N609AW

Part: LEVER — OUT OF RIG (NR 3 ENGINE)

NR 3 THRUST LEVER NEEDS TO BE RE-RIGGED. UNABLE TO SET BELOW 40 PERCENT N1. (M)

Part: CONNECTOR — FAILED (NR 1 GEN BUSS) · airframe 29,895 hrs · 41,225 cycles

ENROUTE, NR 1 GENERATOR FAILED, NO VOLTS OR HZ, NR 1 AC BUSS AND AC ESSENTIAL BUSS FELL OFF LINE. NR 4 GEN FELL OFF LINE MOMENTARILY WITH AC NR 2 BUSS OFF LINE ALSO. RESET NR 4 GENERATOR BUT ONLY ABLE TO REGAIN AC NR 2 BUSS. STARTED APU, APU GENERATOR SHOWED VOLTS AND HZ BUT UNABLE TO POWER AC NR 1 BUSS OR ESSENTIAL BUSS. MAINTENANCE REMOVED AND REPLACED PLUG CONNECTOR 1XB12R.

Part: WARNING LIGHT — ILLUMINATED (COCKPIT) · airframe 27,810 hrs · 38,800 cycles

FAULT LIGHT ILLUMINATED FLAPS STUCK AT 18 DEGREES. MAINTENANCE CLEARED FAULT USING BAE SUPPLEMENT. RAN FLAPS, OPS CHECKED GOOD.

Part: CONNECTOR — DIRTY (ANTI SKID SYSTEM) · airframe 27,252 hrs · 38,170 cycles

DURING TAXI BRAKES SEEM INAFFECTIVE ON YELLOW HYDRAULIC SYSTEM. SWITCHED TO GREEN SYSTEM AND BACK TO YELLOW SYSTEM BRAKING NORMAL. MAINTENANCE REMOVED THE ANTI-SKID CONTROL BOX AND CLEANED CONNECTION OPERATIONAL CHECK GOOD. VISUALLY OBSERVED BRAKES ON YELLOW AND GREEN SYSTEM WHEN APPLIED.

Part: SCOOP — CRACKED (NR 1 ENGINE) · airframe 27,180 hrs · 38,084 cycles

NR 1 ENGINE OUT BOARD DOOR NACA SCOOP AND ATTACHMENTS CRACKED. MAINTENANCE REPAIRED FAN DOOR NACA SCOOP AS REQUIRED ALSO REPAIRED APLITTER ANGLE IAW SRM AND FAX BARA/AVR/5228/00.

Part: PIN — CRACKED (NLG) · airframe 27,180 hrs · 38,084 cycles

WHILE PERFORMING INSPECTION OF NLG RETRACTION BOSS FOUND EVIDENCE OF VISUAL FRETTING OF ATTACH PIN. FURTHER INSPECTION REVEALED TORQUE AT 20 FT LBS AND SIGNS OF CRACKING VISUALLY CONFIRMED BY NDT SIDEWALL BAD. MAINTENANCE REPLACED NOSE DIAPHAGM PER RIL HC53H9416.

Part: GIRT BAR — DISENGAGED (PASSENGER DOOR)

AFT PASSENGER CABIN DOOR AFTER OPENING, GIRT BAR DISENGAGED FROM DOOR. FOUND NO PARTIAL DEPLOYMENT OF SLIDE, RE-ENGAGED GIRT BAR TO DOOR. RECONNECTED SLIDE AUTODEPLOY LANYARD. OPS CHECKED DOOR AND GIRT BAR. OPS CHECKS SATISFACTORY. ACFT TT: 23,562 HOURS. ACFT TC: 33,928. (X)

Part: ACTUATOR — LEAKING (AFT AIRSTAIR)

ATW - FLT 581 - YELLOW HYDRAULIC FLUID LOST, WITH ASSOCIATED FLUID AT REAR AIRSTAIR AND LAVATORY. FOUND AFT AIRSTAIR, FORWARD ACTUATOR LEAKING, CLEANED, CAPPED OFF LINE AND DEFERRED AND PLACARDED, C/W OVERWEIGHT LANDING INSPECTION.

