N463AP

Part: SKIN — DAMAGED (FUSELAGE)

REPAIR TO RIGHT SIDE OF FUSELAGE AT FRAMES 11-13 AT LAP 'E' AREA. C/W REPAIR IAW BAE 146 SRM AND FAX CW/RJ/0754-99, CW/RJ/0761-99 AND DRAWING HC537H9411. (X)

Part: ANGLE — CRACKED (PASSENGER DOOR)

FORWARD PASSENGER DOOR, INTERNAL ANGLE CRACKED. REPLACED ANGLE. (X)

Part: STIFFENER — CRACKED (RT WING)

RIGHT WING TRAILING EDGE UPPER SHROUD SKIN STIFFENER, NR 176 BETWEEN RIBS 7 AND 8, CRACKED FORWARD END. REPAIRED RT WING TRAILING EDGE UPPER SHROUD SKIN STIFFENER BETWEEN RIBS 7 AND 8 IAW BAE FAX DJR/RJ0630-98. (X)

Part: STIFFENER — CRACKED (LT WING)

LEFT WING TRAILING EDGE UPPER SHROUD SKIN STIFFENER, NR 178 BETWEN RIBS 8 AND 9, CRACKED FORWARD END. REPLACED LT WING TRAILING EDGE UPPER SHROUD SKIN STIFFENER BETWEEN RIBS 8 AND 9. (X)

Part: STIFFENER — CRACKED (LT WING)

LEFT WING TRAILING EDGE UPPER SHROUD SKIN STIFFENER NR 176 BEWEEN RIBS 7 AND 8 CRACKED, FORWARD END. REPLACED LEFT WING TRAILING EDGE UPPER SHROUD SKIN STIFFENER BETWEEN RIBS 7 AND 8. (X)

Part: STIFFENER — CRACKED (LT WING)

LEFT WING TRAILING EDGE UPPER SHROUD SKIN STIFFENER NR 177 BETWEEN RIBS 8 AND 9 CRACKED FORWARD END. REPAIRED LEFT WING SKIN TRAILING EDGE, UPPER WING SKIN TRAILING EDGE STIFFENER BETWEEN RIBS 8 AND 9 IAW BAE FAX DJR/RJ0630-98. (X)

Part: STIFFENER — CRACKED (RT WING)

RIGHT WING TRAILING EDGE UPPER SHROUD SKIN STIFFENER, NR 172 BETWEEN RIBS 3 AND 4, CRACKED FORWARD END. REPLACED RT WING TRAILING EDGE UPPER SHROUD SKIN STIFFENER BETWEEN RIBS 3 AND 4. (X)

Part: STIFFENER — CRACKED (LT WING)

UPPER WING SKIN TRAILING EDGE STIFFENER IS CRACKED AT FORWARD END LOCATED BETWEEN RIBS 9 AND 10, LEFT WING. REPAIRED LT WING SKIN TRAILING EDGE UPPER WING SKIN STIFFENER BETWEEN RIBS 9 AND 10 IAW BAE FAX DJR/RJ0630-98. (X)

Part: SLIDE — OUT OF POSITION (PAX DOOR)

WHILE INSPECTIONG GIVE BAR MECHANISM ON FORWARD PASSENGER DOOR SLIDE PARTIALLY DEPLOYED. REMOVED AND REPLACED FORWARD PASSENGER DOOR SLIDE IAW MM. (M)

Part: SLIDE — DEPLOYED (PASSENGER DOOR)

ORD - FLT 545 - WHILE INSPECTING GIVE BAR MECHANISM ON FORWARD PASSENGER DOOR, SLIDE PARTIALLY DEPLOYED. REMOVED AND REPLACED FORWARD PASSENGER DOOR SLIDE IAW MM.

