N645GT

Part: OXYGEN BOTTLE — LOW PRESSURE (ZONE 200) · airframe 109,186 hrs · 21,252 cycles

OXYGEN BOTTLE NOT FULL. R & R 1 AFT PORTABLE O2 BOTTLE IAW AMM 35-31-01/401 & IPC 35-31-01-50. OPS & LEAK CHKD GOOD.

Part: SWITCH — FAULTED · airframe 109,153 hrs · 21,245 cycles

RUDDER TRIM SWITCH WOULD NOT MOVE TRIM IN FLIGHT(<P>PERFORMED OPERATIONAL TEST OF RUDDER TRIM SYSTEM, ALL CHECKS OK &AMP; SWITCH OPERATION CHECKED GOOD PER AMM 27-21-00. NO FAULTS NOTED. RAN TEST OF SWITCH NUMEROUS TIMES. ALL CHECK OK PER FIM 27-21</P>)

Part: BATTERY — INOPERATIVE (ZONE 200) · airframe 109,143 hrs · 21,244 cycles

EMERGENCY LIGHT BATTERY INOP ON ROW 23KH(<P>R/R ROW 23KH EMERGENCY LIGHT BATTERY IAW AMM 33-51-07 &AMP; IPC 33-51-07-04. OPS CHK OK.</P>)

Part: ATTACH FITTING — MISSING (ZONE 800) · airframe 109,097 hrs · 21,229 cycles

AIRCRAFT EXTERIOR: DURING ACCOMPLISHMENT OF TASK CARD A-53-406-00-00. FOUND LEFT HAND OVER WING EMERGENCY EXIT HINGED DROP-DOWN STEP WITH OUTER STEP SUPPORT CABLES UNATTACHED FROM DOOR DUE TO MISSING ATTACH FITTINGS FROM STEP. MISSING UPON AIRCRAFT ARRIVAL. LT OVERWING EMERGENCY WINDOW EXIT STEP PANEL NEW FITTING P/N 145T6088-1 INSTALLED AND SECURED IAW B767 AMM 52-21-01-402-202 &AMP; AMM 20-10-23-964-001. PART EFFECTIVITY VERIFY WITH B767 AIPC 52-21-01-02 ITEM 20. NO FURTHER DEFECTS NOTED.

Part: WIRE — DAMAGED (ZONE 200) · airframe 109,079 hrs · 21,229 cycles

LH OVERWING EMERGENCY WINDOW EXIT WIRES TO PLUG WERE FOUND DAMAGED WHEN WINDOW WAS REMOVED FOR INSPECTION.(<P>VISUALLY INSPECTED WIRES ON LH OVERWING EMERGENCY WINDOW EXIT, FOUND THE OUTER JACKET OF INSULATION OF TWO WIRES HAVE DAMAGED. REPAIRED INSULATION OF TWO WIRES IAW B767 SWPM 20-10-13 PAR. C. NO FURTHER DEFECTS NOTED AT THIS TIME.</P>)

Part: LIGHT — NO DISCREPANCY (ZONE 200) · airframe 108,986 hrs · 21,206 cycles

EXTERIOR EMERGENCY LIGHTS INOP. LEFT SIDE L4 DOOR AND OVER THE WING(<P>PERFORMED EMERGENCY LIGHT TEST IAW B767 AMM 33-51-06-862. OPS CHECK GOOD</P>)

Part: BULB — INOPERATIVE (ZONE 200) · airframe 108,911 hrs · 21,189 cycles

R4 EXTERIOR EMERGENCY LIGHT BULB INOPERATIVE. REPLACED THE LIGHT BULB IAW AMM 33-51-06. OPS CHK OK</P>)

Part: BULB — BURNED OUT (ZONE 200) · airframe 108,911 hrs · 21,189 cycles

R4 EMERGENCY LIGHT BULB BURNT(<P>R/R SLIDE EMERGENCY ESCAPE LIGHT PER AMM 33-51-016-902-082. OPS CHK GOOD. NO DEFECTS NOTED AT THIS TIME.</P>)

Part: OXYGEN BOTTLE — DETACHED (ZONE 200) · airframe 108,836 hrs · 21,174 cycles

CREW WALK AROUND, O2 BOTTLE BROKE OFF THE WALL. REATTACHED O2 BOTTLE BRACKET IAW AMM 20-30-01. NO FURTHER DEFECTS NOTED.

Part: LAMP — INOPERATIVE (ZONE 200) · airframe 108,825 hrs · 21,171 cycles

COCKPIT EMERGENCY EXIT LIGHTS OUT. REPLACED THE LAMP IAW AMM 33-51-01. OPS CHECK GOOD.

Part: ELEC CONNECTOR — DAMAGED (TE FLAPS) · airframe 108,738 hrs · 21,151 cycles

CONFIG WARNING AND FLAPS AFTER CLEAN UP. NOSE GEAR EXTENSION EXPERIENCED A LOUD BANG. SPD LIM MESSAGE NEXT TO 250 KNOTS ON SPEED TAPE WITH FLAPS UP. RESEATED PUSHED BACK ELEC CONNECTOR D1756 PIN 2 IAW SWPM 20-61-00, NO FURTHER DEFECTS NOTED.

Part: HOOK AND LOOP — WORN (EVAS) · airframe 108,691 hrs · 21,143 cycles

EVAS HOOK AND LOOP STRIP SEEMS WORN. R & R CAPT & FO GLARESHIELD HOOK AND LOOP IAW EO 6725A287. NO FURTHER DEFECTS NOTED.

Part: BATTERY — INOPERATIVE (ZONE 800) · airframe 108,548 hrs · 21,113 cycles

SQUIB TEST L SLIDE LIGHT DOES NOT WORK WITH TEST 1.(<P>FOUND SQUIB TEST SWITCH STUCK AND BATTERY VOLTAGE LOW AT POSITION M961 &AMP; 962 PER FIM 25-65 FT 817 &AMP; WDM 25-65-11. R/R SQUIB TEST PANEL IAW AMM 26-21-04 &AMP; R/R BATTERY IAW AMM 25-65-17. OPS CHK GOOD. DMI 232628 CLOSED.

Part: SEAL — BROKEN (PBE) · airframe 108,268 hrs · 21,049 cycles

AFT GALLEY PBE SEAL BROKEN. MEL 35-20-01-01 CAT C. R/R PBE SEAL &AMP; BRACKET IAW AMM 25-64-00 &AMP; IPC 25-64-06-01. OPS CHK GOOD. NO FURTHER DEFECTS NOTED.

Part: HANDLE — BROKEN (R1 DOOR ASSIST) · airframe 107,913 hrs · 20,959 cycles

R1 ENTRY DOOR ASSIST HANDLE BROKEN.(<P>R/R R1 ENTRY ASSIST HANDLE PER AMM 52-11-02 &AMP; AMM 20-11-00. OPS CHK OK.</P>)

Part: LAMP — INOPERATIVE (ZONE 200) · airframe 107,912 hrs · 20,958 cycles

EXIT ROW LIGHTS INOP.(<P>.R/R LAMP AT ROW 19KH IAW AMM 33-20-01. OPS CHK GOOD</P>)

Part: POWER SUPPLY — INOPERATIVE (ZONE 200) · airframe 107,692 hrs · 20,904 cycles

RIGHT SIDE AFT EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERY AT 38H. B EMER LIGHT LIGHT INOP AT R L2 DOOR(<P>R/R PWR SUPPLY IAW AMM 33-51-07. OPS CHKS NORMAL. OK FOR SERVICE. R/R BATTERY AT POS 38H IAW AMM 33-17-07. R/R BATTERY AT 38A IAW 33-31-07. OPS CKS NORMAL</P>)

Part: BRACKET — BROKEN (ZONE 200) · airframe 107,690 hrs · 20,903 cycles

MID CABIN PBE BRACKET MOUNT BROKEN(<P>INSTALLED BRACKET IAW AMM 35-31-02-401. OK FOR SERVICE. THIS ACTION CLEARS MDDR 220822.</P>)

Part: SEAL — DAMAGED (RT TE FLAP) · airframe 107,690 hrs · 20,903 cycles

RH OUTBOARD FLAP WITH SEAL DAMAGED AT INBOARD SIDE(<P>REMOVED DAMAGED SEAL AT INBOARD SIDE BY R/H OUTBOARD FLAP AREA, LOCATED, CLEANED, PREPARED, TRIMMED, SECURED AND INSTALLED NEW SEAL AS REQUIRED, AT R/H OUTBOARD FLAP AREA, BY INBOARD SIDE, PER BOEING 767-300 AMM 20-10-23-964-001. NO FURTHER DEFECTS NOTED</P>)

Part: SEAL — DAMAGED (RT AILERON) · airframe 107,690 hrs · 20,903 cycles

RH INBOARD AILERON WITH SEAL DAMAGED(<P>REMOVED DAMAGED SEAL AT RH INBOARD AILERON, LOCATED, CLEANED, PREPARED, SECURED, TRIMMED, INSTALLED NEW SEAL AS REQUIRED AT RH INBOARD, AILERON AREA, PER BOEING 767-300 AMM 20-10-23-964-001. NO FURTHER DEFECTS NOTED</P>)

Part: FAIRING — DAMAGED (NR 1 NACELLE) · airframe 107,690 hrs · 20,903 cycles

ENG #1 AFT FAIRING WITH SERVERAL SCREW MISSING(<P>LOCATED, CLEANED, PREPARED, SECURED AND INSTALLED MISSING FASTENER AT ENG #1, AFT FAIRING PER BOEING 767-300 SRM 51-40-02-0H-0. NO FURTHER DEFECTS NOTED</P>)

Part: SEAL — DAMAGED (LT AILERON) · airframe 107,690 hrs · 20,903 cycles

LEFT INBOARD AILERON WITH SEAL DAMAGED(<P>REMOVED DAMAGED SEAL AT L/H INBOARD AILERON AREA, LOCATED, CLEANED, PREPARED, SECURED, TRIMMED, INSTALLED NEW SEAL AS REQUIRED AT L/H INBOARD AILERON, PER BOEING 767-300 AMM 20-10-23-964-001. NO FURTHER DEFECTS NOTED.</P>)

Part: MESH — DAMAGED (THRUST REVERSER) · airframe 107,690 hrs · 20,903 cycles

ENGINE #1 O/B T/R, WIRE MESH DAMAGED(<P>TRIMMED, CLEANED, PREPARED, SEALED, BONDED AND REPAIRED WIRE MESH AREA AT ENG #1, O/B T/R AS REQUIRED, PER BOEING 767-300 AMM 78-31-00-308-074-H00. NO FURTHER DEFECTS NOTED</P>)

Part: FAIRING — DAMAGED (NR 2 NACELLE) · airframe 107,690 hrs · 20,903 cycles

ENG #2 AFT FAIRING WITH SEVERAL SCREWS MISSING(<P>LOCATED, CLEANED, PREPARED, SECURED AND INSTALLED MISSING HARDWARE AT #2 ENG, AFT FAIRING, PER BOEING 767-300 SRM 51-40-02-0G-0. NO FURTHER DEFECTS NOTED</P>)

Part: SEAL — DETERIORATED (ZONE 200) · airframe 107,690 hrs · 20,903 cycles

WINDOW 1RH WEATHER SEAL DETERIORATED(<P>REMOVED DETERIORATED, SEALANT AT WINDOW 1RH, WEATHER SEALANT, LOCATED, CLEANED, PREPARED, APPLIED, MASKED AND RESTORE WEATHER AERODYNAMIC SEALANT REPAIR AT 1RH WINDOW, PER BOEING 767-300 AMM 56-11-00-398-026. NO FURTHER DEFECTS NOTED</P>)

Part: BRUSH BLOCK — WORN (APU STARTER) · airframe 107,690 hrs · 20,903 cycles

APU STARTER MOTOR BRUSH WEAR INDICATOR WORNOUT(<P>ACCOMPLISHED R/R OF APU STARTER MOTOR IN REFERENCE TO B767 AMM :49-41-01. OPS TEST NORMAL. NO LEAKS NOTED</P>)

Part: SEAL — DAMAGED (R2 WINDOW) · airframe 107,690 hrs · 20,903 cycles

RH WINDOW #2 PRESSURE BULB SEAL DAMAGED AT REAR CORNER(<P>REPAIRED DAMAGED AREA AT RH WINDOW #2 PRESSURE BULB SEAL, REAR CORNER AREA, APPLIED SEALANT, CLEANED, PREPARED, MASKED AS REQUIRED PER BOEING 767-300 AMM 56-11-00-368-059. NO FURTHER DEFECTS NOTED.</P>)

Part: SEAL — DAMAGED (ELT) · airframe 107,690 hrs · 20,903 cycles

LH AFT CLOSET PORTABLE ELT AUTO RELEASE SEAL DAMAGED P/N 1151324-1M366 S/N 1151324-08345(<P>REMOVED AND REPLACED PORTABLE ELT IAW B767-300 AMM 25-63-03. OPS CHK OK</P>)

Part: SEAL — DETERIORATED (ZONE 200) · airframe 107,690 hrs · 20,903 cycles

WINDOW 1 LH, WEATHER SEAL DETERIORATED(<P>REMOVED DETERIORATED WEATHER SEALANT AT WINDOW 1LF, LOCATED, CLEANED, PREPARED, MASKED AND APPLIED SEALANT, RESTORED WEATHER AERODYNAMIC SEALANT REPAIR AS REQUIRED AT 1LF WINDOW AREA, PER BOEING 767-300 AMM 56-11-00-398-026. NO FURTHER DEFECTS NOTED</P>)

Part: BATTERY — LEAKING (MEGAPHONE) · airframe 107,690 hrs · 20,903 cycles

FWD LH OVHD BIN MEGAPHONE BATTERIES LEAKING(<P>REMOVED &AMP; REPLACED FWD LH MEGAPHONE AS REQUIRED PER 767 AMM 25-63-02, OPS CHK OK</P>)

Part: PBE — MISSING (ZONE 200) · airframe 107,690 hrs · 20,903 cycles

MID CABIN PBE MISSING FROM A/C(<P>INSTALLED MID CABIN PBE AS REQUIRED PER 767 AMM 35-31-02 &AMP; OPS CHECK OK</P>)

Part: SEAL — DAMAGED (RT TE FLAP) · airframe 107,690 hrs · 20,903 cycles

RH INBOARD MID FLAP , MID FLAP WITH SEAL DAMAGED AT INBOARD SIDE(<P>REMOVED DAMAGED AREA AT SEAL LOCATION BY RH INB. MID FLAP, INBOARD SIDE, CLEANED, PREPARED, APPLIED SEALANT AND INSTALLED RE-INFORCEMENT FABRIC AS REQUIRED PER BOEING 767-300 AMM 52-09-00-358-056. NO FURTHER DEFECTS NOTED</P>)

Part: SEAL — DAMAGED (LT TE FLAP) · airframe 107,690 hrs · 20,903 cycles

LEFT O/B FLAP WITH SEAL DAMAGED AT INBOARD SIDE(<P>REMOVED DAMAGED SEAL AT L/H O/B FLAP, BY I/B SIDE AREA, LOCATED, CLEANED, PREPARED, SECURED, TRIMMED, SECURED AND INSTALLED NEW SEAL, AS REQUIRED, AT L/H O/B FLAP, BY I/B SIDE AREA, PER BOEING 767-300 AMM 20-10-23-964-001. NO FURTHER DEFECTS NOTED</P>)

Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 107,592 hrs · 20,884 cycles

2 INTERIOR EMERGENCY LIGHTS INOP AT R4 DOOR.(<P>R/R EMERGENCY BATTERY PACK AT ROW 38KH IAW B767 AMM 33-51-07 &AMP; AIPC 33-51-07, OPS CHECK GOOD.</P>)

Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 106,966 hrs · 20,743 cycles

R4 DOOR AT FLT ATTENDANT BULK HEAD EMERGENCY LIGHTS INOP(<P>R/R EMERGENCY BATTERY PACK AT ROW 38 IAW AMM 33-51-07 &AMP; IPC 33-51-07. OPS CHECK GOOD</P>)

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 106,961 hrs · 20,742 cycles

PASSENGER CABIN, FLOOR STRUCTURE, BTW STA 1197+22 TO STA 1197+44 AT RBL 40, INTERCOSTAL WITH CRACK AT UPPER CHORD(<P>PASSENGER CABIN, FLOOR STRUCTURE, BTW STA 1197+22 TO STA 1197+44 AT RBL 40, INTERCOSTAL WAS REPLACED IAW SRM 51-10-02-0G-0 PAR 9 REV 125 15/APR/2024. NO FURTHER DEFECTS NOTED</P>)

Part: SKIN — DEBONDED (LT NR 3 SLAT) · airframe 106,961 hrs · 20,742 cycles

LH WING SLAT #3 SURFACE OUTER SIDE AREA UPPER SKIN WITH ONE DISBOND.(<P>LH WING SLAT #3 T/E WEDGE UPPER SKIN WAS REPAIRED IAW SRM 57-43-02-2R-1 FIG 201 SHEET 2 NOTE D PAG 1-3 AND SRM 51-70-10-2R-4 REPAIR 4 FIG 202 SHEET 1 PAG 8,16 REV 125 APR 15/2024. NO FURTHER DEFECTS NOTED</P>)

Part: CONDUIT — MISSING (RT MLG WW) · airframe 106,961 hrs · 20,742 cycles

RH MAIN LANDING GEAR WHEEL WELL, UP LOCK DOOR SENSOR S-264, WIRE COVER PROTECTION, MISSING(<P>RH MAIN LANDING GEAR WHEEL WELL, UP LOCK DOOR SENSOR S-264, WIRE COVER PROTECTION, MISSING FLEXIBLE ELECTRICAL CONDUIT S264 WAS REPLACED IAW SWPM 20-10-91 REV 86 DATE 15/JUN/24 OPERATIONAL TEST OF S264 WAS PERFORMED SATISFACTORY IAW AMM 32-61-02-702-018 REV 142 DATE 22/APR/24</P>)

Part: SKIN — DENTED (LT TE FLAP) · airframe 106,961 hrs · 20,742 cycles

TRAILING EDGE, INBOARD FLAP LH, WITH DENTS.(<P>TRAILING EDGE, INBOARD FLAP, MAIN FLAP WAS REPAIRED IAW SRM 57-53-01-2R-1 FIG. 201. SHEET 5. PAG 1-6 AND 51-70-17-0G-0 PAR. 4H. FIG 19. PAG 16,17 AND 47. REV 125. 15APR2024. NO FURTHER DEFECTS NOTED</P>)

Part: LINE — LEAKING (HYD SYSTEM) · airframe 106,961 hrs · 20,742 cycles

LEFT MLG TRUNNION BACKUP STRUCTURE, WITH EVIDENCE OF THE LEAK HYDRAULIC.(<P>LEFT MLG TRUNNION BACKUP STRUCTURE LINE WAS INSTALLED CORRECTLY IAW AMM 32-11-01-404-056, REV 142, APR 22, 2024; TORQUE APPLIED 270 IN-LB, S/N 0422127314, DATE 29-AUG-2024. CHECK FOR LEAKS WAS PERFORMED, NO LEAKS FOUND. NO FURTHER DEFECTS NOTED</P>)

Part: FUEL LINE — BENT (FUEL CELL) · airframe 106,961 hrs · 20,742 cycles

LH WING, INSIDE FUEL TANK, BTW WBL 97.95 AND RIB NO.1, BTW STRINGER L-5 AND L-6, "AUX TANK SCAVENGE" FUEL LINE BENT.(<P>LH WING, INSIDE FUEL TANK, BTW WBL 97.95 AND RIB NO.1, BTW STRINGER L-5 AND L-6, "AUX TANK SCAVENGE" FUEL LINE WAS REPLACED I.A.W AMM 28-22-07-404-008 REV.142 DATE: 22 APR 24. NO FURTHER DEFECTS NOTED</P>)

Part: HYDRAULIC LINE — LEAKING (LT MLG BRAKE) · airframe 106,961 hrs · 20,742 cycles

LH MAIN LANDING GEAR BRAKE ASSY #2 PRESSURE PIPE WITH LEAK. (DUE TO WEAR)(<P>LH MAIN LANDING GEAR BRAKE ASSY #2 PRESSURE LINE WAS REPLACED IAW AMM 32-41-06-404-009-004 REV. 142 DATE: 22 APR 2024, TORQUE S/N: 0224902097, DATE: 21 FEB 2025. APPLIED 400 LB/IN. LEAK TEST WAS PERFORMED I.A.W AMM 32-41-06-404-009-004 REV. 142 DATE: 22 APR 2024. STEP "K", NO LEAK FOUND. NO FURTHER DEFECTS NOTED</P>)

Part: SKIN — DENTED (LT SPOILER) · airframe 106,961 hrs · 20,742 cycles

LH WING, UPPER SURFACE, SPOILER #6, UPPER RIGHT SURFACE, WITH DENT(<P>LH WING, UPPER SURFACE, SPOILER #6 WAS REPAIRED IAW SRM 57-70-01-2R-1 FIG. 201. PAGE 1-5 AND SRM 51-70-04-0G-0 PAR. 5. L. PAGE. 19 AND SRM 51-70-03-0G PAR. 5 .L. FIG 16. PAGE. 15 AND 41 REV 125 APR/15/2024. NO FURTHER DEFECTS NOTED</P>)

Part: JUMPER — DETERIORATED (LT MLG) · airframe 106,961 hrs · 20,742 cycles

LEFT MAIN LANDING GEAR BODY DOOR, DETERIORATED WIRE JUMPER ON HINGE OF MLG DRAG BRACE DOOR 733.(<P>LEFT MAIN LANDING GEAR BODY DOOR, JUMPER ON HINGE OF MLG DRAG BRACE DOOR 733 WAS REPLACED I.A.W AMM 32-12-08-404-007 REV 142 DATE 22 APR 2024 BONDING TEST I.A.W SWPM 20-20-00 REV 86 15 JUN 2024 BONDING METER S/N 1249 DATE 05/JUN/25 BONDING VALUE: 0.5 MILLIOHMS. NO FURTHER DEFECTS NOTED</P>)

Part: SLEEVE — WORN (NR 2 ENGINE) · airframe 106,961 hrs · 20,742 cycles

ENGINE 2, EXHAUST PANEL, EXHUAST SLEEVE PADS WITH WEAR AT 4 HRS POSITION.(<P>ENGINE 2, EXHAUST PANEL, EXHAUST SLEEVE PADS WITH WEAR AT 4 HRS POSITION WERE REPLACED IAW AMM TASK 20-11-00-910-802 REV 142 DATE 22 APR 24, 45INLB WERE APPLIED S/N 1222912598 DUE DATE 07</P> / <P>MAR 25. NO FURTHER DEFECTS NOTED</P>)

Part: SEAL — MISSING (THRUST REVERSER) · airframe 106,961 hrs · 20,742 cycles

LEFT ENGINE, LEFT T/R REVERSER, UPPER FIRE SEAL SECCION MISSING (TRAILING EDGE)(<P>LEFT ENGINE, LEFT T/R REVERSER, UPPER FIRE SEAL WAS REPLACED IAW SRM 51-10-02-0G-0 PAR 9 REV 125 15/APR/2024. NO FURTHER DEFECTS NOTED</P>)

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 106,961 hrs · 20,742 cycles

FORWARD CARGO COMPARTMENT, AT STGR 32R AND BTW STA 434 AND STA 456, STRINGER STRUCTURE WITH EVIDENCE OF CORROSION.(<P>FORWARD CARGO COMPARTMENT, AT STGR 32R AND BTW STA 434 AND STA 456, STRINGER WAS REPLACED IAW SRM 51-10-02-0G-0 PAR 9 REV 125 15/APR/2024. NO FURTHER DEFECTS NOTED</P>)

Part: KEELBEAM — CORRODED (ZONE 100) · airframe 106,961 hrs · 20,742 cycles

MIDDLE LWR FUSELAGE KEEL BEAM AFT SECTION BTW B STA 999 AND B STA 1009 AND STGR 39-L AND STGR 39-R AROUND FASTENERS WITH CORROSION.(<P>MIDDLE LWR FUSELAGE KEEL BEAM AFT SECTION BTW B STA 999 AND B STA 1009 AND STGR 39-L AND STGR 39-R AROUND FASTENERS DAMAGE WAS REPAIRED IAW TRE6753702 ISSUED DATE 09/JUL/24 / FAA FORM 8100-9 DATE 17/JUL/24 &AMP; BAC CMA TLS 24-0177. NO FURTHER DEFECTS NOTED</P>)

Part: SKIN — CRACKED (ZONE 600) · airframe 106,961 hrs · 20,742 cycles

RH WING LOWER SKIN STG L-9.5 BTW RIB 30-30 WITH CRACK(<P>RH WING LOWER SKIN STG L-9.5 BTW RIB 30-30 CRACK WAS REPAIRED IAW TRE 6757262 R1 ISSUED DATE 11/JUL/2024, SB AP767-57-016 REV 17/JUL/2019. NO FURTHER DEFECTS NOTED</P>)

Part: SKIN — CRACKED (ZONE 600) · airframe 106,961 hrs · 20,742 cycles

RH WING LOWER SKIN STG L-6.5 BTW RIB 31-32 WITH CRACK(<P>RH WING LOWER SKIN STG L-6.5 BTW RIB 31-32 CRACK WAS REPAIRED IAW TRE6757261 ISSUED DATE 04/JUL/24 , EO NO: 6757A140 DATE 31/AUG/21, FAA FORM 8100-9 DATE 10/AUG/2024 &AMP; BAC MSG CMA TLS 24-0174. NO FURTHER DEFECTS NOTED</P>)

Part: VALVE — NO TEST (NR 2 ENGINE) · airframe 106,961 hrs · 20,742 cycles

ENGINE 2 DURING HEALT CHECK PRV ACTUATOR LEAKAGE (THUM) TEST, OUT OF LIMITS.(<P>ENGINE 2 PRV WAS REPLACED IAW AMM TASK 36-11-18-404-018-001 REV 142 DATE 22 APR 24, 120 INLB &AMP; 270 INLB S/N 406744400 DUE DATE 12 MAR 25,</P>)

Part: FUEL LINE — LOOSE (ZONE 100) · airframe 106,961 hrs · 20,742 cycles

AREA UNDER AFT GALLEY, STA 1602, LBL 37, FUEL TUBE WITH LOOSE(<P>AREA UNDER AFT GALLEY, STA 1602, LBL 37, FUEL TUBE WAS INSTALLED CORRECTLY IAW AMM 28-25-05-404-042 &AMP; AMM 20-11-00-910-802 REV 142 DATE 22 APR 24, 25INLB WERE APPLIED S/N 1023906329 DUE DATE 16 NOV 24. NO FURTHER DEFECTS NOTED</P>)

Part: TERMINAL — DETERIORATED (ZONE 400) · airframe 106,961 hrs · 20,742 cycles

ENGINE 1, ACCESS PANEL 415AL, DETERIORATED WIRE PROTECTION OF FEDDER T1 TERMINAL.(<P>A-71-820-00-01/004 ENGINE 1, ACCES PANEL 415AL TERMINAL 1 FEEDER PROTECTION WAS REPLACED WITH SATISFACTORY TEST IAW SWPM 20-30-07 REV 86 DATE 15/JUN/24 AMM 24-11-01-404-002-004. NO FURTHER DEFECTS NOTED</P>)

Part: SHROUD — BENT (ZONE 100) · airframe 106,961 hrs · 20,742 cycles

AFT CARGO COMPARTMENT, APROX LBL 37 BTW STA 1197+44 AND 1197+66, APU FUEL LINE SHROUD, BENT.(<P>AFT CARGO COMPARTMENT, APROX LBL 37 BTW STA 1197+44 AND 1197+66, APU FUEL LINE SHROUD WAS REPLACED IAW AMM 28-25-05-404-169 REV 142 DATE 22 APR 24, 450 INLB WERE APPLIED S/N 0422127314, BONDING TEST OK 0.5 MILLIOHMS S/N 2568 DUE DATE 14 FEB 25, LEAK TEST WAS PERFORMED, NO FOUND LEAKS</P>)

Part: SKIN — CRACKED (ZONE 600) · airframe 106,961 hrs · 20,742 cycles

RH WING, LOWER SKIN INNER SURFACE BETWEEN RIB 28 AND RIB 29 AT STGR L 9.5 WAS FASTENER HOLD WITH CRACK..(<P>RH WING, LOWER SKIN INNER SURFACE BETWEEN RIB 28 AND RIB 29 AT STGR L 9.5 WAS REPAIRED IAW TRE6757263 ISSUED DATE 10 JUL 24 AND APROV WITH CMA-TLS-24-0176-05B AND FAA FORM 8100-9 DATE 09 AUG 24. NO FURTHER DEFECTS NOTED</P>)

Part: DUCT — PUNCTURED (ZONE 400) · airframe 106,961 hrs · 20,742 cycles

ENGINE 1, ACCESS PANEL 432ET, PUNCTURE ON DUCT ON VALVE WING THERMAL ANTI ICE.(<P>ENGINE 1, ACCESS PANEL 432ET, DUCT ON VALVE WING THERMAL ANTI ICE WAS REPLACED IAW AMM 30-11-02-404-012</P> / <P>REV 142 DATE 22 APR 24. NO FURTHER DEFECTS NOTED</P>)

Part: PCA — LEAKING (ZONE 300) · airframe 106,961 hrs · 20,742 cycles

VERTICAL STABILIZER STRUCTURE SURFACE RUDDER AREA CENTER PCA WITH HYDRAULIC LEAK.(<P>VERTICAL STABILIZER STRUCTURE SURFACE RUDDER AREA CENTER PCA WAS REPLACED, TESTED, ADJUSTED AND TEST LEAK WAS PERFORMED I.A.W AMM 27-21-02-422-038 REV.142 DATE: 22/APR/24 NO LEAK WAS FOUND. TORQUE APPLIED 1000 LN/IN, 500 LB/IN AND 270 LB/IN S/N: 422127196 DATE: 29/AUG/24. NO FURTHER DEFECTS NOTED</P>)

Part: PCA — LEAKING (ZONE 300) · airframe 106,961 hrs · 20,742 cycles

VERTICAL STABILIZER STRUCTURE SURFACE RUDDER AREA UPPER PCA WITH HYDRAULIC LEAK.(<P>VERTICAL STABILIZER STRUCTURE SURFACE RUDDER AREA UPPER PCA WAS REPLACED, TESTED, ADJUSTED AND TEST LEAK WAS PERFORMED I.A.W AMM 27-21-02-422-038 REV.142 DATE: 22/APR/24 NO LEAK FOUND. TORQUE</P> / <P>APPLIED 1000 LN/IN, 500 LB/IN AND 270 LB/IN S/N: 422127196 DATE: 29/AUG/24E FOUND. NO FURTHER DEFECTS NOTED</P>)

Part: PCA — LEAKING (ZONE 300) · airframe 106,961 hrs · 20,742 cycles

RH WING, OUTBORD AILERON, INTERIOR PCA, WITH EVIDENCE OF HYD LEAK, AND ACTUATOR SEAL WITH WEAR(<P>RH WING, OUTBOARD AILERON, INTERIOR PCA WAS REPLACED IAW AMM TASK 27-11-49-422-028 REV 142 DATE 22 APR 24, 140INLB &AMP; 135INLB WERE APPLIED S/N 1123126519 DUE DATE 28 NOV 24, 840INLB &AMP; 270INLB WERE APPLIED S/N 0224902047 DUE DATE 21 FEB 25, OPERATIONAL TEST AND LEAK TEST WAS PERFORMED, NO LEAKS WERE FOUND. NO FURTHER DEFECTS NOTED</P>)

Part: WIRE — DETERIORATED (LT MLG WW) · airframe 106,961 hrs · 20,742 cycles

LEFT MAIN LANDING GEAR, TRUNNION DOOR 735, DETERIORATED WIRE JUMPER, IN UPPER HINGE OF TRUNION DOOR.(<P>LEFT MAIN LANDING GEAR, TRUNNION DOOR 735, BONDING JUMPER WAS REPLACED, IN UPPER HINGE OF TRUNION DOOR. I.A.W. SWPM 20-20-10 REV. 86 DATE: JUN 15/2024. BONDING METER S/N: 1539 DATE: 22/JAN/2025. BONDING VALUE: 1.0 MILLIOHMS. NO FURTHER DEFECTS NOTED</P>)

Part: TORQUE LINK — EXCESS PLAY (NLG) · airframe 106,961 hrs · 20,742 cycles

NOSE LANDING GEAR TORQUE LINK, WITH SCREWS OF THE PANEL WITH FREE PLAY EXCESSIVE(<P>NOSE LANDING GEAR TORQUE LINK, SCREWS OF THE PANEL WERE TIGHTENED IAW AMM TASK 20-11-00-910-802 REV 142 DATE 22 APR 24, 150INLB WERE APPLIED S/N 0821902157 DUE DATE 11 DEC 24. NO FURTHER DEFECTS NOTED</P>)

Part: TORQUE LINK — EXCESS PLAY (NLG) · airframe 106,961 hrs · 20,742 cycles

NOSE LANDING GEAR TORQUE LINK, WITH SCREWS OF THE PANEL WITH FREE PLAY EXCESSIVE(<P>NOSE LANDING GEAR TORQUE LINK, SCREWS OF THE PANEL WERE INSTALLED CORRECTLY IAW AMM TASK 20-11-00-910-802 REV 142 DATE 22 APR 24, TORQUE, 58 IN/LB WERE APPLIED S/N: 0522902549 DUE DATE 16 SEP 24. NO FURTHER DEFECTS NOTED</P>)

Part: FIREWALL — WORN (APU BAY) · airframe 106,961 hrs · 20,742 cycles

APU COMPARTMENT AREA LOWER FRONT FIRE WALL BRACKET LOCK AND FIRE WALL WITH WORN.(<P>APU COMPARTMENT AREA LOWER FRONT BRACKET WAS INSPECTED AND ONLY DAMAGE ON FIRE WALL. FIRE WALL WAS REPLACED IAW SRM 51-10-02-0G-0 PAR 9 SRM 51-10-08-02-0G-0 REV 125 15/APR/2024. NO FURTHER DEFECTS NOTED</P>)

Part: JUMPER — DETERIORATED (NR 1 NACELLE) · airframe 106,961 hrs · 20,742 cycles

ENGINE 1, ACCESS PANEL 416AR, DETERIORATED GROUND JUMPER OF HIGH STAGE VALVE.(<P>ENGINE 1, ACCESS PANEL 416AR, JUMPER OF HIGH STAGE VALVE WAS REPLACED I.A.W AMM 70-20-00-702-002-H00 AND AMM 36-11-18-404-018-001 REV. 142 DATE 22 APR 2024 BONDING VALUE 1 MILLIOHM, BONDING TEST OK BONDING METER S/N:1534 DATE: 22/JAN/25. NO FURTHER DEFECTS NOTED</P>)

Part: INSULATION — MISSING (THRUST REVERSER) · airframe 106,961 hrs · 20,742 cycles

ENGINE #2, INSIDE REVERSER, VARIOUS FIRE INSULATION MISSING(<P>ENGINE #2, INSIDE REVERSER, FIRE INSULATION WAS REPAIRED IAW AMM 78-31-00-308-072-H00 REV 125 15/APR/2024. NO FURTHER DEFECTS NOTED</P>)

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 106,961 hrs · 20,742 cycles

PASSENGER CABIN, FLOOR STRUCTURE, BTW STA 1087 TO STA 1109 AT RBL 40, INTERCOSTAL WITH CRACK AT UPPER CHORD.(<P>PASSENGER CABIN, FLOOR STRUCTURE, BTW STA 1087 TO STA 1109 AT RBL 40, INTERCOSTAL WAS REPLACED IAW SRM 51-10-02-0G-0 PAR 9 REV 125 15/APR/2024. NO FURTHER DEFECTS NOTED</P>)

