N662GT

Part: FIRST AID KIT — OPEN (ZONE 200) · airframe 86,612 hrs · 17,372 cycles

FIRST AID KIT FOUND WITH BROKEN SEAL(<P>REMOVED AND REPLACED FIRST AID KIT AT AFT FLIGHT ATTENDANT STATION IAW AMM 25-64-03. NO FURTHER DEFECTS NOTED</P>)

Part: ANTENNA — FAULTED (ZONE 100) · airframe 86,230 hrs · 17,294 cycles

COULD NOT RECEIVE ON EITHER HF RADIO. CONFIRMED WITH ATC W/ CPDLC THAT WE WERE TRANSMITTING. REMOVED AND REPLACED HF RADIO ANTENNA IAW AMM 23-11-04. OPS CHECK GOOD.

Part: OXYGEN BOTTLE — NOT REPORTED (ZONE 200) · airframe 86,133 hrs · 17,277 cycles

AFT CENTER PORTABLE O2 BOTTLE REQ REPLACEMENT(<P>REMOVED AND REPLACED PORTABLE O2 BOTTLE IAW B767 AMM 35-31-01. OPS &AMP; LK CHK OK. NO FURTHER DEFECTS.</P>)

Part: BATTERY — FAULTED (ZONE 200) · airframe 86,117 hrs · 17,275 cycles

DURING DAILY CHECK, FOUND LT EMERGENCY ESCAPE SQUIB TEST BAD. REMOVED AND REPLACED LT EMERGENCY OFF WING BATTERY IAW AMM 25-65-17-404-008-001 & AIPC 25-67-17-10A. OPS CHK GOOD.

Part: OXYGEN MASK — NO TEST (ZONE 200) · airframe 86,088 hrs · 17,267 cycles

CAPT OXYGEN FLOW INDICATOR NOT SHOWING YELLOW CROSS WHEN TESTING. REMOVED AND REPLACED CAPT OXYGEN MASK STOWAGE BOX IAW AMM 35-11-51. OPS CHECKS GOOD.

Part: OIL SYSTEM — LEAKING (NR 1 ENGINE) · airframe 85,917 hrs · 17,232 cycles

OIL QUANTITY ON RIGHT ENGINE DROPPED TO 8 QUARTS.(<P>ALL ITEMS FOR ACTION TAKEN TO CORRECT IAW B767 AMM 79-21 &AMP; 79-31. LP 1219035 M9: SERVICED #1 ENG 4 QTS &AMP; SERVICED #2 ENG 8 QTS IAW B767 AMM 12-15-03. NO FURTHER DEFECTS NOTED.</P>)

Part: LAMP — INOPERATIVE (ZONE 200) · airframe 85,734 hrs · 17,197 cycles

EMERGENCY LIGHT AT SEAT 6CA INOP.(<P>REMOVED AND REPLACED LAMP IAW AMM 33-51-05. OPS CHECKS GOOD.</P>)

Part: FIRST AID KIT — OUT OF DATE (ZONE 200) · airframe 85,726 hrs · 17,196 cycles

GALLEY AREA FIRST AID KIT OUT OF DATE.(<P>LP 1896471 M2: REMOVED AND REPLACED FIRST AID KIT IAW AMM 25-64-03. MDDR 231085 CLEARED.&NBSP; NO FURTHER DEFECTS NOTED.</P>)

Part: HANDLE — LOOSE (ZONE 800) · airframe 85,572 hrs · 17,167 cycles

R1 EMERGENCY DOOR HANDLE LOOSE(<P>PERFORMED OPS CHK OF R1 DOOR &AMP; NO DEFECTS NOTED IAW B767 AMM 52-11-00</P>)

Part: PAWL — OUT OF ADJUST (ZONE 800) · airframe 85,368 hrs · 17,125 cycles

R1 DOOR HARD TO CLOSE FROM INSIDE. (REQ. ADJUSTMENT)(<P>ADJUSTED DOOR HANDLE CLUTCH PAWL PER AMM 52-11-00. OPS CHECK NORMAL. NO FURTHER DEFECTS NOTED.</P>)

Part: SEAL — DELAMINATED (ZONE 800) · airframe 85,368 hrs · 17,125 cycles

RIGHT OVERWING EMERGENCY EXIT MAKES EXCESSIVE NOISE.(<P>FOUND RH, FWD EMERGENCY EXIT DOOR SEAL DELAMINATED, REPAIRED DOOR SEAL IAW AMM 52-09-00. REINSTALLED RH FWD OVERWING EMERGENCY EXIT DOOR IAW 52-21-01. NO FURTHER DEFECTS NOTED.</P>)

