N588FE
Service difficulty reports · 346
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 = 'N588FE' 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 = 'N588FE' 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 FDEA200903180944Frame · dentedCABIN, RT STA 1661 LONGERON 12 FOUND DENTED. REPAIRED AS PER SRM 53-30-00 FIGURE 1 VOLUME I REVISION 40. REPETITIVE INSPECTION REQUIRED, INITIAL INSPECTION AT 14,500 CYCLES AND REPETITIVE INSPECTION AT 9,500 CYCLES TO BE CARRIED OUT AS PER SRM 53-30-00 FIGUSDR FDEA200903180943Frame · dentedCABIN, LT STA 1721 LONGERON 12 FRAME FOUND DENTED. REPAIRED AS PER SRM 53-30-00 FIGURE 1 VOLUME I REVISION 40. REPETITIVE INSPECTION REQUIRED, INITIAL AT 14,500 CYCLES AND REPETITIVE INSPECTION AT EVERY 9,500 CYCLES. TO BE CARRIED OUT AS PER SRM 53-30-00 FSDR FDEA200903170938Seal · crackedLT WING TRAILING EDGE PANEL NR 541GB CUT-OUT STRIP FOUND CRACKED. REMOVED AND REPLACED CRACKED SEAL AT LT WING TRAILING EDGE PANEL NR 541GB AS PER SRM 51-34-01 VOL. II REV. 40. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100 REV. 107.SDR FDEA200903170937Support Fitting · crackedCRACK INDICATION FOUND DURING HFEC OPEN HOLE INSPECTION ON DIAMETER 0.460 INCH HOLE AT MAIN CARGO DOOR LOWER JAMB NR 7 SUPPORT FITTING AT HOLES A, B, C AND D. SUPPORT FITTING REMOVED AND REPLACED AS PER SRM 51-31-01 VOLUME II REVISION 40. REPAIR CLASSIFIED ASSDR FDEA200903170936Support Fitting · crackedCRACK INDICATION FOUND DURING HFEC OPEN HOLE INSPECTION ON DIAMETER 0.460 INCH AT MAIN CARGO DOOR LOWER JAMB NR 2 SUPPORT FITTING AT HOLES B, C AND D. SUPPORT FITTING REMOVED AND REPLACED AS PER SRM 51-31-01 VOL. II REV. 40. REPAIR CLASSIFIED AS MAJOR AS PERSDR FDEA200903170935Support Fitting · crackedCRACK INDICATION FOUND DURING HFEC OPEN HOLE INSPECTION ON DIAMETER 0.460 INCHES AT MAIN CARGO DOOR LOWER JAMB NR 1 SUPPORT FITTING AT HOLES A, C AND D. SUPPORT FITTING REMOVED AND REPLACED AS PER SRM 51-31-01 VOLUME II REVISION 40. REPAIR CLASSIFIED AS MAJORSDR FDEA200903170934Skin · crackedLT WING LEADING EDGE LOWER PANEL NR 526GB CUT-OUT AT STA XOS=996 FOUND CRACKED. REPAIR CARRIED-OUT AT LT WING LEADING EDGE LOWER PANEL NR 526GB CUT-OUT AT STA XOS= 996 AS PER SRM 57-10-00 FIG. 41 VOL. I REV. 40. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-SDR FDEA200903170933Skin · crackedLT WING LEADING EDGE SKIN AT STA XOS=997 FOUND WITH CRACK APPROXIMATELY 10 INCHES LONG. REPAIR CARRIED OUT AS PER EA 1-5740-127781, THIS REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 107.SDR 07FDEA04070Web · corrodedLEFT AIRCONDITIONING COMPARTMENT CENTER LOWER INBOARD WEB FOUND WITH CORROSION. 10-01-07 REPAIR CARRIED OUT AS PER FEDEX EA 1-5310-115193. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.SDR 07FDEA03802Trunnion · corrodedCENTER LANDING GEAR RIGHT MOUNTING. TRUNNION FITTING FORWARD AND AFT HOLE FOUND WITH CORROSION. 