Douglas DC-8-73

Service difficulty reports · 821

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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 aircraft_model_key = 'DC873'
  ORDER BY difficulty_date DESC"

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SDR DHL2007803502Frame · crackedRT WING OUTBD L/E INNER SECTION LWR FORMER CRACKED 0.500" AT STA 622.250. REMOVED FASTENERS IAW SRM 51-1-21. FABRICATED TWO ANGLES DOUBLERS (AL7075T6 0.032") IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED AREA AND ANGLES IAW SRM 51-1-8B. INSTALLED ANGMay 23, 2007 · N803DH · Doug DC873 · Wing SparSDR DHL2007806521Skin · misrepairedREPAIR ON FWD UPPER JAMB CORNER OF "D" CARGO DOOR IS NOT IN ACCORDANCE WITH DWG SR08530019 (STA 1400.000 - 1420.000 L-25R TO L-27R) MAJOR REPAIR. PERFORMED MAJOR REPAIR IAW AD2005-18-07 S/B DC8 53-078, DOUGLAS DWG NR SR08530019, 5750776. REMOVED EXISTING NONApr 2, 2007 · N802DH · Doug DC873 · Cargo/Baggage DoorsSDR ASTAR20070017Generator · failedNR 4 GEN HAD TO BE RESET AFTER ENG START BEFORE IT CAME ON LINE. WITHIN 2 MIN OF PARALLELING GENS, AND PULLING OUT OF THE BLOCKS, NR 4 GEN UNPARALLELED LIGHT ILLUM. ABNORMAL PROC WAS COMPLETED, RESTORING NR 4 GEN TO THE PARALLELED STATUS. WITHIN 2 MIN OF REMar 24, 2007 · N805DH · Doug DC873 · AC Generation SystemSDR ASTAR200700015Lead · damagedON APPROACH TO IAH, NR 1 "GEN UNPARALLELED" LIGHT ILLUMINATED 20-30 SECONDS LATER THERE WAS A BURNING ODOR , THEN CLEARED. TRANSFERRED TO DMI LOG ITEM NR 28522 IAW DC8 MEL 24-1 CAT "C" SP PROC. C/W; NR 1 GEN DISCONNECTED. PLACARDS INSTALLED, SOURCE OF ODOR Mar 23, 2007 · N805DH · Doug DC873 · Electrical Power System WiringSDR DHL2007802539Bulkhead · corrodedFWD ACCY COMPT FWD PRESSURE BULKHEAD CAP SHOWS CORROSION AT STA 8.000 L-29R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 01-30-07, DWG NR ACG2-53-110 REV IR DATED 01-26-07. REMOVED FASTENERS IAW SRM 51-1-21, SRM 51-1-20D. CUT OUT DAMAGEDFeb 13, 2007 · N802DH · Doug DC873 · Fuselage Main, BulkheadSDR DHL2007802536Access Door · delaminatedRT WING T/E UPPER ACCESS DOOR NR 510 DELAMINATED (XA 475.000 - 507.000). REMOVED AND REPLACED DELAMINATED ACCESS DOOR NR 510 RT WING T/E IAW SRM 51-3-0, SRM 51-3-1 (TORQUE).Feb 11, 2007 · N802DH · Doug DC873 · Wing, Plate/SkinSDR DHL2007802537Rib · crackedNR 1 LT STUB WING UPPER INTERNAL RIB CRACKED STA XS 530.168 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW EA NR 06783 IAW DOUGLAS DWG NR 9753297. REMOVED CRACKED RIB IAW SRM 51-1-21, SRM 51-1-20D. INSTALLED NEW RIB IAW DOUGLAS DWG NR 9753297, SRM 51-1-21, SRM Feb 8, 2007 · N802DH · Doug DC873 · Wing, Rib/BulkheadSDR DHL2007802535Longeron · corrodedAFT ACCY COMPT L-30L CORRODED, STA 1746.