Part: SPRING — DAMAGED (ZONE 800) · airframe 85,162 hrs · 17,078 cycles

R1 DOOR DIFFICULT TO CLOSE.(<P>.REPLACED SPRING CARTRIDGE ON R1 DOOR HANDLE &AMP; OPS CHK OK IAW AMM 52-11-25</P>)

Part: BULB — INOPERATIVE (ZONE 200) · airframe 84,888 hrs · 17,014 cycles

EMERGENCY LIGHT INOP AT SEAT 3HK. REMOVED AND REPLACED BULB AT SEAT 3HK IAW AMM 33-51-01.&NBSP; OPS CHECK GOOD.

Part: SLIDE — NOT REPORTED (ZONE 800) · airframe 84,818 hrs · 16,997 cycles

L4 EMERG SLIDE REQUIRES REPLACEMENT(<P>R/R SLIDE/RAFT ASSY EVACUATION IAW AMM 25-66-01. OPS CHK OK</P>)

Part: DOOR — BINDING (ZONE 800) · airframe 84,692 hrs · 16,973 cycles

R1 DOOR HARD TO CLOSE FROM INSIDE(<P>PERFORMED GENERAL VISUAL INSPECTION AND OPERATIONAL CHECK PER AMM 51-11-00-715-128. VISUAL CHECK AND OPS CHECK GOOD.</P>)

Part: WINDOW FRAME — CORRODED (ZONE 200) · corrosion level 2 · airframe 84,622 hrs · 16,956 cycles

LH PASSENGER CABIN BETWEEN STA 785.9 AND STA 808 AND STGR 14LH TO STGR 16LH WINDOW FRAME WITH CORROSION(<P>CORROSION WAS REMOVED, EVALUATED, AND FOUND WITHIN PERMISSIBLE DAMAGE TOLERANCE AS CATEGORY A IAW CMA TLS 24-0200-08B. NO FURTHER DEFECTS NOTED</P>)

Part: WINDOW FRAME — CORRODED (ZONE 200) · corrosion level 2 · airframe 84,622 hrs · 16,956 cycles

LH PASSENGER CABIN BETWEEN STA 999 AND STA 1021 AND STGR 14LH TO STGR 16LH WINDOW FRAME WITH CORROSION(<P>CORROSION WAS REMOVED, EVALUATED AND FOUND WITHIN PERMISSIBLE DAMAGE TOLERANCE AS CATEGORY C IAW CMA TLS 24-0200-08B. NO FURTHER DEFECTS NOTED</P>)

Part: SKIN — DENTED (NR 6 SLAT) · airframe 84,622 hrs · 16,956 cycles

SLAT 6, INSIDE UPPER AREA WS 314.3 APPROX WITH DENT(<P>DENT WAS REPAIRED IAW SRM 51-70-10-2R-4 &AMP; SRM 51-70-10-2R-0. NO FURTHER DEFECTS NOTED</P>)

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 84,622 hrs · 16,956 cycles

PASSENGER CARGO STRUCTURE FLOOR, BTW STA 325 FLOOR BEAM WITH CORROSION LBL 57 APROX.(<P>BEAM WAS REPAIRED IAW SRM 53-00-51-11-1. NO FURTHER DEFECTS NOTED</P>)

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 84,622 hrs · 16,956 cycles

CORROSION ON SEAT TRACK RBL 53 AND BETWEEN STA 400 TO STA 433 AT PASSENGER CABIN(<P>SEAT TRACK WAS REPLACED IAW SRM 51-10-02-0G-0 PAR 9. NO FURTHER DEFECTS NOTED.</P>)

Part: WINDOW FRAME — CORRODED (ZONE 200) · corrosion level 2 · airframe 84,622 hrs · 16,956 cycles

RH PASSENGER CABIN BETWEEN STA 720 AND STA 742 AND STGR 14 RH TO STGR 16RH WINDOW FRAME WITH CORROSION(<P>CORROSION WAS REMOVED, EVALUATED AND FOUND WITHIN PERMISSIBLE DAMAGE TOLERANCE AS CATEGORY A IAW CMA TLS 24-0201-08B. NO FURTHER DEFECTS NOTED</P>)

Part: WINDOW FRAME — CORRODED (ZONE 200) · corrosion level 2 · airframe 84,622 hrs · 16,956 cycles

