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 ABXA060211Skin · corrodedRIGHT HORIZONTAL STABILIZER INBOARD LEADING EDGE SECTION AT UPPER TRAILING EDGE MID AREA AT XSTA 140, HAD INTERGRANULAR CORROSION AROUND SCREW HOLES. INSTALLED REPAIR IAW REA D855-53086-MR, REV. A, ON RIGHT HORIZONTAL STABILIZER INBOARD LEADING EDGE SECTION ATSDR ABXA060212Panel · corrodedRIGHT HORIZONTAL STABILIZER OUTBOARD LEADING EDGE SECTION AT INBOARD UPPER LEADING EDGE HAD INTERGRANULAR CORROSION AT HILOC HOLE. INSTALLED REPAIR IAW REA D855-53090-MR, REV. IR AT RIGHT STABILIZER LEADING EDGE AT XSTA 178.75.SDR ABXA060192Skin · corrodedRIGHT HORIZONTAL STABILIZER LEADING EDGE OUTBOARD SECTION UPPER TRAILING EDGE HAD INTERGRANULAR CORROSION AT 3 LOCATIONS: XFS 260, 316 AND 332. CUT OUT DAMAGED AREA AND INSTALLED REPAIR IAW REA D855-53089-MR, REV B.SDR ABXA060193Skin · crackedTHREE CRACKS ALONG THE UPPER EDGE OF CUTOUT, IN THE INNER SKIN OF THE AFT CARGO DOOR. TRIMMED OUT CRACKED IAW REA D852-53568.SDR ABXA060191Skin · corrodedRIGHT HORIZONTAL STABILIZER LEADING EDGE OUTBOARD UPPER SKIN HAD INTERGRANULAR CORROSION AT XFS 178.750. CUT OUT DAMAGED AREA AND INSTALLED REPAIR IAW REA D855-53088-MR, REV A.SDR ARWA20060304Engine · leakingDURING CRUISE, NR 2 ENGINE LOSS OF ALL OIL QUANTITY AND PRESSURE; PRECAUTIONARY ENGINE SHUTDOWN AS PER CHECKLIST (TIME 0655). REMOVED AND REPLACED NR 2 ENGINE IN ACCORDANCE WITH ARROW AIR TASK CARD NR DC8-N-003. LEAK CHECKED, NO LEAKS NOTED; OPERATIONAL CHECKSDR ABXA060207Skin Panel · corrodedPERMANENT REPAIR OF CORROSION ON LONGERON L36 (KEEL BEAM) PER COI 50571 AND SKIN PANELS AT STA. 670 AND 683 PER COI 50570 AND COI 50572. REPAIR ACCOMPLISHED IAW REA D853-53093 - MR, REV. A, ON KEEL BEAM AND SKIN PANELS AT STA. 665 - 700.SDR ABXA060208Longeron · damagedREMOVE AND REPLACE EXISTING DISCREPANT LONGERON 24 RIGHT IN RIGHT WHEEL WELL, STA. 857 - 980, DUE TO PREVIOUS DAMAGE WITH AN INTERIM REPAIR IAW REA D853-52752-MR. REMOVED AND REPLACED LONGERON 24 RIGHT IN RIGHT WHEEL WELL IAW REA D853-53079-MR, REV. A.SDR ABXA060209Skin · corrodedLEFT WING LEADING EDGE UPPER AFT EDGE OF OUTER MOST LEADING EDGE ASSEMBLY AT XFS 291 - 422 LEFT, HAD EXFOLIATION AROUND SCREWS. ACCOMPLISHED REPAIR IAW REA D857-53573-MR, REV. A, AT LEFT WING OUTER MOST LEADING EDGE ASSEMBLY.SDR ABXA060206Longeron · corrodedFORWARD CARGO COMPARTMENT LNOGERON 31 LEFT HAD CORROSION AT STA. 520. ACCOMPLISHED REPAIR IAW REA D853-53595-MR, REV. IR, ON LONGERON 31 LEFT.SDR ABXA060205Longeron · corrodedCORROSION AT LONGERON 31 LEFT, F.S. 560 - 600. ACCOMPLISHED