# Service difficulty reports: N621FE

A list on [N621FE](https://openairdocs.org/aircraft/N621FE.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 · 288 reports

- [SDR FDEA202609201373](https://openairdocs.org/sdr/FDEA202609201373.md): Test Switch · inoperative · Sep 20, 2026 · N621FE · Doug MD11F · Emergency Equipment
  > R1 DOOR EVACUATION SLIDE REMOTE PRESSURE PRESS TO TEST SWITCH INOP. REPLACED R1 DOOR EVAC SLIDE REMOTE PRESSURE PRESS TO TEST KIT. OPS CHECK GOOD.
- [SDR FDEA202608101106](https://openairdocs.org/sdr/FDEA202608101106.md): Power Supply · no test · Aug 10, 2026 · N621FE · Doug MD11F · Emergency Lighting
  > ON PREFLIGHT EMERGENCY LIGHT TEST RECEIVED MESSAGE, EMER LT BAT 1 LO. REPLACED EMERGENCY LIGHT POWER SUPPLY. OPS CHKD NORMAL.
- [SDR FDEA202605090577](https://openairdocs.org/sdr/FDEA202605090577.md): Bearing · worn · May 9, 2026 · N621FE · Doug MD11F · Nacelle/Pylon Structure
  > AFT SPHERICAL BEARING WORN. COMPLIED WITH EA 1-5450-T0386066 P2
- [SDR FDEA202605050552](https://openairdocs.org/sdr/FDEA202605050552.md): Pylon · not reported · May 5, 2026 · N621FE · Doug MD11F · Nacelle/Pylon, Main Frame
  > WS-C 00091735 MOD TYPE T MOD NO. 1-5450-T0386268 REV NO. PS P2 NACELLES/PYLON - WING PYLON/STRUT - NO. 1 PYLON, INSPECTION AND REPAIR OF DAMAG COMPLY WITH E..A. 1-5450-T0386268 REV NO. POS. P2. EA: 1-5450-T0386268 P2 COMPLIED WITH REV NO. PS PT.2 E.A
- [SDR FDEA202605050551](https://openairdocs.org/sdr/FDEA202605050551.md): Pylon · not reported · May 5, 2026 · N621FE · Doug MD11F · Nacelle/Pylon, Main Frame
  > WS-C 00091735 MOD TYPE T MOD NO. 1-5450-T0386268 REV NO. PS P1 NACELLES/PYLON - WING PYLON/STRUT - NO. 1 PYLON, INSPECTION AND REPAIR OF DAMAG COMPLY WITH E..A. 1-5450-T0386268 REV NO. POS. P1. COMPLY WITH E..A. 1-5450-T0386268 REV NO: PS P1 EA: 1-5
- [SDR FDEA202605050550](https://openairdocs.org/sdr/FDEA202605050550.md): Pylon · not reported · May 5, 2026 · N621FE · Doug MD11F · Nacelle/Pylon, Main Frame
  > WS-C 00091735 MOD TYPE T MOD NO. 1-5450-T0386269 REV NO. PS P2 NACELLES/PYLON - WING PYLON/STRUT - NO. 3 PYLON, INSPECTION AND REPAIR OF DAMAG COMPLY WITH E..A. 1-5450-T0386269 REV NR POS. P2 PLND. COMPLY WITH E..A. 1-5450-T0386269 REV NO: PS P2
- [SDR FDEA202605050549](https://openairdocs.org/sdr/FDEA202605050549.md): Pylon · not reported · May 5, 2026 · N621FE · Doug MD11F · Nacelle/Pylon, Main Frame
  > WS-C 00091735 MOD TYPE T MOD NO. 1-5450-T0386269 REV NO. PS P1 NACELLES/PYLON - WING PYLON/STRUT - NO. 3 PYLON, INSPECTION AND REPAIR OF DAMAG COMPLY WITH E..A. 1-5450-T0386269 REV NO. POS. P1. COMPLY WITH E..A. 1-5450-T0386269 REV NO: PS P1 EA: E.A
- [SDR FDEA202507301340](https://openairdocs.org/sdr/FDEA202507301340.md): Power Unit · faulted · Jul 30, 2025 · N621FE · Doug MD11F · Electrical Power System
  > EMER PWR TST FAIL LEVEL 1 ALERT ILLUMINATED. PER QRH, TURNED EMER PWR SWITCH OFF AND WAITED FOR BAT CHARGING MESSAGE TO GO OUT, THEN TURNED EMER PWR SWITCH ON AND ALL APPEARED NORMAL, UNTIL APU PWR DROPPED OFFLINE AGAIN AND EMER PWR ON LEVEL 1 ALERT ILLUM
- [SDR FDEA202501220118](https://openairdocs.org/sdr/FDEA202501220118.md): Seat Track · corroded · Jan 22, 2025 · N621FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 1029 X = -75.25 FOUND WITH CORROSION. MAIN DECK CARGO COMPARTMENT AT SEAT TRACK STATION 1029, X = -75.25, CORROSION EVALUATED, FOUND EXFOLIATED AND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 1
