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.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR ABXA030473Cylinder · leakingHYDRAULIC QUANTITY GRADUALLY DECREASED DOWN TO 7 GALLONS. LOSS OF HYDRAULICS EMERGENCY PROCEDURE FOLLOWED. MAINTENANCE FOUND RT BOGIE TRIM CYLINDER LEAKING. REPLACED RT BOGIE TRIM CYLINDER IAW MM 32-33-01-2.SDR ARWA20031105Compressor · stalledON FLIGHT 410, THE NR 4 ENGINE COMPRESSOR STALLED, FOLLOWED BY LOSS OF POWER. ACCOMPLISHED IN FLIGHT ENGINE SHUTDOWN AS PER FOM; ENGINE SHUTDOWN AT 14:35, THE WINDMILLING OIL PRESSURE WAS ZERO.SDR ARWA20031103Axle · damagedRED DOOR NOT LATCHED, LIGHT WOULD NOT GO OUT AFTER MLG RETRACTION. RECYCLED PER ABNORMAL CHECKLIST, NO HELP. RED GEAR NOT LATCHED. LIGHT WOULD NOT GO OUT AFTER GEAR RETRACTION. RECYCLED PER ABNORMAL CHECK LIST, NO HELP. UPON INSPECTION OF MLG FOUND NR 7 WHSDR ABXA030438Latch · wornRED GEAR UNSAFE LIGHT AND LEFT GEAR DOOR NOT LATCHED LIGHT CAME ON. BOTH LIGHTS WENT OUT AFTER PERFORMING ALTERNATE UPLATCH CHECK ABNORMAL, THRU FLAP EXTENSION. GEAR CYCLED. CHECKED GEAR DOOR LATCH MECHANISM, CHECKED TARGET, CLEANED AND LUBED SWITCH AND CYCSDR ARWA20031101Brake Assy · damagedAIRCRAFT DOES NOT TAXI UNDER IT'S OWN POWER. FOUND NR 6 BRAKE ASSEMBLY DAMAGED. REMOVED AND REPLACED BRAKE ASSEMBLY IAW DC8 MM 32-42-1 AND MAIN WHEEL ASSEMBLY IAW MM 32-40-1. OPERATIONAL CHECK NORMAL.SDR ABXA030437Seat · defectiveFLIGHT ENGINEER'S SEAT VERTICAL HOLD WOULD NOT HOLD WHILE SEAT WAS FACING FORWARD. FELL 3 TIMES DURING TAKEOFF AND INITIAL CLIMB. REPLACED SYSTEMS ENGINEER SEAT PER ABX DC8 AMM 25-11-06-2-001. LUBED AND OPS CHECKED GOOD.SDR U2R2004F00001Fastener · mismanufacturedREPAIRED L2 DOOR AT LOWER FORWARD CORNER FS1620 IAW MM.SDR U2R2004F00000Spar Cap · crackedDURING REPETIVE COMPLIANCE WITH AD AND SB, DETECTED 2 CRACKS AT RT WING FRONT SPAR LOWER CAP, REPAIRED IAW SB. REMAINING HOLES STRESS COINED TO CONDITION 1, OPTION 2.SDR U2RB102903Spar Cap · crackedDURING REPETITIVE COMPLIANCE WITH A/D 2001-06-02 & S/B 57-90 R5 DETECTED 2 EACH CRACK INDICATIONS IN NON ADJACENT ATTACHMENT HOLES OF THE FORWARD LEG OF THE RIGHT WING FRONT SPAR LOWER CAP. REPAIRED 2 EACH CRACKED HOLES IAW DC-8 S/B 57-90 R5 TABLE 4, CONDITIOSDR ARWA20031003Warning Light · false activationLANDING GEAR DOOR NOT LATCH LIGHT ILLUMINATED AFTER TAKEOFF; PERFORMED ABNORMAL CHECKLIST, LIGHT WENT OUT. CLEANED, INSPECTED & LUBRICATED LANDING GEARS AND DOORS IAW DC8 MM 