N767MW

Part: FLASHLIGHT — INOPERATIVE (FWD CABIN) · airframe 55,416 hrs · 38,190 cycles

LEFT FWD MID JUMPSEAT EMERGENCY FLASHLIGHT INOPERATIVE.

Part: FIRE LOOP — OPEN (RT ENGINE) · airframe 55,358 hrs · 38,167 cycles

"R ENG FIRE LP 1" EICAS STATUS MSG DISPLAYED.(<P>TRANSFERRED RT ENG FIRE LOOP 1 TO MDDR 120017 IAW MEL 26-11-01-01. NO MX PROCEDURES. PLACARD INSTALLED MBCB NOV 12 2019. AIRCRAFT RELEASED TO ETOPS 120 MIN.</P><P>REF LOG PAGE 1076278 - ITEM M3: ACCOMPLISHED FIM 26-11 FT 806 AND 26-11 FT 804. FOUND RIGHT ENGINE UPPER FIRE WALL LOOP 1 OPEN. REMOVED AND REPLACED DETECTOR ASSY (FIRE WALL) IAW B767 AMM 26-11-02. FIRE DETECTION SYSTEM OPS CHECK GOOD. THIS CLEARS MDDR 120017. PLACARD REMOVED.&NBSP;</P>)

Part: CONTROL PANEL — DEFECTIVE (COCKPIT) · airframe 55,356 hrs · 38,166 cycles

DURING FLIGHT, RECEIVED "LEFT SIDE WINDOW" EICAS ADVISORY MESSAGE. COMPLIED WITH QRH PROCEDURES.&NBSP;&NBSP;(<P>TRANSFERRED LEFT SIDE WINDOW TO MDDR 119952 IAW DDG 30-41-01-03, MX PROCEDURES C/W AND PLACARDS INSTALLED.</P><P>LP 1076278 - M2: T/S L SIDE WINDOWS PER FIM 30-41 FT 804, NO DEFECTS NOTED. MEGGED WIRES, WINDOW, NO DEFECTS NOTED. REMOVED AND REPLACED WINDOW HEAT CONTROL PANEL IAW B767 AMM 30-41-02. WINDOW HEAT SYSTEM OPS CHECK GOOD. THIS CLEARS MDDR 119952. PLACARD REMOVED AND MCC NOTIFIED.&NBSP;</P>)

Part: BATTERY — FAILED (APU) · airframe 55,356 hrs · 38,166 cycles

APU BATTERY AT 14 VOLTS, WILL NOT HOLD CHARGE OVER 24 HOURS.&NBSP;(<P>REMOVED AND REPLACED APU BATTERY IAW B767 AMM 24-31-04. APU AND APU BATTERY CHARGING SYSTEM OPS CHECK GOOD.&NBSP;</P>)

Part: CONTROL UNIT — FAILED (WINDOW HEAT) · airframe 55,342 hrs · 38,159 cycles

L SIDE WINDOW EICAS MSG. PERFORMED WINDOW HEAT BITE PER FIM 30-41 FT 804, NO FAULTS NOTED AT THIS TIME. REPLACED LH WINDOW HEAT CONTROL UNIT. CKS GOOD IAW AMM 30-41-01.

Part: START VALVE — FAULTY (LT ENGINE) · airframe 55,327 hrs · 38,150 cycles

L ENGINE STARTER EICAS MSG ON ENG START, LEFT ENG. PERFORMED MANUAL START VALVE OPERATION, ENG START NORMAL. DEFERRED LEFT ENG START VALVE IAW DDG 80-00-02-01, CAT 'C', DUE 29-SEP-19. MX PROCEDURES C/W. PLACARD INSTALLED. MDDR 117952 ASSIGNED. LP 1072485 - M5: REMOVED AND REPLACED LEFT ENG STARTER VALVE ASSY IAW AMM 80-11-02. START VALVE OPS CKS GOOD ON DRY MOTOR OF ENG. THIS CLEARS MDDR 117952. PLACARD REMOVED AND MCC NOTIFIED.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 55,174 hrs · 38,093 cycles

EICAS STATUS MESSAGE RT&NBSP; &NBSP;ENG OH LP 1 DISPLAYED(<P>C/W ENGINE FIRE DETECTION SYSTEM BITE IAW FIM 26-11 F/T 804 MSG CLEARED AND SYSTEM CK NORMAL ON GROUND NO DEFECTS NOTED&NBSP;</P>)

Part: CONTROLLER — FAULTY (WINDOW HEAT) · airframe 55,174 hrs · 38,093 cycles

LSIDE WINDOW HEAT EICASMSG AND WINDOW HEAT INOP LIGHT ILLUMINATED (L3)(<P>TRANSFERRED L3 WINDOW HEAT TO MDDR 109179 IAW MEL 30-41-01-03 MAINT PROCEDURES C/W PLACARD INSTALLED.</P><P>27MAR: LP 952150, ITEM M3: ACCOMPLISHED FIM 30-41 FT 804 SIDE WINDOW BATB. B776 SHOWED CONTROLLER FAULT. R&AMP;R L3 WINDOW HEAT CONTROLLER IAW AMM 30-41-01. WINDOW HEAT OPS OK GOOD. MAINT PROCEDURE CLEARED, PLACARD REMOVED. THIS CLEARS MDDR 109179.</P>)

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 55,165 hrs · 38,089 cycles

TROUBLESHOOT EMERGENCY LIGHTS.&NBSP;(<P>REMOVED AND INSTALLED NEW EMERGENCY LIGHT BATTERY PACK #10 IAW AMM 33-51-07-022-001 AND 33-51-07-422-012. OPERATIONAL TEST OF THE NEW EMERGENCY LIGHT BATTERY PACK CHECKS GOOD IAW AMM 33-51-07-712-009.&NBSP;</P>)

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 55,165 hrs · 38,089 cycles

TROUBLESHOOT EMERGENCY LIGHTS.&NBSP;(<P>REMOVED AND INSTALLED NEW EMERGENCY LIGHT BATTERY PACK #6 IAW AMM 33-51-07-022-001 AND 33-51-07-422-012. OPERATIONAL TEST OF THE NEW EMERGENCY LIGHT BATTERY PACK CHECKS GOOD IAW AMM 33-51-07-712-009.&NBSP;</P>)

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 55,165 hrs · 38,089 cycles

TROUBLESHOOT EMERGENCY LIGHTS.&NBSP;(<P>REMOVED AND INSTALLED NEW EMERGENCY LIGHT BATTERY PACK #12 IAW AMM 33-51-07-022-001 AND 33-51-07-422-012. OPERATIONAL TEST OF THE NEW EMERGENCY LIGHT BATTERY PACK CHECKS GOOD IAW AMM 33-51-07-712-009.&NBSP;</P>)

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 55,165 hrs · 38,089 cycles

TROUBLESHOOT EMERGENCY LIGHTS.&NBSP;(<P>REMOVED AND INSTALLED NEW EMERGENCY LIGHT BATTERY PACK #11 IAW AMM 33-51-07-022-001 AND 33-51-07-422-012. OPERATIONAL TEST OF THE NEW EMERGENCY LIGHT BATTERY PACK CHECKS GOOD IAW AMM 33-51-07-712-009.&NBSP;</P>)

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 55,165 hrs · 38,089 cycles

TROUBLESHOOT EMERGENCY LIGHTS.&NBSP;(<P>REMOVED AND INSTALLED NEW EMERGENCY LIGHT BATTERY PACK #3 IAW AMM 33-51-07-022-001 AND 33-51-07-422-012. OPERATIONAL TEST OF THE NEW EMERGENCY LIGHT BATTERY PACK CHECKS GOOD IAW AMM 33-51-07-712-009.&NBSP;</P>)

Part: FUEL FILTER — WARNING MESSAGE (LT ENGINE) · airframe 55,149 hrs · 38,081 cycles

DURING CLIMB POWER EICAS MSG "L ENG FUEL FILTER" DISPLAYED&NBSP;(<P>ACCOMPLISHED FIM 73-11 F/T 804 BLOCKS 1 AND 21. REMOVED AND REPLACED LH ENG FUEL FILTER I.A.W. AMM 73-11-02, FILTER CONTAMINANTS NOT FOUND. PERFORMED GROUND ENG RUN I.A.W AMM 71-00-00, NO LEAKS NOTED, MSG CLEARED, SYSTEM OPS CHECK GOOD&NBSP;</P>)

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 55,133 hrs · 38,073 cycles

EICAS STATUS CAB ALT AUTO 1&NBSP;(<P>PERFORMED CABIN PRESSURE CONTROLLER BITE CHECK IAW FIM 21-31-00 NO FAULTS, RESET CONTROLLER MESSAGE CLEARED&NBSP;</P>)

Part: SMOKE DETECTOR — WARNING MESSAGE (FWD CARGO) · airframe 55,087 hrs · 38,060 cycles

FWD CARGO DETECTOR 2 STATUS MESSAGE DISPLAYED(<P>C/W FIM 26-16 FT 816 , RELAMPED DETECTOR NO HELP, REMOVED AND REPLACED FWD CARGO # 2 DETECTOR ASSY I.A.W AMM 26-16-01 , CARGO DETECTION SMOKE OPS CHECK GOOD MESSAGE CLEARED&NBSP;</P>)

Part: FIRE LOOP — WARNING MESSAGE (RT ENGINE) · airframe 55,081 hrs · 38,057 cycles

RT ENGINE FIRE LOOP1 MESSAGE(<P>TRANSFER&NBSP; TO MDDR 104597 IAW MEL26-11-0101 NO MAINT PROCEDURES REQUIRED PLACARD INSTALLED</P>)

Part: DISPLAY — INOPERATIVE (COCKPIT) · airframe 55,078 hrs · 38,055 cycles

CENTER RADAR DISPLAY INOP. REMOVED AND REPLACED CENTER WX RADAR DISPLAY UNIT AS PER AMM 34-43-06 DISPLAY UNIT. GROUND OPS CHECK GOOD.