REPAIR OF LONGERON 31 LEFT, F.S. 560 - 600 IAW REA D853-53592-MR, REV. IR.SDR ABXA060210Skin · corrodedRIGHT HORIZONTAL STABILIZER LEADING EDGE OUTBOARD UPPER SKIN HAD INTERGRANULAR CORROSION AT XFS 178.750. CUT OUT DAMAGED AREA AND INSTALLED REPAIR IAW REA D855-53088-MR, REV. A.SDR ARWA20060303Pin · unknownFIRST OFFICER'S COURSE DEVIATION INDICATOR (CDI) DOES NOT CORRESPOND TO OMNI BEARING SELECTOR (OBS) IN FLIGHT. FIRST OFFICER'S HEADING "BUG" DOES NOT CORRESPOND TO SELECTED HEADING. REMOVED AND REPLACED PIN NR 1 AT PTO-117 IN ACCORDANCE WITH M/M 20-50-1 AND SDR ABXA060204Longeron · corrodedSEVERAL AREAS OF CORROSION ON LONGERON 24 LEFT, F.S. 857 - 980 IN LEFT WHEEL WELL. REPLACED LONGERON 24 LEFT, F.S. 857 - 980 IN LEFT WHEEL WELL IAW REA D853-53080-MR, REV.A.SDR ARWA20060302Proximity Switch · malfunctioned"GEAR NOT LATCHED" LIGHT ILLUMINATED AFTER GEAR UPLATCH CHECK; CONTINUED OPERATION AS PER ABNORMAL CHECKLIST. PERFORMED PROXIMITY SWITCHES TEST IN ACCORDANCE WITH M/M 32-60-0. REMOVED AND REPLACED CONTROL BOX PROXIMITY SWITCHES SYSTEM OPERATIONAL CHECK NORMASDR ABXA060172Fitting · corrodedLEFT WHEEL WELL AT STA 902 AND HORIZONTAL PRESSURE PANEL ABOVE LONGERON 24 LEFT, SMALL ATTACH FITTING HAD EXFOLIATING CORROSION. REMOVED AND REPLACED SMALL ATTACH FITTING AT LEFT WHEEL WELL, STA 902 AND HORIZONTAL PRESSURE PANEL ABOVE LONGERON 24 LEFT IAW DC8SDR ABXA060203Skin · corrodedRIGHT FUSELAGE SKIN HAD BULGE AND RIVETS POPPED OFF AT STA. 1600, LONGERON 27 RIGHT. EXISTING REPAIR REMOVED AND SKIN AND INNER DOUBLER CUT TO REMOVE ALL CORROSION. COMPLETED REPAIR IAW REA D853-53635-MR.SDR ABXA060190Skin · corrodedRIGHT FUSELAGE SKIN HAD BULGE AND RIVETS POPPED OFF AT STA 1600, LONGERON 27 RIGHT. EXISTING REPAIR REMOVED, AND SKIN AND INNER DOUBLER CUT TO REMOVE ALL CORROSION. COMPLETED REPAIR IAW REA D853-53635-MR.SDR ABXA060171Fitting · crackedRIGHT WHEEL WELL, FORWARD PRESSURE PANEL AT STA 857, RIGHT UPPER CORNER HAD CRACKED FITTING. REMOVED AND REPLACED CRACKED FITTING AT RIGHT WHEEL WELL AT STA 857 RIGHT SIDE IAW DC8 SRM 51-3-0.SDR ABXA060132Warning Light · illuminatedAFTER TAKEOFF WHEN GEAR WAS RETRACTED, RED UNSAFE LIGHT STAYED ON, LEFT MAIN GEAR DOOR LIGHT WAS ON. CYCLED GEAR, OPS CHECKED NORMAL. REMOVED AND REPLACED LEFT MAIN LANDING GEAR DOOR UPLATCH AND INDICATION IAW DC8 MM 32-60-00 AND ALSO CHECKED MIN ROLLER CLEASDR ABXA060170Rib · brokenRIGHT WING LEADING EDGE, OUTBOARD CLOSURE RIB, FORWARD EDGE OF THE HORIZONTAL FLANGE AT WING STA XS 526, BROKEN OFF. ACCOMPLISHED BLEND OUT REPAIR AT RIGHT WING LEADING EDGE