N607AW

Part: BOLT — CORRODED (ELEVATOR)

FOUND CORROSION ELEVATOR HINGE A-FRAME ATTACHMENT BOLTS TWO EACH. REPLACED NEW. (M)

Part: ANGLE — CORRODED (INTERCOSTAL)

FOUND CORROSION ON INTERCOSTAL AT CETNER JOINT PLATE 80 INCHES FROM DOOR 1L. REPLACED ANGLE, IAW BAE SRM 51-42-00 AND 51-23-00. (M)

Part: FLAP TRACK — WORN (T/E FLAP)

NR 2 FLAP TRACK, WEAR FOUND ON NR 2 LT LOWER ROLLER THAT MEASURES .033 INCHES DEEP. REQUESTED REPAIR FROM BAE SYSTEMS REF AVMAX FAX 607-1907002. MAINTENANCE REMOVED LOWER CARRIAGE NR 2 LEFT. ROLLERS REPLACED IAW CMM 57-50-22. CARRIAGE REINSTALLED IAW AMM 27-50-64. FUNCTION TESTED SERVICEABLE. BLACKLASH MEASURED AT 8 MM. OK TO REMAIN IN SERVICE AT THIS TIME. REF BAE FAX BARA/AVR/6741/04-MK. (M)

Part: INTERCOSTAL — CRACKED (FUSELAGE)

FOUND INTERCOSTAL CRACKED BETWEEN FRAMES 21/22 AT STRINGER 21 RT IN FORWARD CARGO BAY. MAINTENANCE REPLACED INTERCOSTAL IAW SRM 51-23-00, 51-42-00, AND 51-43-00. (M)

Part: INTERCOSTAL — CRACKED (FUSELAGE)

FOUND INTERCOSTAL CRACKED BETWEEN FRAMES 22/23 AT STRINGER 21 RIGHT IN FORWRAD CARGO COMPARTMENT. MAINTENANCE REPLACED INTERCOSTAL IAW BAE SRM 51-23-00, 51-42-00 AND 51-43-00. (M)

Part: STRINGER — CORRODED (FUSELAGE)

FOUND CORROSION ON CENTER LINE STRINGER IN FORWARD CARGO PIT BETWEEN FORWARD AND AFT RADIO ALT ANTENNAS. MAINTENANCE REPLACED STRINGER WITH MANUFACTURED REPAIR PART IAW SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FOUND CORROSION ON FLOOR SUPPORT MEMBER ADJACENT TO FLOORBEAM 15.52 INCHES FROM DOOR 1L. MAINTENANCE REPLACED JOINT PLATE WITH MANUFACTURED REPAIR PART IAW BAE SRM 51-20

Part: APU — INOPERATIVE (APU BAY)

SMOKE IN CABIN WHEN APU IS SUPPLYING AIR TO PACKS. MAINTENANCE PERFORMED PACK BURNOUT AND REMOVED AND REPLACED APU. (M)

Part: STRINGER — CORRODED (FUSELAGE)

FOUND STRINGER 34R HAS CORROSION. MAINTENANCE REPAIRED STRINGER 34R BETWEEN FRAMES 20B AND 21 IAW BAE FAX BARA/AVR/6609/03-DC AND IAW BAE SRM 51-43-00. (M)

Part: FLAP TRACK — WORN (NR 1)

RT NR 1 FLAP TRACK WEAR UPPER AND LOWER RAILS OUTBOARD FACE. MAINTENANCE REQUESTED REPAIR FROM BAE SYSTEMS REF AVMAX FAX 1734-6070003. LPI C/O ON BLENDED FLAP TRACK AS REQUIRED IAW BARA/AVR/6606/03-DC, NO CRACKS FOUND. (M)

Part: STRUCTURE — DAMAGED (TE FLAP)

RIGHT FLAP AT THE NR 4 POSITION BETWEEN RIBS 33 AND 34 OVERSIZE BUSHING REQUIRED. MAINTENANCE REQUESTED REPAIR FROM BAE SYSTEMS REF AVMAX FAX 134-6070002. (M)

