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.

SDR RRXA98371Skin · crackedDURING A MAINTENANCE VISIT, FOUND RIGHT WING, LEADING EDGE, LOWER SKIN SURFACE WITH .55 INCH CRACK, AT STA XFS 526.76. REMOVED DAMAGED SECTION, FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA APPROVED TIMCO ENGINEERING SKETCH REO-05316.Aug 21, 1998 · N603AL · Doug DC873F · Wing, Plate/SkinSDR UPS98827487Fitting · gougedFLAP SPLIT AFTER REACHING 35 DEG POSITION. AT 35 DE. FLAPS WERE WITHIN 4 DEG. FOUND LEFT CENTER FLAP ACTUATOR DISCONNECTED AT ROD END, BOLT MISSING. LEFT CENTER FLAP FITTING GOUGED. REPLACING ACTUATOR AND FITTING.Aug 20, 1998 · N805UP · Doug DC873F · Trailing Edge Flap ActuatorSDR RRXA98372Fitting · damagedDURING A MAINTENANCE VISIT, FITTING (P/N 5616132-2), AT WHEEL WELL AND LONGERON 24 RIGHT FOUND DAMAGED. REMOVED FITTING, FABRICATED NEW FITTING BY MATERIAL SUBSTITUTION. ORIGINAL MATERIAL 7075-T411, SUBSTITUTED WITH 7075T-T6 IAW FAA APPROVED TIMCO ENGINEERINAug 20, 1998 · N603AL · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL9880323CFloor · puncturedAT C CHECK, AFT LOWER CARGO COMPT FLOOR BETWEEN STA 520- 560 HAS PUNCTURES AND SCRATCHES. REMOVED AND INSTALLED NEW PANEL PER SRM 25-51-1, N/R 365.Aug 20, 1998 · N803DH · Doug DC873F · Fuselage Floor PanelSDR UPS98827636Clip · crackedINSPECTION TYPE C-CK, MAIN CABIN STA 759 SEAT TRACK E ATTACH CLIP CRACKED. REMOVED 7 REPLACED ATTACH CLIP FITTING IAW DC8 SRM 51-1-2, 51-1-20D.Aug 19, 1998 · N806UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS98827605Clip · crackedINSPECTION TYPE C-CK, SEAT TRACK FRAME ATTACH CLIP CRACKED. REMOVED ATTACH CLIP FITTING IAW DC8 SRM 51-3-0. INSTALLED NEW FITTING SRM 51-3-0.Aug 19, 1998 · N806UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS98827603Clip · crackedINSPECTION TYPE C-CK, SEAT TRACK E STA 781 XCW-29 FRAME ATTACH CLIP CRACKED. REMOVED AND REPLACED SEAT TRACK E IAW 51-1-20, DC8 SRM 51-3-0.Aug 19, 1998 · N806UP · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA98386Trap Panel · damagedDURING GROUND SERVICE, FOUND AILERON BUS CABLE CUT THROUGH LEFT SIDE OF TRAPEZOIDAL PANEL, (P/N 5616481), LEFT WHEEL WELL AT STA 865. REMOVED AND REPLACED CABLE SECTION. FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA APPROVED TIMCO DER ENGINEERING SKETCH Aug 18, 1998 · N2674U · Doug DC873F · Wing Miscellaneous StructureSDR UPS98827638Frame · corrodedINSPECTION TYPE C-CK, FRAME AT FS 870 LOWER LT SKIN PANEL HAS CORROSION AT RB ATTACHMENT. REMOVED DAMAGED SECTION OF FRAME, FORMED FRAME AND SPLICE IAW REO 0530 1 AND DC8 SRM 51-1-4. HEAT TREATED FRAME AND SPLICE, REMOVED INTERCOSTAL TO ALLOW ACCESS. FAB FRAug 17, 1998 · N806UP · Doug DC873F · Fuselage Main, FrameSDR UPS98827637Angle · corrodedINSPECTION TYPE C-CK, FRAME SUPPORT ANGLE STA 865 HAS CORROSION IN LOWER LEG, DOUBLER HAS CORROSION OUTER AND INNER SKIN PANEL. REMOVED CORROSION IAW DC8 SRM 51-1-8, OUT OF LIMITS IAW DC8 SRM 53-2-0 FOR MED INTERCOSTAL IAW DC8 SRM 51-1-4 