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 UPS98827663Skin · crackedINSPECTION TYPE:C RT WING L/E LWR SKIN CRACKED 2 PLCS XFS 304-310 7 FWD OF TE AND 5 FWD OF T/E. REPAIRED IAW DC8-5720-4087-B.Aug 28, 1998 · N706UP · Doug DC871F · Wing, Plate/SkinSDR UPS98827660Angle · crackedINSPECTION TYPE:C RT WING I/B SLOT O/B VERTICAL ANGLE CRACKED. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT ANGLE IAW SRM 51-1-20 AND DWG 9753293.Aug 28, 1998 · N706UP · Doug DC871F · Wing Miscellaneous StructureSDR UPS98827653Rib · crackedINSPECTION TYPE:C LT WING L/E RIB AT W/S XFS 297.5 IS CRACKED AT THE AFT UPPER END. REPAIRED IAW SRM 57-2-0.Aug 28, 1998 · N706UP · Doug DC871F · Wing, Rib/BulkheadSDR UPS98827689Weight · corrodedINSPECTION TYPE-C, RT WING I/B AILERON BALANCE WEIGHT IS CORRODED. REMOVED AND REPLACED I/B AILERON IAW MM 27-11-01.Aug 27, 1998 · N706UP · Doug DC871F · AileronsSDR UPS98827678Doubler · crackedINSPECTION TYPE-C, RT WING FUEL TANK ACCESS PANEL LAND IS CRACKED AT THE AFT O/B CORNER (XCW 78.5). REPAIRED AREA IAW SRM 57-2-1 FIG 36.Aug 27, 1998 · N706UP · Doug DC871F · Wing Miscellaneous StructureSDR UPS98827676Fitting · corrodedINSPECTION TYPE-C, LONGERON 36 END FITTING AT STA 8 IS CORRODED OUT OF LIMITS. REMOVED, FABRICATED AND REPLACED FITTING IAW DWG 9755865.Aug 27, 1998 · N706UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS98827656Skin · crackedINSPECTION TYPE:C RT WING L/E UPPER SURFACE CRACKED IN 2 PLACES FWD OF TE XFS 360.25 AND 385.25. REPAIRED IAW SRM 57-2-1.Aug 27, 1998 · N706UP · Doug DC871F · Wing, Plate/SkinSDR UPS98827654Skin · crackedINSPECTION TYPE:C RT WING UPPER SKIN CRACKED AT STA 76 STR 10 AFT ROW OF FASTENERS. REPAIRED IAW SRM 57-2-1.Aug 27, 1998 · N706UP · Doug DC871F · Wing, Plate/SkinSDR UPS98827655Skin · crackedINSPECTION TYPE:C THE FUSELAGE SKIN IS CRACKED AT THE UPPER FWD CORNER OF THE D PIT DOOR CUTOUT. REPAIRED IAW SRM 53-2-0.Aug 26, 1998 · N706UP · Doug DC871F · Fuselage Main, Plate/SkinSDR UPS98827679Skin · corrodedINSPECTION TYPE-C, EXTERNAL FUSELAGE SKIN AT STA 58 AND LONGERON 34R IS CRACKED AND CORRODED. REMOVED AND REPLACED BELLY SKIN FROM STA -136 TO 70 IAW DC8-5330 -8942 C.Aug 25, 1998 · N706UP · Doug DC871F · Fuselage Main, Plate/SkinSDR RRXA98413Doubler · damagedDURING A MAINTENANCE VISIT, FOUND EXTEROIR, SKIN DOUBLER GOUGED AND TORN, AT STA 330 AND LONGERON 36. REMOVED DAMAGED SECTION, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA APPROVED TIMCO DER ENGINEERING SKETCH REO-05348.Aug 25, 1998 · N8076U · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA9800067Pressure Syst · malfunctionedEN ROUTE AT FLIGHT LEVEL 35.0, THE AIRCRAFT CABIN BEGAN TO CLIMB RAPIDLY, MANUAL CONTROL OF PRESSURIZATION WAS ATTEMPTED. PACK FLOWS WERE INCREASED TO 90 PERCENT CAPACITY WITH MINIMAL