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 RRXA97126Frame · misdrilledDURING A MAINTENANCE VISIT, FOUND MISDRILLED HOLES IN FRAME RADIUS, AT Y=660 AND LONGERON 18R. PLUGGED MISDRILLED HOLES WITH E RIVETS. FABRICATED AND INSTALLED 2 GUSSETTS, 1 STRAP AND SHIM IAW DER APPROVED COTNEY ENGINEERING SKETCH C44-R49.May 19, 1997 · N994CF · Doug DC862 · Fuselage Main, FrameSDR RRXA97125Frame · misdrilledDURING A MAINTENANCE VISIT, FOUND MISDRILLED HOLES IN FRAME RADIUS, AT Y=1160 AND 11 INCHES ABOVE LONGERON 21L. FABRICATED AND INSTALLED REPAIR ANGLE AND SHIMS IAW DER APPROVED ENGINEERING SKETCH C44-R39.May 19, 1997 · N994CF · Doug DC862 · Fuselage Main, FrameSDR RRXA97124Plating · crackedDURING A MAINTENANCE VISIT, FOUND TOP PLATING OF LT LEADING EDGE CRACKED, AT XW=257.5. REMOVED DAMAGED AREA 0.85, FABRICATED AND INSTALLED 1 FILLER AND 2 DOUBLERS IAW DER APPROVED COTNEY ENGINEERING SKETCH C44-R44.May 19, 1997 · N994CF · Doug DC862 · Wing, Plate/SkinSDR RRXA97122Jamb Plate · crackedDURING A MAINTENANCE VISIT, FOUND MAIN CARGO DOOR UPPER JAMB PLATE BROKEN OUT AND CORRODED EDGES. REMOVED DAMAGED AREA, REMOVED CORROSION AND TREATED IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED FILLER AND DOUBLER REPAIR IAW DER APPROVED ENGINEERING SKETCH May 19, 1997 · N994CF · Doug DC862 · Cargo/Baggage DoorsSDR RRXA97121Frame · misdrilledDURING A MAINTENANCE VISIT, FOUND MISDRILLED HOLES IN FRAME RADIUS, AT Y=1300 AND LONGERON 21L. PLUGGED HOLES WITH E RIVETS, FABRICATED AND INSTALLED REPAIR IAW DER ENGINEERING SKETCH C44-R37 AND DC-8 SRM 51-1-8 AND 51-1-21.May 19, 1997 · N994CF · Doug DC862 · Fuselage Main, FrameSDR RRXA97120Frame · misdrilledDURING A MAINTENANCE VISIT, FOUND MISDRILLED HOLES IN FRAME, AT Y=280 LT AND GUSSET. FABRICATED AND INSTALLED REPAIR ANGLE, 4 CLIPS AND 5 GUSSETS IAW DER APPROVED ENGINEERING SKETCH C44-R28. TREATED AREA IAW DC-8 SRM 51-1-8 AND 51-1-20B.May 19, 1997 · N994CF · Doug DC862 · Fuselage Main, FrameSDR RRXA97119Frame · misdrilledDURING A MAINTENANCE VISIT, FOUND MISDRILLED HOLES IN FRAME DOUBLER, AT Y=440, AND 12 INCHES ABOVE LONGERON 21R. FABRICATED AND INSTALLED REPAIR IAW DER APPROVED ENGINEERING SKETCH C44-R26.May 19, 1997 · N994CF · Doug DC862 · Fuselage Main, FrameSDR RRXA97118Frame · misdrilledDURING A MAINTENANCE VISIT, FOUND MISDRILLED HOLES IN FRAME, AT Y=1080, AND 28 INCHES ABOVE LONGERON 21L. PLUGGED HOLES WITH E RIVETS, FABRICATED AND INSTALLED REPAIR IAW DER APPROVED COTNEY ENGINEERING SKETCH C44-R32 AND DC-8 SRM 51-1-8 AND 51-1-21.May 19, 1997 · N994CF · Doug DC862 · Fuselage Main, FrameSDR RRXA97117Frame · misdrilledDURING A MAINTENANCE VISIT, FOUND