N574FE
Service difficulty reports · 611
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 = 'N574FE' 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 = 'N574FE' 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 07FDEA01690Fitting · corrodedLEFT WING OUTBOARD FLAP INBOARD AFT HINGE FORWARD FITTING INBOARD CENTER HOLE FOUND WITH CORROSION DURING ACCOMPLISHMENT OF EO 1-5750-7-5008. ORIGINAL HOLE DIAMETER = 0.580"; FINAL HOLE DIAMETER = 0.656". [SUP 05-14-07] COMPLIED WITH FEDEX EA 1-5750-109875, SDR 07FDEA01689Fitting · corrodedLEFT WING OUTBOARD FLAP INBOARD AFT HINGE FORWARD FITTING INBOARD CENTER HOLE FOUND WITH CORROSION DURING ACCOMPLISHMENT OF EO 1-5750-7-5008. ORIGINAL HOLE DIAMETER = 0.580"; FINAL HOLE DIAMETER = 0.657". [SUP 05-14-07] COMPLIED WITH FEDEX EA 1-5750-109875,SDR 07FDEA01688Skin · delaminatedRIGHT WING OUTBOARD FLAP CENTER TRAILING EDGE LOWER SURFACE FOUND DELAMINATED 4" BY 4" (LENGTH X WIDTH). [SUP 05-15-07] REMOVED AND REPLACED AS PER AMM 20-50-02.SDR 07FDEA01687Skin · delaminatedRIGHT WING, OUTBOARD FLAP INBOARD TRAILING EDGE UPPER SURFACE FOUND DELAMINATED 5" BY 7" (LENGTH X WIDTH). REMOVED AND REPLACED AS PER AMM 20-50-02. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.SDR 07FDEA01686Frame · chafedFOUND LEFT MAIN FRAME STA 535 AT 9G NET SUPPORT YOKE AREA FOUND CHAFFED AT LONGERON 23L. [SUP 05-10-07] REPAIR CARRIED OUT AS PER FEDEX AIRCRAFT ENGINEERING STANDARD REWORK DRAWING NR: SRZ 53-503. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR 07FDEA01670Skin · crackedRIGHT WING, CRACK INDICATIONS (APPROX 0.0156 INCH DEPTH) REVEALED IN SIX (6) EACH FASTENER HOLES TOWARDS THE EDGE OF ACCESS DOOR CUTOUT LOWER SKIN (BETWEEN XOR=683.4 AND XOR=713.6). [SUP 05-14-07] REPAIRED AS PER FEDEX EA 1-5710-109877, REPAIR CLASSIFIED ASDR 07FDEA01669Skin · crackedLEFT WING, CRACK INDICATIONS (APPROX 0.0156 INCH DEPTH ) REVEALED IN FIVE (5) EACH FASTENER HOLES TOWARDS THE EDGE OF ACCESS CUTOUT LOWER SKIN ACCESS DOOR (BETWEEN XOR=683.4 AND XOR=713.6). REPAIRED AS PER FEDEX EA 1-5710-109878, REPAIR CLASSIFIED AS MAJOR SDR 07FDEA01668Stiffener · crackedLEFT WING LEADING EDGE CAVITY STIFFENER FOUND WITH APPROX 0.25 INCH CRACK AT XOS 667. [SUP 05-15-07] REPAIRED AS PER FEDEX EA 1-5720-109874, WINGS - LEADING EDGE STRINGER - CRACK REPAIR. REPAIR CLASSIFIED AS MINOR PER GMMM 6-2-100.SDR 07FDEA01659Angle · crackedRIGHT WING, LEADING EDGE CAVITY AT ABOUT XOS 659 STRIP ANGLE FOUND WITH APPROX 0.5 INCH CRACKED. [SUP 05-14-2007] FIXED LEADING EDGE STRINGER, CRACK REPAIR. CLASSIFIED AS MINOR REPAIR AS PER FEDEX GMM 6-2-100.SDR 07FDEA01658Angle · crackedRIGHT WING, LEADING EDGE CAVITY AT ABOUT XOS 774 STRIP ANGLE FOUND WITH APPROX 0.3124 INCH CRACKED. [SUP 05-14-07] RT FIXED LEADING EDGE STRINGER, CRACK REPAIR. REPAIR CLASSIFIED AS MINOR PER FEDEX GMM 6-2-100.SDR 07FDEA01657Link · wornCENTER LANDING GEAR, WHEEL WELL BRACKET LOCK LINK CHAMPER FOUND WORN. [SUP 05-04-07] REPAIRED AS PER SRM 53-40-00 VOLUME I, FIGURE 10. REPAIR CALSSIFIED AS MINOR PER GMM 6-2-100.SDR 07FDEA01646Rib · crackedRIGHT WING LEADING EDGE PERFORMANCE FILLET