N592FE
Service difficulty reports · 362
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 = 'N592FE' 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 = 'N592FE' 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 FDEA202010042413Doubler · crackedRIGHT WING LEADING EDGE BEADED DOUBLER AT APPROXIMATELY XORS 683, BEHIND SLAT NR 6 INBOARD SECTION, FOUND CRACKED. RIGHT WING LEADING EDGE BEADED DOUBLER AT APPROXIMATELY XORS 683, BEHIND SLAT NR 6 INBOARD SECTION, REPAIR CARRIED OUT, AS PER MD-11, SRM 57-40-SDR FDEA202010042412Angle · chafedMAIN DECK AT STATION 535 LONGERON 20, EXISTING REPAIR OUTER ANGLE FOUND CHAFED, AS MARKED. MAIN DECK AT LEFT ON FRAME STATION 535 LONGERON 20 REPAIR CARRIED OUT IN ACCORANCE WITH SRM 53-20-07-2R FIGURE 202 REPAIR 1. REPAIR CLASSIFIED AS MAJOR, PER GMM 6-2-1SDR FDEA202010042411Angle · chafedMAIN DECK AT LEFT STATION 535 LONGERON 24, EXISTING REPAIR OUTER ANGLE FOUND CHAFED, AS MARKED. MAIN DECK AT LEFT ON FRAME STATION 535 LONGERON 24 REPAIR CARRIED OUT IN ACCORDANCE WITH SRM 53-20-07-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR, PER GMMSDR FDEA202010042409Seat Track · corrodedMAIN DECK SEAT TRACK CROWN AT STATION 1541 X=27.5 FOUND CORROSION, AS MARKED. MAIN DECK AT STATION 1541 X=27.5 LEFT SEAT TRACK CROWN CORROSION. REMOVED AND FOUND TO EXCEED LIMIT, AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CORRODED SEAT TRACK REPSDR FDEA202010042407Seat Track · corrodedMAIN DECK SEAT TRACK CROWN AT STATION 1541 X=47.5 FOUND CORROSION, AS MARKED. MAIN DECK COMPARTMENT AT STATION 1541 X=47.5 SEAT TRACK CROWN BASE AREA CORROSION. REMOVED AND FOUND TO EXCEED LIMIT, AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CORRODESDR FDEA202010022397Doubler · crackedLEFT WING LEADING EDGE BEADED DOUBLER AT APPROXIMATELY BETWEEN XORS 505- 540, INSIDE LEFT REFUEL PANEL CUTOUT, FOUND CRACKS. LEFT WING LEADING EDGE BEADED DOUBLER AT APPROXIMATELY BETWEEN XORS 505-540, INSIDE LEFT REFUEL PANEL CUTOUT. REPAIR CARRIED OUT, ASSDR FDEA202010022396Former · crackedLEFT HAND WING, FIXED LEADING EDGE FORMER AT APPROXIMATELY XORS 480-500, BEHIND SLAT NR 4 MID SECTION, FOUND CRACKED. LEFT HAND WING, FIXED LEADING EDGE CRACKED FORMER AT APPROXIMATELY XORS 480-500, BEHIND SLAT NR 4 MID SECTION, REMOVED AND REPLACED WITH FABRSDR FDEA202010022395Seat Track · corrodedMAIN DECK COMPARTMENT, SEAT TRACK AT STATION 1671 X= -8.5 FOUND CORROSION, AS MARKED. MAIN DECK COMPARTMENT AT STATION 1671 X= -8.5 SEAT TRACK CORROSION REMOVED AND FOUND TO EXCEED LIMIT, AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CORRODED SEAT TRSDR FDEA202010022394Seat Track · corrodedMAIN DECK COMPARTMENT, SEAT TRACK AT STATION 1671 X=8.5 FOUND CORROSION, AS MARKED. MAIN DECK COMPARTMENT AT STATION 1671 X=8.5 SEAT TRACK CORROSION REMOVED AND FOUND TO EXCEED LIMIT, AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CORRODED SEAT TRACK SDR FDEA202010012381Seat Track · corrodedMAIN DECK COMPARTMENT, SEAT