# Service difficulty reports: N377FE, cancelled Mar 2, 2024

A list on [N377FE, cancelled Mar 2, 2024](https://openairdocs.org/deregistered/N377FE-2024-03-02.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 2 · 95 reports

- [SDR FDEA201502200555](https://openairdocs.org/sdr/FDEA201502200555.md): Limit Switch · failed · Feb 20, 2015 · N377FE · Doug MD1010F · Emergency Equipment
  > R1 DOOR ARM & DISARM LEVER IS DIFFICULT TO MOVE IN EITHER DIRECTION. THE LEVER MUST BE PUSHED AGAINST THE STOP TO EXTINGUISH THE DISARM LIGHT. REMOVED AND REPLACED THE R1 DOOR GIRT BAR LIMIT SWITCH. LUBED ARM LEVER ASSY, OPS CHECKED NORMAL, NO ADJUSTMENT R
- [SDR FDEA201412114106](https://openairdocs.org/sdr/FDEA201412114106.md): Lamp · inoperative · Dec 11, 2014 · N377FE · Doug MD1010F · Escape Slide
  > L1 DOOR SLIDE LIGHT WILL NOT TEST. REMOVED & RE LAMPED L1 DOOR SLIDE PRESS INDICATION LIGHT ASSEMBLY & REINSTALLED. OPERATIONS CHECK IS GOOD.
- [SDR FDEA201408042330](https://openairdocs.org/sdr/FDEA201408042330.md): Skin · cracked · Aug 4, 2014 · N377FE · Doug MD1010F · Wing, Plate/Skin
  > RIGHT WING FOUND CRACK AT UPPER RT INBD CORNER OF TAI CUT OUT. FACTED IN ERROR WITH NO DEFECTS SEQ 225 WRI 57-10-4400. COMPLIED WITH EA 8-5720-T0310225 P1 BY REPAIRING USING SRM 57-40-01 FIG 201.
- [SDR FDEA201408042329](https://openairdocs.org/sdr/FDEA201408042329.md): Skin · cracked · Aug 4, 2014 · N377FE · Doug MD1010F · Wing, Plate/Skin
  > EVIDENCE OF CRACKING AT UPPER INBD CORNER OF LT WING TAI DUCT CUT OUT ON THE FIXED LE SKIN. COMPLIED WITH EA 8-5720-T0310221 P1 BY REPAIRING USING SRM 57-40-01 FIG 201.
- [SDR FDEA201405131044](https://openairdocs.org/sdr/FDEA201405131044.md): Skin · cracked · May 13, 2014 · N377FE · Doug MD1010F · Wing, Plate/Skin
  > POST FLIGHT WALK AROUND, FOUND POSSIBLE CRACK AT RT REFUELING DOOR INBD RADIUS ON WING. INSTALLED DOUBLER IAW SRM 57-10-00 & EA 8-5710-T0308147.
- [SDR FDEA201401050022](https://openairdocs.org/sdr/FDEA201401050022.md): Slide · faulty · Jan 5, 2014 · N377FE · Doug MD1010F · Escape Slide
  > L1 DOOR LOW BOTTLE PRESS INDICATOR LIGHT ILLUMINATED. REMOVED L1 DOOR SLIDE LOWER COVER & TROUBLESHOOT IAW ASM 25-61-0. FOUND CONTINUITY AT LIGHT ASSEMBLY JACK CONNECTOR. REPLACED L1 DOOR SLIDE IAW AMM 25-61-02-4.