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-2-2 FIG 4A. REMOVED CORROSION IAW SRM 51-1-18 PG 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG 2P. REMOVED FASTENERS IAW SRM 51-1-20D. CUT OUT DAMAGED SECTION AND Feb 8, 2007 · N802DH · Doug DC873 · Fuselage Main, Longeron/StringerSDR DHL2007802531Door Frame · cracked"B" CARGO DOOR AFT LWR JAMB CORNER 0.750" CRACK STA 560.000 L-31R TO L-32R. PERFORMED MAJOR REPAIR IAW AD2005-18-07 S/B 53-078 REV 1 JAN 25-01, FAA FORM 8100-9 DATED 02-05-07, BOEING MSG 1-274569547-4 DATED 02-05-07. REMOVED EXISTING REPAIR DOUBLER IAW SRM 5Feb 8, 2007 · N802DH · Doug DC873 · Fuselage Main, StructureSDR DHL2007802538Longeron · corrodedAFT ACCY COMPT SHOWS CORROSION AT STA 1660.000 L-24L (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-2-2 FIG 4A. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG 2P. REMOVED FASTENERS IAW SRM 51-1-20D. CUT OUT DAMAGED SECFeb 6, 2007 · N802DH · Doug DC873 · Fuselage Main, Longeron/StringerSDR DHL2007802530Panel · delaminatedLT WING T/E LWR PANEL DELAMINATED (STA XW 97.000 - XRS 162.000). REMOVED AND REPLACED LT WING T/E LWR PANEL IAW SRM 51-3-0, SRM 51-3-1 (TORQUE).Feb 6, 2007 · N802DH · Doug DC873 · Wing, Plate/SkinSDR DHL2007802532Fillet · delaminatedFOUND FUSELAGE LWR FILLET PANEL NR 732 DELAMINATED (STA 990.000 - 1050.000). REMOVED AND REPLACED LWR FILLET PANEL NR 732 IAW SRM 51-3-0, SRM 51-3-1 (TORQUE).Feb 5, 2007 · N802DH · Doug DC873 · Aerodynamic FairingsSDR DHL2007802529Skin · crackedRT NR 3 ENGINE NACELLE INLET COWL SHOWS CRACK 0.500" ON SKIN STA YN 138.000 AT 3 O'CLOCK POS (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 01-30-07, DWG NR AC62-54-105 REV IR DATED 01-19-07. REMOVED FASTENERS IAW SRM 51-1-21, SRM 51-1-20D.Feb 3, 2007 · N802DH · Doug DC873 · Nacelle/Pylon, Plate/SkinSDR DHL2007802528Vane · misrepairedRT OTBD SLOT VANE HAS A NON STANDARD REPAIR STA XOLDI 6.224 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 01-30-07, DWG NR AC62-57-106 REV IR DATED 01-22-07. REMOVED EXISTING NON STANDARD REPAIR IAW SRM 51-1-21, SRM 51-3-0. CUT OUT DAMAGEFeb 3, 2007 · N802DH · Doug DC873 · Trailing Edge FlapsSDR DHL2007802527Splice · crackedLT WING CTR L/E INTERNAL SPLICE DOUBLER STA XFS 341.500 CRACKED 1" (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 01-31-07, DWG NR AC62-57-109 REV IR DATED 01-23-07. REMOVED FASTENERS IAW SRM 51-1-20D. CUT OUT DAMAGED INTERNAL DOUBLER SEGMFeb 3, 2007 · N802DH · Doug DC873 · Wing Main, Frame StructureSDR DHL2007802521Vane · misrepairedLT OTBD SLOT VANE HAS A NON STANDARD REPAIR, STA XS 512.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 01-31-07, DWG AC62-57-108 REV IR DATED 01-23-07. REMOVED EXISTING NON STANDARD REPAIR IAW SRM 51-1-21, SRM 51-3-0. CUT OUT DAMAGED SFeb 3, 2007 · N802DH · Doug DC873 · Trailing Edge FlapsSDR DHL2007802520Vane · misrepairedLT OTBD VANE SLOT HAS A NON STANDARD REPAIR, STA XOLDI 6.224 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 01-31-07, DWG NR AC62-57-107 REV JR DATED 01-23-07. REMOVED EXISTING NON STANDARD REPAIR IAW SRM 51-1-21, SRM 51-1-20D. CUT OUT DAMFeb 3, 2007 · N802DH · Doug DC873 · Wing Main, Frame StructureSDR DHL2007802526Vane · misrepairedRT OTBD SLOT VANE HAS A NON STANDARD REPAIR, STA XS 512.