Part: STRUCTURE — DAMAGED (TE FLAP)

RIGHT FLAP AT THE NR 4 POSITION BETWEEN RIBS 33 AND 34 OVERSIZE BUSHING REQUIRED. BUSHING LOCALLY MANUFACTURED AT AAO AND CAD PLATED IAW BAE FAX BARA/AVR/6605/03-DC. BUSHING INSTALLED IAW FLAP EO EO2/021/657. (M)

Part: SKIN — DAMAGED (FUSELAGE)

FOUND CRACKS ON THE LEFT AND RIGHT FUSELAGE ABOVE STRINGER 13 JUST AFT OF FRAME 29 EMANATING FROM THE RIVIT LOCATIONS. MAINTENANCE CUT OUT DAMAGE TO SKIN IAW BAE FAX BARA/AVR/6603/03-DC. NDT HFEC CARRIED OT IAW BAE FAX BARA/AVR/6603/03-DC, NO CRACKS NOTED. INSTALLED FREEZE PLUG IAW BAE FAX BARA/AVR/6603/03-DC. (M)

Part: SKIN — CRACKED (FUSELAGE)

FOUND CRACKS ON THE LEFT AND RIGHT FUSELAGE ABOVE STRINGER 13 JUST AFT OF FRAME 29 EMANATING FROM THE RIVET LOCATIONS. MAINTENANCE REQUESTED REPAIR FROM BAE SYSTEMS REF FAX 1734-6070004. (M)

Part: WIRE — BURNED (FWD CARGO BAY)

APU GENERATOR INOPERATIVE. DURING MAINTENANCE CORRECTIVE ACTION FOUND 3 APU GENERATOR WIRES IN FORWARD CARGO BAY CEILING BURNED AND EVIDENCE OF ARCHING ON CARGO LINER. MAINTENANCE REPLACED THE 3 PHASE APU GENERATOR WIRES AND CRIMP SLEEVES, PER BAE MM 24-00-00, FROM FWD BREAK TO APU CONTACTOR. (M)

Part: SKIN — CRACKED (FUSELAGE)

RIGHT FUSELAGE SKIN AT FRAME 32 ABOVE STRINGER 19 HAS A .0250 INCH CRACK ORIGINATING AT FASTENER. REPAIR I/P. (M)

Part: FUEL CONTROL — MALFUNCTIONED (NR 3 ENGINE)

AT FL280, OAT -40 DEGREES C, TMS OFF, ANY REDUCTION IN POWER OF NR 3 ENGINE FUEL FLOW WOULD DROP TO 300 NR A FEW SECONDS. OTHER ENGINE INSTRUMENTS WOULD DROP ACCORDINGLY. REMOVED AND REPLACED NR 3 FUEL CONTROL ASSEMBLY. OPS AND LEAK CHECKS GOOD AT THIS TIME. (M)

Part: SLIDE — UNSERVICEABLE (PAX DOOR) · airframe 29,564 hrs · 43,021 cycles

FOUND THE FWD PAX DOOR EVACUATION SLIDE CABLE RELEASE NOT ATTACHED TO GIRT BAR. MAINTENANCE REMOVED AND REPAIRED EVACUATION SLIDE.

Part: SLIDE — WILL NOT TEST (PAX DOOR) · airframe 29,310 hrs · 42,734 cycles

LIGHTS ON EMERGENCY ESCAPE SLIDE NOT ILLUMINATE DUE TO PIN IN BATTERY NOT BEING PULLED OUT UPON DEPLOYMENT. SNAP THAT HOLDS PIN LANYARD BECAME DETACHED INSTEAD. MAINTENANCE REMOVED AND REPLACED EMERGENCY SLIDE ASSEMBLY.