Part: ENGINE — UNKNOWN · airframe 55,037 hrs · 38,041 cycles

DURING TAKEOFF, RIGHT ENGINE THRUST 94.2 N1, AUTOTHROTTLE SET 92.2 N1, AND REQUIRED A MANUAL ADJUSTMENT TO SET REQUIRED THRUST, LEFT ENGINE NORMAL, DISCONNECTED CDP SENSE LINE AND EXAMINED FOR BLOCKAGE AND LEAKAGE WITH NO NO DEFECTS NOTED, INSTALLED CDP SENSE LINE AND PERFORMED LEAK CHECK DURING GROUND ENGINE IDLE RUNS, NO LEAKS NOTED PERFORMED ADJUSTMENT OF APPROACH IDLE CHECK IAW AMM 71-01-02 AND FUCNTION CHECK NORMAL , ALL REQUIREMENT OF ECM ITEM 2018P-731 HAVE BEEN ACCOMPLISHED.

Part: FIRE LOOP — INOPERATIVE (RT ENGINE) · airframe 54,978 hrs · 38,019 cycles

RT ENG FIRE LOOP 1 INOP. REMOVED AND REPLACED RT ENG UPPER AFT FIRE LOOP DETECTOR ASSY IAW AMM 26-11-02. STATUS MSG CLEARED, FIRE TEST NORMAL.

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 54,974 hrs · 38,017 cycles

COCKPIT EMERGENCY LIGHT ASSY ABOVE DOOR INOP. REMOVED AND REPLACED COCKPIT EMERGENCY LIGHT ASSY IAW AMM 33-51-11. OPS CK GOOD.

Part: CIRCUIT CARD — FAULTY (RT ENGINE) · airframe 54,967 hrs · 38,013 cycles

EICAS MSG "RT ENG SPEED CARD" DISPLAYED. C/W FIM 73-21 FT 815. R&R RIGHT ENG N2 SPEED CARD IAW AMM 73-21-54. MSG CLEARED. PERFORMED GROUND ENG RUN IAW CHECK LIST, NO MESSAGES AND OPS CK GOOD.

Part: O-RING — DAMAGED (APU) · airframe 54,967 hrs · 38,013 cycles

EVIDENCE OF OIL SEEP AT APU OIL COOLING LINES AT OIL COOLER BYPASS VALVE ON APU. R&R O-RING FOR OIL COOLER TO OIL COOLER BYPASS VALVE IAW AMM 49-27-10. NO LEAKS NOTED.

Part: CIRCUIT CARD — FAULTY (RT ENGINE) · airframe 54,967 hrs · 38,013 cycles

EICAS MESSAGE RT ENGINE SPEED CARD DISPLAYED. C/W FIM 73-21 FT 815. REMOVED AND REPLACED N2 SPEED CARD IAW AMM 73-21-54SG CLEARED PERFORMED GROUND ENGINE RUN NO MESSAGES AND OPS CHECK GOOD.

Part: UNKNOWN — MALFUNCTIONED (MAIN BATTERY) · airframe 54,964 hrs · 38,012 cycles

AIRCRAFT MAIN BATTERY SHOWS 3 VOLTS. SWAPPED MAIN BATTERY WITH APU FOR TROUBLESHOOTING MAIN AIRCRAFT BATTERY SHOWS CHARGED NO OTHER DEFECTS IAW AMM 24-31-01.

Part: TRANSCEIVER — FAULTY (WEATHER RADAR) · airframe 54,905 hrs · 37,990 cycles

LEFT RADAR SYSTEM DISPLAYS INTERMITTENT SPIKES ON BOTH CA & FO EHSI. REMOVED AND REPLACED LEFT RADAR RT IAW AMM 34-43-01 GROUND OPS CHECK GOOD AND TEST OPS CHECK GOOD.

Part: CONTROLLER — DEFECTIVE (CABIN TEMP) · airframe 54,879 hrs · 37,983 cycles

AFT CABIN TEMP WAS INOPERATIVE. PERFORMED A BITE TEST OF THE ZONE TEMP CONTROLLER FAULT TRIM VALVE, FOUND AFT ZONE TEMP VALVE MOTOR CIRCUIT BREAKER TRIPPED. REMOVED AND REPLACED ZONE TEMP TRIM AIR VALVE. OPS CHECKED GOOD IAW AMM 21-61-01. FOUND THE ZONE TEMP CONTROLLER FAULT LIGHT REMAINED. REMOVED AND REPLACED THE CABIN ZONE TEMP CONTROLLER IAW AMM 21-61-03. ZONE TEMP OPS CHECKED GOOD IN MANUAL & AUTO.

Part: FAN — NOT REPORTED (E/E BAY) · airframe 54,836 hrs · 37,969 cycles

FWD EQUIPMET COOLING EXHAUST FAN. REMOVED AND REPLACED FWD EQUIP COOLING EXHAUST FAN 1 IAW AMM 21-58-06. OPS CHECKED GOOD,

Part: ANTI-ICE VALVE — MALFUNCTIONED (RT WING) · airframe 54,802 hrs · 37,953 cycles

RIGHT WING ANTI-ICE LIGHT FLASHED ON AND OFF DURING FLIGHT. R & R THE RT WING ANTI-ICE VALVE ASSY IAW AMM 30-11-02. VALVE AND LIGHT GROUND OPS CHECKED GOOD.

Part: WARNING MESSAGE — FALSE ACTIVATION (ANTI ICE SYS) · airframe 54,793 hrs · 37,949 cycles

RIGHT WING ANTI-ICE EICAS MESSAGE CAME ON IN FLIGHT. ACCOMPLISHED A RT WING ANTI-ICE TEST IAW AMM 30-11-02 -714-022, AND OPS TESTED OK ON GROUND. OK FOR SERVICE.

Part: ROD — DAMAGED (RT NACELLE) · airframe 54,788 hrs · 37,947 cycles

NR 2 ENGINE RT NACELLE PANEL, FWD HOLD OPEN ROD LOCK RELEASE COLLAR WILL NOT RELEASE. REMOVED AND REPLACED THE 2 ENGINE FORWARD HOLD OPEN ROD.

Part: CABLE — NOT REPORTED (VBV) · airframe 54,788 hrs · 37,947 cycles

VBV FLEX CABLE FAILED RIG TEST ON THE NR 2 ENGINE. REMOVED AND REPLACED VBV FLEX CABLE, RIGGED VBV AND VSV SYSTEM, FUNCTIONAL CHECK GOOD.

Part: WARNING LIGHT — FALSE ACTIVATION (ANTI ICE VALVE) · airframe 54,785 hrs · 37,946 cycles

RIGHT WING ANTI-ICE VALVE EICAS AFTER TAKE OFF, CHECKLIST COMPLIED WITH. AFTER LANDING AND SWITCH TO OFF, VALVE LIGHT REMAINED OUT, ACCOMPLISHED WING ANTI-ICE TEST IAW AMM 30-11-02, ANTI-ICE OPS CHECKED GOOD.

Part: WARNING MESSAGE — FALSE ACTIVATION (RT ANTI ICE) · airframe 54,782 hrs · 37,944 cycles

RIGHT WING ANTI-ICE VALVE EICAS ILLUMINATED AFTER TAKE OFF, CHECK LIST COMPLIED WITH. AFTER LANDING AND SWITCH TO OFF, VALVE LIGHT REMAINED OUT, ACCOMPLISHED WING ANTI-ICE TEST IAW AMM 30-11-02-214. ANTI-ICE OPS CHECKED NORMAL.

Part: FILTER — WARNING MESSAGE (FUEL SYS) · airframe 54,717 hrs · 37,915 cycles

INTERMITTENT RIGHT ENGINE FUEL FILT EICAS MESSAGE AT HIGH THRUST SETTINGS&NBSP;(<P>ACCOMPLISHED FIM 73-11 F/T 804. FOUND CONTAMINATION ON FILTER ELEMENT (NO METAL) REMOVED AND REPLACED FILTER ELEMENT IAW AMM 73-11-02. PERFORMED OPS OF DIFFERENTIAL PRESSURE SWITCH IAW AMM 73-34-00. SWITCH OPS CHECK GOOD. GROUND RUN ENGINE IAW AMM 71-20-00. LEAK AND OPS CK GOOD&NBSP;&NBSP;</P>)

Part: CONTROLLER — FAULTED (LT A/C PACK) · airframe 54,678 hrs · 37,901 cycles

LEFT PACK EICAS MAINT MESSAGE. ACCOMPLISHED FIM 21-51-F/T 803, PACK CONTROLLER FAULTED. REMOVED AND REPLACED LEFT PACK CONTROLLER IAW AMM 21-51-14, LEFT PACK SYS TESTED OK.

Part: ACTUATOR — MALFUNCTIONED (APU) · airframe 54,672 hrs · 37,897 cycles

EICAS APU FAULT. REMOVED AND REPLACED APU INLET DOOR MAGNETIC ACTUATOR IAW AMM 49-15-02, INSPECTED APU PLENUM AND INTAKE DUCT FOR FOD AND FOD DAMAGE TO MISSING PART , NO DAMAGED OR FOD FOUND IAW AMM 49-15-03, APU OPS CHECKED NORMAL.