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 01-31-07, DWG NR AC62-57-104 REV A DATED 01-31-07. REMOVED NON STANDARD REPAIR IAW SRM 51-1-21, SRM 51-3-0, SRM 51-1-20D. CUT OUT DAFeb 2, 2007 · N802DH · Doug DC873 · Trailing Edge FlapsSDR DHL2007802522Skin · crackedL1 DOOR CUT OUT WITH 0.600" CRACK APPROX AT STA 25.000 L-15L TO L-16L (FUS SKIN) MAJOR REPAIR. CORR.: PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 01-31-07, DWG# AC62-53-101 REV. IR DATED 01-15-07. REMOVED EXISTING INTERIM REPAIR IAW SRM 51-1-21, SRM 51-3-Feb 2, 2007 · N802DH · Doug DC873 · Passenger/Crew DoorsSDR DHL2007802534Hinge Fitting · crackedLT NR 4 AILERON HINGE FITTING IS CRACKED. REMOVED AND REPLACED NR 4 LT AIL HINGE SUPPORT FITTING IAW MM 20-16-0 PG 201-207. REFER TO NR 069055 FOR LT INBD AIL REMOVAL/REINSTALLATION AND NR 071624 FOR OPS CK.Feb 2, 2007 · N802DH · Doug DC873 · AileronsSDR DHL2007802533Floorbeam · crackedAFT ACCY COMPT FLOORBEAM SHOWS CRACK 5" AT STA 1700.000 BL 0 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 01-30-07, DWG NR AC62-53-102, REV IR DATE 01-15-07. REMOVED FASTENERS IAW SRM 51-1-21, SRM 51-3-0. CUT OUT DAMAGED SECTION IAW DWG Feb 2, 2007 · N802DH · Doug DC873 · Fuselage Main, Floor BeamSDR DHL2007802525Skin · delaminatedNR 2 LT SPOILER PANEL DELAMINATED. REMOVED AND REPLACED NR 2 LT SPOILER PANEL IAW MM 27-61-1 PG 201-206. REFER TO NR 071624 FOR OPS CHECK.Jan 30, 2007 · N802DH · Doug DC873 · SpoilersSDR DHL2007802524Skin · delaminatedNR 5 LT SPOILER PANEL DELAMINATED. REMOVED AND REPLACED NR 5 LT SPOILER PANEL IAW MM 27-61-1 PG 201-206. REFER TO NR 071624 FOR OPS CHECK.Jan 30, 2007 · N802DH · Doug DC873 · SpoilersSDR DHL2007802516Frame · brokenFOUND LT WING CTR L/E UPPER INTERNAL FORMER BROKEN 1" STA XS 521.000. REMOVED FASTENERS IAW SRM 51-1-21. FABRICATED DOUBLER (AL7075"0" 0.063") IAW SRM 57-3-3 FIG 4. HEAT TREATED FROM 7075"0" TO 7075T6 IAW SRM 51-1-1 PG 1-13-17. CLEANED, TREATED AND PRIMED AJan 30, 2007 · N802DH · Doug DC873 · Wing, Rib/BulkheadSDR DHL2007802519Rib · crackedLT INBD FLAP RIB HAS FOUR CRACKS OF 1" AND 1.500" STA XW 125.