Part: SKIN — CHAFED (FUSELAGE)

FUSELAGE SKIN CHAFED APPROX 13 INCHES LONB BY FORWARD RIGHT WING ROOT FAIRING BETWEEN FRAMES 25/26. REF W/C 6075 FOR BLEND AND NDT. FIT EXTERNAL PATCH OVER CHAFED AREA UNDER RT WING ROOT FAIRING ON FUSELAGE SKIN BETWEEN FRAMES 25/26 PER SRM 53-00-12 FIGURE 201 INC STRINGERS ABOVE AND BELOW CHAFE PER FAX REF DJH/RJO248-98. (M)

Part: PROX SWITCH — FAILED (LT MLG)

WITH GEAR HANDLE SELECTOR UP, LEFT MAIN GEAR INDICATES GEAR INTRANSIT, RID LIGHT IN GEAR HANDLE ALSO ILLUMINATED. NO AURAL GEAR WEARING. STANDBY GEAR INDICATORS ALL OFF. REMOVED AND REPLACED LEFT MLG LEG UPLOCK HARNESS AND PROXIMITY SWITCH IAW BAE 146MM, TESTS GOOD. S/N ON 4805.

Part: ARM — FAILED (NLG)

DURING GEAR RETRACTION AT EGE, HEARD A VERY LOUD BANG FROM NOSE WHEEL AREA ACCOMPANIED BY WHEEL ROTATION SOUNDS. GEAR RETRACTION AND EXTENSION NORMAL. REPLACED LEFT EMEREGNCY LOWERING GEAR ASSISTING ARM ASSY. RETRACTED GEAR, FREE FALL OPS CHECKED GOOD. CLOSED NLG DOORS AND SAFTIED AND RII'D. (M)

Part: BOLTS — LOOSE (RIB 0 & 2)

FOUND LOOSE JOBOLTS AT VARIOUS LOCATIONS AT WING TANK RIB '0' AND RIB 2 LT/RT. COMPLETED LOOSE JOBOLT REPLACEMENT AT RIB 0 AND RIB 2 LT/RT PER RIL HC571H9033. NOTE, 6 POSITIONS WERE OVERSIZED.

Part: STALL BAR — OUT OF POSITION (RT WING)

RIGHT WING SHORT SECTION OF STALL BAR PULLING OVER CORNER SCREWS. REMOVED LEFT WING STALL TRIGGER AND REPAIR PER FAX REF DJH/R JO268 USING FAX GCB/RJ1344-94 AND REINSTALLED STALL TRIGGER. (M)

Part: STALL BAR — LOOSE (LT WING)

LEFT WING INBOARD SECTION OF STALL BAR LOOSE, PULLING OVER SCREW HEADS. REMOVED LT WING STALL TRIGGER AND REPAIRED PER FAX REF DJH/RJO268-98 USING FAX GCB/RJ1344-94. REINSTALLED STALL TRIGGER. (M)

Part: WIRE — BROKEN (FIRE WARNING)

NR 1 ENGINE POWER LEVER FIRE WARNING LIGHT DOES NOT ILLUMINATE DURING FIRE TEST, WIRE BAD. REMOVED AND REPLACED BOTH WIRES IN POWER LEVER FIRE WARNING. TESTED PER MM. (M)

Part: BULKHEAD STRIP — CORRODED (LAVATORY)

FORWARD LAVATORY BULKHEAD I2109 LOWER METAL STRIP ON BOTTOM OF BULKHEAD IS CORRODED. INSTALLED LOWER METAL STRIP ON FORWARD LAVATORY BULKHEAD I2109 OLD UNIT PREVIOUSLY REMOVED. (M)

Part: STIFFENER — CRACKED (LT WING)

LEFT WING TE TOP SKIN, TWO STIFFENERS CRACKED AT FORWARD END BETWEEN RIB 8/9. REPLACED LEFT WING TRAILING EDGE TOP SKIN STIFFENER BETWEEN RIB 8/9 (P/N HC572H0626-0000). REPAIRED LEFT WING TRAILING EDGE TOP SKIN STIFFENER BETWEEN RIB 8/9 (P/N HC572H0627-002) IAW BAE FAX JM/RJO241-98. (M)