- [SDR FDEA202501220117](https://openairdocs.org/sdr/FDEA202501220117.md): Seat Track · worn · Jan 22, 2025 · N621FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 1330 X = -47.5 FOUND CROWN WORN. MAIN DECK CARGO COMPARTMENT AT SEAT TRACK STATION 1330, X = -47.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAG
- [SDR FDEA202501220116](https://openairdocs.org/sdr/FDEA202501220116.md): Seat Track · worn · Jan 22, 2025 · N621FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 1059 X = 47.5 FOUND CROWN WORN. MAIN DECK CARGO COMPARTMENT AT SEAT TRACK STATION 1059, X = 47.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE
- [SDR FDEA202501220115](https://openairdocs.org/sdr/FDEA202501220115.md): Seat Track · worn · Jan 22, 2025 · N621FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 1015 X = 47.5 FOUND CROWN WORN. MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 1015, X = 47.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE
- [SDR FDEA202501220114](https://openairdocs.org/sdr/FDEA202501220114.md): Seat Track · worn · Jan 22, 2025 · N621FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 885 X = 8.5 FOUND CROWN WORN. MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 885, X = 8.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CRO
- [SDR FDEA202501210111](https://openairdocs.org/sdr/FDEA202501210111.md): Access Door · cracked · Jan 21, 2025 · N621FE · Doug MD11F · Wing, Plate/Skin
  > DURING HIGH FREQUENCY EDDY CURRENT INSPECTION ON RIGHT HAND WING SLAT OF ACTUATOR ACCESS DOOR FORWARD CORNER #5 FOUND 01 EACH CRACK APPROXIMATELY 0.5. STATION XOS 490. CRACK AT RIGHT HAND WING SLAT OF ACTUATOR ACCESS DOOR FORWARD CORNER #5 STATION XOS 4
- [SDR FDEA202501200107](https://openairdocs.org/sdr/FDEA202501200107.md): Skin · corroded · Jan 20, 2025 · N621FE · Doug MD11F · Fuselage Main, Plate/Skin
  > AFT FUSELAGE STATION 2140 RIGHT HAND PANEL #347DF CUTOUT SURFACE CORROSION. SURFACE CORROSION AT AFT FUSELAGE - STATION 2140 RIGHT HAND PANEL #347DF CUTOUT PER MD-11 SRM 53-70-01-2R FIGURE 201, REPAIR 3. REPAIR CARRIED OUT PER MD-11 SRM 53-70- 01-2R FIGUR
- [SDR FDEA202501200106](https://openairdocs.org/sdr/FDEA202501200106.md): Support Angle · cracked · Jan 20, 2025 · N621FE · Doug MD11F · Fuselage Miscellaneous Structure
  > AFT FUSELAGE LOWER TORQUE BOX UPPER PANEL ON LOWER SURFACE AT ACTUATOR SUPPORT ANGLES AREA CRACKED. (0.5") AT STATION 2122.881, X = - 10. 0.5" CRACK AT STATION 2122.881, X = - 10 AFT FUSELAGE - LOWER TORQUE BOX UPPER PANEL ON LOWER SURFACE AT ACTUATOR A
- [SDR FDEA202501180104](https://openairdocs.org/sdr/FDEA202501180104.md): Seat Track · worn · Jan 18, 2025 · N621FE · Doug MD11F · Fuselage Floor Panel
  > MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 1541 X= -47.5 FOUND CROWN WORN. MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 1541, X = -47.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE
- [SDR FDEA202501180103](https://openairdocs.org/sdr/FDEA202501180103.md): Seat Track · worn · Jan 18, 2025 · N621FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 755 X= 8.5 FOUND CROWN WORN. MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 755, X = 8.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROW
- [SDR FDEA202501160079](https://openairdocs.org/sdr/FDEA202501160079.md): Seat Track · worn · Jan 16, 2025 · N621FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK Ï¿½ CARGO COMPARTMENT SEAT TRACK AT STATION 1425 X= 47.5 FOUND CROWN WORN. MAIN DECK Ï¿½ CARGO COMPARTMENT AT SEAT TRACK STATION 1425, X = 47.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMA
- [SDR FDEA202501160078](https://openairdocs.org/sdr/FDEA202501160078.md): Seat Track · worn · Jan 16, 2025 · N621FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK Ï¿½ CARGO COMPARTMENT SEAT TRACK AT STATION 1425 X= -27.5 FOUND CROWN WORN. MAIN DECK Ï¿½ CARGO COMPARTMENT AT SEAT TRACK STATION 1425, X = -27.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DA
- [SDR FDEA202501160077](https://openairdocs.org/sdr/FDEA202501160077.md): Seat Track · worn · Jan 16, 2025 · N621FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 1411 X= -8.5 FOUND CROWN WORN. MAIN DECK CARGO COMPARTMENT AT SEAT TRACK STATION 1411, X = -8.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1.
- [SDR FDEA202501160076](https://openairdocs.org/sdr/FDEA202501160076.md): Seat Track · worn · Jan 16, 2025 · N621FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 1431 X= -47.5 FOUND CROWN WORN. MAIN DECK CARGO COMPARTMENT AT SEAT TRACK STATION 1431, X = -47.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE
- [SDR FDEA202501160080](https://openairdocs.org/sdr/FDEA202501160080.md): Seat Track · worn · Jan 16, 2025 · N621FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 1431 X= 8.5 FOUND CROWN WORN. MAIN DECK CARGO COMPARTMENT AT SEAT TRACK STATION 1431, X= 8.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CRO
- [SDR FDEA202501160082](https://openairdocs.org/sdr/FDEA202501160082.md): Seat Track · worn · Jan 16, 2025 · N621FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 6-10 X= 47.5 FOUND CROWN WORN. MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 6-10, X= 47.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1.
- [SDR FDEA202501160081](https://openairdocs.org/sdr/FDEA202501160081.md): Seat Track · worn · Jan 16, 2025 · N621FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 1411 X= 8.5 FOUND CROWN WORN. MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 1411, X= 8.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CRO
- [SDR FDEA202501140067](https://openairdocs.org/sdr/FDEA202501140067.md): Seat Track · worn · Jan 14, 2025 · N621FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 5-10 X= -47.5 FOUND CROWN WORN. MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 5-10, X= -47.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1.
- [SDR FDEA202501140066](https://openairdocs.org/sdr/FDEA202501140066.md): Seat Track · worn · Jan 14, 2025 · N621FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 5-10 X= -8.5 FOUND CROWN WORN. MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 5-10, X= -8.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CRO
- [SDR FDEA202501140065](https://openairdocs.org/sdr/FDEA202501140065.md): Seat Track · worn · Jan 14, 2025 · N621FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 5-10 X= 47.5 FOUND CROWN WORN. MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 5-10, X= 47.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. C
- [SDR FDEA202409111296](https://openairdocs.org/sdr/FDEA202409111296.md): Connector · disconnected · Sep 11, 2024 · N621FE · Doug MD11F · Door System Wiring
  > FWD CARGO DOOR A ALERT ON CLIMB OUT. EMERGENCY DECLARED. FOUND FORWARD CARGO DOOR CLOSED LIMIT WARNING SWITCH CONNECTOR ( P1-1703) UNSECURED. SECURED CONNECTOR AND PERFORMED ADJ/TEST OF CARGO DOOR WARNING INDICATION SYSTEM. OPS CHECK GOOD A/C OK FOR SERVICE.
