N586FE
Service difficulty reports · 500
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 = 'N586FE' 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 = 'N586FE' 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 FDEA201709122492Hinge Bracket · corrodedRIGHT WING OTBD FLAP OUTBD HINGE (WING SIDE) BARREL NUT UPPER HOLE BORE FOUND CORRODED. THE BORE WAS REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-TO335331, PART 1, STEP 2C.SDR FDEA201709122491Hinge Bracket · corrodedRIGHT WING OTBD FLAP OUTBD HINGE (WING SIDE) LOWER MOUNT OTBD HOLE BORE FOUND CORRODED. THE BORE WAS REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09. A BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-TO335331, PART 1, STEP 2B, AND STEP 2.SDR FDEA201709122490Hinge Bracket · corrodedRIGHT WING OUTBD FLAP OUTBD HINGE (WING SIDE) LOWER MOUNT INBD HOLE BORE FOUND CORRODED. THE BORE WAS REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09. A BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-TO335331, PART 1, STEP 2B, AND STEP 2.SDR FDEA201709122489Hinge Bracket · corrodedRIGHT WING OTBD FLAP OUTBD HINGE (WING SIDE) UPPER MOUNT OTBD HOLE BORE FOUND CORRODED. THE BORE WAS REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-TO335331, PART 1, STEP 2A.SDR FDEA201709122488Hinge Bracket · corrodedLEFT WING OUTBD FLAP OUTBD HINGE (WING SIDE) ACTUATOR OUTBD LUG HOLE BORE FOUND CORRODED. THE HOLE BORE WAS REWORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-09. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0335322, PART 1, STEP 2D.SDR FDEA201709122487Hinge Bracket · corrodedLEFT WING OUTBD FLAP OUTBD HINGE (WING SIDE) BARREL NUT HOLE SPOT SURFACE FOUND CORRODED. SURFACE REWORKED IAW CMM 57-44-09. A REPAIR SHIM FABRICATED AND INSTALLED IAW CMM 57-44-09.SDR FDEA201709122486Hinge Bracket · corrodedLEFT WING OUTBD FLAP OUTBD HINGE (WING SIDE) ACTUATOR INBD LUG HOLE BORE FOUND CORRODED. THE BORE WAS REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0335322, PART 1, STEP 2D.SDR FDEA201709122485Hinge Bracket · corrodedLEFT WING OUTBD FLAP OUTBD HINGE (WING SIDE) BARREL NUT LOWER HOLE BORE FOUND CORRODED. THE BORE WAS REWORKED AND FOUND TO BE OUT OF LIMITS IAW CMM 57-44-09. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0335322, PART 1, STEP 2C.SDR FDEA201709122484Hinge Bracket · corrodedLEFT WING OUTBD FLAP OUTBD HINGE (WING SIDE) BARREL NUT UPPER HOLE BORE FOUND CORRODED. BORE REWORKED AND FOUND TO BE OUT OF LIMITS IAW CMM 57-44-09. A BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0335322, PART 1, STEP 2C.SDR FDEA201709122483Hinge Bracket · corrodedLEFT WING OUTBD FLAP OTBD HINGE (WING SIDE) LOWER MOUNT OTBD HOLE FWD AND AFT SURFACE FOUND CORRODED. MOUNT BORE, FWD AND AFT SURFACE REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09. A REPAIR SHIM WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0335322, PART 1SDR FDEA201709122482Hinge Bracket · corrodedLEFT WING OUTBD FLAP OUTBD HINGE (WING SIDE) LOWER MOUNT INBD HOLE FWD AND AFT SURFACE FOUND CORRODED. BORE FWD AND AFT SURFACE REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09. A REPAIR SHIM WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0335322, PART 1, STEPSDR