CLOSURE RIB IAW REA D857-53072.SDR ABXA060167Latch · crackedAFT CARGO COMPARTMENT, FORWARD DOOR, LOWER CUT OUT LOCKING LATCH, NR 1 FROM FORWARD END APPEARED CRACKED AT ATTACH UPPER FORWARD CORNER. REMOVED AND REPLACED FITTING LATCH NR 1 AT AFT CARGO COMPARTMENT FORWARD DOOR LOWER CUT OUT IAW DC8 SRM 51-1-20D.SDR ABXA060169Angle · corrodedRIGHT WHEEL WELL FORWARD BULKHEAD SHELF ANGLE CORRODED. LOCATED 14" INBOARD OF LONGERON 24 RIGHT. REMOVED AND REPLACED CORRODED ANGLE INBOARD OF LONGERON 24 RIGHT AT RIGHT WHEEL WELL FORWARD BULKHEAD.SDR ABXA060168Strap · crackedAFT CARGO COMPARTMENT FORWARD BULKHEAD REINFORCEMENT STRAP AT STATION 980 AND JUST ABOVE LONGERON 33 LEFT, CRACKED. STOP DRILLED CRACK AND INSTALLED REPAIR ANGLE AT REINFORCEMENT STRAP AT STA 980, JUST ABOVE LONGERON 33 LEFT IN AFT CARGO COMPARTMENT, FORWARD SDR ABXA060163Finger Doubler · corrodedAFT CARGO COMPARTMENT, CORROSION AT FINGER DOUBLER, LONGERON 31 LEFT, STA 1495 - 1510. CUT OUT DAMAGED FINGER DOUBLER, FABRICATED AND INSTALLED FINGER DOUBLER SECTION IAW REA D853-53073.SDR ABXA060165Repair · crackedRIGHT WING LEADING EDGE EXTERIOR TOP SURFACE REPAIR DOUBLER WAS CRACKED JUST INBOARD AND AFT OF OUTBOARD SLOT. REMOVED AND REPLACED DAMAGED EXISTING REPAIR DOUBLER FORM UPPER SKIN TRAILING EDGE SECTION IAW DC8 SRM 57-2-1.SDR ABXA060164Rib · crackedRIGHT WING LEADING EDGE, RIB AND ANGLE CRACKED AT STA 520. STOP DRILLED CRACKS IN RIB, FABRICATED L-STRAP REPAIR, FABRICATED NEW ANGLE, REMOVED OLD ANGLE AND INSTALLED L-STRAP REPAIR AND NEW ANGLE IAW REA D857-53074-MR AND DC8 SRM 57-2-0, (3 CRACKS - RIB FWD SDR ABXA060166Support Bracket · corrodedRIGHT WING ROOT TOP FAIRING SUPPORT BRACKET WAS WORN AND WITH CORROSION AT REAR SPAR, TOP SURFACE. REPLACED FAIRING SUPPORT BRACKET IAW DC8 SRM 51-1-2 AT RIGHT WING ROOT TOP FAIRING.SDR ABXA060126Pin · corrodedFORWARD TRUNNION MAIN LANDING GEAR PIN CORRODED BEYOND LIMITS (LEFT). LEFT MAIN GEAR FORWARD TRUNNION PIN REMOVED AND REPLACED IAW DC8 MM 32-11-01-4.SDR ABXA060125Pin · shearedLEFT MAIN LANDING GEAR ACTUATOR LOWER ATTACH POINT PIN SHEARED DURING RETRACTION. REMOVED AND REPLACED LEFT MAIN LANDING GEAR ACTUATOR LOWER PIN AS PER AAR FORM 0909-02, REV 3. OPS CHECKED GOOD IAW DC8 AMM 32-32-0.SDR ARWA20060203Connector · dirtyBLOCK TURNBACK PRIOR TO TAKEOFF DUE TO HYDRAULIC QUANTITY LOSS. CHECKED HYDRAULIC RESERVOIR, FOUND FULL; CLEANED CONNECTOR AT HYDRAULIC QUANTITY TRANSMITTER IN ACCORDANCE WITH M/M 20-50-1; CHECKED HYDRAULIC QUANTITY, FOUND NORMAL READING.SDR ABXA060081Fuel Control · defectiveNR 3 ENGINE FAILED TO