- [SDR FDEA201311242864](https://openairdocs.org/sdr/FDEA201311242864.md): Sensor · faulty · Nov 24, 2013 · N377FE · Doug MD1010F · Pneumatic Indicating System
  > ON CLIMB OUT LEVEL 3 BLED AIR 1 TEMP HI COMPLIED WITH QRH NO FURTHER INDICATION DURING RETURN. RELEASED FOR SERVICE IAW MEL 36-10-02-A. REMOVED AND REPLACED PNEU TEMP SENSOR B3-18 PER FIM 36-10-11 STEP K AND MM 36-22-01-2. NO FAULTS NOTED. TAXIED A/C TO RUN
- [SDR FDEA201310152510](https://openairdocs.org/sdr/FDEA201310152510.md): Spar · corroded · Oct 15, 2013 · N377FE · Doug MD1010F · Nacelle/Pylon, Frame/Spar/Rib
  > NR 1 PYLON UPPER SPAR CAP INBD LANDING IS CORRODED. CLEANED CORRISION AND BLENDED LANDING PER SRM 51-21-01 VOL II AND EA 8-5450-T0303216.
- [SDR FDEA201310152512](https://openairdocs.org/sdr/FDEA201310152512.md): Channel · cracked · Oct 15, 2013 · N377FE · Doug MD1010F · Nacelle/Pylon Miscellaneous Structure
  > NR 1 PYLON, BRACKET BETWEEN LT AND RT LOWER SPARS CRACKED APPROXIMATELY 3 INCHES LONG. REMOVED CRACKED CHANNEL, FABRICATED NEW CHANNEL, IAW DWG AUB7009. INSTALLED CHANNEL IAW SRM 51-33-01, VOL II.
- [SDR FDEA201309252314](https://openairdocs.org/sdr/FDEA201309252314.md): Bulkhead · cracked · Sep 25, 2013 · N377FE · Doug MD1010F · Fuselage Main, Bulkhead
  > NLG WHEEL WELL, RT BULKHEAD WEB CRACKED. ABOUT 3.5 INCHES LONG, AT BS 480, X= -6. INSTALLED FILLER SHIM AND DOUBLER IAW SRM 53-30-30 VOL.1 FIG.6.
- [SDR FDEA201303050497](https://openairdocs.org/sdr/FDEA201303050497.md): Proximity Sensor · misinstalled · Mar 5, 2013 · N377FE · Doug MD1010F · Landing Gear Position and Warning
  > AFTER TAKEOFF, RAISED LANDING GEAR; RT MAIN INDICATED UNSAFE (RED) ON FWD PANEL AND SYNOPTIC. FOLLOWED QRH PROCEDURE, SLOWED AND CYCLED GEAR AFTER SECOND RETRACTION, ALL INDICATIONS WERE NORMAL. FOUND PROXIMITY SENSOR LINK LOWER BOLT NOT INSTALLED THROUG
- [SDR FDEA201302260462](https://openairdocs.org/sdr/FDEA201302260462.md): Wire · burned · Feb 26, 2013 · N377FE · Doug MD1010F · Landing Gear System Wiring
  > WIRE B9502-108-16 HAS BURN SIGNS, LOCATED BELOW THE RT OBSERVER CONSOLE THRU ACCESS PANEL ABN7643-139. REPAIRED WIRE B9502-108-16 IAW SWP 20-10-03, SECTION 7D. INSTALLED SPLICE: WDM 46-20-21. REPOSITIONED HARNESS TO PREVENT CHAFING.
