N610AW

Part: ECU — MALFUNCTIONED (TE FLAPS)

WHEN FLAPS SELECTED FOR 24-33 DEGREES ON TO ASE, FLAP FAULTS AND INOPERATIVE LIGHTS ILLUMINATED FLAPS STUCK AT 24 DEGREES AIRCRAFT RETURNED TO DEN. MAINTENANCE FOUND CODE 4 ON FLAP ECU, RESET ECU, NO FAULTS. NOTED. (M)

Part: WIRE — LOOSE (SLIDE BATTERY)

DURING SLIDE DEPLOYMENT FOR FUNCTION TEST LIGHTS CAME ON AND THEN OFF AFTER FULL DEPLOYMENT, INSPECTION FOUND WIRES PULLED OUT OF BATTERY CONNECTORS. MAINTENANCE REMOVED AND REPLACED EVACUATION SLIDE AND DISCREPANCY FORWARDED TO SLIDE SHOP. (M)

Part: PANEL — CHAFED (NR 4 PYLON)

NR 4 PYLON PANEL 481 AT LOWER FORWARD RIGHT ATTACH HOLE CHAFED BADLY FROM LOOSE AND VIBRATING SCREW. HOLE WORN EXCESSIVELY. REPAIRED PANEL IAW BARA/AVR/6361/03-D. (M)

Part: SKIN — CRACKED (WING LE)

CRACKED IN HALF ABOVE PYLON NR 2 LEADING EDGE FIXED STRUCTURE. REMOVED AND REPLACED DOUBLER, P/N HC572H1080-001. 2 INCH CRACK TO NUTPLATE. PIECE INTACT, BUT CRACKED ALL THE WAY THROUGH. CAUSE OF DAMAGE, NORMAL FATIGUE. (M)

Part: PANEL — DAMAGED (LT WING LE)

LT WING LEADING EDGE PANEL 464AT HAS SEVERAL ELONGATED HOLES. REPAIRED IAW RIL HC5459009 AND FAX BARA/AVR/6365/03-DC.

Part: SKIN — DAMAGED (LT WING LE)

LEFT WING INBOARD LEADING EDGE HAS 1 HOLE ENLARGED IN TOP SKIN ABOVE NR 2 PYLON. REPAIRED IAW RIL HC572H9066 AND FAX BARA/AVR/6362/03-DC. (M)

Part: SCREW — DAMAGED (RT WING)

RIGHT WING SHORT STALL BAR PULLING OVER CORNER MOUNT SCREWS. REPAIRED SCREWS AS REQ'D IAW AVRO FAX DJR/RJO638-98, GCB/RJ1344-94, JEN/RJ1331-94. OK FOR SERVICE IAW BAE 146 MM. (M)

Part: BRACKET — CRACKED (HYDRAULIC SYSTEM)

LEFT WING TE HYDRAULIC LINE CLAMP BRACKET CRACKED AT RIB 5. REPLACED BRACKET.

Part: BRACKET — CRACKED (LT WING)

LEFT WING TE HYD LINE CLAMP BRACKET CRACKED AT RIB 5. REPLACED BRACKET. (M)

Part: STIFFENER — CRACKED (LT WING)

LEFT WING TOP SKIN STIFFENER AFT OF REAR SPAR BETWEEN RIBS 5 AND 6 IS CRACKED AT FORWARD END. REPAIRED IAW BAE RDO DJR/RJ0630-98. REF: W/C 5035 FOR ALODINE PRIME AND PAINT.

Part: BEARING — WORN (TE FLAP TAB)

RIGHT WING INNER FLAP TAB NR 1 HINGE BEARING IS WORN. REMOVED AND REPLACED RIGHT NR 1 FLAP TAB HINGE BEARING.

Part: SKIN — DENTED (FRAME 47)

DENT LEFT FUSELAGE AT FRAME 47 BETWEEN STRINGERS 14 AND 16. REPAIRED DENT IAW BAE FAX REF DJR/RJ0620-98.

Part: STIFFENER — CRACKED (LT WING)

LEFT WING TOP WING STIFFENER AFT OF REAR SPAR BETWEEN RIBS 8 AND 9 IS CRACKED AT FORWARD ENG. REPAIRED IAW BAE RDO EJR/RJ0630-98. REF: W/C 5035 FOR ALODINE, PRIME AND PAINT.

Part: ANGLE — CRACKED (LT WING)

LEFT WING T/E, LOWER SHROUD STIFFENER, AND AFT TAG ANGLE CRACKED BETWEEN RIBS 7 AND 8. REPLACED LEFT WING T/R LOWER SHROUD STIFFENER AND AFT TAG ANGLE BETWEEN RIBS 7 AND 8.

Part: FLOOR — BROKEN (CARGO COMPT)

NR 7 LEFT BIN FLOOR SOFT. REPAIRED COMPOSITE STRUCTURE IAW DRAWING AW-25-20-9804-06 OF PS-1.

Part: FLOOR — BROKEN (CARGO COMPT)

NR 5 RIGHT BIN FLOOR NEEDS OVERLAY. REPAIRED COMPOSITE STRUCTURE IAW DRAWING AW-25-20-9804-6 OF PS-1.

Part: FLOOR — BROKEN (CARGO COMPT)

NR 1 RT BIN FLOOR SOFT. REPAIRED COMPOSITE STRUCTURE IAW DRAWING AW-25-20-9804-06 OF PS-1.

Part: FLOOR — BROKEN (CARGO COMPT)

NR 6 RIGHT BIN FLOOR SOFT. REPAIRED COMPOSITE STRUCTURE IAW DRAWING AW-25-20-9084-06 OF PS-I.

