Douglas DC-8-73F

Service difficulty reports · 15,471

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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.

SDR DHL9980605CSkin · delaminatedAT C CHECK, RIGHT WING FLIGHT SPOILER NR 2 IS DELAMINATED REMOVED AND REPLACED FLIGHT SPOILER PANEL NR 2 IAW DC8 MM 27-60-1 PG 201. PERFORMED ADJUSTMENT AND OPS CK IAW DC8 MM 27-60 PG 501, NR CARD NR 0053.Aug 23, 1999 · N806DH · Doug DC873F · SpoilersSDR DHL9980604CPanel · delaminatedAT C CHECK, LT WING UPPER SIDE T/E PANEL DELAMINATED LOCATED AT IB AILERON AREA BETWEEN XW 589 TO XW 624. REMOVED DELAMINATED PANEL FROM XW 589 TO XW 624. INSTALLED OVERHAULED PANEL IAW DC8 SRM 51-1-15 PG 1. NR CARD NR 0052.Aug 23, 1999 · N806DH · Doug DC873F · Wing, Plate/SkinSDR DHL9980603CPanel · delaminatedAT C CHECK, RIGHT WING LOWER T/E AILERON POWER PACK PANEL IS DELAMINATED. REMOVED DELAMINATED PANEL AT RT WING LOWER SURFACE T/E POWER PACK ACCESS IAW DC8 SRM 51-3-0 PG 2 FIG 52A. INSTALLED REPAIRED PANEL IAW DC8 SRM 51-3-0 PG 1. NR CARD NR 0049.Aug 23, 1999 · N806DH · Doug DC873F · Wing, Plate/SkinSDR DHL9980602CPanel · delaminatedAT C-CHECK, RT WING LOWER T/E PANEL APPROX STA 670 DELAMINATED. REMOVED AND REPLACED PANEL IAW DC8 SRM 51-3-0, N/R CARD NR 0048.Aug 23, 1999 · N806DH · Doug DC873F · Wing, Plate/SkinSDR DHL9980601CSkin · delaminatedAT C CHECK, RT WING AIL CONTROL TAB DELAMINATED. REMOVED AND REPLACED CONTROL TAB PER DC8 MM 27-11-4 PG 201. NR CARD NR 0047Aug 23, 1999 · N806DH · Doug DC873F · Aileron TabsSDR UPS99830436Clip · crackedINSPECTION TYPE:C123, FS 1620 AND LONG 14R, THE INTERCOSTAL ATTACH CLIP WAS CRACKED. REMOVED, FABRICATED AND REPLACED THE CLIP IAW DWG 5772656 AND SRM 51-1-21.Aug 21, 1999 · N867UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS99830433Splice · crackedINSPECTION TYPE:C1, RT WING L/E SPLICE AT XFS 710 WAS CRACKED. REMOVED, FABRICATED AND REPLACED THE SPLICE IAW SRM 57-3-3 AND 51-3-0.Aug 21, 1999 · N813UP · Doug DC873F · Wing Miscellaneous StructureSDR UPS99830435Skin · crackedINSPECTION TYPE:C123, THE RT I/B UPPER SLOT SKIN WAS CRACKED AT THE SPLICE PAN, UNDER THE UPPER SLOT DOOR. REMOVED, FABRICATED AND REPLACED THE SLOT SKIN IAW DWG 5769859 AND SRM 51-1-21 AND 51-3-0.Aug 20, 1999 · N867UP · Doug DC873F · Trailing Edge FlapsSDR UPS99830412Battery Pack · dischargedINSPECTION TYPE:N/A, EMERGENCY LIGHTS INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT'S BATT PACK. OPS CHECK GOOD.Aug 20, 1999 · N802UP · Doug DC873F · Emergency LightingSDR RRXA991510Floor Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, UPPER CARGO COMPARTMENT FLOOR PANEL CORRODED (EXFOLIATION) REQUIRES REPAIR DOUBLERS. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. REPAIRED FLOOR PANELS IAW DC8 Aug 20, 1999 · N791FT · Doug DC873F · Fuselage Floor PanelSDR RRXA991508Floor Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, UPPER CARGO COMPARTMENT FLOOR PANEL CORRODED (EXFOLIATION) REQUIRES SKIN REPLACEMENT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FILLED GAP WITH HYSOLEA934NA.Aug 20, 1999 · N791FT · Doug DC873F · Fuselage Floor PanelSDR UPS99830485Skin · corrodedINSPECTION TYPE:C3, R-2 DOOR CUTOUT FUSELAGE SKIN, UNDER SCUFF PLATE HAS CORROSION. REMOVED CORROSION IAW DC8 SRM 51-1-8, ORIGINAL MATL .080 REMAINING MATL .049 NOT WITHIN LIMITS IAW DC8 SRM 53-2-0. FABBED