Douglas DC-8-63F

Service difficulty reports · 1,883

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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 = 'DC863F'
  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 ABXA050311Finger Doubler · corrodedCORROSION FOUND ON FINGER DOUBLER AT STA 1540, LONGERON 31 RIGHT, RIGHT BUTT LINE 25. REPAIRS ACCOMPLISHED AT STA 1540 - 1560, LONGERON 31 RIGHT IAW REA D853-52525.Oct 24, 2005 · N826AX · Doug DC863F · Fuselage Main, Plate/SkinSDR ABXA050297Keelbeam · corrodedSTA. 680 KEELBEAM INSIDE HEAVY CORROSION ON KEELBEAM TO PRESSURE WEB FOUND DURING ACCOMPLISHMENT OF NR HY-055. REMOVED CORROSION AT KEELBEAM STA. 680, BEHIND BULKHEAD AS REQUIRED REF. SRM 51-1-8 AND REA D853-52595-MR FOR REPAIR PROCEDURE TO REINFORCE KEELBEAMOct 24, 2005 · N826AX · Doug DC863F · Fuselage Main, KeelSDR ABXA050298Finger Doubler · corrodedAFT LOWER CARGO HAD CORRODED FINGER DOUBLER ON INTERIOR SKIN LOCATED AT STA 1480, LEFT BUTT LINE 32, STRINGER 31 LEFT. REPAIRED FINGER DOUBLERS AT STA 1480 AND 1500, LONGERON 31 LEFT IAW REA D853-52524.Oct 24, 2005 · N826AX · Doug DC863F · Fuselage Main, Plate/SkinSDR ABXA060027Keelbeam · corrodedBS 700 - 740, LEFT BUTT LINE 10, LEFT SIDE OF KEELBEAM, CORROSION ON THE LOWER CENTER WING SPLICE DOUBLER. CLEANED CORROSION, TREATED, AND PRIMED IAW DC8 SRM 51-1-8, 53-2-0, LWR NR 200302015. FABRICATED AND INSTALLED REPAIR DOUBLER IAW REA D853-52564.Oct 23, 2005 · N826AX · Doug DC863F · Fuselage Main, KeelSDR ARWA20051004Compressor · stalledLOG PAGE NR 117333, DURING TAKEOFF, NR 2 ENGINE COMPRESSOR STALLED. PERFORM NR 2 ENGINE INLET AND EXHAUST SECTION INSPECTION FOR DAMAGE IAW M/M 71-00 AND PERFORMED OPERATIONAL RUN IAW M/M 71-00; FOUND ALL PARAMETERS IN LIMITS, COULD NOT DUPLICATE FAILURE. NOTOct 22, 2005 · N661AV · Doug DC863F · Turbine Engine Compressor SectionSDR ABXA060034Floorbeam · crackedMAIN CABIN, STA 900, RIGHT BUTT LINE 54, FLOORBEAM CRACKED ON AFT SIDE UPPER CAP, FROM OUTBOARD END OF BEAM TOWARD INBOARD THROUGH TWO FASTENER HOLES. REPAIRED AREA IAW REA D853-52925 BY TRIMMING OUT CRACKED AREA AND INSTALLING A FILLER.Oct 20, 2005 · N826AX · Doug DC863F · Fuselage Main, Floor BeamSDR ABXA060026Floorbeam · corrodedMAIN CABIN, BS 120, RIGHT BUTT LINE 50, FLOORBEAM HAD EXCESSIVE MATERIAL LOSS. REMOVED DAMAGED AREA AND REPLACED WITH ANGLE DOUBLER AND FILLER ON FLOORBEAM BS 120, RIGHT BUTT LINE 50 IAW DC8 SRM 51-1-8, 53-2-0, 51-3-0, 53-7-3, 53-0, 51-2-0, 51-1-8, 51-3-1, 51Oct 20, 2005 · N826AX · Doug DC863F · Fuselage Main, Floor BeamSDR ABXA050366Floorbeam · corrodedFOUND MAIN CABIN, STA 70, RIGHT BUTT LINE 43-51, LOWER SIDE OF FLOORBEAM CORRODED OUT OF LIMITS. FOUND LOWER SIDE OF FLOORBEAM CORRODED OUT OF LIMITS