# Service difficulty reports: N614FE

A list on [N614FE](https://openairdocs.org/aircraft/N614FE.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 8 · 388 reports

- [SDR FDEA202408131116](https://openairdocs.org/sdr/FDEA202408131116.md): Computer · failed · Aug 13, 2024 · N614FE · Doug MD11F · Autopilot System
  > PDIS 614 22-10 5555 13AUG24 06:12 NRT FACT NO PROF ON TAKEOFF. R/I 13AUG24 07:54 NRT REASON CODE: PREMATURE REMOVAL/INSTALLATION OFF MPN: 4059001-908 POS: 2 SRL: 99030834 ON MPN: 4059001-908 CPN: 2211
- [SDR FDEA202408121113](https://openairdocs.org/sdr/FDEA202408121113.md): Smoke Detector · failed · Aug 12, 2024 · N614FE · Doug MD11F · Smoke Detection
  > AT BLOCK IN, GOT INTERMITTENT LVL 3 CABIN SMOKE WITH NO ACTUAL OTHER SMOKE INDICATIONS, NOR ANY SMOKE INDICATIONS FROM SENSORS ON AIR SYNOPTIC PAGE. NO FSS ACTIVATION. USED PAN PAN PAN. INDICATIONS WOULD QUICKLY APPEAR, LAST A FEW SECONDS, THEN GO OUT.
- [SDR FDEA202305100842](https://openairdocs.org/sdr/FDEA202305100842.md): Transmitter · loose · May 10, 2023 · N614FE · Doug MD11F · Trailing Flap Position Indicating System
  > AFTER TAKEOFF RECEIVED AN MLG AURAL WARNING WITH MLG RAISED. HELD SPEED TO 240KTS & CONTINUED CLIMB. LEVELED AT 8K FT &CYCLED MLG. WITH MLG DOWN & LOCKED WARNING STOPPED. RAISED MLG & CONTINUED CLIMB TO FL230 & WARNING RETURNED AS MLG WAS RAISED. RETURNE
- [SDR FDEA202211112754](https://openairdocs.org/sdr/FDEA202211112754.md): Flange · cracked · Nov 11, 2022 · N614FE · Doug MD11F · Vertical Stabilizer
  > DURING ULTRASONIC INSPECTION FOR VERTICAL CRACKS BEHIND SERVICE REPAIR SR10550013 PER DRAWING NUMBER SN10550000 REVISION C ON LEFT HAND SIDE LOWER VERTICAL STABILIZER FORWARD FLANGE OF UPPER REAR SPAR CAP, STATION 2164, EXISTING CRACK INDICATION FOUND FR
- [SDR FDEA202210302698](https://openairdocs.org/sdr/FDEA202210302698.md): Hinge · worn · Oct 30, 2022 · N614FE · Doug MD11F · Fuselage, Door Hinge
  > CABIN-UPPER CARGO DOOR, DOOR HINGE FITTING (FUSELAGE SIDE) PART NUMBER ACA7223-1 FOUND 1ST TO 11TH LOBES FROM FORDWARD FOUND OUT OF LIMIT. LOBE HOLES NUMBER 1 TO NUMBER 11 FROM FORWARD AT CABIN - UPPER CARGO DOOR, DOOR HINGE FITTING REWORKED AND FOUND NUM
- [SDR FDEA202210302697](https://openairdocs.org/sdr/FDEA202210302697.md): Hinge · worn · Oct 30, 2022 · N614FE · Doug MD11F · Fuselage, Door Hinge
  > CABIN- UPPER CARGO DOOR, DOOR HINGE FITTING FOUND 1ST TO 11TH LOBES FROM FORWARD FOUND OUT OF LIMITS. LOBE REWORKED AND FOUND NUMBER 1 TO NUMBER 5 HOLES EXCEED LIMIT. NUMBER 6 TO NUMBER 11 HOLES WITHIN LIMIT AS PER MD- 11 SRM52-30-16-1A FIGURE 101 SHEE
