N525FE
Service difficulty reports · 261
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 = 'N525FE' 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 = 'N525FE' 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 FDEA201506262088Light · inoperativeDURING EMER LT TEST, FOUND L1 DOOR JAMB LIGHT INOPERATIVE. RELAMPED, NO HELP. RELAMPED LIGHT ASSY. OPS NORMAL.SDR FDEA201506242089Actuator · malfunctionedWHEN EXTENDING SLATS WITH SYS NR 3 ONLY, THE SLATS ON THE LT WING EXTEND MUCH SLOWER CAUSING A ROLL TO THE RIGHT. R & R LT OTBD SLAT ACTUATOR NR 3 HYD IAW AMM 27-82-02-4. PERFORMED OPERATIONS & LEAK CHECK IAW 27-82-02-4. R & R LT INBD & OTBD SLAT BALANCE RSDR FDEA201506181857Skin · corrodedAFT ACCESSORY COMPARTMENT ZONE 316 INTERIOR RT SIDE AFT HORIZONTAL STAB FILLET AREA LOWER FASTENERS HAVE CORROSION. FURTHER EVALUATION FOUND CORRODED SKIN. REPAIRED CORROSION AREA IAW SRM 53-70-01-2R FIGURE 201.SDR FDEA201506171830Skin · crackedNUMBER 1 PYLON FARING 437CR, PN AUB7555-1, EXTERNAL SKIN HAS APPROX 3" CRACK IN CTR SECTION. IAW EA, ENGINEERING DISPOSITION IS REQUIRED FOR FINDING. FABRICATED FILLER & DOUBLER IAW SRM 54-50-02 REPAIR 9 FIG 201 SHEET 3 OF 4. OK TO INSTALL REPAIR. INSTALLESDR FDEA201506081723Seat Track · damagedMAIN CARGO DECK RBL 57 BS 1590 SEAT TRACK DAMAGED IN TWO PLACES. SMOOTHED AND BLENDED OUT DAMAGE IAW SRM 53-00- 52-1A. FOUND OUT OF LIMITS IAW SRM 53-00-52-1A SHT 1. THE SEAT TRACK WAS REPLACED IAW SRM 53-00-52-2R.SDR FDEA201503140922Panel · damagedL1 DOOR SLIDING CEILING PANEL DAMAGED. SLIDING PANEL FOR THE L1 DOOR DAMAGED & HAS BEEN REMOVED. REPAIRED IAW MM 25-23-23-2.SDR FDEA201411053523Light · inoperativeL1 DOOR TEST LIGHT INOPERATIVE. LAMPED L1 DOOR TEST LIGHT IAW AMM 25-61-04-4. LIGHT OPERATIONS OK.SDR FDEA201311262878Life Vest · missingFIRST OFFICER`S LIFE VEST IS MISSING. INSTALLED NEW LIFE VEST AT FIRST OFFICER'S SEAT LOCATION IAW FX MD11, SERVICE CHECKED ACFT OK FOR FLIGHT.SDR FDEA201310202556Battery · failedEMERGENCY LIGHT BATTERY 1 LOW. R & R BATTERY SUPPLY IAW MM 33-51-01-4, OPS CHECKED NORMAL.SDR FDEA201306301421Structure · corrodedRT WING OTBD FLAP INBD FWD (WING SIDE) HINGE BARREL NUT HOLE SURFACE CORROSION.SDR FDEA201306241384Bulkhead Web · damagedNR 1 PYLON YN 286 BULKHEAD DAMAGED. REPAIRED IAW EA1-5450-81823B PART 2. REPAIR CLASSIFIED MINOR AS PER GMM 6-2-100 REVISION 116.SDR FDEA201306241383Bulkhead Web · damagedNR 1 PYLON YN 286 BULKHEAD DAMAGED. REPAIRED IAW EA 1-5450-81823B PART 2. REPAIR CLASSIFIED MINOR AS PER GMM 6-2-100 REVISION 116SDR FDEA201306241382Bulkhead Web · damagedNR 1 PYLON YN 286 BULKHEAD DAMAGED. REPAIRED.SDR FDEA201306211365Frame · crackedLT WING INBD FLAP INBD FAIRING FRAME, AT YIFH 57 CRACKED. REMOVED AND REPLACED FRAME IAW SRM 51-31-01 REVISION 52 & EO 1-5100-7-5001 B3 PART 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 116SDR