Part: SWITCH — DIRTY (LOWER DOORS)

LOWER DOOR NOT SHUT ON MWS PANEL, CAME ON DURING TAKEOFF ROLL. ABORTED TAKEOFF AND VERIFIED ALL DOORS SHUT. CLEANED AND INSPECTED LOWER DOOR SWITCHES, ALL CHECKED GOOD. (X)

Part: BEARING — FAILED (LT MLG)

REMOVED NR 1 TIRE ASSY, FOUND NR 1 WHEEL INNER BEARING SEIZED ONTO THE AXEL. REMOVED AND REPLACED LEFT MLG AXEL, WHEELS AND NR 1 HEAT PACK AND BRAKE. NR 1 BRAKE P/N AHA1413, SN HB182 TMS 2861. CYCLES 3,131. NR 1 CARBON HEAT PACK PN AH09068, SN AWAC170. TMS 478. CYCLES, 544. NR 1 WHEEL PN AHA1489 SN GT145, TMS 342. CYCLES, 412. (X)

Part: COMPRESSOR — DAMAGED (NR 1 ENGINE)

NR 1 ENGINE VIBRATION 2.5 AIRBORN ENGINE SHUTDOWN BY EMERGENCY CHECKLIST. INSPECTED AND FOUND BLADES MISSING FROM NR 3 AND NR 4 WHEEL AND DAMAGE TO NR 2 WHEEL AND SUSPECT DAMAGE TO NR 1 WHEEL. AIRCRAFT TO BE FERRIED TO ATW. (M)

Part: COMPRESSOR — FAILED (BLADE)

DEN - FLT 595 - NR 1 ENGINE: VIBRATION 2.5 AIR-BORN. ENGINE SHUT DOWN BY EMERGENCY CHECKLIST. INSPECTED AND FOUND BLADES MISSING FROM NR 3 AND NR 4 WHEEL AND DAMAGE TO NR 2 WHEEL AND SUSPECT DAMAGE TO NR 1 WHEEL. AIRCRAFT TO BE FERRIED TO ATW. ACFT TT: 19,327 HOURS. ACFT TC: 22,789.

Part: PIN — FAILED (NLG ACTUATOR)

UPON REMOVAL OF NOSE LANDING GEAR RETRACTION JACK, FOUND PIN AT GEAR BAY SIDEWALL SHEARED. RETRACTION JACK REMOVED FOR E.O. E98/002/632. REMOVED AND REPLACED THE NLG RETRACTION JACK PIN AS REQUIRED DURING REMOVAL AND REPLACMENT OF JACK STREET. ACFT TT: 23,562 HOURS. ACFT TC: 33,928.

Part: ACTUATOR — FAILED (NLG)

UPON REMOVAL OF NOSE LANDING GEAR RETRACTION JACK FOUND PIN AT GEAR BAY SIDEWALL SHEARED. RETRACTION JACK REMOVED FOR EO E98/002/632. REMOVED AND REPLACED THE NLG RETRACTION JACK PIN AS REQ'D DURING REMOVING AND REPLACING OF JACK STREET. (M)

Part: TRIM — BINDS (ELEV)

ELEVATOR TRIM BINDS AT ALL SPEEDS, ALL ALTITUDES WHEN MOVED FORWARD OF 3 ON THE TRIM INDICATOR.

Part: TRIM — BINDS (ELEV)

AT 20,000 FT 290 KTS ELEV TRIM BINDS WHEN TRYING TO TRIM NOSE DOWN, NOSE UP FEELS NORMAL. PERFORMED ELEV TRIM CIRCUIT FRICTION TST, ALSO PERFORMED CLUTCH FRICTION TEST, INSPECTED CIRCUIT AND INTERCONNECT CIRCUIT AT ELEV, BOTH TESTS AND VISUAL ACCOMPLISHED WITH NO DEFECTS NOTED. GEN W/C FOR CHANGE OF LT AND RT TRIM SCREW JACKS. DAMPER HTR TESTS OK. (M)

Part: PANEL — LOOSE (RT WING TE)

ATW - FLT 505 - ON CLIMB-OUT ACCELERATING THROUGH 240-250 KNOTS, FELT SLIGHT AIRFRAME VIBRATION. AS SPEED INCREASED, VIBRATION INCREASED. REPLACED PANEL ON RT TRAILING EDGE OF WING AND SEAL.