Part: CONDUIT — BROKEN (LT MLG WW) · airframe 106,961 hrs · 20,742 cycles

LEFT MAIN LANDING GEAR DOOR UPLOCK, BROKEN CONDUIT PROTECTION OF WIRE BUNDLES OF SENSORS S260 AND S238.(<P>CONDUIT OF SENSOR S260 AND S238 IN MLG LH WERE REPLACED I A W SWPM 20-10-91 REV 86 DATE15-JUN-24 WITH OPERATIONAL TEST SATISFACTORY I A W AMM 32-61-02-702-018 REV 142 DATE 22-APR-24</P>)

Part: SEAL — DAMAGED (THRUST REVERSER) · airframe 106,961 hrs · 20,742 cycles

LEFT ENGINE, RIGHT T/R REVERSER, UPPER FIRE SEAL DAMAGED (TRAILING EDGE)(<P>LEFT ENGINE, RIGHT T/R REVERSER, UPPER FIRE SEAL WAS REPAIRED AIW AMM 78-31-00-308-072-H00 REV 142 22/APR/2024. NO FURTHER DEFECTS NOTED</P>)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 106,864 hrs · 20,719 cycles

OVERHEAD EMERGENCY LIGHTS INOP AFT CABIN RT SIDE ROW 38-28(<P>R/R AFT RH EMERG LT BATT PACK IAW 767 AMM 33-51-07 &AMP; IPC 33-51-07. OPS CHK OK.</P>)

Part: NONE — NONE (R4 DOOR SLIDE) · airframe 106,854 hrs · 20,717 cycles

R4 DOOR SLIDE PRESSURE READING TOO HIGH(<P>INSPECTED DOOR PRESSURE GAUGE TO BE WITHIN LIMITS IAW AMM 25-66-03. NO DEFECTS NOTED AT THIS TIME</P>)

Part: SLIDE — LOW PRESSURE (R4 DOOR) · airframe 106,835 hrs · 20,716 cycles

R4 DOOR SLIDE PRESSURE READING TOO HIGH(<P>INSPECTED DOOR PRESSURE GAUGE WITHIN LIMITS IAW AMM 25-66-02. NO DEFECTS NOTED AT THIS TIME.</P>)

Part: CONNECTOR — UNSECURE (DOOR SLIDE) · airframe 106,734 hrs · 20,694 cycles

GREEN SQUIB TEST LIGHT WILL NOT ILLUMINATE ON TEST FOR RIGHT SIDE EMERGENCY SLIDE(<P>RESECURED CONNECTOR TO EMERGENCY BATTERY PER AMM 25-65-00. TEST IS GOOD, NO FURTHER DEFECTS NOTED.</P>)

Part: DOOR — UNSECURE (C/P ESCAPE ROPE) · airframe 106,466 hrs · 20,640 cycles

FO'S "EMERGENCY ESCAPE ROPE" DOOR PANEL REQUIRES SECURING(<P>FOUND FO'S ESCAPE ROPE LATCH SIEZED PARTLY RETRACTED. LUBED AND FREED LATCH. OPS CHECK GOOD IAW AMM 25-61-02.</P>)

Part: POWER SUPPLY — UNKNOWN (UNKNOWN) · airframe 106,066 hrs · 20,551 cycles

LEFT OVER WING EMERGENCY EXIT LIGHTING INOP.(<P>R/R EMERGENCY PWR SUPPLY M737 PER AMM 33-51-07. OPS NORMAL.</P>)

Part: POWER SUPPLY — UNKNOWN (UNKNOWN) · airframe 106,066 hrs · 20,551 cycles

R1 EMERGENCY EXIT LIGHTING INOP, R2 EMERGENCY EXIT LIGHTING INOP & RIGHT OVERWING EMERGENCY EXIT LIGHTS INOP(<P>LP 1691904 M13: REMOVED AND REPLACED PWR SUPPLY M730 IAW AMM 33-51-07. OPS CHECKS GOOD.</P> / <P>LP 1691904 M14: R/R EMERGENCY POWER SUPPLY M732 IAW B767 AMM 33-51-07. OPS CHECK GOOD. NO FURTHER DEFECTS AT THIS TIME.</P> / <P>LP 1691905 M16: REMOVED &AMP; REPLACED PWR SUPPLY M734 IAW AMM 33-51-07. OPS CHECKS GOOD</P> / <P>LP 1691905 M17: REMOVED AND REPLACED PWR SUPPLY M731 IAW AMM 33-51-07. OPS CHECKS GOOD.</P> / <P>PN'S: 36177, 52545, 15866 &AMP; 17434</P>)

Part: BULB — UNKNOWN (UNKNOWN) · airframe 105,891 hrs · 20,514 cycles

OVERWING EMERGENCY EXIT EXTERNAL LIGHTS INOP(<P>R/R EMER LIGHTS BULB AT R1 DOOR LEFT AFT FUSELAGE PER AMM 33-51-06. OPS CHECK GOOD.</P>)

Part: BATTERY — UNKNOWN (UNKNOWN) · airframe 105,932 hrs · 20,522 cycles

EMERGENCY LIGHT EXIT SIGNS INOP AT R3 AND L3 DOORS(<P>REMOVED AND REPLACED BATTERY PER AMM 33-51-07. OPS CHK GOOD.</P>)

Part: BULB — UNKNOWN (UNKNOWN) · airframe 105,932 hrs · 20,522 cycles

OVERWING EMERGENCY EXIT EXTERNAL LIGHTS INOP AT R1, R3, AND LEFT AFT FUSELAGE SINGLE BULB.(<P>REMOVED AND REPLACED EMERGENCY LIGHT BULBS AT R1, R3, AND LEFT AFT FUSELAGE PER AMM 33-51-06.</P>)

Part: VALVE — UNKNOWN (UNKNOWN) · airframe 105,881 hrs · 20,512 cycles

ETOPS VERIFICATION FLIGHT ACCOMPLISHED. ENG 1 ANTI-ICE DUCT PRESS LOW, SYS OPS ABNORMAL(<P>INSPECTED PNEUMTAIC DUCT ASSY FROM ENGINE TO INLET IAW AMM 36-00-00. NO LEAKS OR DEFECTS PER AMM 54-52-02. REMOVED AND REPLACED PRV IAW AMM 36-11-18. OPS CHECK GOOD, NO FAULTS NOTED. REMOVED AND REPLACED PRV CONTROLLER IAW AMM 36-11-19. OPS CHECK GOOD, NO FAULTS NOTED.</P>)

Part: OXYGEN BOX — UNKNOWN (UNKNOWN) · airframe 105,751 hrs · 20,485 cycles

FLIGHT MECHANICS REPORTED O2 AT 1700 IN HHN AND DOWN TO 1200 IN BWI, CHECK FOR LEAK.(<P>ACCOMPLISHED TROUBLESHOOTING PER AMM TASK 35-11-00-795-106. LEAK CHECKED &AMP; NO LEAKS FOUND. DISCONNECTED CREW O2 MASK. WHEN DISCONNECTED, F/O O2 MASK O2 PRESSURE STABILIZED. LEFT MASK DISCONNECTED FOR TROUBLESHOOTING PURPOSE. O2 PRESSURE AT 1750, O2 PRESSURE DROP DOWN TO 1350. RECONNECTED F/O'S O2 MASK PER AMM 35-11-51. REMOVED O2 STOWAGE BOX PER AMM 35-11-51. UPON CHECKING FOUND LEAK IN 2ND OBSERVER O2 BOX. SECURED LINE &AMP; INSTALLED OBSERVERS O2 BOX PER AMM 35-11-51. LEAK CHECK GOOD AT THIS TIME.&NBSP;</P>)

Part: LAMP — UNKNOWN (UNKNOWN) · airframe 105,509 hrs · 20,431 cycles

EXTERIOR EMERGENCY PATH LIGHT INOP LH SIDE OF FUSELAGE(<P>RELAMPED PER AMM 33-50-06. OPS CHECK GOOD</P>)

Part: CHARGER — UNKNOWN (UNKNOWN) · airframe 104,969 hrs · 20,311 cycles

LEFT FWD EMERGENCY LIGHTING INOP.(<P>REMOVED AND REPLACED LEFT FWD EMERGENCY LIGHTING CHARGING ASSY. OPS CHECK OK IAW 767AMM 33-51-07.</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 104,839 hrs · 20,284 cycles

FLIGHT ATTENDANT REPORTED SMELL OF ELECTRICAL SMOKE AFTER TAKEOFF(<P>PERFORMED SMOKE AND FUMES INSPECTION IAW AMM 767 05-51-56 AND TASK 21-00-21-102-030, NO DAMAGE FOUND. ALL SYSTEM CHECKED OK</P>)

Part: CYLINDER — UNKNOWN (UNKNOWN) · airframe 104,519 hrs · 20,218 cycles

FORWARD CLOSET #119 MOUNTED PORTABLE O2 BOTTLE PRESSURE LOW.(<P>R/R PORTABLE OXYGEN CYLINDER FWD CLOSET IAW AMM 35-31-01. DMI 182537 CLOSED. PLACARD REMOVED</P>)

Part: SMOKE GOGGLES — NONE · airframe 104,381 hrs · 20,185 cycles

CAPT SMOKE GOGGLES SCRATCHED.(<P>R/R CAPT SMOKE GOGGLES PER B767 AMM 25-60-01. NO FURTHER DEFECTS NOTED</P>)

Part: NONE — NONE · airframe 104,328 hrs · 20,174 cycles

1 EMK INCOMPLETE ( EMERGENCY MEDICAL EQUIPMENT, EMERGENCY MEDICAL KIT (EMK) AND/OR ASSOCIATED EQUIPMENT, NOT REQUIRED BY FAR )(<P>REMOVED AND REPLACED EMK IAW AMM 25-60-00</P>)

Part: FUEL TANK — LEAKING (MAIN) · airframe 104,204 hrs · 20,147 cycles

LH WING CENTER SECTION LOWER SURFACE WITH FUEL LEAK EVIDENCE AT / STG L10 AND LBL62.0.(<P>FUEL LEAK EVIDENCE WAS REPAIRED PER AMM 28-11-00-308-013 REQUIREMENTS.</P>)

Part: SKIN PANEL — DELAMINATED · airframe 104,204 hrs · 20,147 cycles

DELAMINATION DAMAGES ON VERTICAL STABILIZER SKIN PANEL BETWEEN FSS 18.037 / FSS 92.5, FSS 245.653 / FS 321.046 AND AUXILIARY /FR (REPAIR WAS ACCOMPLISHED PER BOEING SR# 3-5540076887 AND SRM 55-30-01 REPAIR SRM 51-70-10 REQUIREMENTS.)

Part: SPRING — BENT · airframe 104,204 hrs · 20,147 cycles

MID SERVICE DOOR ESCAPE SYSTEM DEPLOYMENT, GIRT BAR CARRIER WITH / BENT AFT SPRING.(GIRT BAR CARRIER AFT SPRING, WAS REPLACED ON RH MID SERVICE DOOR PER AMM 25-66-03-404-098 REQUIREMENTS.)

Part: SUPPORT BEAM — CRACKED · airframe 104,204 hrs · 20,147 cycles

CRACK EVIDENCE OF FAN COWL SUPPORT BEAM FITTING OF LH ENGINE / STRUT(<P>FAN COWL SUPPORT BEAM FITTING P/N 311T2114-7 WAS REPLACED PER DRAWING TRE6754167 AND IPC 54-50-53-02 REQUIREMENTS&NBSP;</P>)

Part: FASTENER — DAMAGED · airframe 104,204 hrs · 20,147 cycles

LIGHTNING STRIKE DAMAGES ON FASTENER HEADS OF FWD CARGO DOOR, OUTER SKIN BETWEEN STA 498.6 AND STA 606.4 AND BELOW INTERCOSTAL #7.(<P>REPAIR WAS ACCOMPLISHED PER BOEING SR# 3-5542193486.</P>)

Part: SPRING — INOPERATIVE · airframe 104,204 hrs · 20,147 cycles

AFT ENTRY DOOR GAS SPRING WAS FOUND INOP.(AFT ENTRY DOOR GAS SPRING WAS REPLACED PER AMM 25-66-03-004-053 & 25-66-03-404-067 REQUIREMENTS.)

Part: SPRING — INOPERATIVE · airframe 104,204 hrs · 20,147 cycles

FORWARD ENTRY DOOR GAS SPRING WAS FOUND INOP.(FWD ENTRY (L1) DOOR GAS SPRING WAS REPLACED PER AMM 25-66-03-404-067 REQUIREMENTS)

Part: SKIN — FOULED · airframe 104,204 hrs · 20,147 cycles

RH WING CENTER SECTION, LOWER SURFACE WITH FUEL LEAK EVIDENCE AT / STG L10 AND RBL97.0(<P>FUEL LEAK EVIDENCE WAS REPAIRED PER AMM 28-11-00-308-013 REQUIREMENTS.</P>)

Part: SHEAR TIE — CORRODED · airframe 104,204 hrs · 20,147 cycles

CORROSION ON SHEAR TIE BETWEEN BODY STA 1562 AND STRINGER S-39LH / S-39RH, BULK CARGO COMPARTMENT AREA, SECTION 46.(SHEAR TIE WAS REPLACED PER PRODUCTION DRAWING AND SRM 51-10-02 PARA 9 REQUIREMENTS.)

Part: SPRING — INOPERATIVE · airframe 104,204 hrs · 20,147 cycles

MID ENTRY DOOR GAS SPRING WAS FOUND INOP.(<P>MID ENTRY (L2 & R2) DOOR GAS SPRING WERE REPLACED PER AMM 25-66-03-404-067 REQUIREMENTS)

Part: PCA — OUT OF ADJUST · airframe 104,204 hrs · 20,147 cycles

RH HORIZONTAL STABILIZER, INBOARD PCA FREEPLAY OUT LIMIT.(<P>PCA WAS REPLACED AND THE PCA INPUT ROD WAS ADJUSTED PER AMM 27-31-05-424-027 REQUIREMENTS)

Part: FUEL CELL — LEAKING · airframe 104,204 hrs · 20,147 cycles

FUEL LEAK EVIDENCE ON FASTENERS AREA UPPER SKIN BETWEEN WS 564 / AND WS 590.2. RH WING(<P>FUEL LEAK WAS REPAIRED PER AMM 28-11-00-368-034 REQUIREMENTS.</P>)

Part: SWITCH — BROKEN · airframe 104,204 hrs · 20,147 cycles

DMI L NAV SWITCH BROKEN. L NAV INOP.(MODE CONTROL PANEL WAS REPLACED PER AMM 22-11-02-002-001 & 22-11-02-402-008 REQUIREMENTS.)

Part: FUEL TANK — LEAKING (LT WING) · airframe 104,204 hrs · 20,147 cycles

LH WING CENTER SECTION LOWER SURFACE WITH FUEL LEAK EVIDENCE AT / STG L6 AND LBL62.0.(<P>FUEL LEAK EVIDENCE WAS REPAIRED PER AMM 28-11-0-308-013 REQUIREMENTS.</P>)

Part: SHEAR TIE — CORRODED · airframe 104,204 hrs · 20,147 cycles

CORROSION ON SEVERAL SHEAR TIES LOCATED AT BODY STA 1417 AND STRINGER S-36LH / S-37RH, AFT CARGO COMPARTMENT, SECTION 46.(SHEAR TIES WERE REPLACED PER PRODUCTION DRAWING AND SRM 51-10-02 PARAGRAPH 9 REQUIREMENTS.)

Part: PRESSURE VALVE — INOPERATIVE · airframe 104,204 hrs · 20,147 cycles

ENGINE # 2 PRV ALWAYS IN PARTIAL POSITION.(<P>AFFECTED PART WAS REPLACED AND TESTED PER AMM 36-11-18-703-115 REQUIREMENTS</P>)

Part: SKIN — FAILED INSP · airframe 104,204 hrs · 20,147 cycles

DEVIATIONS WERE FOUND DURING THE ACCOMPLISHMENT OF SB767-57-010 PART 8 AT LH WING LOWER SKIN REPAIR AT STGR 9.5 AND WSTA 990.2(THE REPAIR WAS ACCOMPLISHED PER BOEING SR# 3-5538397542)

Part: ANGLE — BROKEN · airframe 104,204 hrs · 20,147 cycles

BROKEN VERTICAL ANGLE LOCATED IN SUPPORT FRAME AT STA 1087 AND RBL 26 OF THE AFT CARGO COMPARTMENT AREA.(<P>VERTICAL ANGLE WAS REPLACED PER PRODUCTION DRAWING AND SRM 51-10-02-0G-0 REQUIREMENTS.</P>)

Part: SLIDE — INOPERATIVE · airframe 103,409 hrs · 19,985 cycles

"L1 DOOR SLIDE INOP. ( MAIN ENTRY DOOR/SLIDES/EMERGENCY EXITS PASSENGER CONFIGURATION PASSENGERS CARRIED )" REMOVED DEPLOYED SLIDE TRANS TO MDDR 167176 CAT A DDG 52-11-04-01A / REF LO 1533453 REPLACED L1 SLIDE ARM DISARM FUNCTION CKS GOOD IAW AMM 25-66-01&NBSP;</P> / <DIV DATA-CCP-TIMESTAMP="1655823336025">&NBSP;</DIV>)

Part: TRANSDUCER — NONE · 19,920 cycles

COCKPIT O2 INDICATION SHOWED 1990 PSI DURING PREFLIGHT. ATTEMPTED DRAIN BUT PRESSURE/FLOW RATE DECREADED RAPIDLY. MX FOUND BOTTLE EMPTY.(<P>INDICATION TRANSFERRED TO MDDR 164350. REMOVED AND REPLACED O2 BOTTLE IAW AMM 12-15-08. LEAK CHECK GOOD.</P> / <P>LOGPAGE 1513521 - ITEM #1: REMOVED AND REPLACED TRANSDUCER REF AMM 35-11-03. THIS CLEARS MDDR 164350.</P>)

Part: O-RING — LEAKING · airframe 103,017 hrs · 19,902 cycles

ENGINE #2 HAS PNEUMATIC LEAK @ LOCATION "K" AS PER EO # 1936A088(<P>REMOVED AND REPLACED LEAKING "O" RING AT LOCATION "K" REF 767 AMM 20-16-19-404. ACCOMPLISHED</P> / <P>PNEUMATIC LEAK CHECK PER B767 EO 1936A088 NO LEAKS NOTED</P>)

Part: BOTTLE — LOW PRESSURE · airframe 103,017 hrs · 19,902 cycles

AFT MID CLOSET PORTABLE OXYGEN BOTTLE PRESS LOW P/N 9700-CIA BF23A S/N 525829 REMOVED AND REPLACED AFT MID CLOSET PORTABLE O2 BOTTLE PER B767-300 AMM 35-31-01

Part: SCREW — MISSING · airframe 103,017 hrs · 19,902 cycles

SCREW MISSING RIGHT PYLON INBOARD UPPER MIDDLE(<P>INSTALLED NEW&NBSP; FASTENER AT R/H&NBSP; PYLON I/B&NBSP; SIDE PANEL PER B767-300 AMM 20-11-00-910-802.</P>)

Part: CABLE — SHORTED · airframe 1,030 hrs · 19,902 cycles

#1 ENGINE VIB INDICATION INTERMITTENT T/S PER W/D ; 77-31-11. REPLACED SHORTED OUT L ENG T677 FAN ACCELEROMETER CABLE IAW SWPM 20-10-11 W/D 77-31-11 AVM. SYS OPS TEST OK IAW AMM 77-31-00/501. L ENG ; DRY RUN UP / GROUND TEST #2 OK IAW&NBSP; AMM 71-00-00/795. MDDR 163377 CLEARED UP.

Part: SEALANT — DEFECTIVE · airframe 103,017 hrs · 19,902 cycles

RIGHT ENG. INBD T/R LOWER BIFURCATION SEALANT IS FULL OF AIR BUBBLES AT AFT AREA PREPARED, CLEANED AND REPAIRED DAMAGED&NBSP; FIRE RETARDANT AT R/H&NBSP; ENG&NBSP; I/B&NBSP; T/REV&NBSP; PER&NBSP; B767-300 AMM; 78-31-00-308-072-H00

Part: STOP — MISSING · airframe 103,017 hrs · 19,902 cycles

CAPT'S SHOULDER HARNESS STOP MISSING R STRAP(<P>INSTALLED CAPT'S SHOULDER HARNESS STOP &AMP; OPS CHECK GOOD PER B767-300 AMM 25-11-01</P>)

Part: FIRE LOOP — DAMAGED · airframe 103,017 hrs · 19,902 cycles

ENG #1 WIRING OF FIRE LOOP LOWER DAMAGED LOCATED AT 6 O'CLOCK FWD OF PRESSURE SWITCH REPAIRED #1 ENG FIRE LOOP WIRED DETECTOR TS683 PER W/D 26-11-11 ; SWPM 20-10-14 OPS CHECK OK AMM 26-11-00

Part: DUCT SEAL — DAMAGED · airframe 103,017 hrs · 19,902 cycles

ENG #1 BOTH C/DUCT INTERNAL AREA WITH SEALANT DAMAGEDPREPARED, CLEANED AND REPAIRED DAMAGED FIRE RETARDANT SEAL AT #1 ENG L/H &AMP; R/H C/DUCTPER B767-300 AMM 78-31-00-308-072

Part: PLUG — DAMAGED · airframe 103,017 hrs · 19,902 cycles

ENG #1 STARTER OVER FLOW PLUG WITH LANYARD DAMAGED(<P>REMOVED &AMP; REPLACED #1 ENG STARTER OVERFLOW PLUG PER&NBSP; B767-300 AMM 12-13-02. NO LEAKS</P>)

Part: STATIC LINE — DAMAGED · airframe 103,017 hrs · 19,902 cycles

LEFT O/B AILERON WITH STATIC DISCHARGE DAMAGED(<P>REMOVED AND REPLACED DAMAGED DAMAGED STATIC DISCHARGER AT L/H O/B&; AILERON PER B767-300; 23-61-01-022-008 AMM 23-61-01-402-013. PERFORMED STATIC DISCHARGER RESISTANCE TEST AS PER 767-300 AMM 23-61-01-732-155</P>)

Part: LIGHT — INOPERATIVE · airframe 102,755 hrs

EMER LIGHT CELING INOP AT ROW 24A/C AND ROW 17K/H PERFORMED OPERATIONAL TEST OF EME LIGHT AISLE (CEILING) AT ROW 24AC AND 17KH PER AMM 33-51-05, OPS CHECK GOOD.

Part: SIGN — INOPERATIVE · airframe 102,755 hrs · 19,842 cycles

EMG LIGHT EXIT SIGN INOP AT L2 DOOR(<P>TIGHTENED LOOSE CONNECTOR SIGN, OPS CK C/W. IAW MM 33-55-00.</P>)

Part: KIT — NONE · airframe 102,345 hrs · 19,758 cycles

FWD CLOSET FIRST AID KIT DUE TIME CHANGE P/N S6-01-0005-306 NSN DUE 22 FEB 22.(<P><SPAN>REMOVED &AMP; REPLACED&NBSP; FWD CLOSET FIRST&NBSP; AID KIT AS&NBSP; REQUIRED PER&NBSP; AMM 25-64-00. CK'D&NBSP; OK .</SPAN></P> / <P><SPAN>&NBSP; EXP TAG. P/N S6-01-0005-306.</SPAN></P>)

Part: BRACKET — NONE · airframe 102,345 hrs · 19,758 cycles

LEFT ENGINE O/B CORE COWL HOLD OPEN ROD SUPPORT BRACKET IS BROKEN .(<P>REMOVED AND REPLACED BROKEN BRACKET AT L/H ENGINE O/B CORE COWL HOLD OPEN ROD SUPPORT</P> / <P>PER&NBSP; B767-300 SRM 51-40-02-0G-0.</P>)

Part: CLAMP — NONE · airframe 102,345 hrs · 19,758 cycles

# 2 ENG. CLAMP BROKEN SENSE LINE OF HPSOV VALVE .(<P><SPAN>REPOSITIONED&NBSP; # 2 ENG. HPSOV&NBSP; CONTROL PRESSURE LINE&NBSP; &NBSP;AND INSTALLED NEW SERVICEABLE CLAMP&NBSP; AS REQUIRED IAW AMM 36-11-07.</SPAN></P> / <P><SPAN>EXP TAG.&NBSP; &NBSP;P/N&NBSP; BACC10HS07.</SPAN></P>)

Part: KIT — NONE · airframe 102,345 hrs · 19,758 cycles

AFT LAST L/H OVHD BIN FIRST AID KIT DUE TIME CHANGE P/N S6-01-0005-306 NSN DUE 28 FEB 22.(<P><SPAN>REMOVED &AMP; REPLACED&NBSP; AFT LAST&NBSP; L/H&NBSP; OVHD BIN FIRST AID KIT&NBSP; AS REQUIRED PER AMM 25-64-00. CK'D&NBSP; OK .</SPAN></P> / <P><SPAN>EXP TAG.&NBSP; P/N S6-01-0005-306.</SPAN></P>)

Part: NONE — NONE · airframe 102,345 hrs · 19,758 cycles

# 2 ENG. HPSOV VALVE INPROPERLY INSTALL .(<P><SPAN>POSITIONED&NBSP; # 2 ENG.&NBSP; HPSOV&NBSP; TO&NBSP; &NBSP;CORRECT&NBSP; &NBSP;CONFIGURATION&NBSP; IAW AMM 36-11-07</SPAN></P>)

Part: NONE — NONE · airframe 102,345 hrs · 19,758 cycles

RH MLG SCRAPER RING DISLODGED .(<P>PERFORMED SCRAPPER RING REPLACEMENT PER AMM&NBSP; 32-11-25.</P> / <P>PERFORMED RH MLG STRUT SERVICING PER AMM 12-15-01.</P> / <P>ACCOMPLISHED R/H MLG EXTENSION AND RETRACTION SYSTEM OPERATIONAL TEST PER M/M 32-32-00. OPS &AMP; INDICATION NORMAL.</P>)

Part: EVAS UNIT — NONE · airframe 102,345 hrs · 19,758 cycles

CAPTN EVAS WITH BLOWER INOP .(<P><SPAN>REMOVED &AMP; REPLACED&NBSP; CAPT. EVAS&NBSP; PER AMM 25-60-99. OPS CHECK GOOD .</SPAN></P> / <P><SPAN>P/N OFF 107STC-019&NBSP; &NBSP;S/N 028EE02P&NBSP; &NBSP;S/N ON 053DD05P.&NBSP; 5Y2903909</SPAN></P>)

Part: NONE — NONE · airframe 102,345 hrs · 19,758 cycles

# 2 ENG. SEVERAL FAN BLADES WITH NICKS .(<P><SPAN>BLENDED CUT&NBSP; SEVERAL FAN BLADE&NBSP; AT&NBSP; # 2 ENG.&NBSP; FOUND WITHIN LIMITS PER B767-300&NBSP; &NBSP;AMM 72-31-02-308-045-H00.&NBSP;</SPAN></P> / <P><SPAN>PERFORMED NDT&NBSP; SPOT&NBSP; FLOURESCENT&NBSP; PENETRANT&NBSP; &NBSP;INSP. NO NICK ON&NBSP; CRACKS NOTED REF.&NBSP; AMM 70-11-06</SPAN></P>)

Part: NONE — NONE · airframe 102,345 hrs · 19,758 cycles

DURING COKPIT PREPARATION FOR RUN UP UPPER EICAS DIPLAY FAIL .(<P><SPAN>REMOVED/REPLACED&NBSP; UPPER&NBSP; EICAS&NBSP; D.U&NBSP; N10013&NBSP; &AMP;&NBSP; OPS&NBSP; CHECK&NBSP; OK&NBSP; &NBSP;ANN&NBSP; &NBSP;31-41-01</SPAN></P>)

Part: NONE — NONE

3 EXTERIOR EMERGENCY LIGHTS INOP.(<P>RELAMPED 3 EXTERIOR EMERGENCY ESCAPE LIGHTS IAW AMM 33-51-06. OPS CHECK GOOD.</P>)

Part: NONE — NONE · airframe 102,169 hrs · 19,716 cycles

L PACK TEMP EICAS DISPLAYED(<P>PERFORMED LEFT PACK TEMP CONTROLLER BITE TEST IAW 21-51-00-705-001. EICAS MSG CLEARED.</P>)

Part: NONE — NONE · airframe 102,115 hrs · 19,701 cycles

DURING BEFORE START EICAS MSG LEFT PACK TEMP.(<P>PERFORMED LH PACK TEMP CONTROLLER BITE. NO FAULTS FOUND AT THIS TIME PER 21-51-FT803</P>)

Part: NONE — NONE

AFTER LANDING APU FAILED TO START. 3 ATTEMPTS. APU FAULT LIGHT MESSAGE.(<P>PERFORMED APU BITE PER FIM 49-11 FT 987. NO FAULTS NOTED AT THIS TIME. PERFORMED OPS CHECK OF APU PER AMM 49-11-00. OPS CHECK GOOD.</P>)

Part: NONE — NONE

EICAS MSG R ENG PRV AFTER TAKEOFF. MESG WENT AWAY PRIOR TO INITIATIN NNC(<P>PERFORMED AIR SUPPLY BITE CHECK, MESSAGE CLEARED IAW AMM 36-11-00.</P>)

Part: NONE — NONE

LEFT PACK INOP IN AUTO MODE (PACK TEMPERATURE CONTROL SYSTEMS (-200/-300), AUTO MODE)(<P>DEFERRED TO MEL 21-51-03-01, MDDR 155908, CAT C.</P> / <P>LOG PAGE 1420176 : REMOVED AND REPLACED LH PACK FLOW PC ASSY PER AMM 21-51-09, OPS CK GOOD. THIS CLEARS DMI 155908.</P>)

Part: IDG — NONE

LEFT GENERATOR DRIVE LIGHT INOP. ( GENERATOR DRIVE LIGHTS, -200/-300, EICAS MESSAGE OPERATIVE(<P>TRANSFERRED TO MEL 24-11-01-01A MDDR 155475, CAT B, DUE DATE 23OCT21. PLACARD INSTALLED. MAINT PROCEDURE C/W.&NBSP;&NBSP;</P> / <P>REF LOG 1420053 ITEM 15 BWI 21OCT21 - REMOVED AND REPLACED IDG IAW AMM 21-11-01- OPS CKS GOOD. THIS CLEARS MDDR 155475.</P>)

Part: NONE — NONE

CATERING NOTIFIED MX THAT SLIDE PACK FELL OUT OF DOOR UPON OPENING L4 DOOR(<P>REMOVED AND REPLACED L4 DOOR SLIDE PACK IAW AM 25-66-01, OPERATIONAL CHECK GOOD</P>)

Part: RELAY — NONE

AFT CROSSFEED VALVE INDICATION LIGHT INOP(<P>OK TO DEFER IAW MEL 28-40-01-02-01A MDDR 155264 CAT C DUE 27OCT21. PLACARD INSTALLED.&NBSP;</P> / <P>18OCT21 - 1420031 - ITEM# 6 - BWI - R&AMP;R AFT FUEL XFEED RELAY (K2151) PER FIM 28-22 FT 821. OPS CHK GOOD AT THIS TIME . THIS CLEARS DMI 155264.</P>)

Part: GENERATOR — NONE · airframe 101,975 hrs · 19,670 cycles

L GEN OFF(<P>TRANSFERRED TO MEL 24-00-01-01 MDDR 155212 CAT B, DUE DATE: 19OCT21. MAINT PROCEDURES C/W. PLACARD INSTALLED. DISPATCH JD 0912Z.</P> / <P>19OCT21 - 1420033 - ITEM# 10 - BWI -&NBSP;<SPAN>REMOVED AND REPLACED LEFT IDG AND OPS CHECK GOOD IAW AMM 24-11-01. THIS CLEARS MDDR 155212, PLACARDS REMOVED.</SPAN><SPAN>DISPATCH T&AMP;I:&NBSP; 0348&NBSP; DL</SPAN></P>)

Part: BATTERY — NONE

EMG EXIT LIGHT SIGN INOP AT L1 &AMP; R1 DOOR(<P>REMOVED AND REPLACED EMG EXIT LIGHT BAT UNDER FA SEAT PER AMM 33-51-07, OPS CK GOOD AT THIS TIME&NBSP;</P>)

Part: NONE — NONE

MOMENTARY EICAS MSG "L PACK TEMP" AT 6000'(<P>PERFORMED BITE CK ON LEFT PACK TEMP CONTROLLER. PREVIOUS FLT FLAGGED (TEMP CONT VALVE) RESET L PACK CONTROLLER IAW 21-51-00 AND PERFORMED OPS CK IAW 21-51-00 PER AMM OF COOLING PACK SYSTEM. OPS CK GOOD &AMP; L PACK CONTROLLER BITE PASSED.</P>)

Part: RELAY — NONE

AFT EQUIP EXH FAN #1 INOP ( AFT EQUIPMENT/LAV/GALLEY EXHAUST (VENT) FANS )(<P STYLE="MARGIN: 0IN; MARGIN-BOTTOM: .0001PT;"><SPAN>TRANSFERRED TO MEL 21-58-05, CAT C, DUE ON 15OCT21, MDDR 154607.</SPAN></P> / <P STYLE="MARGIN: 0IN 0IN 0.0001PT;"><SPAN>11OCT21 - 1315007 €“ ITEM #19 - BWI - R&AMP;R FAN 1 CURRENT SENSOR PER AMM 21-26-04 AND WDM 21-26-11. PERFORMED OPS CK PER AMM 71-76-00. FAN 1 STILL DOESN'T RUN. MDDR 154607 REMAINS OPEN.</SPAN></P> / <P>&NBSP;</P> / <P STYLE="MARGIN: 0IN 0IN 0.0001PT;"><SPAN>12OCT21 - 1315008 €“ ITEM #22 - BWI - T/S FOUND RELAY K835 INOP PER WDM 21-26-11. R&AMP;R RELAY K835 PER SWPM 20-81-22. OPS CK (B15) VENT FAN 1 IS NORMAL PER AMM 21-26-0. THIS CLEARS DMI 154607. PLACARD REMOVED &AMP; MCC NOTIFIED.</SPAN></P> / <P>&NBSP;</P>)

Part: FAN — INOPERATIVE

AFT EQUIPMENT EXH FAN #2 INOP.TRANSFERRED TO MDDR 154372 IAW MEL 21-58-05, CAT C.. 04OCT21 - LP 1484060 - ITEM# 9 - BWI - REMOVED AND REPLACED AFT EQUIP EXHAUST FAN #2 IAW 21-26-01. OPS CHECK GOOD. THIS CLOSES MDDR 154372. PLACARD REMOVED. TI: BM 1324Z

Part: ACTUATOR — WARNING MESSAGE

LEFT PACK TEMP EICAS MESSAGE(<P>TRANSFERRED TO MEL 21-51-03-01, MDDR #154077, CAT "C".LP1484059 - REMOVED AND REPLACED LH PACK RAM AIR INLET DOOR ACTUATOR IAW AMM 21-53-01, OPS TEST GOOD. THIS CLEARS DMI 154077, PLACARDS REMOVED.