MISDRILLED HOLE IN FRAME RADIUS, AT Y=1020 AND LONGERON 21L. PLUGGED HOLE, FABRICATED AND INSTALLED REPAIR IAW DER COTNEY ENGINEERING SKETCH C44-R29.May 19, 1997 · N994CF · Doug DC862 · Fuselage Main, FrameSDR RRXA97116Frame · misdrilledDURING A MAINTENANCE VISIT, FOUND MISDRILLED HOLES IN FRAME RADIUS, AT Y=560 AND LONGERON 21L. PLUGGED MISDRILLED HOLES WITH E RIVETS, FABRICATED AND INSTALLED 1 ANGLE REPAIR IAW DER APPROVED COTNEY ENGINEERING SKETCH C44-47.May 19, 1997 · N994CF · Doug DC862 · Fuselage Main, FrameSDR RRXA97114Frame · misdrilledDURING A MAINTENANCE VISIT, FOUND MISDRILLED HOLES IN FRAME RADIUS, AT Y=1140 AND 11 INCHES ABOVE LONGERON 21L. PLUGGED 3 HOLES WITH E RIVETS, FABRICATED AND INSTALLED REPAIR IAW DER APPROVED COTNEY ENGINEERING SKETCH C44-R36 AND DC-8 SRM 51-1-21.May 19, 1997 · N994CF · Doug DC862 · Fuselage Main, FrameSDR RRXA97113Frame · misdrilledDURING A MAINTENANCE VISIT, FOUND MISDRILLED HOLE IN FRAME, AT Y=1140 AND 25 INCHES ABOVE LONGERON 21R. PLUGGED HOLE WITH E RIVET, FABRICATED AND INSTALLED REPAIR IAW DER APPROVED COTNEY ENGINEERING SKETCH C44-R10 AND DC-8 SRM 51-1-20D.May 19, 1997 · N994CF · Doug DC862 · Fuselage Main, FrameSDR RRXA97112Frame · misdrilledDURING A MAINTENANCE VISIT, FOUND MISDRILLED HOLES, AT Y=1240, 25 INCHES AND 3 INCHES ABOVE LONGERON 21R. FABRICATED AND INSTALLED REPAIRS IAW DER APPROVED COTNEY ENGINEERING SKETCH C44-R12 AND DC-8 SRM 51-1-8 AND 51-1-20D.May 19, 1997 · N994CF · Doug DC862 · Fuselage Main, FrameSDR RRXA97110Longeron · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION TO FUSELAGE SKIN AT LT REAR CARGO PIT Y=1230 TO 1240. ALSO, FOUND CORROSION ON LONGERON 31L. REMOVED FASTENERS AND OPEN AREA, REMOVED CORROSION FROM SKIN AND LONGERONS FORM Y=1190 TO Y=1310, TREATED AND PRIMED AREAMay 19, 1997 · N994CF · Doug DC862 · Fuselage Main, Longeron/StringerSDR RRXA97109Floorbeam · crackedDURING A MAINTENANCE VISIT, FOUND CRACK ON FLOORBEAM, AT Y=500 AND 6 INCHES INBD FROM LT O/B END OF BEAM TOP FLANGE. FABRICATED AND INSTALLED 1 ANGLE DOUBLER AND 1 DOUBLER SHIM AND FILLER IAW DER APPROVED COTNEY ENGINEERING SKETCH C44-R38 AND DC-8 SRM 51-1-8May 19, 1997 · N994CF · Doug DC862 · Fuselage Main, Floor BeamSDR RRXA97108Frame · misdrilledDURING A MAINTENANCE VISIT FOUND MISDRILLED HOLES IN FRAME RADIUS, AT Y=1060 AND 11 ABOVE LONGERON 21L. PLUGGED HOLES WITH E RIVETS, FABRICATED AND INSTALLED REPAIR IAW DER APPROVED COTNEY ENGINEERIG SKETCH C44-R35 AND DC-8 SRM 51-1-8 AND 51-1-21.May 19, 1997 · N994CF · Doug DC862 · Fuselage Main, FrameSDR RRXA97107Frame · misdrilledDURING A MAINTENANCE VISIT, FOUND MISDRILLED HOLE 5 PLACES JUST