Douglas DC-10-30F

Service difficulty reports · 1,152

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  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE aircraft_model_key = 'DC1030F'
  ORDER BY difficulty_date DESC"

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SDR 2019F00027Slide Raft · defectiveAIRCRAFT DECLARED AN IFE FOR SMOKE IN THE COCKPIT. UPON LANDING CREW DEPLOYED THE LEFT FORWARD DOOR (DOOR 1L) SLIDE/RAFT BUT IT FAILED TO FULLY INFLATE. FLIGHT CREW WENT TO DEPLOY THE SLIDE/RAFT LOCATED IN THE NUMBER 1 RIGHT DOOR (DOOR 1R) THE SLIDE/RAFT FELMay 21, 2018 · Doug DC1030F · Escape SlideSDR FDEA201708222473Channel · chafedLWR RT NR 2 ENG FAN COWL & IDG SHOW DEEP CHAFED IN STRUCTURE. TAPE/RED MARK REPAIRED AJC7415-6 CHAFED SECTION REF 55-00-01 FIG 7 SH 1-4 PG 25-28 VOL I.Aug 22, 2017 · N307FE · Doug DC1030F · Vertical Stabilizer Miscellaneous StructureSDR CA151123011Circuit Breaker · faulty(CAN) IN FLIGHT, THE AIRCRAFT EXPERIENCED A LT EMERGENCY AC BUSS ELECTRICAL FAILURE. THE FLIGHT CREW ACCOMPLISHED THE APPROPRIATE CHECKLIST PROCEDURES AND DECLARED AN EMERGENCY, DIVERTED AND LANDED UNEVENTFULLY. THE MAINTENANCE INSPECTION FOUND A REMOTE CONTRONov 22, 2015 · Doug DC1030F · AC Power Distribution SystemSDR CA150303009Thrust Reverser · damaged(CAN) AFTER LANDING, THE FLIGHT CREW NOTICED THE NR 2 ENGINE THRUST REVERSER PRESSURE AND UNLOCK LIGHT REMAINED ILLUMINATED AFTER BEING SELECTED TO CLOSE. UPON INSPECTION, MAINTENANCE DETERMINED THE RT THRUST REVERSER ASSY WAS DAMAGED AND STUCK IN THE DEPLOYEFeb 17, 2015 · Doug DC1030F · Engine Thrust ReverserSDR CA150212009Dimmer · failed(CAN) IN FLIGHT, THE FLIGHT CREW NOTICED SMOKE EMITTING FROM THE COCKPIT OVERHEAD PANEL. THE ELECTRICAL SMOKE PROCEDURE CHECKLIST WAS CARRIED OUT AND THE SMOKE CEASED. THE CREW COMPLETED A FUEL DUMP BEFORE RETURNING TO BASE FOR AN UNEVENTFUL LANDING. MAINTENANFeb 11, 2015 · Doug DC1030F · Instrument PanelSDR CA141208005Switch · intermittent(CAN) AT TOP OF CLIMB, THE NR 2 ENGINE OIL STRAINER CLOGGED LIGHT ILLUMINATED. CREW COMPLETED THE INFLIGHT SHUT DOWN PROCEDURE. AFTER LANDING SAFELY, THE OIL STRAINER FILTER WAS REMOVED/INSPECTED AND WAS FOUND CLEAN AND WITHOUT ANY CONTAMINATION. OIL STRAINER Dec 5, 2014 · Doug DC1030F · Engine Oil Indicating SystemSDR CA140321017Line · split(CAN) THE NR 3 ENGINE WAS SHUTDOWN IN FLIGHT DUE TO LOW OIL PRESSURE CAUSED BY OIL DEPLETION. THE FLIGHT CONTINUED TO THE NEAREST SUITABLE AIRPORT WHERE MAINTENANCE DISCOVERED A RETURN OIL SCAVENGE LINE SPLIT AND LEAKING. FURTHER INVESTIGATION IDENTIFIED VIBRMar 17, 2014 · Doug DC1030F · Turbine Engine Oil SystemSDR CA131218026Control Handle · sticking(CAN) ON APPROACH, AFTER EXTENDING THE GEAR THE FLT DECK