N529FE
Service difficulty reports · 240
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 = 'N529FE' 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 = 'N529FE' 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 FDEA201907301755Seat Track · corrodedMAIN DECK FLOOR SEAT TRACK AT STATION 1441 X = 8.5 FOUND CORROSION . MAIN DECK FLOOR SEAT TRACK AT STATION 1441 X = 8.5 , CORROSION REMOVED AND FOUND TO EXCEED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1 . CORRODED SEAT TRACK REPAIREDSDR FDEA20190731753Seat Track · damagedMAIN DECK FLOOR SEAT TRACK AT STATION 1282 X = - 47.5 FOUND CROWN DAMAGED . MAIN DECK FLOOR SEAT TRACK AT STATION 1282 X = - 47.5 , DAMAGED CROWN EDGE BLEND OUT AND FOUND TO EXCEED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1 . CROWN DAMAGED SDR FDEA2019081521737Trunnion · crackedNOSE LANDING GEAR WHEEL WELL LEFT TRUNNION FITTING SUSPECTED CRACKED AT BS 595, REPAIRED IAW SRM 53-10-14-2R, FIGURE 202, REPAIR 2. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201905171092Power Supply · inoperativeMDIS 529 33-50 6878 17MAY19 MEM FACT U DURING EMERGENCY LIGHT TEST, RECIEVED EMER BATT LOW (1). R/I 17MAY19 17:32 MEM U REASON CODE : PREMATURE REMOVAL/INSTALLATION OFF MPN: 60-4411-5 POS: ONL SRL: 0163 TAG NBR: 4G9021 ON MPN: 60-4411-5 CPN: 330SDR FDEA2019032200697Strut · crackedQC DETECTED A CRACK WHILE INSPECTING THE LEFT MAIN GEAR AND THE WORK CARD IS CALLING FOR A GEAR CHANGE. REPLACED LH MLG STRUTSDR FDEA201901010003Slide · unsecureL1 DOOR EVACUATION SLIDE/RAFT FELL OUT. INSTALLED L1 DOOR EVAC SLIDE/RAFT REF AMM 25-61-15-4. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE.SDR FDEA201811303395Steering Sys · malfunctionedNOSEWHEEL STEERING ONLY WAS APPROX. 50% EFFECTIVE. TILLER WOULD GO TO FULL THROW LEFT OR RIGHT BUT NOSEWHEEL WOULD ONLY MAKE A GRADUAL TURN - MUCH TO LARGE OF A RADIUS - WITHOUT STEPPING ON INBOARD BRAKE. NOSE STRUT IS EXTENDED MORE THAN NORMAL ACCORDING SDR FDEA2018081412014Pressure Switch · failedLEVEL 3 ALERT FOR THE NR 2 ENGINE ANTI-ICE DUCT FAILURE, COMPLIED WITH QRH. REMOVED AND REPLACED THE NR 2 ENGINE ANTI- ICE VALVE IAW AMM 30-22-01, AND THE PRESSURE SWITCH IAW AMM 30-22-02. THE NR 2 ENGINE ANTI-ICE SYSTEM OPERATED NORMAL AND NO LEAKS FOUND SDR FDEA201806271586Duct · leakingRECIEVED A NR 2 ENGINE A-DUCT WARNING, DURING CLIMBOUT, FOLLOWED SHORTLY BY A LEVEL 1 NR 2 ENGINE ANT-ICE OFF ALERT. LANDED AT NEAREST SUITABLE AIRPORT DUE TO WARNINGS. NO ENGINE EXCEEDANCES DURING THE NR 2 ENGINE WINDMILLING AND SHUTDOWN. INSTALLED A SSDR FDEA201806051398Tire · blownCLIMBING OUT OF CDG, TIRE PRESS LO ALERT CONFIG PAGE SHOWED NR 5 TIRE PRESS DECREASING ALSO NR 6 WAS AMBER BUT NOT DECREASING. LATER TIRE FAIL ALERT ON NR 5 WHEN PRESS WENT BELOW 50 PSI. AFTER NR 5 PRESS WENT TO 0 PSI , NR 5 TIRE DISAPPEARED FROM DISPLAY. NR 6SDR FDEA201712243442Cable · frozenENROUTE, RUDDER PEDALS AND TRIM WHEEL BECAME FROZEN/LOCKED. UNUSABLE UNTIL TAT REACHED 10 DEGREES. OPENED PANEL 364AR AND REMOVED ABOUT 1 INCH OF POOLED WATER INSIDE COMPARTMENT. CLEANED AND LUBRICATED BOTH TRIM AND RUDDER CABLES INSIDE COMPARTMENT IAW AMM SDR FDEA201708302412Control Valve · failedAFTER TAKE OFF, RECEIVED A LEVEL 