# Service difficulty reports: N602FE

A list on [N602FE](https://openairdocs.org/aircraft/N602FE.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 11 · 506 reports

- [SDR FDEA202309281664](https://openairdocs.org/sdr/FDEA202309281664.md): Smoke Detector · damaged · Sep 28, 2023 · N602FE · Doug MD11F · Smoke Detection
  > LVL 3 CABIN SMOKE ALERT. COMPLIED WITH QRH. A MID-CABIN SMOKE DETECTOR TRIANGLE FLASHED ON AND OFF DURING EVENT. ALERT WAS OUT DURING LANDING. FSS DID NOT ACTIVATE. REMOVED AND REPLACED THE MAIN CABIN #5 SMOKE DETECTOR IAW AMM 26-15-01-4. ALL SMOKE DETEC
- [SDR FDEA202303310535](https://openairdocs.org/sdr/FDEA202303310535.md): Engine · inoperative · Mar 31, 2023 · N602FE · Doug MD11F · Engine Controls
  > ON APPROACH TO 18R IN MEM, AIRCRAFT WAS STRUCK ON THE NOSE BY LIGHTNING. SUBSEQUENTLY LOST CONTROL OF THE NUMBER 2 ENGINE. ATTEMPTED TO TROUBLESHOOT BUT NO RESPONSE FROM THE ENGINE WITH THROTTLE MOVEMENT. RAN QRH AND SHUTDOWN ENGINE. EMERGENCY DECLARED.
- [SDR FDEA202302180299](https://openairdocs.org/sdr/FDEA202302180299.md): None · leaking · Feb 18, 2023 · N602FE · Doug MD11 · Hydraulic Power System
  > HYDRAULIC 3 FAILED AT SLAT RETRACTION AFTER TAKE-OFF. ***EMERGENCY DECLARED*** FOUND PRESSURE LINE AT SWEDGE GOING TO HORIZONTAL STAB TRIM MOTOR #1 SEPERATED. PERFORMED PERMANENT PIPING TYPE 1 REPAIR ON PRESSURE LINE GOING TO HORIZONTAL STAB TRIM MOTOR #
- [SDR FDEA202211262844](https://openairdocs.org/sdr/FDEA202211262844.md): Msc · faulted · Nov 26, 2022 · N602FE · Doug MD11F · Pitot/Static Anti-Ice System
  > AT FL 370 IN ICING CONDITIONS, RECEIVED A IAS FLAG. HAD AUTOPILOTS DISCONNECT CAPTAINS & FOS AIRSPEEDS SPLIT SIGNIFICANTLY. DECIDED TO DESCEND IN VFR CONDITIONS WHILE RUNNING AIRSPEED UNRELIABLE CHECKLIST. WHILE RUNNING CHECKLIST, CAPTAIN LOOKED LIKE IT
- [SDR FDEA202211172812](https://openairdocs.org/sdr/FDEA202211172812.md): Structure · cracked · Nov 17, 2022 · N602FE · Doug MD11F · Landing Gear Doors
  > RH MLG DOOR CRACKED AT TOP HINGE AREA REOVED AND REPLACED DOOR PER AMM MD11 32-14-20-4.
- [SDR FDEA202208111962](https://openairdocs.org/sdr/FDEA202208111962.md): Engine · failed · Aug 11, 2022 · N602FE · Doug MD11F · Fuel Controlling System
  > ENGINE NR 2 FLAMED OUT DUE TO FUEL STARVATION, CAUSED BY NOT COMPLETING FUEL MANUAL CHECKLIST. NO FAULT STORED IN CFDS RELATED WITH NR 2 ECU. DID NR 2 ECU R-T-S TEST AND PASSED IAW AMM 73-21-05-1. DID NR 2 FUEL BOOST PUMP PRESSURE CHECK AND NO DEFECT FOU
- [SDR FDEA202206301628](https://openairdocs.org/sdr/FDEA202206301628.md): Emer Power · no test · Jun 30, 2022 · N602FE · Doug MD11F · Electrical Power System
  > EMER PWR TST FAIL AFTER TURNING SWITCH TO ARM POSITION. PERFORMED EMERGENCY POWER TEST PER MD11 AMM 24-24-00-5. OPS CHECK GOOD.
