of positionDURING PREFLIGHT NOTICED #2 FIRE HANDLE SLIGHTLY OUT OF NORM POSITION. PUSHED HANDLE INTO NORM, NO ABNORMAL INDICATIONS. AFTER TAKEOFF GOT LEVEL 1 GEN 2 OFF ALERT ACCOMPANIED WITH FIRE IND IN #2 FIRE HANDLE, NO OTHER INDICATIONS OR WARNINGS. NOTICED FIRE HANDLSDR FDEA201712063339Warning Message · false activationON SHORT FINAL TO VOBL RWY 9 WITH A/P DISCONNECTED HAD MULTIPLE LEVEL 2 WARNING FLASH 2 TO 3 TIME. USE MANUAL SPOILERS AUTOBRAKES INOP WERE 2 THAT STOOD OUT. ATC REPORTED A 100 DIFFERENCT IN ALT REPORTED AND WHAT WAS INDICATED IN COCKPIT. NIL CURRENT FAUSDR FDEA201612144454Light · inoperativeREMOTE BOTTLE LIGHT INOPERATIVE ON THE R1 DOOR.SDR FDEA201612144453Light · inoperativeREMOTE BOTTLE LIGHT INOPERATIVE ON THE R1 DOOR.SDR FDEA201609093159Actuator · failedAFT LOWER CARGO DOOR WILL NOT CLOSE. INSTALLED ACTUATOR, AFT-LOWER-CARGO DOOR. OPS CHECK GOOD.SDR FDEA201608242968Controller · malfunctionedRECEIVED A LAT FUEL IMBAL WARING AFTER 35 MIN OF FLIGHT. FUEL SYSTEM IN MANUAL AND PROPERLY CONFIGURED. RIGHT 17.8, CENTER 14.8, LEFT 20.2. QRH COMPLIED WITH TO CORRECT IMBALANCE. CREW VERBAL AFTER FUEL WAS BALANCED AND MESSAGE CLEARED. RECEIVED LAT FUEL SDR FDEA201605241727Hinge · corrodedRIGHT WING, OTBD FLAP, INBD FWD HINGE, WING SIDE, BARREL NUTS HOLE SURFACE CORROSION. CORROSION AT RT WING, OTBD FLAP, INBD FWD HINGE, WING SIDE, BARREL NUT HOLE SURFACE REWORKED IAW CMM 57-44-08. EXISTING THICKNESS: UPPER 0.368", LOWER 0.365". MATERIAL REMOVSDR FDEA201605241726Hinge · corrodedLEFT WING, OTBD FLAP, INBD FWD HINGE, WING SIDE, BARREL NUTS, HOLE SURFACE CORROSION.
CORROSION AT LT WING, OTBD FLAP 11B, FWD HINGE, WING SIDE, BARREL NUT, HOLE SURFACE REWORKED IAW CMM 57-44-08. EXISTING THICKNESS: UPPER 0.371", LOWER: 0.3955", MATERIALSDR FDEA201605191665Doubler · chafedRIGHT WING FIXED LE SKIN, INSPECTION CARRIED OUT IAW WRI 57307476 & FOUND EXISTING REPAIR DOUBLER WITH CHAFED MARK AT STATION XOS 906. CHAFED DAMAGE HAS BEEN REMOVED & NEW REPAIR DOUBLER REPAIR ACCOMPLISHED IAW EA 1-5710-79779C P 2. REPAIR CLASSIFIED AS MAJOSDR FDEA201605181659Skin · crackedRIGHT WING LE SLAT EXTERIOR SKIN TE FOUND CRACK AT STATION XOS 816. TRIMMED OUT & DOUBLER REPAIR CARRIED OUT IAW EA 1-5750-T0325443 PART 1 P1. REPAIR CLASSIFIED AS MAJOR REPAIR IAW GMM 6-2-100. REFER TO WRI 57507879 FOR WORK DETAILS. REPAIR IS A CATEGORY BSDR FDEA201605181658Doubler · corrodedLEFT WING FIXED LE LOWER SKIN ATTACHMENT, DOUBLER FOUND CRACK AT STATION XOS 993. ACCOMPLISHED REPAIR IAW SRM 57-40-03-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201605171640Fitting · corrodedLEFT WING, OTBD FLAP VANE HORN FITTING B FWD HOLE CORROSION. CORROSION REWORKED AND FOUND EXCEEDED LIMIT IAW SRM 57-50-02-2R, FIG 201, EXISTING SIZE: LENGTH 0.915", WIDTH: 0.621". FINAL SIZE: LENGTH 1.0395", WIDTH: 0.7395", MAXIMUM ALLOWABLE SIZE: LENGTH 0.9SDR FDEA201605171639Fitting · corrodedLEFT WING, OTBD FLAP VANE HORN FITTING C FWD HOLE CORROSION. CORROSION REWORKED AND FOUND EXCEEDED LIMIT IAW SRM 57-50-02-2R, FIG 201, EXISTING SIZE: LENGTH 0.918", WIDTH: 0.653". FINAL SIZE: LENGTH 1.019", WIDTH: 0.718", MAXIMUM ALLOWABLE SIZE: LENGTH 0.940SDR FDEA201605171638Fitting · corrodedLEFT WING, OTBD FLAP VANE HORN FITTING D FWD HOLE CORROSION. CORROSION REWORKED AND FOUND EXCEEDED LIMIT IAW SRM 57-50-02-2R, FIG 201, EXISTING SIZE: LENGTH 0.858", WIDTH: 0.598", FINAL SIZE: LENGTH 0.9495", WIDTH: 