ACCELERATE IN-FLIGHT. EET 20 DEGREES N2 48%, FF AT 1000 LBS. ATTEMPTED RE-LIGHT TO NO AVAIL. SHUT DOWN NR 3 ENGINE AT 0518Z, 4 PSI INDICATED ON OIL PRESSURE. REMOVED AND REPLACED FUEL CONTROL UNIT ON NR 3 ENGINE AND TRIMMED NR 3 ENGINSDR ABXA060127Pin · corrodedAFT TRUNNION MAIN LANDING GEAR PIN HAD PITTING THROUGH OUT PIN. LEFT MAIN GEAR AFT TRUNNION PIN REMOVED AND REPLACED IAW DC8 MM 32-11-01-4.SDR U2RA1013Frame · corrodedDURING COCKPIT AREA CORROSION INSPECTION PER AD92-22-07 (CPCP 5), LEVEL 2 CORROSION WAS FOUND ON RT FRAME AT FS -67, L23R AND ADJACENT AREA. AFFECTED AREA IS IN PROCESS OF BEING REPAIRED.SDR U2RA1013865Frame · corrodedDURING COCKPIT AREA CORROSION INSPECTION PER AD92-22-07 (CPCP 5), LEVEL 2 CORROSION WAS FOUND ON RT FRAME AT FS -67, L23R AND ADJACENT AREA. AFFECTED AREA IS IN PROCESS OF BEING REPAIRED.SDR ARWA20060202Engine · vibrationSHUT-DOWN NR 3 ENGINE IN FLIGHT DUE TO VIBRATION. COMPLIED WITH ALL CHECKLIST. C/W RED BORDER NR 019421 NR 3 ENGINE P-679000 REPLACEMENT. COMPLY WITH RED BORDER NR 019421; REMOVED AND REPLACED NR 3 ENGINE IN ACCORDANCE WITH MAINTENANCE MANUAL 71-00-00. OPESDR ARWA20060218Skin · corrodedDURING "C" CHECK INSPECTION, THE FOLLOWING WAS FOUND; AFT ACCESSORY COMPARTMENT INTERIOR STA 1620-STA 1640 BETWEEN L-32L & L-33L SKIN WITH CORROSION; N/R 1022- AFT ACCESSORY COMPARTMENT INTERIOR STA 1620 BETWEEN L-30L & L-31L SKIN WITH CORROSION. REPAIR INNERSDR ARWA20060207Skin · corrodedDURING "C" CHECK INSPECTION, THE FOLLOWING WAS FOUND; LOWER FUSELAGE STA 1690 THRU STA 1720, L-31L THRU L-31R SKIN PANEL WITH CORROSION AT SEVERAL PLACES. REPAIRED FUSELAGE TAIL SECTION PLATING BETWEEN FS 1690 TO FS 1720 AND L-28R TO L-34 IN ACCORDANCE WITH DSDR ARWA20060217Skin · corrodedDURING "C" CHECK INSPECTION, THE FOLLOWING WAS FOUND; I/B AILERON BETWEEN XA 565 AND SA 542 LOWER SKIN WITH CORROSION. REMOVED SKIN AND BONDED DOUBLER AND REPLACED BY SOLID SKIN BETWEEN XA 542 AND XW 563 IN ACCORDANCE WITH DRAWING NR AIPSAC-N784AL-07/05. ISSSDR ARWA20060216Skin · corrodedDURING "C" CHECK INSPECTION, RT ELEVATOR XE 276 THRU XE 280 LOWER SURFACE WITH CORROSION. REMOVED RT ELEVATOR SKIN UPPER SURFACE XAE 0 TO XE 103 AND XE 273 TO XH 285 AND REPLACED WITH SOLID SKIN IN ACCORDANCE WITH DRAWING NR AIPSAC-N784AL-05-05. ISSUED FAA FSDR ARWA20060215Skin · delaminatedDURING "C" CHECK INSPECTION, RT ELEVATOR XE 28.843 LOWER SURFACE WITH DELAMINATION. REMOVED RT ELEVATOR SKIN UPPER SURFACE BETWEEN XAE 0 TO SE 103 AND XE 273 TO XE 285 AND REPLACED WITH SOLID SKIN IN ACCORDANCE WITH DRAWING AIPSAC-N784AL-05/05. ISSUED