N616AW

Part: CABLE — UNSERVICEABLE (UPPER PYLON)

NR 2 THRUST LEVER WILL NOT MOVE BELOW CRUISE AT 31K (31,000 FEET), OK AFTER 14K (14,000 FEET). REMOVED AND REPLACED UPPER PYLON TELEFLEX CABLE. ON INSPECTION OF THE UNSERVICEABLE TELEFLEX CABLE. CONFIRMED THAT A CRIMP ALONG THE LENGTH OF THE CABLE CAUSED IT TO BIND, POSSIBLEY CAUSED DURING MAINTENANCE. NO OTHER ADVERSE CONDITIONS OR TRENDS NOTED. (M)

Part: BLEED BAND — OUT OF TOLERANCE (NR 2 ENGINE)

UPON APPLICATION OF TAKEOFF POWER, NR 2 ENGINE DID NOT RESPOND WHILE TGT WENT TO 950 DEGREES FOR AN ESTIMATED 5 SECONDS BEFORE SECURING. MAINTENANCE FOUND NR 2 ENGINE BLEED BAND OUT OF TOLERANCE. ADJUSTED AS REQUIRED AND PERFORMED 4 POINT RUN. ALL RUNS WITHIN PARAMETERS IAW MM.

Part: ATTACH ANGLE — CRACKED (FUSELAGE)

FLOOR BEAM TO CROSSMEMBER ATTACH ANGLE CRACKED AT STA 183.15 FORWARD SIDE AND LBL 47 OUTBOARD SIDE. CROSSMEMBER ATTACH ANGLE REPLACED IAW SRM.

Part: SKIN — DENTED (FUSELAGE)

DENT IN A VERTICAL DIRECTION AT STRINGER 26L BETWEEN FRAME 12 AND 13. FABRICATED A REPAIR PATCH. PERFORMED A DETAILED VISUAL INSPECTION TO ENSURE SOUND CRACK FREE STRUCTURE REMAINS.

Part: BRACKET — CRACKED (LT SPOILER)

LEFT INBOARD SPOILER OUTBOARD END BRACKET CRACKED AT FORWARD TOP EDGE. CARRIED OUT IAW MFG NWH/RJ/0723-02.

Part: DOOR — CRACKED (NR 4 COWLING)

NR 4 ENGINE INBOARD AFT COWL DOOR HAS A CRACK NEXT TO DRAIN TUBE. REPAIRED CRACK IAW BAE PROCEDURE REF NR NWH/RJ/0726-02 AND RIL HC7IIH9012. (M)

Part: RETAINER — DAMAGED (E/E BAY DOOR)

ELECTRICAL EQUIPMENT BAY DOOR RETAINING ANGLE ON FORWARD FRAME DAMAGED. ANGLE REPAIRED IAW BAE PROCEDURE REF NR CH/RJ/0734-02. (M)

Part: STRUCTURE — CHAFED (PAX DOOR)

FOUND LEFT AFT PAX DOOR AIRSTAIR HOOK CUTOUT HAS CHAFING FROM HOOK. REPAIRS CARRIED OUT IAW BAE PROCEDURE REF NR CH/RJ/0735/02. (M)

Part: CAGE — CRACKED (CARGO DOOR)

REAR CARGO DOOR UPPER AFT INNER SEAL RETAINER CAGE IS CRACKED APPROX 2 INCHES IN LENGTH. REPLACED UPPER AFT INNER CAGE IAW SRM 51-42-00. REPAIRS CARRIED OUT PER BARA/AVR/5007/00. (M)

Part: FRAME — CHAFED (NR 3 COWLING)

NR 3 ENGINE FORWARD INBOARD COWL DOOR HAS CHAFE MARKS ON FORWARD MOST FRAME. REPAIRED IAW BAE RIL HC711H9089. (M)

Part: TRIM TAB — DENTED (LT AILERON)

DENTS FOUND IN LEFT AILERON TRIM TAB. INSPECTION CARRIED OUT IAW MM.

Part: PANEL — DENTED (RT WING)

DENTS FOUND IN LEFT AND RIGHT WINGS TRAILING EDGE PANELS BETWEEN RIB 14A AND 15B. INSPECTION CARRIED OUT IAW MFG MM.

Part: A/C PACK — ODOR (NR 2) · airframe 23,411 hrs · 31,644 cycles

SMOKY SMELL IN CABIN AFTER TAKEOFF, CREW SHUT OFF APU AIR AND SWITCHED TO ENGINE AIR, OPERATED ON NR 2 PACK AND SMOKY SMELL DISSIPATED. MAINTENANCE PERFORMED DUCT CONTAMINATION CLEARING PROCEDURE COULD NOT DUPLICATE SMELL, SYSTEM OPERATES NORMALLY ON ALL ENGINES AND APU AIR.

