Douglas DC-8-62

Service difficulty reports · 2,778

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 = 'DC862'
  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 RRXA000864Frame · misdrilledDURING A MAINTENANCE VISIT, FOUND MISDRILLED HOLES TO THE UPPER CARGO COMPT AT STA 1060 AND L21R TO L21L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. PLUGGED HOLES, FABRICATED DOUBLER AND GUSSET PLATDec 28, 1999 · N994CF · Doug DC862 · Fuselage Main, FrameSDR RRXA001629Frame · misdrilledDURING A MAINTENANCE VISIT, FOUND MISDRILLED HOLES IN THE UPPER CARGO COMPT AT FS 480 AND L21R TO L21L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. PLUGGED MISDRILLED HOLES, FABRICATED DOUBLERS FROM Dec 23, 1999 · N994CF · Doug DC862 · Fuselage Main, FrameSDR RRXA000973Frame · misdrilledDURING A MAINTENANCE VISIT, FOUND NUMEROUS MISDRILLED HOLES IN THE UPPER CARGO COMPT FS 360 AND L21R TO L21L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. PLUGGED MISDRILLED AND DISCREPANT HOLES, FABRDec 23, 1999 · N994CF · Doug DC862 · Fuselage Main, FrameSDR RRXA000972Frame · misdrilledDURING A MAINTENANCE VISIT, FOUND MISDRILLED HOLES IN THE UPPER CARGO COMPT FS 380 AND L21R TO L21L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. PLUGGED MISDRILLED AND DISCREPANT HOLES, FABRICATED DODec 23, 1999 · N994CF · Doug DC862 · Fuselage Main, FrameSDR RRXA000971Frame · misdrilledDURING A MAINTENANCE VISIT, FOUND MISDRILLED HOLES IN THE UPPER CARGO COMPT FS 400 AND L21R TO L21L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. PLUGGED MISDRILLED AND DISCREPANT HOLES, FABRICATED DODec 23, 1999 · N994CF · Doug DC862 · Fuselage Main, FrameSDR RRXA000968Frame · misdrilledDURING A MAINTENANCE VISIT, FOUND MISDRILLED HOLES IN THE UPPER CARGO COMPT FS 460 AND L21R TO L21L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. PLUGGED MISDRILLED HOLES, FABRICATED DOUBLER FROM 7075Dec 23, 1999 · N994CF · Doug DC862 · Fuselage Main, FrameSDR RRXA000967Frame · misdrilledDURING A MAINTENANCE VISIT, FOUND MISDRILLED HOLES IN THE UPPER CARGO COMPT AT STA 500 AND L21R TO L21L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. PLUGGED DISCREPANT AND MISDRILLED HOLES, FABRICATEDec 22, 1999 · N994CF · Doug DC862 · Fuselage Main, FrameSDR RRXA000866Frame · misdrilledDURING A MAINTENANCE VISIT, FOUND NUMEROUS MISDRILLED HOLES TO THE FRAME AT STA 270 AND L21R TO L21L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED DOUBLER FROM 7075-T6 AND INSTALLED IAW DC-Dec 22, 1999 · N994CF · Doug DC862 · Fuselage Main, FrameSDR RRXA000970Frame · misdrilledDURING A MAINTENANCE VISIT, FOUND MISDRILLED HOLES IN THE UPPER CARGO COMPT FS 420 AND L21R TO L21L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. PLUGGED DISCREPANT AND MISDRILLED HOLES PER EO NR 99-236 WITH APPDec 21, 1999 · N994CF · Doug DC862 · Fuselage Main, FrameSDR RRXA000969Frame · misdrilledDURING