Douglas DC-8-61

Service difficulty reports · 942

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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 = 'DC861'
  ORDER BY difficulty_date DESC"

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SDR CKSA96355Skin · crackedDURING SEVERE TURBULENCE INSPECTION FOUND: RIGHT INBOARD AILERON TRAILING EDGE DENTED AND CRACKED. REPAIRED AILERON TRAILING EDGE IAW DC-8 SRM 57-2-0, DC-8 MIP-1 SECTION 15, NON-ROUTINE TASK CARD NR 81824.Dec 8, 1996 · N812CK · Doug DC861 · AileronsSDR CKSA96354Spar Cap · crackedDURING SEVERE TURBULENCE INSPECTION FOUND: FORWARD LOWER SPAR CAP CRACKED AT OUTBOARD SPLICE. REPAIRED LOWER SPAR CAP CRACK IAW AIA ENGINEERING SKETCH NR'S AIA/E/2335, AIA/E/2337, AIA/E/2340, DC-8 MIP-1 SECTION 15, NON-ROUTINE TASK CARD NR 82127.Dec 8, 1996 · N812CK · Doug DC861 · Wing SparSDR CKSA96353Spar Cap · crackedDURING SEVERE TURBULENCE INSPECTION FOUND: FORWARD UPPER SPAR CAP CRACKED AT OUTBOARD SPLICE. REPAIRED UPPER SPAR CAP CRACK IAW AIA ENGINEERING SKETCH NR'S AIA/E/2234, AIA/E/2341, AIA/E/2336, DC-8 MIP-1 SECTION 15, NON-ROUTINE TASK CARD NR 82126.Dec 8, 1996 · N812CK · Doug DC861 · Wing SparSDR CKSA96352Spar Cap · crackedDURING SEVERE TURBULENCE INSPECTION FOUND: RIGHT WING AFT SPAR LOWER CAP CRACKED AT STA 408 SPLICE. REPAIRED IAW DRAWING AIA/E/2285, AIA/E/2342, AIA/E/2343 AND DAC DRAWING NR 5613922. REFERENCE REPORT 96AA-156, DC-8 MIP-1 SECTION 15, NON-ROUTINE TASK CARD NDec 8, 1996 · N812CK · Doug DC861 · Wing SparSDR CKSA96351Door · damagedDURING SEVERE TURBULENCE INSPECTION FOUND: INBOARD AFT COWL DOOR NR 2 TRAILING EDGE DAMAGED APPROXIMATELY 24 INCHES LONG. PATCHED COWL DOOR TRAILING EDGE IAW DC-8 SRM 78-2-0, DC-8 MIP-1 SECTION 15, NON-ROUTINE TASK CARD NR 81974.Dec 8, 1996 · N812CK · Doug DC861 · Service DoorsSDR CKSA96350Door · damagedDURING SEVERE TURBULENCE INSPECTION FOUND: NR 2 ENGINE LEFT FORWARD COWL DOOR DENTED AND HAS SMALL HOLE. REPAIRED SMALL HOLE AND REMOVED DENT IAW DC-8 SRM 78-2-0, DC-8 MIP-1 SECTION 15, NON-ROUTINE TASK CARD NR 81785.Dec 8, 1996 · N812CK · Doug DC861 · Service DoorsSDR CKSA96349Door · damagedDURING SEVERE TURBULENCE INSPECTION FOUND: LEFT HAND INBOARD SLOT DOOR DAMAGED. REMOVED AND REPLACED LEFT HAND WING INBOARD SLOT DOOR IAW DMM 27-80-1 PAGE 201, DC-8 MIP-1 SECTION 15, NON-ROUTINE TASK CARD NR 81808.Dec 8, 1996 · N812CK · Doug DC861 · Leading Edge DevicesSDR CKSA96348Fairing · damagedDURING SEVERE TURBULENCE INSPECTION FOUND: FLAP FAIRING TRAILING EDGE PANEL STA 98 LOWER LEFT WING DAMAGED. REMOVED AND REPLACED FLAP FAIRING TRAILING EDGE PANEL STA 98 LOWER WING IAW SRM 51-1-21, DC-8 MIP-1 SECTION 15, NON-ROUTINE TASK CARD NR 82111.Dec 8, 1996 · N812CK · Doug DC861 · Trailing Edge FlapsSDR CKSA96347Panel · damagedDURING SEVERE TURBULENCE INSPECTION FOUND: LEFT WING LOWER TRAILING EDGE PANEL AT STA 106 HAS HOLE IN IT. REMOVED AND REPLACED LOWER TRAILING EDGE PANEL AT STA 106 IAW SRM 53-01-0, DC-8 MIP-1 SECTION 15, NON-ROUTINE TASK CARD NR 82156.Dec 8, 1996 · N812CK · Doug DC861 · Wing, Plate/SkinSDR CKSA96346Fitting · crackedDURING SEVERE TURBULENCE INSPECTION FOUND: LEFT WING TRAILING EDGE FITTING STA 98 CRACKED. REMOVED AND REPLACED LOWER WING TRAILING EDGE FITTING STA 98 IAW SRM 53-01-0, DC-8 MIP-1 SECTION 15, NON-ROUTINE TASK CARD NR 82112.Dec 8, 1996 · N812CK · Doug DC861 · Wing Miscellaneous StructureSDR CKSA96345Plating · damagedDURING SEVERE TURBULENCE INSPECTION FOUND: SKIN UNDER OUTBOARD SLOT PANEL DAMAGED APPROXIMATELY 1 HOLE. REMOVED AND REPLACED PLATING IAW DC-8 SRM 51-1-21, 51-1-20D, 51-3-0, 54-3-1 FIGURE 31A, DC-8 MIP-1 SECTION 15, NON-ROUTINE TASK CARD NR 82012.Dec 8, 1996 · N812CK · Doug DC861 · Leading Edge DevicesSDR CKSA96344Exhaust Gate · tornDURING SEVERE TURBULENCE INSPECTION FOUND: LEFT OUTBOARD FLAP EXHAUST GATE TORN UPPER AND LOWER SURFACE APPROXIMATELY 12 INCHES BOTH SIDES. REINSTALLED EXHAUST GATE IAW DC-8 MM 27-51-5, DC-8 MIP-1 SECTION 15, NON-ROUTINE TASK CARD NR 81818.Dec 8, 1996 · N812CK · Doug DC861 · Trailing Edge FlapsSDR CKSA96343Skin · damagedDURING SEVERE TURBULENCE INSPECTION FOUND: LEFT HAND OUTBOARD SLOT LEADING EDGE DAMAGED. REPAIRED PER SRM 57-2-1 FIGURE 2H, DC-8 MIP-1 SECTION 15, NON-ROUTINE TASK CARD NR 82125.Dec 8, 1996 · N812CK · Doug DC861 · Leading Edge DevicesSDR CKSA96342Angle · crackedDURING SEVERE TURBULENCE INSPECTION FOUND: NR 3 PYLON INBOARD STUB WING ATTACH ANGLE CRACKED. REPAIRED NR 3 PYLON STUB WING ANGLE IAW DC-8 SRM 54-2-1 FIGURE 19, DC-8 MIP-1 SECTION 15, NON-ROUTINE TASK CARD NR 84763.Dec 8, 1996 · N812CK · Doug DC861 · Nacelle/Pylon StructureSDR CKSA96341Skin · crackedDURING SEVERE TURBULENCE INSPECTION FOUND: WING LEADING EDGE LOWER SURFACE AT WING PYLON INTERSECTION CRACKED NR 1. REPAIRED WING LEADING EDGE SKIN CRACK IAW DC-8 SRM 54-2-1 FIGURE 21, DC-8 MIP-1 SECTION 15, NON-ROUTINE TASK CARD NR 82081.Dec 8, 1996 · N812CK · Doug DC861 · Wing, Plate/SkinSDR CKSA96340Web · damagedDURING SEVERE TURBULENCE INSPECTION FOUND: NR 1 PYLON INBOARD STUB WING UPPER WEB DAMAGED APPROXIMATELY 2 INCH HOLE. REMOVED AND REPLACED WEB PLATING IAW DC-8 SRM 51-1-21, 54-3-1 FIGURE 31A, DC-8 MIP-1 SECTION 15, NON-ROUTINE TASK CARD NR 82015.Dec 8, 1996 · N812CK · Doug DC861 · Nacelle/Pylon StructureSDR CKSA96339Skin · damagedDURING SEVERE TURBULENCE INSPECTION FOUND: NR 1 PYLON SKIN DAMAGED AT STA YOP.270 INBOARD SIDE, APPROXIMATELY 3 INCH LONG HOLE. REPAIRED