Douglas DC-8-63F

Service difficulty reports · 1,883

Newest first. General aviation reporting is voluntary.

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 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 AR091051Latch Hook · frozenMIAMI - AFTER TAKEOFF, DOOR NOT LATCHED LIGHT ON. RECYCLED GEAR AND ACCOMPLISHED APPROPRIATE CHECK LIST, LIGHT REMAINED ON. RETURN TO MIAMI. TROUBLESHOOTING FOUND LEFT DOOR UPLATCH HOOK AND ATTACH FITTING HARDWARE FROZEN. DISASSEMBLED, CLEANED, RE-LUBED, RSep 10, 1995 · N661AV · Doug DC863F · Landing Gear Door Retract SectionSDR 95ZZZM521Valve · failedTWENTY MINUTES INTO FLIGHT FROM MIA, LANDING GEAR DOOR NOT LATCHED LIGHT ILLUMINATED. COULD NOT EXTINGUISH LIGHT, AIRCRAFT RETURNED TO MIA WITHOUT INCIDENT. MAINTENANCE TROUBLESHOOTING DETERMINED MLG DOOR 'J' HANDLE TO BE INTERNALLY BYPASSING (MLG DOOR CONTRSep 7, 1995 · N661AV · Doug DC863F · Landing Gear Door Retract SectionSDR 95ZZZM498Skin · corrodedDURING PREFLIGHT, FOUND EVIDENCE OF CORROSION BETWEEN FS 500 AND FS 520 BETWEEN L-28R AND L-29R. OPEN UP SKIN, CUT OUT AREA OF CORROSION AND FABRICATE REPAIR DOUBLER AND FINGER DOUBLERS AS PER DWG NR 30942-14. INSTALLED DOUBLERS AND FILLERS AS PER DWG NR ARWAug 31, 1995 · N441J · Doug DC863F · Fuselage Main, Plate/SkinSDR IXXA199575Link Assy · out of adjustON CLIMB-OUT OF ATL, WITH LANDING GEAR RETRACTED AND ALL INDICATIONS NORMAL, NOSE GEAR DOOR VIBRATION WAS EXPERIENCED AT 250 KNOTS. THE AIRCRAFT WAS SLOWED TO 230 KTS, THE GEAR WAS CYCLED, AND AN UPLATCH CHECK WAS PERFORMED. ALL INDICATIONS WERE NORMAL, BUT Aug 30, 1995 · N786AL · Doug DC863F · Landing Gear Door Retract SectionSDR IXXA199570Cabin Compressor · failedBETWEEN IAH AND BRO, THE NR 2 CABIN COMPRESSOR STALLED AND CREATED LOUD NOISE AND OILY FUMES IN THE COCKPIT. MAINTENANCE DETERMINED THAT THE CABIN COMPRESSOR HAD SEIZED. THE NR 2 CABIN COMPRESSOR WAS DEFERRED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. (M)Aug 10, 1995 · N906R · Doug DC863F · Cabin Compressor SystemSDR IXXA199569Windshield · smoke odorKNGU/BIKF - BETWEEN KNGU AND BIKE, AN ELECTRICAL SMELL AND A SMALL AMOUNT OF SMOKE WERE NOTED COMING FROM THE FIRST OFFICER'S WINDSHIELD AREA. IN KNGU, NO SOURCE COULD BE DETERMINED FOR THE SMELL. THE WINDSHIELD HEAT WAS DEFERRED AS A PRECAUTION FOR FURTHER Jul 25, 1995 · N784AL · Doug DC863F · Windshield/Door Rain/Ice RemovalSDR IXXA199568Fuel Pump · low outputHUF - DURING DESCENT AT AROUND 10,000 FEET, NR 3 ENGINE FLAMED OUT. ENGINE SHUT-DOWN PROCEDURES WERE ACCOMPLISHED. ON THE GROUND IN HUF, DETERMINED