Part: BOLT — WORN (RT AIRBRAKE)

RIGHT AIRBRAKE UPPER ATTACH POINT BOLT PLATING IS WORN OFF, BOLT WAS FROZEN IN BEARING. REMOVED AND REPLACED HINGE PIN AND BUSH. INSTALLED DURING AIRBRAKE INSTALLATION. SEE W/C NR 3019 FOR INSTALLATION. (M)

Part: ANGLE — CRACKED (PAX DOOR)

LEFT FORWARD PAX DOOR HANDLE BOX AREA 2 CRACKED ANGLES. REPLACED LEFT FORWARD PAX DOOR HANDLE BOX AREA ANGLES REF P/N'S ABOVE. REPAIR ACCOMPLISHED IAW BAE DRAWINGS HC521H0508 AND HC521H0507 AND BAE FAX REF DJR/RJO318-97. (M)

Part: STIFFENER — CRACKED (RT WING)

RIGHT WING TE TOP SKIN STIFFENER CRACKED AT AFT END BETWEEN RIBS 3/4. REMOVED AND REPLACED STIFFENER. (M)

Part: SKIN — CHAFED (RT MLG DOOR)

RIGHT MLG DOOR INTERNAL SKIN, FORWARD EDGE, APPROX 1ST 6 INCHES DOWN HAS EVIDENCE OF CHAFING ON FRAME NR 29 WHEN L/G IS UP AND LOCKED. BLENDED OUT CHAF IN DRUM, MINOR DAMAGE WITHIN LIMITS, PRC COATED FOR ABRASION. (M)

Part: ATTACH LINKS — CORRODED (RT WING)

RIGHT WING TO FUSELAGE AFT ATTACH LINKS HAVE SURFACE CORROSION ON ENDS (PAINT MISSING). CLEANED, PRIMED AND PAINTED ENDS. (M)

Part: PULLEY — SEIZED (RT WING)

RIGHT WING LOWER AILERON TRIM CABLE PULLEY SEIZED OUTBOARD OF NR 4 FLAP TRACK. REMOVED AND REPLACED TRIM CABLE PULLEY'S AS NEEDED IAW MM. (M)

Part: BOLTS — LOOSE (LT WING)

PERFORM RIL HC571H9033 LT RIB 2 OUTBOARD JOBOLTS. PERFORMED RIL HC571H9033 ON LEFT RIB 2 OUTBOARD JOBOLTS. (M)

Part: BRACKET — CRACKED (RT WING)

RIGHT WING TE HYD LINE CLAMP BRACKET CRACKED AT FALSE SPAR ABOVE NR 2 FLAP TRACK. REPLACED RIGHT WING TE HYD LINE CLAMP BRACKET. (M)

Part: STIFFENER — CRACKED (RT WING)

RIGHT WING TE TOP SKIN STIFFENER CRACKED AT FORWARD END BETWEEN RIBS 8/9. REPLACED RT WING TRAILING EDGE TOP SKIN STIFFENER BETWEEN 7/8. (M)

Part: STIFFENER — CRACKED (RT WING)

RIGHT WING TE TOP SKIN STIFFENER CRACKED AT FORWARD END BETWEEN RIBS 7/8 (OUTBOARD STIFFENER). REPLACED RT WING TRAILING EDGE TOP SKIN STIFFENER BETWEEN RIB 7/8. (M)

Part: SKIN — CHAFED (LT MLG DOOR)

LEFT MLG DOOR INTERNAL SKIN FORWARD EDGE APPROX 1ST 6 INCHES FROM TOP EDGE HAS EVIDENCE OF CHAFING ON FRAME NR 29 WHEN GEAR IS UP AND LOCKED. TRANSFER TO W/O BX1879 FOR REPAIR. (M)

Part: FALSE SPAR — CRACKED (RT WING)

RIGHT WING TE FALSE SPAR CRACKED JUST INBOARD OF INBOARD LIFT SPOILER JACK. REPAIRED PER FAX JM/RJ0240-98, PER DRAWING HC572H9036. OPPOSITE HAND TO DRAWING. (M)

