Douglas DC-8-63F

Service difficulty reports · 1,883

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 = 'DC863F'
  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 RRXA98149Skin · crackedDURING A MAINTENANCE VISIT, FOUND LEFT WING, LEADING EDGE, SLANT CRACKED AT XFS=207.5. FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA APPROVED DER TIMCO ENGINEERING SKETCH REO-04400.Mar 30, 1998 · N865F · Doug DC863F · Wing, Plate/SkinSDR ARWA980310Switch · failedDURING TAXI AND T/O CHECK, AILERON REVERSION LIGHT DID NOT GO OUT WITH THE AILERON POWER LEVEL ON. RECYCLED, NO HELP. REMOVED AND REPLACED AILERON MANUAL CONTROL INDICATING SWITCH, GROUND OPS CHECKED NORMAL PER MM 27-11-14.Mar 30, 1998 · N661AV · Doug DC863F · Aileron Tab Control SystemSDR ABXA9800312Angle · crackedKEEL BEAM AREA AT APPROXIMATELY STATION 930 TO 935 RIGHT SIDE, THE KEEL ANGLE HAS A 5 INCH CRACK. REPAIRED IAW ABX REA D853-22758 AND DC8 SRM 52-2-0.Mar 28, 1998 · N814AX · Doug DC863F · Fuselage Miscellaneous StructureSDR RRXA98183Panel · misdrilledDURING A MAINTENANCE VISIT, FOUND LEFT WING TRAILING EDGE, PANEL MISDRILLED HOLE, (P/N 5611015-502). FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA APPROVED DER TIMCO ENGINEERING SKETCH REO-04513.Mar 25, 1998 · N865F · Doug DC863F · Wing, Plate/SkinSDR ARWA980306Ballast · failedSMELL OF ELECTRICAL INSULATION BURNING AFTER LANDING. REMOVED AND REPLACED BALLAST ASSY, OPERATION CHECKED NORMAL IAW MM 33-00-0.Mar 24, 1998 · N441J · Doug DC863F · Passenger Compartment LightingSDR RRXA98180Bracket · corrodedDURING A MAINTENANCE VISIT FOUND FAN ATTACHMENT MOUNT BRACKET CORRODED IN VARIOUS AREAS, REPLACEMENT PART NOT AVAILABLE. REMOVED BRACKET, TREATED AREA IAW DC-8 SRM 51-1-8. CLEANED BRACKET BY GLASS BEADED AREAS TO REMOVE CORROSION. USED FAA TIMCO DER ENGINEEMar 23, 1998 · N865F · Doug DC863F · Air Distribution FanSDR RRXA98178Skin · corrodedDURING A MAINTENANCE VISIT, FOUND FUSLAGE SKIN CORRODED AT STA 70 BETWEEN LONGERONS 28 RIGHT AND 34 RIGHT. 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-04Mar 20, 1998 · N865F · Doug DC863F · Fuselage Main, Plate/SkinSDR RRXA98071Airspeed Ind · malfunctionedCAPTAINS AIRSPEED IND WENT TO ZERO ON CLIMBOUT. AFTER BEING AIRBORNE FOR 15 MINUTES A/S INDICATOR CAME UP TO 300 KTS AND REMAINED THERE. DISCONNECTED ALL PITOT LINES FROM CAPT'S AIRSPEED IND, WATER TRAP, AND PITOT TUBE. BLEW OUT PITOT LINES W/NITROGEN, REPLMar 19, 1998 · N957R · Doug DC863F · Airspeed/Mach IndicatorSDR RRXA98175Rib · crackedDURING A MAINTENANCE VISIT, FOUND LEFT WING LEADING EDGE, RIB UPPER CAP CRACKED AT XFS=57.750. FABRICATED AND INSTALLED