- [SDR FDEA202210302696](https://openairdocs.org/sdr/FDEA202210302696.md): Hinge · worn · Oct 30, 2022 · N614FE · Doug MD11F · Fuselage, Door Hinge
  > CABIN-UPPER CARGO DOOR, DOOR HINGE FITTING PART NUMBER ACA7332-1 FOUND 1ST TO 9TH LOBES FROM FORWARD FOUND OUT OF LIMIT. LOBE HOLES NUMBER 1 TO NUMBER 9 FROM FORWARD AT CABIN-UPPER CARGO DOOR. DOOR HINGE FITTING PART NUMBER ACA7332-1 REWORKED AS PER MD-11
- [SDR FDEA202210262672](https://openairdocs.org/sdr/FDEA202210262672.md): Floor Panel · delaminated · Oct 26, 2022 · N614FE · Doug MD11F · Fuselage Floor Panel
  > CABIN - UPPER CARGO FLOOR PANEL #231HF FOUND DELAMINATED BETWEEN STATION 595 TO STATION 675 CABIN - UPPER CARGO, DELAMINATED FLOOR PANEL #231HF BETWEEN STATION 595 TO STATION 675 REMOVED AND REPLACED AS PER AMM 53-21-04-4. FLOOR PANEL #231HF FABRICATED
- [SDR FDEA202210262671](https://openairdocs.org/sdr/FDEA202210262671.md): Floor Panel · delaminated · Oct 26, 2022 · N614FE · Doug MD11F · Fuselage Floor Panel
  > CABIN FLOOR PANEL #262LF FOUND DELAMINATED FROM STATION 1321 TO STATION 1361. CABIN - DELAMINATED FLOOR PANEL #262LF FROM STATION 1321 TO STATION 1361 REMOVED AND REPLACED AS PER AMM 53-21-04-4. FLOOR PANEL #262LF FABRICATED AS PER FEDEDX DRAWING SRZ-25-00
- [SDR FDEA202210112549](https://openairdocs.org/sdr/FDEA202210112549.md): Beam · cracked · Oct 11, 2022 · N614FE · Doug MD11F · Service Doors
  > CABIN - R3 DOOR #7 STOP BEAM FOUND CRACK. CABIN AT R3 DOOR CRACKED #7 BEAM REMOVED AND REPLACED AS PER SRM 51-31-01-0G. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. ORIG SUB DATE: 10/11/2022
- [SDR FDEA202210102527](https://openairdocs.org/sdr/FDEA202210102527.md): Frame · cracked · Oct 10, 2022 · N614FE · Doug MD11F · Vertical Stabilizer, Spar/Rib
  > EMPENNAGE: WHILE ACCOMPLISHING INSPECTION, ZONE 360 RIGHT SIDE FRAME FOUND CRACKED. FRAME REMOVED AND REPLACED PER MD-11 SRM 51-31-01-OG. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. FRAME FABRICATED IAW DRAWING AJC7593 REVISION Z.
- [SDR FDEA202210102526](https://openairdocs.org/sdr/FDEA202210102526.md): Frame · cracked · Oct 10, 2022 · N614FE · Doug MD11F · Vertical Stabilizer, Spar/Rib
  > EMPENNAGE: WHILE ACCOMPLISHING INSPECTION, ZONE 360 LEFT HAND SIDE FRAME FOUND CRACKED. FRAME REMOVED AND REPLACED IAW SRM 51-31-01-OG. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. FRAME FABRICATED IAW DRAWING AJC7593 REVISION Z.