- [SDR FDEA202205081149](https://openairdocs.org/sdr/FDEA202205081149.md): Check Valve · malfunctioned · May 8, 2022 · N602FE · Doug MD11F · Fuel Indicating System
  > ENROUTE HNL OVER PHX LVL 2 FUEL QTY/USED CHECK, POSSIBLE FUEL ALERT. DID A FUEL USED SUMMARY AND DETERMINED 3,000 LBS SHORT OF FUEL AND STILL DECREASING. COMPLIED WITH QRH AND ISOLATED ALL TANKS. FUEL STABILIZED 8000# LOW. WE DUMPED 6000# TO LOWER LAN
- [SDR FDEA202204201002](https://openairdocs.org/sdr/FDEA202204201002.md): Panel · delaminated · Apr 20, 2022 · N602FE · Doug MD11F · Fuselage Floor Panel
  > CABIN - FLOOR PANEL #231LF FOUND DELAMINATED AT STATION 675 - 735. DELAMINATED FLOOR PANEL #231LF AT CABIN STATION675 - 735 REMOVED AS PER AMM 53-21- 04. FLOOR PANEL #231LF FABRICATED AS PER FEDEX DRAWING SRZ-25-005 REVISION R. FLOOR PANEL #231LF INSTALLED
- [SDR FDEA202204190990](https://openairdocs.org/sdr/FDEA202204190990.md): Splice · cracked · Apr 19, 2022 · N602FE · Doug MD11F · Fuselage Main, Structure
  > CENTER CARGO BILGE AREA AFTER REMOVAL SPLICE FOR ACCESS AT STATION 5-123 LONGERON 48 LEFT HAND FOUND OUTBROAD SPLICE CRACKED. CENTER CARGO BILGE AREA STATION 5-123 LONGERON 48 LEFT HAND OUTBOARD CRACKED SPLICE REMOVED AND REPLACED AS PER SRM 51-33-01-OG. S
- [SDR FDEA202204120926](https://openairdocs.org/sdr/FDEA202204120926.md): Longeron · cracked · Apr 12, 2022 · N602FE · Doug MD11 · Fuselage Main, Structure
  > CENTER CARGO COMPARTMENT BILGE AT STATION 5-113LONGERON 48 LEFT HAND AFTER REMOVAL OF UPPER DAMAGED SPLICE FOUND LONGERON 48 LEFT HAND CRACKED AT STATION 1538. CENTER CARGO COMPARTMENT BILGE CRACKED LEFT HAND LONGERON 48 AT STATION 1538 REPAIRED AS PER
- [SDR FDEA202204120925](https://openairdocs.org/sdr/FDEA202204120925.md): Splice · corroded · Apr 12, 2022 · N602FE · Doug MD11F · Fuselage Main, Structure
  > CENTRE CARGO BILGE AT STATION 5-113 LONGERON 48 LEFT HAND SPLICE FITTING FOUND CORROSION. CENTRE CARGO BILGE AT STATION 5-113 LONGERON 48 LEFT HAND SPLICE FITTING CORROSION EVALUATED FOUND EXFOLIATED AND EXCEEDED LIMIT AS PER SRM 53-00-00-2R FIGURE 5 R
- [SDR FDEA202204100910](https://openairdocs.org/sdr/FDEA202204100910.md): Rib · cracked · Apr 10, 2022 · N602FE · Doug MD11F · Wing, Plate/Skin
  > WHILE PERFORMING INTERNAL BORESCOPE INSPECTION (SPECIAL/NONROUTINE MAINTENANCE FORM NUMBER N00976), RIGHT HAND WING NUMBER 8 SLAT INTERNAL RIB FOUND CRACK AT LOOSE RIVETS AREA. RIGHT HAND WING NUMBER 8 SLAT INTERNAL LOOSE RIVETS AND CRACKED RIB AT STATION
- [SDR FDEA202204100909](https://openairdocs.org/sdr/FDEA202204100909.md): Rib · cracked · Apr 10, 2022 · N602FE · Doug MD11F · Wing, Plate/Skin
  > WHILE PERFORMING INTERNAL BORESCOPE INSPECTION (SPECIAL/NONROUTINE MAINTENANCE FORM NUMBER N00974), RIGHT HAND WING NUMBER 6 SLAT INTERNAL RIB FOUND CRACK AT LOOSE RIVETS AREA. RIGHT HAND WING NUMBER 6 SLAT INTERNAL LOOSE RIVETS AND CRACKED RIB AT STATION
- [SDR FDEA202204090904](https://openairdocs.org/sdr/FDEA202204090904.md): Seat Track · corroded · Apr 9, 2022 · N602FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > CABIN - RIGHT HAND STATION 5-73 X = - 8.5 SEAT TRACK FLANGE FOUND CORRODED. CORROSION REMOVED AND FOUND EXCEEDED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CORRODED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AT EXISTING SPL