DECREASE IN CABIN. DESCENT INITIATED AND AT LEVEL OFF CABIN COULD BE MAINAug 25, 1998 · N824BX · Doug DC871F · Cabin Pressure Control SystemSDR RRXA98412Bushing · damagedDURING A MAINTENANCE VISIT, FOUND RIGHT SIDE, MAIN LANDING GEAR, SIDE BRACE, LINK ASSEMBLY, BORE BUSHING WAS REMOVED TO REMOVE CORROSION, DURING PROCEDURES OVERSIZED HOLE. REPAIRED HOLE AND BUSHING, IAW FAA APPROVED TIMCO DER ENGINEERING SKETCH REO-05311.Aug 21, 1998 · N8076U · Doug DC871F · Main Landing GearSDR RRXA98410Support · damagedDURING A MAINTENANCE VISIT, FOUND PREVIOUS REPAIR TO FLOOR SUPPORT STRUT, DAMAGED CAUSED BY IMPACT FROM CARGO. REMOVED DAMAGED SECTION, FABRICATED AND INSTALLED REPAIR IAW FAA APPROVED TIMCO ENGINEERING SKETCH REO-05298.Aug 21, 1998 · N8076U · Doug DC871F · Fuselage Miscellaneous StructureSDR RRXA98340Skin · damagedDURING A MAINTENANCE VISIT, FOUND LEFT WING, PANEL 57-88 MOD, SKIN DOUBLER WITH 2 EACH ELONGATED HOLES. REMOVED DAMAGED SECTION, FABRICATED AND INSTALLED REPAIR IAW FAA APPROVED TIMCO DER ENGINEERING SKETCH REO-05260.Aug 21, 1998 · N500MH · Doug DC871F · Fuselage Main, Plate/SkinSDR RRXA98411Stiffener · corrodedDURING A MAINTENANCE VISIT, FOUND VERTICAL STABILIZER, INNER SPAR STIFFENER WITH CORROSION BEYOND LIMITS IAW DC-8 SRM. REMOVED DAMAGED SECTION, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA APPROVED TIMCO DER ENGINEERING SKAug 20, 1998 · N8076U · Doug DC871F · Vertical StabilizerSDR UPS98827512Fitting · crackedINSPECTION TYPE-C, STA 8 STR 22R END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4711722 AND SRM 51-1-20D.Aug 18, 1998 · N715UP · Doug DC871F · Fuselage Miscellaneous StructureSDR RRXA98408Fitting · corrodedDURING A MAINTENANCE VISIT, FOUND FITTING (P/N 5641008-502) WITH CORROSION DAMAGE BEYOND LIMITS IAW DC-8 SRM AT STA 798. REMOVED DAMAGED FITTING, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED NEW FITTING BY MATERIAL SUBSTITUTION, INSTALLED IAW FAA APPROVED TIAug 18, 1998 · N8076U · Doug DC871F · Fuselage Miscellaneous StructureSDR RRXA98409Skin · chafedDURING A MAINTENANCE VISIT, FOUND RIGHT WING, OUTBOARD FLAP, LOWER SKIN WITH CHAFING CAUSED BY FAIRING RUBBING THE SKIN. REMOVED DAMAGED SECTION, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA APPROVED TIMCO DER ENGINEERINGAug 17, 1998 · N8076U · Doug DC871F · Trailing Edge FlapsSDR RRXA98407Frame · damagedDURING A MAINTENANCE VISIT, FOUND FRAME WITH ELONGATED HOLES, AT STA 1000 AND FOUND LONGERON 35 LEFT WITH CORROSION DAMAGE. REMOVED DAMAGED SECTIONS FROM FRAME, AND CORROSION FROM LONGERON 35L, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIAug 17, 1998 · N8076U · Doug DC871F · Fuselage Main, FrameSDR RRXA98341Skin · crackedDURING A MAINTENANCE VISIT, FOUND RIGHT WING, INBOARD AILERON UPPER O/B SKIN, CRACKED. REMOVED DAMAGED