Part: WARNING LIGHT — FALSE ACTIVATION · airframe 54,671 hrs · 37,896 cycles

DURING TAKE OFF ROLL, THE RT ENGINE BLEED OFF EICAS AND OFF LIGHT ILLUMINATED ZERO DUCT PRESSURE INDICATED. COMPLIED WITH FIM 36-20 FT 104. RT ENGINE PRSOV FAULT, INSPECTED RT ENG PRSOV VALVE, SENSE LINES, AND ELECTRICAL CONNECTOR , BITE CHECKED THE AIR SUPPLY , NO FAULTS, PERFORMED GROUND RUN OF RT ENGINE , PNEUMATICS OPS CHECKED GOOD IAW AMM 71-00-00.

Part: CONTROL CARD — FAILED (RT A/C PACK) · airframe 54,661 hrs · 37,891 cycles

RIGHT PACK OFF LIGHT NOT ILLUMINATED AND RT PACK OFF EICAS WITH PACK OFF. ACCOMPLISHED FIM 21-51 F/T 810. REPLACED RT PACK CONTROL CARD. RT PACK LIGHT AND EICAS OPS CHECKED GOOD IAW AMM 21-51-09.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 54,655 hrs · 37,887 cycles

R2 EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMPS, OPS CHECKED GOOD IAW AMM 33-51-00.

Part: SLEEVE — NOT REPORTED (NR 1 IDG) · airframe 54,654 hrs · 37,886 cycles

NR 1 ENG IDG GENERATOR POWER FEEDER SHRINK SLEEVING REQUIRES REPLACEMENT. REMOVED AND REPLACED NR 1 ENG IDG POWER FEEDER COLD SHRINK SLEEVES ON ALL 3 TERMINALS IN ACCORDANCE WITH SWPM 20-30-14 AND AMM 24-11-01-404-*003-003.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 54,654 hrs · 37,886 cycles

FWD CARGO COMPARTMENT RT SIDE MAIN CABIN FLOOR INTERCOSTAL IS CRACKED IN TWO PLACES, STA 390 TO STA 412, RBL 36. REMOVED, FABRICATED AND INSTALLED FWD CARGO COMPARTMENT RT SIDE MAIN CABIN FLOOR INTERCOSTAL IAW SRM 51-40-02-0G-0.

Part: SKIN — DAMAGED (LT WING TE FLAP) · airframe 54,654 hrs · 37,886 cycles

CHAFED, CREASE TYPE DENT ON UPPER LEADING EDGE SURFACE OF THE LT WING, INBD T/E FLAP. REMOVED AND REPLACED THE LT WING TE FLAP SKIN IAW SRM 51-40-04-0G-0.

Part: SKIN — GOUGED (NR 1 PYLON) · airframe 54,654 hrs · 37,886 cycles

NR 1 PYLON RT SIDE, ABOVE CORE COWL CENTER HINGE, THE ACCESS DOOR CUTOUT INNER SKIN IS GOUGED. ACCOMPLISHED BLEND OUT AT NR 1 ENGINE PYLON NACELLE STRUT SKIN INNER SURFACE IAW EA 767-5451-28-A6972.

Part: FRAME — CRACKED (BS 742) · airframe 54,654 hrs · 37,886 cycles

FWD CARGO FRAME CRACKED AT BS 742 APPROX, 25 INCHES FROM LT CARGO SIDE WALL. REMOVED, FABRICATED, AND INSTALLED FRAME IAW SRM 51-40-02-0G-0, AND DWG 140T2540.

Part: LINE — LEAKING (PITOT PROBE) · airframe 54,654 hrs · 37,886 cycles

LEFT AUX PITOT PROBE S2 IS LEAKING. TIGHTENED THE S2 LINE AND PERFORMED AND LEAK CHECKED GOOD IAW AMM 34-11-00-730-807.

Part: SPRING — BROKEN (CHECK VALVE) · airframe 54,654 hrs · 37,886 cycles

FWD CARGO BAY E/E COOLING SUPPLY FAN CHECK VALVE FLAPPERS HAS A BROKEN SPRING. REMOVED AND REPLACED E/E COOLING SUPPLY FAN CHECK VALVE, OPS AND LEAK CHECKED GOOD IAW AMM 21-58-02

Part: STRINGER — CORRODED (BS 1235-1251) · corrosion level 2 · airframe 54,654 hrs · 37,886 cycles

AFT CARGO BAY AT BS 1241, STRINGER 36R HAS CORROSION. REMOVED, FABRICATED AND INSTALLED A NEW SECTION OF THE STRINGER IAW SRM 53-00-03-2R-2, REPAIR 2.

Part: VALVE — NO TEST (PNEUMATIC SYS) · airframe 54,654 hrs · 37,886 cycles

LEFT PACK LOW LIMIT VALVE PNEUMATIC CHECK FAILED TO TEST. THE LOW LIMIT VALVE DID NOT OPEN AFTER 5 MINUTES. RECONFIGURED AIRCRAFT AND PERFORMED AN OPS CHECK IAW AMM 21-51-11-702, OPS CHECKED GOOD.

Part: SHUTOFF VALVE — NO TEST (NR 2 ENGINE) · airframe 54,654 hrs · 37,886 cycles

NR 2 ENGINE PRSOV FAILED A FUNCTIONAL CHECK. REMOVED AND REPLACED THE PRSOV, OPS CHECKED GOOD IAW AMM 36-11-09.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 54,654 hrs · 37,886 cycles

MAIN CABIN RIGHT AFT EMERGENCY EXIT LENS HAS A PIECE BROKEN OFF AT BS 1430. REPLACED THE LENS IAW AMM 33-51-01.

Part: TRACK — DAMAGED (FWD CARGO DOOR) · airframe 54,654 hrs · 37,886 cycles

FWD CARGO DOOR AFT CUTOUT CENTER GUILD TRACK LANDING IS WORN AND HAS A GROOVE. FWD CARGO DOOR AFT CUTOUT CENTER GUIDETRACK REPAIRED IAW EA 767-5330-28-A6983.

Part: CLAMP — WORN (START VALVE) · airframe 54,654 hrs · 37,886 cycles

DURING REMOVAL OF THE NR 2 ENGINE START VALVE, FOUND AFT VEE CLAMP THREADS WORN. INSTALLED NEW NR 2 ENGINE START VALVE VEE CLAMP IAW AMM 80-11-02-404-022-G00.

Part: CONNECTOR — CONTAMINATED (PITOT PROBE) · airframe 54,654 hrs · 37,886 cycles

CAPTAIN`S PITOT PROBE HAD CONTAMINATION. REMOVED AND REPLACED BACKSHELL ON CAPT PITOT PROBE CONNECTOR IAW SWPM 20-61-00, OPS CHECKED GOOD.

Part: ISOLATION VALVE — UNKNOWN · airframe 54,654 hrs · 37,886 cycles

INSPECTED ISOLATION BYPASS VALVES, VALVE FAILED VISUAL INSPECTION. REMOVED AND REPLACED THE ISOLATION BYPASS VALVE IAW AMM 36-11-04/401.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 54,654 hrs · 37,886 cycles

BULK CARGO COMPARTMENT FLOOR STRINGER AT STA 1518, LBL14 HAS A CRACK. REMOVED AND REPLACED STRINGER BETWEEN STA 1417 AND STA 1540, LBL 14 AT BULK CARGO COMPT FLOOR AREA IN REF SRM 51-40-02-0G-0.

Part: DENSITOMETER — FAILED (FUEL QTY) · airframe 54,654 hrs · 37,886 cycles

FUEL QTY BITE EICAS MESSAGE DISPLAYED. REMOVED AND REPLACED DENSITOMETER UNIT M597 AND MAIN FUEL TANK COMPENSATOR AT RT MAIN FUEL TANK IAW AMM 28-41-03 AND AMM 28-41-02, OPS CHECK GOOD IAW 28-41-00.

Part: WIRE — BROKEN (FUEL FLOW) · airframe 54,654 hrs · 37,886 cycles

NR 1 ENGINE READS 13.6 FUEL FLOW ON EICAS. REPAIRED A BROKEN WIRE W744-302 B-24 AND PERFORMED AN ENGINE RUN, FUEL FLOW INDICATION NORMAL IAW SWPM 20-30-12 AND AMM 71-00-00-501.

Part: FLOOR SUPPORT — CRACKED (BS 390) · airframe 54,654 hrs · 37,886 cycles

FWD CARGO, LT SIDE MAIN CABIN FLOOR SUPPORT CRACKED AT BS 390, LBL 36. REMOVED, FABRICATED, AND INSTALLED A REPLACEMENT IAW SRM 51-40-02-0G-0, AND DWG 141T5140.

Part: CONNECTOR — DAMAGED (TEMP CONTROLLER) · airframe 54,654 hrs · 37,886 cycles

NO GO LIGHT COMES ON AT POS 7 OF TEST SWITCH ON THE STANDBY PACK TEMP CONTROLLER. CLEANED AND INSPECTED THE CONNECTOR TS5133. PERFORMED PACK STANDBY CONTROLLER BITE TEST, BITE TESTED GOOD IAW SWPM 20-60-01 AND SWPM 20-60-06.