DAMAGED SKIN NR 1 PYLON IAW DC-8 SRM 54-2-1, 51-1-20D, 51-1-21, DC-8 MIP-1 SECTION 15, NON-ROUTINE TASK CARD NR 82014.Dec 8, 1996 · N812CK · Doug DC861 · Nacelle/Pylon, Plate/SkinSDR CKSA96338Angle · crackedDURING SEVERE TURBULENCE INSPECTION FOUND: NR 1 PYLON INBOARD UPPER SPAR WEB CRACKED AT STA YOP.270 APPROXIMATELY 2 INCHES LONG. REPAIRED NR 1 PYLON UPPER SPAR WEB ANGLE IAW DC-8 SRM 51-1-20D, 51-1-21, 54-2-1 FIGURE 5, DC-8 MIP-1 SECTION 15, NON-ROUTINE TASDec 8, 1996 · N812CK · Doug DC861 · Nacelle/Pylon StructureSDR CKSA96337Angle · damagedDURING SEVERE TURBULENCE INSPECTION FOUND: NR 1 PYLON INBOARD SIDE AT STA YOP.270 HAS TEMPORARY REPAIR ANGLE INSTALLED. REMOVED AND REPLACED ANGLE IAW DC-8 SRM 51-1-20D, 51-3-0, 54-3-1 FIGURE 31A, DC-8 MIP-1 SECTION 15, NON-ROUTINE TASK CARD NR 82013.Dec 8, 1996 · N812CK · Doug DC861 · Nacelle/Pylon StructureSDR CKSA96336Skin · damagedDURING SEVERE TURBULENCE INSPECTION FOUND: LEFT WING UPPER SKIN DAMAGED AT STA 140 TO 150 JUST FORWARD OF CENTER SPAR DENTS AND HOLE APPROXIMATELY 2 INCHES DIAMETER. REPAIRED LEFT WING UPPER SKIN IAW DC-8 SRM 57-2-1 FIGURE 39, DC-8 MIP-1 SECTION 15, NON-ROUTDec 8, 1996 · N812CK · Doug DC861 · Wing, Plate/SkinSDR CKSA96335Apron · damagedDURING SEVERE TURBULENCE INSPECTION FOUND: NR 1 PYLON APRON FORWARD OUTBOARD SECTION DAMAGED APPROXIMATELY 24L BY 3W. REPAIRED APRON PER SRM 54-2-1, DC-8 MIP-1 SECTION 15, NON-ROUTINE TASK CARD NR 81975.Dec 8, 1996 · N812CK · Doug DC861 · Nacelle/Pylon StructureSDR CKSA96334Angle · damagedDURING SEVERE TURBULENCE INSPECTION FOUND: NR 2 PYLON INBOARD FORWARD SIDE OF STUB WING HAS TEMPORARY REPAIR ANGLE INSTALLED AT STA YIP.230. REMOVED TEMPORARY ANGLE AND REPLACED ANGLE IAW DC-8 SRM 51-1-20, 51-3-0, 54-3-1 FIGURE 26, DC-8 MIP-1 SECTION 15, NONDec 8, 1996 · N812CK · Doug DC861 · Nacelle/Pylon StructureSDR CKSA96333Rib · damagedDURING SEVERE TURBULENCE INSPECTION FOUND: LEFT HAND OUTBOARD FLAP 2ND RIB OUTBOARD OF EXHAUST GATE DAMAGED. REMOVED AND REPLACED RIB IAW DC-8 SRM 51-1-21, 57-2-5 AND 57-7-1, DC-8 MIP-1 SECTION 15, NON-ROUTINE TASK CARD NR 82005.Dec 8, 1996 · N812CK · Doug DC861 · Trailing Edge FlapsSDR CKSA96332Door · damagedDURING SEVERE TURBULENCE INSPECTION FOUND: LEFT HAND OUTBOARD SLOT DOOR DAMAGED. REMOVED AND REPLACED LEFT HAND OUTBOARD SLOT DOOR IAW DC-8 MM 27-41-2, DC-8 MIP-1 SECTION 15, NON-ROUTINE TASK CARD NR 81805.Dec 8, 1996 · N812CK · Doug DC861 · Leading Edge DevicesSDR CKSA96331Skin · damagedDURING SEVERE TURBULENCE INSPECTION FOUND: NR 2 PYLON DAMAGED INBOARD SIDE UPPER STATION YIP.230 APPROXIMATELY 1 HOLE. REPAIRED INBOARD PYLON INBOARD SIDE SKIN IAW DC-8 SRM 54-2-1 FIGURE 7, DC-8 MIP-1 SECTION 15, NON-ROUTINE TASK CARD