N572FE
Service difficulty reports · 258
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 = 'N572FE' 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 = 'N572FE' 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 FDEA201106272444Frame · dentedUPON REMOVAL OF SIDEWALL PANEL, CABIN - LT STA, 1761 L-11 FRAME FOUND DENTED. REPAIRED AS PER SRM 53-00-07 FIG 201 REV 46. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REV 112.SDR FDEA201106272441Frame · dentedCABIN RT STA 1721, L-11 FRAME FOUND DENTED. REPAIRED AS PER SRM 53-00-07 FIG 201 REV 46. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REV 112.SDR FDEA201106272440Frame · dentedCABIN RT STA 1701 L-11, FRAME FOUND DENTED. REPAIRED AS PER SRM 53-00-07 FIG 201 REV 46. REPAIRED CLASSIFIED MAJOR AS PER GMM 6-2-100 REV 112.SDR FDEA201012244746Wire · burnedRT SIDE TURN OFF LIGHT INOP - SCAN LIGHT SEEMS OK. RELEASED FOR SERVICE IAW MEL: 33-43-01 CATEGORY: C EXPIRATION: 31DEC10 "MEL 33-43-01: RT RUNWAY TURNOFF LIGHT - INOP." C/B CHECKS NORMAL , QUICK TURN NO TIME TO WORK THIS TURN. FOUND BOTH ELEC WIRES BURSDR FDEA201006252147Wire Harness · failedAT APPROX 100 KTS TAKEOFF ROLE ENG NR 1 OIL QUANTITY INDICATED 0. TAKEOFF REJECTED AT 118 KTS. QRH PROCEDURES ACCOMPLISHED. RELEASED FOR SERVICE IAW MEL: 79-31-01 CATEGORY: B EXPIRATION: 28JUN10 "MEL 79-31-01: ENG NR 1, OIL QTY INDICATION - INOP. BEFORE EACSDR FDEA200911143956Actuator · leakingODOR OF ENG OIL SMOKE IN COCKPIT. RAN CHECKLISTS AND WAS UNABLE TO DETERMINE SOURCE. DIVERTED. FOUND LT ENG THRUST REVERSER ACTUATOR LEAKING ON DUCTS. REPLACED ACTUATOR IAW MM 78-33-14-4 1. RE-ACTIVATED REG AIR VALVE AND RAN ENG AT HIGH PWR FOR APPROX 15SDR FDEA200911133955Actuator · leakingODOR OF ENG OIL SMOKE IN COCKPIT. RAN CHECKLISTS AND UNABLE TO DETERMINE SOURCE. DIVERTED. RELEASED FOR SERVICE IAW MEL: 36-12-01. CHECKED NR 1, 2 & 3 PACK COALESCER FILTERS. NR 1 FILTER WATER SEPARATOR HAD CONTAMINATION. OPENED NR 1 SYS DUCTS IN CAC & NSDR FDEA200911113925Warning Message · illuminatedDURING T/O ROLL BETWEEN 50-60 KTS RECEIVED ENG OIL FILTER LEVEL 2 ALERT. DO NOT KNOW WHICH ENGINE BECAUSE ALERT WENT OUT AFTER THROTTLES IDLE. REJECTED TAKE-OFF AND RETURNED TO RAMP IAW FIM 79-00-03 NO CONTAMINATION AND FAULT'S FOUND. SYS IS OK. ALL 3 FILTESDR FDEA200907282811Skin · corrodedHORIZONTAL STABILIZER RT UPPER PLANK NR 35R BARREL NUT BORE CORROSION REWORKED, FOUND EXCEEDED EO LIMITATIONS. REPAIRED AS PER EA 1-5510-131624, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REV. 107SDR FDEA200907282810Skin · corrodedHORIZONTAL STABILIZER RT UPPER PLANK NR 34R BARREL NUT BORE SIDEWALL BEARING SURFACE CORROSION REWORKED. FOUND EXCEEDED EO LIMITATIONS. REPAIRED AS PER E.A. 1-5510-131624, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 107.SDR FDEA200907272768Skin · cloggedRT WING - AFTER REMOVAL OF RUBSTRIP AND GANG CHANNEL ON FUEL TANK PANEL CUTOUT NR 639CB, 01 EACH FASTENER HOLE FOUND PLUGGED. REPAIR CARRIED OUT AS PER E.A. 1-5730-132661, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 107.SDR FDEA200907222702Skin · misrepairedEXISTING REPAIR AT RT WING OTBD AILERON UPPER SKIN. EXISTING REPAIR AT RT WING OTBD AILERON UPPER SKIN EVALUATED AND FOUND NOT IAW SRM REPAIR. RT WING OTBD AILERON UPPER SKIN REPAIRED IAW EA NR 1-5750-132127, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISDR FDEA200907222709Longeron · misrepairedFABRICATED LONGERON 52 FORWARD REPAIR SPLICE FOUND NOT IN ACCORDANCE WITH EA 1-5310-131626 STEP 3. RE-ACCOMPLISHED E.A. 1-5310-131626, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 107.SDR FDEA200907222708Longeron · misrepairedFABRICATED LONGERON 52 AFT REPAIR SPLICE FOUND NOT IN ACCORDANCE WITH E.A. 1-5310-131617 STEP 3. RE-ACCOMPLISHED E.A. 1-5310-131617, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 107.SDR FDEA200907222707Longeron · misrepairedFABRICATED AFT REPAIR SPLICE FOUND NOT IN ACCORDANCE WITH E.A. 1-5310-131616 STEP 2. COMPLIED WITH E.A. 1-5310-131616, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REV 107.SDR FDEA200907222706Channel · crackedRIGHT HAND WING LOWER WING FUEL TANK ACCESS DOOR 639CB CUTOUT / U-CHANNEL FOUND CRACKED. REMOVED AND REPLACED AS PER SRM 51-42-04 VOLUME II, REVISION 40. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100, REVISION 107.SDR FDEA200907222705Hinge Fitting · chafedRIGHT HAND WING INBOARD FLAP OUTBOARD HINGE INBOARD FACE AFT OF ACTUATOR MOUNT HOLE FOUND WITH CHAFING MARK. COMPLIED WITH E.A. 1-5750-132126, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REV 107.SDR FDEA200907222704Hinge Fitting · chafedLEFT HAND WING INBOARD FLAP OUTBOARD HINGE (FLAP SIDE) INBOARD FACE, AROUND AFT ATTACHMENT FITTING FOUND WITH CHAFING MARK. REPAIR CARRIED OUT AS PER E.A. 1-5750-132125, THIS REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 107.SDR FDEA200907222703Hinge Fitting · chafedLEFT HAND WING INBOARD FLAP OUTBOARD HINGE (FLAP SIDE) INBOARD FACE, AFT OF ACTUATOR MOUNT FITTING FOUND WITH CHAFING MARK. REPAIR CARRIED OUT AS PER E.A. 1-5750-132125, THIS REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 107.SDR FDEA200907092555Attach Fitting · corrodedRT WING - OTBD T/E FLAP VANE FOUND ATTACHMENT FITTING 'F' (NR 4 FITTING FROM INBD) HOLE CORROSION. REWORKED AS PER E.A. 1-5750-132681, REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100, REVISION 107.SDR FDEA200907092554Support · corrodedLT WING OTBD T/E FLAP AT FLAP VANE FOUND VANE ATTACHMENT FITTING "E" (NR 2 FITTING FROM INBD) CORRODED. REWORKED AS PER E.A. 1-5750-132680. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100, REVISION 107.SDR FDEA200906302397Rub Strip · corrodedRT WING/LWR WING FUEL TANK ACCESS DOOR NR 639CB CUTOUT/RUB STRIP CORRODED. RT WING LWR WING FUEL TANK ACCESS DOOR NR 639CB CUTOUT CORRODED. RUB STRIP REMOVED AND REPLACED IAW SRM 51-42-04 VOLUME II REVISION 40. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100 RESDR FDEA200906302396Skin · corrodedREFERENCE EO 1-5510-7-5000D1 PT.1: HOR STAB LT UPPER PLANK NR 08L BARREL NUT BORE CORROSION REWORKED EXCEEDED EO LIMITATIONS. REPAIR CARRIED OUT IAW EA 1-5510-131625, REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 107.SDR FDEA200906302394Skin · corrodedREFERENCE EO 1-5510-7-5000D1 PT.1: HOR STAB LT UPPER PLANK NR 02L BARREL NUT BORE CORROSION REWORKED EXCEEDED EO LIMITATIONS. REPAIR CARRIED OUT IAW EA 1-5510-131625, REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 107.SDR FDEA200906302393Skin · corrodedREFERENCE EO 1-5510-7-5000D1 PT.1: HOR STAB RT UPPER PLANK NR 27R BARREL NUT BORE BOTTOM CORROSION REWORKED EXCEEDED EO LIMITATIONS. REPAIR CARRIED OUT IAW EA NR 1-5510-131624, REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 