N615AW

Part: FCU — MALFUNCTIONED (FLAPS) · airframe 24,980 hrs · 33,152 cycles

ON CLIMBOUT FLAPS STUCK AT 24 DEGREES ON RETRACTION AND FLAP INOP LIGHT ILLUMINATED. MAINTENANCE RESET FLAP COMPUTER.

Part: SLIDE — FAILED (DOOR) · airframe 24,729 hrs · 32,871 cycles

SLIDE DID NOT DEPLOY, HUNG LIMP. MAINTENANCE REMOVED AND REPLACED EVACUATION SLIDE AFTER PULLING PULL HANDLE TO INFLATE.

Part: SMOKE DETECTOR — DIRTY (AFT LAV) · airframe 23,718 hrs · 31,735 cycles

CREW REPORTS ACFT LAV SMOKE DETECTOR WENT OFF AND ELECTRIC ODOR WAS NOTED BY PASSENGER IN REAR OF ACFT. MAINTENANCE ISPECTED AND FOUND NO EVIDENCE OF ELECTRIC ODOR IN AIRCRAFT, FOUND AFT LAV SMOKE DETECTOR DIRTY. CLEANED AND OPS CHECKED GOOD. INSPECTED LAV AND LIGHTS, NO DEFECTS NOTED.

Part: SLIDE — OUT OF POSITION (RIGHT)

RIGHT FORWARD EVAC SLIDE NEAR DEPLOYMENT. REMOVED AND REPLACED SLIDE. (M)

Part: SLIDE — LOOSE (PASSENGER DOOR)

MKE - FLT 619 - RIGHT FORWARD EVACUATION SLIDE NEAR DEPLOYMENT. REMOVED AND REPLACED SLIDE.

Part: FILTER — LEAKING (HYDRAULIC SYSTEM)

ORD - FLT 502 - F/S REPORTS STRONG TOXIC SMELL IN CABIN. MAINTENANCE FOUND O-RING FOR YELLOW HYDRAULIC SYSTEM HP FILTER BLOWN OUT. REMOVED AND REPLACED YELLOW HP FILTER O-RINGS. NO LEAKS NOTED.

Part: ACTUATOR — FAILED (SPOILER)

MKE - FLT 619 - AIRFRAME VIBE AT 280 KNOTS WAS WRITTEN ON TERMINATION ATW LAST NIGHT, EXTENSIVE T/S REVEALED NO DEFECT. MAINTENANCE REQUESTED CHECK FLIGHT AND CONFIRMED VIBE WHEN ROLLING TO RIGHT, SUSPECT SPOILER. REMOVED AND REPLACED RT ROLL SPOILER ACTUATOR, OPS CHECKED GOOD.

Part: APU — ODOR (CABIN)

LAX - FLT 676 - AFTER GALLEY SHED ELECTRICAL SMELL, CONTINUED WITH APU RUNNING APU GENERATOR ON. CHECKED GALLEY AREA, NO ABNORMALITIES NOTED. PERFORMED PACK BURN OUT PROCEDURE. ODOR DISAPPEARED.

Part: SWITCH — TRIPPED (GALLEY)

LAX - FLT 676 - GALLEYS WILL NOT POWER UP AND F/A NOTICED ELECTRICAL SMELL IN REAR GALLEY. RESET MASTER START SWITCH, REF BLK 2.

Part: TANK — LEAKING (LT WING)

ATW - LEFT WING TANK FUEL LEAK RE-INSPECTED. ONE HY-LOCK FASTENER FOUND BAD. REPLACED HY-LOCK AND RESEALED TANK.

Part: STEP — CORRODED (AIRSTAIR)

ATW - FORWARD AIRSTAIRS 2ND STEP FROM TOP IS CORRODED. REMOVED AND REPLACED SECOND STEP FROM TOP ON FORWARD AIRSTAIR.

Part: FRAME — CHAFED (RT MLG)

MINOR CHAFE FRAME 29 WHER RIGHT MAIN LANDING GEAR DOOR EDGE WAS JUST CONTACTING FRAME 29. MEASURES .750 INCH IN LENGTH AND DEPTH .025 ONE SMALL AREA. MOST CHAFED .005 OR LESS. PERFORMED ET TO ABOVE CHAFED AFTER BLENDING AND FOUND TO BE CRACK FREE. BLENDED, ALODINED, PRIMED AND PAINTED IAW BAE FAX GCR/0752-97. (M)

Part: FRAME — CRACKED (FUSELAGE)

CRACK ON AFT FRAME LOWER SIDE 1 INCH LONG IN STRUCTURE AFT OF FRAME 50. REF FAX GCR/0746-97, REPAIRED CRACK PER FAX DJH/RJ0749-96 BUT ON LEFT SIDE. (M)

Part: COVER — OUT OF ADJUST (PAX DOOR SLIDE)

AFT PAX DOOR EVAC SLIDE COVER FAILED ITS PULL TEST. REF AIRCRUISER CMM. RII BUY BACK. ADJUSTED HOLDING CLIP, PULL TEST WITHIN CMM LIMITS.

