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 RRXA99638Floor · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO FLOOR PANEL AT STA 1000 AND BL 27 RIGHT, DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 53-7-3. (CORROSION DAMAGE RECOSDR RRXA99634Hinge · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO MAIN CARGO DOOR FWD HINGE SEGMENT AT STA 130 AND LONGERON 6 LEFT, DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRO 853SDR RRXA99633Fitting · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO ATTACHMENT ANGLE BETWEEN STA 645 TO STA 669 AND LONGERON 21 LEFT, DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FITTING IAW DC-8 SRM 5SDR RRXA99632Fitting · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO FITTING AT STA 440 AND LONGERON 21 RIGHT, DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FITTING IAW DAC DWG 4597643 AND DC-8 SRM 51-1SDR RRXA99631Fitting · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO FITTING AT STA 822 BETWEEN LONGERONS 21 RIGHT AND 22 RIGHT, DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. INSTALLED NEW FITTING IAW DC-8 SRM 51-1-20D. (CORROSIONSDR RRXA99630Seat Track · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO SEAT TRACK BETWEEN STA 180 TO STA 185 AND BL 65 RIGHT, DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. INSTALLED NEW SEAT TRACK IAW DC-8 SRM 51-3-0. (CORROSION DAMASDR DHL98806001Controller · malfunctionedAIRCRAFT FAILED TO PRESSURIZE AFTER TAKEOFF FROM SUVA IN AUTOMATIC AND MANUAL. FLOWS MAX ONLY 5 PSI. REMOVED AND REPLACED CABIN PRESSURIZATION CONTROLLER PER MM 21-51-0.SDR DHL98805003Skin · crackedSKIN CRACK ON RT WING 14 INBOARD OF NR 4 PYLON. REPAIRED PER DACO S/B 57-100.SDR DHL9880418CVent Box · crackedAT C-CHECK, NR 1 ALT VENT BOX CRACKED. REMOVED AND REPAIRED BOX AND REINSTALLED PER MM 28-10-10. N/R 1073SDR DHL9880408CSkin · crackedAT C-CHECK, RT WING LOWER SURFACE STA 347 HAS A CRACK. CUT OUT DAMAGED AREA, INSTALLED DOUBLER AND FILLER PER DRAWING 18R5761025, 13 X 8. N/R 401SDR RRXA99655Fitting · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO FITTING AT STA 200 BETWEEN LONGERONS 34 RIGHT TO 35 RIGHT, DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FITTING IAW DC-8 SRM 53-2-0.SDR RRXA99652Doubler · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO FINGER DOUBLER BETWEEN STA 260 TO STA 350 AND LONGERON 31 LEFT, DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FINGER DOUBLER IAW DACSDR RRXA99651Fitting · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO FITTING AT STA 270 BETWEEN LONGERONS 34 LEFT TO 35 LEFT, DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FITTING IAW DC-8 SRM 51-1-20D.SDR RRXA99629Longeron · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO LONGERON 24 RIGHT BETWEEN STA 857 TO STA 980, DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. INSTALLED NEW LONGERON 24 RIGHT IAW TIMCO WORKCARD 90453100. (CORROSIOSDR UPS98827921Frame · corrodedINSPECTION TYPE-C, FS 1220 FRAME AND ANGLE CORRODED 33R TO 35R C-3 DOOR BATHTUB AREA. REMOVED, FABRICATED AND INSTALLED REPLACEMENT FITTING IAW DHC SK-818-903.SDR UPS98827919Doubler · corrodedINSPECTION