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 DHL2006809001Control Panel · smokeSMOKE SEEN COMING FROM LONG TRIM IND AREA OR CENTER PEDESTAL. SMOKE CLEARED IMMEDIATELY WHEN PEDESTAL LIGHTS SWITCH WAS PLACED IN OFF. FOUND CRACKED LONG TRIM PANEL PULLED & COLLARD PED & OVERHEAD SW PANEL C/B FOR LIGHTS DEFERRED IAW DC8 MEL 33-1 DMI 24805. SDR UPS06846688Fitting · crackedINSPECTION TYPE:C1 STA 902 LONGERON 4L FITTING IS CRACKED. REMOVED AND REPLACED LONGERON END FITTING AT STA 902 L4L IAW SRM 51-3-2, 51-1-20D AND SRM 51-1-21.SDR UPS06846665Fitting · crackedFOUND STA 680 L2L FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-21, 51-1-20D AND 51-3-0.SDR UPS06846664Fitting · crackedFOUND STA 902 L9L FITTING CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-3-0, 51-1-20D AND 51-1-21.SDR UPS06846663Fitting · crackedFOUND STA 1690 LONGERON END FITTING CRACKED LONGERON 24R. REMOVED AND REPLACED FITTING IAW SRM 51-1-21,51-1-21 AMD 51-3-0.SDR UPS06846530Battery Pack · inoperativeEMERGENCY LIGHT BATTERY INOP. REPLACED BATTERY PACK.SDR UPS06846681Fitting · crackedSTA 680 LONGERON 6L FITTING IS CRACKED. REMOVED AND REPLACED LONGERON END FITTING AT STA 680 L6L IAW SRM 51-1-20D, SRM 51-1-21, 51-3-0.SDR DHL2006801507Skin · crackedLT INBD FLAP LWR SURFACE HAS TWO CRACKS OF 0.500" AND 0.125" AT STA XW 12.000 AND XW 66.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-7-1 FIG 1. REMOVED DAMAGED PANEL PLATING IAW SRM 57-1-0, SRM 51-1-21. FABRICATED NEW PLATING (AL 2024T3 0.032") ANDSDR UPS06846641Fitting · crackedFOUND STA 680 LONGERON 3L FITTING CRACKED. REMOVED AND REPLACED LONGERON END FITTING AT STA 680 L3L IAW SRM 51-01-20D, 51-03-00-0, 51-03-01-0.SDR UPS06846747Stiffener · corrodedINSPECTION TYPE:C1 RT W/W STA 857 BULKHEAD VERTICAL STIFFENER CORRODED BEYOND LIMITS RBL 46, 13" BELOW CEILING. REMOVED VERTICAL STIFFENER AT STA 857 RBL40 IAW SRM 51-01-21, AND SRM 51-01-20D. FABRICATED AND INSTALLED ANGLES,"L" ANGLES, AND VERTICAL STIFFENESDR UPS06846735Skin · crackedINSPECTION TYPE:C1 EXTERIOR SKIN CRACK, TORN ON RMLG IB DOOR AT STRUT EXTENSION. CUT OUT DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER IAW SRM 52-06-03, 52-02-00-0, AND 51-1-21.SDR UPS06846692Skin · corrodedFOUND STRUCTURE CORRODED FWD OF LT BOTTLE BOLT BARREL NUT, LT W/W FWD UPPER OB CORNER. REPAIRED EXTERNAL SKIN CORROSION AT STA 857 LONGERON 24L AT BAYONET FITTING IAW UPS ENGINEERING FILE NR DC8-53-20543, SAA EA NR 008-5320-01-A0137, BAC SERVICE REQUEST 1-176SDR UPS06846690Stiffener · corrodedHEAVY CORROSION UNDER VERTICAL STIFFENER ON LT W/W 857 BULKHEAD LBL 45, 13" BELOW CEILING. REMOVED VERT STIFFENER AT FS 857 LBL45 IAW