2 FLAP DISAGREE. MATCHED FLAPS BACK TO 10'. RAN QRH INBOARD FLAPS WOULD NOT MOVED PAST 10'. MADE A FLAPS 10'. LANDED AT THE NEAREST SUITABLE AIRPORT. INSTALLED A NEW INBOARD WING FLAP CONTROL VALVE IAW AMM 27-52-03-4. PERSDR FDEA201707141936Skin · crackedDURING AN HFEC INSPECTION, FOUND TWO FASTENER HOLES 31 AND 34 WITH CRACK INDICATIONS, AT THE RIGHT WING LOWER PANEL OUTER WING ACCESS DOOR AT XORS 696.730. REPAIRED IAW SRM 57-20-02-2R, FIG 201, REPAIR 5. REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201707141935Skin · crackedDURING HFEC INSPECTION, FOUND ONE FASTENER HOLE 31 HAD A CRACK INDICATION AT RIGHT WING LOWER PANEL OUTER WING ACCESS DOOR AT XORS 696.730. REPAIRED IAW SRM 57-20-02-2R, FIG. 201, REPAIR 5. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201707121920Seat Track · damagedMAIN DECK SEAT TRACK AT BS 710, LBL 75.25 CROWN FOUND DAMAGED. REPAIRED IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201707121933Support · crackedLEFT WING LEADING EDGE LOWER SURFACE SUPPORT FORMER AT XOS 1084 FOUND CRACKED. REMOVED IAW SRM 51-31-01-0G. A NEW SUPPORT FORMER FABRICATED IAW DRAWING ARB2920, REV BB, AND INSTALLED IAW SRM 51-31-01-0G. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201707121924Seat Track · corrodedMAIN DECK SEAT TRACK AT BS 1671, RBL 27.5 FOUND CORRODED. REPAIRED IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201707121922Seat Track · corrodedMAIN DECK SEAT TRACK AT BS 1169, LBL 8.5 FOUND CORRODED. REPAIRED IAW SRM 53-00-52-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201707121921Seat Track · corrodedMAIN DECK SEAT TRACK AT STATION 5-75, RBL 47.5 FOUND CORRODED. REPAIRED IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201707121919Seat Track · damagedMAIN DECK SEAT TRACK AT BS 795, LBL 75.25 CROWN FOUND DAMAGED. REPAIRED IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201707121923Seat Track · corrodedMAIN DECK FLOOR SEAT TRACK AT BS 1451, RBL 8.5 FOUND CORRODED. REPAIRED IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201707111912Skin · crackedDURING HFEC INSPECTION, FOUND A CRACK ON THE RIGHT WING FIXED LEADING EDGE SKIN, APPROX. 1/2 INCH IN LENGTH AT CORNER NR 11 FUEL ACCESS DOOR FORWARD INBOARD CORNER. REPAIRED IAW SRM 57-40-01-2R, FIG 201, REPAIR 18. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.SDR FDEA201707111911Former · crackedRIGHT WING-FIXED LEADING EDGE FORMER ASSEMBLY AT XOS 801 FOUND CRACKED. THE FORMER WAS REMOVED IAW SRM 51-31-01-0G. A NEW FORMER FABRICATED IAW DRAWING ARB2922 REV B, AND INSTALLED IAW SRM 51-31-01-0G. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.SDR FDEA201707111910Doubler · crackedLEFT WING FIXED LEADING EDGE RIB DOUBLER AT XOS 667 FOUND CRACKED. THE RIB DOUBLER WAS REMOVED IAW SRM 51-31-01-0G . A NEW DOUBLER WAS FABRICATED IAW DRAWING ARB3954, REV K, AND INSTALLED IAW SRM 51-31-01-0G, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201707111909Doubler · crackedLEFT WING FIXED LEADING EDGE RIB DOUBLER AT XOS 789 FOUND CRACKED. THE RIB DOUBLER WAS REMOVED IAW SRM 51-31-01-0G. A NEW DOUBLER WAS FABRICATED IAW DRAWING ARB3954 REV K, AND INSTALLED IAW SRM 51-31-01-0G. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100SDR FDEA201707111908Seat Track · damagedMAIN DECK SEAT TRACK AT BS 1306, RBL 75.25, FOUND THE CROWN DAMAGED. REPLACED FROM BS 1263 TO 1390, IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201606011784Longeron · corrodedLOWER FUSELAGE AFT OF LOWER BEACON, RIVET HEAD POPPED & SKIN BULGING. REPLACE FACTORY SPLICE & LONGERON.SDR FDEA201604141223Cover · looseR1 DOOR EMER EXIT LIGHT COVER, TAB IS BROKEN ON BACK OF COVER. REMOVED AND REPLACED R1 DOOR EMERGENCY EXIT LIGHT COVER IN REF AMM 33-27-05-4-0.SDR FDEA201509232918Valve · malfunctionedDURING CLIMB OUT WE GOT A LEVEL 1 ENG 2 ANTI-ICE OFF. THE MEL WE WERE OPERATING UNDER HAD NR 2 ENG ANTI-ICE VLV SECURED OPEN, THIS INDICATED A POSSIBLE PNEUMATIC LEAK IN NR 2 ANTI-ICE DUCT. DIVERTED & LANDED WITHOUT INCIDENT. R & R NR 2 INLET COWL ANTI-ICE SDR FDEA201508282716Brake Sys · malfunctionedTAXI OUT BRAKING RESPONSE GOOD & NORMAL, AFTER FIRST OFFICER LANDING USING MEDIUM AUTO BRAKES, INITIAL BRAKE APPLICATION WAS VERY INEFFECTIVE UNTIL APPLIED HEAVY PRESS TO BEGIN SLOWING THE ACFT FROM 20 KTS GND SPEED. INSPECTED ALL MAIN & CTR LG BRAKES IAW AMSDR FDEA201508132542Doubler · crackedRIGHT WING LE COMPARTMENT AT APPROX STATION XOS 789, FOUND WITH CONTOUR LONGITUDINAL FRAME DOUBLER CRACKED. LONGITUDINAL FRAME DOUBLER REMOVED IAW SRM 51-31-01-0G, NEW FRAME DOUBLER FABRICATED IAW DWG ARB3954 REVISION K. NEW FRAME DOUBLER INSTALLED IAW SRM 5SDR FDEA201508122536Doubler · crackedLEFT WING LE AT APPROX STATION XOS 602, FOUND PANEL SUPPORT FRAME DOUBLER WITH SIGNS OF CRACK. REMOVED IAW SRM 51-31-01-0G, NEW FRAME DOUBLER FABRICATED IAW DWG ARB2933 REVISION T SHEET 2. NEW DOUBLER INSTALLED IAW SRM 51-31-01-0G. REPAIR CLASSIFIED MAJOR ISDR FDEA201508172576Hinge · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE, UPPER MOUNT INBD HOLE, SURFACE CORROSION. REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-09. EXISTING THICKNESS 0.711", MATERIAL REMOVED 0.006", REMAINING THICKNESS 0.705", MINIMUM ALLOWABLE THICKNESS 0.720". RESDR FDEA201508092519Hinge · corrodedRIGHT WING, FLAP SIDE, OTBD FLAP INBD HINGE, PIVOT HOLE BORE FOUND CORROSIONS. CORROSION REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-52-04. EXISTING DIAMETER =1.150", FINAL DIAMETER =1.158", MAXIMUM ALLOWABLE DIAMETER =1.150". REPAIR ACCOMPLISHED IAW EA 1- 5SDR FDEA201508092518Hinge · corrodedLEFT WING, FLAP SIDE, OTBD FLAP, INBD HINGE, PIVOT HOLE BORE FOUND CORROSIONS. CORROSION REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-52-04. EXISTING DIAMETER =1.149", FINAL DIAMETER =1.190", MAXIMUM ALLOWABLE DIAMETER =1.150". REPAIR ACCOMPLISHED IAW EA 1- SDR FDEA201508082516Hinge · corrodedRIGHT WING, FLAP SIDE, INBD FLAP OTBD HINGE, OTBD PIVOT HOLE BORE FOUND CORROSIONS. CORROSION REWORKED & FOUND EXCEEDED LIMIT IAW CMM 57-52-03. EXISTING DIAMETER = 1.256", FINAL DIAMETER =1.260", MAXIMUM ALLOWABLE DIAMETER =1.220". REPAIR ACCOMPLISHED IAW ESDR FDEA201508082515Hinge · corrodedRIGHT WING, FLAP SIDE, INBD FLAP OTBD HINGE, INBD PIVOT HOLE BORE FOUND CORROSIONS. CORROSION REWORKED & FOUND EXCEEDED LIMIT IAW CMM 57-52-03. EXISTING DIAMETER = 1.256", FINAL DIAMETER =1.260", MAXIMUM ALLOWABLE DIAMETER =1.220". REPAIR ACCOMPLISHED IAW SDR FDEA201508082514Hinge · corrodedLEFT WING, FLAP SIDE, INBD FLAP OTBD HINGE, OTBD PIVOT HOLE BORE FOUND CORROSIONS. CORROSION REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-52-03. EXISTING DIAMETER = 1.328", FINAL DIAMETER =1.338", MAXIMUM ALLOWABLE DIAMETER =1.220". REPAIR ACCOMPLISHED IAW EA SDR FDEA201508072509Hinge · corrodedRIGHT WING, WING SIDE, OTBD FLAP INBD HINGE, OTBD ACTUATOR HOLE BORE FOUND CORROSIONS. ASSEMBLY R & R IAW AMM 57-53-01-4. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.SDR FDEA201508072508Hinge · corrodedRIGHT WING, WING SIDE, OTBD FLAP INBD HINGE, LOWER MOUNT OTBD HOLE BORE FOUND CORROSIONS. ASSEMBLY R & R IAW AMM 57-53-01-4. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.SDR FDEA201508072507Hinge · corrodedRIGHT WING, WING SIDE, OTBD FLAP INBD HINGE, LOWER MOUNT OTBD HOLE BORE FOUND CORROSIONS. ASSEMBLY R & R IAW AMM 57-53-01-4. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.SDR FDEA201508072506Hinge · corrodedRIGHT WING, WING SIDE, OTBD FLAP INBD HINGE, LOWER MOUNT INBD HOLE BORE FOUND CORROSIONS. ASSEMBLY R & R IAW AMM 57-53-01-4. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.SDR FDEA201508072505Hinge · corrodedRIGHT WING, WING SIDE, OTBD FLAP INBD HINGE, SIDE LOAD FITTING BARREL NUT HOLE SPOT FACE FOUND CORROSIONS. ASSEMBLY R & R IAW AMM 57-53-01-4. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.SDR FDEA201508072504Hinge · corrodedRIGHT WING, WING SIDE, OTBD FLAP INBD HINGE, PIVOT HOLE BORE FOUND CORROSIONS. ASSEMBLY R & R IAW AMM 57-53-01-4. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.SDR FDEA201508072503Seat Track · damagedMAIN DECK FLOOR SEAT TRACK AT BS 750 X= 8 FOUND CROWN DAMAGED. REPAIRED IAW SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.SDR FDEA201508072502Hinge Bracket · corrodedRIGHT WING, WING SIDE, OTBD FLAP OTBD HINGE, BARREL NUT HOLE SPOT FACE FOUND CORRODED. CORROSION REMOVED, FOUND WITHIN LIMITS. REPAIR CLASSIFIED MINOR IAW GMM 6-2-100.SDR FDEA201508072501Hinge · corrodedRIGHT WING, WING SIDE, OTBD FLAP OTBD HINGE, LOWER MOUNT OTBD HOLE BORE FOUND CORROSIONS. CORROSION AT HOLE 3, REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-09. EXISTING HOLE DIAMETER = 0.580", FINAL HOLE DIAMETER =0.595", MAXIMUM ALLOWABLE HOLE DIAMETER =0.5SDR FDEA201508072500Hinge · corrodedRIGHT WING, WING SIDE, OTBD FLAP OTBD HINGE, LOWER MOUNT INBD HOLE BORE FOUND CORROSIONS. CORROSION AT HOLE NR 3, REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-09. EXISTING HOLE DIAMETER = 0.580", FINAL HOLE DIAMETER =0.595", MAXIMUM ALLOWABLE HOLE DIAMETER =SDR FDEA201508072499Hinge · corrodedLEFT WING, WING SIDE, OTBD FLAP OTBD HINGE, PIVOT HOLE BORE FOUND CORROSIONS. CORROSION REWORKED & FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING HOLE DIAMETER =2.3105", FINAL HOLE DIAMETER =2.334", MAXIMUM ALLOWABLE HOLE DIAMETER =2.3135". REPAIR BUSHING SDR FDEA201508072498Skin · corrodedLEFT WING LE DROOP PANEL, UPPER SURFACE SKIN FOUND CRACKED FROM STATION XDLE 329.774 - XDLE 325.114. REPAIRED IAW SRM 57-40-01-2R FIGURE 201 REPAIR 5. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.
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