N611AW

Part: SKIN — LIGHTNING STRIKE (FUSELAGE)

DAMAGE NOTED ON LEFT SIDE OF FUSELAGE DURING LIGHTNING STRIKE INSPECTION. EXIT BURN MARK LOCATED 8 INCHES AFT OF FRAME 19C BETWEEN STRINGER 21 AND 22 AT CENTER AND APPROX .375 INCH IN DIAMETER BY .010 INCHES DEPTH. MAINTENANCE BLENDED DAMAGE TO A SMOOTH MIRROR FINISH TO A DEPTH OF .010 INCH PER BAE SYSTEMS FAX BARA/AVR/6534/03-DC ET PROVED CRACK FREE. (M)

Part: CONDUIT — DAMAGED (FUSELAGE)

FLANGED CONDUIT P/N HC535B0285-000 IS KINKED AND HAS TWO HOLES. MAINTENANCE WELDED CONDUIT IAW BAE FAX BARA/AVR/6411/03-DC. (M)

Part: ODOR — DETECTED (FWD GALLEY) · airframe 26,929 hrs · 35,402 cycles

AFTER TAKEOFF, FLIGHT ATTENDANT REPORTED SMELL IN FWD GALLEY AREA, GALLEY LOAD SHED, SMELL DISSIPATED. MAINTENANCE INSPECTED FWD CABIN AND GALLEY AREA, RAN ENGINES, USED ENGINE AIR WITH GALLEY POWER ON, NO SMELL NOTED.

Part: COMPUTER — MALFUNCTIONED (LE FLAPS) · airframe 25,804 hrs · 34,144 cycles

AFTER TAKEOFF, FLAPS RETRACTED TO BETWEEN 0-18 DEGREES AND THEN STOPPED. AFTER CHECKLIST, RETRACTED TO 18 DEGREES RETURNED TO LANDING FLAP FAULT ILLUMINATED. MAINTENANCE RESET C/B L9, D24, E12, RERACKED FLAP COMPUTER, CLEARED FLAP FAULT. OP CHECKED GOOD.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 25,719 hrs · 34,050 cycles

THREE LIGHTS IN FRONT OF PASSENGER CABIN NOT ILLUMINATING. MAINTENANCE CLEANED AND RESECURED CONNECTOR PLUG TO EMERGENCY POWER SUPPLY ABOVE ROW 7, OPS CHECKED GOOD.

Part: PROXIMITY SENSOR — MALFUNCTIONED (MLG) · airframe 25,473 hrs · 33,798 cycles

UNSAFE RIGHT MLG INTRANSIT LIGHT ON WITH GEAR SELECTED UP ALSO ASSOCIATED GEAR HANDLE LIGHT ON. MAINTENANCE CLEANED DOOR UPLOCK PROXY SENSORS AND GEAR PROXY SENSORS, PERFORMED GEAR SWING, 3 CYCLES, ALL INDICATIONS NORMAL.

Part: FIRE BOTTLE — DAMAGED (ENGINE)

ENGINE NOSE COWL WO NR BY8402 HAD FIRE BOTTLE CL978M HAS WORN THREADS ON JUNCTION BOX AND CONTROL HEAD. REM AND REPLACED FIRE BOTTLE. (M)

Part: MASK — CRACKED (CABIN)

FORWARD AFT FACING F/A OXYGEN BOTTLE, MASK FACE PIECE CRACKED. REPLACED OXYGEN MASK, OPS CHECKS OK. (M)

Part: VALVE — FAILED (CABIN)

CABIN OXYGEN SYSTEM FAILED LEAK CHECK. TROUBLESHOOT SYSTEM. REPLACED PAX ISO VLV, 5 QUICK DISC (OUTLETS), 4 RT BOX ASSY. SEE W/C'S FOR PARTS CHANGED, SYSTEM LEAK CHECKS OK. (M)

Part: OXYGEN BOX — LEAKING (CABIN)

FOUND OXYGEN BOX AT 4 RT LEAKING THROUGH MASK WITH PIN INSTALLED. REPLACED OXYGEN BOX ASSY, OPS AND LEAK CHECKS OK.

