# Service difficulty reports: N616FE

A list on [N616FE](https://openairdocs.org/aircraft/N616FE.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 6 · 267 reports

- [SDR FDEA202312141937](https://openairdocs.org/sdr/FDEA202312141937.md): Unknown · unknown · Dec 14, 2023 · N616FE · Doug MD11F · Fire Protection System Wiring
  > ON CLIMB OUT WE GOT AN INTERMITTENT FIRE DET 2 FAULT AND AN INTERMITTENT FIRE INDICATION ON #2 ENGINE INCLUDING FIRE WARNING BELL AND RED LIGHTS IN #2 FIRE HANDLE AND #2 FUEL LEVER. FIRE INDICATIONS HAPPENED TWICE AND LASTED ABOUT 1 SECOND. ALL ENGINE IND
- [SDR FDEA202307031139](https://openairdocs.org/sdr/FDEA202307031139.md): Switch · failed · Jul 3, 2023 · N616FE · Doug MD11F · Fuel Indicating System
  > LEVEL 2 FUEL QTY/USED CHK ALERT OCCURRED WHILE FUEL SYSTEM IN AUTO AND WAS TRANSFERRING FUEL TO FILL THE WING TANKS. FLIGHT DID A MAINTENANCE DIVERSION TO IAD, EMERGENCY DECLARED. ACCOMPD A/C EXTERIOR INSPECTION. NO FUEL LEAKAGE NOTED. ACCOMPLISHED FSC FAU
- [SDR FDEA202209112284](https://openairdocs.org/sdr/FDEA202209112284.md): None · none · Sep 11, 2022 · N616FE · Doug MD11F · Standard Practices/Structures
  > EXISTING REPAIR AT LOWER FUSELAGE SKIN RIGHT HAND SIDE STATION 1191 BETWEEN LONGERON 46 RIGHT TO LONGERON 47 RIGHT REQUIRES REPLACEMENT (REFER M MOD NUMBER: SRM000078194N90 & WRI 53102005) LOWER FUSELAGE SKIN RIGHT HAND SIDE STATION 1191 BETWEEN LONGERO
- [SDR FDEA202209082253](https://openairdocs.org/sdr/FDEA202209082253.md): Support · corroded · Sep 8, 2022 · N616FE · Doug MD11F · Fuselage Miscellaneous Structure
  > CENTER CARGO - FORWARD SUPPORT CHORD STATION 1841 X = 11 FOUND CORROSION CENTER CARGO - FORWARD SUPPORT CHORD STATION 1841 X = 11 CORROSION REMOVED AS PER SRM 51-21-01-0G AND FOUND EXCEED LIMIT AS PER SRM 53-00-00-2R FIGURE 206 REPAIR GENERAL. SUPPORT CH
- [SDR FDEA202209082252](https://openairdocs.org/sdr/FDEA202209082252.md): Longeron Splice · cracked · Sep 8, 2022 · N616FE · Doug MD11F · Fuselage Main, Longeron/Stringer
  > CENTER CARGO - BILGE STATION 5-113 TO STATION 1541 LONGERON 50 RIGHT SPLICE FOUND CRACKED CENTER CARGO - BILGE STATION 5-113 TO STATION 1541 LONGERON 50 RIGHT CRACKED SPLICE REMOVED AND REPLACED WITH FABRICATED MACHINED SPLICE AS PER SRM 51-33-01- 0G. SPL
- [SDR FDEA202209082251](https://openairdocs.org/sdr/FDEA202209082251.md): Longeron Splice · cracked · Sep 8, 2022 · N616FE · Doug MD11F · Fuselage Main, Longeron/Stringer
  > CENTER CARGO - BILGE STATION 5-113 TO STATION 1541 LONGERON 50 LEFT SPLICE FOUND CRACKED CENTER CARGO - BILGE STATION 5-113 TO STATION 1541 LONGERON 50 LEFT CRACKED SPLICE REMOVED AND REPLACED WITH FABRICATED MACHINED SPLICE AS PER SRM 51-33-01- 0G. SPLIC
- [SDR FDEA202209072230](https://openairdocs.org/sdr/FDEA202209072230.md): Panel Latch · delaminated · Sep 7, 2022 · N616FE · Doug MD11F · Fuselage Floor Panel