NR 81996.Dec 8, 1996 · N812CK · Doug DC861 · Nacelle/Pylon, Plate/SkinSDR CKSA96330Door · missingDURING SEVERE TURBULENCE INSPECTION FOUND: LEFT HAND INBOARD SLOT DOOR LEADING EDGE MISSING. REPAIR DONE ON RO#230452 INSTALLED IAW DC-8 SRM 51-1-20D AND 51-3-0, DC-8 MIP-1 SECTION 15, NON-ROUTINE TASK CARD NR 81809.Dec 8, 1996 · N812CK · Doug DC861 · Leading Edge DevicesSDR CKSA96329Skin · crackedDURING SEVERE TURBULENCE INSPECTION FOUND: LEFT INBOARD AILERON LOWER SURFACE CRACKED APPROXIMATELY .5 INCH LONG. REPAIRED PER DC-8 SRM 57-2-0 AND 57-2-1. TREATED AND PRIMED PER 51-1-8, DC-8 MIP-1 SECTION 15, NON-ROUTINE TASK CARD NR 81816.Dec 8, 1996 · N812CK · Doug DC861 · AileronsSDR CKSA96328Skin · dentedDURING SEVERE TURBULENCE INSPECTION FOUND: DENT IN NR 2 PYLON INBOARD SIDE ABOVE ENGINE EXHAUST. REPAIRED DENT IAW DC-8 SRM 54-2-1 FIGURE 7, DC-8 MIP-1 SECTION 15, NON-ROUTINE TASK CARD NR 81793.Dec 8, 1996 · N812CK · Doug DC861 · Nacelle/Pylon, Plate/SkinSDR CKSA96327Skin · damagedDURING SEVERE TURBULENCE INSPECTION FOUND: HOLE IN NR 2 PYLON INBOARD SIDE ABOVE ENGINE EXHAUST. REPAIRED HOLE IAW DC-8 SRM 54-2-1 FIGURE 7, DC-8 MIP-1 SECTION 15, NON-ROUTINE TASK CARD NR 81792.Dec 8, 1996 · N812CK · Doug DC861 · Nacelle/Pylon, Plate/SkinSDR CKSA96326Door · crackedDURING SEVERE TURBULENCE INSPECTION FOUND: NR 1 ENGINE RIGHT UPPER NACELLE DOOR CRACKED AND DENTED. INSTALLED NEW DOOR PER MM 71-10-0, DC-8 MIP-1 SECTION 15, NON-ROUTINE TASK CARD NR 81784.Dec 8, 1996 · N812CK · Doug DC861 · Service DoorsSDR CKSA96325Door · damagedDURING SEVERE TURBULENCE INSPECTION FOUND: NR 1 ENGINE LEFT UPPER NACELLE DOOR DAMAGED. INSTALLED NEW DOOR PER MM 71-10-0, DC-8 MIP-1 SECTION 15, NON-ROUTINE TASK CARD NR 81780.Dec 8, 1996 · N812CK · Doug DC861 · Service DoorsSDR ABXA9600678Gear Indication · malfunctionedON FINAL WHEN GEAR HANDLE PUT IN DOWN POSITION, NO NOSE GEAR GREEN LIGHT, HAD GEAR UNSAFE LIGHT. RECYCLED GEAR, GOT NORMAL INDICATION. PERFORMED ADJUSTMENT TEST OF NOSE LANDING GEAR SYSTEM IAW DC-8 MM 32-31-0. OPERATIONAL CHECK OF INDICATION AND MECHANICAL Dec 5, 1996 · N853AX · Doug DC861 · Landing Gear Position and WarningSDR ABXA9600676Fire Loop · malfunctionedCREW REPORTED, THEY EXPERIENCED A BRIEF FIRE BELL AND MASTER FIRE WARNING LIGHT ON DESCENT. UNABLE TO VERIFY WHICH ENGINE, SUSPECT NR 2 ENGINE DUE TO PREVIOUS HISTORY. CHECKED ALL ENGINE FIRE SENSING ELEMENTS IAW DC-8 MM 26-10-1, ALL TESTED GOOD. REPLACED NNov 27, 1996 · N851AX · Doug DC861 · Fire DetectionSDR ABXA9600677Gear Indication · malfunctionedON FIRST GEAR EXTENSION ATTEMPT, NOSE GEAR GREEN LIGHT WOULD NOT COME ON. RECYCLED GEAR, HAD A GOOD INDICATION ON SECOND TRY. AIRCRAFT JACKED AND GEAR SWING COMPLIED