Part: DOOR WARNING — ACTIVATED (LT MLG)

AFTER GEAR RETRACTION, LEFT MAIN GEAR INTRANSIT LIGHT 'RED' REMAINED ON AND RED LT IN GR HANDLE. COULD NOT DUPLICATE MEGGED AND UPLOCK HARNESSES. GEAR UPLOCK, 50M OHM EACH DOOR UPLOCK .5M OHM. REMOVED AND REPLACED HARNESS, FROZE SENSORS, CLEANED SENSORS, ONE DOZEN GEAR SWINGS ALL GOOD. (M)

Part: PAN — BROKEN (PILOT SEAT)

CAPTAIN'S SEAT ASSY SEAT PAN BROKEN AT FWD RT CORNER. PAN ALSO HAS SEVERAL OTHER CRACKS. MADE NEW SEAT PAN IAW PS1 DRAWING AW-25-10-9707-06 INSTALLED PER DRAWING ALSO.

Part: HINGE — CRACKED (NR 2 TE FLAP)

DURING ADJUSTMENT/CHECK OF RT NR 2 CARRIAGE FLAP CANOE, FOUND HINGE ASSY CRACKED AT TOP FORWARD TRANSVERSE BEAD. DRESSED OUT CRACKED AREA (JM/RJ085-97). C/W FLUORSCENT DYE PENETRANT AND EDDY CURRENT INSPECTIONS. INSPECTED ENTIRE HINGE ASSY FOR CRACKS, NO DEFECTS EVIDENT. REPAIRED IAW JM/RJ0850-97. INSPECTED ALL ATTACHMENTS AND STRUCTURES, FOUND OK IAW BAE 146 MM.

Part: BRACKET — CRACKED (FUSELAGE)

PSU RAIL RT OTBD, STAND-OFF BRACKET AT FRAMES 39-40 CRACKED AND RIVETS LOOSE. REPLACED BRACKET.

Part: BULKHEAD FRAME — CHAFED (PRESS BULKHEAD)

THERE IS AN L-SHAPED CHAFE MARK ON FRAME 32 PRESSURE BULKHEAD, NEAR CENTERLINE BEHIND RT MLG DOOR UPLOCK ASSY. NEEDS INVESTIGATION. BLENDED ABOVE AREA IAW BAE FAX JM/FJ0844-97. REPROTECTED, PRIMED AND PAINTED.

Part: BRACKET — CRACKED (PASSENGER DOOR)

FORWARD PASSENGER DOOR - DOOR HANDLE SUPPORT BRACKET CRACKED. CHECKED WITH ET CRACK DEFECT NOTED. ITEM MARKED WITH TAG. MFG ABOVE BRACKET PER BAE DRAWING AND PS1 PN AW524H970206-000. INSTALLED PER SRM AND BAE FAX DJR/RJ0318-97 2 EACH UNF BOLTS.

Part: FRAME — CRACKED (FUSELAGE)

ATW - RIGHT SIDE OF ECS BAY AT FRAME NR 47 HAS A CRACK IN THE SHEAR ANGLE AT STR 9 THAT IS APPROX .25 INCH LONG IN THE BEND RADIUS. NOTE: VERIFIED WITH EDDY CURRENT. REPAIR SHEAR ANGLE IAW BAE REPAIR INSTRUCTIONS HC539H9014.

Part: INTERCOSTAL — CRACKED (CABIN)

REAR FUSELAGE AREA - CENTER FLOOR SUPPORT INTERCOSTAL CRACKED UNDER GUSSET PLATE BETWEEN FRAMES 41 AND 43. MARKED WITH GREEN DOT. REPAIRED INTERCOSTAL IAW BAE FAX REF DJR/RJ0839-97.

Part: RIB — CRACKED (LT WING)

ATW - LT WING TIP REMOVEABLE RIB PANEL HAS A FEW CRACKS IN IT. PATCHED SAID CRACKS IAW BAE STD PRACTICES AND AIR WISC MM PSI REF: AW-57-20-9412-06.

Part: ANGLE — CRACKED (CARGO COMPT)

REAR CARGO BAY FLOOR SUPPORT ANGLE CRACKED AT SCREW HOLE FRAME 34. SPLICED 8 INCH SECTION TO SUPPORT ANGLE PER SRM 51-71-11, DAMAGED AREA REMOVED.

Part: STIFFENER — CRACKED (LT WING)

LT WING, TRAILING EDGE AND SHROUD UPPER SKIN STIFFENER IS CRACKED AT FORWARD END IN AREA BETWEEN WING RIBS 7 AND 8. REPAIRED STIFFENER REF FAX JM/RJ0818-97. (M)

Part: STIFFENER — CRACKED (RT WING)

RT WING TOP TE SKIN STIFFENER CRACKED AT FWD END AT RIB NR 9, JUST INBOARD OF RIB 9. REPAIRED CRACKED STIFFENER IAW FAX NR'S JM/RJ0317/97 AND NR JM/RJO317/97 AND NR JM/RJO818-97. (M)

Part: INTERCOSTAL — BROKEN (CARGO COMPT)

ATW - FORWARD CARGO INTERCOSTAL BROKEN BETWEEN FRAMES 23 AND 23 LT SIDE. REPAIRED INTERCOSTAL IAW BAE 146 SRM AND REINSTALLED IAW BAE 146 SCM. REF: 51-71-11. REPAIRED, OK FOR SERVICE.