Part: HANDLE — OUT OF ADJUST (PAX DOOR)

FORWARD PAX DOOR, SLIDE ARMING HANDLE HITS THE HANDLE RECESS NOT ALLOWING THE GIRT BAR TO FULLY ENGAGE INTO LUGS. REMOVED UPPER DOOR COVER AND ARMING HANDLE RECESS RECONTURED RECESS PAINTED AND REINSTALLED RECESS AND UPPER DOOR COVER, OPS CHECKED GOOD. (M)

Part: STIFFENER — CRACKED (RT WING)

RIGHT WING TE LOWER SHROUD SKIN STIFFENER CRACKED BETWEEN RIB 7/8. REPLACED STIFFENER IN RIGHT WING TE LOWER SHROUD SKIN BETWEEN RIBS 7/8. (M)

Part: BULKHEAD — CRACKED (NR 1 ENGINE)

NR 1 ENGINE LEFT AFT COWL DOOR BULKHEAD AT VENT TUBE AREA CRACKED. REPAIRED CRACK IN FLANGE OF BULKHEAD BY PATCHING IAW BAE/AIR WISC SRM STANDARD PRACTICES. (M)

Part: DOOR — DAMAGED (NR 3 ENGINE)

NR 3 ENGINE AFT INBOARD FAN DOOR LOWER DOOR SPLITTER AREA HAS CHAFED STIFFENER, 2ND FROM FORWARD. REPLACED ABOVE STIFFENER PER SRM. (M)

Part: BRACKET — CRACKED (LT WING)

LEFT WING, FORWARD HYD LINE CLAMP BRACKET, RIB 5, CRACKED. REPLACED BRACKET. (M)

Part: DOOR — CRACKED (NR 1 ENGINE)

NR 1 ENGINE AFT LEFT COWL DOOR SECOND STIFFENER ON LOWER SPLITTER ASSY CRACKED. REPLACED SECOND STIFFENER ON NR 1 ENGINE LEFT COWL DOOR. (M)

Part: SKIN — CHAFED (NR 3 ENGINE DOOR)

NR 3 ENGINE AFT INBOARD FAN DOOR INNER TITANIUM SKIN CHAFED THROUGH. REPLACED PAN AND PATCHED SMALL AREA 2.25 BY 3.5 USING TAZ PER PSI. (M)

Part: MASK — TORN (CABIN)

CAIN OXYGEN MASKS FOR PASSENGERS FILTERS TORN SEAT 3A, 10B, 12A, 12B, 14C, 15C, 13E, 10F. REMOVED AND REPLACED FILTER TO PER COMPONENT MM TO 3A, 10B, 12A, 12B, 14C, 15C, 13E, 10F. (M)

Part: BRACKET — CRACKED (FUSELAGE)

ANGLE BRACKET, P/N HC361JO137-006 CRACKED. LOCATED AT RIGHT ECS DUCT FRAME 45 SUPPORT OVERTEMP SWITCH BRACKET. MANUFACTURED BRACKET IAW AIR WISC/BAE SRM STANDARD PRACTICES. DRILLED TO FIT IAW BAE FAX JM/RJ 0418-98. ALODINED AND PRIMED. SEE ADDITIONAL W/C FOR BRACKET INSTALLATION. (M)

Part: STIFFENER — CRACKED (LT WING)

LEFT WING TRAILING EDGE SHROUD TOP SKIN STIFFENER IN AREA BETWEEN RIBS 9/10 IS CRACKED AT FORWARD END. REPAIRED LEFT WITH TE SHROUD TOP SKIN STIFFENER BETWEEN RIBS 9/10 IAW BAE FAX NR JM/RJO417-98, REF REINSPECTION W/C 5020. (M)

Part: STIFFENER — CRACKED (RT WING)

RIGHT WING TE TOP SHROUD SKIN STIFFENER CRACKED AT FORWARD END INBOARD OF RIB 9. REPAIRED RIGHT WING TE TOP SHROUD SKIN STIFFENER BETWEEN RIBS 8/9 IAW BAE FAX NR JM/RJ0417-98. (M)

Part: BULKHD LONGERON — CRACKED (MLG WW)