AND DAC DWG 5616306. Aug 17, 1998 · N806UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS98827607Seat Track · corrodedINSPECTION TYPE C-CK, SEAT TRACK STA 1300 C TRACK HAS CORROSION. REMOVED DAMAGED AREA OF SEAT TRACK, SPLICED NEW TRACK IAW DC8 SRM 53-2-3.Aug 17, 1998 · N806UP · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR UPS98827597Frame · corrodedINSPECTION TYPE-C CK, LWR FRAME AT FS 857 LT HAS CORROSION AND CRACK ON RADIUS ON INTERCOSTAL (ABF SENSE ANTENNA SUPPORT ATTACHMENT ANGLE). REMOVED AND REPLACED INTERCOSTAL AND REPAIRED RIB WITH STACKED ANGLE REPAIR IAW REO-05372 DC8 SRM 53-2-0 FIG 1B. ALODIAug 17, 1998 · N806UP · Doug DC873F · Fuselage Main, FrameSDR DHL9880328CIntercostal · crackedAT C CHECK, NR 1 PIT DOOR COVER LOWER FILET CORNER INTERCOSTAL CRACKED. REMOVED, FABRICATED AND INSTALLED NEW INTERCOSTAL PER SRM 51-1-21. N/R 1025.Aug 17, 1998 · N803DH · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL9880327CCover · crackedAT C CHECK, RT T/E FLAP O/B FLAP I/B HINGE SUPPORT BRACKET STA 204.125, UPPER AREA RUB COVER IS CRACKED. REMOVED AND FABRICATED AND REPLACED COVER PER SRM 51-3-0. N/R 1023.Aug 17, 1998 · N803DH · Doug DC873F · Wing Miscellaneous StructureSDR DHL9880326CAngle · crackedAT C CHECK, RT WING T/E FLAP WELL LOWER AREA AT STA 178. FOUND CRACK ON ANGLE SUPPORT INBOARD AREA NEXT TO FAIRING CUTOUT. REMOVED AND FABRICATED NEW ANGLE PER SRM 51-1-21. N/R 1022.Aug 17, 1998 · N803DH · Doug DC873F · Wing Miscellaneous StructureSDR UPS98827582Fitting · crackedINSPECTION TYPE-C CK, MAIN CABIN STA 759XC-46 AT TOP OF L/W TANK FLOORBEAM ATTACH FITTING CRACKED. REMOVED AND REPLACED CRACKED FITTING.Aug 16, 1998 · N806UP · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL9880316CFrame · crackedAT C CHECK, LT FWD LOWER EMERG EXIT DOOR CUTOUT FRAME CRACKED. REPAIRED FRAME PER SRM 51-1-19, N/R 671.Aug 16, 1998 · N803DH · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS98827426Light · inoperativeEMER EXIT LIGHTS INOP. ALLOWED SUFFICIENT TIME FOR BATTERY PACK TO R-CHARGE, SYS OPS CHK NORMAL.Aug 13, 1998 · N801UP · Doug DC873F · Emergency LightingSDR UPS98827421Battery Pack · dischargedEMER LIGHTS BATTERY AND RELAY UNIT CHANGED PER MMOC REQUEST (CAUTIONARY). REMOVED AND REPLACED EMER LIGHTS BATTERY PACK AND RELAY UNIT PER 33-50-01, OPS CHECK GOOD.Aug 13, 1998 · N801UP · Doug DC873F · Emergency LightingSDR DHL9880310CBulkhead Web · crackedAT C CHECK, MAIN CARGO AFT PRESSURE BULKHEAD WEB CRACKED IN 2 PLACES BETWEEN L 10L AND L11L, ONE CRACK 3 INCHES LONG FROM LBL 25 TO LBL 28 AND FROM LBL 34 TO LBL 36. CUT OUT DAMAGED AREA AND FABRICATED NEW REAPIR PER DACO DRWING SR 08530007, 16 BY 29. REPAIRAug 13, 1998 · N803DH · Doug DC873F · Fuselage Main, BulkheadSDR DHL9880302CSkin · crackedAT C CHECK, PANEL ON LT FAIRING 564B UPPER AILERON SURFACE OUTER SKIN FWD EDGE CRACKED. STOP DRILLED CRACK, FABRICATED EXTERNAL DOUBLER 1.0 BY 3.5 PER SRM 55-2-0. N/R 1013.Aug 13, 1998 · N803DH · Doug DC873F · AileronsSDR UPS98827622Angle · corrodedINSPECTION TYPE C-CK, LAV SEAT CONTAINER BOTTOM ATTACH ANGLES HAS CORROSION AND BARE METAL ON BOTTOM SIDE. REMOVED CORROSION IAW DC8 SRM 51-1-8, FAB ANGLES IAW DOUGLAS DWG DC-8- 380-001. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED IAW DC8 SRM 51-1-21.Aug 10, 1998 · N806UP · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA99622Stiffener · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION ON STIFFENER AND MISSING LOWER FLANGE CORNER AT STA 970 TO 980, BL 30R. DAMAGE EXCEEDED LIMITATIONS IAW DC8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FRAME IAW DAC DRG 5646Aug 10, 1998 · N603AL · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA99616Flfoorbeam · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION ON UPPER LEG ON FLOORBEAM FWD AT STA 1280, BL 60R. DAMAGE EXCEEDED LIMITATIONS IAW DC8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR TO DAMAGED FLOORBEAM IAW TIMCO DWG DC-8Aug 10, 1998 · N603AL · Doug DC873F · Fuselage Main, Floor BeamSDR UPS98827600Fitting · crackedINSPECTION TYPE C-CK, UPPER FITTING AT FS 920 ABOVE LONG 24L HAS CRACK. REMOVED EXISTING FITTING, DRILLED NEW FITTING IAW DC8 SRM 51-3-2. FITTING INSTALLATION TO BE COMPLETED ON UPS N/R 840692.Aug 9, 1998 · N806UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS98827599Fitting · crackedINSPECTION TYPE C-CK, UPPER FITTING AT FS 940 ABOVE LONGERON 24 HAS CRACK IN ATTACHMENT HOLES. REMOVED EXISTING FITTING AND DRILLED NEW FITTING IAW DC8 SRM 51-3-2. FITTING INSTALLATION TO BE COMPLETED ON N/R 840692.Aug 9, 1998 · N806UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS98827598Fitting · crackedINSPECTION TYPE-C CK, AFT CARGO UPPER FITTING AT FS 960 ABOVE LONGERON 24L HAS CRACK IN ATTACHMENT HOLE. REMOVED EXISTING FITTING, DRILLED NEW FITTING IAW DC8 SRM 51-3-2. FITTING INSTALLATION TO BE COMPLETED ON UPS N/R 840692.Aug 9, 1998 · N806UP · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL9880317DDump Well · crackedAT C CHECK, FUEL DUMP WELL AREA CRACKED. STOP DRILLED CRACK, FABRICATED REPAIR PER SRM 51-1-21, .5 BY 5.5, N/R 755.Aug 9, 1998 · N803DH · Doug DC873F · Wing Miscellaneous StructureSDR DHL9880301CStringer · corrodedAT C CHECK, STRINGER 35 JUST FWD OF AIR COND COMPT DOOR CUT OUT HAS LT SIDE CORROSION. REMOVED CORRODED INTERCOSTAL BETWEEN 8 AND 35 AND INSTALLED NEW PER SRM 51-1-21. N/R 893.Aug 9, 1998 · N803DH · Doug DC873F · Fuselage Main, Longeron/StringerSDR DHL9880333CFloor · crackedAT C CHECK, PANEL ON RACK NR 1 A, B FLOOR PANEL NR 5 RT STA 50-62 DIRTY AND CRACKED. FABRICATED DOUBLER REPAIR PER SRM 51-4-1. INSTALLED PER SRM 51-1-21. N/R 826.Aug 8, 1998 · N803DH · Doug DC873F · Fuselage Floor PanelSDR DHL9880332CThreshold · crackedAT C CHECK, PANEL RACK NR 1 A,B LT MID SERVICE DOOR THRESHOLD PLATE HAS CRACK EDGE. WELDED PER DPS 10.225. N/R 827.Aug 8, 1998 · N803DH · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL9880331CThreshold · crackedAT C CHECK, RT FWD SERVICE DOOR THRESHOLD