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-7-1 FIG 2 PG 6 (SHEET 4). REMOVED CRACKED RIV IAW SRM 57-1-0 PG.1, SRM 51-1-21, SRM 51-1-20D. FABRICATED RIB (AL2024"0" 0.050") IAW SRM 57-7-1Jan 29, 2007 · N802DH · Doug DC873 · Leading Edge DevicesSDR DHL2007802517Frame · crackedFOUND LT OTBD FLAP FORMER 1.500" CRACKED STA XF 165.000. REMOVED CRACKED FORMER IAW SRM 51-1-21. FABRICATED NEW FORMER (AL7075"0" 0.050") IAW SRM 57-2-0 PG 1. HEAT TREATED FORMER FROM 7075"0" TO 7075T6 IAW SRM 51-1-1 PG 13-17. CLEANED, TREATED AND PRIMED FJan 28, 2007 · N802DH · Doug DC873 · Trailing Edge FlapsSDR DHL2007802518Door · crackedR2 DOOR AFT UPPER CORNER CRACKED 1.250" LENGTH. PERFORMED MAJOR REPAIR IAW AD200-20-08 S/B DC8 53-075, DOUGLAS DWG SR08530021 AND 5750776. REMOVED FASTENERS IAW SRM 51-1-21. CUT OUT DAMAGED SECTION IAW DOUGLAS DWG SR08530021. PERFORMED NDT INSPECTION IAW NJan 26, 2007 · N802DH · Doug DC873 · Passenger/Crew DoorsSDR DHL2007802514Skin · misrepairedNR 4 RT STUB WING LWR SURFACE HAS A NON STANDARD REPAIR AT STA XFS 562.500. PERFORMED MAJOR REPAIR IAW SRM 57-2-1A FIG 1 PG 3. REMOVED NON STANDARD REPAIR IAW SRM 51-1-21, SRM 51-1-20D. FABRICATED EXT REPAIR DOUBLER (AL7075T6 0.080") AND INTERNAL DOUBLER (AJan 26, 2007 · N802DH · Doug DC873 · Wing, Plate/SkinSDR DHL2007802511Splice · crackedRT WING CTR LE UPPER INTERNAL SPLICE 2" CRACK STA XOLD 6.2246. REMOVED CRACKED SPLICE IAW SRM 51-1-21, SRM 51-3-0, SRM 51-1-20D. FABRICATED SPLICE (AL7075T6 0.080") IAW BOEING MSG NR 1-275396206-21 DATED JAN 23,2007. CLEANED, TREATED AND PRIMED AREA AND SPLJan 25, 2007 · N802DH · Doug DC873 · Wing Miscellaneous StructureSDR DHL2007802504Seat Track · wornMAIN CARGO COMPT NR 4 TRACK LUG WORN (STA 1670.000 - 1705.000). CUT OUT NR 4 TRACK DAMAGED SEGMENT AND FABRICATED (3EA) SPLICES (AL7075T6 0.100"/0.125"/0.160") IAW SRM 53-2-3 PG 49-50. CLEANED, TREATED AND PRIMED AREA AND SPLICES IAW SRM 51-1-8B. INSTALLED Jan 25, 2007 · N802DH · Doug DC873 · Fuselage, Seat/Cargo Attach FittingsSDR DHL2007802513Angle · crackedLT OTBD FLAP "T" ANGLE CRACKED 1" STA XF 165.000. REMOVED CRACKED T ANGLE IAW SRM 51-1-21. FABRICATED NEW T-ANGLE (EXTRUSION P/N 1243286) IAW SRM 57-7-0 FIG 3, SRM 51-2-0 FIG 50. CLEANED, TREATED AND PRIMED AREA AND T-ANGLE IAW SRM 51-1-8B. INSTALLED T-ANGJan 24, 2007 · N802DH · Doug DC873 · Trailing Edge FlapsSDR DHL2007802512Angle · crackedRT OUTBD FLAP SHOWS "T" ANGLE WITH CRACK 1" AT STA XT 165.000. REMOVED CRACKED T-ANGLE IAW SRM 51-1-21. FABRICATED NEW T-ANGLE (EXTRUSION P/N 1213286) IAW SRM 57-7-0 FIG 3, SRM 51-2-0 FIG 50. CLEANED, TREATED AND PRIMED AREA AND T-ANGLE IAW SRM 51-1-8B. INJan 24, 2007 · N802DH · Doug DC873 · Trailing Edge FlapsSDR DHL2007802509Skin · crackedRT WING UPPER SKIN 0.750" CRACKED STA XRS 74.000 S-14R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-2-1 FIG 10 SHEET 1. REMOVED FASTENERS IAW SRM 51-1-20D. CUT OUT DAMAGED SECTION IAW SRM 57-2-1 FIG 10 SHEET 1. PERFORMED NDT INSP IAW DC8 NDT SPM PART Jan 24, 2007 · N802DH · Doug DC873 · Wing, Plate/SkinSDR DHL2007802508Rib · crackedRT INBD FLAP RIB 1" CRACK STA XW 125.