FRAME 29 MAIN LANDING GEAR BAY ROOF PRESSURE BULKHEAD, LONGERONS NR 3, NR 9, NR 15 CRACKED. REPAIRED PRESS BULKHEAD LONGERONS NR 3, NR 9, AND NR 15 PER REPAIR DRAWING HC536H9211 AND SRM, AND FAX'S NUMBERED D-JH/R-JO419-98, D-JH/R-J0421-98, AND D-JH/R-J0422-98 ALL DATED 21 MAY, 1998, AND FAX D-JR/R-J0207-97 DATED 21 MAY, 1998, AND FAX D-JR/R-JO207-97 DATED 26 FEB 1997. (M)

Part: STIFFENER — CRACKED (RT WING)

RIGHT WING TE SHROUD TOP SKIN STIFFENER CRACKED AT FORWARD END BETWEEN RIBS 7/8. REPAIRED RIGHT WING TE TOP SHROUD SKIN STIFFENER BETWEEN RIBS 7/8. (M)

Part: DOOR — DAMAGED (NR 4 ENGINE)

NR 4 ENGINE AFT OUTBOARD FAN DOOR LOWER DOOR SPLITTER AREA, STIFFENER AT FORWARD CORNER CHAFED BADLY. REPLACED NR 4 ENGINE AFT OUTBOARD FAN DOOR LOWER DOOR SPLITTER AREA, STIFFENER AT FORWARD CORNER. (M)

Part: DOOR — DAMAGED (NR 4 ENGINE)

NR 4 ENGINE AFT OUTBOARD FAN DOOR LOWER DOOR SPLITTER AREA 2ND STIFFENER FROM FORWARD CHAFED. REPLACED NR 4 ENGINE AFT OUTBOARD FAN DOOR LOWER DOOR SPLITTER AREA, 2ND STIFFENER FROM FORWARD. (M)

Part: STIFFENER — CRACKED (LT WING)

LEFT WING TE SHROUD TO PSKIN STIFFENERS ARE CRACKED AT FORWARD END IN AREA BETWEEN RIBS 8/9. REPAIRED LEFT WING TE SHROUD TO SKIN STIFFENER BETWEEN RIBS 8/9. (M)

Part: STIFFENER — CRACKED (LT WING)

LEFT WING TE TOP SKIN STIFFENER IS CRACKED AT FORWARD END IN AREA BETWEEN RIBS 7/8. REPAIRED LEFT WING TE TOP SKIN STIFFENER BETWEEN RIBS 7/8 IAW BAE FAX NR JM/RJO417-98. REF W/C 5022 FOR REINSPECTION. (M)

Part: GUSSET — CORRODED (FRAME 15)

NR 2 GUSSET PLATES CORRODED LEFT SIDE FRAME 15 FLOORBEAM. REPLACED TWO GUSSET PLATES LEFT SIDE FRAME 15 FLOORBEAM. (M)

Part: STIFFENER — CRACKED (RT WING)

TOP RIGHT WING T/E SKIN STIFFENER TWIX WING RIBS 3/4 CRACKED AT AFT END. REPAIRED RIGHT WING TE TOP SHROUD SKIN STIFFENER BETWEEN RIBS 3/4. (M)

Part: FALSE SPAR — CRACKED (RT WING)

RIGHT WING TE HAS TEMP REPAIR (STOP DRILL) TO CRACK IN FALSE SPAR CAP BETWEEN RIBS 7/8, NEEDS PERM REPAIR. REPAIRED RIGHT WING TE BETWEEN RIBS 7/8. (M)

Part: STIFFENER — CRACKED (LT WING)

LEFT WING TE SHROUD BOTTOM SKIN STIFFENER CLEATS ARE CRACKED IN AREA BETWEEN RIBS 8/9. REPLACED BOTH CLEATS AS PER POSITIONS ABOVE USING BAE STANDARD PRACTICES AND PROCEDURES. (M)

Part: SILL — CORRODED (SERVICE DOOR)

FORWARD VESTIBULE, SERVICE DOOR SILL PLATE HAS SEVERAL SMALL SPOTS OF SURFACE CORROSION. REMOVED AND REPLACED SILL PLATE WITH NEW. (M)

Part: GUSSET — CORRODED (FRAME 15)