- [SDR FDEA202210062487](https://openairdocs.org/sdr/FDEA202210062487.md): Anchor Fitting · corroded · Oct 6, 2022 · N614FE · Doug MD11F · Fuselage Main, Attach Fittings
  > : AFT ACCESSORY COMPARTMENT, LONGERON - 33 RIGHT TO LONGERON - 35 RIGHT, ATTACHMENT ANCHOR NUT SURROUNDING AREA FOUND WITH CORROSION. ANCHOR NUT AREA AT AFT ACCESSORY COMPARTMENT, LONGERON - 33 RIGHT TO LONGERON - 35 RIGHT, STATION 2144 TO STATION 2164 RE
- [SDR FDEA202210062486](https://openairdocs.org/sdr/FDEA202210062486.md): Fitting · damaged · Oct 6, 2022 · N614FE · Doug MD11F · Vertical Stabilizer, Attach Fittings
  > TO CARRY OUT BANJO FORWARD AND AFT FITTING HIGH FREQUENCY EDDY CURRENT SURFACE INSPECTION AT STATION 2164. REPAIR CARRIED OUT ALONG STATION 2164 RIGHT HAND BANJO FITTING FORWARD AND AFT FLANGE AREA IAW EA 1-5530-T0313159 B P4. REPAIR CLASSIFIED AS MAJOR I
- [SDR FDEA202210062485](https://openairdocs.org/sdr/FDEA202210062485.md): Fitting · cracked · Oct 6, 2022 · N614FE · Doug MD11F · Vertical Stabilizer, Attach Fittings
  > WHILE ACCOMPLISHING LEFT HAND BANJO FORWARD FITTING INSPECTION, FOUND LEFT HAND BANJO AFT FITTING SUSPECTED CRACK AT STATION 2164. LEFT HAND BANJO FITTING FORWARD AND AFT FLANGE AREA REPAIR CARRIED OUT PER E.A #: 1-5530-T0313159 B P4. REPAIR CLASSIFIED A
- [SDR FDEA202210052464](https://openairdocs.org/sdr/FDEA202210052464.md): Floor Support · corroded · Oct 5, 2022 · N614FE · Doug MD11F · Fuselage Miscellaneous Structure
  > LOWER CENTER CARGO COMPARTMENT STATION 1841 WEB LOWER FLOOR SUPPORT FOUND WITH CORROSION. LOWER CENTER CARGO COMPARTMENT STATION 1841 WEB, CORROSION AT LOWER FLOOR SUPPORT EVALUATED FOUND EXFOLIATED AND EXCEEDED LIMIT AS PER SRM 53-00-00-2R FIGURE 202 R
- [SDR FDEA202210052467](https://openairdocs.org/sdr/FDEA202210052467.md): Stringer · cracked · Oct 5, 2022 · N614FE · Doug MD11F · Fuselage Main, Longeron/Stringer
  > CENTER UPPER AUX TANK - STRINGER 47 AT XCW 48 FOUND CRACK. REPAIR CARRIED OUT AS PER SRM 57-10-03-2R REPAIR 1 FIGURE 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
- [SDR FDEA202210052466](https://openairdocs.org/sdr/FDEA202210052466.md): Stringer · cracked · Oct 5, 2022 · N614FE · Doug MD11F · Fuselage Main, Longeron/Stringer
  > CENTER UPPER AUX TANK - STRINGER 47 AT STATION XCW - 17 FOUND CRACK. REPAIR CARRIED OUT AS PER SRM 57-10-03-2R REPAIR 1 FIGURE 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
- [SDR FDEA202210052465](https://openairdocs.org/sdr/FDEA202210052465.md): Stringer · cracked · Oct 5, 2022 · N614FE · Doug MD11F · Fuselage Main, Longeron/Stringer
  > CENTER UPPER AUX TANK - STRINGER 47 AT XCW 19 FOUND CRACK. CENTER UPPER AUX TANK STRINGER 47 AT XCW 19 CRACKED AREA REPAIR CARRIED OUT AS PER SRM 57-10-03-2R REPAIR 1 FIGURE 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
- [SDR FDEA202210012437](https://openairdocs.org/sdr/FDEA202210012437.md): Doubler · corroded · Oct 1, 2022 · N614FE · Doug MD11F · Wing Main, Frame Structure
  > LEFT WING Ï¿½ UPPER WING SURFACE MAIN LANDING GEAR SUPPORT UPPER DOUBLER AT XORS 283 FOUND CORROSION. LEFT WING UPPER WING SURFACE MAIN LANDING GEAR SUPPORT UPPER DOUBLER BETWEEN AUX SPAR AND YW 467 AREA CORROSION REMOVED AND FOUND EXCEED LIMIT AS PER S
- [SDR FDEA202210012436](https://openairdocs.org/sdr/FDEA202210012436.md): Skin · cracked · Oct 1, 2022 · N614FE · Doug MD11F · Wing, Plate/Skin
  > LEFT WING Ï¿½ FIXED LEADING EDGE NUMBER 12 SLAT TRACK CUTOUT CORNER AT XOS 776.5 FOUND CRACK. REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 7 FIGURE 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
- [SDR FDEA202210012435](https://openairdocs.org/sdr/FDEA202210012435.md): Doubler · cracked · Oct 1, 2022 · N614FE · Doug MD11F · Wing, Plate/Skin
  > LEFT WING Ï¿½ FIXED LEADING EDGE RIB DOUBLER AT XOS 906 FOUND CRACK.
