# Service difficulty reports: N606FE A list on [N606FE](https://openairdocs.org/aircraft/N606FE.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. Page 1 of 9 · 403 reports - [SDR FDEA202310011681](https://openairdocs.org/sdr/FDEA202310011681.md): Casting · cracked · Oct 1, 2023 · N606FE · Doug MD11F · Cargo/Baggage Doors > FWD 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 FDEA202309091569](https://openairdocs.org/sdr/FDEA202309091569.md): Tire · leaking · Sep 9, 2023 · N606FE · Doug MD11F · Tire > APPROX 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 FDEA202206021362](https://openairdocs.org/sdr/FDEA202206021362.md): Transducer · failed · Jun 2, 2022 · N606FE · Doug MD11F · Wheel/Ski/Float > RECEIVED 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 FDEA202201020004](https://openairdocs.org/sdr/FDEA202201020004.md): Hinge Bracket · corroded · Jan 2, 2022 · N606FE · Doug MD11F · Trailing Edge Flaps > RIGHT 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 M - [SDR FDEA202201020003](https://openairdocs.org/sdr/FDEA202201020003.md): Hinge Bracket · corroded · Jan 2, 2022 · N606FE · Doug MD11F · Trailing Edge Flaps > RIGHT 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 FDEA202201020002](https://openairdocs.org/sdr/FDEA202201020002.md): Hinge Bracket · corroded · Jan 2, 2022 · N606FE · Doug MD11F · Trailing Edge Flaps > LEFT 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 FDEA202201020001](https://openairdocs.org/sdr/FDEA202201020001.md): Hinge Bracket · corroded · Jan 2, 2022 · N606FE · Doug MD11F · Trailing Edge Flaps > LEFT 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-11 - [SDR FDEA202112263146](https://openairdocs.org/sdr/FDEA202112263146.md): Fitting · cracked · Dec 26, 2021 · N606FE · Doug MD11F · Vertical Stabilizer > DURING 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 FROM - [SDR FDEA202112263145](https://openairdocs.org/sdr/FDEA202112263145.md): Fitting · cracked · Dec 26, 2021 · N606FE · Doug MD11F · Vertical Stabilizer > DURING 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 FDEA202112263147](https://openairdocs.org/sdr/FDEA202112263147.md): Floor Support · corroded · Dec 26, 2021 · N606FE · Doug MD11F · Fuselage Miscellaneous Structure > UPON 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 FOU - [SDR FDEA202112263144](https://openairdocs.org/sdr/FDEA202112263144.md): Floor Support · corroded · Dec 26, 2021 · N606FE · Doug MD11F · Fuselage Miscellaneous Structure > LOWER 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. CORRO - [SDR FDEA202112263143](https://openairdocs.org/sdr/FDEA202112263143.md): Web · cracked · Dec 26, 2021 · N606FE · Doug MD11F · Fuselage Floor Panel > LOWER 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 FDEA202112263141](https://openairdocs.org/sdr/FDEA202112263141.md): Skin · cracked · Dec 26, 2021 · N606FE · Doug MD11F · Wing, Plate/Skin > RIGHT 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 FDEA202112263149](https://openairdocs.org/sdr/FDEA202112263149.md): Panel · delaminated · Dec 26, 2021 · N606FE · Doug MD11F · Fuselage Floor Panel > CABIN 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 271EF - [SDR FDEA202112263148](https://openairdocs.org/sdr/FDEA202112263148.md): Panel · delaminated · Dec 26, 2021 · N606FE · Doug MD11F · Fuselage Floor Panel > CABIN 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 #232DF - [SDR FDEA202112263142](https://openairdocs.org/sdr/FDEA202112263142.md): Panel · delaminated · Dec 26, 2021 · N606FE · Doug MD11F · Fuselage Floor Panel > CABIN 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 FDEA202112243136](https://openairdocs.org/sdr/FDEA202112243136.md): Hinge Bracket · corroded · Dec 24, 2021 · N606FE · Doug MD11F · Trailing Edge Flaps > RIGHT 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 BUSHIN - [SDR FDEA202112243135](https://openairdocs.org/sdr/FDEA202112243135.md): Hinge Bracket · corroded · Dec 24, 2021 · N606FE · Doug MD11F · Trailing Edge Flaps > LEFT 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 FDEA202112243134](https://openairdocs.org/sdr/FDEA202112243134.md): Hinge Bracket · corroded · Dec 24, 2021 · N606FE · Doug MD11F · Trailing Edge Flaps > RIGHT 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 57 - [SDR FDEA202112243133](https://openairdocs.org/sdr/FDEA202112243133.md): Hinge Bracket · corroded · Dec 24, 2021 · N606FE · Doug MD11F · Trailing Edge Flaps > RIGHT 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 57-5 - [SDR FDEA202112243132](https://openairdocs.org/sdr/FDEA202112243132.md): Hinge Bracket · corroded · Dec 24, 2021 · N606FE · Doug MD11F · Trailing Edge Flaps > LEFT 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 FDEA202112243131](https://openairdocs.org/sdr/FDEA202112243131.md): Hinge Bracket · corroded · Dec 24, 2021 · N606FE · Doug MD11F · Trailing Edge Flaps > LEFT 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 FDEA202112233129](https://openairdocs.org/sdr/FDEA202112233129.md): Skin · cracked · Dec 23, 2021 · N606FE · Doug MD11F · Wing, Control Surfaces > LEFT 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 AS - [SDR FDEA202112233128](https://openairdocs.org/sdr/FDEA202112233128.md): Doubler · cracked · Dec 23, 2021 · N606FE · Doug MD11F · Wing, Plate/Skin > LEFT 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 INNE - [SDR FDEA202112233127](https://openairdocs.org/sdr/FDEA202112233127.md): Doubler · cracked · Dec 23, 2021 · N606FE · Doug MD11F · Wing, Plate/Skin > LEFT 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 INNE - [SDR FDEA202112233126](https://openairdocs.org/sdr/FDEA202112233126.md): Doubler · cracked · Dec 23, 2021 · N606FE · Doug MD11F · Wing, Plate/Skin > LEFT 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 