N589FE
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 = 'N589FE' 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 = 'N589FE' 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 FDEA201105241952Seat Track · corrodedCABIN LT STATION 455 TO 475 X=27.5 SEAT TRACK FOUND CORROSION. CABIN LT STATION 455 TO 475 X=27.5 SEAT TRACK REMOVED AND REPLACED AS PER SRM 51-31-01 REVISION 46. SEAT TRACK FABRICATED AS PER DRAWING ACA7713 REVISION D. REPAIR CLASSIFIED MAJOR AS PER GMM 6-SDR FDEA201105201898Skin · crackedVERTICAL STABILIZER RT REAR CENTER SPAR TO REAR SPAR LWR PANEL FOUND CRACKED. REPAIRED AS PER SRM 55-30-02 FIG 201 REPAIR 2 REV 46. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REV 112.SDR FDEA201105201897Access Panel · crackedFOUR FASTENER HOLES FOUND CRACKED DURING HFEC OPEN HOLE INSPECTION AT RT WING LWR SKIN ACCESS CUTOUT BETWEEN STA XORS=683.4 AND STA XORS=713.6 04 EA CRACK FASTENER HOLES ON RT WING FUEL TANK ACCESS PANEL 636AB CUTOUT CARRIED OUT REPAIR AS PER DRAWING SG1157000SDR FDEA201105201896Access Panel · crackedTWO FASTENER HOLES FOUND CRACK INDICATION DURING HFEC OPEN HOLE INSPECTION AT LT WING LOWER SKIN ACCESS DOOR. CUTOUT CARRIED OUT REPAIR AS PER DRAWING SG11570004 REV B. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100 REV 112.SDR FDEA201105201895Longeron · crackedCRACK INDICATION APPROX 1.2" IN LENGTH FOUND DURING X-RAY INSPECTION AT BS 6-100, L6L FWD SECTION EDGE. CRACK AT BS 6-100, L6L FWD SECTION EDGE REPAIRED AS PER SRM 53-00-05 FIG 202 REV 46. LONGERON FABRICATED AS PER DRAWING AEA7001 REV NEW. REPAIR CLASSSDR FDEA201105181866Seat Track · corrodedBS 415 TO 475 LBL 107.25 SEAT TRACK FOUND CORRODED. SEAT TRACK REMOVED AND REPLACED AS PER SRM 51-33- 01 REV 46. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REV 112.SDR FDEA201105181868Seat Track · corrodedBS 1396 TO 1410 RBL 77.25 SEAT TRACK FOUND CORRODED. REMOVED AND REPLACED AS PER SRM 51-33-01 REVISIOIN 46. SEAT TRACK FABRICATED AS PER DRAWING AEA7325 REVISION J. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 112.SDR FDEA201105181867Seat Track · corrodedBS 1551 RBL 8.5 SEAT TRACK FOUND CORRODED. REPAIRED AS PER SRM 53-00-52 FIG 201 REVISION 46. SEAT TRACK FABRICATED AS PER DRAWING AFA7795 REVISION K. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 112.SDR FDEA201105181865Frame · dentedBS 1701 L11L FRAME FOUND DENT. REPAIRED AS PER SRM 53-00-07 FIG 201 REVISION 46. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 112.SDR FDEA201105181864Frame · dentedBS 1681 L11L FRAME FOUND DENTED. REPAIRED AS PER SRM 53-00-07 FIG 201 REVISION 46. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 112. INITIAL INSPECTION AT 14500 AND REPETITIVE INSPECTION AT 9500 USING HFEC METHOD.SDR FDEA201105181863Frame · dentedBS 1741 L11L FRAME FOUND DENT. REPAIRED AS PER SRM 53-00-07 FIG 201 REVISION 46. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 112.SDR FDEA201105181862Frame · dentedBS 1661 L11L FRAME FOUND DENT. REPAIRED AS PER SRM 53-00-07 FIG 201 REV 46. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REV 112.SDR FDEA201105081780Warning Light · false activationFSS DISCHARGE LIGHT ILLUMINATED ON FLT STA 7L AND 7R SHOWING RED ON FSS PANEL WITH TEMP INDICATION 500F. SUPPRESSION FLUID DRAINING FROM BOOM AT 2R, NO SMOKE, FUMES OR INDICATION OF FIRE CONFIRMED BY CFR CREW. REACIVATED THE PORTABLE FIRE EXTINGUISHER BOTTLSDR FDEA201101290410Line · looseAFTER EXTENDING LANDING GEAR, RECEIVED A "HYD 3 QTY LO" ALERT. QTY STABILIZED AT 1.7 ON ARRIVAL FOUND NR 3 HYD SYS QTY IND READ 2.8 AFTER ENG SHUTDOWN. FOUND STAB COMP DOOR AREA & NR 3 LEFT EDP SUCTION HOSE ELBOW AREA HYD STAIN. SERVICED NR 3 HYD SYS TO 7.5 ISDR FDEA201003120790Valve · malfunctionedON SLATS RETRACT UNCOMMAND ROLL TO THE RT, REQUIRE FULL LT AILERON AND RUDDER, NO SLAT DISAGREEMENT, NO ALERT, MOVE SLAT HANDLE BACK TO SLATS EXTEND, ACFT UNDER CONTROL, MADE NORMAL FLAPS 35 LANDING PVG WITHOUT INCIDENT. INSTALLED THE LT OTBD SLATS BALANCESDR FDEA200908163023Frame · damagedREWORK REQUIRED ON EXISTING FRAME REPAIR AT BS 535 LONGERON 25 LT FRAME. CARRIED OUT REPAIR IAW EA 1-5310-132181, REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REV 107.SDR FDEA200908163022Frame · damagedREWORK REQUIRED ON EXISTING FRAME REPAIR AT BS 535 LONGERON 21 LEFT FRAME. CARRIED OUT REPAIR IAW EA 1-5310-132181, REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REV 107.SDR FDEA200908032880Frame · dentedMAIN DECK CARGO COMPARTMENT SIDEWALL, BS 1641 RT FRAME INNER FLANGE FOUND DENTED AT LONGERON 12 POSITION. MAIN DECK CARGO COMPARTMENT SIDEWALL BS 1641 RT FRAME AT LONGERON 12 POSITION DENT INNER FLANGE, REPAIR CARRIED OUT AS PER SRM 53-00-07 FIG. 201. REPAIRSDR FDEA200908022868Skin · cracked09 EA FASTENER HOLES FOUND WITH CRACK INDICATIONS DURING OPEN HOLE HFEC INSP AT RT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STA XORS=690 AND STA XORS=700 AS MARKED. REPAIR CARRIED OUT AS PER EA 1-5710-132734.SDR FDEA200908022867Skin · cracked10 EA FASTENER HOLES FOUND WITH CRACK INDICATIONS DURING OPEN HOLE HFEC INSP AT LTW LWR SKIN ACCESS DOOR CUTOUT BETWEEN STA XORS=690 AND STA XORS=700 AS MARKED. REPAIR CARRIED OUT AS PER EA 1-5710-132735. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100 REV.SDR FDEA200907312862Hinge Bracket · corrodedLEFT WING - WING SIDE OTBD FLAP OTBD HINGE OTBD ACTUATOR HOLE FOUND CORROSIONS. REWORKED AS PER EA 1-5750-132167. BUSHING FABRIACATED AS PER CMM 57-44-09 REV. 64 AND INSTALLED AS PER EA 1-5750-132167. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV. 107.SDR FDEA200907312861Hinge Bracket · corrodedLT WING - OTBD FLAP OTBD HINGE (WING SIDE) INBD ACTUATOR HOLE FOUND CORROSION. REWORKED AS PER EA 1-5750-132167. BUSHING FABRICATED AS PER CMM 57-44-09 REV. 64 AND INSTALLED AS PER EA 1-5750-132167, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV.107.SDR FDEA200907312860Hinge Bracket · corrodedRT WING - WING SIDE OTBD FLAP OTBD HINGE OTBD ACTUATOR HOLE FOUND CORROSIONS. REWORKED AS PER EA 1- 5750-132168. BUSHING FABRICATED AS PER EA 1-5750-132168. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REV. 107.SDR FDEA200907312859Hinge Bracket · corrodedRT WING - OTBD FLAP OTBD HINGE (WINGSIDE) LWR MOUNT OTBD HOLE FOUND CORROSION. REWORKED AS PER EA 1-5750-132168. BUSHING FABRICATED AS PER CMM 57-44-09 REV. 64 AND INSTALLED AS PER EA 1-5750-132168. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV. 107.SDR FDEA200907312857Hinge Bracket · corrodedLT WING - FLAP SIDE INBD FLAP OTBD HINGE OTBD PIVOT HOLE FOUND CORROSIONS. HINGE REWORKED AS PER EA 1-5750-132166. BUSHING FABRICATED AS PER MD-11 CMM 57-52-03 REV. 64. AND INSTALLED AS PER EA 1-5750-132166. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 RESDR FDEA200907312853Cargo Track · corrodedMAIN DECK CARGO COMPARTMENT FLOOR TRACK X= -75.25 FLANGE FOUND CORRODED BETWEEN STA 1189 TO STA 1209. CORROSION REMOVED AS PER SRM 51-21-01 VOL. 2 REV. 40, MATERIAL REMOVED 0.042", ORIGINAL THICKNESS 0.080", REMAINED THICKNESS 0.038", AND FOUND EXCEEDED LIMISDR FDEA200907312852Cargo Track · corrodedMAIN DECK CARGO COMPARTMENT FLOOR TRACK X=-75.25 FLANGE FOUND CORRODED BETWEEN STA 1285 AND 1305. CORROSION REMOVED AS PER SRM 51-21-01 VOL. 2 REV. 40, MATERIAL REMOVED 0.045", ORIGINAL THICKNESS 0.080", REMAINED THICKNESS 0.035" AND FOUND EXCEEDED LIMIT ASDR FDEA200907312851Spar Cap · corrodedRT WING - REAR SPAR UPPER CAP UPPER SURFACE FOUND CORROSIONS AT XORS 1043. REPAIRED AS PER EA 1-5710-132171. CLASSIFIED MINOR AS PER GMM 6-2-100 REV 107.SDR FDEA200907312850Spar Cap · corrodedRT WING - REAR SPAR UPPER CAP UPPER SURFACE FOUND CORROSION AT XORS 1040. REPAIRED AS PER EA 1-5710-132171. CLASSIFIED MINOR AS PER GMM 6-2-100 REV. 107.SDR FDEA200907312849Cargo Track · corrodedMAIN DECK CARGO COMPARTMENT FLOOR TRACK X=-75.25 FLANGE FOUND CORRODED AT BS 1371. CORROSION REMOVED AS PER SRM 51-21-01 VOL. 2 REV. 40. FOUND TO EXCEEDED LIMITS AS PER SRM 53-70-00 FIG. 3 VOL. 1 REV. 40. REPAIR CARRIED OUT AS PER SRM 53-00-52 FIG 201 REPAIRSDR FDEA200907312848Skin · dentedRIGHT WING INBD FLAP LWR SURFACE FOUND DENT LOCATED 8 INCHES FROM OTBD EDGE AND 22 INCHES FROM L/E. REPAIRED AS PER SRM 57-10-00 REV. 41. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100 REV. 107.SDR FDEA200907302837Longeron · corrodedAFT CARGO STA 1953, LONGERON 51L FOUND CORRODED. REMOVED AND REPLACED AS PER SRM 51-31-01 REVISION 41. LONGERON FABRICATED AS PER DRAWING AGA7810. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 107.SDR FDEA200907292822Skin · misrepairedEXISTING REPAIR AT FUSELAGE EXTERIOR, AFT OF CENTER CARGO DOOR CUTOUT, STA. 1811, LONGERON 39-R. EXISTING REPAIR AT FUSELAGE EXTERIOR, AFT OF CTR CARGO DOOR CUTOUT STA 1811, LONGERON 39-R EVALUATED AND FOUND NOT CARRIED OUT IAW SRM REPAIR SCHEME. SASCO 391. SDR FDEA200907292821Skin · misrepairedEXISTING REPAIR AT FUSELAGE EXTERIOR, AFT OF CENTER CARGO DOOR CUTOUT, STA 1801, LONGERON 41-R. EXISTING REPAIR DOUBLER EXTERIOR, AFT OF CTR CARGO DOOR CUTOUT, STA 1801, LONGERON 41-R EVALUATED AND FOUND NOT CARRIED OUT IAW SRM REPAIR SCHEME, SASCO 391. EXISSDR FDEA200907292816Skin · misrepairedEXISTING REPAIR AT FUSELAGE EXTERIOR AFT OF R1 DOOR, STA 495 LONGERONS 27-R TO 28-R EXISTING REPAIR AT FUSELAGE EXTERIOR, AFT OF R1 DOOR, STA. 495, LONGERON 27R TO 28R EVALUATED AND FOUND NOT IAW SRM REPAIR. SASCO 225. EXISTING REPAIR DOUBLER AND FINGER DOUBSDR FDEA200907292820Skin · misrepairedLHW - EXISTING REPAIR FOUND ON I/B FLAP UPPER SURFACE AT STA. X1FH 137. LHW EXISTING REPAIR AT I/B FLAP UPPER SURFACE AT STA. XIFH 13 7 EVALUATED AND FOUND NOT IAW SRM REPAIR. SASCO 225. EXISTING REPAIR DOUBLER REMOVED AS PER SRM 51-31-01 VOL. 2 REV. 40 AND SDR FDEA200907292827Longeron Splice · corrodedAFT CARGO - STA 1953 LONGERON 51L FOUND SPLICE JOINT CORRODED. REMOVED AND REPLACED PER SRM 51-31-01 REV. 41. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV. 107.SDR FDEA200907292826Beam · crackedCRACK INDICATION FOUND ON 1ST LAYER WEB FROM TOP DURING HFEC OPEN HOLE INSPECTION ON 0.520" HOLE AT MAIN CARGO DOOR NR 7 LWR JAMB FITTING AT HOLE D. REPAIR CARRIED OUT AS PER EA 1-5310-132174, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV. 107.SDR FDEA200907292825Beam · crackedCRACK INDICATION FOUND ON FIRST LAYER WEB FROM TOP DURING HFEC OPEN HOLE INSP ON 0.520" HOLE AT MAIN CARGO DOOR NR 2 LWR JAMB FITTING AT HOLE C. REPAIR CARRIED OUT AS PER EA 1-5310-132174. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV. 107.SDR FDEA200907282812Skin · canningLEFT WING - INBD FLAP UPPER SURFACE FWD INBD SECTION FOUND OIL CANNING.SDR 08FDEA00422Door · wornRT MLG WW, FOUND DOOR ASSEMBLY PANEL NR 741AL WITH EDGES WORN. REPAIRED AS PER EA 1-5280-117392, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR 08FDEA00376Seat Track · crackedMAIN DECK, AFTER FLOOR PANEL REMOVAL FOR WIRING MOD, FOUND SEAT TRACK UNDER FLOOR PANEL AT STA 635, X = 55 CRACKED. SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR 08FDEA00371Seat Track · crackedMAIN DECK, AFTER FLOOR PANEL REMOVAL TO FACILITATE SEAT TRACK REPAIR, FOUND SEAT TRACK UNDER FLOOR PANEL AT STA 635, X = -11 CRACKED. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2SDR 08FDEA00370Seat Track · crackedMAIN DECK, AFTER FLOOR PANEL REMOVAL TO FACILITATE SEAT TRACK REPAIR, FOUND SEAT TRACK UNDER FLOOR PANEL AT STA 635, X = 11 CRACKED. SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMSDR 08FDEA00369Seat Track · crackedMAIN DECK, AFTER FLOOR PANEL REMOVAL TO FACILITATE SEAT TRACK REPAIR, FOUND SEAT TRACK UNDER FLOOR PANEL AT STA 635, X = 33 CRACKED. SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STA 625 TO STA 665, X = 33" PER SRM 53-70-00 FIGURE 1 VOLUME I. SDR 08FDEA00348Support Fitting · crackedHFEC OPEN HOLE INSPECTION CARRIED OUT AND FOUND 01 EACH HOLE WITH CRACK INDICATION AT RIGHT WING OUTBOARD FLAP, AFT SIDE OF FLAP HINGE SUPPORT FITTING. RT OUTBOARD FLAP ASSY REMOVED AND REPLACED AS PER AMM 27-50-30-4. ADJUSTMENT AND TEST CARRIED OUT AS SDR 08FDEA00346Longeron Splice · crackedMAIN DECK, LONGERON SPLICE FITTING AT STA 6-5, L24R FOUND CRACK NEAR FASTENER. REMOVED AS PER SRM 51-31-01 VOLUME II. NEW SPLICE FABRICATED AS PER DRAWING ADA8429 AND INSTALLED AS PER SRM 51-31-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR 06FDEA03583Access Panel · crackedLEFT WING 519CB LT LEADING ACCESS PANEL FWD INBD CUTOUT FOUND CRACK. REPAIR CARRIED OUT AT LEFT WING 519CB LT LEADING ACCESS PANEL FWD INBD CUTOUT AS PER SRM 57-10-00 FIGURE 21 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.SDR 06FDEA03470Frame · bentMAIN DECK CARGO, FRAME AT RT INTERIOR FUSELAGE STA 1761, L11-13 FOUND BENT. REPAIR CARRIED OUT AT MAIN DECK CARGO FRAME, RT INTERIOR FUSELAGE STA 1761, L11-13 AS PER SRM 53-30-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.SDR 06FDEA03469Seat Track · corrodedFOUND MAIN DECK CARGO, SEAT TRACK FLANGE (STA 1521, RT=75.25) UNDER FLOOR PANEL CORRODED. REPAIR CARRIED OUT AT MAIN DECK CARGO SEAT TRACK FLANGE (STA 1521,RH=75.25) AS PER SRM 53-70-00 FIGURE 3 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.
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