SPLICE REPAIR IAW FAA APPROVED DER TIMCO ENGINEERING SKETCH REO-04474.Mar 18, 1998 · N865F · Doug DC863F · Wing, Rib/BulkheadSDR ARWA980305O-Ring · failedAFTER T/O, CAPTAIN AIRSPEED DECREASING AND ALTIMETER READING LOW, BOTH UNREALIABLE. FOUND DAMAGED O-RING ON STATIC SIDE OF CAPTAIN A/S INDICATOR. REMOVED AND REPLACED O-RIGN, OPS CK. SYSTEM OK IAW MM 34-12-0.Mar 18, 1998 · N661AV · Doug DC863F · Airspeed/Mach IndicatorSDR RRXA98174Floorbeam · damagedDURING A MAINTENANCE VISIT, FOUND FLOORBEAM WITH TOOL DAMAGE AT STA 857.188 BL 25 RIGHT. FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA APPROVED DER TIMCO ENGINEERING SKETCH REO-04472.Mar 17, 1998 · N865F · Doug DC863F · Fuselage Main, Floor BeamSDR ABXA9800252Proximity Box · defectiveDURING APPROACH LEFT LANDING GEAR INDICATION LIGHT WOULD NOT ILLUMINATE AFTER GEAR RETRACTION. RECYCLED GEAR, LIGHT CAME ON AFTER 10 MINUTES OF FLIGHT. REPLACED LEFT MAIN LANDING GEAR PROXIMITY BOX. ACCOMPLISHED GEAR SWING IAW DC8 MM 32-60-00. OPS CHECKED Mar 17, 1998 · N812AX · Doug DC863F · Landing Gear Position and WarningSDR RRXA98182Skin · holeDURING A MAINTENANCE VISIT REMOVED DRAIN MAST, NO LONGER REQUIRED AT STA 1726.656 BETWEEN LONGERONS 28 LEFT AND 30 LEFT. FABRICATED AND INSTALLED BLANKED PLATES TO COVER HOLES IAW FAA APPROVED DER TIMCO ENGINEERING SKETCH REO-0442.Mar 16, 1998 · N865F · Doug DC863F · Fuselage Main, Plate/SkinSDR RRXA98181Skin · corrosionDURING A MAINTENANCE VISIT, FOUND CORROSION ON FUSELAGE SKIN AT STA 80 TO STA 90 BETWEEN LONGERONS 27 RIGHT AND 28 RIGHT. REMOVED DAMAGED SECTION, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA APPROVED DER TIMCO ENGINEERINMar 16, 1998 · N865F · Doug DC863F · Fuselage Main, Plate/SkinSDR RRXA98176Fitting · corrosionDURING A MAINTENANCE VISIT, FOUND LOWER CARGO DOOR JAMB, ZEE FITTING CORRODED BEYOND LIMITATIONS IAW DC-8 SRM AT STA 123 AND LONGERON 33 LEFT. FABRICATED AND INSTALLED NEW FITTING IAW FAA APPROVED DER TIMCO ENGINEERING SKETCH REO-04484.Mar 16, 1998 · N865F · Doug DC863F · Fuselage Miscellaneous StructureSDR RRXA98170Spar Cap · misdrilledDURING A MAINTENANCE VISIT, FOUND TOOL DAMAGE TO LEFT WING, FRONT SPAR CAP AT XFS=304. FABRICATED AND INSTALLED SPLICE REPAIR IAW FAA APPROVED DER TIMCO ENGINEERING SKETCH REO-04456.Mar 16, 1998 · N865F · Doug DC863F · Wing SparSDR RRXA98168Panel · damagedDURING A MAINTENANCE VISIT, NEWLY FABRICATED LEFT SIDE INBOARD FLAP FILLET PANEL NEEDS REPLACEMENT OF BEADED SECTION WITH FLAT SHEET. BEADED SECTION OF LEFT SIDE INBOARD FLAP FILLET PANEL, WAS PLACED WITH FLAT SHEET IAW FAA APPROVED DER TIMCO ENGINEERING SKETMar 16, 1998 · N865F · Doug