Part: STIFFENER — CRACKED (RT WING)

RT WING TOP TE SKIN STIFFENER CRACKED AT FWD END BETWEEN RIBS 8/9, JUST OUTBOARD OF RIB 8. REPAIRED CRACKED STIFFENER IAW FAX NR'S JM/RJO317/97 AND NR JM/RJO818-97. (M)

Part: STIFFENER — CRACKED (RT WING)

ATW - RIGHT WING TOP T/E SKIN STIFFENER CRACKED AT FWD END JUST INBD OF RIB NR 8. REPAIRED STIFFENER, REF FAX JM/RJ0317/97, AND JM/RJ0818-97.

Part: WEB — CRACKED (FUSELAGE)

RT SIDE OF STRUCTURE AFT OF FRAME NR 50 HAS A WEB THAT RUNS VERTICALLY FROM THE REAR FLANGE OF FRAME NR 50 DOWN TO THE LOWER BLADE OF THE SPEED BRAKE HINGE THAT HAS A SMALL CRACK ACROSS THE UPPER TOP RIVET HOLE AT OUTER FLANGE. CRACK VERIFIED WITH EDDY CURRENT AND PENETRANT INSPE P/N OF FR IS HC539J0027-001. REPAIRED WEB, DIAPHRAM IAW BAE SRM 51-71-11. (M)

Part: FRAME — CRACKED (FUSELAGE)

LEFT SIDE OF STRUCTURE AFT OF FRAME 50 HAS A FRAME ABOVE THE UPPER HINGE BLADE FOR SPEED BRAKE THAT HAS A CRACK ACROSS THE 3RD RIVET HOLE DOWN ON OUTER FLANGE THAT ATTACHES TO SKIN. VERIFIED WITH EDDY CURRENT. REPLACED LEFT UPPER WEB DIAPHRAM. (M)

Part: FRAME — CRACKED (FUSELAGE)

ATW - RIGHT SIDE OF STRUCTURE AFT OF FR 50 HAS A FRAME THAT IS CRACKED LOCATED ABOVE UPPER HINGE BLADE FOR AIRBRAKE BACKSIDE OF FR 50. CRACK IS UNDER OUTER CORNER OF GUSSET PLATE ACROSS THAT RIVET HOLE AND GOES INWARD TO INNER AND EDGE OF FRAME. REPLACED UPPER RIGHT WEB DIAPHRAGM.

Part: INSERTS — CORRODED (FWD LAVATORY)

FORWARD LAV MODULE, METAL INSERTS IN FLOOR CORRODED. REPLACED AS NEEDED. INSTALLED PERMACEL AFTER REPLACMENT OF INSERTS. REPLACED INSERTS AS NEEDED AND INSTALLED NEW PERMACEL ON UNDER SIDE OF FORWARD LAV MODULE.

Part: BRACKET — CRACKED (NR 2 ENGINE)

NR 2 ENGINE SHOULDER COWL TERMINAL BOARD FWD BRACKET CRACKED. REPLACED NR 2 ENG SHOULDER COWL TERMINAL BOARD FWD BRACKET.

Part: ANGLE — CRACKED (RT WING)

ATW - RT WING T/E LOWER SKIN STIFFENER AFT TAG ANGLE CRACKED BETWEEN RIBS 3 AND 4. REPLACED ANGLE.

Part: BRACKET — BROKEN (COCKPIT)

FWD CLOSET WALL BEHIND FO'S SEAT, LOWER CORNER ATTACH BRACKET BROKEN. FABRICATED AND REPLACED FWD CLOSET WALL BRACKET BEHIND FO'S SEAT (LOWER ATTACH BRACKET).

Part: ANGLE — CRACKED (RT WING)

RT WING T/E LOWER SKIN STIFFENER AFT TAG ANGLE CRACKED AT RIB NR 4. REPLACED ANGLE.

Part: ANGLE — CRACKED (RT WING)

ATW - RT WING T/E LOWER SKIN STIFFENERS AFT TAG ANGLE CRACKED BETWEEN RIBS 5 AND 6. REPLACED ANGLE.

Part: SILL — CORRODED (SERVICE DOORWAY)

AFT VESTIBULE SILL PLATE FOR SERVICE DOOR SIDE HAS SEVERAL SPOTS OF CORROSION. REMOVED AND REPLACED AFT VESTIBULE SERVICE DOOR SILL PLATE.

Part: SEAL CAGE — CRACKED (CARGO DOOR)

REAR CARGO DOOR LOWER AFT SEAL CAGE CRACKED. REPLACED LOWER AFT SEAL CAGE.

Part: BOLTS — LOOSE (WING RIB)

ATW - AIR WISC EO E92/083/657 RECC ATTACH BOLTS AND NUTS ON RT SIDE, A, B, C, D ARE LOOSE ON THE REAR SPAR ROOT ATTACHMENT FITTING AT WING RIB 2. REPLACED FASTENERS IAW BAE REPAIR INSTRUCTIONS HC53H9043. BOLTS A, C, D ORIG SIZE. BOLT B FIRST OVERSIZE, RESEALED SRV CNTR TANK FOR LEAK CHECK CARD J029 FAX JM/RJ0808-97. ACCEPTABLE USE HLT FASTENERS.