RH PASSENGER CABIN BETWEEN STA 654+121 AND STA 676 AND STGR 14RH TO STGR 16RH WINDOW FRAME WITH CORROSION(<P>CORROSION WAS REMOVED, EVALUATED AND FOUND WITHIN PERMISSIBLE DAMAGE TOLERANCE AS CATEGORY C IAW CMA TLS 24-0205-08B. NO FURTHER DEFECTS NOTED</P>)

Part: WINDOW FRAME — CORRODED (ZONE 200) · corrosion level 2 · airframe 84,622 hrs · 16,956 cycles

LH PASSENGER CABIN BETWEEN STA 764 AND STA 785.9 AND STGR 14LH TO STGR 16LH WINDOW FRAME WITH CORROSION(<P>CORROSION WAS REMOVED, EVALUATED AND FOUND WITHIN PERMISSIBLE DAMAGE TOLERANCE AS CATEGORY A IAW CMA TLS 24-0200-08B. NO FURTHER DEFECTS NOTED</P>)

Part: WINDOW FRAME — CORRODED (ZONE 200) · corrosion level 2 · airframe 84,622 hrs · 16,956 cycles

LH PASSENGER CABIN BETWEEN STA 1197.88 AND STA 1197.110 AND STGR 14LH TO STGR 16LH WINDOW FRAME WITH CORROSION(<P>CORROSION WAS REMOVED, EVALUATED AND FOUND WITHIN PERMISSIBLE DAMAGE TOLERANCE AS CATEGORY C IAW CMA TLS 24-0202-05B. NO FURTHER DEFECTS NOTED.</P>)

Part: WINDOW FRAME — CORRODED (ZONE 200) · corrosion level 2 · airframe 84,622 hrs · 16,956 cycles

RH PASSENGER CABIN BETWEEN STA 1417 AND STA 1439 AND STGR 14 RH TO STGR 16RH WINDOW FRAME WITH CORROSION(<P>CORROSION WAS REMOVED, EVALUATED, AND FOUND WITHIN PERMISSIBLE DAMAGE TOLERANCE AS CATEGORY C IAW CMA TLS 24-0204-05B. NO FURTHER DEFECTS NOTED</P>)

Part: WINDOW FRAME — CORRODED (ZONE 200) · corrosion level 2 · airframe 84,622 hrs · 16,956 cycles

RH PASSENGER CABIN BETWEEN STA 785.9 AND STA 808 AND STGR 14 RH TO STGR 16RH WINDOW FRAME WITH CORROSION(<P>CORROSION WAS REMOVED, EVALUATED AND FOUND WITHIN PERMISSIBLE DAMAGE TOLERANCE AS CATEGORY C IAW CMA TLS 24-0201-08B. NO FURTHER DEFECTS NOTED</P>)

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 84,622 hrs · 16,956 cycles

CORROSION ON SEAT TRACK RBL 20 AND BETWEEN STA 340 TO STA 390 AT PASSENGER CABIN(<P>SEAT TRACK WAS REPLACED PER DWG 141T5120. NO FURTHER DEFECTS NOTED</P>)

Part: DOOR FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 84,622 hrs · 16,956 cycles

LOWER HALF FUSELAGE, FWD CARGO CARGO COMPARTMENT DOOR CUTOUT BETWEEN BS 544 AND 566 LOWER MAIN SILL UPPER SURFACE WITH CORROSION(<P>SUPPORT WAS REPLACED BY NEW ONE &AMP; NO FURTHER DEFECTS NOTED PER AMM 53-00-00</P>)

Part: FRAME — CORRODED (ZONE 100) · airframe 84,622 hrs · 16,956 cycles

AFT AREA BULK CARGO ON THE STA 1540 AND STG 36LH FRAME WITH CORROSION.(<P>SHEAR TIE WAS REPLACED BY NEW ONE PER DWG 146T1222. NO FURTHER DEFECTS NOTED</P>)

Part: WINDOW FRAME — CORRODED (ZONE 200) · corrosion level 2 · airframe 84,622 hrs · 16,956 cycles

LH PASSENGER CABIN BETWEEN STA 654+121 AND STA 676 AND STGR 14LH TO STGR 16LH WINDOW FRAME WITH CORROSION(<P>CORROSION WAS REMOVED, EVALUATED AND FOUND WITHIN PERMISSIBLE DAMAGE TOLERANCE AS CATEGORY A IAW CMA TLS 24-0203. NO FURTHER DEFECTS NOTED</P>)

Part: WINDOW FRAME — CORRODED (ZONE 200) · corrosion level 2 · airframe 84,622 hrs · 16,956 cycles