WITH, NO DEFECTS NOTED IAW DC-8 MM 32-60-0.Nov 23, 1996 · N853AX · Doug DC861 · Landing Gear Position and WarningSDR ABXA9600672Fire Loop · defectiveINFLIGHT, MASTER FIRE WARNING AND BELL. NO LIGHTS IN LEVER ILLUMINATED. FIRE WARNING TESTED, NR 2 ENGINE WOULD NOT TEST, TRIED SEVERAL TIMES. SECURED ENGINE NR 2, FUEL DUMPED. CHECKED FIRE LOOPS AND WIRES TO NR 2 ENGINE DETECTOR AMP, NO PROBLEMS FOUND. RENov 22, 1996 · N851AX · Doug DC861 · Fire DetectionSDR ABXA9600665Retract Mech · out of adjustAFTER GEAR RETRACTION, GEAR UNSAFE LIGHT REMAINED ILLUMINATED, LANDING GEAR AND DOOR LATCHING INDICATOR INDICATED RIGHT MAIN GEAR DOOR UNLATCHED. AFTER CYCLING GEAR SEVERAL TIMES, GEAR UNSAFE LIGHT EXTINGUISHED AND NOT LATCHED LIGHT EXTINGUISHED. ADJUSTED RINov 12, 1996 · N848AX · Doug DC861 · Landing Gear Door Retract SectionSDR ABXA9700032Trapezoidal Ftg · crackedFOUND CRACK 1.46 INCHES IN LENGTH ON THE FORWARD END OF TRAPEZOIDAL FITTING, LEFT SIDE. REMOVED TRAPEZOIDAL FITTING, CLEANED AREA AND ANTI-CORROSION TREATED IAW SRM 51-1-8. INSTALLED NEW TRAPEZOIDAL FITTING.Nov 11, 1996 · N853AX · Doug DC861 · Fuselage Miscellaneous StructureSDR CKSA96193Fire Loop · groundedFIRE WARNING NR 3 ENGINE. THE LIGHT IN HANDLE WENT OUT APPROXIMATELY 45 SECONDS AFTER SHUTDOWN. FIRE BELL AND WARNING LIGHTS REACTIVATED INTERMITTENTLY FOR APPROXIMATELY 5 MINUTES, DID NOT FIRE BOTTLE. INSPECTED NR 3 ENGINE, FOUND NO EVIDENCE OF FIRE. INSPNov 2, 1996 · N24UA · Doug DC861 · Fire DetectionSDR CKSA96192Fire Loop · chafedFIRE WARNING NR 3 ENGINE. DISCHARGED ONE FIRE BOTTLE. RIGHT WING INBOARD FIRE BOTTLE REMOVED. INSPECTED NR 3 ENGINE AND FOUND NO EVIDENCE OF FIRE. FOUND FIRE LOOP CHAFING. ADJUSTED AND OPS CHECKED GOOD PER DC-8 MM 26-10-1. REPLACED FIRE BOTTLE PER DC-8 MMNov 1, 1996 · N24UA · Doug DC861 · Fire DetectionSDR 96ZZZX5829Tee Cap · crackedDURING INSPECTION OF AFT PRESSURE BULKHEAD AT STA Y=1766 IAW PSI 53.08.009/010C AND NDI 53-10-18, FOUND TWO CRACKS AT CORNER RADIUS OF THE TEE CAP AT LONGERON 10 RT AND LONGERON 10 LEFT. REPAIRED CRACKS BY INSTALLING A REPAIR ANGLE IAW SRM 53-2-5, PAGES 15 ANOct 30, 1996 · N30UA · Doug DC861 · Fuselage Main, BulkheadSDR 96ZZZM1539Bulkhead Tee · crackedDURING INSPECTION OF AFT PRESSURE BULKHEAD AT STATION Y=1766 IAW PSI 53.08.009/010C AND NDI 53-10-18, FOUND TWO CRACKS AT CORNER RADIUS OF THE TEE CAP AT LONGERON 10 RIGHT AND LONGERON 10 LEFT. REPAIRED CRACKS BY INSTALLING A REPAIR ANGLE IAW SRM 53-2-5 PAGE Oct 30, 1996 · N30UA · Doug DC861 · Fuselage Main, BulkheadSDR ABXA9700419Tab · delaminatedDURING OFF WING INSPECTION, FOUND TAB DELAMINATED. OVERHAULED AILERON CONTROL TAB IAW T.P.S. 1001, REV.E, AND DAC D.W.G. 5642831. PERFORMED WEIGHT AND