DOUBLER, LOCAT ED, DRILLED, COUNTERSUNK, DEBURRED IAAug 19, 1999 · N801UP · Doug DC873F · Fuselage Main, Plate/SkinSDR UPS99830383Fitting · crackedINSPECTION TYPE:C1 THE INTERCOSTAL TO FRAME ATTACH FITTING IS CRACKED AT FS 680, AT LONGERON 11R. REMOVED AND REPLACED THE FITTING IAW SRM 51-1-20D.Aug 19, 1999 · N813UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS99830382Fitting · crackedINSPECTION TYPE:C1 THE LONGERON 32R SPLICE FITTING AT FS 450 IS CRACKED. REMOVED AND REPLACED THE SPLICE FITTING IAW SRM 51-1-20D.Aug 19, 1999 · N813UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS99830376Doubler · crackedINSPECTION TYPE:C1 RT WING L/E LWR SKIN INTERNAL DOUBLER AT XFS 336 IS CRACKED AT THE DRAIN HOLE. REMOVED, FABRICATED, AND REPLACED DOUBLER IAW DWG 5769589 AND SRM 51-1-20D AND 51-1-21.Aug 19, 1999 · N813UP · Doug DC873F · Wing Miscellaneous StructureSDR RRXA991498Support · damagedDURING A MAINTENANCE VISIT, REMOVED AND REPLACED FLAP LINK SUPPORT ASSY LT MID STA 219. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. REMOVED AND REPLACED FLAP LINK SUPPORT IAW DC8 M/M 27-51-12 AND FAA APPROVED TENNAug 19, 1999 · N791FT · Doug DC873F · Trailing Edge Flap ActuatorSDR UPS99830547Intercostal · crackedINSPECTION TYPE:C3, LEFT WING, TRAILING EDGE STA 339, INTERCOSTAL CRACKED FITTING CHAFED OUT OF LIMITS. REMOVED INTERCOSTAL, FABRICATED AND INSTALLED INTERCOSTAL AND NEW SUPPORT FITTING (P/N 5707538-3) IAW DC8 SRM 57-5-1 & 51-1-21.Aug 18, 1999 · N801UP · Doug DC873F · Wing Miscellaneous StructureSDR RRXA991494Skin · crackedDURING A MAINTENANCE VISIT FOUND RT W/W FWD PRESS WEB CRACKED IN RECESS OF REMOVEABLE PANEL O/B OF PANEL AT STA 849 XCW 64. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW PRESSURE WEB IAWAug 18, 1999 · N791FT · Doug DC873F · Fuselage Main, Plate/SkinSDR RRXA991492Door Track · bentDURING A MAINTENANCE VISIT FOUND A PIT RT TRACK WORN AND BENT AT STA 360. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. REPAIRED TRACK IAW FAA APPROVED TENNESSEE TECHNICAL SERVICES DER ENGINEERING SKETCH NR EO-99-10Aug 18, 1999 · N791FT · Doug DC873F · Cargo/Baggage DoorsSDR DHL99802001Static Wicks · damagedIN PRECIP BOTH VHF AND HF WILL TRANSMIT BUT NOT RECEIVE. REPLACED 10 STATIC WICKS AND NR 1 VHF ANTENNA PER MM 23-60-0 AND 23-10-0.Aug 18, 1999 · N802DH · Doug DC873F · Static Discharge SystemSDR RRXA991493Panel · missingDURING A MAINTENANCE VISIT FOUND ROBBED PYLON PANEL ASSY FOR A/C N8085U NR 3 PYLON (EO). DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW PANEL IAW FAA APPROVED TENNESSEE TECHNICAL SERVICESAug 17, 1999 · N791FT · Doug DC873F · Nacelle/Pylon, Plate/SkinSDR UPS99830333Window · failedINSPECTION TYPE:N/A, CAPTINS CLEARVIEW SIDE WINDOW ARCING. REMOVED AND REPLACED CAPTAINS CLEARVIEW WINDOW IAW MM 56-10-03. TEST ED PER 56-10-03. SYSTEM OPS CK NORMAL.Aug 16, 1999 · N819UP · Doug DC873F · Flight Compartment WindowsSDR UPS99830331Battery Pack · dischargedINSPECTION TYPE:IN, EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY PACK, ON (P/N 60-12 23-5) (S/N 321), OFF (P/N 5708458-503) (S/N 001).Aug 16, 1999 · N807UP · Doug DC873F · Emergency LightingSDR RRXA991422Skin · crackedDURING A MAINTENANCE VISIT, FOUND RT W/W FWD PRESS WEB CRACKED IN RECESS OF REMOVABLE PRESS PANEL O/B OF PANEL BETWEEN STA 849 - XCW 64. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW WEBAug 16, 1999 · N604AL · Doug DC873F · Fuselage Main, Plate/SkinSDR UPS99830504Fitting · corrodedINSPECTION TYPE:C1, BATH TUB FITTING FS 280, LONG 33R TO 34R IS CORRODED OUT OF LIMITS. REMOVED AND REPLACED THE FITTING IAW SRM 51-1-20D.Aug 15, 1999 · N813UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS99830432Jamb · crackedINSPECTION TYPE:C1, THE RT FWD SERVICE DOOR JAMB AT LONG 19R, AT THE LWR AFT CORNER OF THE JAMB IS CRACKED BEYOND LIMITS, FS 192. CUT OUT THE DAMAGED AREA AND REPAIRED THE WEB IAW SRM 53-2-0.Aug 15, 1999 · N813UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS99830389Longeron · corrodedINSPECTION TYPE:C2 LONGERON 5R AT FS -12 TO 8 IS CORRODED BEYOND LIMITS. CUT OUT DAMAGED SECTION AND SPLICED IN A NEW LONGERON IAW SRM 53-2-2.Aug 15, 1999 · N813UP · Doug DC873F · Fuselage Main, Longeron/StringerSDR UPS99830524Splice · crackedINSPECTION TYPE:C1, LONGERON 34R SPLICE FITTING AT FS 640 TO 660 IS CRACKED. REMOVED, FABRICATED AND REPLACED THE SPLICE FITTING IAW SRM 51-3-0 AND DWG 5800471.Aug 14, 1999 · N813UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS99830503Splice · crackedINSPECTION TYPE:C1, THE LONGERON 30R SPLICE FITTING AT FS 640 TO 660 IS CRACKED. REMOVED AND REPLACED THE FITTING IAW SRM 51-1-20D.Aug 14, 1999 · N813UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS99830499Frame · corrodedINSPECTION TYPE:C123, FS 1040 FRAME CAP IS CORRODED BEYOND LIMITS BETWEEN LBL 28 TO RBL 28. REMOVED AND REPLACED THE FRAME CAP IAW SRM 51-1-20D.Aug 14, 1999 · N867UP · Doug DC873F · Fuselage Main, FrameSDR UPS99830431Doubler · corrodedINSPECTION TYPE:C2, THE FINGER DOUBLER AT FS -12 TO -32 AT LONG 21L IS CORRODED BEYOND LIMITS. CUT OUT DAMAGED SECTION OF THE FINGER DOUBLER, FABRICATED A REPLACEMENT SECTION AND INSTALLED IAW SRM 53-3-3 FIG 1 & SRM 51-1-21.Aug 14, 1999 · N813UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS99830409Rib · crackedINSPECTION TYPE:C234, RT WING L/E RIB AT XFS 640 WAS CRACKED AT THE AFT LWR FASTENER. STOP DRILLED CRACK AND REPAIRED THE RIB IAW SRM 57-2-0 FIG 2.Aug 14, 1999 · N867UP · Doug DC873F · Wing, Rib/BulkheadSDR UPS99830430Fitting · crackedINSPECTION TYPE:C1, LONG 35R SPLICE FITTING AT FS 1040 TO 1060 IS CRACKED. REMOVED AND REPLACED THE FITTING IAW SRM 51-1-20D.Aug 13, 1999 · N813UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS99830429Fitting · crackedINSPECTION TYPE:C1, LONG 31L SPLICE FITTING AT FS 1040 TO 1060 WAS CRACKED. REMOVED AND REPLACED THE FITTING IAW SRM 5-1-20D.Aug 13, 1999 · N813UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS99830428Fitting · crackedINSPECTION TYPE:C1, THE RT O/B SLOT, LWR DOOR, INNER FITTING IS CRACKED AT XS 475. REMOVED AND REPLACED THE FITTING IAW SRM 51-1-21.Aug 13, 1999 · N813UP · Doug DC873F · Trailing Edge FlapsSDR UPS99830390Fitting · crackedINSPECTION TYPE:C1 LONGERON 31R SPLICE FITTING IS CRACKED AT FS 1040 TO 1060. REMOVED AND REPLACED THE SPLICE FITTING IAW SRM 51-1-20D.Aug 13, 1999 · N813UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS99830393Rib · crackedINSPECTION TYPE:C1 RT WING L/E RIB AT XFS 316.5 IS CRACKED AT THE AFT UPPER FASTENER. STOP DRILLED CRACK AND REPAIRED THE RIB IAW SRM 57-2-0.Aug 12, 1999 · N813UP · Doug DC873F · Wing, Rib/BulkheadSDR UPS99830392Rib · crackedINSPECTION TYPE:C1 LT WING L/E RIB AT XS 454.976 