Mcdonnell Douglas DC-8-71

Service difficulty reports · 341

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 = 'DC871'
  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 IXXA96104Coalescer · looseEN ROUTE FROM BNA-FLL AT FLT LEVEL 350, OIL SMOKE/MIST WAS NOTED IN THE COCKPIT. THE RIGHT PACK SYSTEM WAS SUSPECTED AND SHUT DOWN FOR THE REMAINDER OF THE FLIGHT. MAINTENANCE FOUND AND SECURED A LOOSE CLAMP AT THE WATER SEPARATOR/COALESCER. OPERATIONALLY CHJul 4, 1996 · N826BX · Doug DC871 · Humidity Control SystemSDR IXXA96103Downlock Sw · intermittentON DESCENT INTO SAN, LANDING GEAR UNSAFE LIGHT ILLUMINATED ACCOMPANIED BY THE WARNING HORN WHEN FLAPS SELECTED TO 50 DEGREES. GEAR CYCLED SEVERAL TIMES UNTIL SAFE INDICATION WAS OBTAINED. LANDING WAS UNEVENTFUL. MAINTENANCE REPLACED THE LEFT DOWNLOCK SWITCHJun 27, 1996 · N826BX · Doug DC871 · Landing Gear Position and WarningSDR IXXA96120Control Cable · brokenON TAXI OUT AND FLIGHT CONTROL CHECKS AT ATL, AILERONS FELT STIFF WITH VERY LITTLE SPOILER PRESSURE DROP. THE AIRCRAFT RETURNED TO RAMP. MAINTENANCE INSPECTED THE FLIGHT CONTROL CABLES AND FOUND THE LEFT AILERON BUS CABLE BROKEN. MAINTENANCE REPLACED THE BRJun 26, 1996 · N824BX · Doug DC871 · Aileron Control SystemSDR IXXA96102Downlock Sw · dirtyUPON GEAR EXTENTION INTO TOL, LEFT GEAR INDICATION LIGHT ILLUMINATED IMMEDIATELY. ALL GEAR LIGHTS ILLUMINATED WITH GEAR UNSAFE LIGHT. GEAR WAS CYCLED, EXTENTION WAS NORMAL EXCEPT LEFT GEAR LIGHT CAME ON IMMEDIATELY. MAINTENANCE FOUND LEFT GEAR DOWNLOCK SWITJun 25, 1996 · N826BX · Doug DC871 · Landing Gear Position and WarningSDR IXXA9688Control Valve · intermittentANTI-SKID FAIL LIGHT ILLUMINATED ON TAKEOFF ROLL DEPARTING ICT TO OKC. GEAR WAS RECYCLED AND THE LIGHT EXTINGUISHED. AIRCRAFT LANDING AT OKC WAS UNEVENTFUL. MX REPLACED THE RIGHT OUTBOARD ANTI-SKID DUAL CONTROL SERVO VALVE. THE SYSTEM OPERATIONALLY CHECKEDJun 11, 1996 · N823BX · Doug DC871 · Brake Anti-Skid SectionSDR IXXA9687Air Distr · odorEN ROUTE TOL-BFI - A STRONG SMELL OF HOT ELECTRICAL EQUIPMENT WAS NOTED IN THE VICINITY OF THE CIRCUIT BREAKER PANEL BULKHEAD. MX POWERED UP ALL EQUIPMENT ON THE GROUND WITH NO DEFECTS NOTED. AIRCRAFT WAS RETURNED TO SERVICE. (M)Jun 9, 1996 · N829BX · Doug DC871 · Air Distribution SystemSDR IXXA9685Air Distr · odorEN ROUTE FROM TOL-DFW - THE FLIGHT CREW NOTED A FAINT SULPHUR LIKE ODOR PRESENT AT TIMES IN COCKPIT, POSSIBLY COMING FROM THE COCKPIT LIGHTING. ON THE GROUND IN DFW, THE COCKPIT LIGHTS WERE OPERATED AND INSPECTED. THE COCKPIT LIGHTING SYSTEMS OPERATED NORMALJun 1, 1996 · N829BX · Doug DC871 · Air Distribution SystemSDR IXXA9684Eng Anti-Ice · odorEN ROUTE BETWEEN DFW AND TOL, THE USE OF THE NR 2 ENGINE ANTI-ICE PRODUCED AN ODOR SIMILAR TO A BURNED