Part: FLOOR — BROKEN (CARGO COMPT)

NR 3 RIGHT BIN FLOOR SOFT. REPAIRED COMPOSITE STRUCTURE IAW AW-25-20-9804-06 OF PS-1.

Part: FLOOR — BROKEN (CARGO COMPT)

NR 5 LEFT BIN FLOOR SOFT. REPAIRED COMPOSITE STRUCTURE IAW DRAWING AW-25-20-9804-06 OF PS-1.

Part: FLOOR — BROKEN (CARGO COMPT)

NR 9 RIGHT BIN FLOOR NEEDS OVERLAY. REPAIRED COMPOSITE STRUCTURE IAW DRAWING AW-25-20-9804-06 OF PS-1. ACFT TT: 19,327 HOURS. ACFT TC: 22,789.

Part: FLOOR — BROKEN (CARGO COMPT)

NR 7 RT BIN FLOOR NEEDS OVERLAY. REPAIRED COMPOSITE STRUCTURE IAW DRAWING AW 25-20-9804-06 OF PS-1.

Part: FLOOR — BROKEN (CARGO COMPT)

NR 2 RIGHT BIN FLOOR SOFT. REPAIRED COMPOSITE STRUCTURE IAW DRAWING AW-25-20-9804-06 OF PS-1.

Part: FLOOR — BROKEN (CARGO COMPT)

NR 9 LEFT BIN FLOOR NEEDS OVERLAY. REPAIRED COMPOSITE STRUCTURE IAW DRAWING AW-25-20-9804-06 OF PS-1.

Part: FLOOR — BROKEN (CARGO COMPT)

NR 1 LEFT BIN FLOOR SOFT. REPAIRED COMPOSITE STRUCTURE IAW DRAWING AW-25-20-9804-6 OF PS-1.

Part: FLOOR — BROKEN (CARGO COMPT)

NR 4 LEFT BIN FLOOR NEEDS OVERLAY. REPAIRED COMPOSITE STRUCTURE IAW DRAWING AW-25-20-9804-06 OF PS-1, COMPLETED WEIGHT CHANGE NOTIFICATION FORM (ATTACHED) AND TRANSFERRED TESTING STEPS 1-4 FROM ABOVE DRAWING TO ANOTHER WORK CARD. (M)

Part: FLOOR — BROKEN (CARGO COMPT)

NR 3 LEFT BIN FLOOR NEEDS OVERLAY. REPAIRED COMPOSITE STRUCTURE IAW DRAWING AW-25-20-9804-06 OF PS-1.

Part: FLOOR — BROKEN (CARGO COMPT)

NR 2 LEFT BIN FLOOR NEEDS OVERLAY. REPAIRED COMPOSITE STRUCTURE IAW DRAWING AW-25-20-9804-06 OF PS-1.

Part: FLOOR — BROKEN (CARGO COMPT)

NR 8 LEFT BIN FLOOR SOFT. REPAIRED COMPOSITE STRUCTURE IAW DRAWING AW-25-20-9804-96 (PART OF PS-1).

Part: FLOOR — BROKEN (CARGO COMPT)

NR 8 RIGHT BIN FLOOR SOFT. REPAIRED COMPOSITE STRUCTURE IAW DRAWING AW-25-30-9804-06 OF PS-1.

Part: SKIN — DENTED (FUSELAGE)

DENT AT BOXING JT RT FUSELAGE FORWARD OF REAR CARGO DOOR DUE REPAIR IN 3,000 CYCLES. CURRENT CYCLES: 29,794. REPAIR DUE BY 32,794 CYCLES. REPAIRED DENT IAW BAE FAX REF DJR/RJ0610-98. REF: W/C 1049 NDT.

Part: FLOOR — BROKEN (CARGO COMPT)

NR 6 LEFT BIN FLOOR SOFT. REPAIRED COMPOSITE IAW DRAWING AW-25-20-9084-06 OF PSI-1.

Part: FLOOR — BROKEN (CARGO COMPT)

NR 4 RIGHT BIN FLOOR NEEDS OVERLAY. REPAIRED COMPOSITE STRUCTURE IAW DRAWING AW-25-20-9804.

Part: MOUNT — CRACKED (RT SPOILER)

RIGHT LIFT SPOILER VALVE MOUNT PLATE CRACKED. REPLACED MOUNT PLATE. (M)

Part: RIVET — LOOSE (RT WING)

RIGHT WING TE SHROUD TOP STIFFENER BETWEEN RIB 4/5 HAS LOOSE RIVET, AFT END. REMOVED AND REPLACED LOOSE RIVET. (M)

Part: BRACKET — CRACKED (RT HYD SYSTEM)

RIGHT WING TE LOWER HYDRAULIC LINE BRACKET CRACKED AT RIB NR 5. REMOVED BRACKET AND FABRICATED NEW BRACKET PER DRAWING HC9 32H0211. INSTALLED BRACKET AND ATTACHED LINES TO BRACKET. (M)

Part: STIFFENER — CRACKED (RT WING)

RT WING T/E SHROUD TOP STIFFENER CRACKED AT FORWARD END BETWEEN RIBS 9 AND 10. REPAIRED PER BAE FAX JM/RJ0317/97 USING 2024T3 .040 INCH AND AW FAX HC/142-97 AND DJR/RJ0630-98.