THE ENGINE WOULD LIGHT OFF, BUT HANG AT AROUND 40 PERCENT N2 RPM. TROUBLESHOOTING INDICATED THE OUTPUT OF THEJul 25, 1995 · N786AL · Doug DC863F · Engine Fuel PumpSDR 95ZZZM258Plank · crackedDURING PREFLIGHT, FOUND CRACK AT NR 1 INTERMEDIATE PYLON PLANK, PREVIOUS REPAIR. REMOVED PREVIOUS REPAIR, FABRICATE NEW DOUBLER AND TRIPLER, TREATED, PRIMED AND INSTALLED IAW DAC GL PO 1505.Jul 14, 1995 · N661AV · Doug DC863F · Nacelle/Pylon, Plate/SkinSDR 95ZZZM262Seal · leakingAIR TURN BACK WITH 4 TC'S ON, CABIN CLIMB AT 1,000 FT/MIN WHEN AIRCRAFT REACHED 20,000 FEET CARGO DOOR SEAL LEAKING, CABIN WENT TO 11,000 FEET. INSTALLED NEW BACKUP SEAL ON ENTIRE MAIN CARGO DOOR AFTER AIRCRAFT WAS LEAK CHECKED AT BLAST FENCE WITH SMOKE CANISJul 13, 1995 · N441J · Doug DC863F · Cargo/Baggage DoorsSDR 95ZZZM260Fitting · crackedDURING REPAIRS ON MAIN CARGO DOOR ACT SUPPORT FITTING, FOUND THE SIDE SUPPORT BRACKET CRACKED. REMOVED CRACKED FITTING, FABRICATED NEW FITTING AUTHORIZED BY DAC FILE C1-P63-15M/060 DATE JULY 10, 1995 IAW DRAWING 4777865 LOCATE DRILLED UP, TREATED PRIME AND INJul 10, 1995 · N661AV · Doug DC863F · Cargo/Baggage DoorsSDR 95ZZZM257Plank · crackDURING PREFLIGHT, FOUND CRACK ON NR 1 PYLON OUTBOARD SIDE LOWER PLANK STATION YN 277.8. REMOVED FASTENERS IN AREA FABRICATE DOUBLER FROM 7075-T6 .125 AND TRIPLERS FROM 7075-T6 .190 AND .160, LOCATE DRILL UP. TREATED AND PRIMED AND INSTALLED IAW DOUGLAS NR GLJul 7, 1995 · N661AV · Doug DC863F · Nacelle/Pylon, Plate/SkinSDR 95ZZZM259Fitting · crackedAFTER REMOVING NR 1 PYLON INTERMEDIATE PLANK FOR REPAIR, FOUND A CRACKED TEE FITTING ON THE INBOARD SIDE OF PYLON AT YN 336.750. REMOVED FITTING, FABRICATED NEW FITTING AS PER DOUGLAS DRAWING NR 5753022, TEE FITTING NR 3753027-2 UNDER DOUGLAS AT AUTHORIZATIONJul 5, 1995 · N661AV · Doug DC863F · Nacelle/Pylon StructureSDR IXXA199561Bearing · damagedEINN/DTW - IN CRUISE BETWEEN EINN AND DTW, THE NR 3 ENGINE OIL FILTER BYPASS LIGHT ILLUMINATED WITH NORMAL PRESSURE, BUT OIL TEMP CLIMBED SOMEWHAT ABOVE THE NORMAL RANGE. WHEN THE THROTTLE WAS RETARDED, THE BYPASS LIGHT REMAINED ON, ENGINE WAS PRECAUTIONARILYJun 30, 1995 · N786AL · Doug DC863F · Turbine Engine Combustion SectionSDR CKSA95062Fitting · corrodedKYIP - DURING B-CHECK INSPECTION, FOUND LONGERON 30L AT FS 1660, CORRODED. REPAIRED PER DC-8 SRM 53-2-2. REPLACED LONGERON END FITTING, STA 1660 LONGERON 30L. (X)Jun 28, 1995 · N867BX · Doug DC863F · Fuselage Miscellaneous StructureSDR CKSA95061Skin · corrodedKYIP - DURING B-CHECK INSPECTION, FOUND FUSELAGE SKIN BULGING FROM