Part: RETRACT MECH — MALFUNCTIONED (TE FLAPS)

DEN - FLT 669 - FLAPS WOULD NOT MOVE FROM THE 24 DEGREE POSITION IN THE AIR. CLEARED FLAP FAULT AND OPS TESTED GOOD.

Part: AIR DISTRIBUTION — ODOR (CABIN)

ATW - WHEN SWITCHING AIR FROM APU TO ENG AIR, NR 1 PACK GIVES A STRONG OIL BURNING SMELL FOR A FEW MINUTES THEN IT CLEARS. OPS CHECKED NR 1 PACK ON THE GROUND WITH APU AND ENG AIR, NO SMELL NOTICED.

Part: LINE — FAILED (LT MLG)

GREEN HYD SYSTEM LOW QTY AND LOW PRESS IN FLT. REPLACED HYD RETURN HOSE TO LEFT MLG RETRACTION JACK. (M)

Part: TERMINAL BLOCK — CORRODED (CABIN)

TWO TERMINAL BLOCKS BELOW THE INBOARD AIRSTAIR DRIP TRAY FOR THE PAX DOOR ARE CORRODED AND NEEDS TO BE CLEANED. REPLACED TERMINAL BLOCKS AA AND AB IN ZONE 131-00-00 AND OPENED WORK CARD FOR TEST. (M)

Part: SEAT RAIL — CORRODED (CABIN)

FORWARD RIGHT I/N SEAT RAIL HAS CORROSION PAST LIMITS (FWD 23 INCHES). REMOVED 24 INCHES OF SEAT RAIL RT INBOARD FORWARD AND SPLICED IN NEW SECTION OF SEAT RAIL PER SRM 53-00-32 PAGES 202, 203 AND 204. ANODIZED REPLACEMENT PART TO MIL-A-8625F PER BAE FAX DJR/RJO641-97. GEN W/C FOR REINSPECT EVERY 1000 CYC.

Part: BRACKET — WORN (NLG DOOR)

NLG AFT DOOR STOP ASSY MATERIAL MORE THAN 50 PERCENT WORN. REPLACED DOOR STOP BRACKET. DOOR CLEARANCES TO BE CHECKED ON GEAR SWING INSTALLATION. (M)

Part: ROLLER — CORRODED (NR 1 TE FLAP)

LEFT FLAP NR 1 CARRIAGE ROLLER ASSY TO LICK ATTACH BOLT CORRODED. REMOVED AND REPLACED CORRODED ROLLER TO CARRIAGE ATTACH BOLT.

Part: SEAT RAIL — CORRODED (CABIN)

FORWARD LEFT .1B SEAT RAIL HAS CORROSION PAST LIMITS, APPROX 64 INCH LENGTH. REMOVED 65 INCHES FORWARD SECTION OF LEFT INBOARD SEAT RAIL ASSY AND SPLICED REPLACEMENT SEC PER SRM 53-00-32 PAGE 202, 203, 204. ANODIZED REPLACED PART PER MIL-A-8625F AND FAX BAE DJR/RJ0641-97. REMOVED AND REPLACED .0 PERCENT THICK STRAP USING 7075 AND T6 .090 PER BAE FAX DJR/RJ0644-97. GEN W/C'S FOR REINSPECTION OF SEAT RAIL.

Part: TRACK — WORN (LT TE FLAP)

LEFT NR 1 FLAP TRACK SHOWS WEAR ON OUTBOARD SURFACES OF UPPER AND LOWER RAILS. BLENDED WORN AREAS IAW BAE ATW FAX DJR/RJ0647-97. MAX CLEARANCE WITH NEWPADS IS .092 INCH REF FAX FOR EXTENDED WEAR LIMIT.