- [SDR FDEA201302070293](https://openairdocs.org/sdr/FDEA201302070293.md): Control Unit · failed · Feb 7, 2013 · N377FE · Doug MD1010F · Brake Anti-Skid Section
  > ANTI-SKID LT FAIL ALERT DURING PREFLIGHT CLEARED AFTER SUBSEQUENT SELF TEST. EXTENDED GEAR AND ANTI-SKID LT FAILED AGAIN. COMPLETED CHECKLIST AND DECLEARED EMERGENCY. LANDING AND BRAKING NORMAL. R & R ANTI-SKID CONTROL UNIT IAW MM 32-45-01-4. OPS CHECK IA
- [SDR FDEA201210053570](https://openairdocs.org/sdr/FDEA201210053570.md): Anti-Skid Sys · malfunctioned · Oct 5, 2012 · N377FE · Doug MD1010F · Brake Anti-Skid Section
  > LEFT ANTI-SKID FAIL GO AROUND, RAN QRH ON SECOND GEAR EXTENSION NO ANTI-SKID FAIL. PERFORMED RTS ON VIA 1 ALL CHECKS GOOD. PERFORMED BITE TEST ON ANTI SKID CONTROL UNIT IAW PLACARDED INSTRUCTIONS, ALL TESTS GOOD. PERFORMED OPS TEST OF ANTI SKID SYS IAW AMM
- [SDR FDEA201209183349](https://openairdocs.org/sdr/FDEA201209183349.md): Tee Fitting · cracked · Sep 18, 2012 · N377FE · Doug MD1010F · Fuselage Main, Structure
  > LEFT SIDEWALL TO SPAR ATTACH TEE FITTING HAS A THREE INCH CRACK 1.5" DOWN FROM SPAR CAP. REMOVED TEE FITTING IAW SRM 51-35-01. FABRICATED PART APB 7078-1 IAW DWG APB 7078. INSTALLED TEE FITTING IAW STM 51-33-01. S
- [SDR FDEA201204041253](https://openairdocs.org/sdr/FDEA201204041253.md): Sensor · failed · Apr 4, 2012 · N377FE · Doug MD1010F · Landing Gear Position and Warning
  > RIGHT MLG INTERMITTENT RED UNSAFE UP & LOCKED. BOTH PRIMARY & SECONDARY, QRH FOLLOWED. REMOVED RT MLG DOWNLOCK SENSOR D1-43. REPLACED PINS AND CONNECTOR ON NEW DOWN LOCK SENSOR PER MM 20-30-02-2-0. INSTALLED RT MAIN GEAR DOWN LOCK SENSOR 'A' PER MM 32-61-
- [SDR FDEA201108253479](https://openairdocs.org/sdr/FDEA201108253479.md): Power Supply · failed · Aug 25, 2011 · N377FE · Doug MD1010F · Emergency Lighting
  > WHILE PREPPING ACFT FOR DEPARTURE, EMERGENCY LIGHT TEST FAIL. INDICATED EMERGENY LIGHT BATTERY 1 LOW. FOUND EMERGENCY LIGHT BATTERY POWER SUPPLY FAULTY. R & R EMERGENCY LIGHT BATTERY POWER SUPPLY IAW MM 33-51-01-4. EMERGENCY LIGHTS, OPS CHECKED GOOD.
- [SDR FDEA201102100521](https://openairdocs.org/sdr/FDEA201102100521.md): Bulb · wrong part · Feb 10, 2011 · N377FE · Doug MD1010F · Escape Slide
  > L1 DOOR SLIDE PRESSURE, PRESS TO TEST LIGHT INOPERATIVE. FOUND WRONG BULBS INSTALLED IN LIGHT SOCKET, INSTALLED PROPER BULBS PER STANDARD MAINT. PRACTICES, OPS CHECKED GOOD.