Part: SEAT TRACK — CORRODED (BS 852) · airframe 54,654 hrs · 37,886 cycles

MAIN CABIN RT SIDE SEAT TRACK HAS CORROSION AT BS 852. REMOVED AND REPLACED THE SEAT TRACK SECTION, BETWEEN BS 795 TO 878, RBL 88.5 IAW SRM 53-00-52-2R-3, REPAIR 3.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 54,654 hrs · 37,886 cycles

DURING CEILING PANEL INSTALLATION, FOUND A WIRE TERMINAL BROKEN AT THE MID LT EXIT SIGN. TERMINATED THE WIRE IAW SWPM 20-30-11 AND WPM 33-51-13, OPS CHECKED GOOD IAW 33-51-01.

Part: SLEEVE — INADEQUATE (FEEDER CABLE) · airframe 54,654 hrs · 37,886 cycles

NR 2 GENERATOR POWER FEEDER SHRINK SLEEVE INADEQUATE. REMOVED AND REPLACED SLEEVE IAWI 20-30-14 AND AMM 24-11-01-404-003-003.

Part: SKIN — CHAFED (RT WING TE FLAP) · airframe 54,654 hrs · 37,886 cycles

RIGHT INBD SIDE OF AFT FLAP HAS CHAFE DAMAGE FROM FWD FLAP SEAL RETAINER. REMOVED AND REPLACED THE RT WING FLAP SKIN IAW SRM 51-40-04-0G-0.

Part: FLOORBEAM — CRACKED (BS 1502) · airframe 54,654 hrs · 37,886 cycles

BULK CARGO FLOORBEAM ANGLE CRACKED AT BS 1502, LBL 18. REPAIRED THE FLOORBEAM IAW SRM 51-40-02-0G-0.

Part: INTERCOSTAL — BENT (BS 610-615) · airframe 54,654 hrs · 37,886 cycles

FWD CARGO AFT CUTOUT, UPPER CEILING FRAME INTERCOSTAL IS BENT BS 610. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM 51-40-02-0G-0.

Part: VALVE — NO TEST (A/C PACK) · airframe 54,654 hrs · 37,886 cycles

PACK LOW LIMIT VALVE PNEUMATIC CHECK, FAILED TEST ON STEP 1 B 4, LOW LIMIT VALVE DID NOT OPEN AFTER 5 MINUTES. REMOVED AND REPLACED RT LOW LIMIT VALVE AND OPS CHECK GOOD IAW AMM 21-51-11 AND AMM 21-51-11-702.

Part: PRESSURE SWITCH — NO TEST (FUEL FILTER) · airframe 54,654 hrs · 37,886 cycles

NR 2 ENGINE FUEL FILTER BYPASS DIFFERENTIAL PRESSURE SWITCH FAILED A FUNCTIONAL CHECK. REMOVED AND REPLACED THE NR 2 ENGINE FUEL FILTER BYPASS DIFFERENTIAL PRESSURE SWITCH, OPS CHECKED GOOD IAW AMM 73-34-01 AND AMM 71-00-00.

Part: CABLE ASSY — MALFUNCTIONED (VSV FEED BACK) · airframe 54,654 hrs · 37,886 cycles

NR 2 ENGINE SLOW TO SPOOL. REMOVED AND REPLACED THE NR 2 ENGINE VSV FEED BACK CABLE ASSY, OPS CHECKED GOOD AND ACCELERATION NORMAL IAW AMM 75-31-03, AND AMM 71-00-00.

Part: WIRE — DAMAGED (FWD CARGO) · airframe 54,654 hrs · 37,886 cycles

SINGLE WIRE KNICKED AND SLIGHTLY CRUSHED IN LEFT SIDE WALL BETWEEN BS 698 - 720 ON FWD CARGO BAY. REPAIRED THE WIRE 744-02-24 IAW SWPM 20-10-13, OPS CHECKED GOOD IAW AMM 73-34-00.

Part: LANYARD — BROKEN (OVERWING EXIT) · airframe 54,654 hrs · 37,886 cycles

LT OFF WING SLIDE COMPARTMENT DOOR INTEGRATOR, LOCK PIN "A" LANYARD BROKEN (ACCESS DOOR 195ML). REMOVED AND REPLACED LT OFF WING SLIDE COMPARTMENT DOOR INTEGRATOR, LOCK PIN "A" LANYARD IAW AMM 25-65-12-404-013-001.

Part: SPRING — BROKEN (CHECK VALVE) · airframe 54,654 hrs · 37,886 cycles

RIGHT PACK BAY TRIM AIR CHECK VALVE FLAPPER HAS BROKEN SPRING. REMOVED AND REPLACED THE RT PACK BAY TRIM AIR CHECK VALVE, OPS AND LEAK CHECKED GOOD IAW AMM 21-61-05</P>)

Part: RELAY — FAILED (SMOKE DETECTOR) · airframe 54,654 hrs · 37,886 cycles

FWD CARGO BAY SMOKE TEST, NR 1 FROM FWD DOES NOT GIVE INDICATION WHEN SMOKE IS APPLIED TO ORIFICE. REMOVED AND REPLACED THE RELAY K331 AT P35 IAW SWPM 20-81-22, OPS CHECKED GOOD IAW AMM 26-16-00.

Part: FITTING — LOOSE (PITOT/STATIC SYS) · airframe 54,669 hrs · 37,895 cycles

FO PITOT SYSTEM LEAKS. FOUND FO PITOT FITTING BEHIND PROBE LOOSE. TIGHTENED AND LEAK CHECK GOOD PER AMM 34-11-00.

Part: MEDICAL KIT — MISSING (COCKPIT) · airframe 54,654 hrs · 37,886 cycles

EMERGENCY MEDICAL KIT MISSING IN THE COCKPIT. REPLACED THE MEDICAL KIT IAW T/C A-25-018-01, AND T/C 1102.

Part: CONNECTOR — DAMAGED (PITOT TUBE) · airframe 54,654 hrs · 37,886 cycles

FIRST OFFICER`S PITOT PROBE FOUND MISSING BACK SHELL. REMOVED AND REPLACED THE CONNECTOR IAW SWPM 20-61-00. OPS CHECKED GOOD.

Part: STARTER — LEAKING (NR 2 ENGINE) · airframe 54,654 hrs · 37,886 cycles

NR 2 ENGINE BELOW ACCESSORY GEAR BOX, PNEUMATIC STARTER HAS EVIDENCE OF A LEAK. REMOVED AND REPLACED THE NR 2 ENGINE STARTER, OPS AND LEAK CHECKED GOOD IAW AMM 80-11-01, AND 67 71-00-00</P>)

Part: STRUCTURE — DAMAGED (NR 2 PYLON) · airframe 54,654 hrs · 37,886 cycles

WHILE RESTORING NR 2 PYLON, FOUND THE RT LOWER FWD STRUCTURE CRACKED AND EXFOLIATED. REMOVED, FABRICATED AND INSTALLED NEW STRUCTURE IAW SRM 51-40-02-09-0, AND DWG 313T3310.

Part: DUCT — CRACKED (APU) · airframe 54,654 hrs · 37,886 cycles

APU SUPPLY DUCT AT LEFT WHEEL WELL BETWEEN BS 1024 AND 1043 IS CRACKED AT WELD POINT WHERE LINE IS CONNECTED. REMOVED AND REPLACED APU SUPPLY DUCT. LEAK CHECKED GOOD IAW AMM 36-11-01.

Part: SHUTOFF VALVE — NO TEST (NR 1 ENGINE) · airframe 54,654 hrs · 37,886 cycles

NR 1 ENGINE PRSOV FAILED A FUNCTIONAL CHECK. REMOVED AND REPLACED THE PRSOV. OPS CHECKED GOOD IAW AMM 36-11-09.

Part: FAULT MESSAGE — FALSE ACTIVATION (EQUIP COOLING) · airframe 54,663 hrs · 37,892 cycles

EQUIP COOLING EICAS MESSAGE DISPLAYED. PERFORMED FIM 21-58, FT 873. RESET ALL FAULTS, OPS CHECKED, NO FAULTS FOUND IAW AMM 21-58-00.

Part: CONTROLLER — MALFUNCTIONED (RT ENGINE) · airframe 54,642 hrs · 37,880 cycles

RIGHT ENGINE BLEED VALVE CAUTION MESSAGE DURING DESCENT. EMOVED AND REPLACED RT ENGINE HPSOV CONTROLLER IAW AMM 36-11-08. OPS CHECKED GOOD ON GROUND.

Part: WARNING MESSAGE — FALSE ACTIVATION (RT BLEED VALVE) · airframe 54,632 hrs · 37,879 cycles

RIGHT ENGINE BLEED VALVE CAUTION DESCENDING OUT OF FL 390. ACCOMPLISHED FIM 36-11 FT 954. NO DEFECTS NOTED TO SENSE, MUSCLE OR LINES. NO DEFECTS TO WIRING OR CONNECTORS PERFORMED HPSOV OPS CHECK IAW AMM 36-11-07, OPS CHECKED NORMAL. GROUND RUN ENGINE, RT ENGINE BLEED AIR OPS OK NORMAL.

Part: SHUTOFF VALVE — MALFUNCTIONED (RT ENGINE) · airframe 54,610 hrs · 37,873 cycles

EICAS MESSAGE RT ENGINE BLEED , BLEED LIGHT FLASHING TWICE WITH LOW ENGINE POWER. REMOVED AND REPLACED THE HPSOV IAW AMM 36-11-07. OPS CHECKED OK.