CORROSION AT STATION 1660, LONGERON 30L. REPAIRED FUSELAGE SKIN AT STATION 1660, LONGERON 30L IAW EA NR 95-178. (M)Jun 28, 1995 · N867BX · Doug DC863F · Fuselage Main, Plate/SkinSDR ABXA9500571Switch · faultyLANDING GEAR UNSAFE LIGHT REMAINED ILLUMINATED. UPLATCH CHECK OK, WARNING HORN AUDIBLE WITH FLAPS OUT OF ZERO POSITION. RECYCLED GEAR, NO CHANGE NOTED. FOUND THROTTLE SWITCH AT FAULT. CORRECTED PROBLEM, GEAR INDICATION OPS CHECKED GOOD IAW DC-8 SUPPLEMENTAJun 28, 1995 · N819AX · Doug DC863F · Landing Gear Position and WarningSDR ABXA9500561Uplatch · lack of lubeRIGHT MAIN LANDING GEAR DOOR FAILED UPLATCH CHECK. RECYCLED GEAR. LIGHT EXTINGUISHED. CLEANED, INSPECTED AND LUBED THE RIGHT MAIN GEAR DOOR UPLATCH. PERFORMED ADJUSTMENT TEST IAW MAB 32-6. OPS CHECKED GOOD.Jun 21, 1995 · N819AX · Doug DC863F · Landing Gear Retraction/Extension SystemSDR 95ZZZX3390Engine · failedAFTER 27 MINUTES IN FLIGHT FROM SAN JUAN, PR, WITH DESTINATION MIAMI, FL, THE CREW DESCRIBED THE PROBLEM AS: IN CLIMB-OUT OF 10,000 FEET, GOT LOUD BANG AND ACFT YAW. NR 1 EPR DOWN AND EGT APPROACHING 600 CELSIUS. SHUT ENGINE DOWN AT 17037 AND RETURNED TO SJJun 18, 1995 · N441J · Doug DC863F · Engine (Turbine/Turboprop)SDR ABXA9500557Line · defectiveAFTER LIFT OFF, LOST ALL HYDRAULIC PRESSURE, RESERVOIR LOW PRESSURE AND AILERON MANUAL CONTROL LIGHTS ILLUMINATED. HYDRAULIC QUANTITY INDICATED FULL, WAS NOT ABLE TO RECOVER PRESSURE WITH AUX PUMP. REPAIRED .5 INCH STEEL HYDRAULIC LINE BEHIND ACCESS PANELS 5Jun 16, 1995 · N811AX · Doug DC863F · Hydraulic System, MainSDR 95ZZZX3972Jamb · crackedMAIN CARGO DOOR LOWER AFT DOOR, THRESHOLD HAS A CRACK. REPAIRED CRACKED CORNER FILLET AT MAIN CARGO DOOR JAMB, AFT LOWER CORNER IAW TIMCO REO DC08-53-1565.Jun 14, 1995 · N959R · Doug DC863F · Fuselage Miscellaneous StructureSDR 95ZZZX3385Smoke Detector · inopLOG BOOK ITEM NR 6, LOG PAGE 63734. SMOKE DETECTOR LIGHT ON IN-FLIGHT AT 39,000, CABIN CLEAR. REMOVED AND REPLACED SMOKE DETECTOR CONTROLLER IAW MM 26-10-0. OPS NORMAL.Jun 13, 1995 · N661AV · Doug DC863F · Smoke DetectionSDR 95ZZZX3396Plating · crackedON A ROUTINE A-CHECK, MAINTENANCE FOUND .6250 INCH CRACK AT APPROXIMATELY L/E STATION XFS 207 TOP SIDE, LEFT WING. REMOVED FASTENERS, CUT OUT CRACKED AREA. FABRICATED AND INSTALLED DOUBLER FROM 7075-T6.071 AND FILLER FROM 7075T-6.063. INSTALLED, TREATED, PRJun 5, 1995 · N661AV · Doug DC863F · Wing, Plate/SkinSDR 95ZZZX3395Plating · corrodedON A ROUTINE A-CHECK, MAINTENANCE FOUND LEVEL 3 CORROSION AT APPROXIMATELY L/E STA XFS 257 TOP SIDE, LEFT