107.SDR FDEA200906302391Skin · corrodedREFERENCE EO 1-5510-7-5000D1 PT.1: HOR STAB LT UPPER PLANK NR 16L BARREL NUT BORE CORROSION REWORKED EXCEEDED EO LIMITATIONS. REPAIR CARRIED OUT IAW EA 1-5510-131623, REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 107.SDR FDEA200906302390Skin · corrodedREFERENCE EO 1-5510-7-5000D1 PT 1: HOR STAB LT UPPER PLANK NR 06L BARREL NUT BORE CORROSION REWORKED EXCEEDED EO LIMITATIONS. REPAIR CARRIED OUT IAW NR 1-5510-131625, REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 107.SDR FDEA200906302389Skin · corrodedEO 1-5510-7-5000D1 PT.1: HOR STAB LT UPPER PLANK, NR24L BARREL NUT BORE CORROSION REWORKED EXCEEDED EO LIMITATIONS. REPAIR CARRIED OUT IAW EA NR1-5510-131623, REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 107.SDR FDEA200906292384Spar Cap · corrodedRT WING T/E REAR SPAR UPPER CAP AREA AROUND XORS 1042 FOUND WITH CORROSION. REPAIR CARRIED OUT AS PER E.A. 1-5710-132655, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100 REVISION 107.SDR FDEA200906272352Spar Cap · corrodedHORIZONTAL STABILIZER LEFT HAND UPPER PLANK NR 36 LEFT BARREL NUT BORE CORROSION REWORK FOUND EXCEEDED E.O. NR 1-5510-7-5000 D1 PART 1 LIMITATION. HORIZONTAL STABILIZER LEFT HAND UPPER PLANK NR 36 LEFT BARREL NUT BORE CORROSION REPAIRED PER E.A. NR 1-5510SDR FDEA200906272351Spar Cap · corrodedCORROSION-LT WING REAR SPAR UPPER CAP OTBD OF NR 5 SPOILER PANEL INBD AROUND XORS 799. REPAIR CARRIED OUT AS PER E.A. 1-5710-132654, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100 REVISION 107.SDR FDEA200906272350Spar Cap · corrodedCORROSION-LT WING REAR SPAR UPPER CAP FWD OF NR5 SPOILER PANEL INBD AREA BETWEEN XORS 714 TO 738. REPAIR CARRIED OUT AS PER E.A. 1-5710-132654, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100 REVISION 107.SDR FDEA200906272349Fitting · corrodedHORIZONTAL STABILIZER RT OPERATING BULKHEAD REQUIRED TO TRIM APPROX 0.190" AND FOUND EXCEEDED EO 1-5510-7-5000D1 PT1 LIMITATION (MAX 0.150 INCH) WHILE FACILITATE OVERLAPPED NR 35R BARREL NUT BORE REWORK. REPAIRED AS PER E.A. 1-5510-131629, REPAIR CLASSIFIED SDR FDEA200906272348Trunnion · crackedCRACK-LOWER FASTENER HOLE AT 5:00 POS ON LONGERON APPROX .1250 INCH UPON CRACK AREA REMOVAL FROM NLG TRUNNION FITTING. NOSE LANDING GEAR TRUNNION FITTING LT LOWER LONGERON FABRICATED IAW DWG ACA3796 REVISION A. LONGERON REMOVED AND REPLACED IAW SRM 51-31-01, SDR FDEA200906262312Skin · corrodedAFT ACCESSORY COMPARTMENT RT SKIN, (ACCESS PANEL 347DF LWR 2 EACH ANCHOR NUT MOUNTING AREA) FOUND SEVERE CORROSION. REPAIR CARRIED OUT AS PER E.A. 1-5330-132667, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 107.SDR FDEA200906262311Longeron Splice · corrodedFWD CARGO COMPARTMENT BILGE AREA STA 1119 THRU 6-10 LONGERON 52 SPLICE FITTING FOUND CORRODED. REMOVED AND REPLACED AS PER SRM 51-33-01 VOLUME II REVISION 40. SPLICE FITTING FABRICATED AS PER DRAWING ADA8424 REVISION A. REPAIR CLASSIFIED AS MAJOR PER GMM 6-SDR FDEA200906252309Hinge Bracket · corrodedLT WING OTBD FLAP INBD HINGE (WING SIDE) LWR ATTACHMENT INBD BORE FOUND CORRODED. REPAIR CARRIED OUT AS PER E.A. 1-5750-132122, THIS REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 107.SDR FDEA200906252308Hinge Bracket · corrodedLT WING OTBD FLAP INBD HINGE (WING SIDE) LWR ATTACHMENT OTBD BORE FOUND