Part: MOUNTING — CRACKED (RT SPOILER)

ATW - RT LIFT SPOILER VALVE MOUNTING PLATE CRACKED. REMOVED AND REPLACED RT SPOILER VALVE MOUNTING PLATE. NO DISCONNECTING OF VALVE REQUIRED.

Part: COWL — CHAFED (NR 2 ENGINE)

NR 2 ENGINE LT FWD COWL DOOR AFT FRAME CHAFED AT LATCH AREA AND AT MID-AREA DUE TO CONTACT WITH HYDRAULIC LINE. REPLACED CAP STRIP ON NR 2 ENG LT FWD COWL DOOR AFT FRAME.

Part: FLOOR — BUCKLED (CABIN)

REF FAX LM/115-97, LM/116-97, JM/RJ0096-97, AND DJR/RJ0098-97. MLG PRESS FLOOR BETWEEN FRAMES 29 AND 32 OTBD SEAT RAILS 19 INCHES, 20 INCHES OTBD CENTERLINE HV BUCKLE APPROX .125 INCH DEEP. DV DUE EA 500 CYC. REPORT FINDINGS AI (R) REMOVE FLOOR STS. CUR 23082, DUE 23583 CYC. PERFORMED DV INSP MINOR BUCKLE MLG PRESS FLOOR TOP/BOTTOM SURFACES. NO DEFECTS NOTED PER BAE FAX JM/RJ0808-97. REPAT INSP 1,000 FLIGHTS.

Part: SUPPORT — CRACKED (CARGO COMPT)

FRONT CARGO BAY CENTER CARGO FLOOR SUPPORT AT 19C CORRODED AND CRACKED. AREA MARKED. REPLACED FREIGHT ANGLE AT FR 19C IAW BAE 146 SRM.

Part: JOBOLTS — DAMAGED (RT WING)

REPLACED JOBOLTS ON RT WING CENTER TANK RIB 2 INBOARD PER RIL HC571H9033. PERFORMED RIL HC571H9033 TO RIB 2 INBD CENTER TANK. REPLACED JOBOLTS WITH MRL FASTENERS.

Part: BRACKET — CRACKED (LT WING)

ATW - LT WING BRACKET FOR HYD LINES THAT PASS THROUGH THE AFT END OF THE SPOILER HINGE RIB AT WING RIB NR 5 IS CRACKED. REPLACED BRACKET.

Part: ANGLE — CRACKED (FUSELAGE)

FREIGHT ANGLE AT FRAME 19D CRACKED CENTER SECTION. REPLACED FREIGHT ANGLE AT FRAME 19D IAW BAE 146 SRM.

Part: JOBOLTS — DAMAGED (LT WING RIB)

PERFORM RIL HC571H9033 LT RIB 2 OUTBOARD. PERFORMED RIL HC571H9033 TO LEFT RIB 2 OUTBOARD (WING TANK) SIDE. REPLACEMENT OF JOBOLTS WITH MRL FASTENERS. (M)

Part: JOBOLTS — DAMAGED (LT WING)

ATW - PERFORMED RIL HC571H9033 LT RIB 2 INBD (JOBOLTS). PERFORMED RIL HC571H9033 LT RIB 2 INBD (CENTERTANK) SIDE. REPLACEMENT OF JOBOLTS WITH MRL FASTENERS.

Part: JOBOLTS — DAMAGED (LT WING)

ATW - PERFORMED RIL HC571H9033 LT CENTER TANK RIB ZERO (JOBOLTS). C/W RIL 571H9033 TP; LT SIDE RIB ZERO. REPLACEMENT OF JOBOLTS WITH MRL FASTENERS.

Part: JOBOLTS — DAMAGED (RT WING)

JOBOLTS ON RIGHT CENTER TANK RIB ZERO NEED TO BE REPLACED PER RIL HC571H9033. C/W RIL HC571H9033 RT CENTER TANK RIB ZERO REPLACING OF JOBOLTS.

Part: ANGLE — CRACKED (FUSELAGE)

MLG BAFFLE UPPER SUPPORT ANGLE FWD END HAS A 2.3750 INCH LONG CRACK THROUGH 3 RIVETS. SEE FAX LM/115-97, JM/RJ0096-97, LM/116-97, LM/116-97, AND DJR/RJ0098-97. TO BE REPAIRED AT HEAVY CHECK. REPLACED UPPER ANGLE.

Part: GUSSET — CRACKED (FUSELAGE)

SUB FRAME AFT OF FRAME 50 LOWER OUTBOARD LEFT CORNER GUSSET PLATE CRACKED. REPLACED GUSSET PLATE. (M)

Part: SHROUD — CRACKED (LT WING)

ATW - LT WING UPPER TRAILING EDGE SHROUD LOWER LIP HAS A 2 INCH CRACK IN IT IN AREA BETWEEN WING RIBS 5 AND 6. REF: W/C NR 5042 FOR SHEET METAL FORMING AND HEAT TREATING TO 2024T-81 SPEC. REPAIRED IAW FAX DJR/RJ0192-97 ISS 2.