WING. REMOVED FASTENERS, CUT OUT AREAS OF CORROSION, FABRICATED AND INSTALLED DOUBLER FROM 7075-T6.090 AND 2 EACH FILLERS FROM 7075-T6. REPAIRED AND AREJun 5, 1995 · N661AV · Doug DC863F · Wing, Plate/SkinSDR 95ZZZX3185L/E Skin · crackedON A ROUTINE A-CHECK, MAINTENANCE FOUND .6250 INCH CRACK AT APPROXIMATELY L/E STATION XFS 207 TOP SIDE, LEFT WING.Jun 5, 1995 · N661AV · Doug DC863F · Wing, Plate/SkinSDR 95ZZZX3178Plating · corrodedON A ROUTINE 'A' CHECK, MAINTENANCE FOUND LEVEL 3 CORROSION AT APPROXIMATELY L/E STA XFS 257 TOP SIDE, LEFT WING.Jun 5, 1995 · N661AV · Doug DC863F · Wing, Plate/SkinSDR 95ZZZM90Frame · corrodedDURING 'A' CHECK, MAINTENANCE FOUND LEVEL 2 CORROSION ON CIRCUMFERENTIAL FRAME AT FS 1040, LONGERON 30L. CUTOUT DAMAGED AREA. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DER DWG ARW 12564-74.May 31, 1995 · N661AV · Doug DC863F · Fuselage Main, FrameSDR 95ZZZM89Door Jamb · corrodedDURING AN 'A' CHECK INSPECTION, MAINTENANCE FOUND LEVEL 2 CORROSION ON NR 3 BAG BIN DOOR JAMB AT APPROXIMATELY MIDWAY HIGH. MECHANICALLY REMOVED CORROSION PER DC8 SRM 51-1-8. TREATED AND PRIMED ARE IAW DC8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLERMay 31, 1995 · N661AV · Doug DC863F · Fuselage Miscellaneous StructureSDR 95ZZZM87Skin · crackedPREVIOUS FUSELAGE PLATING REPAIR AFT OF NLG RT SIDE IS LOOSE AND RIVET HEAD SHEARED (NLG DOOR CUTOUT). REMOVED DOUBLER. FOUND PROPAGATION OF PREVIOUS STOP DRILLED CRACK. CUT TO DAMAGED AREA APPROXIMATELY 6 INCHES BY 8 INCHES FABRICATED AND INSTALLED FILLER May 31, 1995 · N661AV · Doug DC863F · Fuselage Main, Plate/SkinSDR 95ZZZM190Frame Cap · corrodedCIRCUMFERENTIAL FRAME CAP AT FS 1120 BETWEEN LONGERONS 33L AND 34L HAS LEVEL 3 CORROSION. REMOVED CORROSION FROM CAP. FABRICATED AND INSTALLED DOUBLER IAW DER DWG ARW 26494-64.May 31, 1995 · N661AV · Doug DC863F · Fuselage Main, FrameSDR 95ZZZX3179Eel Battery Pack · dischargedEMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED EMERGENCY BATTERY PACK. SYSTEM OPS CHECK NORMAL IAW DC-8 MM 33-50-00.May 29, 1995 · N441J · Doug DC863F · Emergency LightingSDR 95ZZZM88Fitting · corrodedLONGERON SPLICE FITTING AT FS 1050 ON LONGERON 35R IS CRACKED. REMOVED LONGERON SPLICE FITTING, LOCATED FITTING. DRILLED UP NEW FITTING. TREATED AND PRIMED AREA. INSTALLED, TREATED, AND PRIMED NEW FITTING IAW SRM 51-1-8 AND 51-1-20.May 25, 1995 · N661AV · Doug DC863F · Fuselage Miscellaneous StructureSDR 95ZZZM86Fitting · corrodedSPLICE FITTING AT FS 1050 ON TOP SIDE OF L-31R HAS LEVEL 2 CORROSION. REMOVED SPLICE FITTING. REMOVED LIGHT