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 ABXA070051Drive Link · crackedLEFT INBOARD FLAP DRIVE LINK AT STA XW 98.00 FOUND CRACKED WHILE COMPLYING WITH JC 8020401 AND ASB 27-269, AD 088-10-7. REMOVED AND REPLACED LINK, DETAILS IN WORK PACK 600264601.SDR N921R63501Skin · dentedFOUND FUSELAGE EXTERIOR STA 78 BTW L17L AND L18L SKIN WITH DENT. REPAIRED SKIN OF FUSELAGE EXTERIOR STA 78 BTW L-17L AND L-18L IAW DC8 SRM 53-2-0, TR NR 53-170 CPCP 5000 0551.SDR N921R63504Skin · dentedFOUND FUSELAGE EXTERIOR STA 78 BTW L-17L AND L-18L SKIN WITH DENT. REPAIRED SKIN OF FUSELAGE EXTERIOR STA 78 BTW L-17L AND L-18L IAW DC8 SRM 53-2-0, TR NR 53-170 CPCP 5000-0551.SDR N921R54017Splice · corrodedLWR FUSELAGE EXTERIOR STA 1766 L-33L MANUFACTURING SPLICE WITH CORROSION. REMOVED SPLICE IAW DPS 3.67.27, FABRICATED NEW SPLICE IAW DC8 SRM 53-4-1 AND DPS 3.69.4. PRIMED NEW SPLICE IAW DC8 SRM 51-1-8 AND INSTALLED NEW SPLICE IAW DC8 SRM 51-1-21 CPCP 5000 055SDR N921R54815Skin · dentedLT WING XW 68 INBOARD FLAP TRAILING EDGE LOWER SURFACE WITH DENT ( L=3 1/8, A=2 1/2, Y=.0935). CUTOUT DAMAGED AREA AND FABRICATED FILLER, SPLICE AND SKIN IAW DC8 SRM 57-2-5 AND DC8 SRM 57-7-1. TREATED AND PRIMED REPAIR AREA AND PARTS IAW DC8 SRM 51-1-8. INSSDR N921R53410Door Frame · crackedFUSELAGE STA 8 NLG W/W DOOR JAMB RT CORNER SKIN WITH 1" CRACK. REPAIRED SKIN IAW FLIGHT VEHICLES CONSULTING INC DWG NR 51-07030-1 REV NEW 01-25-07 PAGE 1 AND 2. ISSUED FAA FORM 8110-3 CPCP 4000 0551.SDR N921R53309None · noneFUSELAGE STA 8 NLG WW DOOR JAMB LT CORNER SKIN WITH TEMPORARY REPAIR. REPAIRED SKIN IAW FLIGHT VEHICLES CONSULTING INC DWG NR 53-07030-1 REV NEW 01-25-09 PAGE 1/3. ISSUED FAA FORM 8110-3. CPCP 4000 0551SDR N921R53506Skin · damagedFUSELAGE STA 32 NLG DOOR SKIN HAS 2 NICKS. REPAIRED SKIN OF FUSELAGE STA 32 NLG RT DOOR IAW DC8 SRM 52-2-0 CPCP 4000 0551.SDR N921R53905Skin · corrodedLOWER FUSELAGE EXTERIOR STA 720 L-17L SKIN WITH CORROSION. OPENED SKIN AREA IAW DPS 3-67-27, FOUND CORRODED INNER DOUBLER, REMOVED INNER DOUBLER IAW DPS 3-67-27. FABRICATED NEW INNER DOUBLER IAW DC8 SRM 53-5-3 & DPS 3-69-4. TREATED AND PRIMED AREA AND NEW DSDR N921R50502Skin · dentedRUDDER ZR 138 LEFT SKIN AFT SECTION WITH DENT. REMOVED LT SKIN SECTION IAW DPS 3.67-27. FABRICATED NEW SKIN IAW DPS 3.69-4. TREATED AND PRIMED AREA AND NEW SKIN