Part: SKIN — CHAFED (RT TE FLAP TAB)

RIGHT FLAP TAB UPPER SKIN AT RIB 34 HAS TWO .011 INCH DEEP CHAFED AREAS, (.005 TO .008). BLENDED CHAFE MARKS TO SMOOTH PROFILE AS NEEDED IAW BAE FAX DJR/RJO234-98. DV AND NDT INSPECTION C/W IAW BAE FAX DJR/RJO234-98, AREA CRACK FREE. APPLIED SURFACE REPROTECTION AND TOP COAT PAINT IAW MM. (M)

Part: SKIN — CHAFED (RT TE FLAP)

RIGHT FLAP UPPER SKIN BETWEEN RIB 29/30 HAS .020 INCH DEEP BY 1 INCH LONG CHAFE. BLENDED CHAFE MARK TO A SMOOTH PROFILE AS NEEDED IAW BAE FAX DJR/RJO236-98. DV AND NDT INSPECTION C/W IAW BAE FAX DJR/RJO236-98, AREA CRACK FREE. APPLIED SURFACE REPROTECTION AND APPLIED PAINT IAW MM.

Part: BOLT — SCRATCHED (RUDDER ACT)

UPPER RUDDER ACTUATOR AFT ATTACHMENT BOLT HAS SCRATCH THAT GOES BELOW PLATING. REMOVED AND REPLACED UPPER RUDDER ACTUATOR AFT ATTACHMENT BOLT IAW AMM. (M)

Part: BEARING — WORN (RUDDER)

RUDDER TOP 'A FRAME HINGE POINT HAS A BAD BEARING. 'A' FRAME REMOVED FOR REPAIR. INSTALLED SERVICEABLE RUDDER TOP 'A' FRAME IAW BAE MM. (M)

Part: MOUNT — CRACKED (RT SPOILER)

RIGHT WING ROOT, LIFT SPOILER CONTROL VALVE MOUNT PLATE CRACKED. REMOVED AND REPLACED PLATE. (M)

Part: DOOR — DAMAGED (RT MLG)

RIGHT MLG DOOR LOWER FORWARD CORNER IS DEFORMED OUTWARD APPROX .167 FROM CONTOUR, APPROX 3.55 IN LENGTH. REPAIRED IAW BAE SRM 52-81-11, FIG 204, TYPE 2. (M)

Part: CONTROL CABLE — CORRODED (RT AILERON)

RIGHT WING AILERON INTERCONNECT CABLES AT WING ROOT PULLEY CORRODED. REMOVED AND REPLACED FUSELAGE INTERCONNECT CABLES (AILERON) IAW BAE MM. GENERATED WC TO PERFORM AILERON FUNCTIONAL CHECK AND PRI 2 WC TO RE-CHECK TENSION AT 4000 FLT INTERVAL. (M)

Part: CONTROL CABLE — CORRODED (LT AILERON)

LEFT CLAD INTERCONNECT CABLE FOR AILERONS SHOWS EVIDENCE OF CORROSION AT DIFFERENTIAL SECTOR BETWEEN RIBS 14/15. REMOVED AND REPLACED LEFT CLAD INTERCONNECT CABLE (AILERON) IAW BAE MM. GENERATED W/C TO PERFORM AILERON FUNCTIONAL CHECKS AND PRIORITY 2 WC TO RECHECK TENSION AT 4000 FLT INTERVAL. (M)

Part: CABLE GUARD — SEIZED (RT AILERON)

RIGHT WING ROOT, OUTBOARD CABLE GAURD SEIZED AND BOTH PULLEYS WORN FOR CENTER SECTION AILERON INTERCONNECT CABLES. REMOVED AND REPLACED PULLEYS EXTRACTED SEIZED GUARD AND REPLACED WITH NEW GUARD, RIGHT WING ROOT. (M)

Part: SEAL — DAMAGED (CARGO DOOR)

REAR CARGO DOOR LOWER SEAL CAGE IS BENT, DEFORMED IN SEVERAL AREAS. REPLACED REAR CARGO DOOR LOWER SEAL CAGE. (M)

Part: SEAL — BENT (CARGO DOOR)