INDICATION FOR THE GEAR, GREEN, FAILED TO ILLUMINATE ON BOTH THE FRONT AND REAR PANELS, ONLY THE RED UNSAFE LIGHTS ILLUMINATED. THE CREW CYCLED THE GEAR WITH THE SAME RESULT, SO THEY COMPLETED A MISSEDDec 13, 2013 · Doug DC1030F · Landing Gear SelectorSDR CA130405007Wheel Half · cracked(CAN) 0.700" LONG CRACK FOUND ON OTBD WHEEL HALF DURING ROUTINE O/H PROCEDURES. METHOD USED TO DETECT CRACK WAS HFEC. CRACK ORIGINATES ON MATING SURFACE, BETWEEN SPOKE AND BOLT HOLE.Apr 3, 2013 · Doug DC1030F · Wheel/Ski/FloatSDR FDEA201211063883Skin · dentedLT OTBD FLAP BOTTOM SKIN HAS A CLUSTER OF SHARP DENTS JUST INBD OF VANE ROLLER ACCESS PANEL 557DB. INSPECTED DAMAGE AREA FOUND TO BE SERIES OF GOUGE SHARP CREASE DENTS TO INCLUDE ONE LOSE FASTENER - OUT OF LIMITS IAW SRM 57-10-00 PG 162A TO 48, HFEC DENT IAW Nov 6, 2012 · N318FE · Doug DC1030F · Wing, Plate/SkinSDR CA130702005Acm · failed(CAN) NR 1 ACM COOLING TURBINE WHEEL SHAFT FAILED DURING GROUND RUNS, TURBINE EXITED ACFT THROUGH EXHAUST DOOR. THE ACM WAS REPLACED AND THE ACFT RETURNED TO SERVICE.Mar 19, 2012 · Doug DC1030F · Cabin Cooling SystemSDR FDEA201103261187Switch · failedON INITIAL CLIMBOUT, RECEIVED ENG 2 OIL FILTER ALERT. USED MIN IDLE POWER AS ALERT WENT ON AND OFF SEVERAL TIMES FOR SEVEAL MINUTES EVENTUALLY REMAINED ON STEADY AT MIN IDLE. RED TABS FOR ALERT SHUTDOWN NR 2 ENGINE, RETURN TO DEPARTURE. NO OTHER ABNORMAL ENMar 26, 2011 · N320FE · Doug DC1030F · Engine Oil Indicating SystemSDR FDEA201007212632Door Frame · crackedMAIN CABIN CRACK ON WEB L3 DOOR LOWER JAMB AT STA 1251 REPAIRED IAW SRM 53-50-00 FIG 19, SH 1, VOL 1.Jul 21, 2010 · N320FE · Doug DC1030F · Fuselage Main, StructureSDR FDEA201006252146Skin · gougedEXISTING GOUGE IN FUSELAGE SKIN ADJACENT TO NOSE JACK POINT ALIGNMENT HOLE REPAIRED IAW EA 8-5330-123164.Jun 25, 2010 · N315FE · Doug DC1030F · Fuselage Main, Plate/SkinSDR CA100528012Bolt · corrodedDURING A RECENT SCHEDULED MX CHECK AND NR 2 ENGINE CHANGE PERSONNEL NOTICED EXCESSIVE PLAY AT THE TAIL PYLON THRUST LINK ASSY, PN AVB7320-501, LOWER ATTACHMENT. FURTHER INVESTIGATION IDENTIFIED THAT THE ATTACH BOLT, PN RA11005-12-2, WAS WORN AND CORRODED. NEMay 28, 2010 · Doug DC1030F · Engine Mount SectionSDR FDEA201005071481Sill · corrodedMODERATE CORROSION ON INTERIOR STRUCTURE OF LOWER AFT CARGO COMPT DOOR SILL. REPAIRED IAW EA 8-5310-123168 AND SRM 53-50-00 FIG.22, FIG.1, FIG.9, FIG.15A VOL.1.May 7, 2010 · N320FE · Doug DC1030F · Fuselage Miscellaneous StructureSDR 22AA201000070Proximity Switch · inoperativeAFTER TAKEOFF WITH GEAR HANDLE UP ALL (4) RED UNSAFE LIGHTS REMAINED ILLUMINATED. COMPLETED APPROPIATED CHECK LIST, NO CHANGE IN THE LIGHTS INDICATION. NOTIFIED ATC, FLIGHT CONTROL AND MX CONTROL. RETURNED TO DEPARTURE. IAW TAFI 32-30-00, R & R PROXIMITY ELECTMay 3, 2010 · N478CT · Doug DC1030F · Landing Gear Position and WarningSDR FDEA201004291395Skin · wornRT WING L/E DROOPED EXT FOUND DEEP WEAR ON SKIN. REPAIRED AREA IAW SRM 57-10-00, VOL I, FIG 39.Apr 29, 2010 · N315FE · Doug DC1030F · Wing, Plate/SkinSDR FDEA201004261362Relay · malfunctionedAFTER TAKEOFF, ENG ANTI-ICE ON, RECEIVED AIR SYS 2 LEVEL 1 ALERT. 