# Service difficulty reports: N578FE

A list on [N578FE](https://openairdocs.org/aircraft/N578FE.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 · 364 reports

- [SDR FDEA202111142890](https://openairdocs.org/sdr/FDEA202111142890.md): None · none · Nov 14, 2021 · N578FE · Doug MD11F · Fire Bottle, Fixed
  > AFT ACCESSORY COMP. RH SIDE HAS CORROSION AROUND NUT PLATES. MWT REPAIRED PER SRM
- [SDR FDEA202108232073](https://openairdocs.org/sdr/FDEA202108232073.md): Slide · detached · Aug 23, 2021 · N578FE · Doug MD11F · Escape Slide
  > UPON RETURNING BACK TO AIRCRAFT FOR MAINTENACE FOUND R1 DOOR ARMED/DISARM HANDLE ARMED FROM OUTSIDE. WHILE OPENING DOOR FROM INSIDE R1 DOOR OPENED AND SLIDE FELL OUT OF AIRCRAFT. SLIDE DID NOT DEPLOY. ALSO FOUND BOTH R1 AND L1 DOOR SLIDE MECHANICAL SAF
- [SDR FDEA202106281605](https://openairdocs.org/sdr/FDEA202106281605.md): Longeron · corroded · Jun 28, 2021 · N578FE · Doug MD11F · Fuselage Main, Longeron/Stringer
  > CENTER CARGO - BILGE STATION 5-11 LONGERON 25 FOUND SURFACE CORROSION. DUPLICATED SDR RAISED, PLEASE REFER TO SNRM #N01050, WORK ORDER 00079485 WITH SDR #21-1568 FOR THE DETAILS.
- [SDR FDEA202106181568](https://openairdocs.org/sdr/FDEA202106181568.md): Longeron · corroded · Jun 18, 2021 · N578FE · Doug MD11F · Fuselage Main, Longeron/Stringer
  > CENTER CARGO - BILGE STATION 5-11 LONGERON 52 FOUND WITH SURFACE CORROSION. CENTER CARGO BILGE STATION 5-11 LONGERON 52 SURFACE CORROSION REMOVED AS PER SRM 51-21-01-OG AND FOUND EXCEEDED LIMIT. LONGERON 52 CARRIED OUT REPAIR AS PER EA 1-5310-T0362561 PART
- [SDR FDEA202106161553](https://openairdocs.org/sdr/FDEA202106161553.md): Support · corroded · Jun 16, 2021 · N578FE · Doug MD11F · Fuselage Miscellaneous Structure
  > AFT CARGO - LEFT HAND SLOPE PANEL #187EL FORWARD SUPPORT STRUCTURE FOUND ONE EACH LOCATION WITH SURFACE CORROSION. AFT CARGO LEFT HAND SLOPE PANEL #187EL FORWARD SUPPORT STRUCTURE ( FRAME) SURFACE CORROSION REMOVED AS PER SRM 51-21-01-OG AND FOUND EX
- [SDR FDEA202106161552](https://openairdocs.org/sdr/FDEA202106161552.md): Floorbeam · cracked · Jun 16, 2021 · N578FE · Doug MD11F · Fuselage Main, Floor Beam
  > CENTER CARGO - FLOOR BEAM STATION 1741 CENTER SECTION FOUND CRACKED. CENTER CARGO FLOOR BEAM STATION 1741 CENTER SECTION CRACKED CARRIED OUT REPAIR AS PER EA 1-5321-T0362363 PART 1. TITLE: FUSELAGE - CARGO COMP FLOORS - LOWER CENTER CARGO FLOOR BEAM REPAIR
- [SDR FDEA202106161551](https://openairdocs.org/sdr/FDEA202106161551.md): Longeron · corroded · Jun 16, 2021 · N578FE · Doug MD11F · Fuselage Miscellaneous Structure