FORWARD CARGO DOOR BOTTOM HALF SEAL CAGE IS DISTORTED, BENT IN NUMEROUS AREAS. REPLACED FORWARD CARGO DOOR BOTTOM AFT SEAL CAGE P/N HC523J0 063-202. STRAIGHTENED BEND IN PORTION OF BOTTOM FORWARD SEAL CAGE. (M)

Part: BEARING — WORN (RUDDER)

RUDDER BEARING BAD AT MAIN (RIB 6) 'A' FRAME SUPPORT. ALLOW AND EXCESSIVE UP AND DOWN FLOAT OF RUDDER ASSY .25 INCH APPROX. REMOVED AND REPLACED RUDDER MAIN 'A' FRAME (RIB 6) HINGE BEARING. (M)

Part: CONTROL CABLE — CORRODED (ELEVATOR)

LEFT AND RIGHT ELEVATOR CABLES ARE CORRODED AT PULLEYS IN VERTICLE STAB. REMOVED AND REPLACED LEFT AND RIGHT ELEVATOR CABLES FROM REAR PRESS BULKHEAD TO COMPENSATORS AND ADJUSTED IAW MM 27-31-00. W/C GENERATED FOR FUNCTION TEST. (M)

Part: SILL — CRACKED (PAX DOOR)

AFT PASSENGER DOOR, AFT SIDE OF DOOR SILL PLATE IS CRACKED ABOUT 1 INCH LONG. REMOVED DAMAGED SILL PLATE, DRILLED AND FITTED NEW SILL PLATE ON AFT PASSENGER DOOR, AFT SIDE INSTALLED NEW SILL PLATE AND PAINTED RIVET HEADS AND BUCKTAILS. (M)

Part: BRACKET — CRACKED (MLG WW)

UPPER ATTACH ANGLE BRACKET FOR MLG BAY DIAPHRAM HAS A CRACK. REPLACED UPPER ATTACH ANGLE BRACKET FOR MLG BAY DIAPHRAM. (M)

Part: HYDRAULIC LINE — LEAKING (NLG)

ORD - FLT 504 - SUSPECT HYDRAULIC FLUID FUMES IN AIRCRAFT. FOUND LEAKING NLG DOWN LINE. REPLACED LINE, GREEN SYSTEM.

Part: AIR DISTRIBUTION — FUMES (CABIN)

ORD - FLT 504 - NOTICED FUMES IN CABIN ON GROUND WHILE ON APU AIR. RAN BOTH PACKS TO FULL HOT. NO FUMES NOTED.

Part: DOUBLER — CRACKED (BS 47.2)

RIGHT STIFFENER (STATION 47.20) AT FRAME 29 IN HYDRAULIC BAY HAS CRACKED DOUBLER PLATE AT BOTTOM END OF STIFFENER. REPLACED RIGHT STIFFENER (STATION 47.20) AT FRAME 29 IAW BAE DRAWING NR HC536H0090 AND AIR FAX NR DS/W/TS/25913/96.

Part: TRIM CHAIN — CORRODED (LT AILERON)

LEFT AILERON TRIM SCREWJACK CHAIN APPEARS TO BE CORRODED. LEFT TRIM CABLE TURNBUCKLES LOOSE. REMOVED AND REPLACED LEFT AILERON TRIM CHAIN IAW 27-12-17. A DJUSTED CABLES AND COMPLIED WITH FUNCTION TEST IAW 27-12-00. CHECKS OK. (M)

Part: FLOORBEAM — CRACKED (CABIN)

THREE FLOORBEAMS ARE CRACKED AT FRAME 29 BEAM 3, 13 AND 19. REPAIRED CRACKS IAW BAE DRAWING HC536H9211 AND FAX AIRAMS/T/BAE/25858/96.

Part: SERVO VALVE — MALFUNCTIONED (AIR BRAKES)

ATW - FLT 509 - AIR BRAKE OPENED DURING CRUISE WITHOUT BEING SELECTED. CORRECTIVE ACITON: REMOVED AND REPLACED AIRBRAKE SERVO VALVE, OPS TEST GOOD, LEAK CHECKS GOOD. S/N OFF: FYH165948. S/N ON FHY144505.

