Douglas DC-8-71F

Service difficulty reports · 8,938

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 = 'DC871F'
  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 UPS99828601Intercostal · crackedINSPECTION TYPE-C3, FS 1660 AT LONG 17R, THE INTERCOSTAL FLANGE IS CRACKED. REPAIRED INTERCOSTAL IAW SRM 53-2-0.Jan 18, 1999 · N713UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS99828489Shear Tie · crackedINSPECTION TYPE-C, SHEAR TIE CRACKED AT FS 1480, BETWEEN LONG 34L AND 35L. CUT OUT DAMAGED SHEAR TIE AND REPAIRED IAW SRM 53-2-0 FIG 2A.Jan 18, 1999 · N701UP · Doug DC871F · Fuselage Miscellaneous StructureSDR RRXA991018Skin · damagedDURING A MAINTENANCE VISIT, FOUND SCRAPE, CENTER FUSELAGE, SKIN/PLATE, AT STA 1360, LONGERON 23 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. BLENDED AREA IAW DC8 SRM 51-1-0, TREATED AND PRIMED IAW DC8 SRM 51Jan 18, 1999 · N8085U · Doug DC871F · Fuselage Main, Plate/SkinSDR UPS99828600Stiffener · corrodedINSPECTION TYPE-C3, FS 1160 AT LONG 33R, THE STIFFENER IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED STIFFENER IAW SRM 51-1-20D.Jan 17, 1999 · N713UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS99828599Web · corrodedINSPECTION TYPE-C3, FS 340 TO 350, LONG 33L-33R, THE TORQUE BOX WEB IS CORRODED BEYOND LIMITS. REMOVED, FABRICATED AND REPLACED WEB IAW DWG 9754007 AND SRM 51-1-20D.Jan 15, 1999 · N713UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS99828518Web · corrodedINSPECTION TYPE-C3, FS 1210 ABOVE LONG 35R, THE TORQUE BOX WEB IS CORRODED BEYOND LIMITS. REPAIRED TORQUE BOX WEB IAW EO DC8-5350-7876-A.Jan 15, 1999 · N713UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS99828517Fitting · corrodedINSPECTION TYPE-C3, DOOR JAMB BACKUP FITTING AT FS 320 BETWEEN LONG 34R AND 35R HAS SEVERE CORROSION. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.Jan 15, 1999 · N713UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS99828516Fitting · corrodedINSPECTION TYPE-C3, DOOR JAMB BACKUP FITTING AT FS 280 BETWEEN LONG 34R AND 35R HAS SEVERE CORROSION. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.Jan 15, 1999 · N713UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS99828515Fitting · corrodedINSPECTION TYPE-C3, DOOR JAMB BACKUP FITTING AT FS 220 BETWEEN LONG 32R AND 33R HAS SEVERE CORROSION. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.Jan 15, 1999 · N713UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS99828467Fitting · crackedINSPECTION TYPE:C3, STA 450 AT STR 34R, THE SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3750330 AND SRM 51-1-20D.Jan 15, 1999 · N713UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS99828463Fitting · damagedINSPECTION TYPE:C3, STA 450 AT LONG 35L, THE SPLICE FITTING IS DAMAGED. REMOVED AND REPLACED FITTING IAW DWG 3750330 AND SRM 51-1-20D.Jan 15, 1999 · N713UP · Doug DC871F · Fuselage Miscellaneous StructureSDR RRXA991299Frame · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, FRAME, BETWEEN STA 280 AND STA 287, AND BETWEEN LONGERONS 28 LEFT AND LONGERON 29 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED RJan 15, 1999 · N8085U · Doug DC871F · Fuselage Main, FrameSDR RRXA991026Angle · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION, CENTER FUSELAGE, FRAME ATTACH ANGLE, FWD PIT, AT STA 140, LONGERON 31 LEFT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED ATTACH ANGLE IAW DC8 SRJan 15, 1999 · N8085U · Doug DC871F · Fuselage