- [SDR FDEA202307121202](https://openairdocs.org/sdr/FDEA202307121202.md): Actuator · unknown · Jul 12, 2023 · N621FE · Doug MD11F · Pressure Regulator/Outflow Valve
  > CLIMBING THROUGH 4000 FEET CABIN SEL MAN FOLLOWED BY CABIN RATE LEVEL 1. CABIN PRESSURE WOULD NOT STABILIZE INITIALLY IN MANUAL MODE. CABIN WAS INDICATING -5000 FEET. RETURNED TO INDY AND GOT THE CABIN TO STABILIZE ON DOWNWIND MANUALLY. SHGN 12JUL23 04:0
- [SDR FDEA202301260165](https://openairdocs.org/sdr/FDEA202301260165.md): None · none · Jan 26, 2023 · N621FE · Doug MD11F · Standard Practices/Structures
  > AGING AIRCRAFT - EXISTING REPAIR AT FUSELAGE SKIN RIGHT HAND SIDE STATION 1082 LONGERON 32 RIGHT. EXISTING REPAIR AT FUSELAGE SKIN RIGHT HAND SIDE STATION 1082 LONGERON 32 RIGHT EVALUATED AND FOUND REPAIRED IN ACCORDANCE WITH SRM 53-00-01-2R REPAIR 7 FIGUR
- [SDR FDEA202301200142](https://openairdocs.org/sdr/FDEA202301200142.md): Fastener · missing · Jan 20, 2023 · N621FE · Doug MD11F · Fuselage Floor Panel
  > CENTER ACCESSORY COMPARTMENT - BELOW CABIN FLOOR AND RIGHT OF FUSELAGE CENTER LINE AT STATION 6-80 TO 6-100, X= -8.5 HAS SEVERAL FLOOR PANEL FASTENERS MAKING CONTACT WITH THE SEAT TRACK FLANGE CAUSING DAMAGE. CABIN FLOOR AND RIGHT OF FUSELAGE CENTER LINE
- [SDR FDEA202301200141](https://openairdocs.org/sdr/FDEA202301200141.md): Fastener · missing · Jan 20, 2023 · N621FE · Doug MD11F · Fuselage Floor Panel
  > CENTER ACCESSORY COMPARTMENT - BELOW CABIN FLOOR AND LEFT OF FUSELAGE CENTER LINE AT STATION 6-80 TO 6-100, X=8.5 HAS SEVERAL FLOOR PANEL FASTENERS MAKING CONTACT WITH THE SEAT TRACK FLANGE CAUSING DAMAGE. CABIN FLOOR AND LEFT OF FUSELAGE CENTER LINE AT S
- [SDR FDEA202301200140](https://openairdocs.org/sdr/FDEA202301200140.md): Floor Panel · delaminated · Jan 20, 2023 · N621FE · Doug MD11 · Fuselage Floor Panel
  > MAIN DECK CARGO COMPARTMENT, FLOOR PANEL 241DF BS 755 - 795, FOUND DELAMINATED. FLOOR PANEL 241DF AT MAIN DECK CARGO REMOVED IAW AMM 53-21-04. THE NEW FLOOR PANEL WAS FABRICATED IAW DRAWING SRZ-25-005, REVISION R. THE NEW FLOOR PANEL WAS INSTALLED IAW AMM
- [SDR FDEA202301180130](https://openairdocs.org/sdr/FDEA202301180130.md): Floor Panel · delaminated · Jan 18, 2023 · N621FE · Doug MD11F · Fuselage Floor Panel
  > CABIN - MAIN DECK CARGO COMPARTMENT FLOOR PANEL 231BF AT STATION 459 - 536 FOUND DAMAGED. DAMAGED FLOOR PANEL 231BF AT MAIN DECK CARGO COMPARTMENT STATION 459 - 536 REMOVED AS PER AMM 53-21-04. FLOOR PANEL 231BF FABRICATED AS PER FEDEX DRAWING SRZ- 25-005
- [SDR FDEA202301160110](https://openairdocs.org/sdr/FDEA202301160110.md): Skin · cracked · Jan 16, 2023 · N621FE · Doug MD11F · Wing, Plate/Skin
  > 02 EACH FASTENER HOLES NUMBER 10 AND NUMBER 15 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. 02 EACH CRACKED FASTENER
- [SDR FDEA202301160113](https://openairdocs.org/sdr/FDEA202301160113.md): Rib · cracked · Jan 16, 2023 · N621FE · Doug MD11F · Leading Edge Devices