IAW DC8 SRM 51-1-8. INSTALLED NEW SKIN IAW DC8 SRM 51-1-21.SDR N921R40407Frame Splice · corrodedMAIN CARGO COMPARTMENT STA 520, L-17R FRAME SPLICE WITH CORROSION. REMOVED FRAME SPLICE IAW DPS 3-67-29. FABRICATED NEW FRAME SPLICE IAW DPS 3-69-4, PRIMED SPLICE IAW DC8 SRM 51-1-8. INSTALLED FRAME SPLICE IAW DC8 SRM 51-1-27 CPCP 5730-0551.SDR N921R28116Stringer Splice · crackedFWD CARGO COMPARTMENT BTW STA 440 AND 460, L31L SPLICE FITTING WITH 3/4" CRACK. REMOVED AND REPLACED SPLICE FITTING OF FWD CARGO COMPARTMENT BTW STA 440 AND STA 460, L31L IAW DC8 SRM 51-1-20 AND SRM 53-4-1 CPCP 557L 0551.SDR N921R28211Finger Doubler · corrodedFWD CARGO COMPARTMENT STA. 480, L31R FINGER DOUBLER WITH CORROSION. CLEANED CORROSION IAW DC8 SRM 51-1-8. FOUND TO BE WITHIN LIMITS IAW DC8 SRM 53-2-0. TREATED & PRIMED AREA IAW DC8 SRM 51-1-8 CPCP 557R 0551.SDR N921R72213Longeron · corrodedFOUND FUSELAGE STA 1540 L29L SKIN RIVETS SHEARED AND LONGERON 29L WITH CORROSION. REPAIRED LONGERON 29L AT FS 1540 IAW DC8 SRM 53-2-2 FIGURE 8.SDR N921R19512Stringer Splice · crackedFOUND MAIN CARGO COMPARTMENT STA 680, L4R AFT SPLICE FITTING WITH CRACK. REMOVED AND REPLACED FITTING IAW DC8 SRM 51-1-20 AND 53-4-1 CPCP 5730-0553.SDR ABXA070016Bolt · brokenLEFT MAIN LANDING GEAR STRUT LEAKED. FOUND TORSION LINK APEX BOLT DAMAGED/BROKE ON LEFT MAIN LANDING GEAR. REPLACED TORSION LINK APEX BOLT ON LEFT MAIN LANDING GEAR REPACK ON (AVBORNE) NR WX-314, IAW DC8 MM. REPLACED LEFT MAIN LANDING GEAR DOOR RETRACT ACTUSDR ABXA060311Engine · leakingNR 3 ENGINE SHUT DOWN IN FLIGHT (STA SDF) DUE TO LOSS OF OIL. FERRIED AIRCRAFT BACK TO ILN. REMOVED AND REPLACED NR 3 ENGINE PER JOB CARD 8090507 IN WORK PACK 600261630.SDR U2RA09900Downlock Switch · corrodedON LANDING AT KYIP, RT MAIN GEAR DOWN AND SAFE GREEN LIGHT WOULD NOT ILLUMINATE. FLEW BY TOWER TO SEE IF LANDING GEAR WAS DOWN. EMERGENCY VEHICLES STANDING BYE ON LANDING. AFTER ENGINE SHUTDOWN LIGHT CAME ON. COMPLIED WITH MURRAY ABNORMAL CHECK LIST. REMOSDR U2RA0990Downlock Switch · corrodedON LANDING AT KYIP-RT MAIN GEAR DOWN AND SAFE GREEN LIGHT WOULD NOT ILLUMINATE. FLEW BY TOWER TO SEE IF LANDING GEAR WAS DOWN. EMERGENCY VEHICLES STANDING BYE ON LANDING. AFTER ENGINE SHUTDOWN LIGHT CAME ON, COMPLIED WITH MURRAY ABNORMAL CHECK LIST. REMOVESDR ARWA20061005Bellcrank · brokenON POST