Miscellaneous StructureSDR IXXA9900001Indication · malfunctionedON DESCENT INTO TOL, WHEN THE CREW EXTENDED THE LANDING GEAR, THE NOSE GEAR DOWN AND LOCK INDICATION LIGHT FAILED TO ILLUMINATE, ACCOMPANIED BY A LANDING GEAR UNSAFE LIGHT. THE CREW CYCLED THE LANDING GEAR WITH THE WARNING INDICATIONS REMAINING THE SAME. MAIJan 15, 1999 · N820BX · Doug DC871F · Landing Gear Position and WarningSDR UPS99828670Fitting · corrodedINSPECTION TYPE-C3, LONG 34L SPLICE FITTING AT FS 1260 TO 1280 IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED SPLICE FITTING IAW SRM 51-1-20D.Jan 14, 1999 · N713UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS99828596Longeron · corrodedINSPECTION TYPE-C3, LONG 31R AT FS 1600 TO 1670 IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED LONGERON FROM FS 1570 TO 1660 IAW SRM 51-1-20D.Jan 14, 1999 · N713UP · Doug DC871F · Fuselage Main, Longeron/StringerSDR UPS99828540Spacer · corrodedINSPECTION TYPE-C, AIRCRAFT STRUCTURE UNDER VERTICAL FITTING AT FS 780 AND RBL 55 IS BADLY CORRODED. REMOVED AND REPLACED SHIM PLATE IAW SRM 51-3-0.Jan 14, 1999 · N701UP · Doug DC871F · Fuselage Miscellaneous StructureSDR RRXA991033Skin · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION, WING, L/E SKIN, UNDER FASTENER RIGHT WING L/E UPPER SURFACE AT STA XFS 13.750 AT FRONT SPAR. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLEJan 14, 1999 · N8085U · Doug DC871F · Wing, Plate/SkinSDR RRXA991031Frame · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION, CENTER FUSELAGE, DOOR FRAME, R2 FWD FRAME INSIDE WEB AT STA 1680. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8.. FABRICATED AND INSTALLED FITTINGS IAW DC8 SRM 51-2-0 AND Jan 14, 1999 · N8085U · Doug DC871F · Fuselage Miscellaneous StructureSDR RRXA991029Frame · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION, CENTER FUSELAGE, FRAME, AT STA 1306 UPPER CAP UNDER NUT PLATES AND WEB BETWEEN LONGERONS 34 LEFT AND LONGERON 34 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRJan 14, 1999 · N8085U · Doug DC871F · Fuselage Main, FrameSDR RRXA991020Skin · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION, CENTER FUSELAGE, L/E SKIN, LEFT WING L/E UPPER SURFACE UNDER SCREW HEADS FROM XFS 7.50 TO XFS 32.5. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLEDJan 14, 1999 · N8085U · Doug DC871F · Wing, Plate/SkinSDR UPS99828592Doubler · corrodedINSPECTION TYPE-C3, INTERNAL DOUBLER AROUND A PIT DOOR IS CORRODED AND CUT AT LONG 31R. REMOVED, FABRICATED AND REPLACED DOUBLER IAW DWG 9754003 AND SRM 51-1-20D.Jan 13, 1999 · N713UP · Doug DC871F · Fuselage Miscellaneous StructureSDR RRXA991318Frame · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, FRAME, AT STA 1793, BETWEEN LONGERONS 35 LEFT AND LONGERON 35 RIGHT IN CHANNEL. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLERS IJan 13, 1999 · N8085U · Doug DC871F · Fuselage Main, FrameSDR RRXA991303Support · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, SUPPORT STRAP, FWD PIT BETWEEN STA 120 AND STA 140 AND BETWEEN LONGERONS 36 AND LONGERON 35 LEFT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INJan 13, 1999 · N8085U · Doug DC871F · Fuselage Miscellaneous StructureSDR RRXA991298Frame · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, FWD ACCESSORY COMPT FRAME AT STA 70, BETWEEN LONGERONS 31 LEFT AND LONGERON 33 LEFT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLJan 13, 1999 · N8085U · Doug DC871F · Fuselage Main, FrameSDR RRXA991297Angle · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, FWD PIT FRAME ATTACH ANGLE AT STA 160, LONGERON 31 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED ANGLE IAW DC8 SRM 51-2-0 FIG 50 Jan 13, 1999 · N8085U · Doug DC871F · Fuselage Miscellaneous StructureSDR RRXA991296Angle · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, FWD PIT FRAME ATTACH ANGLE AT STA 140, LONGERON 31 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED ATTACH ANGLE IAW DC8 SRM 51-1-4 Jan 13, 1999 · N8085U · Doug DC871F · Fuselage Miscellaneous StructureSDR RRXA991295Frame · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, FWD PIT FRAME AT STA 120, BETWEEN LONGERONS 30 RIGHT AND LONGERON 33 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED ANGLE DOUBLER Jan 13, 1999 · N8085U · Doug DC871F · Fuselage Main, FrameSDR RRXA991294Stiffner · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, FWD PIT AT STA 100, BETWEEN BL 21 RIGHT AND BL 33 RIGHT, HORIZONTAL STIFFENER. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED STIFFENER IJan 13, 1999 · N8085U · Doug DC871F · Fuselage Miscellaneous StructureSDR RRXA991293Angle · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE UNDER NR 3 O-BOTTLE CRADDLE ABOVE FRAME AT STA 100, LONGERON 28 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER AND FJan 13, 1999 · N8085U · Doug DC871F · Fuselage Miscellaneous StructureSDR RRXA991292Frame · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, FWD AT STRAP, FRAME, AT STA 160, BETWEEN LONGERONS 36 AND LONGERON 35 LEFT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED STRAP AND REPAJan 13, 1999 · N8085U · Doug DC871F · Fuselage Main, FrameSDR RRXA99003Control Box · failedMAIN GEAR SPOILER INOPERATIVE, LT ILLUMINATED EN ROUTE. INSPECTED AND TESTED MAIN GEAR GROUND SPOILERS, OPS CHECKS NORMAL. NO DEFECTS NOTED. REMOVED AND REPLACED ANTI SKID CONTROL BOX, OPS NORMAL.Jan 13, 1999 · N8079U · Doug DC871F · Brake Anti-Skid SectionSDR UPS99828669Frame · corrodedINSPECTION TYPE-C3, FS 1080 FRAME AT LONG 35R, THE LOWER FLANGE IS CORRODED BEYOND LIMITS. REPAIRED FRAME IAW SRM 53-2-0 FIG 2.Jan 12, 1999 · N713UP · Doug DC871F · Fuselage Main, FrameSDR UPS99828589Fitting · corrodedINSPECTION TYPE-C3, LONG 33R END FITTING AT FS 1560 IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.Jan 12, 1999 · N713UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS99828536Doubler · corrodedINSPECTION TYPE-C3, INTERNAL DOUBLER FROM FS 8 TO 70, LONG 29L TO 33L IS CORRODED BEYOND LIMITS. REMOVED, FABRICATED AND REPLACED DOUBLER IAW SRM 51-1-21 AND 53-3-1.Jan 12, 1999 · N713UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS99828514Doubler · crackedINSPECTION TYPE-C3, LT WING L/E LWR SKIN, THE INTERNAL DOUBLER AT XOLDI 6.225 IS CRACKED. REMOVED, FABRICATED AND REPLACED DOUBLER IAW DWG 5769891 AND SRM 51-1-20D, 51-1-21.Jan 12, 1999 · N713UP · Doug DC871F · Wing Miscellaneous StructureSDR UPS99828513Doubler · corrodedINSPECTION TYPE-C3, LONG 31L FINGER DOUBLER FS 1490 TO 1530 IS CORRODED BEYOND LIMITS. REMOVED, FABRICATED AND REPLACED DOUBLER IAW DWG 5615374 AND SRM 51-1-21.Jan 12, 1999 · N713UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS99828488Floorbeam · corrodedINSPECTION TYPE-C, UPPER TANG OF FLOORBEAM AT FS 879, RBL 68 IS CORRODED. REPAIRED FLOORBEAM IAW DHC SK701-677.Jan 12, 1999 · N701UP · Doug DC871F · Fuselage Main, Floor BeamSDR UPS99828337Retract