AT STA 70, RIGHT BUTT LINE 43-51. FABRICATED FILLER AND DOUBLER AND INSTALLED. ALL WORK IAW DC8 SRM 51-1-8,Oct 20, 2005 · N826AX · Doug DC863F · Fuselage Main, Floor BeamSDR ABXA050352Floorbeam · corrodedFOUND MAIN CABIN, STA 920, RIGHT BUTT LINE 31, FLOORBEAM CORRODED AT NUTPLATES. REMOVED CORROSION STA 920, RIGHT BUTT LINE 31. MATERIAL LOSS OUT OF LIMITES. FABRICATED REPAIR ANGLES AND INSTALLED IAW DWG K04881 OUT OF 7075 "0", PO NR 1108502 0.063", HEAT TROct 20, 2005 · N826AX · Doug DC863F · Fuselage Main, Floor BeamSDR ABXA050351Floorbeam · corrodedFOUND MAIN CABIN, STA 680, RIGHT BUTT LINE 26, LOWER SIDE OF FLOORBEAM CORRODED. REMOVED CORROSION IAW DC8 SRM 51-1-8, ORIGINAL MATERIAL THICKNESS 0.178", REMAINING THICKNESS 0.107" AND OUT OF LIMITS IAW DC8 SRM 53-2-0. VERIFIED REPAIR AINGLE AS AND10134-1407Oct 20, 2005 · N826AX · Doug DC863F · Fuselage Main, Floor BeamSDR ABXA050296Skin · corrodedFUSELAGE SKIN, STA 1100 TO 1120 AT RT AFT BODY FAIRING, SKIN CORRODED. REMOVED CORROSION AND INSTALLED REPAIRS BETWEEN STA 1100 LONGERON 29 RT TO STA 1120 LONGERON 30 RT IAW REA D853-52518-MR AND SRM 51-1-8, PG 20.Oct 20, 2005 · N826AX · Doug DC863F · Fuselage Main, Plate/SkinSDR ARWA20051005Brake Assy · damagedLOG PAGE NR 117327. NR 2 MAIN WHEEL TIRE BLOWN; NR 2 BRAKE DAMAGED. REMOVED AND REPLACED NR 2 MAIN WHEEL IAW M/M 32-40-1; REMOVED AND REPLACED NR 2 BRAKE ASSEMBLY IAW MM 32-42-1, NO LEAKS NOTICE.Oct 20, 2005 · N661AV · Doug DC863F · BrakeSDR ABXA050365Longeron · corrodedFORWARD CARGO BAY, CORROSION IN LONGERON 36, STA 598 OUT OF LIMITS. REPAIRED LONGERON 36 IAW DC8 SRM 53-2-2 AND SPLICE WITH NEW SECTION FROM EXTRUSION P/N: S2645716 IAW DC8 SRM 53-2-2-, PG 6.Oct 19, 2005 · N826AX · Doug DC863F · Fuselage Main, Longeron/StringerSDR ABXA050339Stiffener · corrodedLOWER AFT CARGO FORWARD BULKHEAD LEFT SIDE FRAME CORRODED AT BOTTOM STA 980, 30 LEFT. REMOVED OLD STIFFENER IAW DC8 SRM 51-3-1 AND 51-1-21 WHICH HAD CORROSION OUT OF LIMITS IAW DC8 SRM 53-2-0 AND REPLACED WITH NEW STIFFENER PO NR 1122166 IAW DC8 SRM 51-1-21 AOct 19, 2005 · N826AX · Doug DC863F · Fuselage Miscellaneous StructureSDR ABXA050338Air Duct · dentedNR 4 ENGINE L/S TRANSITION AIR DUCT HAD SEVERAL DENTS. 2 DENTS AT 9 AND 11 O'CLOCK POSITIONS OUT OF LIMITS IAW DC8 SRM 51-1-9A. CLEANED UP AREA OF DENTS AT 9 AND 11 O'CLOCK POSITIONS AND REPAIRED IAW DC8 SRM 51-1-9A. 2 MORE DENTS AT 11 O'CLOCK POSITION ARE WIOct 19, 2005 · N826AX · Doug DC863F · Engine (Turbine/Turboprop)SDR ABXA050337Case · wornNR 2 ENGINE EXHAUST NOZZLE 6 O'CLOCK POSITION, CASE WORN. REMOVED DAMAGED EXISTING DOUBLERS IAW DC8 SRM 51-1-21. FABRICATED NEW DOUBLERS IAW SSRM DWG NR 78-841 FROM 0.051 301 1/2HD PO NR 1121624, PRIMED CONTACT SURFACE IAW