- [SDR FDEA202210012434](https://openairdocs.org/sdr/FDEA202210012434.md): Doubler · cracked · Oct 1, 2022 · N614FE · Doug MD11F · Wing, Plate/Skin
  > LEFT WING Ï¿½ FIXED LEADING EDGE BEADED DOUBLER AT XOS 664 FOUND CRACK.
- [SDR FDEA202210012433](https://openairdocs.org/sdr/FDEA202210012433.md): Doubler · cracked · Oct 1, 2022 · N614FE · Doug MD11F · Wing, Plate/Skin
  > LEFT WING Ï¿½ FIXED LEADING EDGE BEADED DOUBLER AT XOS 655 FOUND CRACK.
- [SDR FDEA202210012432](https://openairdocs.org/sdr/FDEA202210012432.md): Doubler · cracked · Oct 1, 2022 · N614FE · Doug MD11F · Wing, Plate/Skin
  > LEFT WING Ï¿½ FIXED LEADING EDGE BEADED DOUBLER AT XOS 544 FOUND CRACK.
- [SDR FDEA202210012431](https://openairdocs.org/sdr/FDEA202210012431.md): Doubler · cracked · Oct 1, 2022 · N614FE · Doug MD11F · Wing, Plate/Skin
  > RIGHT WING Ï¿½ FIXED LEADING EDGE BEADED DOUBLER AT STATION XOS 655 FOUND CRACK.
- [SDR FDEA202210012430](https://openairdocs.org/sdr/FDEA202210012430.md): Doubler · cracked · Oct 1, 2022 · N614FE · Doug MD11F · Wing, Plate/Skin
  > RIGHT WING Ï¿½ FIXED LEADING EDGE RIB DOUBLER AT STATION XOS 789 FOUND CRACK.
- [SDR FDEA202210012428](https://openairdocs.org/sdr/FDEA202210012428.md): Floor Support · corroded · Oct 1, 2022 · N614FE · Doug MD11F · Fuselage Miscellaneous Structure
  > LOWER CENTER CARGO COMPARTMENT STATION 1841 WEB UPPER FLOOR SUPPORT FOUND WITH CORROSION. LOWER CENTER CARGO COMPARTMENT STATION 1841 WEB, CORROSION AT UPPER FLOOR SUPPORT EVALUATED FOUND EXFOLIATED AND EXCEEDED LIMIT AS PER SRM 53-00-00-2R FIGURE 202
- [SDR FDEA202209292385](https://openairdocs.org/sdr/FDEA202209292385.md): Spar Cap · corroded · Sep 29, 2022 · N614FE · Doug MD11F · Wing Spar
  > RIGHT WING TRAILING EDGE REAR SPAR LOWER CAP AT XORS 1078 FOUND CORROSION. RIGHT WING TRAILING EDGE REAR SPAR LOWER CAP AT XORS 1078 CORROSION REMOVED AND FOUND EXCEED LIMITS IAW SRM 57-00-10-1A ALLOWABLE DAMAGE 1 FIG 101. CORRODED LOWER REAR SPAR CAP AT XO
- [SDR FDEA202206211479](https://openairdocs.org/sdr/FDEA202206211479.md): Floorboard · delaminated · Jun 21, 2022 · N614FE · Doug MD11F · Fuselage Floor Panel
  > FLOOR PANEL L/H 253DF IS DELAM WITH LARGE HOLE. FABRICATED NEW MAIN DECK FLOOR BOARD PANEL # 253DF PER FEDEX DRWG SRZ-25-005 ADA8396.. (MAJOR REPAIR)
- [SDR FDEA202205081153](https://openairdocs.org/sdr/FDEA202205081153.md): Windshield · cracked · May 8, 2022 · N614FE · Doug MD11F · Flight Compartment Windows
  > PDIS 614 56-10 2933 06MAY22 YYZ OPEN U RIGHT WINDSHIELD CRACKED DUE TO ARCING. TURNED OFF WINDSHIELD HEAT. STOPPED CRACKING. FACT 08MAY22 22:56 YYZ REPLACED R/H WINDSHIELD PANEL ASSY I.A.W WITH MD11 AMM 56-11-01-4-1.