SECTION, FABRICATED AND INSTALLED REPAIR IAW FAA APPROVED TIMCO DER ENGINEERING SKETCH REO-05281.Aug 17, 1998 · N500MH · Doug DC871F · AileronsSDR RRXA98416Fitting · damagedDURING A MAINTENANCE VISIT, (BER) LOWER AFT, CARGO SEPARATOR FIITING (PN: 5711283-516), AT STA 985. MANUFACTURED NEW FITTING IAW DWG DAC 5711283, DPS4.999 AND DC-8 SRM 51-1-1A. USE FAA APPROVED TIMCO DER ENGINEERING SKETCH REO-05273 FOR MATERIAL SUBSTITUTIONAug 15, 1998 · N500MH · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS98827424Wire · brokenNO LIGHT ON AFTER EMER EXIT LIGHTS DISARMED. SEE PREVIOUS WRITE UP P 294088. RECONNECTED BROKEN WIRE AT CONNECTOR P1-1345 PINS 7 AND 11 AT BATTERY PACK. OPS CK SYS NORMAL.Aug 12, 1998 · N752UP · Doug DC871F · Light System WiringSDR RRXA98404Floorbeam · corrodedDURING A MAINTENANCE VISIT, FOUND FLOORBEAM, UPPER FLANGE WITH CORROSION DAMAGED BEYOND LIMITS IAW DC-8 SRM AT STA 1300. REMOVED DAMAGED SECTION, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR STRAPS IAW FAA APPROVED TIMCO ENGINEERING SKETAug 12, 1998 · N8076U · Doug DC871F · Fuselage Main, Floor BeamSDR RRXA98406Panel · crackedDURING A MAINTENANCE VISIT FOUND LEFT WING, HYDRAULIC SERVICE DOOR, PANEL (-3), CRACKED AND CHAFED ON FLANGE. REMOVED DAMAGED SECTION, FABRICATED AND INSTALLED REPAIR IAW FAA APPROVED TIMCO DER ENGINEERING SKETCH REO-05230.Aug 11, 1998 · N8076U · Doug DC871F · Hydraulic Compartment DoorsSDR RRXA98405Frame · corrodedDURING A MAINTENANCE VISIT, FOUND FRAME INBOARD FLANGE WITH CORROSION DAMAGED BEYOND LIMITS IAW DC-8 SRM AT STA 1260 BETWEEN LONGERONS 25 LEFT AND 26 LEFT. REMOVED DAMAGED SECTION, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAWAug 11, 1998 · N8076U · Doug DC871F · Fuselage Main, FrameSDR IXXA9800066Relay · defectiveDURING CLIMBOUT, THE NR 1 ENG FIRE WARNING SOUNDED WITH THE MASTER FIRE WARNING LIGHT ILLUMINATED. THE FLT CREW SECURED THE ENG FOLLOWING COMPANY PROCEDURES AND DISCHARGED THE FIRE BOTTLE. THE FIRE WARNING LIGHT EXTINGUSHED FOLLOWING FIRE BOTTLE DISCHARGE. Aug 11, 1998 · N828BX · Doug DC871F · Fire DetectionSDR UPS98827448Web · crackedINSPECTION TYPE-C, STA 520 AT STR 32R, THE TORQUE BOX WEB IS CRACKED. REPAIRED AREA IAW SRM 53-2-0 AND DWG 5616520.Aug 10, 1998 · N715UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS98827422Skin · corrodedTWO RIVETS POPPED ON FUSELAGE SKIN ABOUT SIX FEET AFT OF NR 4 PIT DOOR. COMPLIED WITH EO DC8-5330-10186A.Aug 10, 1998 · N729UP · Doug DC871F · Fuselage Main, Plate/SkinSDR UPS98827415Doubler · corrodedINSPECTION TYPE:C COCKPIT SUB-FLOOR FINGER DOUBLER AT STA -10 TO-20 BLB50 HAS HEAVY CORROSION. REMOVED, FABRICATED AND REPLACED DOUBLER IAW DWG 5612298 AND SRM 51-1-21.Aug 10, 1998 · N715UP · Doug DC871F · Fuselage Miscellaneous StructureSDR RRXA98403Doubler · corrodedDURING A