MATCH, BUT THE ODOR DISSIPATED OVER THE COURSE OF THE FLIGHT. IN TOL, A GROUND RUN WAS ACCOMPLISHED WITH THE AIRCRAFT CLOSED. BOTH AIR CONDITIONING PACKS WJun 1, 1996 · N829BX · Doug DC871 · Engine Anti-Icing SystemSDR IXXA9683Fire Warning · shortedEN ROUTE FROM DEN-TOL - THE NR 4 ENGINE FIRE WARNING SHORT CIRCUIT LIGHT CAME ON INTERMITTENTLY, FOLLOWED BY A STEADY LIGHT. AFTER THREE MINUTES, THE SYSTEM WOULD NO LONGER TEST. SHORTLY THEREAFTER, THE FIRE WARNING LIGHT ILLUMINATED AND THE ENGINE WAS SHUT May 30, 1996 · N824BX · Doug DC871 · Fire DetectionSDR IXXA9679Air Distr · odorIN CRUISE BETWEEN BFI AND TOL, IT WAS NOTED THAT A SMOKEY OR OILY SMELL WAS COMING OUT OF THE AIR CONDITIONING SYSTEM IN THE COCKPIT AND COURIER AREAS. IN TOL, MAINTENANCE CLEANED THE RECIRC FAN SCREEN, SERVICED THE LAV, AND RAN THE AIR CONDITIONING PACKS. NMay 17, 1996 · N829BX · Doug DC871 · Air Distribution SystemSDR IXXA9677Channel · crackedDURING ROUTINE C-CHECK INSPECTION, A CRACK WAS FOUND IN THE INBOARD FLAP, OUTBOARD END, UPPER CENTER CHANNEL SECTION. THE CRACKED PART WAS REMOVED, FABRICATED AND INSTALLED IAW EO 8-57-067-96, AND THE AIRCRAFT SRM 51-2-0. (X)Apr 13, 1996 · N829BX · Doug DC871 · Trailing Edge FlapsSDR IXXA9673Panel · delaminatedDURING ROUTINE C-CHECK INSPECTION, A LEFT WING TRAILING EDGE HONEYCOMB PANEL WAS FOUND DELAMINATED ON THE LEFT WING UPPER SURFACE BETWEEN STATIONS XRS 436. AND XA 588.5. THE PANEL WAS REPAIRED IAW DRAWING 8-57-066-96, WHICH IS FAA DER APPROVED. (X)Apr 12, 1996 · N829BX · Doug DC871 · Wing, Plate/SkinSDR IXXA9671Skin · crackedDURING ROUTINE C-CHECK INSPECTION, THE FUSELAGE PLATING AT THE EXTERNAL POWER RECEPTACLE WAS FOUND CRACKED. THE CRACK WAS LOCATED BETWEEN LONGERONS 31 AND 32 RT, AT FS -50. THE CRACK WAS REMOVED, REPAIR FILLERS, DOUBLERS WERE FABRICATED AND INSTALLED IAW DRAApr 11, 1996 · N829BX · Doug DC871 · Fuselage Main, Plate/SkinSDR IXXA9670Splice Fitting · crackedDURING ROUTINE C-CHECK INSPECTION, LONGERON 33 LEFT, SPLICE FITTING, AT STA 1694, WAS FOUND CRACKED. THE CRACK WAS .375 INCH IN LENGTH AT THE FORWARD END OF THE FITTING. THE CRACK WAS REMOVED FROM THE SPLICE FITTING AND REINSTALLED IAW DRAWING COO-SJO-96-013Apr 11, 1996 · N829BX · Doug DC871 · Fuselage Miscellaneous StructureSDR IXXA9676Skin · damagedDURING ROUTINE C-CHECK INSPECTION, THE FUSELAGE EXTERIOR PLATING WAS FOUND DAMAGED. DAMAGE WAS LOCATED AT THE FORWARD LOWER, RIGHT AFT CORNER OF THE NR 1 BASKET DOOR CUT-OUT, AT FS 340. THE DAMAGED AREA WAS REMOVED. THE REPAIR WAS ACCOMPLISHED BY FABRICATINApr 9, 1996 · N829BX · Doug DC871 · Fuselage Main, Plate/SkinSDR IXXA9675Skin · damagedDURING ROUTINE C-CHECK INSPECTION, DAMAGED WAS NOTED TO THE LOWER FORWARD CARGO COMPARTMENT DOOR CUT-OUT AT THE FORWARD