  > CABIN - MAIN DECK CARGO COMPARTMENT FLOOR PANEL #231GF BELOW BALLMAT AREA FOUND DELAMINATED AT ( STATION 595 TO STATION 675) DELAMINATED FLOOR PANEL #231GF AT MAIN DECK STATION 595 - STATION 675 REMOVED AS PER AMM 53-21-04. FLOOR PANEL #231GF FABRICATED A
- [SDR FDEA202209072229](https://openairdocs.org/sdr/FDEA202209072229.md): Floor Panel · damaged · Sep 7, 2022 · N616FE · Doug MD11F · Fuselage Floor Panel
  > CABIN - MAIN DECK CARGO COMPARTMENT FLOOR PANEL #233FF BELOW BALLMAT AREA FOUND FORWARD EDGE BROKEN AT ( STATION 575 TO STATION 735) FLOOR PANEL #233FF WITH FORWARD BROKEN EDGE AT MAIN DECK STATION 575 - STATION 735 REMOVED AS PER AMM 53-21-04. FLOOR PANE
- [SDR FDEA202209072228](https://openairdocs.org/sdr/FDEA202209072228.md): Floor Panel · delaminated · Sep 7, 2022 · N616FE · Doug MD11F · Fuselage Floor Panel
  > CABIN - MAIN DECK CARGO COMPARTMENT FLOOR PANEL #231HF BELOW BALLMAT AREA FOUND DELAMINATED AT ( STATION 595 - STATION 675) DELAMINATED FLOOR PANEL #231HF AT MAIN DECK STATION 595 - STATION 675 REMOVED AS PER AMM 53-21-04. FLOOR PANEL #231HF FABRICATED AS
- [SDR FDEA202209052199](https://openairdocs.org/sdr/FDEA202209052199.md): Skin · delaminated · Sep 5, 2022 · N616FE · Doug MD11F · Wing, Plate/Skin
  > RIGHT HAND WING TRAILING EDGE INBOARD ISLAND UPPER SKIN INTERNAL FINGER DOUBLER FOUND DETACH AT STATION XW 390. RIGHT HAND WING TRAILING EDGE INBOARD ISLAND UPPER SKIN AT STATION XW 390 REPAIR CARRIED OUT AS PER SRM 57-50-01-2R REPAIR 6 FIGURE 203. REPAIR
- [SDR FDEA202209052200](https://openairdocs.org/sdr/FDEA202209052200.md): Skin · dented · Sep 5, 2022 · N616FE · Doug MD11F · Trailing Edge Flaps
  > LEFT HAND WING TRAILING EDGE INBOARD FLAP UPPER SKIN FOUND WITH DENT AT STATION XIFH 231 LEFT HAND WING TRAILING EDGE INBOARD FLAP UPPER SKIN AT STATION XIFH 231 REPAIR CARRIED OUT AS PER SRM 57-00-01-2R RPAIR 2 FIGURE 201 AND EA: 1-5750-T0370697 P1 TIT
- [SDR FDEA202209052201](https://openairdocs.org/sdr/FDEA202209052201.md): Trunnion · cracked · Sep 5, 2022 · N616FE · Doug MD11F · Fuselage, Landing Gear Attach Fittings
  > HIGH FREQUENCY EDDY CURRENT INSPECTION ON LEFT HAND NOSE LANDING GEAR TRUNION FITTING STATION Y = 585 EXISTING TRIMMED OUT AREA FOUND CRACK APPROXIMATE 0.2" CRACK APPROXIMATE 0.2" FOUND AT LEFT HAND NOSE LANDING GEAR TRUNION FITTING STATION Y = 585 REPAI
- [SDR FDEA202209052198](https://openairdocs.org/sdr/FDEA202209052198.md): Skin · cracked · Sep 5, 2022 · N616FE · Doug MD11F · Wing, Plate/Skin
  > 03 EACH FASTENER HOLES #12, #35, #36 FOUND CRACK INDICATION DURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION AT LEFT HAND WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STATION XORS = 683.4 AND STATION XORS = 713.6 LEFT HAND WING LOWER SKIN ACCESS DOO
- [SDR FDEA202209052197](https://openairdocs.org/sdr/FDEA202209052197.md): Skin · cracked · Sep 5, 2022 · N616FE · Doug MD11F · Wing, Plate/Skin
  > 05 EACH FASTENER HOLES #12, #14, #16, #17, #36 FOUND CRACK INDICATION DURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION AT RIGHT HAND WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STATION XORS = 683.4 AND STATION XORS = 713.6 RIGHT HAND WING LOWER S