- [SDR FDEA201012264753](https://openairdocs.org/sdr/FDEA201012264753.md): Pressure Switch · inoperative · Dec 26, 2010 · N377FE · Doug MD1010F · Engine Anti-Icing System
  > ON DESCENT TURNED ON ENG - WING ANTI-ICE RECEIVED "A WING A-ICE L DISAG ALERT SHORTLY AFTER RECEIVED AN AIR MANF 1 FAIL" COMPLIED WITH QRH AND DIVERTED, WITHOUT INCIDENT. R & R LT MANIFOLD FAILURE DETECTION PRESSURE SWITCH IAW MM 36-23-03-4. ALSO REPLACED NR
- [SDR FDEA200912024335](https://openairdocs.org/sdr/FDEA200912024335.md): Frame · cracked · Dec 2, 2009 · N377FE · Doug MD1010F · Fuselage Main, Frame
  > MAIN CARGO STA 1721, RT LONGERON NR 13, FRAME CRACKED N1080 WAS GENERATED TO REPAIR ALL AFFECTED AREAS. THIS CRACKED FRAME SECTION AT THE ABOVE STA AND LONGERON WERE REMOVED WITH NEW SECTIONS AND SPLICES. THIS IS A CATEGORY "B" REPAIR AND REQUIRE A 12,000 CYC
- [SDR FDEA200912024334](https://openairdocs.org/sdr/FDEA200912024334.md): Frame · cracked · Dec 2, 2009 · N377FE · Doug MD1010F · Fuselage Main, Frame
  > MAIN CARGO, STA 1741, RT, LONGERON NR 13, FRAME CRACKED N1079 WAS GENERATED TO REPAIR ALL AFFECTED AREAS. THIS CRACKED FRAME SECTION AT THE ABOVE STA AND LONGERON WERE REMOVED WITH NEW SECTIONS AND SPLICES. N THIS IS A CATEGORY "B" REPAIR AND REQUIRE A 12,000
- [SDR FDEA200912024333](https://openairdocs.org/sdr/FDEA200912024333.md): Frame · cracked · Dec 2, 2009 · N377FE · Doug MD1010F · Fuselage Main, Frame
  > MAIN CARGO, STA NR 1781, LT LONGERON NR 13, FRAME CRACKED N1078 WAS GENERATED TO REPAIR ALL AFFECTED AREAS. THIS CRACKED FRAME SECTION AT THE ABOVE STA AND LONGERON WERE REMOVED WITH NEW SECTIONS AND SPLICES. THIS IS A CATEGORY "B" REPAIR AND REQUIRE A 12,00
- [SDR FDEA200912024332](https://openairdocs.org/sdr/FDEA200912024332.md): Frame · cracked · Dec 2, 2009 · N377FE · Doug MD1010F · Fuselage Main, Frame
  > MAIN CARGO, STA NR 1761, LT LONGERON NR 13 FRAME CRACKED. N1076 WAS GENERATED TO REPAIR ALL AFFECTED AREAS. THIS CRACKED FRAME SECTION AT THE ABOVE STA AND LONGERON WERE REMOVED WITH NEW SECTIONS AND SPLICES. THIS IS A CATEGORY "B" REPAIR AND REQUIRE A 12,00
- [SDR 08FDEA02166](https://openairdocs.org/sdr/08FDEA02166.md): None · none · Jun 5, 2008 · N377FE · Doug MD1010F · Standard Practices/Structures
  > REJECTED TAKEOFF AT IND AT 100 KTS OAT 31C WEIGHT 386,200. REJECTED FOR PREDICITIVE WINDSHEAR ALERT. NO OBSERVED OR REPORTED WINDSHEAR. PERFORMED BRAKE INSPECTION PER AMM 32-57-00-6. NO DEFECTS NOTED. ACN RELEASED FOR SERVICE PER MEL/CDL: 34-41-01-01-A CA
- [SDR 07FDEA05144](https://openairdocs.org/sdr/07FDEA05144.md): Bolt · sheared · Dec 27, 2007 · N377FE · Doug MD1010F · Nacelle/Pylon Miscellaneous Structure
  > NR 3 PYLON, TOMBSTONE LOWER SPHERICAL BEARING ATTACH BOLT SHEARED AT 6 O'CLOCK POSITION, DOT NR 1. REMOVED AND REPLACED 6 BOLTS, P/N 77711-9-105, PLATE -P/N AUB7125-1, RETAINER P/N AUB7126-501 AND PLI WASHERS REF AMM 54-00-01-4.
- [SDR 07FDEA02439](https://openairdocs.org/sdr/07FDEA02439.md): Mec · failed · Jul 10, 2007 · N377FE · Doug MD1010F · Fuel Controlling System
  > NR 1 ENGINE FLAMED OUT ON ROLLOUT. FIRST INDICATION WAS GEN 1 OFF FOLLOWED BY AIR SYS 1 LOW PRESS. REMOVED AND REPLACED FUEL PUMP AND MEC.