  > AFT CARGO - STATION 1897 LONGERON 44 RIGHT FOUND WITH SURFACE CORROSION. AFT CARGO - STATION 1897 LONGERON 44 RIGHT SURFACE CORROSION REMOVED AS PER SRM 51-21-01-OG AND FOUND CRACKED. CRACKED LONGERON 44 RIGHT AT STATION 1897 CARRIED OUT REPAIR AS PER SRM
- [SDR FDEA202106121518](https://openairdocs.org/sdr/FDEA202106121518.md): Seat Track · corroded · Jun 12, 2021 · N578FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > FORWARD CABIN - SEAT TRACK FROM STATION 430 TO STATION 450 X = 88 FOUND WITH CORROSION. FORWARD CABIN - CORROSION AT SEAT TRACK STATION 430 TO STATION 450, X = 88 EVALUATED FOUND EXFOLIATED AND EXCEEDED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE
- [SDR FDEA202106111498](https://openairdocs.org/sdr/FDEA202106111498.md): Seat Track · cracked · Jun 11, 2021 · N578FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > CABIN - MAIN DECK CARGO COMPARTMENT AFT FLOOR SUPPORT AT STATION 1899 X = 25 FOUND SEAT TRACK CROWN CRACKED. CABIN - MAIN DECK CARGO COMPARTMENT, CRACKED AFT FLOOR SUPPORT AT SEAT TRACK CROWN AREA STATION 1899, X = 25 REMOVED AND REPLACED FROM STATION 18
- [SDR FDEA202106111499](https://openairdocs.org/sdr/FDEA202106111499.md): Seat Track · corroded · Jun 11, 2021 · N578FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > CABIN - MAIN DECK CARGO COMPARTMENT SEAT TRACK FOUND CORROSION AT STATION 1596 X = - 8.5. CABIN - MAIN DECK CARGO COMPARTMENT AT SEAT TRACK STATION 1596 X = - 8.5, CORROSION REMOVED AND EXCEEDED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1.
- [SDR FDEA202106101485](https://openairdocs.org/sdr/FDEA202106101485.md): Skin · chafed · Jun 10, 2021 · N578FE · Doug MD11F · Wing, Plate/Skin
  > RIGHT WING Ï¿½ FIXED LEADING EDGE UPPER SURFACE SKIN FOUND CHAFFED AT XIS 265. RIGHT WING FIXED LEADING EDGE UPPER SURFACE SKIN FOUND CHAFFED AT XIS 265 REPAIR CARRIED OUT AS PER EA# 1-5730-T0362334 P1. TITLE: WINGS Ï¿½ PLATES AND SKINS Ï¿½ RH WING Ï¿½ CHA
- [SDR FDEA202106101484](https://openairdocs.org/sdr/FDEA202106101484.md): Doubler · cracked · Jun 10, 2021 · N578FE · Doug MD11F · Wing, Plate/Skin
  > LEFT WING Ï¿½ FIXED LEADING EDGE BEADED DOUBLER AT XOS 645 FOUND CRACK. LEFT WING FIXED LEADING EDGE DOUBLER AT XOS 645 REPAIR CARRIED OUT AS PER SRM 57- 40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
- [SDR FDEA202106101483](https://openairdocs.org/sdr/FDEA202106101483.md): Stringer · cracked · Jun 10, 2021 · N578FE · Doug MD11F · Wing, Longeron/Stringer
  > RIGHT WING Ï¿½ FIXED LEADING EDGE STRINGER AT XOS 664 FOUND CRACK. RIGHT WING FIXED LEADING EDGE STRINGER AT XOS 664 REPAIR CARRIED OUT AS PER SRM 57- 40-03-2R REPAIR 2 FIGURE 202. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