TRACK AT STATION 5-63 X=8.5 FOUND CORROSION, AS MARKED. MAIN DECK COMPARTMENT AT STATION 5-63 X=8.5 SEAT TRACK EXFOLIATED AND FOUND TO EXCEED LIMIT, AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CORRODED SEAT TRACK REPAIRESDR FDEA202010012380Seat Track · corrodedMAIN DECK COMPARTMENT, SEAT TRACK AT STATION 1358 X=8.5 FOUND CORROSION, AS MARKED. MAIN DECK COMPARTMENT STATION 1358 LEFT X=8.5 SEAT TRACK CORROSION. REMOVED AND FOUND TO EXCEED LIMIT, AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CORRODED SEAT TRSDR FDEA202010012383Seat Track · corrodedMAIN DECK COMPARTMENT, SEAT TRACK AT STATION 1199 X= -8.5 FOUND CORROSION, AS MARKED. MAIN DECK COMPARTMENT, STATION 1199 X= -8.5 SEAT TRACK CORROSION REMOVED AND FOUND TO EXCEED LIMIT, AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CORRODED SEAT TRACSDR FDEA202010012382Seat Track · corrodedMAIN DECK COMPARTMENT, SEAT TRACK AT STATION 1525 X=8.5 FOUND CORROSION, AS MARKED. MAIN DECK COMPARTMENT STATION 1525 X=8.5 SEAT TRACK CORROSION REMOVED AND FOUND TO EXCEED LIMIT, AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CORRODED SEAT TRACK REPSDR FDEA202010012378Seat Track · corrodedMAIN DECK COMPARTMENT, SEAT TRACK AT STATION 1381 X=27.5 FOUND CORROSION, AS MARKED. MAIN DECK COMPARTMENT STATION 1381 X=27.5 LEFT SEAT TRACK CORROSION REMOVED AND FOUND TO EXCEED LIMIT, AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CORRODED SEAT TRSDR FDEA202010012379Seat Track · corrodedMAIN DECK COMPARTMENT, SEAT TRACK AT STATION 1388 X= -8.5 FOUND CORROSION, AS MARKED. MAIN DECK COMPARTMENT STATION 1388 RIGHT X= -8.5 SEAT TRACK CORROSION REMOVED AND FOUND TO EXCEED LIMIT, AS PER SRM 53-00-52-1A FIGURE 101. ALLOWABLE DAMAGE 1. CORRODED SESDR FDEA202009302359Web · crackedCENTER CARGO STATION 1841 APPROXIMATELY X= -3 FOUND WEBBING PUNCTURED. CENTER CARGO STATION 1841 APPROXIMATELY X=0 TO X= -23 REPAIR CARRIED OUT, PER MD-11 SRM 53-00-00-2R FIGURE 211. REPAIR CLASSIFIED AS MAJOR, PER GMM 6-2-100.SDR FDEA202006120736Control Unit · malfunctionedGEN 3 ON MEL. AT GEAR DOWN GOT "GEN 1 OFF" A/C WENT ON EMERGENCY POWER LOST ALL ASSOCIATED SYSTEMS. GEN 1 CAME BACK ONLINE EXITING THE RUNWAY. PERFORMED T/S AND REPL EPCU IAW AMM 24-08-01-4 REF WRI: 24-00 4955.SDR FDEA2020041320736Generator · malfunctionedGEN 3 ON MEL. AT GEAR DOWN GOT "GEN 1 OFF" A/C WENT ON EMERGENCY POWER LOST ALL ASSOCIATED SYSTEMS. GEN 1 CAME BACK ONLINE EXITING THE RUNWAY.SDR FDEA201909162255Smoke Detector · false activationPDIS 592 26-12 3896 14SEP19 MEM FACT U LOGPAGES:2863413 CABIN SMOKE DETECT @ 9000 FT SHGN 14SEP19 11:38 MEM U PERFORMED GVI OF CARGO SMOKE DETORS, ALL DISPLAYED GREEN. PERFORMED OPERATIONAL TEST OF CARGO SMOKE SYSTEM, REF AMM 26-15-1-5. NO SDR FDEA201907251688Bracket · failedPDIS 592 32-12 3641 25JUL19 MEM OPEN U LOGPAGES:3095639 AFTER T/O GEAR SHOWED LEFT MAIN PRIMARY/SECONDARY INDICATION UNSAFE. CYCLED GEAR AND GOT GOOD DOWN INDICATION. AFTER FOLLOWING