Part: CONTROL CABLE — CORRODED (RT AILERON)

RIGHT AILERON CABLES CORRODED AT BELLCRANK AT RIB NR 10. REMOVED AND REPLACED BOTH RIGHT MAIN AILERON OUTER CONTROL CABLES, TENSIONED AND SAFETIED IAW BAE MM.

Part: CONTROL CABLE — CORRODED (LT AILERON)

LEFT OUTER AILERON CONTROL CABLE HAS RUST ON OUTER CABLE QUANDRANT. REMOVED AND REPLACED BOTH LEFT MAIN AILERON OUTER CONTROL CABLES, TENSIONED AND SAFETIED IAW BAE MM .

Part: STIFFENER — CRACKED (LT WING)

LEFT WING, TRAILING EDGE AREA AFT OF REAR SPAR HAS A CRACKED STIFFENER ON LOWER SHROUD SKIN BETWEEN WING RIBS NR 7 AND 8. REPLACED STIFFENER AND PAINTED.

Part: STIFFENER — CRACKED (LT WING TE)

LEFT WING T/E SHROUD AREA BETWEEN WING WIBS NR 8 AND 9 HAS THE TWO UPPER SKIN STIFFENERS WITH CRACKS AT THEIR FWD ENDS. REPAIRED OUTBOARD STIFFENER PER FAX JM/RJ0317/97, REPLACED INBOARD STIFFENER PER SRM ALSO REF BAE FAX RA/RJO595-97.

Part: BRACKET — CRACKED (LT WING)

LEFT WING T/E AREA AT WING RIB NR 8 HAS A CRACKED HYD LINE BRACKET WHICH IS ALLOWING HYD LINE TO CHAF ON THE TAIL RIB. HYD LINE IS GOING OUT OT OUTBOARD LIFT SPOILER JACK. INSPECTED LINE OK. REPLACED CRACKED BRACKET.

Part: BRACKET — CRACKED (NR 4 ENGINE COWL)

NR 4 ENGINE LEFT FAN DOOR HAS ONE BRACKET CRACKED AND ONE RIVET HEAD SHEARED ON BOTTOM SPLITTER. REPLACED ONE SHEARED RIVET HEAD AND ONE BRACKET ON NR 4 ENGINE LEFT FAN DOOR AS WRITTEN ABOVE.

Part: ANGLE — CRACKED (FUSELAGE)

CENTER MLG BAFFLE UPPER ATTACHMENT ANGLE CRACKED THROUGH TWO RIVETS 1.5625 INCHES IN LENGTH. REPAIR/REPLACE NO LATER THAN 34926 TCA AS PER AVRO FAX DJR/RJ1322-96, ANGLE MANUFACTURED OF L166 MATERIAL. REMOVED AND REPLACED ABOVE BAFFLE ANGLE USING .040 L166 (2024 T3) AND SRM.

Part: MOUNT BOLT — DAMAGED (LT ELEVATOR)

LEFT ELEVATOR NR 2 HINGE A FRAME UPPER MOUNT BOLT FAILS DETAILED VISUAL INSPECTION. REPLACED UPPER MOUNT BOLT WITH SERVICEABLE BOLT.

Part: JAMB — CRACKED (NR 4 ENGINE)

NR 4 ENGINE RIGHT FAN DOOR BOTTOM EDGE MEMBER NEEDS A CRACK DRESSED OUT AND TREATED. DRESSED OUT DOOR EDGE MEMBER CRACK AT REQUESTED AT THIS TIME. REPAINTED ENTIRE AREA OF REPAIR. PERFORMED EC ON AREA ABOVE THAT WAS DRESSED OUT AND FOUND IT TO BE CRACK FREE 8/4/97.