Part: COVER — OUT OF ADJUST (PAX DOOR SLIDE)

FORWARD SERVICE DOOR EVAC SLIDE COVER FAILED ITS PULL TEST. REF AIRCURISER COMM, RII BUY BACK. ADJUSTED HOLDING CLIP AND REPOSITIONED SLIDE IN PACK TO CLEAR COVER. PULL TEST WITHIN LIMITS OF CMM. (M)

Part: OXYGEN MASK — FAILED (CABIN)

OXYGEN MASK AT 15 LT FLOW IND INOP. REPLACED OXYGEN MASK ASSY T 15 LT, OPS CHECK, LEAK CHECK AND FLOW CHECK OK.

Part: OXYGEN BOX — LEAKING (CABIN)

OXYGEN BOX AT 6 LT LEAKS FROM MANIFOLD. REPLACED OXYGEN BOX ASSY AT 6 LT, OPS LEAKS, FLOW CHECKS OK.

Part: OXYGEN MASK — FAILED (LT COCKPIT)

CAPTAINS OXYGEN MASK DOES NOT FLOW CONT IN EMERGENCY. REPLACED CAPTAIN OXYGEN MASK, OPS CHECK AND LEAK CHECK OK.

Part: OXYGEN MASK — FAILED (CABIN)

OXYGEN MASK AT 16, 17, 18 RT HAS HOLE IN REBREATHER FELT, ON PER BOX. REPLACED OXYGEN MASK AT 16, 17, 18 ONE PER BOX. OPS LEAK AND FLOW CHECKS OK.

Part: OXYGEN LINE — LEAKING (CABIN)

1 LT PSU OXYGEN BOX FEED LINE LEAKING. REMOVED AND REPLACED FEED LINE, LEAK AND OPS CHECKS, FLOW CHECKS OK.

Part: DOUBLER — CRACKED (LT WING)

SMALL CRACK IN DOUBLER ABOVE NR 2 PYLON ON LEFT WING L/EDGES AT RIB 5A AREA. REF SRM 57-41-11 FIG 3 SHEET 1 ITEM 4, 2024-T81. REF ASSY DRAWING HC572H1001 ITEM 75, P/N HC572H1081-000. REPLACED DOUBLER, REF BAE DRAWING NR HC572H1081 AND SRM CHAPTER 51. (M)

Part: RIVETS — SHEARED (FUSELAGE)

FRAME 26 AFT SIDE LEFT AND RIGHT FLOOR SUP ANGLE OUTBOARD RIVETS SHEARED. REPLACED RIVETS.

Part: RIVETS — LOOSE (VERT STAB)

VERTICAL STAB TO FUSELAGE CLOSING ANGLE ON LEFT AND RIGHT SIDES AT AFT ENDS HAVE RIVETS WORKING, 3 ON THE LEFT AND 2 ON THE RIGHT CIRCLED IN BLACK PEN. REMOVED RIVETS ON LEFT AND RIGHT VERTICAL STAB TO FUSELAGE CLOSING ANGLES, 3 ON LEFT AND 2 ON RIGHT. INSTALLED NEW RIVETS, PRIMED AND PAINTED.

Part: SKIN — CHAFED (RT MLG DOOR)

RIGHT MLG DOOR INNER SKIN HAS A SPOT ON FORWARD EDGE THAT HAS BEEN CHAFING AND IS WORN THIN. SPOTS MARKED WITH BLACK PEN. PERFORMED PT TO THE ABOVE CHAFE AFTER BLENDING AND FOUND TO BE CRACK FREE AT THIS TIME. REPAIRED PER BAE FAX REF GCR/0752/97.

Part: SKIN — DAMAGED (LT MLG DOOR)

LEFT MLG DOOR INNER SKIN UPPER AREA BELOW FORWARD HINGE HAS A CHAF THAT IS RIGHT NEXT TO HINGE REINFORCING THATS APPROX .375LX .375WX .018 INCH DEEP. COMPLIED WITH NDT OF ABOVE REFERENCED DAMAGE AREA AND FOUND IT TO BE FREE OF CRACKS. INSTALLED CHERRY MAA RIVET AS REQUIRED IAW AVRO FAX GCR/0755-97.