10-01-07 COMPLIED WITH FEDEX E.A. 1-5310-115190. CLASSIFIED AS A MAJOR REPAIR AS PER FEDEX GMM 6-2-100.SDR 07FDEA03801Trunnion · corrodedCENTER LANDING GEAR LEFT MOUNTING. TRUNNION FITTING FORWARD AND AFT HOLE FOUND WITH CORROSION. 10-01-07 COMPLIED WITH FEDEX E.A. 1-5310-115189. CLASSIFIED AS A MAJOR REPAIR AS PER FEDEX GMM 6-2-100.SDR 07FDEA03794Trunnion · crackedFASTENER HOLE FOUND CRACK AT 9 AND 3 O'CLOCK POSITION ON LONGERON AT RIGHT SIDE NOSE LANDING GEAR TRUNNION. 09-28-07 REPAIR CARRIED OUT AT FASTENER HOLE, 9 AND 3 O'CLOCK POSITION ON LONGERON AT RT NLG TRUNNION AS PER SRM 51-31-01 VOLUME II. REPAIR CLASSIFISDR 07FDEA03554Frame · dentedMAIN DECK - STA 1601, LONGERON 10R-11R FRAME FOUND DENTED. 09-26-07 REPAIR CARRIED OUT AS PER SRM 53-30- 00 FIG. 1 VOL.I. DAMAGE TOLERANCE INSPECTION REQUIREMENT REQUIRES INITIAL INSPECTION AT 14500 CYCLES FROM THE CURRENT 9821 CYCLES AND REPETITIVE SDR 07FDEA03553Trunnion · crackedRIGHT NOSE LANDING GEAR TRUNNION FITTING SUSPECT WITH CRACK. 09-28-07 REPAIR CARRIED OUT AT RT NLG TRUNNION FITTING AS PER SRM 53-40-00 FIGURE 23 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.SDR 07FDEA03552Trunnion · crackedLEFT NOSE LANDING GEAR TRUNNION FITTING SUSPECT WITH CRACK. 09-28-07 REPAIR CARRIED OUT AT LT HAND NOSE LANDING GEAR TRUNNION FITTING AS PER SRM 53-40-00 FIGURE 23 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.SDR 07FDEA03512Duct · crackedLEFT WING, LEADING EDGE TELESCOPING DUCT CUTOUT I/B AND O/B CORNERS FOUND CRACKS. 10-01-07 REPAIR CARRIED OUT AS PER FEDEX EA 1-5710-115191. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.SDR 07FDEA00520Actuator · brokenAFTER GEAR RETRACTION ON TAKEOFF (FROM ALA RWY 05) RECEIVED RED UNSAFE GEAR INDICATION ON RT MAINS INDICATED ON GEAR HANDLE INDICATORS AS WERE AS CONF SYNOPTIC. RAN RED TABS. RETURNED TO ALA AFTER DUMPING AP PXLY 100.000 LBS CONFIG SYNOPTIC SHOWED RIGHT GEARSDR 06FDEA1240Doubler · crackedLT WING, AT STA XOS 762 LEADING EDGE CAVITY BEADED DOUBLER FOUND CRACKED. LEFT WING AT STA XOS 762 LEADING EDGE CAVITY CRACKED BEADED DOUBLER. REPAIR CARRIED OUT AS PER SRM 57-10-00 FIGURE 25 VOLUME I. THIS REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100.SDR 06FDEA1239Doubler · crackedLT WING, AT STA XOS 697 LEADING EDGE CAVITY BEADED DOUBLER FOUND CRACKED. LEFT WING AT STA XOS 697 LEADING EDGE CAVITY CRACKED BEADED DOUBLER. REPAIR CARRIED OUT AS PER SRM 57-10-00 FIGURE 25 VOLUME I. THIS REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100.SDR 06FDEA1238Doubler · crackedLT WING, AT STA XOS 670 LEADING EDGE CAVITY BEADED DOUBLER FOUND CRACKED. LEFT WING AT STA XOS 670 LEADING EDGE CAVITY CRACKED BEADED DOUBLER REPAIR CARRIED OUT AS PER SRM 57-10-00 FIGURE 25 VOLUME I. THIS REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100.SDR 06FDEA1237Doubler · crackedLT WING, AT STA XOS 647 LEADING EDGE CAVITY BEADED DOUBLER FOUND CRACKED. LEFT WING AT STA XOS 647 LEADING EDGE CAVITY CRACKED BEADED DOUBLER REPAIR CARRIED OUT AS PER SRM 57-10-00 FIGURE 25 VOLUME I. THIS REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100.SDR 06FDEA1235Access Door · crackedFUSELAGE - AIRCON NR 2 COMPARTMENT ACCESS DOOR EXTERIOR CRACKED. CRACKED AIRCON NR 2 COMPARTMENT ACCESS DOOR EXTERIOR SKIN. REMOVED AND REPLACED AS PER SRM 51-35-01 VOLUME II. NEW SKIN FABRICATED AS PER DRAWING NR ACA3822. THE ACCESS DOOR REMOVED AND REINSSDR 06FDEA1213Support Fitting · crackedRIGHT WING OUTBOARD FLAP OUTBOARD LOWER FASTENER HOLES COMMON TO INBOARD HINGE SUPPORT FITTING ARC4009 FOUND OUTBOARD LOWER HOLE REVEALED CRACK INDICATION. OUTBOARD LOWER HOLE AT RIGHT WING OUTBOARD FLAP OUTBOARD LOWER FASTENER HOLES COMMON TO INBOARD HINGE SSDR 06FDEA1217Seat Track · corrodedMAIN DECK COMPARTMENT SEAT TRACK FOUND WITH CORROSION AT STA 1531 TO 5-73 RBL 75. MAIN DECK COMPARTMENT, CORRODED SEAT TRACK AT STA 1531 TO STA 5-73 RBL 75. REMOVED AND REPLACED AT STA 1531 TO STA 5-123 RBL 75 AS PER SRM 53-70-00 FIGURE 1 VOLUME I. THIS RSDR 06FDEA1216Seat Track · corrodedMAIN DECK COMPARTMENT SEAT TRACK FOUND WITH CORROSION AT STA 1501 - 1531 RBL 08. MAIN DECK COMPARTMENT, CORRODED SEAT TRACK AT STA 1491 TO 1531 RBL 08. REMOVED AND REPLACED AS PER SRM 53-70-00 FIGURE 1 VOLUME I. THIS REPAIR IS CLASSIFIED AS MAJOR PER GMSDR 06FDEA1215Seat Track · corrodedMAIN DECK COMPARTMENT SEAT TRACK FOUND WITH CORROSION AT STA 5-10 TO 5-93 LBL 08. MAIN DECK COMPARTMENT, CORRODED SEAT TRACK AT STA 5-10 TO STA 5-93 LBL 08. REMOVED AND REPLACED AT STA 5-10 TO STA 5-123 LBL 08 AS PER SRM 53-70-00 FIGURE 1 VOLUME I. THIS RSDR 06FDEA1214Seat Track · corrodedMAIN DECK COMPARTMENT SEAT TRACK FOUND WITH CORROSION AT STA 1341 - 1361 RBL 75. CORRODED SEAT TRACK ON MAIN DECK COMPARTMENT AT STA 1279 TO STA 1373 RBL 75. REMOVED AS PER SRM 51-31-01 VOLUME II. NEW SEAT TRACK REWORKED AND INSTALLED AS PER SRM 53-70-0SDR 06FDEA1203Frame · dentedMAIN DECK COMPARTMENT RIGHT FUSELAGE FRAME FOUND WITH DENT AT STA 1681 LONGERON 12R. DENT MARK ON MAIN DECK COMPARTMENT RIGHT FUSELAGE FRAME AT STA 1681 LONGERON 12R EXISTING REPAIR DOUBLER REPAIRED AS PER SRM 53-30-00 FIGURE 1 VOLUME I. ACCOMPLISH AN INITIASDR 06FDEA1202Frame · dentedMAIN DECK COMPARTMENT RIGHT FUSELAGE FRAME FOUND WITH DENT AT STA 1701 LONGERON 12R. DENT ON MAIN DECK COMPARTMENT RIGHT FUSELAGE FRAME AT STA 1701 LONGERON 12R REPAIRED AS PER SRM 53-30-00 FIGURE 1 VOLUME I. ACCOMPLISH AN INITIAL INSPECTION AT OR BEFORE REASDR 06FDEA1195Spar · damagedRIGHT WING, REAR SPAR AT STA XORS 564 UPPER CHORD FOUND ELONGATED HOLE. ELONGATED HOLE ON RIGHT WING