- [SDR FDEA202204090903](https://openairdocs.org/sdr/FDEA202204090903.md): Seat Track · corroded · Apr 9, 2022 · N602FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > CABIN - LEFT HAND STATION 5-73 X = 8.5 SEAT TRACK FLANGE FOUND CORRODED. REMOVED AND FOUND EXCEEDED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CORRODED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 5-43 TO EXISTIN
- [SDR FDEA202204090902](https://openairdocs.org/sdr/FDEA202204090902.md): Seat Track · corroded · Apr 9, 2022 · N602FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > CABIN - RIGHT HAND STATION1259 - 1301, X = - 107.25 SEAT TRACK FLANGE FOUND CORRODED. CORROSION REMOVED AND FOUND EXCEEDED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CORRODED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FR
- [SDR FDEA202204090901](https://openairdocs.org/sdr/FDEA202204090901.md): Spar Cap · corroded · Apr 9, 2022 · N602FE · Doug MD11F · Wing Main, Frame Structure
  > LEFT WING - TRAILING EDGE REAR SPAR LOWER CAP FOUND CORROSION AT STATION XORS 1051 AFTER REMOVAL OF OUTBOARD ISLAND. LEFT WING TRAILING EDGE REAR SPAR LOWER CAP AT STATION XORS 1051 CORROSION REMOVED AND FOUND EXCEED LIMIT AS PER SRM 57-00-10-1A FIGURE 10
- [SDR FDEA202204060878](https://openairdocs.org/sdr/FDEA202204060878.md): Longeron · corroded · Apr 6, 2022 · N602FE · Doug MD11F · Fuselage Main, Longeron/Stringer
  > AFTER REMOVAL OF CORRODED LONGERON 52 SPLICE FITTING AT STATION 1119 - 6-10 LONGERON 52 CORRODED AT 6-10. FOUND LONGERON 52 CORRODED AT 6-10. CORROSION AT LONGERON 52 STATION 6-10 EVALUATED, FOUND EXFOLIATED AND EXCEEDED LIMIT AS PER SRM 53-00-00-2R F
- [SDR FDEA202204060876](https://openairdocs.org/sdr/FDEA202204060876.md): Access Door · cracked · Apr 6, 2022 · N602FE · Doug MD11F · Wing, Plate/Skin
  > DURING HIGH FREQUENCY EDDY CURRENT INSPECTION ON RIGHT HAND WING SLAT OF ACTUATOR ACCESS DOOR FORWARD INBOARD CORNER FOUND 01EA CRACK APPROXIMATELY 0.2 INCH. RIGHT HAND WING SLAT ACTUATOR ACCESS DOOR FORWARD INBOARD CORNER CRACKED AREA AT STATION XOS
- [SDR FDEA202204050846](https://openairdocs.org/sdr/FDEA202204050846.md): Skin · cracked · Apr 5, 2022 · N602FE · Doug MD11 · Wing, Plate/Skin
  > RIGHT HAND WING SLAT TRACK NUMBER 9 CUTOUT LOWER OUTBOARD CORNER SKIN AT APPROXIMATELY STATION XOS 607 FOUND WITH CRACK. RIGHT HAND WING SLAT TRACK NUMBER 9 CUTOUT LOWER OUTBOARD CORNER SKIN AT APPROXIMATELY STATION XOS 607 CRACKED AREA REPAIR CARRIED OUT
- [SDR FDEA202204050845](https://openairdocs.org/sdr/FDEA202204050845.md): Doubler · cracked · Apr 5, 2022 · N602FE · Doug MD11 · Wing, Plate/Skin
  > LEFT HAND WING OUTBOARD LEADING EDGE COMPARTMENT BEADED DOUBLER AT STATION XOS 759 TO 763 FOUND CRACK. LEFT HAND WING OUTBOARD LEADING EDGE COMPARTMENT BEADED DOUBLER AT STATION XOS 759 TO 763 CRACKED AREA REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 1
- [SDR FDEA202204050843](https://openairdocs.org/sdr/FDEA202204050843.md): Doubler · cracked · Apr 5, 2022 · N602FE · Doug MD11 · Wing, Plate/Skin
  > RIGHT HAND WING LEADING EDGE COMPARTMENT BEADED DOUBLER AT STATION XOS 789 TO 795 FOUND CRACK. RIGHT HAND WING LEADING EDGE COMPARTMENT BEADED DOUBLER AT STATION XOS 789 TO 795 CRACKED AREA REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203.