Part: FRAME — CRACKED (FUSELAGE)

ATW - SUB-FRAME OF FRAME 50 LOWER OTBD LT CORNER CRACKED AND HAS A PIECE MISSING FRAME FLANGE. REPAIRED IAW BAE FAX REF GCR/0746/97, DJH/RJ0749-96 AND DJH/RJ0781-97.

Part: RIB — CRACKED (NR 4 PYLON)

IN PYLON NR 4 RIB NR 5 IS CRACKED IN THE LOWER FLANGE RADIUS NEAR THE PYLON CENTERLINE. VIEW THROUGH ACCESS PANEL NR 482CL, .250 INCH LONG. REF RIL HC546H9018 .25 INCH CRACK REPORTED RIB 5 NR 4 PYLON MAY REMAIN IN SERVICE GENERATED W/C FOR REINSPECTION. (M)

Part: RIB — BROKEN (RT WING)

SMALL ALUMINUM BRACKET AT RT WING TIP RIB 20 BROKEN TAB, BRACKET IS USED FOR CONDUIT TUBE AT FLUX VALVE WIRING. FABRICATED BRACKET PER DRAWING HC923H0759 AND REPLACED BRACKET AT RIB 20 IAW BAE 146 SRM.

Part: SILL — CORRODED (PAX DOOR)

AFT PASSENGER DOOR SILL PLATE CORRODED. REPLACED SILL PLATES AFT PASS DOOR. (M)

Part: BOLT — CHIPPED (RT SPOILER)

ATW - BOLT AT RT CENTER LIFT SPOILER AFT JACK ATTACH POINT HAS CHROME PLATING CHIPPING OFF. REF: SSI 57-51-116. INSTALLED A NEW BOLT IN RT MID-SPOILER AFT JACK ATTACH POINT.

Part: SWITCH — CORRODED (AVIONICS FAN)

FORWARD CARGO AVIONIC FAN PRESSURE SWITCH CORRODED. REMOVED AND REPLACED AVI-FAN PRESS SWITCH IAW BAE146 MM. GEN W/C FOR OPS CHECK. REF: W/C NR 1061.

Part: LONGERONS — CRACKED (MLG WW)

FRAME 29 MLG BAY PRESS FLOOR LONGERONS NR 3 AND 18 CRACKED AT FWD END. REPAIRED CRACKS IAW BAE REPAIR DRAWING HC536H9211 AND BAE FAX REF DJR/RJ0207-97.

Part: THERMOSTAT — FAILED (RUDDER)

DIODE UNDER PANEL 323AR HAS TERMINAL END CORRODED OFF (DIODE IS TAGGED). REPLACED RUDDER DAMPER HEATER THERMOSTAT HV3.

Part: SKIN — DAMAGED (FUSELAGE)

TWO EACH SKIN CREASES BETWEEN RT FRAME 19D AND FRAME 20 ABOVE AND FWD OF A PREVIOUS PATCH REPAIR DUE RE-INSPECTION PER FAX DJR/RJ0657 EVERY 360 CYCLES UNTIL REPAIR AT NEXT HEAVY CHECK. CURRENT CYCLES 23,083, DUE REINSPECTION AT OR BEFORE 23,443 TCA. REPAIRED. REF: W/C 80808/58 NR 120. NO FURTHER INSPECTION REQUIRED.

Part: SKIN — CREASED (FUSELAGE)

TWO EACH SKIN CREASES ABOVE/FWD OF A PREVIOUS PATCH REPAIR BETWEEN FRAMES 19D AND 20 ON THE RT FUSELAGE DUE REPAIR AT NEXT HEAVY CHECK PER FAX DJR/RJ0657-97. A REPAIR SCHEME REQUEST WAS SUBMITTED THIS DATE. DUE REPAIR BY NEXT HEAVY CHECK OR 12/97 WHICH EVER SOONER. REPAIRED IAW BAE SRM 53-00-12 FIG 202.

Part: JOBOLTS — DAMAGED (RT WING)

REPLACED JOBOLTS ON RIGHT WING CENTER TANK RIB 2 OUTBOARD PER RIL HC571H9033. PERFORMED RIL HC571H9033 TO RIGHT WING RIB 2 OUTBOARD. REPLACED JOBOLTS WITH MRL FASTENERS.

Part: NAV LIGHT — BROKEN (AFT FUSELAGE)

LOWER ONE-THIRD OF TAIL NAV BROKEN. REPLACED TAIL LIGHT ASSY LIGHTS AND STROBE, CHECKED GOOD CLEARANCES CHECKED IAW 27-63-24 PAGE 209.