45 SECS LATER RECEIVED MANF 2 FAIL LEVEL 3 ALERT. COMPLIED WITH QRH & DIVERTED. AFTER 4 MINS WITH NR 2 ENG AT IDLE, LEVEL 3 ALERT OUT. RELEASED FOR SERVICE IAW MEL: 36-23-01-02. ON MANF FAIL DApr 26, 2010 · N321FE · Doug DC1030F · Pneumatic Indicating SystemSDR FDEA201004211265Longeron · corrodedLT WING UPPER SIDE WING TO FUSELAGE FILLETS. AFTER REMOVING THE FILLETS 151 FT AND 151 ET WITH NRC NR N00866 THE FOLLOWING DEFECT HAVE BEEN FOUND EXFOLIATION CORROSION ON LONGERON. PERFORMED REPAIR IAW E.A. 8-5310-137606Apr 21, 2010 · N320FE · Doug DC1030F · Fuselage Main, Longeron/StringerSDR FDEA201004131170Panel · delaminatedRT WING UPPER SURFACE T/E. REMOVING WING PANEL ARC0340-504 WITH N00458. FOUND DELAMINATION ON AFT EDGE. (REMOVED PART). REPAIRED DELAMINATION IAW SRM 51-71-00 PAR.16 VOL.2Apr 13, 2010 · N320FE · Doug DC1030F · Wing, Plate/SkinSDR FDEA201003190931Skin · corrodedCTR CARGO COMPT BILGE, 2 EA U/S ANCHOR PLATE ON SKIN. DURING ANCHOR PLATE REPLACEMENT FOUND CORROSION ON SKIN. REPAIRED SKIN IAW SRM 53-20-00 FIG.13 SH.6 VOL.1.Mar 19, 2010 · N320FE · Doug DC1030F · Fuselage Main, Plate/SkinSDR FDEA201003090704Web · crackedCOCKPIT AREA FOUND CRACKS ON WEB. REPAIRED CRACK IAW SRM 53-00-01, FIG 4, SHT 2, VOL I.Mar 9, 2010 · N320FE · Doug DC1030F · Fuselage Miscellaneous StructureSDR FDEA201003040649Warning Light · illuminatedAT CRUISE ALTITUDE 350, RECEIVED LEVEL 3 ALERT "AIR MANF 2 FAIL" COMPLIED WITH QRH AND PROCEEDED TO NEAREST SUITABLE KOKC FOUND SYSTEM TEST GOOD PER AMM 36-23-01-4.AS PRECAUTIONARY PERFORMED DECAY CHECK ON ALL 3 MANIFOLDS PER AMM 36-00-01-5.ALL MANIFOLDSMar 4, 2010 · N314FE · Doug DC1030F · Central WarningSDR 22AA201000066Skin · crackedDURING "C" CHECK, LOWER FUSELAGE, ALONG LONGERON 44L, ALONG STA 1701 FUSELAGE SKIN FOUND CRACKED THROUGH. NON-ROUTINE NR 0425, CRACK AREA AT LONGERON 44L ALONG STATION 1701 FUSELAGE SKIN REPAIRED IAW SRM 53-20-00 FIGURE 6 VOLUME I REVISION 96.Feb 24, 2010 · N478CT · Doug DC1030F · Fuselage Main, Plate/SkinSDR 22AA201000065Roller Tray · corrodedDURING "C" CHECK, CTR CARGO COMPARTMENT LT OTBD CARGO ROLLER TRAY FOUND CORRODED AFTER CARGO SIDE GUIDE RAIL REMOVED TO FACILITATE FOR STRUCTURE REPAIR AT STA 1697 TO STA 1781. NON-ROUTINE NR 0450, CTR CARGO COMPARTMENT LT OTBD CARGO ROLLER TRAY REPAIR CARRIEFeb 24, 2010 · N478CT · Doug DC1030F · Fuselage Floor PanelSDR 22AA201000064Seat Track · corrodedDURING "C" CHECK, CABIN CORROSION FOUND ON INNER SURFACE OF SEAT TRACK AT STATION 1139 TO STATION 1156, X= 47.5. NON-ROUTINE NR 0314, SEAT TRACK FROM STATION 1129 TO STATION 1169, X= 47.5 CARRIED OUT REPAIR IAW SRM 53-70-00 FIGURE 1 VOLUME 1 REVISION 96.Feb 24, 2010 · N478CT · Doug DC1030F · Fuselage, Seat/Cargo Attach FittingsSDR 22AA201000063Intercostal · corrodedDURING "C" CHECK, CTR CARGO COMPARTMENT BILGE, INTERCOASTAL FOUND CORRODED AFTER SIDE GUIDE RAIL, REMOVED TO FACILITATE FOR STRUCTURE REPAIR AT STA 1764, L42 TO L43L (REFER CNTRL NR 0425). NON-ROUTINE NR 0449, CTR CARGO COMPARTMENT BILGE, INTERCOASTAL REPAIR Feb 24, 2010 · N478CT · Doug DC1030F · Fuselage Miscellaneous StructureSDR 22AA201000062Skin · corrodedDURING "C" CHECK, CABIN CORROSION FOUND ON CTR WING SECTION SURFACE AT STA 1156 TO STA 1221 X = 107.5 (RT). NON-ROUTINE 0220, CTR WING SECTION SURFACE AT STA 1156 TO STA 1221 X = 107.5 (RT) CORROSION REMOVED AND REPROTECTED IAW SRM 51-21-01 VOLUME II AT S 21 FFeb 24, 2010 · N478CT · Doug DC1030F · Wing, Center BoxSDR 22AA201000061Rib · crackedDURING "C" CHECK, NR 2 ENGINE RT CORE COWL AFT RIB LOWER SIDE FOUND WITH CRACK. NON-ROUTINE NR 0297, CRACK AREA AT NR 2 ENGINE RT CORE COWL AFT RIB LOWER SIDE AREA REPAIRED IAW EN 1017-10 WORK INSTRUCTIONS AND FAA APPROVED FORM 8110-3 DATED 12 MARCH 2010.Feb 24, 2010 · N478CT · Doug DC1030F · Nacelle/Pylon, Frame/Spar/RibSDR 22AA201000060Rib · crackedDURING "C" CHECK, NR 2 ENGINE LT CORE COWL AFT RIB LOWER SIDE FOUND WITH CRACK. NON-ROUTINE NR 0296, CRACK AREA AT NR 2 ENGINE LT CORE COWL AFT RIB LOWER SIDE AREA REPAIRED IAW EN 1017-10 WORK INSTRUCTIONS AND FAA APPROVED FORM 8110-3 DATED 12 MARCH 2010.Feb 24, 2010 · N478CT · Doug DC1030F · Nacelle/Pylon, Frame/Spar/RibSDR 22AA201000059Longeron · crackedDURING "C" CHECK, NR 2 ENG RT CORE COWL UPPER LONGERON FOUND WITH CRACK. NON-ROUTINE NR 0202, CRACKED UPPER LONGERON AT NR 2 ENGINE RT CORE COWL AREA REPAIRED IAW 1017-10 WORK INSTRUCTIONS AND FAA APPROVED FROM 8110-3 DATED 12 MARCH 2010.Feb 24, 2010 · N478CT · Doug DC1030F · Nacelle/Pylon, Longeron/StringerSDR 22AA201000057Skin · wornDURING "C" CHECK, NR 2 ENG LT CORE COWL UPPER AFT RUB STRIP FOUND WORN TO COWLING SKIN. NON-ROUTINE NR 0198, WORN COWLING SKIN AREA AT NR 2 ENG LT CORE COWL UPPER AFT RUB STRIP AREA REPAIRED IAW EN 1017-10 WORK INSTRUCTIONS AND FAA APPROVED FORM 8110-3 DATED Feb 24, 2010 · N478CT · Doug DC1030F · Nacelle/Pylon, Plate/SkinSDR 22AA201000056Longeron · crackedDURING "C" CHECK, NR 2 ENGINE LT CORE COWL UPPER LONGERON FOUND WITH CRACK. NON-ROUTINE NR 0197, CRACK AREA AT NR 2 ENGINE LT CORE COWL UPPER LONGERON AREA REPAIRED IAW EN 