Part: MASK — TORN (ROW 9)

OXYGEN MASK AT 9 RT FACE PIECE TORN. REPLACED OXYGEN MASK 9 RT, OPS AND LEAK CHECKS OK. (M)

Part: OUTLETS — LEAKING (CABIN)

FOUND OXYGEN OUTLETS AT RT 6, 14, 17, 20, AND 21 LEAKING. REPLACED OUTLETS AT RT 6, 14, 17, 20, AND 21. LEAK CHECK OK. (M)

Part: MANIFOLD — LEAKING (CABIN)

FOUND 4 RT OXYGEN BOX, 2 MASK LEAKING WITH PINS INSTALLED, OXYGEN MASK FACE PIECE TORN. REPLACED 4 RIGHT OXYGEN MANIFOLD, OPS AND LEAK CHECKS OK. REPLACED MASK ASSY, LEAK AND OPS CHECKS OK. (M)

Part: DOOR — CHAFED (NR 3 ENG COWL)

NR 3 ENGINE INBOARD FAN DOOR LOWER SPLITTER AREA, 2ND STIFFENER FROM FORWARD CHAFED. REPLACED THE NR 3 ENGINE INBOARD FAN DOOR LOWER SPLITTER AREA, 2ND STIFFENER FROM FORWARD. (M)

Part: STIFFENER — CRACKED (LT WING)

LT WING TOP SKIN TE SHROUD OUTBOARD STIFFENER CRACKED AT FORWARD END BETWEEN RIBS 8/9. REPAIRED ABOVE STIFFENER PER BAE FAX JM/RJO317/97 USING 2 024T3 .050. (M)

Part: DOOR — DAMAGED (NR 1 ENGINE COWL)

NR 1 EIGNE INBOARD REAR COWL DOOR HAS A HOLE WORN THROUGH THE TOP 3RD RIB BACK FROM THE FRONT CORNER OF THE DOOR. REPLACED THE TOP THIRD RIB FROM THE FRONT EDGE OF THE NR 1 INBOARD REAR COWL DOOR SPLITTER. (M)

Part: INTERCOSTAL — CRACKED (AFT AIRSTAIR)

AFT AIRSTAIR OUTBOARD RAIL INTERCOSTAL CRACK AT FLOOR, AFT END. REMOVED AND REPLACED AFT AIRSTAIR OUTBOARD RAIL INTERCOSTAL AT AFT END OF RAIL. WORK DONE IAW BAE MM 51-00-00. (M)

Part: TREAD PLATE — CORRODED (LEFT)

LEFT FORWARD TREAD PLATE (E804) HAS CORROSION ON INNER SURFACE. REMOVED CORROSION ON LT FORWARD TREAD PLATE 9E804). (M)

Part: BRACKET — CRACKED (LT WING)

LEFT WING HYD LINE CLAMP BRACKET CRACKED AT FALSE SPAR, RIB NR 3. REMOVED AND REPLACED ABOVE BRACKET. (M)

Part: FLOORBEAM — CRACKED (FRAME 29)

CABIN PRESSURE FLOORBEAM NR 13 CRACKED AT FRAME 29. REPAIRED PER DRAWING HC536H9211 AND FAX REF DJR/RJO207-97.

Part: FLOORBEAM — CRACKED (FRAME 29)

CABIN PRESS FLOORBEAMS NR 9 CRACKED AT FRAME 29. REPAIRED PER DRAWING HC536H9211 AND FAX REF DJR/RJO207-97. (M)

Part: FLOORBEAM — CRACKED (FRAME 29)

CABIN PRESS FLOORBEAM NR 15 CRACKED AT FRAME 29, RIGHT INBOARD SEAT RAIL. REPAIRED PER DRAWING HC536H9211 AND FAX REF DJR/RJO207-97. (M)

Part: COWL — CRACKED (NR 2 ENGINE)

NR 2 ENGINE PYLON SHOULDER COWL HAS CRACKED SKIN BETWEEN THE BIG HYD PIPE AND THE DRAIN TUBE. REPAIRED ABOVE CRACK USING .040 TA 2 PER FAX KG/0603-91 AND SRM. (M)

Part: FLOORBEAM — CRACKED (FRAME 29)

CABIN PRESS FLOORBEAM NR 19 (RIGHT OUTBOARD SEAT RAIL) CRACKED AT FRAME 29. REPAIRED PER FAX REF DJR/RJO207-97 AND REPAIR DRAWING HC536H9211. (M)

Part: FLOORBEAM — CRACKED (FRAME 29)

CABIN PRESS FLOORBEAM NR 3 CRACKED AT FRAME 29, LT OUTBOARD SEAT RAIL. REPAIRED PER DRAWING HC536H9211 AND FAX REF DJR/RJO207-97. (M)

Part: FLOORBEAM — CRACKED (FRAME 29)

CABIN PRESS FLOORBEAM NR 3 CRACKED AT FRAME 29, LEFT OUTBOARD SEAT RAIL. REPAIRED PER DRAWING HC536H9211 AND FAX REF DJR/RJO207-97. (M)

Part: STEP — CORRODED (AFT AIRSTAIRS)

AFT AIRSTAIRS, SECOND FROM THE TOP STEP CORRODED. REPLACED STEP.