Part: IGNITER — WARNING MESSAGE · airframe 101,820 hrs · 19,638 cycles

LEFT ENGINE IGNITION STATUS MESSAGE ( IGNITION SYSTEMS, ER OPERATIONS ALLOWED )(<P>TRANSFER TO MDDR 153888, MEL 74-00-01A, CAT A.</P> / <P>REF LOGPAGE 1315560 # 7 - REMOVED AND INSPECTED #1 IGNITION LEAD. REMOVED AND REPLACED #1 ENGINE #1 IGNITOR IAW AMM 74-11-01. PERFORMED IDLE ENGINE RUN OPS CKS. OPS CHK GOOD. THIS CLEARS MDDR 153888. MCC NOTIFIED.</P>)

Part: BOTTLE — LOW PRESSURE · airframe 101,806 hrs · 19,636 cycles

FOUND PORTABLE O2 BOTTLE @ 0 PSI IN FWD GALLEY.(<P>REMOVED AND REPLACED PORTABLE O2 BOTTLE PER AMM 35-31-01.</P>)

Part: ACTUATOR — INOPERATIVE (SPAR VALVE)

LT ENGINE NO LIGHT FOR SPAR VALVE DURING ENGINE START. ( SPAR VALVE LIGHTS (-200/-300) )(<P>TRANSFERED TO MEL 28-40-02, MDDR 153862, CAT C.</P> / <P>27 SEP - 21 - LP 1484033 ITEM 1 - SHJ- REMOVED AND REPLACED LH ACTUATOR ASSY VALVE SPAR PERFORMED OPERATIONAL TEST OK IAW AMM 28-22-11 PLACARD REMOVED CLEARS MDDR 153862</P>)

Part: EVAS UNIT — DETACHED

DURING TAKEOFF FIRST OFFICER EVAS SEAL LID CAME OFF(<P>INSPECTED AND REATTACHED LID PER AMM 25-60-99.</P>)

Part: CIRCUIT CARD — UNSECURE (DUCT LEAK) · 19,623 cycles

L DUCT LEAK LIGHT ILLUMINATED(<P>RESEATED LEFT DUCT LEAK CARD M091 AND OPS CHECKED GOOD IAW AMM 26-00-00</P>)

Part: CONNECTOR — DISCONNECTED (OUTLET SENSOR)

"L PACK TEMP" ADVISORY MESSAGE DURING PUSH BACK.(<P>TRANSFERRED TO MDDR 153334 PER MEL 21-51-03-01, CAT C, DUE DATE: 20SEP21, PLACARD INSTALLED. DISPATCH: JT @ 1833Z</P> / <P>LOG PAGE 1346539: INSPECTED LEFT PACK. FOUND COMPRESSOR OUTLET SENSOR CANNON PLUG DISCONNECTED. RECONNECTED AND OPS CHECKED GOOD I/A/W AMM 21-51-06. THIS CLEARS MDDR 153334.</P>)

Part: CONTROL VALVE — INOPERATIVE (RT A/C PACK TEMP) · 19,621 cycles

R/H PACK AUTO MODE INOP ( PACK TEMPERATURE CONTROL SYSTEMS (-200/-300) , AUTO MODE )(<P>TRANSFERRED TO MEL 21-51-03-01, MDDR# 153268, CAT C. 19SEP2021. PLACARD INSTALLED.</P> / <P>LOG PAGE 1346540: REMOVED AND REPLACED RT TEMP CONTROL VALVE AND OPS CHECKED GOOD IAW AMM 21-51-12. THIS CLEARS MDDR 153268.</P>)

Part: VALVE — INOPERATIVE (FUEL CROSSFEED)

AFT FUEL CROSSFEED INOP(<P>REMOVED AND REPLACED AFT FUEL X-FEED VALVE ACTUATOR IAW AMM 28-22-12.</P> / <P>LOG PAGE 1346521: PERFORMED OPS CK OF AFT FUEL CROSSFEED VALVE&NBSP; &AMP; INSTALLED SAFETY WIRE AND SEALANT IAW AMM 28-22-12. OPS CK GOOD, NO FAULT.</P>)

Part: LIGHT — INOPERATIVE (STAB TRIM) · airframe 101,698 hrs · 19,617 cycles

"STAB TRIM " ANNUNCIATOR LIGHT INOP. REMOVED / REPLACED STAB TRIM LIGHT ANNUNCIATOR P5 PANEL OPS CHECKOK AMM 33-16-02 REV 133.

Part: ACTUATOR — FAULTED (RT WING SLIDE) · airframe 101,698 hrs · 19,617 cycles

EMOVED &AMP; REPLACED DOOR OPENING ACTUATORS DUE TO RH WING ESCAPE SLIDE OPS CHECK(<P><SPAN>REMOVED AND REPLACED&NBSP; RH&NBSP; AFT DOOR&NBSP; OPENING&NBSP; ACTUATOR&NBSP; &NBSP;PER&NBSP; AMM&NBSP; 25-65-1</SPAN></P> / <P><SPAN>REMOVED :&NBSP; REPLACED&NBSP; &NBSP;R/H&NBSP; &NBSP; DOOR OPENING&NBSP; &NBSP; PER&NBSP; MM&NBSP; 25-65-10</SPAN></P>)

Part: SLIDE — FAULTED (RT WING) · airframe 101,698 hrs · 19,617 cycles

REMOVED & REPLACED RH WING ESCAPE SLIDE DUE TO OPS CHECK. REMOVED & REPLACED R/H WING ESCAPE SLIDE AS PER 767 MM 25-65-01.

Part: SQUIB — FAULTED (RT SLIDE) · airframe 101,698 hrs · 19,617 cycles

REMOVED & REPLACED SPOILER OVERRIDE ACTUATOR SQUIB DUE TO RH WING SLIDE OPS CHECK SQUIB FOR SPOILER OVERRIDE ACTUATOR PART OF THE SPOILER ACTUATOR REPLACED IN NR 49.

Part: PACKING — LEAKING (NR 2 ENGINE) · airframe 101,698 hrs · 19,617 cycles

ENG #2 PRVC LOC E IS LEAKING(<P><SPAN>REMOVED, REPLACED AND LEAK&NBSP; CHECKED PACKING&NBSP; &NBSP;AT LOCATION&NBSP; ' E "&NBSP; REF&NBSP; E.O&NBSP; 1936A088&NBSP; &NBSP; &NBSP;NO LEAKS</SPAN></P>)

Part: ACTUATOR — FAULTED (RT WING SLIDE) · airframe 101,698 hrs · 19,617 cycles

REMOVED &AMP; REPLACED THE LATCH OPENING ACTUATORS DUE TO RH WING ESCAPE SLIDE SYSTEMS OPS CHECK(<P>LATCH OPENING&NBSP; ACTUATOR&NBSP; IN ORDER&NBSP;&NBSP;</P> / <P>REMOVED &AMP;&NBSP; REPLACED&NBSP; THE&NBSP; LATCH&NBSP; OPENING&NBSP; ACTUATOR&NBSP; IAW&NBSP; AMM&NBSP; &NBSP;25-65-11.</P>)

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 101,698 hrs · 19,617 cycles

L/H FUSELAGE STATION 900 EMERGENCY LIGHT INOP .(<P><SPAN>RELAMPED&NBSP; LH.&NBSP; &NBSP;FUSELAGE&NBSP; EMG.&NBSP; LT&NBSP; &AMP;&NBSP; OPS&NBSP; &NBSP;CHECK&NBSP; OK&NBSP; AMM&NBSP; &NBSP;33-51-00&NBSP; &NBSP;REV&NBSP; 133</SPAN></P>)

Part: PACKING — LEAKING (NR 2 ENGINE) · airframe 101,698 hrs · 19,617 cycles

ENG #2 PRVC LOC K IS LEAKING .(<P><SPAN>REMOVED, REPLACED &AMP; LEAK CHECKED&NBSP; PACKING&NBSP; &NBSP;AT LOCATION&NBSP; " K "&NBSP; &NBSP;REF&NBSP; J/C&NBSP; E.O&NBSP; 1936A088</SPAN></P> / <P><SPAN>NO LEAKS</SPAN></P>)

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 101,698 hrs · 19,617 cycles

R2 DOOR EXTERIOR EMERGENCY LIGHT INOP .(<P><SPAN>RELAMPED&NBSP; R2&NBSP; DOOR&NBSP; EXT. EMG&NBSP; LT.&NBSP; &AMP;&NBSP; OPS&NBSP; CHECK&NBSP; OK&NBSP; &NBSP;AMM&NBSP; &NBSP;33-51-00&NBSP; REV&NBSP; 133</SPAN></P>)

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 101,698 hrs · 19,617 cycles

IN€ŒTERNAL EMERGENCY LIGHT OVER SEAT ROW 32K-H INOP(<P><SPAN>RELAMPED&NBSP; EMG&NBSP; LT&NBSP; CEILING SEAT ROW 32K-H&NBSP; &AMP; OPS&NBSP; CHECK&NBSP; OK AMM 33-51-00/175.</SPAN></P>)

Part: CYLINDER — NOT REPORTED (RT WING SLIDE) · airframe 101,698 hrs · 19,617 cycles

REMOVE &AMP; REPLACE INFLATION CYL OF RH WING SLIDE DUE TO OPS CHECK OF ( RH WING SLIDE )(<P><SPAN>REMOVED &AMP; REPLACED&NBSP; RH&NBSP; INFLATION&NBSP; CYLINDER&NBSP; PER&NBSP; AMM&NBSP; 25-65-02</SPAN></P>)

Part: STATUS MESSAGE — FALSE ACTIVATION (WX RADAR SYS) · airframe 101,688 hrs · 19,616 cycles

WXR SYS STATUS MSG. RESET FAULT. OPS CHK GOOD IAW AMM 34-43-00.

Part: PRESSURE SWITCH — FAULTED (LT ENGINE OIL) · airframe 101,665 hrs · 19,612 cycles

LEFT ENG OIL PRESS LIGHT INOP. TRANSFER TO MDDR 152653(<P>R/R LEFT ENG LOW OIL PRESS SW IAW B767 AMM 79-32-01-404-088-H00.PERFORMED PRESSURE TRANSMITTER TEST IAW B767 AMM 71-00-00-945-229-NO.3 .OPS CHECK GOOD. LEAK CHECK GOOD. THIS CLEARS DMI 152653 PLACARD REMOVED.</P>)

Part: PUMP — FAILED (RT FUEL BOOST)

RT FWD PUMP EICAS MESSAGE(<P>REPLACED RH FWD FUEL BOOST PUMP IAW B767 AMM 28-22-03. OPS CHECK BAD. BAD FROM STOCK. SEE LP 1481004 ITEM M3.&NBSP;</P> / <P>REPLACED RH FWD FUEL PUMP IAW B767 AMM 28-22-03. OPS AND LEAK CHECKS GOOD.&NBSP;</P>)

Part: TRANSMITTER — FAILED (OIL PRESSURE)

ABORTED LEFT ENGINE START. NO OIL PRESSURE INDICATION AT IDLE N2(<P>REMOVED AND RELACED LH ENG OIL PRESSURE TRANSMITTER IAW B767 AMM 79-32-01. LK OPS CHECK GOOD.</P>)

Part: WARNING LIGHT — ILLUMINATED (LT ENG OIL PRESS)

LEFT ENG OIL PRESS LIGHT INOP.(<P>TRANSFERRED TO MDDR 152218 IAW MEL 79-33-01-01, CAT C.</P>)

Part: CLAMP — LOOSE (ANTI-ICE DUCT) · airframe 101,545 hrs · 19,590 cycles

WITH ENG ANTI-ICE ON L DUCT PRESS DROPS SIGNIFICANTLY(10PSI)(<P>FOUND CLAMP LOOSE AT INLET COWL CONNECTION. TIGHTENED CLAMP RAN BOTH ENGINES, LEFT AND RIGHT. PRESSURES WERE WITHIN 1 PSI PER B767 AMM 30-21-60.</P>)

Part: GASKET — OUT OF ADJUST (ANTI ICE DUCT) · 19,592 cycles

WITH ENG ANTI ICE ON LEFT DUCT PRESSURE DROPS TO 10 PSI (RT ABOVE 30).(<P>ADJUSTED GASKET ON NOSE COWL ANTI-ICE DUCT PER B767 AMM 30-11-03. LEAK CHECK GOOD. ENGINE RUN TO 80% N2.</P>)

Part: IDG — FAULTED (RT GENERATOR) · airframe 101,529 hrs · 19,587 cycles

R GEN OFF IN FLIGHT. PER QRH TRIED TO RESET BREAKER, BREAKER FAILED TO RE-SET.(<P>REMOVED &AMP; REPLACED RT IDG, OPS TEST GOOD PER B767 AMM 24-11-01.</P>)

Part: THERMAL SWITCH — FAULTED (LT ENGINE)

L/H PYLON DUCT LEAK LIGHT COMES INTERMITTENTLY(<P>REMOVED AND REPLACED LH ENGINE STRUT THERMAL SWITCH TS237 PER WDM 26-18-12, OPS CHECK GOOD PER AMM 26-18-00.</P>)

Part: PITOT HEAD — FAULTED (FIRST OFFICER'S) · airframe 101,255 hrs · 19,526 cycles

UPON STARTING RIGHT ENGINE EICAS MSG "F/O PITOT" DISPLAYED AND "FO PITOT" WARNING LIGHT ON COMPLETED QRH AND CALLED MX.(<P>REMOVED AND REPLACED F/O PITOT PROBE ASSY PER 767 AMM 34-11-01. OPS CHECKS NORMAL. LK CK GOOD. RII INSP C/W.</P>)

Part: CONTROLLER — FAULTED (RT A/C PACK TEMP)

RT PACK TEMP CONTROL INOP IN AUTO ( PACK TEMPERATURE CONTROL SYSTEMS (-200/-300) , AUTO MODE )(<P>TRANSFERRED TO MEL 21-51-03-01, MDDR 149482, CAT C, DUE 10JUL21.</P> / <P>REMOVED AND REPLACED RT PACK TEMP CONTROLLER AND OPS CHECK IAW 21-51-00. THIS CLEARS MDDR 149482. PLAC REMOVED.</P>)

Part: CONNECTOR — DAMAGED (EMERGENCY EXIT) · airframe 101,161 hrs · 19,506 cycles

CABIN PASSENGER EMERGENCY EXIT HATCH LH, INNER ELECTRICAL CONNECTOR WAS FOUND WITH DAMAGE.(<P ><SPAN>ELECTRICAL CONNECTOR WAS CHANGED AND CONTACT PIN&NBSP;</SPAN></P> / <P>&NBSP;</P>)

Part: BULB — MALFUNCTIONED (HEAT EXCHANGER) · airframe 101,161 hrs

ON CLIMB OUT EICAS R PACK TEMP EXTINGUISHED WITH STANDBY ( PACK TEMPERATURE CONTROL SYSTEMS, (-200/-300) (MAY BE INOPERATIVE OFF) )(<P>DEFERED IAW MEL 21-51-03 MDDR 146045 CAT C 8MAY21 PLACARD INSTALL</P><P>30APR2021 - 1276082 ITEM #10 - REMOVED AND REPLACED R/H PACK TEMP CONTROLLER IAW AMM 21-51-14. OPS CHECK GOOD. THIS CLEARS DMI 146045 PLACARDS REMOVED.</P><P>1MAY2021 - 1476083 ITEM #13 - REMOVED AND REPLACED RH PRIMARY HEAT EXCHANGER TEMPERATURE BULB IAW AMM 21-52-08. OPERATIONAL CHECK GOOD INDICATION NORMAL. P/N 28034-1, NSN</P><P><BR /></P>)

Part: CONTROL VALVE — MALFUNCTIONED (RT A/C PACK) · airframe 101,137 hrs · 19,501 cycles

"R PACK TEMP" EICAS MESSAGE DISPLAYED ACCOMPLISHED QRH(<P>REMOVED &AMP; REPLACED PACK TEMP CONTROL VALVE AND OPS CHECK IAW MM 21-51-12.</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (RT A/C PACK) · airframe 101,108 hrs · 19,495 cycles

EICAS MESSAGE R PACK TEMP ON TAXI . QRH CLEARED MESSAGE. AUTO MODE FUNCTIONED NORMALLY AFTER 30 MINUTES(<P>PERFORMED BITE TEST OF R PACK CONTROLLER TEST PASSED NO DEFECTS NOTED. OPS CHECK OF RIGHT PACK GOOD IAW B767 AMM 21-51-14<BR /></P>)

Part: FAN — FAILED (AFT GALLEY) · airframe 101,108 hrs · 19,495 cycles

AFT GALLEY EXHAUST FAN # 2 EXTREMELY NOISY. PULLED BREAKER P 10 ON P11 PANEL, PLACARD INSTALLED. REMOVED AND REPLACED AFT GALLEY FAN NR 2 ASSY IAW AMM 21-26-01. OPS CHECKED GOOD.

Part: CONTAINMENT BAG — OPEN (CABIN) · airframe 101,017 hrs · 19,477 cycles

M/D AFT L/H OVHD BIN RW 40 AVSAX CONTAIMENT BAG VACUUM SEAL BROKEN P/N AS-002-1.(<P>REMOVED AND REPLACED AFT AVSAX CONTAIMENT BAG AS PER B767-300 AMM 25-60-00.</P>)

Part: SHUTOFF VALVE — MALFUNCTIONED (RIGHT) · airframe 101,017 hrs · 19,477 cycles

WARNING RIGHT HPSOV CLOSED AND OPEN SWITCHES DISAGREE .(<P>REMOVED AND REPLACED R/H HPSOV PER MM 36-11-07-424-016-001 AND INSTALL LEAK&NBSP; BITE OK .</P><P>REQUIRES RUN UP, OPS CHK. PERFORMED ENG&NBSP; RUN UP&NBSP; IAW 767 AMM 71-00-00. OPS CHK NORMAL</P>)

Part: SCREEN — MISSING (THRUST REVERSER) · airframe 101,017 hrs · 19,477 cycles

LEFT ENG WIRE MESH MISSING AT 3O' CLOCK POSITION OF T/R PART OF EO6778A019 DUE AT NEXT&NBSP; ACHECK&NBSP;(<P>ACCOMPLISHED REPAIR PER EO1978A227 TALLY 8024</P>)

Part: THRUST REVERSER — DAMAGED (LT ENGINE) · airframe 101,017 hrs · 19,477 cycles

#2 ENG. 1/B T/REV INTERIOR FIRE RETARDENT MATERIAL IS DAMAGED IN SOME AREA(<P>PREPARED CLEANED AND REPAIRED FIRE RETARDENT AT&NBSP; # 2 ENG .I/B&NBSP; T/ REV INSIDE PER&NBSP; B767-300 AMM 78-31-00-308-072-H00.

Part: PACKING — LEAKING (PNEUMATIC SYS) · airframe 101,017 hrs · 19,477 cycles

#1 ENGINE DURING PNEUMATIC LEAK CHECK USING COMPRESSED NITROGEN, CHECK FAILED AT POSITION K(<P>REMOVED AND INSTALLED ENG # 1 PACKING AT POSITION K IAW AMM 36-11-18.</P><P>PERFORMED LEAK CHECK . NO LEAKS NOTED .</P>)

Part: SCREEN — MISSING (THRUST REVERSER) · airframe 101,017 hrs · 19,477 cycles

R ENGINE WIRE MESH MISSING AT 1 AND 5 O'CLOCK POSITION ON T/R PART 2 OF EO6778A019 DUE AT NEXT A&NBSP; CHECK(<P>ACCOMPLISHED REPAIR PER EO1978227 TALLY 8025</P>)

Part: SHUTOFF VALVE — MALFUNCTIONED (RIGHT) · airframe 101,017 hrs · 19,477 cycles

RIGHT HPSOV VALVE NOT CLOSED SIGNAL WAS NO DEFECTED ( WARNING )&NBSP;(<P>REMOVED AND REPLACED R/H HPSOV PER MM 36-11-07-424-016-001.</P><P>REQUIRES RUN UP, OPS CHECK. (LEAK &AMP; BITE CHECK GOOD).</P><P>PERFORMED ENG. RUN UP IAW 767 AMM 71-00-00. OPS CHK NORMAL.</P>)

Part: ESCAPE ROPE — MISINSTALLED (COCKPIT) · airframe 101,017 hrs · 19,477 cycles

FO ESCAPE ROPE DOOR DOESNT LATCH(<P>REINSTALLED ROPE&NBSP;IAW MM 25-61-00. OPS CHECK GOOD.<BR /></P>)

Part: APU — FAILED · airframe 100,920 hrs · 19,457 cycles

APU FAILED AFTER BLOCK IN.(<P>PERFORMED BITE TEST OF APU CONTROL UNIT IAW AMM 49-61-05. NO DEFECTS NOTED. PERFORMED OPERATIONAL TEST OF APU IAW AMM 49-11-00. NO DEFECTS NOTED.</P>)

Part: DECODER — SPARKS (SEAT PSU) · airframe 100,920 hrs · 19,457 cycles

ON FINAL, CABIN CREW REPORTED "SPARKES" FROM ONE OF THE OVERHEAD LIGHTS IN THE PAX CABIN ROW CENTER&NBSP;(<P>FOUND 3 SEAT PSU DECODER, TRANSFERRED TO MDDR 144353 IAW MEL 35-21-01-01A CAT B DUE 28 MAR 21.</P><P>LOG PAGE 1311682: REMOVED AND REPLACED ROW 24/25 PSU DECODER IAW AMM 23-34-08. DURING OPS CHECK FOUND ALL AFT CENTER COLUM READING LIGHTS INOP. REF ITEM 6. PLACARDS REMOVED. DMI 144353 CLEARED.</P>)

Part: LEAD — DAMAGED (APU) · airframe 100,853 hrs · 19,443 cycles

APU DID NOT START AFTER LANDING(<P>TRANSFERRED TO MEL 49-11-01B, MDDR 143683, CAT B, DUE 14MAR21. PLACARD INSTALLED.</P><P>LP 1273745:&NBSP;REMOVED AND REPLACED APU IGNITION LEAD, IGNITOR PLUG, IGNITION EXCITER IAW AMM 49-31-02, 49-31-03, 49-31-03. THIS CLEARS MDDR 143683. IGNITION EXCITER P/N S/N OFF: 000218015975, P/N OFF: 10-617075-6, INGITER PLUG NSN, P/N OFF: 305766-1.<BR /></P>)

Part: COVER PLATE — CRACKED (THRUST REVERSER) · airframe 100,832 hrs · 19,439 cycles

#1 ENG ON INBOARD SIDE COVER PLATE ON LOWER TR ACTUATOR CRACKING(<P>REMOVED AND REPLACED COVER PLATE PER AMM 71-11-04, OPS OK</P>)

Part: CONNECTOR — DAMAGED (APU IGNITER) · airframe 100,832 hrs · 19,439 cycles

APU INOP(<P>DEFER MEL 49-11-01B, MDDR 143512, CAT B, 10MAR21. PLAC INSTALLED.</P><P>LP 1273725: T/S IAW WITH FIM 49-11-993 AND WDM 49-14-11. FOUND PUSHED BACK PIN #2 AT J4 ON IGNITOR BOX. OPS CK C/W 49-00-00. THIS CLEARS MDDR 143512. PLAC REMOVED.</P>)

Part: CONNECTOR — UNSECURE (IGNITER LEAD) · airframe 100,798 hrs · 19,430 cycles

UPON LANDING, TRIED STARTING APU AND RECEIVED "APU FAULT" EICAS MSG THREE START ATTEMPTS.(<P>DEFERRED IAW MEL 49-11-01B MDDR 143393 CAT B 08MAR21 PLACARD INSTALLED. DISP RS 1710.&NBSP; &NBSP;</P><P>LP 1273558: FOUND LOOSE CONNECTOR ON IGNITOR LEAD. IGNITOR PLUG CLEANED AND TIGHTENED. RESET CONNECTOR IAW AMM 49-00-60. OPS CHECK OK. THIS CLEARS MDDR 143393.</P>)

Part: OXYGEN MASK — INOPERATIVE (COCKPIT) · airframe 100,802 hrs · 19,431 cycles

2ND OBS O2 MASK INOP ( OBSERVER SEAT(S), SECOND OBSERVER SEAT (INCLUDING ASSOCIATED / EQUIPMENT) )(<P>DEFERED IAW MEL 25-11-02-02 MDDR# 143198. CAT D 30JUN21.</P><P>03MAR21 - 1273547 - ITEM# 3 - BWI -&NBSP;REMOVED AND REPLACED OXYGEN MASK IAW AMM 35-11-51. OPS CHECKS GOOD. THIS CLEARS DMI 143198 TI: BM @ 1206 FOR REMOVAL

Part: IGNITER — FAILED (APU COMPT) · airframe 100,802 hrs · 19,431 cycles

APU FAULT NO START AFTER TWO ATTEMPTS APU DEFERRED IAW MEL 49-11-01B, MDDR 143195, CAT B, 05MAR2021. PLACARD INSTALLED. DISP GTC 0347Z.04MAR21 - LP 1273548 - ITEM# 6 - BWI -REMOVED AND REPLACED IGNITOR IAW AMM 49-41-02. OPS CHECKS GOOD. THIS CLEARS DMI 143195. TI: BM @ 1252 FOR REMOVAL.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 100,686 hrs · 19,405 cycles

CABIN EMERGENCY LIGHTS ARE OUT FROM 30-39RH(<P>REMOVED AND REPLACED EMERGENCY PWR SUPPLY BATTERY IAW AMM 33-51-07 OPS CHECK GOOD</P>)

Part: FIRE LOOP — LOOSE (RT ENGINE) · airframe 100,605 hrs · 19,385 cycles

STATUS "RT ENGINE FIRE LP 2" RECURRING. RT ENGINE UP AFT LP1 4.4K LP2 4.4K/LOW AFT LP1 4.4K LP2 4.34K LOW FWD LP1 4.4K LP24.5K, WHEN CHECK FWD LOWER LOOP 2 FOUND TERMINAL LOOSE. REINSTALLED PER MM 26-11-02, FIRE WARNING TESTS GOOD, IAW MM 26-11-00.

Part: OXYGEN MASK — UNSERVICEABLE (PORTABLE OXYGEN) · airframe 100,586 hrs · 19,381 cycles

PORTABLE O2 BOTTLE BEHIND SEAT 39G LOW & MASK UNSERVICEABLE. SERVICED PORTABLE O2 BOTTLE, REF AMM CHAP 35-31-01. REPLACED O2 MASK, REF AMM CHAP 35-31-01.

Part: FIRE WARNING — FALSE ACTIVATION (RT ENGINE) · airframe 100,586 hrs · 19,381 cycles

RT ENGINE FIRE LP 2 STATUS MESSAGE INTERMITENT IN FLIGHT. PERFORMED ENGINE FIRE DETECTION SYSTEM BITE PROCEDURE AND RE-POSITION CHAFING FIRE LOOP 2, AS PER FIM 26-11 FAULT TREE 804, NO ACTIVE MESSAGE AT THIS TIME.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 100,392 hrs · 19,340 cycles

EMERGENCY LIGHT INOPERABLE AT FWD CABIN RIGHT SIDE FROM SEAT 1KH TO 8KH. REMOVED AND REPLACED EMERGENCY POWER PACK BATTERY ASSEMBLY, AS PER AMM 33-51-07 AND OPERATIONS CHECK GOOD.

Part: SHUTOFF VALVE — FAULTED · airframe 100,338 hrs · 19,327 cycles

FAULT WARNING A RIGHT PRSOV VALVE OPEN SIGNAL WAS NOT DETECTED. THE PRSOV OPEN POSITION SWITCH HAS FAILED IN THE VALVE NOT OPEN POS. THE VALVE IS NORMALLY EXPECTED TO BE OPEN WHEN THE ENGINE IS RUNNING AT MIN IDLE THROTTLE SETTING AND THE BLEED VALVE IS SWITCHED. REMOVED AND REPLACED VALVE ASSEMBLY PRESSURE REGULATION, IAW AMM 36-11-09. PENDING FOR LEAK CHECK. PERFORMED OP/LEAK CHECK, IAW 767 AMM 36-11-09. OPERATIONS CHECK FOUND NORMAL, NO LEAKS NOTED.

Part: ROD — WORN (ACCESS PANEL) · airframe 100,338 hrs · 19,327 cycles

NR 1 ENGINE AFT STRUT OUTBOARD HYDRAULIC ACCESS PANEL HOLD OPEN ROD SUPPORTING HARDWARE IS WORN AND HAS TOO MUCH PLAY. REMOVED AND REPLACED DAMAGED HOLD OPEN ROD AT NR 1 ENGINE AFT STRUT OUTBOARD ACCESS PANEL DOOR, PER B767-300 AMM 20-11-00-910-802.

Part: PACKING — LEAKING (NR 1 ENGINE) · airframe 100,338 hrs · 19,327 cycles

ENGINE NR 1 WITH EVIDENCE OF OIL LEAK COMING FROM NR 1 BEARING MANIFOLD. REMOVED AND REPLACED PACKINGS AT ENGINE NR 1 MANIFOLD BEARING, IAW 767 AMM 72-31-03, PENDING LEAK CHECK. PERFORMED ENGINE IDLE RUN, IAW 767- AMM 71-00-00, NO LEAKS NOTED.

Part: PCB — FAULTED (SHUTOFF VALVE) · airframe 100,338 hrs · 19,327 cycles

FAULT WARNING A RIGHT HPSOV CLOSE COMMAND WAS NOT DETECTED. THE BLEED AIR CONTROL CARD DID NOT GENERATE A 28 VCD. 2.5 SEC HPSOV CLOSE SIGNAL. THIS CONDITION WILL NORMALLY OCCUR WHEN THE BLEED SWITCH IS PLACED IN THE OFF (BAR HIDDEN) POSITION. REMOVED/REPLACED RT BLEED AIR CTL CARD M860, PER AMM 36-11-12/401. OPERATIONS CHECK RT BLEED AIR SUPPLY SYSTEM OK, IAW AMM 36-11-00.

Part: ROD — MISSING (ACCESS PANEL) · airframe 100,338 hrs · 19,327 cycles

NR 1 ENGINE AFT STRUT INBOARD HYDRAULIC ACCESS PANEL HOLD OPEN ROD IS MISSING. LOCATED AND INSTALLED NEW HOLD OPEN ROD AT NR 1 ENGINE AFT STRUT INBOARD ACCESS PANEL DOOR, PER B767-300 AMM 20-11-00-910-802.

Part: CONTROLLER — FAULTED (SHUTOFF VALVE) · airframe 100,338 hrs · 19,327 cycles

FAULT FAILURE RIGHT HPSOV DOES NOT OPEN WHEN COMMAND. THE HPSOV REMAINS CLOSED WHEN THE HPC CONTROL LINE PRESSURE EXCEEDS .14 PSIG. ENGINE SPEED MUST ALSO EXCEED 50% N2 BEFORE A FAULT WILL BE DETECTED. REMOVED/REPLACED HPSOV CONTROLLER, IAW AMM 36-11-08, NO LEAKS NOTED. PENDING OPERATIONS CHECK. PERFORMED OPERATIONS/LEAK CHECK, IAW 767-AMM 36-11-08. OPERATIONS CHECK NORMAL, NO LEAKS NOTED.

Part: ROD — DAMAGED (NR 2 NACELLE) · airframe 100,338 hrs · 19,327 cycles

NR 2 ENGINE AFT STRUT INBOARD HYDRAULIC ACCESS PANEL HOLD OPEN ROD DAMAGED. REMOVED AND REPLACED DAMAGED HOLD OPEN ROD AT NR 2 ENGINE AFT STRUT INBOARD SIDE ACCESS PANEL, PER B767-300 AMM 20-11-00-910-802.

Part: ENGINE — DAMAGED (NR 1) · airframe 100,338 hrs · 19,327 cycles

NR 1 ENGINE REQUIRES TO REMOVE BLADES FOR FACILITATE REPAIR AND RE-INSTALL AS REQUIRED. REMOVED NR 1 ENGINE BLADES 8EA ,IAW B767 AMM 72-31-02. RE-INSTALLED 8 BLADES, AS PER AMM 72-31-02 ON ENGINE NR 1. PENDING RE-TORQUE POST ENGINE RUN. PERFORMED SPINNER RE-TORQUE POST ENGINE RUN UP, IAW AMM 72-31-02. PERFORMED MPA AS REQUIRED, IAW AMM 71-00-00 MAX VIB 1.5 UNITS.

Part: LINER — DELAMINATED (NR 1 INLET) · airframe 100,338 hrs · 19,327 cycles

NR 1 ENGINE INLET AT POSITION 4 O'CLOCK ACOUSTIC PANEL FOUND DELAMINATED. REMOVED AND REPLACED DAMAGED ACOUSTIC PANEL LINER AT NR 1 ENGINE INLET AT POSITION 4 O'CLOCK, PER B767-300 AMM 72-33-01-004-001-H00 AMM 72-33-01-004-011-H00.

Part: CHANNEL — DAMAGED (NR 1 NACELLE) · airframe 100,338 hrs · 19,327 cycles

ENGINE PYLON NR 1 AND NR 2 INBOARD AND OUTBOARD DOORS HOLD OPEN RODS CHANNEL DAMAGED. REMOVED AND REPLACED 4 EA DAMAGED CHANNEL AT ENGINE PYLON NR 1 AND NR 2 INBOARD AND OUTBOARD DOORS BY HOLD OPEN ROD, PER B767-300 SRM 51-40-02-0G-0.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 100,338 hrs · 19,327 cycles

L2 DOOR EMERGENCY LIGHT INOPERABLE. RELAMPED L2 DOOR EMERGENCY LIGHT. OPERATIONS CHECK OK, IAW AMM 33-51-03.

Part: OXYGEN BOX — FAULTED (COCKPIT) · airframe 100,338 hrs · 19,327 cycles

CENTER OBSERVER'S OXYGEN BOX RESET SWITCH DOES NOT RESET. REMOVED AND REPLACED CENTER OBSERVER'S OXYGEN BOX, IAW 767-300 AMM 35-11-51. OPERATIONS CHECK GOOD.

Part: SWITCH — FAILED (EMERGENCY LIGHTS) · airframe 100,338 hrs · 19,327 cycles

EMERGENCY LIGHT SWITCH INOPERABLE AT FLIGHT ATTENDANT'S PANEL BEHIND R3 DOOR. REMOVED & REPLACED P-22 "EMERGENCY LIGHT" SWITCH, PER W/D 33-51-11 AND SWPM 20-80-13. EMERGENCY LIGHT SYSTEM OPERATIONS CHECK OK, PER AMM 33-51-00/501.

Part: GASKET — LEAKING (FUEL/OIL COOLER) · airframe 100,338 hrs · 19,327 cycles

NR 2 ENGINE FUEL LEAK IN IDG FUEL/OIL COOLER LOCATED IN PORT OF FUEL IN. REMOVED AND REPLACED NR 2 ENGINE IDG FUEL/OIL HEAT EXCHANGER "FUEL IN " TUBE GASKET, IAW AMM 24-11-10 PENDING LEAK CHECK. ACCOMPLISHED ENGINE IDLE RUN, IAW 767 AMM 71-00-00, NO LEAKS NOTED.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 100,289 hrs · 19,314 cycles

EMERGENCY AISLE LIGHT IS OUT ABOVE SEAT NR 27 AC. REMOVED AND REPLACED AISLE EMERGENCY LIGHT LAMP. OPERATIONS CHECKED OKAY, IAW AMM 33-51-05.

Part: ACOUSTIC LINER — DAMAGED (RT ENGINE) · airframe 100,246 hrs · 19,303 cycles

RT ENGINE ACOUSTIC PANEL AFT OF FAN BLADE AT 08:00 POSITION HAS DAMAGE 18" L X 6" W, AT 11:00 POSITION HAS DAMAGE 12" L X 3.5" W, AT 04:00 POSITION HAS DAMAGE 7" L X 8" W, AT 02:00 POSITION HAS DAMAGE 3.5" L X 8" W, AT 06:00 POSITION HAS DAMAGE 9.5" L X 3" W. DAMAGE IS OK, PER AMM 72-00-00-993-846-H00 TABLE 642 OK FOR 10FC OR 100 FH. ENTERED INTO NON-MELS 138323, 138324, 138325, 138327, AND 138328. REF NON-MEL NR 138323. REMOVED AND REPLACED ACOUSTICAL LINER SEGMENT AT POS 8 O'CLOCK, PER AMM 72-33-01. OPERATIONS CHECK GOOD. ENGINE NR 2, MCC NOTIFIED, THIS CLEARS NON MEL 138323. P/N OFF 1753M39G03. S/N OFF-3AB69GC1. REMOVED AND REPLACED ACOUSTICAL LINER SEGMENT AT 11 O'CLOCK POS ENGINE NR 2, PER AMM 72-33-01. OPERATIONS CHECK GOOD. MCC NOTIFIED, THIS CLEARS NON MEL 138234. P/N OFF 1753M39G03. S/N OFF 3AB6CRAT. ITEM 12 / BWI - REF NON-MEL 138325 -&NBSP;REMOVED AND REPLACED ACOUSTICAL LINER SEGMENT ENG #2 PER AMM 72-33-01. OPS CK GOOD.&NBSP;MCC NOTIFIED, THIS CLEARS NON MEL 138325. P/N OFF - 1753M39G03. S/N OFF- 3AB60GCT.</P><P>29NOV20 / LOG 1194276 / ITEM 13 / BWI - REF NON-MEL 138327 - REMOVED AND REPLACED ACOUSTICAL LINER SEGMENT ON ENG #2 AT 2 O'CLOCK POS PER AMM 72-33-01.&NBSP;OPS CK GOOD, MCC NOTIFIED.&NBSP;THIS CLEARS NON MEL 138327. P/N OFF - 1753M39G03. S/N OFF - 3AB6D6AG.</P><P>ITEM 14 / BWI - REF NON-MEL 138328. REMOVED AND REPLACED ACOUSTICAL LINER SEGMENT ON ENGINE NR 2 AT 8 O'CLOCK POS, PER AMM 72-33-01. OPERATIONS CHECK GOOD. MCC NOTIFIED, THIS CLEARS NON MEL NR 138328.

