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 IXXA08SMN118SSkin · damagedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT INBOARD FLAP SKIN UPPER PLATING NICKED AT STATION XW 112.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGE PLATING. FABRICATED NEW SKIN. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. INSTSDR IXXA08SMN117SSkin · dentedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT ELEVATOR UPPER SKIN DENTED AT STATION XE 200.2379. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGE SKIN. FABRICATED NEW SKIN AND FINGER DOUBLER. BONDED PARTS AS NEEDED WITH HYSOL. CLEANED, TREATESDR IXXA08SMN116SSkin · dentedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT ELEVATOR UPPER SKIN DENTED AT STATION XE 137.531 TO STATION XE 142.062. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGE SKIN. FABRICATED NEW SKIN AND FINGER DOUBLER. BONDED PARTS AS NEEDED WITH HYSDR IXXA08SMN115SFitting · crackedDURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT INTERCOSTAL SUPPORT FITTING CRACKED AT STATION 902.000 LONGERON19 RIGHT. REMOVED CRACKED INTERCOSTAL SUPPORT. FABRICATED NEW INTERCOSTAL SUPPORTS. PERFORMED NDT INSPECTION. CLEANED, TREATED ANDSDR DHL2008805532Fitting · crackedCENTER WING REAR SPAR UPPER CAP FITTING CRACKED STA 857.000. REMOVED CRACKED FITTING IAW SRM 51-1-20D, CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-20D AND SRM 51-3-1 (TORQUE).SDR DHL2008805533Stiffener · corrodedRT MLG W/W STIFFENER CORRODED AT STA 857.000. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18 AND FOUND OUT OF LIMITS IAW SRM 53-2-0 PG 2P. REMOVED CORRODED ANGLE IAW SRM 51-1-20D, SRM 51-1-21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW ANGLSDR UPS08851934Control Cable · damagedCREW ENTRY DOOR WILL NOT OPEN. REPLACED LOWER HINGED SEAL PUSH/PULL CONTROL CABLE AND ADJUSTED PER MM 52-11-01-5. PRESSURIZED A/C. NO LEAKS NOTED ON FWD ENTRY DOOR AND LOWER SEAL.SDR DHL2008805506Skin · damagedLT WING INBD L/E LWR SURFACE HAS ELONGATED HOLES AT STA XILD 42. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 03-24-08, EVA D853-00046, DWG AF12-57-101 REV IR DATED 02-22-08. REMOVED FASTENERS IAW SRM 51-1-21, SRM 51-3-0. CUT OUT DAMAGED SECTION IAW DWGSDR DHL2008805537Cargo Track · wornUPPER CARGO COMPT NR 7 TRACK LUG WORN (STA 290.000 - 340.000) MAJOR REPAIR. PERFORMED MAJOR REPAIR IAW SRM 53-2-3 PG 49-50. REMOVED TRACK DAMAGED SEGMENT IAW SRM 53-2-3. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW TRACK SEGMENT IAW SRM SDR DHL2008805536Cargo Track · wornUPPER CARGO COMPT NR 3 TRACK LUG WORN (STA 590.000 - 620.000) MAJOR REPAIR. CUT OUT TRACK SEGMENT AND FABRICATED (3EA) SPLICES (AL7075T6 0.100", 0.125" AND 0.160") IAW SRM 53-2-3 PG 49-50 FIG 14. CLEANED, TREATED AND PRIMED AREA AND SPLICES IAW SRM 51-1-8B. SDR DHL2008805534Rib · wornLT MLG W/W DOOR UPLATCH RAIL RIB WORN AT STA 890.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW JC EC-00840-001D, DWG DOUGLAS NR 5653490. REMOVED WORN RIB IAW SRM 51-1-21, SRM 51-1-20D, SRM 51-3-0. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLEDSDR UPS08851917Fitting · crackedINSPECTION TYPE:C2 BROKEN FITTING IN FWD ACC COMPT STA 640 L35R-L36. FABRICATED AND REPLACED FITTING AT STA 640 AND L35R-L36 IAW DWG 3750 834, SRM 51-1-8, SRM 51-01-20D AND 51-3-0.SDR UPS08851902Battery Pack · dischargedINSPECTION TYPE:N/A EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED EMERGENCY BATTERY PACK IAW MM 33-50-01-2. OPS CHECK OK.SDR UPS08851894Slide · deployedINSPECTION TYPE:N/A ESCAPE SLIDE PARTIALLY DEPLOYED. ESCAPE SLIDE PACK REMOVED FOR REPACKING. REPACKED AND REINSTALLED ESCAPE SLIDE. OK FOR SERVICE. REF MM 25-60-01-2.SDR DHL2008805502Angle · corrodedCORROSION AT RT VERT STAB TO FUSELAGE JOINT LWR ANGLE, STA 1800.000 L-2R - L-3R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-2-5 FIG 16A SHEET 1, 2. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG 2P. CUT OUT DAMAGED SSDR DHL2008805511Flap · damagedRT OUTBD FLAP L/E PLATING HOLES ELONGATED (STA XF 325.000 - 243.000). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 03-12-08, ASTAR EVA D857-00049 REV IR DATED 03-12-08, SEMAN DWG NR ED-4719 DATED 02-25-08. PERFORMED NDT INSP OF DAMAGED AREA IAW DC8 NDT SSDR DHL2008805515Structure · damaged"D" BELLY, FWD LOWER CORNER REPAIR C/W IAW SR08530021 AT SEMANS, HOWEVER, INCORRECT STEEL FASTENERS ARE INSTALLED. REPLACE WITH TITANIUM AS REQUIRED AND ENSURE REPAIR IS IAW SR08530019 AND AD. PERFORMED MAJOR REPAIR IAW FAA FORM 8100-9 DATED 03-07-08, AD2005SDR DHL2008805513Fitting · crackedNR 4 STUB WING INTERIOR FITTING CRACKED 0.500" STA 562.500 CANT (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW DOUGLAS DRAWING NR 5754705. REMOVED CRACKED FITTING IAW SRM 57-1-0 PG 1, SRM 51-1-21, SRM 51-1-20D. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. SDR DHL2008805516Skin · corrodedAFT FUS EXT SKIN CORRODED (STA 1730.000 - 1740.000 L-28R TO L-30R). PERFORMED MAJOR REPAIR IAW FAA FORM 8100-9 DATED 02-29-08, AD2007-02-02, S/B DC8 S3A080, DWG DOUGLAS SR08530032 AND BOEING MSG 1-7761393332 DATE3D 02-29-08, SEMAN DWG ED-4715 DATED 02-21-08. SDR UPS08851908Seat Track · corrodedINSPECTION TYPE:C2 LOWER FLANGE OF SEAT TRACK EXTRUSION EXFOLIATED IN MAIN CABIN, STA 1455-1462 LBL 60. REPAIRED CABIN SEAT TRACK AT STA 1455-1462 LBL 60 IAW SRM 53-02-03-0, AND SRM 53-02-03-0 FIG 008A.SDR DHL2008805501Skin · corrodedFWD ACCY COMPT CORROSION BETWEEN SKIN AND FINGER DOUBLER (STA 30.000 - 50.000 L-32R TO L-33R). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 03-14-08, ASTAR EVA D853-00048 REV IR DATED 02-27-08 (SEMAN DWG ED-4714) DATED 02-18-08. REMOVED CORROSION IAW SRMSDR UPS08851909Seat Track · corrodedINSPECTION TYPE:C2 CORROSION ON SEAT TRACK AT STA 1470 LBL 45. FABRICATED AND REPLACED CABIN SEAT TRACK SECTION AT STA 1470 AND LBL 45 IAW SRM 51-03-00, SRM 51-03-02, SRM 51-03-01 AND SRM 51-1-8.SDR UPS08851880Door · crackedINSPECTION TYPE:N/A PIT 32 DOOR CRACKED. ACCOMPLISHED HFEC INSPECTION PER EO DC8-5230-28827 PAR 6 A2. ACCOMPLISHED STOP DRILL PER EO DC8-5230-28827 PAR 6 A3-A4. NEEDS HFEC. ALSO REMOVED MOUNT BOLTS & 2 EA RIVETS FOR ACCESS. PERFORMED EDDY CURRENT ON STOP SDR UPS08851877Skin · crackedINSPECTION TYPE:N/A CRACK AND CORROSION ON TAIL CONE UPPER SURFACE. C/O DAMAGE AND RADIUSED 4 EA CORNERS. DAMAGE REMOVED. FABRICATED PARTS FILLER & DOUBLER, OK TO INSTALL PER QC. INSTALLED REPAIR. ITEM 371453 ASSIGNED FOR 6000 CYCLES PER DC8 SRM 53-02-01SDR IXXA08SMN097SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT AFT FUSELAGE L-2 DOOR AFT EDGE HAS IMPROPER REPAIR AT FS-1660 LONGERON 19.5. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR DOUBLER. PERFORMED NDT INSPECTION. NO CRACK, NO CORROSION FOUNSDR IXXA08SMN096SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND DOUBLER REPAIR RIGHT AFT FUSELAGE ABOVE AND FWD OF C-PIT DOOR RIVET SPACING EXCEEDED AT FS 1150 LONGERON 21.5 RIGHT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXITING REPAIR. PERFORMED NDT INSPECTION. NSDR IXXA08SMN095SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND DOUBLER AFT LOWER FUSELAGE BELLY SKIN BELOW AND FWD D-PIT DOOR ALUMINUM RIVETS IN FRAMES AT FS 1395, LONGERON 36. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. PERFORMED INSPECTION NDT. NO CRASDR IXXA08SMN102SFitting · crackedDURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT FITTING CRACKED AT STATION 55.000 LONGERON 7LEFT. REMOVED CRACKED FITTING. FABRICATED NEW FITTING. PERFORMED NDT INSPECTION. NO CRACK, NO CORROSION FOUND AFTER INSPECTION. CLEANED, TREATED ANSDR IXXA08SMN101SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING INBOARD FLAP LOWER PANEL SKIN HAS IMPROPER REPAIR AT STATION XW 18.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. FABRICATED NEW SKIN AND BONDED DOUBLER. BONDED PARTS AS NEEDSDR IXXA08SMN098SFitting · crackedDURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT BATH TUB FITTING CRACKED AT STATION 680.000. REMOVED CRACKED FITTING. INSTALLED NEW BATH TUB FITTING IAW DC8 SRM 51-1-20D, AND 51-3-1.
SDR IXXA08SMN109SFitting · crackedDURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT AFT FITTING CRACKED AT STATION 759.000 LBL 22. REMOVED CRACKED FITTING. FABRICATED NEW FITTING. PERFORMED INSPECTION NDT. NO CRACK, NO CORROSION FOUND. CLEANED, TREATED AND PRIMED AREA AND NESDR IXXA08SMN110SFitting · crackedDURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT AFT FITTING CRACKED AT STATION 700.000 LBL 22. REMOVED CRACKED FITTING. FABRICATED NEW FITTING. PERFORMED INSPECTION NDT. NO CRACK, NO CORROSION FOUND. CLEANED, TREATED AND PRIMED AREA AND NESDR IXXA08SMN108SFitting · crackedDURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT FORWARD FITTING CRACKED AT STATION 717.000 RIGHT BOTTOM LINE 22". REMOVED CRACKED FITTING. FABRICATED NEW FITTING. PERFORMED INSPECTION NDT. NO CRACK, NO CORROSION FOUND. CLEANED, TREATED ANDSDR IXXA08SMN107SFitting · crackedDURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT AFT FITTING CRACKED AT BS 822.000 LEFT BOTTOM LINE 22". REMOVED CRACKED FITTING. FABRICATED NEW FITTING. PERFORMED NDT INSPECTION. NO CRACK, NO CORROSION FOUND. CLEANED, TREATED AND PRIMED ARSDR IXXA08SMN106SFitting · crackedDURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT AFT FITTING CRACKED AT STATION 781.000 RIGHT BOTTOM LINE 22". REMOVED CRACKED FITTING. FABRICATED NEW FITTING. PERFORMED NDT INSPECTION. NO CRACK, NO CORROSION FOUND. CLEANED, TREATED AND PRISDR IXXA08SMN105SFitting · crackedDURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT FORWARD FITTING CRACKED AT STATION 717.000 LEFT BOTTOM LINE 22". REMOVED CRACKED FITTING. CLEANED, TREATED AND PRIMED AREA. INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D, DC8 SRM 51-3-1, AND DC8 SSDR IXXA08SMN104SFitting · crackedDURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT AFT FITTING CRACKED AT STATION 759.000 RIGHT BOTTOM LINE 22". REMOVED CRACKED FITTING. CLEANED, TREATED AND PRIMED AREA. INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D, DC8 SRM 51-3-1, AND DC8 SRM SDR IXXA08SMN103SSkin · deformedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT INBOARD FLAP UPPER PANEL DEFORMED AT STATION XW 104.000 TO STATION XW 115.