Part: STRUCTURE — CORRODED (GALLEY)

FOUND CORROSION AROUND MOUNTING HOLES FOR GALLEY. REMOVED CORROSION, TREATED, PRIMED AND PAINTED APPLICABLE AREAS AROUND GALLEY MOUNTING HOLES. (M)

Part: RIVETS — FAILED (FRAME 26)

CABIN FLOOR OUTBOARD SUPPORT ANGLE HAS 2 POPPED RIVETS AT FRAME 26 (RIGHT SIDE AFT OF FRAME). REPLACED RIVETS. (M)

Part: SILL — CORRODED (PAX DOOR)

PAX DOOR SILL PLATE SOME LIGHT SURFACE CORROSION, MARKED W/DOT. REMOVED CORROSION, TREATED, PRIMED AND PAINTED APPLICABLE AREA. (M)

Part: DOOR — CHAFED (NR 3 ENG COWL)

NR 3 ENGINE INBOARD FAN DOOR INNER TITANIUM DISHING CHAFED THROUGH. REPAIRED CHAGED AREA OF NR 3 ENGINE INBOARD FAN DOOR INNER SKIN IAW 146 RIL HC711H9047. (M)

Part: DOOR — CHAFED (NR 4 ENG COWL)

NR 4 ENGINE INBOARD FAN DOOR INNER TITANIUM SKIN CHAFED THROUGH JUST ABOVE DISHING AREA. REPAIRED CHAFED AREA IAW RIL HC711H9047. (M)

Part: STAIR — CORRODED (AFT AIRSTAIR)

AFT AIRSTAIRS, SECOND FROM THE TOP STEP CORRODED. REPLACED STEP.

Part: BRACKET — CRACKED (RT WING)

RIGHT WING TE HYD CLAMP BRACKET CRACKED AT FALSE SPAR, RIB 6. ALSO, HYD CLAMP LOOSE OUTBOARD OF RIB 6. REPLACED ONE RIGHT WING TRAILING EDGE HYD CLAMP BRACKET (P/N HC932HO178-003) AT FALSE SPAR, RIB 6. TIGHTENED BOLTS SECURING HYD CLAMP OUTBOARD OF RIB 6. (M)

Part: STRUCTURE — WORN (NR 3 PYLON)

NR 3 PYLON SHOULDER COWL AFT LORD MOUNT ATTACH HOLES WORN AND SLOPPY AT SHOULDER COWL STRUCTURE. REPAIR PER RI HC710H9033. REPAIRED NR 3 PYLON SHOULDER COWL AFT LORD MOUNT ATTACH STRUCTURE HOLES IAW BAE REPAIR DRAWING HC710H9003. (M)

Part: CONTROL CABLE — CORRODED (AILERONS)

BOTH CENTER AILERON INTERCONNECT CABLES ARE CORRODED. REMOVED AND REPLACED BOTH CENTER AILERON INTERCONNECT CABLES, GENERATED NEW WC FOR TRAVEL CHECKS AND FREEDOM OF MOVEMENT. (M)

Part: ANGLE — CRACKED (RT WING)

RIGHT WING TE LOWER SKIN, INBOARD STIFFENER BETWEEN RIBS 8/9 TAG ANGLE CRACKED AFT END OF STIFFENER. REPLACED SAID TAG ANGLE AND FOUND SERVICEABLE. (M)

Part: TRIM STRIP — CORRODED (FRAME 18)

FRAME 18 TRIM STRIP FOR UNDER RIGHT BULKHEAD BADLY CORRODED, REPLACED. REMOVED AND REPLACED FRAME 18 TRIM STRIP.