Part: APU — MALFUNCTIONED · airframe 54,590 hrs · 37,868 cycles

APU FAILED TO START DURING TAXI IN. ACCOMPLISHED APU BITE PROCEDURES IAW FIM 49-11 /FT 103. NO CODES OR FAULTS FOUND. INSPECTED APU, APU BATTERY, AND STARTER. NO DEFECTS NOTED. PLUGGED IN GROUND POWER UNIT IN , APU STARTED NORMAL . OPERATED APU NUMEROUS STARTS & STOP. APU OPS CHECKED GOOD.

Part: VALVE — MALFUNCTIONED (INTERCONNECT) · airframe 54,572 hrs · 37,861 cycles

EICAS MAINTENANCE MESSAGE FOR EQUIP COOLING BITE DISPLAYED. ACCOMPLISHED EQUIP COOLING BITE TEST IAW FIM 21-58 F/T 873 FOUND INTERCONNECT VALVE TO BE STICKING AND SLOW, REMOVED AND REPLACED INTERCONNECT VALVE IAW AMM 21-58-01, VALVE OPS CHECKED GOOD, NO MESSAGE, GOOD BITE CHECK OF CONTROLLER.

Part: TRANSCEIVER — FAILED (WX RADAR SYS) · airframe 54,571 hrs · 37,860 cycles

DURING CLIMB, THE LEFT WEATHER RADAR FAILED DISPLAYED IN FLT, SWITCHED TO RT WEATHER RADAR AND OPS CHECKED GOOD. REMOVED AND REPLACED THE LEFT RADAR R/T IAW AMM 34-43-01. PERFORMED AN OPS CHECK , OPS CHECKED GOOD.

Part: VALVE — MALFUNCTIONED (RT A/C PACK) · airframe 54,563 hrs · 37,857 cycles

RIGHT PACK TEMP EICAS ILLUMINATED. RIGHT PACK INOPERATIVE ILLUMINATED. OPS CHECKED GOOD IN STANDBY. ACCOMPLISHED FIM 21-51 FT 803 , REMOVED AND REPLACED RT PACK TEMP CONTROL VALVE IAW AMM 21-51-12. RT PACK OPS CHECKED NORMAL. NO MESSAGES.

Part: CONTROL VALVE — FAILED (CABIN TEMP) · airframe 54,561 hrs · 37,856 cycles

AFT CABIN TEMP WILL NOT STAY WARM. C/W FIM 21-51-00 BITE CHECK, RT PACK CONTROLLER, RT PACK TEMP CONTROL VALVE FAULTED. R & R THE RT PACK TEMP CONTROL VALVE IAW AMM 21-51-12. RT PACK CONTROL VALVE LEAK AND OPS CHECKED GOOD. ALL ZONES CONTROLLABLE ON GROUND.

Part: SOLENOID — FAILED (RT ENGINE) · airframe 54,548 hrs · 37,850 cycles

RIGHT ENGINE EEC OFF EICAS AND OFF LIGHT ILLUMINATED ON POWER TRANSFER DURING ENGINE START. RESET AND OPS NORMAL FOR FULL FLIGHT, COMPLIED WITH FIM 73-21 FT 805 AND FIM 71-01FT 804 REMOVED AND REPLACED THE RT ENGINE PMC IAW AMM 73-21-02, NO HELP, RE INSTALLED PMC TO RIGHT ENGINE. FUTHER TROUBLE SHOOTING EEC OPS CHECKED GOOD. COMPLIED WITH EEC BITE TEST IAW FIM 71-01 FT 804. REMOVED AND REPLACED THE RIGHT ENGINE, FIXED FAILED SOLENOID IAW AMM 73-21-13 BITE TESTED GOOD, NO FAULTS. PERFORMED ENGINE START & EEC OPS CHECKED NORMAL.

Part: STARTER — INOPERATIVE (APU) · airframe 54,502 hrs · 37,828 cycles

APU WILL NOT START ON GROUND 22-24 RPM MAXIMUM, NO ACCELERATION. ACCOMPLISHED FIM 49-11, F/T 960. R & R THE APU STARTER IAW AMM 49-41-01. APU OPS CHECKED GOOD.

Part: DUCT — TORN (APU BLEED) · airframe 54,497 hrs · 37,826 cycles

DURING AN APU INSPECTION, FOUND PNEUMATIC DUCT, FLEXIBLE DUCT FROM APU TO AIR SUPPLY DUCT TORN AND AFT CLAMP BROKEN. REPLACED THE FLEXIBLE PNEUMATIC DUCT ASSY AND CLAMPS ON APU AIR SUPPLY DUCT IAW AMM 49-53-01. LEAK AND OPERATIONAL CHECKED GOOD.

Part: COWLING — BENT (LT ENGINE) · airframe 54,436 hrs · 37,806 cycles

LT ENG O/B CORE COWL LEADING EDGE CORNER BENT DOWN FROM FLUSH. REMOVED FASTENERS REWORKED ARE IAW SRM 51-10-01. REINSTALLED FASTENERS IAW SRM 51-40-02. REPAIRS MADE BY STRUCTURES, ALSO ACCOMPLISHED NDT, HFEC INSPECTION AREA REWORKED NO CRACKS INDICATIONS NOTED.

Part: WARNING MESSAGE — FALSE ACTIVATION (ANTI ICE SYSTEM) · airframe 54,429 hrs · 37,803 cycles

LEFT WING ANTI-ICE EICAS MESSAGE DISPLAYED AFTER SYSTEM WAS SELECTED OFF. COMPLIED WITH FIM 30-11 F/T 803/805, LT WING ANTI-ICE OPS CHECKED NORMAL, NO DEFECT NOTED.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 54,370 hrs · 37,779 cycles

FLASHLIGHT IN THE COCKPIT NOT HOLDING CHARGE OR SWITCHING ON WHEN SELECTED. REMOVED AND REPLACED IAW AMM 25-64-00. OPS CHECKED SATISFACTORY.

Part: O-RING — WORN (OIL CAP) · airframe 54,346 hrs · 37,769 cycles

LT ENGINE OIL CAP O-RING WORN, LEAKING OIL. REPLACED LT ENG OIL CAP O-RING, LKS CK NML IAW AMM 79-11-03.

Part: ACM — INOPERATIVE (RIGHT) · airframe 54,331 hrs · 37,763 cycles

RT PACK TEMP INOPERATIVE. REMOVED AND REPLACED THE RT ACM AND NOZZLE.

Part: IGNITER — DEFECTIVE (LT ENGINE) · airframe 54,333 hrs · 37,764 cycles

ON LT ENGINE START, NO LIGHT OFF WITH WITH NR 1 IGNITOR. ENG START NORMAL USING BOTH. REMOVED AND REPLACED LT ENGINE SYSTEM NR 1 IGNITER IAW AMM 74-21-02. OPS CHECK NORMAL. P/N OFF CH31905. REMOVED AND REPLACED LT ENGINE SYSTEM 1 IGNITER LEAD IAW AMM 74-21-01. OPS CHECK NORMAL.

Part: IGNITION LEAD — BROKEN (NR 1) · airframe 54,331 hrs · 37,763 cycles

DURING LEFT ENGINE START, NO LIGHT OFF WITH NR 1 IGNITOR. ENGINE START WAS NORMAL USING BOTH. FOUND THE NR 1 IGNITION LEAD BROKEN,

Part: SWITCH — FAILED (LT GENERATOR) · airframe 54,331 hrs · 37,763 cycles

LEFT GENERATOR DRIVE DISCONNECT SWITCH FELL APART. REMOVED AND REPLACED THE LT GENERATOR DRIVE DISCONNECT SWITCH ASSY PER BOEING SOPM 20-11-05 STEP 5, A+F. OPS CHECKED GOOD IAW MM 24-11-00-745 +001.

Part: ACM — FAULTY (AC BAY) · airframe 54,329 hrs · 37,762 cycles

RT PACK TEMP INOP. REMOVED AND REPLACED RT PACK ACM AND NOZZLE. OPS AND LEAK CHECK GOOD AS PER AMM 21-51-03; 21-53-05. P/N OFF FOR NOZZLE 2203085-1 S/N OFF FOR NOZZLE 72-191.

Part: O-RING — DAMAGED (APU) · airframe 54,331 hrs · 37,763 cycles

O-RING APU OIL CAP DAMAGED. REPLACED O-RING IAW AMM 49-11-00 AND LEAK CHECK. NO LEAKS NOTED.

Part: LINE — DAMAGED (BOOST PUMP) · airframe 54,322 hrs · 37,759 cycles

RT AFT FUEL PUMP LIGHT CAME ON 35 MINUTES INTO FLIGHT , PERFORMED QRH . PERFORMED FIM 28-22 FT 819 BLEED AFT RT BOOST PUMP PRESSURE SENSE LINE IAW AMM 28-42-01 NO DEFECTS NOTED OPS CHECK NORMAL.

Part: SHUTOFF VALVE — FAULTY (BLEED AIR SYS) · airframe 54,279 hrs · 37,746 cycles

LEFT ENGINE BLEED VALVE, PLACE ON MEL 36-11-02-01, MDDR 68970, LOG PAGE 715797. R & R LT ENGINE HPSOV IAW AMM 36-11-07 LEAK CHECK NORMAL. OPS CHECK NORMAL MDDR CLEARED.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 54,245 hrs · 37,734 cycles

EICAS MSG FIRE/OVERHEAT SYS C/W QRH 8.25 STATUS MSG RT ENGINE O/H LP2. RT ENGINE O/H LP1. PERFORMED FIM 26-11, F/T 804R. RT ENGINE FAULT CARD M10274 IAW AMM 26-10-01 INSPECTED. RT ENGINE OVERHEAT DETECTORS, NO DEFECTS NOTED INSP BLEED DUCTS, CLAMPS FOR LEAKS NO DEFECTS NOTED FIRE/OVERHEAT SYS OPS CK GOOD AT THIS TIME.