FLIGHT FOUND NOSE GEAR DOOR BROKEN LINK. REMOVED TORQUE TUBE AND BELL CRANK IN ACCORDANCE WITH M/M 32-22-2. INSTALLED BELL CRANK AND REINSTALLED NOSE GEAR DOOR LINKAGE IN ACCORDANCE WITH M/M 32-33-2; OPERATIONAL CHECK IN ACCORDANCE WITH M/M 32-22-1 ASDR ARWA20061004Wire · damagedLOST ALL HYDRAULIC PRESSURE DURING TAXI. REPAIR WIRE ON HYDRAULIC PRESSURE TRANSMITTER IAW MM 20-51-00; OPERATIONAL CHECK NORMAL IAW MM 20-00-00.SDR ARWA20061001Compressor · stalledLOG PAGE NR 124562. ABORTED TAKEOFF AT 105 KTS FOLLOWING NR 4 ENGINE COMPRESSOR STALL. INSPECTED NR 4 ENGINE COMPRESSOR SURGE BLEED VALVE AND TIGHTEN ALL SENCE LINES IAW MM 75-30-01/201; OPERATIONAL CHECK NORMAL ON ENGINE RUN IAW M/M 71-00/501.SDR ABXA060271Battery · dischargedON PRE-D CHECK, FOUND EMERGENCY LIGHTS INOPERATIVE. SUSPECT EMERGENCY LIGHT SWITCH WAS ON OVERNIGHT WITH NO EXTERNAL POWER. REMOVED AND REPLACED EMERGENCY LIGHTING BATTERY AND RELAY UNIT RACK ASSEMBLY IAW DC8 AMM 33-50-01-2-0001. OPS CHECKED GOOD.SDR ABXA060233Door · missingNR 4 ENGINE RIGHT COWL DOOR BLOWOUT PANEL MISSING. REPLACED NR 4 ENGINE RIGHT COWL BLOWOUT PANEL AND DOOR FORWARD DOOR LATCH IAW DC8 MM 71-10 AND DC8 MM CHAPTER 20. OPS CHECKED GOOD.SDR ABXA060232Battery · dischargedA/C EMERGENCY BATTERY PAC WOULD NOT RECHARGE. REMOVED AND REPLACED EMERGENCY LIGHTING BATTERY AND RELAY UNIT. SYSTEM OPS CHECKED GOOD IAW MM 33-50-01.SDR ARWA20060705Hinge Fitting · crackedDURING SERVICE CHECK INSPECTION FOUND LEFT WING OUTBOARD FLAP HINGE BASE FITTING AT STATION 219 CRACKED; O/B FITTING. REMOVED LEFT OUTBOARD FLAP ASSEMBLY IAW M/M 27-51-2 FOR REPAIR. PERFORMED WING FLAP SYSTEM ADJUSTMENT AND TEST IN ACCORDANCE DC-8 M/M 27-50-SDR ABXA060201Ctc · defectiveNR 2 CTC SMOKED AND MADE LOUD NOISE, STA. MIA. REMOVED AND REPLACED NR 2 CTC IAW DC8 MM 21-10-01-4. OPS CHECKED GOOD.SDR ARWA20060704Hinge Fitting · crackedDURING DAILY CHECK INSPECTION THE FOLLOWING WAS FOUND; LT OUTBOARD WING FLAP STATION XW 219, LT HINGE BASE FITTING CRACK. REMOVED LEFT O/B WING FLAP ASSEMBLY IN ACCORDANCE WITH M/M 27-51-2. INSTALLED LT OUTBOARD WING FLAP ASSY IN ACCORDANCE WITH M/M 27-51-2.SDR ARWA20060701Skin · corrodedDURING C-CHECK INSPECTION, THE FOLLOWING WAS FOUND; LEFT ELEVATOR XE 195-313 T/E LOWER SKIN WITH CORROSION.SDR ARWA20060702Panel · corrodedDURING C-CHECK INSPECTION, THE FOLLOWING