Part: SLIDE — CRACKED (LT CABIN)

LEFT FORWARD EVAC SLIDE PACK BOARD CRACKED AT TOP MOUNT PP PIN. REMOVED SLIDE ASSY AND PLACED ON W/O, P/N 31050-105, S/N 0093, REF W/C 8012 FOR INSTALLATION. (M)

Part: ENGINE — FAILED (NR 1)

SBA - FLT 586 - NR 1 ENGINE FAILED ON CLIMB-OUT FROM SBA TO DEN - DIVERTED TO LAS. UNDER FURTHER INVESTIGATION.

Part: ENGINE — FAILED (NR 1)

NR 1 ENGINE FAILED ON CLIMB-OUT FROM SBA TO DEN. DIVERTED TO LAS. REMOVED AND REPLACED NR 1 ENGINE IAW AWAC ENDING CHANGE CHECKLIST AND AIRCRAFT MM. (M)

Part: VALVE — FAILED (NR 3 COWL)

NR 3 NOSE COWL FLOW CONTROL VALVE WAS FOUND TO HAVE A RIVET IN THE FAIL/SAFE MODE TO BE WORN EXCESSIVELY. REPLACED VALVE. (M)

Part: FIRE WIRE — CHAFED (NR 2 ENGINE)

ATW - NR 2 ENGINE INBOARD FIRE EXTINGUISHER WIRES ARE CHAFED BY NOSE COWL DISCONNECT. REPLACED WIRES 2WB170 AND 2WB173. SEE ENGINE CHANGE CHECK LIST FOR TEST OF FIRE EXTINGUISHING SYSTEM. `

Part: STIFFENER — CRACKED (RT WING)

ATW - RIGHT WING UPPER SHROUD SKIN OUTER STIFFENER CRACKED AT FORWARD FASTENER (BETWEEN RIBS 8 AND 9). REPAIRED TRAILING EDGE STIFFENER IAW SRM AND AVRO FAX JM/RJ0317/97.

Part: SKIN — CRACKED (LT WING)

LEFT WING TOP TRAILING EDGE SHROUD HAS A STIFFENER WITH A CRACK AT FORWARD END APPROXIMATELY .75 INCH LONG LOCATED IN AREA BETWEEN WING RIBS 5 AND 6. REPAIRED TRAILING EDGE STIFFENER IAW SRM AND AVRO FAX JM/RJ0317/97.

Part: STIFFENER — CRACKED (LT WING)

ATW - LEFT WING TOP TRAILING EDGE SHROUD HAS A STIFFENER WITH A CRACK AT FORWARD END APPROXIMATELY 1.25 INCHES LONG LOCATED IN AREA BETWEEN WING RIBS 4 AND 5. REPAIRED TRAILING EDGE STIFFENER IAW SRM AND AVRO FAX JM/RJ0317/97.

Part: STIFFENER — CRACKED (LT WING)

ATW - LEFT WING TOP TRAILING EDGE SHROUD HAS A STIFFENER WITH A CRACK AT ITS FORWARD END APPROXIMATELY 1 INCH LONG. LOCATED IN AREA BETWEEN WING RIBS 7 AND 8. REPAIRED TRAILING EDGE STIFFENER IAW SRM AND AVRO FAX JM/RJ0317/97.

Part: STIFFENER — CRACKED (LT WING)

ATW - LEFT WING TOP TRAILING EDGE SHROUD HAS A STIFFENER WITH A CRACK AT ITS FORWARD END APPROXIMATELY 1 INCH LONG LOCATED IN AREA BETWEEN WING RIBS 8 AND 9. REPAIRED TRAILING EDGE STIFFENER IAW SRM AND AVRO FAX JM/RJ0317/97.

Part: STIFFENER — CRACKED (RT WING)

ATW - RIGHT WING UPPER SHROUD SKIN STIFFENER CRACKED AT FORWARD FASTENER (BETWEEN RIBS 7 AND 8). REPAIRED TRAILING EDGE STIFFENER IAW SRM AND AVRO FAX JM/RJ0317/97.

Part: RIB — DAMAGED (RT WING)

ATW - RT WING JO-BOLT RIB NR 2 USED 3 OVERSIZED FASTENERS DUE TO TOOLING MARKS REAMING OUTBOARD. RT WING RIB NR 2 STRINGERS 2A, 7A; RT INBOARD RIB NR 2, STRINGERS 7F: HC571H9003, PC/RJ0652-95, DJR/RJ0634. REAMED HOLES TO OVERSIZE, SPOT FACED, COUNTERSUNK, DEBURRED, ALODINED, PRIMED, AND INSTALLED OVERSIZE FASTENERS IN RT WING RIB NR 2 OUTBOARD STRINGERS 2A, 7A AND INBOARD RIB NR 2, STR 7F, P/BAE AVRO RIL HC571H9033 AND FAXES JM/RJ0312/97, PCR.