  > WHILE CARRYING OUT INTERNAL BORESCOPE INSPECTION ON LEFT HAND NUMBER 7 SLAT LOOSE RIVETS AREA (SNRM N00517), FOUND THE SLAT INTERNAL RIB CRACK AT STATION XOS 963.009. RIB AT LEFT HAND NUMBER 7 SLAT INTERNAL AT STATION XOS 963.009 AREA REPAIRED AS PER E
- [SDR FDEA202301160112](https://openairdocs.org/sdr/FDEA202301160112.md): Rib · cracked · Jan 16, 2023 · N621FE · Doug MD11F · Leading Edge Devices
  > WHILE CARRYING OUT INTERNAL BORESCOPE INSPECTION ON LEFT HAND NUMBER 7 SLAT LOOSE RIVETS AREA (SNRM N00517), FOUND THE SLAT INTERNAL RIB CRACK AT STATION XOS 983.612. RIB AT LEFT HAND NUMBER 7 SLAT INTERNAL AT STATION XOS 983.612 AREA REPAIRED AS PER E
- [SDR FDEA202301160111](https://openairdocs.org/sdr/FDEA202301160111.md): Rib · cracked · Jan 16, 2023 · N621FE · Doug MD11F · Leading Edge Devices
  > WHILE CARRYING OUT INTERNAL BORESCOPE INSPECTION ON LEFT HAND NUMBER 7 SLAT LOOSE RIVETS AREA (SNRM N00517), FOUND THE SLAT INTERNAL RIB CRACK AT STATION XOS 968.159. RIB AT LEFT HAND NUMBER 7 SLAT INTERNAL AT STATION XOS 968.159 AREA REPAIRED AS PER E
- [SDR FDEA202301140094](https://openairdocs.org/sdr/FDEA202301140094.md): None · none · Jan 14, 2023 · N621FE · Doug MD11F · Standard Practices/Structures
  > AGING AIRCRAFT - EXISTING REPAIR FOUND AT MAIN DECK CARGO COMPARTMENT LEFT HAND FRAME STATION 1561 LONGERON 12 LEFT EXISTING REPAIR AT MAIN DECK CARGO COMPARTMENT LEFT HAND FRAME STATION 1561 LONGERON 12 LEFT EVALUATED AND FOUND REPAIRED IN ACCORDANCE WITH
- [SDR FDEA202301140092](https://openairdocs.org/sdr/FDEA202301140092.md): Seat Track · cracked · Jan 14, 2023 · N621FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > AGING AIRCRAFT - EXISTING REPAIR AT MAIN DECK CARGO COMPARTMENT SEAT TRACK BETWEEN STATION 625 TO STATION 645 X = 27.5 LEFT HAND SIDE EXISTING REPAIR AT MAIN DECK CARGO COMPARTMENT SEAT TRACK BETWEEN STATION 625 TO STATION 645 X = 27.5 LEFT HAND SIDE EVALU
- [SDR FDEA202301140097](https://openairdocs.org/sdr/FDEA202301140097.md): Doubler · cracked · Jan 14, 2023 · N621FE · Doug MD11F · Wing, Plate/Skin
  > LEFT WING OUTBOARD FIXED LEADING EDGE LOWER SKIN BEADED DOUBLER FOUND CRACK AT STATION XOS 704. LEFT HAND WING OUTBOARD FIXED LEADING EDGE LOWER SKIN DOUBLER AT STATION XOS 704 REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIF
- [SDR FDEA202301140096](https://openairdocs.org/sdr/FDEA202301140096.md): Doubler · cracked · Jan 14, 2023 · N621FE · Doug MD11F · Wing, Plate/Skin
  > RIGHT WING OUTBOARD FIXED LEADING EDGE LOWER SKIN BEADED DOUBLER FOUND CRACK AT STATION XOS 704. RIGHT HAND WING OUTBOARD FIXED LEADING EDGE LOWER SKIN DOUBLER AT STATION XOS 704 REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLAS
- [SDR FDEA202301140095](https://openairdocs.org/sdr/FDEA202301140095.md): Doubler · cracked · Jan 14, 2023 · N621FE · Doug MD11F · Wing, Plate/Skin