Part: RIVETS — LOOSE (RT MLG DOOR)

RIGHT MLG DOOR INNER SKIN HAS ABOUT 8 RIVETS THAT ARE WORKING. RIVETS MARKED WITH BLACK PEN. REPLACED LOOSE RIVETS ON RIGHT MLG DOOR INNER SKIN.

Part: ANGLE — BROKEN (FUSELAGE)

ANGLE ATTACH FOR INTERCOSTAL BETWEEN FRAME 19 AND 20 IS BROKEN AT FRAME 20 BELOW GIL-LINER FORWARD CARGO AREA. FABRICATED AND INSTALLED PART PER DRAWING, HC536H0558-000, AND SRM CHAPTER 51. (M)

Part: PIN — DEFECTIVE (LT TE FLAP)

LEFT FLAP TRACK NR 3 ONE OF THE LOWER CARRIAGE TO SCREWJACK TRUNNION PINS HAS A DEFECT INDICATION FOUND ON NDT. INSTALLED A NEW PIN ON LEFT NR 3 SCREWJACK TRUNNION.

Part: INTERCOSTAL — BENT (BAGG COMPT)

INTERCOSTAL BETWEEN FRAME 21 AND 22 BY FWD CORNER OF FWD BAGGAGE PIT DOOR IS BENT. REPLACED INTERCOSTAL.

Part: RIVET — SHEARED (NR 3 PYLON)

RIVET HEAD SHEARING TOP SIDE OF RIB LE ABOVE NR 3 PYLON MARKED. REPLACED RIVET.

Part: TIP — CRACKED (RT WING)

RIGHT WING TIP FAIRING PANEL CRACKED 2 PLACES. ALSO, REQUIRES REINFORCEMENT PER EO E96/008/634 BLOCK 9. REPAIRED 2 CRACKS IN RIGHT WING TIP FAIRING IAW AW 57-20-9412-06. C/W EO E96/008/634 BLK 9.

Part: SUPPORT — CRACKED (CARGO COMPT)

REAR CARGO BAY CRACKED FLOOR SUPPORT FRAME 34 CENTER SECTION MARKED. REPLACED FRAME 34, CENTER FLOOR SUPPORT.

Part: SUPPORT — CRACKED (CARGO COMPT)

REAR CARGO BAY CRACKED FLOOR SUPPORT FRAME 34 LEFT OUTBOARD SECTION, MARKED. REPLACED FRAME 34, LEFT FLOOR SUPPORT.

Part: SKIN — WORN (RT TE FOREFLAP)

RIGHT FOREFLAP HAS STREAKING RIVETS IN TOP SKIN OUTBOARD END. DRILLED OFF AND REPLACED STREAKING RIVETS TOP SKIN OUTBOARD END OF RIGHT FOREFLAP END.

Part: BRACKET — CRACKED (LT WING)

LEFT WING TRAILING EDGE SHROUD AREA, BOTTOM SKIN STIFFENER BRACKET CRACKED ON FLANGE AFT BETWEEN RIBS 8 AND 9. REPLACED STIFFENER BRACKET ON LEFT WING TRAILING EDGE SHROUD AREA BOTTOM SKIN. ALL WORK ACCOMPLISHED IAW BAE SRM AND STD PRACTICES. (M)

Part: BRACKET — CRACKED (LT WING)

LT WING TRAILING EDGE SHROUD AREA AT INBOARD LIFT SPOILER JACK RIB, THERE IS A BRACKET THAT SECURES HYD LINE THATS CRACKED. REMOVED BRACKET, REPAIRED BRACKET BY WELDING IAW BAE FAX REPAIR REF DJH/RJ0737-97 DATED 10-02-97 AND FOUND UNIT SERVICEABLE. INSTALLED BRACKET, ALL WORK ACCOMPLISHED IAW BAE MM STD PRACTICES. (M)

Part: BRACKET — CRACKED (LT WING)

LEFT WING INBOARD LIFT SPOILER OUTBOARD HINGE RIB HAS A BRACKET FOR SECURING HYD LINES THATS CRACKED, RIB 5 LT. REPLACED ANGLE P/N HC932H0211-000 ON LEFT WING INBOARD LIFT SPOILER OUTBOARD HINGE RIB SECURING HYD LINES. (M)

Part: STIFFENER — CRACKED (LT WING)