PLATE HAS TWO CRACKS. CLEANED AND WELDED PER DPS 10.225. N/R 826.Aug 8, 1998 · N803DH · Doug DC873F · Fuselage Main, Plate/SkinSDR DHL9880330CThreshold · bentAT C CHECK, PANEL ON RACK NR 1 RT MID SERVICE DOOR STA 1080 THRESHOLD PLATE INBD EDGE IS BENT AND RT END HAS CRACK. WELDED PLATE PER DOUGLAS PROCESS STANDARDS 10.225. N/R 825.Aug 8, 1998 · N803DH · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL9880329CThreshold · crackedAT C CHECK, PANEL ON RACK NR 1 A, B LT AFT SERVICE DOOR THRESHOLD PLATE HAS CRACK AT SIDE OF PREVIOUS WELD REPAIR AND SPOT OF BULGE. REMOVED AND REPAIRED THRESHOLD PLATE PER SRM 51-1-8, N/R 824.Aug 8, 1998 · N803DH · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL9880321CFairing · crackedAT C CHECK, RT WING TO BODY FAIRING NR 262G CRACKED AT INTERNAL FWD CORNER. FABRICATED REAPAIR DOUBLER, 3 BY 2 PER SRM 53-2-0, N/R 874.Aug 8, 1998 · N803DH · Doug DC873F · Aerodynamic FairingsSDR DHL9880320CFloor · crackedAT C CHECK, PANEL ON RACK NR 2 FLOOR PLATE, STA 25/45, DOUBLER CRACKED. REMOVED AND REPLACED DOUBLER PER SRM 51-1-4, 7 BY 3. N/R 821.Aug 8, 1998 · N803DH · Doug DC873F · Fuselage Floor PanelSDR DHL9880319CSkin · missingAT C CHECK, LT WING UPPER SURFACE AT REAR SPAR STA APPROX 337 MISSING SHEETMETAL. FABRICATED NEW SECTION OF STRIP AND INSTALLED PER SRM 51-1-8, 20 BY .25, N/R 754.Aug 8, 1998 · N803DH · Doug DC873F · Wing, Plate/SkinSDR DHL9880303CFloor · corrodedAT C CHECK, MAIN CARGO COMPT AFT LOWER FLOOR AREA AT STA 1700-1730 FLOOR PANELS DETERIORATED AND CORRODED UPPER AND LOWER SURFACES. FABRICATED REPAIR FOR ANGLE SUPPORT PER SRM 51-1-4, 2 BY 3FT, N/R 808.Aug 8, 1998 · N803DH · Doug DC873F · Fuselage Floor PanelSDR UPS98827641Bracket · crackedINSPECTION TYPE C-CK, LT MLG WHEEL WELL STA 857 ABOVE REAR SPAR, CORNER BRACKET HAS A VISIBLE CRACK THROUGH RADIUS AND FASTENER HOLES O/B SIDE OF I/B PRESSURE PANEL. REMOVED AND REPLACED BRACKET IAW DC8 SRM 51-1-24 AND 51-1-20D.Aug 7, 1998 · N806UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS98827640Angle · corrodedINSPECTION TYPE C-CK, LT MLG WHEEL WELL, STA 857 ANGLE ABOVE REAR SPAR HAS CORROSION ON FWD SIP AT JUST O/B OF I/B PRESSURE PANEL 48 IN LT OF C/L. REMOVED CORROSION WAS OUT OF LIMITS. REMOVED AND REPLACED ANGLE IAW DC8 SRM 51-1-8/ 51-1-20D/ 53-2-0.Aug 7, 1998 · N806UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS98827633Splice · corrodedINSPECTION TYPE C-CK, MAIN CABIN STA 1000 FLOORBOARD B SPLICE HAS CORROSION. REMOVED CORROSION FROM SPLICES IAW DC8 SRM 51-1-8. FOUND SPLICES TO BE OUT OF LIMITS MAT ID IAW DC8 SRM 53-7-3 7075-T6 .090 PO 263213. FABRICATED PARTS IAW DC8 SRM 53-7-3. ALODINEAug 7, 1998 · N806UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS98827629Floorbeam · crackedINSPECTION TYPE C-CK, MAIN CABIN STA 920 FLOORBEAM AT SCW-40 CRACKED AND HAS CORROSION. CUT OUT DAMAGED AREA IAW REO 05244, FAB AND DRILLED REPAIR ANGLE, STRAP AND FILLER IAW REO 05244. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED REPAIR ANGLE STRAP ANAug 7, 1998 · N806UP · Doug DC873F · Fuselage Main, Floor BeamSDR UPS98827627Floorbeam · corrosionINSPECTION TYPE C-CK, MAIN CABIN STA 902 FLOORBEAM AT XCW-39 CRACKED AND HAS CORROSION. BLENDED OUT CORROSION TO UPPER FWD FLANGE LWR SURFACE IAW DC8 SRM 53 -2-0 MAT ID 7075-T6 .125 REPAIR STRAP, FILLER 7075-T6 .090 PO 248989 , 263213. FAB REPAIR STRAP IAW RAug 7, 1998 · N806UP · Doug DC873F · Fuselage Main, Floor BeamSDR UPS98827626Floorbeam · corrosionINSPECTION TYPE C-CK, MAIN CABIN STA 822 XCW-30 FLOORBEAM HAS CORROSION. REMOVED CORROSION AND DOCUMENTED REMAINING MAT THICK ON REO 05281, MAT ID .190 7075-T6 PO 234881 FOR FILLER AND 60-4139 L-ANGLE EXTRUSION 7075-T6 511 FOR REPAIR ANGLE. TRIMMED DAMAGE, FAug 7, 1998 · N806UP · Doug DC873F · Fuselage Main, Floor BeamSDR UPS98827625Floorbeam · corrodedINSPECTION TYPE C-CK, MAIN CABIN STA 781 SCW-29 AND -36 FLOORBEAM HAS CORROSION AROUND PLATE. REMOVED DAMAGED AREA IAW REO 05223, FABBED FILLER AND L-ANGLE IAW REO 0 5223. LOCATED AND DRILLED UP L-ANGLE AND FILLER IAW REO 05223. ALODINED AND PRIMED IAW DC8 Aug 7, 1998 · N806UP · Doug DC873F · Fuselage Main, Floor BeamSDR UPS98827623Frame · corrodedINSPECTION TYPE C-CK, MAIN CABIN STA 781 XCW0 FRAME HAS CORROSION AT SEAT TRACK ATTACH POINT. REMOVED BOLT STA 781 IAW DC8 SRM 51-3-0. REMOVED CORROSION IAW DC8 SRM 51-1-8. MAT REMOVED OUT OF LIMITS IAW DC8 SRM 53-2-0. FAB FLOORBEAM REPAIR ANGLE, SUPPORT RAug 7, 1998 · N806UP · Doug DC873F · Fuselage Main, FrameSDR UPS98827619Seat Track · corrosionINSPECTION TYPE C-CK, MAIN CABIN STA 879 TO 1080 SEAT TRACK A HAS CORROSION. REMOVED CORROSION IAW DC8 SRM 51-1-8. NOT WITHIN LIMITS IAW DC8 SRM 53-2-3. REMOVED DAMAGED SECTION OF SEAT TRACK STA 590 TO 1030, DRILLED NEW SECTION IAW DC8 SRM 51-1-4. ALODINEDAug 7, 1998 · N806UP · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR UPS98827604Clip · crackedINSPECTION TYPE C-CK, MAIN CABIN STA 759 XCW-26 UNDER AFT SIDE SEAT TRACK E FITTING FRAME ATTACH CLIP CRACKED. REMOVED ATTACH CLIP (FITTING) IAW DC8 SRM 51-1-2 & 51-1-20D. LOCATED AND DRILLED NEW FITTING (P/N 375522-1) PO NR 267866 IAW DC8 SRM 51-3-2. INSTAug 7, 1998 · N806UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS98827602Fitting · crackedINSPECTION TYPE C-CK, MAIN CABIN STA 781 XCWX29 UNDER SEAT TRACK C FRAME ATTACH CLIP CRACKED. REMOVED ATTACH CLIP (FITTING) IAW DC8 SRM 51-1-2 & 51-1-20D. LOCATED AND DRILLED NEW FITTING (P/N 3773906-1), PO NR 267861 IAW DC8 SRM 51-3- 2. INSTALLED NEW FITTIAug 7, 1998 · N806UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS98827601Clip · crackedINSPECTION TYPE C-CK, MAIN CABIN STA 822 XCW-29 UNDER SEAT TRACK E FRAME ATTACH CLIP CRACKED. REMOVED ATTACH CLIP (FITTING) IAW DC8 SRM 51-1-2 & 51-1-20D. LOCATED AND DRILLED NEW FITTING (P/N 373906-1) PO NR 267866 IAW DC8 SRM 51-3-2. INSTALLED NEW FITTING Aug 7, 1998 · N806UP · Doug DC873F · Fuselage Miscellaneous Structure
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