Part: STIFFENER — CRACKED (RT WING)

RIGHT WING TE SHROUD TOP STIFFENER CRACKED AT FORWARD END BETWEEN RIBS 5/6. REMOVED AND REPLACED RIGHT WING TE SHROUD TOP STIFFENER. (M)

Part: BRACKET — CRACKED (RT HYD SYSTEM)

RIGHT WING TE TOP HYDRAULIC LINE CLAMP BRACKET CRACKED RIB NR 6. REMOVED AND REPLACED BRACKET. (M)

Part: BEARING — WORN (RT AILERON)

RIGHT AILERON OUTBOARD HINGE 'A' FRAME BEARINGS WORN. REMOVED AND REPLACED RIGHT AILERON OUTBOARD 'A' FRAME. W/C GEN FOR FUNCTIONAL CHECK. (M)

Part: STIFFENER — CRACKED (RT WING)

TE RIGHT WING TOP SHROUD STIFFENER OUTBOARD CRACKED AT FORWARD END BETWEEN RIB 8/9. REPLACED RIGHT WING TRAILING EDGE SHROUD TO STIFFENER BETWEEN RIBS 8/9. (M)

Part: STIFFENER — CRACKED (RT WING)

RIGHT WING TE SHROUD TOP STIFFENER CRACKED AT FORWARD END AND RIVET POPPED (AFT END) BETWEEN RIBS 3/4. REPLACED RIGHT WING TRAILING EDGE SHROUD TOP STIFFENER BETWEEN RIBS 3/4. (M)

Part: SUB FRAME — CRACKED (FRAME 50)

SUB-FRAME AFT OF FRAME 50 CRACKED AT LOWER LT CORNER. REPAIRED SUB-FRAME AFT OF FRAME 50 AT LOWER LT CORNER IAW BAE FAX DJR/RJ0602-98.

Part: SKIN — DENTED (FRAME 20)

COMPLIED WITH REPAIR OF 2 DENTS AT FRAME 20, STRINGER 20, PORT SIDE IAW SRM 53-00-12 FIG 202 WITHIN 3000 CYCLES, CURRENT CYCLES 29320, DUE BY 32320 CYCLES. REPAIRED DENTS IAW BAE FAX REF DJR/RJO595-98. (M)

Part: RIVET — LOOSE (LT WING)

NUMEROUS LOOSE RIVETS AT LT WING T/E LOWER SKIN, AFT OF REAR SPAR. REMOVED AND REPLACED NUMEROUS LOOSE RIVETS ON LT WING T/E LOWER SKIN AFT OF REAR SPAR.

Part: SKIN — DENTED (FRAME 9)

REPAIR DENT ON LEFT SIDE OF FUSELAGE AT FRAME 9, 3.25 INCHES BELOW SKIN LAP B AND 4.00 INCHES FORWARD OF FRAME 9 IN 3,000 CYCLES. CURRENT TCA 29,540 DUE AT 32,540 TAC.

Part: STIFFENER — CRACKED (LT WING)

LEFT WING TOP SKIN STIFFENER AFT OF REAR SPAR BETWEEN RIBS 7/8 IS CRACKED AT FORWARD END. REMOVED AND REPLACED TOP SKIN STIFFENER AFT OF REAR SPAR BETWEEN RIBS 7/8. (M)

Part: LONGERON — CRACKED (FUSELAGE)

ATTACHMENT ANGLE/GUSSET AT THE AFT END OF THE UPPER MOST LEFT AIRBRAKE HINGE LONGERON IS CRACKED. FABRICATED LEFT GUSSET PLATE PER BAE DRAWING HC539H0229. REPLACED LEFT GUSSET PLATE AT UPPER MOST LEFT AIRBRAKE HINGE LONGERON.

Part: FRAME — CHAFED (NR 1 ENG COWL)

NR 1 ENGINE FORWARD LEFT COWL DOOR LOWER AFT FRAME CHAFED NEAR LATCH. REPAIRED NR 1 ENGINE LEFT FORWARD COWL DOOR LOWER AFT FRAME IAW SRM 54-10-11.

Part: BRACKET — BROKEN (NR 4 ENGINE)

NR 4 ENGINE BRACKET AT LOWER FUEL/OIL HEAT EXCHANGER BROKEN. REPAIRED NR 4 ENGINE BRACKET AT LOWER FUEL/OIL HEAT EXCHANGER BY WELDING IAW ALLIED SIGNAL/TEXTRON MM.

Part: FRAME — CHAFED (NR 1 ENGINE COWL)

NR 1 ENGINE FORWARD RIGHT COWL DOOR, LOWER AFT FRAME CHAFED NEAR LATCH. REPAIRED NR 1 ENGINE RIGHT FORWARD COWL DOOR LOWER AFT FRAME IAW SRM 54-10-11. (M)

Part: INTERCOSTAL — CRACKED (FRAMES 41-43)

AFT VEST, CENTER FLOOR INTERCOSTAL BETWEEN FRAMES 41 AND 43 IS CRACKED ABOUT 1.25 INCHES AT FORWARD END. REMOVED AND REPLACED AFT VEST, CENTER FLOOR INTERCOSTAL WITH NEW PART. REPLACED INTERCOSTAL HC538J0430-006.

Part: INTERCOSTAL — CRACKED (FUSELAGE)

AFT END OF FORWARD VEST INTERCOSTAL AT A/C CENTERLINE IS CRACKED IN THE TOP FLANGE RADIUS. REPAIRED AFT FORWARD VEST CENTERLINE INTERCOSTAL. REF SRM 53-20-32, AT 51-71-11, PAGE 3.