DC8 51-1-8. INSTALLED NEW DOUBLER Oct 17, 2005 · N826AX · Doug DC863F · Fuel Injector NozzleSDR ABXA050336Pressure Panel · corrodedDOUBLER CORRODED TOP OF RIGHT WHEEL WELL PRESSURE DECK IN MAIN CARGO, STA 980, RIGHT BUTT LINE 30. REMOVED, FABRICATED, AND INSTALLED DOUBLER AT TOP OF RIGHT WHEEL WELL PRESSURE DECK IN MAIN CARGO STA 980 RIGHT BUTT LINE 30 IAW DC8 SRM 51-1-21, 51-1-14, 51-9-Oct 17, 2005 · N826AX · Doug DC863F · Fuselage Main, BulkheadSDR ABXA050316Doubler · corrodedCORRODED DOUBLER IN MAIN CARGO BELOW FLOOR LEVEL AGAINST ABOVE LEFT WHEEL WELL PRESS DECK, STA 940, LEFT BUTT LINE 67. REMOVED, FABRICATED AND REPLACED DOUBLERS IN MAIN CARGO BELOW FLOOR LEVEL AGAINST ABOVE LEFT PRESS DECK STA 940, LEFT BUTT LINE 67 IAW DC8 SOct 17, 2005 · N826AX · Doug DC863F · Fuselage Main, Plate/SkinSDR ABXA050315Cowling · scoredNR 1 ENGINE, OUTBOARD FORWARD COWL HOLD OPEN ROD HAD SCORED INNER SIDE OF COWL. REMOVED PREVIOUS REPAIR, FABRICATED NEW DOUBLER, AND APPLIED COMPOSITIE REPAIR IAW DC8 SRM 51-1-9A, TREATED DOUBLER IAW LWR 200302015 AND PRIMED IAW DC8 SRM 51-1-8.Oct 17, 2005 · N826AX · Doug DC863F · Engine Cowling SystemSDR ABXA050314Attach Angle · crackedFORWARD CARGO BAY DENT ON GILLINER ATTACH ANGLE, STA. 160, BETWEEN LONGERON 36 LEFT TO 35 LEFT. REMOVED DENT IN FORWARD CARGO BAY GILLINER ATTACH ANGLE STA 160, LONGERON 36 LEFT - 35 LEFT, FOUND TO BE CRACKED, REPAIRED. REMOVED GILLINER ATTACH ANGLE IAW DC8 Oct 16, 2005 · N826AX · Doug DC863F · Fuselage Main, Attach FittingsSDR ABXA050312Frame · tool damageFORWARD CARGO BAY DRILL START IN FRAME RADIUS, STA 120, ABOVE LONGERON 31 RIGHT, RIGHT BUTT LINE 33. ORIGINAL MATERIAL 7075-T6 0.090" PER DC8 SRM 53-4-1, PG 125. FABRICATED REPAIR ANGLE FROM 7075-0 FIG 2, HEAT TREATED IAW DC8 SRM 51-1-4, SHIM FROM 7075-T6 0.Oct 16, 2005 · N826AX · Doug DC863F · Fuselage Main, FrameSDR ABXA060018Fitting · crackedAFT CARGO, RT SIDE, STA. 1580 HAD CRACKED FITTING, RBL 58, LONGERON 21 RT. REMOVED AND REPLACED CRACKED FITTING AT STA. 1580, RBL 58 IAW SRM 51-1-21 AND 51-3-1.Oct 14, 2005 · N826AX · Doug DC863F · Fuselage Main, Attach FittingsSDR ABXA050335Floorbeam · corrodedMAIN DECK AFT ACCESSORY COMPARTMENT, STA 1660, LEFT BUTT LINE 44, LONGERON 22 LEFT, FLOORBEAM HAD CORROSION. CLEANED UP SURFACE CORROSION WITH NEGLIGIBLE MATERIAL LOSS EXCEPT FOR AROUND ONE FASTENER HOLE. REPAIRED CORROSION DAMAGE IAW DC8 SRM 51-1-8, PG 20, Oct 14, 2005 · N826AX · Doug DC863F · Fuselage Main, Floor BeamSDR ABXA060017Angle · corrodedCORROSION LOWER ANGLE ON PRESSURE WEB ON FWD BULKHEAD STA. 857, FORWARD OF RT. WHEEL WELL, APPROXIMATELY LONGERON 24. WING TO BODY ANGLE AT STA. 857 CORRODED BEYOND LIMITS. ANGLE REMOVED FROM LBL13 - RBL 57.5 AND NEW SECTION