DC863F · Trailing Edge FlapsSDR RRXA98167Skin · gougedDURING A MAINTENANCE VISIT, FOUND RIGHT WING OUTBOARD FLAP, LOWER SKIN GOUGED AT XRS=240. FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA APPROVED DER TIMCO ENGINEERING SKETCH REO-04441.Mar 16, 1998 · N865F · Doug DC863F · Trailing Edge FlapsSDR RRXA98165Longeron · corrosionDURING A MAINTENANCE VISIT, FOUND LONGERON 34 RIGHT WITH CORROSION DAMAGE AT STA 1160. REMOVED DAMAGED SECTION, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED SPLICE REPAIR IAW FAA APPROVED DER TIMCO ENGINEERING SKETCH REO-04437.Mar 16, 1998 · N865F · Doug DC863F · Fuselage Main, Longeron/StringerSDR RRXA98148Skin · corrosionDURING A MAINTENANCE VISIT, FOUND LEFT WING, LEADING EDGE WITH CORROSION DAMAGE AT XFS=820. REMOVED DAMAGED SECTION, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA APPROVED DER ENGINEERING SKETCH REO-04393.Mar 16, 1998 · N865F · Doug DC863F · Wing, Plate/SkinSDR ABXA9800301Skin · crackedLEFT WING LEADING EDGE BETWEEN PYLONS INTERNAL UPPER DOUBLER IS CRACKED ABOVE SLOT ACTUATOR. REPAIRED IAW DC8 SRM 51-3-0 AND 51-1-20D.Mar 16, 1998 · N814AX · Doug DC863F · Wing, Plate/SkinSDR ABXA9800251Control Box · defectiveLANDING GEAR UNSAFE LIGHT WAS ON WITH NOSE LANDING GEAR UNLATCHED INDICATION. RECYCLED GEAR, NO HELP. REPLACED PROXIMITY CONTROL BOX AND NOSE LANDING GEAR UPLIMIT SWITCH IAW DC8 MM 32-60-0. OPS CHECKED GOOD.Mar 16, 1998 · N812AX · Doug DC863F · Landing Gear Position and WarningSDR ABXA9800238Panel · crackedLEFT WING LOWER 69.5 SKIN PANEL HAS CRACK INDICATIONS IN FIVE PLACES. REPAIRED IAW ABX REA D857-21963 MR.Mar 16, 1998 · N815AX · Doug DC863F · Wing, Plate/SkinSDR ABXA9800237Tee Cap · corrodedLEFT AUX TANK TEE CAP CORRODED AT WING STA XFS 45.00 TO XFS 107.50. REPAIRED IAW REA D857-21955 MR.Mar 16, 1998 · N815AX · Doug DC863F · Wing Miscellaneous StructureSDR ABXA9800236Frame · brokenSTA 1400 MAIN FRAME ABOVE LONGERON 35R HAS BOTTOM LEG BROKEN OUT. REPAIRED IAW REA D853-21958MR.Mar 16, 1998 · N815AX · Doug DC863F · Fuselage Main, FrameSDR ABXA9800235Panel · crackedSKIN PANEL ON RIGHT WING HAS CRACK INDICATIONS AT 7 LOCATIONS. REPAIRED IAW REA D857-21983MR.Mar 16, 1998 · N815AX · Doug DC863F · Wing, Plate/SkinSDR ABXA9800304Shear Tie · corrodedFORWARD SHEAR TIE AT STATION 1000 HAS HEAVY CORROSION AT LONGERON 33R. REPAIRED IAW DC8 SRM 53-20-0 AND DWG 9755888.Mar 15, 1998 · N814AX · Doug DC863F · Fuselage Miscellaneous StructureSDR ABXA9800302Doubler · crackedFINGER DOUBLER CRACKED AT STATION 450, LONGERON 31L. CORROSION OUT OF LIMITS. REPAIRED IAW ABX REA D853-22748.Mar 15, 1998 · N814AX · Doug DC863F · Fuselage