EDGE. THE DAMAGE WAS REMOVED, REPAIR FILLER AND DOUBLERS WERE FABRICATED AND INSTALLED IAW DRAWING 8-53-27-96, WHICH IS FAA DER APPROVED. Apr 9, 1996 · N829BX · Doug DC871 · Fuselage Main, Plate/SkinSDR IXXA9674Panel · delaminatedDURING ROUTINE C-CHECK INSPECTION, A RIGHT WING TRAILING EDGE FIXED PANEL WAS FOUND DELAMINATED. THE PANEL WAS DELAMINATED BETWEEN WING STATIONS XA 589.0 AND XA 624.0. REPAIR OF THE PANEL WAS ACCOMPLISHED INSTALLING AN EXTERNAL DOUBLER IAW DRAWING 8-57-064-9Apr 9, 1996 · N829BX · Doug DC871 · Wing, Plate/SkinSDR IXXA9672Skin · crackedDURING ROUTINE C-CHECK INSPECTION, AN EXTERNAL FUSELAGE SKIN CRACK, LOCATED AT FS 336.5 AND LONGERON 36, WAS FOUND. THE DAMAGED SKIN WAS REMOVED, FILLERS AND DOUBLERS FABRICATED AND INSTALLED. THE REPAIR WAS IAW WITH DRAWING 8-53-29-96, WHICH IS FAA DER APPRApr 9, 1996 · N829BX · Doug DC871 · Fuselage Main, Plate/SkinSDR IXXA9646Brakes · looked upDURING LANDING AT BOS, THE NR 5 BRAKE EXPERIENCED SHINGLED LININGS, CAUSING THE BRAKE TO LOCK UP AND BLOW THE NR 5 MAIN TIRE. THE NR 5 BRAKE AND MAIN TIRE WERE REPLACED, AND THE AIRCRAFT WAS RETURNED TO SERVICE. THE NR 6 MAIN TIRE CHANGE WAS CARRIED OVER TO Mar 28, 1996 · N823BX · Doug DC871 · Landing Gear Brake SystemSDR IXXA9639Switch · dirtyMKE - WHEN LANDING GEAR WAS RETRACTED ON TAKEOFF, DOOR WARNING LIGHT REMAINED ILLUMINATED. THE GEAR WAS CYCLED, BUT THE INDICATION REMAINED THE SAME. UPON ARRIVAL AT TOL, MAINTENANCE INSPECTED THE MLG DOOR AND FOUND THE LANDING GEAR DOOR STRIKER AND SWITCH DMar 22, 1996 · N823BX · Doug DC871 · Entrance StairsSDR RRXA9600009Engine · lost powerKPDX/KSJC - FLT 502 - NR 1 ENGINE LOST POWER DURING CLIMB. OIL PRESSURE WENT TO ZERO WHILE ENGINE STILL ROTATING AT 20 PERCENT N2. SHUT-DOWN PROCEDURES ACCOMPLISHED. MAINTENANCE INSPECTED THE NR 1 ENGINE INLET AND EXHAUST, NO DEFECTS NOTED. MAINTENANCE REMFeb 29, 1996 · N8177U · Doug DC871 · Engine (Turbine/Turboprop)SDR RRXA9600008Fire Wire · chafedKLRD/KDAY - FLT 019 - ON DESCENT, NR 4 ENGINE SHORT CIRCUIT LIGHT ILLUMINATED FOLLOWED BY AN INTERMITTENT FIRE BELL. PRECAUTIONARY SHUT DOWN OF NR 4 ENGINE WAS ACCOMPLISHED. MAINTENANCE REPAIRED A CHAFED WIRE AT THE FORWARD END OF RT AFT FIRE LOOP. AN OPERAFeb 29, 1996 · N8177U · Doug DC871 · Fire DetectionSDR IXXA9634Web · crackedDURING THE D-CHECK INSPECTION, FOUND CRACKS ON RT WEB AT FS 781.500. REPAIR WAS ACCOMPLISHED PER DACO SRM 53-8-1, 51-1-4, 51-1-8, 53-2-0, AND 51-1-21. (X)Feb 26, 1996 · N820BX · Doug DC871 · Fuselage Miscellaneous StructureSDR IXXA9633Frame · crackedDURING THE D-CHECK INSPECTION, FOUND CRACKS ON FRAME AT FS 781.500, L35R. REPAIR WAS PERFORMED PER DACO SRM 53-8-1,51-1-4, 51-1-8, AND 51-1-21. (X)Feb 26, 1996 · N820BX · Doug DC871 · Fuselage Main, FrameSDR