OUTBOARD RIB FOUND CRACKED. [SUP 05-16-07] RIB REMOVED AND REPLACED AS PER SRM 51-35-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR 07FDEA01645Rib · crackedLEFT WING NR 1 SLAT INBOARD RIB ATTACHED TO THE PERFORMANCE FAIRING FOUND WITH ONE (1) INCH CRACK AT THE LOWEST STUD AREA. [SUP 05-14-07] REMOVED AND REPLACED AS PER SRM 51-35-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR PER FEDEX GMM 6-2-100.SDR 07FDEA01644Rib · crackedRIGHT WING, NR 1 SLAT INBOARD RIB FOUND WITH 0.05 INCH CRACKED. [SUP 05-14-07] RIB REMOVED & REPLACED ON RT WING, NR 1 SLAT INBOARD AS PER SRM 51-35-01 VOL.II. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100.SDR 07FDEA01643Skin · gougedRIGHT WING, LEADING EDGE SLAT NR 3 TRAILING EDGE LOWER SURFACE FOUND WITH GOUGE MARK. [SUP 05-16-07] SURFACE SMOOTHENED OFF AND REPROTECTED AS PER SRM 51-21-01 VOLUME II. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.SDR 07FDEA01608Spar · corrodedLEFT WING, REAR SPAR UPPER CAP SURFACE AT ABOUT STA XORS 1046 FOUND WITH CORROSION. [SUP 05-14-07] REPAIRED AS PER FEDEX EA 1-5710-109868, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR 07FDEA01607Spar · corrodedRIGHT WING, REAR SPAR LOWER CAP AT ABOUT STA XORS 1046-1050 FOUND WITH CORROSION. [SUP 05-14-07] REMOVED AS PER SRM 51-21-01 VOLUME II. MATERIAL REMOVED= 0.064", ORIGINAL THICKNESS= 0.108", REMAINING THICKNESS= 0.044", AND EXCEEDED LIMITS AS PER SRM 57SDR 07FDEA01605Spar · corrodedRIGHT WING, REAR SPAR UPPER CAP AT ABOUT STA XORS 1042 FOUND WITH CORROSION. [SUP 05-14-07] REMOVED AS PER SRM 57-21-01 VOLUME II. MATERIAL REMOVED =0.043" ORIGINAL THICKNESS =0.136", REMAINING THICKNESS =0.093" AND FOUND EXCEEDED LIMITS AS PER 57- 20SDR 07FDEA01603Frame · dentedMAIN DECK CARGO COMPARTMENT, MAIN FRAME STA 1681 AT LONGERON 12R FOUND WITH DENT. [SUP 05-08-07] REPAIRED AS PER SRM 53-30-00 VOLUME I, FIGURE 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR 07FDEA01602Frame · dentedMAIN DECK CARGO COMPARTMENT, MAIN FRAME STA 1681 AT LONGERON 12L FOUND WITH DENT. [SUP 05-08-07] REPAIRED AS PER SRM 53-30-00 VOLUME I, FIGURE 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR 07FDEA01601Frame · dentedMAIN DECK CARGO COMPARTMENT, MAIN FRAME STA 1701 AT LONGERON 12R FOUND WITH DENT. [SUP 05-08-07] REPAIRED AS PER SRM 53-30-00 VOLUME I, FIGURE 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR 07FDEA01600Frame · dentedMAIN DECK CARGO COMPARTMENT, MAIN FRAME STA 1701 AT LONGERON 12L FOUND WITH DENT. [SUP 05-08-07] REPAIRED AS PER SRM 53-30-00 VOLUME I, FIGURE 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR 07FDEA01599Frame · dentedMAIN DECK CARGO COMPARTMENT, MAIN FRAME STA 1721 AT LONGERON 12R FOUND WITH DENT. [SUP 05-08-07] REPAIRED AS PER SRM 53-30-00 VOLUME I, FIGURE 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR 07FDEA01598Frame · dentedMAIN DECK CARGO COMPARTMENT, MAIN FRAME STA 1721 AT LONGERON 12L FOUND WITH DENT. [SUP 05-08-07] REPAIRED AS PER SRM 53-30-00 VOLUME I, FIGURE 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR 07FDEA01597Vane · misrepairedLEFT WING, INBOARD FLAP VANE LOWER SURFACE FOUND WITH EXISTING REPAIR WHICH IS NOT COVERED BY SRM. [SUP 05-16-07] REMOVED AND REPLACED AS PER AMM 27-50-22-04. ADJUSTMENT CARRIED OUT AS PER AMM 27-50-22-05. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.SDR 07FDEA01596Vane · delaminatedRIGHT WING, INBOARD FLAP VANE LOWER SURFACE FOUND DELAMINATED. [SUP 05-15-07] REMOVED AND REPLACED AS PER AMM 27-50-22-4. ADJUSTMENT CARRIED OUT AS PER AMM 27-50-22-5. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.SDR 07FDEA01595Frame · chafedLEFT MAINFRAME STA 535 AT 9G NET SUPPORT YOKE AREA FOUND CHAFED. [SUP 05-10-07] REPAIR CARRIED OUT AS PER FEDEX AIRCRAFT ENGINEERING STANDARD REWORK DRAWING NR: SRZ 53-503. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR 07FDEA01591Structure · crackedRIGHT WING, TELESCOPIC DUCT CUT-OUT FOUND WITH 0.4375 INCH CRACK. [SUP 05-14-07] REPAIRED AS PER SRM 57-10-00 VOLUME I (T.R.), FIGURE 42. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR 07FDEA01590Structure · crackedLEFT WING, TELESCOPIC DUCT CUT-OUT FOUND WITH 0.5 INCH CRACK. [SUP 05-14-07] REPAIRED AS PER SRM 57-10-00 VOLUME I (T.R.) FIGURE 42. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.SDR 07FDEA01589Slat Track · crackedRIGHT WING, LEADING EDGE SLAT TRACK NR 14 CUT-OUT FOUND WITH 0.4375 INCH CRACK. [SUP 05-16-07] CUTOUT CRACKED AREA TRIMMED OUT AND REPAIRED AS PER SRM 57-10-00 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR 07FDEA01588Slat Track · crackedRIGHT WING, LEADING EDGE SLAT TRACK NR 12 CUT OUT FOUND WITH 1.5 INCH CRACK. [SUP 05-14-07] TRIMMED OUT AND REPAIRED AS PER SRM 57-10-00 FIGURE 21 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR 07FDEA01551Fitting · crackedNOSE LANDING GEAR, LEFT TRUNNION FITTING WITH 1.25 INCH CRACKED. [SUP 05-14-07] REPAIRED PER SRM 53-40-00 VOLUME I, FIGURE 23 OPTION 2. COMPLIED WITH FEDEX EA 1-5310-109864. REPAIR CLASSIFIED AS MAJOR PER FEDEX GMM 6-2-100.SDR 06FDEA2985Odor · detectedPASSING 18,000 AFTER TURNING WINSHIELD ANTI ICE ON GET ACRID, ELECTRICAL SMELL AND FUMES. LWR R/L 1/4 OF FRONT WINDSCREENS FOGGED OVER. SMELL SOON DISSIPATED. VISUALLY INSPECTED WINDSHIELDS AND ASSOCIATED WIRING, NO DEFECTS FOUND. PERFORMED ADJUSTMENT AND SDR 06FDEA1569Motor · burnedCLIMBING THROUGH 10,000 FEET & LOUD HIGH PITCH NOISE FOLLOWED BY STRONG ELECTRIC ODOR. RETURNED TO KIX. NOISE STOPPED IN DESCENT. ODOR RETURNED IN DESCENT. ACN RELEASED FOR SERVICE PER MEL/CDL: 21-26-06-B CATEGORY: C EXPIRATION: 02MAY06 MEL 21-26-06-B: NSDR 05FDEA03723Frame · damagedCENTER CARGO BAY, STA 1841 LOWER FRAME SKIN FOUND DAMAGED. CENTER CARGO COMPT STA 1841 LOWER FRAME DAMAGE WEB REMOVED AND NEW WEB INSTALLED AS PER DRAWING AGA 7170, SRM 51-33-01 VOL II AND SRM 51-35-01, VOL II. NEW WEB P/N FX AGA 7170-3 LT AND FX AGA 7170-4SDR 05FDEA03648Skin · bulgedFOUND RHW IN SPAR UPPER SKIN AT APPROX XORS 280 STRINGER 13 FOUND WITH SKIN BULGE. CARRIED OUT REPAIR AS PER EA 1-5720-87644.SDR 05FDEA03594Fitting · damagedCRACK FOUND ON RT AFT CTR FASTENER HOLE AT BANJO NR 4 FTG FAYING SURFACE. VIEW LOOKING I/B AT 2 O'CLOCK DIRECTION. CRACK LENGTH FROM THE EDGE OF THE BANJO