BELOW WINDOW, AT Y=460 AND BETWEEN LONGERONS 20R AND 21R. FABRICATED AND INSTALLED DOUBLER REPAIR IAW FAA DER APPROVAL BY COTNEY ENGINEERING SKETCH C44-R27, AND IAW DC-8 SRM 51-1-21.May 19, 1997 · N994CF · Doug DC862 · Fuselage Main, FrameSDR RRXA97105Frame · misdrilledDURING A MAINTENANCE VISIT, FOUND MIS-DRILLED HOLE IN VERTICAL LEG OF FRAME AND DOUBLER, AT Y=780 AND BETWEEN LONGERONS 18R AND 20R. *S/D* FABRICATED AND INSTALLED REPAIR IAW FAA DER COTNEY ENGINEERING SKETCH C44-R07.May 19, 1997 · N994CF · Doug DC862 · Fuselage Main, FrameSDR RRXA97104Frame · misdrilledDURING A MAINTENANCE VISIT, FOUND MIS-DRILLED HOLE IN FRAME AND FRAME INTERCOASTAL ATTACHMENT ANGLE, AT Y=1240, 14 ABOVE LONGERON 21 RIGHT. *S/D* FABRICATED AND INSTALLED REPAIR ANGLES IAW FAA DER COTNEY ENGINEERING SKETCH C44-R12 AND DC-8 SRM 51-1-8, 51-1-2May 19, 1997 · N994CF · Doug DC862 · Fuselage Main, FrameSDR RRAX97128Frame · misdrilledDURING A MAINTENANCE VISIT, FOUND MISDRILLED HOLE IN FRAME RADIUS, AT Y=700 AND LONGERON 21R. FABRICATED AND INSTALLED REPAIR ANGLE AND SHIMS IAW DER APPROVED ENGINEERING SKETCH C44-R51.May 19, 1997 · N994CF · Doug DC862 · Fuselage Main, FrameSDR RRXA97115Frame · misdrilledDURING A MAINTENANCE VISIT, FOUND MISDRILLED HOLES IN FRAME FITTING, AT Y=800 AND LONGERON 21R. PLUGGED HOLES, FABRICATED STRAP AND SHIMS IAW DER APPROVED COTNEY ENGINEERING SKETCH C44-R09. TREATED, PRIMED AND INSTALLED REPAIR IAW DC-8 SRM 51-1-20D.May 17, 1997 · N994CF · Doug DC862 · Fuselage Main, FrameSDR RRXA97111Frame · misdriiledDURING A MAINTENANCE VISIT, FOUND MISDRILLED HOLE IN FRAME RADIUS, AT Y=1200 AND 25 INCHES ABOVE LONGERON 21R. FABRICATED AND INSTALLED REPAIR IAW DER APPROVED COTNEY ENGINEERING SKETCH C44-R11 AND DC-8 SRM 51-1-20D.May 17, 1997 · N994CF · Doug DC862 · Fuselage Main, FrameSDR CKSA97200Coupling · not secureON CLIMBOUT AT FL300, EXPERIENCED PRESSURE PROBLEMS AND WAS UNABLE TO CONTROL CABIN. DESCENDED TO FL180 AND CABIN THEN STABILIZED AT 10,000 FT. PROCEEDED TO SKBO AND DUMPED APPROX 21,000 LBS OF FUEL STARTED AT 0515Z DUMPED FOR 5 MINUTES THEN REPOSITIONED SWIMay 15, 1997 · N803CK · Doug DC862 · Cabin Pressure Control SystemSDR RRXA97159Doubler · corrosionDURING A MAINTENANCE VISIT, FOUND CORROSION AND BULGED AND POPPED RIVETS ON DOUBLER, AT Y=188 TO Y=208 AND X=+50. *S/D* REMOVED CORROSION FROM FINGER DOUBLER AND WEB IAW DC-8 SRM 51-1-8. REMOVED AND REPLACED FINGER DOUBLER IAW FAA DER COTNEY ENGINEERING SKEMay 12, 1997 · N994CF · Doug DC862 · Fuselage Miscellaneous StructureSDR ABXA9700996Hose · leakingDURING CLIMBOUT, RIGHT AFTER GEAR RETRACTION, HYDRAULIC QUANTITY DROPPED TO NEAR STANDPIPE