FORWARD VESTIBULE, GUSSET PLATE ON FLOORBEAM AT FRAME 15 AND 2ND INTERCOSTAL FROM RIGHT SIDE HAS SOME SURFACE CORROSION AND APPEARS TO BE MADE OF TOO THIN OF MATERIAL AREA IS MARKED WITH BLACK PEN. REPLACED GUSSET PLATE FORWARD VESTIBULE FRAME 15 2ND INTERCOSTAL FROM RIGHT. (M)

Part: FRAME — CORRODED (GALLEY)

FORWARD VESTIBULE, FLOOR PANEL (UNDER GALLEY UNIT) HAS SOME SURFACE CORROSION IN A COUPLE SPOTS ALONG AFT EDGE. REMOVED SURFACE CORROSION FORWARD VESTIBULE AT AFT EDGE OF GALLEY ASSY FRAME 15 TREATED AND PAINTED. (M)

Part: STIFFENER — CRACKED (RT WING)

RIGHT WING TE SHROUD LOWER SKIN STIFFENER CLEATS CRACKED BETWEEN RIBS 8/9, AFT END OF STIFFENER. REPLACED BOTH CLEATS OF RT WING TE SHROUD LOWER SKIN STIFFENER, CLEATS CRACKED BETWEEN RIBS 8/9, AFT END. (M)

Part: GUSSETT — CORRODED (FUSELAGE)

FORWARD VESTIBULE, CENTER GUSSET PLATE ON THE 2ND INTERCOSTAL FROM RIGHT SIDE IS CORRODED. REPLACED FORWARD VESTIBULE GUSSET PLATE CENTER ON NR 2 INTERCOSTAL FROM RIGHT. (M)

Part: FLOOR STRIP — CORRODED (CABIN)

FLOOR STRIPS FOR FORWARD CABIN BULKHEADS NEED CLEANED, CORROSION REMOVED, PAINTED, ETC. CLEANED, REMOVED CORROSION ALODINED, PRIMED, PAINTED, AND REATTACHED PHONELLIC STRIPS. (M)

Part: FLOORBEAM — CORRODED (FRAME 15)

FORWARD VESTIBULE FLOORBEAM AT FRAME 15 HAS A SMALL SPOT OF CORROSION APPROX 5 INCHES OUTBOARD OF 3RD INTERCOSTAL FROM LEFT SIDE, INLINE WITH CLOSET WALL AT C/PIT ENTRANCE AND IS MARKED WITH BLACK PEN. BLENDED AREA TO LIMITS AND SURFACE TREATMENT AS PER BAE SRM. (M)

Part: FRAME — CORRODED (FRAME 18)

FORWARD VESTIBULE, FORWARD END OF SEAT RAIL, INBOARD RIGHT FLOORBEAM AT FRAME 18 IS CORRODED. REMOVED SURFACE CORROSION FORWARD VESTIBULE FRAME 18 INBOARD SEAT RAIL RIGHT SIDE TREATED, PRIMED AND PAINTED. (M)

Part: PLATE — WORN (NLG DOOR)

WHILE CMP/WITH SSI 52-82-101-WEAR WAS DICV'D ON BOTTOM AFT CORNERS OF NOSE GEAR DOORS WHERE THEY ABUT TAB ON SPADE DOOR. TAB IS ALSO WORN. MANUFACTURED 2 BUTMENT PLATES FOR LT/RT NOSEGEAR DOORS IAW BAE DRAWING HC528H0161. INSTALLED LT/RT NOSEGEAR DOOR ABUTMENT PLATES IAW AIR WISC/BAE STD PRACTICES OF SRM. SEE ADDITIONAL W/C FOR REPLACEMENT OF 'STOP'. (M)

Part: BRACKET — CORRODED (CABIN SEAT)

FORWARD VESTIBULE, STEW SEAT MOUNT BRACKETS ON 2ND AND 3RD INTERCOSTALS FROM LEFT SIDE ARE LIGHTLY CORRODED. REMOVED CORROSION TREATED PRIMED AND PAINTED FORWARD F/A SEAT MOUNT BRACKETS. (M)

Part: INTERCOSTAL — CRACKED (FRAME 41-43)