Part: DOOR — CHAFED (NR 4 ENG COWL)

NR 4 INBOARD COWL FAN DUCT DOOR HAS VARIOUS CHAFES AT LOWER PAN AREA. REPAIRED CHAFED AREA BY PATCHING IAW BAE SRM STD PROCEDURES.

Part: COMPRESSOR — STALLED (NR 4 ENGINE)

ON CLIMB-OUT NR 4 ENGINE MADE 2 MUFFLED 'BANGS' AND N1, N2, TGT, STARTED DROPPING. SENT ATW MX TO ORD, LOCKED DOWN ENGINE AND FERRIED TO ATW. (M)

Part: COMPRESSOR — STALLED (NR 4 ENGINE)

NR 4 ENGINE MADE SEVERAL MUFFLED BANGS, THEN BEGAN SPOOLING DOWN ON N1, N2 AND TGT. F/A'S REPORTED SPARKS FROM TAILPIPE. ENGINE WAS SECURED USING EMERGENCY CHECKLISTS. (M)

Part: RELAY — FAILED (RT MLG)

RED LIGHT ON GEAR HANDLE REMAINED ON AFTER GEAR RET. RETURNED FOR LANDING, RED LIGHT OUT WITH GEAR HANDLE DOWN. REPLACED RELAYS GF6 NLG UPLOCK AND GF7 RIGHT MLG UPLOCK, RETRACTED GEAR 4 TIMES, GEAR INDICATED NORMALLY. (M)

Part: WARNING UNIT — MALFUNCTIONED (LANDING GEAR)

AFTER TAKEOFF RAISING GEAR RED LIGHT IN HANDLE REMAINED ON. REMOVED AND REPLACED AUDIBLE WARNING UNIT, OPS CHECKED GOOD ON CHECK FLIGHT. (M)

Part: FUEL CONTROL — MALFUNCTIONED (NR 4 ENGINE)

DEN - FLT 655 - NR 4 ENGINE, 2 PERCENT LOW N1 AT TAKEOFF AT 882 DEGREES, TARGET 92.5, ACTUAL 90.5 PERCENT N1. UNABLE TO DUPLICATE, NR 4 ENGINE CHECKED AT 871C AT RATED TAKEOFF. REMOVED AND REPLACED NR 4 FCU PER BANDOCH (PRECAUTIONARY) RESISTANCE CHECK OK. BLEED BAND ACT OK, PLUGGED OFF CUSTOMER BLEED PORT, POPPET VALVE CHECK, BLEED BAND DURING RUN, NO CHANGE.

Part: RIB — DAMAGED (RT WING)

ATW - DUE TO TOOLING MARKS, RT RIB 2 INBOARD STR 1A AND STR 7A AND RT RIB ZERO STR 7H, HOLES NEED TO BE OVERSIZED TO ELIMINATE MARKS. OVERSIZED HOLES AND INSTALLED OVERSIZE FASTENERS ON RT RIB 2 INBOARD STR 1A MRL 3210-12-700, STR 7A MRL 3210-12-800 AND RT RIB ZERO STR 7H MRL 3210-12-500 PER RIL HC571H9033 AND FAX NR DJR/RJ0379-97.

Part: WALL TRIM — CORRODED (FWD LAVATORY)

ATW - FORWARD LAVATORY WALL EDGE TRIM SHOWS SIGNS OF CORROSION ON LOWER END. REMOVED AND REPLACED CORRODED AREA OF WALL TRIM.

Part: SKIN — CORRODED (LT WING)

ATW - FOUND EXFOLIATION CORROSION ON INNER SKIN OF LT FORWARD PANEL 511JB PN HC573H0090-000. REMOVED BOOST PUMP CANISTER AND SEAT PANEL TO HST FOR REPAIR. PLACED ON W/O BV5999. INSTALLED SERVICEABLE PANEL.

Part: NUTPLATE STRIP — BROKEN (NR 4 PYLON)

ATW - NR 4 PYLON HORSESHOE PANEL (481AT) AFT NUTPLATE ATTACH STRIPS LT AND RT, BOTTOM 4 NUTPLATES NEED REPLACEMENT. ALSO, INBOARD AFT NUTPLATE STRIP IS BROKEN. REPAIRED ABOVE NUTPLATE STRIP PER BAE REPAIR HC546H9017 AND FAX DJR/RJ0378-97. PANEL 481AT IS NOW A NON-STANDARD PANEL AND IS MARKED IAW REPAIR DRAWING.

Part: SKIN — CORRODED (RT WING)

ATW - FOUND EXFOLIATION CORROSION ON INNER SKIN OF RT FUEL PANEL 611JB PN HC573H0090-001. REMOVED BOOST PUMP CANISTER AND SENT PANEL TO HST FOR REPAIR REF W/O BV6000. INSTALLED SERVICEABLE PANEL.

Part: OXYGEN MASK — DAMAGED (CABIN)

ATW - PASSENGER OXYGEN MASK RE-BREATHER FELT TORN AT SEATS 4, 8, AND 10 RT. REPLACED MASK ASSY, OPS FLOW, LEAK CHECKS OK.

Part: CONTROL CABLE — CORRODED (RT ELEVATOR)

ATW - THE RIGHT MAIN ELEVATOR CABLES ARE CORRODED AT THE UPPER MOST PULLEY IN THE VERTICAL STABILIZER. REMOVED AND REPLACED RT MAIN ELEVATOR CABLES IN THE TAIL, TENSIONED AND SAFETIED IAW BAE MM. GENERATED NEW WC FOR ELEVATOR FUNCTION CHECK.