Miscellaneous StructureSDR ABXA9800303Fitting · corrosionCORRODED VERTICAL FITTING RBL 65 STATION 920. REPAIRED IAW DC8 SRM 51-1-20D.Mar 14, 1998 · N814AX · Doug DC863F · Fuselage Miscellaneous StructureSDR RRXA98171Skin · misdrilledDURING A MAINTENANCE VISIT, FOUND TOOL DAMAGE TO LEFT WING, LEADING EDGE LOWER SKIN AT XFS=285 AND XFS=526. FABRICATED AND INSTALLED REPAIR DOUBLER TO XFS=285 AND 526, IAW FAA APPROVED DER TIMCO ENGINEERING SKETCH REO-04457.Mar 13, 1998 · N865F · Doug DC863F · Wing, Plate/SkinSDR ABXA9800315Shear Tie · crackedSHEAR TIE CRACKED, STATION 1160 BETWEEN LONGERON 34R TO 35R. REPAIRED IAW DC8 SRM 51-1-20D.Mar 13, 1998 · N814AX · Doug DC863F · Fuselage Miscellaneous StructureSDR ABXA9800305Longeron · corrodedLONGERON 31R AT STATION 25 HAS HEAVY CORROSION. REPAIRED IAW DC8 SRM 51-1-20.Mar 13, 1998 · N814AX · Doug DC863F · Fuselage Main, Longeron/StringerSDR RRXA98169Fitting · chafedDURING A MAINTENANCE VISIT, FOUND LEFT WING CANOE FITTING CHAFED AT STA 97.9. FABRICATED AND INSTALLED REPAIR IAW FAA APPROVED DER TIMCO ENGINEERING SKETCH REO-04453.Mar 12, 1998 · N865F · Doug DC863F · Wing Miscellaneous StructureSDR RRXA98164Access Panel · misdrilledDURING A MAINTENANCE VISIT, FOUND TOOL DAMAGE TO LEFT WING ACCESS PNL: 506B. FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA APPROVED DER TIMCO ENGINEERING SKETCH REO-04436.Mar 12, 1998 · N865F · Doug DC863F · Wing, Plate/SkinSDR ABXA9800314Fitting · crackedSHEAR TIE AT STATION 1150 BETWEEN LONGERON 30R AND 33R HAS 6 INCH CRACK. REPAIRED IAW SRM 51-1-20D.Mar 12, 1998 · N814AX · Doug DC863F · Fuselage Miscellaneous StructureSDR ABXA9800310Stringer · corrodedSTRINGERS 34R AND 34L AT STATION 1460 CORRODED BEYOND LIMITS. REPAIRED IAW DC8 SRM 53-2-0 AND 51-1-20.Mar 12, 1998 · N814AX · Doug DC863F · Fuselage Main, Longeron/StringerSDR ABXA9800307Rib · crackedLEFT WING LEADING EDGE RIB CRACKED AT WS 354 UPPER AFT. REPAIRED IAW DC8 SRM 51-1-20D.Mar 12, 1998 · N814AX · Doug DC863F · Wing, Rib/BulkheadSDR ABXA9800248Rib · crackedRIGHT WING LEADING EDGE RIB AT STATION XFS 791.25 IS CRACKED AT THE AFT LOWER END. REPAIRED IAW SRM 57-2-0 AND DWG K 05056.Mar 12, 1998 · N814AX · Doug DC863F · Wing, Rib/BulkheadSDR ABXA9800219Rib · crackedRIGHT WING LEADING EDGE RIB AT STA XFS 822.50 IS CRACKED AT THE AFT LOWER END. REPAIRED IAW DC8 SRM 57-2-0 AND DWG K 05056.Mar 12, 1998 · N814AX · Doug DC863F · Wing, Rib/BulkheadSDR ABXA9800217Rib · crackedRIGHT WING LEADING EDGE RIB AT STA XFS 747.5 IS CRACKED AT THE AFT UPPER END. REPAIRED IAW DC8 SRM 57-2-0 AND DWG K 05056.Mar 12, 1998 · N814AX · Doug DC863F · Wing, Rib/BulkheadSDR ABXA9800216Rib · crackedRIGHT WING LEADING EDGE RIB AT STA XFS 628.75 IS CRACKED AT THE AFT UPPER END. REPAIRED IAW DC8 SRM 57-2-0 AND DWG K 05056.Mar 12, 1998 · N814AX · Doug DC863F · Wing, Rib/BulkheadSDR ABXA9800317Spar · crackedRIGHT WHEEL WELL AT FWD LOWER OUTBOARD END, REAR SPAR LOWER CHORD HAS NUMEROUS CRACKS. REPAIRED IAW ABX REA D857-22747 MR.Mar 11, 1998 · N814AX · Doug DC863F · Wing SparSDR RRXA98163Skin · crackedDURING A MAINTENANCE VISIT, FOUND LEFT WING AILERON CRACKED AT XA=621.625. FABRICATED AND INSTALLED SPLICE REPAIR IAW FAA APPROVED DER TIMCO ENGINEERING SKETCH REO-04435.Mar 9, 1998 · N865F · Doug DC863F · AileronsSDR RRXA98162Fitting · damagedDURING A MAINTENANCE VISIT, FOUND BATHTUB, DOOR JAMB FITTING DAMAGED AT STA 1170. FABRICATED NEW FITTING IAW DAC DWG 3754930. ORIGINAL MATERIAL NOT AVAILABLE FOR PURCHASE, REO-04434 PROVIDED SUBSTITUTION 7075-T651 FOR 7075-T6.Mar 9, 1998 · N865F · Doug DC863F · Fuselage Miscellaneous StructureSDR RRXA98161Seat · crackedDURING A MAINTENANCE VISIT, FOUND FIRST OBSERVER SEAT BACK CLOSE-OUT WEB CRACKED. CRACK ORIGINATED AT LIGHTNING HOLE AND ENDED AT EDGE. SRM DOES NOT GIVE A SPECIFIC REPAIR. FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA APPROVED DER TIMCO ENGINEERING SKETCMar 9, 1998 · N865F · Doug DC863F · Flight Compartment EquipmentSDR ABXA9800291Doubler · corrodedINTERNAL FINGER DOUBLER CORRODED AND CRACKED AT STATION 105, LONGERON 31R. REPAIRED IAW ABX REA D853-22748 MR.Mar 9, 1998 · N814AX · Doug DC863F · Fuselage Miscellaneous StructureSDR ABXA9800306Splice · crackedLONGERON 31L SPLICE FITTING CRACKED BETWEEN STATION 440 TO 460. REPAIRED IAW DC8 SRM 51-1-20D.Mar 7, 1998 · N814AX · Doug DC863F · Fuselage Miscellaneous StructureSDR ABXA9800292Cusp · corrodedMAIN CABIN LOWER CUSP CORRODED BEYOND LIMITS AT STATION 460 TO STATION 560 RIGHT SIDE. REPAIRED IAW DC8 SRM 53-2-5.Mar 7, 1998 · N814AX · Doug DC863F · Fuselage Miscellaneous StructureSDR RRXA98160Skin · damagedDURING A MAINTENANCE VISIT, REMOVED DRAIN MAST, NO LONGER REQUIRED AT STA 400 AND STA 418 BETWEEN LONGERONS 35 RIGHT AND 36. FABRICATE AND INSTALLED BLANK-OFF PLATES TO COVER REMAINING HOLES IAW FAA APPROVED DER ENGINEERING SKETCH REO-04428.Mar 6, 1998 · N865F · Doug DC863F · Fuselage Main, Plate/SkinSDR RRXA98156Frame · corrosionDURING A MAINTENANCE VISIT, FOUND FRAME WITH CORROSION DAMAGE AT 1060 BETWEEN LONGERONS 34 RIGHT AND 36. REMOVED DAMAGED SECTION, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED SPLICE REPAIR IAW FAA APPROVED DER TIMCO ENGINEERING SKETCH REO-04417Mar 6, 1998 · N865F · Doug DC863F · Fuselage Main, Frame
Back to Douglas DC-8-63F