QRH, CYCLED GEAR AND PROBLEM REMAINED. ALL INDICATIONS FOR GEASDR FDEA201905030991Shutoff Valve · failedPDIS 592 29-02 3353 03MAY19 IND FACT U LOGPAGES:3094152 DURING CLIMB OUT TO FL 390 WE RECIVED A LVL 1 HYD 3 ELEV OFF ALERT NO.3 QUANTITY WAS 4.5.W/3-2 NRMP INOP. DURING CRUISE QTY LEVEL WENT TO 4.1. DESCENT INTO IND WE CONFIGURED W/FLAPS 15 ANDSDR FDEA201901290222Washer · wornCENTER LANDING GEAR RT TRUNNION PIN NUT HAS GAP BETWEEN WASHER AND NUT. REMOVED AND REPLACED CENTER LANDING GEAR RT TRUNNION PIN WASHER AND NUT IAW DAC DWG NYG 6210 VIEW G-G.SDR FDEA201811283392Rod · shearedCOMPRESSOR STALL CLIMBING OUT OF 12,000 FT NR 1 ENG FL330 2ND COMPRESSOR STALL. WHILE ON DESCENT FOR LANDING OBSERVED THE FOLLOWING AT 6000 NR 1 EGT 512 EGT, 85% N1, NR 2 38 EGT, 77 %, NR 3 351 EGT 77%. CREW DEBRIEF, NR 2 ENG EGT WAS 358 NOT 38. NR 1 ENG THROSDR FDEA201811193304Transmitter · false activationTIRE FAIL AFTER GEAR RETRACTION. REMOVED AND REPLACE TIRE PRESSURE TRANSMITTER. OK FOR SERIVCESDR FDEA201811143215Switch · stuckDURING FLIGHT, LEFT SIDE CREW ENTRANCE DOOR SLIDE/RAFT INSIDE LIGHT CAME ON FOR REMAINING OF FLIGHT. FOUND LIGHT SWITCH STUCK IN. REMOVED SWITCH AND READJUSTED SWITCH, OPS CHECKS GOOD.SDR FDEA2018101602832Floor Support · corrodedMAIN DECK AFT FLOOR SUPPORT AT STA 1887-2007 X= -2 FOUND CORROSION ON FLANGE AT STA 1950 AS MARKED MAIN DECK AFT FLOOR SUPPORT AT STA 1887 TO STA 2007, X= -2 CORROSION ON FLOOR SUPPORT FLANGE AT STA 1950, X= -2 REMOVED AND FOUND TO EXCEED LIMIT AS PER SRM 53-0SDR FDEA2018101602831Floor Support · corrodedMAIN DECK AFT FLOOR SUPPORT AT STA 1887-2007 X= -2 FOUND CORROSION ON FLANGE AT STA 1970 AS MARKED MAIN DECK AFT FLOOR SUPPORT AT STA 1887 TO STA 2007, X= -2 CORROSION ON FLOOR SUPPORT FLANGE AT STA 1970, X= -2 REMOVED AND FOUND TO EXCEED LIMIT AS PER SRM 53-0SDR FDEA2018101602830Floor Support · corrodedMAIN DECK AFT FLOOR SUPPORT AT STA 1887-2007 X= -2 FOUND CORROSION ON FLANGE AT STA 1988 AS MARKED MAIN DECK AFT FLOOR SUPPORT AT STA 1887 TO STA 2007, X= -2 CORROSION ON FLOOR SUPPORT FLANGE AT STA 1988, X= -2 REMOVED AND FOUND TO EXCEED LIMIT AS PER SRM 53- SDR FDEA201810092819Floor Support · corrodedMAIN DECK AFT FLOOR SUPPORT AT STA 1887-2007 X= 2 FOUND CORROSION ON FLANGE AT STA 1929 AS MARKED. MAIN DECK AFT FLOOR SUPPORT AT STA 1887-2007 X= 2, CORROSION ON FLOOR SUPPORT FLANGE AT STA 1929 REMOVED AND FOUND TO EXCEED LIMIT PER SRM 53-00-00-2R FIGURE 206SDR FDEA201810092817Floor Support · corrodedMAIN DECK AFT FLOOR SUPPORT AT STA 1887-2007 X= 2 FOUND CORROSION ON FLANGE AT STA 1895 AS MARKED. MAIN DECK AFT FLOOR SUPPORT AT STA 1887-2007 X= 2, CORROSION ON FLOOR SUPPORT FLANGE AT STA 1895 REMOVED AND FOUND TO EXCEED LIMIT PER SRM 53-00-00-2R FIGURE 206SDR FDEA201810092816Bushing · corrodedRIGHT WING INBD FLAP OUTBD HINGE (WING SIDE) ACTUATOR ATTACHED OUTBD LUG HOLE FOUND CORROSION. CORROSION REWORKED AND FOUND WITHIN LIMIT AS PER CMM 57-44-07. REPAIR BUSHING