FDEA201306211366Floor Skin · misrepairedCOCKPIT FLOOR UNDERNEATH OBSERVER SEAT AT BS 360 MISREPAIRED. REPAIRED IAW SRM 53-10-51 FIGURE 201 REPAIR 1 REVISION 52 & EO 1-5100-7-5001 B3 PART 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 116.SDR FDEA201306201354Frame · misrepairedFUSELAGE FRAME AT BS 1921, LONGERON 51R MISREPAIRED. REPAIRED IAW EA1-5310-T0300934 PART 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 116.SDR FDEA201306201353Skin · misrepairedLEFT WING INBD FLAP BETWEEN XIFH 159.300 TO XIFH 165.300 MISREPAIRED. REPAIRED IAW EA 1-5750-166138. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 116.SDR FDEA201306201352Skin · misrepairedRUDDER SKIN MISREPAIRED. REPAIRED IAW EA 1-5540-T0300978. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 116.SDR FDEA201306201351Skin · misrepairedRUDDER SKIN MISREPAIRED. REPAIRED PER SRM 55-40-01 REPAIR 4 FIGURE 201 REVISION 52 AND EA1-5540-T0300978. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 116.SDR FDEA201306181330Stringer · misrepairedLEFT WING INBD FLAP FAIRING AFT LOWER AREA MISREPAIRED. SRM 51-31-01 REV.52 & EO1-5100-7-5001 B3 PART 1. .REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 116SDR FDEA201306181325Hinge Fitting · corrodedRIGHT WING OTBD FLAP AFT HINGE FWD MOUNT INBD (2A) FOUND WITH CORROSION. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-52-04, REV 76. REPAIR ACCOMPLISHED IAW EA 1-5750-T0300851, PART 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.SDR FDEA201306181318Fitting · corrodedRT WING OTBD FLAP VANE FITTING (F) MOUNTING HOLE FOUND WITH CORROSION. REWORKED AND FOUND EXCEEDED LIMIT IAW SRM 57-50-02, FIG 201, REVISION 52. REPAIR BUSHING FABRICATED IAW SRM 57-50-02, FIG 201, REV 52 AND INSTALLED IAW AMM 27-50-02-04, REV 76.1. RT OTBSDR FDEA201306161311Skin · misrepairedLT WING INBD FLAP SKIN MISREPAIRED. REPAIRED IAW EA 1-5750-166138. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.SDR FDEA201306161309Skin · crackedTEN FASTENER HOLES FOUND CRACK INDICATION DURING OPEN-HOLE HIGH FREQUENCY EDDY CURRENT(HFEC) INSPECTION AT LEFT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN XORS 683.4 AND 713.6. REPAIRED IAW SRM 57-20-02, REPAIR 5, FIG 201, REV 52. REPAIR CLASSIFIED MAJOR ISDR FDEA201306161308Skin · crackedNINE FASTENER HOLES FOUND CRACK INDICATION. DURING OPEN-HOLE HIGH FREQUENCY EDDY CURRENT (HFEC) INSPECTION AT RT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN XORS 683.4 AND 713.6. REPAIRED IAW SRM 57-20-02, REPAIR 5, FIG 201, REV 52. REPAIR CLASSIFIED MAJOR ISDR FDEA201306161307Wedge · delaminatedLEFT WING OTBD FLAP UPPER SURFACE INBD LOWER T/E CORNER DELAMINATED. REPAIRED IAW EA 1-5750-T0300875. REPAIR CLASSIFIED MINOR IAW GMM 6-2-100 REV 116.SDR FDEA201306151302Structure · corrodedRIGHT WING OTBD FLAP, INBD FWD (WING SIDE) HINGE ACTUATOR HOLE INBD BORE CORROSION.SDR