RH PASSENGER CABIN BETWEEN STA 1197 AND STA 1197+22 AND STGR 14 RH TO STGR 16RH WINDOW FRAME WITH CORROSION(<P>CORROSION WAS REMOVED, EVALUATED, AND FOUND WITHIN PERMISSIBLE DAMAGE TOLERANCE AS CATEGORY C IAW CMA TLS 24-0208-05B. NO FURTHER DEFECTS NOTED</P>)

Part: WINDOW FRAME — CORRODED (ZONE 200) · corrosion level 2 · airframe 84,622 hrs · 16,956 cycles

LH PASSENGER CABIN BETWEEN STA 654+66 AND STA 654+88 AND STGR 14LH TO STGR 16LH WINDOW FRAME WITH CORROSION(<P>CORROSION WAS REMOVED, EVALUATED, AND FOUND WITHIN PERMISSIBLE DAMAGE TOLERANCE AS CATEGORY C IAW CMA TLS 24-0203-05B. NO FURTHER DEFECTS NOTED</P>)

Part: PLATE — CORRODED (ZONE 800) · airframe 84,622 hrs · 16,956 cycles

OVERWING EMERGENCY EXIT LH AFT DOOR, INTERNAL STRUCTURE. CORROSION EVIDENCE ON LOWER PLATE(<P>CORROSION WAS REWORKED, EVALUATED AND FOUND WITHIN ALLOWABLE LIMITS IAW SRM 52-20-02-1A-A. NO FURTHER DEFECTS NOTED</P>)

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 84,622 hrs · 16,956 cycles

CAPTAIN SEAT AFT SEAT TRACK WITH CORROSION AT CONTROL CABIN.(<P>SEAT TRACK WAS REPLACED PER AMM 25-11-01-400-803-001</P>)

Part: WINDOW FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 84,622 hrs · 16,956 cycles

LH PASSENGER CABIN BETWEEN STA 632 AND STA 654 AND STGR 14LH TO STGR 16LH WINDOW FRAME WITH CORROSION(<P>CORROSION WAS REMOVED, EVALUATED, AND FOUND WITHIN PERMISSIBLE DAMAGE TOLERANCE AS CATEGORY C IAW CMA TLS 24-0203-05B. NO FURTHER DEFECTS NOTED</P>)

Part: WINDOW FRAME — CORRODED (ZONE 200) · corrosion level 2 · airframe 84,622 hrs · 16,956 cycles

RH PASSENGER CABIN BETWEEN STA 1351 AND STA 1373 AND STGR 14 RH TO STGR 16RH WINDOW FRAME WITH CORROSION(<P>CORROSION WAS REMOVED, EVALUATED AND FOUND WITHIN PERMISSIBLE DAMAGE TOLERANCE AS CATEGORY A IAW CMA TLS 24-0204-05B. NO FURTHER DEFECTS NOTED</P>)

Part: WINDOW FRAME — CRACKED (ZONE 200) · corrosion level 2 · airframe 84,622 hrs · 16,956 cycles

RH PASSENGER CABIN BETWEEN STA 1329 AND STA 1351 AND STGR 14 RH TO STGR 16RH WINDOW FRAME WITH CORROSION(<P>CORROSION WAS REMOVED, EVALUATED AND FOUND WITHIN PERMISSIBLE DAMAGE TOLERANCE AS CATEGORY A IAW CMA TLS 24-0204-05B. NO FURTHER DEFECTS NOTED.</P>)

Part: ACCESS PANEL — PUNCTURED (ZONE 500) · airframe 84,622 hrs · 16,956 cycles

LH WING, OUTBOARD FLAP T. E. (ACCESS PANEL 566 JT) INTERNAL SURFACE HONEYCOMB WITH PUNCKTURE(<P>PUNCTURE WAS REPAIRED IAW SRM 57-53-01-2R-1 &AMP; SRM 51-70-10-2R-4. NO FURTHER DEFECTS NOTED</P>)

Part: PLATE — CORRODED (ZONE 800) · airframe 84,622 hrs · 16,956 cycles

OVERWING EMERGENCY EXIT FWD LH DOOR INTERNAL STRUCTURE, EVIDENCE. OF CORROSION ON LOWER PLATES(<P>CORROSION WAS REWORKED, EVALUATED AND FOUND WITHIN ALLOWABLE LIMITS IAW SRM 52-20-02-1A-1. NO FURTHER DEFECTS NOTED.</P>)

Part: WINDOW FRAME — CORRODED (ZONE 200) · corrosion level 2 · airframe 84,622 hrs · 16,956 cycles