- [SDR 06FDEA2000](https://openairdocs.org/sdr/06FDEA2000.md): Spar · corroded · May 23, 2006 · N377FE · Doug MD1010F · Fuselage Main, Frame
  > LT WHEEL WELL STA 1370 JUST ABOVE REAR SPAR, HAS AREA OF CORROSION. REMOVED CORROSION AT EDGE MEMBER, OUT OF LIMITS IAW DC10 SRM 51-21-01-VOL II AND DC10 SRM 53-00-01 FIG 1A VOL I. REMOVED AND REPLACED EDGE MEMBER, ANGLE SECTION, GASKET, RUB STRIP AND INSTAL
- [SDR 06FDEA1912](https://openairdocs.org/sdr/06FDEA1912.md): Doubler · cracked · May 13, 2006 · N377FE · Doug MD1010F · Wing, Plate/Skin
  > LEFT OUTER WING TO CENTER WING LOWER SURFACE SPLICE DOUBLER HAS A CRACK STARTING AT FASTENER HOLE ON AFT END, XFS 145 AND FS 1370. REPAIRED IAW FEDEX EA 8-5710-96375- WINGS, CENTER WING BOX SPLICE PLATE CRACKED. FINGER REPAIR, MAJOR REPAIR.
- [SDR 06FDEA1787](https://openairdocs.org/sdr/06FDEA1787.md): Repair · unknown · May 11, 2006 · N377FE · Doug MD1010F · Standard Practices/Structures
  > REPAIR EVALUATION AGING AIRPLANE PROGRAM EXISTING REPAIR AT STA 304-328 LONGERON 26L-38L. OPS 1401/ T 8-5330-86848 COMPLIED WITH CARD T-8-5330-83848-FUSELAGE-REPAIR EVALUATION AGING AIRPLANE PROGRAM EXISTING REPAIR AT STA.304-328 LONGERON 26L-38L. MAJOR
- [SDR 04FDEA03454](https://openairdocs.org/sdr/04FDEA03454.md): Valve · malfunctioned · Dec 21, 2004 · N377FE · Doug MD1010F · Landing Gear Brake System
  > AFTER GEAR EXTENSION, RECEIVED LVL 2 LT ANTI SKID FAIL. EXECUTED GO-AROUND, FOLLOWED QRH PROCEDURES. ALERT MOMENTARILY EXTINGUISHED AFTER CYCLING ANTI SKID SWITCH, BUT RE-APPEARED ON NEXT GEAR EXTENSION. HISTORY OF SAME PROBLEM. T/S PER FIM 32-40-08 & M/M
- [SDR 04FDEA03386](https://openairdocs.org/sdr/04FDEA03386.md): Hinge Bracket · gouged · Dec 7, 2004 · N377FE · Doug MD1010F · Vertical Stabilizer
  > VERTICAL STABILIZER REAR SPAR, UPPER RUDDER HINGE FITTING BENT AND GOUGED. REMOVED AND REPLACED UPPER RUDDER HINGE SUPPORT BRACKET IAW MD10-10 MM 55-53-01-2 AND EA 8- 5530-83844, STABILIZER- VERTICAL STABILIZER RUDDER HINGE BRACKET, REPAIR. REFERENCE NON-RO
- [SDR 04FDEA03329](https://openairdocs.org/sdr/04FDEA03329.md): Skin · damaged · Dec 2, 2004 · N377FE · Doug MD1010F · Fuselage Main, Plate/Skin
  > AFT REPAIR AT STATION 966 TO 1001, LONGERON 37 RIGHT TO 42 RIGHT NEEDS EVALUATION TO DETERMINE IF REPAIR IS MAJOR OR MINOR AND IF REPAIR IS IN ACCORDANCE WITH FAA APPROVED DATA AND REPETITIVE INSPECTION REQUIREMENTS. REMOVED EXISTING DAMAGED PORTION OF SKIN
- [SDR 04FDEA03272](https://openairdocs.org/sdr/04FDEA03272.md): Skin · corroded · Nov 30, 2004 · N377FE · Doug MD1010F · Fuselage Main, Plate/Skin