- [SDR FDEA202209032147](https://openairdocs.org/sdr/FDEA202209032147.md): Skin · cracked · Sep 3, 2022 · N616FE · Doug MD11F · Fuselage Main, Plate/Skin
  > FUSELAGE: RIGHT HAND AIRCON COMPARTMENT SERVICE DOOR CUTOUT UPPER AFT CORNER FOUND CRACKED AT STATION 535 LONGERON 33 RIGHT FUSELAGE: RIGHT HAND AIRCON COMPARTMENT SERVICE DOOR CUTOUT UPPER AFT CORNER AT STATION 535 LONGERON 33 RIGHT REPAIR CARRIED OUT A
- [SDR FDEA202209022143](https://openairdocs.org/sdr/FDEA202209022143.md): Longeron Splice · cracked · Sep 2, 2022 · N616FE · Doug MD11F · Fuselage Main, Longeron/Stringer
  > AFT CARGO - RIGHT HAND TUNNEL STATION 1863.125 - STATION 1871 LONGERON 38 RIGHT SPLICE FOUND CRACKED AFT CARGO - RIGHT HAND TUNNEL STATION 1863.125 - STATION 1871 LONGERON 38 RIGHT CRACKED SPLICE REMOVED AND REPLACED WITH FABRICATED MACHINED SPLICE AS PER
- [SDR FDEA202209022142](https://openairdocs.org/sdr/FDEA202209022142.md): Seat Track · worn · Sep 2, 2022 · N616FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > CABIN - MAIN DECK CARGO COMPARTMENT FLOOR SEAT TRACK AT STATION 5-5, X = - 8.5 FOUND CROWN WORN CABIN - MAIN DECK CARGO COMPARTMENT FLOOR SEAT TRACK AT STATION 5-5, X = - 8.5 CROWN WORN MARK REMOVED AND FOUND EXCEED LIMIT AS PER SRM 53-00-52-1A FIGURE 10
- [SDR FDEA202209022140](https://openairdocs.org/sdr/FDEA202209022140.md): Seat Track · cracked · Sep 2, 2022 · N616FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > CABIN - SEAT TRACK STATION 755 X = 8.5 FOUND CRACKED CABIN CRACKED SEAT TRACK AT STATION 755 X = 8.5 REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM EXISTING SPLICE STATION 625 TO STATION 765 X = 8.5 AS PER SRM 53-00- 52-2R FIGURE 201 REPAIR 1. REPAIR CLA
- [SDR FDEA202209022141](https://openairdocs.org/sdr/FDEA202209022141.md): Seat Track · worn · Sep 2, 2022 · N616FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > CABIN - MAIN DECK CARGO COMPARTMENT FLOOR SEAT TRACK AT STATION 5-5, X = - 47 FOUND CROWN WORN CABIN - MAIN DECK CARGO COMPARTMENT FLOOR SEAT TRACK CROWN AT STATION 5-5 X = - 47 WORN MARK REMOVED AND FOUND EXCEED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 A
- [SDR FDEA202209012132](https://openairdocs.org/sdr/FDEA202209012132.md): Frame · chafed · Sep 1, 2022 · N616FE · Doug MD11F · Fuselage Main, Frame
  > CABIN - MAIN DECK CARGO COMPARTMENT LEFT HAND FRAME STATION 535 BETWEEN LONGERON 22 - LONGERON 25 LEFT HAND EXISTING REPAIR LOWER FOUND HAVE CHAFFING MARKS. CABIN - MAIN DECK CARGO COMPARTMENT LEFT HAND FRAME STATION 535 LOWER EXISTING OUTER REPAIR ANGLE
- [SDR FDEA202209012131](https://openairdocs.org/sdr/FDEA202209012131.md): Frame · chafed · Sep 1, 2022 · N616FE · Doug MD11 · Fuselage Main, Frame
  > CABIN - MAIN DECK CARGO COMPARTMENT LEFT HAND FRAME STATION 535 BETWEEN LONGERON 18 - LONGERON 21 LEFT HAND EXISTING REPAIR UPPER FOUND HAVE CHAFFING MARKS. CABIN - MAIN DECK CARGO COMPARTMENT LEFT HAND FRAME STATION 535 UPPER EXISTING OUTER REPAIR ANGLE