AFT VEST, UNDER FLOOR INTERCOSTAL BETWEEN FRAMES 41 AND 42 IS CRACKED, CENTER INTERCOSTAL, CRACK IS APPROX 2.5 TO 3 INCHES LONG. COMPLIED WITH PATCH REPAIR IAW AIR WISC/BAE SRM STANDARD PRACTICES REF CHAPTER 51. COMPLIED WITH ALODINE, PRIMER AND PAINTING. (M)

Part: BRACKET — CRACKED (FRAME 32)

MLG DOOR UPLOCK COVER BRACKET ON THE RIGHT SIDE OF WEB AT FRAME 32 IN MLG BAY IS CRACKED. REPLACED SAID BRACKET P/N HC536H0826-000U. (M)

Part: SPRING — FAILED (TRASH BIN)

FORWARD VESTIBULE TRASH BIN DOOR ASSY, NEEDS CLEANED. ANGLE REPAIR, DOOR SPRINGS, ETC. REMOVED AND REPLACED SPRINGS. REPAIRED ANGLE AND CLEANED AND INSPECTED. (M)

Part: RIB — CRACKED (NR 2 PYLON)

NR 2 PYLON BOX STRUCTURE HAS A CRACK IN THE LOWER OUTBOARD FLANGE OF RIB NR 5 THAT IS APPROX .5 INCH LONG. NR 2 PYLON CRACK OF APPROX .5 INCH LONG IS ACCEPTABLE AND HAS BEEN REPORTED TO BAE RDO PER P/C HC646H9018. GENERATED W/C FOR REINSPECTION. (M)

Part: BRACKET — CRACKED (NR 3 ENGINE)

NR 3 ENGINE NOSE COWL INBOARD FIREBOTTLE HAS ONE ATTACH BRACKET MOUNTED TO FIREWALL THAT IS CRACKED BADLY. REMOVED NR 3 NOSE AND TRANSFERRED DISCREPANCY TO W/C. (M)

Part: SILL — CORRODED (PAX DOOR)

PASSENGER DOOR SILL PLATE CORRODED FRAME 15. REMOVED AND REPLACED FORWARD PAX DOOR SILL PLATE. (M)

Part: BRACKET — CRACKED (FRAME 32)

STRUCTURAL INSPECTION MLG BAY, POS N/A WEB AT FRAME 32, DETAILED VISUAL INSPECTION. PERFORMED DV ON WEB AT FRAME 32 IN LEFT AND RIGHT MLG BAY. FOUND CRACKED BRACKET RT MLG DOOR UPLOCK CVR, FOUND MINOR NICKS SURFACE WEB.

Part: WIRE — CHAFED (NR 1 FIRE BOTTLE)

NR 1 MOTOR OUTBOARD FIRE BOTTLE DISCHARGE INDICATION WIRES ARE CHAFED, BOTTLE NEEDS CHANGED. CHANGED NR 1 OUTBOARD FIRE BOTTLE DUE TO CHAFED WIRES. S/N OFF CK6766M, S/N ON CK6767M. (M)

Part: BRACKET — CRACKED (NR 1 FIRE BOTTLE)

NR 1 MOTOR INBOARD FIRE BOTTLE BRACKET CRACKED AT STRAP ATTACHMENT AREA. REPLACED CRACKED FIRE BOTTLE BRACKET INBOARD ON NR 1 ENGINE. (M)

Part: SLIDE — DAMAGED (NR 1)

NR 1 ESCAPE SLIDE PACK BOARD CRACKED AT HINGE POINT (APPROX 5 INCHES) MRR NEEDS FILE. REMOVED AND REPLACED NR 1 SLIDE ASSY PERFORMED COVER PULL TEST AND FOUND SERVICEABLE. UPDATED BATTERY EFF CHECKED FOR INSTALLED SLIDE S/N 0238. DOOR ARM CHECK C/W. NO DEFECTS NOTED, S/N OFF 0415, S/N ON 0238. (M)

Part: SLIDE — DEPLOYED (CABIN)

FUNCTION CHECK SLIDE (BELOW) AND THEN REMOVE FOR DETAILED INSPECTION REF CHECK LS. REPORT TASK ON STEP 543 IN COMPUTER. AT INSTALLATION C/W COVER LATCH PULL CHECK COMPLIED WITH FUNCTION CHECK NR 3 POS (S/N 0389) SLIDE ASSEMBLY AND REMOVED FOR DETLD INSPECTION C/W CHECKLIST 5-60-36-06 ETC.