Part: MOUNT PLATE — CRACKED (RT SPOILER)

LIFT SPOILER VALVE MOUNT PLATE CRACKED IN RT WING ROOT. REMOVED VALVE, REPLACED PLATE AND REINSTALLED VALVE, GEN W/C DO LEAK AND OPS CHECK.

Part: STIFFENER — CRACKED (LT WING)

LEFT WING TRAILING EDGE AREA AFT OF REAR SPAR BETWEEN WING RIBS NR 7 AND 8 HAS AN UPPER SKIN STIFFENER THATS CRACKED AT FORWARD END. REPAIRED IAW ATTACHED FAXES RA/RJO595-97 AND OTHERS RELATED.

Part: SMOKE HOOD — DAMAGED (CABIN)

REQ MAINTENANCE CHECK, AFT PBE FOR SERVICEABILITY. REMOVED AND REPLACED AFT PBE MAS ASSY. (M)

Part: TMS — SMOKING (COCKPIT)

DURING PREFLIGHT, OBSERVED ELECT SMOKE COMING FROM UNDER NR 2 NAV SEL AREA OF GLARESHIELD. ELECT ODOR ALSO NOTED. DEPOWERED AIRCRAFT, INSPECTED GLARESHIELD WIRING, FO'S PANEL, MWS PBSI, CTR PANEL, NO EVIDENCE OF OVERHEATING, OR SMOKE, PULLED THRUST MANAGEMENT SYSTEM CDU, SMELLED SMOKE ODOR, RECOLLARD DEACT TMS SYS C/B'S, REPOWERED A/C, OPS LTS AND SYSTEMS, NO SMOKE OR ODOR.

Part: AIR DISTRIBUTION — ODOR (COCKPIT)

NOTICED ODOR COMING FROM F/O'S GLARESHIELD. REPOSITIONED INSULATION FROM F/O'S INSTRUMENT PANEL. NO OTHER DEFECTS NOTED. (M)

Part: COFFEEMAKER — FAILED (GALLEY)

AFTER LANDING NOTICED ODOR IN COCKPIT AND CABIN. COMPLIED PACK BURN OUT CHECK. INSPECTED ALL C/B PANELS NO DEFECTS NOTED. REPLACED SUSPECT COFFEEMAKER. ODOR DID NOT REOCCUR. (M)

Part: GIRT BAR — FROZEN (SERVICE DOOR)

RIGHT FORWARD SERVICE DOOR SLIDE WILL NOT DISARM. NOTED GIRT BAR FROZEN AT THE FLOOR ABUTMENTS DUE TO EXCESSIVE WATER/ICE SPILLAGE ON THE FLOOR IN THE GALLEY AREA. INSPECTED AND OPERATED THE DOOR AND ASSOCIATED ARMING AND DISARMING MECHANISMS NUMEROUS TIMES. NO DEFECTS NOTED. (M)

Part: CIRCUIT BOARD — FAILED (E/E/ BAY)

DEN - FLT 584 - ON LANDING ROLL-OUT, MAN. SPLR. FAULT AND GREEN FAIL LIGHTS ILUM. YEL SPLR DEPLOYED. CORRECTIVE ACTION: REF W.C. NR 10 FOR WORK PERFORMED. OHMED WIRES FROM GA42 AND GA43 TO AND THROUGH SQUAT SWITCHES. CYCLED GEAR DURING OHM CHECK. TESTED SYS FOR PROPER OPS AND NO FAULT FOUND. REMOVED AND REPLACED PCB GA42 AND GA43 AND RELAY GA19 FOR PRECAUTION TIS. SYS TESTED GOOD. S/N OFF: 119433/91136. S/N ON: 109661/117011.