Part: CABLES — RUSTED (RT AILERON CONTL)

BOTH UPPER AND LOWER AILERON CONTROL CABLES RT WING ROOT ARE RUSTED AND NEED REPLACED. CORRECTIVE ACTION: REMOVED AND REPLACED UPPER AND LOWER RT AILERON CONTROL CABLES IAW A.M.M. SEE WORK CARD NR 2069 FOR FUNCTION CHECKS.

Part: ENGINE — MALFUNCTIONED (NR 1)

AIRCRAFT RETURNED TO DEN NR 1 ENGINE TGT IND FULL SCALE AND FLAGGED. N1 WNET TO 60 PERCENT AND WF WENT TO 600 LBS. TMS WAS ON AT THE TIME. LOCKED DOWN ENGINE AND FERRIED TO ATW FOR REPAIR. BUSBAR BROKE.

Part: SKIN — BIRD STRIKE (FWD FUSELAGE)

DEN - FLT 353 - EN ROUTE, BIRD STRIKE ON NOSE OF AIRCRAFT. AIR RETURN. INSPECTED AIRCRAFT IAW BAE MM 05-50-21. BIRD STRIKE INSPECTION. NO DEFECTS NOTED ON AIRCRAFT OR ENGINES.

Part: ISO VALVE — FAILED (LEFT ENGINE)

ORD - FLT 372 - YELLOW HYDRAULIC HI-TEMP WARNING LIGHT CAME ON, 25 MINUTES INTO FLIGHT, LIGHT WENT OUT APPROXIMATELY 10 MINUTES LATER. REMOVED AND REPLACED LEFT ENGINE HYDRAULIC PUMP ISO VALVE. OPS AND LEAK CHECK GOOD. S/N OFF 785VB137. S/N ON 1185VB154.

Part: MANIFOLD — CRACKED (NR 2 ENGINE)

DURING ROUTINE MAINTENANCE, FOUND NR 2 ENGINE LEFT FUEL MANIFOLD HAD EVIDENCE OF A FIRE AND AN INDICATION OF A CRACK. REPLACED THE MANIFOLD.

Part: ENG — FAILED (NR 1 ENG)

AFTER TAKEOFF CLIMBING OUT OF ASE NR 1 ENGINE LOW OIL PRESS LT FLICKERED ON AND OFF COUPLE OF TIMES, CREW FOLLOWED ENG LOW OIL PRESS CHECKLIST, LATER THE LOW OIL PRESS LT CAME BACK ON, OIL QTY WAS BOUNCING OFF EMPTY, CREW SHUT ENGINE DOWN AND PROCEEDED TO DEN. (W)

Part: HOSE — KINKED (PAX 02 BOTTLE)

OXYGEN PASSENGER BOTTLE S/N 101 (CONTROL HEAD S/N) HAS ITS MASK HOSE KINKED AND OXYGEN WILL NOT FLOW TO THE MASK. REMOVED AND REPLACED OXYGEN MASK ASSY. OPS CHECKED OK AT THIS TIME. (W)

Part: PIVOT PIN — WORN (RT WING FLAP)

RT WING NR 3 FLAP TRACK, PIVOT PINS INBOARD AND OUTBOARD AFT POINT ARM TO CARRIAGE BAD. NEW PINS INSTALLED IN BOTH POSTIONS. (W)

Part: PIPE — HOLE CHAFED (PANEL 441AL)

NR 4 NOSE COWL, PANEL 441AL, PIPE FROM FIRE BOTTLE TO RELIEF INDICATOR HAS HOLE WORN THROUGH FROM SUPPORT CLAMP. RUBBER BAD ON CLAMP. INSTALLED NEW PIPE FOR NR 4 LT FIRE BOTTLE DISCHARGE INDICATOR LINE IAW BAE 146 MM. BOTTLE AND SQUIBB NOT DISTURBED. (W)

Part: CONTROL CABLE — CORRODED (ELEV TRIM)