Part: SEAL — LEAKING (NR 2 PACK)

ATW - FLT 515 - LEFT ZONE HI-TEMP LIGHT ILLUMINATED, NR 2 PACK AUTO SHUT DOWN WITH APU AIR ON. INSPECTION FOUND PERISEALS LEAKING AT COUPLING OF VERTICAL FIN TO FUSELAGE. REMOVED AND REPLACED PERISEALS. OPS CHECKS GOOD.

Part: RETRACT MECH — MALFUNCTIONED (TE FLAPS)

ORD - FLT 562 - FLAPS FAULTED AND STUCK AT APPROXIMATELY 16 DEGREES ON APPROACH TO ORD. CLEARED FLAP FAULT.

Part: RETRACT MECH — MALFUNCTIONED (TE FLAPS)

FLAPS FAULTED AND STUCK AT APPROX 16 DEGREES ON APPROACH. CLEARED FLAP FAULT.

Part: PBE — MALFUNCTIONED (CABIN)

DEN - FLT 580 - PLEASE INSPECT TOP FORWARD CABIN PBE FOR SERVICEABILITY. CORRECTIVE ACTION: REMOVED AND REPLACED PBE TOP FORWARD CABIN. S/N OFF E9445482. S/N ON V8916022.

Part: RETRACT MECH — MALFUNCTIONED (TE FLAPS)

ORD - FLT 528 - AFTER TAKEOFF DURING CLIMB-OUT OF ORD, FLAPS WOULD NOT RETRACT FROM 18 DEGREES. FLAP FAULT AND INOP CAPTIONS ILLUMINATED. AIRCRAFT RETURNED TO ORD. CORROECTIVE ACTION: PERFORMED CLEARING PROCEDURE AND SAFETY LANE 2 CHECKS. OPS CHECKS NORMAL.

Part: CONTROL CABLE — CORRODED (LT AILERON)

ATW - LEFT AILERON INTERCONNECT OUTBOARD CABLE NEEDS TO BE REPLACED DUE TO CORROSION. REMOVED AND REPLACED LEFT AILERON INTERCONNECT OUTBOARD CABLE ASSY IAW 27-11-44.

Part: CONTROL CABLE — WORN (RT AILERON)

ATW - RIGHT AILERON INTERCONNECT OUTBOARD CABLE WORN THROUGH TUBING. REMOVED AND REPLACED RIGHT AILERON INTERCONNECT OUTBOARD CABLE ASSY IAW MM 27-11-44.

Part: BULKHEAD — GOUGED (LT MLG WW)

ATW - LT MLG BAY, FRAME 29 BULKHEAD, HAS A GOUGE APPROXIMATELY 7 INCHES LONG WITH 3 DAMAGED RIVET HEADS AND IS APPROXIMATELY .012 INCH DEEP. MEASURED DEPTH AGAIN WITH PAINT STRIPPED. REPAIRED LT MLG AT FRAME 29. REFER TO WC NR 1063 FOR NDT. EPOXY PRIMED AND TOPCOATED. REF FAX HC/137-96 S/N 3145. HC/134-96, JM/RJ0477-96, JM/RJ0473-96, DR/RJ0498-96.

Part: BULKHEAD — GOUGED (RT MLG WW)

ATW - RT MLG BAY FRAME 29 BULKHEAD HAS A GOUGE APPROXIMATELY 8.50 INCHES LONG WITH 4 DAMAGED RIVET HEADS AND IS APPROXIMATEY .009 INCH DEEP. AFTER REMOVAL OF PAINT, RE-MEASURED DEPTH FOUND TO BE .007 INCH DEEP AND REPORTED TO BAE. NDT WAS ACCOMPLISHED ON WC NR 1063. BLENDED, REPLACED 7 RIVETS AND FINISHED, AND TOP COATED AS DESCRIBED IN BAE FAX REF DJR/RJ0498-96 ALLOWABLE PER FAX DJR/RJ0498.

Part: GUSSET — CORRODED (FRAME 20)

ATW - TWO GUSSET PLATES ON FRAME 20, LT SIDE, FOR AIRSTAIR RAILS HAVE SPOTS OF SURFACE CORROSION. OUTBOARD GUSSET HAS SPOT ON UNDERSIDE TOO. REMOVED ALL CORROSION ON GUSSET PLATES ON FRAME 20. TREATED, PRIMED AND PAINTED.

Part: RIVETS — MISSING (FRAME 26)

ATW - FLOOR SUPPORT BEAM AT FRAME NR 26, MOST OUTBOARD LEFT, HAS 2 RIVETS MISSING THAT ATTACH THE ANGLE STRIP TO FRAME UNDER PANEL 231JF. REPLACED 2 EACH RIVETS AT ABOVE MENTIONED LOCATION IAW SRM.

Part: ANGLE STRIP — CORRODED (CABIN FLOOR)

ATW - CABIN FLOOR ANGLE STRIP ON LT SIDE OF CABIN BETWEEN FRAMES 19A AND 20 HAS SEVERAL SPOTS OF SURFACE CORROSION - MARKED WITH BLACK PEN. REMOVED CORROSION, ALODINED, PRIMED AND PAINTED AS REQUIRED ABOVE MENTIONED AREAS.