  > RIGHT WING OUTBOARD FIXED LEADING EDGE LOWER SKIN BEADED DOUBLER FOUND CRACK AT STATION XOS 675. RIGHT HAND WING OUTBOARD FIXED LEADING EDGE LOWER SKIN DOUBLER AT STATION XOS 675 REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLAS
- [SDR FDEA202301140093](https://openairdocs.org/sdr/FDEA202301140093.md): Door Frame · cracked · Jan 14, 2023 · N621FE · Doug MD11F · Fuselage Main, Structure
  > MAIN DECK CARGO L3 DOOR JAMB AFT LOWER CORNER AREA BS 1305.25 - 1315.42 FOUND CRACKED. L3 DOOR JAMB AFT LOWER CORNER AREA STATION 1305.25 TO STATION 1315.42 SKIN CRACKED REPAIRED AS PER SRM 53-40-15-2R REPAIR 3 FIGURE 201. REPAIR CLASSIFIED AS MAJOR PER G
- [SDR FDEA202301120085](https://openairdocs.org/sdr/FDEA202301120085.md): Seat Track · cracked · Jan 12, 2023 · N621FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > CABIN - MAIN DECK CARGO COMPARTMENT FLOOR SEAT TRACK AT STATION 635 X = -47.5 FOUND CRACKED. CABIN - MAIN DECK CARGO COMPARTMENT FLOOR CRACKED SEAT TRACK AT STATION 635 X = -47.5 REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 625 TO STATION 665
- [SDR FDEA2023012710083](https://openairdocs.org/sdr/FDEA2023012710083.md): Seat Track · cracked · Jan 12, 2023 · N621FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK CARGO COMPARTMENT FLOOR SEAT TRACK AT STATION 695 X = -8 FOUND CRACKED. CABIN - MAIN DECK CARGO COMPARTMENT FLOOR CRACKED SEAT TRACK AT STATION 695 X=-8.5 REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM EXISTING SPLICES STATION 645 TO STATION
- [SDR FDEA202301120081](https://openairdocs.org/sdr/FDEA202301120081.md): Seat Track · cracked · Jan 12, 2023 · N621FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > AGING AIRCRAFT - EXISTING REPAIR AT MAIN DECK CARGO COMPARTMENT SEAT TRACK BETWEEN STATION 745 TO STATION 781 X = -8.5 RIGHT HAND SIDE EXISTING REPAIR AT MAIN DECK CARGO COMPARTMENT SEAT TRACK BETWEEN STATION 745 TO STATION 781 X = -8.5 RIGHT HAND SIDE EV
- [SDR FDEA202301120080](https://openairdocs.org/sdr/FDEA202301120080.md): Seat Track · cracked · Jan 12, 2023 · N621FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > AGING AIRCRAFT - EXISTING REPAIR AT MAIN DECK CARGO COMPARTMENT SEAT TRACK BETWEEN STATION 745 TO STATION 801 X = 27.5 LEFT HAND SIDE EXISTING REPAIR AT MAIN DECK CARGO COMPARTMENT SEAT TRACK BETWEEN STATION 745 TO STATION 801 X = 27.5 LEFT HAND SIDE EVALU
- [SDR FDEA2023012720084](https://openairdocs.org/sdr/FDEA2023012720084.md): Seat Track · cracked · Jan 12, 2023 · N621FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > CABIN - MAIN DECK CARGO COMPARTMENT FLOOR SEAT TRACK AT STATION 695 X = 27.5 FOUND CRACKED. CABIN - MAIN DECK CARGO COMPARTMENT FLOOR CRACKED SEAT TRACK AT STATION 695 X= 27.5 REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM EXISTING SPLICES STATION 64

Next page: https://openairdocs.org/aircraft/N621FE/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 = 'N621FE' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N621FE/reports

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