TYPE-C, CORROSION BLEND OUT AT FS 1637 BETWEEN L32 TO 33R INTERNAL DOUBLER OUT OF LIMITS. REPAIRED IAW DHC SK-818-916.SDR UPS98827917Doubler · corrodedINSPECTION TYPE-C, CORROSION BLEND OUT AT FS 1616 BETWEEN L33 TO 32R ON INTERNAL DOUBLER OUT OF LIMITS. REPAIRED IAW DHC SK 818-913 AND SRM 51-1-8.SDR UPS98827888Skin · crackedINSPECTION TYPE-C, RT WING L/E TOP SKIN AT STA XFS 610 IS CRACKED. CUT OUT DAMAGED AREA AND REPAIRED IAW SRM 57-2-1 FIG 38.SDR UPS98827887Skin · crackedINSPECTION TYPE-C, RT WING L/E TOP SKIN AT STA XFS 317.5 IS CRACKED AT THE FRONT SPAR. CUT OUT DAMAGE AND REPAIRED IAW SRM 57-2-1 FIG 38.SDR DHL9880419CStructure · crackedAT C-CHECK, AFT PASSENGER DOOR FWD CORNER HAS A .625 INCH CRACK INSIDE CORNER. CUT OUT CRACKED AREA, FABRICATED FILLER AND ANGLE REPAIR AND INSTALLED PER DER NR 18R53210228, .5 X 3.5. N/R 1036SDR UPS98827909Frame · crackedINSPECTION TYPE-C, THE D-PIT DOOR FRAME IS CRACKED IN 3 PLACES AT THE AFT UPPER CORNER. REPAIRED IAW SRM 52-4-1 AND 52-2-0.SDR UPS98827890Rib · crackedINSPECTION TYPE:C LT WING L/E RIB UPPER ARM CRACKED BY AFT FASTENER AT STA XFS 597.5. REPAIRED IAW SRM 57-2-0.SDR UPS98827886Rib · crackedINSPECTION TYPE-C, LT WING L/E RIB CRACKED ON UPPER ARM BY AFT FASTENER AT STA XFS 578.75. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.SDR UPS98827885Rib · crackedINSPECTION TYPE-C, LT WING L/E RIB UPPER ARM CRACKED BY AFT FASTENER AT STA XFS 616.25. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.SDR UPS98827884Rib · crackedINSPECTION TYPE-C, LT WING L/E RIB UPPER ARM CRACKED BY AFT FASTENER AT STA XFS 610. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.SDR UPS98827920Fitting · crackedINSPECTION TYPE-C, 960 FITTING CRACKED ABOVE LONG 24R RT W/W. REMOVED AND REPLACED FITTINGS IAW SRM 51-1-20D AND 53-2-0.SDR UPS98827918Pan · crackedINSPECTION TYPE-C, LT WING O/B SLOT O/B PAN CRACKED. REMOVED AND REPLACED SLOT PAN IAW SRM 51-1-20D.SDR UPS98827889Skin · crackedINSPECTION TYPE:C LT WING L/E SKIN UPPER SURFACE CRACKED BY 2EA FASTENERS AT STA XFS 610.000. REPAIRED IAW SRM 57-2-1.SDR UPS98827883Skin · crackedINSPECTION TYPE-C, LT WING L/E UPPER SURFACE HAS .25 INCH CRACK BY ATTACH SCREW AT STA XFS 735. CUT OUT DAMAGE AND REPAIRED IAW SRM 57-2-1 FIG 38.SDR RRXA98434Ballast · failedSMOKE IN COCKPIT COMING FROM F/O'S RIGHT CONSOLE AND SUITCASE. FOUND GLARESHIELD BALLAST BURNED RT SIDE BY F/O'S LEG. TRANSFERRED TO DMI NR 809410 IAW MEL CHAP 33-1 CAT DUE DATE 10/6/98 PLACARD INSTALLED. (CLOSED 09/27/98 KLAX) REMOVED AND REPLACED BALLASTSDR DHL98802002Bolt · shearedON S/O PREFLIGHT, FOUND RT MAIN LANDING GEAR OVER CENTER ARM ATTACH FITTING SHEARED OFF AND MISSING. INSTALLED UNIVERSAL LINK BOLT PER DC-8 MM 32-11-1.SDR UPS98827916Skin · gougedINSPECTION TYPE-C, THE FUSELAGE SKIN AT THE AFT LWR CORNER OF THE C-PIT DOOR IS GOUGED. REPAIRED IAW UPS EO DC8-5330-10808-A.SDR UPS98827908Angle · crackedINSPECTION TYPE-C, RT VERT STAB TO EMPENNAGE DRAG ANGLE CRACKED AND CORRODED IN HORIZONTAL LEG LOC APROX 11-14 AFT OF VERT STAB FRONT SPAR. REPAIRED IAW SRM 53-2-5.SDR UPS98827882Shear Tie · crackedINSPECTION TYPE-C, FS 660 FRAME AT LONG 22R IS CRACKED. REMOVED DAMAGED