0.649", MAXIMUM ALLOWABLE SIZE: LENGTH 0.940SDR FDEA201605171637Hinge · corrodedRIGHT WING, INBD FLAP OTBD AFT HINGE, FLAP SIDE, PIVOT HOLE OTBD BORE CORROSION. CORROSION REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-52-03. EXISTING DIA: 1.282", FINAL DIA: 1.315", MAXIMUM ALLOWABLE DIA: 1.220". REPAIR BUSHING FABRICATED AND INSTALLED IAW SDR FDEA201605171636Hinge · corrodedRIGHT WING, INBD FLAP OTBD AFT HINGE, FLAP SIDE, PIVOT HOLE INBD BORE CORROSION. CORROSION REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-52-03. EXISTING DIA: 1.283", FINAL DIA: 1.315". MAXIMUM ALLOWABLE DIA: 1.220". REPAIR BUSHING FABRICATED AND INSTALLED ISDR FDEA201605171635Hinge · corrodedRIGHT WING, OTBD FLAP INBD FWD HINGE, WING SIDE, ACTUATOR OTBD HOLE BORE CORROSION. CORROSION REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-08. EXISTING DIA: 1.282", FINAL DIA: 1.288", MAXIMUM ALLOWABLE DIA: 1.220". REPAIR BUSHING FABRICATED AND INSTALLEDSDR FDEA201605171634Hinge · corrodedRIGHT WING, OTBD FLAP INBD FWD HINGE, WING SIDE, ACTUATOR INBD HOLE BORE CORROSION. CORROSION REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-08. EXISTING DIA: 1.250", FINAL DIA: 1.254", MAXIMUM ALLOWABLE DIA: 1.220". REPAIR BUSHING FABRICATED BY MACHINING ASDR FDEA201605171633Hinge · corrodedRIGHT WING, OTBD FLAP INBD FWD HINGE, WING SIDE, LOWER MOUNT OTBD HOLE BORE CORROSION. CORROSION REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-08. EXISTING DIA: 0.708", FINAL DIA: 0.722". MAXIMUM ALLOWABLE DIA: 0.709". SHOULDER BUSHING FABRICATED BY MACHISDR FDEA201605171632Hinge · corrodedRIGHT WING, OTBD FLAP INBD FWD HINGE, WING SIDE, LOWER MOUNT INBD HOLE BORE CORROSION. CORROSION REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-08. EXISTING DIA: 0.708", FINAL DIA: 0.722". MAXIMUM ALLOWABLE DIA : 0.709". SHOULDER BUSHING FABRICATED BY MACHSDR FDEA201605171631Hinge · corrodedRIGHT WING, OTBD FLAP INBD FWD HINGE, WING SIDE, UPPER MOUNT OTBD HOLE BORE CORROSION. CORROSION REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-08. EXISTING DIA: 0.943", FINAL DIA: 0.953". MAXIMUM ALLOWABLE DIA: 0.944". REPAIRED BUSHING, FABRICATED BY MACSDR FDEA201605171630Hinge · corrodedRIGHT WING, OTBD FLAP OTBD FWD HINGE, WING SIDE, ACTUATOR OTBD HOLE BORE CORROSION. CORROSION REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-09. EXISTING DIAMETER 1.251 INCH, FINAL DIAMETER 1.254 INCH & MAX ALLOWABLE DIAMETER 1.220 INCH;. REPAIRED BUSHING, FASDR FDEA201605171629Hinge · corrodedRIGHT WING, OTBD FLAP OTBD FWD HINGE, WING SIDE, BARREL NUT LOWER HOLE BORE CORROSION. CORROSION AT HOLE NR 7 REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-09. EXISTING DIAMETER 0.382 INCH, FINAL DIAMETER 0.410 INCH & MAXIMUM ALLOWABLE DIAMETER 0.391 INCH. RSDR FDEA201605171628Hinge · corrodedRIGHT WING, OTBD FLAP OTBD FWD HINGE, WING SIDE, BARREL NUT UPPER HOLE BORE CORROSION. CORROSION HOLE NR 7 REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-09. EXISTING DIAMETER 0.382 INCH, FINAL DIAMETER 0.410 INCH & MAX ALLOWABLE DIAMETER 0.391 INCH. REPAIREDSDR FDEA201605171627Hinge · corrodedRIGHT WING, OTBD FLAP OTBD FWD HINGE, WING SIDE, LOWER MOUNT OTBD HOLE BORE CORROSION. CORROSION AT HOLE 3 REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-09. EXISTING DIAMETER 0.598 INCHES, FINAL DIAMETER 0.604 INCHES, MAX ALLOWABLE DIAMETER 0.584 INCHES. REPSDR FDEA201605171626Hinge · corrodedRIGHT WING, OTBD FLAP OTBD FWD HINGE, WING SIDE, LOWER MOUNT INBD HOLE BORE CORROSION. CORROSION AT HOLE 3 REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-09. EXISTING DIAMETER 0.598 INCHES, FINAL DIAMETER 0.604 INCHES, MAX ALLOWABLE DIAMETER 0.584 INCHES. REPSDR FDEA201605171625Hinge · corrodedRIGHT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE, UPPER MOUNT INBD HOLE BORE CORROSION. CORROSION HOLE NR 2 REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-09. EXISTING DIAMETER 0.944 INCHES, FINAL DIAMETER 0.951 INCHES, MAX ALLOWABLE DIAMETER 0.944 INCHES. REPSDR FDEA201605171624Hinge · corrodedLEFT WING INBD FLAP, OTBD AFT HINGE, FLAP SIDE, PIVOT HOLE OTBD BORE CORROSION. CORROSION REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-52-03. EXISTING DIAMETER 1.222 INCH, FINAL DIAMETER 1.237 INCH & MAX ALLOWABLE DIAMETER 1.220 INCH. REPAIRED BUSHING, FABRICASDR FDEA201605171623Hinge · corrodedLEFT WING INBD FLAP, OTBD AFT HINGE, FLAP SIDE, PIVOT HOLE INBD BORE CORROSION. CORROSION AT HOLE INBD BORE REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-52-03. EXISTING DIAMETER 1.2235 INCH, FINAL DIAMETER 1.237 INCH & MAX ALLOWABLE DIAMETER 1.220 INCH. REPAIRSDR FDEA201605171622Hinge · corrodedLEFT WING OTBD FLAP, INBD FWD HINGE, WING SIDE, ACTUATOR OTBD HOLE BORE CORROSION. CORROSION AT HOLE NR 8 REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-08. EXISTING DIAMETER 1.218 INCH, FINAL DIAMETER 1.226 INCH & MAXIMUM ALLOWABLE DIAMETER 1.220 INCH. REPAISDR FDEA201605171621Hinge · corrodedLEFT WING OTBD FLAP, INBD FWD HINGE, WING SIDE, ACTUATOR INBD HOLE. BORE CORROSION. CORROSION AT HOLE NR 8 REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-08. EXISTING DIAMETER 1.252 INCH, FINAL DIAMETER 1.255 INCH & MAXIMUM ALLOWABLE DIAMETER 1.220 INCH. REPSDR FDEA201605171620Hinge · corrodedLEFT WING OTBD FLAP, INBD FWD HINGE, WING SIDE, LOWER MOUNT INBD HOLE SURFACE CORROSION. CORROSION REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-08. EXISTING THICKNESS 0.437 INCHES, MATERIAL REMOVED FWD SIDE 0.006 INCHES, AFT SIDE 0.016 INCHES, REMAINING THICSDR FDEA201605171619Hinge · corrodedLEFT WING OTBD FLAP, INBD FWD HINGE, WING SIDE, LOWER MOUNT OTBD HOLE BORE CORROSION. CORROSION AT HOLE NR 7 REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-48-08. EXISTING DIAMETER 0.708 INCHES, FINAL DIAMETER 0.731 INCHES, MAX ALLOWABLE DIAMETER 0.709 INCHES. RSDR FDEA201605171618Hinge · corrodedLEFT WING OTBD FLAP, INBD FWD HINGE, WING SIDE, LOWER MOUNT INBD HOLE BORE CORROSION. CORROSION REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-08. EXISTING DIAMETER 0.727 INCHES, FINAL DIAMETER 0.731 INCHES & MAX ALLOWABLE DIAMETER 0.709 INCHES. REPAIR BUSHINSDR FDEA201605171617Hinge · corrodedLEFT WING OTBD FLAP, INBD FWD HINGE, WING SIDE, UPPER MOUNT HOLE OTBD BORE CORROSION. REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-08. EXISTING DIAMETER 0.942 INCHES, FINAL DIAMETER 0.950 INCHES & MAX ALLOWABLE DIAMETER 0.944 INCHES. REPAIR BUSHING FABRICATSDR FDEA201605171616Hinge · corrodedLEFT WING OTBD FLAP, INBD FWD HINGE, WING SIDE, BARREL NUT LOWER HOLE BORE CORROSION. CORROSION REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-08, EXISTING DIAMETER 0.627 INCHES, FINAL DIAMETER 0.629 INCHES & MAX ALLOWABLE DIAMETER 0.621 INCHES. REPAIR BUSHING
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