Part: RIB — DEFECTIVE (RT WING)

ATW - PERFORMED BAE AVRO RIL HC571H9033 TO RIGHT WING RIB ZERO AND FAXES PC/RJ0652-95 AND DJR/RJ0634-96. C/W BAE AVRO RIL HC571H9033 TO RIGHT WING RIB ZERO AND FAX ES PC/RJ0652-95 AND DJR/RJ0634-96.

Part: RIB — DEFECTIVE (LT WING)

ATW - PERFORMED BAE AVRO RIL HC571H9033 TO LEFT WING RIB ZERO AND FAXES PC/RJ0652-95 AND DJR/RJ0634-96. C/W RIL HC571H9033 AND FAXES PC/RJ0652-95 AND DJR/RJ0634-9.

Part: RIB — DAMAGED (LT WING)

ATW - LT WING RIB NR 2, 4 OVERSIZED J-BOLT FASTENERS DUE TOOLING MARKS REAMING AT POS'S . OUTBOARD STRINGERS 1A, 6A, 7A AND INBOARD STRINGERS B4A.1A A 70, 12 DIA.ALTOTNRS800, 12 DIA.HC571H9003, PC/RJ0652-95, DJR/RJ0634. REAMED HOLES TO OVERSIZE SPOT FACED, COUNTERSUNK, DEBURRED, ALODINED, PRIMED, AND INSTALLED O/S FASTENERS IN LT WING RIB NR 2 INBOARD STRINGER 4A WITH 12-800 FASTENERS AND OUTBOARD A AND 7A WITH 12-800 AND OUTBOARD 1A WITH 12-700: RIL HC571H9033; FAXES PC/RJ0652-95, DJR/RJ0634.

Part: DOOR — DAMAGED (PASSENGER COMPT)

ATW - REAR PASSENGER ENTRANCE DOOR: REAR EDGE MEMBER CRACKED AT DAMPENER MOUNT BOLT AREA (DOOR PN HC521H0901-008A, SN DH/120 RAR). REPAIRED AFT PASSENGER DOOR PER BAE REPAIR DRAWING HC521H9032 AND FAX REF NR JM/RJ0215-97. (SEE W/O BV6988 AND BV6989). REF W/C 8015 NDT.

Part: STIFFENER — CRACKED (RT WING)

ATW - RIGHT WING UPPER SHROUD SKIN STIFFENER CRACKED AT FORWARD FASTENER (BETWEEN RIBS 7 AND 8). REPAIRED T/E STIFFENER IAW SRM AND AVRO FAX JM/RJ0317/97.

Part: RIB — DEFECTIVE (LT WING CENTER)

ATW - PERFORMED BAE AVRO RIL HC571H9033 TO LEFT WING RIB NR 2 AND FAX ES PC/RJ0652-95 AND DJR/RJ0634-96. PERFORMED BAE AVRO RIL HC571H9033 INSTALLATION OF MRL FASTENERS TO RIB NR 2 CROWN FITTINGS IN LEFT WING INBD AND OTBD. REF: FAXES PC/RJO 652-95 AND DJR/RJ0634-96.

Part: RIB — DEFECTIVE (RT WING)

ATW - PERFORMED BAE AVRO RIL HC571H9033 TO RIGHT WING AND RIB NR 2 AND FAXES PC/RJ0652-95 AND DJR/RJ0634-96. INSTALLED JO-BOLTS TO RIB NR 2 PER INSTRUCTIONS STATED ABOVE.

Part: SKIN — LIGHTNING STRIKE (RT AILERON)

ATW - RIGHT AILERON TRAILING EDGE LIGHTNING STRIKE DAMAGE. REFERENCED IN AVRO FAXES DJH/RJ1163-96 AND DJR/RJ-1164-96 AND AWAC FAXES LM 209-96 AND 210-96. REQUIRES REPAIR AT NEXT HEAVY CHECK, BUT NO LATER THAN 4-30-97. REFERENCE SRM 57-60-11 PG 208 FOR REPAIR. ESTIMATE 24 MHS FOR REPAIR. REPAIRED IAW SRM 57-60-11 PG 208 AND PG 209 AND BAE FAX NR DJH.

