Douglas DC-8-73F
Service difficulty reports · 15,471
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 = 'DC873F' 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 = 'DC873F' 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 UPS04843492Window · inoperativeCAPTAIN SLIDING WINDOW WILL NOT OPEN. LUBED UPPER CATCH ON SLIDING WINDOW. OP CHECKS GOOD. WINDOW OPENS EASILY.SDR IXXA0500088SVane · damagedDURING A ROUTINE C-CHECK INSPECTION, FOUND LEADING WING EXTENDED LEADING EDGE OUTBOARD VANE FORWARD OUTER PLATING INTERIM REPAIR AROUND STATION XOLDO 67.000. MAJOR REPAIR ACCOMPLISHED. REMOVED INTERIM REPAIR, REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION ASDR IXXA0500085SDoubler · damagedDURING A ROUTINE C CHECK INSPECTION, FOUND RT WING OUTBOARD L/E INTERIM REPAIR AT STA XFS 710.000. ACCOMPLISHED MAJOR REPAIR BY REMOVING EXISTING REPAIR AND THE DAMAGED AREA. PERFORMED NDT INSPECTION. FABRICATED EXTERNAL DOULBER AND FILLER IN ACCORDANCE WITHSDR DHL2004873511Bracket · crackedNR 1 ALT TANK AFT BOOSTER PUMP BRACKET CRACKED. REMOVED AND REPLACED BRACKET ON NR 1 ALT TANK AFT BOOSTER PUMP IAW SRM 51-1-20D PG 9-21.SDR DHL2004801013Uplock Switch · dirtyAFTER TAKEOFF, RIGHT DOOR UNSAFE LIGHT ILLUMINATED PERFORMED ABNORMAL PROCEDURE LIGHT EXTINGUISHED BUT NOISE CAME FROM UNDERSIDE OF A/C. CLEANED UPLATCH SWITCHES AND ADJUSTED MAIN GEAR DOOR UPLATCH MECH IAW 32-31-3. PERFORMED MAIN GEAR DOOR UPLATCH TEST, OPSSDR IXXA0500110SSkin Panel · corrodedDURING A ROUTINE C CHECK INSPECTION, FOUND RT INNER WING EXTENDED LEADING EDGE SLANT PANEL UPPER CAP CORROSION DAMAGE BETWEEN STA XFS 63.500 AND XFS 107.500. MAJOR REPAIR ACCOMPLISHED BLEND OUT ON CORRODED AREA REMAINING OUT OF LIMITS IAW DC8 SRM 57-2-1 FIG 3SDR IXXA0500100SFloorbeam · corrodedDURING A ROUTINE C CHECK INSPECTION, FOUND FOWARD CARGO COMPARTMENT FLOORBEAM CORRODED AT STA 560.000 RBL 60. MAJOR REPAIR ACCOMPLISHED BLEND OUT OF DAMAGED AREA. FOUND OUT OF LIMITS IAW DC8 SRM 53.2.0 FIG 1F. FABRICATED REPAIR ANGLE IAW EC8 SRM 53-2-0 FIG 1SDR DHL2004873531Stiffener · corrodedAFT CARGO COMPT STIFFENER CORRODED AT FS 980.000, L-27R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 51-2-1 FIG 1, TR 51-130, SRM 53-4-1 FIG 51 PG 183-184. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG 2P. FABRICATED CHSDR DHL2004873506Doubler · crackedRUDDER ACCESS DOOR NR 61A DOUBLER CRACKED 0.500. REMOVED CRACKED DOUBLER IAW DC8 SRM 51-1-21 PG 1. FABRICATED NEW DOUBLER (AL2024-T3 0.032) IAW DC8 SRM 55-2-0 PG 1. CLEANED, TREATED AND PRIMED AREA AND DOUBLER IAW DC8 SRM 51-1-8B. INSTALLED NEW DOUBLER IAWSDR UPS04843472Window · stuckINSPECTION TYPE:N/A CAPT'S L2 WINDOW WILL NOT OPEN. UPPER WINDOW FRAME LOCK BAR STUCK WOULD NOT RELEASE. CLEANED & LUBRICATED MECHANISM. OPS CHECK NORMAL IAW MM 56-10-03-5.SDR DHL2004806005Downlock Switch · faultyLEFT GEAR EXTENDED LIGHT WAS SLOW TO ILLUMINATE. WARNING HORN DID NOT SOUND WITH FLAPS 35 DEGREES SELECTED. REMOVED AND REPLACED LEFT MAIN GEAR DOWNLOCK SWITCH & PERFORMED GEAR SWING IAW DC-8 M/M 32-60-0, OPS CHECKS SERVICEABLE P/N H14-1003.SDR UPS04843449Slide · inoperativeINSPECTION TYPE:N/A, DEPARTURE - ESCAPE SLIDE GIRT BAR WOULD NOT ATTACH TO THE FLOOR MOUNTS. DEFERRED PER MEL M290986. REMOVED AND REPLACED CONTAINER FOR EVAC SLIDE, OPS CKS GOOD. M290986 CLOSED.SDR IXXA0500087SHinge · crackedDURING A ROUTINE C-CHECK INSPECTION FOUND LT OB FLAP HINGE CRACKED AT STATION XC 337.000. MAJOR REPAIR ACCOMPLISHED. REMOVED CRACKED SUPPORT FITTING IAW SRM 51-1-21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW SUPPORT FITTING IAW SRM 51-1-SDR DHL2004873513Structure · crackedRUDDER RIGHT L/E CRACKED 3.000M ZR 172.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 55-1-0 PG 1, SRM 55-6-1 FIG 1. REMOVED CRACKED PLATING IAW SRM 51-1-21 PG 1. FABRICATED NEW PLATING (ALCLAD 2024-T3 0.040) IAW SRM 55-6-1 PG 2 FIG 1. CLEANED, TREATEDSDR DHL2004873514Skin · corrodedRUDDER LT SIDE SKIN CORRODED BETWEEN ZR 253.000 AND ZR 271.000 NEXT FRONT SPAR (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW BOEING MESSAGE NR 1-RROU7 FAA FORM 8110-3 DATED 10-26-04. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 55-2-0SDR IXXA0400119OEngine · malfunctionedDURING TAKEOFF, NR 4 ENGINE OIL PRESSURE FLUXING 45-35PSI WITH OIL QUANTITY DROPPING SHUT DOWN ENGINE WINDMILLING OIL PRESSURE OPSI AT 1302 (LANDING WEIGHT 270.0) AN INSPECTION IS ON GOING. AS SOON AS INFORMATION BECOME AVAILABLE IT WILL BE PROVIDED.SDR DHL2004873517Fitting · crackedMAIN CARGO COMPT FITTING ATTACHING BEAM TO PRESSURE BULKHEAD CRACKED 0.500, STA 980.000 BL 0 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1. REMOVED CRACKED FITTING IAW SRM 51-1-21 PG 1-2, SRM 51-1-20D PG 21. CLEANED, TREATED AND PRIMED AREA IAWSDR DHL2004873508Fitting · crackedAFT CARGO COMPT SPLICE FITTING CRACKED 1.000, STA 1050.000 L-31L (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW DC8 SRM 53-1-0 PG 1. REMOVED CRACKED SPLICE FITTING IAW DC8 SRM 51-1-20D PG 1. CLEANED, TREATED AND PRIMED AREA IAW DC8 SRM 51-1-8B. INSTALLED NEW SSDR DHL2004804005Bulb · inoperativeNR 8 