Part: PRESSURE SWITCH — MALFUNCTIONED (APU FUEL) · airframe 100,246 hrs · 19,303 cycles

APU DC PUMP ALWAYS ON PER MX MESSAGE. TRANSFERRED TO DMI 138340, IAW MEL 28-25-01, CAT C. REMOVED AND REPLACED DC PUMP FUEL PRESSURE SWITCH, PER AMM 28-25-03. MESSAGE CLEARED,

Part: MONITOR — MALFUNCTIONED (E/E COOLING) · airframe 100,226 hrs · 19,299 cycles

E/E COOLING MONITOR "EADI-L EHSI-L VOR-L" ALL SHOW ZERO AIRFLOW. PERFORMED OPERATIONS TEST OF E/E COOLING MONITOR, IAW AMM 21-58-34. NO FAULTS NOTED, ALL INDICATOR BALLS CAME IN VIEW FOR MORE THAN 15 SEC. SYSTEM OK AT THIS TIME.

Part: ANTI-ICE VALVE — FAILED (RT ENGINE) · airframe 100,224 hrs · 19,298 cycles

RT ENGINE ANTI-ICE EICAS MESSAGE INDICATED IN FLIGHT. REMOVED AND REPLACED RT ENGINE ANTI ICE VALVE, IAW B767 AMM 30-21-00. LEAK CHECK NOTED. OPERATIONS CHECK GOOD.

Part: PLENUM — DAMAGED (HEAT EXCHANGER) · airframe 100,208 hrs · 19,296 cycles

DURING REMOVAL FOUND PRIMARY HEAT EXCHANGER PLENUM DAMAGED. REMOVED AND REPLACED PRIMARY HEAT EXCHANGER PLENUM, AS PER AMM 21-51-02-404-019.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 100,100 hrs · 19,269 cycles

CEILING (AISLE) EMERGENCY LIGHT INOPERATIVE ABOVE 38AC. REMOVED AND REPLACED AISLE CEILING EMERGENCY LIGHT LAMP. OPERATIONS CHECKS GOOD, IAW AMM 33-51-05.

Part: LAMP — INOPERATIVE (EXTERIOR LIGHT) · airframe 100,100 hrs · 19,269 cycles

LEFT EXTERIOR BODY MOUNTED SLIDE EMERGENCY LIGHT IS INOPERATIVE, MOST AFT FROM THE OVERWING EXIT DOORS. REMOVED AND REPLACED LEFT HANDSIDE BODY MOUNTED AFT SLIDE LIGHT LAMP. OPERATIONS CHECKS GOOD, IAW AMM 33-51-00.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 100,100 hrs · 19,269 cycles

DOOR R4 EXTERIOR EMERGENCY LIGHT IS OUT. REMOVED AND REPLACED DOOR R4 EXTERIOR LIGHT. OPERATIONS CHECKS GOOD, IAW AMM 33-51-00.

Part: SKIN — DELAMINATED (RT NACELLE) · airframe 100,064 hrs · 19,259 cycles

RIGHT ENGINE INBOARD IN COWL HAS DELAMINATED SKIN (UNDERNEATH) ABOUT 52 INCHES BY 17 INCHES. REMOVED AND REPLACED RT ENGINE INBOARD FAN COWL, PER AMM 71-11-04/401. LATCHES ADJUSTED, PER AMM 71-11-05. OPERATIONS CHECK OK.

Part: CONTACTOR — DIRTY (RT BLEED) · airframe 100,025 hrs · 19,249 cycles

RT ENGINE BLEED OFF EICAS MESSAGE AFTER ENGINE START. TRANSFERRED TO MEL 36-11-01-02A MDDR 136530 CAT C PLACARD INSTALLED. MAINT PROCEDURES C/W DISPATCH NOTED DPP 1441Z. CLEANED CONTACT AND RE-SEATED M840 RT ENGINE BLEED. GROUND OPERATIONS CHECK COMPLIED WITH ON ENGINE RUN, IAW 36-11-00. THIS CLEARS MDDR 134530. PLACARD REMOVED. DISP GTC 06:43Z.

Part: CONTROLLER — MALFUNCTIONED (A/C PACK TEMP) · airframe 99,764 hrs · 19,193 cycles

RIGHT HAND PACK TEMP CONTROL INOPERABLE IN AUTO. TRANSFERED TO MDDR 134982, IAW MEL 21-51-03-01, CAT C. CONTROLLER FAULT ON BTIE TEST FOR RIGHT HAND PACK TEMP CONTROLLER. REMOVED AND REPLACED RT PACK TEMP CONTROLLER, IAW AMM 21-51-14. OPERATIONS TESTED GOOD, NO FAULTS. DMI 134982 CLEARED. PLACARD REMOVED.

Part: FUEL LINE — LEAKING (RT ENGINE) · airframe 99,721 hrs · 19,184 cycles

ON POST FLIGHT WALK AROUND FOUND FUEL LEAK RT ENGINE. ON RIGHT ENG RETORQUED & "FUEL IN" TUBE ON IDG FUEL OIL HEAT EXCHANGER, IAW 24-11-10. RAN ENG, PER 71-00-00, LEAK CK GOOD.

Part: SEALANT — DETERIORATED (THRUST REVERSER) · airframe 99,688 hrs · 19,177 cycles

NR 2 ENGINE INBOARD AND OUTBOARD T/R COWLING INNER SIDE PROTECTOR HEAT SEALANT IS DETERIORATED, MISSING IN SEVERAL AREAS. PREPARED, CLEANED, AND REPAIRED PROTECTOR HEAT SEALANT NR 2 ENG INBOARD AND OUTBOARD T/R COWLING INNER SIDE, PER B767-300 AMM 78-31-00-308-072-H00.

Part: SENSOR — MALFUNCTIONED (LT FAN AIR TEMP) · airframe 99,688 hrs · 19,177 cycles

LEFT FATS DOES NOT COMMAND THE FAV CLOSED. FATS ON ORDER P/N 773384-5. REMOVED LEFT ENG FAN AIR TEMP SENSOR (FATS), IAW AMM 36-11-17. INSTALLED LEFT ENG FAN AIR TEMP SENSOR, IAW AMM 36-11-17. OPS TEST PENDING. OPS CHK FOUND NORMAL POST ENG RUN UP.

Part: VALVE — MALFUNCTIONED (PNEUMATIC SYS) · airframe 99,688 hrs · 19,177 cycles

RIGHT FATS DOES NOT COMMAND THE FAV OPEN. T/S NR/ 00019; FAV ON ORDER P/N 773855, REF NR 19 FOR FAMV.

Part: MODULATING VALVE — MALFUNCTIONED (RIGHT) · airframe 99,688 hrs · 19,177 cycles

RIGHT FAV DOES NOT CLOSE WHEN COMMANDED. FAV P/N 773855-6 ON ORDER. RT ENG T/S W/D 36-11-21. FAV TERMINAL STUDS BROKEN. FAV ON ORDER. REMOVED AND REPLACED NR 2 ENGINE FAN AIR MODULATING VALVE, IAW AMM 36-11-16. OPS CHECK FOUND NORMAL POST ENG RUN UP.

Part: INDICATION SYS — MALFUNCTIONED (LT HPSOV) · airframe 99,688 hrs · 19,177 cycles

LEFT HPSOV CLOSED AND OPEN SWITCHES DISAGREE. CHECKED TERMINAL CONDITION AT HPSOV, FOUND OK. CHECKED WIRING, PER WDM 36-11-61. WIRING CHECKED OK. PERFORMED OPERATION TEST AIR SUPPLY DISTRIBUTION SYS OK, PER AMM 36-11-00-715. ENG LEFT RUN UP OK, NO MSG, PER AMM 71-00-00.

Part: MEDICAL KIT — INADEQUATE (CABIN) · airframe 99,675 hrs · 19,174 cycles

ONE EMK IS INCOMPLETE, 2 SERVICEABLE EMK'S ON AIRCRAFT,EMERGENCY MEDICAL EQUIPMENT, EMERGENCY MEDICAL KIT (EMK). TRANSFERRED TO MDDR 134412, IAW MEL 25-64-01-02B CAT D. REMOVED AND REPLACED AFT EMK, IAW 25-60-00. THIS CLEARS MDDR 134412. PLACARD REMOVED.

Part: BLADE — CHIPPED (NR 2 ENGINE) · airframe 99,640 hrs · 19,167 cycles

NR 2 ENG NR 6 BLADE LEADING ENGINE IS CHIPPED. PERFORMED BLEND REPAIR ON RT ENG NR 6 BLADE, IAW AMM 72-31-02. NO FURTHER DEFECTS NOTED.

Part: RADAR — UNKNOWN (WX SYSTEM) · airframe 99,525 hrs · 19,144 cycles

DURING FLIGHT RADAR CONSISTENTLY FAILED TO PAINT SIGNIFICANT CONVECTIVE ACTIVITY. PERFORMED OPERATIONAL TEST OF SYS 1 AND SYS 2 OF WTX RADAR. OPS CHECKED GOOD IAW AMM 34-43-00.

Part: LIGHT — INOPERATIVE (SPAR VALVE) · airframe 99,525 hrs · 19,144 cycles

LEFT SPAR VALVE LIGHT INOPERABLE. DEFERRED LT FUEL SPAR VALVE INDICATION, MDDR 133512 IAW MEL 28-40-02 (M) PROCEDURE COMPLIED WITH, VALVE OPERATED NORMAL. CLEARED LEFT SPAR VALVE, CAT C VALVE SWITCH OPERATIONS CK C/W IAW AMM 28-22-11. THIS CLEARS MDDR 133512. PLACARD REMOVED.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 99,525 hrs · 19,144 cycles

CEILING EMG LIGHTS LEFT SIDE INOP FROM ROWS 1-8(<P>REMOVED AND REPLACED BATTERY PACK ASSY FOR LEFT CEILING LIGHTSIAW B767 AMM 33-51-07. OPS CHECK NORMAL IAW 33-51-00</P>)

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 99,525 hrs · 19,144 cycles

AISLE MOUNTED EMERGENCY LIGHT IS INOPERATIVE AT SEAT 24 ABC(<P>REMOVED AND REPLACED LAMP OPS CHECKS GOOD IAW AMM 33-51-00</P>)

Part: RELAY — MALFUNCTIONED (APU FUEL PUMP) · airframe 99,525 hrs · 19,144 cycles

DC APU FUEL PUMP ON AT ALL TIMES(<P>RESET DC PUMP CONTROL CB AND RESEATED DC PUMP RELAY K191. OPS CHECKED GOOD IAW B767AMM 28-25-00</P>)

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 99,525 hrs · 19,144 cycles

RIGHT AFT BODY EM EXIT LIGHT INOP(<P>REMOVED AND REPLACED RT AFT BODY EM EXIT LIGHT IAW B767 AMM 33-51-06. OPS CHECK NORMAL</P>)

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 99,500 hrs · 191,139 cycles

EME LIGHT AT R2 &AMP; L2 EXITS INOP.(<P>RECHARGED BATTERY, OPS CK C/W IAW 33-16-00</P>)

Part: SENSOR — MALFUNCTIONED (A/C PACK TEMP) · airframe 99,484 hrs · 19,136 cycles

RT PACK PRIMARY HEAT EXCHANGE TEMP SENSOR DATA MISSING REMOVED AND REPLACED TEMP SENSOR IAW B767 AMM 21-52-08, OPS CHECKED GOOD

Part: CONTROLLER — MALFUNCTIONED (RT A/C PACK) · airframe 99,420 hrs · 19,121 cycles

R PACK TEMP REMOVED AND REPLACED RT TEMP SENSOR TS 199 AND STBY SENSOR IAW 21-51-08 (OFF PART: PN624014-2, NSN). NO HELP. TRANSFERRED TO MEL 21-53-03-01, AUTO MODE, REMOVED AND REPLACED RH PACK TCV IAW AMM 21-51-12 AND REPLACED RT PACK CONTROLLER IAW AMM 21-51-00 OPS CHECK GOOD. REPLACED RH PACK PRIMARY HEAT EXCHANGER TEMP SENSOR DUE DATA MISSING; OPS CHECK OK IAW AMM 21-52-08.

Part: WARNING MESSAGE — FALSE ACTIVATION (RT A/C PACK) · airframe 99,330 hrs · 19,103 cycles

RT PACK TEMP MESSAGE. PERFORMED A PACK BITE IAW AMM 21-51-844. CLEARED MESSAGE. OPS CHECKED OK.

Part: UNKNOWN — NOISE (AFT GALLEY) · airframe 99,250 hrs · 19,085 cycles

LOUD NOISE IN AFT GALLEY WITH APU AIR SELECTED ON(<P>PERFORMED DVI AND APU BLEED LEAK TEST IAW AMM 36-11-00, NO DEFECTS. REMOVED, INSPECTED, REINSTALLED APU BLEED CHECK VALVE IAW AMM 36-11-11, NO DEFECTS. INSPECTED APU AIR SUPPLY VALVE AND OPS TEST IAW AMM 36-11-10, NO DEFECTS. OPS CHECKED APU AIR ON AND OFF SEVERAL TIMES, COULD NOT DUPLICATE LOUD NOISE, APU BLEED AIR OK PER AMM 49-52-00.<BR /></P>)

Part: VALVE — ILLUMINATED (CABIN TEMP) · airframe 99,169 hrs · 19,066 cycles

EICAS FOR FWD CABIN TEMP FWD CABIN CONTROL INOPERATIVE. R & R TRIM AIR MODULATING VALVE IAW AMM 21-61-07. OPS CHECKED GOOD.

Part: OIL SYSTEM — LOW (APU) · airframe 99,129 hrs · 19,055 cycles

APU AUTO SHUT DOWN IN FLT. "LOW" OIL QTY INDICATED ON EICAS STATUS. SERVICED APU 1.0 QT. PERFORMED EXTERNAL LEAK CHECK. NO LEAKS NOTED. OPS CHECKED GOOD IAW 49-41-81.

Part: STARTER — MALFUNCTIONED (RT ENGINE) · airframe 99,062 hrs · 19,040 cycles

RIGHT ENGINE STARTER CAUTION MESSAGES ON ENG START. NO N2 RISE NOTED. REMOVED AND REPLACED RT ENGINE STARTER IAW AMM 80-11-1 OPS CHECK OK.

Part: MASK — LEAKING (COCKPIT) · airframe 99,014 hrs · 19,031 cycles

COCKPIT 2ND OBS OXYGEN MASK HARNESS LEAKING. REPLACED 2ND OBS O2 MASK IAW MM 35-11-51. PERFORMED SYSTEM TEST IAW MM 35-51-00. OPS CHECK GOOD.

Part: MASK — DEFECTIVE (COCKPIT) · airframe 99,014 hrs · 19,031 cycles

COCKPIT 1ST OBS MASK HARNESS NO INFLATE. REMOVED AND REPLACED 1ST OBS MASK PER AMM 35-11-51 AND PERFORMED SYSTEM TEST AMM 35-51-00. OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 99,014 hrs · 19,031 cycles

L1 DOOR EXTERIOR LIGHT INOP. RELAMPED L1 DOOR EXTERIOR EMERGENCY LIGHT. OPS CHECK OK. PER AMM 33-51-03.

Part: APU — MALFUNCTIONED · airframe 98,888 hrs · 18,998 cycles

ON ARRIVAL, APU DID NOT START. PERFORMED A BITE, NO FAULTS NOTED. APU OIL QTY SHOWED ZERO. AFTER RESET APU OIL SHOWED FULL. STARTED NORMAL IAW AMM 45-41-00.

Part: ECU — MALFUNCTIONED (APU) · airframe 98,818 hrs · 18,982 cycles

APU WILL NOT START ON THE GROUND. RESET ECU, OPS CK COMPLIED WITH IAW 49-60-00.

Part: TUBE — MALFUNCTIONED (AC BAY) · airframe 98,784 hrs · 18,974 cycles

COCKPIT TEMPS EXTREMELY HOT WITH PACKS MAX COLD. REMOVED AND REPLACED REHEATER INLET TUBE IAW AMM CH 21-51-21. OPERATIONAL CHECK GOOD.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 98,707 hrs · 18,956 cycles

AFTER PRE DEPARTURE INSPECTION, FOUND LT AND RT EMERGENCY EXIT LIGHTED SIGNS INOP(<P>REMOVED AND REPLACED EMR LIGHT PWR SUPPLY M1209 AND OPS CHECK OK IAW MM 33-51-00.</P>)

Part: ENGINE — LEAKING (RIGHT) · airframe 98,642 hrs · 18,941 cycles

DURING WALK AROUND, AFTER AIRCRAFT SITTING FOR 4 HOURS, FOUND PUDDLE OF OIL UNDERNEATH RIGHT ENGINE.(<P>RIGHT ENGINE REMOVED AND REPLACED. ACCOMPLISHED IAW ATLAS W/C A-71-999-04-02. ALL OPS CHK NORMAL.</P>)

Part: INDICATOR — FAILED (COCKPIT) · airframe 98,642 hrs · 18,941 cycles

DURING OP CHECK OF SEI THE SEI FAILED(<P>REMOVED AND REPLACED SEI (STAND BY ENGINE INDICATOR) AS PER B767-300 AMM 77-41-00 AND CHECKS GOOD.</P>)

Part: SOLENOID VALVE — FAULTY (FUEL SYSTEM) · airframe 98,624 hrs · 18,936 cycles

AFTER LEFT ENGINE SHUTDOWN INITIATED FUEL VALVE LEFT SIDE DID NOT CLOSE FOR FORTY SECONDS.(<P>REMOVED AND REPLACED LEFT ENGINE HP FUEL SHUTOFF SOLENOID VALVE IAW AMM 73-21-23. OPS CHECK GOOD.</P>)

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 98,618 hrs · 18,935 cycles

APU FAULT ON LANDING.(<P>FOLLOWED FAULT TREE FIM 49-11 FT 987 - FOR APU ECU BITE - NO DATA DISPLAYED.</P><P>APU OPERATING NORMALLY AT THIS TIME IAW AMM 49-11-00.</P>)

Part: OIL SYSTEM — LOW (APU) · airframe 98,583 hrs · 18,928 cycles

APU FAULT UPON LANDING(<P>INSPECTED APU SIGHT GLASS AND FOUND TO BE LOW. SERVICED APU WITH 02 QUARTS OF OIL IAW B767 AMM 12-13-04. OPS CHECK GOOD. APU STARTED FIRST ATTEMPT. NO DEFECTS NOTED.</P>)

Part: CONTROL VALVE — FAILED (AC BAY) · airframe 98,593 hrs · 18,930 cycles

RH PACK TEMP CONTROL VALVE FAILED ON THE BITE CHECK.(<P>REMOVED AND REPLACED RH PACK TEMP CONTROL VALVE. OPS CHECK OK IAW AMM 21-51-12.</P>)

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 98,548 hrs · 18,921 cycles

APU FAULT ON LANDING.(<P>PERFORMED APU BITE PER FIM 49-11 FT 987, NO FAULTS NOTED AT THIS TIME. OPS CHECK GOOD PER B767 AMM 49-11-00.</P>)

Part: SLIDE RAFT — NOT REPORTED (L1 DOOR) · airframe 98,535 hrs · 18,918 cycles

L1 DOOR SLIDE/RAFT REPLACEMENT REQUIRED.(<P>REMOVED AND REPLACED SLIDE/RAFT IAW AMM 25-66-01 EXP DATE 23MAY22.</P>)

Part: MEDICAL KIT — NOT REPORTED (CABIN) · airframe 98,534 hrs · 18,918 cycles

EMK POS 01 LH FWD REQUIRES REPLACEMENT(<P>REMOVED AND REPLACED EMK POS 01 LH FWD IAW AMM 25-64-03.</P>)

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 98,502 hrs · 18,910 cycles

EICAS MESSAGE "R PACK TEMP"(<P>PERFORMED R PACK BITE TEST OF CONTROLLER, NO DEFECTS NOTED. OPS CHECKED GOOD. ALL SYSTEMS OK. REF B767 FIM 21-51 FT 803.</P>)

Part: TRANSCEIVER — MALFUNCTIONED (WEATHER RADAR) · airframe 98,471 hrs · 18,903 cycles

RADAR SYSTEM 1 WEATHER FAIL MULTIPLE TIMES(<P>REMOVED AND REPLACED TRANSCEIVER PER AMM 34-43-01. OPS CHECK NORMAL.</P>)

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 98,413 hrs · 18,891 cycles

AFTER TAKEOFF "WXR FAIL" #1 RADAR. ASSOCIATED "WRX SYS" STATUS MESSAGE.(<P>PERFORMED BITE CHECK ON WXR IAW MM 34-43-00. NO DEFECTS NOTED.</P>)

Part: PUMP — MALFUNCTIONED (FUEL SYSTEM) · airframe 98,393 hrs · 18,886 cycles

RT AFT MAIN BOOST PUMP INOP.(<P>TRANSFERRED TO MEL 28-22-01, MDDR 126137, CAT C, MBCB 01APR20. PLACARD INSTALLED. MAINT PROCEDURES C/W, AC RESTRICTED TO ETOPS 120.</P><P>LP&NBSP;<SPAN>1138686:&NBSP;</SPAN><SPAN>REMOVED AND REPLACED RH AFT MAIN BOOST PUMP ASSY IAW AMM 28-22-03. OPS CK GOOD, DMI 126137 CLEARED, PLACARD REMOVED.</P><P>LP&NBSP;1138688:&NBSP;"RH AFT FUEL PUMP" EICAS MSG, RE-OPENED DMI 126137,&NBSP; DDG 28-22-01, CAT 'C'.&NBSP;</P><P>LP&NBSP;1138699: T/S PER FIM 28-22 TREE 812 AND AMM 28-22-00-210-501. REMOVED AND REPLACED BOOST PUMP IAW AMM 28-22-03. THIS CLEARS MDDR 126137.&NBSP;<BR /></P>)

Part: HOOK AND LOOP — DEFECTIVE (COCKPIT) · airframe 98,315 hrs · 18,871 cycles

COCKPIT SMOKE VISION SYS INOP (COCKPIT SMOKE VISION SYSTEM (CSVS) (STC ST00731LA)).(<P>TRANSFERRED TO MDDR #125643 PER MEL 25-63-06, CAT 'D', DUE 09JUL20, PLACARD INSTALLED. DISPATCH&NBSP; NOTED.</P><P><SPAN>LP 1226536:&NBSP;</SPAN>CLEANED &AMP; INSTALLED NEW VELCRO AT CA &AMP; FO GLARESHIELD AREA&NBSP; PER AMM 20-30-01-992-001. THIS CLEARS MDDR 125643.</P>)

Part: OXYGEN MASK — LEAKING (OBSERVERS) · airframe 98,161 hrs · 18,840 cycles

1ST OBSERVER SEAT OXYGEN MASK LEAKING.(<P>DEFERRED&NBSP;IAW DDG 25-11-02-01A, MDDR 124970, CAT "A".</P><P>LP&NBSP;1226318 - ITEM M8: REMOVED AND REPLACED 1ST OBSERVER OXYGEN MASK IAW AMM 35-11-00. NO DEFECTS NOTED. STOWED MASK IAW AMM 35-11-51. THIS CLEARS MDDR 124970.</P>)

Part: ACTUATOR — INOPERATIVE (RT A/C PACK) · airframe 98,151 hrs · 18,838 cycles

RIGHT PACK TEMP EICAS MESSAGE ON TAKE OFF ROLL.(<P>DEFERRED IAW MEL 21-51-03-01, MDDR 124975, CAT C, DUE 03MAR20, PLACARD INSTALLED.</P><P>LP 1226318: PERFORMED OPERATION TEST AND BITE CHECK OF CONTROLLER IAW AMM 21-61-00. NO MESSAGE NOTED, NO DEFECT NOTED. THIS CLEARS MDDR 124975.</P><P>LP&NBSP;1226322: RE-OPENED MDDR 124975, CAT 'C', DUE 3MAR20. PLACARD INSTALLED.</P><P>LP 1226329: REMOVED AND REPLACED RIGHT PACK DOOR INLET DOOR ACTUATOR IAW B767 AMM 21-53-03/401. OPS CHECK NORMAL IAW AMM 21-53-00/001. THIS CLEARS MDDR 124975.</P>)

Part: OXYGEN BOTTLE — INOPERATIVE (CABIN) · airframe 98,124 hrs · 18,832 cycles

ONE PORTABLE OXYGEN DISPENSING UNIT INOP AT MID CABIN BULK HEAD. (PORTABLE OXYGEN DISPENSING UNITS (BOTTLE AND MASK)). (REF LOG PAGE 1113589: REF MDDR 124817 PORTABLE O2 MASK MISSING)(<P>TRANSFERRED TO MDDR 124817 IAW MEL 35-31-01, CAT 'D'.&NBSP;</P><P>LP&NBSP;<SPAN>1113589:&NBSP;</SPAN><SPAN>INSTALLED MISSING PORTABLE BOTTLE O2 MASK IAW N645GT LOPA. THIS CLEARS DMI 124817. MX PROCEDURES C/W. PLACARD REMOVED.</SPAN></P>)

Part: VALVE — MALFUNCTIONED (DUCT PRESSURE) · airframe 98,090 hrs · 18,827 cycles

RIGHT DUCT PRESSURE FLUCTUATED DURING TAKE OFF AND CLIMBED WITH HIGH THRUST SETTINGS.(<P>REMOVED AND REPLACED RT ENG PRV IAW 36-11-18-004-001-001. OPS CHECK GOOD.<BR /></P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (EQUIP COOLING) · airframe 98,087 hrs · 18,825 cycles

AFTER TOUCHDOWN AT RMS, EICAS MSG, FWD EQPT COOLING.(<P>TROUBLESHOT SYSTEM IAW SSM 21-58-01 DIAGRAM AND OPS TEST IAW AMM 21-58-00, OPS CHECK TESTS NORMAL AT THIS TIME.<BR /></P>)

Part: UNKNOWN — UNKNOWN (DUCT PRESSURE) · airframe 98,087 hrs · 18,825 cycles

RIGHT DUCT PRESSURE FLUCTUATING DURING ENG START AND ALL PHASES OF FLIGHT.(<P>PERFORMED OPS TEST OF AIR SUPPLY CONTROL SYSTEM IAW AMM 36-23-00, BIT OPS TEST PASSED. COULD NOT DUPLICATE FAULTS ON GROUND.<BR /></P>)

Part: RELAY — FAILED (EXHAUST FAN) · airframe 98,065 hrs · 18,821 cycles

FOUND EQUIPMENT COOLING EICAS MESSAGE WITH NO COOLING LIGHT WERE ILLUMINATED UPON LANDING.(<P>REPLACED CENTER FAN CONTROL CARD, EXHAUST FAN CONTROL RELAY K1009 IAW FIM TASK 2158 TREE 905 AND EQUIPMENT COOLING IND. CARD PER MCC. DOESN'T HELP, T/S CONTINUES, THE OLD CARDS INSTALLED BACK ON THE AIRCRAFT.</P><P>REF LOG PAGE 1226298 - ITEM M13: REMOVED AND REPLACED K2091 RELAY PER WDM 24-15-72. OPS CHECK GOOD.</P>)

Part: SENSOR — MALFUNCTIONED (NR 1 BLEED) · airframe 98,042 hrs · 18,817 cycles

#1 ENG BLEED OFF EICAS CAUTION DURING TAKEOFF AND CLIMB PORTION OF FLIGHT. ITEM M2: L DUCT PRESSURE INDICATED 10-15 PSI FOR DURATION.(<P>TRANSFER TO MDDR #124368 IAW MEL 36-12-02-01, CAT 'C', DUE DATE 16FEB20. ALL MX PROCEDURES C/W, ETOPS 120.</P><P>LP 1226297&NBSP;- M12: REMOVED AND REPLACED FAN AIR TEMP SENSOR AIR FILTER PER AMM 36-11-17 (OFF PART: PN&NBSP;<SPAN>727604-4, NSN</SPAN><SPAN>). OPS AND LEAK CHECK GOOD. THIS CLEARS MDDR 124368.</SPAN></P><P><SPAN>LP&NBSP;</SPAN><SPAN>1226301:&NBSP;</SPAN><SPAN>REOPENED MDDR 124368 AS PER MEL 36-12-02-01, CAT C, DUE DATE 16FEB20. ALL MX PROCEDURES COMPLIED WITH.</SPAN></P><P><SPAN>LP 1113575:&NBSP;</SPAN><SPAN>REMOVED AND REPLACED FAN AIR TEMP SENSOR IAW 36-11-17 AND OPS CHK GOOD. THIS CLEARS MDDR 124368.

Part: WARNING LIGHT — FALSE ACTIVATION (LT ENGINE BLEED) · airframe 98,048 hrs · 18,818 cycles

MOMENTARY AND INTERMITTENT EICAS L ENG BLEED OFF MESSAGE. EXTINGUISHED AFTER APPROX 15 SEC. LT PRESSURE 12PSI, RT PRESSURE 30PSI.(<P>PERFORMED BLEED CONTROL SUPPLY SYSTEM BIT TEST IAW AMM 36-26-00. NO FAULTS NOTED AT THIS TIME. SYSTEM TESTS OK.</P>)

Part: HOUSING — WORN (CARGO DOOR) · airframe 98,031 hrs · 18,815 cycles

BULK CARGO DOOR OUTER SKIN HOUSING WITH WEAR.(<P>THE DAMAGED HOUSING WAS REPLACED IN ACCORDANCE WITH DRAWING 146T6301 AND CMM 52-36-16 PAR. 4F REV. 5 30MAY11.</P>)

Part: STRAP — CORRODED (BS 654) · airframe 98,031 hrs · 18,815 cycles

TWO CRACKS IN THE FWD CARGO COMPARTMENT STABILIZATION STRAP BETWEEN STA 654+110 / 654+121 AND / LBL 39.25.(<P>CRACKS WERE REPAIRED IN ACCORDANCE WITH SR 3-4611920191 AND SRM 53-30-51-01-1 DETAIL II.</P>)

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 98,048 hrs · 18,818 cycles

FLIGHT DECK EMERGENCY EXIT LIGHT INOPERATIVE.(<P>EMERGENCY EXIT LIGHT WAS REPLACED IAW AMM 33-51-01-402-030. TEST WAS SATISFACTORY.</P>)

Part: SKIN — CRACKED (RT WING) · airframe 98,031 hrs · 18,815 cycles

CRACK INDICATION ON THE RH WING, LOWER SKIN, AT OUTBOARD SEGMENT OF STRINGER L-9.5 / BETWEEN WING STATION 990.2 AND WING STATION 1046.2.(<P>CRACK WAS REPAIRED IN ACCORDANCE WITH EO 6757A088.</P>)

Part: SKIN — CORRODED (BS 654-676) · airframe 98,031 hrs · 18,815 cycles

BULGE ON FUSELAGE SKIN FORWARD OF BS 676 BETWEEN STRINGER S-35L / S-36L.(<P>BULGE WAS REPAIRED AT STA 654+121 / 676 BETWEEN STRINGER S-35 / S-36 IAW&NBSP;<SPAN>SRM 53-00-01-1A-1&NBSP;</SPAN><SPAN>TRE 6753334 AND FAA FORM 8100-9, REFERENCE ID: 202001150013-000301.</SPAN></P>)

Part: SKIN — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 98,031 hrs · 18,815 cycles

CORROSION DAMAGES WERE FOUND ON THE HORIZONTAL STABILIZER TOP SKIN, CENTER SECTION, BETWEEN RIB 1 TO 2 NEAR FWD EDGE 3 SPOTS OF CORROSION, BETWEEN RBL 13.83/41.50 AND STGR 9/10.(<P>REPAIR FOR CORROSION ON THE HORIZONTAL STABILIZER CENTER SECTION, UPPER SKIN, BETWEEN STGR 9/10 AND RBL 13.83/41.50 WAS PERFORMED, IAW SRM 51-10-01-1A-1 REV 112 15DEC19.</P>)

Part: VALVE — MALFUNCTIONED (FAN AIR) · airframe 98,031 hrs · 18,815 cycles

LEFT DUCT PRESSURE MODULATED FROM 0 PSI TO NORMAL @ 12,000 FT. LEFT DUCT INDICATED 0 PSI @ FL 230, 5 MIN LATER RECORDS TO 14 PSI (RIGHT INDICATED 34 PSI). EICAS MESSAGE LEFT ENGINE BLEED OFF WAS ALSO INTERMITTENT&NBSP;(<P>FAN AIR VALVE WAS REPLACED DURING C-CHECK FOR RELIABILITY. NEW FAV FAILED DURING TEST FLIGHT, BFS. ORIGINAL FAV INSTALLED BACK ON #1 ENGINE PER AMM 36-11-16/401. ASM CHECK CARRIED OUT WITH NO DEFECTS NOTED.</P>)

Part: TARGET — OUT OF ADJUST (FUEL DOOR) · airframe 97,904 hrs · 18,789 cycles

CENTER FUEL PUMPS DID NOT INHIBIT BEFORE ENGINE START. MX RESET FUELING DOOR.(<P>ADJUSTED TARGET ON FUELING DOOR IAW AMM 52-49-04 AND OPS CHECKED GOOD IAW AMM 28-22-00.</P>)

Part: LIGHT — INOPERATIVE (CABIN) · airframe 97,835 hrs · 18,775 cycles

ISLE EMERGENCY LIGHT OUT @ R2 LAV.(<P>REINSTALLED EMERGENCY LIGHT AND LENS PER AMM 33-51-10, OPS CHECK NORMAL.</P>)

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 97,767 hrs · 18,764 cycles

L4 AFT POSITION F/A FLASHLIGHT INOP.&NBSP;(<P>TRANSFERRED TO MDDR 120713 PER MEL 25-63-04A, CAT 'C', DUE DATE: 27-NOV-19. PLACARD INSTALLED.&NBSP;</P><P>LP 1114730 - M2: REMOVED AND REPLACED L/H AFT POSITION FLASHLIGHT BATTERY AND PERFORMED OPERATIONAL CHECK IAW AMM 25-64-00. OPS CHECK GOOD. THIS CLEARS MDDR 120713. DISPATCH NOTIFIED AND PLACARD REMOVED.</P>)

Part: ACTUATOR — MALFUNCTIONED (SPOILER OVERRIDE) · airframe 97,730 hrs · 18,759 cycles

PERFORMED SQUIB TEST, FOUND IT EMER ESCAPE LEFT LIGHT WOULD NOT TEST AFTER MAINTENANCE RELEASE OF AIRCRAFT.(<P>REMOVED AND REPLACED SPOILER OVERRIDE ACTUATOR IAW B767 AMM 25-65-20, OPS CHECKS GOOD.<BR /></P><P>LP 1114713 -&NBSP;M3:&NBSP;REMOVED AND REPLACED RIGHT OFF-WING ESCAPE SYSTEM EMERGENCY BATTERY PACK (M962). OPS CHECK GOOD IAW B767 AMM 25-65-17/401. OFF PART (PN: 2013-1A, SN: 55022).</P>)

Part: UNKNOWN — MALFUNCTIONED (APU) · airframe 97,666 hrs · 18,747 cycles

AFTER LANDING, APU DID NOT START, TWO ATTEMPTS.(<P>PERFORMED OPERATIONAL CHECK IAW AMM 49-60-00, APU STARTED, NO FAULTS NOTED.</P>)

Part: BLEED AIR SYS — FLUCTUATES (APU) · airframe 97,572 hrs · 18,733 cycles

APU BLEED PRESSURE FLUCTUATED BETWEEN 15 AND 22 PSI PRIOR TO START WITH NO LOAD.(<P>PERFORMED BITE TEST OF PNEUMATIC SYSTEM IAW AMM 36-23-00, NO FAULTS FOUND. OPS CHECKED APU AIR IAW B767 AMM 36-00-00.</P>)

Part: WARNING LIGHT — FALSE ACTIVATION (SPAR VALVE) · airframe 97,572 hrs · 18,733 cycles

DUE TO CREW VERBAL "RIGHT SPAR VALVE LIGHT INOP", OPS CHECK OF LEFT AND RIGHT SPAR VALVE REQUIRED.(<P>OPS CHECKED OPERATION OF LEFT AND RIGHT FUEL SPAR VALVE IAW B767 AMM 28-22-00, OPS CHECK OK.</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (RT A/C PACK) · airframe 97,546 hrs · 18,729 cycles

"RIGHT PACK TEMP" EICAS MESSAGE ILLUMINATED ON FINAL. WE TURNED THE RIGHT PACK OFF AND WE RECEIVED "RIGHT ENGINE BLEED OFF" MESSAGE WITH OVER 60% N1.(<P>TROUBLESHOT AND FOUND NO PACK TEMP ISSUES. OPS CHECKED RIGHT PACK IAW B767 AMM 21-51-00, OPS CHECK GOOD. SEE ITEM M3 FOR "R ENGINE BLEED OFF" MESSAGE. RAN ENGINE, NO FAULTS INDICATED. PRSOV OPS CHECKED GOOD IAW AMM 36-11-09. NO "RT BLEED OFF" EICAS DISPLAYED.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHTS) · airframe 97,521 hrs · 18,725 cycles

DURING CABIN INSPECTION, FOUND EMERGENCY LIGHTS INOP @ 22H, 34 &AMP; 35C, AND 17C.(<P>REPAIRED WIRING CONNECTOR AT SEATS 34 &AMP; 35C, AND 17C IAW B767 20-10-13. RECONNECTED LOOSE CONNECTOR @ 22H AND OPS CHECKED GOOD PER B767 AMM 33-51-05.