- [SDR FDEA202209012130](https://openairdocs.org/sdr/FDEA202209012130.md): Doubler · cracked · Sep 1, 2022 · N616FE · Doug MD11F · Wing, Plate/Skin
  > RIGHT HAND WING FIXED LEADING EDGE SKIN INTERNAL BEADED DOUBLER FOUND CRACK AT STATION XOS 817. RIGHT HAND WING FIXED LEADING EDGE SKIN INTERNAL DOUBLER AT STATION XOS 817 REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS
- [SDR FDEA202209012129](https://openairdocs.org/sdr/FDEA202209012129.md): Doubler · cracked · Sep 1, 2022 · N616FE · Doug MD11F · Wing, Plate/Skin
  > RIGHT HAND WING FIXED LEADING EDGE SKIN INTERNAL BEADED DOUBLER FOUND CRACK AT STATION XOS 638. RIGHT HAND WING FIXED LEADING EDGE SKIN INTERNAL DOUBLER AT STATION XOS 638 REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS
- [SDR FDEA202209012128](https://openairdocs.org/sdr/FDEA202209012128.md): Doubler · cracked · Sep 1, 2022 · N616FE · Doug MD11F · Wing, Plate/Skin
  > RIGHT HAND WING FIXED LEADING EDGE SKIN INTERNAL BEADED DOUBLER FOUND CRACK AT STATION XOS 545. RIGHT HAND WING FIXED LEADING EDGE SKIN INTERNAL DOUBLER AT STATION XOS 545 REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS
- [SDR FDEA202209012127](https://openairdocs.org/sdr/FDEA202209012127.md): Doubler · cracked · Sep 1, 2022 · N616FE · Doug MD11F · Wing, Plate/Skin
  > RIGHT HAND WING FIXED LEADING EDGE SKIN INTERNAL BEADED DOUBLER FOUND CRACK AT STATION XOS 708. RIGHT HAND WING FIXED LEADING EDGE SKIN INTERNAL DOUBLER AT STATION XOS 708 REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS
- [SDR FDEA202209012126](https://openairdocs.org/sdr/FDEA202209012126.md): Doubler · cracked · Sep 1, 2022 · N616FE · Doug MD11F · Wing, Plate/Skin
  > LEFT HAND WING FIXED LEADING EDGE SKIN INTERNAL BEADED DOUBLER FOUND CRACK AT STATION XOS 738. LEFT HAND WING FIXED LEADING EDGE SKIN INTERNAL DOUBLER AT STATION XOS 738 REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS M
- [SDR FDEA202205141207](https://openairdocs.org/sdr/FDEA202205141207.md): Warning Light · false activation · May 14, 2022 · N616FE · Doug MD11F · Landing Gear Position and Warning
  > MDIS 616 32-60 1759 14MAY22 ANC FACT U UNSAFE RT MAIN GEAR INDICATION ON BOTH LIGHT AND CONFIG DISP. CYCLED GEAR PER QRH SHOWED UP/LOCKED. PER CAPT FACT 14MAY22 16:17 ANC U INSPECTED RIGHT MAIN GEAR. THE UPLOCK HOOK AND SENSORS. DOOR REM
- [SDR FDEA202203280721](https://openairdocs.org/sdr/FDEA202203280721.md): Hinge · corroded · Mar 28, 2022 · N616FE · Doug MD11F · Fuselage, Door Hinge
  > B CHECK #135 REV NO. PS ACCOMPLISH MAINTENANCE "B" CHECK - REP INSPECTION #135 NOTE: DURING B-CHK INSPECTION FOR THE FWD LOWER CARGO DOOR. THE UPPER HINGE WAS FOUND WORN AND CORRODED. THIS ISSUE WAS GENERATED ON NON ROUTINE N00027. UPPER HINGE REPLAC
- [SDR FDEA202108312169](https://openairdocs.org/sdr/FDEA202108312169.md): Power Supply · no test · Aug 31, 2021 · N616FE · Doug MD11F · Emergency Lighting