NR 4 FTG APPROX 1/8 INCH LONG. CORRECTIVE ACTION: SNRM N1614: BANJO FTG R/H NO.4 AFT CENTER FASTENER SDR 05FDEA03564Longeron · crackedFOUND CENTER CARGO COMP, AFTER REMOVAL OF CRACKED LONGERON SPLICE AT STA 1641 TO 1661 LONGERON 44R FOR REPLACEMENT, LONGERON 44R FOUND CRACK AT STA 1652 TO 1658. REPAIRED AS PER SRM 53-10-01.SDR 05FDEA03563Longeron · crackedFOUND CENTER CARGO COMP AFTER REMOVAL OF CRACKED LONGERON SPLICE AT STA 1641 TO 1661 LONGERON 44R FOR REPLACEMENT, LONGERON 44R FOUND CRACK AT STA 1646 TO 1651. REPAIRED AS PER SRM 53-10-00.SDR 05FDEA03478Skin · crackedRT WING DROOP L/E UPPER SKIN FOUND WITH CRACK. RT WING DROOP L/E UPPER SKIN CRACK CARRIED OUT REPAIR AS PER SRM 57- 10-00 FIG.26 VOL.I. THIS REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.SDR 05FDEA03445Floorbeam · crackedAFT INTERMEDIATE FUSELAGE, FLOORBEAM LOWER CAP FOUND CRACK AT STA 1801 LBL 8 TO RBL 8. REPAIRED AS PER EA 1-5310-87655. CLASSIFIED MAJOR REPAIR PER GMM 6-2-100.SDR 05FDEA03444Frame · damagedCENTER CARGO COMPT STA 1841 RT LOWER FRAME ASSY CORNER FOUND CRACK DURING REMOVAL. REPAIRED PER SRM 53-00-00 FIG.3 VOL.I. NEW ANGLE P/N FX AGA 7171-20 FABRICATED PER DRAWING AGA 7171. MAJOR REPAIR PER GMM 6-2-100.SDR 05FDEA03443Bulkhead · damagedAFT CABIN STA 2007 RBL 103 TO 107, Z=-18, AFT PRESSURE BULKHEAD T-CHORD FOUND REPAIR PATCH . SNRM N0845: WORK ACCOMPLISHED AS PER EA#1-5310-87647 TITLE: FUSELAGE- MAIN FRAME- PRESSURE BULKHEAD BODY STA. Y = 2007.000, TEE CHORD REPAIR. CLASSIFIED MAJOR REPSDR 05FDEA03438Structure · corrodedHORIZ STAB RT BARREL NUT BORE NR 10 FOUND WITH CORROSION. REWORK/REPAIR AD 2003-22-08 EA 1-5510-87628, ATTACHMENT 25. MAJOR REPAIR IAW FEDEX GMM 6-2-100.SDR 05FDEA03437Structure · corrodedHORIZ STAB RT BARREL NUT BORE NR 8 FOUND WITH CORROSION. REWORK/REPAIR AD 2003-22-08 EA 1-5510-87628, ATTACHMENT 24. MAJOR REPAIR IAW FEDEX GMM 6-2-100.SDR 05FDEA03436Intercostal · corrodedFWD CARGO COMPT AT STA 6-30 LT LOWER INTERCOSTAL ASSY BETWEEN LONGERON 42 TO LONGERON 43 FOUND CORRODED DURING REMOVAL.SDR 05FDEA03435Frame · corrodedFWD CARGO COMPT AT STA 6-30 RT LOWER FRAME ASSY BETWEEN LONGERON 42 TO LONGERON 43 FOUND CORRODED DURING REMOVAL. FRAME REMOVED AS PER SRM 51-35-01 VOL.II. NEW FRAME FABRICATED AS PER DWG ACA 7049 AND NEW FRAME INSTALLED AS PER SRM 51-35-01 VOL.II. MINOR SDR 05FDEA03417Structure · corrodedHORIZONTAL STAB RT BARREL NUT BORE NR 35 FOUND WITH CORROSION. HOR. STAB. BARREL NUT BORE 35 RT REPAIRED IAW STABILIZERS-HORIZONTAL STABILIZER- BARREL NUT BORE REWORK/ REPAIR AD 2003-22-08 EA1-5510-87628, ATTACHMENT 45. MAJOR REPAIR IAW FEDEX GMM 6-2-100.SDR 05FDEA03416Structure · corrodedHORIZONTAL STAB LT BARREL NUT BORE NR 35 FOUND WITH CORROSION. REWORK/ REPAIR AD 2003-22-08 EA 1-5510-87628, ATTACHMENT 39. MAJOR REPAIR IAW FEDEX GMM 6-2-100.SDR 05FDEA03415Structure · corrodedHORIZONTAL STAB LT BARREL NUT BORE NR 4 FOUND WITH CORROSION. HORIZONTAL STAB BARREL NUT BORE NR 4 LT REPAIRED IAW STABILIZERS- HORIZONTAL STABILIZER- BARREL NUT BORE REWORK/ REPAIR AD 2003-22-08 EA 1-5510-87628, ATTACHMENT 43. MAJOR REPAIR IAW FEDEX
Back to N574FE