12-81-1. ACCOMPLISHED GEARS SWING IAW DC8 MM 32-30-0. NO DEFECTS NOTED.SDR ARWA20031001Link · brokenON APPROACH, WHEN SELECTING FLAPS 23 DEGREES AIRCRAFT ROLLED TO THE LEFT WITH SPLIT FLAP INDICATION, ON POST FLIGHT FOUND RT INBOARD FLAP BRACKET BROKEN. RECORD FOR 27-268. REMOVED AND REPLACED RT INBOARD FLAP IAW MM 27-51-4. OPERATIONAL CHECK NORMAL IAW 27SDR ABXA030392Switch · dirtyDURING DESCENT, LANDING GEAR WAS EXTENDED TO FACILITATE DESCENT. WHEN GEAR WAS RETRACTED, LANDING GEAR UNSAFE LIGHT ILLUMINATED. LANDING GEAR AND DOOR LATCHING "NOT LATCHED" LIGHT ILLUMINATED WITH SELECTOR IN LEFT DOOR POSITION. PERFORMED ABNORMAL PROCEDURE. WSDR ARWA20030914Bleed Valve · stuckUNABLE TO OBTAIN MAX POWER INDICATION WITH NR 1 TROTTLE AT IT'S FULL FORWARD STOP POSITION. FOUND NR 1 ENGINE SURGE BLEED VALVE STUCK OPEN; REMOVED AND REPLACED NR 1 ENGINE SURGE BLEED VALVE IAW DC-8 MM 75-30-3; OPERATIONAL CHECK NORMAL IAW MM 71-00.SDR ARWA20030910Structure · brokenDURING AN A-CHECK INSPECTION, THE FOLLOWING WAS FOUND; NR 1 PYLON EDGE BROKEN, AFT OF LT FORWARD MOUNT.SDR ARWA20030909Structure · crackedDURING AN A-CHECK INSPECTION, THE FOLLOWING WAS FOUND; NR 1 PYLON WITH CRACK, AFT OF RT FORWARD MOUNT.SDR ARWA20030901Cylinder · brokenAFTER TAKE-OFF, WHEN GEAR WAS RETRACTED; NOT LATCHED AND DOORS NOT LATCHED. LIGHT REMAINED ILLUMINATED. PERFORMED LANDING GEAR SYSTEM ABNORMAL CHECK LIST AND RETURNED TO MNMG. FOUND RT GEAR BOGIE TRIM CYLINDER BROKEN AT FORWARD ATTACH POINT; REMOVED AND RESDR ARWA20030807Door Frame · crackedDURING ROUTINE INSPECTION THE FOLLOWING WAS FOUND; AFT SERVICE DOOR JAMB, AFT TOP CORNER WITH CRACK OF 1.125 INCH. REPAIRED THE AFT SERVICE DOOR JAMB AFT TOP CORNER IAW SRM 53-2-0 FIG 16, SHEETS 4, 5, 6, 7 & 8 TEMPORARY REVISION 53-156, DATED 12/20/02. (EA 10SDR ARWA20030806Door Frame · crackedDURING ROUTINE INSPECTION THE FOLLOWING WAS FOUND; AFT ENTRANCE DOOR JAMB AFT BOTTOM CORNER WITH CRACKS OF 0.625 & 0.437 INCH. REPAIRED THE AFT ENTRANCE DOOR JAMB AFT BOTTOM CORNER IAW SRM 53-2-0 FIG 18, SHEETS 1, 5, 6, 7 & 8, TEMPORARY REVISION 53-134 & TEMPSDR ARWA20030801Bleed Valve · inoperativeCOMPRESSOR STALL NR 2 ENGINE COMMENCING THE TAKE OFF ROLL. REJECTED TAKE OFF (RTO). REMOVED AND REPLACED NR 2 PRESSURE RATIO SURGE BLEED VALVE IAW MM 75-30-3. OPERATIONAL CHECK ON RUN UP IAW MM 71-0 FOUND NORMAL.SDR ABXA030323Engine · overheatedDURING TAKEOFF, NR 3 ENGINE EGT WENT TO 600 DEGREES. RETARDED THROTTLE AND EGT DECREASED