FABRICATED AND INSTALLED AS PER CMM 57-44-07 AND EA 1-5750-T0332063 B PART 1. REPAIR CLSDR FDEA201810092815Bushing · corrodedRIGHT WING INBD FLAP OUTBD HINGE (WING SIDE) ACTUATOR ATTACHED INBD LUG HOLE FOUND CORROSION. CORROSION REWORKED AND FOUND WITHIN LIMIT AS PER CMM 57-44-07. REPAIR BUSHING FABRICATED AND INSTALLED AS PER CMM 57-44-07 AND EA 1-5750-T0332063 B PART 1. REPAIR CLASDR FDEA201810092814Bushing · corrodedLEFT WING INBD FLAP OUTBD HINGE (WING SIDE) ACTUATOR ATTACHED OUTBD HOLE BORE FOUND CORROSION. CORROSION REWORKED AND FOUND WITHIN LIMIT AS PER CMM 57-44-07. REPAIR BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER CMM 57-44-07 AND EA 1-5750-T0332062 A PARTSDR FDEA201810092813Bushing · corrodedLEFT WING INBD FLAP OUTBD HINGE (WING SIDE) ACTUATOR ATTACHED INBD HOLE BORE FOUND CORROSION. REWORKED AND FOUND WITHIN LIMIT AS PER CMM 57-44-07. REPAIR BUSHING FABRICATED AND INSTALLED AS PER CMM 57-44-07 AND EA 1-5750-T0332062 A PART 1. REPAIR CLASSIFIED ASSDR FDEA201810042776Hinge Bracket · corrodedRIGHT WING OUTBOARD FLAP OUTBOARD HINGE (WING SIDE) BARREL NUT HOLE SURFACE FOUND CORROSION. CORROSION REWORKED AND FOUND BEYOND REWORK LIMIT AS PER CMM57-44-09. NEW REPAIR SHIM FABRICATED AND INSTALLED PER CMM57-44-09 AND EA NR 1-5750-73336C PT 3 STEP 1. REPASDR FDEA201809302746Support Frame · corrodedDURING REPLACEMENT OF RT MLG RETRACT SUPPORT FRAME LOWER TWO MOUNT BOLT PLI WASHER FOUND BOLT HOLE OF SUPPORT FRAME CORROSION. CORROSION REWORKED, FOUND EXCEEDED LIMIT PER SRM 57-20-14-2R PARA 4C STEP (1)(A)(1) REPAIR 1. NEW REPAIR BUSHING FABRICATED AND INSSDR FDEA201809302749Support Frame · corrodedDURING REPLACEMENT OF LT MLG RETRACT SUPPORT FRAME LOWER FWD MOUNT BOLT PLI WASHER, FOUND BOLT HOLE OF SUPPORT FRAME CORROSION. CORROSION REWORKED AND FOUND EXCEEDED LIMIT PER SRM 57-20-14-2R PARA 4C STEP (1) (A)(1) REPAIR 1. REPAIR BUSHING FABRICATED AND INSTSDR FDEA201809302748Support Frame · corrodedDURING REPLACEMENT OF RT MLG RETRACT SUPPORT FRAME LOWER AFT MOUNT BOLT PLI WASHER, FOUND BOLT HOLE OF SUPPORT FRAME CORROSION. CORROSION REWORKED AND FOUND EXCEEDED LIMIT PER SRM 57-20-14-2R PARA 4C STEP (1) (A)(1) REPAIR 1. REPAIR BUSHING FABRICATED AND INSTSDR FDEA201809302747Support Frame · corrodedAFTER REMOVED RT MLG RETRACT SUPPORT FRAME FOR REPAIR, FOUND UPPER AFT BOLT HOLE OF SUPPORT FRAME CORROSION. CORROSION REWORKED AND FOUND EXCEEDED LIMIT PER SRM 57-20-14-2R PARA 4C STEP (1)(A)(1) REPAIR 1. REPAIR BUSHING FABRICATED AND INSTALLED PER EA 1-5740-SDR FDEA201809252705Bracket · corrodedRIGHT WING OUTBD FLAP INBD (WING SIDE) CLEVIS FITTING HOLE BORE FOUND CORROSION. CORROSION REWORKED AND FOUND EXCEEDED LIMIT PER CMM57-44-16. OVERSIZED BUSHING AND REPAIR WASHER FABRICATED AND INSTALLED PER CMM57-44-16 AND EA 1-5740-130969A PT 2 STEPS 2, 2A SDR FDEA201809252704Hinge Bracket · corrodedRIGHT WING OUTBD FLAP OUTBD HINGE (WING SIDE) FWD MOUNT INBD HOLE BORE FOUND CORROSION. HOLE NR 6 