Mech · malfunctionedINSPECTION TYPE-N/A, NOSE GEAR WOULD NOT RETRACT AFTER T/O. AIR TURNBACK. PER TROUBLESHOOTING PG 101 NOSE GEAR FAILS TO RETRACT, CHECKED CONTROL VALVE, RIGGING AND CABLE TENSION PER MM 32-31-00 PG 204. NO DEFECTS NOTED. GEAR OPERATES NORMAL. NO DEFECTS NOJan 12, 1999 · N700UP · Doug DC871F · Landing Gear Retraction/Extension SystemSDR RRXA991311Web · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, MEMBRANE, LT UPPER CUSP BETWEEN STA 1400 AND STA 1380 AT LONGERON 21 LEFT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER Jan 12, 1999 · N8085U · Doug DC871F · Fuselage Miscellaneous StructureSDR RRXA991310Web · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, WEB AREA AT STA 540, LONGERON 21 LEFT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC8 SRM 53-2-0 AND 51-1-21. (COJan 12, 1999 · N8085U · Doug DC871F · Fuselage Miscellaneous StructureSDR RRXA991288Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, WING, L/E UPPER SURFACE FROM STA XFS 7.50 TO STA XFS 32.5. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLER IAW FAA APPROVED TENNESSEE TECHNIJan 12, 1999 · N8085U · Doug DC871F · Wing, Plate/SkinSDR RRXA991287Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, WING, L/E UPPER SURFACE AT STA XFS 13.750. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM.. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLER AND FILLER IAW DC8 SRM 57-2-1 FIG 37. (CORROSIOJan 12, 1999 · N8085U · Doug DC871F · Wing, Plate/SkinSDR RRXA991035Angle · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION, CENTER FUSELAGE, CUSP ANGLE, LT, AT STA 1620, L2 DOOR FRAME FITTING AND LONGITUDIAL ANGLE. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED L2 DOOJan 12, 1999 · N8085U · Doug DC871F · Fuselage Miscellaneous StructureSDR RRXA991034Frame · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION, CENTER FUSELAGE, FRAME, AFT COMPT AT STA 660 ATTACH POINT, LONGERON 34 LEFT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED FILLER AND DOUBLER IAJan 12, 1999 · N8085U · Doug DC871F · Fuselage Main, FrameSDR UPS99828587Intercostal · corrodedINSPECTION TYPE-C3, FS 1060 TO 1080 AT LONG 35L, THE INTERCOSTAL LWR T IS CORRODED BEYOND LIMITS. REMOVED, FABRICATED AND REPLACED T IAW DWG 9759629 AND SRM 51-1-20D.Jan 11, 1999 · N713UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS99828585Clip · corrodedINSPECTION TYPE-C3, FS 1080, FWD SIDE AT LONG 35L, THE INTERCOSTAL ATTACH CLIP IS CORRODED BEYOND LIMITS. REMOVED, FABRICATED AND REPLACED CLIP IAW SRM 51-3-0 AND 51-1-20D.Jan 11, 1999 · N713UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS99828512Doubler · corrodedINSPECTION TYPE-C3, THE INTERNAL DOUBLER AT FS 340 TO 400, RT IS CORRODED BEYOND LIMITS, LONG 35L. REMOVED, FABRICATED AND REPLACED DOUBLER IAW DWG 9755878 AND SRM 51-1-21.Jan 11, 1999 · N713UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS99828511Rib · crackedINSPECTION TYPE-C3, TWO INCH CRACK IN RT WING T/E RIB AT XRS 127. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0.Jan 11, 1999 · N713UP · Doug DC871F · Wing, Rib/BulkheadSDR RRXA991367Frame · corrosionDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, FRAME, ACCY COMPT AT LONGERON 34 LEFT, STA 660 ATTACHMENT POINT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED FILLER AND DOUBLER IAW DJan 11, 1999 · N8085U · Doug DC871F · Fuselage Main, Frame
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