  > WHEN TESTING EMERGENCY LIGHTS RECEIVED LEVEL 1 EMER LT BAT 1 LO RELEASED FOR SERVICE PER MEL: 33-50-04 CATEGORY: C EXPIRATION: 04SEP21 "MEL 33-50-04: EMER LIGHTS - INOP. R/R'D EMERGENCY LIGHTING POWRSUPPLY MPN: 60-4411-5; S/N ON IS 0106
- [SDR FDEA202009172232](https://openairdocs.org/sdr/FDEA202009172232.md): Bearing · migrated · Sep 17, 2020 · N616FE · Doug MD11F · Engine Mount Section
  > ENGINE NR 3 PYLON AFT MOUNT BEARING FOUND MIGRATED. ENGINE NR 3 PYLON AFT BULKHEAD AT STATION YWN 418.162. REMOVED AND REPLACED, AS PER MD-11 SRM 54-01-42-OG AND DOUGLAS DRAWING NR AUB 7500 REV ' AS '. REPAIR CLASSIFIED AS MAJOR, PER GMM 6-2-100. REFER TO
- [SDR FDEA202009162224](https://openairdocs.org/sdr/FDEA202009162224.md): Former · cracked · Sep 16, 2020 · N616FE · Doug MD11F · Wing Main, Frame Structure
  > LEFT HAND WING - LEADING EDGE FORMER AT APPROXIMATELY XORS 980, BEHIND #8 SLAT CENTER AREA, FOUND CRACKED AS MARKED. LEFT HAND WING LEADING EDGE FORMER AT APPROXIMATELY XORS 980, BEHIND #8 SLAT CENTER AREA REMOVED AND REPLACED WITH FABRICATED FORMER AS
- [SDR FDEA202009162223](https://openairdocs.org/sdr/FDEA202009162223.md): Former · cracked · Sep 16, 2020 · N616FE · Doug MD11F · Wing Main, Frame Structure
  > RIGHT HAND WING, FIXED LEADING EDGE FORMER BETWEEN XOS 1010-1030, BEHIND NR 8 SLAT INBOARD SIDE, FOUND CRACKED AS MARKED. RIGHT HAND WING FIXED LEADING EDGE CRACKED FORMER BETWEEN XOS 1010-1030, BEHIND NR 8 SLAT INBOARD SIDE. REMOVED AND REPLACED WITH FABRIC
- [SDR FDEA202009152213](https://openairdocs.org/sdr/FDEA202009152213.md): Doubler · cracked · Sep 15, 2020 · N616FE · Doug MD11F · Wing, Plate/Skin
  > AGING AIRCRAFT, EXISTING REPAIR FOUND AT RT WING FIXED LEADING EDGE LOWER SURFACE BETWEEN XOS 890 TO XOS 910. EXISTING REPAIR AT RT WING FIXED LEADING EDGE LOWER SURFACE BETWEEN XOS 890 TO XOS 910 EVALUATED AND FOUND REPAIRED IAW SRM 57-40-03-2R REPAIR 1 FI
- [SDR FDEA202009142194](https://openairdocs.org/sdr/FDEA202009142194.md): Skin · cracked · Sep 14, 2020 · N616FE · Doug MD11F · Wing, Plate/Skin
  > 01 EACH FASTENER HOLES #16 FOUND CRACK INDICATION DURING OPEN-HOLE HFEC INSPECTION AT LEFT HAND WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STATION XORS=690 AND STATION XORS=700. LEFT HAND WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STATION XORS = 690 AND
- [SDR FDEA202009142193](https://openairdocs.org/sdr/FDEA202009142193.md): Skin · cracked · Sep 14, 2020 · N616FE · Doug MD11F · Wing, Plate/Skin
  > 01 EACH FASTENER HOLES #14 FOUND CRACK INDICATION DURING OPEN-HOLE HFEC INSPECTION AT LEFT HAND WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STATION XORS=690 AND STATION XORS=700. LEFT HAND WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STATION XORS = 690 AND
- [SDR FDEA202009142192](https://openairdocs.org/sdr/FDEA202009142192.md): Skin · cracked · Sep 14, 2020 · N616FE · Doug MD11F · Wing, Plate/Skin