LH PASSENGER CABIN BETWEEN STA 1263 AND STA 1285 AND STGR 14LH TO STGR 16LH WINDOW FRAME WITH CORROSION(<P>CORROSION WAS REMOVED, EVALUATED, AND FOUND WITHIN PERMISSIBLE DAMAGE TOLERANCE AS CATEGORY A IAW CMA TLS 24-0202-05B. NO FURTHER DEFECTS NOTED</P>)

Part: WINDOW FRAME — CORRODED (ZONE 200) · corrosion level 2 · airframe 84,622 hrs · 16,956 cycles

LH PASSENGER CABIN BETWEEN STA 1241 AND STA 1263 AND STGR 14LH TO STGR 16LH WINDOW FRAME WITH CORROSION(<P>CORROSION WAS REMOVED, EVALUATED, AND FOUND WITHIN PERMISSIBLE DAMAGE TOLERANCE AS CATEGORY C IAW CMA TLS 24-0202-05B. NO FURTHER DEFECTS NOTED.</P>)

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 84,622 hrs · 16,956 cycles

CORROSION ON FLOOR STRUCTURE STA 348 AND RBL 23 TO RBL33 AT PASSENGER CABIN.(<P>CORROSION WAS REWORKED, EVALUATED AND FOUND WITHIN ALLOWABLE DAMAGE LIMITS PER SRM 53-00-51-1A-1. NO FURTHER DEFECTS NOTED.</P>)

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 84,622 hrs · 16,956 cycles

PASSENGER COMPARTMENT FLOOR LEVEL. CORROSION ON FITTINGS GALLEY SUPPORTS AT B.STA 303 RBL 11 APPROX. (2 EA)(<P>TWO SUPPORTS (2 EA) WERE REPLACED IAW DWG 141T5262. NO FURTHER DEFECTS NOTED</P>)

Part: ANGLE — CRACKED (ZONE 100) · airframe 84,622 hrs · 16,956 cycles

CRACK ON INTERCOSTAL ANGLE BTW STA 283-287 LBL 38 AT MAIN EQUIPMENT CENTER (E/E)(<P>INTERCOSTAL WAS REPLACED BY NEW ONE PER DWG 1415140. NO DEFECTS NOTED</P>)

Part: WINDOW FRAME — CORRODED (ZONE 200) · corrosion level 2 · airframe 84,622 hrs · 16,956 cycles

RH PASSENGER CABIN BETWEEN STA 999 AND STA 1021 AND STGR 14 RH TO STGR 16RH WINDOW FRAME WITH CORROSION(<P>CORROSION WAS REMOVED, EVALUATED, AND FOUND WITHIN PERMISSIBLE DAMAGE TOLERANCE AS CATEGORY C IAW CMA TLS 24-0201-08B. NO FURTHER DEFECTS NOTED</P>)

Part: WINDOW FRAME — CRACKED (ZONE 200) · corrosion level 2 · airframe 84,622 hrs · 16,956 cycles

RH PASSENGER CABIN BETWEEN STA 1285 AND STA 1307 AND STGR 14 RH TO STGR 16RH WINDOW FRAME WITH CORROSION(<P>CORROSION WAS REMOVED, EVALUATED, AND FOUND WITHIN PERMISSIBLE DAMAGE TOLERANCE AS CATEGORY C IAW CMA TLS 24-0204-05B. NO FURTHER DEFECTS NOTED</P>)

Part: SUPPORT — CORRODED (ZONE 100) · airframe 84,622 hrs · 16,956 cycles

FUSELAGE UPPER LOBE INTERIOR PAX CABIN, AT STA 785.9 AND S-18L PLATE WITH CORROSION(<P>SUPPORT WAS REPLACED PER 25-20-00 &AMP; IPC 25-21-51-40. NO FURTHER DEFECTS NOTED</P>)

Part: STIFFENER — CORRODED (ZONE 100) · corrosion level 2 · airframe 84,622 hrs · 16,956 cycles

AFT CARGO COMPARTMENT AT STA 1087 AND STGR 36R, STIFFENER WITH CORROSION(<P>STIFFENER WAS REPLACED BY NEW ONE IAW DWG 146T1201. NO FURTHER DEFECTS NOTED</P>)

Part: WINDOW FRAME — CRACKED (ZONE 200) · corrosion level 2 · airframe 84,622 hrs · 16,956 cycles

RH PASSENGER CABIN BETWEEN STA 1197+110 AND STA 1197+132 AND STGR 14 RH TO STGR 16RH WINDOW FRAME WITH CORROSION(<P>CORROSION WAS REMOVED, EVALUATED AND FOUND WITHIN PERMISSIBLE DAMAGE TOLERANCE AS CATEGORY C IAW CMA TLS 24-0204-05B. NO FURTHER DEFECTS NOTED</P>)