Part: SKIN — DAMAGED (FUSELAGE)

ATW - LEFT FUSELAGE DAMAGE AT FRAME 20A. STR 17 REQUIRES REPAIR PER AVRO FAX DJR/RJ0994-96 DATED 8-28-96 NO LATER THAN 5-31-97. REPAIRED IAW BAE SRM 53-00-12 AND FAX NR DS/W/27797/97. MAJOR REPAIR REPORT COMPLETED RJ5562.

Part: INTERCOSTAL — CRACKED (CABIN)

ATW - AFT VESTIBULE FLOORS' SUPPORT STRUCTURE HAS AN INTERCOSTAL BETWEEN FRS NR 40 AND 43 WITH A 3 INCH LONG CRACK IN RADIUS OF TOP FLANGE. REPAIRED IAW BAE FAX REF NR MHRJ0350-97.

Part: CONTROL CABLE — CORRODED (LT ELEVATOR)

ATW - THE LEFT MAIN ELEVATOR CABLES ARE CORRODED AT THE UPPER MOST PULLEY IN THE VERTICAL STABILIZER. REMOVED AND REPLACED LT MAIN ELEVATOR CABLES IN THE TAIL, TENSIONED AND SAFETIED IAW BAE MM. GENERATED NEW WC FOR FUNCTIONAL TEST.

Part: JO BOLTS — LOOSE (LT/RT WING)

ATW - DURING GV ZONAL INSPECTION, FOUND EVIDENCE OF LOOSE JO BOLTS AT RIB ZERO AND RIB 2, LT/RT. REPORT FINDINGS TO AVRO/AIR. REPLACEMENT REQUIRED PER RIL HC571H9033. REMOVED AND REPLACED JO BOLTS ON RIB ZERO AND RIB 2, LT AND RT, STRINGERS 1-7 PER RIL HC571H9033. REF W/C'S; J120, J121, J122 , J123, J116, AND J117.

Part: COTTER PIN — MISSING (RUDDER)

ATW - RUDDER ATTACH BOLT MISSING COTTER PIN SAFETY OVER TOP OF BOLT LOCATED AT RIB NR 6 RUDDER HINGE FITTING. INSTALLED COTTER PIN AT RIB 6, RUDDER HINGE.

Part: BOLT — FAILED (FUSELAGE)

ATW - FRAME 29, LT AND RIGHT SIDE AT STR 12, .50 INCH BOLT; LEFT NUT SHOWS SIGNS OF TURNING, RIGHT HEAD APPEARS TO BE CRACKED. REMOVED BOLT, FOUND LEFT BOLT SHEARED UNDER HEAD, RIGHT BOLT CRACKED UNDER HEAD AND PART THROUGH HEAD. SENT BOLTS TO BAE FOR INSPECTION. HOLES FOUND WITHIN LIMITS. REPLACED WITH MS BOLTS PER FAX DJR/RJ0022-96 TORQUED AND WITCO BOND APPLIED. TESTED OK.

Part: JO BOLTS — DAMAGED (LT WING)

ATW - LEFT WING RIB 2 INBOARD AND OUTBOARD JO-BOLTS, STRINGERS 1-7, NEED REPLACEMENT PER RIL HC571H9033. REF W/C J118. REPLACED ABOVE JO-BOLTS LEFT WING RIB 2 PER RIL HC571H9033.

Part: CONTROL CABLE — CORRODED (RT AILERON)

ATW - THE RIGHT MAIN AILERON CABLES AT THE WING ROOT AFT LOWER PULLEY ARE CORRODED. REMOVED AND REPLACED RIGHT MAIN AILERON CABLES IN THE FUSELAGE AND WING ROOT AREA, TENSIONED AND SAFETIED IAW BAE MM. GENERATED W/C TO C/W A FUNCTIONAL TEST OF THE AILERONS.

Part: CABLES — CORRODED (ELEVATOR TRIM)

ATW - THE ELEVATOR TRIM CABLES AT THE RIGHT WING ROOT AREA ARE CORRODED. REMOVED AND REPLACED ALL 4 ELEVATOR TRIM CABLES, TENSIONED AND SAFETIED IAW BAE MM. GENERATED WC FOR FUNCTIONAL TEST OF ELEVATOR TRIM SYSTEM.

Part: ANGLE — CRACKED (BS 4138)

ATW - FLOOR BEAM 19 AT FRAME 32, INTERCOSTAL CRACKED IN RADIUS AREA. REPAIRED FLOOR BEAM ANGLE AT STA 41.38 (RT) AT FRAME 32 IAW BAE DRAWING NR HC536H9211 AND FAX NR DJR/RJ0207-97.

Part: ANGLE — CRACKED (BS 20.63)

ATW - FLOOR BEAMS 3, 7, AND 15 AT FRAME 29 - INTERCOSTALS CRACKED IN RADIUS AREA. REPAIRED FLOOR BEAM ANGLES AT STATIONS 20.63 (LT/RT) AND 41.38 LT, AT FRAME 29 IAW BAE DRAWING NR HC536H9211 AND FAX NR DJR/RJ0207-97.

Part: CABLES — CORRODED (LT AILERON)

ATW - LEFT MAIN AILERON CABLES AT LEFT WING ROOT FORWARD PULLEY ARE CORRODED. REMOVED AND REPLACED BOTH WING ROOT MAIN AILERON CABLES (LEFT), TENSIONED AND SAFETIED IAW BAE MM. GENERATED W/C FOR FUNCTIONAL TEST.

Part: CONTROL CABLE — CORRODED (RT AILERON)

ATW - THE RIGHT AILERON INTERCONNECT SHEATHED CABLE IS CORRODED AT OUTBOARD PULLEY AND QUAD. REMOVED AND REPLACED RIGHT SHEATHED CABLE, TENSIONED, AND SAFETIED. GENERATED W/C FOR AILERON FUNCTIONAL TEST.