IXXA9632Blkhd Cover · crackedDURING THE D-CHECK INSPECTION, FOUND CRACKS ON THE BULKHEAD COVER AT FS 857.125. REPAIR WAS PERFORMED PER DACO SRM 51-1-4, 51-1-8, 51-1-21, AND 53-2-0. (X)Feb 26, 1996 · N820BX · Doug DC871 · Fuselage Main, BulkheadSDR IXXA9631Skin · dentedDURING THE D-CHECK INSPECTION, FOUND DENTS IN THE OUTER SKIN OF THE AFT LOWER CARGO DOOR. REPAIR WAS PERFORMED PER DACO SRM 52-4-1,52-2-0, 51-1-4, 51-1-8, AND 51-1-21A. (X)Feb 26, 1996 · N820BX · Doug DC871 · Cargo/Baggage DoorsSDR IXXA9630Fitting · crackedDURING THE D-CHECK INSPECTION, FOUND A CRACK ON THE NR 1 PYLON SUPPORT FITTING AT FS YN 387 IN 2EA LOCATIONS. MANUFACTURED FITTING PER DACO DRAWING 5756790 AND INSTALL FITTING PER DACO DRAWINGS 5756791, 5756801, AND DACO SRM 51-00, 51-1-20, 51-3-0, AND 51-1-8Feb 26, 1996 · N820BX · Doug DC871 · Nacelle/Pylon StructureSDR IXXA9629Skin · crackedDURING THE D-CHECK INSPECTION, FOUND A CRACK ON THE AFT PASSENGER DOOR ON THE LOWER AFT CORNER. A REPAIR WAS PERFORMED PER DACO SRM 53-2-0, 51-1-20D, 51-1-21A, 51-1-8, 51-00, AND DRAWING CF-N820BX-13/96. (X)Feb 26, 1996 · N820BX · Doug DC871 · Passenger/Crew DoorsSDR IXXA9628Angle · corrosionDURING THE D-CHECK INSPECTION, FOUND CORROSION ON FLOOR SUPPORT ANGLE AT FS 580, L33R TO L33L, IN THE FWD CARGO COMPARTMENT. A REPAIR WAS ACCOMPLISHED PER DACO SRM 51-1-21, 51-1-8, AND 51-00. (X)Feb 26, 1996 · N820BX · Doug DC871 · Fuselage Miscellaneous StructureSDR IXXA9627Angle · corrosionDURING THE D-CHECK INSPECTION, FOUND CORROSION ON FLOOR SUPPORT ANGLE AT FS 600, L34R TO L34L, IN THE FWD CARGO COMPARTMENT. A REPAIR WAS ACCOMPLISHED PER DACO SRM 51-1-21, 51-1-8, AND 51-00. (X)Feb 26, 1996 · N820BX · Doug DC871 · Fuselage Miscellaneous StructureSDR IXXA9626Support · corrosionDURING THE D-CHECK INSPECTION, FOUND CORROSION ON STRUT SUPPORT LOWER LT SIDE AT FS 1460 IN THE AFT CARGO COMPARTMENT. A REPAIR WAS ACCOMPLISHED PER DACO SRM 51-1-21, 51-1-8, AND 51-00. (X)Feb 26, 1996 · N820BX · Doug DC871 · Fuselage Miscellaneous StructureSDR IXXA9625Le Formers · crackedDURING THE D-CHECK INSPECTION, FOUND TWO CRACKED FORMERS AT FS NR 422. REPAIR WAS ACCOMPLISHED PER DACO SRM 57-3-1 AND 57-0 CODE 5 AND DRAWING CF-N820, 7/96 DATED 1/18/96 WHICH HAS APPROVAL ON FAA FORM 8110-3 DATED 1/22/96. (M)Feb 26, 1996 · N820BX · Doug DC871 · Wing Miscellaneous StructureSDR IXXA9624Skin · crackedDURING THE D-CHECK INSPECTION, FOUND DAMAGE ON RIGHT LOWER FLAP AT FS NR 215. REPAIR WAS ACCOMPLISHED BY INSTALLING NEW SKIN PANEL PER DRAWING CF-N820BX, 2/96 DATED 1/6/96 AND WAS APPROVED BY FAA FORM 8110-3 DATED. (M)Feb 26, 1996 · N820BX · Doug DC871 · Trailing Edge FlapsSDR IXXA9623Jamb · dentedDURING THE D-CHECK INSPECTION, FOUND DENTS AND SCRATCHES AT FWD CARGO DOOR UPPER DOOR JAMB OF 'A' PIT