INTO NORMAL RANGE. OTHER INSTRUMENTS DECREASED AS WELL. SECURED ENGINE PER ABNORMAL PROCEDURES. EGT AT 600 DEGREES FOR APPROXIMATELY 15 SECONDS. NR 3 ENGINE WAS SHUTDSDR ARWA20030709Cylinder · inoperativeAFTER LANDING, LOST ALL HYDRAULIC FLUIDS. FOUND RT BOGIE TRIM CYLINDER IAW MM 32-33-1 ALTERNATE METHOD. OPERATIONAL CHECK NORMAL.SDR ABXA030309Angle · corrodedCORROSION ON FORWARD EDGE OF ANGLES AT UPPER OUTBOARD CORNER OF RIGHT WHEEL WELL. REPAIRED AREA IAW DC-8 SRM 51-1-8, 51-1-20D, 51-1-21, 51-3-0 AND ABX JOB CARD 8078002.SDR ABXA030310Door Frame · crackedL2 DOOR, UPPER AFT CORNER OF DOOR CUTOUT CRACKED. REMOVED AND REPLACED DOUBLER, TRIPLER AND FILLER IAW DC-8 SRM 53-2-0, 51-1-8, 51-1-20D, 51-1-21 AND 51-1-11.SDR ABXA030311Skin · corrodedMAIN CARGO COMPARTMENT CORROSION ON CENTER WING UPPER SKIN AND DOUBLER FROM FS 760 - 855, LEFT BUTTLINE 3 - 23. REMOVED CORROSION, FABRICATED REPAIR DOUBLER AND BUSHINGS, ALODINED, PRIMED, INSTALLED AND LEAK CHECKED IAW REA D857-47555MR AND REA D857-47547MR, SDR ARWA20030705Spring · brokenLOG PAGE 102010. AFTER TAKEOFF, DOORS NOT LATCHED LIGHT ILLUMINATED. FOUND BROKEN SPRING AT RT MAIN LANDING GEAR DOOR CONTROL VALVE MECHANISM. REPLACED SPRING IAW MM 32-32-7, PERFORMED GEAR SWING IAW MM 32-30-0; FOUND NORMAL SYSTEM.SDR ABXA030312Panel · damagedCOI 43055-01, NR 3 PYLON INBOARD STRESS PANEL. REPAIRED AREA IAW REA D854-47544MR, REV A.SDR ARWA20030606Pin · damagedON WALK-AROUND FOUND LT MAIN LANDING GEAR EYEBOLT ACTUATOR WITH EXCESSIVE GAP AT PIN BOSS ATTACHMENT. REMOVED LT MAIN LANDING GEAR ROUTED TO SHOP FOR ACTUATOR PIN REPLACEMENT, REINSTALLED SERVICIABLE MAIN LANDING GEAR IAW MM 32-11-0, OPERATIONAL LEAK CHECK OKSDR ARWA20030602Transmitter · inoperativeAFTER BRAKE RELEASE, WHILE SETTING MAX POWER, NUMBER ONE ENGINE OIL PRESSURE ROSE TO 60 PSI. REMOVED AND REPLACED PRESSURE TRANSMITTER IAW MM 79-32-1. ACCOMPLISHED ENGINE RUN UP IAW ARROW AIR J/C 72-000-30-02SDR ARWA20030512Skin · corrodedDURING C-CHECK INSPECTION THE FOLLOWING WAS FOUND; FUSELAGE EXTERIOR SURFACE WITH CORROSION, STATION 510, L-35R. REPAIRED FUSELAGE LOWER SKIN AT FUSELAGE STA 510 AND L-35R IAW AVITAS ENGINEERING REPAIR ORDER AROW-031RO-5, PAGE 1 & 2, DATED 05/01/03 AND REPAIRSDR ARWA20030511Skin · corrodedDURING C-CHECK INSPECTION THE FOLLOWING WAS FOUND; AFT FUSELAGE INNER SKIN WITH CORROSION BETWEEN STATION 1660 AND STATION 1680, BETWEEN L-24R AND L-25R. REMOVED CORROSION IAW DC8 SRM 51-1-8, FOUND TO