  > 01 EACH FASTENER HOLES #13 FOUND CRACK INDICATION DURING OPEN-HOLE HFEC INSPECTION AT LEFT HAND WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STATION XORS=690 AND STATION XORS=700. LEFT HAND WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STATION XORS = 690 AND
- [SDR FDEA202009142198](https://openairdocs.org/sdr/FDEA202009142198.md): Seat Track · corroded · Sep 14, 2020 · N616FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK-UPON OPEN UP FLOOR PANEL FOR MODIFICATION, SEAT TRACK AT STATION 1700 X= -107.25 FOUND CORROSION AS MARKED. MAIN DECK RIGHT STATION 1700 X= -107.25 SEAT TRACK CORROSION REMOVED AND FOUND TO EXCEED LIMIT, AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE D
- [SDR FDEA202009122179](https://openairdocs.org/sdr/FDEA202009122179.md): Seat Track · corroded · Sep 12, 2020 · N616FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > CABIN LEFT HAND STATION 1425 X=47.5 SEAT TRACK FOUND CORROSION AS MARKED. CABIN LEFT HAND STATION 1425 X=47.5 SEAT TRACK CORROSION FOUND EXFLOLIATED AND EXCEED LIMIT, AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CORRODED SEAT TRACK REPAIRED BY SECTI
- [SDR FDEA202009092155](https://openairdocs.org/sdr/FDEA202009092155.md): Seat Track · corroded · Sep 9, 2020 · N616FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > CABIN - LEFT HAND STATION 6-12 X = 27.5 SEAT TRACK FOUND CORROSION AS MARKED. CABIN LEFT HAND STATION 6-12 X=27.5 SEAT TRACK CORROSION REMOVED AND FOUND TO EXCED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CORRODED SEAT TRACK REPAIRED B
- [SDR FDEA202009092154](https://openairdocs.org/sdr/FDEA202009092154.md): Seat Track · worn · Sep 9, 2020 · N616FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > CABIN RIGHT STATION 1421 X= -8.5 SEAT TRACK CROWN FOUND WORN, AS MARKED. CABIN RIGHT HAND STATION 1421 X= - 8.5 SEAT TRACK CROWN WORN AREA SMOOTHED OUT AND FOUND TO EXCEED LIMIT, AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. WORN SEAT TRACK REPAIRED
- [SDR FDEA202009082143](https://openairdocs.org/sdr/FDEA202009082143.md): Seat Track · corroded · Sep 8, 2020 · N616FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > CABIN, LEFT STATION 1551 X=8.5 SEAT TRACK FOUND CORROSION. CABIN LEFT HAND STATION 1551 X=8.5 SEAT TRACK CORROSION REMOVED AND FOUND TO EXCEED LIMIT, AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CORRODED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK R
- [SDR FDEA202009082142](https://openairdocs.org/sdr/FDEA202009082142.md): Seat Track · corroded · Sep 8, 2020 · N616FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > CABIN, LEFT STATION 1530 X=8.5 SEAT TRACK FOUND CORROSION. CABIN LEFT HAND STATION 1530 X=8.5 SEAT TRACK CORROSION REMOVED AND FOUND TO EXCEED LIMIT, AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CORRODED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK
- [SDR FDEA202007021430](https://openairdocs.org/sdr/FDEA202007021430.md): Unknown · malfunctioned · Jul 2, 2020 · N616FE · Doug MD11F · Hydraulic System, Main
  > LEVEL 1 HYD 1 OFF. QTY 7.5 TEMP 77 C SYS 2&3 TEMPS 43 AND 36 DEGRESS RESPECTIVELY.