LEFT WING TRAILING EDGE SHROUD TOP SKIN STIFFENER BETWEEN RIBS 5 AND 6 IS CRACKED AT FWD ADN BRACKET AT ITS AFT END IS CRACKED ON ITS LOWER FLANGE. REPAIRED LT WING TRAILING EDGE SHROUD TOP SKIN STIFFENER BETWEEN RIBS 5 AND 6 IAW BAE FAX REF GCR/0754-97 DATED 10-13-97. REPLACED SAID BRACKET AT AFT END. WORK ACCOMPLISHED IAW BAE STD PRACTICES. (M)

Part: BOLT — CORRODED (RT SPOILER)

RIGHT OUTBOARD LIFT SPOILER INBAORD HINGE BOLT FAILED VISUAL INSPECTION FOR CORROSION AND PITTING IN THE THREADS. REMOVED AND REPLACED HINGE BOLT. (M)

Part: RIVET — MISSING (CARGO COMPT)

FRONT CARGO BAY RIVET MISSING LOWER LONGERON FOR HYDRAULIC BAY DOOR, FORWARD FRAME 26. INSTALLED RIVET. (M)

Part: BRACKET — CRACKED (RT WING)

HYD LIFT SPOILER LINE CLAMP BRACKET CRACKED, RIGHT WING TE, RIB NR 5. REMOVED CRACKED BRACKET. REPLACED HYD LIFT SPOILER LINE CLAMP BRACKET ON TRAILING EDGE OF RIGHT WING AT RIB 5. (M)

Part: INTERCOSTAL — MISDRILLED (CARGO COMPT)

FRONT CARGO BAY EXTRA HOLES DRILLED NEAR NUT PLATES TOP INTERCOSTAL (P/N HC536H0555-00) BETWEEN FRAME 24 AND 25 TIE DOWN RINGS. REMOVED AND REPLACED INTERCOSTAL. (M)

Part: SUPPORT — BROKEN (CARGO COMPT)

FRONT CARGO BAY TIE DOWN RING SUPPORT BROKEN FRAME 21 RT MARKED. REPLACED RING SUPPORT.

Part: MOUNT PLATE — CRACKED (RT SPOILER)

RIGHT LIFT SPOILER CONTROL VALVE MOUNT PLATE CRACKED. REPLACED LIFT SPOILER VALVE MOUNT PLATE. GEN W/C FOR OPS AND LEAK CHECK. (M)

Part: SUPPORT — BENT (CARGO COMPT)

FRONT CARGO BAY FLOOR SUPPORT RT BETWEEN FRAME 20 AND 21 BENT. REPLACED FLOOR SUPPORT.

Part: STIFFENER — CRACKED (RT WING)

RIGHT WING TE TOP SKIN STIFFENER CRACKED AT FWD END, INBOARD OF RIB NR 9. REPLACED RIGHT WING TRAILING EDGE TOP SKIN STIFFENER INBOARD OF RIB NR 9. (M)

Part: ANGLE — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT ANGLE RT OUTBOARD FRAME 18-19A CORRODED. REMOVED CORRODED ANGLE AND INSTALLED NEW ANGLE RT OUTBOARD FRAME 18-19A.

Part: CONTROL CABLE — CORRODED (RT AILERON)

RIGHT AILERON CONTROL CABLE 35B-C IS CORRODED AT LOWER PULLEY UNDER FWD WING ROOT FAIRING. REMOVED AND REPLACED BOTH RT WING ROOT MAIN AILERON CABLES, TENSIONED AND SAFETIED. GEN W/C FOR FUNCTIONAL TEST REF 5067. (M)

Part: BRACKET — CRACKED (FUSELAGE)

LEFT BOTTOM ANGLE BRACKET CRACKED, FRO FRAME, AFT OF FRAME 50. FABRICATED GUSSET PLATE PER PRODUCTION DRAWING HC539H0229, AND INSTALLED PLATE PER SRM.

Part: FLOOR — CORRODED (COCKPIT)

FLOOR FRAME 43 TO 44 RIGHG SIDE INBOARD SEAT TRACK CORRODED, REF 53-51-01-03. REMOVED AND REPLACED AFT VEST INBOARD SEAT TRACK RAIL BETWEEN FRAME 43 TO 44 RIGHT SIDE. (M)

Part: CONTROL CABLE — CORRODED (LT AILERON)

AILERON INTERCONNECT CENTER FORWARD CABLE IS CORRODED AT LEFT WING ROOT PULLEY. REMOVED AND REPLACED BOTH FORWARD AND AFT CENTER LOOP INTERCONNECT CABLES, TENSIONED AND SAFETIED. GEN W/C FOR FUNCTION TEST, REF 5067.