FAA FOSDR ARWA20060214Finger Doubler · corrodedDURING "C" CHECK INSPECTION, MAIN CARGO COMPARTMENT STA.920, STA.940, STA.960, XCW 0 - XCW 23 CENTER WING SECCTION RT FINGER DOUBLER WITH CORROSION. REPAIRED FUSELAGE CENTER SECTION PRESSURE PANEL BETWEEN STA 920 AND FS 940 IN ACCORDANCE WITH DRAWING AIPSAC-SDR ARWA20060213Skin · corrodedDURING "C" CHECK INSPECTION, FUSELAGE EXTERIOR BETWEEN STA 1690 & STA 1734 AND L-26L THRU L-28L SKIN WITH CORROSION. REPAIRED FUSELAGE TAIL SECTION PLATING BETWEEN FS 1696 TO FS 1766 AND L-24L TO L-28L IN ACCORDANCE WITH DRAWING NR AIPSAC-N784AL-03/05, SHEETSSDR ARWA20060212Skin · damagedDURING "C" CHECK INSPECTION, LT O/B AILERON BETWEEN XA 678 AND XA 685 LOWER SKIN RIVETS SHEARED. REMOVED LT O/B AILERON PLATING BETWEEN XA 662 & XA 724 AND REPLACED WITH SOLID SKIN IN ACCORDANCE WITH DRAWING NR AIPSAC-N784AL-09/05, ISSUED FAA FORM 8110-3 APPRSDR ARWA20060210Structure · crackedDURING "C" CHECK INSPECTION THE FOLLOWING WAS FOUND; NR 3 PYLON FOOT STOOL I/B SIDE WITH 1 - 3/4" CRACK. REMOVED AND REPLACED NR 3 PYLON FOOT STOOL FITTING IN ACCORDANCE WITH DC8 S/B AS7-99 REVISION 1 DATED 09/03/93 AND DC8 S/B AS7-87, REVISION NR 2, DATED 01SDR ARWA20060209Skin · corrodedDURING "C" CHECK INSPECTION THE FOLLOWING WAS FOUND; AFT ACCESSORY COMPT INTERIOR STA 1620 BETWEEN L-30L AND L-31L SKIN WITH CORROSION. REPAIRED INNER DOUBLER BETWEEN FS 1620 AND FS 1680 AND L-26L AND L31L IN ACCORDANCE WITH DRAWING NR AIPSAC-N784AL-06/05, ISSDR ARWA20060206Skin · corrodedDURING "C" CHECK INSPECTION, THE FOLLOWING WAS FOUND; LOWER FUSELAGE STATION 1490 THROUGH STATION 1690L, L-31L THRU L31R SKIN PANEL WITH CORROSION AT SEVERAL PLACES. REMOVED AND REPLACED SKIN FROM FUSELAGE STA 1490 TO FS STA 1690 IN ACCORDANCE WITH AIPSAR EA SDR ABXA060124Splice · crackedRIGHT SIDE CABIN STA. 680, LONGERON 11 RIGHT, AFT UPPER SPLICE FITTING HAD A CRACK. REMOVED AND REPLACED SPLICE FITTING AT RIGHT SIDE MAIN CABIN, STA 680, LONGERON 11 RIGHT AFT IAW DC8 SRM 51-1-20 AND 51-3-0.SDR ABXA060123Fitting · crackedLEFT CENTER WING FLOOR AREA AT FS 759, LEFT BUTT LINE 48, SUPPORT FITTING HAD CORROSION AT BASE ATTACH NUTS. CLEANED AREA IAW DC8 MM 12-06-00, FITTING FOUND CRACKED. REMOVED AND REPLACED WITH NEW FITTING IAW DC8 SRM 51-1-20D.SDR ABXA060121Fitting · corrodedAFT CARGO COMPARTMENT AREA BELOW C-3 DOOR HAD CORROSION ON FITTING APPROXIMATELY FS 1195, RIGHT BUTT LINE 19. REMOVED AND REPLACED FITTING AT C-3 DOOR AREA FS 1195, RIGHT BUTT LINE 19 IAW DC8 SRM 51-1-20D AND 53-2-0.
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