INSTALLED IAW SRM 51-1-20.Oct 12, 2005 · N826AX · Doug DC863F · Fuselage Miscellaneous StructureSDR ABXA050364Angle · corrodedFOUND CORNER ANGLE ON PRESSURE WEB CORRODED ON FORWARD BULKHEAD IN RIGHT WHEEL WELL, STA 857, RIGHT BUTT LINE 48. NEW CORNER ANGLE FABRICATED IAW REA D853-52555. ANGLE INSTALLED IAW DC8 SRM 51-1-20 AT STA 857, RIGHT BUTT LINE 48.Oct 12, 2005 · N826AX · Doug DC863F · Fuselage Miscellaneous StructureSDR ABXA050348Skin · damagedLOWER FUSELAGE SKIN, STA 400, LONGERON 31 RIGHT, FASTENER HEADS SHEARED. REMOVED DAMAGED FASTENERS, NOTED CORROSION ON INTERNAL FINGER DOUBLER AT STA 440 LONGERON 31 RIGHT. REPAIRED FINGER DOUBLER IAW REA D853-52523. ELONGATED AND OVER-SIZED HOLES AT STA 44Oct 12, 2005 · N826AX · Doug DC863F · Fuselage Main, Plate/SkinSDR ABXA050349Fitting · crackedUPPER FORWARD MOST SUPPORT ANGLE WAS CRACKED IN 2 PLACES ON TOP OF L-24 FITTING IN RIGHT WHEEL WELL. REMOVED AND REPLACED CRACKED FITTING TOP OF L-24 RIGHT WHEEL WELL STA 880, P/N: 5750198-502 IAW DC8 SRM 51-1-20D.Oct 12, 2005 · N826AX · Doug DC863F · Fuselage Main, Attach FittingsSDR ABXA050350Fitting · corrodedFOUND STA 900, L-24, CORROSION ON FORWARD SECTION AND AFT OF FITTING AT ATTACH POINT TO L-24. REMOVED AND REPLACED FITTING WITH NEW PART IAW DC8 SRM 51-10-1. POSITIONED, DRILLED UP HOLES, REAMED AND INSTALLED FITTING AT STA 879 (900) L-24 IN LEFT WHEEL WELL Oct 12, 2005 · N826AX · Doug DC863F · Fuselage Main, Attach FittingsSDR ABXA060015Cusp Web · corrodedCORROSION ON CUSP LINE EXTRUSION, STA. 1020 TO STA. 114O, LONGERON 21 RT. CORRODED BEYOND LIMITS. REMOVED AND REPLACED CUSP EXTRUSION IAW SRM 53-2-5, FIG. 15 AND 15A.Oct 11, 2005 · N826AX · Doug DC863F · Fuselage Miscellaneous StructureSDR ABXA060016Floorbeam · corrodedCORROSION RUNNING THE ENTIRE FLOORBEAM, FORMER AND FASTENERS AT STA. 1640, LONGERON 22 RT, UNDERSIDE AFT. CORRODED BEYOND LIMITS AT RBL 53-60. REMOVED END CAP AND DOUBLER L/S. REMOVED CORROSION IAW SRM 53-2-0, PG 2P, FIG 1F AND INSTALLED END CAPS AND DOUBLER. Oct 11, 2005 · N826AX · Doug DC863F · Fuselage Main, Floor BeamSDR ABXA050347Support Fitting · crackedSUPPORT FITTING WAS CRACKED ON LONGERON 24 RIGHT IN RIGHT MAIN LANDING GEAR WHEEL WELL AT APPROXIMATELY STA 940. REMOVED SUPPORT FITTING BRACKET ON LONGERON 24 STA 940 RIGHT MAIN LANDING GEAR, NEW BRACKET FABRICATED BY OUTSIDE VENDOR, REF REA D853-52521, PO NOct 11, 2005 · N826AX · Doug DC863F · Fuselage Miscellaneous StructureSDR ABXA050363Keelbeam · corrodedCORROSION FOUND ON SURFACE OF KEEL BEAM IN MID CARGO BAY BILGE AREA, STA 610 TO 710 APPROXIMATELY BUTT LINE 0. MULTIPLE BLENDED AREAS ON BOTH HORIZONTAL LEGS RANGING FROM 0.010" MIN TO MAX BLEND DEPTH OF 0.141". REMOVED CORROSION ON UPPER SURFACE OF