CORRODED. COMPLIED WITH E.A. 1-5750-132122, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 107.SDR FDEA200906252307Hinge Bracket · corrodedLT WING OTBD FLAP INBD HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT INBD BORE FOUND CORRODED. REPAIR CARRIED OUT AS PER E.A. 1-5750-132121, THIS REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 107.SDR FDEA200906252295Skin · corrodedHORIZONTAL STABILIZER RT UPPER PLANK NR 1 BARREL NUT BORE CORROSION REWORKED, FOUND EXCEEDED EO 1-5510-7-5000 PART 1 LIMITATIONS. REPAIR CARRIED OUT AS PER E.A. 1-5510-131620, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 107.SDR FDEA200906252294Skin · corrodedHORIZONTAL STABILIZER RT UPPER PLANK NR 15R BARREL NUT BORE CORROSION REWORKED, FOUND EXCEEDED EO 1-5510-7-5000, PART 1 LIMITATIONS. REPAIRED AS PER E.A. 1-5510-131622, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REV. 107SDR FDEA200906252293Longeron Splice · corrodedCTR CARGO BILGE AREA AT STA 5-113 TO STA 1541 SPLICE FITTING ON LONGERON 52 FOUND CORROSION. REMOVED AND REPLACED AS PER SRM 51-33-01 VOLUME II REVISION 40. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 107.SDR FDEA200906252292Longeron · corrodedCTR CARGO BILGE AREA AT STA 1621 LONGERON 52 FOUND CORROSION. REPAIR CARRIED OUT AS PER E.A. 1-5310-131626, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 107.SDR FDEA200906252291Skin · crackedRT WING DROOP L/E UPPER SURFACE OTBD END TO FASTENER HOLE, FOUND CRACKED. RIGHT HAND WING DROOP LEADING EDGE UPPER SKIN REPAIRED AS PER SRM 57-10-00 FIGURE 30 VOLUME I REVISION 40. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100 REVISION 107.SDR FDEA200906232244Structure · corrodedBARREL NUT HOLES INSPECT/REPAIR - LT NR 26 FITTING FOUND BORE HOLE CORROSION. REMOVED AND REPLACED AS PER SRM 51-33-01 VOLUME II REVISION 40. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 107.SDR FDEA200906232243Skin · crackedLT WING NR 3 SLAT, WING L/E TELESCOPIC DUCT DOOR CUT-OUT AREA FOUND CRACKED AT INBD AND OTBD SIDE. REPAIR CARRIED OUT AS PER E.A. 1-5730-131723, THIS REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 107.SDR FDEA200906232242Skin · crackedRT WING NR 3 SLAT, WING L/E TELESCOPIC DUCT DOOR CUT-OUT AREA FOUND CRACKED AT INBD AND OTBD SIDE. REPAIR CARRIED OUT AS PER E.A. 1-5730-131722, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 107.SDR FDEA200906222235Hinge Bracket · corrodedRT WING - OTBD FLAP OTBD HINGE (WING SIDE) LOWER ATTACHMENT OTBD BORE FOUND CORRODED. RT WING OUTBOARD FLAP OUTBOARD HINGE (WING SIDE) LOWER ATTACHMENT OUTBOARD BORE REWORKED & FOUND EXCEEDED LIMIT AS PER CMM 57-44-09 REVISION 64. . REPAIR CARRIED OUT AS SDR FDEA200906222234Hinge Bracket · corrodedRT WING INBD FLAP OTBD HINGE (FLAP SIDE) PIVOT PIN ATTACHMENT INBD BORE FOUND CORRODED. REWORKED AND FOUND EXCEEDED LIMIT AS PER CMM 57-52-03 REVISION 64. REPAIR CARRIED OUT AS PER EA 1-5750-130979, THIS REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISSDR FDEA200906222233Hinge Bracket · corrodedRT WING INBD FLAP OTBD HINGE (FLAP SIDE) PIVOT PIN ATTACHMENT OTBD BORE FOUND CORRODED. REWORKED AND FOUND EXCEEDED LIMIT AS PER CMM 57-52-03 REVISION 64. REPAIR CARRIED OUT AS PER EA 1-5750-130979, THIS REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100 REVIS
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