A MAINTENANCE VISIT, FOUND MISDRILLED HOLES IN THE UPPER CARGO COMPT FS 440 AND L21R TO L21L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE,TREATED AREA IAW DC-8 SRM 51-1-8. PLUGGED MISDRILLED AND DISCREPANT HOLES PER EO NR 99-236 WITH APPRDec 21, 1999 · N994CF · Doug DC862 · Fuselage Main, FrameSDR RRXA001514Floorbeam · crackedDURING A MAINTENANCE VISIT, FOUND A CRACK TO THE RT FLOORBEAM UPPER LOWER CARGO COMPT FS 235 AND XCW 69, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED ANGLES FROM 2024-T3 AND INSTALLED IAW DDec 21, 1999 · N994CF · Doug DC862 · Fuselage Main, Floor BeamSDR ABXA9900858Striker · looseRED GEAR UNSAFE LIGHT ILLUMINATED WITH GEAR UP AT 1700 FT. PERFORMED GEAR UPLATCH CHECK. DISCRIMINATOR PANEL NOT LATCHED LIGHT ILLUMINATED IN LEFT LANDING GEAR DOOR POSITION. RECYCLED GEAR AND RED UNSAFE LIGHT WENT OUT. LEFT UPLATCH SWITCH STRIKER WAS HITTDec 21, 1999 · N805AX · Doug DC862 · Landing Gear Position and WarningSDR ABXA9900855Indicator · malfunctionedDURING CLIMB, RED GEAR UNSAFE LIGHT ILLUMINATED WITH GEAR UP. DURING UPLATCH CHECK, THE LEFT GEAR DOOR LIGHT ILLUMINATED WHEN SELECTED. AFTER GEAR RECYCLE, BOTH LIGHTS EXTINGUISHED. CHECKED MAIN GEAR DOOR SWITCHES IAW DC8MM. NO DEFECTS NOTED. OPS CHECKED Dec 20, 1999 · N805AX · Doug DC862 · Landing Gear Position and WarningSDR ABXA9900866Window · out of adjustFIRST OFFICER'S WINDOW WOULD NOT OPEN. ADJUSTED LOWER AFT HOOK IAW DC8 MM.Dec 16, 1999 · N805AX · Doug DC862 · Flight Compartment WindowsSDR ABXA9900815Battery Pack · dischargedDURING PREFLIGHT, FOUND EMERGENCY LIGHTS INOPERATIVE. REPLACED EMERGENCY LIGHTS BATTERY PACK IAW DC8 MM 33-50-01. OPS CHECKED GOOD.Dec 3, 1999 · N805AX · Doug DC862 · Emergency LightingSDR K4HA99106Skin · corrodedPERU - LEFT WING LEADING EDGE SURFACE SKIN CORROSION. ATTACHMENT POINTS WS 485.000 TO WS 710.000. REMOVED L/E SKIN, FABRICATED NEW SKIN AND INSTALLED IAW SRM 51-2-21. REF: AIA EA: D8-57-078 . WORK ACCOMPLISHED UNDER AIA FORM M-40 CONTROL NR 26719. (X)Nov 27, 1999 · N803CK · Doug DC862 · Wing, Plate/SkinSDR K4HA99092Skin · crackedPERU - DURING ROUTINE ACCOMPLISHMENT OF SCHEDULED C-CHECK AND CPCP CARDS, FOUND RT CENTER WING AREA UPPER SKIN SURFACE CRACK, 1.25 INCH CRACK. RT CENTER WING AREA UPPER SURFACE SKIN AT STA WFS 65000. CUT OUT DAMAGED AREA, FABRICATED FILLER AND DOUBLER AND INNov 27, 1999 · N803CK · Doug DC862 · Wing, Plate/SkinSDR RRXA991586Valve · inoperativeDURING FLIGHT AT FL 26.0 MADE AN EMERGENCY DESCENT DUE TO LOSS OF CABIN PRESSURIZATION. REPLACED LEFT AND RIGHT PRESSURIZATION VALVES. PERFORMED PRESSURIZATION CHECK PER MM 21-31-00 WITH ENGINES 2 AND 3 RUNNING. PRESSURIZED TO 8.0 PSID, NO LEAK OR DEFECTS NNov 24, 1999 · N993CF · Doug DC862 · Cabin Pressure Control SystemSDR IXXA9900032Fan · failedEN ROUTE FROM QPG TO NKW, AN ELECTRICAL ODOR WAS SENSED IN THE COCKPIT WHEN THE RIGHT RECIRCULATING FAN WAS