Douglas DC-8-73F

Service difficulty reports · 15,471

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 = 'DC873F'
  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 RRXA003658Seat Track · wornDURING A MAINTENANCE VISIT FOUND A WORN SEAT TRACK AT STA 1395-1402 X=24.75, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW TRACK IAW DC-8 SRM 51-2-0 AND 5Nov 7, 2000 · N603AL · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR RRXA003657Seat Track · wornDURING A MAINTENANCE VISIT FOUND A WORN SEAT TRACK AT STA 1216-1223 X=24.75, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED PART IAW DC-8 SRM 53-2-3 AND 53-2-3Nov 7, 2000 · N603AL · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR RRXA003644Seat Track · wornDURING A MAINTENANCE VISIT FOUND A WORN SEAT TRACK AT FE'S STA IN COCKPIT, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC-8 SRM 51-1-24, 51-1-12 AND Nov 7, 2000 · N603AL · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR RRXA003643Seat Track · wornDURING A MAINTENANCE VISIT FOUND WORN SEAT TRACKS L/H & R/H IN THE COCKPIT, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED NEW PART AND INSTALLED IAW DC-8 SRM 51-1-20D AND 51-Nov 7, 2000 · N603AL · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR RRXA003642Frame · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE EMERGENCY OVER WING EXIT DOOR FRAME RT SIDE AFT AT STA 798, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. REPAIRED IAW COTNEY COMPANY DWG M20-R01.Nov 7, 2000 · N603AL · Doug DC873F · Fuselage Main, FrameSDR RRXA000030Longeron · gougedDURING A MAINTENANCE VISIT FOUND GOUGE, LONGERON 10 LEFT, BETWEEN STA 80 AND STA 100 LT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW E.O. #00-016 WITNov 7, 2000 · N792FT · Doug DC873F · Fuselage Main, Longeron/StringerSDR UPS00834421Battery Pack · dischargedINSPECTION TYPE:N/A, EMERGENCY LIGHT BATTERY PACK DEAD. REPLACED BATTERY PACK. OPS CK OK.Nov 7, 2000 · N813UP · Doug DC873F · Emergency LightingSDR RRXA003675Angle · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE FLOOR PANEL ATTACHING ANGLE R/H SIDE AT STA 200 AND 220 BL 65R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND Nov 6, 2000 · N603AL · Doug DC873F · Fuselage Floor PanelSDR RRXA003663Seat Track · wornDURING A MAINTENANCE VISIT FOUND A WORN SEAT TRACK AT STA X=45.5, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW PART IAW DC-8 SRM 51-1-24 AND 53-2-3.Nov 6, 2000 · N603AL · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR RRXA003662Seat Track · wornDURING A MAINTENANCE VISIT FOUND A WORN SEAT TRACK AT STA X=24.75, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW PART IAAW DC-8 SRM 53-2-3.Nov 6, 2000 · N603AL · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR RRXA003641Track · wornDURING A MAINTENANCE VISIT FOUND A WORN SEAT TRACK AT STA 1485 BL-0, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED PART IAW DC-8 SRM 53-2-3 AND 51-1-24.Nov 6, 2000 · N603AL · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR RRXA003622Angle · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE FLOOR PANEL ATTACHING ANGLE IN THE MAIN CABIN R/H SIDE BETWEEN STA'S 834.5 AND 857 AND L65R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 Nov 6, 2000 · N603AL · Doug DC873F · Fuselage Floor PanelSDR RRXA003621Angle · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE FLOOR PANEL ATTACHING ANGLE IN THE MAIN CABIN R/H SIDE BETWEEN STA'S 