Douglas DC-8-62F

Service difficulty reports · 1,163

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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 = 'DC862F'
  ORDER BY difficulty_date DESC"

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SDR RRXA11080Fitting · crackedDURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO LONGERON END FITTING AT STA 1530 AND L32L, DAMAGE EXCEEDED LIMITATION IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-2Apr 19, 2001 · N996CF · Doug DC862F · Fuselage Main, StructureSDR RRXA11079FittingDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO BATHTUB FITTING AT STA.540 BETWEEN L33L-L34L, DAMAGE EXCEEDED LIMITATION IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRMApr 19, 2001 · N996CF · Doug DC862F · Fuselage Main, StructureSDR RRXA11078Web · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO WEB AT STA. 1310-1520 AND RBL46, DAMAGE EXCEEDED LIMITATION IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 53-4-1 AND 5Apr 19, 2001 · N996CF · Doug DC862F · Fuselage Main, StructureSDR RRXA11161Fitting · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO BATHTUB FITTING AT STA.500 AND L32L, DAMAGE EXCEEDED LIMITATION IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 53-2-0 Apr 18, 2001 · N996CF · Doug DC862F · Fuselage Main, StructureSDR RRXA11077Fitting · crackedDURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO END FITTING AT STA 1520-1530 AND L32L, DAMAGE EXCEEDED LIMITATION IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-20D AND DWG 4641326.Apr 18, 2001 · N996CF · Doug DC862F · Fuselage Main, Attach FittingsSDR RRXA11160Fitting · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO BATHTUB FITTING SPLICE ANGLE AT STA.560 AND L33R, DAMAGE EXCEEDED LIMITATION IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-Apr 17, 2001 · N996CF · Doug DC862F · Fuselage Main, StructureSDR RRXA11076Fitting · crackedDURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO LONG END FITTING AT STA. 1530-1540 AND L32R, DAMAGE EXCEEDED LIMITATION IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-3-0 AND DWG 4641324.Apr 15, 2001 · N996CF · Doug DC862F · Fuselage Main, Attach FittingsSDR RRXA11075Stiffener · crackedDURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO AFT SIDE OF APB HORIZ STIFFNER INSIDE HOLE 60 AT STA 1606 AND BL=0 AND 24 ABOVE FLOOR LEVEL, DAMAGE EXCEEDED LIMITATION IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTAApr 14, 2001 · N996CF · Doug DC862F · Fuselage Miscellaneous StructureSDR RRXA11074Shim · damagedDURING A MAINTENANCE VISIT REQUIRED TO REPLACE CLASS 3 REPAIR TO LT SIDE AFT OF FILLET FAIRING AT STA. 1200-1220, DAMAGE EXCEEDED LIMITATION IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. REMOVED CLASS 3 REPAIR AND INSTALLED CLASS 1 REPAIR IAWApr 13, 2001 · N996CF · Doug DC862F · Fuselage Miscellaneous StructureSDR RRXA11073Doubler · crackedDURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO R/H L/E INTERNAL WRAP AROUND DOUBLER AT STA. XFS572.5, DAMAGE EXCEEDED LIMITATION IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-Apr 12, 2001 · N996CF · Doug DC862F · Wing, Plate/SkinSDR RRXA11072Skin · crackedDURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO R/H WING O/B L/E SKIN L/E I/B AT STA. XFS 710, DAMAGE EXCEEDED LIMITATION IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM Apr 12, 2001 · N996CF · Doug DC862F · Wing, Plate/SkinSDR RRXA11071Rib · crackedDURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO RT WING O/B L/E LOWER RIB AT STA. XFS 791.25, 785, 772.5, DAMAGE EXCEEDED LIMITATION IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 57-2-0 FIG 2 AND Apr 12, 2001 · N996CF · Doug DC862F · Wing, Rib/BulkheadSDR RRXA11070Rib · crackedDURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO L/H WING O/B L/E LOWER RIB AT STA. XFS653.75, DAMAGE EXCEEDED LIMITATION IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 5Apr 12, 2001 · N996CF · Doug DC862F · Wing Main, Frame StructureSDR RRXA11069Rib · crackedDURING A MAINTENANCE VISIT FOUND CRACK TO LT WING O/B L/E UPPER RIBS AT STA. XFS 803.75 TO 791.25 AND XFS 766.25. DAMAGE EXCEEDED LIMITATION IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8.. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 57-2-0 FIApr 12, 2001 · N996CF · Doug DC862F · Wing, Rib/BulkheadSDR RRXA11068Rib · crackedDURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO RT WING O/B L/E LOWER RIB AT STA. XFS603.75. DAMAGE EXCEEDED LIMITATION IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 57-2-0 FIG 2.Apr 12, 2001 · N996CF · Doug DC862F · Wing, Rib/BulkheadSDR RRXA11067Rib · crackedDURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO LT WING O/B L/E UPPER RIBS AT STA. XFS 635 TO 641.25 AND XFS 610, DAMAGE EXCEEDED LIMITATION IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAOR AND INSTALLED IAW DC-8 SRM 57-2-0 FIApr 12, 2001 · N996CF · Doug DC862F · Wing, Rib/BulkheadSDR RRXA11091Rib · crackedDURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO LT I/B FLAP O/B RIB AT STA. XW122, DAMAGE EXCEEDED LIMITATION IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 57-2-0FIG2A, 51-1-21 AND EO# QC-069 REV. 7Apr 11, 2001 · N996CF · Doug DC862F · Trailing Edge FlapsSDR RRXA11140Fitting · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO LONGERON END FITTING AT STA.1525 AND L33L, DAMAGE EXCEEDED LIMITATION IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 53-2-5 FIG8C-1.Apr 10, 2001 · N996CF · Doug DC862F · Fuselage Main, Attach FittingsSDR RRXA010033Indicator · faultyON TAKEOFF ROLL NR 1 ENG EGT TEMP WENT TO 575 DEGREES AND WAS CLIMBING OUTSIDE TEMP 22 EPR 1.88 N1 & FF WERE EVEN ACFT SPEED WAS 70 KNOTS. PERFORMED EGT INDICATOR AND HARNESS TEST IAW MM 77-20-4, & BARFIELD TEST SET INSTRUCTIONS FOUND NR 1 EGT INDICATOR TO Apr 10, 2001 · N997CF · Doug DC862F · Engine EGT/TIT Indicating SystemSDR RRXA11162Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO L/H WING UPPER T/E PANEL ABOVE MLG TRUNNION AT STA. XW60-70, DAMAGE EXCEEDED LIMITATION IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-3-0, 51-Apr 6, 2001 · N996CF · Doug DC862F · Wing, Plate/SkinSDR ARWA0010402Landing Gear · collapsedEMERGENCY TURNBACK DUE TO NOSE