SMOKE DETECTER INOP. DEF PER MEL 26-6-1 PLACARD INSTALLED DMI NR 18370. REFER TO DMI 18370. NR 8 POSITITON SMOKE DETECTOR WILL NOT TEST. RELAMPED NR 8 SMOKE DETECTOR AND OPS CHECKED GOOD AS PER MM 26-10-5. THIS CLEARS DMI 18370. (BULB P/N 327).SDR DHL2004806004Life Vest · missingAFT COURIER SEAT AT CABIN ENTRY AREA MISSING LIFE PRESERVER. INSTALLED SERVICABLE VEST IN AFT COURIER SEAT IAW M/M 25-60-0 DATE CHECKED 10/4 RE-CHECK DUE 10/6.SDR DHL2004806003Life Vest · missingFWD COURIER SEAT AT CABIN ENTRY AREA MISSING LIFE PRESERVER. INSTALLED SERVICEABLE VEST IN FWD COURIER IN SEAT IAW M/M 25-60-0 DATE CHECKED 6/4 RE-CHECK DUE 6/9.SDR DHL2004801012Fire Loop · malfunctionedENG NR 2 FIRE LOOP B SHORT CIRCUIT LIGHT ILLUMINATED ON TAXI OUT. DEFERRED NR 2 ENG "B" FIRE LOOP PER MEL 26-2-3 CAT C DMI 18369 PLACARD INSTALLED.SDR DHL2004873502Fitting · crackedAFT CARGO COMPT SPLICE FITTING CRACKED 0.250, FS 1345.00, L-34R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1. REMOVED CRACKED SPLICE FITTING IAW SRM 51-1-20D PG 21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW SPLICE FITTINSDR DHL2004873501Bracket · crackedNR 1 ALT TANK FWD BOOSTER PUMP BRACKET CRACKED. REMOVED AND REPLACED BRACKET ON NR 1 ALT TANK FWD BOOSTER PUMP IAW SRM 51-1-20D PG 9-21.SDR DHL2004873503Fitting · crackedAFT CARGO COMPT SPLICE FITTING CRACKED 0.250, FS 1345.000, L-35R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1. REMOVED CRACKED SPLICE FITTING IAW SRM 51-1-20D PG 21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW SPLICE FITTISDR DHL2004873515Skin · crackedRT RUDDER SKIN CRACKED 0.250, STA ZR 161.000 (HOIST POINT) MAJOR REPAIR. PERFORMED MAJOR REPAIR IAW BOEING MSG 1-RJ0SG AND BOEING MSG 1-RL7IU. REMOVED CRACKED SKIN IAW BOEING MSG 1-RJ0SG AND BOEING MSG 1-RL7IU, SRM 51-1-21 PG 1. FABRICATED NEW SKIN (2024-T3SDR DHL2004873516Skin · crackedLEFT OUTBOARD SLOT DOOR SKIN CRACKED 0.500, STA XS 478.897 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG 1, SRM 57-3-3 FIG 21. REMOVED LEFT OUTBOARD SLOT DOOR SKIN IAW SRM 51-1-21 PG 1. FABRICATED NEW SKIN (AL2024-T6 0.050) IAW SRM 57-3-3 FIG 21.SDR DHL2004873510Fitting · crackedAFT CARGO COMPT AFT SPLICE FITTING CRACKED 0.500 (STA 1690.000 - 1700.000, L-28R) MAJOR REPAIR. PERFORMED MAJOR REPAIR IAW DC8 SRM 53-1-0 PG 1. REMOVED CRACKED AFT SPLICE FITTING IAW DC8 SRM 51-1-20D PG 21. CLEANED, TREATED AND PRIMED AREA IAW DC8 SRM 51-1-SDR DHL2004873509Fitting · crackedAFT CARGO COMPT AFT SPLICE FITTING CRACKED 0.500 (STA 1690.000 - 1700.000, L-32R) MAJOR