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED THE RIB IAW SRM 57-2-0.Aug 12, 1999 · N813UP · Doug DC873F · Wing Miscellaneous StructureSDR UPS99830391Rib · crackedINSPECTION TYPE:C1 RT WING L/E RIB AT XFS 366.5 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED THE RIB IAW SRM 57-2-0.Aug 12, 1999 · N813UP · Doug DC873F · Wing, Rib/BulkheadSDR UPS99830330Light · inopINSPECTION TYPE:IN, EMERGENCY EXIT LIGHT IN COCKPIT DOME AND ENTRY INOP. REMOVED AND REPLACED BATTERY PACK, CK OK. ON (P/N 5708458-503) (S/N 10389), OFF (S/N 339) (P/N 60-1223-5).Aug 12, 1999 · N803UP · Doug DC873F · Emergency LightingSDR RRXA991499Support · damagedDURING A MAINTENANCE VISIT, REMOVED AND REPLACED FLAP LINK SUPPORT ASSY LT O/B AT STA 340. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. REMOVED AND REPLACED FLAP LINK SUPPORT IAW DC8 M/M 27-51-12 AND IAW FAA APPROVAug 12, 1999 · N791FT · Doug DC873F · Trailing Edge Flap ActuatorSDR UPS99830502Longeron · corrodedINSPECTION TYPE:C1, LONGERON 34R IS CORRODED BEYOND LIMITS AT FS 270. CUT OUT DAMAGED SECTION OF LONGERON 34R BETWEEN FS 250 & 290 AND SPLICED IN A NEW SECTION IAW SRM 53-2-2 FIG 10.Aug 11, 1999 · N813UP · Doug DC873F · Fuselage Main, Longeron/StringerSDR UPS99830501Frame · crackedINSPECTION TYPE:C1, FS -131, 8 BELOW THE SUBFLOOR, THE FRAME O/B FLANGE IS CRACKED AND CORRODED. STOP DRILLED THE CRACK, REMOVED THE CORROSION, AND REPAIRED THE FRAME CAP IAW DH SK813-878. FRAME CAP WITHIN LIMITS AFTER CORROSION REMOVAL IAW SRM 53-2-0.Aug 11, 1999 · N813UP · Doug DC873F · Fuselage Main, FrameSDR UPS99830498Longeron · crackedINSPECTION TYPE:C123, LONGERON 24R IS CRACKED AT FS 940. STOP DRILLED CRACK AND REPAIRED LONGERON IAW SRM 53-2-2 FIG 5.Aug 11, 1999 · N867UP · Doug DC873F · Fuselage Main, Longeron/StringerSDR UPS99830427Stiffener · corrodedINSPECTION TYPE:C1, SPOT OF HEAVY CORROSION ON THE HORIZONTAL FITTING AT RBL 35, FS 869. REMOVED AND REPLACED THE FITTING IAW SRM 51-1-20D.Aug 11, 1999 · N813UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS99830424Fitting · crackedINSPECTION TYPE:C1, FS 759, RBL 48, THE FWD FITTING WAS CRACKED AT THE BOTTOM I/B FASTENER. REMOVED AND REPLACED THE FITTING IAW SRM 51-1-20D.Aug 11, 1999 · N813UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS99830388Doubler · crackedINSPECTION TYPE:C1 RT WING L/E LWR SKIN INTERNAL DOUBLER AT XFS 570 IS CRACKED AT THE DRAIN HOLE. REMOVED, FABRICATED, AND REPLACED THE DOUBLER IAW DWG 5769600 AND SRM 51-1-21.Aug 11, 1999 · N813UP · Doug DC873F · Wing Miscellaneous StructureSDR UPS99830387Rib · crackedINSPECTION TYPE:C1 RT WING L/E RIB AT XS 497.491 IS CRACKED AT THE AFT UPPER FASTENER. STOP DRILLED CRACK AND REPAIRED THE RIB IAW SRM 57-2-0.Aug 11, 1999 · N813UP · Doug DC873F · Wing Miscellaneous StructureSDR UPS99830386Doubler · corrodedINSPECTION TYPE:C1 FS 920 TO 902, RBL 68, THE FINGER DOUBLER HAS SEVERAL POPPED RIVET HEADS AND BULGING. REMOVED, FABRICATED, AND REPLACED THE FINGER DOUBLER IAW DWG 5645332 AND SRM 51-1-20D.Aug 11, 1999 · N813UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS99830385Rib · crackedINSPECTION TYPE:C1 RT WING L/E RIB AT XS 478.897 IS CRACKED AT THE AFT UPPER FASTENER. STOP DRILLED CRACK AND REPAIRED THE RIB IAW SRM 57-2-0 FIG 2.Aug 11, 1999 · N813UP · Doug DC873F · Wing, Rib/Bulkhead
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