N607FE
Service difficulty reports · 454
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 = 'N607FE' 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 = 'N607FE' 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 FDEA201005051459Rib · crackedRT WING - SLAT ASSEMBLY NR 6, XOS 858 RIB FOUND CRACKED. RT WING SLAT ASSY NR 6 R & R IAW AMM 27-80-30-4, REV 64. SLAT ADJUSTMENT AND TEST CARRIED OUT IAW AMM 27-80-30-4, REV 64 FOUND SATISFACTORY.SDR FDEA201005051458Skin · damagedLEFT HAND WING - FUEL TANK ACCESS PANEL NR 536AB CUT-OUT, 01 EACH FASTENER HOLE FOUND DAMAGED. COMPLIED WITH EA NR 1-5710-125559 REV A, PART 2. REPAIR CLASSIFIED MINOR IAW GMM 6-2-100, REV 110.SDR FDEA201005051457Rib · crackedRT WING - SLAT ASSY NR 6, XOS 863 RIB FOUND CRACKED. AFTER REMOVAL OF EXISTING REPAIR DOUBLER. RT WING - SLAT ASSY NR 6 R & R IAW AMM 27-80-30-4, REV 64. SLAT ADJUSTMENT AND TEST CARRIED OUT IAW AMM 27-80-30-4 REV 64. FOUND SATISFACTORY.SDR FDEA201005051456Skin · crackedRT WING - STA XORS 683.400 TO XORS 713.600 LOWER SKIN ACCESS DOOR CUT OUT 01 EACH FASTENER HOLES FOUND CRACKED DURING HFEC OPEN HOLE INSPECTION. REPAIRED IAW EA NR 1-5710-137992, REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 110.SDR FDEA201005051454Skin · crackedLT WING - STA XORS 683 TO XORS 713.600 LOWER SKIN ACCESS DOOR CUT OUT 06 EACH FASTENER HOLES FOUND CRACKED DURING HFEC OPEN HOLE INSP. REPAIRED IAW EA NR 1-5710-137991, REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 110.SDR FDEA201005011409Rib · crackedLT WING - NR1 SLAT INBD EDGE RIB FOUND CRACKED. R & R IAW SRM 51-31-01 REV 43. OPERATION AND ADJUSTMENT TEST CARRIED OUT IAW AMM 27-80-20-4 REVISION 64 FOUND SATISFACTORY. REPAIR CLASSIFIED MINOR IAW GMM 6-2-100, REV 110.SDR FDEA201004301408Rib · crackedLT WING - L/E PERFORMANCE FILLET OTBD EDGE FORMER FOUND CRACKED. LT WING - L/E PERFORMANCE FILLET OTBD EDGE CRACKED RIB STOP DRILLED AND REPAIR AS IAW SRM 57-40-71 FIG 201, REPAIR 1, REVISION 43. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 110.SDR FDEA201004301407Wedge · delaminatedLT WING-OTBD FLAP, T/E WEDGE, INBD UPPER SURFACE FOUND DELAMINATED. LT WING - OTBD FLAP T/E WEDGE REPAIRED IAW EA 1-5750-137979, REPAIR CLASSIFIED AS MINOR REPAIR IAW GMM 6-2-100 REV 110.SDR FDEA201004291393Skin · chafedFUSELAGE - CTR CARGO COMPARTMENT DOOR CUTOUT AFT JAMB EXTERIOR SKIN FOUND EXISTING DOUBLER REPAIR. CTR CARGO COMPARTMENT DOOR CUT OUT AFT JAMB EXISTING REPAIR DOUBLER EVALUATED FOUND REPAIR IAW SRM 53-00-15 FIG 202, REV 43. CHAFFED DOUBLER AT CENTER CARGOSDR FDEA201004291392Skin · chafedFUSELAGE - FWD CARGO COMPARTMENT DOOR CUTOUT AFT JAMB EXTERIOR SKIN FOUND EXISTING REPAIR DOUBLER. FWD