Part: RAIL — CORRODED (AIR STAIR DOOR)

ATW - FORWARD AIR STAIR INBOARD RAIL IS CORRODED. REMOVED AND REPLACED INBOARD RAIL FOR FORWARD AIR STAIRS.

Part: CABLES — CORRODED (AILERON)

ATW - THE AILERON CENTER INTERCONNECT CABLES (BOTH) ARE CORRODED AT THE WING ROOT PULLEYS. REMOVED AND REPLACED BOTH CENTER AILERON INTERCONNECT CABLES, TENSIONED AND SAFETIED. GENERATED SEPARATE WC FOR AILERON FUNCTIONAL TEST.

Part: HYD LINE — LEAKING (GREEN HYD SYSTEM)

TWENTY MINUTES INTO FLIGHT, HYDRAULIC LOOK UP AND GREEN HYDRAULIC QTY LIGHT CAME ON, GREEN QTY FELL TO .125. INSPECTED RIGHT MAIN GEAR RETRACTION LINE TO CYLINDER (FLEX) LEAKING. INSTALLED A FLEX LINE (REPLACEMENT) TO RETRACT CYLINDER, PRESSURE CHECK OK, SERVICED HYD.

Part: PACK — ODOR (NR 1)

NR 1 PACK SMELLS 'OILY' AND CAUSES A HAZE IN CABIN, IF ALLOWED TO REACH 40 DEGREES CELSIUS. CORRECTIVE ACTION: RAN NR 1 PACK PER DUCT CLEARING PROCEDURE MM, REF 49-50-00. NO 'OIL' SMELL OR HAZE NOTED DURING PROCEDURE.

Part: FUEL CONTROL — MALFUNCTIONED (NR 1 ENGINE)

WITH ENGINES AT FLIGHT IDLE, AND IN CLEAR (VFR CONDITION) NR 1 ENGINE N1 PLUS N2 ROLLED BACK TO APPROXIMATELY 30 PERCENT. PRECAUTIONARY SHUT DOWN OF NR 1 ENGINE EMERGENCY CHECK LIST COMPLETED. (M)

Part: ENGINE — MALFUNCTIONED (NR 3)

NR 3 ENGINE VIBRATION WENT TO 1.5, RETARDED THRUST LEVER AND IT STAYED AT 1.5. NO VIBES FELT OR ABNORMAL INDICATIONS. 10 MINUTES LATER TGT WENT TO 1000 DEGREES, CREW SHUT DOWN ENGINE. DIVERTED TO ATW. REMOVED AND REPLACED NR 3 ENGINE.

Part: STIFFENERS — CRACKED (FRAME NR 29)

DURING STEP 3 INSPECTION FOR CRACKS AT STIFFENERS ON FRAME 29, REF EO E95/003/653, 3 CRACKED STIFFENERS WERE DISCOVERED, 25.94 RIGHT, AND 25.94 LEFT AND 31.13 LEFT. REPAIRED CRACKS IAW EO NR E95/005/653 ORIG PER NOTE NR 1 OF REPAIR DRAWING AW-53-20-9506-06, ET CUT AWAY FLANGE OF STIFFENERS COMPLIED WITH, NO CRACKS.

Part: SKIN — GOUGED (FUSELAGE)

SKIN AROUND FRONT CARGO DOOR, FORWARD LOWER SECTION ABOUT 13 INCHES UP FROM CORNER, HAS A .016 INCH DEEP GOUGE APPROXIMATELY .25 INCH BY .375 INCH IN SIZE WITH METAL ROLLED UP AT BOTTOM. BLENDED REPAIRED AREA AT FORWARD CARGO BAY AS DESCRIBED ABOVE IAW AVRO FAX DJH/RJ1304-95. PERFORMED ET ON THE ABOVE BLENDED AREA AND FOUND TO BE CRACK FREE NOW 10/20/95. REPRO WITH ALOCROM 1200. FOLLOWED BY EPOXIDE PRIME.

Part: ANGLE — CRACKED (FRAME NR 35)

FREIGHT ANGLE FOR FRAME 35 (LOWER) CENTER AREA CRACKED. REPLACED FREIGHT ANGLE.

Part: ANGLE — CRACKED (FRAME 36)

FREIGHT ANGLE FOR FRAME 36, LOWER CENTER AREA CRACKED. REPAIRED FREIGHT ANGLE AS PER 146 SRM.

Part: SKIN — GOUGED (FUSELAGE)

SKIN AROUND REAR CARGO BAY DOOR FORWARD LOWER SECTION ABOUT 10 INCHES UP FROM CORNER HAS A .013 INCH DEEP GOUGE APPROXIMATELY .125 INCH BY .5 INCH INSIDE WITH METAL ROLLED UP AT BOTTOM OF GOUGE MARKED WITH PINK MARKER. BLEND REPAIRED AREA AFT CARGO BAY AS DESCRIBED ABOVE IAW AVRO FAX DJH/RJ1304-95. PERFORMED ET ON ABOVE AREA. FOUND CRACK FREE 10/20/95.

Part: TRACK — CORRODED (AIRSTAIR)

AFT AIRSTAIR INBOARD TRACK IS CORRODED AT VERY AFT END, CORROSION IS GREATER THAN .005 INCH REF SRM 51-10-02. RAIL ALREADY REMOVED. INSTALLED AFT AIRSTAIR INBOARD TRACK ASSY AND APPLIED PRC TO PROTECT RAIL.

