Douglas DC-8-62

Service difficulty reports · 2,778

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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 IXXA0100020Skin · crackedDURING ROUTINE B-CHECK INSPECTION, A CRACK WAS DETECTED ON THE CREW ENTRY DOOR SKIN LOWER CORNER AT FUSELAGE STATION 241. REPAIR ACCOMPLISHED STOP DRILLING CRACK, FABRICATION AND INSTALLATION A REPAIR DOUBLER IN ACCORDANCE WITH DACO STRUCTURAL REPAIR MANUAL 5Feb 15, 2001 · N799AL · Doug DC862 · Passenger/Crew DoorsSDR IXXA0100019Skin · crackedDURING ROUTINE B-CHECK INSPECTION, A CRACK WAS DETECTED ON THE FUSELAGE EXTERNAL PLATING AT FUSELAGE STATION 242, BETWEEN LONGERONS 28L AND 29L. REPAIR ACCOMPLISHED STOP DRILLING CRACK. FABRICATION AND INSTALLATION A REPAIR DOUBLER IN ACCORDANCE WITH DACO STFeb 15, 2001 · N799AL · Doug DC862 · Fuselage Main, Plate/SkinSDR IXXA0100005Door · missingAFTER AN UNEVENTFUL LANDING AND DURING POST FLIGHT INSPECTION AT WRI. MAINTENANCE FOUND THE RIGHT MAIN LANDING GEAR LOWER FLYING DOOR MISSING FROM THE GEAR. NO OTHER DAMAGE TO THE AIRCRAFT WAS NOTED. THE AIRCRAFT WAS FERRIED TO A MAINTENANCE FACILITY FOR REFeb 12, 2001 · N728PL · Doug DC862 · Landing Gear DoorsSDR IXXA01000052Door · missingAFTER AN UNEVENTFUL LANDING AND DURING POST FLIGHT INSPECTION AT WRI. MAINTENANCE FOUND THE RIGHT MAIN LANDING GEAR LOWER FLYING DOOR MISSING FROM THE GEAR. NO OTHER DAMAGE TO THE AIRCRAFT WAS NOTED.Feb 12, 2001 · N728PL · Doug DC862 · Landing Gear DoorsSDR ARWA0010203Link · brokenFLAP IND HAS SPLIT NEEDLES. FOUND LEFTI/B FLAP LINK BROKEN ON THE O/B HINGE. REMOVED AND REPLACED WITH NEW P/N 5751152-501. REFERENCE MM 27-51-4. OPS CHECK SATISFACTORY.Feb 7, 2001 · N802BN · Doug DC862 · Trailing Flap Position Indicating SystemSDR ARWA0010201Oil Cooler · damagedRETURNED TO MKJP SHORTLY AFTER THE TAKEOFF DUE TO HIGH OIL TEMP NR 1 ENGINE. PRECAUTIONARY ENGINE SHUTDOWN AT 22:28Z TEMP 142 DEGREES, FOLLOW BY ABNORMAL CHECK LIST OIL PRESSURE WAS 47 PSL. WINDMILLING OIL PRESSURE 8 PSI. REMOVED AND REPLACED NR 1 ENGINE FUFeb 3, 2001 · N8968U · Doug DC862 · Engine Fuel/Oil CoolerSDR ARWA0010103Bleed Valve · dirtyAT THE BEGINNING OF TAKEOFF ROLL NR 2 ENGINE HAD COMPRESSOR STALL. ENGINE PARAMETER WERE TAKEOFF, EPR WAS 1.88; DROPPED TO 1.75 N2 AND RECOVERED, FUEL FLOW DMI AND EGT WAS NORMAL. PERFORMED VISUAL CHECK AIR BLEED VALVE, CLEANED AND LUBRICATED IAW M/M 75-30-Jan 28, 2001 · N1808E · Doug DC862 · Compressor Bleed ValveSDR ARWA0010102Ballast · smokeDURING DESCENT, CO-PILOTS RADAR SCREEN HAD EVIDENCE OF SMOKE. TURNED OFF AND PULLED C/B. CHECKED WEATHER RADAR SYSTEM WIRING IAW W/D 34-10-0, FOUND NORMAL. GROUND OPERATIONAL CHECK IAW FDW M/M 34-41-0. NORMAL, NO TROUBLE FOUND. REF TO ITEM NR 1, FOUND EVIDJan 25, 2001 · N1808E · Doug DC862 · Weather Radar SystemSDR IXXX0100002Switch · defectiveENROUTE FROM OKO TO QPG, THE LANDING GEAR UNSAFE WARNING LIGHT ILLUMINATED DURING THE GEAR UPLATCH CHECK. THE FLIGH CREW CYCLED THE LANDING GEAR WITH THE WARNING INDICATION REMAINING THE SAME. THE FLIGHT RETURNED TO OKO FOR AN UNEVENTFUL LANDING. MAINTEANCE INJan 8, 2001 · N799AL · Doug DC862 · Landing Gear Retraction/Extension