N606FE
Service difficulty reports · 403
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 = 'N606FE' 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 = 'N606FE' 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 FDEA202310011681Casting · crackedFWD LOWER CARGO DOOR WILL NOT FULLY OPEN. DURING EVALUATION, FOUND LOWER FWD CARGO DOOR ACTUATOR MOUNT CASTING MPN: ADA7254-503 CRACKED. R/R ACTUATOR SUPPORT ASSEMBLY REF AMM 20-50-02-2.SDR FDEA202309091569Tire · leakingAPPROX 1HR INTO FLIGHT AT FL 380 WE RECEIVED LVL 1 TIRE PRESS LOW ON THE #5 TIRE. OVER TEH NEXT 5 MINUTES PRESSURE DECAYED UNTIL WE RECEIVED TIRE FAIL ALERT. FOLLOWED QRH PROCEDURES. PRESSURE SLOWLY DECAYED FOR THE REST OF THE FLIGHT TO 0 PSI. EMERGENCY SDR FDEA202206021362Transducer · failedRECEIVED TIRE FAIL ANNUNCIATION ON TAKEOFF ROLL. COMPLIED WITH QRH. ***EMERGENCY DECLARED*** REMOVED AND REPLACED MAIN WHEEL #5 TIRE PRESSURE TRANSMISSION AMM 32-46-08-4 AND AIR PRESSURE SDR FDEA202201020004Hinge Bracket · corrodedRIGHT WING-WING SIDE INBOARD FLAP OUTBOARD HINGE ACTUATOR ATTACH OUTBOARD LUG HOLE BORE FOUND CORROSION. CORROSION AT RIGHT WING-WING SIDE INBOARD FLAP OUTBOARD HINGE ACTUATOR ATTACH OUTBOARD LUG HOLE BORE (#4 HOLE) REWORKED AND FOUND WITHIN LIMIT AS PER MSDR FDEA202201020003Hinge Bracket · corrodedRIGHT WING-WING SIDE INBOARD FLAP OUTBOARD HINGE ACTUATOR ATTACH INBOARD LUG HOLE BORE FOUND CORROSION. CORROSION AT RIGHT WING-WING SIDE INBOARD FLAP OUTBOARD HINGE ACTUATOR ATTACH INBOARD LUG HOLE BORE (#4 HOLE) REWORKED AND FOUND WITHIN LIMIT AS PER MD-SDR FDEA202201020002Hinge Bracket · corrodedLEFT WING-WING SIDE INBOARD FLAP OUTBOARD HINGE ACTUATOR ATTACH OUTBOARD LUG HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING-WING SIDE INBOARD FLAP OUTBOARD HINGE ACTUATOR ATTACH OUTBOARD LUG HOLE BORE (#4 HOLE) REWORKED AND FOUND WITHIN LIMIT AS PER MD-SDR FDEA202201020001Hinge Bracket · corrodedLEFT WING-WING SIDE INBOARD FLAP OUTBOARD HINGE ACTUATOR ATTACH INBOARD LUG HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING-WING SIDE INBOARD FLAP OUTBOARD HINGE ACTUATOR ATTACH INBOARD LUG HOLE BORE (#4 HOLE) REWORKED AND FOUND WITHIN LIMIT AS PER MD-11SDR FDEA202112263146Fitting · crackedDURING ULTRASONIC INSPECTION FOR VERTICAL CRACKS BEHIND SERVICE REPAIR SR10550013 PER DRAWING NO. SN10550000 REVISION C ON RIGHT HAND SIDE LOWER VERTICAL STABILIZER FORWARD FLANGE OF UPPER REAR SPAR CAP, STATION 2164, EXISTING CRACK INDICATION FOUND FROMSDR FDEA202112263145Fitting · crackedDURING ULTRASONIC INSPECTION FOR VERTICAL CRACKS BEHIND SERVICE REPAIR SR10550012 PER DRAWING NO. SN10550000 REVISION C ON LEFT HAND SIDE LOWER VERTICAL STABILIZER FORWARD FLANGE OF UPPER REAR SPAR CAP, STATION 2164, EXISTING CRACK INDICATION FOUND FROM SDR FDEA202112263147Floor Support · corrodedUPON REMOVAL OF AFT FLOOR PANEL SUPPORT AT STATION 1841 FOR REPAIR, LOWER CENTER CARGO COMPARTMENT FLOOR BULKHEAD WEB AT STATION 1841 X=-32 FOUND