Part: GIRT BAR — CORRODED (PAX DOOR)

AFT PAX DOOR ESCAPE SLIDE GIRT BAR HAS CORROSION AROUND THE SLIDE GIRT EXTENSION BOLT HOLES. REPLACED GIRT BAR ASSEMBLY IAS BAE MM. ALSO, SEE W/CARD 8089 6/70 FOR SILE ASSY REPLACEMENT.

Part: FRAME — CRACKED (FUSELAGE)

CRACK IN LOWER RIGHT CORNER OF UPPER FRAME (REF SR/53-40-31 PAGE 3 ITEM 14) IN AIRBRAKE BAY, CIRCLED IN RED. REPAIRED CRACK IN FRAME PER REPAIR DRAWING, DJH/RJO749-96. ATTACHED AND FAX NR DS/W/TS/28840/97.

Part: CONTROL CABLE — CORRODED (LT AILERON)

LEFT AILERON INTERCONNECT CABLE CORRODED AT OUTBOARD END. REMOVED AND REPLACED LEFT AILERON INTERCONNECT SHEATHED CABLE TENSIONED, SAFETIED AND COMPLIED WITH AILERON SYSTEM FUNCTIONAL AND TRAVEL CHECKS IAW BAE MM. (M)

Part: CABLES — CORRODED (RT AILERON)

BOTH RIGHT AILERON MAIN CIRCUIT CONTROL CABLES ARE CORRODED AT WING ROOT PULLEYS. REMOVED AND REPLACED BOTH RIGHT MAIN AILERON CENTER CABLES, TENSIONED, SAFETIED AND COMPLIED WITH AILERON SYSTEM FUNCTIONAL AND TRAVEL CHECK IAW BAE MM.

Part: CONTROL CABLE — CORRODED (LT AILERON)

LEFT MAIN AILERON CABLES ARE CORRODED AT THE FRA NR 24-25 PULLEY JUST PRIOR TO CABLE ENTERING THE FUSELAGE. REMOVED AND REPLACED BOTH LEFT MAIN AILERON CENTER CABLES, TENSIONED, SAFETIED, AND COMPLIED WITH AILERON SYSTEM FUNCTIONAL AND TRAVEL CHECKS IAW BAE MM. (M)

Part: CABLES — CORRODED (LT/RT AILERON)

BOTH AILERON INTERCONNECT CABLES ARE CORRDED AT WING ROOT PULLEYS. REMOVED AND REPAIRED BOTH CENTER AILERON INTERCONNECT CABLES, TENSIONED, SAFETIED, AND COMPLIED WITH AILERON SYSTEM FUNCTIONAL AND TRAVEL CHECKS IAW BAE MM. (M)

Part: DOWNLOCK SWITCH — FAILED (NLG)

ORD - FLT 541 - EMERGENCY NLG DOWNLOCK INDICATOR LIGHT INOPERABLE. REMOVED AND REPLACED BACK-UP NLG DOWNLOCK INDICATOR SWITCH.

Part: NAV SYSTEM — MALFUNCTIONED (NR 1)

NR 1 NAV AND TACAN INOP, NR 2 OK. RE-RACKED NR 1 LEDEX RELAY, COMPLIED WITH 4OIL RAMP TEST OF NR 1 NAV SYSTEM. NO DEFECTS NOTED. COMPLIED WITH SELF TEST OF NR 1 TACAN SYSTEM. NO DEFECTS NOTED. (M)

Part: OIL LINE — LEAKING (NR 4 ENGINE)

ORD - FLT 505 - NR 4 ENGINE SECURED DUE TO DECREASING OIL QUANTITY AND OIL PRESSURE. CORRECTIVE ACTION: TIGHTENED AFT OIL LINE TO THE FUEL/OIL HEAT EXCHANGER.