TURNED ON. THE FLIGHT CREW SECURED THE FAN AND THE ODOR SUBSIDED AND THE FLIGHT CONTINUED TO NKW. MAINTENANCE INSPECTED THE FAN AND WAS FOUND DEFECTIVENov 23, 1999 · N728PL · Doug DC862 · Air Distribution SystemSDR RRXA991585Controller · malfunctionedAT FL 260, AIRCRAFT EXPERIENCED A RAPID CLIMB IN CABIN PRESSURE CREW DESCENDED TO FL 120 AND LANDED IN (MKE). PRESSURIZED A/C TO 1.5 DPSI NO MAJOR LEAKS NOTED. INSPECTED ALL DOOR SEALS, AIRCRAFT EXTERIOR AND OUT FLOW VALVE. NO DEFECTS NOTE. A/C IS SAFE FORNov 19, 1999 · N993CF · Doug DC862 · Cabin Pressure Control SystemSDR K4HA99089Skin · corrodedPERU - DURING ROUTINE ACCOMPLISHMENT OF SCHEDULED C-CHECK AND CPCP TASK CARDS, FOUND CORROSION ON STUB WING NR 2 AT STA XRS-220.00 TO XRS-260.00. SPOTS OF CORROSION ALONG LEADING EDGE OF STUB WING. (X)Nov 18, 1999 · N803CK · Doug DC862 · Wing, Plate/SkinSDR ABXA9900776Engine · low powerDURING FUNCTIONAL CHECK FLIGHT (FCF), ON INITIAL LEVEL-OFF, WHEN POWER WAS REDUCED TO IDLE, NR 3 ENGINE N1 WAS LOWER THAN OTHER ENGINES. WHEN THROTTLES WERE ADVANCED, NR 3 ENGINE DID NOT ACCELERATE. LOW OIL PRESSURE LIGHT ILLUMINATED. INDICATED OIL PRESSURNov 9, 1999 · N801AX · Doug DC862 · Engine (Turbine/Turboprop)SDR ABXA9900796Skin · crackedDURING C-CHECK, CRACK INDICATIONS WERE FOUND IN SEVERAL RIGHT WING UPPER AFT SKIN PANEL 505F ATTACH HOLES. REPAIRED IAW ABX REA D857-33607MR.Nov 8, 1999 · N801AX · Doug DC862 · Wing, Plate/SkinSDR ABXA9900770Skin · crackedDURING C-CHECK, FOUND CRACK INDICATIONS IN LEFT WING UPPER AFT SKIN PANEL 505F. REPAIRED IAW ABX REA D857-33611MR.Nov 8, 1999 · N801AX · Doug DC862 · Wing, Plate/SkinSDR ABXA9900765Longeron · crackedDURING C-CHECK, FOUND LONGERON 34 AND 36 RIGHT, STATION 1185 CRACKED AT PRODUCTION SPLICE. REPAIRED IAW ABX REA D853-33152MR.Nov 3, 1999 · N801AX · Doug DC862 · Fuselage Main, Longeron/StringerSDR ARWA991003Adc · failedMIA - FLT 431 - MODE C INOPERATIVE BOTH TRANSPONDERS. REMOVED AND REPLACED NR 2 AIR DATA COMPUTER. PERFORMED OPS CHECK, TESTED AND INSPECTED BOTH ATC TRANSPONDERS. FOUND TO COMPLY WITH FAR 43 APPENDIX 'E' PAR SMALL "C" OPS NORMAL. PERFORMED PITOT STATIC LEOct 28, 1999 · N8969U · Doug DC862 · Air Data ComputerSDR ABXA9900754Generator · defectiveFAULT ON NR 4 GENERATOR. UNABLE TO RESET IAW ABNORMAL CHECKLIST. SECURED ENGINE, MAINTAINED POSITIVE ENGINE OIL PRESSURE. INSPECTED MAIN OIL FILTER, FOUND NO CONTAMINATION. CHECKED OIL QUANTITY, RAN ALL ENGINES, ENGINE RUN WAS NORMAL. CHECKED AIRCRAFT WIRIOct 28, 1999 · N808AX · Doug DC862 · AC Generator-AlternatorSDR ARWA991002Switch · failedMIA - FLT 751 - AIR TURNBACK, ON GER RETRACT DOOR NOT LATCHED. LIGHT REMAINS ILLUMINATED. PERFORMED ABNORMAL CHECKLIST 4 TIMES. LIGHT REMAINS ON. TROUBLESHOT, FOUND LEFT MAIN GEAR DOOR SWITCH FAULTY. REMOVED AND REPLACED SWITCH. OPS CHECK NORMAL IAW MM 3Oct 24, 1999 · N810BN · Doug DC862 · Landing Gear Door Retract