CARGO COMPARTMENT DOOR CUT OUT AFT JAMB EXISTING REPAIR DOUBLER EVALUATED FOUND REPAIR IAW SRM 53-00-15 FIGURE 202, REV 43. CHAFED DOUBLER AT FWD CARGO CSDR FDEA201004291391Skin · chafedFUSELAGE - FWD CARGO COMPARTMENT DOOR CUTOUT FWD JAMB EXTERIOR SKIN FOUND EXISTING REPAIR DOUBLER. FWD CARGO COMPARTMENT DOOR CUT OUT FWD JAMB EXISTING REPAIR DOUBLER EVALUATED FOUND REPAIR IAW SRM 53-00-15 FIG 202, REVISION 43. CHAFED DOUBLER AT FWD CARGO SDR FDEA201002030307Anti-Ice System · failedAFTER DEPARTURE WE ENCOUNTERED ICING CONDITIONS, SO WE SELECTED ANTI ICE. WHEN WING ANTI ICE SELECTED, WE RECEIVED AIR SYS 3 OFF FOLLOWED BY WING ANTI ICE R DISAGREE, WE THEN FOLLOWED QRH PROCEDURES AND SELECTED WING A/I OFF. ALERT EXTINGUISHED BUT WING A/I SDR FDEA200902230666Anti-Ice Valve · failedPDIS: WHEN SELECTED WING ANTI-ICE ON DEPARTURE FROM LFPGR`CVD DISAG-ALERT. RAN QRH PROCEDURES WHICH FAILED TO OPEN OR CLOSE RT WING ANTI-ICE VALVE STUCK IN TRANSIT. DIVERTED TO LIMC. DUMPED APPROX 125.000 LBS FUEL. ON SYNOPTIC AIR PAGE CONFIRMED AMBER RT WSDR FDEA200812225260Selector Valve · malfunctionedLEFT MAIN GEAR FAILED TO RETRACT ON TAKEOFF. AFT CYCLING GEAR IAW QRH GEAR AGAIN REMAINED EXTENDED APPROXIMATELY 3-4 MINUTES LATER WITH NO CREW ACTION GEAR RETRACTED ON ITS OWN. HYD NORMAL. ALTITUDE APPROX 26000 AND 230 KTS WHEN RETRACTION FINALLY OCCURED.SDR 08FDEA04586Strap · crackedLEFT WING, OUTBOARD FLAP INBOARD HINGE (WINGSIDE) TENSION STRAP FITTING FOUND CRACKED. R & R AS PER SRM 51-33-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR 08FDEA04379Skin · crackedCRACK FOUND ON 7 EACH FASTENER HOLES ON RIGHT WING AT LOWER WING SKIN OUTER ACCESS DOOR CUTOUT AT PANEL NR 636AB. 7 CRACKED FASTENER HOLES ON RT WING LOWER WING SKIN REPAIRED AS PER E.A. 1-5710-125558, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.SDR 08FDEA04378Skin · damagedCHIPPED EDGE FOUND ON 1 FASTENER HOLE ON LEFT WING AT LOWER WING SKIN OUTER ACCESS DOOR CUTOUT AT PANEL NR 536AB. REPAIR CARRIED OUT AT LEFT HAND WING AT LOWER WING SKIN. 01 EACH HOLE AT OUTER ACCESS DOOR CUTOUT AT PANEL NR 536AB AS PER E.A. 1-5710-125559, SDR 08FDEA04377Skin · crackedCRACK FOUND ON 3 FASTENER HOLES ON LEFT WING AT LOWER WING SKIN OUTER ACCESS DOOR CUTOUT AT PANEL NR 536AB. 3 CRACKED FASTENER HOLES ON LEFT HAND WING AT LOWER WING SKIN REPAIRED AS PER EA 1-5710-125557, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.SDR 08FDEA04376Seat Track · corrodedMAIN DECK CARGO, CORROSION ON SEAT TRACK FLANGE AT STA 1481 TO STA 1531, X = -75. REPAIR CARRIED OUT AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR 08FDEA04375Seat Track · corrodedMAIN DECK CARGO, CORROSION ON SEAT TRACK FLANGE AT STA 