Part: ATTACH STRUCT — DAMAGED (NR 3 PYLON)

NR 3 MOTOR (PYLON) AFT MOUNT FOR SHOULDER COWL HAS MOUNTING HOLES ENLONGATED WHERE SHOULDER COWL ATTACHES TO LORD MOUNT, SEE REPAIR HC710H9003 FOR FIX. REPAIRED NR 3 ENGINE SHOULDER COWL AFT DOOR LORD MOUNT ATTACH STRUCTURE IAW BAE FAX PJN/1954-91. (M)

Part: REINFORCE PLATE — DAMAGED (FUSELAGE)

CHAFING DISCOVERED ON FUSELAGE REINFORCING PLATE BELOW RIGHT FORWARD FUSELAGE WING, LUG DAMAGE TYPICALLY CAUSED BY ARMPIT FAIRING. MEASURES .010 INCH - .014 INCH DEEP. PERFORMED EDDY CURRENT INSPECTION AFTER BLENDING AS PER FAX DJH/RJ1230-95. NO CRACK INDICATIONS WERE EVIDENT AT EITHER DAMAGED AREA. BLENDING, ALODINED, PRIMED AND PAINTED CHAFED AREA RIGHT FUSELAGE APPLIED TEMP RUB STRIP WITH SEALANT.

Part: SKIN — WORN (LT TE FLAP)

LEFT INBOARD TRAIL FLAP TOP SIDE HAS 2 SPOTS OF WEAR THROUGH PAINT, NEED FURTHER INVESTIGATION FOR LIMITS. BLENDED DAMAGED AREA TO A SMOOTH DEPRESSION. PERFORMED ET TO BLENDED AREA. NO DEFECTS FOUND. INSPECTION RIVET NO DAMAGE NOTED, TREATED PRIMED AND TOP COATED. REPROTECTED WITH ALOCROM FOLLOWED BY PRIMER AND TOPCOAT ALL IAW DJH/RJ1301-95.

Part: CARRIAGE — WORN (NR 2 TE FLAP)

RIGHT NR 2 UPPER FLAP CARRIAGE HAS A WEAR MARK APPROXIMATELY .040 INCH TO .050 INCH DEEP IN THE VERY UPPER INBOARD EDGE ADJACENT TO THE BONDING LEAD ATTACHMENT TO THE FLAP. BLENDED WEAR MARK TO A SMOOTH DEPRESSION AS PER AVRO FAX. PERFORMED EDDY CURRENT TO BLENDED AREA AND FOUND TO BE CRACK FREE. REPROTECTED THE DAMAGED AREA W/ALOCROM, PRIMED, TOPCOATED AND REPOSITIONED BONDING.

Part: FASTENER — MISSING (FRAME 32)

FRAME 32 IN CABIN APPROXIMATELY 9 INCHES ABOVE FLOOR LINE ON RIGHT SIDE, IS MISSING A HI-LOK FASTENER. INSTALLED MISSING HI-LOK FASTENER.

Part: BOLT — CORRODED (NR 3 FLAP TRACK)

FORWARD FLAP ATTACH BOLT AT LEFT FLAP TRACK NR 3 IS CORRODED. REMOVED, CLEANED AND INSPECTED BOLT, REINSTALLED BOLT. NO CORROSION FOUND.

Part: TERMINAL BLOCK — CORRODED (HORIZ STAB)

FOUND CORRODED TERMINAL BLOCK AFT OF HORIZONTAL STABILIZER REAR SPAR RIGHT SIDE INBOARD AT VERTICLE FIN TERMINAL BLOCK LABELED UB25. LOCATED ON ELEVATOR CONTROL BOX STRUCTURE. REMOVED AND REPLACED TERMINAL BLOCK UB25 AND REPLACED WIRE LUGS TO UB25. ELEVATOR FDR INDICATION, OPS CHECK OK.

Part: CRANK — CORRODED (RT MLG)

RIGHT MLG DIRECTIONAL CRANK AFT BUSHING SURFACE SHOWS SIGNS OF CORROSION. TRANSFER TO W/O BT4300, GEN W/C TO INSTALL SERVICEABLE CRANK, NR 7021.

Part: BOLT — CRACKED (RT SPOILER)

AFT JACK BOLT FOR RIGHT MID LIFT SPOILER CRACKED UNDER HEAD. REMOVED AND REPLACED AFT JACK BOLT FOR RIGHT MID LIFT SPOILER.

Part: BOLT — FAILED TEST (NR 3 FLAP TRACK)

LEFT NR 3 FLAP TRACK CARRIAGE TO FLAP ATTACH BOLT HAS FAILED UT INSPECTION AND NEEDS NEW BOLT INSTALLED. REMOVED AND REPLACED FLAP ATTACH BOLT.

Part: BUSHINGS — DAMAGED (NR 3 TE FLAP)

PIN ASSY FLAP UPPER CARRIAGE TO LEVER FOUND BUSHING WITH PLATING LOSS SCRAPED. SSI NR 57-55-129, NR 3 RIGHT FLAP. REMOVED AND REPLACED FLAP UPPER CARRIAGE TO LEVER BUSHING, NR 3 RIGHT FLAP.

Part: BOLT — DAMAGED (RT SPOILER)

RIGHT WING INNER LIFT SPOILER FORWARD JACK BOLT HAS DAMAGED THREADS. INSTALLED NEW BOLT.