Part: RIVETS — LOOSE (TE FLAP FAIRING)

ATW - RT NR 3 FLAP CANOE INBOARD OPERATING STRUT RIVETS LOOSE. REPLACED LOOSE RIVETS IAW FAX'S DJR/RJ0296-97 AND DJR/RJ0638-96.

Part: FIRE WIRE — CHAFED (NR 3 ENGINE)

ATW - NR 3 ENGINE PYLON AREA: FIRE WIRES CHAFED. MARKED WITH TAG. REPLACED WIRES 3WB172. SEE ENGINE CHANGE CHECK LIST FOR TEST OF FIRE EXTINGUISHING AND INDICATION.

Part: MANIFOLD — DEFECTIVE (NR 3 ENGINE)

NR 3 ENGINE OUTBOARD FUEL MANIFOLD SHOWED DEFECTS DURING THE ET CHECK WITH SLIGHT SOOTING INSIDE THE COWL. REPLACED MANIFOLD ASSEMBLY. (M)

Part: SLIDE — BROKEN (PAX DOOR)

LEFT FORWARD PAX DOOR EVAC SLIDE BACKBOARD IS BROKEN. REPLACED THE SLIDE.

Part: STRUCTURE — WORN (VERT STAB)

VERTICAL STABILIZER LEADING EDGE, BOTH LEFT AND RIGHT DE-ICE SUPPLY DUCT WEARING INTO AUXILLIARY STRUCTURE. REMOVED DUCTS AND REPAIRED AUX STRUCTURE AT VERTICLE STAB RIB 1 AREA IAW AVRO FAX DJR/RJ0930-96. NEW W/C GENERATED FOR DUCT INSTALLATION.

Part: SEAT RAIL — CORRODED (CABIN)

FORWARD LEFT SEAT RAIL IS CORRODED OUTBOARD SIDE FRAME 18 TO FRAME 19A, REPLACEMENT REQUIRED. REMOVED AND REPLACED FORWARD LEFT OUTBOARD SEAT RAIL PER A/C SRM STANDARD PRACTICES.

Part: BOLTS — CORRODED (VERT STAB)

VERTICAL STABILIZER TRAILING EDGE; TOP AND CENTER HINGE BOLTS HAVE INDICATIONS OF CORROSION. REMOVED FOR DV. CORRECTIVE ACTION: REMOVED, CLEANED, AND INSTALLED VERTICAL STABILIZER TO RUDDER, TOP, AND CENTER HINGE BOLTS. NO CORROSION NOTED ON BOLTS.

Part: PIN — CRACKED (NR 2 TE FLAP)

LEFT NR 2 FLAP TRACK CROSSHEAD PIN IS CRACKED INBOARD SIDE. INSTALLED A NEW CROSSHEAD PIN.

Part: BOLT — CRACKED (NR 2 TE FLAP TAB)

LEFT NR 2 FLAP TAB CROSSHEAD BOLT HAS CRACK INDS IN UNDER CUT OF BOLT. INSTALLED NEW CROSSHEAD BOLT.

Part: GUSSET — CORRODED (FUSELAGE)

GUSSET PLATE ON FRAME 18 IS CORRODED TO LIMITS. NEEDS TO BE REPLACED. CORRECTIVE ACTION: REMOVED AND REPLACED GUSSET PLATE ON FRAME 18.

Part: GUSSET — CORRODED (FUSELAGE)

GUSSET PLATE ON FRAME 15 AFT OF GALLEY IS CORRODED TO LIMITS. NEEDS TO BE REPLACED. CORRECTIVE ACTION: REMOVED AND REPLACED GUSSET PLATE ON FRAME 15 AFT OF GALLEY.

Part: GUSSET — CORRODED (FUSELAGE)

CENTER GUSSET PLATES ON INTERCOSTALS IN FORWARD VEST AREA ARE CORRODED. NEED REPLACEMENT. CORRECTIVE ACTION: REMOVED AND REPLACED GUSSET PLATES ON CENTER INTERCOSTALS CENTER PLATES IN FORWARD VEST AREA.

Part: SUPPORT PLATES — CORRODED (AIRSTAIR)

FORWARD AIRSTAIR AFT SUPPORT PLATES BEHIND AIRSTAIR RAILS ARE CORRODED, NEED REPLACEMENT. CORRECTIVE ACTION: DOWTY MADE PART. REMOVED AND REPLACED FORWARD AIRSTAIR AFT SUPPORT PLATES.