SectionSDR IXXA9900026Unknown · odorEN ROUTE FROM AVB TO RMS, THE FLIGHT CREW SENSED AN ODOR IN THE COCKPIT WHEN THE OVER HEAD FLORESENT LIGHTING SYSTEM WAS ILLUMINATED. THE CREW TURNED THE LIGHTS OFF AND THE ODOR SUBSIDED, THE FLIGHT CONTINUED TO RMS FOR AN UNEVENTFUL LANDING. MAINTENANCE INSOct 21, 1999 · N61CX · Doug DC862 · Air Distribution SystemSDR ARWA991001Fire Loop · failedMIA - FLT 447 - AT 14,000 FT ALT, NR 1 ENGINE FIRE WARNING SOUNDED. ENGINE SHUTDOWN. OIL QTY AND OIL PRESSURE NORMAL AND OIL TEMP HIGH AT 140 DEGREES. REMOVED AND REPLACED NR 1 ENGINE MAIN OIL SCREEN. NO CONTAMINATION FOUND. REMOVED DISCHARGED FIRE BOTTLEOct 16, 1999 · N802BN · Doug DC862 · Fire DetectionSDR ABXA9900792Vane · delaminatedLEFT FLAP VANE ASSEMBLY WAS 50 PERCENT DELAMINATED. REPAIRED UNIT COMPLETE.Oct 14, 1999 · N801AX · Doug DC862 · Trailing Edge FlapsSDR ABXA9900691Skin · corrodedSKIN CORRODED AT STATION 240, BELOW LONGERON 3 LEFT. REPAIRED IAW ABX REA D853-32664MR.Sep 2, 1999 · N808AX · Doug DC862 · Fuselage Main, Plate/SkinSDR ABXA9900690Fitting · crackedLONGERON SPLICE FITTING CRACKED AT STATION 390 AND LONGERON 33 -35 RIGHT. REPAIRED IAW ABX REA D853-32693MR.Sep 2, 1999 · N808AX · Doug DC862 · Fuselage Miscellaneous StructureSDR RRXA991377Valve · malfunctionedAFTER TAKEOFF, DURING RIGHT TURN AIRCRAFT HAD STUDDERING, TURNING OUT OF TURN SAME BUFFETING EFFECT IN AIRFRAME. DID NOT FEEL IN YOKE, NO VISIBLE ENGINE INDICATIONS OF MALFUNCTION. NO LEFT TURNS MADE). FOUND RUDDER PRESSURE REDUCER VALVE BYPASSING. REMOVEDAug 31, 1999 · N993CF · Doug DC862 · Rudder Control SystemSDR 99T64R297ARSkin · corrodedNR 0928 - PREVIOUS REPAIR SKIN CORRODED AND CORROSION EMANATING FROM UNDER REPAIR DOUBLER RIGHT WING UPPER SKIN STATION XW 50 STRINGER 11. REMOVED DOUBLERS. REMOVED CORROSION AND REINSTALLED DOUBLERS IAW BOEING MESSAGE M-7200-99-0228. ARROW AIR (M)Aug 14, 1999 · N1808E · Doug DC862 · Wing, Plate/SkinSDR ABXA9900689Skin · crackedRIGHT WING UPPER INBOARD AFT SKIN PANEL HAD CRACK ABOVE REAR SPAR AT STATION XCW 69.5. REPAIRED IAW ABX REA D857-31961MR.Aug 9, 1999 · N804AX · Doug DC862 · Wing, Plate/SkinSDR ABXA9900688Skin · crackedLEFT WING UPPER INBOARD AFT SKIN PANEL HAD A CRACK ABOVE REAR SPAR AT STATION XCW 69.5. REPAIRED IAW ABX REA D857-31961MR.Aug 9, 1999 · N804AX · Doug DC862 · Wing, Plate/SkinSDR ABXA9900638Skin · crackedRIGHT WING UPPER INBOARD AFT SKIN PANEL CRACKED ABOVE REAR SPAR AT STATION XCW 69.5. REPAIRED IAW DC8 SRM 57-2-1 AND ABX REA D857-31961MR.Aug 9, 1999 · N804AX · Doug DC862 · Wing, Plate/SkinSDR ABXA9900637Skin · crackedLEFT WING UPPER INBOARD AFT SKIN PANEL HAD CRACK ABOVE REAR SPAR AT STATION XCW 69.5. REPAIRED IAW DC8 SRM 57-2-1 AND ABX REA D857-31961MR.Aug 9, 1999 · N804AX · Doug DC862 · Wing, Plate/SkinSDR ABXA9900687Frame · crackedCHANNEL FRAME CRACKED AT STATION 1114.5, NR 3 CARGO COMPARTMENT. REPAIRED IAW ABX