- [SDR FDEA202106071456](https://openairdocs.org/sdr/FDEA202106071456.md): Doubler · corroded · Jun 7, 2021 · N578FE · Doug MD11F · Wing, Plate/Skin
  > RIGHT WING - UPPER WING SURFACE MAIN LANDING GEAR SUPPORT UPPER DOUBLER FOUND CORROSION AT BETWEEN XW 212 AND XW 229.5 RIGHT WING - UPPER WING SURFACE MAIN LANDING GEAR SUPPORT UPPER DOUBLER CORROSION REMOVED AND FOUND EXCEED LIMIT AS PER SRM 57-20-01-1A F
- [SDR FDEA202106071455](https://openairdocs.org/sdr/FDEA202106071455.md): Doubler · corroded · Jun 7, 2021 · N578FE · Doug MD11F · Wing, Plate/Skin
  > LEFT WING - UPPER WING SURFACE MAIN LANDING GEAR SUPPORT UPPER DOUBLER FOUND CORROSION AT YW 467 LEFT WING - UPPER WING SURFACE MAIN LANDING GEAR SUPPORT UPPER DOUBLER CORROSION REMOVED AND FOUND EXCEED LIMIT AS PER SRM 57-20-01-1A FIGURE 101 ALLOWABLE D
- [SDR FDEA202106071459](https://openairdocs.org/sdr/FDEA202106071459.md): Doubler · cracked · Jun 7, 2021 · N578FE · Doug MD11F · Wing, Plate/Skin
  > RIGHT WING Ï¿½ FIXED LEADING EDGE RIB DOUBLER AT XOS 789 FOUND CRACK. CRACKED RIB DOUBLER REMOVED AS PER SRM 51-31-01-0G AND FABRICATED DOUBLER PER DOUGLAS DRAWING ARB3954 REVISION K. INSTALLED FABRICATED DOUBLER AT RIGHT WING FIXED LEADING EDGE AT XOS 789
- [SDR FDEA202106071458](https://openairdocs.org/sdr/FDEA202106071458.md): Doubler · cracked · Jun 7, 2021 · N578FE · Doug MD11F · Wing, Plate/Skin
  > RIGHT WING Ï¿½ FIXED LEADING EDGE BEADED DOUBLER AT XOS 664 FOUND CRACK. RIGHT WING FIXED LEADING EDGE DOUBLER AT XOS 664 REPAIR CARRIED OUT AS PER SRM 57- 40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
- [SDR FDEA202106071457](https://openairdocs.org/sdr/FDEA202106071457.md): Doubler · cracked · Jun 7, 2021 · N578FE · Doug MD11F · Wing, Plate/Skin
  > RIGHT WING Ï¿½ FIXED LEADING EDGE BEADED DOUBLER AT XOS 785 FOUND CRACK. RIGHT WING FIXED LEADING EDGE DOUBLER AT XOS 785 REPAIR CARRIED OUT AS PER SRM 57- 40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
- [SDR FDEA202106071460](https://openairdocs.org/sdr/FDEA202106071460.md): Skin · cracked · Jun 7, 2021 · N578FE · Doug MD11F · Wing, Plate/Skin
  > RIGHT WING Ï¿½ FIXED LEADING EDGE LOWER SURFACE NO.14 SLAT TRACK CUTOUT SKIN AT XOS 891 FOUND CRACK. RIGHT WING FIXED LEADING EDGE LOWER SURFACE NO.14 SLAT TRACK CUTOUT SKIN AT XOS 891 REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 7 FIGURE 201. REPAIR C
- [SDR FDEA201910312794](https://openairdocs.org/sdr/FDEA201910312794.md): Indication Sys · faulty · Oct 31, 2019 · N578FE · Doug MD11F · Fuel Quantity Indicator