GEAR MALFUNCTION. ON ROLLOUT NOSE GEAR COLLAPSED AT 70 KTS. EMERGENCY UNITS APPLIED FOAM FIRE PROTECTION ON RUNWAY AND PURPLE DRY CHEMICAL WAS USED IN COCKPIT AREA PRECAUTIONARY.Apr 4, 2001 · N791AL · Doug DC862F · Nose/Tail Landing GearSDR RRXA11163Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO SKIN AT STA.212 AND L15L, DAMAGE EXCEEDED LIMITATION IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DHSK 996-492. (CORROSION DAApr 3, 2001 · N996CF · Doug DC862F · Fuselage Main, StructureSDR RRXA11145Frame · bentDURING A MAINTENANCE VISIT FOUND BENT DAMAGE TO FRAME AT STA1180 AND L20L-L21L, DAMAGE EXCEEDED LIMITATION IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DHSK 996-505.Apr 3, 2001 · N996CF · Doug DC862F · Fuselage Main, StructureSDR RRXA010021Wire · damagedNR 1 EGT INDICATOR WENT TO ZERO ON GAUGE. PERFORMED INFLIGHT SHUTDOWN OF NR 1 ENGINE PER QRH PROCEDURES. WINDMILLING OIL PRESSURE 30 PSI AT 0633Z. REPAIRED WIRING AT NR 1 ENGINE DISCONNECT. PERFORMED ENGINE RUN-UP, NR 1 ENGINE EGT INDICATES NORMAL IAW 27-2Mar 14, 2001 · N996CF · Doug DC862F · Engine EGT/TIT Indicating SystemSDR RRXA010022O-Ring · leakingLOST HYDRAULICS DOWN TO THE STAND-PIPE. PERFORMED PROCEDURES PER QRH ABNORMAL CHECKLIST. REPLACED O-RINGS ON SLOT VALVE PER DC8 MM 29-10-20, LK AND OPS CK GOOD AT THIS TIME.Mar 13, 2001 · N996CF · Doug DC862F · Hydraulic System, MainSDR RRXA010026Connector · faultyON TAKEOFF ROLL, NR 1 EGT WENT TO ZERO. AFTER REDUCING POWER TO IDLE, RETURNED TO NORMAL. REMOVED AND REPLACED NR 1 EGT BULKHEAD CONNECTORS. PERFORMED ENGINE RUN, NR 1 EGT OPERATION CHECKED NORMAL IAW DC-8 MM 77-20-0.Mar 3, 2001 · N996CF · Doug DC862F · Engine EGT/TIT Indicating SystemSDR RRXA010015Hydraulic Line · rupturedON TAXI IN A/C LOST ALL HYD FLUID. FOUND FLEX LINE ON STOW PUMP RUPTURED. REMOVED AND REPLACED FLEX LINE. LEAK AND OP CK''S GOOD. A/C RETURNED TO SERVICE.Mar 2, 2001 · N997CF · Doug DC862F · Hydraulic System, MainSDR RRXA001100Track · separatedPOST FLIGHT FOUND LOWER GUIDE AND TRACK FOUND HANGING OUT OF COWLING. REPLACED LOWER TRACK ASSY WITH LIKE SERVICEABLE ITEM - OPS CHECKS T/R ON GROUND IAW DC-8 MM 78-30-0. OPS CHECKS GOOD.Dec 23, 2000 · N996CF · Doug DC862F · Engine Collector/Tailpipe/NozzleSDR RRXA001094O-Ring · damagedRADAR SPOKE IS FUZZY AND TILT POINTS TO THE GROUND AT ALL TIMES. REPLACED DAMAGED O-RING ON BACK OF RADAR RT WAVE GUIDE. PERFORMED FUNCTIONAL TEST PER DC-8 MM 34-41-0, SYSTEM OPS NORMAL ON GROUND.Dec 16, 2000 · N997CF · Doug DC862F · Weather Radar SystemSDR RRXA001093Skin · damagedRIGHT O/B FLAP TRAILING EDGE ONE FOOT FROM O/B SIDE 1 X 4 INCH TEAR. REMOVED DAMAGED SECTION OF FLAP T/E AND FABRICATED LIKE SECTION AS OUTLINED IN DC8 SRM 57-7-0. INSTALLED SAME PER DC-8 SRM 51-1-21A & 51-1-22.Dec 14, 2000 · N996CF · Doug DC862F · Trailing Edge FlapsSDR IXXA0000041Uplock · misriggedEN ROUTE FROM HIK TO SUU, THE GEAR DOOR NOT LATCH LIGHT ILLUMINATED DURING THE LANDING GEAR UPLATCH CHECK. THE FLIGHT CREW FOLLOWED COMPANY PROCEDURE, PLACED THE GEAR LEVER IN THE UP POSITION DETENT AND CONTINUED TO SUU FOR AN UNEVENTFULL LANDING. MAINTENANCNov 5, 2000 · N41CX · Doug DC862F · Landing Gear Position and WarningSDR IXXA0000040Sensor · defectiveEN ROUTE FROM QPG TO HIK, THE LANDING GEAR DOOR NOT LATCH LIGHT ILLUMINATED DURING CRUISE. THE FLIGHT CREW FOLLOWED COMPANY PROCEDURES AND CONTINUED TO HIK FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED THE GEAR DOOR WARNING INDICATION SYSTEM WHICH LOCATEDNov 5, 2000 · N41CX · Doug DC862F · Landing Gear Position and WarningSDR IXXA0000031Control Valve · misriggedEN ROUTE FROM GSO TO TOL FOLLOWING ROUTINE MAINTENANCE, THE RIGHT MAIN LANDING GEAR FAILED TO RETRACT AFTER TAKEOFF. THE FLIGHT CREW CYCLED THE GEAR WITH NO SUCCESS. THE FLIGHT RETURNED TO GSO FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED THE LANDING GEASep 5, 2000 · N41CX · Doug DC862F · Landing Gear Retraction/Extension SystemSDR IXXA0000018Line · defectiveEN ROUTE FROM KWI TO HIK, THE FLIGHT CREW NOTICED THE MAIN HYDRAULIC SYSTEM FLUID QUANTITY DECLINING. THE FLIGHT CREW FOLLOWED COMPANY EMERGENCY PROCEDURES, DECLAIRED AN EMERGENCY, AND CONTINUED TO HIK FOR AN UNEVENFUL LANDING. MAINTENANCE INSPECTED THE AIRCMay 3, 2000 · N8974U · Doug DC862F · Hydraulic System, MainSDR RRXA000285Frame · crackedREPAIR CRACK ON FRAME AT STA 340 BETWEEN L20L AND L21L AND CRACKED WEB PN5772787-13. FABRICATED AND INSTALLED REPAIR ITEM PER EWA SKETCH 04-30-2000-001. BOEING REF BCAG/LBD-ISCC-04300May 1, 2000 · N997CF · Doug DC862F · Fuselage Main, FrameSDR RRXA000198Pin · brokenAFTER TAKE OFF FROM DEN UPON GEAR RETRACTION A LOUD NOISE WAS HEARD AND THE LEFT MAIN GEAR REMAINED DOWN. PER VERIFIED ALT GEAR DOOR LIGHT ON AND SPOILER PRESS REMAINED UP. BOTH DOORS NOT LATCHED AND GEAR NOT LATCHED, REMAINED ON. FOUND EYE BOLT-PIN ON LT Mar 31, 2000 · N997CF · Doug DC862F · Landing Gear Retraction/Extension SystemSDR ARWA000302Thrust Reverser · wornMHLM - FLT 541 - ON POST FLIGHT, FOUND NR 1 ENGINE LOWER REVERSER TRACK DAMAGED. TROUBLESHOT AND FOUND THAT THE LOWER TRACK FORWARD YOKE ASSY EYEBOLT SEPARATED FROM ENGINE CASE ATTACH POINT. NO OTHER DAMAGE TO THE ENGINE. REMOVED AND REPLACED LOWER TRACK ANMar 18, 2000 · N791AL · Doug DC862F · Engine Thrust ReverserSDR RRXA000182Engine · leakingDURING CLIMBOUT, NOTED NR 1 ENGINE LOW OIL PRESS LIGHT ILLUMINATED. NR 1 OIL PRESS 20 PSI AND DROPPING, OIL TEMP DECREASING, NR 1 OIL QUANTITY 1.5 GAL AND DECREASING EVEN AFTER ENGINE WAS SHUTDOWN. PERFORMED INFLIGHT ENGINE SHUTDOWN AND QRH PROCEDURES INITIAFeb 2, 2000 · N997CF · Doug DC862F · Engine (Turbine/Turboprop)SDR RRXA991477Skin · corrodedDURING POST-FLIGHT INSPECTION FOUND THREE (3) POPPED RIVETS TO EXTERNAL SKIN BETWEEN STA 225 TO STA 255 AND LONGERON 21 RIGHT. REMOVED RIVETS FROM SKIN PANEL FROM STA 225 TO STA 255 AND LONGERON 21 RIGHT TO GAIN ACCESS TO REMOVE CORROSION. TREATED AREA IAW DOct 1, 1999 · N998CF · Doug DC862F · Fuselage Main, Plate/SkinSDR RRXA991469Skin · corrodedDURING LINE INSPECTION FOUND 6 EACH POPPED FASTENERS ON EXTERNAL SKIN AT STA 270 AND LONGERON 21 RIGHT. INSPECTED ENTERNAL AREA AND FOUND DOUBLER WITH CORROSION DAMAGE BEYOND LIMITS. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLEDSep 16, 1999 · N997CF · Doug DC862F · Fuselage Main, Plate/SkinSDR ARWA990801Egt Indicator · malfunctionedMIA - FLT 628 - AIR TURNBACK. DURING CLIMB, NR 4 ENGINE INDICATED 40 DEGREES LOWER THAN OTHER ENGINES, HOWEVER, WHEN LEVELED OFF AND AFTER SETTING CRUISE POWER, EGT CONTINUED DECREASING UNTIL IT INDICATED 100 DEGREES CELSIUS LOWER THAN OTHER ENGINES. PERFORMAug 6, 1999 · N791AL · Doug DC862F · Engine EGT/TIT Indicating SystemSDR ARWA990702Valve · leakingMIA - FLT 9038 - DURING CLIMB, F/O'S AIRSPEED INDICATOR WAS SHOWING 10 KTS LOWER THAN THE CAPT AND THE DIFFERENCE INCREASED WITH THE ALTITUDE UP TO 50 KTS LOWER FL230. SELECTED F/O'S STATIC SELECTOR TO ALT FOR LANDING. REMOVED AND REPLACED KNOB ALT PITOT SELJul 3, 1999 · N791AL · Doug DC862F · Airspeed/Mach IndicatorSDR RRXA99804Packing · missingHYDRAULIC OIL LOW LIGHT CAME ON HYDRAULIC QUANTITY DECREASING, RESERVOIR LOW PRESSURE LIGHT ON. EMERGENCY PROCEDURE INITIATED. EMERGENCY DECLARED. FOUND HYD LINE MISSING PACKING REPLACED PACKING RAN ENGINES AND AUX PUMP. NO LEAKS NOTED, OPS NORMAL.May 19, 1999 · N997CF · Doug DC862F · Hydraulic System, MainSDR RRXA99897Actuator · failedON TEST OF FUEL DUMP SYSTEM, WHEN DUMP SWITCH WAS PLACED TO DRAIN THE CHUTES WOULD NOT MOVE TO DRAIN. TRIED MANUAL DRAIN, NO HELP. FUEL CONTINUED TO DUMP TO STAND PIPES. REMOVED AND REPLACED DUMP CHUTE ACTUATOR IAW DC8 MM 28-30-2, OPS CK GOOD AT THIS TIME.May 15, 1999 · N997CF · Doug DC862F · Fuel Dump SystemSDR RRXA991186Fitting · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, FWD CARGO COMP C-2 DOOR CUT-OUT BETWEEN STA 500 AND STA 560, BL 34 RIGHT AT FITTINGS. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED NEW AND INSTALLED FApr 18, 1999 · N997CF · Doug DC862F · Fuselage Miscellaneous StructureSDR RRXA991176Angle · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, ATTACH ANGLE, RT W/W AT STA 879, BL 0, WL 16 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW ANGLE IAW DC8 SRM 51-1-4 (PAGE 1);Apr 6, 1999 · N997CF · Doug DC862F · Fuselage Miscellaneous StructureSDR RRXA991225Floor Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSEALAGE, LT CABIN FLOOR BETWEEN STA 680 AND STA 700 AT BL 54 LEFT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLER IAW DC8 SRM 53-2-3 PGS Apr 5, 1999 · N997CF · Doug DC862F · Fuselage Floor PanelSDR RRXA991226Floorbeam · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSEALAGE, CABIN FLOOR PLANK AT STA 1460 AND BL 6 LEFT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC8 SRM 51-1-8 PGS 16 ANDApr 1, 1999 · N997CF · Doug DC862F · Fuselage Main, Floor BeamSDR RRXA991224Floorbeam · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, CABIN FLOOR PLANK BETWEEN STA 1500 AND STA 1520 AT BL 36 LEF. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC8 SRM 5Apr 1, 1999 · N997CF · Doug DC862F · Fuselage Main, Floor BeamSDR TC8A99008Connector · looseON TAXI-OUT, SPOILER HYDRAULIC PRESSURE WENT TO 2200 PSI AND REMAINED THERE. FOUND LOOSE CONNECTOR AT TRANSMITTER CONNECTOR. SECURED IAW 27-0-0.Mar 31, 1999 · N187SK · Doug DC862F · Hydraulic Pressure Indicator
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