BE OUT OF LIMITS IAW DC8 SRM 53-2-0, REMOVED DAMAGED AREA SDR ARWA20030510Skin · corrodedDURING C-CHECK INSPECTION THE FOLLOWING WAS FOUND; FUSELAGE EXTERIOR LOWER SURFACE RIVET PLUNGED, STATION 540, BY L-36. FOUND TO BE OUT OF LIMITS IAW DC8 SRM 53-2-0. REMOVED CORROSION IAW DC8 SRM 51-1-8, FOUND TO BE OUT OF LIMITS IAW DC8 SRM 53-2-0, TRIMMED SDR ARWA20030509Doubler · corrodedDURING "C" CHECK INSPECTION THE FOLLOWING WAS FOUND; AFT LOWER CARGO COMPARTMENT STATION 1620, BETWEEN L-26R AND L-31R INNER SKIN WITH SEVERAL SPOTS OF CORROSION. REPAIRED FUSELAGE INNER DOUBLER AT FS 1620, BETWEEN L-25R AND L-31R IAW MFG ENGINEERING REPAIR OSDR ARWA20030508Fitting · crackedN/R 421. DURING "C" CHECK INSPECTION THE FOLLOWING WAS FOUND; RT MAIN LANDING GEAR WHEEL WELL STATION 879, L-24R FITTING WITH CORROSION AND 3 INCH CRACK. REMOVED AND REPLACED FITTING OF R/H MAIN LANDING GEAR WHEEL WELL STA 879, L-24R IAW SRM 51-1-20D AND SRSDR ARWA20030507Angle · crackedDURING "C" CHECK INSPECTION THE FOLLOWING WAS FOUND; AFT LOWER CARGO COMPARTMENT AFT DOOR SUPPORT ANGLE WITH CRACK; STATION 1420. REMOVED ANGLE IAW DPS 3.67-27, FABRICATED NEW ANGLE IAW DPS 3.69-4, PRIMED NEW ANGLE IAW DC8 SRM 51- 1-8 AND INSTALLED ANGLE AIW DSDR ARWA20030506Bulkhead · crackedDURING (C) CHECK INSPECTION THE FOLLOWING WAS FOUND; STATION 1766 AFT PRESSURE BULKHEAD, L-3R UUPER EAP WITH 2 INCH CRACK. TRIMMED OUT DAMAGED AREA AND FABRICATED REPAIR PART IAW REPAIR ORDER AROW-031RO-2, PAGE 1 TO 2, DATED 05/01/03 AND REPAIR DRAWING NUMBERSDR ARWA20030505Clip · crackedNR 194. DURING "C" CHECK INSPECTION THE FOLLOWING WAS FOUND;FORWARD LOWER CARGO COMPARTMENT STATION 300, BETWEEN L-33R & L-34R FITTING WITH CRACK. REMOVED AND REPLACED FITTING ON FOWARD LOWER CARGO COMPARTMENT STA.300 BETWEEN L-33R & L-34R IAW WITH SRM 51-SDR ABXA030170Seal · tornGEAR UNSAFE LIGHT REMAINED ILLUMINATED WITH GEAR RETRACTED. CYCLED GEAR AND LIGHT WENT OUT. RIGHT MAIN LANDING GEAR DOOR IDENTIFIED ON FLIGHT ENGINEER'S LANDING GEAR AND DOOR LATCHING PANEL. CLEANED UP LATCH SWITCH. OPS CHECKED GOOD IAW DC-8 AMM 32-60-00-2SDR ABXA030146Pressure Switch · defectiveAT FL 330, RAT -15, NR 3 ENGINE OIL PRESSURE LIGHT ILLUMINATED WITH 51 PSI AND OIL TEMP. OF 110 DEG. DURING IDLE, TEMP WAS 115 DEGREES, RPESSURE OF 48 PSI. OIL PRESSURE LIGHT FLICKERED AT IDLE. PERFORMED ENGINE SECURING PROCEDURE. NR 3 ENGINE N2 40 PERCENT ANDSDR ARWA20030502Pressure Switch · failedNR 1 ENGINE LOST OIL