- [SDR FDEA201911042853](https://openairdocs.org/sdr/FDEA201911042853.md): Hydraulic Line · leaking · Nov 4, 2019 · N616FE · Doug MD11F · Hydraulic System, Main
  > PDIS 616 29-02 8465 03NOV19 EWR FACT U LOGPAGES:3153051 RECEIVED AT CRUISE "HYD 3 ELEV OFF" ALERT LEV1. QTY HYD 3 WAS 5.9 WELL BELOW CYAN LINE.FOLLOWED QRH.QTY CONTINUED TO DECREASE TO 2.4 THEN AUTO SHUT DOWN. #3 HYD SYSTEM WENT DOWN TO 2.0 S
- [SDR FDEA201812133497](https://openairdocs.org/sdr/FDEA201812133497.md): Switch · failed · Dec 13, 2018 · N616FE · Doug MD11F · Door Warning System
  > THE "CABIN DOOR FWD R" LEVEL 1 ALERT WILL NOT GO AWAY AFTER ARMING R1. THE "DOOR DISARM" LIGHT BY R1 EXTINGUISHES. REPLACED R1 DOOR DOWN LIMIT SWITCH. DOOR WARNING SYS OPS NORMAL.
- [SDR FDEA201810313063](https://openairdocs.org/sdr/FDEA201810313063.md): Transmitter · failed · Oct 31, 2018 · N616FE · Doug MD11F · Tire
  > "TIRE FAIL" ANNUNCIATED WHEN LEVELING AT FL350 LEFT NOSE WHEEL INDICATED LOW PRESS THEN TIRE FAIL. REMOVED AND REPLACED LT NOSE WHEEL TIRE PRESS TRANS, REF AMM 32-46-04-4, OPS CHKD GOOD.
- [SDR FDEA201809142546](https://openairdocs.org/sdr/FDEA201809142546.md): Fitting · corroded · Sep 14, 2018 · N616FE · Doug MD11F · Trailing Edge Flaps
  > RT O/B FLAP VANE HORN FITTING "F" FOUND HOLE BORE CORROSION. RT O/B FLAP VANE HORN FITTING 'F' HOLE BORE REWORKED AND FOUND EXCEED LIMIT AS PER SRM 57-50-02-2R FIGURE 201 REPAIR 5. OVERSIZED BUSHING FABRICATED AS PER EA 1-5750-T0342271 PART 1 STEP 1B. REPAIR C
- [SDR FDEA201809142545](https://openairdocs.org/sdr/FDEA201809142545.md): Fitting · corroded · Sep 14, 2018 · N616FE · Doug MD11F · Trailing Edge Flaps
  > RT O/B FLAP VANE HORN FITTING "E" FOUND HOLE BORE CORROSION. RT O/B FLAP VANE HORN FITTING 'E' HOLE BORE REWORKED BY MACHINING AND FOUND EXCEED LIMIT AS PER SRM 57-50-02-2R FIGURE 201 REPAIR 5. OVERSIZED BUSHING FABRICATED AS PER EA 1-5750-T0342271 PART 1 ST
- [SDR FDEA201809142544](https://openairdocs.org/sdr/FDEA201809142544.md): Hinge Bracket · corroded · Sep 14, 2018 · N616FE · Doug MD11F · Wing, Control Surface Attach Fittings
  > LT WING O/B FLAP O/B FWD (WING SIDE) HINGE BARREL NUT HOLE SURFACE CORROSION. HINGE BARREL NUT HOLE SURFACE REWORKED AS PER CMM 57-44-09, REPAIR SHIM FABRICATED AND INSTALLED AS PER CMM 57-44-09 AND EA 1-5750-T0342161 P1 STEP 2. REPAIR CLASSIFIED AS MINOR PER
- [SDR FDEA201809142543](https://openairdocs.org/sdr/FDEA201809142543.md): Hinge Bracket · corroded · Sep 14, 2018 · N616FE · Doug MD11F · Wing, Control Surface Attach Fittings
  > LT WING O/B FLAP O/B FWD (WING SIDE) HINGE LOWER BARREL NUT HOLE BORE CORROSION. HINGE LOWER BARREL NUT HOLE BORE (NR 7 HOLE) REWORKED AND FOUND EXCEED LIMIT AS EPR CMM 57-44-09, OVERSIZED BUSHING FABRICATED AND INSTALLED AS PER CMM 57-44-09 AND EA 1-5750-T034

Next page: https://openairdocs.org/aircraft/N616FE/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 = 'N616FE' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N616FE/reports

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