  > REPAIR AT STATION 1957 TO 1993 LONGERON 49 LEFT TO 49 RIGHT NEED ENGINEERING EVALUATION TO DETERMINE IF REPAIR IS MAJOR OR MINOR AND IF REPAIR IS IN ACCORDANCE WITH FAA APPROVE DATA AND REPETITIVE INSPECTION REQUIREMENT. CUT AND REMOVE SKIN IAW EA8-5330-83838
- [SDR 04FDEA03270](https://openairdocs.org/sdr/04FDEA03270.md): Skin · damaged · Nov 30, 2004 · N377FE · Doug MD1010F · Fuselage Main, Plate/Skin
  > REPAIR AT STATION 304 TO 328 LONGERON 26 LEFT AND 38 LEFT NEEDS ENGINEERING EVALUATION TO DETERMINE IF REPAIRS IS MAJOR OR MINOR AND IF REPAIR IS IN ACCORDANCE WITH FAA APPROVED DATA AND REPETITIVE REQUIREMENTS. EVALUATED REPAIR IAW FEDEX EA 8-5330-83848, FUS
- [SDR 04FDEA03269](https://openairdocs.org/sdr/04FDEA03269.md): Skin · damaged · Nov 30, 2004 · N377FE · Doug MD1010F · Fuselage Main, Plate/Skin
  > REPAIR AT STATION 330 BETWEEN LONGERONS 37 RIGHT TO 38 RIGHT NEEDS ENGINEERING EVALUATION TO DETERMINE IF REPAIR IS MAJOR OR MINOR AND IF REPAIR IS IN ACCORDANCE WITH FAA APPROVED DATA AND REPETITIVE REQUIREMENTS. CUT OUT DAMAGED AREA OF SKIN, FABRICATED AND
- [SDR 04FDEA03268](https://openairdocs.org/sdr/04FDEA03268.md): Skin · damaged · Nov 30, 2004 · N377FE · Doug MD1010F · Fuselage Miscellaneous Structure
  > EXTERNAL DOUBLER ON LEFT HAND LOWER FUSELAGE SKIN STATION 470 TO 475 BETWEEN LONGERON 30 LEFT AND 31 LEFT APPEARS NOT TO BE PER THE SRM. REMOVED OLD REPAIR IAW DC10 SRM 51-33-01 VOL 2. FABRICATED AND INSTALLED NEW DOUBLERS IAW DC10 SRM 53-20-00 VOL 1, FIGURE
- [SDR 04FDEA03267](https://openairdocs.org/sdr/04FDEA03267.md): Skin · damaged · Nov 30, 2004 · N377FE · Doug MD1010F · Fuselage Main, Plate/Skin
  > REPAIR AT STATION 470-475 LONGERON 30 RIGHT TO 30 LEFT, NEEDS ENGINEERING EVALUATION TO DETERMINE IF REPAIR IS MAJOR OR MINOR AND IF REPAIR IS IN ACCORDANCE WITH FAA APPROVED DATA AND REPETITIVE INSPECTION REQUIREMENTS. REMOVED EXISTING REPAIR. REPLACED DOUB
- [SDR 04FDEA03266](https://openairdocs.org/sdr/04FDEA03266.md): Skin · damaged · Nov 30, 2004 · N377FE · Doug MD1010F · Fuselage Main, Plate/Skin
  > REPAIR AT STATION 1942 LONGERON 50 RIGHT TO 51 RIGHT NEEDS ENGINEERING EVALUATION TO DETERMINE IF REPAIR IS MINOR OR MAJOR AND IF REPAIR IS IN ACCORDANCE WITH FAA APPROVED DATA AND REPETITIVE INSPECTION REQUIREMENT. REMOVED OLD REPAIR IAW DC10 SRM 51-35-01 VO
- [SDR 04FDEA03265](https://openairdocs.org/sdr/04FDEA03265.md): Panel · delaminated · Nov 29, 2004 · N377FE · Doug MD1010F · Trailing Edge Flaps