- [SDR FDEA202107291887](https://openairdocs.org/sdr/FDEA202107291887.md): Tire · underserviced · Jul 29, 2021 · N614FE · Doug MD11F · Tire
  > RECEIVED LVL 2 TIRE FAIL FOR #3 TIRE TIRE PRESSURE LEAKED OUT AFTER TAKE OFF. T/S PER FIM 32-40-00-2 FIG 119, TIRE #3 BELOW 50PSI. REMOVED AND REPLACED #3 AND #4 TIRES REF AMM 32-41-01-4. PRESSURE CHECK GOOD.
- [SDR FDEA202011172884](https://openairdocs.org/sdr/FDEA202011172884.md): Finger Doubler · delaminated · Nov 17, 2020 · N614FE · Doug MD11F · Wing, Plate/Skin
  > RIGHT WING TRAILING EDGE INBOARD ISLAND UPPER FORWARD SKIN LOWER SURFACE FINGER DOUBLER AT XW 385 FOUND DELAMINATION. RIGHT WING TRAILING EDGE INBOARD ISLAND UPPER FORWARD SKIN LOWER SURFACE FINGER DOUBLER AT XW 385 REPAIR CARRIED OUT, AS PER SRM 57-50-01-2R
- [SDR FDEA202011082793](https://openairdocs.org/sdr/FDEA202011082793.md): Skin · cracked · Nov 8, 2020 · N614FE · Doug MD11F · Wing, Plate/Skin
  > WING, LEFT HAND WING FIXED LEADING EDGE LOWER SKIN AT SLAT TRACK NUMBER 14 CUT OUT OUTBOARD STATION XOS 892 FOUND CRACK WING LEFT HAND WING FIXED LEADING EDGE LOWER SKIN AT SLAT TRACK NUMBER 14 CUT OUT OUTBOARD STATION XOS 892. REPAIR CARRIED OUT, AS PER SRM
- [SDR FDEA202011082792](https://openairdocs.org/sdr/FDEA202011082792.md): Doubler · delaminated · Nov 8, 2020 · N614FE · Doug MD11F · Wing, Plate/Skin
  > LEFT WING, TRAILING EDGE INBOARD ISLAND UPPER FORWARD SKIN LOWER SURFACE FINGER DOUBLER AT XW 383 FOUND DELAMINATION. LEFT WING TRAILING EDGE INBOARD ISLAND UPPER FORWARD SKIN LOWER SURFACE FINGER DOUBLER AT XW 383. REPAIR CARRIED OUT, AS PER SRM 57-50-01-
- [SDR FDEA202011082795](https://openairdocs.org/sdr/FDEA202011082795.md): Former · cracked · Nov 8, 2020 · N614FE · Doug MD11F · Wing Main, Frame Structure
  > WING LEFT HAND WING FIXED LEADING EDGE COMPARTMENT XOS 584 FORMER ASSEMBLY FOUND CRACK.
