N377FE, cancelled Mar 2, 2024

Service difficulty reports · 95

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Query with SQL
duckdb -csv -c "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"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR FDEA201502200555Limit Switch · failedR1 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 RFeb 20, 2015 · N377FE · Doug MD1010F · Emergency EquipmentSDR FDEA201412114106Lamp · inoperativeL1 DOOR SLIDE LIGHT WILL NOT TEST. REMOVED & RE LAMPED L1 DOOR SLIDE PRESS INDICATION LIGHT ASSEMBLY & REINSTALLED. OPERATIONS CHECK IS GOOD.Dec 11, 2014 · N377FE · Doug MD1010F · Escape SlideSDR FDEA201408042330Skin · crackedRIGHT 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.Aug 4, 2014 · N377FE · Doug MD1010F · Wing, Plate/SkinSDR FDEA201408042329Skin · crackedEVIDENCE 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.Aug 4, 2014 · N377FE · Doug MD1010F · Wing, Plate/SkinSDR FDEA201405131044Skin · crackedPOST 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.May 13, 2014 · N377FE · Doug MD1010F · Wing, Plate/SkinSDR FDEA201401050022Slide · faultyL1 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.Jan 5, 2014 · N377FE · Doug MD1010F · Escape SlideSDR FDEA201311242864Sensor · faultyON 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 RUNNov 24, 2013 · N377FE · Doug MD1010F · Pneumatic Indicating SystemSDR FDEA201310152510Spar · corrodedNR 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.Oct 15, 2013 · N377FE · Doug MD1010F · Nacelle/Pylon, Frame/Spar/RibSDR FDEA201310152512Channel · crackedNR 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.Oct 15, 2013 · N377FE · Doug MD1010F · Nacelle/Pylon Miscellaneous StructureSDR FDEA201309252314Bulkhead · crackedNLG 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.Sep 25, 2013 · N377FE · Doug MD1010F · Fuselage Main, BulkheadSDR FDEA201303050497Proximity Sensor · misinstalledAFTER 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 THROUGMar 5, 2013 · N377FE · Doug MD1010F · Landing Gear Position and WarningSDR FDEA201302260462Wire · burnedWIRE 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.Feb 26, 2013 · N377FE · Doug MD1010F · Landing Gear System WiringSDR FDEA201302070293Control Unit · failedANTI-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 IAFeb 7, 2013 · N377FE · Doug MD1010F · Brake Anti-Skid SectionSDR FDEA201210053570Anti-Skid Sys · malfunctionedLEFT 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 Oct 5, 2012 · N377FE · Doug MD1010F · Brake Anti-Skid SectionSDR FDEA201209183349Tee Fitting · crackedLEFT 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. SSep 18, 2012 · N377FE · Doug MD1010F · Fuselage Main, StructureSDR FDEA201204041253Sensor · failedRIGHT 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-Apr 4, 2012 · N377FE · Doug MD1010F · Landing Gear Position and WarningSDR FDEA201108253479Power Supply · failedWHILE 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.Aug 25, 2011 · N377FE · Doug MD1010F · Emergency LightingSDR FDEA201102100521Bulb · wrong partL1 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.Feb 10, 2011 · N377FE · Doug MD1010F · Escape SlideSDR FDEA201012264753Pressure Switch · inoperativeON 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 NRDec 26, 2010 · N377FE · Doug MD1010F · Engine Anti-Icing SystemSDR FDEA200912024335Frame · crackedMAIN 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 CYCDec 2, 2009 · N377FE · Doug MD1010F · Fuselage Main, FrameSDR FDEA200912024334Frame · crackedMAIN 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 Dec 2, 2009 · N377FE · Doug MD1010F · Fuselage Main, FrameSDR FDEA200912024333Frame · crackedMAIN 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 12,00Dec 2, 2009 · N377FE · Doug MD1010F · Fuselage Main, FrameSDR FDEA200912024332Frame · crackedMAIN 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 12,00Dec 2, 2009 · N377FE · Doug MD1010F · Fuselage Main, FrameSDR 08FDEA02166None · noneREJECTED 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 CAJun 5, 2008 · N377FE · Doug MD1010F · Standard