  > PDIS 578 28-41 3074 31OCT19 HNL OPEN U LOGPAGES:2605567 APPROX. 2.2 HRS INTO FLIGHT LEVEL 2 FUEL QTY/USED CHK ALERT CAME ON. COMPLIED WITH QRH PROCEDURE FUEL USED CALCULATING FUEL USED HAD FUEL AT 175K. FUEL GAUGES ADDED UP TO 166K. DIFF OF 9
- [SDR FDEA201908091820](https://openairdocs.org/sdr/FDEA201908091820.md): Restrictor · malfunctioned · Aug 9, 2019 · N578FE · Doug MD11F · Trailing Edge Flap Control System
  > AFTER TAKEOFF WHEN RETRACTING FLAPS RECEIVED LEVEL 2 FLAP DISAG. FLAP INDICATED 6,6,7,7 WITH HANDLE IN UP/0 EXT POSITION. RAN QRH. (DUMPED FUEL FROM 75.2 TO 50.0 POUNDS.) MATCHED UP FLAP HANDLE TO 7 MARK, BUT FLAP INDICATED 0. NORMAL LANDING. IDENTIFIED PARTS
- [SDR FDEA201907101526](https://openairdocs.org/sdr/FDEA201907101526.md): Battery · discharged · Jul 10, 2019 · N578FE · Doug MD11F · Emergency Equipment
  > R1 DOOR SLIDE WILL NOT TEST. REPLACED BATTERIES IN R1 DOOR SLIDE REMOTE PRESSURE INDICATOR REFERENCE AMM 25-61-04-4. OPS CHECKS GOOD REFERENCE AMM 25-61-04-5.
- [SDR FDEA201905071009](https://openairdocs.org/sdr/FDEA201905071009.md): Seat Track · damaged · May 7, 2019 · N578FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > REFERENCE WORK ROUTINE ITEM # 25502426, MAIN DECK CARGO COMPARTMENT FLOOR SEAT TRACK FOUND WITH BROKEN LOBE AT STATION 1673 X = - 8 ( MEL # 25-57-02-B) MAIN DECK CARGO COMPARTMENT DAMAGED SEAT TRACK AT STATION 1673 X = - 8 REPAIRED BY SECTIONAL SEAT TRACK REP
- [SDR FDEA2019022650497](https://openairdocs.org/sdr/FDEA2019022650497.md): Battery Pack · weak · Feb 25, 2019 · N578FE · Doug MD11F · Emergency Lighting
  > EMER LT BAT 1 LO. PART 25FEB19 10:27 ICN U IDENTIFIED PARTS EMERG EXIT LIGHTS " RELEASED FOR SERVICE PER MEL: 33-50-04 CATEGORY: C EXPIRATION: 07MAR19 MEL 33-50-04: EMER LIGHTS - INOP." THE PART NIS IN ICN.
- [SDR FDEA201901010002](https://openairdocs.org/sdr/FDEA201901010002.md): Controller · malfunctioned · Jan 1, 2019 · N578FE · Doug MD11F · Airfoil Anti/De-ice System
  > PDIS 578 30-10 1981 01JAN19 MEM FACT U LOGPAGES:2850976 ON CLIMBOUT PRIOR TO ENTERING CLOUDS WE SELECT AIRFRAME AND ENGINE ANTI ICE ON. GOT A/I DISAG. ALERT AND YELLOW ON RIGHT WING ANTI ICE VALVE. NO ICEING ENCOUNTERED SELECTED ANTI-ICE OFF AND NOW SHOW RIGHT
- [SDR FDEA201812053441](https://openairdocs.org/sdr/FDEA201812053441.md): Fuel Sys · unknown · Dec 5, 2018 · N578FE · Doug MD11F · Aircraft Fuel System
  > SUSPECTED FUEL LEAK ENROUTE 2 HOURS INTO FLIGHT FUEL WAS 4000 LBS LOWER THAN EXPECTED. 15 MINUTES LATER RECEIVED FUEL QTY CHK ALERT. RAN QRH CHECKLIST & DETERMINED LEAK WAS IN UPPER AUX ESTIMATE 10000 LBS OF FUEL LEAKED.PULLED AND RESET FUEL QTY NORMAL POWER A
- [SDR FDEA201809202632](https://openairdocs.org/sdr/FDEA201809202632.md): Warning System · activated · Sep 20, 2018 · N578FE · Doug MD11F · Cabin Pressure Control System