Part: BRACKETS — CRACKED (SERVICE DOORWAY)

BRACKET FOR PSU'S ON UPPER LONGERON OF AFT SERVICE DOOR OPENING BETWEEN FRAME 39 AND 40 IS CRACKED. FABRICATED NEW PART IAW DRAWING, HC252H3212 AND SRM STANDARD PRACTICES CHAPTER 51, AND INSTALLED. (M)

Part: CONTROL CABLE — WORN (RT AILERON)

RIGHT AILERON INTERCONNECT CABLE, OUTBOARD CABLE WORN ALMOST THROUGH ALUMINUM CLAD. REMOVED AND REPLACED RT OUTBOARD CONNECT CABLE, TENSIONED AND SAFETIED. GEN W/C FUNCTIONAL TEST 5067.

Part: STALL TRIGGER — WORN (CABIN)

RIGHT STALL TRIGGER INBOARD SCREW HOLES ENLONGATED. REPAIRED IAW BAE FAX REF HC/211-97, DJR/RJO699-97 AND JM/RJO247-97. (M)

Part: ANGLE — CRACKED (CARGO COMPT)

FREIGHT ANGLE CRACKED CENTER OF FRAME 35 AFT CARGO BAY. REMOVED AND REPLACED WITH NEW FREIGHT ANGLE PIECE CENTER OF FRAME 35 IN AFT CARGO BAY. (M)

Part: ANGLE — CRACKED (CARGO COMPT)

TWO SMALL FREIGHT ANGLES CRACKED AT 7:00 POSITION, FRAME 21 FORWARD CARGO. REPLACED ANGLES.

Part: RIVET — SHEARED (NR 2 ENG COWL)

NR 2 ENGINE RIVET SHEARED AT LORD MOUNT BRACKET. INSTALLED BOLTS AT POSITIONS B, C, D. REF BAE RIC HC545H9009 AND BAE FAX PJN/1196R-92, NR 2 PYLON. (M)

Part: RIVET — SHEARED (NR 2 ENG COWL)

NR 2 ENGINE AFT OUTBOARD COWL DOOR RIVET SHEARED TOP SPLITTER ASSY AFT STIFFENER. REPLACED SHEARED RIVET. (M)

Part: ANGLE — CRACKED (MLG WW)

TOP ATTACHMENT ANGLE FOR CENTER DIAPHRAM THAT SEPARATES MLG BAYS HAS 1 INCH CRACK IN BAND RADIUS ABOVE THE BOLT HOLE THATS THE 6TH ONE BACK. REPLACED TOP ATTACHMENTS ANGLE.

Part: THRESHOLD — CORRODED (PAX DOOR)

AFT PAX DOOR THRESHOLD Z-MEMBER CORRODED FORWARD HALF. REPLACED Z-MEMBER. (M)

Part: SUPPORT — CRACKED (CARGO COMPT)

FORWARD CARGO BAY CENTER FLOOR SUPPORT CRACKED AT CENTER NUT PLATE HOLES FRAME 20. REPLACED FLOOR SUPPORT.

Part: RIVET — FAILED (NR 1 ENGINE COWL)

NR 1 ENGINE AFT INBOARD COWL DOOR RIVET SHEARED TOP SPLITTER AFT STIFFENER. REPLACED SHEARED RIVET. (M)

Part: RIVET — SHEARED (NR 1 ENGINE COWL)

NR 1 ENGINE AFT INBOARD COWL DOOR RIVET SHEARED BOTTOM SPLITTER 2 SECOND STIFFENER. REPLACED SHEARED RIVET. (M)

Part: DOOR — CHAFED (NR 2 ENGINE COWL)

NR 2 ENGINE FORWARD INBAORD COWL DOOR CHAFED AT LOWER AFT CORNER. REPAIRED FORWARD DOOR IAW BAE SRM CHAPTER 54-10-11 PAGE 242-243. (M)

Part: COWL — CRACKED (NR 3 ENGINE)

NR 3 ENGINE SHOULDER COWL SMALL CRACK FWD OF SCAVENGE HYDRALINE FITTING. CRACK IS APPROX .25 INCH LONG AROUND A SPOT WELD. REPAIRED IAW SRM AND DS/W/TS/28402/97 BAE FAX, NR 3 SHOULDER COWL CRACK. (M)

Part: BRACKET — LOOSE (NR 4 ENG MOUNT)

NR 4 ENGINE SHOULDER COWL LORD MOUNT BRACKET LOOSE FROM PYLON BOX. REPLACED BRACKET AND INSTALLED BOLTS AT POSITIONS B, C, D REF BAE RIL HC546H009 AND BAE FAX PJN/1196R/92.