822 AND 834.5 AND L65R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 Nov 6, 2000 · N603AL · Doug DC873F · Fuselage Floor PanelSDR RRXA003620Angle · corrodedDURING A MAINTENANC EVISIT FOUND CORROSION DAMAGE TO THE FLOOR PANEL ATTACHING ANGLE IN THE MAIN CABIN R/H SIDE BETWEEN STA'S 798 AND 822 AND L65R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRNov 6, 2000 · N603AL · Doug DC873F · Fuselage Floor PanelSDR RRXA003619Angle · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE FLOOR PANEL ATTACHING ANGLE IN THEMAIN CABIN R/H SIDE BETWEEN STA'S 279 AND 781.5 AND L65R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SNov 6, 2000 · N603AL · Doug DC873F · Fuselage Floor PanelSDR RRXA003671Seat Track · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE TRACK UNDER LAV AT STA 52-62 RT X-59 343, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED NEW TRACK AND INSTALLED IAW DC-8 SRM 53-2-3, 51-1-24.Nov 5, 2000 · N603AL · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR RRXA003669Seat Track · wornDURING A MAINTENANCE VISIT FOUND A WORN SEAT TRACK AT STA 148-156 X-24.756, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 52-2-3.Nov 5, 2000 · N603AL · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR RRXA003640Rib · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE RIB IN RADIUS ON THE LT WING T/E, FLAPWELL BELOW #3 FLT SPOILER O/B SIDE, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND Nov 5, 2000 · N603AL · Doug DC873F · Wing, Rib/BulkheadSDR RRXA003637Seat Track · wornDURING A MAINTENANCE VISIT FOUND A WORN SEAT TRACK AT STA 595-603 X-45.50, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED PART IAW DC-8 SRM 53-2-3, 53-2-34 ANDNov 5, 2000 · N603AL · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR RRXA003636Seat Track · wornDURING A MAINTENANCE VISIT FOUND A WORN SEAT TRACK AT STA 506-514 X24.750, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED PART IAW DC-8 SRM 53-2-3.Nov 5, 2000 · N603AL · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR RRXA003635Seat Track · wornDURING A MAINTENANCE VISIT FOUND A WORN SEAT TRACK AT STA 510-520 X0, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED PART IAW DC-8 SRM 53-2-7, 53-2-3 AND 51-30-Nov 5, 2000 · N603AL · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR RRXA003634Seat Track · wornDURING A MAINTENANCE VISIT FOUND A WORN SEAT TRACK AT STA 506-513 X-45.50, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED PART IAW DC-8 SRM 53-2-34 AND 51-1-12Nov 5, 2000 · N603AL · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR RRXA003633Seat Track · wornDURING A MAINTENANCE VISIT FOUND A WORN SEAT TRACK AT STA 418-425, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED PART IAW DC-8 SRM 51-1-30, 51-1-24 AND 51-1-2Nov 5, 2000 · N603AL · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR RRXA003632Seat Track · wornDURING A MAINTENANCE VISIT FOUND A WORN SEAT TRACK AT STA 328 X24.750, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED PART IAW DC-8 SRM 53-2-3.Nov 5, 2000 · N603AL · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR RRXA003631Seat Track · wornDURING A MAINTENANCE VISIT FOUND A WORN SEAT TRACK AT STA 328 X24.720, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED NEW PART AND INSTALLED IAW DC-8 SRM 51-3-0 AND 51-1-24.Nov 5, 2000 · N603AL · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR RRXA003630Seat Track · wornDURING A