Part: WINDOW FRAME — CORRODED (ZONE 200) · corrosion level 2 · airframe 84,622 hrs · 16,956 cycles

LH PASSENGER CABIN BETWEEN STA 1197.110 AND STA 1197.132 AND STGR 14LH TO STGR 16LH WINDOW FRAME WITH CORROSION(<P>CORROSION WAS REMOVED, EVALUATED AND FOUND WITHIN PERMISSIBLE DAMAGE TOLERANCE AS CATEGORY A IAW CMA TLS 24-0202-05B. NO FURTHER DEFECTS NOTED</P>)

Part: WINDOW FRAME — CRACKED (ZONE 200) · airframe 84,622 hrs · 16,956 cycles

RH PASSENGER CABIN BETWEEN STA 1153 AND STA 1175 AND STGR 14 RH TO STGR 16RH WINDOW FRAME WITH CORROSION(<P>CORROSION WAS REMOVED, EVALUATED AND FOUND WITHIN PERMISSIBLE DAMAGE TOLERANCE AS CATEGORY C IAW CMA TLS 24-0204-05B. NO FURTHER DEFECTS NOTED</P>)

Part: DOOR — CORRODED (ZONE 800) · airframe 84,622 hrs · 16,956 cycles

FWD CARGO COMPARTMENT DOOR INNER SURFACE, CORROSION AT 15'' FROM LOWER EDGE AND 5'' FROM AFT EDGE.(<P>CORROSION WAS REWORKED, EVALUATED AND FOUND WITHIN ALLOWABLE DAMAGE LIMITS IAW SRM 52-30-02-1A-1. NO FURTHER DEFECTS NOTED</P>)

Part: WINDOW FRAME — CORRODED · corrosion level 2 · airframe 84,622 hrs · 16,956 cycles

RH PASSENGER CABIN BETWEEN STA 1395 AND STA 1417 AND STGR 14 RH TO STGR 16RH WINDOW FRAME WITH CORROSION(<P>CORROSION WAS REMOVED, EVALUATED AND FOUND WITHIN PERMISSIBLE DAMAGE TOLERANCE AS CATEGORY C IAW CMA TLS 24-0204-05B. NO FURTHER DEFECTS NOTED</P>)

Part: WINDOW FRAME — CRACKED (ZONE 200) · corrosion level 2 · airframe 84,622 hrs · 16,956 cycles

RH PASSENGER CABIN BETWEEN STA 1263 AND STA 1285 AND STGR 14 RH TO STGR 16RH WINDOW FRAME WITH CORROSION(<P>CORROSION WAS REMOVED, EVALUATED, AND FOUND WITHIN PERMISSIBLE DAMAGE TOLERANCE AS CATEGORY C IAW CMA TLS 24-0204-05B. NO FURTHER DEFECTS NOTED</P>)

Part: PLATE — CORRODED (ZONE 800) · airframe 84,622 hrs · 16,956 cycles

OVERWING EMERGENCY EXIT RH FWD DOOR, INTERNAL STRUCTURE. CORROSION EVIDENCE ON LOWER PLATES(<P>CORROSION WAS REWORKED, EVALUATED AND FOUND WITHIN ALLOWABLE LIMITS IAW SRM 52-20-02-1A-1. NO FURTHER DEFECTS NOTED</P>)

Part: DOOR — NO DISCREPANCY (ZONE 800) · airframe 84,622 hrs · 16,956 cycles

FWD CARGO COMPARTMENT DOOR INNER SURFACE, CORROSION AT 15'' FROM LOWER EDGE AND 40'' FROM FWD EDGE.(<P>REWORKED, EVALUATED AND FOUND WITHIN ALLOWABLE DAMAGE LIMITS IAW SRM 52-30-02-1A-1. NO FURTHER DEFECTS NOTED</P>)

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 84,622 hrs · 16,956 cycles

FIRST OFFICER FORWARD SEAT TRACKS (2EA) WITH CORROSION(<P>SEAT TRACK WAS REPLACED PER AMM 25-11-01-822-095-001. NO FURTHER DEFECTS NOTED</P>)

Part: WINDOW FRAME — CRACKED (ZONE 200) · corrosion level 2 · airframe 84,622 hrs · 16,956 cycles