MAINTENANCE VISIT, FOUND INNER DOUBLER WITH CORROSION DAMAGE BEYOND LIMITS IAW DC-8 SRM AT STA 1216 BETWEEN LONGERONS 34 RIGHT TO LONGERON 36. REMOVED DAMAGED SECTION, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAAAug 10, 1998 · N8076U · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS98827451Doubler · corrodedINSPECTION TYPE-C, STA 1541 TO 1590 AT STR 31L, THE FINGER DOUBLER IS CRACKED AND CORRODED. REMOVED, FABRICATED AND REPLACED DOUBLER IAW DWG 5615674 AND SRM 51-1-21.Aug 8, 1998 · N715UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS98827447Longeron · corrodedINSPECTION TYPE-C, A/S COMP, STA 35, STR 36 IS CRACKED AND CORRODED. REMOVED FABRICATED AND INSTALLED LONGERON IAW DWG 3615532 AND SRM 51-1-20D.Aug 7, 1998 · N715UP · Doug DC871F · Fuselage Main, Longeron/StringerSDR UPS98827446Fitting · corrodedINSPECTION TYPE-C, A/C COMP AT STA 70, STR 21R TIE FITTING UNDER CUSP HAS HEAVY CORROSION. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D, AND SRM 51-3-0.Aug 7, 1998 · N715UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS98827441Fitting · crackedINSPECTION TYPE-D, INTERCOSTAL AFT END FITTING FOUND TO BE CRACKED AT FWD SIDE OF FS 1140 FRAME AT LONG 33R. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.Aug 7, 1998 · N755UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS98827454Intercostal · crackedINSPECTION TYPE-C STA 1240 TO 1260 AT STR 33L, THE INTERCOSTAL IS CRACKED. REMOVED, FABRICATED AND REPLACED INTERCOSTAL IAW DWG 9753792 AND SRM 51-1-20D.Aug 6, 1998 · N715UP · Doug DC871F · Fuselage Miscellaneous StructureSDR RRXA98402Frame · corrodedDURING A MAINTENANCE VISIT, FOUND FRAME UPPER FLANGE WITH CORROSION DAMAGE BEYOND LIMITS IAW DC-8 SRM AT STA 1260 BETWEEN LONGERONS 34 LEFT AND 35 RIGHT. REMOVED DAMAGED SECTION, TREATED AREA IAW FAA APPROVED TIMCO DER ENGINEERING SKETCH REO-05188.Aug 6, 1998 · N8076U · Doug DC871F · Fuselage Main, FrameSDR RRXA98397Fitting · mismanufacturedDURING A MAINTENANCE VISIT, PERFORMED REQUIREMENTS IAW SB 32-171, LEFT AND RIGHT MAIN LANDING GEAR DOOR ACTUATOR ATTACH FITTING NEEDED TO BE SPOTFACED TO INSTALL FASTENERS.Aug 6, 1998 · N8076U · Doug DC871F · Landing Gear Door ActuatorSDR RRXA98339Skin · corrodedDURING A MAINTENANCE VISIT, FOUND BELLY SKIN WITH CORROSION DAMAGE BEYOND LIMITS IAW DC-8 SRM, AT STA 1890 BETWEEN LONGERONS 36 TO 32 RIGHT. REMOVED CORROSION DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA APPROVED Aug 6, 1998 · N500MH · Doug DC871F · Fuselage Main, Plate/SkinSDR RRXA98338Longeron · corrodedDURING A MAINTENANCE VISIT, FOUND LONGERON 31 RIGHT WITH CORROSION DAMAGE, AT STA 1080. REMOVED DAMAGED SECTION, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA APPROVED DER TIMCO ENGINEERING SKETCH REO-05194.Aug 6, 1998 · N500MH · Doug DC871F · Fuselage