SystemSDR ARWA0001204Switch · defectiveAFTER TAKE OFF KATL, DOOR NOT LATCHED LIGHT ILLUMINATED AFTER GEAR RETRACTION. PERFORMED ABNORMAL PROCEDURE. UNABLE TO EXTINGUISH LIGHT; AIRCRAFT DIVERTED TO MIA & LANDED WITHOUT INCIDENTS.CORRECTIVE ACTION: REMOVED AND REPLACED LEFT AND RIGHT DOORS MICRO SWIDec 23, 2000 · N1808E · Doug DC862 · Door Warning SystemSDR ARWA0001203Uplock · dirtyAFTER GEAR RETRACTION GEAR NOT LATCHED UP LIGHT ON, ON UPLATCH CHECK LANDING GEAR FALLS OUT. FOUND MLE UPLATCH MECHANISM DRY; CLEANED & LUBRICATED MLE UPLATCH MECHANISM IAW MM 12-81-1; PERFORMED LANDING GEAR SWING IAW 32-11-1 CHECK OK.Dec 21, 2000 · N810BN · Doug DC862 · Landing Gear Position and WarningSDR ARWA0001201Uplock Switch · failedDOOR NOT LATCHED LIGHT ILLUMINATED AFTER TAKEOFF PERFORMED ABNORMAL CKLIST LIGHT REMAIN ON. REMOVED AND REPLACED RT MAIN LANDING GEAR DOOR UPLOCK SWITCH, OPERATIONAL CHECK LANDING GEAR DOOR INDICATION SYSTEM IAW 32-60-0 AND FOUND NORMAL.Dec 6, 2000 · N810BN · Doug DC862 · Door Warning SystemSDR ABXA000493Valve · leakingFLIGHT CREW REPORTED A LOSS OF HYDRAULIC PRESSURE WITH AN ASSOCIATED HYDRAULIC QUANTITY LOSS INDICATION. THE FLIGHT CREW PERFORMED EMERGENCY PROCEDURES. MAINTENANCE INSPECTED AND REPLACED THE SLOT CONTROL VALVE IAW DC-8 MM 27-80-00. OPS CHECKED GOOD.Nov 13, 2000 · N808AX · Doug DC862 · Hydraulic System, MainSDR ARWA0001102Bolt · brokenDURING INSPECTION FOR HYDRAULIC LEAK AT NR 3 PYLON FOUND VEE FITTING BOLT BROKEN. REPLACED BROKEN BOLT WITH INCONEL BOLT IAW SB 57-98.Nov 13, 2000 · N69UA · Doug DC862 · Hydraulic System, MainSDR IXXA0000039Compressor · failedEN ROUTE FROM NBW TO NGU, SMOKE WAS EMITTED INTO THE COCKPIT WHEN THE NUMBER THREE TURBO COMPRESSOR WAS OPERATED. THE FLIGHT CREW SECURED THE COMPRESSOR, SMOKE SUBSIDED. THE FLIGHT CONTINUED TO NGU FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED THE TURBO Oct 31, 2000 · N61CX · Doug DC862 · Cabin Compressor SystemSDR IXXA0000038Fan · odorEN ROUTE FROM JON TO HIK, AN ODOR WAS SENSED IN THE CABIN WHEN THE RIGHT RECIRULATION FAN WAS TURNED ON. THE FLIGHT CREW SECURED THE FAN AND THE ODOR SUBSIDED. THE FLIGHT CONTINUED TO HIK FOR AND UNEVENFUL LANDING. MAINTENANCE INSPECTED THE FAN AND IT WAS FOct 31, 2000 · N799AL · Doug DC862 · Air Distribution FanSDR ABXA000454Pin · damagedGEAR UPLATCH CHECK FAILED. RIGHT MAIN GEAR DOOR INDICATED UNLATCHED. PERFORMED ALTERNATE PROCEDURE, RECYCLED GEAR, NO HELP. CONTINUED FLIGHT AT RESTRICTED SPEED IAW DC8 OPS MANUAL. REPLACED RIGHT MAIN GEAR DOOR HINGE PINS. PERFORMED MAIN GEAR DOOR ADJUST/Sep 29, 2000 · N804AX · Doug DC862 · Landing Gear Door Retract SectionSDR ABXA000430Engine · seizedNR 1 ENGINE SEIZED ON CLIMBOUT. NOTED EGT 800 DEGREES C, OIL QTY ZERO. REPLACED NR 1 ENGINE IAW JOB CARD 8090507.Sep 22, 2000 · N801AX · Doug DC862 · Engine (Turbine/Turboprop)SDR RRXA003162Fitting · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE SPLICE FITTING IN THE FWD LWR CARGO COMPT BETWEEN STA''S 600 AND 620 AND L31R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.Aug 9, 2000 · N990CF · Doug DC862 · Fuselage Miscellaneous StructureSDR RRXA003161Fitting · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE SPLICE FITTING IN THE AFT ACCESSORY COMPT AT STA 1340 AND 1360 AND L29R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.Aug 9, 2000 · N990CF · Doug DC862 · Fuselage Miscellaneous StructureSDR RRXA001041Controller · failedAUTO PRESSURIZATION FAILED SHORTLY AFTER TAKEOFF, DURING MANUAL CONTROL THROUGH FL 290 CABIN CLIMBED UNCONTROLLABLY AT 2000 FPM. DEFERRED PER MEL 21-10 CAT C. DMI CNTL NR C9037012-7913 DUE 8-14-00. PLACARD INSTALLED.Aug 4, 2000 · N995CF · Doug DC862 · Cabin Pressure ControllerSDR RRXA001040Control Panel · failedNR 1 TRANSPONDER SQUAKS 7777 NO MATTER WHAT THE INPUT (THE VARIOUS CODES) ON THE BOX IS, NR 2 TRANSPONDER INOP (NO SQUAK) FOR VARIOUS CODES. REMOVED AND REPLACED ATC CONTROL PANEL, NR 1 AND NR 2 TRANSPONDER, OP CHECKS GOOD IAW DC-8 M/M CH 34-53.Aug 2, 2000 · N993CF · Doug DC862 · ATC Transponder SystemSDR ABXA000359Line · leakingSLOW LOSS OF HYDRAULICS OBSERVED ON HYDRAULIC QUANTITY GAUGE. NEEDLE WENT FROM FULL TO HALFWAY BETWEEN N AND STANDPIPE. EMERGENCY PROCEDURES ACCOMPLISHED. REPLACED NR 3 ENGINE HYDRAULIC PUMP PRESSURE LINE AND RESEALED PUMP FITTING AT PUMP. SERVICED HYDRAULJul 27, 2000 · N804AX · Doug DC862 · Hydraulic System, MainSDR IXXA0000025Fan · defectiveEN ROUTE FROM ASI TO ANU, THE FLIGHT CREW DETECTED SMOKE IN THE COCKPIT ACCOMPANIED BY THE LEFT RECIRCULATION FAN SHUTING DOWN, SMOKE SUBSIDED. THE FLIGHT CONTINUED TO ANU FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECT THE LEFT RECIRCULATION FAN AND FOUND ITJul 12, 2000 · N728PL · Doug DC862 · Air Distribution FanSDR IXXA0000026Compressor · damagedEN ROUTE FROM JON TO HIK, DURING CRUISE THE NUMBER TWO ENGINE EXPERINCED A COMPRESSOR STALL FOLLOWED BY PARTIAL POWER REDUCION. THE FLIGHT CREW SECURED THE ENGINE FOLLOWING COMPANY PROCEDURES. THE FLIGHT CONTINUED TO HIK FOR AN UNEVENTFUL LANDING. MAINTENANJul 11, 2000 · N799AL · Doug DC862 · Turbine Engine Compressor SectionSDR IXXA0000024Ballast · defectiveEN ROUTE FROM HIK TO KWA, WHEN THE FLIGHT CREW ILLUMINATED THE COCKPIT LIGHTING SYSTEM SMOKE WAS DETECTED IN THE COCKPIT. THE FLIGHT CREW EXTINGUISHED THE LIGHTING SYSTEM AND THE SMOKE SUBSIDED. THE FLIGHT CONTINUED TO KWA FOR AN UNEVENTFUL LANDING. MAINTENJul 10, 2000 · N799AL · Doug DC862 · Flight Compartment LightingSDR RRXA001005Warning Light · illuminatedON CLIMBOUT (APPROX 5,000 FEET) NR 2 ENGINE FIRE WARNING/MASTER CAUTION ILLUMINATION/AURAL WARNING. SHUTDOWN NR 2 ENGINE, DISCHARGED BOTH FIRE BOTTLES.Jun 28, 2000 · N995CF · Doug DC862 · Fire DetectionSDR IXXA0000022Fan · defectiveEN ROUTE FROM EDI TO TOL, THE FLIGHT CREW SENSED AN ODOR IN THE COCKPIT WHEN THE LEFT RECIRULATION FAN WAS TURNED ON. THE FLIGHT CREW SECURED THE FAN, THE ODOR SUBSIDED AND THE FLIGHT CONTINUED TO TOL FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED THE THE Jun 23, 2000 · N61CX · Doug DC862 · Air Distribution FanSDR RRXA001003Downlock Switch · inoperativeNR 2 DURING MANUAL EXTENSION CHECKS 0 HYD PRESS. NO NOSE GEAR GREEN LIGHT AND BOTH GEAR NOT LATCHED LT AND GEAR DOOR (RED) LIGHTS STAYED ON. CYCLED GEAR SEVERAL TIMES, NO HELP. RAN EMERGENCY CHECK LIST. RETURNED TO