FDEA201709122481Hinge Bracket · corrodedLEFT WING OUTBD FLAP OUTBD HINGE (WING SIDE) LOWER MOUNT OUTBD HOLE BORE FOUND CORRODED. THE BORE WAS REWORKED AND FOUND TO BE OUT OF LIMITS IAW CMM 57-44-09. A BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0335322, PART 1, STEP 2 AND 2A.SDR FDEA201709122480Hinge Bracket · corrodedLEFT WING OUTBD FLAP OUTBD HINGE ( WING SIDE ) LOWER MOUNT INBD HOLE BORE FOUND CORRODED., THE BORE WAS REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09. A BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0335322, PART 1, STEP 2 AND 2A.SDR FDEA201709122479Hinge Bracket · corrodedLEFT WING OUTBD FLAP OTBD HINGE ( WING SIDE ) UPPER MOUNT OTBD HOLE BORE FOUND CORRODED. BORE REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09. A BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0335322, PART 1, STEP 2B.SDR FDEA201709112477Support Fitting · corrodedRIGHT WING OUTBOARD FLAP VANE NR 1 SUPPORT FITTING ECCENTRIC HOLE BORE FOUND CORRODED. BORE REWORKED AND FOUND OUT OF LIMITS IAW SRM 57-50-02-2R, FIG 201. AN OVERSIZED WAS FABRICATED IAW EA 1-5750-T0335352, PART 1, STEP 3, TEST CARRIED OUT IAW AMM 27- 50-32SDR FDEA201709112476Support Fitting · corrodedLEFT WING OUTBOARD FLAP VANE NR 5 SUPPORT FITTING BORE FOUND CORRODED. BORE REWORKED AND FOUND OUT OF LIMITS IAW SRM 57-50-02-2R, FIG 201. AN OVERSIZED BUSHING WAS FABRICATED IAW EA1-5750-T0335345, PART 1, STEP 1A. INSTALLED IAW AMM 27-50-32-4. LT WING FLAPSDR FDEA201709022451Hinge Bracket · corrodedRIGHT WING INBOARD FLAP OUTBOARD HINGE (FLAP SIDE) PIVOT OUTBOARD LUG HOLE BORE FOUND CORRODED. BORE REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-52-03. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-135692F, PART 5, STEP 2 AND 3. REPAIR CSDR FDEA201709022450Hinge Bracket · corrodedRIGHT WING INBOARD FLAP OUTBOARD HINGE (FLAP SIDE) PIVOT INBOARD LUG HOLE BORE FOUND CORRODED. BORE REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-52-03. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-135692F, PART 5, STEP 2 AND 3. REPAIR CLASSDR FDEA201709022449Hinge Bracket · corrodedLEFT WING INBOARD FLAP OUTBOARD HINGE (FLAP SIDE) PIVOT OUTBOARD LUG HOLE BORE FOUND CORRODED. BORE REWORKED AND FOUND OUT OF LIMITS CMM 57-52-03. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-135691F, PART 5, STEP 2 & 3. REPAIR CLASSIFSDR FDEA201709022448Hinge Bracket · corrodedLEFT WING INBOARD FLAP OUTBOARD HINGE (FLAP) PIVOT INBOARD LUG HOLE BORE FOUND CORRODED. BORE REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-52-03. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-135691F, PART 5, STEP 2 & 3. REPAIR CLASSIFIEDSDR FDEA201709022447Hinge Bracket · corrodedRIGHT WING INBOARD FLAP OUTBOARD HINGE (WING SIDE) PIVOT HOLE BORE FOUND CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-07. A NEW REPAIR BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0330927 A, PART 1, STEP 1F. REPAIR CLASSIFIED AS MAJOR IASDR FDEA201709022446Hinge Bracket · corrodedLEFT WING INBOARD FLAP OUTBOARD HINGE (WING SIDE) PIVOT HOLE BORE FOUND CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-07. A REPAIR BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0330926 B, PART 1, STEP 1F. REPAIR CLASSIFIED AS MAJOR IAW GMSDR FDEA201708312438Beam · crackedMAIN DECK R3 DOOR LOWER BEAM FORWARD STOPPER AREA FOUND CRACKED. THE BEAM WAS REMOVED AND REPLACED IAW SRM 51-31-01-0G. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201708312437Seat Track · damagedMAIN DECK SEAT TRACK AT BS 755, LBL 27.5 FOUND TO HAVE CROWN DAMAGE. THE SEAT TRACK WAS REPLACED FROM BS 725 TO 765 IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201708312436Seat Track · damagedMAIN DECK SEAT TRACK AT BS 755, RBL 47.5 FOUND TO HAVE CROWN DAMAGE. THE SEAT TRACK WAS REPLACED FROM BS 725 TO 765 IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201708312435Cargo Track · crackedMAIN DECK CARGO TRACK AT BS 755, RBL 8.5 FOUND CRACKED. THE CARGO TRACK WAS REPLACED BETWEEN BS 725 TO 765 IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201708312434Cargo Track · crackedMAIN DECK CARGO TRACK AT BS 638, RBL 8.5 FOUND CRACKED. THE CARGO TRACK WAS REPLACED BETWEEN BS 625 TO 705 IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201708312433Cargo Track · crackedMAIN DECK CARGO TRACK AT BS 695, LBL 27.5 FOUND CRACKED. THE CARGO TRACK WAS REPLACED FROM BS 625 TO 745 IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100SDR FDEA201708312432Cargo Track · crackedMAIN DECK CARGO TRACK AT BS 755, LBL 8.5 FOUND CRACKED. THE CARGO TRACK WAS REPLACED FROM BS 485 TO 745, IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201708312431Seat Track · damagedSEAT TRACK AT BS 755, RBL 27.5 FOUND WITH CROWN DAMAGE. THE SEAT TRACK WAS REPLACED BETWEEN BS 745 TO 785 IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201708312430Seat Track · damagedSEAT TRACK AT BS 998, LBL 47.5 FOUND WITH CROWN DAMAGE. THE SEAT TRACK WAS REPLACED FROM BS 949 TO 1029, IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201708312427Seat Track · damagedSEAT TRACK AT BS 1681, LBL 47.5 FOUND THE CROWN DAMAGED. THE SEAT TRACK WAS REPLACED FROM BS 1631 TO 1731, LBL 47.5 IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201708312426Seat Track · damagedSEAT TRACK AT BS 1681, LBL 27.5 FOUND WITH CROWN DAMAGE. THE SEAT TRACK WAS REPLACED FROM BS 1651 TO 1710, LBL 27.5 IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201708312425Seat Track · damagedSEAT TRACK AT BS 755, LBL 47.5 FOUND THE CROWN DAMAGED. REPLACED THE SEAT TRACK AT EXISTING SPLICES FROM BS 725 TO 765, IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201708312424Cargo Track · crackedCARGO TRACK AT BS 775, LBL 75.5 CRACKED. REPLACED THE CARGO TRACK FROM BS 725 TO EXISTING SPLICE AT BS 765, IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201708312423Longeron Splice · crackedCROWN AREA LONGERON SPLICE AT STA 5-0, LONGERON 4L FOUND CRACKED. THE LONGERON SPLICE WAS REMOVED AND REPLACED IAW SRM 51-33-01-0G. A NEW LONGERON SPLICE WAS FABRICATED IAW DWG AEA 7634, REV B. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201708312422Skin · crackedLEFT WING DROOPED LEADING EDGE UPPER SKIN FOUND CRACKED AT XDLE 325. REPAIRED IAW SRM 57-40-01-2R, FIG 201, REPAIR 5. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201708312421Angle · damagedMAIN DECK, FUSELAGE FRAME AT BS A 535, LONGERON 24L FOUND A DAMAGED REPAIR ANGLE. THE REPAIR WAS REMOVED AND THE REPAIR REACCOMPLISHED IAW SRM 53-20-07-2R, FIG 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201708312420Angle · damagedMAIN DECK FUSELAGE FRAME AT BS 535, LONGERON 19L FOUND A DAMAGED REPAIR ANGLE. DAMAGED REPAIR ANGLE REMOVED AND REPAIR REACCOMPLISHED IAW SRM 53-20-07-2R, FIG 202, REPAIR 1.SDR FDEA201708312418Doubler · crackedLEFT WING FIXED LEADING EDGE BEADED DOUBLER FOUND CRACKED AT XOS 627 - 628. REPAIRED IAW SRM 57-40-02-2R, FIG 203, REPAIR 15. REPAIR CLASSIFED AS MAJOR IAW GMM 6-2-100.SDR FDEA201708312429Seat Track · damagedMAIN DECK FLOOR SEAT TRACK AT STA 972, X=-47.5 FOUND CROWN DAMAGED AS MARKED. REPAIRED SEAT TRACK AS PER SRM 53-00-52-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR FDEA201708312428Seat Track · damagedMAIN DECK FLOOR SEAT TRACK AT STA 5-23, X=75.25 FOUND CROWN DAMAGED. REPAIRED SEAT TRACK AT EXISTING SPLICE STA 5-0, X=75.25 TO STA 5-63, X=75.25 AS PER SRM 53-00-52-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR FDEA201708312419Former · crackedRT WING FIXED LEADING EDGE FORMER FOUND CRACK AT STA XOS 584 AS MARKED. REMOVED AND REPLACED WITH NEW FABRICATED FORMER PER SRM 51-33-01-0G. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. NEW FORMER PN: FX ARB2931-14 FABRICATED AS PER DRAWING ARB 2931 REV H.SDR FDEA201705121399Link · lack of lubeHIGH SPEED REJECT DUE TO QUESTIONABLE RUDDER AUTHORITY. REJECTION SPEED 30 KNTS. ON INITAL CONFIGURATION CHECK OF LEFT RUDDER THROW FELT NORMAL WITH GREEN BOXES FOR UPPER AND LOWER RUDDER. RIGHT RUDDER VERY STIFF WITH ONLY TOP RUDDER GREEN BOX. ON SECONSDR FDEA201608122882Indication Sys · false activationHYD 1 FAIL, LEVEL 2 ALERT RT AFTER T/O, IND 23L. REF TO QRH. RAISED GEAR, SLATS CLIMBED TO 230. DECLARED EMERGENCY. PLANNED FOR FLAPS 35/EXT LAND. ALERT CAME ON AFTER GEAR RAISED, PRIOR TO FLAP RETRACTION. REPLACED NR 1 HYD RESEVOIR QTY INDICATION ARM, SDR FDEA201602160586Hydraulic Line · rupturedLANDING GEAR FAILED TO RETRACT. FOUND THE MAIN HYD HOSE RUPTURED & LEAKING AT THE RT GEAR TRIM CYLINDER. ALSO FOUND TRIM CYLINDER INTERLOCK FUSE TRIPPED. INSTALLED FLEX HOSE IAW AMM 20-10-01-2 & 20-40-01-2. RESET TRIM CYLINDER INTERLOCK FUSE IAW AMM 32-37-SDR FDEA201510153229Skin · corrodedMAIN DECK CTR WING TANK, LEFT HAND UPPER SURFACE AT BS 1227, BETWEEN X= 8.5 & X= -8.5, FOUND CORRODED. REPAIRED IAW EA 1-5730-T0320743 PT 1. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.SDR FDEA201510153228Fuel Tank · corrodedMAIN DECK CTR WING TANK RIGHT HAND UPPER SURFACE AT BS 1227, BETWEEN X= -8.5 & X= -27.5 FOUND CORRODED. REPAIRED IAW EA 1-5730-T0320743 PT 1. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.SDR FDEA201510123174Doubler · chafedAGEING ACFT, EXISTING REPAIR DOUBLER ON FUSELAGE EXTERIOR SKIN AT CTR CARGO DOOR, LOWER AFT JAMB AT STATION 1781. EXISTING REPAIR CHAFED AT EDGE OF DOUBLERS, CARRIED OUT REPAIR IAW EA 1-5330-T0320626A PT 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100. REFER SDR FDEA201510123177Skin · corrodedMAIN DECK CTR WING TANK, RT UPPER SURFACE AT STRINGER 15, BETWEEN XCW=-27 & X=- 51, FOUND CORRODED. REPAIRED IAW EA 1-5730-T0320742 PT 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
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