Part: STATUS MESSAGE — FALSE ACTIVATION (IDG VALVE) · airframe 97,430 hrs · 18,708 cycles

LEFT IDG VALVE STATUS MESSAGE.&NBSP;(<P>CLEARED STATUS MESSAGE IAW AMM 31-41-00.</P>)

Part: UNKNOWN — MALFUNCTIONED (APU) · airframe 97,288 hrs · 18,684 cycles

APU FAILED TO START WITH EGT RISING INTO HIGH 100 & RPM MAX OF 12%. STARTED THIRD ATTEMPT. SHUTDOWN APU. INSPECTED ENGINE OIL, FOUND NORMAL. CHECKED ECU, NO FAULTS AND NO DATA INDICATED. RESTARTED NORMAL IAW AMM 49-11-00.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 97,223 hrs · 18,672 cycles

APU FAULT, 3RD ATTEMPT AT 17:23Z. CLEARED FAULT. OPS CHECK COMPLIED WITH, APU START IAW 49-60-00.

Part: FIRE BOTTLE — DEFECTIVE (CABIN) · airframe 97,195 hrs · 18,663 cycles

FWD CABIN A ZONE FIRE EXTINGUISHING QTY GAUGE ERRATIC, DAILY CHECK. REMOVED & REPLACED FIRE EXTINGUISHER IAW AMM 26-24-00.

Part: ACTUATOR — FAILED (SPAR VALVE) · airframe 97,158 hrs · 18,654 cycles

ON DAILY CHECK, FOUND LEFT SPAR VALVE LIGHT DID NOT ILLUMINATE WITH FUEL SWITCH ON. REMOVED AND REPLACED THE LT SPAR FUEL SHUTOFF VALVE ACTUATOR IAW AMM 28-22-11, OPS TESTED GOOD.

Part: WIRE HARNESS — FAILED (EMERGENCY LIGHTS) · airframe 97,158 hrs · 18,654 cycles

IN SEAT EMERGENCY LIGHTS INOPERATIVE ATSEATS 3CA, 4CA, AND 2CA. REMOVED AND REPLACED THE EMERGENCY LIGHT HARNESS ASSY. OPS CHECKED GOOD IAW AMM 33-51-10.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 97,195 hrs · 18,663 cycles

EMERGENCY LIGHT IN CELLING INOP FROM ROWS 30-39. REMOVED AND REPLACED LIGHT BATTERY PACK CHARGE IAW AMM 35-51-00, OPS CHECK C/W.

Part: FUSE — BLOWN (EMERGENCY LIGHTS) · airframe 97,158 hrs · 18,654 cycles

EMERGENCY LIGHTS IN ROW 30 THRU 40, SEATS ROWS A AND C INOP. REPLACED A BLOWN FUSE IN POWER SUPPLY 9010 AND REPAIRED CHAFED WIRES AT SEAT 31A IAW AMM 33-59-00.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHTS) · airframe 97,134 hrs · 18,649 cycles

ESCAPE PATH LIGHTING (SEAT MOUNTED) INOP AT SEATS 14H, 22H, AND 34C.&NBSP;(<P>FOUND CONNECTORS DISCONNECTED AT ALL THREE SEATS. RECONNECTED, AND OPS CHECK GOOD IAW AMM 33-51-10.</P>)

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 97,134 hrs · 18,649 cycles

ISLE RED EMERGENCY PATH LIGHTING LENS MISSING @ L4 LAV.&NBSP;(<P>REPLACED MISSING RED ESCAPE PATH LENS IAW AMM 33-51-10.</P>)

Part: UNKNOWN — FAULT MESSAGE (APU) · airframe 97,139 hrs · 18,650 cycles

APU FAULT DURING APU START. NO APU FAULTS STORED IN ECU MAINTENANCE. APU STARTED ON FIRST ATTEMPT IAW AMM 49-11-00. APU RELIABILITY COLD SOAK START WAS ACCOMPLISHED ON FLT LEG KWI-HHN. START WAS SUCCESSFUL ON FIRST ATTEMPT.

Part: HEAT EXCHANGER — MALFUNCTIONED · airframe 97,128 hrs · 18,648 cycles

EICAS MSG: L PACK TEMP, OPERATES STDBY N. TROUBLESHOOTING FOUND PRIMARY AND SECONDARY HEAT EXCHANGE SWAPPED. REMOVED AND RECONNECTED CONNECTORS IN CORRECT POSITION AND OPS CHECKED GOOD PER AMM 21-51-00.

Part: WARNING MESSAGE — FALSE ACTIVATION (FWD EQUIP BAY) · airframe 97,104 hrs · 18,641 cycles

SHORTLY AFTER T/O, FWD EQUIPMENT OVERHEAT EICAS MESSAGE. PLACED EQUIPMENT COOLING SELECTOR IN STANDBY, THEN OVERRIDE PER QRH. AFTER 30 MIN, SWITCH TO AUTO, THEN TO STANDBY FOR REMAINDER OF FLIGHT. COMPLIED WITH SYSTEM TEST IAW AMM 21-58-00. NO FAULTS NOTED.

Part: SHUTOFF VALVE — NO TEST (NR 2 ENGINE) · airframe 97,088 hrs · 18,637 cycles

NR 2 ENGINE HPSOV FAILED TO TEST. REMOVED AND REPLACED THE NR 2 ENGINE HIGH PRESSURE SHUTOFF VALVE IAW 36-11-07. OPS CHECKED NORMAL IAW AMM 71-00-00.

Part: RELAY — MALFUNCTIONED · airframe 97,088 hrs · 18,637 cycles

EICAS IDLE DISAGREES. REMOVED AND REPLACED SOLENOID RELAY K0433. REMOVED AND REPLACED AIR COND RELAY K207 IAW WD 73-21-19. ENGINE RUN UP NORMAL, NO MESSAGE IAW AMM 71-00-00.

Part: A/C PACK — MALFUNCTIONED (LEFT) · airframe 97,086 hrs · 18,636 cycles

LEFT PACK TEMP ALERT MESSAGE IN CRUISE AT FL 410. CLEARED WITH QRH, DIRECTED TO STBY MODE. RESET L/R PACK CONTROL CB'S. PERFORMED GND TEST ON L PACK CONTROLLER, OPS CHECK IND OK PER AMM 21-51-00.</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (LT A/C PACK) · airframe 97,048 hrs · 18,629 cycles

L PACK TEMP EICAS. RESET, BITE, AND CHECKED FAULT. OPS CHECK OK IAW AMM 21-51-00.

Part: UNKNOWN — MALFUNCTIONED (WEATHER RADAR) · airframe 97,014 hrs · 18,621 cycles

WEATHER RADAR SHOWS A PRESENCE OF FALSE RETURNS IN CLEAR CONDITIONS, IN A CIRCULAR PATTERN AT 40 NM, REGARDLESS OF RANGE.(<P>PERFORMED RADAR BITE CHECK, NO ISSUES NOTED AT THIS TIME IAW AMM 34-43-00.</P>)

Part: CONTROL VALVE — MALFUNCTIONED (AC BAY) · airframe 96,997 hrs · 18,618 cycles

LEFT PACK BITE MESSAGE. (<P>REMOVED AND REPLACED LEFT PACK TEMP CONTROL VALVE IAW AMM 21-51-12.</P>)

Part: CONTROL VALVE — MALFUNCTIONED (ANTI-ICE SYSTEM) · airframe 96,948 hrs · 18,607 cycles

"L WING ANTI-ICE" EICAS CAUTION MSG DISPLAYED, ACCOMPLISHED QRH.&NBSP;(<P>REMOVED AND REPLACED L WING ANTI ICE CONTROL VALVE AND OPS CHECKED GOOD IAW AMM 30-11-02.</P>)

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 96,926 hrs · 18,601 cycles

FWD EQUIPMENT OVERHEAT MSG AFTER TAKEOFF. (<P>PERFORMED THE SUPPLY FAN/ EXHAUST FAN SYSTEM TEST IAW AMM 21-58-00. OPS CHECK GOOD AT THIS TIME.<BR /></P>)

Part: UNKNOWN — MALFUNCTIONED (AC SYSTEM) · airframe 96,936 hrs · 18,603 cycles

AFTER 3 HOURS OF FLIGHT TIME AT FL 340 - 34C CABIN TEMP WILL NOT COOL BELOW FWD 26 MID 29 AFT 28 SET TO MAX COOL.&NBSP;(<P>BITE CHECKED ALL 3 PACK BOXES, NO FAULTS FOUND. SYSTEM IS OPERATING NORMAL NOW PER AMM 21-51-16.</P>)

Part: RELAY — FAILED (AC BAY) · airframe 96,936 hrs · 18,603 cycles

LEFT PACK TEMP EICAS.&NBSP;(<P>TRANSFERRED TO MDDR # 115061 AS PER MEL 21-51-03-01, CAT C, DUE DATE: 30-JUL-19.&NBSP;</P><P>LP 1055488 - M6: REMOVED AND REPLACED&NBSP;RELAY K58 TCM TEMP VALVE. OPS CHECKED IAW AMM 21-51-00. NO FAULTS FOUND. THIS CLEARS MDDR 115061. PLACARD REMOVED.&NBSP;</P>)

Part: MODULATING VALVE — MALFUNCTIONED (BLEED AIR SYS) · airframe 96,936 hrs · 18,603 cycles

L ENG BLEED OFF EICAS, L ENG BLEED OVHT EICAS.&NBSP;(<P>TRANSFERRED TO MDDR # 115060 AS PER MEL 36-12-02-01, CAT C, DUE DATE: 30-JUL-19.</P><P>LP 1055488 - M7:&NBSP;REMOVED AND REPLACED FAN AIR VALVE MODULATING VALVE&NBSP;AND OPS CHECK NORMAL IAW AMM 36-11-16. THIS CLEARS MDDR 115060. PLACARD REMOVED.</P>)

Part: SENSOR — FAILED (AC BAY) · airframe 96,890 hrs · 18,593 cycles

LEFT AND RIGHT PRIMARY HEAT EXCHANGER IN SENSORS HAVE NO VALUES ON ECS/MSG EICAS PAGE. (<P>REMOVED AND REPLACED LEFT AND RIGHT PRIM HX IN SENSORS PER AMM 21-51-06. SENSORS VALUES ARE RIGHT 127, LEFT 130.&NBSP;&NBSP;</P><P><BR /></P>)

Part: SENSOR — FAULTY (AC BAY) · airframe 96,867 hrs · 18,589 cycles

AFTER ONE HOUR FLIGHT TIME @ FL 400, CABIN ZONE TEMPERATURES WERE READING 33C/32C/33C RESPECTIVELY.&NBSP; ALL THREE TEMP SELECTORS WERE FULL COLD. USED QRH PROCEDURE. FOLLOWED PROCEDURE UNTIL LEFT PACK WAS OFF AND RIGHT PACK WAS IN STBY POSITION. TEMPERATURES FINALLY DROPPED TO 22/22/22 AFTER 3 HOURS FLIGHT TIME.&NBSP;(<P>CLEANED CABIN TEMP SENSOR FILTERS IAW AMM 21-61-09. REPLACED LEFT PACK OUTLET TEMP SENSOR AND COMPRESSOR OUTLET TEMP SENSOR IAW AMM 21-51-06. RESEATED CONNECTOR AND OPS CHECK RT PACK RAM AIR DOOR ACTUATOR IAW AMM 21-53-03.&NBSP;&NBSP;<BR /></P>)

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 96,806 hrs · 18,579 cycles

&NBSP;MOMENTARY PACK TEMP ON APPROACH ( EICAS MESSAGE CLEARED )&NBSP;(<P>OPS CHECK IAW AMM 21-50-00. NO DEFECTS NOTED&NBSP;</P>)

Part: CONTROL VALVE — MALFUNCTIONED (AC BAY) · airframe 96,798 hrs · 18,578 cycles

DURING CLIMB FWD EQPT OVHT MESSAGE&NBSP;(<P>REPLACED L PACK TEMP CTR VALVE. CKS GOOD PER AMM 21-51-12</P>)

Part: TERMINAL — CORRODED (FIRE DETECTOR) · airframe 96,736 hrs · 18,566 cycles

UPON SHUTDOWN, STATUS MESSAGE " RT ENGINE FIRE LP 1" REMAINED IN VIEW.&NBSP;(<P>DEFERRED IAW MEL 26-11-01-01, CAT 'C', MDDR 114001. PLACARD INSTALLED.&NBSP;</P><P>LP 1081861 - M5:&NBSP;T/S PER FIM 26-11-804. FOUND CORRODED TERMINALS ON FIRE DETECTOR, CLEANED AND RE-TIGHTENED. FOUND LOOSE PIN IN D42205 RT ENG STRUT, RESEATED OPS CK C/W IAW AMM 26-11-00. THIS CLEARS MDDR 114001. PLACARD REMOVED.</P>)

Part: CONTROLLER — FAULTED (AC BAY) · airframe 96,712 hrs · 18,561 cycles

RIGHT PACK CONTROLLER SHOWS FAULT.&NBSP;(<P>REMOVED AND REPLACED RIGHT PACK CONTROLLER IAW AM 21-51-04. OPS CHECK GOOD.&NBSP;</P>)

Part: ACTUATOR — MALFUNCTIONED (AC BAY) · airframe 96,712 hrs · 18,561 cycles

AFTER LEVEL 350, COCKPIT BECAME ABNORMALLY HOT. SOON AFTER, FA REPORTED CABIN EXCESSIVELY HOT. ALL ATTEMPT TO COOL CABIN UNSUCCESSFUL. SOON AFTER, FA'S REPORTED CABIN DANGEROUSLY HOT WITH PAX IN DISTRESS AND BECOMING ILL.&NBSP; &NBSP; &NBSP;(<P>REMOVED AND REPLACED LEFT PACK ACTUATOR IAW AMM 21-53-03. OPS CHECK GOOD AT THIS TIME&NBSP;</P>)

Part: CONTROL VALVE — FAILED (RT A/C PACK) · airframe 96,688 hrs · 18,556 cycles

R PACK TEMP EICAS AFTER LEVEL OFF AT FL 410. EIACAS MSG WENT OUT AFTER STBY N SELECTED.(<P>REMOVED AND REPLACED&NBSP;R PACK TEMP CONTROL VALVE IAW AMM 21-51-12, OPS TEST OK. ALSO CHANGED K50 RELAY IAW SWPM 20-81-11 PER FIM 21-51 FT 803, OPS CHECK OK.<BR /></P>)

Part: CONNECTOR — DISCONNECTED (RT A/C PACK) · airframe 96,654 hrs · 18,550 cycles

"R PACK TEMP" EICAS MSG AFTER V LIST CONTROLLER IN STBY N. BITE INDICATED TEMP CONTROL VALVE FAULT. RE-SEATED THE CONNECTOR AND OPS CHECK GOOD IAW AMM 21-51-00.

Part: CONTROL VALVE — FAILED (APU SURGE) · airframe 96,654 hrs · 18,550 cycles

APU FAILED TO START. REMOVED AND REPLACED SURGE CONTROL VALVE IAW AMM 49-53-01. OPS CHECKED GOOD.

Part: DRIVE UNIT — MALFUNCTIONED (WEATHER RADAR) · airframe 96,654 hrs · 18,550 cycles

WX RADAR FAIL MSG ON HSI DISPLAY.&NBSP; "WXR SYS" STATUS MSG.(<P>REMOVED AND REPLACED WX RADAR DRIVE UNIT AND ANTENNA IAW AMM 34-43-05.

Part: CONNECTOR — LOOSE (SHUTOFF VALVE) · airframe 96,629 hrs · 18,544 cycles

RIGHT PACK TEMP EICAS MESSAGE WENT TO STANDBY(<P>RE SECURED RT PACK FLOW SHUT OFF VALVE CONNECTOR AND OPS CHECKED GOOD IAW AMM 21-51-804 FIM&NBSP;</P>)

Part: WIRE — DAMAGED (NR 1 FIRE LOOP) · airframe 96,596 hrs · 18,538 cycles

EICAS MESSAGE DISPLAYED "R ENG FIRE LOOP 1". CHECKED RT ENG FIRE LP 1, NO DEFECTS NOTED. CHECK CONNECTIONS ON FIRE LOOP 1, NO DEFECTS NOTED IAW 26-11-00. COULD NOT DUPLICATE FAULT, OPS CHECK GOOD. ITEM REMAINS OPEN. REMOVED AND REPLACED UPPER ACT FIRE LOOP ASSY RT ENG PER AMM 26-11-02. REPAIRED WIRE TERMINAL ON RT ENG AFT LOWER LOOP IAW SRPM 20-30-22.

Part: COOLING FAN — FAILED (EQUIPMENT) · airframe 96,575 hrs · 18,534 cycles

FWD EQUIPMENT EXH FAN STATUS MESSAGE. SMOKE, FIRE, FUMES NNC COMPLETED WITH, NO CIRCUIT BREAKERS POPPED. ELECTRICAL ODOR IN COCKPIT. FOUND CIRCUIT BREAKER POPPED ON EQUIPMENT COOLING FAN. REMOVED AND REPLACED FWD EQUIPMENT COOLING FAN IAW AMM 21-58-06-02-01. OPS CHECK GOOD. MCC NOTIFIED.

Part: SENSOR — LOOSE (DUCT PRESSURE) · airframe 96,575 hrs · 18,534 cycles

ON CLIMB OUT, RIGHT DUCT PRESSURE FLUCTUATES FROM 25 TO 50 PSI. CRUISE AND DESCENT PRESSURES ARE NORMAL. TIGHTENED FAN AIR TEMP SENSOR, INSPECTED PRSOV FILTERS IAW AMM 36-11-09. PERFORMED AIR SUPPLY BITE TEST IAW AMM 36-11-09. PRSOV TESTED GOOD IAW B767 AMM 36-11-09.

Part: CONNECTOR — LOOSE (FIRE LOOP 1) · airframe 96,529 hrs · 18,524 cycles

RT ENG FIRE LP 1 MESSAGE WON'T CLEAR. T/S PER FIM TASK 26-11 FAULT TREE 804. FOUND LOWER FWD LOOP AND UPPER AFT LOOP TOUCHING METAL. RE-POSITIONED LOOP TO PREVENT TOUCHING METAL. OPS CKS GOOD. FOUND LOOSE CONNECTOR AND TIGHTENED AND OPS CHECK IAW AMM 26-11-00.

Part: ECU — FAILED (APU) · airframe 96,512 hrs · 18,520 cycles

APU FAULT. DURING THE APU TROUBLESHOOTING, FOUND THE ECU UNABLE TO SHOW ANY KIND OF MESSAGE AND CODE. REMOVED AND REPLACED ECU IAW AMM 49-61-05-40. REMOVED AND REPLACED APU STARTER IAW AMM 49-41-01-004-001 & 49-41-01-404-007. APU STARTED & RAN NORMAL. REMOVED AND REPLACED THE PRESSURE SENSOR IAW AMM 49-61-04-002-001-402-006. APU OPS CHECKED GOOD. REMOVED AND REPLACED SURGE CONTROL VALVE IAW AMM 49-53-01-401. NO HELP. REMOVED AND REPLACED ECU IAW AMM 49-61-05. OPS CK NORMAL.

Part: CONTROLLER — MALFUNCTIONED (RT A/C PACK) · airframe 96,512 hrs · 18,520 cycles

DURING CRUISE, CABIN TEMPERATURE EXCESSIVELY HOT. RIGHT PACK INOP. REMOVED AND REPLACED ZONE TEMP CONTROLLER IAW AMM 21-61-03. OPS CHECK NORMAL.

Part: BLEED VALVE — MALFUNCTIONED (LT ENGINE) · airframe 96,483 hrs · 18,514 cycles

ON CLIMB; LEFT PACK, LEFT BLEED OVERHEAT, LEFT ENGINE BLEED EICAS MESSAGES. RESET BLEED VALVE AT CRUISE, CLEARED MESSAGE.&NBSP;(<P>PERFORMED BITE CHECK IAW AMM 36-11-00. NO DEFECTS NOTED.&NBSP;</P>)

Part: ACM — DAMAGED (AC BAY) · airframe 96,410 hrs · 18,497 cycles

ON POST FLIGHT FOUND DAMAGE TO LH PACK COOLING TURBINE, PLENUM, &AMP; COMPRESSOR&NBSP;(<P>REPLACED LT ACM IAW AMM 21-51-03 AND DISCHARGE DUCT SEAL. LEAK CHECKS GOOD&NBSP;</P>)

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 96,372 hrs · 18,488 cycles

RT PACK TEMP EICAS MESSAGE ON DESCENT. (<P>PERFORMED FIM TASK 21-51 TASK 803. OPS CHECK PASSED.</P>)

Part: UNKNOWN — MALFUNCTIONED (APU) · airframe 96,372 hrs · 18,488 cycles

APU WILL NOT START ON THE GROUND 3X.(<P>OPS CHECKED OK BY MX IAW AMM 49-00-00.</P>)

Part: CONNECTOR — DEFECTIVE (BOOST PUMP) · airframe 96,319 hrs · 18,477 cycles

RT AFT FUEL BOOST PUMP INOPERATIVE&NBSP;(<P>REMOVED AND REPLACED CONNECTOR ON RT AFT FUEL BOOST PUMP OPS CHECK GOOD IAW AMM 28-22-03 AND SWPM 20 -61-00 THIS CLEARS MDDR 110840 PLACARD REMOVED</P>)

Part: OIL SYSTEM — LOW (APU) · airframe 96,280 hrs · 18,467 cycles

APU FAULT EICAS MSG, APU DIDN'T START AFTER 3 ATTEMPTS.(<P>SERVICED THE APU WITH 1 QT. OPS CHECK GOOD IAW AMM 49-00-00.</P>)

Part: SWITCH — INTERMITTENT (FUEL DOOR) · airframe 96,280 hrs · 18,467 cycles

FUEL DOOR SWITCH INTERMITTENT. NO CENTER PUMP INHIBIT.(<P>REMOVED AND REPLACED FUEL DOOR SWITCH PER WDM 20-30-12. OPS CHECK GOOD.</P>)

Part: PUMP — MALFUNCTIONED (FUEL SYSTEM) · airframe 96,252 hrs · 18,463 cycles

R AFT FUEL PUMP EICAS, RIGHT AFT FUEL BOOST PUMP CB POPPED. QRH COMPLETE. REPEAT WRITE-UP.&NBSP;(<P>TRANSFERRED FUEL PUMP TO MEL 28-22-01 MDDR 110840. PLACARD INSTALLED AND MAINT PROCEDURES C/W. AIRCRAFT RESTRICTED TO ETOPS 120.</P><P>LP 1079323-M2&NBSP; FOUND B1 WIRE W048-49-16 LOOSE ON CB C371. INSPECTED AND TIGHTENED. OPS CHECK PUMP ON GROUND IAW AMM 28-22-00, NO DEFECT NOTED. CLEARED MDDR 110840.</P><P>LP 1079324 - 1: RE-OPENED MDDR 110840.</P><P>LP 1079340 - M5: REMOVED AND REPLACED CONNECTOR ON RT AFT FUEL BOOST PUMP OPS CHECK OK PER AMM 28-22-03 AND SWPM 20-61. THIS CLEARS DMI 110840. PLACARD REMOVED. DISP UP 2027<BR /></P><P>LP 1074280 - M6:&NBSP;<SPAN>REPLACED WIRE HARNESS FLOW D1551-D4410 PER FIM 28-22 FT 820 PER SWPM 20-10-13.&NBSP;</SPAN><SPAN>&NBSP;&NBSP;</SPAN></P><P>LP 1074281 - M7: PERFORMED FIM 28-22 FT 820 WIRING CHECK.&NBSP;</P><P>LP 1074281 - M8: R/R R/H AFT BOOST IAW AMM 28-22-03. OPS AND LEAK CHECK C/W.&NBSP;THIS CLEARS MDDR 110840. PLACARD REMOVED.</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (RT A/C PACK) · airframe 96,215 hrs · 18,455 cycles

INTERMITTENT RIGHT PACK TEMPERATURE EICAS MESSAGE IN FLIGHT.&NBSP;&NBSP;(<P>PERFORMED FIM 21-51 FT 803 SYSTEM FAULTED TEMP CONTROL VALVE. PERFORMED TABLE B PROCEDURES, TEMP CONTROL VALVE OPS CHECK NORMAL.&NBSP;VERIFIED NO FAULTS NOTED.&NBSP;&NBSP;</P>)

Part: WARNING LIGHT — FALSE ACTIVATION (RT A/C PACK) · airframe 96,197 hrs · 18,451 cycles

DURING TAXI, R PACK TEMP EICAS MESSAGE. RAN CHECKLIST. PACK CONTROL SELECTOR SET TO STBY, LT EXTINGUISHED.(<P>COLD NOT DUPLICATE. PERFORMED BITE CHECK IAW AMM 34-10-00.</P>)

Part: WIRE HARNESS — FAILED (BOOST PUMP) · airframe 96,192 hrs · 18,450 cycles

RIGHT AFT FUEL PUMP FAILED. COMPLIED WITH QRH POCEDURES. REMOVED AFT FUEL PUMP RIGHT ACCESS PANEL AND DE PINNED D1540 PIN 2 TO INSPECT. RE-INSTALLED PINS AND CLOSED ACCESS PANELS. DMI 110638 REMAINS OPEN. REMOVED AND REPLACED WIRE HARNESS WO478 PER EO 6728A011T AND SWPM 20-10-11, -12, -19. C/W CDCCL'S AMM 28-00-00. RIGHT AFT BOOST PUMP OPS CHECK OK REF AMM 28-22-00..

Part: PUMP — INOPERATIVE (RIGHT) · airframe 96,182 hrs · 18,448 cycles

RIGHT AFT FUEL PUMP INOP(<P>TRANSFERRED TO MEL 28-22-01 MDDR 110519&NBSP; CAT 'C'. PLACARD INSTALLED. MX PROCEDURES C/W. AIRCRAFT RESTRICTED TO ETOPS 120.&NBSP;</P><P>LP 1047034 - M11:&NBSP;MEGGED WIRES W476-302B-16, 302R, 302Y, AND W580-168-14,169,170. RE-TORQUED K10702 &AMP; CBC371 REF SWPM 20-81-22. FOUND INCORRECT WIRE BEND IN RT WHEEL WELL CONNECTOR D4410P. ROUTED WIRE CORRECTLY. REF SWPM 20-10-11. THIS CLEARS MDDR 110519. REMOVED PLACARD. MCC NOTIFIED.&NBSP;</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (WEATHER RADAR) · airframe 96,150 hrs · 18,442 cycles

STATUS MSG "WXR SYS".&NBSP;(<P>PERFORMED OPS CHECK OF WXR SYSTEM IAW B767 AMM 34-43-00. NO FAULTS FOUND AT THIS TIME.&NBSP;</P>)

Part: RELAY — FAILED (BOOST PUMP) · airframe 96,093 hrs · 18,432 cycles

RIGHT AFT FUEL PUMP PRESSURE LIGHT ILLUMINATED.&NBSP;(<P>TRANSFERRED TO MDDR 110147 AS PER MEL 28-22-01 CAT "C". MAINTENANCE PROCEDURES C/W. AIRCRAFT RESTRICTED TO ER 120.&NBSP;</P><P>LP 1042361 - M4: R/R RIGHT FLT BOOST PUMP ASSY IN&NBSP;ACCORDANCE WITH AMM 28-22-03. (P/N: 5006003D, S/N: 1575)</P><P>LP 1042364 - 01: R AFT FUEL PUMP EICAS MSG AT FL 390. QRH PROCEDURES COMPLETED. REPEAT WRITE-UP, SEE LP 1042353.</P><P>LP 1042370:&NBSP; REMOVED AND REPLACED GFI CONTROL RELAY K10702 RIGHT AFT FUEL PUMP IAW AMM 28-22-18. OPS CHECK AT THIS TIME.

Part: STOWAGE BOX — LEAKING (OXYGEN MASK) · airframe 96,117 hrs · 18,437 cycles

POSSIBLE O2 LEAK. REMOVED AND REPLACED 2ND OBSERVERS O2 MASK STORAGE BOX ASSYEMBLY IAW B767 AMM 35-11-51. OPS AND LEAK CHECK GOOD.<BR /></P>)

Part: LINE — LOOSE (HYD SYSTEM) · airframe 96,077 hrs · 18,427 cycles

LEFT ENGINE LEAKING OIL AROUND IDG AREA.(<P>FOUND L/H ENG HYD RETURN LOOSE. RE-TORQUED HYD ENG RETURN LINE REF AMM 29-11-05. MOTORED ENG, NO LEAKS NOTED.<BR /></P>)

Part: START VALVE — MALFUNCTIONED (LT ENGINE) · airframe 95,985 hrs · 18,408 cycles

DURING LEFT ENGINE START, VALVE LIGHT DID NOT EXTINGUISH WITH START SELECTOR ON GND.(<P>DEFERRED&NBSP;IAW MEL 80-00-02-01 MDDR 109620.&NBSP;</P><P>LP 1042487- M2: REMOVED AND REPLACED START VALVE IAW AMM 80-11-02. OPS CHECK OK. CLEARED MDDR 109620 AND PLACARD REMOVED.</P>)

Part: SLEEVE — DAMAGED (APU DUCT) · airframe 95,976 hrs · 18,406 cycles

APU SURGE BLEED DUCTHAS A HOLE.(<P>REMOVED AND REPLACED APU SURGE BLEED DUCT SLEEVE. REF: AMM 79-53-01.</P>)

Part: ENGINE — OIL CONSUMPTION (NR 1) · airframe 95,976 hrs · 18,406 cycles

REPLACE #1 ENGINE DUE OIL CONSUMPTION.(<P>REMOVED AND REPLACED #1 ENGINE. ACCOMPLISHED ENGINE RUN UP. NO DEFECTS AND NO LEAKS EVERYTHING NORMAL.PER AMM 71-00-00.</P>)

Part: FIRE LOOP — MALFUNCTIONED (NR 1) · airframe 95,976 hrs · 18,406 cycles

EICAS MSG ENGINE 1 O/H LOOP 1 AFTER ENGINE CHANGE.(<P>REMOVED AND REPLACED #1 ENGINE OVHT. DETECTOR. PER AMM 26-11-02. ACCOMPLISHED FIRE/OVHT. SYSTEM TEST OK. PER AMM 26-11-00.</P>)

Part: PACKING — LEAKING (PNEUMATIC SYSTEM) · airframe 95,976 hrs · 18,406 cycles

DURING PNEUMATIC LEAK CHECK USING COMPRESSED NITROGEN AT #2 ENGINE CHECK FAILED AT LOCATION "K".(<P>REMOVED AND REPLACED #2 ENGINE PRV DAMAGED "O" RING AT ELBOW FITTING COMPRESS INLET. IAW AMM 36-11-18 NO LEAKS NOTED. REF: EO1936A088 LOCATION K.</P>)

Part: SMOKE DETECTOR — FALSE ACTIVATION (LAVATORY) · airframe 95,963 hrs · 18,403 cycles

LAVATORY SMOKE EICAS(<P>L4 LAV POSITION TRANSFERED TO MEL 26-26-03-01A MDDR 109171 CAT C DUE 03APR PLACARD INSTALLED MAINTENANCE PROCEDURES C/W DETECTOR ISOLATED L4 DETECTOR INOP ONLY&NBSP;</P>)

Part: SENSOR — UNSECURE (SMOKE DETECTOR) · airframe 95,913 hrs · 18,393 cycles

LAVATORY SMOKE EICAS MESSAGE SHOWED DURING DESCENT&NBSP;(<P>REMOVED AND RE SECURED SMOKE DETECTOR SENSOR - OPS CHECKED GOOD IAW AMM 26-13-00&NBSP;</P>)

Part: LINKAGE — LACK OF LUBE (RAM AIR INLET) · airframe 95,913 hrs · 18,393 cycles

RIGHT PACK TEMP EICAS MESSAGE, SHOWED ON FINAL APPROACH.&NBSP;&NBSP;(<P>FAULT RAM INLET ACTUATOR LUBED LINKAGE AND OPS CHECKED GOOD IAW AMM 21-51-14.&NBSP;</P>)

Part: PUMP — FAILED (FUEL SYSTEM) · airframe 95,867 hrs · 18,385 cycles

"R AFT FUEL PUMP" EICAS MESSAGE. (<P>TRANSFER TO MEL 28-22-01 CAT C MDDR 108759. </P><P>LOG PAGE 1042385: REMOVED AND REPLACED RT AFT FUEL PUMP IAW AMM 28-22-03.&NBSP;NO MSG SHOWN, LEAK AND OPS CHECK OK. MCC NOTIFIED, THIS CLEARS MDDR 108759.</P>)

Part: CONNECTOR — DIRTY (RAM AIR ACTUATOR) · airframe 95,859 hrs · 18,383 cycles

R PACK TEMP EICAS MESSAGE DISPLAYED.(<P>PREVIOUS FAULT RAM INLET ACTUATOR, CLEANED CONNECTOR ON RT RAM INLET ACTUATOR PER AMM 21-51-14.</P>)

Part: CONTROLLER — MALFUNCTIONED (AC BAY) · airframe 95,783 hrs · 18,368 cycles

R PACK TEMP EICAS MESSAGE IN FLIGHT.(<P>ACCOMPLISHED FIM 21-51 TREE 803 AND BIT RIGHT PACK TEMP INLET ACT, RESET OF RT PACK TEMP CONTROLLER , OK AND OPS CHECK OF RT PACK OK AS PER AMM 21-51-00.&NBSP;</P>)

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 95,772 hrs · 18,365 cycles

CENTER L FUEL PUMP CAUTION MESSAGE.(<P>PERFORMED CENTER L FUEL PUMP OPERATIONAL CHECK IAW AMM 28-22-00 OK FOR SERVICE.</P>)

Part: RADAR — MALFUNCTIONED (NR 1 WX SYSTEM) · airframe 95,625 hrs · 18,337 cycles

#1 WEATHER RADAR INOP&NBSP;(<P>OPS CHECKED WEATHER RADAR #1, GOOD IAW B767 AMM 34-43-00</P>)

Part: WARNING MESSAGE — FALSE INDICATION (WEATHER RADAR) · airframe 95,630 hrs · 18,338 cycles

STATUS WXR SYS MSG(<P>PERFORMED FIM 34-43- FT 805 WXR BITE PROCEDURES, NO FAULTS NOTED.</P>)

Part: FUEL FILTER — WARNING MESSAGE (RT ENGINE) · airframe 95,625 hrs · 18,337 cycles

R ENG FUEL FILT EICAS MSSAGE ON ALL CLIMB SEGMENTS(<P><SPAN>R/R / R/H ENGINE FUEL FILTER IAW AMM 73-11-02. OPS NORMAL LEAK CHECK GOOD.</SPAN></P>)

Part: CONTROL VALVE — FAILED (RT A/C PACK) · airframe 95,522 hrs · 18,315 cycles

RH PACK TEMP IN FLIGHT, OPS NORMAL PER QRH IN SWITCH N POSITION&NBSP;(<P>FOUND TEMP CONTROL VALVE ON PACK CONTROLLER ( RH ) , REMOVED AND REPLACED RH PACK TEMP CONTROL VALVE I.A.W AMM 21-51-12 OPS TEST GOOD NO FAULTS OR EICAS MSG&NBSP;</P>)

Part: START VALVE — UNKNOWN (NR 2 ENGINE) · airframe 95,506 hrs · 18,312 cycles

ENG #2 START VALVE STOCK&NBSP; CLOSED(<P>RECYCLED&NBSP; START VALVE&NBSP; OPS CHECK GOOD IAW AMM 80-00-00</P>)

Part: UNKNOWN — MALFUNCTIONED (AC BAY) · airframe 95,361 hrs · 18,284 cycles

EICAS MESSAGE LEFT PACK&NBSP;(<DIV>FOUND PACK FLOW AND SHUTOFF VALVE WOULD NOT OPEN. REMOVED AND RECONNECTED ALL ELECTRICAL CONNECTORS - VALVE OPS CHECK GOOD IAW AMM 21-51-01</DIV>)

Part: FIRE WARNING — FALSE ACTIVATION (COCKPIT) · airframe 95,351 hrs · 18,282 cycles

UPON LANDING FIRE WARNING BELL ACTIVATED WITH NO EICAS MSG.(<P>RESET WARN ELEX A AND WARN ELEX B CB'S AND OPS CHECKED GOOD IAW AMM 26-11-01.</P>)

Part: VALVE — MALFUNCTIONED (BLEED AIR SYS) · airframe 95,388 hrs · 18,290 cycles

LT FAN AIR VALVE CLOSED AND OPEN SWITCH DISAGREE.(<P>REPLACED FAN AIR VALVE</P>)

Part: SHUTOFF VALVE — MALFUNCTIONED (BLEED AIR SYS) · airframe 95,388 hrs · 18,290 cycles

LT HPSOV CLOSED AND OPEN SWITCHES DISAGREE.(<P>RPELACED HPSOV.</P>)

Part: SLIDE — DEPLOYED (R2 DOOR) · airframe 95,334 hrs · 18,279 cycles

R2 MID CABIN DOOR SLIDE DEPLOYED(<P>TRANSFER TO MDDR 105857 IAW MEL 52-11-04-01A CAT A PLACARD INSTALLED. MAINTENANCE PROCEDURES C/W, SLIDE REMOVED.&NBSP; LP: 1009981-M1: REMOVED AND REPLACED THE R2 DOOR SLIDE IAW AMM 25-66-01. THIS CLEARS MDDR 105857</P>)

Part: SHUTOFF VALVE — FAULTY (AC BAY) · airframe 95,286 hrs · 18,270 cycles

LT PACK INOP(<P>TRANSFERRED TO MEL 21-51-01-01, MDDR 105657.</P><P>LP-1009969-M2 RE-SEATED CONNECTOR ON LEFT PACK FLOW CONTROL AND SHUT OFF VALVE OPS CHECK LEFT PACK OPS CHECK GOOD IAW AMM 21-51-01. LP 1009970-M1&NBSP; &NBSP;REOPENED MDDR 105657</P><P>REF LOG PAGE 1009974 ITEM M4; REMOVED AND REPLACED LEFT PACK FLOW SHUTOFF VALVE AND OPS CHECKED GOOD IAW AMM 21-51-01. THIS ACTION CLEARS MDDR 105657.&NBSP;</P>)

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 95,280 hrs · 18,267 cycles

EMERGENCY LIGHT ON SEAT 20AC 32AC DOES,T STAY ON WHILE SWITCH IS ON LOW BATTERY VOLTAGE(<P>REMOVED AND REPLACED BATTERY PACK AND TESTED OK IAW AMM 33-51-07</P>).