REAR SPAR STA XORS 564 UPPER CHORD REPAIRED AS PER FEDEX EA NR 1-5710-95804, TITLE: WINGS, RIGHT WING AFT SPAR UPPER CAP AFT TANG AT STATION XORS = 564 (REAR SDR 06FDEA1198Doubler · crackedLT WING, AT STA XOS 624 LEADING EDGE CAVITY BEADED DOUBLER FOUND CRACKED. CRACK ON LEFT WING STA XOS 624 LEADING EDGE CAVITY BEADED DOUBLER REPAIRED AS PER FEDEX EA NR 1-5730-95801, TITLE: WINGS, LEADING EDGE BEADED DOUBLER, PERMANENT REPAIR. THIS REPAIR IS SDR 06FDEA1197Doubler · crackedLT WING AT STA XOS 632 LEADING EDGE CAVITY BEADED DOUBLER FOUND CRACKED. CRACK ON LEFT WING STA XOS 632 LEADING EDGE CAVITY BEADED DOUBLER REPAIRED AS PER FEDEX EA NR1-5730-95801, TITLE: WINGS, LEADING EDGE BEADED DOUBLER PERMANENT REPAIR. THIS REPAIR IS SDR 06FDEA1196Spar Cap · corrodedRIGHT WING REAR SPAR UPPER END CAP BETWEEN STA XORS 949 TO XORS 981 FOUND CORROSION. CORROSION AT RIGHT WING REAR SPAR UPPER END CAP BETWEEN STA XORS 949 TO XORS 981 REMOVED AS PER SRM 51-21-01 VOLUME II. MINIMUM ORIGINAL THICKNESS =0.182" (0.197"-0.015"),SDR 06FDEA1194Spar Cap · corrodedLT WING REAR SPAR UPPER END CAP STA XORS 1042 FOUND CORROSION. CORRODED AREA ON LEFT WING REAR SPAR UPPER END CAP STA XORS 1042 REPAIRED AS PER FEDEX EA NR 1-5710-95805, TITLE: WINGS, LEFT REAR SPAR UPPER CAP AFT TANG CORROSION CENTERED AT STATION XORS = 1042SDR 06FDEA1201Frame · dentedMAIN DECK COMPARTMENT LEFT FUSELAGE FRAME FOUND WITH DENT AT STA 1681 LONGERON 12L. DENTED FRAME ON MAIN DECK COMPARTMENT LEFT FUSELAGE AT STA 1681 LONGERON 12L REPAIRED AS PER SRM 53-30-00 FIGURE 1 VOLUME I. ACCOMPLISH AN INITIAL INSPECTION AT OR BEFORE REASDR 06FDEA1193Spar · corrodedLT WING, REAR SPAR AT STA XORS 590 - 593 UPPER CHORD UPPER SURFACE FOUND CORROSION. CORROSION AT LEFT WING REAR SPAR STA XORS 590-593 UPPER CHORD UPPER SURFACE REPAIRED AS PER FEDEX E.A. NR 1-5710-95800, TITLE: WINGS, LEFT HAND REAR SPAR UPPER CAP CORROSIONSDR 06FDEA1199Frame · dentedFOUND MAIN DECK COMPARTMENT LT FUSELAGE FRAME FOUND WITH DENT AT STA 535 BETWEEN STRINGER 20-21L. MAIN DECK COMPARTMENT LT FUSELAGE DENTED FRAME AT STA 535 BETWEEN STRINGER 20-21L, REPAIR CARRIED OUT AS PER DWG SRZ-53-503. REPAIR CLASSIFIED AS MAJOR AS PESDR 06FDEA1200Frame · dentedFOUND MAIN DECK COMPARTMENT LT FUSELAGE FRAME FOUND WITH DENT AT STA 535 BETWEEN STRINGER 23-24L. MAIN DECK COMPARTMENT LT FUSELAGE DENTED FRAME AT STA 535 BETWEEN STRINGER 23-24L, REPAIR CARRIED OUT AS PER DWG SRZ-53-503. REPAIR CLASSIFIED AS MAJOR AS PERSDR 06FDEA1171Repair · chafedCENTER CARGO, DOOR CUTOUT FWD LOWER SECTION APPROX CARGO FLOOR LEVEL REPAIR DOUBLER FOUND CHAFED. CHAFED REPAIR DOUBLER ON CENTER CARGO DOOR CUTOUT FORWARD LOWER SECTION APPROX CARGO FLOOR LEVEL REPAIRED AS PER SRM 53-50-00 FIGURE 16 VOLUME I. THIS REPAIR ISSDR 06FDEA1175Doubler · crackedRT WING AT STA XOS 550 LEADING