1017-10 WORK INSTRUCTIONS AND FAA APPROVED FORM 8110-3 DATED 12 MARCH 2010.Feb 24, 2010 · N478CT · Doug DC1030F · Nacelle/Pylon, Longeron/StringerSDR 22AA201000055Longeron · crackedDURING "C" CHECK, NR 2 ENGINE LT CORE COWL LOWER LONGERON FOUND WITH CRACK. NON-ROUTINE NR 0196, CRACK AREA AT NR 2 ENGINE LT CORE COWL LOWER LONGERON AREA REPAIRED IAW EN 1017-10 WORK INSTRUCTIONS AND FAA APPROVED FORM 8110-3 DATED 12 MARCH 2010.Feb 24, 2010 · N478CT · Doug DC1030F · Nacelle/Pylon, Longeron/StringerSDR 22AA201000054Rib · wornDURING "C" CHECK, NR 2 ENGINE LT CORE COWL AFT MOST RIB FOUND WITH WEAR MARK. NON-ROUTINE NR 0195, WORN AREA AT NR 2 ENGINE LT CORE COWL AFT MOST RIB AREA REPAIRED IAW EN 1017-10 WORK INSTRUCTIONS AND FAA APPROVED FORM 8110-3 DATED 12 MARCH 2010.Feb 24, 2010 · N478CT · Doug DC1030F · Nacelle/Pylon, Frame/Spar/RibSDR 22AA201000053Longeron · crackedDURING "C" CHECK, NR 3 ENGINE RT CORE COWL LOWER LONGERON CRACKED AT APPROX AT MID AND AFT FRAME SECTION. NON-ROUTINE NR 0163, CRACK AREA AT MID AND AFT SECTION OF LOWER LONGERON AT NR 3 ENGINE RT CORE COWL AREA REPAIRED IAW EN 1018-10 WORK INSTRUCTIONS AND FFeb 24, 2010 · N478CT · Doug DC1030F · Nacelle/Pylon, Longeron/StringerSDR 22AA201000052Longeron · crackedDURING "C" CHECK, NR 3 ENGINE LT CORE COWL LOWER LONGERON AFT SECTION FOUND CRACKED. NON-ROUTINE NR 0159, CRACK AREA AT NR 3 ENGINE LT CORE COWL LOWER LONGERON AFT SECTION REPAIRED IAW EN 1018-10 WORK INSTRUCTIONS AND FAA APPROVED FORM 8110-3 DATED 12 MARCH 2Feb 24, 2010 · N478CT · Doug DC1030F · Nacelle/Pylon, Longeron/StringerSDR 22AA201000051Longeron · crackedDURING "C" CHECK, NR 1 ENG, RT CORE COWL LOWER LONGERON AND STRAP FOUND CRACKED. NON-ROUTINE NR 0125, CRACKED STRAP AND LOWER LONGERON AT NR 1 ENGINE RT CORE COWL AREA REPAIRED IAW EN 1016-10 WORK INSTRUCTIONS AND FAA APPROVED FORM 8110-3 DATED 12 MARCH 2010.Feb 24, 2010 · N478CT · Doug DC1030F · Nacelle/Pylon, Longeron/StringerSDR 22AA201000050Longeron · crackedDURING "C" CHECK, NR 1 ENG LT CORE COWL LOWER LONGERON FOUND CRACKED. NON-ROUTINE NR 0124, CRACK AREA AT NR 1 ENGINE LT CORE COWL LOWER LONGERON AREA REPAIRED IAW EN 1016-10 WORK INSTRUCTIONS AND FAA APPROVED FORM 8110-3 DATED 12 MARCH 2010.Feb 24, 2010 · N478CT · Doug DC1030F · Nacelle/Pylon, Longeron/StringerSDR 22AA201000049Longeron · crackedDURING "C" CHECK, NR 1 ENGINE LT CORE COWL UPPER LONGERON FOUND CRACK. NON-ROUTINE NR 0123, CRACK AREA AT NR 1 ENG LT CORE COWL UPPER LONGERON AREA REPAIR IAW EN 1016-10 AND FAA APPROVED FORM 8110-3 DATED 12 MARCH 2010.Feb 24, 2010 · N478CT · Doug DC1030F · Nacelle/Pylon, Longeron/StringerSDR FDEA201002230494Clamp · looseBASED ON MX REPORT, DECIDED TO GIVE A LITTLE EXTRA TIME FOR ACCELERATION . IT WAS