AREA AND REPAIRED IAW DWG 3646688 AND SRM 51-1-20D.SDR UPS98827881Shear Tie · crackedINSPECTION TYPE-C, FS 640 BETWEEN LONG 26L AND 27L THE SHEAR TIE IS CRACKED. REMOVED, FABRICATED AND INSTALLED SHEAR TIE AND SPLICE IAW SRM 53-2-0 FIG 2A AND 51-1-20D.SDR DHL98803002Fuel Control · out of adjustCLIMBED FROM FL 290 TO FL 370, AFTER LEVELING OFF NR 4 ENGINE FLAMED OUT. DESCENDED TO 290 AND PERFORMED INFLIGHT RESTART. PERFORMED INSPECTION PER CFM MM 71-00-00 FAULT NR 51. FOUND SPECIFIC GRAVITY OFF INDEX MARK. RESET TO PROPER INDEX .87 PER MM 73-21-SDR DHL9880430CPanel · delaminatedAT C-CHECK, LEFT WING T/E HINGED PANEL STA XRS 693 TO 763 DELAMINATED. REMOVED AND REPAIRED DELAMINATED PANEL, REINSTALLED PER SRM 51-1-3. N/R 033SDR UPS98827863Angle · crackedINSPECTION TYPE-C, LT WING L/E VERTICAL ANGLE CRACKED AT LWR END AT STA XS 250.089. REMOVED, FABRICATED AND INSTALLED ANGLE IAW DWG 9753293 AND SRM 51-3-0, 51-1-20D.SDR UPS98827862Rib · crackedINSPECTION TYPE-C, LT WING L/E RIB UPPER ARM CRACKED BY AFT FASTENER AT STA XFS 379.0. STOP DRILLED CRACKED AND REPAIRED IAW SRM 57-2-0 FIG 2.SDR UPS98827861Rib · crackedINSPECTION TYPE-C, LT WING L/E RIB LWR ARM CRACKED AT AFT O/B FASTENER AT STA XOLDI 6.225. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.SDR UPS98827860Doubler · crackedINSPECTION TYPE-C, LT WING L/E LWR ACCESS PANEL DOUBLER CRACKED BETWEEN STA'S XFS 303 AND XFS 310.25. REMOVED, FABRICATED AND INSTALLED DOUBLER IAW DWG 5641252 AND SRM 51-1-20D AND 51-1-21.SDR UPS98827704Battery Pack · dischargedINSPECTION TYPE-N/A, EMERGENCY LIGHTS WILL NOT TEST. REMOVED AND REPLACED EMERGENCY LIGHTS BATTERY PACKS, OPS CK GOOD PER MM 34-50-01. (P/N 60-1223-5) (S/N 356) ON, (P/N 5708458-503) (S/N UPS2964) OFF.SDR DHL98807007Cap · missingSUSPECT FUEL LEAK IN NR 4 MAIN TANK AS VERIFIED BY VISUAL INDICATIONS AND LOSS OF FUEL BY GAUGE. FOUND OVERWING FUEL CAP MISSING ON PANEL 606A.SDR DHL98801004Antenna · inoperativeWEATHER RADAR INOP. REPLACED ANTENNA PER MM.SDR DHL9880411CCowl · crackedAT C-CHECK, NR 2 STRUCTURE FIXED LEFT SIDE COWL PRIMARY COWL UPPER AFT END CORNER CRACKED. REMOVED CRACKED CHANNEL AND FABRICATED AND INSTALLED NEW CHANNEL PER SRM 51-1-4, 5 X 1.5. N/R 506SDR DHL9880409CFairing · crackedAT C-CHECK, RIGHT WING, WING TO BODY FAIRING AT BS 680 SUPPORT STRUCTURE HAS METAL LINES CRACKED. REMOVED SUPPORT AND FABRICATED AND INSTALLED PER MM 51-1-8. N/R 403SDR DHL9880425CPanel · delaminatedAT C-CHECK, LEFT WING UPPER T/E PANEL AT XW 0 TO XRS 22.750 AFT OF REAR SPAR HAS DENTS WITH DELAMINATION. REMOVED AND INSTALLED NEW PANEL PER SRM 51-3-0. N/R 028SDR DHL9880424CFitting · crackedAT C-CHECK, RT WHEEL WELL LONGERON 24 VERTICAL FITTING AT STA 940 CRACKED. REMOVED AND REPLACED FITTING PER SRM 51-1-8. N/R 833SDR DHL9880423CFitting · crackedAT C-CHECK, RT WHEEL TRAPAZOIDAL FITTING CRACKED. FABRICATED TEMPLATE AND RELOCATED HOLES FROM OLD FITTING. INSTALLED PER S/B 53-61. N/R 832SDR DHL9880422CFitting · crackedAT C-CHECK, RT WHEEL WELL LONGERON 24 VERTICAL FITTING IS CRACKED. REMOVED CRACKED FITTING AND INSTALLED FITTING PER SRM 51-1-20D, 51-3-0. N/R 831
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