WAS FOUND; LT HORIZONTAL STABILIZER BETWEEN XE 312.500 AND XE 149.000 T/E UPPER PANELS WITH CORROSION.SDR ARWA20060703Skin · corrodedDURING C-CHECK INSPECTION, THE FOLLOWING WAS FOUND; FUSELAGE EXTERIOR STATION 25, L-33R SKIN WITH CORROSION.SDR ARWA20060602O-Ring · leakingPRIOR TO DESCENT, OBSERVED A LOSS OF HYDRAULIC QUANTITY TO THE STAND PIPE LEVEL FOLLOWED BY A LOSS OF PRESSURE. REMOVED AND REPLACED DAMAGE O-RING ON NR 2 ENGINE HYDRAULIC PUMP PRESSURE LINE FITTING IN ACCORDANCE WITH M/M 20-12-0 PAGE 211. OPERATIONAL CHECK SDR ARWA20060501Striker · unknownAFTER NORMAL GEAR RETRACTION, RED DOORS NOT LATCHED, LIGHT ILLUMINATED ON UP-LATCH CHECK; PERFORMED ABNORMAL CHECKLIST, LIGHT REMAINED ON. REMOVED AND REPLACED LT MAIN GEAR INBOUND DOOR LATCH STRIKER IN ACCORDANCE WITH M/M 32-31-4; ALSO REPLACED BOTH TARGET ASDR ABXA060222Spar · corrodedLEFT WING REAR SPAR AFT FACE HAD CORROSION AT WING ROOT XRS 5. ACCOMPLISHED REPAIR IAW REA D857-53586-MR, REV. IR AT LEFT WING REAR SPAR.SDR ABXA060221Skin · damagedRIGHT ELEVATOR LOWER SKIN AT XS 77.0, HAD "OIL CAN" CONDITION AT HINGE NR 2 SMALL ACCESS HOLE. ACCOMPLISHED REPAIR IAW REA D855-53583-MR, REV. IR AT RIGHT ELEVATOR.SDR ABXA060220Skin · damagedUPPER CARGO MAIN CARGO DOOR FUSELAGE CUT OUT PLATING DAMAGE, SEVERAL AREAS MISSING STA. 160 - 180, LONGERON 6 LEFT. ACCOMPLISHED REPAIR AT DOOR CUT OUT IAW REA D853-53588-MR, REV. IR.SDR ABXA060219Skin · corrodedLEFT INBOARD HORIZONTAL STABILIZER LEADING EDGE SECTION OUTBOARD UPPER SURFACE AT XSTA 177, HAD INTERGRANULAR CORROSION AT SCREW HOLE AREA. INSTALLED REPAIR AT LEFT INBOARD STABILIZER LEADING EDGE SECTION OUTBOARD UPPER SURFACE IAW REA D855-53575-MR, REV. B.SDR ABXA060160Wire · crushedNR 4 CTC CAUSED VERY LOUD HOWL, VIBRATION AND SMOKE ODOR IN COCKPIT. FOUND NR 4 CTC WIRING METAL OVERBRAID CRUSHED 1/2" FROM UPPER CONNECTOR. REPAIRED WIRING IAW REA D821-53653 AS REQUIRED. SYSTEM OPS CHECKED GOOD.SDR ARWA20060401Wire · brokenDURING TAKEOFF ROLL, WARNING HORN SOUNDED. REPAIRED BROKEN WIRE AT SPOILER SWITCH IN ACCORDANCE WITH DC-8 M/M 20-50-0. OPERATIONAL CHECK TAKEOFF WARNING SYSTEM NORMAL IN ACCORDANCE WITH DC-8 M/M 27-63-0.SDR ABXA060161Engine · fodIMMEDIATELY AFTER TAKEOFF FROM ILN, NR 3 FIRE WARNING LIGHT AND BELL CAME ON. AFTER APPROXIMATELY 5 SECONDS, THEN LIGHT WENT OUT. FIRE WARNING