Part: AIR DIST — ODOR (CABIN)

ORD - PREVIOUS CREW REPORTS VISUAL SMOKE AND OIL SMELL IN CABIN DURING IN-FLIGHT PORTION OF THE FLIGHT. GROUND RAN ENGINES AND APU, TEST FLIGHT C/W. NO DUPLICATE.

Part: SEAL RETAINER — BROKEN (RT TE FLAPS)

AT 295 KTS, THERE IS A NOTICEABLE AIRFRAME VIBRATION FROM LEFT SIDE OF AIRCRAFT AT ROW 10. VIBRATION REDUCES AS SPEED DECREASES AND GOES AWAY BELOW 265 KTS. FOUND RT FLAP SEAL RETAINER BROKEN, REPLACED. FOUND SEAL LOOSE ON PANELS 281CT AND 282CT. SECURED SEALS.

Part: LIGHTS — INOPERATIVE (CABIN)

EMERGENCY LIGHT INOP IN LAVATORY. RESET SWITCHES, OPS CHECKED GOOD.

Part: JO-BOLTS — LOOSE (CTR TANK RIB)

LOOSE JO-BOLTS REQUIRE REPLACEMENT IN CENTER TANK RIB 0 AND RIB 2 LEFT AND RIGHT. REPLACED JO-BOLTS.

Part: POPPET VALVE — DIRTY (NR 1 ENGINE)

ENGINE 1 DOES NOT MAKE TAKEOFF POWER. CLEANED NR 1 ENGINE POPPET VALVES SUCCESSFULLY GROUND RAN NR 1 ENGINE TO ACTIVE TAKEOFF POWER.

Part: CONTROL MECH — MALFUNCTIONED (SPEED BRAKES)

ATW - FLT 265 - UNCOMMANDED OPENING OF AIR BRAKE ON APPROACH INTO ATW. ADJUSTED AND TESTED COMMAND AND FEED BACK POTENTIOMETER IAW 27-63-00, PAGE 501, PARAGRAPH 1C. CLEANED AND ADJUSTED LEVER FRICTION DAMPENERS AND TESTED IAW 27-63-00, PAGE 509. TESTED SENSOR IAW PAGE 504P.2ABCD. OK FOR SERVICE.

Part: SKIN — CRACKED (NR 3 PYLON)

NR 3 ENGINE PYLON - PRE-COOLER DUCT RIVETS LOOSE AND SKIN CRACKED AFT OF SHOULDER COWL. REMOVED DUCT ASSY. REPAIRED CRACK IAW PS-1 REPAIR DRAWING NR HC711H9006, REINSTALLED DUCT ASSY.

Part: BOLT — CRACKED (NR 2 PYLON)

NR 2 ENGINE YOKE TO PYLON BOLT, LEFT TOP TO BE REMOVED FOR MAINTENANCE INSPECTION OF CRACK INDICATION ON THREAD RUN-OUT AREA. REF: P/N HC712H0041-000. SSI 54-00-123. CARD NR 268. REPLACED NR 2 ENGINE YOKE TO PYLON BOLT AT LEFT TOP POSITION.

Part: BOLT — CRACKED (NR 3 PYLON)

NR 3 PYLON - LOWER RT BOLT, P/N HC574H0036-20D, REQUIRES REMOVAL FOR VERIFICATION OF CRACK INDICATIONS, REF SSI 57-20-174. REMOVED AND REPLACED RT LOWER NR 3 PYLON BOLT, P/N HC574H0036-200, IAW A.M.M.

Part: SKIN — DAMAGED (PASSENGER DOOR)

LEFT REAR PASSENGER DOOR OUTER SKIN HAS A 1 INCH LONG SCRAPE AT THE BOTTOM AFT CORNER (WITH DOOR CLOSED). INSPECTED SCRAPED AREA AT LOWER AFT CORNER OF REAR PASSENGER DOOR. DAMAGED AREA FOUND TO BE MINOR. TREATED DAMAGED AREA AND REPAINTED.