BALANCE IAW DC-8 SRM 51-4-2.Oct 23, 1996 · N851AX · Doug DC861 · Aileron TabsSDR CKSA96163Fire Amplifier · malfunctionedNR 2 ENGINE SHUTDOWN AT 2345Z DUE TO FIRE WARNING. FIRE WARNING CAME ON THEN OFF, MONITORED ENGINE NORMAL. THEN GANG TESTED FIRE LOOP, TEST FAILED. AT THAT TIME FIRE HANDLE LIGHT CAME ON, SO NR 1 AND NR 2 FIRE BOTTLE DISCHARGED. LIGHT REMAINED ON AND NO TEOct 21, 1996 · N817CK · Doug DC861 · Fire DetectionSDR 96ZZZM1442Wire · looseCABIN ALTITUDE WARNING HORN 'ON' DURING CRUISE FLIGHT. CABIN ALTITUDE ABOVE 10,000 FEET AT FL 310 AND MANIFOLD AIR PRESSURE LIGHT 'ON'. ABNORMAL CHECKLIST COMPLETED, CONDITION CONTINUED. FOUND R263 WIRE LOOSE TO GND. TIGHTENED, CHECKED AT ENGINE RUN. PRESOct 18, 1996 · N27UA · Doug DC861 · Air Conditioning System WiringSDR 96ZZZM1494Bogie Cylinder · damagedA/C RETURNED TO MIAMI FOR RED GEAR LIGHT STAYS ON AFTER GEAR RETRACTION. FOUND LEFT BOGIE UNLOCK CYLINDER DAMAGED. REMOVED AND REPLACED BOGIE CONTROL VALVE IAW MM 32-53-1 AND ALSO REMOVED AND REPLACED LEFT BOGIE CYLINDER ACTUATOR IAW MM 32-53-2. OPS CHECK FOct 13, 1996 · N27UA · Doug DC861 · Landing Gear Retraction/Extension SystemSDR ABXA9600647Oil Pump · failedNR 3 ENGINE OIL PRESSURE CLIMBED TO 62 PSI, OIL TEMP WAS 100 DEGREES CELSIUS. OIL PRESSURE THEN BEGAN TO FLUCTUATE BETWEEN 55 TO 62 PSI. ENGINE SECURED AT 0430 Z, ENGINE WINDMILLED FOR 17 MINUTES. MINIMUM OIL PRESSURE DURING WINDMILLING WAS15 PSI. REPLACEDOct 11, 1996 · N849AX · Doug DC861 · Turbine Engine Oil SystemSDR ABXA9700031Link · crackedBOTH THE INBOARD AND OUTBOARD OVERCENTER LINKS CRACKED ON THE RIGHT WING NR 4 SPOILER. REPLACED NR 4 SPOILER OVERCENTER LINKS AND OPS CHECKED SPOILER IAW DC-8 MM 27-61.Oct 8, 1996 · N852AX · Doug DC861 · Drag Control SystemSDR ABXA9600632Engine · failedNR 2 OIL PRESSURE LIGHT ILLUMINATED, OIL PRESSURE FLUCTUATED BELOW 35 PSI TO 20 PSI. SECURED ENGINE AT 1243 Z, RPM NEVER FELL BELOW 24 PERCENT N-2 UNTIL TOUCHDOWN. HIGHEST WAS 35 PERCNET N-2, APPROXIMATELY 5 PSI OIL PRESSURE. REPLACED NR 2 ENGINE IAW ABX ENOct 2, 1996 · N845AX · Doug DC861 · Engine (Turbine/Turboprop)SDR ABXA9600631Door Seal · looseDURING ENGINE START, FORWARD CABIN DOOR OPEN LIGHT ILLUMINATED. COULD NOT OPEN DOOR FROM THE INSIDE. FOUND A STRIP OF METAL LOOSE ON THE LOWER FORWARD DOOR SEAL. RESECURED AS REQUIRED.Sep 24, 1996 · N847AX · Doug DC861 · Passenger/Crew DoorsSDR CKSA96138Connector · looseNR 2 ENGINE FIRE WARNING CAME ON FOR 1 TO 2 SECONDS ON DESCENT AND WENT OFF WITH NO ACTION TAKEN. REPAIRED WIRE CONNECTOR AT UPPER AFT FIRE LOOP SYSTEM, OPS CHECKS NORMAL IAW DC8 MM CHAPTER 26-10-0.Sep 19, 1996 · N817CK · Doug DC861 · Fire Detection
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