- [SDR FDEA202011082794](https://openairdocs.org/sdr/FDEA202011082794.md): Doubler · cracked · Nov 8, 2020 · N614FE · Doug MD11F · Wing, Plate/Skin
  > WING LEFT HAND WING FIXED LEADING EDGE COMPARTMENT XOS 667 DOUBLER FOUND CRACK.
- [SDR FDEA202011052775](https://openairdocs.org/sdr/FDEA202011052775.md): Trunnion · cracked · Nov 5, 2020 · N614FE · Doug MD11F · Fuselage, Landing Gear Attach Fittings
  > CRACK INDICATION FOUND APPROXIMATELY 0.125 INCHES IN LENGTH DURING HIGH FREQUENCY EDDY CURRENT INSPECTION ON LEFT HAND SIDE NOSE LANDING GEAR TRUNNION FITTING EXISTING TRIM OUT AT STATION 583. LEFT HAND SIDE NOSE LANDING GEAR TRUNNION FITTING EXISTING TRI
- [SDR FDEA202011052781](https://openairdocs.org/sdr/FDEA202011052781.md): Seat Track · worn · Nov 5, 2020 · N614FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK CARGO COMPARTMENT CABIN, FOUND SEAT TRACK AT STATION 760, X= -47.5 CROWN WORN. MAIN DECK CARGO COMPARTMENT CABIN AT SEAT TRACK STATION 760, X= -47.5, WORN CROWN EVALUATED AND FOUND TO EXCEED LIMIT, AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE
- [SDR FDEA202011042770](https://openairdocs.org/sdr/FDEA202011042770.md): Seat Track · worn · Nov 4, 2020 · N614FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK CARGO COMPARTMENT CABIN, FOUND SEAT TRACK AT STATION 1018, X= -8.5 CROWN WORN. MAIN DECK CARGO COMPARTMENT CABIN AT SEAT TRACK STATION 1018, X= -8.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT, AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1.
- [SDR FDEA202011042769](https://openairdocs.org/sdr/FDEA202011042769.md): Seat Track · worn · Nov 4, 2020 · N614FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK CARGO COMPARTMENT CABIN, FOUND SEAT TRACK AT STATION 1060, X=47.5 CROWN WORN. MAIN DECK CARGO COMPARTMENT CABIN AT SEAT TRACK STATION 1060, X=47.5 WORN. CROWN EVALUATED AND FOUND EXCEEDED LIMIT, AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1.
- [SDR FDEA2019121323225](https://openairdocs.org/sdr/FDEA2019121323225.md): Terminal · damaged · Dec 12, 2019 · N614FE · Doug MD11F · Smoke Detection
  > APPROX 20 MIN AT CRUISE, FL 360, APU FIRE LIGHT ILLUMINATED WITH TRI-TONE ALERT FIRE BELL. APU WAS NOT OPERATING. PULLED APU FIRE HANDLE & ROTATED. PER QRH, WAITED 30 SECS, TRI-TONE ALERT CAME BACK ON & FIRE HANDLE REMAINED ILLUMINATED. MANIPULATING WIRE
- [SDR FDEA201909242335](https://openairdocs.org/sdr/FDEA201909242335.md): Flex Line · failed · Sep 24, 2019 · N614FE · Doug MD11F · Crew Oxygen System
  > AFTER APPROXIMATELY 30MIN OF FLIGHT WE HEARD A LOUD EXCAPING OF AIR COMING FROM THE COURRIER SECTION. WE NOTICED THAT THE O2 SYSTEM READINGS ON SYSTEM 1 & 3 WERE DECREASING, #2 REMAINED @ 2000 PSI. NO AIR WAS AVAILABLE THROUGH THE OXYGEN MASKS IN THE COURRIE
- [SDR FDEA201904160809](https://openairdocs.org/sdr/FDEA201904160809.md): Warning Light · illuminated · Apr 16, 2019 · N614FE · Doug MD11F · Emergency Lighting
  > EMER LT BAT 1 LO DURING PREFLIGHT.