CORROSION. LOWER CENTER CARGO COMPARTMENT FLOOR BULKHEAD AT STATION 1841 X=-32 WEB CORROSION REMOVED AND FOUSDR FDEA202112263144Floor Support · corrodedLOWER CENTER CARGO COMPARTMENT FLOOR PANEL SUPPORT FOUND CORROSION AT STATION = 1841 X= 45. LOWER CENTER CARGO COMPARTMENT FLOOR SUPPORT AT STATION 1841 X=45 CORROSION REMOVED AND FOUND EXCEED LIMIT AS PER SRM 53-00-00-2R FIGURE 205 REPAIR GENERAL. CORROSDR FDEA202112263143Web · crackedLOWER CENTER CARGO COMPARTMENT FLOOR BULKHEAD WEB AT STATION 1841 X= 12 FOUND CRACKED. LOWER CENTER CARGO COMPARTMENT FLOOR BULKHEAD CRACKED WEB AT STATION 1841 X=0 TO X=60 REMOVED AND REPLACED WITH FABRICATED WEB AS PER SRM 51-31-01-0G. WEB FABRICATED SDR FDEA202112263141Skin · crackedRIGHT HAND WING # 11 SLAT TRACK LOWER CUTOUT FOUND CRACKED AT INBOARD SIDE XORS 623 AREA. RIGHT HAND WING # 11 SLAT TRACK LOWER CUTOUT AT INBOARD SIDE XORS 623 CRACKED AREA REPAIR CARRIED OUT AS PER SRM 57-40-02-2R FIGURE 201 REPAIR 7. REPAIR CLASSIFIED SDR FDEA202112263149Panel · delaminatedCABIN Ï¿½ FLOOR PANEL 271EF AT STATION 1361 TO STATION 1421 FOUND DELAM. DELAM FLOOR PANEL 271EF AT CABIN STATION 1361 TO STATION 1421 REMOVED AS PER AMM 53-21-04-4. FLOOR PANEL 271EF FABRICATED AS PER FEDEX DRAWING SRZ-25-005 REVISION R. FLOOR PANEL 271EFSDR FDEA202112263148Panel · delaminatedCABIN Ï¿½ FLOOR PANEL #232DF AT STATION 495 TO STATION 505 FOUND DELAM. DELAM FLOOR PANEL #232DF AT CABIN STATION 495 TO STATION 505 REMOVED AS PER AMM 53- 21-04-4. FLOOR PANEL #232DF FABRICATED AS PER FEDEX DRAWING SRZ-25-005 REVISION R. FLOOR PANEL #232DFSDR FDEA202112263142Panel · delaminatedCABIN Ï¿½ FLOOR PANEL #271GF AT STATION 1437 FOUND DELAM. DELAM FLOOR PANEL #271GF AT CABIN STATION 1437 REMOVED AS PER AMM 53-21-04-4. FLOOR PANEL #271GF FABRICATED AS PER FEDEX DRAWING SRZ-25-005 REVISION R. FLOOR PANEL #271GF INSTALLED AS PER AMM 53-21-SDR FDEA202112243136Hinge Bracket · corrodedRIGHT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE FOUND CORROSION. CORROSION AT RIGHT WING-WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE (#3 HOLE) REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM 57-44-07. OVERSIZED REPAIR BUSHINSDR FDEA202112243135Hinge Bracket · corrodedLEFT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING-WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE (#3 HOLE) REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM 57-44-07. OVERSIZED REPAIR BUSHING SDR FDEA202112243134Hinge Bracket · corrodedRIGHT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE PIVOT OUTBOARD LUG HOLE BORE FOUND CORROSION. CORROSION AT RIGHT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE PIVOT OUTBOARD LUG HOLE BORE (A AND B HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57SDR FDEA202112243133Hinge Bracket · corrodedRIGHT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE PIVOT INBOARD LUG HOLE BORE FOUND CORROSION. CORROSION AT RIGHT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE PIVOT INBOARD LUG HOLE BORE (G AND F HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-5SDR FDEA202112243132Hinge Bracket · corrodedLEFT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE PIVOT OUTBOARD LUG HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE PIVOT OUTBOARD LUG HOLE BORE (A AND B HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57- SDR FDEA202112243131Hinge Bracket · corrodedLEFT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE PIVOT INBOARD LUG HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE PIVOT INBOARD LUG HOLE BORE (G AND F HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-52-SDR FDEA202112233129Skin · crackedLEFT HAND WING # 8 SLAT LOWER SURFACE ( COVE PANEL ) ZONE 624 STATION XOS 1097 FOUND CRACK BETWEEN TRACK # 17 AND # 18. LEFT HAND WING # 8 SLAT LOWER SURFACE ( COVE PANEL ) ZONE 624 STATION XOS 1097 CRACKED BETWEEN TRACK # 17 AND # 18 REPAIR CARRIED OUT ASSDR FDEA202112233128Doubler · crackedLEFT HAND WING, FOUND BEADED DOUBLER CRACKED AT STATION XOS = 755. LEFT HAND WING STATION XOS = 755 CRACKED BEADED DOUBLER REPAIRED AND REPAIR PARTS INSTALLED AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15 AT LEFT HAND WING FIXED LEADING EDGE COMPARTMENT INNESDR FDEA202112233127Doubler · crackedLEFT HAND WING, FOUND BEADED DOUBLER CRACKED AT STATION XOS = 662. LEFT HAND WING STATION XOS = 662 CRACKED BEADED DOUBLER REPAIRED AND REPAIR PARTS INSTALLED AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15 AT LEFT HAND WING FIXED LEADING EDGE COMPARTMENT INNESDR FDEA202112233126Doubler · crackedLEFT HAND WING, FOUND BEADED DOUBLER CRACKED AT STATION XOS = 615. LEFT HAND WING STATION XOS = 615 CRACKED BEADED DOUBLER REPAIRED AND REPAIR PARTS INSTALLED AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15 AT LEFT HAND WING FIXED LEADING EDGE COMPARTMENT INNESDR FDEA202112223117Seat Track · corrodedCABIN FLOOR SEAT TRACK AT STATION 595 TO STATION 655 X = - 75.25 FOUND CORROSION. CABIN FLOOR AT SEAT TRACK STATION 595 TO STATION 655 , X = - 75.25 CORROSION EVALUATED FOUND EXFOLIATED AND EXCEEDED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE SDR FDEA202112223116Seat Track · corrodedCABIN - FLOOR SEAT TRACK AT STATION 595 TO STATION 601 X = - 47.5 FOUND CORROSION. CABIN - FLOOR SEAT TRACK AT STATION 595 TO STATION 601 , X = - 47.5 CORROSION EVALUATED , FOUND EXFOLIATED AND EXCEEDED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMSDR FDEA202112153091Skin · crackedLEFT HAND WING # 8 SLAT LOWER SURFACE ( COVE PANEL ) ZONE 624 STATION XOS 1097 FOUND CRACK BETWEEN TRACK # 17 AND # 18. LEFT HAND WING # 8 SLAT LOWER SURFACE ( COVE PANEL ) ZONE 624 STATION XOS 1097 CRACKED BETWEEN TRACK # 17 AND # 18 REPAIR CARRIED OUT ASSDR FDEA2020051320928Wire · pulledSHORTLY AFTER T.O KIND RCVD LEVEL 1 ALERT "TAT PROB HEAT" FOLLWED QRH PROCEDURES AND DISCOVERED THE ASSOCIATED CIRCUIT BREAKER "POPPED". FOUND RED WIRE B608-3-20 PULLED OUT OF