Part: OVERHEAT SYS — FALSE ACTIVATION (LT BLEED) · airframe 95,209 hrs · 18,251 cycles

DURING CLIMB, AT APPROXIMATELY 8000 FEET, LEFT BLEED OVERHEAT LIGHT WAS FOLLOWED BY LEFT ENGINE BLEED OFF EICAS MESSAGE. QRH WAS FOLLOWED AND MESSAGE CLEARED.(<P>OPS CHECK OK IAW AMM 36-22-00. NO DEFECTS NOTED.<BR /></P>)

Part: ANTI-ICE VALVE — FAULTY (RT WING) · airframe 95,123 hrs · 18,223 cycles

RIGHT WING ANTI-ICE VALVE DOES NOT MOVE OR WORK CORRECTLY. LIGHT TEST OK. VERIFIED EICAS MESSAGE FOR RT WING DEICE VALVE IS WORKING MM 30-11-00. REMOVED AND REPLACED RIGHT WING ANTI ICE VALVE IAW AMM 30-11-02. THIS OPS CHECK NORMAL.

Part: CONNECTOR — LOOSE (SMOKE DETECTOR) · airframe 95,000 hrs · 18,197 cycles

LAV SMOKE EICAS CHIME ON DURING DECENT&NBSP;(<P>FOUND L4 LAV SMOKE DETECTOR SENSOR CONNECTOR LOOSE ,SECURED CONNECTOR AND OPS CHECKED GOOD IAW B767AMM 26-13-01&NBSP;</P>)

Part: PUMP — MALFUNCTIONED (FUEL BOOST) · airframe 94,977 hrs · 18,194 cycles

RIGHT FWD FUEL PUMP C/B POPPED. REMOVED AND REPLACED RIGHT FWD BOOST PUMP IAW B767 AMM 28-22-03 NORMAL OPERATION OBSERVED.

Part: GROUND WIRE — LOOSE (BOOST PUMP) · airframe 94,923 hrs · 18,181 cycles

RIGHT FWD FUEL BOOST PUMP WAS INOPERATIVE. FOUND CONNECTOR GROUND LOOSE. TIGHTENED, CHECKED GOOD IAW AMM 28-22-03.

Part: SWITCH — DIRTY (SPAR VALVE) · airframe 94,794 hrs · 18,150 cycles

NO RIGHT ENG SPAR VALVE INDICATION DURING START. ENG STARTING NORMALLY. CLEANED GATE VALVE SWITCH ON SPAR VALVE. OPS CHECK C/W.

Part: SIGN — DISCONNECTED (CABIN) · airframe 94,754 hrs · 18,141 cycles

EMER LIGHT SIGN INOP AT R2 DOOR LOWER. RECONECT EMER LIGHT SIGN AT R2 DOOR LOWER, OPS CHECK C/W IAW MM 33-50-00.

Part: ANTI-ICE VALVE — MALFUNCTIONED (LT WING) · airframe 94,754 hrs · 18,141 cycles

LEFT WING ANTI ICE EICAS MESSAGE ON CLIMB. WING ANTI ICE WERE OFF. REMOVED AND REPLACED LEFT WING ANTI ICE VALVE V52 IAW AMM 30-11-02. OPS CHECK NORMAL, NO LEAK NOTED.

Part: GENERATOR — INOPERATIVE (APU) · airframe 94,743 hrs · 18,139 cycles

APU INOP. REMOVED AND REPLACED APU GENERATOR IAW AMM 24-21-01. OPS CHECK NORMAL AND NO OIL LEAK NOTED.

Part: CONNECTOR — DIRTY (FUEL SYSTEM) · airframe 94,695 hrs · 18,129 cycles

RIGHT ENGINE SPAR VALVE SLOW TO CYCLE ON START. CLEANED SPAR VALVE CONNECTOR, OP'S CHECK NORMAL IAW AMM 28-22-01.

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 94,695 hrs · 18,129 cycles

RIGHT PACK DOES NOT TURNOFF VIA PACK CONTROL SWITCH. RE-LAMPED RIGHT PACK LIGHT OP'S CHECK NORMAL IAW AMM 33-13-00.

Part: CONNECTOR — UNSECURE (CABIN) · airframe 94,695 hrs · 18,129 cycles

EMERGENCY LIGHT AT 6K INOP. SECURED CONNECTOR AT SEAT 6K EMERG. LIGHT OP'S CHECK GOOD IAW WDM 33-51-18.

Part: CONTROL VALVE — NOT REPORTED (AC BAY) · airframe 94,695 hrs · 18,129 cycles

AS PER MCC REQUEST REMOVE AND REPLACE RIGHT PACK FLOW CONTROL VALVE. REMOVED AND REPLACED RIGHT PACK FLOW CONTROL VALVE. OP'S CHECK NORMAL, NO LEAKS IAW AMM & 21-51-01.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 94,578 hrs · 18,107 cycles

SELECTED SYS 2 WX RADAR INFLIGHT WX FAIL MESSAGE ON HSI AND WXR SYS STATUS MESSAGE. PERFORMED WEATHER RADAR BITE CHECK IAW AMM 34-43-00 NO DEFECTS NOTED AT THIS TIME.

Part: CONTROL VALVE — MALFUNCTIONED (AC BAY) · airframe 94,489 hrs · 18,094 cycles

RT PACK TEMP, COMPLETED QRH. REMOVED AND REPLACED ACM TEMP CONTROL VALVE. OPS CHECKED GOOD IAW AMM 21-51-01.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 94,485 hrs · 18,093 cycles

RIGHT PACK TEMP. PERFORMED BIT FOUND TEMP CONTROL VALVE FAULTED PREVIOUS FLIGHT, NO FAULTS INDICATED AT THIS TIME PER FIM 21-51- FT 807. SYSTEM OPS CHECKED GOOD PER AMM 21-51-00.

Part: CONTROL VALVE — MALFUNCTIONED (AC BAY) · airframe 94,423 hrs · 18,077 cycles

RT PACK INOP. REMOVED AND REPLACED RIGHT PACK FLOW CONTROL AND SHUTOFF VALVE AND OPS CHECKED GOOD IAW 21-51-01.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 94,392 hrs · 18,068 cycles

RIGHT PACK OFF LIGHT AND RIGHT PACK OFF EICAS ON DURING FLIGHT. RIGHT PACK OFF LIGHT INTERMITTENT WHILE RIGHT PACK OFF EICAS STAYS ON. PERFORMED TEST IAW AMM 21-51-00. CLEARED EXISTENT FAULT, OPS CHECK GOOD AT THIS TIME.

Part: APU — MALFUNCTIONED (APU BAY) · airframe 94,392 hrs · 18,068 cycles

APU FAIL AFTER RIGHT ENGINE START, UPON LANDING APU INDICATED NO OIL. SHOWED FULL ON DEPARTURE. REPLACED APU IAW AMM 49-11-01. OPS CHECK NORMAL.

Part: OIL SYSTEM — LOW (APU) · airframe 94,471 hrs · 18,090 cycles

APU FAIL DURING PUSH BACK BEFORE ENGINE START. RESET ECU AUTO SHUT DOWN ADDED OIL AND RESTARTED APU. OPS CHECK NORMAL AT THIS TIME IAW AMM 49-11-22-00 AND 49-11-00.

Part: UNKNOWN — MALFUNCTIONED (WEATHER RADAR) · airframe 94,354 hrs · 18,060 cycles

LEFT RADAR GIVING UNUSUAL RETURNS, DEEP RED RETURNS EVEN AT +8* TILT. PERFORMED RADAR BITE OK. CK OK IAW AMM 34-43-00.

Part: CONTROL PANEL — FAULTY (COCKPIT) · airframe 94,370 hrs · 18,063 cycles

WXR SYS STATUS MESSAGE AFTER SWITCHING TO SYS 2 ON CONTROL HEAD, AND WXR FAIL AMBER MESSAGE LOWER LEFT ON EHSI. REMOVED AND REPLACED F/O'S EFIS CONTROL PANEL IAW 34-22-02, OPS CHECK C/W.

Part: VALVE — MALFUNCTIONED (FUEL SYSTEM) · airframe 94,313 hrs · 18,052 cycles

NO 'SPAR VALVE' LIGHT DURING LEFT ENGINE START. RESET SPAR VALVE C/B, OPS CHECKS C/W IAW AMM 28-60-20.

Part: CONTROL PANEL — FAULTY (COCKPIT) · airframe 94,313 hrs · 18,052 cycles

WXR SYS STATUS MESSAGE AFTER SWITCHING TO SYS 2 ON CONTROL HEAD, AND WXR FAIL AMBER MESSAGE LOWER LEFT ON EHSI. REMOVED AND REPLACED F/O'S EFIS CONTROL PANEL IAW 34-22-02 OPS CHECK C/W.

Part: PUMP — INOPERATIVE (FUEL SYSTEM) · airframe 94,261 hrs · 18,041 cycles

RIGHT AFT FWD BOOST PUMP INOP. REMOVED AND REPLACED RT AFT FWD BOOST PUMP IAW AMM 28-22-00. LEAKS AND OPERATION CHECKS COMPLIED WITH.

Part: CONNECTOR — LOOSE (BATTERY CHARGER) · airframe 94,235 hrs · 18,035 cycles

MAIN BAT CHARGER STATUS MESSAGE DISPLAYED. C/W FIM 24-31 FAULT TREE 803 MESSAGE CLEARED. FOUND BATTERY CHARGER CONNECTOR LOOSE, SECURED CONNECTOR.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 94,200 hrs · 18,026 cycles

RIGHT AFT FUEL PUMP CAUTION MESSAGE ON GROUND. TRANSFERRED TO MEL 28-22-01 MDDR 98078 CAT "C".

Part: DUCT — DAMAGED (E&E BAY) · airframe 94,193 hrs · 18,025 cycles

RIGHT EICAS COOLING AIR DUCT DAMAGED RESULTING IN INSUFFICIENT EICAS COMPUTER COOLING. COMPLETED PART 1 TEMPORARY REPAIR PER EO 6721A013 ITEM REQUIRES RE-INSPECTION (PART2).

Part: FIRE LOOP — DEFECTIVE (LT ENGINE) · airframe 94,168 hrs · 18,021 cycles

STATUS MESSAGE LT ENG FIRE LP 1. REMOVED AND REPLACED FIRE LOOP LEFT ENGINE IAW AMM 26-11-00.

Part: SHUTOFF VALVE — MALFUNCTIONED (BLEED AIR SYS) · airframe 94,137 hrs · 18,013 cycles

RT ENG HPSOV EICAS MESSAGES. BLEED LIGHT ANNUNCIATION WHEN THRUST REDUCED. REPLACED RIGHT ENG HPSOV CONTROLLER IAW AMM 36-11-08, OPS CHECK. S/N OFF 2D17101114 P/N 773289-15. REPLACED RIGHT ENG HPSOV IAW AMM 36-11-07, OPS CHECK OK.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 94,107 hrs · 18,008 cycles

RT ENG HPSOV EICAS MESSAGE IN FLIGHT, FOLLOWED QRH. RESET HPSOV MESSAGE, RAN BITE CHECK. OPS CHECK OK IAW 36-10-00.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 93,998 hrs · 17,982 cycles

FWD CARGO COMPT SHEAR TIE AT STA 566 (BILGE) BETWEEN S39L AND S39R HAS CORROSION. REMOVED AND REPLACED SHEAR TIE AT STA 566 BETWEEN S39L AND S39R PER SRM 51-40-05-06-0.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 93,998 hrs · 17,982 cycles

AFT CARGO COMPT BILGE FRAME AT STA 197+88 RBL48 HAS CORROSION. REMOVED CORROSION BEYOND LIMITS PER SRM 53-00-07-1A-1 FIG 101 ITEM D. FABRICATED AND INSTALLED REPAIR ANGLE & SHIM PER SRM 53-00-07-2R-4 REPAIR 4.

Part: CHIP DETECTOR — CONTAMINATED (APU) · airframe 93,998 hrs · 17,982 cycles

APU COMPRESSOR CHIP DETECTOR WAS FOUND TO HAVE SILVER COLOR PARTICLES PER TC A-49-014-C1. DRAINED FILLED APU OIL PER AMM 49-27-00-608. ACCOMPLISHED ECM 2018P-615, NO PARTICLES FOUND AFTER APU RUN.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 93,998 hrs · 17,982 cycles

FUSELAGE FRAME STRUCTURE AT FWD CARGO COMPT BELOW FLOOR STA742 BETWEEN S35L AND 38R HAS CORROSION. REMOVED, FABRICATED AND INSTALLED REPAIR CHORD AND SHEAR TIE AT STA 742 BETWEEN S35L AND 38R PER DWG 140T2102 SRM 53-00-07-1A-2 AO2 REV107 FIG 101 DETAIL II AND V.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 93,998 hrs · 17,982 cycles

MAIN CABIN STA 287 BETWEEN LBL6 AND LBL 20 FLOORBEAM UPPER T-CAP CORRODED. UPON FURTHER INSP FOUND CORROSION ON EXISTING REPAIR DOUBLER. REMOVED FABRICATED AND INSTALLED REPAIR DOUBLER AT STA 287 BETWEEN LBL6 AND LBL20 PER SRM 53-00-51-2R-2 AND SRM 51-40-02-06-0.

Part: RIB — CHAFED (NR 1 COWLING) · airframe 93,998 hrs · 17,982 cycles

NR 1 ENGINE CORE COWL O/B 2ND RIB FROM FWD CHAFED. REMOVED FABRICATED & INSTALLED NR 1 ENGINE O/B CONE COWL 2ND RIB FROM FWD PER SRM 54-42-02-1R-2 REPAIR 2.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 93,998 hrs · 17,982 cycles

FWD CARGO COMPT AND SHEAR TIE AT STA 645 (BILGE AREA) HAS CORROSION BETWEEN STR 36R AND STR 35R. REMOVED AND REPLACED FWD CARGO COMPT SHEAR TIE AT STA645 (BILGE AREA) STR BETWEEN STR 36R AND STR35R PER SRM 51-40-05-06-0.

Part: IMPELLER — BROKEN (EQUIP FAN) · airframe 93,998 hrs · 17,982 cycles

FWD EQUIP BAY FAN HAS BROKEN IMPELLER. REMOVED AND REPLACED FWD EQUIP BAY FAN AMM 21-58-06. OPS CHK GOOD.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 93,998 hrs · 17,982 cycles

CORROSION ON FWD CARGO COMPARTMENT SHEAR TIE ON FRAME AT STA 120 BETWEEN STR 37L AND 38L. REMOVED, FABRICATED AND INSTALLED NEW SHEAR TIE ON FWD CARGO COMPARTMENT FRAME AT STA 720 BETWEEN STR 37L AND STR 38L PER SRM 51-40-02-06-0.

Part: PANEL — DAMAGED (LT WING) · airframe 93,998 hrs · 17,982 cycles

LT WING L/E PANEL545AL HAS DAMAGED SCREW HOLES IN 2 PLACES. ACCOMPLISHED REPAIR ON LT WING L/E PANEL 545AL PER EA 767-5731-28-A7356 I/R.

Part: WARNING SWITCH — FAILED (CABIN PRESSURE) · airframe 93,998 hrs · 17,982 cycles

CABIN ALTITUDE WARNING SWITCH FAILED FUNCTIONAL CHECK PER TC A-21-012-01. REMOVED AND REPLACED CABIN ALTITUDE WARNING SWITCH PER AMM 21-33-05. OPS CHECK GOOD.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 93,998 hrs · 17,982 cycles

FWD CARGO COMPT SHEAR TIE AT STA 654 & 44 BETWEEN S39L & S39R HAS CORROSION. REMOVED & REPLACED SHEAR TIE AT STA654 & 44 S39L & 39R PER SRM 51-40-05-06-0.

Part: SKIN — CHAFED (RT WING) · airframe 93,998 hrs · 17,982 cycles

RT WING L/E PLATE AFT OF PNL 611GB HAS CHAFING. CHAFFING DAMAGE BEYOND LIMITS PER SRM 57-41-01-1A-1. REMOVED L/E SKIN AFT OF PNL 611GB WITH PLATE P/N114 T101BU10.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 93,998 hrs · 17,982 cycles

MAIN CABIN FLOORBEAM UPPER CHORD STA 654+121 LBL 75 HAS CORROSION. ACCOMPLISHED REPAIR ON MAIN CABIN FLOORBEAM UPPER CHORD STA 654+121 LBL 75 PER EA 767-5340-28-A7334 IR REF NRC A043198.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 93,998 hrs · 17,982 cycles

MAIN CABIN FLOOR SEAT RACK HAS CORROSION STA 348 TO 370 RBL 46. REMOVED, FABRICATED AND INSTALLED NEW SEAT TRACK SECTION AT MAIN CABIN FLOOR STA 348 TO STA 429 PER SRM 51-40-02-06-0 AND SRM 53-00-52-2R.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 93,998 hrs · 17,982 cycles

AFT CARGO BILGE AREA FRAME AT STA 1197 LBL44 TO RBL44 HAS CORROSION. REMOVED AND REPLACED FRAME CHORD AT AFT CARGO COMP BILGE STA1107 LBL 44 TO RBL 44 PER SRM 51-40-02-06-0.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 93,998 hrs · 17,982 cycles

FWD CARGO COMPT SHEAR TIE ON FRAME AT STA 588 BETWEEN STR39L & 39R. REMOVED SHEAR TIE A FRAME STA 588 BETWEEN S39L & S39R. FABRICATED AND INSTALLED REPAIR SHEAR TIE AT STA 588 BETWEEN S39L AND S39R PER SRM 51-30-01 & SRM 51-21-01.

Part: FRAME SPLICE — CORRODED (FUSELAGE) · airframe 93,998 hrs · 17,982 cycles

CORROSION ON FUSELAGE FRAME SPLICE AT MAIN CABIN STA 554 BETWEEN STA 16L AND 17L. REMOVED, LOCATED AND DRILLED AND INSTALLED FUSELAGE FRAME SPLICE AT MAIN CABIN STA 544 BETWEEN STA 554 BETWEEN STA 16L AND 17L PER SRM 51-40-02-06-0.

Part: FAIRING — CHAFED (THRUST REVERSER) · airframe 93,998 hrs · 17,982 cycles

NR 1 ENG OTBD TR BULLNOSE FAIRING IS CHAFED IN 3 PLACES BETWEEN 9 AND 11 O'CLOCK POSITION. ACCOMPLISHED REPAIR ON NR 1 ENG OTBD TR BULLNOSE FAIRING PER EA 767-7832-28-A7363 I/R AND EO 6778A046.

Part: SKIN — CHAFED (LE SLAT) · airframe 93,998 hrs · 17,982 cycles

RT WING SLAT NR 11 INNER SURFACE HAS 4EA AREAS OF CHAFING AND BARE METAL. CUTOUT DAMAGED AREA ON RT WING NR 11 SLAT 2.5'X4' HONEYCOMB 2.5"X4" FABRICATED REPAIR DOUBLERS AND FILLERS AND INSTALLED PER SRM 57-43-02-2R-1 AND 51-70-10 PARA 14 AND 5.

Part: SKIN — CORRODED (CABIN DOOR) · airframe 93,998 hrs · 17,982 cycles

MAIN CABIN HATCH DOOR SKIN IS CORRODED OUT STA 1518 TO 1540. REMOVED FABRICATED AND INSTALLED MAIN CABIN HATCH DOOR UPPER SKIN PER DWG 414TM3222.

Part: VALVE — FAULTY (AC BAY) · airframe 93,998 hrs · 17,982 cycles

AUX FWD TRIM AIR VALVE SHOWS BLANK INTERMITTENTLY ON EICAS. REMOVED AND REPLACED AUX FWD AIR TRIM MOTOR VALVE ASSY PER AMM 21-61-07-004-006 AND 21-61-07-404-041. OPS CHECK GOOD.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 93,998 hrs · 12,982 cycles

AFT CARGO BILGE FRAME ANGLE AT STA 1197+132 AT LBL13 HAS CORROSION. REMOVED AND REPAIRED AFT CARGO COMP SHEAR TIE ANGLE AT STA 1197+132 AT LBL13 PER SRM 51-40-02-06-0.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 93,998 hrs · 17,982 cycles

CORROSION ON MAIN CABIN SEAT TRACK INBD FLANGE AT STA 358 LBL 54. REMOVED AND REPLACED MAIN CABIN SEAT TRACK FROM STA 340 TO STA 423 PER DWG 4175120 AND SRM 51-40-02-06-0.

Part: TIP CAP — DAMAGED (RT HORIZ STAB) · airframe 93,998 hrs · 17,982 cycles

RT HORIZ STAB T/E OUTB/D TIP HAS DAMAGE. ACCOMPLISHED EA 767-5510-28-A7315.

Part: SMOKE DETECTOR — INOPERATIVE (E&E BAY) · airframe 93,998 hrs · 17,982 cycles

TEST OF EQUIP COOLING SWITCH, FWD EQPT SMOKE MESSAGE ON EICAS DID NOT APPEAR AND SMOKE ANNUNCIATION LIGHT DID NOT ILLUMINATE. REMOVED AND REPLACED EQUIPMENT COOLING SMOKE DETECTOR T5164 PER AMM 21-58-19-002-042 AND 21-58-19-422-11 OPS CHECK GOOD.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 93,998 hrs · 17,982 cycles

FWD ENTRY DOOR CUTOUT LWR SILL UPPER SURFACE HAS 2EA CRACKED BRACKET. REMOVED 2EA CRACKED BRACKET PER SRM 57-40-02-06-0. FABRICATED AND INSTALLED 2EA BRACKET AT FWD ENTRY DOOR CUTOUT LWR SILL UPPER SURFACE PER AWG 5602 AND 141T8310.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 93,998 hrs · 17,982 cycles

MAIN CABIN SEAT TRACK AT STA358-384 RBL 11 HAS CORROSION. REMOVED, FABRICATED AND INSTALLED MAIN CABIN SEAT TRACK AT 358 TO STA400 PER DWG 141T5120.

Part: SKIN — DELAMINATED (RT ELEVATOR) · airframe 93,998 hrs · 17,982 cycles

RT INBD ELEVATOR LOWER SURFACE IS DELAMINATED AREA APPROX 34" FROM INBD END AND 12" FROM T/F. ACCOMPLISHED REPAIR ON RT INBD ELEVATOR LOWER SKIN PER EO 1955A038 REV 0.

Part: FRAME — CORRODED (FUSELAGE) · airframe 93,998 hrs · 17,982 cycles

FWD CARGO FRAME WEB STA 720 BETWEEN STA 37L-38L CORRODED. ACCOMPLISHED BLENDOUT REPAIR ON FWD CARGO FRAME W86 STA 720 BETWEEN STA STA 37L AND 38L PER EA 767-5310-28-A7332I.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 93,998 hrs · 17,982 cycles

CORROSION ON MAIN CABIN SEAT TRACK CROWN LBL88 STA 472 TO 554. REMOVED AND REPLACED MAIN CABIN SEAT TRACK AT STA 432 TO STA 621 PER SRM 51-40-02-06-00 AND DWG 143T5200.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 93,998 hrs · 17,982 cycles

FWD CARGO COMPT SHEAR TIE ON FRAME STA (BILGE AREA) BETWEEN S34L AND S35L HAS CORROSION. REMOVED AND REPLACED SHEAR TIE AT BILGE AREA FRAME STA 654 BETWEEN S34L AND S35L PER SRM 51-40-05-06-0.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 93,998 hrs · 17,982 cycles

FWD CARGO COMPT SHEAR TIE ON FRAME AT STA 720. (BILGE AREA) BETWEEN S34L AND S35L HAS CORROSION. REMOVED AND REPLACED CORRODED SHEAR TIE AT FWD CARGO COMPT FRAME AT 720 (BILGE AREA) BETWEEN S34L AND S35L PER SRM 51-40-02-06-0.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 93,998 hrs · 17,982 cycles

CORROSION ON FWD CARGO COMPARTMENT SHEAR TIE ON FRAME AT STA 698 BETWEEN STR 37L AND 38L. REMOVED, FABRICATED AND INSTALLED SHEAR TIE IN FWD CARGO COMP AT STA 698 BETWEEN STR 37L AND 38L PER 51-40-02-06-0 AND DWG 140T2102.

Part: SKIN — CORRODED (LE SLAT) · corrosion level 2 · airframe 93,998 hrs · 17,982 cycles

RT WING SLAT NR 11 HAS CORROSION ON UPPER SURFACE I/B SLAT TRACK. REMOVED CORRODED DOUBLER ON RT WING SLAT NR 11 PER SRM 51-70-10 PALA7. FABRICATED & INSTALLED REPAIR DOUBLER AND FILLER PER SRM 57-43-02-01-1 DETAILIII & SRM 57-43-02-02 R.

Part: LENS — CRACKED (COCKPIT) · airframe 93,998 hrs · 17,982 cycles

CABIN ALTITUDE LIGHT ON P5 PANEL IS CRACKED AND DOES NOT ILLUMINATE. REMOVED AND REPLACED CABIN ALTITUDE LENS/LED CAP MODULE PER AMM 33-13-00-862-06T OPS CHECK GOOD.

Part: WIRE — BROKEN (ANIT-ICE SYSTEM) · airframe 93,998 hrs · 17,982 cycles

NR 2 ENGINE ANTI-ICE PRESSURE SWITCH GIVES NO INDICATION ON EICAS DURING TEST. REPAIRED BROKEN WIRES D4252J & D742 (W375-100-10) SPLICED BROKEN WIRES (W375-100-18) RING OUT GOOD PER WPM 20-10-13. EICAS CHECK GOOD.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 93,998 hrs · 17,982 cycles

AFT CARGO COMPT BILGE FRAME AT STA 1197 RBL 48 HAS CORROSION. REMOVED AND REPLACED CORRODED SHEAR TIE AT BILGE STA 1197 RBL40 PER SRM 53-00-07-2R-4 FIG 201.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 93,998 hrs · 17,982 cycles

MAIN CABIN SEAT TRACK CORRODED AT I/B AND OBD FLANGES STA 358 TO 373 LBL 33. REMOVED, FABRICATED AND INSTALLED SEAT TRACK SECTION IN MAIN CABIN STA 360 TO STA 422 PER SRM 51-40-02-06-0 AND SRM 53-00-52-2R.

Part: PRESSURE SWITCH — CORRODED (ANTI-ICE SYSTEM) · airframe 93,998 hrs · 17,982 cycles

NR 2 ANTI-ICE PRESSURE SWITCH CORRODED, NR 2 ENGINE. REMOVED AND REPLACED NR 2 ENGINE ANTI ICE PRESSURE SWITCH PER AMM 30-21-404-022 AND 30-21-01-004. OPS CHECK GOOD.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 93,998 hrs · 17,982 cycles

BULK CARGO FLOOR SUPPORT ANGLE IS CORRODED AT STA 1417 RBL36. REMOVED, FABRICATED AND INSTALLED BULK CARGO FLOOR SUPPORT ANGLE STA 1417 RBL36 PER SRM 51-40-02-06-0 AND DWG N45T2506.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 93,998 hrs · 17,982 cycles

MAIN CABIN SEAT TRACK AT STA 358-384 LBL 11 HAS CORROSION. REMOVED, FABRICATED AND INSTALLED MAIN CABIN SEAT TRACK AT 346 TO STA 422 LBL11 PER DWG 141T5120.

Part: SKIN — CHAFED (NR 2 PYLON) · airframe 93,998 hrs · 17,982 cycles

NR 2 PYLON FAN COWL SEGMENT SUPPORT BEAM UPPER SKIN CHAFED. ACCOMPLISHED BLENDOUT REPAIR ON NR 2 PYLON FAN COWL SEGMENT SUPPORT BEAM UPPER SKIN PER EA 767-5452-28-A7325IR.

Part: BARREL — CRACKED (THRUST REVERSER) · airframe 93,998 hrs · 17,982 cycles

NR 1 OTBD TR INNER BARREL UPPER FAIRING CRACKED. REMOVED AND INSTALLED NEW NR 1 OTBD TR INNER BARREL UPPER AFT FAIRING PER B767-5140-02-06-0 REF NRC A042191.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 93,998 hrs · 17,982 cycles

AFT ENTRY DOOR COUTOUT LOWER SILL UPPER SURFACE HAS 2 CRACKED BRACKETS. REMOVED AND REPLACED AFT ENTRY DOOR LOWER SILL 2EA BRACKETS PER SRM 51-40-02-06-0.

Part: SKIN PANEL — CHAFED (LT WING) · airframe 93,998 hrs · 17,982 cycles

LT WING L/B LOWER SURFACE IS CHAFED BELOW NR 6 SLAT. REMOVED AND REPLACED SKIN PANEL/PLATE BELOW NR 6 SLAT ON LT WING PER SRM 5140-02-06-0.

Part: ANGLE — CHAFED (LT WING) · airframe 93,998 hrs · 17,982 cycles

LT WING L/B FUELING DOOR INNER ANGLE CHAFED. REMOVED AND REPLACED LT WING FUEL DOOR ANGLE BRACKET PER SRM 51-40-02-06-0.

Part: CLAMP — FAILED (PNEUMATIC DUCT) · airframe 93,900 hrs · 17,960 cycles

APU INOPERATIVE. REMOVED AND REPLACED THE PNEUMATIC DUCT CLAMP ON APU PNEUMATIC OUTPUT DUCT AND OPS CHECKED GOOD IAW AMM 36-00-00 .

Part: CLAMP — BROKEN (APU) · airframe 93,900 hrs · 17,960 cycles

APU PNEUMATIC INOPERATIVE. TROUBLESHOT AND FOUND THE AIR SUPPLY DUCT CLAMP BROKEN.

Part: WARNING MESSAGE — FALSE ACTIVATION (FUEL PUMP) · airframe 93,841 hrs · 17,947 cycles

CENTER RIGHT FUEL PUMP EICAS WITH CENTER FUEL IN FLIGHT. OPS CHECKED IAW AMM 28-22-00, COULD NOT DUPLICATE.

Part: WARNING MESSAGE — ILLUMINATED (EQUIP COOLING) · airframe 93,841 hrs · 17,947 cycles

AFTER TAKEOFF, FWD EQUIPMENT COOLING EICAS, QRH EQUIPMENT COOLING STBY. ACCOMPLISHED AN ADJUSTMENT AND TEST OF THE EQUIPMENT COOLING SYSTEM IAW AMM 21-53-00.

Part: CONTROL VALVE — MALFUNCTIONED (APU) · airframe 93,852 hrs · 17,949 cycles

APU AUTO SHUTDOWN WITH A REVERSE FLOW MESSAGE. REMOVED AND REPLACED THE APU SURGE CONTROL VALVE IAW AMM 49-53-01, OPS CHECKED NORMAL.

Part: IGNITER — INOPERATIVE (APU) · airframe 93,854 hrs · 17,950 cycles

APU WOULD NOT IGNITE. R&R IGNITER ON APU REF AMM 49-41-02 OPS CK NORMAL.

Part: CONTROL VALVE — FAULTY (APU) · airframe 93,854 hrs · 17,950 cycles

APU AUTO SHUTDOWN. REMOVED AND REPLACED APU SURGE CONTROL VALVE REF AMM 49-53-01 OPS CHECK NORMAL.