KEEL BEAOct 10, 2005 · N826AX · Doug DC863F · Fuselage Main, KeelSDR ARWA20051002Line · leakingLOST HYD FLUID FROM MAIN HYD RESERVOIR AFTER LANDING. UPON INSPECTION; FOUND FLEX LINE LEAKING ON RT MAIN GEAR TRUCK O/B HYD MANIFOLD NEXT TO BOGGIE TRIM ACTUATOR. REMOVED & REPLACED LINE WITH E EACH FLEX LINE FROM FAK. REPLACED DAMAGE LINE IN HYD SYSTEM ONOct 8, 2005 · N441J · Doug DC863F · Hydraulic System, MainSDR ARWA20050909Bleed Valve · failedDURING TAKEOFF AT MAX POWER 1.87 GPR BETWEEN 60 AND 80 KNOTS, HAD A LOUD BANG ON NR 2 ENGINE COMPRESSOR N2 INDICATOR SWUNG VIOLENTLY. ABORTED TAKEOFF AND SECURED NR 2 ENGINE WITH APPROPRIATE CHECKLIST. REMOVED AND REPLACED NR 2 SURGE BLEED VALVE ON ENGINE NRSep 10, 2005 · N661AV · Doug DC863F · Compressor Bleed ValveSDR ARWA20050803Link Assy · vibrationAFTER TAKEOFF AND GEAR RETRACTION, EXPERIENCED CONTINUOUS VIBRATION AND NOISE FROM NOSE WHEEL WELL AREA. RETURNED AND LANDED TO INVESTIGATE. REMOVED AND REPLACED RT NOSE DOOR LINK ASSEMBLY IAW MM. PERFORMED ADJUSTMENT TEST SYSTEM IAW M/M. TEST GOOD.Aug 17, 2005 · N441J · Doug DC863F · Nose/Tail Landing GearSDR ARWA20050705Wire · damagedAFTER LANDING, FIRE WARNING CAME ON; ENGINE NR 4. COMPLETED APPROPIATE CHECKLIST. REPAIRED WIRING ON NR 4 FIRE WARNING LOOP CONNECTOR (AFT) IN ACCORDANCE WITH M/M 20-50-1. CHECK GOOD IN ACCORDANCE WITH M/M 26-10-0 AND M/M 71-00.Jul 30, 2005 · N661AV · Doug DC863F · Fire DetectionSDR ARWA20050704Fire Loop · chafedNR 4 ENGINE FIRE WARNING ON CLIMB-OUT, MROL SECURED ENGINE IN ACCORDANCE WITH ARROW PROCEDURES "NOTED HIGH OIL TEMPERATURE AFTER SHUTDOWN, OIL PRESSURE 20 PSI IN-CRUISE, 10 PSI ON APPROACH. INSPECTED NR 4 ENGINE; FOUND NR 4 FIRE LOOP CHAFING AGAINST ENGINE COJul 27, 2005 · N661AV · Doug DC863F · Fire DetectionSDR ARWA20050908Skin · corrodedDURING "C" CHECK INSPECTION, THE FOLLOWING WAS FOUND; RT INBOUND AILERON BETWEEN XA 565 AND XA542 LOWER SKIN WITH CORROSION.Jul 18, 2005 · N784AL · Doug DC863F · AileronsSDR ARWA20050906Skin · corrodedDURING C-CHECK INSPECTION, THE FOLLOWING WAS FOUND; FUSELAGE EXTERIOR STA 1690 THROUGH STA 1734, L-29L, SKIN WITH CORROSION.Jul 14, 2005 · N784AL · Doug DC863F · Fuselage Main, Plate/SkinSDR ARWA20050907Structure · crackedDURING "C" CHECK INSPECTION, THE FOLLOWING WAS FOUND; NR 2 PYLON FOOT STOOL INBOUND SIDE WITH CRACK, APPROXIMATELY 5/8".Jul 12, 2005 · N784AL · Doug DC863F · Nacelle/Pylon Miscellaneous StructureSDR ARWA20050905Structure · crackedDURING C-CHECK INSPECTION, THE FOLLOWING WAS FOUND; NR 3 PYLON FOOT STOOL INBOUND SIDE WITH 1.750 INCH CRACK.Jul 12, 2005 · N784AL · Doug DC863F · Nacelle/Pylon Miscellaneous StructureSDR ARWA20050904Skin · corrodedDURING C-CHECK INSPECTION, THE FOLLOWING WAS FOUND; AFT