Part: PROCESSING UNIT — MALFUNCTIONED (FUEL SYSTEM) · airframe 54,189 hrs · 37,718 cycles

CENTER TANK FUEL QTY INDICATING BLANK. TRANSFERRED TO MEL 28-41-01-02-01, MDDR 67060. R & R FQIS PROCESSOR UNIT IAW AMM 28-41-08. ALL INDICATION SATISFACTORY.

Part: DOOR — UNKNOWN (CABIN) · airframe 54,127 hrs · 37,692 cycles

RT WING SLIDE EICAS MSG, EMER DOOR LIGHT OVERHEAD PANEL, HAPPENED AT GEAR DOWN FLAPS 20, IAW QRH. R&R RT WING SLIDE PER AMM 25-65-01. R&R OVERWING SLIDE DOOR LATCHES IAW AMM 25-65-09 OPS CHECK NORMAL. CHECKED DOOR FOR PROPER FIT AND CLOSING PER AMM 25-56-01, ALL NORMAL. R&R RT OVERWING SLIDE DOOR OPENING ACTUATOR (FWD) IAW AMM 25-65-10. R&R RT OVERWING SLIDE DOOR OPENING ACTUATOR (AFT) IAW AMM 25-65-10. R&R RT OVERWING SLIDE DOOR LATCH OPENING ACTUATOR PER AMM 25-65-11. R&R RT OVERWING SLIDE DOOR CONTROL CABLE PER AMM 25-65-04 OPS CKS NORMAL. R&R RT OVER WING SLIDE DOOR INTEGRATOR PER AMM 25-65-07 OPS CKS NORMAL.

Part: SHUTOFF VALVE — MALFUNCTIONED (BLEED AIR SYS) · airframe 54,117 hrs · 37,688 cycles

LOG PAGE 709442 NR 5. LT ENG BLEED OFF LT EXTINGUISHED & WHEN SHOULD BE ILLUMINATED, IN SWITCH, & LOG PAGE 709442 NR 6 & LT ENG BLEED VLV EICAS MSG & LOG PAGE 709443 NR 7 & LT ENG BLEED LIGHT ILLUMINATED INTERMITTENTLY. R & R HIGH PRESS SOV. OPERATIONS CHECKED GOOD IAW AMM 36-23-11 & AMM 36-11-51.

Part: WIRE — BROKEN (IGNITION SYS) · airframe 54,117 hrs · 37,688 cycles

RIGHT ENG NR 1 IGNITION INOPERATIVE. FOUND BROKEN WIRE AT RELAY K607 PIN A1 IN P11 NR 1 IGN SYS. RE-TERMINATED WIRE W040-714-22 IAW SWPM 20-81-12 & WDM 74-31-21. OPERATIONS CHECKED RT NR 1 IGN IAW AMM 74-00-00. OPERATIONS CHECKED GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 54,115 hrs · 37,684 cycles

SEVERAL EMER LIGHTS BATTERY PACKS FAILED IN CABIN. TROUBLESHOOTING REVEALED LIGHT BATTERY PACKS INOPERATIVE, M961, M962 & M737. R & R BATTERY PACKS WITH SERVICEABLE UNITS IAW 33-51-07. OPERATIONS CHECKED OK.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 54,115 hrs · 37,684 cycles

LEFT AFT DOOR EXTERIOR LIGHT IS INOPERATIVE, EMER. TROUBLESHOOTING REVEALED AFT DOOR EXTERIOR LIGHT BURNED OUT. R & R BULB GE767. OPERATIONS CHECKED GOOD IAW AMM 33-51-00.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 54,115 hrs · 37,684 cycles

RIGHT EXTERIOR EMER LIGHT JUST AFT OF CARGO DOOR INOPERATIVE. TROUBLESHOOTING REVEALED LIGHT POWER LUG BROKEN. R & R LIGHT ASSEMBLY HOUSING, PN 30-1564-4 & SN 0037 IAW WMD 33-51-21. OPERATIONS CHECKED GOOD.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 54,115 hrs · 37,684 cycles

LEFT EXTERIOR EMERGENCY LIGHT JUST AFT OF WING INOPERATIVE. TROUBLESHOOTING REVEALED LT EXTERIOR EMERGENCY LIGHT BULB BURNED OUT. R & R THE BULB. OPS CHECKED GOOD IAW AMM 33-51-00.

Part: BATTERY — DISCHARGED (CABIN) · airframe 54,072 hrs · 37,675 cycles

LEFT FWD EXT EMER LIGHTS INOPERATIVE. R & R M736 EMER LIGHT BATTERY & CHARGER IAW AMM 33-51-07. OPERATIONS CHECKED NORMAL.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 54,032 hrs · 37,662 cycles

EMERGENCY EXIT LIGHTS AT L1 & ABOVE WING & LT SIDE INOPERATIVE. R & R EMER LIGHT BATTERY PACK & POWER SUPPLY IAW AMM 33-51-07. EMER LIGHTS OPERATIONS CHECKED GOOD UNIT M738 REPLACED.

Part: RELAY — FAILED (CABIN) · airframe 53,985 hrs · 37,648 cycles

LEFT SIDE EXTERIOR EMER FLASH ON & OFF WITH EMER LIGHTS IN NORMAL. TROUBLE SHOT IAW WDM 33-51-21. R & R LT SIDE RELAY K371 IAW AMM 20-10-01. OPERATIONS CHECKED GOOD.

Part: FUEL FILTER — DEFECTIVE (LT ENGINE) · airframe 53,954 hrs · 37,641 cycles

AFTER TAKEOFF CAUTION MESSAGE, LEFT ENGINE FUEL FILTER. MESSAGE CHANGED TO STATUS MESSAGE, LEFT ENGINE FUEL FILTER. R & R LEFT ENGINE FUEL FILTER IAW FIM 73-11 FT 804 & 73-11-02. OPERATIONS CHECKED, NO LEAKS NOTED.

Part: IDG — LOW (LT ENGINE) · airframe 53,943 hrs · 37,637 cycles

LEFT ENG, IDG OUT TEMP, MTC STATUS MSG. TROUBLE SHOT IAW FIM 24-20 TREE 807. ALL CHECKED OK. SERVICED LT ENG IDG IAW AMM 12-13-03. MSG CLEARED, OPERATIONS CHECKED GOOD & LEAK CHECKED GOOD.

Part: ACM — MALFUNCTIONED (AC BAY) · airframe 53,890 hrs · 37,617 cycles

RIGHT PACK INOPERATIVE. REMOVED AND REPLACED RT ACM PER AMM 21-51-03, OPS CHECK NORMAL, THIS CLEARS MEL 21-51-01-01 MDDR 57449.

Part: PUMP — FAILED (FWD RIGHT) · airframe 53,791 hrs · 37,572 cycles

FORWARD RT FUEL PUMP PRESS LIGHT ILLUMINATED. R & R RT FWD FUEL PUMP PRESS SWITCH IAW AMM 28-42-01. OPS & LEAK CHECKED OK.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 53,789 hrs · 37,571 cycles

FUEL QTY INDICATOR STATUS MSG, TOTALIZER INOPERATIVE. RESET FQIS THROUGH BITE TEST IAW FIM 28-41 FAULT TREE & SYS TESTED OK.

Part: INLET — CONTAMINATED (AC BAY) · airframe 53,760 hrs · 37,556 cycles

IN DESCENT STRANGE ODOR, CHEMICAL, SOLVENT SMELL. STOPPED AFTER LANDING. FOUND DE-ICE FLUID & GLYCOL IN RAM AIR INLETS & REAR EQUIPMENT COOLING INLET. CLEANED AREA IAW AMM 12-25-01. RAN AC PACKS & NO ODOR WAS NOTED.

Part: CONNECTOR — UNSECURE (FUEL SYSTEM) · airframe 53,721 hrs · 37,541 cycles

RIGHT FWD FUEL PUMP. RT FWD PRESS LIGHT ON. DURING TROUBLESHOOTING CONFIRMED PUMP OPERATION IS NORMAL. RT FWD FUEL PUMP PRESS SWITCH CONFIRMED FAILED. DURING ADDITIONAL TROUBLESHOOTING FOUND CONNECTOR NOT PROPERLY SECURED. CLEANED CONNECTOR & SEVERAL OPERATIONS CHECKED NORMAL IAW AMM 28-22-03.

Part: ACM — MALFUNCTIONED (AC BAY) · airframe 53,709 hrs · 37,535 cycles

RIGHT PACK INOPERATIVE LIGHT ON. R & R RT PACK ACM IAW AMM 21-51-03. OPERATIONS CHECKED GOOD.

Part: MONITOR — MALFUNCTIONED (EEC) · airframe 53,685 hrs · 37,529 cycles

MAINTENANCE MSG EEC MONITOR. R & R EEC MONITOR IAW AMM 77-35-01.

Part: PROCESSOR — FAULTY (FUEL SYSTEM) · airframe 53,685 hrs · 37,529 cycles

MAINTENANCE MSG FUEL QTY BITE. FAULTS BOTH CHANNELS REPLACED FQ PROCESSOR.