SRM 51-01-21. FABRICATED AND INSTALLED REPAIR ANGLE, REPLACEMENT STIFFENER AND SUPPORT ANGLES AT FS 857 LBL45 IAW DWG 564343SDR UPS06846614Skin · corrodedFUSELAGE SKIN AT SPLICE BETWEEN FUSELAGE AND TAILCONE BETWEEN LONGERON 34L- 34R HAS CORROSION APPEARS TO GO UNDER DOUBLER ON FUSELAGE SIDE STA 1890. REMOVED DOUBLER, REMOVED CORROSION FROM SKIN AND FOUND TO BE WITHIN LIMITS. FABRICATED AND INSTALLED DOUBLER SDR IXXA06SMN100SAccess Door · crackedDURING ROUTINE C CHECK INSPECTION, LEFT HAND VERTICAL STABILIZER ACCESS DOOR EDGE CRACKED. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 06119 DATE 03-07-06, SEMAN DWG ED 4187 DATE 03-06-06, EO SEMAN 2006150 DATE 03-07-06. REMOVED FASTENERS IAW DC-8 SRM 51-1-21SDR IXXA06SMN102SSkin · dentedDURING ROUTINE C-CHECK INSPECTION, LT WING OUTBOARD AILERON L/E DENTED, XA 662.000. PERFORMED MAJOR REPAIR IAW DC-8 SRM 57-8-1 FIG 4. PERFORMED NDT INSPECTION DETECT CRACK IAW DC-8 NDT SPM PART 06-10-01-001. CRACK FOUND 0.250 LENGTH ENCLOSED SMN FORM 242-2.SDR DHL2006801514Intercostal · corrodedFOUND UPPER CARGO COMPT INTERCOSTAL CORRODED (STA 1120.000 - 1140.000 RH L-1). REMOVED CORROSION ON INTERCOSTAL (STA 1120.000- 1140.000) IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG 2P. REMOVED CORRODED INTERCOSTAL IAW SRM 51-1-20D, SRM 51SDR UPS06846615Skin · dentedDENTS 2 EACH AFT OF SERVICE DOOR L-2 AT STA 1670 L17L. CUT OUT DAMAGE, FABRICATED AND INSTALLED DOUBLER AND FILLER IAW SRM53-2-1 FIG 10.SDR DHL2006801508Skin · corrodedRIGHT RUDDER EXTERNAL SKIN CORRODED, STA ZR 257.906 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 55-6-1 FIG 1. REMOVED CORROSION FROM RIGHT RUDDER EXTERNAL SKIN STA ZR 257.906 IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 55-2-0 PG 12. REMOVED CORSDR DHL2006801503Frame · crackedRT OUTER WING OTBD L/E CRACK 0.500" ON FORMER STA XFS 822.50. REMOVED FASTENERS IAW SRM 51-1-21. PERFORMED STOP HOLE AND FABRICATED ANGLE DOUBLER (AL7075T6 0.040") IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED AREA AND ANGLE DOUBLER IAW SRM 51-1-8B. SDR DHL2006801500Doubler · crackedNR 4 RT STUB WING INTERNAL DOUBLER CRACK STA XFS 523.000 (MAJOR REPAIR) AND NON STANDARD REPAIR (EXTERNAL DOUBLER) ALSO CORRODED. PERFORMED MAJOR REPAIR IAW SRM 57-2-1A FIG 1. REMOVED EXISTING EXTERNAL DOUBLER AND CRACKED INTERNAL DOUBLER IAW SRM 51-1-21, SRSDR DHL2006801504Frame · crackedRT OUTER WING OTBD L/E CRACK 0.500" ON FORMER STA XFS 791.250. REMOVED FASTENERS IAW SRM 51-1-21. FABRICATED ANGLE DOUBLER (AL7075T6 0.040") AND PERFORMED STOP HOLE IAW SRM 57-2-0 PG. 9-10. CLEANED, TREATED AND PRIMED AREA AND ANGLE DOUBLER IAW SRM 51-1-8B.SDR DHL2006801502Frame · crackedFOUND RT OUTER WING OUTBD L/E FRAME CRACK 0.500" STA 766.250. REMOVED FASTENERS IAW SRM 51-1-21. FABRICATED ANGLE DOUBLER (AL 7075T6 0.040") AND PERFORMED STOP HOLE IA SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED AREA AND DOUBLER IAW SRM 51-1-8B. INSTALSDR DHL2006801501Skin · wornLEFT OUTBOARD FLAP UPPER PANEL SKIN WORN STA XF 416.000 (NEAR SLIDING HINGE COVER TRACK) MAJOR REPAIR. PERFORMED MAJOR REPAIR IAW BOEING MESSAGE 1-169339902-2 DATED 03-08-06. REMOVED DAMAGED PLATING IAW SRM 57-1-0, SRM 51-1-21. FABRICATED NEW PLATING (AL202SDR UPS06846618Doubler · corrodedFOUND L24R HEAVILY CORRODED AT STA 25. REMOVED, FABRICATED AND INSTALLED LONGERON 24R AND LONGERON FITTING IAW SRM53-2-0 FIG 1F, SH 1, 51-1-21. REPAIRED SKIN INTERNAL DOUBLER STA 25-55 L21R IAW SAA EA NR 008-5310-01-A0126 AND UPS EO DC8-5330- 24021-A.SDR UPS06846447Battery Pack · inoperativeEMERGENCY EXIT LIGHTS DO NOT WORK. REMOVED AND REPLACED EMERG EXIT LIGHTS BATTERY PACK. OPS CHECK GOOD REF MM CH 33-50-01-2.SDR DHL2006804002Fire Detector · malfunctionedNR 1 ENG FIRE IND PERFORMED ABNORMAL CHECK LIST BLOW BOTH FIRE BOTTLES. RIGHT CORE DETECTOR AT FAULT. REPLACED RIGHT CORE DETECTOR PER DC8 MM 26-10-1 AND PERFORMED ADJ/TEST PER MM 26-10-0. OPS CHECK NORMAL.SDR DHL2006807003Fuel · contaminatedNR2 ENG ROLLED BACK IN CRUISE. SELECTED X FEED, IMMEDIATELY RESTORED NORMAL OPERATIONS. NR 2 MAIN TANK INDICATED 20300 NR LANDED AT NEAREST SUITABLE. AIRFIELD SUMP NR 2 MAIN TANK REMOVED AND REPLACED NR 2 ENGINE MAIN FUEL FILTER, PERFORMED LEAK CHECK OF FILTSDR DHL2006804001Fire Loop · out of positionAT FL 350 IN LIGHT TURBULENCE UNCOMMANDED FIRE LIGHT/BELL TEST LASTING ABOUT 10 SECONDS ON ENGINE NR 1. THE BELL SOUNDED AT APPROX 1/2 VOLUME COMPARED TO NORMAL. LOOP "A" WAS IN USE. INSPECTED NR 1 ENGINE "A" LOOP FOR DEFECTS. NO DEFECTS NOTED. DEFERRED SDR IXXA06SMN080SSkin · crackedDURING ROUTINE C-CHECK INSPECTION, EMPENNAGE 1 INCH CRACK, STA 1766.000, L-28L. REPAIRED PER ALL APPLICABLE DATA.SDR IXXA06SMN083SSkin · misrepairedDURING C CHECK, LT ELEVATOR UPPER SURFACE HAS NON STANDARD REPAIR AT STA XE 32.937. PERFORMED MAJOR REPAIR IAW DC8 SRM 55-4-1 FIG 1. REMOVED PANEL PLATING WITH STANDARD REPAIR IAW DC8 SRM 55-1-0, DC8 SRM 51-1-21. FABRICATED NEW PLATING AND BONDED FINGER DOUSDR IXXA06SMN082SElevator · improperDURING ROUTINE C-CHECK INSPECTION, LT ELEVATOR UPPER SURFACE HAS NON - STANDARD REPAIR AT STA XE 99.281. PERFORMED MAJOR REPAIR IAW DC8 SRM 55-4-1 FIG 1. REMOVED PANEL PLATING WITH STANDARD REPAIR IAW DC8 SRM 55-1-0, DC8 SRM 51-1-21. FABRICATED NEW PLATING SDR IXXA06SMN099SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, RIGHT