1260 TO STA 1273, X = -8. REPAIR CARRIED OUT AT STA 1271 TO STA 1331, X = -8 AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR 08FDEA04336Hinge · corrodedRIGHT WING OUTBOARD FLAP INBOARD HINGE (WING SIDE) LOWER ATTACHMENT OUTBOARD HOLE AFT SPOTFACE FOUND SURFACE CORROSION. SURFACE CORROSION REPAIRED AS PER E.A. 1-5750-122592, THIS REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR 08FDEA04334Hinge Fitting · corrodedRIGHT WING OUTBOARD FLAP OUTBOARD HINGE (WING SIDE) LOWER OUTBOARD BORE HOLE FOUND WITH CORROSION. RT WING OUTBOARD FLAP OUTBOARD HINGE (WING SIDE) LOWER OUTBOARD BORE HOLE CORROSION REPAIRED AS PER E.A. 1-5750-122590, THIS REPAIR CLASSIFIED AS MAJOR PER GMMSDR 08FDEA04333Hinge · corrodedRIGHT WING OUTBOARD FLAP OUTBOARD HINGE (WING SIDE) LOWER INBOARD BORE HOLE FOUND WITH CORROSION. REPAIRED AS PER E.A. 1-5750-122590, THIS REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR 08FDEA04332Hinge · corrodedRIGHT WING OUTBOARD FLAP INBOARD HINGE (WINGSIDE) LOWER ATTACHMENT OUTBOARD HOLE FORWARD SPOTFACE FOUND SURFACE CORROSION. SPOTFACE CORROSION REPAIRED AS PER E.A. 1-5750-122592, SHIM FABRICATED AND INSTALLED AS PER CMM 57-44-08. REPAIR CLASSIFIED AS MAJOR SDR 08FDEA04323Hinge Fitting · corrodedLEFT HAND WING: OUTBOARD FLAP OUTBOARD HINGE (WING SIDE) ACTUATOR HOLE OUTBOARD BORE HOLE FOUND WITH CORROSION. CORROSION REMOVED AND FOUND EXCEEDED LIMIT AS PER CMM 57-44-09. REPAIR CARRIED OUT AS PER EA 1-5750-122591, THIS REPAIR CLASSIFIED AS MAJOR PERSDR 08FDEA04320Hinge Fitting · corrodedLEFT WING OUTBOARD FLAP OUTBOARD HINGE (WING SIDE) ACTUATOR HOLE INBOARD BORE HOLE FOUND WITH CORROSION. CORROSION REMOVED AND FOUND EXCEEDED LIMIT AS PER CMM 57-44-09. REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-122591, THIS REPAIR IS CLASSIFIED AS MAJOR PSDR 08FDEA04319Stiffener · crackedEMPENNAGE: AFT FUSELAGE AFT BULKHEAD STA 2164 AFT SURFACE LOWER LATERAL STIFFENER FOUND CRACKED AT LEFT HAND AND RIGHT HAND SIDE. REMOVED AND REPLACED AS PER SRM 51-35-01 VOLUME II AND SRM 51-32-01 VOLUME II. NEW STIFFENER REWORKED AS PER DRAWING AJC7001.SDR 08FDEA04318Door Frame · crackedCRACK INDICATION FOUND ON SECOND LAYER WEB FROM TOP DURING HFEC OPEN HOLE INSPECTION ON 0.520" HOLES AT MAIN CARGO DOOR NR 7 LOWER JAMB AT HOLES A AND B. CARRIED OUT REPAIR AS PER FEDEX EA 1-5310-125556, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR 08FDEA04317Door Frame · crackedCRACK INDICATION FOUND ON SECOND LAYER WEB FROM TOP DURING HFEC OPEN HOLE INSPECTION ON 0.520" HOLES AT MAIN CARGO DOOR NR 6 LOWER JAMB AT HOLE A. CARRIED OUT REPAIR AS PER FEDEX E.A. 1-5310-125556, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR 08FDEA04316Support