Part: BOLTS — CORRODED (LT SPOILER)

LEFT WING OUTBOARD LIFT SPOILER FOUND BOTH FORWARD AND AFT JACK BOLTS HAVE PLATING MISSING ON BOLT SHANK. REPLACED FWD AND AFT JACK BOLTS. (M)

Part: JO-BOLTS — LOOSE (CTR WING)

CENTER WING SECTION LEFT SIDE AT RIB 2 HAS 2 JO-BOLT FASTENERS ON TOP SKIN STRINGER JOINT FITTINGS THAT ARE LOOSE AND WILL NOT TORQUE UP. SSI 57-10-117. REMOVED 2 JO-BOLT FASTENERS AND INSTALLED OVERSIZE MEL FASTENERS PER RIL NR HC571H9033 AND AVRO FAX'S GCB/RJ1186-95 PG 1/2;GCB/RJ1179-95.

Part: CONTROL CABLE — CORRODED (LT AILERON)

LEFT AILERON INTERCONNECT CABLE C2C-D IS CORRODED BEYOND MAINTENANCE MANUAL LIMITS, CABLE 63C AND 63B TURN BUCKLE HAS BARREL UNSAFETIED AND SLACKENED. REMOVED AND REPLACED LEFT AILERON INTERCONNECT CABLE IAW 146 MM 27-11-44 THROUGH STEP N6 PG 414. GENERATED W/C FOR COMPLETION.

Part: RIVETS — MISSING (FRAME NR 19)

FRAME 19 RIGHT SIDE BELOW THE 3RD ABUTMENT DIAPHRAM THERE ARE 2 RIVETS MISSING IN STRUCTURE. INSTALLED ABOVE RIVETS.

Part: BOLT — CORRODED (NR 2 TE FLAP)

RIGHT NR 2 FLAP CARRIAGE UPPER CARRIAGE TO FLAP BOLT HAS FLAKING PROTECTIVE COATING AND IS CORRODED. REMOVED AND REPLACED CARRIAGE TO FLAP BOLT NR 2 POS.

Part: TERM BLOCK — CORRODED (NR 3 SPOILER)

TERMINAL BLOCK AT RIGHT NR 3 LIFT SPOILER JACK IS CORRODED. REPLACED TERMINAL BLOCK 'M' AT RIGHT OUTER SPOILER JACK. W/C GENERATED FOR OP CHECK. (M)

Part: BOLT — FAILED (LT ELEVATOR)

LEFT ELEVATOR NR 4 HINGE, LOWER 'A' FRAME BOLT FAILED NDT INSPECTION. INSTALLED NEW LOWER LEFT NR 4 'A' FRAME BOLT AND SAFETIED.

Part: INTERCOSTAL — CRACKED (FUSELAGE)

ZONE 100, INTERNAL, BETWEEN FRAMES 14 AND 15 INTERCOSTAL IS CRACKED AT FUSELAGE CENTER LINE. SSI 53-10-127. REPLACED INTERCOSTAL.

Part: BOLT — BROKEN (LT AILERON)

LEFT AILERON RIB 18 UPPER 'A' FRAME FAIL/SAFE BOLT BROKEN. REMOVED AND REPLACED RIB 18 UPPER 'A' FRAME FAIL/SAFE BOLT.

Part: PIVOT PIN — DEFECTIVE (NR 4 FLAP TRACK)

RIGHT WING OUTER FLAP TRACK NR 4 INSPECTION OF FLAP TRACK PIVOT PIN, LOWER CARRIAGE TO INTERCARRIAGE LEVER FOUND DEFECT ALONG SHANK OF BOLT FROM BOLT HEAD TO THREADS. INSPECTION CARD NR 267 SSI NR 57-55-127. INSTALLED NEW PIVOT PIN ASSY AT RIGHT OUTBOARD NR 4 FLAP TRACK LOWER CARRIAGE ON INBOARD INNER CARRIAGE LEVER.

Part: BOLTS — CORRODED (RT SPOILER)

RIGHT WING ROLL SPOILER INBOARD HINGE BOLT P/N HC72H0909-204 HAS CORROSION IN THREADS, CLEANED AND FOUND DEEP PIT IN THREAD AREA. SCRAP BOLT. INSTALLED NEW BOLT ASSY ON RIGHT ROLL SPOILER INBD HINGE.

Part: MANIFOLD — DIRTY (NR 1 ENGINE)

FOUND EVIDENCE OF SOOT IN THE RT REAR COWL AREA OF NR 1 ENGINE. RIGHT MANIFOLD FAILED ET. REPLACED RT MANIFOLD ASSY ON NR 1 ENGINE.

Part: CONTROLS — OSCILLATED (ELEVATOR)

DEN - FLT 365 - AIRCRAFT EXPERIENCED A PITCH OSCILLATION ON CLIMB-OUT FROM MLI IN FREEZING PRECIPITATION AT FL 210 AND 250 KNOTS. INSPECTION A/C AND C/W BAE OSCILLATION INCIDENT CHECKLIST. NO DEFECTS NOTED.

Part: SKIN — DENTED (FUSELAGE FWD LT)

AIRCRAFT HAS DENT ON FWD LEFT FUSELAGE FWD OF FRAME P APPROXIMATELY 7 INCHES ABOVE SKIN LAP JOINT, COMPLIED WITH PERMENANT REPAIR WITHIN 400 CYCLES, CURRENT TC AT TIME OF DAMAGE WAS 22471 TC, DUE BY 22871 TOTAL CYCLES, REF AVRO FAX'S DJR/RJ0243-95 AND DJR/RJ0234-95. COMPLIED WITH REPAIR IAW REPAIR DRAWING HC537H9305 STEPS 1-14.