NECESSARY TO GO FULL QUADRANT TO GET CLOSE TO TAKEOFF POWER. WHEN THE AUTOFLIGHT TILE WAS PRESSED ENG 1 AND 2 REACHED TAKEOFF POWER, ENG NR 3 WAS LAGGING ABOUT 15 PERCENT BELOWFeb 23, 2010 · N314FE · Doug DC1030F · Compressor Bleed ControlSDR FDEA201002180447Skin · dentedRT HORIZONTAL STAB EXTERIOR SURFACE FOUND DEEP NICK ON SKIN. (REMOVED PART). REPAIRED EDGE FWD SKIN IAW SRM 55-10-00 FIG.13 VOL.1, REPAIRED LEADING REAR SKIN IAW SRM 55-00-01 FIG.3 SH.2 VOL.1Feb 18, 2010 · N320FE · Doug DC1030F · Horizontal Stabilizer, Plate/SkinSDR FDEA201002180448Skin · wornLT WING L/E DEEP WEARS & 4 EA FASTENERS U/S ON LOWER SKIN. REPAIRED AREA IAW EA 8-5710-137482 & SRM 57-10-00 FIG 83, VOL I.Feb 18, 2010 · N315FE · Doug DC1030F · Wing, Plate/SkinSDR FDEA201002150426Skin · crackedLT WING INBD FLAP UPPER SURFACE FOUND CRACK ON SKIN. REPAIRED SKIN IAW SRM 57-10-00, FIG 85, SHT 2 & 4 VOL I.Feb 15, 2010 · N315FE · Doug DC1030F · Trailing Edge FlapsSDR 22AA201000048Frame · corrodedDURING "C" CHECK , AFT CARGO COMPARTMENT BILGE AREA FRAME (STA 1996) LOWER CHORD CORRODED AT LBL 15 TO RBL 15 AS MARKED. NON-ROUTINE NR 0610, AFT CARGO COMPARTMENT BILGE AREA FRAME (STA 1996) LOWER CHORD, LBL 15 TO RBL 15 CORROSION, REMOVED AND REPROTECTED IAWFeb 13, 2010 · N524MD · Doug DC1030F · Fuselage Main, FrameSDR 22AA201000047Longeron · crackedDURING "C" CHECK, NR 2 ENG RT CORE COWL LOWER LONGERON AND STRAP FOUND CRACKED. NON-ROUTINE NR 394, CRACKED LONGERON AND STRAP AT NR 2 ENG RT CORE COWL LOWER LONGERON AREA REPAIRED IAW EN 1006-10 WORK INSTRUCTIONS AND FORM 8110-3 DATED 26 FEB 2010.Feb 13, 2010 · N524MD · Doug DC1030F · Nacelle/Pylon, Longeron/StringerSDR 22AA201000046Longeron · crackedDURING "C" CHECK, NR 2 ENG RT CORE COWL UPPER LONGERON FOUND WITH CRACK AT 02 LOCATIONS. NON-ROUTINE NR 392, CRACKED LONGERON 02 EACH LOCATIONS AT NR 2 ENGINE RT CORE COWL UPPER AREA REPAIRED IAW EN 1006-10 WORK INSTRUCTIONS AND FORM 8110-3 DATED 26 FEB 2010.Feb 13, 2010 · N524MD · Doug DC1030F · Nacelle/Pylon, Longeron/StringerSDR 22AA201000045Longeron · crackedDURING "C" CHECK, NR 1 ENGINE LT CORE COWL UPPER LONGERON FOUND WITH CRACK. NON-ROUTINE NR 324, CRACKED NR 1 ENG LT CORE COWL UPPER LONGERON AREA REPAIRED IAW EN 1006-10 WORK INSTRUCTIONS AND FORM 8110-3 DATED 26 FEB 2010.Feb 13, 2010 · N524MD · Doug DC1030F · Nacelle/Pylon, Longeron/StringerSDR 22AA201000044Longeron · crackedDURING "C" CHECK, NR 3 ENGINE LT CORE COWL UPPER LONGERON FOUND WITH CRACK. NON-ROUTINE NR 323, CRACKED LONGERON AT NR 3 ENG LT CORE COWL UPPER AREA REPAIRED IAW EN 1006-10 WORK INSTRUCTIONS AND FORM 8110-3 DATED 26 FEB 2010.Feb 13, 2010 · N524MD · Doug DC1030F · Nacelle/Pylon, Longeron/Stringer
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