Part: JOBOLTS — DAMAGED (RT WING RIB)

PERFORM RIL HC571H9033 RT WING RIB 2 OUTBOARD. INSTALLED JOB0LTS TO OUTBOARD RIB 2 RIGHT WING PER RIL HC57 1H9033. (M)

Part: JOBOLTS — DAMAGED (LT WING RIB)

PERFORM RIL HC571H9033 LT WING RIB 0. REMOVED AND REPLACED JO-BOLT FASTENERS AT LEFT SIDE RIB 0 IAW HC571H9033. SEE W/C 82103/75 FOR REPORT AND SIZES USED. (M)

Part: JOBOLTS — DAMAGED (RT WING RIB)

PERFORM RIL HC571H9033 RT WING RIB 2 INBOARD. INSTALLED JOBOLTS TO INSIDE PORTION OF RIB 2 RT SIDE. INSTALLED JOBOLTS TO INSIDE PORTION OR RIB 2 RT SIDE. (M)

Part: FAIRING — CRACKED (LT WING TIP)

LEFT WING TIP FAIRING AT RIB 20 FALSE RIB IS CRACKED. REPAIRED IAW BAE SRM 51-71-11 FIG 2. (M)

Part: JOBOLTS — DAMAGED (RT WING RIB)

PERFORM RIL HC571H9033 RT WING RIB 0. INSTALLED JOBOLTS TO RIB 0 RT SIDE. (M)

Part: ANGLE — LOOSE (FUSELAGE)

FRAME 26 AFT SIDE LEFT AND RT FLOOR SUPPORT ANGLE OUTBOARD RIVETS SHEARED. REPLACED RIVETS. (M)

Part: TRIM — CORRODED (LAVATORY)

FORWARD LAV INSIDE DIVIDER WALL, METAL LOWER TRIM PIECE CORRODED 6-8 INCHES LONG. REPLACED CORRODED TRIM PIECE ON FWD LAV DIVIDER WALL. (M)

Part: PANEL — CHAFFED (WING)

PANEL 474AT IS CHAFFED AT INBOARD LOWER CORNER, ABOVE NR 3 PYLON. REPAIRED CHAFED PANEL IAW BAE FAX REF DJR/RJ0715-97. (M)

Part: PANEL — CHAFFED (LT WING)

LEFT LEADING EDGE PANEL CHAFED AT TOP INBOARD ATTACHMENT PANEL 464AT, INBOARD ATTACHMENT STRINGER CHAFED, PANEL CHAFED .045 INCH, STRIP CHAFED .035 INCH. REPLACED CHAFED STRIP. REPAIRED PANEL PER BAE FAX REF DJR/RJ0715-97. (M)

Part: STALL TRIGGER — ELONGATED (LEFT)

LEFT STALL TRIGGER INBOARD SCREW HOLES ELONGATED. REPAIRED IAW BAE FAX FEF DJR/RJ0699-97 AND JM/RJ0247-97. (M)

Part: PANEL — DAMAGED (FUSELAGE)

ATW - WHERE THE FORWARD LOWER EDGE OF PANEL 282BT, RT DE-ICE LIGHT PANEL, CONNECTS TO FUSELAGE, HAS A WEAR MARK IN FUSELAGE. REPAIRED IAW BAE SRM 53-00-12 FIG 202.

Part: STEPS — CORRODED (AFT AIRSTAIRS)

AFT AIRSTAIRS HAS 1ST, 3RD, AND 4TH STEPS FROM BOTTOM CORRODED. REMOVED AND REPLACED CORRODED STEPS. (M)

Part: SELECTOR VALVE — MALFUNCTIONED (LANDING GEAR)

EN ROUTE TO ATW GREEN HYD TEMP ILLUMINATED, FOLLOWED ABNORMAL PROCEDURE CHECKLIST, LANDING AT ATW UNEVENTFUL, BRAKE TEMP WENT TO 700 DEGREE LEFT SIDE WHILE USING BRAKES TO STEER DURING TAXI. REMOVED AND REPLACED LANDING SELECTOR VALVE. (M)

Part: WARNING LIGHT — ILLUMINATED (COCKPIT)

AROUND ROTATION CONFIGURATION WARNING ILLUMINATED AND AIR BRAKE LIGHT WAS ILLUMINATED. NO FURTHER INCIDENTS IN FLIGHT. OPS CHECKED AIRBRAKE PER MM AND COULD NOT DUPLICATE. OK FOR SERVICE NR 915. (M)

Part: RAIL — CORRODED (AIRSTAIR)

ATW - FORWARD VESTIBULE AREA: FORWARD OUTBOARD AIRSTAIR RAIL SPOT CORROSION ON FORWARD END. REMOVED AND REPLACED FORWARD OUTBOARD LOWER ARM RAIL FOR AIRSTAIRS. FORWARD POSITION. ALSO REINSTALLED FORWARD OUTBOARD AIRSTAIR RAIL IN FORWARD VESTIBULE AREA.