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN AND BONDED DOUBLER. BONDED PARTS AS NEEDEDSDR IXXA08SMN100SSkin · dentedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING INBOARD FLAP SKIN UPPER PART DENTED AT STATION XW 114.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGE AREA. FABRICATED NEW SKIN. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. INSTSDR IXXA08SMN099SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING INBOARD FLAP SKIN UPPER PART HAS IMPROPER REPAIR AT STATION XW 114.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. FABRICATED NEW SKIN, BONDED DOUBLER. BONDED PARTS AS NEEDED SDR UPS08851879Skin · puncturedINSPECTION TYPE:N/A RIGHT WING O/B FLAP UPPER SKIN HAS PUNCTURE DAMAGE 2 INCHES I/B OF CUTOUT (ACTUATOR) AND 18 INCHES AFT OF LEADING EDGE. DAMAGE MEASURES .375" X .250". ACCOMPLISHED REPAIR PER DC8 SRM 57-02-01-0 FIG 002Q. CLASS B REPAIR. RAN FLAPS, NO INTSDR UPS08851861Outflow Valve · malfunctionedCLIMBING THRU FL250 CABIN PRSR/ALT WARNING HORN SOUNDED. CABIN ATL WAS 13000 FT AND CLIMBING AT 4000 FPM. LOCKED OUTFLOW VLV CLOSED AND TURNED BOTH PACKS TO MAX. NO OTHER LIGHTS OR INDICATIONS. WENT BACK TO AUTO AND WORKED OK. BOTH PACKS WERE AT MINIMUM ASDR IXXA08SMN094SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND DOUBLER AFT LOWER FUSELAGE BELLY BELOW AND AFT OF D-PIT DOOR RIVET SPACING EXCEEDED ON SIDE FOUR, ALSO ALUMINUM FASTENERS IN FRAMES AT FS 1446 LONGERON 36. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGESDR IXXA08SMN093SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND DOUBLER, AFT LOWER FUSELAGE BELLY BELOW D-PIT DOOR RIVET SPACING EXCEEDED AT FS 1421 LONGERON 36. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. PERFORMED INSPECTION NDT. NO CRACK, NO CORROSIONSDR IXXA080022SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND IMPROPER REPAIR AT RIGHT WING UPPER AFT SKIN PANEL. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACK, NO CORROSION FOUND. CLEANED, TRSDR IXXA08SMN092SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND IMPROPER REPAIR AT LEFT WING UPPER AFT SKIN PANEL. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACK, NO CORROSION FOUND. CLEANED, TRESDR IXXA08SMN091SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND IMPROPER REPAIR AT FUSELAGE SKIN FORWARD OF FLAT AFT PRESSURE BULKHEAD AT LONGERON 28. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR DOUBLERS. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION.SDR UPS08851863Slide · low pressureCREW ESCAPE SLIDE SHOWS LOW PRESSURE. DEFERRED CREW EMERGENCY ESCAPE SLIDE PER MEL 52-7-4. PLACARD INSTALLED. R&R EMERGENCY EVAC SLIDE PER MM 25-60-01-2. THIS CLEARS M371295 PLACARD REMOVED.SDR DHL2008805524Fitting · crackedAFT CARGO COMPT BILGE FITTING CRACKED 2" (STA 1160.000 - 1180.000, L-35L) MAJOR REPAIR. PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1. REMOVED CRACKED FITTING IAW SRM 53-1-0 PG 1, SRM 51-1-20D. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FSDR DHL2008805520Skin · delaminatedRT ELEV GEAR TAB LWR SKIN DELAMINATED 1.500". CUT OUT DAMAGED SECTION IAW SRM 55-2-2 PAR 4D, PAR 2 FIG 3. FABRICATED DOUBLER (AL2024T3 0.016") IAW SRM 55-4-0 PG 10. BONDED CORE AND DOUBLER IAW SRM 51-1-9 PAR 4. REFER TO NR 108672 FOR WEIGHT AND BALANCE.
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