LEVEL FOLLOWED BY A LOSS OF HYDRAULIC PRESSURE. REPLACED FLEX LINE AT LEFT MAIN GEAR BUNGEE CYLINDER AND THE LEFT AND RIGHT ENGINE DRIVEN PUMPS. SERVICED SYSTEM IAW DCMay 12, 1997 · N802AX · Doug DC862 · Hydraulic System, MainSDR RRXA97137Frame · crackedDURING A MAINTENANCE VISIT, FOUND MIS-DRILLED HOLE AND CRACKED IN FRAME AND FRAME INTERCOSTAL, AT Y=1240, AND 14 INCHES ABOVE UPPER CARGO COMPARTMENT FLOOR. *S/D* FABRICATED AND INSTALLED REPAIR ANGLE AND 3 EACH CLIPS IAW FAA DER COTNEY ENGINEERING SKETCH C4May 6, 1997 · N994CF · Doug DC862 · Fuselage Main, FrameSDR RRXA97140Floorbeam · misdrilledDURING A MAINTENANCE VISIT, FOUND MISDRILLED HOLE IN FLOORBEAM, AT Y=1460 AND X=-47.5. FABRICATED AND INSTALLED REPAIR IAW DER APPROVED COTNEY ENGINEERING SKETCH C44-R34, AND DC-8 SRM 51-1-20D.Apr 29, 1997 · N994CF · Doug DC862 · Fuselage Main, Floor BeamSDR RRXA97152Skin · gougedDURING A MAINTENANCE VISIT, FOUND INNER SKIN GOUGED, AT Y=512 AND BETWEEN LONGERONS 32R AND 33R. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DER APPROVED ENGINEERING SKETCH C44-R21.Apr 26, 1997 · N994CF · Doug DC862 · Fuselage Main, Plate/SkinSDR RRXA97141Floorbeam · misdrilledDURING A MAINTENANCE VISIT, FOUND MISDRILLED HOLE IN FLOORBEAM, AT Y=1420 AND X=+18. FABRICATED AND INSTALLED REPAIR ANGLE IAW DER COTNEY ENGINEERING SKETCH C44-R46. TREATED AREA IAW DC-8 SRM 51-1-8.Apr 25, 1997 · N994CF · Doug DC862 · Fuselage Main, Floor BeamSDR RRAX97145Pressure Panel · corrodedDURING A MAINTENANCE VISIT, FOUND PRESSURE PANEL CORRODED BEYOND LIMITATIONS, AT Y=920 AND X=+70. REMOVED CORROSION DAMAGE IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DER APPROVED COTNEY ENGINEERING SKETCH C44-R14.Apr 23, 1997 · N994CF · Doug DC862 · Fuselage Miscellaneous StructureSDR RRXA97160Floorbeam · corrosionDURING A MAINTENANCE VISIT, FOUND FLOORBEAM CORRODED PAST LIMITS IAW DC-8 SRM, AT Y=1440 AND X=-10.5. REMOVED AND TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DER APPROVED ENGINEERING SKETCH C44-R13.Apr 22, 1997 · N994CF · Doug DC862 · Fuselage Main, Floor BeamSDR RRXA97146Pressure Panel · corrodedDURING A MAINTENANCE VISIT, FOUND SUBFLOOR DOUBLER WITH 2 AREAS OF CORROSION DAMAGE, AT Y=902 TO Y=920 AND X=+4. REMOVED CORROSION DAMAGE IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FINGER DOUBLER AND SUBFLOOR PANEL IAW DER APPROVED COTNEY ENGINEERING Apr 21, 1997 · N994CF · Doug DC862 · Fuselage Miscellaneous StructureSDR RRXA97150Floorbeam · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION ON FLOORBEAM DAMAGE BEYOND LIMITS IAW DC-8 SRM, AT Y=920 AND X=+49.5. REMOVED CORROSION AND TREATED IAW DC-8 SRM. FABRICATED