INNE - [SDR FDEA202112223117](https://openairdocs.org/sdr/FDEA202112223117.md): Seat Track · corroded · Dec 22, 2021 · N606FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings > CABIN 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 FDEA202112223116](https://openairdocs.org/sdr/FDEA202112223116.md): Seat Track · corroded · Dec 22, 2021 · N606FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings > CABIN - 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 DAM - [SDR FDEA202112153091](https://openairdocs.org/sdr/FDEA202112153091.md): Skin · cracked · Dec 15, 2021 · N606FE · Doug MD11F · Wing, Control Surfaces > LEFT 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 AS - [SDR FDEA2020051320928](https://openairdocs.org/sdr/FDEA2020051320928.md): Wire · pulled · May 12, 2020 · N606FE · Doug MD11F · Ice/Rain Protection System Wiring > SHORTLY 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 FDEA2020051320926](https://openairdocs.org/sdr/FDEA2020051320926.md): Seal · damaged · May 12, 2020 · N606FE · Doug MD11F · Pneumatic Distribution System > ON 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 FDEA2020032310597](https://openairdocs.org/sdr/FDEA2020032310597.md): Hydraulic Line · leaking · Mar 21, 2020 · N606FE · Doug MD11F · Hydraulic System, Main > AFTER 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 NOTED - [SDR FDEA2019111532942](https://openairdocs.org/sdr/FDEA2019111532942.md): Hinge · corroded · Nov 13, 2019 · N606FE · Doug MD11F · Wing, Control Surface Attach Fittings > RIGHT 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 DIFFEREN - [SDR FDEA201911082910](https://openairdocs.org/sdr/FDEA201911082910.md): Support · corroded · Nov 8, 2019 · N606FE · Doug MD11F · Trailing Edge Flaps > LEFT 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 FDEA201911082909](https://openairdocs.org/sdr/FDEA201911082909.md): Support · corroded · Nov 8, 2019 · N606FE · Doug MD11F · Trailing Edge Flaps > LEFT 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 FDEA201911082908](https://openairdocs.org/sdr/FDEA201911082908.md): Support · corroded · Nov 8, 2019 · N606FE · Doug MD11F · Trailing Edge Flaps > LEFT 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 FDEA201911082911](https://openairdocs.org/sdr/FDEA201911082911.md): Support · corroded · Nov 8, 2019 · N606FE · Doug MD11F · Trailing Edge Flaps > RIGHT 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 FDEA2019110762892](https://openairdocs.org/sdr/FDEA2019110762892.md): Doubler · corroded · Nov 6, 2019 · N606FE · Doug MD11F · Wing, Plate/Skin > LEFT 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 FDEA201911062895](https://openairdocs.org/sdr/FDEA201911062895.md): Hinge · corroded · Nov 6, 2019 · N606FE · Doug MD11F · Trailing Edge Flaps > LEFT 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 FABRIC - [SDR FDEA2019110762896](https://openairdocs.org/sdr/FDEA2019110762896.md): Hinge · corroded · Nov 6, 2019 · N606FE · Doug MD11F · Trailing Edge Flaps > RIGHT 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 FABR - [SDR FDEA2019110752861](https://openairdocs.org/sdr/FDEA2019110752861.md): Seat Track · corroded · Nov 5, 2019 · N606FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings > MAIN 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 MATERI - [SDR FDEA2019110752856](https://openairdocs.org/sdr/FDEA2019110752856.md): Skin · delaminated · Nov 5, 2019 · N606FE · Doug MD11F · Wing, Plate/Skin > RIGHT 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 FDEA2019110752865](https://openairdocs.org/sdr/FDEA2019110752865.md): Seat Track · corroded · Nov 5, 2019 · N606FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings > MAIN 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 FDEA2019110752864](https://openairdocs.org/sdr/FDEA2019110752864.md): Seat Track · corroded · Nov 5, 2019 · N606FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings > MAIN 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. ORIGINAL - [SDR FDEA2019110752863](https://openairdocs.org/sdr/FDEA2019110752863.md): Seat Track · corroded · Nov 5, 2019 · N606FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings > MAIN 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 R - [SDR FDEA2019110752862](https://openairdocs.org/sdr/FDEA2019110752862.md): Seat Track · corroded · Nov 5, 2019 · N606FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings > MAIN 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 MATERI - [SDR FDEA201911152860](https://openairdocs.org/sdr/FDEA201911152860.md): Seat Track · corroded · Nov 5, 2019 · N606FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings > MAIN 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 STAT - [SDR FDEA2019110752859](https://openairdocs.org/sdr/FDEA2019110752859.md): Seat Track · damaged · Nov 5, 2019 · N606FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings > MAIN 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 IA - [SDR FDEA2019110752858](https://openairdocs.org/sdr/FDEA2019110752858.md): Seat Track · damaged · Nov 5, 2019 · N606FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings > MAIN 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 AS - [SDR FDEA2019110752857](https://openairdocs.org/sdr/FDEA2019110752857.md): Seat Track · damaged · Nov 5, 2019 · N606FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings > MAIN 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 Next page: https://openairdocs.org/aircraft/N606FE/reports.md?page=2 ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql 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 ``` This list as a web page: https://openairdocs.org/aircraft/N606FE/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.