CORROSION REWORKED AND FOUND EXCEEDED LIMIT PER CMM57-44-09. OVERSIZED BUSHING FABRICATED AND INSTALLED PER CMM57-44-09 AND EA 1-5750-73336C PT 3 STEP 1. REPAIR CSDR FDEA201809252703Hinge Bracket · corrodedRIGHT WING OUTBD FLAP OUTBD HINGE (WING SIDE) ACTUATOR ATTACHED OUTBD LUG HOLE FOUND CORROSION. HOLE NR 8 CORROSION REWORKED AND FOUND EXCEEDED LIMIT PER CMM57-44-09. OVERSIZED BUSHING FABRICATED AND INSTALLED PER CMM57-44-09 AND EA 1-5750-73336C PT 3 STEP 1. SDR FDEA201809252702Hinge Bracket · corrodedRIGHT WING OUTBD FLAP OUTBD HINGE (WING SIDE) ACTUATOR ATTACHED INBD LUG HOLE FOUND CORROSION. HOLE NR 8 CORROSION REWORKED FOUND EXCEEDED LIMIT PER CMM57-44-09. OVERSIZED BUSHING FABRICATED AND INSTALLED PER CMM57-44-09 AND EA 1-5750-73336C PT 3 STEP 1. REPSDR FDEA201809252701Hinge Bracket · corrodedRIGHT WING OUTBD FLAP OUTBD HINGE (WING SIDE) LOWER MOUNT OUTBD HOLE BORE FOUND CORROSION. HOLE NR 3 CORROSION REWORKED AND FOUND EXCEEDED LIMIT PER CMM57-44-09. SHOULDER BUSHING FABRICATED AND INSTALLED PER CMM57-44-09 AND EA 1-5750-73336C PT 3 STEP 1. REPASDR FDEA201809252700Hinge Bracket · corrodedRIGHT WING OUTBD FLAP OUTBD HINGE (WING SIDE) LOWER MOUNT INBD HOLE BORE FOUND CORROSION. HOLE NR 3 CORROSION REWORKED AND FOUND EXCEEDED LIMIT PER CMM57-44-09. SHOULDER BUSHING FABRICATED AND INSTALLED PER CMM57-44-09 AND EA 1-5750-73336C PT 3 STEP 1. REPAIR SDR FDEA201809252699Hinge Bracket · corrodedRIGHT WING OUTBD FLAP OUTBD HINGE (WING SIDE) PIVOT HOLE BORE FOUND CORROSION. HOLE NR 4 CORROSION REWORKED AND FOUND EXCEEDED LIMIT PER CMM 57-44-09. OVERSIZED BUSHING FABRICATED AND INSTALLED PER CMM57-44-09 AND EA 1-5750-73336C PT 3 STEP 1. REPAIR CLASSIFIESDR FDEA201809252698Hinge Bracket · corrodedRIGHT WING OUTBD FLAP INBD HINGE (WING SIDE) ACTUATOR ATTACHED INBD LUG HOLE SURFACE FOUND CORROSION. CORROSION REWORKED AND FOUND EXCEEDED LIMIT PER CMM57-44-08. REPAIR EVALUATED FOUND ACTUATOR ATTACHED I/B LUG SURFACE REMAINING THICKNESS 0.317" ACCEPTED PER SDR FDEA201809252697Hinge Bracket · corrodedRIGHT WING OUTBD FLAP INBD HINGE (WING SIDE) ACTUATOR ATTACHED OUTBD LUG HOLE FOUND CORROSION. HOLE NR 8 CORROSION REWORKED AND FOUND EXCEEDED LIMIT PER CMM57-44-08. NEW REPAIR BUSHING FABRICATED AND INSTALLED PER CMM57-44-08 AND EA 1-5750-73333C PT 3 STEP 1. SDR FDEA201809252696Hinge Bracket · corrodedRIGHT WING OUTBD FLAP INBD HINGE (WING SIDE) ACTUATOR ATTACHED INBD LUG HOLE FOUND CORROSION. HOLE NR 8 CORROSION REWORKED AND FOUND EXCEEDED LIMIT PER CMM57-44-08. NEW REPAIR BUSHING FABRICATED AND INSTALLED PER CMM57-44-08 AND EA 1-5750-73333C PT 3 STEP 1. ESDR FDEA201809252695Hinge Bracket · corrodedRIGHT WING OUTBD FLAP INBD HINGE (WING SIDE) FWD MOUNT OUTBD HOLE BORE FOUND CORROSION. NR 6 HOLE CORROSION REWORKED AND FOUND EXCEEDED LIMIT PER CMM57-44-08. NEW REPAIR BUSHING FABRICATED AND INSTALLED PER CMM57-44-08 & EA 1-5750-73333C PT 3 STEP 1. EO 1-5750
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