  > ALT FL350 CABIN ALTITUDE LEVEL 3 ALERT. FASE 1S TO QRH. REF FIM 21-33-00-2 FIG 103 CHECKED BOTH CPC'S FOR BLOCKAGE AND NONE FOUND. CFDS FAULTS ACC1 WITH PK 1 RAD ACT IN LAST LEG BUT NO CURENT FAULTS. DEFERED PACK NR 1 RAM AIR ACTUATOR WRI 21-52-1583. PERFORME
- [SDR FDEA201806211550](https://openairdocs.org/sdr/FDEA201806211550.md): Longeron · corroded · Jun 21, 2018 · N578FE · Doug MD11F · Fuselage Main, Longeron/Stringer
  > LOWER CENTER CARGO BILGE AREA FOUND LONGERON 43R WITH CORROSION, AT STA 1649. CARRIED OUT SECTIONAL SPLICE REPAIR BETWEEN STA 1631 TO STA 1650 LONGERON 43R AS PER SRM 53-00-05-2R REPAIR 1 FIGURE 201 AND FIGURE 202. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. C
- [SDR FDEA201806141483](https://openairdocs.org/sdr/FDEA201806141483.md): Skin · cracked · Jun 14, 2018 · N578FE · Doug MD11F · Wing, Plate/Skin
  > DURING HFEC INSPECTION ON LT WING FIXED LEADING EDGE SKIN ADJACENT TO CUTOUT AND ACCESS DOORS, CRACKS FOUND APPROX 1/8 INCH IN LENGTH AT CORNER NR 5 AT SLAT ACTUATOR ACCESS DOOR FWD INBD CORNER, AT STA XOS 490.850. REPAIR CARRIED OUT AT LT WING FIXED LEADING E
- [SDR FDEA201806141482](https://openairdocs.org/sdr/FDEA201806141482.md): Structure · cracked · Jun 14, 2018 · N578FE · Doug MD11F · Fuselage Miscellaneous Structure
  > AFT FUSELAGE FWD UPPER TORQUE BOX RT ACCESS CUTOUT FOUND THE EDGE CRACKED. REPAIRED IAW SRM 53-70-02-2R, FIGURE 201, REPAIR 3. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.
- [SDR FDEA201806131471](https://openairdocs.org/sdr/FDEA201806131471.md): Seat Track · cracked · Jun 13, 2018 · N578FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > FWD CABIN SEAT TRACK WAS FOUND CRACKED AT BS 635, RBL 8.5. THE SEAT TRACK WAS REPLACED BETWEEN BS 625 TO 665 IAW SRM 53-00-52-2R, FIGURE 201 REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.
- [SDR FDEA201806131470](https://openairdocs.org/sdr/FDEA201806131470.md): Seat Track · cracked · Jun 13, 2018 · N578FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > FWD CABIN SEAT TRACK FOUND CRACK AT STA 635 X= 47.5 AS MARKED. SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT FROM STA 605 TO STA 645 X= 47.5 AS PER SRM 53-00-52 FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
- [SDR FDEA201806131469](https://openairdocs.org/sdr/FDEA201806131469.md): Seat Track · cracked · Jun 13, 2018 · N578FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > FWD CABIN SEAT TRACK FOUND CRACK AT BS 635, 27.5. THE SEAT TRACK WAS REPLACED BETWEEN BS 625 - 665 IAW SRM 53-00-52-2R, FIGURE 201, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.