REPAIR. PERFORMED MAJOR REPAIR IAW DC8 SRM 53-1-0 PG 1. REMOVED CRACKED AFT SPLICE FITTING IAW DC8 SRM 51-1-20D PG 21. CLEANED, TREATED AND PRIMED AREA IAW DC8 SRM 51-1-SDR DHL2004873507Fitting · crackedAFT CARGO COMPT AFT SPLICE FITTING CRACKED 0.500 (STA 1690.000-1700.000, L-28L) MAJOR REPAIR. PERFORMED MAJOR REPAIR IAW DC8 SRM 53-1-0 PG 1. REMOVED CRACKED SPLICE FITTING IAW DC8 SRM 51-1-20D PG 21. CLEANED, TREATED AND PRIMED AREA IAW DC8 SRM 51-1-8B. ISDR DHL2004873504Bracket · crackedNR 4 ALT TANK AFT BOOSTER PUMP BRACKET CRACKED. REMOVED AND REPLACED CRACKED BRACKET ON NR 4 ALT TANK AFT BOOSTER PUMP IAW SRM 51-1-20D PG 9-21.SDR UPS04843436Window · brokenCAPTAIN'S SLIDING WINDOW OPENING MECH BROKEN. REPLACED CAPT'S CLEARVIEW WINDOW PER MM 56-10-03-4.SDR DHL2004873505Rib · crackedLT OUTER OUTBOARD WING L/E FORMER CRACKED 0.500 AT XFS 885.000. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. PERFORMED STOP DRILL ON CRACK END IAW SRM 57-2-0 PG 8. FABRICATED ANGLE DOUBLER (ALCLAD 2024-T3 0.032) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMSDR DHL2004809009Mechanism · lack of lubeCABIN ENTRY DOOR STICKS SHUT INFLIGHT VERY HARD TO RE-ENTER COCKPIT. LUBED DOOR PER NAS INC MM 52-10-0 PG 301, OPS CHK'S GOOD.SDR DHL2004873500Rib · crackedLT WING CTR L/E FORMER CRACKED 0.500 AT XFS 447.750. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. FABRICATED ANGLE DOUBLERS (AL 2024-T3 0.040) (2EA) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED AREA AND ANGLE DOUBLER IAW SRM 51-1-8B. INSTALLED ANGLE DOUBSDR UPS04843416Switch · inoperativeEMERGENCY EXIT LIGHTS ARM SWITCH INTERMITTENT. REMOVED AND REPLACED EMERGENCY EXIT LIGHTS ARM SWITCH. OPS CHECK GOOD PER DC8 MM33-50.SDR UPS04843415Battery Pack · dischargedEMERGENCY LIGHTS BATTERY LOW ON PREFLIGHT CHECK. REPLACED EMERGENCY LIGHTS BATTERY PACK. OPS CK GOOD.SDR UPS04843401Battery Pack · inoperativeEMERGENCY EXIT LIGHTS INOP. REPLACED EMERGENCY EXIT LIGHT BATTERY PACK PER MM 25-60.SDR DHL2004801011Battery Pack · inoperativeEMERGENCY LIGHT ARE INOP IN TEST. REMOVED AND REPLACED BATTERY PACK IAW MM 33-50-1. CHECKED OPERATION OK.SDR DHL2004801010Door Frame · contaminatedCOCKPIT DOOR STICKS, ALMOST IMPOSSIBLE TO GET BACK IN COCKPIT. REMOVED DEBRRIS FROM LOWER PART OF DOOR JAMB. COCKPIT DOOR OP'S CHECK OK PER DC-8 MM 52-00-00.SDR UPS04843362Lamp · inoperativeENTRY DOOR EMERGENCY LIGHTS, 1 AFT INOP. RELAMPED EMERGENCY LIGHTS, OPS GOOD.SDR DHL2004801009Fire Loop · malfunctionedIN CRUISE FLT FIRE WARNING INDICATION ON NR 1 ENG. PERFORMED EMERGENCY