Part: RIVET — MISSING (SEAT RAIL)

ATW - SEAT RAIL IN CABIN AT FRAME 30, LT OUTBOARD, IS MISSING A RIVET. LOCATED UNDER FLOOR PANEL NR 231NF FORWARD END. (MARKED WITH BLACK PEN). INSTALLED RIVET AT ABOVE MENTIONED LOCATION IAW SRM.

Part: RIVET — NOT INSTALLED (FLOOR SUPPORT)

ATW - FLOOR SUPPORT BEAM IN CABIN AT FRAME 24, RT MOST OUTBOARD END, HAS A RIVET THAT HAS NOT BEEN BUCKED. (MARKED WITH BLACK PEN). BUCKED ABOVE MENTIONED RIVET IAW SRM.

Part: JO BOLTS — LOOSE (CENTER TANK)

ATW - DURING DV INSPECTION OF THE CENTER TANK, EVIDENCE OF LOOSE JO BOLTS WERE NOTED. UPON EVALUATION, NO CORROSION NOTED AND ALL ACCESSIBLE JO BOLTS IN CENTER TANK RIB ON AND LEFT/RIGHT WING TANK RIB 2 WERE TORQUE CHECKED TO 15. DETAILS REPORTED TO AVRO RDO FOR ACCESS. LOOSE JO BOLTS REPORTED AT RIB 2 AND ZERO TO AVRO RDO IS ACCEPTABLE NOW, WITH FUTURE DV INSPECTION AND TIME LIMITED UNTIL REPLACEMENT NO LATER THAN 240.

Part: JO BOLT — BROKEN (STR 12)

ATW - FRAME 29, LEFT FWD FACE AT STR 12, HAS JO BOLT WITH NUT SPINNING. FOUND BOLT HEAD BROKEN. INSTALLED NEW BOLT AND NUT FRAME 29 LEFT FWD FACE, SEALED WITH WITCOBOND 776 PER SRM.

Part: RIB — LOOSE (LT WING)

ATW - LEFT WING, CENTER LIFT SPOILER INBOARD JACK RIBS, HAS LOOSE ATTACH BOLTS (UPPER AFT). SECURED AND SAFTIED BOLTS AT CENTER LIFT SUPPLIER INBOARD JACK-RIB UPPER AFT END.

Part: FLOOR — CORRODED (CABIN)

ATW - FLOOR PLATE OUTBOARD OF FORWARD AIRSTAIR CLOSET HAS SEVERAL PLACES WITH SURFACE CORROSION. REMOVED SURFACE CORROSION AIRSTAIR CLOSET OUTBOARD SILL AREA, TREATED, PRIMED AND PAINTED.

Part: RAIL — DIRTY (FORWARD AIRSTAIR)

ATW - FORWARD AIRSTAIR, OUTBOARD RAIL, AND 2 SUPPORT BRACKETS NEED CLEANING, INSP'D AND CORROSION TREATED AS NEEDED. REMOVED AND REPLACED OUTBOARD RAIL AND CLEANED. INSPECTED SUPPORT BRACKETS AS NEEDED IAW MM.

Part: CHANNEL — CORRODED (FRAME 15)

ATW - UNDER FLOOR STRUCTURE, CHANNEL IS CORRODED THROUGH, LOCATED FORWARD OF FRAME 15 BETWEEN COCKPIT AND FORWARD LAV WALL ON LEFT SIDE OF AVIONICS ACCESS PANEL. REPLACED UNDER FLOOR CHANNEL BY AVIONICS HATCH, LEFT SIDE, FRAME 12 TO FRAME 15 PER SRM.

Part: GUSSET — CORRODED (FRAME 15)

ATW - FORWARD VEST, FRAME 15 TO FLOOR BEAMS, HAS 3 GUSSET PLATES CORRODED. REMOVED AND REPLACED GUSSET PLATES AS NEEDED IAW SRM.

Part: RAIL — CORRODED (FWD AIRSTAIR)

ATW - FORWARD AIRSTAIR INBOARD RAIL IS CORRODED AT FORWARD END. REMOVED AND REPLACED INBOARD RAIL AS NEEDED IAW MM.

Part: STRUCTURE — CORRODED (FWD LAVATORY)

ATW - SEVERAL PLACES CORRODED ON FLOOR STUCTURE UNDER FWD LAV MODULE. REMOVED SURFACE CORROSION ON FLOOR STRUCTURE UNDER LAV MODULE, TREATED, PRIMED AND PAINTED.

Part: CONTROL CABLE — CORRODED (AILERON)

ATW - AILERON INTERCONNECT CABLES ARE CORRODED AT WING ROOT PULLEYS. REMOVED AND REPLACED BOTH CENTER SECTION AILERON INTERCONNECT CABLES. REF W/C 2079 FOR FUNCTIONAL TEST OF AILERON CONTROLS.

Part: SILL — CORRODED (PASSENGER DOOR)

ATW - FORWARD PASSENGER DOOR SILL PLATE CORRODED AND HAS CORNER PIECE BROKEN OFF. REMOVED AND REPLACED FORWARD PASSENGER DOOR SILL PLATE PER SRM.