Part: SKIN — LIGHTNING STRIKE (CENTER WING)

ATW - LIGHTNING STRIKE AT CENTER WING SECTION 6 INCHES LEFT OF RIB ZERO AND 14.75 INCHES AFT OF FRONT SPAR. C/W BLENDING, TREATING, AND RE-PROTECTION PER BAE 146 SRM AND AVRO FAXES DJH/RJ/0402-97 AND DJH/RJ/0404-97. DPM 119 051097. ACCOMPLISHED NDT OF BLENDED AREA TO ASSURE COMPLETE BLENDING AND NO CRACKS AS WELL AS NO HEAT DAMAGE. FOUND TO BE DEFECT FREE.

Part: SILL — CORRODED (PASSENGER DOOR)

ATW - FORWARD FLOOR BEAMS AND SUPPORT STRUCTURE AREA - FORWARD PASSENGER DOOR SILL PLATE HAS SPOT CORROSION IN SEVERAL AREAS. REPLACED SILL PLATE AT FORWARD PASSENGER DOOR IAW BAE 146 MM - GENERATED W/C FOR REMAINING WORK.

Part: RETRACT MECH — MALFUNCTIONED (TE FLAPS)

ON CLIMB-OUT FROM DEN WHEN FLAPS SELECTED FROM 18-0, FLAP FAULT AND INOP LIGHTS ILLUMINATED, FLAPS STUCK AT 18 DEGREES, AIR RETURN. CLEARED FLAP FAULT, RAN FLAPS NORMALLY. (M)

Part: TRACK LIGHT — INOPERATIVE (CABIN)

FLOOR TRACK LIGHT INOP AT FR32-FR33B. REMOVED AND REPLACED NR 4 BATTERY (POWER) SUPPLY, CHECKS OK.

Part: RIB — DAMAGED (RADOME)

REF AVRO FAX DJR/RJ0379-95, RIGHT FUSELAGE NOSE DAMAGE AT RIB NR 1 BETWEEN UPPER 'E' LAP JOINT AND LOWER RADOME LATCH IS TO BE REASSESSED FOR REPAIR OR FURTHER SERVICE AT NEXT 'C' CHECK OR COMPLETION OF 3000 FLTS WHICHEVER IS SOONER. CURRENT CYCLES 16,863.

Part: ESCAPE SLIDE — INOP (CABIN)

RIGHT AFT ESCAPE SLIDE LIGHTING INOP. REPLACED SLIDE.

Part: CABLE — CORRODED (AILERON)

AILERON INTERCONNECT CABLE HAS CORROSION AT WING ROOT PULLEYS. REMOVED AND REPLACED BOTH CENTER SECTIONS OF AILERON INTERCONNECT CABLE IAW MM 27-11-44. REF W/C 6004 FOR FUNCTIONAL TEST OF AILERON CONTROLS.

Part: STIFFENERS — CRACKED (FS 25.94)

WHILE COMPLIED WITH ITEM 3 OF EO E95/003/653 2 CRACKS WERE DISCOVERED AT FRAME 29 IN HYDRAULIC BAY. CRACKS WERE LOCATED AT BOLT HOLES OF STIFFENER 25.94 LEFT AND 25.94 RIGHT. REPAIRED FRAME 29 STIFFENERS AT 25.94 LEFT AND RIGHT SIDES IAW EO E95/003/653 REV ORIG.

Part: GUSSET — CORRODED (FRAME 15)

ONE GUSSET PLATE CORRODED ON FORWARD VESTIBULE INTERCOSTALS JUST LEFT OF FUSELAGE CENTER LINE AT FRAME 15. FOUND CORROSION BAD ENOUGH TO REPLACE GUSSET PLATE, REPLACED, TREATED AND APPLIED PROTECTIVE FINISH.

Part: GUSSET — CORRODED (FRAME 42-43)

SURFACE CORROSION ON GUSSET PLATES FRAME 42 TO 43 RIGHT INTERCOSTAL FLOOR SUPPORT STRUCTURE. REMOVED AND REPLACED GUSSET PLATES. ALODINE, PRIME AND PAINT COVERED AREA WITH PRC PER SRM.