ACCESSORY COMPT INTERIOR STA 1620 THROUGH STA 1640, BETWEEN L-32L AND L-33L, SKIN WITH CORROSION.Jul 7, 2005 · N784AL · Doug DC863F · Fuselage Main, Plate/SkinSDR ARWA20050903Skin · corrodedDURING "C" CHECK INSPECTION, THE FOLLOWING WAS FOUND; LOWER FUSELAGE STA 1690 THROUGH STA 1720, L-31L THROUGH L-31R, SKIN PANEL WITH CORROSION AT SEVERAL PLACES.Jun 23, 2005 · N784AL · Doug DC863F · Fuselage Main, Plate/SkinSDR ARWA20050902Skin · corrodedDURING "C" CHECK INSPECTION, THE FOLLOWING WAS FOUND; LOWER FUSELAGE STA 1490 THROUGH STA 1690, L-31L THROUGH L-31R, SKIN PANEL WITH CORROSION AT SEVERAL PLACES.Jun 23, 2005 · N784AL · Doug DC863F · Fuselage Main, Plate/SkinSDR ARWA20050606Seal · openUNABLE TO CONTROL PRESSURIZATION DURING CLIMB. PERFORMED AIR TURNBACK - OVERWEIGHT LANDING INTO KMIA WITHOUT ANY FURTHER INCIDENTS. PRESSURIZED AIRCRAFT AND FOUND CABIN ENTRANCE DOOR ANGLE-SEAL UPPER AND LOWER RETAINER PARTIALLY OPEN, LUBE CABIN SEAL IN ACCJun 16, 2005 · N906R · Doug DC863F · Passenger/Crew DoorsSDR ARWA20050605Control Cable · brokenON PRE-FLIGHT RUDDER CONTROL LIGHT OFF WITH AUXILIARY HYDRAULIC PUMP ON AND RUDDER POWER LEVER OFF POSITION. FOUND RUDDER HYDRAULIC SHUT-OFF CABLE BROKEN. REMOVED AND REPLACED CONTROL CABLE IN ACCORDANCE WITH M/M 20-17-0 AND 91-10-0; OPERATIONAL CHECK NORMALJun 15, 2005 · N906R · Doug DC863F · Rudder Control SystemSDR ABXA050154Longeron · corrodedCORROSION DISCOVERED ALONG LONGERON 24 RIGHT, BEHIND THE INBOARD SPLICE FITTING AT STA 980 IN THE RIGHT WHEEL WELL. REMOVED CORROSION FROM THE LONGERON AND FITTING BY BLENDING. ALL REWORKED AREAS ARE WITHIN SRM LIMITS.Jun 14, 2005 · N826AX · Doug DC863F · Fuselage Main, Longeron/StringerSDR ARWA20050603Transmitter · malfunctionedAT 1845Z NR 1 ENGINE OIL PRESSURE WENT -0- PSI, PERFORMED ABNORMAL CHECKLIST AND ENGINE INFLIGHT SHUTDOWN AT 1848Z. REMOVED AND REPLACED NR 1 ENGINE OIL PRESSURE TRANSMITTER IN ACCORDANCE WITH M/M 79-32-1; OPERATIONAL CHECK GOOD IN ACCORDANCE WITH M/M 79-32-0Jun 7, 2005 · N661AV · Doug DC863F · Engine Oil PressureSDR ARWA20050602Indicator · defectivePRIOR TO TAKEOFF SPOOLED ALL FOUR ENGINES; NR 1 ENGINE -0- OIL PRESSURE FOLLOWED BY ABNORMAL CHECKLIST. REMOVED AND REPLACED NR 1 OIL PRESSURE INDICATOR IN ACCORDANCE WITH M/M 79-32-0; OPERATIONAL CHECK IN ACCORDANCE WITH M/M 7100 FOUND NORMAL.Jun 7, 2005 · N661AV · Doug DC863F · Engine Oil PressureSDR ARWA20050601Cable · brokenGUST LOCK HARD TO ENGAGE SUSPECT CABLE BROKEN. R & R GUST LOCK CABLE RUNNING NR 79A IN ACCORDANCE WITH DC8 M/M 27-70-0. RIGGED AND OPERATIONAL CHECK FOUND NORMAL IN ACCORDANCE WITH DC8 M/M 27-70-0.Jun 2, 2005 · N661AV · Doug DC863F · Gust Lock Damper System
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