CHECKLIST, LANDED AT ICT, FIRE WARNING PERSISTED THROUGHT OUT DESENT AND LANDING. TRANSFERED FIRE LOOP A ON DUAL LOOP SYSTEM TO DMI 18127 MEL REF 26-2-3 CAT C. DMI EXPIRES IN 10 CONSECUTSDR IXXA0500073SFrame · crackedDURING A ROUTINE C-CHECK INSPECTION FOUND CRACK ON MAIN CARGO COMPARTMENT FRAME FLANGE 1 INCH AT STA 340.000 L-20L. MAJOR REPAIR ACCOMPLISHED BY REMOVAL OF CRACKED FRAME SEGMENT. FABRICATED NEW FRAME SEGMENT AND SPLICES. HEAT TREATED SPLICES. CLEANED, TREASDR IXXA0500076SSkin · corrodedDURING A ROUTINE C-CHECK INSPECTION FOUND LOWER EXTERNAL FUSELAGE SKIN CORRODED AT STA 1410.000 L-35. MAJOR REPAIR ACCOMPLISHED REMOVAL OF THE CORROSION. FOUND OUT OF LIMITS AND REMOVED THE DAMAGED PLATING. CLEANED, TREATED AND PRIMED AREA. APPLIED THE PRCSDR IXXA0500075SVane · damagedDURING A ROUTINE C-CHECK INSPECTION FOUND LT WING EXTENDED LEADING EDGE O/B VANE PLATING HAS DAMAGE. MAJOR REPAIR ACCOMPLISHED REMOVAL OF THE DAMAGED AREA. AN NDT INSPECTION WAS PERFORMED. FABRICATED REPAIR DOUBELR, FILLER INTERNAL DOUBLER. CLEANED, TREATESDR IXXA0500074SSkin · damagedDURING A ROUTINE C-CHECK INSPECTION FOUND DAMAGE ON THE FUSELAGE EXTERNAL SKIN AT STA 125.000 - 275.000 L-21L. MAJOR REPAIR ACCOMPLISHED REMOVAL OF DAMAGED SECTION. PERFORMED AN NDT INSPECTION, FABRICATED EXTERNAL REPAIR DOUBLER, FILLERS, FINGER DOUBLERS ANDSDR IXXA0500072SVane · damagedDURING A ROUTINE C-CHECK INSPECTION FOUND RT WING EXTENDED LEADING EDGE INBOARD VANE PLATING INTERIM REPAIR AROUND STA XS 247.000. MAJOR REPAIR ACCOMPLISHED BY REMOVAL OF THE FASTENERS WITHIN REPAIR AREA AND THE EXISTING INTERIM REPAIR. REMOVED THE DAMAGED SSDR IXXA0500071SSkin · crackedDURING A ROUTINE C-CHECK INSPECTION FOUND RT WING EXTENED LEADING EDGE OUTBOARD VANE PLATING REPAIR DOUBLER WITH ELONGATED HOLES AND CRACK DAMAGE BETWEEN STA XOLDO 67.000 AND XS 497.491. MAJOR REPAIR ACCOMPLISHED REMOVAL OF EXISTING REPAIR DOUBLER AND REMOVALSDR IXXA0500070SSkin · damagedDURING A ROUTINE C-CHECK INSPECTION FOUND RT OUTER WING INBOARD EXTENDED LEADING EDGE OUTER LOWER PLATING WITH INTERIM REPAIR AROUND STA XFS 710.000. MAJOR REPAIR ACCOMPLISHED REMOVAL OF INTERIM REPAIR. THE DAMAGED SECTION WAS REMOVED AND A NDT INSPECTION WASDR IXXA0500069SFitting · corrodedDURING A ROUTINE C-CHECK INSPECTION FOUND RT FUSELAGE LONGERON 24 FITTING FRAME HAS CORROSION DAMAGE AT STATION 940.000. MAJOR REPAIR ACCOMPLISHED REMOVAL OF FITTING. CLEANED, TREATED AND PRIMED AREA. FABRICATED SPLICES, DOUBLER AND FILLER. PERFORMED HEAT
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