REA D853-31931MR.Aug 4, 1999 · N804AX · Doug DC862 · Fuselage Main, FrameSDR ABXA9900632Frame · crackedCHANNEL FRAME CRACKED AT STATION 1114.5 FRAME AT NR 3 CARGO COMPARTMENT DOOR JAMB. REPAIRED IAW ABX REA D853-31931MR.Aug 4, 1999 · N804AX · Doug DC862 · Fuselage Main, FrameSDR ARWA990704Structure · crackedMIA - FLT 574 - DURING ROUTINE INSPECTION DURING MAIN CARGO DOOR MAINTENANCE, DETECTED APPROXIMATELY 10 INCH CRACK IN STC DOUBLER EMANATING LOWER FORWARD CORNER AT CUSP LINE. AFTER GAINING INTERNAL ACCESS TO AREA, FOUND 5 EACH FLOORBEAM TO LOWER SILL FITTINGSJul 27, 1999 · N802BN · Doug DC862 · Fuselage Main, StructureSDR ARWA990703Outflow Valve · lack of lubeMIA - FLT 627 - UNABLE TO PRESSURIZE AIRCRAFT IN AUTO OR MANUAL DURING TAKEOFF. DUMPED FUEL AND RETURNED TO MIA WITHOUT INCIDENT. AIRCRAFT INVESTIGATED FOR DEFECTS. PRESSURIZATION NORMAL IAW MM 21-30-00. LUBED OUTFLOW VALVE AS PRECAUTIONARY. CHECKED NORMAJul 25, 1999 · N1804 · Doug DC862 · Pressure Regulator/Outflow ValveSDR RRXA991541Strap · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, TO CIRCUMFERENCIAL STRAP AT STA 1180, LONGERON 34 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW CIRCUMFERENCIAL STRAP IAW DC8Jul 23, 1999 · N993CF · Doug DC862 · Fuselage Miscellaneous StructureSDR RRXA991174Plate · damagedREPAIR MAIN CARGO DOOR UPPER JAMB HANGER PLATE PER COTNEY ENG DRW. REPAIRED MAIN CARGO DOOR UPPER JAMBHEADER PLATE PER COTNEY ENG'G DWG EAH 70-1, EMERY DWG NR 70-R01, STC1802SD.Jul 23, 1999 · N990CF · Doug DC862 · Fuselage Miscellaneous StructureSDR RRXA991528Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, RIGHT WING SKIN AT STA XCW=69.5 AND STRINGER 9 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8.. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DAC DWG EAF-MIA-99-0032RR.Jul 22, 1999 · N993CF · Doug DC862 · Wing, Plate/SkinSDR 99T64R348ARDuct · chafedLEFT UPPER NOSE SECTION AC DUCT (HORSE SHOE) DUCT HAS HOLE CHAFFED IN IT. FABRICATED DOUBLER STRAP AND WELDED TO DUCT IAW BOEING MESSAGE M-7200-99-03383. (M)Jul 15, 1999 · N1808E · Doug DC862 · Air Distribution SystemSDR 99T64R344ARSkin · dentedRIGHT WING BOTTOM OUTBOARD OF RIGHT MLG PANEL DENTED IN TWO PLACES STATION XW90. NDT AREA, NO CRACKS NOTED, FILLED DENTS WIT HYSOL EA 934 NA, FABRICATED DOUBLER AND INSTALLED PER EO 99-061. (M)Jul 15, 1999 · N1808E · Doug DC862 · Wing, Plate/SkinSDR 99T64R358ARTube · looseLEFT NOSE SCOOP ANTI-ICE TUBE T PULLED LOOSE FROM DUCT OUTBOARD OF VALVE. REINSTALLED T AND WELDED PER EO 99-061. (M)Jul 9, 1999 · N1808E · Doug DC862 · Airfoil Anti/De-ice SystemSDR 99T64R357ARTube · chafedRIGHT NOSE CHIN SCOOP ANTI-ICE TUBE T PULLED LOOSE AND CHAFFED HALF THROUGH O/B OF VALVE. WELDED CHAFFED AREA, REINSTALLED T TUBE AND WELDED PER EO 99-061. (M)Jul 9, 1999 · N1808E · Doug DC862 · Airfoil Anti/De-ice System
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