RH PASSENGER CABIN BETWEEN STA 1307 AND STA 1329 AND STGR 14 RH TO STGR 16RH WINDOW FRAME WITH CORROSION(<P>CORROSION WAS REMOVED, EVALUATED, AND FOUND WITHIN PERMISSIBLE DAMAGE TOLERANCE AS CATEGORY C IAW CMA TLS 24-0204-05B. NO FURTHER DEFECTS NOTED</P>)

Part: WINDOW FRAME — CRACKED (ZONE 200) · corrosion level 2 · airframe 84,622 hrs · 16,956 cycles

RH PASSENGER CABIN BETWEEN STA 1197+88 AND STA 1197+110 AND STGR 14 RH TO STGR 16RH WINDOW FRAME WITH CORROSION(<P>CORROSION WAS REMOVED, EVALUATED, AND FOUND WITHIN PERMISSIBLE DAMAGE TOLERANCE AS CATEGORY C IAW CMA TLS 24-0204-05B. NO FURTHER DEFECTS NOTED</P>)

Part: WINDOW FRAME — CORRODED (ZONE 200) · corrosion level 2 · airframe 84,622 hrs · 16,956 cycles

RH PASSENGER CABIN BETWEEN STA 1023 AND STA 1041 AND STGR 14 RH TO STGR 16RH WINDOW FRAME WITH CORROSION(<P>CORROSION WAS REMOVED, EVALUATED AND FOUND WITHIN PERMISSIBLE DAMAGE TOLERANCE AS CATEGORY C IAW CMA - TLS 24-0201-08B. NO FURTHER DEFECTS NOTED</P>)

Part: WINDOW FRAME — CRACKED (ZONE 200) · corrosion level 2 · airframe 84,622 hrs · 16,956 cycles

RH PASSENGER CABIN BETWEEN STA 1043 AND STA 1065 AND STGR 14 RH TO STGR 16RH WINDOW FRAME WITH CORROSION(<P>CORROSION WAS REMOVED, EVALUATED, AND FOUND WITHIN PERMISSIBLE DAMAGE TOLERANCE AS CATEGORY C IAW CMA TLS 24-0201-08B. NO FURTHER DEFECTS NOTED</P>)

Part: WINDOW FRAME — CORRODED (ZONE 200) · corrosion level 2 · airframe 84,622 hrs · 16,956 cycles

RH PASSENGER CABIN BETWEEN STA 676 AND STA 698 AND STGR 14 RH TO STGR 16RH WINDOW FRAME WITH CORROSION(<P>CORROSION WAS REMOVED, EVALUATED AND FOUND WITHIN PERMISSIBLE DAMAGE TOLERANCE AS CATEGORY C IAW CMA TLS 24-0205-08B. NO FURTHER DEFECTS NOTED</P>)

Part: WINDOW FRAME — CORRODED (ZONE 200) · corrosion level 2 · airframe 84,622 hrs · 16,956 cycles

LH PASSENGER CABIN BETWEEN STA 1021 AND STA 1043 AND STGR 14LH TO STGR 16LH WINDOW FRAME WITH CORROSION(<P>CORROSION WAS REMOVED, EVALUATED, AND FOUND WITHIN PERMISSIBLE DAMAGE TOLERANCE AS CATEGORY C IAW CMA TLS 24-0200-08B. NO FURTHER DEFECTS NOTED</P>)

Part: PLATE — CORRODED (ZONE 800) · airframe 84,622 hrs · 16,956 cycles

OVERWING EMERGENCY EXIT RH AFT DOOR, INTERNAL STRUCTURE. CORROSION EVIDENCE ON LOWER PLATE(<P>CORROSION WAS REWORKED, EVALUATED AND FOUND WITHIN ALLOWABLE LIMITS IAW SRM 52-20-02-1A-1. NO FURTHER DEFECTS NOTED</P>)

Part: SKATE ANGLE — CRACKED (ZONE 400) · airframe 84,622 hrs · 16,956 cycles

CRACK IN THE SUPPORT OF THE LH ENG PANEL NACELLE(<P>CRACK ON SKATE ANGLE WAS REPAIRED PER CMA TLS 24-0209. NO FURTHER DEFECTS NOTED</P>)

Part: WINDOW FRAME — CORRODED (ZONE 200) · airframe 84,622 hrs · 16,956 cycles

RH PASSENGER CABIN BETWEEN STA 955.1 AND STA 977 AND STGR 14 RH TO STGR 16RH WINDOW FRAME WITH CORROSION(<P>CORROSION WAS REMOVED, EVALUATED AND FOUND WITHIN PERMISSIBLE DAMAGE TOLERANCE AS CATEGORY A IAW SRM 56-20-02-1A-1. NO FURTHER DEFECTS NOTED</P>)