AIRPORT. REMOVED AND REPLACED NLG DOWNLOJun 22, 2000 · N995CF · Doug DC862 · Landing Gear Position and WarningSDR IXXA0000021Seal · leakingEN ROUTE FROM QPG TO OKO, WHEN THE FLIGHT CREW TURNED ON THE NUMBER ONE TURBO COMPRESSOR A SQUEAL WAS HEARD AND AN ODOR WAS SENSED IN THE COCKPIT. THE FLIGHT CREW SECURED THE TURBO COMPRESSOR, THE ODOR SUBSIDED. THE FLIGHT CONTINUED TO OKO FOR AN UNEVENTFUL Jun 8, 2000 · N8974U · Doug DC862 · Cabin Compressor SystemSDR RRXA002459Skin · crackedDURING A MAINTENANCE VISIT FOUND A CRACK IN WELD 3 O CLOCK POSITION INSIDE THRUST REV AFT OF BUCKET, 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 51-1-21 AND EO NR 00Jun 5, 2000 · N995CF · Doug DC862 · Engine Thrust ReverserSDR RRXA002355Cover · damagedDURING A MAINTENANCE VISIT FOUND TEMPORARY REPAIRS DONE TO THE CROSS SLIDE COVER ON B PIT, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW DOOR COVER IAW DC-8 SRM 51-3-0 AND EO NR 00-04Jun 5, 2000 · N995CF · Doug DC862 · Cargo/Baggage DoorsSDR RRXA002351Floorboard · misdrilledDURING A MAINTENANCE VISIT FOUND MISDRILLED AND ELONGATED HOLES IN THE FLOOR PLANK NR 2 STA 233 TO 315, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. PLUGGED HOLES IAW EO NR 00-047 WITH APPROVED 8110-3 DATED 5-16Jun 1, 2000 · N995CF · Doug DC862 · Fuselage Floor PanelSDR RRXA002293Floorboard · misdrilledDURING A MAINTENANCE VISIT FOUND MISDRILLED HOLES TO THE MAIN CABIN FLOOR PLANK ROW 8 AT STA 1240 - 1460, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. PLUGGED DISCREPANT HOLES IAW EO NR 00-047 WITH APJun 1, 2000 · N995CF · Doug DC862 · Fuselage Floor PanelSDR RRXA002250Spoiler Panel · delaminatedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE NR 3 GROUND SPOILER, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED NR 3 PANEL IAW DC-8 MM 27-61-1. (CORROSION DAMAGE RECORDED IN EWMay 31, 2000 · N995CF · Doug DC862 · SpoilersSDR RRXA002242Spoiler Panel · delaminatedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE NR 1 GROUND SPOILER, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED SPOILER IAW MM 27-61-0. (CORROSION DAMAGE RECORDED IN EWA CORROSMay 31, 2000 · N995CF · Doug DC862 · SpoilersSDR RRXA002244Vane · damagedDURING A MAINTENANCE VISIT FOUND SCREW HOLES ELONGATED AND BUSHINGS MISSING ON THE RIGHT WING RIGHT O/B FLAP VANE NR 5, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED BUSHING PER EO NR 00-May 26, 2000 · N995CF · Doug DC862 · Trailing Edge FlapsSDR RRXA002194Vane · damagedDURING A MAINTENANCE VISIT FOUND AN ELONGATED BOLT HOLE ON THE RIGHT O/B FLAP VANE NR 6, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED BUSHING IAW EO NR 00-047 WITH APPROVED 8110-3 DATED May 26, 2000 · N995CF · Doug DC862 · Trailing Edge FlapsSDR RRXA003168Strap · tornDURING A MAINTENANCE VISIT FOUND A TEAR TO THE STRAP BETWEEN STRINGERS AT STA 902 AND 9 - 10 LT, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW PD08-53-049.May 25, 2000 · N990CF · Doug DC862 · Fuselage Miscellaneous StructureSDR RRXA003163Strap · tornDURING A MAINTENANCE VISIT FOUND A TEAR TO THE STRAP BETWEEN STRINGERS AT STA 902 STRINGER 9-10 LT, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW PD 08-53-049.May 25, 2000 · N990CF · Doug DC862 · Fuselage Main, StructureSDR RRXA002639Floorboard · misdrilledDURING A MAINTENANCE VISIT FOUND MISDRILLED AND ELONGATED HOLES TO THE FLOOR PANEL AT STA 500 - 660 ROW 1 LT, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED REPAIR AND INSTALLED IAW EO NR 00-0May 25, 2000 · N995CF · Doug DC862 · Fuselage Floor PanelSDR RRXA002450Floorboard · crackedDURING A MAINTENANCE VISIT FOUND A CRACKED END TO THE FLOOR PLANK AT STA 800 - 1020, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED REPAIR AND INSTALLED IAW EO NR 00-047 WITH APPROVED 8110-3 DAMay 25, 2000 · N995CF · Doug DC862 · Fuselage Floor PanelSDR RRXA002448Floorboard · misdrilledDURING A MAINTENANCE VISIT FOUND MISDRILLED AND ELONGATED HOLES TO THE FLOOR PANEL AT STA 800 - 1000, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED REPAIR AND INSTALLED IAW EO NR 00-047 WITH AMay 25, 2000 · N995CF · Doug DC862 · Fuselage Floor PanelSDR RRXA002339Seat Track · gougedDURING A MAINTENANCE VISIT FOUND A GOUGED SEAT TRACK AT FUSELAGE STA FS 425 XCW 22.5, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. BLENDED DAMAGED AREA IAW DC-8 SRM 53-2-3 AND EO NR 00-047 WITH APPROVMay 25, 2000 · N995CF · Doug DC862 · Fuselage, Seat/Cargo Attach FittingsSDR RRXA002299Seat Track · damagedDURING A MAINTENANCE VISIT FOUND ELONGATED HOLES IN THE SEAT TRACK AT STA 1250 - 1460 AND XCW 47 RT, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED REPAIRED SEAT TRACK IAW DC-8 SRMay 25, 2000 · N995CF · Doug DC862 · Fuselage, Seat/Cargo Attach FittingsSDR RRXA002200Pin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE MLG RETRACT PIN AND PIN BOSS SO MA-AI-3210-01:03 LT MLG RETRACT PIN AND BOSS PIN INSPECTION NEEDED C/W, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8S RM 51-1-8. FABRMay 25, 2000 · N995CF · Doug DC862 · Main Landing Gear Strut/Axle/TruckSDR RRXA002635Floorboard · misdrilledDURING A MAINTENANCE VISIT FOUND NUMEROUS MISDRILLED HOLES TO THE FLOOR PLANK RT UPPER SKIN AT STA 1460 - 1606, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED REPAIR AND INSTALLED IAW EO NR 00-May 24, 2000 · N995CF · Doug DC862 · Fuselage Floor PanelSDR RRXA002485Floorboard · misdrilledDURING A MAINTENANCE VISIT FOUND NUMEROUS MISDRILLED HOLES TO THE NR 3 FLOOR PLANK AT STA 800 - 1000, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED REPAIR AND INSTALLED IAW EO NR 00-047 WITH AMay 24, 2000 · N995CF · Doug DC862 · Fuselage Floor PanelSDR RRXA002460Seat Track · damagedDURING A MAINTENANCE VISIT FOUND GOUGED AND ELONGATED HOLES TO THE SEAT TRACK AT FS 925 - 962 XCW 47 LT, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED NEW PART AND INSTALLED IAW DC-8 SRM 53-2-3, FIG 12, May 24, 2000 · N995CF · Doug DC862 · Fuselage, Seat/Cargo Attach FittingsSDR RRXA002452Floorboard · crackedDURING A MAINTENANCE VISIT FOUND HOLES AND CRACKS TO THE FLOORBOARD AT FS 860 - 1000, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED REPAIR AND INSTALLED IAW EO NR 00-047 WITH APPROVED 8110-3 DMay 24, 2000 · N995CF · Doug DC862 · Fuselage Floor Panel
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