- [SDR FDEA202204050839](https://openairdocs.org/sdr/FDEA202204050839.md): Doubler · cracked · Apr 5, 2022 · N602FE · Doug MD11 · Wing, Plate/Skin
  > RIGHT HAND WING LEADING EDGE COMPARTMENT BEADED DOUBLER AT STATION XOS 637 TO 643 FOUND CRACK. RIGHT HAND WING LEADING EDGE COMPARTMENT BEADED DOUBLER AT STATION XOS 637 TO 643 CRACKED AREA REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203.
- [SDR FDEA202204050837](https://openairdocs.org/sdr/FDEA202204050837.md): Doubler · cracked · Apr 5, 2022 · N602FE · Doug MD11 · Wing, Plate/Skin
  > RIGHT HAND WING LEADING EDGE COMPARTMENT BEADED DOUBLER AT STATION XOS 542 TO 547 FOUND CRACK. RIGHT HAND WING LEADING EDGE COMPARTMENT BEADED DOUBLER AT STATION XOS 542 TO 547 CRACKED AREA REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203.
- [SDR FDEA202204050847](https://openairdocs.org/sdr/FDEA202204050847.md): Skin · cracked · Apr 5, 2022 · N602FE · Doug MD11F · Wing, Plate/Skin
  > RIGHT HAND WING SLAT TRACK NUMBER 12 CUTOUT LOWER OUTBOARD CORNER SKIN AT APPROXIMATELY STATION XOS 776 FOUND WITH CRACK. RIGHT HAND WING SLAT TRACK NUMBER 12 CUTOUT LOWER OUTBOARD CORNER SKIN AT APPROXIMATELY STATION XOS 776 CRACKED AREA REPAIR CARRIED
- [SDR FDEA202204050844](https://openairdocs.org/sdr/FDEA202204050844.md): Doubler · cracked · Apr 5, 2022 · N602FE · Doug MD11F · Wing, Plate/Skin
  > LEFT HAND WING OUTBOARD LEADING EDGE COMPARTMENT BEADED DOUBLER AT STATION XOS 616 TO 621 FOUND CRACK. LEFT HAND WING OUTBOARD LEADING EDGE COMPARTMENT BEADED DOUBLER AT STATION XOS 616 TO 621 CRACKED AREA REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR
- [SDR FDEA202204050842](https://openairdocs.org/sdr/FDEA202204050842.md): Doubler · cracked · Apr 5, 2022 · N602FE · Doug MD11F · Wing, Plate/Skin
  > RIGHT HAND WING LEADING EDGE COMPARTMENT BEADED DOUBLER AT STATION XOS 697 TO 703 FOUND CRACK. RIGHT HAND WING LEADING EDGE COMPARTMENT BEADED DOUBLER AT STATION XOS 697 TO 703 CRACKED AREA REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 2
- [SDR FDEA202204050841](https://openairdocs.org/sdr/FDEA202204050841.md): Doubler · cracked · Apr 5, 2022 · N602FE · Doug MD11F · Wing, Plate/Skin
  > RIGHT HAND WING LEADING EDGE COMPARTMENT BEADED DOUBLER AT STATION XOS 691 TO 697 FOUND CRACK. RIGHT HAND WING LEADING EDGE COMPARTMENT BEADED DOUBLER AT STATION XOS 691 TO 697 CRACKED AREA REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 2
- [SDR FDEA202204050840](https://openairdocs.org/sdr/FDEA202204050840.md): Doubler · cracked · Apr 5, 2022 · N602FE · Doug MD11F · Wing, Plate/Skin
  > RIGHT HAND WING LEADING EDGE COMPARTMENT BEADED DOUBLER AT STATION XOS 643 TO 648 FOUND CRACK. RIGHT HAND WING LEADING EDGE COMPARTMENT BEADED DOUBLER AT STATION XOS 643 TO 648 CRACKED AREA REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203