AT FS NR 250. REPAIR WAS ACCOMPLISHED PER DRAWING CF-N820BX-11/96 DATED 1/27/96 AND APPROVED ON FAA FORM 8110-3 DATED 2/2/96. (M)Feb 26, 1996 · N820BX · Doug DC871 · Fuselage Miscellaneous StructureSDR IXXA9622Cowling · crackedDURING THE D-CHECK INSPECTION, FOUND CRACK ON THE INBOARD COWL ON ENGINE. REPAIR WAS ACCOMPLISHED PER DRAWING CF-N820BX, 10/96 DATED 1/18/96. REPAIR WAS APPROVED ON FAA FORM 8110-3 DATED 1/25/96. (M)Feb 26, 1996 · N820BX · Doug DC871 · Engine Cowling SystemSDR IXXA9621Fitting · crackedDURING THE D-CHECK INSPECTION, FOUND CRACKED FITTING ON THE RIGHT HORIZONTAL STABILIZER L/E AT FS XFS 47. FITTING WAS MANUFACTURED PER DRAWING CF-N820BX-15/96, DATED 2/9/96 AND WAS APPROVED BY FAA FORM 8110-3 DATED 2/20/96. (M)Feb 26, 1996 · N820BX · Doug DC871 · Horizontal Stabilizer StructureSDR IXXA9620Skin · crackedDURING THE D-CHECK INSPECTION, FOUND CRACK AT FS NR 360 TO 380, L30 RT. REPAIR WAS ACCOMPLISHED PER DRAWING CF-N820BX-3/96, DATED 1/9/96. THIS REPAIR WAS PERFORMED IAW DACO SRM AND MAINTENANCE MANUALS AND APPROVED ON FAA FORM 8110-3 DATED 1/31/96. (M)Feb 26, 1996 · N820BX · Doug DC871 · Fuselage Main, Plate/SkinSDR IXXA9619Skin · gougedDURING D-CHECK INSPECTION, GOUGED AREA WAS FOUND AT 'B' PIT DOOR JAMB AT FS NR 505, L31 RT. REPAIR WAS ACCOMPLISHED BY INSTALLING FILLER AND DOUBLER PER DRAWING NR CF-N820BX, 11/96, DATED 1/27/96. THIS DRAWING IS APPROVED UNDER DACO SRM AND MAINTENANCE MANUAFeb 26, 1996 · N820BX · Doug DC871 · Fuselage Main, Plate/SkinSDR RRXA9600007Connector Pin · pushed backFLT EB329 - KDAY-KICT - IN FLIGHT NR 2 ENGINE FIRE WARNING SOUNDED. DISCHARGED 1 BOTTLE AND WARNING STOPPED. APPROXIMATELY 5 MINUTES LATER FIRE WARNING SOUNDED AGAIN, DISCHARGED 2ND BOTTLE FIRE WARNING REMAINED ON. NR 2 ENGINE SHUT DOWN. MAINTENANCE FOUND Feb 13, 1996 · N8079U · Doug DC871 · Fire DetectionSDR IXXA9605Air Distr · odorEN ROUTE BETWEEN MKE AND DEN, THE AIR CONDITIONING PACKS WERE PRODUCING A STRONG, UNIDENTIFIED ODOR. ON THE GROUND IN DEN, THE PACKS WERE OPERATIONALLY CHECKED AND FOUND NOT TO BE PRODUCING AND ODOR AT THAT TIME. A REVIEW OF THE FLIGHT SUGGESTED THAT A SMALLJan 31, 1996 · N824BX · Doug DC871 · Air Distribution SystemSDR RRXA960003Filter · dirtyKOAK/KDAY - FLT 002 - 380 MILES OUT OF KOAK, NR 1 ENGINE FLAMED OUT. RESTART WAS NOT SUCCESSFUL. NR 1 ENGINE RESTART ACCOMPLISHED AT 10,000 FEET. MAINTENANCE REMOVED AND REPLACED NR 1 ENGINE FUEL FILTER, INSPECTED NR 1 ENGINE IGNITION SYSTEM, AND PERFORMED Jan 30, 1996 · N811AL · Doug DC871 · Engine Fuel DistributionSDR UPS805216Fitting · corrodedWHILE IN FOR B-CHECK, FOUND FITTING ON STRINGER 32R AT AFT BULKHEAD OF AIRCON COMP IS CORRODED. REMOVED AND REPLACED FITTING.Jan 13, 1996 · N702UP · Doug DC871 · Fuselage Miscellaneous