Part: ACM — FAILED (RIGHT) · airframe 53,665 hrs · 37,526 cycles

RIGHT PACK INOPERATIVE LIGHT. TROUBLESHOOTING SYS. R & R RT ACM IAW AMM 21-51-03. OPS CHECKED NORMAL.

Part: FUEL FILTER — FAULTED (RT ENGINE) · airframe 53,651 hrs · 37,523 cycles

RIGHT ENG FUEL FILTER EICAS MSG. R & R RT ENG FUEL FILTER IAW AMM 73-11-02. LEAK CHECKED GOOD.

Part: SLIDE — UNWANTED DEPLOY (OVERWING EXIT) · airframe 53,644 hrs · 37,520 cycles

RIGHT OVERWING SLIDE INADVERTENTLY DEPLOYED IN FLIGHT & SEPARATED FROM ACFT. CARRIAGE DEPLOYMENT BOTTLE DEPLETED. R & R RT OFF WING RAMP & SLIDE IAW MM 25-65-01-400.

Part: ACTUATOR — MALFUNCTIONED (OVERWING EXIT) · airframe 53,644 hrs · 37,520 cycles

RIGHT OVERWING SLIDE INADVERTENTLY DEPLOYED IN FLIGHT & SEPARATED FROM ACFT. CARRIAGE DEPLOYMENT BOTTLE DEPLETED. R & R RT OVERWING ESCAPE SYS LATCH DOOR ACTUATOR IAW MM 25-65-11-400.

Part: CLAMP — DEFECTIVE (NR 2 ENGINE) · airframe 536,430 hrs · 37,519 cycles

NUMBER 2 ENG CLAMP BELOW FAN AIR SOV IS MISSING CUSHION. REPLACED CLAMP IAW AMM 70-50-00.

Part: DOOR — FAILED (RT OVERWING SLID) · airframe 53,644 hrs · 37,520 cycles

RIGHT WING SLIDE DOOR OPENED IN FLIGHT. SLIDE DEPARTED ACFT ENROUTE. REPAIRED.

Part: GLOWSTRIP — OUT OF ALIGNMENT (CABIN) · airframe 53,643 hrs · 37,519 cycles

FLOOR MOUNTED GLOW STRIP OUT OF ALIGNMENT IN SEVERAL AREAS. ADJUSTED FLOOR MOUNTED GLOW STRIP & PERFORMED OPERATIONAL CHECK. CHECKED GOOD ALL IAW AMM 33-51-10.

Part: FITTING — BENT (NR 1 COWLING) · airframe 53,643 hrs · 37,519 cycles

NUMBER 1 ENG OTBD CORE COWL 3RD LATCH KEEPER HAS BENT TANG, WELL MARKED. R & R NR 1 ENG OTBD CORE COWL 3RD LATCH STOP ANTI-ROTATION TANG IAW AMM 71-11-07. PERFORMED ADJUSTMENT CHECK, CHECKED GOOD.

Part: IGNITER — WORN (APU) · airframe 53,643 hrs · 37,519 cycles

APU IGNITER PLUG WORN BEYOND LIMITS. INSTALLED NEW APU IGNITER PLUG. OPERATIONS GOOD IAW AMM 49-41-02.

Part: HOLDER — DEFECTIVE (EMERGENCY LIGHT) · airframe 53,643 hrs · 37,519 cycles

L1 SLIDE LIGHT INOPERATIVE. REPLACED LAMP HOLDER.

Part: CLAMP — DAMAGED (NR 2 ENGINE) · airframe 536,430 hrs · 37,519 cycles

NUMBER 2 ENG TURBINE SECTION BETWEEN 5 & 6 O`CLOCK HAS DAMAGED ADEL CLAMP & ATTACH BRACKET IS CHAFING CORE COWL. REPLACED ADEL CLAMP & BRACKET IAW AMM 70-50-00.

Part: HOLDER — DEFECTIVE (CABIN) · airframe 53,643 hrs · 37,519 cycles

RIGHT SIDE EMER LIGHTS INOPERATIVE. BATTERIES RECONDITIONED, SYS CHECKED GOOD. R2 REPLACED LAMP HOLDER,, SYS CHECKED GOOD.

Part: DUCT — DAMAGED (APU) · airframe 53,643 hrs · 37,519 cycles

APU COOLING FAN OUTLET DUCT IS TORN & SEPARATED FROM FAN OUTLET. PROCURED SERVICEABLE APU COOLING FAN OUTLET DUCT & INSTALLED ON TCA-49-064-01.

Part: SEAL — BENT (NR 2 ENGINE) · airframe 53,643 hrs · 37,519 cycles

NUMBER 2 ENG INBD SIDE INNER T/R COWL FAN AIR VLV INLET DUCT FLANGE IS BENT. R & R NR 2 ENG INBD SIDE INNER T/R COWL FAN AIR VLV INLET DUCT FLANGE SEAL IAW MM 70-50-00.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 53,643 hrs · 37,519 cycles

AFT CTR BULKHEAD CEILING EMER LIGHT INOPERATIVE. PERFORMED SATISFACTORY SYS TEST.

Part: COOLING DUCT — DETERIORATED (WEATHER RADAR) · airframe 53,643 hrs · 37,519 cycles

WEATHER RADAR RT COOLING DUCT DETERIORATED. R & R DUCT IAW MM 20-11-00.

Part: DRAIN LINE — CHAFED (APU) · airframe 53,643 hrs · 37,519 cycles

CHAFING WEAR ON AFT FUEL DRAIN LINE LOCATED ON APU DRAIN TUBE CLUSTER. CLEANED & VERIFIED LIMITS AT AFT FUEL DRAIN LINE ON APU. FOUND IN LIMITS IAW AMM 20-20-05.

Part: CABLE — LOOSE (APU) · airframe 53,643 hrs · 37,519 cycles

APU STARTER CABLES LOOSE. SECURED STARTER CABLES.

Part: FASTENER — LOOSE (APU BAY) · airframe 53,643 hrs · 37,519 cycles

TWO EACH FASTENERS LOOSE ON APU INLET PLENUM DRAIN PANEL. R & R IAW SRM 51-40-02.

Part: MOTOR — FAILED (NR 2) · airframe 53,610 hrs · 37,509 cycles

CABIN STATUS MSG CABIN ALT AUTO 2. R & R NR 2 AC MOTOR IAW AMM 21-31-05. OPERATIONS CHECKED GOOD.

Part: FIRE WARNING — FALSE ACTIVATION (COCKPIT) · airframe 53,561 hrs · 37,493 cycles

INFLIGHT EICAS MSG FIRE & OVERHEAT SYS. FOLLOWED QRH PROCEDURES UPON LANDING. STATUS MSG RT ENG OVERHEAT LP1 & LP2. COMPLIED WITH FIM 26-11 FAULT TREE 808 MSG CLEARS AFTER PERFORMING FIRE DETECTION BITE IAW AMM 26-11-00. SYS CHECKED OK FOR SERVICE.

Part: RADOME — DAMAGED (FUSELAGE) · airframe 53,528 hrs · 37,485 cycles

BIRD STRIKE BELOW FIRST OFFICERS FRONT WINDOW ON APPROACH. FOUND RADOME DAMAGED BEYOND LIMITS. R & R RADOME IAW AMM 53-12-01.

Part: BLOWER — FAULTY (DETECTOR) · airframe 53,506 hrs · 37,480 cycles

AFT DETECTOR FAN EICAS STATUS MSG ON MX MSG PAGE. R & R M718 AFT DETECTOR FAN BLOWER ASSEMBLY IAW AMM 26-16-02. OPERATIONS CHECKED NORMAL.

Part: EXCITER — INOPERATIVE (APU) · airframe 53,393 hrs · 37,451 cycles

APU INOPERATIVE, NO IGNITION. R & R APU IGN MODULE & EXCITER IAW AMM 49-41-03, APU OPERATIONS CHECKED NORMAL.

Part: BATTERY — DISCHARGED (MAIN) · airframe 53,367 hrs · 37,439 cycles

UPON ARRIVAL TO ACFT FOUND SHIPS BATTERY TO BE DISCHARGED. R & R SHIPS BATTERY AMM 24-31-01. BATTERY OPERATIONS CHECKED NORMAL.

Part: STARTER — INOPERATIVE (APU) · airframe 53,332 hrs · 37,420 cycles

APU WOULD NOT START ON THE GROUND. R & R APU STARTER IAW AMM 49-41-01/401, OPERATIONS CHECKED NORMAL.

Part: PROBE — FAULTY (PITOT HEAT) · airframe 53,292 hrs · 37,407 cycles

FIRST OFFICER`S PITOT EICAS MESSAGE. REPLACED RT PITOT PROBE IAW AMM 34-11-01. OPERATIONS CHECKED GOOD. ALSO REPLACED CURRENT SENSING RELAY IAW FIM 30-31-00 WDM 30-31-21, OPERATIONS CHECKED NORMAL.

Part: PRESSURE SWITCH — FAULTY (SMOKE DETECTOR) · airframe 53,292 hrs · 37,407 cycles

MAINTENANCE STATUS MESSAGE, AFT DETECTOR FAN. R & R S455 SMOKE DETECTOR PRESS SWITCH, OPERATIONS CHECKED NORMAL IAW AMM 26-16-03.

Part: LAMP — INOPERATIVE (SMOKE DETECTOR) · airframe 53,292 hrs · 37,407 cycles

FORWARD CARGO DET 2 EICAS MESSAGE PRESENT. RELAMPED FWD CARGO DET 2 IAW AMM 26-16-01, OPERATIONS CHECKED OK.