Main, Longeron/StringerSDR RRXA98401Frame · corrodedDURING A MAINTENANCE VISIT, FOUND FRAME FLANGE WITH CORROSION DAMAGED BEYOND LIMITS IAW DC-8 SRM AT STA 1060 AND LONGERON 26 RIGHT. REMOVED DAMAGED SECTION, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR STRAPS IAW FAA APPROVED TIMCO DER EAug 5, 1998 · N8076U · Doug DC871F · Fuselage Main, FrameSDR RRXA98400Floorbeam · corrodedDURING A MAINTENANCE VISIT, FOUND FLOORBEAM, VERTICAL FLANGE WITH CORROSION DAMAGE BEYOND LIMITS IAW DC-8 SRM AT STA 920 AND LONGERON 21 LEFT. REMOVED DAMAGED SECTION, TREATED AREA IAW DC-8 SRM. FABRICATED AND INSTALLED REPAIR STRAPS IAW FAA APPROVED TIMCO DAug 5, 1998 · N8076U · Doug DC871F · Fuselage Main, Floor BeamSDR RRXA98337Frame · crackedDURING A MAINTENANCE VISIT, FOUND FRAME CRACKED, AT STA 867 AND BL 51 L. REMOVED DAMAGED SECTION, FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA APPROVED DER TIMCO ENGINEERING SKETCH REO-05179.Aug 5, 1998 · N500MH · Doug DC871F · Fuselage Main, FrameSDR UPS98827453Longeron · corrodedINSPECTION TYPE-C, STA 8 TO 25, LONG 33L IS CORRODED BEYOND LIMITS. REMOVED, FABRICATED AND REPLACED LONGERON IAW DWG 3642838 AND SRM 51-1-21.Aug 4, 1998 · N715UP · Doug DC871F · Fuselage Main, Longeron/StringerSDR UPS98827409Angle · corrodedINSPECTION TYPE:C STA 380 AT STR 21R, THE CUSP ANGLE IS CORRODED BEYOND LIMITS. REMOVED, FABRICATED AND REPLACED ANGLE IAW DWG 9754069 AND SRM 51- 1-21D.Aug 3, 1998 · N715UP · Doug DC871F · Fuselage Miscellaneous StructureSDR RRXA98336Frame · corrodedDURING A MAINTENANCE VISIT, FOUND FRAME LOWER SECTION WITH CORROSION DAMAGE, AT STA 1580 BETWEEN LONGERONS 35 LEFT TO 35 RIGHT. REMOVED DAMAGED SECTION, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW FAA APPROVED DER TIMCO ENGINEERING Aug 3, 1998 · N500MH · Doug DC871F · Fuselage Main, FrameSDR UPS98827385Fitting · corrodedINSPECTION TYPE:D STA 200 AT STR 27L, THE FLOORBEAM SUPPORT FITTING IS CORRODED. REMOVED, FABRICATED AND REPLACED FITTING IAW DWG 3773077 AND SRM 51-1-20D.Aug 1, 1998 · N755UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS98827462Longeron · corrodedINSPECTION TYPE-C, STA 1440 TO 1520, LONG 31R IS CORRODED BEYOND LIMITS. REMOVED, FABRICATED AND REPLACED SECTION OF LONGERON IAW DWG 3646771 AND SRM 51-1-21.Jul 31, 1998 · N715UP · Doug DC871F · Fuselage Main, Longeron/StringerSDR UPS98827445Skin · corrodedINSPECTION TYPE-C, STA 1440 TO 1450 AT STR 31R, THE SKIN IS CORRODED BEYOND LIMITS. REPAIRED AREA IAW SRM 53-2-1 FIG 7.Jul 31, 1998 · N715UP · Doug DC871F · Fuselage Main, Plate/SkinSDR UPS98827318Splice · crackedINSPECTION TYPE-C, LONG 31R SPLICE FITTING CRACKED FS 1040 TO 1060. REMOVED AND REPLACED FITTING IAW SRM 51-1-21.Jul 31, 1998 · N715UP · Doug DC871F · Fuselage Miscellaneous Structure
Back to Douglas DC-8-71F