QTUANTITY. ENGINE WAS SHUT DOWN. AIRCRAFT LANDED IN KMIA WITHOUT INCIDENTS. FOUND NR 1 ENGINE OIL PRESS DIFFERENTIAL SWITCH LEAKING. REMOVED AND REPLACED SWITCH IAW DC8 MM 79-31-06. PERFORMED ENGINE RUN UP AND OPS CK IAW DC8 MM 71-00 FOUSDR ABXA030138Lock · brokenAFTER PRE-DEPARTURE CHECK WAS COMPLETED. CREW WAS UNABLE TO OPEN COCKPIT DOOR. FOUND DOOR LOCK PLUNGER BROKEN IN LOCKED POSITION. INSTALLED SLIDE LOCK ON FLIGHT COMPARTMENT SIDE OF COCKPIT DOOR. VERIFIED THAT LOCK WAS OPERABLE FROM INSIDE THE COCKPIT. REPLACEDSDR ABXA030137Battery · dischargedMAINTENANCE FOUND EMERGENCY LIGHT VERY WEAK IN TEST. REPLACED EMERGENCY LIGHTS BATTERY RACK ASSEMBLY. OPS CHECKED GOOD IAW DC-8 MM.SDR ARWA20030404Fuel Control · malfunctionedNR 4 ENGINE HUNG START IN SKGO, SLOW TO SPOOL ON GROUND AND SLOW TO SPOOL IN FLIGHT. REMOVED AND REPLACED NR 4 ENGINE FUEL CONTROL UNIT (FCU) IAW DC-8 MM 73-20-1. LEAK CHECK OK. OPERATIONAL CHECK PERFORMED IAW MM 71-00 ON RUN UP FOUND NORMAL.SDR ABXA030128Servo Valve · malfunctionedUNCOMMANDED YAW IN FLIGHT. AUTOPILOT ON. REPLACED RUDDER POWER PACK TRANSFER VALVE IAW DC-8 MM 27-21-6.SDR ABXA030129Computer · defectiveRUDDER UNCOMMANDED LT INPUT AT 3,000 FT, 200 KTS, AND 23 DEGREES FLAPS. AUTOPILOT OFF, YAW DAMPER ON. COULD NOT DUPLICATE PROBLEM. REPLACED YAW DAMPER COMPUTER. OPS CHECKED GOOD IAW DC-8 MM 22-10-00.SDR ABXA030264Frame · damagedREMOVE AND REPLACE STUB FRAME IN MAIN CARGO DOOR AT STA 183.5. REMOVED STUB FRAME, LOCATED AND DRILLED, AND INSTALLED STUB FRAME IAW ABX REA D852-46043MR AND DC-8 SRM 51-1-24.SDR ABXA030118Web · crackedCUSP WEB CRACKED AT FS 300 RIGHT ON MOST OUTBOARD TRACK. REPAIRED AREA IAW DC-8 SSRM 51-1-21 AND DWG. K07142. REF: W/O 600166120.SDR ABXA030255Door Frame · crackedUPPER LATCH HOOK MOUNT HOLE AT STA 196.5 HAD CRACK INDICATION. REMOVED DAMAGED FRAME, LOCATED, DRILLED, AND DEBURRED NEW FRAME, INSTALLED IAW ABX REA D852-46041MR AND DC-8 SRM 51-1-21 AND 51-1-8.SDR ABXA030254Structure · crackedCENTER LATCH HOOK MOUNT HOLE AT STA 203.5 HAD CRACK INDICATION. REPAIRED AREA IAW ABX REA D852-46041MR.SDR ABXA030270Door Frame · damagedCUT AND SPLICE MAIN CARGO DOOR FRAME AT STA 233.5. CUT AND REMOVED DOOR FRAME, AND SPLICED IN NEW SECTION IAW ABX REA D852-46041MR AND DC-8 SRM 51-1-20D.SDR ABXA030260Door Frame · crackedUPPER LATCH HOOK MOUNT HOLE AT STA 153.0 HAD CRACK INDICATION. REPAIRED AREA IAW ABX REA D852-46041MR.
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