FDEA201306151301Structure · corrodedRIGHT WING OTBD FLAP, INBD FWD (WING SIDE) HINGE PIVOT HOLE BORE CORROSION.SDR FDEA201306151300Hinge · corrodedRIGHT WING OTBD FLAP, OTBD FWD (WING SIDE) HINGE PIVOT HOLE CORRODED. REWORKED IAW CMM 57-44-09, REV 76. FOUND OUT OF LIMITS. REPAIRED IAW EA 1-5750-T0300831, PART 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.SDR FDEA201306151299Bulkhead · canningCENTER LANDING GEAR WHEEL WELL-OIL CANNING FOUND AT RT KEEL BEAM WEB , X=31.50, STA.Y=1435, 43" ABOVE FWD DOOR HINGE LINE. OIL CANNING MEASURED 0.228", MAXIMUM ALLOWABLE 0.19". REPAIRED IAW EA 1-5310-T0300744, PART 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100SDR FDEA201306151298Hinge · corrodedLEFT WING OTBD FLAP, OTBD FWD (WING SIDE) HINGE ACTUATOR HOLE OTBD BORE CORRODED. REWORKED AND FOUND EXCEEDED LIMITS IAW CMM 57-44-09, REV 76. REPAIR ACCOMPLISHED IAW EA 1-5750-T0300829, PART 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.SDR FDEA201306151297Hinge · corrodedLEFT WING OTBD FLAP, OTBD FWD (WING SIDE) HINGE ACTUATOR HOLE INBD BORE CORRODED. REWORKED AND FOUND EXCEEDED LIMITS IAW CMM 57-44-09 REV 76. REPAIR ACCOMPLISHED IAW EA 1-5750-T0300829, PART 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.SDR FDEA201306141290Frame · misrepairedMAIN DECK CARGO BS 535, L19LT FRAME MISREPAIRED. REPAIRED IAW SRM 53-20-07, FIG 202, REPAIR 1, REV 52 EO 1-5100-7-5001, B3 PART 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.SDR FDEA201306141289Frame · misrepairedMAIN DECK CARGO BS 535, L24L FRAME MISREPAIRED. REPAIRED IAW SRM 53-20-07, FIG 201, REPAIR 1, REV 52, EO1-5100-7-5001, B3 PART 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.SDR FDEA201306141291Hinge · corrodedLEFT WING OTBD FLAP FWD (WING) HINGE PIVOT HOLE BORE CORROSION. REWORKED AND FOUND EXCEEDED LIMITS IAW CMM 57-44-09, REV 76. REPAIR ACCOMPLISHED IAW EA 1-5750-T0300829, PART 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.SDR FDEA201306141288Support Fitting · crackedDURING HIGH FREQUENCY EDDY CURRENT INSPECTION, OPEN HOLE INSPECTION CARRIED OUT AND FOUND NR 7 LOWER CARGO DOOR FRAME SUPPORT FITTING HOLE "C" WITH CRACK INDICATION AT 12 O'CLOCK POSITION (PLAIN VIEW) AND APPROX 0.080" IN LENGTH. R & R IAW SRM 51-31-01, REV 5SDR FDEA201306141287Support Fitting · crackedDURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION CARRIED OUT AND FOUND NR 4 LOWER CARGO DOOR FRAME SUPPORT FITTING HOLE "D" WITH CRACK INDICATION AT 1 O'CLOCK POSITION AND APPROX 0.085" IN LENGTH. R & R IAW SRM 51-31-01, REV 52 REPAIR CLASSIFIED MAJOR SDR FDEA201306131276Longeron Splice · crackedCENTER CARGO LONGERON SPLICE FITTING FOUND CRACKED AT STA 5-113 TO STA 1541, LONGERON 41RT. LONGERON SPLICE REMOVED IAW SRM 51-33-01, REV 52. NEW SPLICE FABRICATED IAW DWG A5A7115, REVISION D. INSTALLED IAW SRM 51-33-01, REV 52. REPAIR CLASSIFIED MAJOR IAWSDR FDEA201306131275Longeron Splice · crackedCENTER CARGO LONGERON SPLICE FITTING FOUND CRACKED AT STA 5-113 TO STA 1541, LONGERON 39RT. LONGERON SPLICE FABRICATED IAW DWG A5A7114, REV J. R & R SPLICE IAW SRM 51-33-01, REV 52. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.SDR FDEA201306121260Skin · damagedAFT CARGO DOOR FRAME SKIN FOUND WITH CHIPPED AT BS 1960 LONGERON 40 LEFT. REPAIRED IAW SRM 53-00-15 FIGURE 202 REPAIR 8 REVISION 52. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 116SDR FDEA201306121259Skin · crackedLEFT WING L/E SURFACE NR 3 SLAT ANTI-ICE DUCT CUTOUT UPPER AREA CRACKED APPROX 0.25" AT XOS 464. REPAIRED IAW SRM 57-40-01, REPAIR 10, FIG 201, REV 52. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.SDR FDEA201303040494Door · damagedDURING WALK AROUND CHECK, FOUND LT CTR GEAR DOOR MISSING. RT CTR GEAR DOOR TORN. LT CTR GEAR DOOR REMOVED AND REPLACED AS PER AMM32-17-04-4 REV 75.SDR FDEA201302110317Actuator · failed"ON TAKEOFF ROLL AT APPROX 100KTS FELT NOTICEABLE THUD AND LOSS OF THRUST FOLLOWED BY AN ENGINE FAIL LIGHT -ANOTHER ACFT REPORTED FLAMES COMING FROM THE TAIL PIPE ON NR 2 ENGINE ON TAKEOFF -ALL ENGINE INDICATIONS NORMAL AFTER REJECT. NR 2 ENGINE TAILPIPE AND SDR FDEA201208253167Latch · inoperativeEMERGENCY O2 MASK DOOR WILL NOT STAY LATCHED IN LAVATORY. RESET LOCK AND RESECURED PANEL IAW SMP.SDR FDEA201205151810Cylinder · failedLT MAIN LG WOULD NOT RAISE. ( RED LT & UNSAFE ON S/D). JACKED ACFT REF MM 07-11-00-2-0. LT GEAR FAILED TO RETRACT AND LT RETRACT CYLINDER WARM TO THE TOUCH AND BYPASSING. REPLACED LT MLG RETRACT CYLINDER, REF MM 32-33-20-4 AND ALL GEAR OPERATED NORMAL.SDR FDEA201205041740Latch · openOVERHEAD OXYGEN MASK DOOR IN LAVATORY FELL OPEN DURING TAKE OFF ROLL. RESET LATCH RELEASE LEVER AND CLOSED LAVATORY OXYGEN DOOR REF AMM 35-21-07-4. ACFT OK FOR SERVICE.SDR FDEA201107222909Battery · dischargedON PRE-FLIGHT RECEIVED: EMERGENCY POWER TEST FAIL . AFTER BATTERY WAS FULLY CHARGED, PERFORMED EMERGENCY POWER TEST AGAIN IAW AMM 24-34-03-5, TEST PASSED, ACFT OK FOR SERVICE.SDR FDEA201107112634Stiffener · crackedAFT FUSELAGE BULKHEAD STA 2164, CRACK FOUND ON STIFFENER U-ANGLE RT SIDE LOWER ALIGNMENT PIN HOLE AREA. CRACKED STIFFENER REMOVED AND REPLACED WITH REWORKED STIFFENER AS PER SRM 51-35-01 REV 46. STIFFENER REWORKED AS PER DRAWING AJC7001 REV DT. REPAIR CLASSSDR FDEA201107052566Longeron · corrodedUPON REMOVAL OF R3 PLUG DOOR SCUFF PLATE FOR INSPECTION ACCESS FOUND L28R CORRODED AT BS 1273 - 1289.SDR FDEA201012174710Transducer · damagedTAKEOFF IND HAD LT CTR TIRE FAILURE AFTER GEAR RETRACT. ELECTED TO CONTINUE. LANDED WITH CTR GEAR UP. LANDING WEIGHT 398.2 REMOVED HUB CAP AND FOUND TRANSDUCER CONNECTOR PLUG SHEARED OFF. REMOVED AND REPLACED #9 MAIN WHEEL TRANSMISSION UNIT PER
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