CONTACT #3 ON CONNECTOR P1-1032. REPLACED CONNECTOR SOCKET PER SMP. TAT PROBE SDR FDEA2020051320926Seal · damagedON CLIMB OUT OF KIND R'CVD LEVEL ONE ALERT"AIR SYS 1 OFF". FOLLOWED QRH PROCEDURES. INSTALLED NEW SEAL ON I/B SIDE OF ARROW COUPLING REPOSITIONED COUPLING LEAK CHECKED GOOD, REF AMM 36-14-05-2. ACCOMPLISHED PNEU SYS #1 DECAY CHECK REF AMM SDR FDEA2020032310597Hydraulic Line · leakingAFTER LANDING ROLLOUT RCVD LVL2 ALERT "HYD 2 FAIL" OBSERVED HYD QTY DRAIN TO ZERO. CONSULTED QRH. SHUT DOWN NO. 2 ENGINE. REPLACED DAMAGED PART OF #2 HYDRO SYSTEM RESERVOIR PRESSURE LINE IN AFT COMPT REF MD 11 AMM 20-10-01-2 NO LEAKS NOTEDSDR FDEA2019111532942Hinge · corrodedRIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE BARREL NUT HOLE SURFACE FOUND CORROSION. CORROSION AT RIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE BARREL NUT HOLE SURFACE REWORKED AS PER MD-11 CMM57-44-08 AND FOUND EXCEED LIMIT BASE THE DIFFERENSDR FDEA201911082910Support · corrodedLEFT WING - OUTBOARD FLAP VANE NUMBER 4 SUPPORT FITTING ECCENTRIC HOLE FOUND CORRODED. CORROSION AT LEFT WING - OUTBOARD FLAP VANE NUMBER 4 SUPPORT FITTING ECCENTRIC HOLE REWORKED BY MACHINING AND FOUND EXCEED LIMIT AS PER MD-11 SRM 57-50-02-2R REPAIR 5 SDR FDEA201911082909Support · corrodedLEFT WING - OUTBOARD FLAP VANE NUMBER 3 SUPPORT FITTING ECCENTRIC HOLE FOUND CORRODED. CORROSION AT LEFT WING - OUTBOARD FLAP VANE NUMBER 3 SUPPORT FITTING ECCENTRIC HOLE REWORKED BY MACHINING AND FOUND EXCEED LIMIT AS PER MD-11 SRM 57-50-02-2R REPAIR 5 SDR FDEA201911082908Support · corrodedLEFT WING - OUTBOARD FLAP VANE NUMBER 2 SUPPORT FITTING ECCENTRIC HOLE FOUND CORRODED. CORROSION AT LEFT WING - OUTBOARD FLAP VANE NUMBER 2 SUPPORT FITTING ECCENTRIC HOLE REWORKED BY MACHINING AND FOUND EXCEED LIMIT AS PER MD-11 SRM 57-50-02-2R REPAIR 5 SDR FDEA201911082911Support · corrodedRIGHT WING - OUTBOARD FLAP VANE NUMBER 1 SUPPORT FITTING ECCENTRIC HOLE FOUND CORRODED. CORROSION AT RIGHT WING - OUTBOARD FLAP VANE NUMBER 1 SUPPORT FITTING ECCENTRIC HOLE REWORKED BY MACHINING AND FOUND EXCEED LIMIT AS PER MD-11 SRM 57-50-02-2R REPAIR SDR FDEA2019110762892Doubler · corrodedLEFT WING UPPER WING SURFACE MAIN LANDING GEAR SUPPORT UPPER DOUBLER FOUND CORROSION AT XORS 254. LEFT WING UPPER WING SURFACE MAIN LANDING GEAR SUPPORT UPPER DOUBLER STATION XORS 254 CORROSION REMOVED AND FOUND EXCEEDED LIMIT AS PER SRM 57-20-01-1A ALLOWABLE SDR FDEA201911062895Hinge · corrodedLEFT WING FLAP SIDE OUTBOARD FLAP INBOARD HINGE PIVOT INBOARD LUG HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING FLAP SIDE OUTBOARD FLAP INBOARD HINGE PIVOT INBOARD LUG HOLE BORE REWORKED AND FOUND EXCEED LIMIT AS PER CMM57-52-04. OVERSIZED BUSHING FABRICSDR FDEA2019110762896Hinge · corrodedRIGHT WING FLAP SIDE OUTBOARD FLAP INBOARD HINGE PIVOT INBOARD LUG HOLE BORE FOUND CORROSION. CORROSION AT RIGHT WING FLAP SIDE OUTBOARD FLAP INBOARD HINGE PIVOT INBOARD LUG HOLE BORE REWORKED AND FOUND