Part: LIGHT — LOOSE (CABIN) · airframe 53,283 hrs · 37,403 cycles

FOUND EMERGENCY FLOOR LIGHTING STRIP & EXIT IDENTIFIER LOOSE. REATTACHED EXIT IDENTIFIER & COVER STRIP IAW AMM 33-50-00.

Part: FAN — MALFUNCTIONED (E&E BAY) · airframe 53,247 hrs · 37,391 cycles

AFT EQUIPMENT EXHAUST FAN 1 STATUS MESSAGE. TRANSFER TO MEL 21-58, MDDR 45120 CLEARED 22DEC13 LG PG 585140 M4. R & R EXHAUST FAN ASSEMBLY IAW AMM 21-58-06.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 53,243 hrs · 37,390 cycles

L1 & L2 DOOR, EXTERIOR EMERGENCY LIGHTS ARE INOPERATIVE. RELAMPED L1 & L2 EXTERIOR EMERGENCY LIGHTS, OPERATIONS CHECKED NORMAL IAW AMM 33-51-00.

Part: THRUST REVERSER — MALFUNCTIONED (RT ENGINE) · airframe 53,236 hrs · 37,386 cycles

RIGHT REVERSER DID NOT DEPLOY ON ROLLOUT KBNA. RAN REVERSERS IAW AMM 78-31-00, BOTH REVERSERS OPERATION CHECKED NORMAL. PERFORMED VISUAL INSPECTION OF BOTH REVERSERS, NO FAULTS NOTED.

Part: CONTROLLER — MALFUNCTIONED (AC BAY) · airframe 53,236 hrs · 37,386 cycles

AFTER ENG START EICAS MESSAGE L PACK TEMP RECEIVED, RAN CHECKLIST AS REQUIRED. PERFORMED BITE ON LT PACK CONTROLLER, FAULTED RAM EXHAUST ACTUATOR, RESET LT PACK CONTROLLER & PERFORMED TEST ON LT PACK EXHAUST ACTUATOR IAW AMM 21-53-02, OPERATION IS NORMAL. AFTER TEST, PERFORMED ANOTHER BITE OF LT PACK CONTROLLER, NO FAULTS PRESENT.

Part: FILTER — DIRTY (APU) · airframe 53,232 hrs · 37,384 cycles

APU DPI INDICATOR POPPED, FILTER CHANGE REQUIRED. DPI HAS BEEN RESET, DISCOVERED ON CARD A-49-032-01. R & R FILTER & LEAK CHECKED IAW B767 AMM 49-31-04 NO LEAKS FOUND.

Part: BLADE — DAMAGED (RT ENGINE FAN) · airframe 53,150 hrs · 37,360 cycles

DURING WALK AROUND FOUND DAMAGED TO NR 18 FAN BLADE RT ENGINE .6250" FROM BLADE TIP .5 WIDE AND .210 DEEP ON BLADE L/E. ACCOMPLISHED FAN BLADE BLEND OUT REPAIR IAW AMM 72-31-02, ACCOMPLISHED VISUAL INSPECTION OF ENG IAW 05-51-42 AMM.

Part: SWITCH — UNKNOWN · airframe 53,114 hrs · 37,350 cycles

REPLACE APU OIL LEVEL SWITCH IAW ACTION PLAN 767-AP-7695. R & R APU OIL LEVEL SWITCH, IAW AMM; TASK 49-94-03-002-001, AND TASK 49-94-03-402-007.

Part: APU — MALFUNCTIONED · airframe 53,104 hrs · 37,341 cycles

APU COLD SOAK START AT FL-400, SAT -59, UNSUCCESSFUL AFTER 2 ATTEMPS. RERACKED APU ECU, OPS TEST NORMAL. IAW AMM 49-11-00.

Part: BOTTLE — LOW PRESSURE (CABIN) · airframe 53,052 hrs · 37,324 cycles

PORTABLE OXYGEN BOTTLE AT 1000 PSI AT MID CABIN LT SIDE MIDDLE BOTTLE. R & R OXYGEN BOTTLE IAW AMM 35-31-01.

Part: WIRE — BROKEN (BLEED VALVE) · airframe 53,047 hrs · 37,321 cycles

RIGHT ENGINE BLEED VALVE EICAS MESSAGE AT 80 KNOTS AND 90 PERCENT N2. FOUND BROKEN WIRE AT TERMINAL END ON HIGH STAGE VALVE, REPAIRED IAW SWPM 20-30-11, RUN ENGINE AT IDLE FOR 5 MINUTES IAW AMM 71-31-00, PRESSURE NORMAL.

Part: LINE — LOOSE (BLEED SYS) · airframe 53,045 hrs · 37,319 cycles

RT ENGINE BLEED VALVE EICAS MESSAGE, TIGHTENED SENSE LINES ON HPC, PERFORMED AIR SUPPLY BITE IAW AMM 36-25-00, OPS OK. PERFORMED ENG RUN IAW AMM 71-00-00-00, ALL INDICATIONS NORMAL.

Part: WARNING MESSAGE — ILLUMINATED · airframe 53,002 hrs · 37,310 cycles

GROUND PROX STATUS MESSAGE. PERFORMED WIRING CHANGE IAW EO 6734A032 EGPWS SYST BITE AND GROUND CHECK GOOD, DMI 41175 CLEARED.

Part: SEAL — BROKEN (PBE) · airframe 52,976 hrs · 37,302 cycles

RT FORWARD PBE BROKEN SAFETY SEAL. R & R RT FORWARD PBE IAW AMM 25-05-03.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 52,976 hrs · 37,302 cycles

DURING C-CHECK, DISCOVERED L1 DOOR EXTERNAL EMERGENCY LIGHT WAS NOT OPERATING. LIGHT ASSY WAS REPLACED WITH A SUCCESSFUL FUNCTIONAL CHECK.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 52,976 hrs · 37,302 cycles

DURING C-CHECK, LEFT EXTERNAL LIGHT SYS AT BS 1197 WAS BEING TESTED AND FAILED TO ILLUMINATE. R & R WITH SERVICEABLE LIGHT ASSY.

Part: BATTERY — FAILED (ESCAPE SLIDE) · airframe 52,876 hrs · 37,250 cycles

SQUIB TEST FOR RT WING ESCAPE SLIDE DID NOT TEST, ALSO SQUIB DID NOT TEST ON LT WING SPOILER OVERRIDE ACTUATOR.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 54,474 hrs · 37,097 cycles

LEFT OVERWING EMERGENCY EXIT HATCH EXIT SIGN INOP. REMOVED AND REPLACED M737 BATTERY PACK PER 767 AMM 31-51-07. OPERATIONAL CHECK NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 52,359 hrs · 37,052 cycles

EMERGENCY LIGHTS IN AFT CABIN, RT SIDE WILL NOT ILLUMINATE.

Part: IDG — DISCONNECTED (LT ENGINE) · airframe 52,111 hrs · 36,952 cycles

DURING CLIMBOUT AT FL 270 CAPTAINS EADI, FMC CDU MOMENTARILY BLANKED OUT. FMC MESSAGE ILLUMINATED ON EICAS WITH CORRESPONDING DISCRETE FMC LIGHT. CABIN PRESSURIZATION INDICATOR ALSO SPIKED.

Part: PROXIMITY SENSOR — OUT OF TOLERANCE (RT OWING SLIDE) · airframe 52,081 hrs · 36,939 cycles

AT THE BEGINNING OF TAKEOFF ROLL THE EICAS MESSAGE "RT-WING SLIDE" ILLUMINATED. TAKEOFF WAS ABORTED AT 40 KNOTS, MESSAGE EXTINGUISHED.

Part: BATTERY PACK — DISCHARGED (EVAC SLIDE) · airframe 51,883 hrs · 36,859 cycles

RIGHT OVERWING ESCAPE SLIDE SQUIB DOES NOT TEST ON P-61 PANEL. REMOVED AND REPLACED RIGHT OVERWING M962 BATT PACK ASSY. FUNCTIONAL CHECK WAS NORMAL.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS)

DURING PREFLIGHT MX CHECK RT EMERGENCY ESCAPE SLIDE SQUIB TEST WAS INOPERATIVE. R&R ESCAPE SLIDE BATTERY PACK IAW AMM 25-65-17. FUNCTIONAL CHECK WAS NORMAL

Part: BATTERY PACK — DISCHARGED (ESCAPE HATCH)

DURING PREFLIGHT RT OVERWING ESCAPE HATCH SQUIB TEST LIGHT DIM. REMOVED AND REPLACED RT OVERWING ESCAPE HATCH EMERGENCY LIGHT BATTERY PACK. OPS CHECK WAS NORMAL IAW AMM 25-65-00. (S)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

DURING PREFLIGHT, RT OVERWING ESCAPE HATCH SQUID TEST LIGHT DIM. REMOVED AND REPLACED RT OVERWING ESCAPE HATCH EMERGENCY LIGHT BATTERY PACK. OPS CHECK WAS NORMAL IAW AMM. (K)

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT)

DURING 30 DAY CHECK; NOTED R2 DOOR EMERGENCY LIGHT IS INOPERATIVE. RELAMPED IAW MM 33-51-00. OPS CHECK GOOD. (K)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

RT EMERGENCY ESCAPE SPOILER SQUIB DOES NOT TEST PROPERLY. REPLACED RT EMERGENCY ESCAPE SPOILER SQUIB BATTERY ASSY. OPS CHECK GOOD IAW AMM 25-65-17. (K)