EDGE CAVITY BEADED DOUBLER FOUND CRACKED. CRACK ON RIGHT HAND WING STA XOS 550 LEADING EDGE CAVITY BEADED DOUBLER REPAIRED AS PER FEDEX EA 1-5730-95802, TITLE: WINGS - LEADING EDGE BEADED DOUBLER -PERMANENT REPAIR. THIS REPASDR 06FDEA1176Skin · crackedSNRM N00719 : RT WING AT STA XOS 908 FIXED LEADING EDGE FOUND CRACKED. CRACK ON RIGHT HAND WING STA XOS 908 FIXED LEADING EDGE REPAIRED AS PER SRM 57-10-00 FIGURE 37 VOLUME I. NR 7 SLAT ASSEMBLY REMOVED AND INSTALLED AS PER AMM 27-80-30-4 AND RANGE OF MOVESDR 06FDEA1174Stringer · crackedSNRM N00604 : HFEC INSPECTION FOUND CRACK ON LT UPPER WING OB END OF STRINGER S-13L APPROX. 1 INCH LONG. REPAIRED AS PER SRM 57-20-00.SDR 06FDEA1173Stringer · crackedSNRM N00606 : HFEC INSPECTION FOUND CRACK ON LT UPPER WING OB END OF STRINGER S-14L APPROX 13 INCHES LONG. REPAIRED AS PER SRM57-20-00.SDR 06FDEA1172Structure · chafedSNRM N00623 : CENTER CARGO - DOOR CUTOUT AFT LOWER SECTION APPROX FLOOR LEVEL FOUND CHAFED. REPAIRED AS PER SRM 53-50-00.SDR 06FDEA0063Warning Light · unknownAFTER T/O WITH GEAR HANDLE UP, HAD BOTH PRIM AND SEC RT MAIN GEAR DSPL "RED" LIGHT (GEAR NOT UP). RAN QRH, AND 1ST ATTEMPT TO CYCLE GEAR SAME IND. AFTER 2ND ATTEMPT GEAR SHWD PRIM AND SEC "UP AND LOCK" IND. CONT TO DEST. PSEU FAULT RVW GOT FAULT CODE NR 9:SDR 05FDEA02589Nose Cowl · vibrationON TAKEOFF RWY 25L VHHH, AFTER POWER REDUCTION TO CLIMB AT 1500 AFL, GOT A YAW "BUMP" AND NOISE AND VIBRATION "BUZZ" IN AIRFRAME. NO ABNORMAL INDICATIONS INITIALLY, THEN NR 1 COMPRESSOR VIBRATION CLIMBED TO 5.0 AMBER, REDUCED NR 1 THROTTLE AND BUZZ DIMINISHEDSDR 03FDEA01349Fire Loop · shortedAT 1455Z, FL360,M.83.ENG NR 2 FIRE LIGHT CAME ON. INTERMITTENT AT FIRST IT BECAME STEADY AND ENG NR 2 WAS SHUTDOWN IAW CHECKLIST. NO OTHER ADVERSE INDICATIONS OBSERVED EXCEPT FIRE DETECT 2 FAIL LEVEL 1 ALERT. RTB WAS UNEVENTFUL, 1 FIRE BOTTLE WAS DISCHARGEDSDR 03FDEA01270Fire Warning · malfunctionedLOWER AFT CARGO FIRE MASTER WARNING AND ALERT CAME ON DURING CRUISE AT FLT 390 DIVERTED IN DEN MEL 12AUG03 DEN ACN RELEASED FOR SERVICE PER MEL CDL 3A 26-22-01- 02 CATEGORY 3A B EXPIRATION 3A 15AUG03 AFTER DOWN LOAD 2 C INSPECTED AREA FOR SMOKE AND 2 FOR FISDR 03FDEA01115Switch · intermittentAT APPROX 500 FEET CARGO DOOR AFT -A- LEVEL TWO ILLUMINATED. DUMPED TO MAX LANDING WEIGHT. COMPLIED WITH QRH AND RETURNED TO SFS. NOTE: DOOR OPEN LIGHT ALSO ILLUMINATED. ENT BY: 317084 RPT BY: 096537 FACT 18JUL03 22:14 SFS R REMOVED AND REPLACED S1 -SDR 03FDEA00992Nut · corrodedHORIZONTAL STABILIZER, LT UPPER AFT PLANK BARREL NUT BORE NR 34L FOUND CORROSION BEYOND EO 1-5510-7-5000 LIMITATION. LT HOR STAB UPPER AFT PLANK BARREL NUT NR 34L BORE REPAIR CARRIED OUT IAW EA 1-5510-71721, STABILIZERS- HORIZONTAL STABILIZER- BARREL NUT B
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