EXCEED LIMIT AS PER CMM57-52-04. OVERSIZED BUSHING FABRSDR FDEA2019110752861Seat Track · corrodedMAIN DECK FLOOR SEAT TRACK AT STATION 1190 X=-75.25 FOUND CORROSION. MAIN DECK FLOOR SEAT TRACK AT STATION 1190 X= -75.25 CORROSION REMOVED AND FOUND EXCEED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. ORIGINAL MATERIAL THICKNESS: 0.080 MATERISDR FDEA2019110752856Skin · delaminatedRIGHT WING TRAILING EDGE INBOARD ISLAND FORWARD EDGE UPPER SKIN LOWER SURFACE FINGER DOUBLER AT XW 392 FOUND DETACHED. REPAIR CARRIED OUT AT RIGHT WING TRAILING EDGE INBOARD ISLAND FORWARD EDGE UPPER SKIN LOWER SURFACE AT XW 392 IAW SRM 57-50-01-2R, FIGURE SDR FDEA2019110752865Seat Track · corrodedMAIN DECK FLOOR SEAT TRACK AT STATION 1475 X= 75.25 FOUND FLANGE CORROSION. MAIN DECK FLOOR SEAT TRACK AT STATION 1475 X= 75.25 FLANGE CORROSION REMOVED AND FOUND EXCEED LIMIT AS PER SRM 53-00-52-1A FIGURE101 ALLOWABLE DAMAGE 1. ORIGINAL MATERIAL THICKNESS:SDR FDEA2019110752864Seat Track · corrodedMAIN DECK FLOOR SEAT TRACK AT STATION 1571 TO STATION 1621 X=-107.25 FOUND CORROSION. MAIN DECK FLOOR SEAT TRACK AT STATION 1571 TO STATION 1621 X= -107.25 CORROSION REMOVED AND FOUND EXCEED LIMIT AS PER SRM 53-00-52-1A FIGURE101 ALLOWABLE DAMAGE 1. ORIGINALSDR FDEA2019110752863Seat 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 EXCEED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. ORIGINAL MATERIAL THICKNESS: 0.080 MATERIAL RSDR FDEA2019110752862Seat Track · corrodedMAIN DECK FLOOR SEAT TRACK AT STATION 1256 X=-75.25 FOUND CORROSION. MAIN DECK FLOOR SEAT TRACK AT STATION 1256 X= -75.25 CORROSION REMOVED AND FOUND EXCEED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. ORIGINAL MATERIAL THICKNESS: 0.080 MATERISDR FDEA201911152860Seat Track · corrodedMAIN DECK FLOOR SEAT TRACK AT STATION 475 X=-27.5 FOUND CORROSION. MAIN DECK FLOOR SEAT TRACK AT STATION 475 X= -27.5 FOUND EXFOLIATION CORROSION EXCEED LIMIT AS PER MD11 SRM 53-00-52-1A FIGURE101 ALLOWABLE DAMAGE 1. SEAT TRACK REPAIR CARRIED OUT AT STATSDR FDEA2019110752859Seat Track · damagedMAIN DECK FLOOR SEAT TRACK AT BS 755 X= 47.5 FOUND CROWN DAMAGED. MAIN DECK FLOOR SEAT TRACK CROWN DAMAGED AT BS 755 X= 47.5, DAMAGED AREA EVALUATED AND FOUND EXCEED LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. SEAT TRACK REPAIR CARRIED OUT IASDR FDEA2019110752858Seat Track · damagedMAIN DECK FLOOR SEAT TRACK AT 755 X=-47.5 FOUND CROWN DAMAGED. DAMAGED AREA EVALUATED AND FOUND EXCEED LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. SEAT TRACK REPAIR CARRIED OUT IAW SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED ASSDR FDEA2019110752857Seat Track · damagedMAIN DECK FLOOR SEAT TRACK AT BS 755 X=-27.5 FOUND CROWN DAMAGED. AREA EVALUATED AND FOUND TO EXCEED LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. SEAT TRACK REPAIR CARRIED OUT IAW SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED A
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