- [SDR FDEA202204050838](https://openairdocs.org/sdr/FDEA202204050838.md): Doubler · cracked · Apr 5, 2022 · N602FE · Doug MD11F · Wing, Plate/Skin
  > RIGHT HAND WING LEADING EDGE COMPARTMENT BEADED DOUBLER AT STATION XOS 584 TO 588 FOUND CRACK. RIGHT HAND WING LEADING EDGE COMPARTMENT BEADED DOUBLER AT STATION XOS 584 TO 588 CRACKED AREA REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 20
- [SDR FDEA202204040833](https://openairdocs.org/sdr/FDEA202204040833.md): Splice · corroded · Apr 4, 2022 · N602FE · Doug MD11 · Fuselage Main, Structure
  > FORWARD CARGO BILGE FROM STATION 1119 - 6-10 LONGERON 52 SPLICE FITTING FOUND CORROSION. FORWARD CARGO BILGE FROM STATION 1119 TO STATION 6-10 AT LONGERON 52 SPLICE, CORROSION EVALUATED FOUND EXFOLIATED AND EXCEEDED LIMIT AS PER SRM 53-00-00-52- 2R FIGUR
- [SDR FDEA202203190597](https://openairdocs.org/sdr/FDEA202203190597.md): Mfc · failed · Mar 19, 2022 · N602FE · Doug MD11F · Pneumatic Distribution System
  > APPROXIMATELY T/O PLUS 1 HOUR, RECEIVED A LEVEL 1 AIR SYS 2 OFF ALERT. NOTED A RED MANF LIGHT ON R&R ESC PER MM 21-08-01-4, AIR SYSTEM TEST PASS, RAN ALL 3 ENG
- [SDR FDEA202105211351](https://openairdocs.org/sdr/FDEA202105211351.md): Indication Sys · no test · May 21, 2021 · N602FE · Doug MD11F · Emergency Equipment
  > MDIS 602 25-60 1083 21MAY21 LAX OPEN U R1 DOOR EVACUATION SLIDE REMOTE PRESSURE PRESS-TO-TEST INDICATION IS NOT TESTING MEL 21MAY21 12:59 LAX U RELEASED FOR SERVICE PER MEL: 25-61-02 CATEGORY: C EXPIRATION: 31MAY21 "MEL 25-61-02: R1 EVAC
- [SDR FDEA202104210964](https://openairdocs.org/sdr/FDEA202104210964.md): Flange · corroded · Apr 21, 2021 · N602FE · Doug MD11F · Turbine Engine Air Inlet Section
  > NR 2 ENGINE HAS SIGNS OF CORROSION ON FAN CASE FWD FLANGE FROM APPROXIMATELY 4 TO 8 O'CLOCK POS. REFERENCE NONROUTINE N00018 WORK ORDER 79912 ITEM FOUND DURING B-CHECK. CORROSION IS MORE THAN 10 INCHES IN CUMULATIVE CIRCUMFERENCE. CIRCUMFERENCE. REF N1
- [SDR FDEA202103130652](https://openairdocs.org/sdr/FDEA202103130652.md): Retainer · damaged · Mar 13, 2021 · N602FE · Doug MD11F · Fuselage Main, Structure
  > LEFT WHEEL WELL, AFT OUTBOARD DOOR JAMB STRUCTURE, INBOARD FLAP, INBOARD FAIRING SEAL RETAINER CHANNEL DAMAGED DUE TO CONTACT WITH INBOARD FLAP, INBOARD FAIRING. INSTALLED REPAIR DOUBLER PER ENGINEERING AUTHORIZATON 1-5310-T0360413, INSTALLED SEAL AND S
- [SDR FDEA202012183186](https://openairdocs.org/sdr/FDEA202012183186.md): Sensor · making metal · Dec 18, 2020 · N602FE · Doug MD11F · Engine Indicating System
  > AFTER TAKEOFF PASSING 1000', 5 IN SUCCESSION LOUD BANGS WITH HEAVY SHUTTERS. ENGINE INDICATIONS APPEARED NORMAL AND THERE WAS NO YAW ASSOCIATED WITH THE BANG/SHUTTERING. DURING NR 2 ENGINE INLET AND EXHAUST INSPECTION FOUND LEFT HAND FAN STATOR AFT INNER SEG
- [SDR FDEA2020082091933](https://openairdocs.org/sdr/FDEA2020082091933.md): B-Nut · leaking · Aug 19, 2020 · N602FE · Doug MD11F · Hydraulic System, Main