- [SDR FDEA201806131468](https://openairdocs.org/sdr/FDEA201806131468.md): Seat Track · cracked · Jun 13, 2018 · N578FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > FWD CABIN SEAT TRACK FOUND CRACKED AT BS 635 LBL 8.5. REPLACED THE SEAT TRACK BETWEEN BS 625 - 665 IAW SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
- [SDR FDEA201806131467](https://openairdocs.org/sdr/FDEA201806131467.md): Seat Track · corroded · Jun 13, 2018 · N578FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > CABIN, MAIN DECK CARGO SEAT TRACK CORRODED, BS 1311, RBL 27.5. CORROSION REMOVED AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPLACED, BS 1266 TO 1331 IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. REPAIR
- [SDR FDEA201806121456](https://openairdocs.org/sdr/FDEA201806121456.md): Web · cracked · Jun 12, 2018 · N578FE · Doug MD11F · Fuselage Miscellaneous Structure
  > BS 1841, LONGERON 46L WEB WAS FOUND CRACKED. REPAIRED IAW SRM 53-00-00-2R, FIGURE 211, REPAIR GENERAL. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.
- [SDR FDEA201806121455](https://openairdocs.org/sdr/FDEA201806121455.md): Web · cracked · Jun 12, 2018 · N578FE · Doug MD11F · Fuselage Miscellaneous Structure
  > BS 1841, LONGERON 46R WEB WAS FOUND CRACKED. REPAIRED IAW SRM 53-00-00-2R, FIGURE 211, REPAIR GENERAL. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.
- [SDR FDEA201806121454](https://openairdocs.org/sdr/FDEA201806121454.md): Seal · chafed · Jun 12, 2018 · N578FE · Doug MD11F · Wing Miscellaneous Structure
  > RT WING DROOP LEADING EDGE INBD METAL SEAL CHAFED AT STA XDLE 310. REPAIR CARRIED OUT AT R WING DROOP LEADING EDGE INBD SIDE AS PER SRM 57-40-01-2R FIGURE 202 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
- [SDR FDEA201806121450](https://openairdocs.org/sdr/FDEA201806121450.md): Doubler · cracked · Jun 12, 2018 · N578FE · Doug MD11F · Wing, Plate/Skin
  > LT WING LEADING EDGE CAVITY BEADED DOUBLER AT STA XOS 663 FOUND CRACKED. REPAIR CARRIED OUT AT LT WING LEADING EDGE CAVITY BEADED DOUBLER AT XOS 663 AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.
- [SDR FDEA201806121449](https://openairdocs.org/sdr/FDEA201806121449.md): Doubler · cracked · Jun 12, 2018 · N578FE · Doug MD11F · Wing, Plate/Skin
  > RT WING LEADING EDGE CAVITY BEADED DOUBLER AT XOS 613 WAS FOUND CRACKED. REPAIRED THE DOUBLER IAW SRM 57-40-02-2R, FIGURE 203, REPAIR 15. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.
- [SDR FDEA2018061201433](https://openairdocs.org/sdr/FDEA2018061201433.md): Frame · chafed · Jun 9, 2018 · N578FE · Doug MD11F · Fuselage Main, Frame
  > MAIN DECK CARGO, FRAME CHAFED AT BS 535, LONGERON 24R. THE FRAME WAS REPAIRED IAW SRM 53-20-07-2R, FIGURE 201, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.
- [SDR FDEA2018061201432](https://openairdocs.org/sdr/FDEA2018061201432.md): Frame · chafed · Jun 9, 2018 · N578FE · Doug MD11F · Fuselage Main, Frame
  > MAIN DECK CARGO FRAME WAS CHAFED AT BS 535, LONGERON 19R. REPAIRED THE FRAME IAW SRM 53-20-07-2R, FIGURE 202, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
- [SDR FDEA201804201069](https://openairdocs.org/sdr/FDEA201804201069.md): Trim Cylinder · contaminated · Apr 20, 2018 · N578FE · Doug MD11F · Landing Gear Retraction/Extension System
  > PDIS 578 32-30 0989 20APR18 CDG OPEN U LOGPAGES:2925462 AFTER TAKEOFF LANDING GEAR WOULD NOT RETRACT. GEAR HANDLE WOULD NOT MOVE TO UP POSITION. RAN QRH "GEAR HANDLE WILL NOT MOVE TO UP POSITION "NO HELP. RETURNED TO LAND LFPG. ALSO WHEN PUSHING HANDLE RELEASE
- [SDR FDEA201712143388](https://openairdocs.org/sdr/FDEA201712143388.md): Actuator · sheared · Dec 14, 2017 · N578FE · Doug MD11F · Landing Gear Steering System
  > ON TAKE OFF, NOSE GEAR DID NOT RETRACT. HEARD RUMBLING NOISE. UNSAFE NOSE GEAR UP INDICATION. L/H STEERING ACTUATOR EYE END FOUND BROKEN. ACTUATOR REPLACED IAW MD11 MM 32-52-30-4. L/CHK C/OUT NIL LEAK FOUND.