Part: CIRCUIT BOARD — FAILED (E/E BAY)

DEN - FLT 584 - ON LANDING ROLL-OUT, MAN. SPLR. FAULT AND GREEN FAIL LIGHTS ILLUM. YEL SPLR DEPLOYED. CORRECTIVE ACTION: REF W.C. NR 10 FOR WORK PERFORMED. OHMED WIRES FROM GA42 AND GA43 TO AND THROUGH SQUAT SWTICHES. CYCLED GEAR DURING OHM CHECK. TESTED SYS FOR PROPER OPS AND NO FAULT FOUND. RMEOVED AND RPELACED PCB GA42 AND GA43 AND RELAY GA19 FOR PRECAUTION TIS. SYS TESTED GOOD. S/N OFF: 119488/91136. S/N ON: 109661/117011.

Part: FRAME — CRACKED (FUSELAGE)

ATW - UPPER FRAME STRUCTURE AFT OF FRAME NR 50 HAS AN APPROXIMATE 2 INCH LONG CRACK IN FLANGE RADIUS ON LT CORNER. CORRECTIVE ACTION: FABRICATED PARTS FOR REPAIR ON AUXILIARY UPPER FRAME STRUCTURE LT SIDE PER FAX DJH/RJ0749-96. INSTALLED REPAIR PER FAX DJH/RJ0749-96.

Part: RIVETS — LOOSE (VERT STAB)

ATW - LAST 3 RIVETS ON THE VERTICAL STABILIZER TO FUSELAGE CLOSING ANGLE ARE SMOKING (RT). CORRECTIVE ACTION: REMOVED AND REPLACED RIVETS. ON LAST RIVET (MOST AFT) INSTALLED HI LOC BOLT. HLT900-6. GENERATED W/C FOR REINSP PER FAX DJH/RJ0768-96.

Part: WINDOWS — SCRATCHED (CABIN)

ATW - ALL CABIN WINDOWS ARE CRAZED OR SCRATCHED. CORRECTIVE ACTION: REMOVED CABIN WINDOW CRAZING AND SCRATCHES BY POLISHING AND SANDING. SEVEN WINDOWS WERE REPLACED DUE TO BEING OUT OF LIMITS AFTER REMOVAL OF SCRATCHES. UT INSP CABIN WINDOWS WITHIN LIMITS MM. RETURN TO SERVICE 7-5-96.

Part: LONGERON — CRACKED (FUSELAGE)

ATW - RT STRUCTURE AFT OF FRAME 50, THERE IS A DIAPHRAGM BETWEEN THE UPPER AND LOWER SPEED BRAKE LOWER HINGE LONGERONS THAT HAS A CRACK IN THE LIP OF ITS LIGHTNING HOLE, APPROXIMATELY .3750 INCH LONG. CORRECTIVE ACTION: STOP DRILLED CRACK END PER AVRO FAX. NO CRACKS. GEN WC FOR 2000 CYC REINSP. PERF'D ET AND LOCATED END OF CRACK.

Part: SKIN — DENTED (CARGO DOOR)

ATW - FORWARD CARGO DOOR HAS DENT CHAFE ON INNER LINER SKIN FROM TRIM SCREW ADJACENT TO PANEL I802. C/A: INSTALLED PATCH PER 146 SRM 51-71-11, PAGE 4.

Part: RIB — MISDRILLED (LT WING)

ATW - REF RIL HC571H9033 AT POSITIONS LT WING RIB 2 OTBD HOLE 'A' AT STRS 2 AND 5 AND RT WING RIB 2 INBD STR 2 HOLE 'E' AND RT WING RIB 2 OTBD STR 5 HOLE 'A' HAVE BEEN OVERSIZED TO .3750 INCH TO ACCEPT A MRL3210-12 FASTENER. REF 9002. CORRECTIVE ACTION: INSTALLED OVERSIZED MRL3210-12 FASTENER IN FUEL TANK WING STRINGERS. RT WING 2E, RT CTR 5A BOTH AT RIB 2, LT WING 2A AND 5A, BOTH AT RIB 2.