  > HYD 1 OFF LEVEL 1 ALERT 15 MIN INTO CRUISE AT FL380. HYD 1 QTY LO AND HYD 1 PUMP 1R/1L OFF ALERTS CYCLED DURING CONFIGURATION. EMERGENCY DECLARED. SERVICED SYSTEM 1 HYDRAULIC RESERVOIR REF AMM 12-13-02-3. OPERATED NR 1 HYDRAULIC SYSTEM. TRACED LEAK
- [SDR FDEA2020082081928](https://openairdocs.org/sdr/FDEA2020082081928.md): Hydraulic Line · leaking · Aug 18, 2020 · N602FE · Doug MD11F · Hydraulic System, Main
  > HYD 1 OFF LEVEL 1 ALERT, 15 MIN INTO CRUISE AT FL380. HYD 1 QTY LO AND HYD 1 PUMP 1R/1L OFF ALERTS CYCLED DURING CONFIGURATION. EMERGENCY DECLARED. FOUND A FITTING ON ONE OF THE NR 1 BRAKE SYS ACCUMULATORS IN THE LEFT WHEEL WHEEL LOOSE.
- [SDR FDEA202007071452](https://openairdocs.org/sdr/FDEA202007071452.md): Receiver · failed · Jul 7, 2020 · N602FE · Doug MD11F · Ground Proximity System
  > IMMEDIATELY AFTER TAKEOFF, SPURIOUS CAWS WARNINGS BEGAN WITH CONSTANT RAD ALT CALL OUTS. AT ABOUT 4000 FEET MSL 'TAILSTRIKE GO AROUND' ALERT AND AP/AT DISCONNECTED. UNABLE TO RECONNECT AP OR AT AT THIS TIME. AFTER CLIMB TO FL200 AND NO IMPROVEMENT TO CONDIT
- [SDR FDEA2020070211408](https://openairdocs.org/sdr/FDEA2020070211408.md): Fitting · damaged · Jul 1, 2020 · N602FE · Doug MD11F · Vertical Stabilizer Miscellaneous Structure
  > 01 EACH FASTENER HOLE FOUND ELONGATED DURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION AT NUMBER 4 BANJO FITTING RIGHT HAND SIDE AFT 4TH HOLE COUNTING FROM BELOW 01 EACH FASTENER. HOLE ELONGATED DURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION AT
- [SDR FDEA2020070211407](https://openairdocs.org/sdr/FDEA2020070211407.md): Fitting · cracked · Jul 1, 2020 · N602FE · Doug MD11F · Vertical Stabilizer Miscellaneous Structure
  > CRACK INDICATION FOUND ON 01 EACH HOLE DURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION ON SKIN PANEL LAYER AT NUMBER 4 BANJO FITTING. RIGHT HAND SIDE FORWARD EXISTING REPAIR 5TH HOLE COUNTING FROM BELOW CRACK ON 01 EACH HOLE DURING HIGH FREQUENCY EDDY
- [SDR FDEA2020062541325](https://openairdocs.org/sdr/FDEA2020062541325.md): Hinge · corroded · Jun 24, 2020 · N602FE · Doug MD11F · Wing, Control Surface Attach Fittings
  > RIGHT HAND WING OUTBOARD FLAP OUTBOARD HINGE FORWARD (WING SIDE) BARREL NUT HOLE SURFACE CORROSION. CORROSION AT RIGHT HAND WING OUTBOARD FLAP OUTBOARD HINGE FORWARD (WING SIDE) BARREL NUT HOLE SURFACE REWORKED AS PER CMM 57-44-09 AND FOUND EXCEED LIMIT BASED
- [SDR FDEA2020061981268](https://openairdocs.org/sdr/FDEA2020061981268.md): Support Fitting · corroded · Jun 18, 2020 · N602FE · Doug MD11F · Trailing Edge Flaps
  > RIGHT HAND WING TRAILING EDGE - OUTBOARD FLAP VANE NR 5 FROM INBOARD FITTING FOUND CORRODED AROUND HOLE. CORROSION AROUND HOLE WAS REWORKED AND FOUND EXCEEDED LIMITS IAW SRM 57-50-02-2R, REPAIR 5, FIGURE 201. AN OVERSIZED BUSHING WAS FABRICATED IAW SRM 57-