TESTED GOOD. SECURED NR 3 ENGINE AND LANDED. POSITIVE OIL PRESSURE INDICATED. FOUND CHARRED BIRD NEST NEXT TO AFSDR ABXA060159Pump · leakingLOSS OF HYDRAULIC QUANTITY NOTED DURING DESCENT. FOUND STANDBY RUDDER PUMP OVERBOARD DRAIN LEAKING. REMOVED AND REPLACED STANDBY RUDDER PUMP IAW D8C MM 27-24-02. ALSO, CHECKED BYPASS LINE CHECK VALVE OPERATION. OPERATED NORMALLY. REINSTALLED CHECK VALVE. SDR ABXA060217Skin · crackedCRACK IN RIGHT WING LEADING EDGE PANEL ASSEMBLY INNER (WAFFLED) SKIN 8" FROM INBOARD EDGE, STA. XFS 304. STOP DRILLED CRACK AND INSTALLED REPAIR IAW REA D857-53580, REV. IR.SDR ABXA060218Skin · crackedRIGHT WING LEADING EDGE PANEL ASSEMBLY INNER (WAFFLED) SKIN HAD 3 EACH CRACKS AT APPROX. XFS 410 - 423. REPAIRED CRACKS IAW REA D857-53581, REV. IR.SDR ABXA060195Skin · crackedRIGHT WING LEADING EDGE PANEL ASSEMBLY INNER (WAFFLED) SKIN HAD 3 EACH CRACKS AT XFS 410 - 423. REPAIRED CRACKS IAW REA D857-53581, REV IR.SDR ABXA060194Skin · crackedCRACK IN RIGHT WING LEADING EDGE PANEL ASSEMBLY INNER (WAFFLED) SKIN 8 INCHES FROM INBOARD EDGE STA XFS 304. STOP DRILLED CRACK AND INSTALLED REPAIR IAW REA D857-53580, REV IR.SDR ABXA060157Rotary Switch · faultyAFTER TAKEOFF AND GEAR RETRACTED (FROM ILN TO MEM) THE RED GEAR UNSAFE LIGHT REMAINED ILLUMINATED ALONG WITH THE AMBER RIGHT DOOR LIGHT ON F/E'S PANEL. RECYCLED GEAR WITH NO EFFECT. PERFORMED AN UPLATCH CHECK AND ALL LIGHTS EXTINGUISHED WITH A NORMAL UPLATCHSDR ABXA060216Longeron · corrodedEXFOLIATION CORROSION IN LONGERON 27 LEFT, STA. 1220 - 1240. ACCOMPLISHED REPAIR IAW REA D853-53585-MR, REV. IR, ON LONGERON 27 LEFT, STA. 1220 - 1240.SDR ABXA060215Skin · corrodedLEFT HORIZONTAL STABILIZER OUTBOARD LEADING EDGE UPPER STRUCTURE HAD INTERGRANULAR CORROSION ON AFT TRAILING EDGE FROM XFS 178 - 341. ACCOMPLISHED REPAIR OF LEFT HORIZONTAL STABILIZER LEADING EDGE IAW REA D855-53574-MR, REV. A.SDR ABXA060213Panel · corrodedRIGHT HORIZONATL STABILIZER LEADING EDGE OUTBOARD SECTION UPPER TRAILING EDGE INTERGRANULAR CORROSION AT 3 LOCATIONS: XFS260, 316 & 332. CUT OUT DAMAGED AREA AND INSTALLED REPAIR IAW REA D855-53089-MR, REV. B.SDR ABXA060214Skin · crackedTHREE CRACKS ALONG THE UPPER EDGE OF CUT OUT, IN THE INNER SKIN OF THE AFT CARGO DOOR. TRIMMED OUT CRACKS IAW REA D852-53568.
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