Part: APU — SHUTDOWN · airframe 93,823 hrs · 17,943 cycles

APU AUTO SHUTDOWN, UNABLE RESTART. REMOVED AND REPLACED THE APU AND OPS CHECKED GOOD IAW AMM 49-11-01.

Part: FILTER — WARNING MESSAGE (RT ENGINE FUEL) · airframe 93,831 hrs · 17,945 cycles

RIGHT ENGINE FUEL FILTER EICAS MESSAGE DURING CLIMB. MESSAGE DISAPPEARED AFTER 2 MINUTES. REPLACED THE FUEL FILTER IAW AMM 73-11-02 IAW FIM 73-11-FT803. OPS AND LEAK CHECKED GOOD.

Part: VALVE — MALFUNCTIONED (LT ENGINE) · airframe 93,831 hrs · 17,945 cycles

LEFT ENGINE BLEED OVERHEAT, QRH PROCEDURES COMPLETED. REMOVED AND REPLACED THE LEFT ENGINE FAN AIR VALVE IAW AMM 36-11-16. OPS CHECKED GOOD.

Part: WARNING MESSAGE — FALSE ACTIVATION (LT PNEUMATIC) · airframe 93,812 hrs · 17,940 cycles

EICAS MESSAGE FOR THE LT BLEED OVERHEAT FOLLOWED BY LT BLEED VALVE CLOSED, COMPLIED WITH QRH PROCEDURE AND RESUMED NORMAL OPS. PERFORMED A BITE IAW 36-20-01, FAULT TREE 802, OPS CHECKED OK.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHTS) · airframe 93,804 hrs · 17,939 cycles

EMERGENCY LIGHTS INOPERATIVE AT SEATS 37H AND 38H. CONNECTED THE CONNECTORS AT SEATS 37H AND 38H AND CHECKED GOOD IAW 33-51-00.

Part: PUMP — MALFUNCTIONED (FUEL BOOST) · airframe 93,551 hrs · 17,885 cycles

APU SHUTDOWN DURING PILOTS PRE FLIGHT INSPECTION, WHILE TURNING ON FUEL BOOST PUMPS. PERFORMED A BCPU BITE CHECK, RESET FAULT, APU RESTART COMPLIED WITH IAW 49-61-00.

Part: IDG — FAILED (RT GENERATOR) · airframe 93,555 hrs · 17,887 cycles

RIGHT GENERATOR DRIVE EICAS MESSAGE WHEN GOING TO IDLE FOR DESCENT. REMOVED AND REPLACED THE NR 2 ENG IDG IAW AMM 24-11-01-404-024, OPS AND LEAK CHECKED SATISFACTORY.

Part: IDG — DISCONNECTED (RIGHT) · airframe 93,536 hrs · 17,881 cycles

RIGHT GENERATOR DRIVE EICAS MESSAGE. RECONNECTED THE RT IDG, SERVICED & OPS CHECKED IAW AMM 24-11-00 & AMM 12-13-03.

Part: TERMINAL — BROKEN (FIRE LOOP) · airframe 93,478 hrs · 17,867 cycles

RIGHT ENGINE FIRE LOOP 1 STATUS MESSAGE. REPLACED BROKEN TERMINAL AT AFT LOWER FIRE LOOP IAW AMM 20-51-00.

Part: CONNECTOR — UNSECURE · airframe 93,367 hrs · 17,843 cycles

STATUS MESSAGE FOR THE RIGHT ENGINE CONTROL, CAUTION MESSAGE ON LANDING. FOUND A LOOSE CONNECTOR AT P114. SEATED AND SECURED THE CONNECTOR. OPS CHECKED IAW AMM 71-00-01 TASK A87-A88.

Part: SHUTOFF VALVE — MALFUNCTIONED (RT ENGINE) · airframe 93,249 hrs · 17,817 cycles

RIGHT ENGINE BLEED OFF EICAS MESSAGE ON IDLE DURING DESCENT APPROXIMATLEY 8 DIFFERENT MESSAGES DURING DESCENT PHASE. OPS CHECKED PRSOV IAW 36-11-09, PERFORMED FIM 36-10-08. NO FAULTS FOUND INSPECTED. VISUALLY PRSOV NO PROBLEMS FOUND. REMOVED AND REPLACED THE RT ENGINE HPSOV IAW AMM 36-11-07, TESTED OK. REMOVED AND REPLACED THE RT ENGINE HPC IAW AMM 36-11-08, TESTED OK.

Part: STARTER — MALFUNCTIONED (NR 2 ENGINE) · airframe 93,176 hrs · 17,802 cycles

NR 2 ENGINE STARTER MOTOR UNABLE TO SEDUCE. REMOVED AND REPLACED THE STARTER MOTOR . OPS CHECKED NORMAL IAW AMM 80-11-01.</P>)

Part: INTAKE DUCT — DAMAGED (LT ENGINE) · airframe 93,176 hrs · 17,802 cycles

LEFT ENGINE OTBD THRUST REVERSER FAN AIR VALVE INTAKE DUCT HAS A THREE HOLE. REMOVED AND REPLACED THE INTAKE DUCT IAW AMM 36-11-01.

Part: LIGHT — INOPERATIVE (EMERGENCY LIGHT) · airframe 93,176 hrs · 17,802 cycles

EMERGENCY LIGHT AT SEAT 21 A AND C INOPERATIVE. REPAIRED IAW SWPM 20-10-13

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 93,176 hrs · 17,802 cycles

EMERGENCY LIGHTS BY SEAT 17K INOPERATIVE. REPLACED THE LAMPS. OPS CHECKED GOOD IAW AMM 33-51-00.

Part: WARNING MESSAGE — FALSE ACTIVATION (WX RADAR SYS) · airframe 92,992 hrs · 17,763 cycles

DURING FLIGHT, WEATHER FAIL WARNING DISPLAYED ON ND. WEATHER RADAR SYSTEM STATUS MESSAGE DISPLAYED. SWITCHED TO SYSTEM NR 2 TO RESUME RADAR DISPLAY. PERFORMED AN OPS CHECK IAW AMM 34-45-00. NO PROBLEMS FOUND.

Part: CONNECTOR — DIRTY (OIL SYSTEM) · airframe 93,016 hrs · 17,768 cycles

"L OIL FILTER" STATUS MESSAGE INDICATED AFTER START. INSPECTED OIL FILTER DIFFERENTIAL PRESSURE SWITCH, CLEANED CONNECTOR & OPS CHK GOOD IAW AMM 79-35-01.

Part: CONTROL VALVE — FAULTY (AC BAY) · airframe 93,014 hrs · 17,767 cycles

RT PACK OFF INOP. R&R RT FLOW CONTROL VALVE. OPS CK GOOD IAW AMM 21-51-00.

Part: RADAR — FAILED (WX SYSTEM) · airframe 92,940 hrs · 17,750 cycles

NR 1 AND 2 WEATHER RADARS FAILED ON ND. STATUS MESSAGE. PERFORMED A BITE CHECK AND OPS CHECK OF THE WEATHER RADAR IAW AMM 34-43-00. FAIL WS MODE AND W/S WX MODE ARE INOPERATIVE IAW AMM.

Part: LIGHT — INOPERATIVE (ROW 12D) · airframe 92,929 hrs · 17,749 cycles

EMERGENCY LIGHT INOPERATIVE AT ROW 12D. REMOVED AND REPLACED THE EMERGENCY LIGHT ASSY IAW AMM 33-51-10. OPS CHECKED NORMAL.

Part: RADAR — UNKNOWN (NR 1 WX SYSTEM) · airframe 92,940 hrs · 17,750 cycles

NR 1 WEATHER RADAR SYSTEM FAILED EN ROUTE. COULD NOT DUPLICATE. PERFORMED RADAR BITE CHECK IAW AMM 34-43-00. OPS CHECKED OK.

Part: WARNING MESSAGE — FALSE ACTIVATION (ANTI ICE SYSTEM) · airframe 92,892 hrs · 17,740 cycles

DURING CLIMB AT 10.000 FT MSL, AN INTERMITTENT LEFT WING ANTI-ICE MESSAGE. PERFORMED A GROUND TEST IAW AMM 30-11-02. OPS CHECKED GOOD.

Part: PRESSURE SWITCH — FAILED (ANTI ICE SYS) · airframe 92,882 hrs · 17,739 cycles

LEFT WING ANTI-ICE MESSAGE INTERMITTENT DURING CLIMB OUT. COMPLIED WITH QRH. REMOVED AND REPLACED THE LT WING ANTI-ICE PRESSURE SWITCH IAW AMM 30-11-04. OPS TESTED NORMAL ON GROUND.

Part: WARNING MESSAGE — FALSE ACTIVATION (LT ENGINE) · airframe 92,872 hrs · 17,737 cycles

LEFT ENGINE OIL FILTER STATUS MESSAGE AFTER ENGINE START. INSPECTED LEFT ENGINE OIL BYPASS SYSTEM AND OPS CHECKED GOOD IAW AMM 79-35-00</P>)

Part: CONNECTOR — UNKNOWN (START SWITCH) · airframe 92,700 hrs · 17,704 cycles

DURING PUSHBACK, THE RIGHT ENGINE START SWITCH WILL NOT ENGAGE IN THE GROUND POSITION. REMOVED THE CONNECTOR ON P94 FROM START VALVE. CONNECTED THE CONNECTOR AND OPS CHECKED OK IAW AMM 80-12-00.

Part: CONNECTOR — CORRODED (PRESSURE SWITCH) · airframe 92,687 hrs · 17,701 cycles

RIGHT CENTER FUEL PUMP NO LOW PRESSURE LIGHT INDICATION OR ASSOCIATED EICAS WITH TANK EMPTY. CLEANED CORROSION FROM CONNECTOR S-424. OPS CHECKED IAW AMM 28-42-00. NO DEFECTS NOTED.

Part: TRANSCEIVER — INOPERATIVE (WX RADAR SYS) · airframe 92,606 hrs · 17,682 cycles

NR 1 WEATHER RADAR INOPERATIVE. REMOVED & REPLACED THE RADAR RT IAW AMM 34-43-01, OPS CHECKED NORMAL.

Part: WARNING MESSAGE — FALSE ACTIVATION (WEATHER RADAR) · airframe 92,644 hrs · 17,692 cycles

DURING FLIGHT, LENS WEATHER RADAR FAILED LEFT AND RIGHT. OPS CHECKED THE NR 2 WEATHER RADAR GOOD IAW 34-43-00.

Part: BATTERY PACK — CORRODED (EMERGENCY LIGHTS) · airframe 92,606 hrs · 17,682 cycles

EXTERIOR EMERGENCY LIGHTS INOPERATIVE ON RT SIDE OF ACFT, AFT OF FLAPS. FOUND CORROSION ON THE F1 OF POWER PACK, CLEANED CORROSION, OPS CHECKED OK IAW AMM 33-51-00.

Part: WARNING MESSAGE — FALSE ACTIVATION (WX RADAR) · airframe 92,606 hrs · 17,683 cycles

DURING FLIGHT, EICAS FOR THE WEATHER RADAR FAILED, LEFT AND RIGHT RADAR. OPS CHECKED THE NR 2 WEATHER RADAR WAS GOOD IAW AMM 34-43-00. PERFORMED ACTION PLAN AP-13754 AND FIM 34-43 FT 805 SYSTEM OPS CHECKED NORMAL.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT) · airframe 92,644 hrs · 17,692 cycles

EMERGENCY LIGHT INOPERATIVE AT MID CABIN LAVATORY AND ROWS 20AC, 21AC. REPLACED THE LAMPS IN THE MID CABIN LAVATORY FLOOR AND SECURED THE CONNECTOR AT SEATS 20 AND 21 IAW AMM 33-51-00.

Part: WARNING MESSAGE — ILLUMINATED (FUEL PUMP) · airframe 92,606 hrs · 17,682 cycles

FUEL JET PUMP EICAS MESSAGE INOPERATIVE.

Part: WARNING MESSAGE — ILLUMINATED (WX RADAR) · airframe 92,491 hrs · 17,659 cycles

WEATHER RADAR FAILED MESSAGE.

Part: WARNING MESSAGE — FALSE ACTIVATION (RT ENGINE CONTRO) · airframe 92,446 hrs · 17,650 cycles

R ENG CONTROL ADVISORY AND STATUS MESSAGE DISPLAYED AFTER LANDING&NBSP;(<P>C/W FIM 73-21 FT 878 NO FAULTS INDICATED&NBSP;</P>)

Part: OIL SYSTEM — OVERSERVICED (APU) · airframe 92,444 hrs · 17,649 cycles

2 ATTEMPTS APU STARTS IN AIR UNSUCCESSFUL(<P>INSPECTED APU OIL LEVEL IAW AMM 12-13-04 FOUND OVER SERVICED. REMOVED 1 QT AND RAN APU. OPS CHECK GOOD.</P>)

Part: RECEIVER — INOPERATIVE (WX RADAR SYS) · airframe 92,444 hrs · 17,649 cycles

# 1 RADAR SYSTEM INOP&NBSP;(<P>TRANSFERRED TO MDDR # 87000 AS PER MEL 34-43-01 CAT D&NBSP;</P><P>REF LOG PAGE 928116 ITEM M7, PERFORMED BITE TEST PER FIM 34-43 FT 805 BITE TEST GOOD, REMOVED AND REPLACED WEATHER RADAR RECEIVER PER MCC REQUEST IAW AMM 34-43-01. OPS CHECK GOOD. BITE CHECK. THIS CLEARS MDDR 87000&NBSP;</P>)

Part: APU — MALFUNCTIONED · airframe 92,431 hrs · 17,646 cycles

APU FAULT EICAS MESSAGE . 3 ATTEMPTS NO START. CREW REPORTED A SUCCESSFUL COLD SOAK START.

Part: CONNECTOR — DIRTY (SHUTOFF VALVE) · airframe 92,619 hrs · 17,687 cycles

LEFT A/C PACK OFF AND SHUTOFF VALVE DID NOT DISPLAY WITH PACK OFF. CLEANED AND REINSTALLED THE CONNECTORS ON HIGH FLOW AND SHUT OFF VALVE. OPS CHECKED OK IAW AMM 21-81-00.

Part: CIRCUIT BREAKER — MALFUNCTIONED (SPAR VALVE) · airframe 92,398 hrs · 17,642 cycles

LEFT ENGINE SPAR VALVE FAILED OPERATIONAL CHECK. RE-SET C/B PERFORMED OPERATION CHECK REF AMM 28-22-00 SYSTEM CK NORMAL 3 FLIGHTS.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 92,398 hrs · 17,642 cycles

SMALL EMERGENCY LIGHT ABOVE AFT MOST LEFT SIDE EXIT DOOR INOP(<P>REPLACED M734 BATTERY PACK CHARGER IAW AMM 33-51-07. OPS CHECK NORMAL</P>)

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 92,398 hrs · 17,642 cycles

EMERGENCY LIGHTS INOP AT SEATS 38H, 39H, 24H, 20C AND 21C(<P>REPLACED M734 BATTERY PACK CHARGER IAW 33-51-07</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (EEC) · airframe 92,398 hrs · 17,642 cycles

EEC2 STATUS MSG RT PIMU 353 14-8 VSV FEED BACK.(<P>PERFORMED T/S IAW FIM 71-01 TASK A61-A62 ANDAMM 71-00-00 NO DEFECTS NOTED. SYSTEM OK<BR /></P>)

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 92,397 hrs · 17,641 cycles

EXTERNAL MAIN ENTRY DOOR LEFT SIDE EMERGENCY LIGHT INOP(<P>REMOVED AND REPLACED LAMP OPS CHECK GOOD. IAW AMM 33-51-00</P>)

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 92,398 hrs · 17,642 cycles

EMERGENCY EXIT SIGN ABOVE AFT FLT ATTENDANT STATION INOP(<P>REPLACED M734 BATTERY PACK CHARGER. OPS CHECK NORMAL. IAW AMM 33-51-00</P>)

Part: SEAL — LEAKING (PREHEATER) · airframe 92,431 hrs · 17,646 cycles

LEFT PACK REHEATER OUTLETS LEADING TO THE HEAT EXCHANGER AND OUTER OUTLET TO THE ACM LEAKING PNEUMATICS&NBSP;(<P>REMOVED AND REPLACED SEALS AT LEFT PACK REHEATER OUTLETS. NO LEAKS NOTED IAW AMM 21-51-03</P>)

Part: APU — MALFUNCTIONED · airframe 92,389 hrs · 17,639 cycles

APU FAULT EICAS MESSAGE, 3 FAILED ATTEMPTS. STARTED APU SUCCESSFULLY AFTER 10 MINUTES ON THE GROUND IAW AMM 49-11-03.

Part: WARNING MESSAGE — FALSE ACTIVATION · airframe 92,362 hrs · 17,635 cycles

AFTER LANDING, EICAS AND STATUS FOR THE RIGHT ENGINE CONTROL. CLEARED THE STATUS MESSAGE AND PERFORMED MAINTENANCE BITE ON PIMU AND EEC IAW AMM 77-35-00 AND 31-35-00, NO DEFECT NOTED.

Part: APU — MALFUNCTIONED · airframe 92,369 hrs · 17,636 cycles

APU FAULT EICAS AFTER LANDING. APU FAILED TO START. STARTED APU ON FIRST ATTEMPT IAW AMM 49-01-00, CHECKED GOOD.

Part: WIRE — CHAFED (EMERGENCY LIGHTS) · airframe 92,357 hrs · 17,633 cycles

EMERGENCY LIGHTS INOPERATIVE AT THE L2 & R2 DOORS. FOUND A CHAFED WIRE. REPAIRED IAW SWP 20-25-00. OPS CHECKED GOOD.

Part: OIL SYSTEM — UNDERSERVICED (APU) · airframe 92,357 hrs · 17,633 cycles

APU FAILED TO START AFTER LANDING. SERVICED THE APU OIL IAW AMM 12-13-54.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 92,320 hrs · 17,626 cycles

FLOOR EMERGENCY EXIT LIGHT INOPERATIVE AT THE R2 & L2 DOORS. REPLACED THE BATTERY POWER SUPPLY IAW AMM 33-51-07. CHECKED GOOD.

Part: RADAR — MALFUNCTIONED (WX SYS) · airframe 92,256 hrs · 17,611 cycles

WEATHER RADAR FAILED, SYSTEM 1. PERFORMED RADAR BITE CHECKED AND OPS CHECKED, NO FAULTS FOUND IAW MM 34-43-00.

Part: STARTER — FAILED (LT ENGINE) · airframe 92,262 hrs · 17,612 cycles

LEFT ENGINE WILL NOT START. REPLACED THE STARTER IAW AMM 80-11-01.

Part: ECU — MALFUNCTIONED (APU) · airframe 92,254 hrs · 17,609 cycles

APU FAILED TO START ON LANDING. PERFORMED BITE OF ECU, FOUND NO FAULTS, APU STARTED NORMAL AFTER BLOCK IN. OPS CHECKS APU GOOD IAW AMM 49-11-00.

Part: APU — MALFUNCTIONED · airframe 92,198 hrs · 17,601 cycles

APU WILL NOT START DURING BLOCK IN. THREE STARTS ATTEMPS SELF TERMINETED AT 800. INSPECTED APU OIL LEVEL IAW AMM 12-31-04. PERFORMED BITE ON ECU FOUND NO DATA FOR LAST SHUTDOWN . STARTED ON OPS CHECK, APU NORMAL IAW AMM 49-11-00.

Part: CONNECTOR — DIRTY (WX RADAR SYS) · airframe 92,084 hrs · 17,578 cycles

INTERMITTENT RADAR FAILURE MESSAGE. REMOVED THE NR 1 WEATHER RADAR TRANSCEIVER AND CLEANED CONNECTORS. REINSTALLED AND CHECKED GOOD IAW AMM 34-43-00.

Part: PLUG — LEAKING (SCAV PUMP) · airframe 92,072 hrs · 17,575 cycles

NR 2 ENGINE HAS OIL LEAKING FROM STARTER PAD AT GEARBOX. FOUND THE LEAK EMANATING FROM PLUG ON SCAVENGE PUMP HOUSING. TIGHTENED THE PLUG AND TORQUED IAW AMM 20-11-00 AND LEAK CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 91,993 hrs · 17,559 cycles

R2 EMERGENCY LIGHT BULB NOT WORKING. REMOVED AND REPLACED THE BULB IAW AMM 33-51-10. OPS CHECKED GOOD.

Part: COVER — UNSECURE (EMERGENCY LIGHT) · airframe 91,993 hrs · 17,559 cycles

L2 EMERGENCY LENS NOT SECURE. REPOSITION THE COVER AND SECURED IAW AMM 33-51-10. OPS CHECKED GOOD.

Part: UNKNOWN — MALFUNCTIONED (EMERGENCY LIGHT) · airframe 91,938 hrs · 17,546 cycles

EMERG LIGHTS FLASHING CONTINUOSLY IN CABIN. INSPECTED EMERGENCY LIGHTS SYSTEM CKD GOOD IAW 33-51-00.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 91,912 hrs · 17,542 cycles

DURING A POST FLIGHT INSPECTON, EXTEIOR EMERGENCY LIGHTS INOPERATIVE AT THE L1 DOOR AND GROUND FLOOD AFT OF RIGHT FLAG. R & R THE LAMPS, NORMAL OPERATION IAW MM 33-25-10.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 91,875 hrs · 17,534 cycles

ON POST FLIGHT INSPECTION, THE EXTERIOR EMERGENCY LIGHTS FOUND INOPERATIVE. L1 AND GROUND FLOOD AFT OF RIGHT FLAP. REPLACED THE LAMPS. NORMAL OPS IAW AMM 33-52-10.

Part: CONTROLLER — FAILED · airframe 91,875 hrs · 17,534 cycles

LEFT ENGINE PRV ILLUMINATED DURING CLIMB OUT, ALL INDICATIONS NORMAL. REMOVED AND REPLACED LEFT ENGINE BLEED PRINTER CIRCUIT ASSY. SYSTEM TEST PASSED, OPERATIONAL CHECKED NORMAL IAW AMM 36-11-12. REMOVED AND REPLACED THE PRV CONTROLLER IAW AMM 36-11-17. OPS CHECKED GOOD. NO DEFECTS NOTED.

Part: WARNING MESSAGE — FALSE ACTIVATION (LT ENGINE) · airframe 91,856 hrs · 17,530 cycles

LEFT ENGINE PRV MESSAGE DURING CLIMB OUT. PERFORMED AN AIR SUPPLY BITE CHECK IAW AMM 36-23-00. NO FLIGHT FAULTS FOUND. ALL INDICATION BLEED PRESSURE NORMAL IN FLIGHT.

Part: WARNING MESSAGE — FALSE ACTIVATION (LT ENGINE) · airframe 91,849 hrs · 17,528 cycles

LEFT ENGINE PRV MESSAGE DISPLAYED THROUGH OUT CLIMB. PERFORMED A BITE CHECK OF THE BLEED SYSTEM, NO DEFECTS NOTED. CLEARED PRV MESSAGE IAW MM 36-23-00.

Part: VALVE — MALFUNCTIONED (LT ENGINE) · airframe 91,837 hrs · 17,525 cycles

LEFT ENGINE PRV EICAS DURING TAKEOFF. QRH COMPLIED. REMOVED AND REPLACED PRV VALVE IAW MM 36-11-18. LEAK CHECK COMPLIED WITH 36-11-18, BITE CHECKED IAW MM 36-23-00/50.

Part: WARNING MESSAGE — FALSE ACTIVATION (LT ENGINE) · airframe 91,837 hrs · 17,525 cycles

EICAS MESSAGE FOR THE LT ENGINE PRV, QRH PROCEDURES PERFORMED. TROUBLESHOT IAW FIM AND OPS CHECKED IAW MM 36-23-00/501 AND 36-71-00. RAN ENGINES, NO DEFECTS NOTED. ACFT OK TO SERVICE.

Part: WARNING MESSAGE — FALSE ACTIVATION (LT ENG PRV) · airframe 91,837 hrs · 17,525 cycles

EICAS MESSAGE FOR THE LT ENGINE PRV. TROUBLESHOT IAW FIM. OPS CHECKED IAW AMM 36-23-00/501 & 36-11, ENG RAN, NO DEFECTS FOUND.

Part: CONNECTOR — DAMAGED (START VALVE) · airframe 91,837 hrs · 17,525 cycles

EICAS MESSAGE FOR THE LEFT ENGINE START VALVE, STARTER CUT OFF DISPLAYED. INSPECTED THE START VALVE, FOUND PUSH BACK PIN, RESEATED & OPS CHECKED IAW MM 80-11-00.

Part: PIN — DAMAGED (START VALVE) · airframe 91,813 hrs · 17,521 cycles

INTERMITTENT LEFT ENGINE STARTER CUTOUT EICAS MESSAGE , QRH LIST COMPLETED , VALVE LIGHT WAS OFF. INSPECTED START VALVE, FOUND A PUSHED BACK PIN. RESEATED AND OPS CHECKED THE START AMM 80-11-00.

Part: WIRE — DISCONNECTED (EMERGENCY LIGHT) · airframe 91,802 hrs · 17,519 cycles

EMERGENCY LIGHT SEAT 2C INOPERATIVE. RECONNECTED WIRE AND OPS CHECKED NORMAL IAW AMM 33-51-00.

Part: LAMP — INOPERATIVE (RT OVERWING) · airframe 91,802 hrs · 17,519 cycles

RT OVERWING SLIDE LIGHT INOPERATIVE. REPOSITIONED THE SLIDE LIGHT LAMP. OP CHECKED NORMAL IAW AMM 33-51-16.

Part: LIGHT — INOPERATIVE (L1 DOOR) · airframe 91,802 hrs · 17,519 cycles

L1 DOOR OUTSIDE EMERGENCY LIGHT INOPERATIVE. REPOSITIONED THE L1 DOOR EXTERIOR EMERGENCY LIGHT. OP CHECKED NORMAL IAW AMM 33-51-16.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 91,802 hrs · 17,519 cycles

OVERHEAD EMERGENCY LIGHT RH SIDE ROW 39 INOPERATIVE. REMOVED AND REPLACED THE BATTERY PACK IAW AMM 33-51-01. OP CHECKED OK.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 91,802 hrs · 17,519 cycles

RIGHT SIDE AFT OF WING MIDDLE OUTSIDE EMERGENCY LIGHT INOPERAIVE. REPOSITIONED THE EMERGENCY LIGHT. OP CHECKED GOOD IAW AMM 33-51-16.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 91,802 hrs · 17,519 cycles

RIGHT OVERHEAD EMERGENCY LIGHT, ROWS 27 TO 40 INOPERATIVE. REPLACED THE BATTERY PACK IAW AMM 33-51-07. OP CHECKED NORMAL.

Part: FIRE LOOP — MALFUNCTIONED (RT NACELLE) · airframe 91,783 hrs · 17,515 cycles

DURING A TRANSIT CHECK, FOUND RIGHT ENGINE FIRE LOOP 2 STATUS MESSAGE. REMOVED AND REPLACED RIGHT ENGINE UPPER AFT FIREWALL FIRE DETECTOR IAW AMM 26-11-00. OP CHECKED GOOD.

Part: APU — FAULTED · airframe 91,759 hrs · 17,511 cycles

APU DID NOT START, APU FAULT, 3 ATTEMPTS. OPS CHECKED IAW AMM 49-61-00, APU STARTED, NO DEFECTS NOTED.

Part: RADAR — FAULTED (WX SYSTEM) · airframe 91,748 hrs · 17,510 cycles

NR 1 WX RADAR SYSTEM DOES NOT SHOW RETURNS AT ANY ANGLE OR GAIN. PERFORMED AN OPS CHECK OF THE WEATHER RADAR IAW AMM 34-43-00, NO DEFECTS NOTED.

Part: WARNING MESSAGE — FALSE ACTIVATION (RT ENGINE) · airframe 91,726 hrs · 17,505 cycles

ON TOUCHDOWN, HAD A RT ENGINE CONTROL EICAS AND STATUS MESSAGE. PERFORMED RT PIMU BITE , NO FAULTS IAW AMM 77-35-02 , RAN THE ENGINE IAW AMM 71-00-00, SYSTEM NORMAL.

Part: WARNING MESSAGE — FALSE ACTIVATION (RT ENGINE) · airframe 91,680 hrs · 17,493 cycles

RECEIVED A RT ENGINE CONTROL EICAS MESSAGE ON ROLL OUT. OCCURED WHEN THRUST LEVERS WENT FROM REVERSE TO NORMAL. PERFORM FIM 73-21 FT 878. NO FAULTS NOTED. SYSTEM NORMAL.

Part: TRANSMITTER — ERRATIC (OIL QTY) · airframe 91,678 hrs · 17,492 cycles

DURING AN ENGINE MX RUN, DISCOVERED THE NR 1 ENGINE OIL QTY INDICATION ERRATIC. VERIFIED THE NR 1 ENGINE OIL QTY FULL. REMOVED & REPLACED THE OIL QTY TRANSMITTER IAW MM 79-31-01.

Part: LINE — LOOSE (IDG) · airframe 91,525 hrs · 17,459 cycles

OIL LEAK ON NR 2 ENGINE. FOUND LOOSE LINE ON IDG SERVICE PORT. TIGHTENED AND RAN ENGINE FOR LEAKS IAW AMM 71-00-00, NO LEAKS NOTED. ENGINE OK FOR SERVICE.

Part: START VALVE — FAILED (LEFT) · airframe 91,237 hrs · 17,395 cycles

RETURNED TO GATE FOR LT STARTER CUTOUT MESSAGE FOLLOWED BY ENGINE STARTER EICAS MESSAGE. REMOVED AND REPLACED THE LT ENGINE START VALVE IAW AMM 80-11-02 AND OPS CHECKED OK.

Part: FAN — INOPERATIVE (CARGO BAY) · airframe 91,012 hrs · 17,347 cycles

CARGO SMOKE DETECTOR. AIR STATUS MESSAGE, AFT SMOKE FAN INOPERATIVE. REMOVED AND REPLACED THE CARGO SMOKE FAN IAW AMM 26-16-02, OPS CHECKED GOOD.

Part: WARNING MESSAGE — FALSE INDICATION (WX RADAR SYS) · airframe 91,012 hrs · 17,347 cycles

WEATHER RADAR SYS STATUS MESSAGE. PERFORMED AN OPS CHECK OF THE WEATHER RADAR IAW AMM 34-43-00. NO DEFECTS NOTED.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHTS) · airframe 91,022 hrs · 17,349 cycles

DURING DAILY CHECK, FOUND EMERGENCY LIGHTS AT ROWS 19 TO 30 INOPERATIVE, LEFT SIDE OF AIRCRAFT. FOUND BATTERY CONNECTOR LOOSE, SECURED THE CONNECTOR AND OPS CHECKED NORMAL IAW AMM 33-51-00.

Part: RADAR — MALFUNCTIONED (WX SYSTEM) · airframe 90,941 hrs · 17,332 cycles

WEATHER SYSTEM NR 1 INOPERATIVE. PERFORMED FIM 34-43-FT801 AND AMM 31-41-00 SYS, OPS CHECKED NORMAL.

Part: CONNECTOR — FAILED (RT OVERHEAT LOOP) · airframe 90,878 hrs · 17,321 cycles

RIGHT ENGINE OVERHEAT LOOP 2 EICAS MESSAGE. REMOVED AND REPLACED THE CONNECTOR D2854 IAW EO 672A0005 AND SWPM 20-82-13, SYSTEM OPS CHECKED NORMAL.

Part: ENGINE — OIL CONSUMPTION (RT ENGINE) · airframe 90,879 hrs · 17,321 cycles

RT ENGINE HAD EXCESSIVE OIL CONSUMPTION. CONSUMED 6 QTS OF OIL DURING FLIGHT. NR 2 ENGINE CHANGED IAW WC E1029.

Part: LINE — LEAKING (NR 2 ENGINE OIL) · airframe 90,879 hrs · 17,321 cycles

DURING WALK AROUND, FOUND OIL LEAKING FROM THE NR 2 ENGINE. PERFORMED CHECK FOR OIL VENT LINE IAW MM 71-71-02. CAPPED DRAIN LINES.

Part: B-NUT — LOOSE (IDG OIL LINE) · airframe 90,879 hrs · 17,321 cycles

DURING A TRANSIT WALK AROUND, FOUND OIL IN IDG COMPARTMENT. FOUND A LOOSE B-NUT ON THE TRANSFER LINE. TIGHTENED AND RAN, NO OIL LEAK FOUND IAW MM 71-00-00.

Part: O-RING — FAILED (COOLING DUCT) · airframe 90,833 hrs · 17,311 cycles

LEFT MCDU IS LOSING COOLING AIR INFLIGHT, AUTO MODE. REPLACED O-RING ON EQUIPMENT COOLING DUCTS. OPS CHECKED IAW 21-58-00.

Part: FLOW SENSOR — FAILED (E/E COOLING) · airframe 90,783 hrs · 17,299 cycles

FMC CDU FAILED IN CRUISE. E/E COOLING MONITOR SHOWED NO AIRFLOW. REMOVED AND REPLACED THE LOW FLOW SENSOR TS 163 IAW AMM 21-58-17.

Part: LIGHT — INOPERATIVE (SEAT 14H) · airframe 90,771 hrs · 17,297 cycles

EMERGENCY LIGHT AT ROW 14 SEAT H INOPERATIVE. REMOVED AND REPLACED THE EMERGENCY LIGHT IAW AMM 33-51-00, OPS CHECKED NORMAL.

Part: SPINNER — DAMAGED (NR 1 ENGINE) · airframe 90,623 hrs · 17,265 cycles

DURING WALK AROUND, FOUND THE NR 1 ENGINE SPINNER MISSING PAINT. PREPARED, CLEANED, MASKED, PRIMED, AND PAINTED THE NR 1 ENGINE SPINNER BLACK WITH WHITE SWIRLE IAW SRM 51-20-01.

Part: PUMP — INOPERATIVE (FUEL BOOST) · airframe 90,579 hrs · 17,256 cycles

RIGHT AFT FUEL PUMP INOPERATIVE. REMOVED AND REPLACED RT AFT FUEL BOOST PUMP IAW MM 28-22-03. OPS AND LEAK CHECKED OK.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 90,515 hrs · 17,243 cycles

EXTERIOR EMERGENCY LIGHT ON AFT RT SIDE BEHIND FLAP INOPERATIVE. REPLACED THE LAMP IAW AMM 33-51-01, OPS CHECKED GOOD.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHT) · airframe 90,378 hrs · 17,215 cycles

FLOOR EMERGENCY LIGHTS AT SEAT 14H INOPERATIVE. REPLACED THE LAMPT AND SECURED THE WIRE CONNECTOR IAW AMM 33-51-10.

Part: WARNING MESSAGE — FALSE ACTIVATION (APU) · airframe 90,221 hrs · 17,182 cycles

APU FAULT MESSAGE. ACCOMPLISHED APU ECU BITE TEST AND TESTED OK. RESET SUCCESFUL IAW AMM 49-61-05 AND ACCOMPLISHED AN APU OPERATIONAL CHECK IAW AMM 49-11-00 AND STATUS AND OPERATED NORMAL.

Part: WARNING MESSAGE — FALSE ACTIVATION (OIL FILTER) · airframe 90,257 hrs · 17,188 cycles

LEFT OIL FILTER STATUS MESSAGE ILLUMINATED. MESSAGE ILLUMINATED MOMENTARILY DUE TO ENGINE OPERATION IN EXTREME COLD WEATHER. MESSAGE ERASED AND AIRCRAFT OK FOR SERVICE IAW AMM 71-00-00.

Part: SLIDE — INOPERATIVE (L1 DOOR) · airframe 90,084 hrs · 17,156 cycles

L1 SLIDE INOPERATIVE. REMOVED & REPLACED THE L1 DOOR SLIDE IAW AMM 25-66-01.