- [SDR FDEA2020061981267](https://openairdocs.org/sdr/FDEA2020061981267.md): Support Fitting · corroded · Jun 18, 2020 · N602FE · Doug MD11F · Trailing Edge Flaps
  > RIGHT HAND WING TRAILING EDGE - OUTBOARD FLAP VANE NR 4 FROM INBOARD FITTING FOUND CORROSION AROUND A HOLE. CORROSION AROUND HOLE AT THE RIGHT WING TRAILING EDGE, OUTBOARD FLAP VANE NR 4 FROM INBOARD FITTING REWORKED AND FOUND EXCEEDS LIMITS IAW SRM 57-50-02-
- [SDR FDEA2020061981266](https://openairdocs.org/sdr/FDEA2020061981266.md): Support Fitting · corroded · Jun 18, 2020 · N602FE · Doug MD11F · Trailing Edge Flaps
  > RIGHT HAND WING TRAILING EDGE - OUTBOARD FLAP VANE NR 3 FROM INBOARD FITTING FOUND WITH HOLE CORRODED. CORROSION AROUND HOLE AT THE RIGHT WING TRAILING EDGE OUTBOARD FLAP VANE NR 3 FROM INBOARD FITTING REWORKED AND FOUND EXCEEDS IAW SRM 57-50-02-2R, REPAI
- [SDR FDEA2020061981265](https://openairdocs.org/sdr/FDEA2020061981265.md): Support · corroded · Jun 18, 2020 · N602FE · Doug MD11F · Trailing Edge Flaps
  > RIGHT HAND WING TRAILING EDGE - OUTBOARD FLAP VANE NR 2 FROM INBOARD FITTING FOUND WITH HOLE CORRODED. CORRODED HOLE AT RIGHT HAND WING TRAILING EDGE - OUTBOARD FLAP VANE #2 FROM INBOARD FITTING REWORKED AND FOUND EXCEEDED LIMITS IAW SRM 57-50-02-2R, REPAI
- [SDR FDEA2020061981264](https://openairdocs.org/sdr/FDEA2020061981264.md): Support Fitting · corroded · Jun 18, 2020 · N602FE · Doug MD11F · Trailing Edge Flaps
  > RIGHT HAND WING TRAILING EDGE - OUTBOARD FLAP VANE NR 1 FROM INBOARD FITTING FOUND WITH HOLE CORRODED. CORRODED HOLE AT RIGHT HAND WING TRAILING EDGE - OUTBOARD FLAP VANE #1 FROM INBOARD FITTING REWORKED BY MACHINING AND FOUN REPAIR CLASSIFIED AS MINOR P
- [SDR FDEA2020061981269](https://openairdocs.org/sdr/FDEA2020061981269.md): Fitting · cracked · Jun 18, 2020 · N602FE · Doug MD11F · Vertical Stabilizer Miscellaneous Structure
  > ULTRASONIC INSPECTION FOUND CRACK INDICATION ON LOWER VERTICAL STABILIZER NR 4 BANJO FITTING RIGHT HAND SIDE FORWARD FLANGE. REPAIR AREA AND UNABLE TO DETERMINE THE CRACK LENGTH DUE TO REPAIR BLOCKAGE AT APPROXIMATE STATION Y=2164 CRACK ON LOWER VERTICAL STAB
- [SDR FDEA202006161251](https://openairdocs.org/sdr/FDEA202006161251.md): Seat Track · damaged · Jun 16, 2020 · N602FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > CABIN, FOUND SEAT TRACK STATION 630, X = 27.5 CROWN DAMAGED. CABIN, DAMAGED CROWN AT SEAT TRACK STATION 630, X = 27.5 EVALUATED AND FOUND TO EXCEED LIMIT AS PER SRM 53-00-52-1A F FIGURE 101 ALLOWABLE DAMAGE 1. CROWN DAMAGED SEAT TRACK REPAIRED BY SECTIONAL S

Next page: https://openairdocs.org/aircraft/N602FE/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 = 'N602FE' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N602FE/reports

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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.