StructureSDR IXXA9594Uplatch Cable · out of adjustON TAKEOFF FROM TOL TO ONT, THE CREW REPORTED AN UNSAFE GEAR AND DOOR LIGHT AFTER GEAR RETRACTION. THE AIRCRAFT RETURNED TO TOL FOR MAINTENANCE. THE AIRCRAFT WAS FERRIED TO A MAINTENANCE FACILITY FOR LANDING GEAR SYSTEM INSPECTION AND RIG CHECK. A RIG CHECJan 3, 1996 · N824BX · Doug DC871 · Landing Gear Retraction/Extension SystemSDR IXXA9608Engine · flamed outEN ROUTE FROM TOL TO SEA, THE NR 4 ENGINE FLAMED OUT AT 35,000 FEET. TWO UNSUCCESSFUL RESTART ATTEMPTS WERE MADE. THE ENGINE WAS SECURED AND THE AIRCRAFT DIVERETED TO MSO FOR MAINTENANCE. UPON ARRIVAL IN MSO, THE FLIGHT CREW REPORTED THEY SUMPED TANKS AND RJan 2, 1996 · N824BX · Doug DC871 · Engine (Turbine/Turboprop)SDR IXXA199589Connector · deterioratedWHEN THE LANDING GEAR UPLATCH CHECK WAS PERFORMED ON DEPARTURE OUT OF TOL, THE GEAR DOOR WARNING LIGHT REMAINED ON. THE AIRCRAFT ELECTED TO RETURN TO TOL FOR MAINTENANCE. TOL MAINTENANCE INSPECTED THE AIRCRAFT AND DETERMINED THAT THE ELECTRICAL CONNECTOR FOROct 21, 1995 · N824BX · Doug DC871 · Landing Gear Position and WarningSDR IXXA199587Flap Fitting · brokenAT MSP, IT WAS DISCOVERED THAT THE STATION 98 OUTBOARD FLAP BASE FITTING ON LEFT INBOARD FLAP SECTION HAD EXPERIENCED A TYPICAL FAILURE DUE TO A CRACK THAT ORIGINATED IN THE UPPER FLAP VANE ATTACH BOLT HOLE. THE OPPOSING BASE FITTING AT THAT STATION HAD RECIEOct 13, 1995 · N824BX · Doug DC871 · Trailing Edge FlapsSDR IXXA199585Uplatch Switch · failedON DEPARTURE OUT OF BOS, THE LANDING GEAR FAILED THE UPLATCH CHECK. THE LANDING GEAR WAS CYCLED THREE TIMES WITH THE SAME RESULT, WITH THE LANDING GEAR LEVER IN THE UPLATCH CHECK POSITION, THE UNSAFE LIGHT WAS ILLUMINATED WITH NO APPARENT GEAR EXTENSION. INSOct 10, 1995 · N824BX · Doug DC871 · Landing Gear Position and WarningSDR UPS804743Frame · corrodedWHILE IN FOR D-CHECK, MAINTENANCE FOUND RT FRAME CHORD SPLICE FITTING CORRODED AT STA 99 AS SEEN THROUGH PANEL 90B. MAINTENANCE FABRICATED SPLICE AND INSTALLED IAW SRM 51-1-20D, 51-1-20, 51-1-21, AND DC8-53-1476.Oct 4, 1995 · N798UP · Doug DC871 · Fuselage Main, FrameSDR UPS804742Frame · corrodedWHILE IN FOR D-CHECK, MAINTENANCE FOUND FRAME 1260 BETWEEN LONGERONS 35L AND 35R IS OUT OF LIMITS AFTER CORROSION REMOVAL. MAINTENANCE REMOVED CORROSION, FABRICATED REPAIR DOUBLER AND INSTALLED IAW SRM 53-2-0 AND 51-1-20.Oct 4, 1995 · N798UP · Doug DC871 · Fuselage Main, FrameSDR UPS804741Frame · corrodedWHILE IN FOR D-CHECK, MAINTENANCE FOUND FRAME FORMER CORRODED AT STA 1260 BETWEEN LONGERONS 35L AND 35R. MAINTENANCE FABRICATED REPLACEMENT SECTION AND INSTALLED IAW SRM 53-2-02B AND 53-4-1, FIGURE 51 AT STA 1260.Oct 4, 1995 · N798UP · Doug DC871 · Fuselage Main, Frame
Back to Mcdonnell Douglas DC-8-71