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG 1. REMOVED CRACKED RIB IAW SRM 51-1-21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW RIB IAW SRM 57-7-1 FIG 2 SHEET 4, SRM 51-1-21, SRM 51-Jan 24, 2007 · N802DH · Doug DC873 · Trailing Edge FlapsSDR DHL2007802510Skin · crackedLT WING UPPER SKIN CRACKED 1" S-9 AT STA XRS 74.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR ON LT WING UPPER SKIN STA XRS 74.000 S-9 IAW SRM 57-2-1 FIG 17 PG 87-88. REMOVED FASTENERS IAW SRM 51-1-20D. CUT OUT DAMAGED SECTION IAW SRM 57-2-1 FIG 17 PG 87-88. Jan 20, 2007 · N802DH · Doug DC873 · Wing, Plate/SkinSDR DHL2007802507Door Frame · unknownPERFORM REPAIR/MODIFICATION OF FWD PAX DOOR UPPER AFT JAMB CORNER IAW AD2000-20-08, DWG SR08530021 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW AD2000-20-08, S/B DC8 53-075, DOUGLAS DWG SR08530021, 5750776. REMOVED FASTENERS IAW SRM 51-1-21, SRM 51-1-20D. PERJan 20, 2007 · N802DH · Doug DC873 · Fuselage Main, StructureSDR DHL2007802506Door Frame · unknownPERFORM REPAIR/MODIFICATION OF FWD PAX DOOR LWR FWD JAMB CORNER IAW AD2000-20-08, DWG SR08530021 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW AD2000-20-08, S/B DC8 53-075, DOUGLAS DWG NR SR08530021, 5750776. REMOVED FASTENERS IAW SRM 51-1-21, SRM 51-1-20D. PEJan 20, 2007 · N802DH · Doug DC873 · Fuselage Main, StructureSDR DHL2007802515Angle · crackedFOUND LT INBD FLAP T/E ANGLE 1.500" CRACK STA XW 129.000. REMOVED CRACKED REINFORCING ANGLE IAW SRM 51-1-21. FABRICATED NEW REINFORCING ANGLE (AL2024"0" 0.050") IAW SRM 57-7-1 FIG 2 SHEET 1. HEAT TREATED FROM "0" TO AL2024T4 IAW SRM 51-1-1 PG 1-13-17. CLEAJan 18, 2007 · N802DH · Doug DC873 · Trailing Edge FlapsSDR DHL2007802505Angle · crackedAFT CARGO COMPT CRACKED ANGLE AT STA 1420.000 BL 0". REMOVED CRACKED ANGLE IAW SRM 51-1-21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW ANGLE IAW SRM 51-1-21.Jan 18, 2007 · N802DH · Doug DC873 · Fuselage Miscellaneous StructureSDR DHL2007802503Frame · crackedRT WING CTR L/E FORMER 0.500" CRACK STA XFS 291.500. REMOVED FASTENERS IAW SRM 51-1-21. PERFORMED STOP HOLE AND FABRICATED (2) ANGLE DOUBLER (AL7075T6 0.032") IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED AREA AND ANGLE DOUBLER IAW SRM 51-1-8B. INSTAJan 18, 2007 · N802DH · Doug DC873 · Leading Edge DevicesSDR DHL2007802502Floor Support · wornMAIN CARGO COMPT NR 5 TRACK LUGS WORN (STA 132.000 - 175.000). REMOVED DAMAGED TRACK SEGMENT AND SPLICES IAW SRM 51-3-0. CLEANED, TREATED AND PRIMED AREA AND SPLICES IAW SRM 51-1-8B. INSTALLED NEW TRACK SEGMENT AND REINSTALLED SPLICES IAW SRM 53-2-3 PG 49-5Jan 13, 2007 · N802DH · Doug DC873 · Fuselage Miscellaneous StructureSDR DHL2007802501Seat Track · wornMAIN CARGO COMPT NR 7 TRACK LUG WORN STA 786.000. CUT OUT NR 7 TRACK DAMAGED SECTION IAW SRM 53-2-3 PG 17 FIG 6D. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW TRACK PLUG AND CHANNEL IAW SRM 53-2-3 PG 17 FIG 6D, SRM 51-3-0, SRM 51-3-1.Jan 11, 2007 · N802DH · Doug DC873 · Fuselage, Seat/Cargo Attach FittingsSDR DHL2007802500Seat Track · wornMAIN CARGO COMPT NR 1 TRACK PLUG LUG WORN STA 340.000. REMOVED WORN TRACK PLUG IAW SRM 51-3-0. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW TRACK PLUG IAW SRM 51-3-0, SRM 51-3-1 PG 3.Jan 11, 2007 · N802DH · Doug DC873 · Fuselage, Seat/Cargo Attach FittingsSDR DHL2007802523Heat Exchanger · crackedRT PRIMARY HEAT EXCHANGER FWD LWR CORNER REPAIR DOUBLER 0.250" CRACKED, STA -32.000 L-27R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 01-30-07, DWG NR AC62-53-103 REV IR DATED 01-17-07. REMOVED FASTENERS IAW SRM 51-1-21. CUT OUT DAMAGEDJan 2, 2007 · N802DH · Doug DC873 · Air Conditioning SystemSDR DHL2006803002Filter · contaminatedAT 1000FT AGL, NR 3 OIL QUANTITY DROPPED FROM 12 QUARTS TO 2 QUARTS OIL PRESSURE NORMAL NR 3 ENGINE SHUTDOWN AFTER LANDING OIL QUANTITY RETURNED TO 12 QUARTS, ENGINE SHUTDOWN BY FLIGHT CREW. INSPECTED LUB AND SCAVENGE CHIP DETECTORS, NO DEBRIS FOUND. REMOVNov 1, 2006 · N803DH · Doug DC873 · Turbine Engine Oil SystemSDR DHL2006802002Strut · underservicedDURING INITIAL T/O ROLL, UNABLE TO MAINTAIN DIRECTIONAL CONTROL WITH FULL RUDDER PLUS TILLER INPUT. ALL ENG'S INDICATED EQUAL N1. CLOCKS RECORDED 7 SEC OF FLT. TIME INDICATING NOSE STRUT EXTENSION. ATIS WIND REPORTED AT 050 7 KTS RUNWAY 04L WAS USED. SEROct 5, 2006 · N802DH · Doug DC873 · Main Landing Gear Strut/Axle/TruckSDR DHL2006803001Odor · detectedSTRONG SMELL OFF SOMETHING HOT OR OVER HEATING IN A/C STRONGER IN LAV IT GOES AWAY WITH LT PACK OFF. OPERATED LT AND RT PACKS FULL COLD TO FULL HOT IAW MM 21-20-0 BOTH PACK OPERATE NORMAL NO DEFECTS NOTEDSep 7, 2006 · N803DH · Doug DC873 · Air Distribution SystemSDR DHL2006802001Stator Vane · out of adjustENCOUNTERED MAJOR UPDRAFT AT FL 410 ENGNE NR 3 FLAMED OUT PERFORMED INFLIGHT ENGINE START ABNORMAL PROCEDURE NORMAL SYSTEM OPERATION NR 3 RESTARTED. C/W ROUGH AIR INSPECTION PER DC-8 M/M 05-51-0. A/C FOUND SERV. NO DEFECTS. PERFORMED FAULT CODE 50 PER DC-Mar 21, 2006 · N802DH · Doug DC873 · Turbine Engine Air Inlet SectionSDR DHL2005803554Fitting · crackedITEM REF. NR. 039052: AFT CARGO COMPT. FITTING CRACKED 1.500 INCH STA 1080.000 L-21R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PAGE 1. REMOVED CRACKED FITTING IAW SRM 51-3-0 AND SRM 51-1-20D. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTADec 16, 2005 · N803DH · Doug DC873 · Fuselage Main, Attach FittingsSDR DHL2005803556Skin · crackedPERFORM PREVENTATIVE MODIFICATION IAW SB 57-88 REV. 3 ON LT WING LOWER SKIN CRACK AT STA 69.5 REF. SB AND DRAWING JO 60095-506. PERFORMED PREVENTATIVE MODIFICATION IAW AD80-22-01, SB 57-88 REV. 3 DWG NR JO60095-506. REMOVED FASTENERS AND SKI FITTING IAW DWG JODec 16, 2005 · N803DH · Doug DC873 · Wing, Plate/Skin
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