  > RIGHT WING PANEL ARC0613-502, UPPER TRAILING EDGE PANEL AT INBOARD END OF OUTBOARD FLAP DELAMINATED. RIGHT WING PANEL ARC0613-502 REPAIRED BY FABRICATING AND BONDING NEW OUTER SKINS, DOUBLER AND CORE IAW TPS 1001 REV E, DAC DWG ARC0613 AND FEDEX EA 8-5710-815
- [SDR 04FDEA03264](https://openairdocs.org/sdr/04FDEA03264.md): Manifold · worn · Nov 29, 2004 · N377FE · Doug MD1010F · Engine Thrust Reverser
  > NR 1 ENGINE OUTBOARD THRUST REVERSER UPPER COOLING DUCT IS CHAFED IN SEVERAL AREAS. REMOVED COOLING DUCT IAW DC10 SRM 51-31-01 VOL 2. WELD REPAIRED COOLING MANIFOLD IAW FEDEX EA 8-7830-81526, EXHAUST SYSTEM NR 1 OUTBOARD THRUST REVERSER COOLING DUCT MANIFOLD
- [SDR 04FDEA03263](https://openairdocs.org/sdr/04FDEA03263.md): Roller · loose · Nov 29, 2004 · N377FE · Doug MD1010F · Trailing Edge Flaps
  > RIGHT WING LOWER FORWARD INBOARD FLAP LOAD ROLLER HAS EXCESSIVE LATERAL PLAY. REMOVED AND REPLACED RIGHT HAND INBOARD FLAP INBOARD TRACK LOWER ROLLER IAW FEDEX EA 8-5750- 81513, WING- INBOARD FLAP- INBOARD ROLLER TORQUE REQUIREMENT- CLARIFICATION.
- [SDR 04FDEA03262](https://openairdocs.org/sdr/04FDEA03262.md): Roller · worn · Nov 29, 2004 · N377FE · Doug MD1010F · Trailing Edge Flaps
  > RIGHT WING LOWER AFT LOAD ROLLER HAS WORN BEARING SURFACE, CHROME WORN ON INBOARD FLAP TRACK ATTACHMENT AREA. REMOVED AND REPLACED RIGHT HAND INBOARD FLAP INBOARD TRACK AFT LARGE LOAD ROLLER IAW FEDEX EA 8- 5750-81513.
- [SDR 04FDEA03261](https://openairdocs.org/sdr/04FDEA03261.md): Skin · damaged · Nov 29, 2004 · N377FE · Doug MD1010F · Fuselage Main, Plate/Skin
  > REPAIR AT STATION 1140 TO 1151 AT LONGERON 39 LEFT TO 41 LEFT NEEDS ENGINEERING EVALUATION TO DETERMINE MAJOR OR MINOR AND IF DATA AND REPETITIVE INSPECTION REQUIREMENTS. REMOVED PANEL 153AB AND REMOVED DOUBLER IAW DC10 SRM 51-31-01 VOL 2 AND 51-35-01 VOL 2.
- [SDR 04FDEA03260](https://openairdocs.org/sdr/04FDEA03260.md): Door · delaminated · Nov 29, 2004 · N377FE · Doug MD1010F · Fluid Service Doors
  > LEFT HAND WING REFUEL PANEL NEEDS REWORK DUE TO SHIFT OF INNER DOUBLER DURING AUTO-CLAVE CURE AND LACK OF TIMCO ROUTING SHEET BEING ASSIGNED. REPAIRED, REWORKED REFUEL PANEL PART NUMBER ARB1101-503 BY FABRICATING AND BONDING NEW OUTER SKIN AND INNER DOUBLER I
- [SDR 04FDEA03259](https://openairdocs.org/sdr/04FDEA03259.md): Door · delaminated · Nov 29, 2004 · N377FE · Doug MD1010F · Fluid Service Doors
  > LEFT WING REFUEL PANEL, DELAMINATED ON EDGES ADJACENT TO HINGE, AS MARKED. LOWER SKIN, CORE AND BLOCKS BONDED IAW TPS 1001 REV E, DAC DWG ARB1011 AND FEDEX EA 8- 5710-83944, AND DC10 SRM 51-70-00 VOL 2.