- [SDR FDEA201710293102](https://openairdocs.org/sdr/FDEA201710293102.md): Switch · loose · Oct 29, 2017 · N578FE · Doug MD11F · Extinguishing System
  > FOUND WIRES LOOSE ON NR 1 ENG AGENT 1. REMOVED AND REPLACED ENGINE 1, AGENT 1 DISCHARGE SWITCH S1-161 PER AMM 26-21-02-4. SYSTEM OP CHECKS GOOD PER 26-21-01-5. SWITCH PART NUMBER BZ2RT, NO SERIAL NUMBER, MANUFACTURER, MICRO. REMOVED AND REPLACED ENGINE 1,
- [SDR FDEA201707071874](https://openairdocs.org/sdr/FDEA201707071874.md): Warning System · false activation · Jul 7, 2017 · N578FE · Doug MD11F · Door Warning System
  > DURING CLIMBOUT, RECIEVED A LEVEL 2 FWD CARGO DOOR B ALERT. CARGO DOOR FWD CARGO DOOR B ALERT (IDENTIFY) ALERT -INOP. VERIFY DOOR IS CLOSED AND LOCKED PRIOR TO BLOCK-OUT.
- [SDR FDEA201707051855](https://openairdocs.org/sdr/FDEA201707051855.md): Hinge · worn · Jul 5, 2017 · N578FE · Doug MD11F · Fuselage, Door Hinge
  > CENTER CARGO DOOR HINGE WORN. REPLACED THE DOOR.
- [SDR FDEA201703030767](https://openairdocs.org/sdr/FDEA201703030767.md): Tire · failed · Mar 3, 2017 · N578FE · Doug MD11F · Tire Tube
  > 35 MINUTES INTO FLIGHT, RECEIVED A TIRE FAILURE ALERT. THE NR 6 TIRE INDICATIONS WENT BLANK. REMOVED AND REPLACED THE NR 6 TIRE AND WHEEL ASSMBLY. TIRE PRESSURE CHECKED OK ON CONFIGURATION PAGE.
- [SDR FDEA201611174081](https://openairdocs.org/sdr/FDEA201611174081.md): Proximity Sensor · malfunctioned · Nov 17, 2016 · N578FE · Doug MD11F · Door Warning System
  > DURING FLIGHT, RECEIVED A LEVEL 2 CARGO DOOR FWD B ALERT. RAN THE QRH AND THE ALERT REMAINED ON AND RETURNED TO DEPARTURE. R & R THE FORWARD LOWER CARGO DOOR PROXIMITY SENSOR IAW AMM 52-70-01-4. DOOR OPERATED NORMALLY IN OPEN/CLOSE MODE. ELECTRICAL T
- [SDR FDEA201606172032](https://openairdocs.org/sdr/FDEA201606172032.md): Seat Track · damaged · Jun 17, 2016 · N578FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK CARGO APPROXIMATE AT STA 5-4, X=-8.75 SEAT TRACK CROWN FOUND DAMAGED. SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT FROM STA 5-0 TO STA 5-63, X = -8.75 IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Next page: https://openairdocs.org/aircraft/N578FE/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 = 'N578FE' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N578FE/reports

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