Practices/StructuresSDR 07FDEA05144Bolt · shearedNR 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.Dec 27, 2007 · N377FE · Doug MD1010F · Nacelle/Pylon Miscellaneous StructureSDR 07FDEA02439Mec · failedNR 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.Jul 10, 2007 · N377FE · Doug MD1010F · Fuel Controlling SystemSDR 06FDEA2000Spar · corrodedLT 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 INSTALMay 23, 2006 · N377FE · Doug MD1010F · Fuselage Main, FrameSDR 06FDEA1912Doubler · crackedLEFT 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.May 13, 2006 · N377FE · Doug MD1010F · Wing, Plate/SkinSDR 06FDEA1787Repair · unknownREPAIR 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 May 11, 2006 · N377FE · Doug MD1010F · Standard Practices/StructuresSDR 04FDEA03454Valve · malfunctionedAFTER 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 Dec 21, 2004 · N377FE · Doug MD1010F · Landing Gear Brake SystemSDR 04FDEA03386Hinge Bracket · gougedVERTICAL 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-RODec 7, 2004 · N377FE · Doug MD1010F · Vertical StabilizerSDR 04FDEA03329Skin · damagedAFT 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 SKINDec 2, 2004 · N377FE · Doug MD1010F · Fuselage Main, Plate/SkinSDR 04FDEA03272Skin · corrodedREPAIR 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 EA8-5330-83838Nov 30, 2004 · N377FE · Doug MD1010F · Fuselage Main, Plate/SkinSDR 04FDEA03270Skin · damagedREPAIR 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, FUSNov 30, 2004 · N377FE · Doug MD1010F · Fuselage Main, Plate/SkinSDR 04FDEA03269Skin · damagedREPAIR 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 Nov 30, 2004 · N377FE · Doug MD1010F · Fuselage Main, Plate/SkinSDR 04FDEA03268Skin · damagedEXTERNAL 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, FIGURENov 30, 2004 · N377FE · Doug MD1010F · Fuselage Miscellaneous StructureSDR 04FDEA03267Skin · damagedREPAIR 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 DOUBNov 30, 2004 · N377FE · Doug MD1010F · Fuselage Main, Plate/SkinSDR 04FDEA03266Skin · damagedREPAIR 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 VONov 30, 2004 · N377FE · Doug MD1010F · Fuselage Main, Plate/SkinSDR 04FDEA03265Panel · delaminatedRIGHT 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 8-5710-815Nov 29, 2004 · N377FE · Doug MD1010F · Trailing Edge FlapsSDR 04FDEA03264Manifold · wornNR 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 MANIFOLDNov 29, 2004 · N377FE · Doug MD1010F · Engine Thrust ReverserSDR 04FDEA03263Roller · looseRIGHT 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.Nov 29, 2004 · N377FE · Doug MD1010F · Trailing Edge FlapsSDR 04FDEA03262Roller · wornRIGHT 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.Nov 29, 2004 · N377FE · Doug MD1010F · Trailing Edge FlapsSDR 04FDEA03261Skin · damagedREPAIR 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. Nov 29, 2004 · N377FE · Doug MD1010F · Fuselage Main, Plate/SkinSDR 04FDEA03260Door · delaminatedLEFT 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 INov 29, 2004 · N377FE · Doug MD1010F · Fluid Service DoorsSDR 04FDEA03259Door · delaminatedLEFT 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.Nov 29, 2004 · N377FE · Doug MD1010F · Fluid Service DoorsSDR 04FDEA03258Pressure Blkhd · damagedREPAIR 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 ANov 29, 2004 · N377FE · Doug MD1010F · Fuselage Main, BulkheadSDR 04FDEA03257Panel · delaminatedLEFT 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 GEANov 29, 2004 · N377FE · Doug MD1010F · Wing, Plate/SkinSDR 04FDEA03256Panel · dentedLEFT 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 Nov 29, 2004 · N377FE · Doug MD1010F · Wing, Plate/SkinSDR 04FDEA03254Hinge Bracket · corrodedLEFT 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,Nov 29, 2004 · N377FE · Doug MD1010F · Trailing Edge FlapsSDR 04FDEA03253Panel · delaminatedRIGHT 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 PANELNov 29, 2004 · N377FE · Doug MD1010F · Wing Main, Frame Structure
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