- [SDR FDEA2018091192424](https://openairdocs.org/sdr/FDEA2018091192424.md): Floor Support · corroded · Sep 9, 2018 · N614FE · Doug MD11F · Fuselage Miscellaneous Structure
  > MDCC AFT FLOOR SUPPORT FOUND CORROSION AT STA 2007 X =-25. CORROSION REMOVED PER SRM 51-21-01-0G AND FOUND EXCEEDED LIMIT PER SRM 53-00-00-2R FIG 202. ORIGINAL THK 0.080", MATERIAL REMOVED 0.060", REMAINING THK 0.020". CORRODED FLOOR SUPPORT REMOVED PER AMM 20
- [SDR FDEA2018091172417](https://openairdocs.org/sdr/FDEA2018091172417.md): Fitting · corroded · Sep 7, 2018 · N614FE · Doug MD11F · Trailing Edge Flaps
  > LT O/B FLAP VANE HORN FITTING 'F' HOLE BORE CORROSION. BORE REWORKED AND FOUND EXCEED LIMIT PER SRM 57-50-02-2R FIG 201 SHEET 1. EXISTING SLOT HOLE: LENGTH 0.852", WIDTH 0.600", FINAL SLOT HOLE: LENGTH 0.960", WIDTH 0.708". REPAIR LIMIT - LENGTH 0.940", WIDTH
- [SDR FDEA2018091172416](https://openairdocs.org/sdr/FDEA2018091172416.md): Fitting · corroded · Sep 7, 2018 · N614FE · Doug MD11F · Trailing Edge Flaps
  > LT O/B FLAP VANE HORN FITTING 'E' HOLE BORE CORROSION. BORE REWORKED AND FOUND EXCEED LIMIT PER SRM 57-50-02-2R FIG 201 SHT 1. EXISTING SLOT HOLE: LENGTH 0.857", WIDTH 0.581", FINAL SLOT HOLE: LENGTH 0.952", WIDTH 0.652". REPAIR LIMIT - LENGTH 0.940", WIDTH 0.
- [SDR FDEA2018091172415](https://openairdocs.org/sdr/FDEA2018091172415.md): Bracket · corroded · Sep 7, 2018 · N614FE · Doug MD11F · Trailing Edge Flaps
  > LT WING I/B FLAP I/B DRIVE LINK IDLER BRACKET BORE CORROSION. DRIVE LINK IDLER BRACKET BORE REWORKED PER CMM 57-52-03. EXISTING HOLE DIA 1.00", FINAL HOLE DIA 1.316". REPLACEMENT BUSHING FOR ARC3087-1 & ARC3086-1 FABRICATED PER EA 1-5750-T0342037 P1 STEP 4, 4A
- [SDR FDEA2018091172414](https://openairdocs.org/sdr/FDEA2018091172414.md): Hinge · corroded · Sep 7, 2018 · N614FE · Doug MD11F · Trailing Edge Flaps
  > LT WING O/B FLAP O/B AFT (FLAP SIDE) HINGE PIVOT I/B HOLE BORE CORROSION. HINGE PIVOT I/B HOLE BORE REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-52-04. EXISTING HOLE DIA: 1.148' FINAL HOLE DIA: 1.163" MAXIMUM ALLOWABLE HOLE: 1.150" OVERSIZED BUSHING FABRICATE
- [SDR FDEA2018091172413](https://openairdocs.org/sdr/FDEA2018091172413.md): Hinge Bracket · corroded · Sep 7, 2018 · N614FE · Doug MD11F · Trailing Edge Flaps
  > LT WING O/B FLAP I/B AFT (FLAP SIDE) HINGE PIVOT I/B HOLE BORE CORROSION. HINGE PIVOT I/B HOLE BORE REWORKED AND FOUND EXCEED LIMIT PER CMM 57-52-04. EXISTING HOLE DIA 1.148", FINAL HOLE DIA 1.158", MAXIMUM ALLOWABLE HOLE DIA 1.150". OVERSIZED BUSHING FABRICAT

Next page: https://openairdocs.org/aircraft/N614FE/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 = 'N614FE' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N614FE/reports

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