Part: CONNECTOR — DAMAGED (ENGINE ANTI-ICE) · airframe 90,054 hrs · 17,151 cycles

RIGHT ENGINE ANTI-ICE CAUTION MESSAGE RECEIVED DURING INITIAL CLIMB. COMPLIED WITH QRH AND FOUND A LOOSE CONNECTOR AND CORRODED PIN, CLEANED AND LUBED. REINSTALLED THE CONNECTOR. RAN ENGINE AND OPS CHECKED GOOD IAW AMM 30-21-00.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 90,061 hrs · 17,152 cycles

EMERGENCY LIGHTS INOPERATIVE ROW 14-19. REMOVED AND REPLACED THE BATTERY PACK AT BS 774, SYS OPS CHECKED GOOD IAW AMM 33-51-10.

Part: WARNING MESSAGE — FALSE ACTIVATION (LT ENGINE) · airframe 89,881 hrs · 17,117 cycles

LEFT ENGINE ANTI ICE VALVE STATUS MESSAGE. COMPLIED WITH FIM 30-21, FAULT TREE 805 MESSAGE DID NOT RETURN. SYSTEM IS OK.

Part: BONDING WIRE — BROKEN (NLG DOOR) · airframe 89,861 hrs · 17,113 cycles

NR 1 AFT LEFT NLG DOOR AFT HINGE BONDING WIRE BROKEN IN HALF (NRI 3025)(<P>REMOVED AND REPLACED AFT LEFT NLG AFT HINGE BONDING WIRE B767 AMM 32-22-04&NBSP;</P>)

Part: BRACKET — CORRODED · airframe 89,861 hrs · 17,113 cycles

INSIDE ACCESS PANEL 313AL LIGHT SWITCH AND SUPPORT BRACKET ARE CORRODED. REPLACED SUPPORT BRACKET AND CABLE CLIP FROM LIGHT SWITCH. INSIDE ACCESS PANEL IAW SRM 51-30-01, AND SRM 51-40-02.

Part: DUCT — DAMAGED (THRUST REVERSER) · airframe 898,613 hrs · 17,113 cycles

NR 2 ENGINE INBD THRUST REVERSER DUCT OUTER SKIN HAS DAMAGED AREAS. REPAIRED THE DUCT IAW AMM 78-31-00.

Part: QUICK DISCONNECT — DAMAGED (THRUST REVERSER) · airframe 89,861 hrs · 17,113 cycles

NR 2 INBD THRUST REVERSER LOWER MALE QUICK DISCONNECT FOR OPENING SYSTEM DOES NOT ALLOW THE THRUST REVERSER TO LOWER, PUMPS OPEN ONLY AND UPPER FITTING IS DIFFICULT TO DISCONNECT AND RECONNECT. REMOVED AND REPLACED QUICK DISCONNECT IAW MM 20-11-00, NO FURTHER DEFECTS NOTED AT THIS TIME.

Part: STRUCTURE — DAMAGED (THRUST REVERSER) · airframe 898,613 hrs · 17,113 cycles

NR 1 ENGINE OTBD THRUST REVERSER TRANSLATING COWL HAS DAMAGED AT INNER SURFACE, 8:00 POS AFT EDGE REPAIRED IAW CMM 78-32-32, OPS CHECKED GOOD IAW AMM 78-31-00.

Part: ROD — NOT REPORTED (THRUST REVERSER) · airframe 89,861 hrs · 17,113 cycles

NR 1 ENGINE OTBD THRUST REVERSER HOLD OPEN ROD REQUIRES REPLACEMENT. REPLACED IAW AMM 20-11-00.

Part: TAPE — OUT OF POSITION (NR 1 ENGINE) · airframe 89,861 hrs · 17,113 cycles

NR 1 ENGINE, INBD SIDE, 5:30 POSITION, COMBUSTION TURBINE HAS MIGRATED FROM UNDER CLAMPS, TWO AREAS. REMOVED AND REPLACED ANTI CHAFE TAPE ON NR 1 ENGINE INBD SIDE 5:30 POSITION, COMBUSTION/ TURBINE AREA TUBING IAW SOPM 20-60-04</P>)

Part: TRANSMITTER — CRUSHED (VALVE TEMP) · airframe 89,861 hrs · 17,113 cycles

LEFT AC BAY HAS A CRUSHED VALVE TEMP CONTROL TRANSMITTER. REMOVED AND REPLACED THE TRANSMITTER IAW AMM 21-51-12.

Part: STATIC WICK — DAMAGED (HORIZONTAL STAB) · airframe 89,861 hrs · 17,113 cycles

RIGHT HORIZONTAL STAB TIP AFT STATIC DISCHARGE BASE DAMAGED. REMOVED AND REPLACED STATIC DISCHARGER BASE IAW 23-61-01-022-018 STEP 7 AND 23-61-01-402-013 STEP 6.

Part: PIN — DETACHED (R4 DOOR SLIDE) · airframe 89,861 hrs · 17,113 cycles

R4 DOOR SLIDE MISSING SAFTEY PIN. FOUND PIN IN CORNER OF SLIDE INSTALLED SAFETY PIN IAW AMM 25-66-01.

Part: BONDING JUMPER — BROKEN · airframe 89,861 hrs · 17,113 cycles

FAMV BONDING JUMPER BROKEN ON NR 2 ENGINE. REMOVED BROKEN BONDING JUMPER AND INSTALLED NEW FAMV BONDING JUMPER ON ENG #2 IAW B767-300 SWPM 20-20-10</P>)

Part: CHIP DETECTOR — UNKNOWN (APU COMPRESSOR) · airframe 89,861 hrs · 17,113 cycles

SEND OUT APU COMPRESSOR BEARING CHIP DETECTOR FOR EVALUATION BY POWER PLANT ENGINEERING DUE TO SILVER CHIPS ON PROBE.

Part: LINE — CHAFED (NR 1 ENGINE) · airframe 89,861 hrs · 17,113 cycles

NR 1 ENGINE, INBD SIDE UNDER THRUST REVERSER, LINES FOR IGNITERS ARE CHAFFING ON THE T/R, AT THE 5:00 O'CLOCK POSITION, FWD OF ACCESSORY CASE. ADJUSTED THE WIRE CLAMPS IAW SWPM 20-20-12</P>)

Part: PUMP — DAMAGED (FUEL BOOST) · airframe 89,861 hrs · 17,113 cycles

RIGHT FWD BOOST PUMP HAS SIGNIFICANT CORROSION AND EROSION. REMOVED & REPLACED THE BOOST PUMP IAW AMM 28-22-03</P>)

Part: VALVE — NO TEST (THRUST REVERSER) · airframe 89,861 hrs · 17,113 cycles

NR 1 ENGINE THRUST REVERSER PNEUMATIC PRESSURE SWITCH FAILED DIRECTIONAL PILOT VALVE PRESSURE SWITCH TEST. REMOVED AND REPLACED NR 1 ENG DIRECTIONAL PILOT VALVE LEAK CHECKED NO LEAKS NOTED IAW AMM 78-34-01.

Part: STRUCTURE — DAMAGED (THRUST REVERSER) · airframe 89,861 hrs · 17,113 cycles

NR 1 ENGINE INBD THRUST REVERSER TRANSLATING COWL INNER SURFACE HAS 2 DAMAGED AREAS AT 2:00 AND 4:00. REPAIRED IAW CMM 78-32-32. OPS CHECKED GOOD IAW AMM 78-31-00.

Part: SLIDE — NOT REPORTED (L2 DOOR) · airframe 89,861 hrs · 17,113 cycles

L2 ENTRY DOOR ESCAPE SLIDE, INSTALLED OVERHAULED DOOR ESCAPE SLIDE IAW B767 AMM 25-66-01

Part: PACKING — LEAKING (NR 1 ENGINE) · airframe 89,861 hrs · 17,113 cycles

NR 1 ENGINE HAS OIL IN THE FIRST STAGE DISK. REMOVED AND REPLACED THE 1 BEARING MAINIFOLD PACKING IAW SERVICE BULLETIN 72-1401 REV 84.

Part: NONE — NONE (NONE) · airframe 89,861 hrs · 17,113 cycles

AUTO PILOT SERVO ASSYS SHOWS SIGNS OF LEAKING ON ASSYS AND LINES/ STRUCTURE IS WET. PERFORMED LEAK CHECK ON AUTO PILOT SERO ASSYS IAW AMM 29-11-00. NO LEAKS AT THIS TIME. NOT AN SDR.

Part: GROUND WIRE — DAMAGED (BS 1280) · airframe 89,816 hrs · 17,113 cycles

AFT CARGO BS 1280 GROUND WIRE DAMAGED. REPLACED TERMINAL END ON THE GROUND WIRE IAW SWPM 20-30-00

Part: STRUCTURE — DAMAGED (THRUST REVERSER) · airframe 898,613 hrs · 17,113 cycles

NR 2 ENGINE OTBD THRUST REVERSER TRANSLATING COWL INNER SKIN HAS DAMAGED AREA BETWEEN 1:00 AND 4:00 POS AFT EDGE. REMOVED THE NR 2 OTBD THRUST REVERSER TRANSCATING COWL INNER SKIN IAW CMM 78-32-32. OPS CHECKED GOOD IAW AMM 78-31-00.

Part: HOUSING — LEAKING (OIL FILTER) · airframe 89,861 hrs · 17,113 cycles

NR 1 ENGINE INBD SIDE UNDER THRUST REVERSER OIL IS COLLECTING ON THE T/R, ENGINE FILTER HOUSING IS WET ON OUTSIDE & DRIPPING FROM BOTTOM. PERFORMED A LEAK CHECKED IAW B767 AMM 71-00-00 TEST 3.

Part: WIRE — DAMAGED · airframe 89,861 hrs · 17,113 cycles

SEAT TRACK WIRES ALONG RT SIDE CABIN WALL FROM SEAT 3KH TO 6KH REQUIRES SPLICING AFTER SEAT INSTALLATION. SPLICED THE WIRES IAW BSWPM 20-10-13.

Part: PIN — MISSING (L2 DOOR SLIDE) · airframe 89,861 hrs · 17,113 cycles

L2 DOOR SLIDE MISSING SAFETY PIN. FOUND THE PIN IN CORNER OF SLIDE PACK AND INSTALLED IAW AMM 25-66-01.

Part: DEFLECTOR — DAMAGED (THRUST REVERSER) · airframe 89,861 hrs · 17,113 cycles

NR 1 ENGINE OTBD THRUST REVERSER THIRD CASCADE FROM BOTTOM IS DAMAGED ON INBD SIDE ON LE. REMOVED AND REPLACED THE DEFLECTOR IAW AMM 78-31-16.

Part: COVER — DAMAGED (THRUST REVERSER) · airframe 89,861 hrs · 17,113 cycles

NR 1 ENGINE, OTBD THRUST REVERSER, INNER FIRE PROTECTIVE COVERING, LWR 2" X AFT 3', MATERIAL IS LOOSE AND MISSING AND CONTAMINATED FIRE SEALING HAS BEEN REPAIRED IAW AMM 54-54-00-398-003.

Part: STATIC WICK — NO TEST (HORIZONTAL STAB) · airframe 89,861 hrs · 17,113 cycles

RIGHT HORIZONTAL STAB SECOND FROM OTBD STATIC WICK FAILS OPS CHECK. REMOVED AND REPLACED THE STATIC WICK IAW AMM 23-61-01, OPS CHECK GOOD.

Part: CONNECTOR — LOOSE (A/C PACK) · airframe 89,861 hrs · 17,113 cycles

LEFT PACK OFF LIGHT AND EICAS MESSAGE DO NOT ILLUMINATE WITH PACK SELECTED OFF. FOUND CONNECTOR PLUG LOOSE ON LEFT PACK FLOW CONTROL VALVE. OPS CHECKED OK IAW AMM 21-51-00.

Part: STATIC WICK — NO TEST (RT AILERON) · airframe 89,861 hrs · 17,113 cycles

RIGHT OTBD AILERON STATIC WICK FAILED OPS CHECK. REMOVED AND REPLACED THE RT OTBD AILERON STATIC WICK AND TESTED IAW AMM 23-61-01 OPS TESTED GOOD.

Part: START VALVE — FAILED (RT ENGINE) · airframe 89,845 hrs · 17,110 cycles

RT ENGINE STARTER EICAS MESSAGE DURING ENGINE START. CONFIRMED THE START VALVE NOT OPENING. PERFORMED MANUAL START. REMOVED & REPLACED THE NR 2 START VALVE IAW AMM 80-11-02, OPS CHECKED GOOD. MESSAGE NO LONGER DISPLAYED.

Part: SMOKE DETECTOR — MALFUNCTIONED (LAVATORY) · airframe 89,778 hrs · 17,091 cycles

SMOKE DETECTOR AT R2 LAVATORY RIGHT SIDE CENTER WON`T RESET, ON ALL THE TIME. REMOVED AND REPLACED THE SMOKE DETECTOR IAW MM 26-13-00.

Part: WARNING BELL — FALSE ACTIVATION (EQUIP COOLING) · airframe 89,740 hrs · 17,083 cycles

FWD EQUIPMENT COOLING WARNING CHIMES, EQUIPMENT COOLING OVERBOARD CLOSED ON GROUND. RECYCLED OVERBOARD EXHAUST VALVE, PERFORM OPS CHECK OF EQUIPMENT COOLING IAW AMM 21-58-00.

Part: PLUG — BROKEN (APU OIL DRAIN) · airframe 89,739 hrs · 17,082 cycles

DRAIN PLUG ON APU IS BROKEN OFF IN APU. REPLACED APU OIL DRAIN PLUG IAW B767 AMM 12-13-04.</P>)

Part: BRUSHES — WORN (APU STARTER) · airframe 89,739 hrs · 17,082 cycles

STARTER BRUSHES FOR APU WORN BEYONG LIMITS. REMOVED AND REPLACED APU STARTER IAW AMM 48-41-01.

Part: ENGINE — MALFUNCTIONED (APU) · airframe 89,730 hrs · 17,080 cycles

APU WOULD NOT START AFTER LANDING, APU FAULT. CLEARED THE FAULT AND OPS CHECKED THE APU IAW 49-00-00. NO DEFECTS NOTED.

Part: WARNING MESSAGE — FALSE ACTIVATION (WX RADAR SYS) · airframe 89,717 hrs · 17,078 cycles

WEATHER RADAR SYS STATUS MESSAGE DISPLAYED THE SYSTEM HAD FAILED. CLEARED STATUS MESSAGE AND OPS CHECKED IAW MM 34-43-00, NO DEFECTS NOTED AT THIS TIME.

Part: PRESSURE SWITCH — FAILED (GCU) · airframe 89,669 hrs · 17,066 cycles

APU ECU DISPLAYS MINI FLAG. REMOVED & REPLACED THE GCU DIFFERENTIAL PRESSURE SWITCH IAW MM 49-27-15. OPS AND LEAK CHECKED GOOD.

Part: VALVE — MALFUNCTIONED (RT WING) · airframe 89,837 hrs · 1,710,728 cycles

RIGHT ENGINE DID NOT START, START VALVE LIGHT ILLUMINATED. REMOVED AND REPLACED RIGHT ENGINE FUEL SPAR VALVE AND OPS CHECKED GOOD IAW AMM 28-22-11.

Part: ECU — FAILED (APU) · airframe 89,509 hrs · 17,029 cycles

APU RELIABILITY COLD START, THREE ATTEMPTS UNSUCCESSFUL. REMOVED AND REPLACED APU ECU IAW AMM 49-61-05, OPS CHECKED GOOD, NO FAULTS INDICATED.

Part: WARNING MESSAGE — FALSE ACTIVATION (WX RADAR SYS) · airframe 89,487 hrs · 17,019 cycles

WEATHER RADAR SYS STATUS MESSAGE. WXR TESTED IAW AMM 34-43-00/501. MESSAGE CLEARED, TEST PASSED.

Part: IGNITER — FAILED (APU) · airframe 89,403 hrs · 17,003 cycles

APU FAULT AFTER LANDING.. REMOVED AND REPLACED IGNITOR AND OPS CHECK OK IAW AMM 49-41-02 & 49-11-00.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 89,306 hrs · 16,984 cycles

EXT EMERGENCY GROUND FLOOD LIGHT INOPERATIVE AFT OF RT WING. REPLACED THE BULB & OPS CHECKED GOOD IAW AMM 33-51-16.

Part: RELAY — FAILED (FUEL PUMP) · airframe 89,225 hrs · 16,967 cycles

LEFT FWD MAIN FUEL PUMP AUTO FUNCTION INOPERATIVE. TROUBLESHOT IAW WDM 28-28-11, AND FOUND NO GROUND D80269 PIN 32. R & R THE RELAY K513. SYSTEM OPS CHECKED NORMAL IAW 28-25-00.

Part: CONNECTOR — UNSECURE (CABIN) · airframe 89,249 hrs · 16,973 cycles

EMERGENCY LIGHTS AT SEATS 20H INOPERATIVE, EMERGENCY LIGHTS AT SEAT 29H INOPERATIVE. RESECURED CONNECTORS UNDER SEATS. OPS CHECKS NORMAL AMM 33-50-00. OPS CHECK C/W.

Part: CONTROLLER — MALFUNCTIONED (PRESS REGULATOR) · airframe 89,180 hrs · 16,957 cycles

RT ENGINE PRV EICAS MESSAGE. REMOVED AND REPLACED RT ENGINE PRESSURE REGULATOR CONTROLLER ASSY IAW AMM 36-11-19 OPS & LEAK CHECKED GOOD.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 89,168 hrs · 16,954 cycles

RT ENGINE PREVIOUS EICAS ANUNCIATOR PERFORMED BITE TEST ON AIR SUPPLY MODULE. FOUND PREVIOUS FAULT RESET BOX. NO FAULTS MSG CLEARED. EICAS. PERFORMED OPS ;IAW AMM 36-11-18, PREVIOUS OPS NORMAL.

Part: UNKNOWN — MALFUNCTIONED (BLEED AIR SYS) · airframe 89,134 hrs · 16,947 cycles

RIGHT ENGINE PERFORMED BITE ON PNEU CONTROLLER, FOUND RT PRV FAULT. RESET BOX, FOUND NO FAULTS, CLEARS EICAS MSG PERFORMED ADJ TEST IAW 36-11-18, PRV OPS NORMAL.

Part: SHUTOFF VALVE — FAILED (LEFT) · airframe 89,134 hrs · 16,947 cycles

DURING TROUBLESHOOTING OF THE RIGHT BLEED, THE LEFT HPSOV FAILED A BITE CHECK ON THE PNEUMATIC CONTROLLER. REMOVED AND REPLACED THE LEFT HPSOV IAW AMM 36-11-07 OPS CHECKED GOOD.

Part: CONNECTOR — NOT SEATED (ANTI-ICE SYSTEM) · airframe 89,124 hrs · 16,945 cycles

RT ENGINE ANTI-ICE EICAS MESSAGE IN FLIGHT WITH ENGINE ANTI-ICE ON. RT ENGINE ANTI ICE VALVE LIGHT WAS ON FOUND PRSOV NOT SUPPLYING AIR TO ANTI-ICE VALVE. RESEATED CONNECTOR ON PRSOV. OPS CHECKED RT ENGINE ANTI-ICE GOOD IAW AMM 30-21-00, OPS CHECKED PRSOV IAW AMM 36-11-09.

Part: WARNING MESSAGE — ILLUMINATED · airframe 89,122 hrs · 16,944 cycles

RIGHT HP PROV CAUTION MESSAGE AFTER TAKEOFF.

Part: WARNING MESSAGE — FAULTY (COCKPIT) · airframe 89,110 hrs · 16,942 cycles

ECS/MSG PAGE MAINTENANCE MSG, APU BITE, WILL NOT CLEAR. PERFORMED APU CONTROL UNIT BITE TEST. TEST OK IAW AMM TASK 49-60-05-742-045. MAINTENANCE MSG, APU BITE, CLEARED.

Part: CIRCUIT CARD — NOT SEATED (E&E BAY) · airframe 89,035 hrs · 16,926 cycles

STATUS MESSAGE: FORWARD EQ SUPPORT FAN 1. DEFERRED IAW MEL 21-58-03-02-01, MDDR 69660 CAT-C 06SEP16, PLACARD INSTALLED. RESEATED CONTROL CARD M990; M861. OPS CHECK C/W IAW MM 21-58-00, MDDR 69660 CLEARED, PLACARD REMOVED.

Part: STARTER — DEFECTIVE (APU) · airframe 89,033 hrs · 16,925 cycles

APU BATTERY DISCHARGE EICAS MESSAGE AND OVERHEAD LIGHT ON, AFTER GLIDESLOPE CAPTURE, TRANSFERRED TO MEL 49-11-01B, CAT-B MDDR 69615. R & R APU STARTER REF AMM 49-41-01, MDDR CLEARED, NR 69615, OPS CHECK.

Part: RELAY — FAULTY (APU) · airframe 89,022 hrs · 16,922 cycles

APU BITE MESSAGE, ACFT START CIRCUIT MINI FLAG 34 T/S IAW FIM 49-11, FT 991, EXAMINED ECU DH08B PIN J10 TO POSITIVE STARTER TERMINAL M893 NO FAULTS NOTED. CHECKED V ON K117 TERMINAL X1 AND FOUND VOLTAGE BETWEEN 21V AND 23V , REPLACED K197 , R & R APU STARTER MOTOR, OPS AND LEAK CHECK GOOD REF AMM 49-41-01.

Part: THERMOCOUPLE — FAILED (APU) · airframe 88,973 hrs · 16,911 cycles

APU ECU SHOWS EGT NR 2 CIRCUIT FAULT. REMOVED AND REPLACED EGT THERMOCOUPLE ON APU APROX. 3 O'CLOCK POSITION IAW AMM 49-71-01 OPS AND LEAK CHECKED GOOD.

Part: THERMOCOUPLE — FAILED (APU) · airframe 88,973 hrs · 16,911 cycles

APU ECU SHOWS EGT NR 2 CIRCUIT FAULT. REMOVED AND REPLACED EGT THERMOCOUPLE ON APU APPROX. 12 O'CLOCK POSITION IAW AMM 49-71-01 OPS AND LEAK CHECKED GOOD.

Part: MODULE — MALFUNCTIONED (APU) · airframe 88,973 hrs · 16,911 cycles

APU BITE MESSAGE. REMOVED AND REPLACED FLOW SENSING MODULE IAW AMM 49-53-08, NO BITE MESSAGE. APU OPS CHECKED GOOD.

Part: RADAR — MALFUNCTIONED (WX SYSTEM) · airframe 88,894 hrs · 16,893 cycles

WEATHER RADAR SYSTEM STATUS MESSAGE. OPS CHECKED WEATHER RADAR SYSTEM IAW AMM 34-43-00. NO DEFECTS NOTED.

Part: APU — MALFUNCTIONED · airframe 88,886 hrs · 16,891 cycles

APU FAILED TO START AFTER LAND. APU STARTED ON THIRD ATTEMPT IAW AMM 49-41-00.

Part: RELAY — NOT SEATED (FUEL SYSTEM) · airframe 88,701 hrs · 16,855 cycles

LEFT FWD FUEL PUMP EICAS MSG, LT FORWARD FUEL PUMP, ON LANDING, DEFERRED IAW MEL 28-22-01, MDDR 68556. CAT-C DUE. LP 787233, ITEM M3: REF MDDR 68554, RESEATED RELAY K 188 IN P33 PANEL, OPS CHECK C/W IAW MM 28-22-00, OPS NORMAL. THIS CLEARS MDDR 68554, PLACARD REMOVED.

Part: UNKNOWN — MALFUNCTIONED (WEATHER RADAR) · airframe 88,692 hrs · 16,854 cycles

WEATHER FAIL SYSTEM 1, WEATHER RADAR, CHECKED NR 1 WEATHER RADAR SYS IAW AMM 34-43-00, NO DEFECTS NOTED AT THIS TIME. NO IN FLT FAULTS.

Part: APU — MALFUNCTIONED · airframe 88,628 hrs · 16,844 cycles

APU DID NOT START ON ARRIVAL. COULD NOT DUPLICATE, OPS CHECKED IAW AMM 49-11-01 TASK 49-11-00-802-002.

Part: WARNING MESSAGE — FALSE ACTIVATION (EXHAUST FAN) · airframe 88,593 hrs · 16,837 cycles

STATUS MESSAGE AFT EQUIPMENT EXHAUST FAN 2. ERASED MESSAGE OPS CHECK NORMAL IAW AMM 21-58-00.

Part: WARNING MESSAGE — FALSE ACTIVATION (EXHAUST FAN) · airframe 88,593 hrs · 16,837 cycles

AFT EQUIPMENT EXHAUST FAN NR 2 STATUS MESSAGE. ERASED MESSAGE, OPS CHECKED NORMAL IAW AMM 21-58-00.

Part: APU — SHUTDOWN (APU BAY) · airframe 88,546 hrs · 16,826 cycles

APU AUTO SHUTDOWN, APU FAULT EICAS TRANSFERRED TO MEL 49-11-01B, CAT B. REMOVED & REPLACED APU ASSY IAW AMM 49-11-01, OPS CKS NML.

Part: FUSE — FAILED (EMERGENCY LIGHTS) · airframe 88,495 hrs · 16,815 cycles

CABIN ROW 19 L/HOVHD EMERGENCY LIGHT INOP. POWER SUPPLY FUSE BLOWN. REMOVED AND REPLACED THE FUSE IAW AMM 33-51-02.

Part: COVER — LOOSE (EMERGENCY LIGHT) · airframe 88,495 hrs · 16,815 cycles

CABIN L2 DOOR FLOOR RED EMERGENCY LIGHT LENS LOOSE. INSTALLED THE EMERGENCY LIGHT COVER. OPS CHECK OK. PER AMM 33-51-00.

Part: TRANSMITTER — FAILED (ELT) · airframe 88,495 hrs · 16,815 cycles

ELT FAIL OPS TEST. REMOVED AND REPLACED THE ELT AND PERFORMED OPS CHECK OK IAW AMM 23-24-01.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 88,495 hrs · 16,815 cycles

L1 DOOR LOWER FWD EMERGENCY LIGHT LENS LOOSE. LOCATED AND SECURED LIGHT LENS IAW SRM 51-40-02-06-0.

Part: LIFE VEST — MISSING (COCKPIT) · airframe 88,495 hrs · 16,815 cycles

COCKPIT F/O LIFE VEST MISSING. REPLACED MISSING F/O LIFE VEST IAW AMM 25-64-00.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 88,417 hrs · 16,793 cycles

LEFT AND RIGHT EMERGENCY FLOOR PATH LIGHTS INOPERATIVE AT L1 AND L2 DOORS, L2 DOOR EMERGENCY LIGHT INOPERATIVE, EMERGENCY PATH LIGHT AFT CABIN LT SIDE BY LAV MISSSING LIGHT ASSY. R & R BATTERY CHARGER PN OFF 2012-1, SN OFF 34409, FOR L1, L2 DOOR. R & R BATTERY CHARGER, PN OFF 2012-1, SN OFF 366221 FOR L2 DOOR. R & R PATH LIGHTING, PN OFF 207377-2-39.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 88,098 hrs · 16,727 cycles

EMERGENCY LIGHT RIGHT AFTER TE FLAPS INOPERATIVE. RELAMPED RT EMER LIGHT IAW AMM 33-51-16. OPERATIONS CHECKED NORMAL IAW AMM 33-51-00.

Part: BATTERY — DISCHARGED (CABIN) · airframe 88,098 hrs · 16,727 cycles

EMERGENCY SEAT LIGHTS 4H, 6H INOPERATIVE. R & R 6H LIGHT ASSEMBLY IAW AMM 33-51-10 OK. SEAT POSITION 4H FOUND BROKEN WIRE TO LIGHT ASSEMBLY. REPAIRED IAW SWPM 20-10-13. OK OPERATIONS CHECK. FOUND BATTERY NOT HOLDING LOAD. REPLACED BATTERY ON RT STATION 410 IAW AMM 33-51-07 & ALSO FOUND BATTERY FOR LT FWD SECTION NOT HOLDING LOAD. REPLACED BATTERY UNDER L1 FLIGHT ATTENDANT SEAT IAW AMM 33-51-07. PERFORMED OPERATIONS CHECK OF EMER SYS IAW AMM 33-51-00. OPERATIONS CHECKED OK AT THIS TIME.

Part: LENS — MISSING (CABIN) · airframe 88,098 hrs · 16,727 cycles

EMERGENCY LIGHTING LENS MISSING BY SEAT OUTSIDE 6K. REPLACED MISSING EMER LIGHT LENS COVER BY SEAT 6K IAW AMM 33-51-10.

Part: CONTACT — DIRTY (EXTERIOR LIGHT) · airframe 87,895 hrs · 16,681 cycles

EMERGENCY LIGHT INOPERATIVE EXTERIOR RT AFT OF WING. REMOVED LENS COVER, CHECKED LAMP FOUND LAMP GOOD. CLEANED & CONTACT REINSTALLED & OPERATIONS CHECKED NORMAL IAW AMM 33-51-06.

Part: LIGHT — LOOSE (CABIN) · airframe 87,895 hrs · 16,681 cycles

MAIN PAX CABIN ROW 14 LT FLOOR EMER LIGHTING LOOSE. INSTALLED & SECURED PAX CABIN 14 LT FLOOR EMER LIGHT SYS. OPERATIONS CHECKED OK IAW AMM 33-59-00.

Part: UNKNOWN — NOT REPORTED (APU) · airframe 87,489 hrs · 16,602 cycles

UNSUCCESSFUL COLD SOAK APU START. THREE ATTEMPTS AT FL 370 & -62°C SAT. NOTED BY MX, APU OPERATIONS CHECKED NORMAL ON GND IAW AMM 49-11-00. MDDR 64843 MEL 25-AP-01 REMAINS OPEN.

Part: CLUTCH — MALFUNCTIONED (APU) · airframe 87,426 hrs · 16,585 cycles

APU WILL NOT START. WILL NOT EXCEED 9 PERCENT RPM. TROUBLESHOT IAW FIM 694246 NR 7. R & R RELAY K117 IAW MCC REQUEST IAW WDM 24-31-41. REQUIRES OPERATIONS CHECK. APU START SATISFACTORY IAW AMM 49-11-00. LOG PAGE 694248 15 R & R STARTER CLUTCH & OPERATIONS CHECKED SATISFACTORY IAW AMM 49-41-06 DMI CLEARED. LOG PAGE 694248 NR 14 R & R APU STARTER & OPERATION S CHECKED SATISFACTORY IAW AMM 49-41-01 DMI CLEARED.

Part: CHARGER — MALFUNCTIONED (APU BATTERY) · airframe 87,426 hrs · 16,585 cycles

APU BATTERY CHARGER STATUS MESSAGE. R & R APU BATTERY CHARGER IAW AMM 24-31-05. OPERATIONS CHECKED OK.

Part: SWITCH — FAILED (AC BAY) · airframe 87,393 hrs · 16,577 cycles

LEFT & RIGHT PACK MSG & EICAS MX PAGE. TROUBLE SHOT IAW FIM 21-51 FT 807, 844 TO PACK ALTITUDE SWITCH FAILED. PLACED ON MEL 21-51-05 CAT C MDDR 64614.

Part: STARTER — FAILED (APU) · airframe 87,354 hrs · 16,568 cycles

APU INOPERATIVE. DURING INSPECTION FOUND APU STARTER FAILED. REPLACED APU STARTER IAW AMM 49-41-01. OPERATIONS CHECK COMPLIED WITH.

Part: STATUS MESSAGE — FALSE ACTIVATION (COCKPIT) · airframe 87,268 hrs · 16,550 cycles

LEFT FWD FUEL PUMP EICAS MSG UPON LANDING. RESET CB IAW AMM 20-60-05, OPERATIONS CHECKED PUMP IAW AMM 28-22-00. OPERATIONS CHECKED NORMAL IAW FIM 28-22 FT 820.

Part: RELAY — FAILED (ANTI ICE) · airframe 87,264 hrs · 1,654,930 cycles

LEFT ENGINE ANTI-ICE EICAS ON ARRIVAL. QRH COMPLETED. R & R K650 LT ENG TAI CONT TD RELAY IAW WDM 20-21-11. OPERATIONS CHECKED NORMAL IAW MM 30-21-00.

Part: STATUS MESSAGE — FALSE ACTIVATION (COCKPIT) · airframe 87,230 hrs · 16,544 cycles

STATUS MSG, AFT EQ EXH FAN 2. PERFORMED FIM PROCEDURE IAW FIM 21-26 FT 808 NO FAULTS NOTED.

Part: APU — FAILED · airframe 87,230 hrs · 16,543 cycles

APU FAULT LIGHT AFTER LANDING. THREE ATTEMPTS UNSUCCESSFULLY. R & R APU IAW MM 49-11-01. OPERATIONS CHECK & LEAK CHECK OK.

Part: STATUS MESSAGE — FALSE ACTIVATION (COCKPIT) · airframe 87,222 hrs · 16,540 cycles

RIGHT ENG HPSOV STATUS MSG. RT ENG HPSOV BITE CHECK, NO FAULTS NOTED IAW FIM 36-20 TREE 804. RAN ENG IAW MM 71-00-00. RT ENG HPSOV OPERATIONS CHECKED GOOD.

Part: ECU — MALFUNCTIONED (APU) · airframe 87,222 hrs · 16,540 cycles

NO APU DUCT PRESS AFTER ENG START. R & R APU CONTROL UNIT. PERFORMED OPERATIONAL CHECK OK IAW MM 49-61-05.

Part: WAVE GUIDE — UNSECURE (WEATHER RADAR) · airframe 87,164 hrs · 16,529 cycles

SYSTEM 1 RADAR HAS TEMPORARY SPIKES & ECHOES IN DISPLAY. OPERATIONS NORMAL IN SYS 2. REPAIRED GND & SECURED WAVE GUIDE ON WEATHER RADAR RT. OPERATIONS CHECKED OK IAW 34-43-00.

Part: SHUTOFF VALVE — FAULTY (APU) · airframe 87,147 hrs · 16,524 cycles

APU PNEUMATIC FUNCTION ONLY PRODUCING 2 PSI AIR PRESS. WILL RISE AT ENG START SIGNAL. RECEIVED APU BITE P2 SENSOR FLAG 16. R & R VARIABLE VOLUME CHAMBER ON APU. R & R INLET TEMPERATURE SENSOR ON APU. R & R SOLENOID VLV ASSEMBLY ON APU. IAW AMM 49-53-07, 49-61-04 & 49-27-08. OPERATIONAL CHECK ON APU NORMAL IAW 49-11-00. R & R SOV. OPERATIONS CHECKED NORMAL AMM 36-11-10.

Part: SHUTOFF VALVE — INOPERATIVE (APU) · airframe 87,106 hrs · 16,515 cycles

APU PNEUMATIC FUNCTION INOPERATIVE. OPENED MEL 49-11-01-01, REQUIRES TROUBLESHOOTING. R&R VARIABLE VOLUME CHAMBER ON APU. R&R INLET TEMPERATURE SENSOR ON APU. R&R SOLENOID VLV ASSEMBLY ON APU IAW AMM 49-53-07, 49-61-04 & 49-27-08. OPERATIONAL CHECK ON APU NORMAL IAW 49-11-00. R&R SOV. OPERATIONS CHECKED NORMAL IAW AMM 36-11-10.

Part: BLEED AIR SYS — MALFUNCTIONED (APU) · airframe 87,083 hrs · 1,650,949 cycles

APU AIR INOPERATIVE. PERFORMED FIM TK 49-11FT987, FLAG 16 & LRU P2 SENSOR LATCHED, CLEARED & BITE SELF-TESTED NORMAL. APU AIR ON LAST 2 LEGS, NO FAULTS, IAW FIM 49-11 FT 987. OPERATIONS CHECKED NORMAL.

Part: SWITCH — FAULTY (APU) · airframe 86,996 hrs · 16,490 cycles

APU FAULT & APU BATTERY DISCHARGE EICAS MSG. AFTER LANDING APU START IAW MEL 49-11-1B. REPLACED LOW OIL TEMP SWITCH IAW AMM 49-27-14. OPERATIONS CHECKED NORMAL.