Fitting · crackedCRACK INDICATION FOUND DURING HFEC OPEN HOLE INSPECTION ON 0.460" HOLES AT MAIN CARGO DOOR LOWER JAMB NR 7 SUPPORT FITTING AT HOLES A, B, C AND D. REMOVED AND REPLACED AS PER SRM 51-31-01 VOLUME II. BUSHING REPAIR ON HOLES CARRIED OUT AS PER SRM 53-50-00 FISDR 08FDEA04315Support Fitting · crackedCRACK INDICATION FOUND DURING HFEC OPEN HOLE INSPECTION ON 0.460" HOLES AT MAIN CARGO DOOR LOWER JAMB NR 6 SUPPORT FITTING AT HOLES A, B, C AND D. REMOVED AND REPLACED AS PER SRM 51-31-01. BUSHING REPAIR CARRIED OUT AS PER SRM 53-50-00. REPAIR CLASSIFIED ASSDR 08FDEA04314Support Fitting · crackedCRACK INDICATION FOUND DURING HFEC OPEN HOLE INSPECTION ON 0.460" HOLES AT MAIN CARGO DOOR LOWER JAMB NR 5 SUPPORT FITTING AT HOLE A, C AND D. REMOVED AND REPLACED AS PER SRM 51-33-01 VOLUME II. BUSHING REPAIR CARRIED OUT AS PER SRM 53-50-00. REPAIR CLASSIFSDR 08FDEA04313Support Fitting · crackedCRACK INDICATION FOUND DURING HFEC OPEN HOLE INSPECTION ON 0.460" HOLES AT MAIN CARGO DOOR LOWER JAMB NR 4 SUPPORT FITTING AT HOLES A, B, C AND D. CARRIED OUT BUSHING REPAIR AS PER SRM 53-50-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR 08FDEA04312Support Fitting · crackedCRACK INDICATION FOUND DURING HFEC OPEN HOLE INSPECTION ON 0.460" HOLES AT MAIN CARGO DOOR LOWER JAMB NR 3 SUPPORT FITTING AT HOLE B. CARRIED OUT BUSHING REPAIR AS PER SRM 53-50-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR 08FDEA04311Support Fitting · crackedCRACK INDICATION FOUND DURING HFEC OPEN HOLE INSPECTION ON 0.460" HOLES AT MAIN CARGO DOOR LOWER JAMB NR 2 SUPPORT FITTING AT HOLE C. CARRIED OUT BUSHING REPAIR AS PER SRM 53-50-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR 08FDEA04310Support Fitting · crackedCRACK INDICATION FOUND DURING HFEC OPEN HOLE INSPECTION ON 0.460" HOLES AT MAIN CARGO DOOR LOWER JAMB NR 1 SUPPORT FITTING AT HOLES A, B AND C. BUSHING REPAIRED AS PER SRM 53-50-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR 08FDEA03784Compressor · stalledNR 1 ENG COMPRESSOR STALLED ON CLIMB AT ABOUT 8000 FT TWO EVENTS OCCURRED ABOUT 3 MINUTES APART. PRECAUTIONARY ENGINE SHUTDOWN ACCOMPLISHED. PLACED IN WORK. NR 1 ENGINE CHANGE APPROVED. PLANT ENGINEERING. REMOVED AND REPLACED NR 1 ENGINE IAW WORKCARD 71TSDR 07FDEA04341Seat Track · corrodedMCD SEAT TRACK FROM FR 78TO 73 BL 0 HAS 5 AREAS OF CORROSION. REMOVED AND REPLACED SEAT TRACK FROM FR 65-78 IAW SRM 51-40-21 AND SRM 53-10-10.SDR 07FDEA02232Seat Track · corrodedMAIN DECK CARGO COMPARTMENT FLOOR SEAT TRACK AT BS 5-23 TO 5-33 LT X = 75 FOUND WITH CORROSION. [06-29-07] REPAIR CARRIED OUT AS PER SRM 53-70-00 FIG.1 VOL.I. REPAIR CLASSIFIED AS MAJOR REPAIR AS PER FEDEX