Part: RAIL — CORRODED (AIRSTAIRS)

ATW - PER AVRO FAX JM/RJ0562-96 DATE 5-13-96, FORWARD AIRSTAIR RAIL (FLOOR RAIL) CORROSION. CORRECTIVE ACTION: REMOVED AND REPLACED INBD AND OTBD FWD AIRSTAIR RAILS.

Part: BOLTS — DAMAGED (LT WING)

ATW - INSPECT ATTACHMENT BOLTS AND NUTS OF THE REAR SPAR ROOT JOINT ATTACHMENT FITTINGS AT RIB 2 IAW EO E92/083/657C. CORRECTIVE ACTION: C/W EO E92/083/657 REV C AND REPLACED BOLT WASHER AND NUT IN POSITION E, LT REAR WING SPAR. GENERATED CARD FOR LEAK CHECK. SEALED INSIDE OF TANK IN POSITION E.

Part: JO BOLT — LOOSE (LT/RT WING)

ATW - REPLACED JO BOLT AT RIB 2 AND RIB ZERO PER BAE REPAIR INSTRUCTIONS HC571H9033. CORRECTIVE ACTION: REMOVED AND REPLACED ALL JO BOLTS AT RIB 2 (LT AND RT) STRINGER CROWNS AND RIB ZERO STRINGER CROWNS. ALL WORK PERFORMED PER BAE 146 REPAIR INSTRUCTIONS HC571H9033. SEE ADDITIONAL WC'S FOR OPS CHECK AND FUEL PIPE REINSTALLATION.

Part: RIVETS — LOOSE (FUSELAGE)

ATW - BOTH ANGLE BRACKETS OR CLEATS BOTTOM OF FR 50 LOOSE. CORRECTIVE ACTION: REPLACED RIVETS.

Part: SKIN — DENTED (FUSELAGE)

ATW - REF TASK NR 920003151 ZONAL INSP OF LT AIRBRAKE FOUND NUMEROUS DENTS IN OUTER SKIN. CORRECTIVE ACTION: TRANSFERRED TO W/O BU5057. SEE LOG PAGE 30183 FOR ROB TRANSACTION.

Part: ENGINE — FAILED (NR 1)

NR 1 ENGINE VIB INDICATION WENT TO 2.4 FOLLOW BY ERRATIC TGT READING, SHUTDOWN PER ABNORMAL CHECKLIST. REMOVED AND REPLACED NR 1 ENGINE IAW MM. GROUND RAN AND LEAK CHECK OK. (M)

Part: WIRE — LOOSE (LANDING GEAR)

ATW - FLT 322 - GEAR WOULD NOT RETRACT. GEAR HANDLE COULD NOT BE RAISED NORMALLY OR IN OVERRIDE. MANUAL SPOILER FAULT LIGHT ILLUMINATED, WENT OUT WHEN AIRCRAFT LANDED. RESOLDERED 2 WIRES IN RAYCHEM CONNECTOR 131-13-00 DL PINS A1 AND A5. REMOVED AND REPLACED GEAR SELECTOR HANDLE AND CHECKED GEAR FOR PROPER OPERATION.

Part: WINDOW SEAL — TORN (LT COCKPIT)

ATW - FLT 300 - LOUD AIRSPEED RELATED NOISE IN COCKPIT COMING FROM CAPTAIN'S SIDE WINDOW. AIRCRAFT RETURNED TO ATW. REMOVED AND REPLACED CAPTAIN'S DV WINDOW SEAL. SEAL WAS TORN.

Part: AIR VALVE — STUCK (NR 1 ENGINE)

DEN - FLT 366 - NR 1 ENGINE AIR VALVE STUCK OPEN AT ALTITUDE. CLEANED POPPET VALVE - NO FIX, REPLACED THE VALVE.

Part: MAIN GEAR — ICED UP (LT MLG)

LEFT GEAR STAYED DOWN COULD FEEL THE YAW, SHOWED GEAR GEAR INTRANSIT. CLEANED ICE FROM GEAR, SWUNG GEAR SEVERAL TIMES. (W)