CORROSION NOTED ON ELEVATOR TRIM CONTROL CABLES (52AB) UNDER DOGHOUSE PANEL INTO HORIZ STABS (NEED FURTHER EXAMINATION). UPON FURTHER INSPECTION FOUND CORROSION ON INNER STRANDS OF ELEV INTERCONNECT. NO CORROSION ON OTHER CABLES. (W)

Part: SILL PLATE — CORRODED (PAX DOOR)

PASSENGER DOOR SILL PLATE HAS SOME CORROSION FWD VESTIBULE. REMOVED AND REPLACED PASSENGER DOOR (LEFT FWD) WITH NEW SILL PLATE PER SRM STANDARD PRACTICES CHAPTER 51. (W)

Part: CONTROL CABLE — CORRODED (AILERON)

AILERON INTERCONNECT CABLES APPEAR TO HAVE CORROSION AT PULLEYS UNDER BOTH WING ARMPITS. REMOVED AND REPLACED BOTH AILERON INTERCONNECT CABLE CENTER SECTIONS (62BC AND 63BC) IAW MM IAW MM 27-11-00. TRAVEL AND FUNCTIONAL CHECKS OK. (W)

Part: GUSSET — CORRODED (FLOOR BEAM)

SEVERAL FLOOR BEAM GUSSETS CORRODED IN FWD VESTIBULE BETWEEN FRAME 15-18. REMOVED AND REPLACED SEVERAL FLOOR BEAM GUSSETS IN FWD VEST BETWEEN FRAME 15-18, PLACED AIRCRAFT INTERCOSTALS AND FRAME BETWEEN FRAME 15 TO 18. (W)

Part: STUB PIN — CRACKED (LT NR 2 FLAP)

LEFT NR 2 FLAP TRACK STUB PIN INBOARD P/N HC57960282000 FAILED NDT CRACKED INDICATION SSI 57-55-125. REPLACED LEFT NR 2 FLAP TRACK INBOARD STUB PIN. (W)

Part: BOLT — CORRODED (RT ELEV HINGE)

RT ELEVATOR HINGE BOLT NR 1 POSITION CORRODED. REMOVED AND REPLACED RT ELEVATOR HINGE BOLT AS REQ'D IAW MM. (W)

Part: BOLT — CORRODED (LT ELEV HINGE)

LEFT HINGE BOLT NR 1 POSITION CORRODED. REMOVED AND REPLACED BOLT AS REQ'D IAW MM. (W)

Part: FIRE BOTTLE WIRE — CHAFED (NR 4 ENGINE)

NR 4 ENGINE, BARE WIRE ON WIRE BUNDLE GOING TO RIGHT FIRE BOTTLE LOCATED IN PANEL 442AR CHAFING ON TIE WRAP ON ANOTHER WIRE BUNDLE. INSPECT WIRE 4HK365 AND FOUND PTFE INSULATION DAMAGED BUT FOUND KAPTON TAPE TO BE UNDAMAGED. REPAIRED BY INSTALLATION OF HIGH TEMP HEAT SHRINK TUBING IAW WIRING MANUAL STAN PRAC 20-44-04. DAMAGE OF INSULATION WAS APPROX 8 INCHES FROM CANNON PLUG.

Part: BOLT — CORRODED (NR 4 PYLON)

REMOVED NR 4 PYLON FORWARD YOKE TO ENGINE BOLTS FOR NDT (4 EACH) SSI 54-00-123 (1 EACH REJECTED DUE TO CORROSION). REINSTALLED 3 ORIGINAL BOLTS AFTER NDT AND 1 NEW BOLT AT RT LOWER POSITION, TORQUED AND SAFETIED. (W)

Part: BOLT — SCORED (ENG MOUNT)

ENGINE MOUNTS BOLTS (4 EACH) REQUIRE INSPECTION. PERFORMED VISUAL AND FLOURSCENT DYE PENETRANT INSPECTION ON 4 BOLTS. FOUND 1 WITH DEEP SCORE AND INDICATION AT HEAD TO SHANK RADIUS. SCRAPPED THAT BOLT. THREE BOLTS GOOD FOR RETURN TO SERVICE. ISSUED NEW BOLT FROM STOCK TO REPLACE THE ONE SCRAPPED. (W)