Part: SILL — CORRODED (PAX DOOR)

FORWARD PASSENGER DOOR SILL PLATE HAS AREAS OF CORROSION NOTED. UNDER AFT GIRT BAR BRACKET. UNDER SPACER FOR TREAD PLATE, AND IN BEND RADIUS OF THE FLANGE. FOUND ALL CORROSION TO BE MINOR SURFACE CORROSION. CLEANED, TREATED AND REAPPLIED PROTECTIVE FINISH. ONLY EXCEPTION WAS CORROSION IN RADIUS. REMOVED DAMAGE, TREATED ADN REAPPLIED FINISH IAW FAX JM/RJ0711-95 AND ROB.

Part: RIB — CRACKED (RUDDER)

RUDDER LOWER RIB IS CRACKED UP AND LOOSE SECTION. REMOVED AND REPLACED LOWER RUDDER RIB PER SRM STANDARD PRACTICES. PRIMED AND PAINTED RIB AND RIVETS.

Part: ANTI ICE VALVE — INOPERATIVE (EMPENNAGE)

MLI - FLT 365 - TAIL ANTI-ICE VALVE INOP OPEN. REPLACED THE ANTI-ICE VALVE ACTUATOR. REFERENCE OPERATOR CONTROL NR 95ZZZX6231, AND 95ZZZX6232.

Part: PERI SEALS — FAILED (APU)

MLI - FLT 365 - RIGHT ZONE HIGH TEMP OCCURRED WHEN THE APU WAS SUPPLYING THE NR 2 PACK. REPLACED PERI SEALS. REFERENCE OPERATOR CONTROL NR 95ZZZX6231, AND 95ZZZX6233.

Part: ENGINE OIL — REQD SERVICE (NR 1)

MLI - FLT 365 - NR 1 ENGINE OIL LEVEL LOW. FOUND NO EXTERNAL LEAKS, SERVICED WITH 4 QUARTS OF OIL. REFERENCE OPERATOR CONTROL NR 95ZZZX6232, AND 95ZZZX6233.

Part: PITOT TUBE — PLUGGED (NR 1)

NR 1 A/S INDICATOR INOPERATIVE. FOUND NR 1 PITOT TUBE AT HEAD PLUGGED, BLEW OUT FROM INSTRUMENT TO HEAD. OPS AND LEAK CHECKED GOOD.

Part: GUST DAMPENER — FAILED (AILERONS)

DEN - FLT 366 - ON CONTROL CHECK, FOUND AILERONS VERY STIFF TO MOVE EITHER RIGHT OR LEFT, ESPECIALLY NEAR CENTER POSITION. FOUND ROD END BEARING BAD AT RIGHT AILERON GUST DAMPER. REMOVED AND REPLACED RIGHT GUST DAMPER IAW MM 27-70-11. AILERON DISCONNECTED FOR TROUBLESHOOTING, RECONNECTED DISCONNECT SYSTEM IAW 27-11-34. CONTROLS TEST FREE. S/N OFF DBPBAEA193, S/N ON DBP.BAEA65.

Part: GUST DAMPENER — FAILED (AILERONS)

DEN - FLT 357 - ON CONTROL CHECK, FOUND AILERON VERY STIFF TO MOVE EITHER RIGHT OR LEFT ESPECIALLY NEAR CENTER POSITION. FOUND THE RIGHT AILERON GUST DAMPER ROD END ON THE AILERON SIDE FROZEN. SENT A REPLACMENT DAMPER TO DEN.

Part: ESCAPE SLIDE — MALFUNCTIONED (LT AFT DOOR)

LEFT AFT DOOR ESCAPE SLIDE DUE A SCHEDULED DEPLOYMENT BUT DID NOT DEPLOY CORRECTLY, IT WENT AFT OF THE FUSELAGE. REPLACED SLIDE.

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: GEN CONTL UNIT — OFF LINE (NR 1)

NR 1 AC BUS AND ESS AC BUS OFF LINE OCCURRED APPROX 200 FEET PRIOR TO TOUCHDOWN. AIRCRAFT IN LANDING CONFIGURATION APU WAS OPERATIONAL AT THE TIME. RESET NR 1 GCU BUS RESET, GROUND RAN, OPS CHECKS GOOD. AIRCRAFT 73 MINUTES LATE INBOUND DUE TO HEADWINDS. (M)

Part: ENG — FAILED (NR 4)

ON CLIMB-OUT THROUGH 10,400 FEET THERE WAS A LOUD 'BANG' FOLLOWED BY ROLLBACK OF NR 4 ENG N1 AND N2. PRECAUTIONARY SHUTDOWN OF NR 4 ENGINE. REPLACED ENG NR 4 IAW 71-00-00 PG 401.