Part: BOLT — CORRODED (SPOILER)

RT OTBD LIFT SPOILER INBD HINGE BOLT SCRAPED DUE TO CORROSION AROUND THREADS

Part: BOLT — NOT PLATED (RT SPOILER)

RIGHT INBD LIFT SPOILER AFT JACK ATTACHMENT BOLT, PLATING MISSING. CORRECTIVE ACTION: INSTALLED NEW JACK ATTACHMENT BOLT.

Part: SLIDE — FAILED TEST (CABIN)

ATW - RIGHT AFT ESCAPE SLIDE ESCAPE PATH LIGHTS FALED TO ILLUMINATE DURING A SCHEDULED SLIDE DEPLOYMENT. REPLACED SLIDE ASSY.

Part: WIRE HARNESS — FAILED (LT MLG DOOR)

UPON GEAR RETRACTION LEFT MAIN GEAR SHOWS RED UNSAFE WITH GEAR HANDLE LT ON. REMOVED AND REPLACED LEFT MLG DOOR UPLOCK SENSOR HARNESS.

Part: INTERCOSTAL — CORRODED (CABIN)

FORWARD VEST, INTERCOSTAL IN FRONT OF F/A SEAT CORRODED. REMOVED AND REPLACED INTERCOSTAL AND SUPPORT MEMBER WITH ASSOCIATED GUSSET PLATES IN FORWARD VEST FRAME 15 - FRAME 18, IN FRONT OF THE F/A SEAT IAW SRM.

Part: CABLES — CORRODED (AILERON)

AILERON INTERCONNECT CABLES CORRODED AT WING ROOT PULLEY. REMOVED AND REPLACED AILERON INTERCONNECT CABLES PER BAE 146 MM. WORK CARD GENERATED FOR AILERON DISCONNECT TO BE RESET AND INTERCONNECT CABLES TO BE RIGGED W/C 2149.

Part: STIFFENER — CRACKED (FRAME 29)

STIFFENER CRACKED AT FRAME 29 (POSITION 25.94 RT) C/W EO E95/005/653 ORIGINAL ISSUE, RT STA 25.94 ON FRAME 29.

Part: RIB — CRACKED (VERT STABILIZER)

RIGHT SIDE OF VERTICAL STABILIZER, RIB 1, STABILIZER TO FUSELAGE CLOSURE ANGLE HAS 2 INCH CRACK THROUGH FASTENER AT FORWARD EDGE OF VERTICAL STABILIZER. REPAIRED IAW BAE REPAIR DRAWING HC550H9004 AND FAX REF KW/0863-91.

Part: STIFFENER — CRACKED (FRAME 29)

ATW - STIFFENER CRACKED AT FRAME 29 (POSITION 25.94 LT). C/W EO E95/005/653. ORIGINAL ISSUE AT LT STA 25.94 ON FRAME 29.

Part: FIREWALL — CRACKED (APU BAY)

CRACKING HAS BEEN NOTED AT FORWARD FACE OF APU BAY FORWARD FIREWALL IN THE AREA OF THE EXHAUST PIPE. DEACTIVATED APU AND PLACED ON MEL. (W)

Part: MAIN GEAR — ICED UP (MLG)

BOTH MAIN GEAR INDICATED INTRANSIT AFTER MAIN GEAR RETRACTION. SUBSEQUENT EXTENSION NORMAL. REMOVED ICE FROM LANDING GEAR AREA. SWUNG GEAR SEVERAL TIMES. OPS CHECKED OK. (W)

Part: MANIFOLD — CRACKED (NR 2 ENG FUEL)

NR 2 ENGINE FIRE LIGHT ILLUMINATED. ENGINE SECURED. FOUND THE RIGHT FUEL MANIFOLD CRACKED. REPLACING BOTH FUEL MANIFOLDS. (W)

Part: VALVE — DEFECTIVE (NR 4 ENG AIR)

NR 4 ENGINE AIR VALVE INDICATES OPEN WITH SWITCH SELECTED OFF. ORD MAINTENANCE CONFIRMED VALVE IN CLOSED POSITION. DEFERRED INDICATION PER MEL. DEFERRED AND PLACARDED, SE LG PG 21354/03.