MAINTENANCE VISIT FOUND A WORN SEAT TRACK AT STA 68X-45.50, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED NEW PART AND INSTALLED IAW DC-8 SRM 51-1-29, 51-30-02 AND 5Nov 5, 2000 · N603AL · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR RRXA003629Seat Track · wornDURING A MAINTENANCE VISIT FOUND A WORN SEAT TRACK AT STA 772-779 X45.50, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW TRACK IAW DC-8 SRM 51-1-20 AND 51-Nov 5, 2000 · N603AL · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR RRXA003628Seat Track · wornDURING A MAINTENANCE VISIT FOUND A WORN SEAT TRACK AT STA 772-780 X-24.750, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED PART IAW DC-8 SRM 53-2-3.Nov 5, 2000 · N603AL · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR RRXA003627Seat Track · wornDURING A MAINTENANCE VISIT FOUND A WORN CARGO TRACK AT STA 683 AND 693 X-45.50, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED PART IAW DC-8 SRM 53-2-3 AND 51-Nov 5, 2000 · N603AL · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR RRXA003626Seat Track · wornDURING A MAINTENANCE VISIT FOUND A WORN SEAT TRACK BETWEEN STA'S 595-603 X45.50, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED PART IAW DC-8 SRM 51-3-0 AND 51-Nov 5, 2000 · N603AL · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR RRXA003625Seat Track · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE SEAT TRACK BETWEEN STA'S 52-62 RT X-59.343, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED NEW TRACK AND INSTALLED IAW DC-8 SRM 53-2-3 AND 51-1-24.Nov 5, 2000 · N603AL · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR RRXA003624Seat Track · wornDURING A MAINTENANCE VISIT FOUND A WORN SEAT TRACK AT STA 69 L/H X24-156, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED NEW TRACK AND INSTALLED IAW DC-8 SRM 53-2-3.Nov 5, 2000 · N603AL · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR RRXA003676Angle · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE FLOOR PANEL ATTACHING ANGLE AT STA 560 BL 65L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR INov 4, 2000 · N603AL · Doug DC873F · Fuselage Floor PanelSDR RRXA003670Angle · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE FLOOR PANEL ATTACHING ANGLE L/H SIDE AT STA 902-920 AND BL-65, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INNov 4, 2000 · N603AL · Doug DC873F · Fuselage Floor PanelSDR RRXA003679Doubler · gougedDURING A MAINTENANCE VISIT FOUND A LARGE GOUGE TO THE NLG DOOR FUSELAGE EXT R/H SIDE AT STA 52-32, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DCNov 3, 2000 · N603AL · Doug DC873F · Fuselage Main, Plate/SkinSDR RRXA003656Structure · damagedDURING A MAINTENANCE VISIT FOUND A 1/4 INCH HOLE IN THE RIGHT WING TIP CAP RT O/B NEAR THE CENTER, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. REPAIRED HOLE IAW PD 05-57-047.Nov 3, 2000 · N603AL · Doug DC873F · Wing Main, Frame StructureSDR RRXA003639Skin · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE RIGHT SIDE FUSELAGE EXT SKIN AT FWD SERVICE DOOR LOWER AFT CORNER, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLNov 3, 2000 · N603AL · Doug DC873F · Fuselage Main, Plate/SkinSDR RRXA003638Skin · gougedDURING A MAINTENANCE VISIT FOUND A GOUGE IN FUSELAGE EXT SKIN BETWEEN STA 260-280 RT SIDE, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. REPAIRED SKIN IAW EA PD08-53-088 AND DC-8 SRM 53-2-0.Nov 3, 2000 · N603AL · Doug DC873F · Fuselage Main, Plate/SkinSDR RRXA003618Angle · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE BOTTOM CORNER OF DOOR CUTOUT ON T-ANGLE IN THE CARGO COMPT PIT 'C', DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PARNov 3, 2000 · N603AL · Doug DC873F · Fuselage Main, Plate/SkinSDR UPS00834355Fire Detector · will not testINSPECTION TYPE:N/A, PILOT REPORT NR 4 ENGINE FIRE WARNING NO TEST EITHER POSITION. FOUND LOOSE FIRELOOP CONNECTOR. CLEANED AND TIGHTENED CONNECTOR, OPS CK GOOD.Nov 3, 2000 · N874UP · Doug DC873F · Fire DetectionSDR RRXA003678Doubler · crackedDURING A MAINTENANCE VISIT FOUND DENTS AND CRACKS TO THE RT WING O/B EDGE OF WING TIP ASSY, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 57-2-1.Nov 2, 2000 · N603AL · Doug DC873F · Wing, Plate/SkinSDR RRXA003673Fitting · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE LONGERON END AT FS 14 AND L33R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED NEW PART AND INSTALLED IAW DC-8 SRM 51-1-24.Nov 2, 2000 · N603AL · Doug DC873F · Fuselage Main, Longeron/StringerSDR UPS00834354Window · inoperativeINSPECTION TYPE:N/A, CAPTS SLIDING WINDOW WILL NOT CLOSE COMPLETELY. ADJ WINDOW LOCKING MECH.Nov 2, 2000 · N801UP · Doug DC873F · Flight Compartment WindowsSDR UPS00834353Computer · out of adjINSPECTION TYPE:N/A, PILOT REPORT NR 4 ENGINE WILL NOT MAKE T/O POWER. REMOVED AND REPLACED CDP P3 LINE AND ADJ MEC SPECIFIC GRAVITY.Nov 2, 2000 · N818UP · Doug DC873F · Fuel Controlling SystemSDR RRXA003655Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE FUSELAGE EXTERIOR SKIN AT FS 318-325 AND L30L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW EA PD 08-53-082.Nov 1, 2000 · N603AL · Doug DC873F · Fuselage Main, Plate/SkinSDR RRXA001079Latch · out of positionON GEAR RETRACTION DOORS NOT LATCHED AND GEAR NOT LATCHED REMAINED ILLUMINATED UPON PERFORMING UPLATCH CHECK GEAR LIGHTS REMAINED ILLUMINATED RECYCLED GEAR SEVERAL TIMES NO HELP. PERFORMED LANDING GEAR AND GEAR DOOR INSP IAW DC-8 M/M 3-10-0, NO ABNORMALITESOct 30, 2000 · N605AL · Doug DC873F · Landing Gear SelectorSDR RRXA001078Skin · damagedDURING POST FLIGHT INSPECTION FOUND HOLE IN FUSELAGE AT TAIL STAND BRACKET AREA. POSSIBLE CAUSE TAIL STAND FROM PREVIOUS STATION. REPAIRED DAMAGED AREA AT TAIL STAND ATTACHMENT BRACKET AREA ON ACFT LWR FUSELAGE AS PROFILED IN DC-8 SRM 53-2-1.Oct 27, 2000 · N873SJ · Doug DC873F · Fuselage Main, Plate/SkinSDR RRXA001077Flow Valve · failedON CLIMBOUT WITH RT PACK AT MAX FLOW COULD NOT MAINTAIN CABIN ALTITUDE BELOW 10,000 FT. RETURNED TO AIRPORT. REMOVED AND REPLACED FLOW CONTROL VALVE. RAN ENGS AND PRESSURIZED IAW 21-31-0, OPS CHECK GOOD.Oct 27, 2000 · N961R · Doug DC873F · Cabin Cooling SystemSDR RRXA001076Unknown · odorON DESCENT GOT A VERY STRONG SMELL AS IF SOMETHING ELECTRICAL GOT VERY HOT. COULDN''T IDENTIFY WHERE IT WAS COMING FROM, WENT AWAY ON APPROACH. PERFORMED ALL 4 ENG RUN CHECKING ASSOC ELECT SYS''S RAN PACKS AND RECIRC FAN, RAN SUPPLEMENTAL COCKPIT A/C AND HOct 25, 2000 · N792FT · Doug DC873F · Air Distribution SystemSDR RRXA001074Skin · damagedTHERE''S A HALF DOLLAR HOLE AT BOTTOM OF DOOR LEVEL APPROXIMATELY TWO FEET AFT. APPEARS TO HAVE BEEN MADE BY ENTRANCE STAIRS IN DAYTON, DOES NOT MATCH STAIR HEIGHT AT MCO. REMOVED DAMAGE AND INSTALLED DOUBLER IAW MM 53-2-1 FIG 7 PG 115.Oct 24, 2000 · N604AL · Doug DC873F · Fuselage Main, Plate/Skin
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