- [SDR 04FDEA03258](https://openairdocs.org/sdr/04FDEA03258.md): Pressure Blkhd · damaged · Nov 29, 2004 · N377FE · Doug MD1010F · Fuselage Main, Bulkhead
  > REPAIR UNDER RADAR ON PRESSURE BULKHEAD NEEDS ENGINEERING EVALUATION TO DETERMINE IF REPAIR IS MAJOR OR MINOR AND IF IS IN ACCORDANCE WITH FAA APPROVED DATA AND REPETITIVE INSPECTION REQUIREMENTS. PERFORMED FEDEX EA 8-5330-83949, FUSELAGE- REPAIR EVALUATION A
- [SDR 04FDEA03257](https://openairdocs.org/sdr/04FDEA03257.md): Panel · delaminated · Nov 29, 2004 · N377FE · Doug MD1010F · Wing, Plate/Skin
  > LEFT WING PANEL OVER AFT TRUNNION HAS MANY AREAS OF DELAMINATION. REPAIRED AFT TRUNNION PANEL ARC0269-503 BY FABRICATING AND BONDING NEW SKINS, DOUBLERS AND CORE IAW TPS 1001 REV E, DAC GWG ARC0269 AND FEDEX EA 8-5710-83945, WINGS- LEFT HAND MAIN LANDING GEA
- [SDR 04FDEA03256](https://openairdocs.org/sdr/04FDEA03256.md): Panel · dented · Nov 29, 2004 · N377FE · Doug MD1010F · Wing, Plate/Skin
  > LEFT HAND WING UPPER TRAILING EDGE PANEL JUST OUTBOARD OF MAIN LANDING GEAR UPPER SURFACE HAS SEVERAL DENTS. REPAIRED PANEL PART NUMBER ARC0263, BY FABRICATING AND BONDING NEW OUTER SKIN, INNER SKIN, DOUBLER AND CORE IAW RPS 1001 REV E, DAC PRINT ARC0263 AND
- [SDR 04FDEA03254](https://openairdocs.org/sdr/04FDEA03254.md): Hinge Bracket · corroded · Nov 29, 2004 · N377FE · Doug MD1010F · Trailing Edge Flaps
  > LEFT AND INBOARD FLAP OUTBOARD HINGE BOLT HOLE HAS AREA OF CORROSION. BOLT HOLE IS REPLACEMENT BOLT PART NUMBER 3D0031-8-90 STEP 23 OF FEDEX WIC E 8-5710-7-5005 PT1. REMOVED STOP FITTING IAW DAC DWG ARC0154, REMOVED OUTBOARD PANEL IAW MD10 SRM 51-31-01 VOL 2,
- [SDR 04FDEA03253](https://openairdocs.org/sdr/04FDEA03253.md): Panel · delaminated · Nov 29, 2004 · N377FE · Doug MD1010F · Wing Main, Frame Structure
  > RIGHT WING INBOARD FLAP AREA LEFT HAND FALSE SPAR CEILING PANEL INBOARD OF MAIN LANDING GEAR STRUT DELAMINATED/DENTED. REMOVED FILLET PANELS 152FT, 152ET AND SMALL PANEL OUTBOARD OF DAMAGED PANEL IAW DC10 SRM 51-31-01 VOL 2, TO FOM. REMOVED DELAMINATED PANEL

Next page: https://openairdocs.org/deregistered/N377FE-2024-03-02/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 = 'N377FE' AND deregistration_id = 'N377FE-2024-03-02'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N377FE-2024-03-02/reports

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