WING OUTBOARD INNER LEADING EDGE EXTERNAL UPPER SKIN HAS NON STANDARD REPAIR AT STATION XFS 572.500. PERFORMED MAJOR REPAIR IAW DC8 SRM 57-2-1 FIG 38 TR # 57-85 DATE 11-27-2000. REMOVED EXISTING REPAIR DOUBLER IAW DC8SDR IXXA06SMN098SPanel · crackedDURING ROUTINE C CHECK, RT WING NR 4 PYLON PANEL CRACKED, YN 321.000. PERFORMED MAJOR REPAIR IAW DC8-70 SB 54-93 CONDITION V. REMOVED FASTENERS IAW SB 54-93 PAGE 11 FIG 2 DC8 SRM 51-3-0, DC8 SRM 51-1-21. PERFORMED VISUAL INSPECTION TO PYLON ADAPTER PANEL FOR SDR IXXA06SMN096SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, RIGHT WING OUTBOARD. FLAP LOWER AFT SKIN NON STANDARD REPAIR, AT STATION XF 350.000. PERFORMED MAJOR REPAIR IAW DC8 SRM 57-7-1 FIG 4 TR NR 57-94 DATE 10-01-02. REMOVED DAMAGED PANEL PLATING IAW DC8 SRM 57-1-0, DC8 SRM 51-1-SDR IXXA06SMN091SFitting · crackedDURING ROUTINE C CHECK INSPECTION, LEFT WING NR 2 MAIN TANK LOWER FORWARD FITTING CRACKED, AT STATION 74.000, STRINGER-50. REMOVED AND REPLACED CRACKED FITTING ON LEFT WING NR 2 MAIN TANK LOWER PART, STATION 74.000 S-50 IAW DC8 SRM 51-1-20D DC8 SRM 51-3-1.SDR IXXA06SMN090SFitting · crackedDURING ROUTINE C CHECK INSPECTION, LEFT WING NR 2 MAIN TANK LOWER FITTING CRACKED, STA 220.00 STRINGER-59. REMOVED CRACKED FITTING IAW DC8 SRM 51-1-20D. FABRICATED NEW FITTING (AL 7075 T6 51) IAW ATI REPAIR SPECIFICATION NR 2003-05 EA SEMAN NR 20061966 DATE SDR IXXA06SMN089SFrame · corrodedDURING C CHECK, FRAME CORRODED AT STA- 62.000 BETWEEN LONGERON-21 AND LONGERON-22. PERFORMED MAJOR REPAIR IAW DC8 SRM 53-3-3 FIG 3. REMOVED CORROSION IAW DC8 SRM 51-1-8 PAGES 17-18. FOUND OUT OF LIMITS IAW DC-8 SRM 53-2-0 PAGE 2P. REMOVED FRAME SEGMENT ANDSDR IXXA06SMN088SSkin · dentedDURING ROUTINE C CHECK, RT WING L/E DENTED (STA XFS 888.000 920.000). PERFORMED MAJOR REPAIR IAW DC8 SRM 57-3-3 FIG 8. REMOVED DAMAGED PLATING IAW DC8 SRM 57-1-0, DC8 SRM 51-1-21. FABRICATED NEW PLATING (AL 7075 T6 0.050) IAW DC8 SRM 57-3-3 FIG 8 ITEM A, DC-SDR IXXA06SMN086SBulkhead · corrodedDURING ROUTINE C CHECK, FLT CMPT CORR BETWEEN FINGER DOUBLER AND BULKED, STA 67 RBL 53. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 06130 DATE 03-09-06 EO SEMAN 2006174 DATE 03-15-06. REMOVED CORROSION IAW DC8 SRM 51-1-8 PAGES 17, 18. FOUND OUT OF LIMITS IAW SDR IXXA06SMN072SDoubler · crackedDURING ROUTINE C CHECK, LT FUSELAGE NOSE SECTION HEAT EXCHANGER COMPT, LWR AFT JAMB CORNER ACS MODIFICATION DOUBLER REINFORCEMENT DOUBLER CRACKED 1/2 INCH STA 12.000 L-27L. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 06119 DATE 03-07-06 SEMAN DWG NR ED 4183 DASDR IXXA06SMN073SDoubler · crackedDURING ROUTINE C CHECK, RT FUSELAGE NOSE SECTION. HEAT EXCHANGER COMPT LWR AFT JAMB CORNER ACS MODIFICATION DOUBLER REINFORCEMENT DOUBLER CRACKED 1/2 INCH STA 12.000 L-27R. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 06130 DATE 03-15-06 SEMAN DWG NR ED 4184 DASDR IXXA06SMN074SVane · damagedDURING ROUTINE C CHECK, LT WING L/E INBD SLOT VANE HOLES ELONGATED, XILD 7095. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 06119 DATE 03-07-06, SEMAN DWG ED 4186 DATE 03-04-06, EO SEMAN 2006146 DATE 03-07-06. REMOVED FASTENERS IAW DC-8 SRM 51-1-21, DC-8 SRM SDR IXXA06SMN075SPanel · crackedDURING ROUTINE C-CHECK INSPECTION, NR 1 PYLON LT UPPER PART PANEL CRACKED 2 INCHES, YN 321.000. PERFORMED MAJOR REPAIR IAW DC8-70 SB 54-93 CONDITION V. REMOVED FASTENERS IAW SB 54-93 PAGE 11 FIG 2 DC8 SRM 51-3-0, DC8 SRM 51-1-21. PERFORMED VISUAL INSPECTIONSDR IXXA06SMN077SStructure · dentedDURING ROUTINE C-CHECK INSPECTION, LT WING FLAP L/E INBOARD PANEL LWR PART DENTED 3 INCHES, STA XW 79.000. PERFORMED MAJOR REPAIR IAW DC8 SRM 57-7-1 FIG 1. REMOVED DAMAGED PANEL PLATING IAW DC8 SRM 57-1-0, DC8 SRM 51-1-21. FABRICATED PLATING (AL 2024T3 0.0SDR IXXA06SMN069SSkin · wornDURING ROUTINE C-CHECK INSPECTION, EXTERNAL FUS LWR SKIN WORN AT SEVERAL SPOTS; STA 680.000 - STA 720.000. PERFORMED MAJOR REPARI BY REMOVING CORROSION IAW DC8 SRH 51-1-8 PGS 17, 18. FOUND OUT OF LIMITS IAW DC8 SRM 53-2-0 PAGE 2P. REMOVED THE DAMAGED AREA ISDR IXXA06SMN092SRepair · misinstalledDURING ROUTINE C-CHECK INSPECTION, LT WING OUTBOARD FLAP T/E UPPER PANEL HAS NON STANDARD REPAIR BETWEEN XF 415.000 AND XF 418.000. PERFORMED MAJOR REPAIR IAW DC8 SRM 57-2-5 FIG 1 (SHEET 1, 2). REMOVED NON STANDARD REPAIR (EXISTING) IAW DC8 SRM 51-1-21. REMSDR IXXA06SMN093SRepair · misinstalledDURING ROUTINE C-CHECK INSPECTION, LT WING OUTBOARD FLAP L/E UPPER PART HAS NON STANDARD REPAIR WORN 1 INCH, XF 346.00. PERFORMED MAJOR REPAIR IAW DC8 SRM 57-7-1 FIG 4 TR 57-94 DATE 10-01-02. REMOVED DAMAGED PLATING WITH NON STANDARD REPAIR IAW DC8 SRM 57-1-SDR IXXA06SMN094SRepair · misinstalledDURING ROUTINE C-CHECK INSPECTION, RT WING INBOARD FLAP LWR FWD SKIN NON STANDRAD REPAIR, XF 16.000. PERFORMED MAJOR REPAIR IAW DC8 SRM 57-2-5 FIG 2 (SHEET 2, 4) TR 57-91 DATE 09-30-01. REMOVED EXISTING NON STANDARD REPAIR IAW DC8 SRM 51-1-21. REMOVED DAMAGSDR IXXA06SMN095SRepair · misinstalledDURING ROUTINE C-CHECK INSPECTION, RT WING INBOARD FLAP PANEL LWR SKIN NON STANDARD REPAIR, XF 21.000. PERFORMED MAJOR REPAIR IAW DC8 SRM 57-2-5 FIG 2 (SHEET 3, 4) TR 57-91 DATE 09-30-01. REMOVED EXISTING NON STANDARD REPAIR IAW DC8 SRM 51-1-21. REMOVED DAM
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