Part: BOLT — FAILED (NR 4 TE FLAP)

BY MT AND PT METHODS OF NDT, FOUND UPPER CARRIAGE-TO-LEVER PIN ASSY CRACKED IN THE HEAD-TO-SHANK RADIUS. (NR 4 RT CARRIAGE.) REF: SSI 57-55-129. REMOVED AND REPLACED OUTBOARD BOLT ON NR 4 RT FLAP TRACK CARRIAGE (UPPER CARRIAGE-TO-LEVER PIN).

Part: RIBS — BROKEN (RUDDER)

RUDDER RIBS 2 AND 3 ARE CRACKED AND BROKEN. REPAIRED RIBS 2 AND 3 ON BOTTOM OF RUDDER IAW 146 SRM 55-40-11 AND SRM 51-71-11 STANDARD PRACTICES.

Part: SKIN — CHAFED (RT WING)

RIGHT FUSELAGE IS CHAFED WHERE UNDER WING PANEL SEALS RUB ON FUSELAGE. LOCATED BETWEEN FRAME 32 AND FRAME 33A ABOVE CABIN WINDOWS. SSI NR 53-20-159D. INSPECTED AND BLENDED OUT, ALCROMED AND REPRIMED. PERFORMED EO E92/045/653. ORIGINAL REVISION GENERATED WORK CARD FOR CHAFE OVER FRAME 33 THAT RUNS FORE AND AFT AT .003 INCH FOR 7.50 INCHES (REF W/C 6014) AND REF W/C 6016 FOR ND.

Part: PIN — FAILED (TE FLAPS)

LEFT NR 3 LOWER FLAP TRACK CARRIAGE TO SCREW JACK TRUNNION PIN FAILED N.D.T. NOTE: SEVERAL INDICATIONS IN PIN-TO-FLANGE RADIUS. REMOVED AND REPLACED LEFT NR 3 LOWER FLAP TRACK CARRIAGE TO SCREW JACK TRUNNION PIN IAW A.M.M.

Part: ACT BOLT — DAMAGED (RUDDER)

AFT LOWER RUDDER ACTUATOR BOLT IS PITTED AND SHANK IS SCORED. SSI 55-40-105. REMOVED AND REPLACED AFT LOWER RUDDER ACTUATOR BOLT IAW AMM.

Part: ACT BOLT — DAMAGED (RUDDER)

AFT UPPER RUDDER ACTUATOR BOLT IS GALLED AND SCORED. SSI 55-40-105 (INSTALLED BAD BOLT TO FOM). REMOVED AND REPLACED BOLT AND SAFTIED.

Part: BOLT — DAMAGED (NR 4 FLAP TRACK)

LEFT NR 4 FLAP TRACK CROSS HEAD TO LINK CAP BOLT IS BAD AND NEEDS REPLACED. FAILED INSPECTION CHECK. INSTALLED NEW LEFT NR 4 FLAP TRACK CROSS HEAD TO LIND CAP BOLT AS REQUIRED.

Part: RIB — LOOSE (RUDDER)

MISSING AND LOOSE RIVETS IN RUDDER BOTTOM RIB (1). REMOVED AND REPLACED NR 1 RIB ON BOTTOM OF RUDDER IAW BAE 146 SRM AND REPAIR INSTRUCTION HC554H9005.

Part: BOLT — LOOSE (LT WING)

ATW - LEFT WING REAR SPAR ROOT JOINT FITTING AT RIB 2, BOLT 'A' IS LOOSE AND LEAKING. REMOVED AND REPLACED BOLT 'A' AT LEFT WING REAR SPAR JOINT FITTING. BOLT HEAD HAS BEEN SEALED AT 1440. W/C GENERATED FOR LEAK CHECK W/C 5020.

Part: FUEL MANIFOLD — CRACKED (NR 4 ENGINE)

ATW - NR 4 ENGINE, LEFT FUEL MANIFOLD CRACKED, FOUND ON INSPECTION. REPLACED FUEL MANIFOLD.

Part: VALVE ASSY — MALFUNCTION (NR 3 ENG PUMP)

NR 3 ENGINE DRIVEN HYDRAULIC PUMP CAN NOT BE SHUTOFF. REPLACED THE NR 3 ENGINE DRIVE PUMP SHUTOFF VALVE. (W)