Part: HINGE — CORRODED (RUDDER)

ATW - VISIBLE PORTION OF RUDDER HINGE BOLTS AT RIBS 20 AND 29 ARE CORRODED. REMOVED NUTS FROM BOLTS, REMOVED MINOR CORROSION, RE-INSTALLED AND SAFETY NUTS.

Part: BULKHEAD STRIP — CORRODED (FRAME 18)

ATW - FRAME 18 RT BULKHEAD FLOOR STRIP HAS SURFACE CORROSION. REMOVED SURFACE CORROSION, ALODINED, PRIMED AND PAINTED ALLOWABLE PER SRM.

Part: NOZZLE — FRACTURED (FUEL PUMP)

ENGINE SHUT DOWN IN-FLIGHT. FOUND NOZZLE FRACTURED AND ENTERED GEARS CAUSING DRIVE SHAFT TO SHEAR. PUMP IS BEING SENT TO C.E.C.O. (MANUFACTURER) FOR INVESTIGATION.

Part: FUEL CONTROL — FAILED (NR 4 ENGINE)

EN ROUTE TO ORD ON FLT 572 AT CRUISE POWER, NR 4 ENGINE DECELERATED BY ITSELF AND FLAMED OUT. ORD MAINTENANCE FOUND FCU SHAFT SHEARED. REPLACED FCU. (M)

Part: DUCT VALVES — MALFUNCTIONED (APU)

DEN - FLT 381 - RIGHT ZONE HIGH-TEMP LIGHT ILLUMINATED IN-FLIGHT. NO LEAKS NOTED IN THE SPINE AREAS. FOUND A LEAK IN THE APU AIR SUPPLY DUCT TO THE Y-DUCT SUPPLYING THE 2 MANIFOLDS. BOTH DUCT RELIEF VALVES NEED TO BE REPLACED. PLACED APU AIR ON MEL. REPLACED THE DUCT RELIEF VALVES. THE FLIGHT CREW FOUND THERE WERE THREE EMERGENCY LIGHTS INOPERABLE. MAINTENANCE REPLACED THE ASSOCIATED POWER SUPPLY.

Part: EEL — INOPERATIVE (CABIN)

DEN - FLT 381 - RIGHT ZONE HIGH-TEMP LIGHT ILLUMINATED IN-FLIGHT. NO LEAKS NOTED IN THE SPINE AREAS. FOUND A LEAK IN THE APU AIR SUPPLY DUCT TO THE Y-DUCT SUPPLYING THE 2 MANIFOLDS. BOTH DUCT RELIEF VALVES NEED TO BE REPLACED. PLACED APU AIR ON MEL. REPLACED THE DUCT RELIEF VALVES. THE FLIGHT CREW FOUND THERE WERE THREE EMERGENCY LIGHTS INOPERABLE. MAINTENANCE REPLACED THE ASSOCIATED POWER SUPPLY.

Part: STRINGER — DAMAGED (BS 29.54)

ATW - C/W E.O. E95/005/653. ORIGINAL ISSUE ON LT AND RT FRAME 29 STRINGERS AT STA 25.94 FOUND DAMAGED. REPAIRED RT FRAME 29 STRINGER AT STA 29.54 IAW E.O. E95/005/653. ORIGINAL ISSUE. REPAIRED LT FRAME 29 STRINGER AT STA 25.94 IAW E.O. E95/005/653. ORIGINAL ISSUE AND AVRO FAX NR DJR/RJ0592-95.

Part: FUEL MANIFOLD — CRACKED (NR 1 ENGINE)

ATW - FOUND CRACK INDICATION ON 5TH SCALLOP OF RIGHT FUEL MANIFOLD, NR 1 ENGINE. P/N 2-163-620-35, S/N 1777P. AIRCRAFT IN HEAVY CHECK, MAINIFOLD TO BE REPLACED.

Part: EEL WIRE — LOOSE (CABIN)

DEN - FLT 366 - FLOOR TRACK LIGHTING, ROW 10 - ROW 20 INOPERATIVE. FOUND LOOSE WIRE AT ROW 10, REPAIRED, OPS CHECKED GOOD.

Part: FIREWALL — CRACKED (APU BAY)

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

Part: ENGINE — FAILED (NR 4 ENG)

NR 4 ENGINE OIL QUANTITY AND PRESSURE WENT TO ZERO ON A 15 MILE FINAL INTO ORD. ENGINE SECURED. LOCKED DOWN ENGINE AND 3 ENG FERRIED TO ATW FOR ENG CHANGE. (W)

Part: BOLT — BROKEN (RT WING AFT SPAR)

RIGHT WING REAR SPAR LEAKING FUEL, FOUND DURING ACCOMPLISHMENT OF EO E92/083/657. RT WING REAR SPAR ROOT JOING ATTACH FITTING AT RIB 2, BOLT 'C' BROKEN, AND BOLT 'A' FOUND LOOSE. REPLACED BOLTS IAW BAE REPAIR INSTRUCTIONS HC536H9043, AND RESEALED AND LEAK CHECKED.