AND INSTALLED REPAIR IAW DER APPROVED ENGINEERING SKETCH C44-R19.Apr 20, 1997 · N994CF · Doug DC862 · Fuselage Main, Floor BeamSDR RRXA97151Floorbeam · buckledDURING A MAINTENANCE VISIT, FOUND FLOORBEAM BUCKLED, AT Y=1500 AND X=+4 TO X=+15. FABRICATED AND INSTALLED REPAIR IAW DER APPROVED ENGINEERING SKETCH C44-R20.Apr 19, 1997 · N994CF · Doug DC862 · Fuselage Main, Floor BeamSDR RRXA97139Frame · misdrilledDURING A MAINTENANCE VISIT, FOUND MISDRILLED HOLE IN WEB BETWEEN Y=492 AND Y=500 FRAME, ABOVE LONGERON 35R. REMOVED DAMAGED SECTION OF 0.25. TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DER COTNEY ENGINEERING SKETCH C44-RApr 19, 1997 · N994CF · Doug DC862 · Fuselage Main, FrameSDR RRXA97138Web · misdrilledDURING A MAINTENANCE VISIT, FOUND MIS-DRILLED HOLE IN WEB AT FWD SIDE OF X-SLIDE DOOR OPENING, AT Y=500 AND OTBD OF TRACK. *S/D* FABRICATED AND INSTALLED REPAIR IAW FAA DER COTNEY ENGINEERING SKETCH C44-R23 REV A.Apr 19, 1997 · N994CF · Doug DC862 · Fuselage Miscellaneous StructureSDR RRXA97158Fitting · corrodedDURING A MAINTENANCE VISIT, FOUND BATHTUB FITTING CORRODED BEYOND LIMITATIONS IAW DC-8 SRM, AT Y=520 AND BETWEEN LONGERONS 33R AND 34R. *S/D* REMOVED CORRODED FITTING, FABRICATED AND INSTALLED NEW FITTING IAW DC-8 SRM 53-2-0, FIGURE 2D, AND TREATED AREA IAW Apr 18, 1997 · N994CF · Doug DC862 · Fuselage Miscellaneous StructureSDR RRXA97144Frame · misdrilledDURING A MAINTENACE VISIT, FOUND MISDRILLED HOLE IN FRAME RADIUS, AT Y=1380 AND 28 INCHES ABOVE LONGERON 21L. FABRICATED AND INSTALLED REPAIR ANGLE AND SHIMS IAW DER COTNEY ENGINEERING SKETCH C44-R40 AND DC-8 SRM 51-1-8 AND 51-1-20D.Apr 18, 1997 · N994CF · Doug DC862 · Fuselage Main, FrameSDR RRXA97143Frame · misdrilledDURING A MAINTENANCE VISIT, FOUND MISDRILLED HOLE IN FRAME RADIUS, AT Y=1400 AND LONGERON 21L. FABRICATED AND INSTALLED REPAIR ANGLE AND SHIMS IAW DER APPROVED COTNEY ENGINEERING SKETCH C44-R45. TREATED AREA IAW DC-8 SRM 51-1-8 AND 51-1-20D.Apr 18, 1997 · N994CF · Doug DC862 · Fuselage Main, FrameSDR RRXA97157Skin · dentedDURING A MAINTENANCE VISIT, FOUND INNER SKIN DENTED BEYOND LIMITS IAW DC-8 SRM, AT Y=1240 AND BETWEEN LONGERONS 34R AND 36. REMOVED DAMAGED SECTION, FABRICATED AND INSTALLED FILLER AND DOUBLER REPAIR IAW DER APPROVED ENGINEERING SKETCH C44-R42.Apr 17, 1997 · N994CF · Doug DC862 · Fuselage Main, Plate/SkinSDR RRXA97155Bulkhead Web · cutDURING A MAINTENANCE VISIT, FOUND CUT IN BULKHEAD WEB, AT Y=980 AND X=+59. FABRICATED AND INSTALLED REPAIR IAW DER APPROVED COTNEY ENGINEERING SKETCH C44-R30.Apr 17, 1997 · N994CF · Doug DC862 · Fuselage Main, BulkheadSDR RRXA97154Exhaust Nozzle · crackedDURING A MAINTENANCE VISIT, FOUND NR 4 ENGINE NOZZLE AFT OUTSIDE SKIN CRACKED AT TOP RT FAN AIR SLOT. FABRICATED AND INSTALLED EXHAUST NOZZLE SKIN REPAIR IAW DER APPROVED ENGINEERING SKETCH C44-R04.Apr 17, 1997 · N994CF · Doug DC862 · Engine Collector/Tailpipe/NozzleSDR RRXA97149Longeron · crackedDURING A MAINTENANCE VISIT, FOUND CRACKED WEB IN TWO PLACES ON LONGERON 21R, AT Y=280 TO Y=300. FABRICATED AND INSTALLED REPAIR IAW DER APPROVED ENGINEERING SKETCH C44-R18 AND IAW DC-8 SRM 51-1-21.Apr 17, 1997 · N994CF · Doug DC862 · Fuselage Main, Longeron/StringerSDR RRXA97148Frame · misdrilledDURING A MAINTENANCE VISIT, FOUND MISDRILLED HOLES IN FRAME RADIUS AND CUSP FITTING, AT Y=1400 AND LONGERON 21R. FABRICATED AND INSTALLED REPAIR ANGLE AND SHIMS. REPAIRED FRAME IAW DER COTNEY ENGINEERING SKETCH C44-R17. CUSP FITTING WAS IN LIMITS AND REPAIRApr 17, 1997 · N994CF · Doug DC862 · Fuselage Main, FrameSDR RRXA97147Frame · misdrilledDURING A MAINTENANCE VISIT, FOUND MISDRILLED HOLE IN FRAME RADIUS, AT Y=1340 AND LONGERON 21R. FABRICATED AND INSTALLED REPAIR ANGLE AND SHIMS IAW DER APPROVED ENGINEERING SKETCH C44-R16.Apr 17, 1997 · N994CF · Doug DC862 · Fuselage Main, FrameSDR RRXA97142Frame · misdrilledDURING A MAINTENANCE VISIT, FOUND MISDRILLED HOLE IN FRAME, AT Y=1140 AND LONGERON 21L. FABRICATED AND INSTALLED REPAIR ANGLE AND SHIMS IAW DER APPROVED COTNEY ENGINEERING SKETCH C44-R43. ALSO, IAW DC-8 SRM 51-1-20D AND 51-1-8.Apr 17, 1997 · N994CF · Doug DC862 · Fuselage Main, FrameSDR RRXA97156Plating · crackedDURING A MAINTENANCE VISIT, FOUND UPPER LEFT WING PLATING CRACKED, AT XRS=162. FABRICATED AND INSTALLED REPAIR IAW DER COTNEY ENGINEERING SKETCH C44-R41.Apr 16, 1997 · N994CF · Doug DC862 · Wing, Plate/SkinSDR RRXA97153Plating · crackedDURING A MAINTENANCE VISIT, FOUND NR 1 PLYON PLANK CRACKED, AT YN=204 RT. FABRICATED AND INSTALLED REPAIR IAW DER APPROVED ENGINEERING SKETCH C44-R03.Apr 16, 1997 · N994CF · Doug DC862 · Nacelle/Pylon, Plate/SkinSDR IXXA9700050Flap Support · crackedDURING ROUTINE B-CHECK INSPECTION, THE FLAP SUPPORT FITTING AT STATION 219 LEFT WAS FOUND TO BE CRACKED. THE FLAP SUPPORT FITTING WAS REPLACED IN ACCORDANCE WITH DOUGLAS MAINTENANCE MANUAL 27-51-12.Apr 10, 1997 · N728PL · Doug DC862 · Trailing Edge FlapsSDR CKSA97176Seals · rupturedAT FL31.0 CABIN ALTITUDE STARTED TO CLIMB ABOVE 10,000 FT. DESCENDED TO FL20.0 TO MAINTAIN CABIN ALTITUDE OF 10,000 FT. OUTFLOW VALVE WAS CLOSED AND LOCKED. DIVERTED TO ALTERNATE AS PER OPERATIONS DIRECTION. TRANSFERRED TO DMI NR005 IAW DC8 MEL 21-10-2. FApr 9, 1997 · N802MG · Doug DC862 · Air Distribution System
Back to Douglas DC-8-62