CORROSION FROM AREA. DRILLED NEW FITTING. TREATED, PRIMED, AND INSTALLED FITTING IAW SRM 51-1-8 AND 51-1-20A. AREA UNDER FITTING WITHIN LIMITS IAW May 25, 1995 · N661AV · Doug DC863F · Fuselage Miscellaneous StructureSDR 95ZZZM84Longeron · corrodedLEVEL 2 CORROSION FOUND ON OUTBOARD FLANGE OF LONGERON 31R BETWEEN FS 1070 AND FS 1090. MECHANICALLY REMOVED CORROSION FROM LONGERON 31R, TREATED AND PRIMED. INSTALLED REPAIR DOUBLER IAW DER DRAWING ARW 30218-10.May 22, 1995 · N441J · Doug DC863F · Fuselage Main, Longeron/StringerSDR 95ZZZM66Longeron · corrodedLEVEL II CORROSION FOUND ON OUTBOARD FLANGE OF LONGERON 31R BETWEEN FS 1070 AND FS 1090.May 22, 1995 · N441J · Doug DC863F · Fuselage Main, Longeron/StringerSDR 95ZZZM85Blkhd Stiffener · corrodedLEVEL 2 CORROSION FOUND AFT SIDE FS 980.00 BULKHEAD AT LONGERON 30L ATTACHMENT. MECHANICALLY REMOVED CORROSION, TREATED, PRIMED AREA, AND INSTALLED REPAIR DOUBLER IAW DER DRAWING ARW 5598-3.May 18, 1995 · N441J · Doug DC863F · Fuselage Main, BulkheadSDR 95ZZZM67Stiffener · corrodedLEVEL II CORROSION FOUND AFT SIDE FS 980.00 BULKHEAD AT LONGERON 30L ATTACHMENT.May 18, 1995 · N441J · Doug DC863F · Fuselage Miscellaneous StructureSDR CKSA95034Skin · corrosionOSC - EVIDENCE OF CORROSION UNDER SKIN BETWEEN FS 25 AND 35 AT L30R. REMOVED CORROSION AND REPAIRED IAW DC-8 SRM CHAPTER 53-2-0, FIG 18 SHEET 3. TREATED AND PRIMED IAW 51-1-8. (M)May 16, 1995 · N815CK · Doug DC863F · Fuselage Main, Plate/SkinSDR CKSA95033Fitting · corrodedOSC - RIGHT AFT SERVICE DOOR LOWER AFT CORNER 2 EACH FITTINGS CORRODED. REMOVED AND REPLACED FITTINGS IAQ DC-8 SRM 53-2-0. (M)May 16, 1995 · N815CK · Doug DC863F · Service DoorsSDR CKSA95032Seat Track · corrodedOSC - CABIN NR 2 AND NR 3 SEAT TRACKS (DUAL TRACK) APPROXIMATELY 850-990 CORRODED. REPLACED DOUBLE WIDE SEAT TRACK TO TWO SINGLE TRACKS LEFT SIDE FROM STATION 850-990 IAW EA 95-066.J R1 AND SKETCH NR AIA/E/2012. (M)May 16, 1995 · N815CK · Doug DC863F · Fuselage, Seat/Cargo Attach FittingsSDR CKSA95031Angle · corrosionOSC - AFT ACCESSORY COMPARTMENT STATION 1725 AT 28L LONG LOWER LEG HAS EVIDENCE OF CORROSION. REPAIRED LOWER LEG OF LONG 28L AT STATION 1723 IAW DC-8 SRM 53-2-2 FIG 11. (M)May 16, 1995 · N815CK · Doug DC863F · Fuselage Miscellaneous StructureSDR CKSA95030Floorbeam · corrosionOSC - AFT ACCESSORY COMPARTMENT STATION 1660-1670 AT RIGHT OUTBOARD SEAT TRACK FLOORBEAM AND FLOOR HAVE CORROSION. REPAIRED FLOORBEAM AT STATION 1660 RIGHT SIDE IAW EA 95-135.B AND DWG NR SKA95093-1. CLEANED AND TREATED FLOOR IAW SRM 51-1-8. (M)May 16, 1995 · N815CK · Doug DC863F · Fuselage Main, Floor BeamSDR CKSA95029Fitting · corrosionOSC - CORROSION 'D' PIT DOOR FRAME AFT SIDE. REMOVED, CLEANED AND TREATED IAW SRM 51-1-0. REMOVED AND REPLACED 1 BATH TUB FITTING AND GILL LINER ANGLE IAW SRM 53-2-0. (M)May 16, 1995 · N815CK · Doug DC863F · Fuselage Miscellaneous StructureSDR CKSA95028Stringer · corrosionOSC - EVIDENCE OF CORROSION STATION 70 STRINGER 27R TO 34L. REPAIRED CORRODED AREA AT STATION 70 BETWEEN STRINGER 27R AND 34L IAW EA 95-135 AN DAC FAX FILE NR 268167. (M)May 16, 1995 · N815CK · Doug DC863F · Fuselage Main, Longeron/StringerSDR CKSA95027Panel · crackedOSC - INBOARD WING SLOT CRACKED, CENTER AREA. REMOVED AND REPLACED RIGHT INBOARD UPPER SLOT PANEL IAW DC-8 SRM 51-3-0 AND DC-8 MM 27-80-1. (M)May 16, 1995 · N815CK · Doug DC863F · Wing, Plate/SkinSDR CKSA95026Panel · crackedOSC - INBOARD WING SLOT CRACKED, CENTER AREA. REMOVED PANEL, STOP DRILLED CRACK IN INBOARD LEFT UPPER SLOT PANEL IAW EA95-135.1. REINSTALLED PANEL IAW DC-8 SRM 51-3-0 AND DC-8 MM 27-80-1. (M)May 16, 1995 · N815CK · Doug DC863F · Wing, Plate/SkinSDR CKSA95025Stringer · corrosionOSC - EVIDENCE OF CORROSION AT STATION 70 AND STRINGER 30R. REPAIRED AREA AT STATION 70 AND STRINGER 30R IAW EA 95-135 AND DAC FAX FILE NR 268167. (M)May 16, 1995 · N815CK · Doug DC863F · Fuselage Main, Longeron/StringerSDR CKSA95024Stringer · corrosionOSC - EVIDENCE OF CORROSION AT STATION 70 AND STRINGER 31R. REPAIRED AREA AT STATION 70 AND STRINGER 31R IAW EA 95-135 AND DAC FAX FILE NR 268167. (M)May 16, 1995 · N815CK · Doug DC863F · Fuselage Main, Longeron/StringerSDR 95ZZZM69Fitting · corrodedOSC - RIGHT AFT SERVICE DOOR LOWER AFT CORNER 2 EACH FITTINGS CORRODED. REMOVED AND REPLACED FITTINGS IAQ DC-8 SRM 53-2-0. (M)May 16, 1995 · N815CK · Doug DC863F · Service DoorsSDR 95ZZZZ264Control Vlv · defectiveKDAL-KORD - FLT 35 - DOOR WARNING AND UPLATCH WARNING LIGHTS ON AFTER GEAR RETRACTION. RECYCLED GEAR AND WARNING LIGHTS EXTINGUISHED. MAINTENANCE REMOVED AND REPLACED THE MLG CONTROL VALVE. OPERATIONAL CHECK OF THE MLG RETRACTION AND WARNING SYSTEM WAS GOODMay 12, 1995 · N952R · Doug DC863F · Landing Gear Retraction/Extension SystemSDR 95ZZZM189Skin · corrodedLEVEL 3 CORROSION FOUND ON BELLY SKIN UNDER LONGERONS 35L, 35R BETWEEN FS 1060 AND FS 1080 CIRCUMFERENTIALS. CUTOUT DAMAGED SKIN AT LONGERONS 35L AND 35R BETWEEN FS 1060 AND FS 1080. ALSO, CUTOUT DAMAGE SKIN AT FS 1100 LONGERONS 35L. INSTALLED REPAIR FILLERMay 11, 1995 · N661AV · Doug DC863F · Fuselage Main, Plate/Skin
Back to Douglas DC-8-63F