GMM 6-2-100.SDR 07FDEA02198Seat Track · crackedMAIN DECK, SEAT TRACK AT STA 755, X= -27 FOUND CRACK AT LOWER SURFACE. [06-29-07] REPAIR CARRIED OUT AS PER SRM 53-70-00 FIG.1 VOL.I. REPAIR CLASSIFIED AS MAJOR REPAIR AS PER FEDEX GMM 6-2-100.SDR 07FDEA02167Vane · corrodedRT OUTBOARD FLAP VANE NR 4 AND NR 5 TRACK (COUNT FROM INBOARD) UPPER MOUNTING AREA FOUND CORROSION. [06-29-07] REMOVED AND REPLACED AS PER AMM 27-50-30-4. ADJUSTMENT CARRIED OUT AS PER AMM 27-50-32-5 AND OPERATIONAL TEST CARRIED OUT AS PER AMM 27-50-00-860-8SDR 07FDEA02166Structure · crackedAFT ACCESSORY COMPARTMENT, FOUND FRAME CLIP AT STA 2140 CRACKED. REMOVED AND REPLACED AS PER SRM 51-31-01 VOL II.SDR 07FDEA02165Skin · chafedRT WING FIXED LEADING EDGE UPPER SURFACE, XIS 247 FOUND CHAFED AT EXISTING REPAIR. [07-02-07] REPAIR CARRIED OUT AS PER SRM 57-10-00 FIG. 24, VOL I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.SDR 07FDEA02164Skin · chafedLT WING UPPER FIXED LEADING EDGE SURFACE AT XIS 247 FOUND WITH CHAFING MARK. [06-29-07] REPAIR CARRIED OUT AS PER SRM 57-10-00 FIG. 24 VOL I. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100.SDR 07FDEA02163Skin · dentedRT INBOARD FLAP LOWER SURFACE, INBD LOWER SKIN SEGMENT FOUND WITH DENT. REPAIR CARRIED OUT AS PER SRM 57-10-00 FIG. 3 VOL.I. REPAIR CLASSIFIED AS MAJOR REPAIR AS PER FEDEX GMM 6-2-100.SDR 07FDEA02162Skin · dentedFOUND DENT, RT WING FIXED LEADING EDGE, NEAR XW 344. [07-03-07] COMPLIED WITH FEDEX E.A 1-5720-109914. CLASSIFIED AS MINOR REPAIR AS PER FEDEX GMM 6-2-100.SDR 07FDEA02161Rib · crackedLT WING LEADING EDGE RIB AT XOS 584 FOUND CRACKED. [06-29-07] REMOVED AND REPLACED AS PER SRM 51-33-01 VOL.II. NEW FORMER FABRICATED AS PER DOUGLAS DWG ARB2931. REPAIR CLASSIFIED AS MAJOR REPAIR AS PER FEDEX GMM 6-2-100.SDR 07FDEA02160Skin · crackedCRACK FOUND AT LT WING LOWER SURFACE ACCESS PANEL 536AB CUT OUT. CRACK CAN BE SEEN AT NR 5 FASTENER HOLE, COUNTING FROM 6 O'CLOCK POSITION IN A CLOCKWISE DIRECTION. [06-29-07] REPAIR CARRIED OUT AS PER FEDEX E.A. 1-5710-109907, REPAIR CLASSIFIED AS MAJORSDR 07FDEA02159Skin · crackedCRACK FOUND AT LT WING LOWER SURFACE ACCESS PANEL 536AB CUT OUT. CRACK CAN BE SEEN AT NR 4 FASTENER HOLE, COUNTING FROM 6 O'CLOCK POSITION IN A CLOCKWISE DIRECTION. [06-29-07] REPAIR CARRIED OUT AS PER FEDEX E.A. 1-5710-109907, REPAIR CLASSIFIED AS MAJOR RSDR 07FDEA02158Skin · crackedCRACK FOUND AT LT WING LOWER SURFACE ACCESS PANEL 536AB CUT OUT. CRACK CAN BE SEEN AT NR 6 FASTENER HOLE, COUNTING FROM 12 O'CLOCK POSITION IN A CLOCKWISE DIRECTION. [06-29-07] REPAIR CARRIED OUT AS PER FEDEX E.A. 1-5710-109907, REPAIR CLASSIFIED AS MAJO
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