Part: SKIN — DENTED (ZONE 500 FLAP) · airframe 84,622 hrs · 16,956 cycles

WING LH, INBOARD FLAP, AFTER FLAP WITH SEVERAL DENTS(<P>ONE DENT WAS REPAIRED IAW SRM 57-53-01-2R-1 &AMP; SRM 51-70-10-2R-4. NO FURTHER DEFECTS NOTED.</P>)

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 84,622 hrs · 16,956 cycles

CAPTAIN SEAT FORWARD SEAT TRAKS WITH CORROSION(<P>SEAT TRACK WAS REPLACED IAW 25-11-00 &AMP; IPC 25-11-01-03. NO FURTHER DEFECTS NOTED.</P> / <P>PN: 1A098-0181 &AMP; 1A098-0183</P>)

Part: SUPPORT BRACKET — CORRODED (ZONE 100) · corrosion level 2 · airframe 84,622 hrs · 16,956 cycles

AFT CARGO COMPARTMENT, AT STA 1087 AND STGR 36L, POST WITH CORROSION AT LOWER JOINT WITH FLOOR FRAME.(<P>SUPPORT BRACKET WAS REPLACED BY NEW ONE IAW DWG 453T1727. NO FURTHER DEFECTS NOTED</P>)

Part: WINDOW FRAME — CORRODED (ZONE 200) · corrosion level 2 · airframe 84,622 hrs · 16,956 cycles

RH PASSENGER CABIN BETWEEN STA 764 AND STA 785.9 AND STGR 14 RH TO STGR 16RH WINDOW FRAME WITH CORROSION(<P>CORROSION WAS REMOVED, EVALUATED AND FOUND WITHIN PERMISSIBLE DAMAGE TOLERANCE AS CATEGORY C IAW CMA TLS 24-0201-08B. NO FURTHER DEFECTS NOTED</P>)

Part: WINDOW FRAME — CORRODED (ZONE 200) · corrosion level 2 · airframe 84,622 hrs · 16,956 cycles

LH PASSENGER CABIN BETWEEN STA 955.1 AND STA 977 AND STGR 14LH TO STGR 16LH WINDOW FRAME WITH CORROSION(<P>CORROSION WAS REMOVED, EVALUATED AND FOUND WITHIN PERMISSIBLE DAMAGE TOLERANCE AS CATEGORY A IAW CMA TLS 24-0200-08B. NO FURTHER DEFECTS NOTED.

Part: WINDOW FRAME — CRACKED (ZONE 200) · airframe 84,622 hrs · 16,956 cycles

LH PASSENGER CABIN BETWEEN STA 720 AND STA 742 AND STGR 14LH TO STGR 16LH WINDOW FRAME WITH CORROSION(<P>CORROSION WAS REMOVED, EVALUATED, AND FOUND WITHIN PERMISSIBLE DAMAGE TOLERANCE AS CATEGORY A IAW CMA TLS 24-0200-08B. NO FURTHER DEFECTS NOTED</P>)

Part: WEDGE — DELAMINATED (NR 5 SLAT) · airframe 84,622 hrs · 16,956 cycles

SLAT #5, TRAILING EDGE WEDGE, OSS. 389.7 AT UPPER INBD EDGE, PREVIOUS REPAIR DELAMINATED.(<P>DELAMINATION WAS REPAIRED PER SRM 57-43-02-2R-1 &AMP; SRM 51-70-10-2R-4. NO FURTHER DEFECTS NOTED</P>)

Part: FLASHLIGHT — INOPERATIVE (ZONE 200) · airframe 84,622 hrs · 16,956 cycles

AS REPORTED BY F/AS, MID RH EMERGENCY FLASHLIGHT INOP(<P>R/R RH MID EMERGENCY FLASHLIGHT IAW B767 AMM 25-64-00 &AMP; EEL. OPS CHECK GOOD.</P>)

Part: POWER SUPPLY — INOPERATIVE (ZONE 200) · airframe 84,567 hrs · 16,946 cycles

LH AND RH OWE (OVER WING EXIT) LIGHTS INOP(<P>CHARGED EMERGENCY LIGHTS POWER SUPPLY IAW B767 AMM 33-51-07. PERFORMED OPS CHECK OF EMERGENCY LIGHTS IAW B767 AMM 33-51-00, OPS CHECK GOOD. ALL EMERGENCY LIGHTS OPERATE NORMAL</P>)

Part: POWER SUPPLY — NO TEST (EMERGENCY LIGHTS) · airframe 84,412 hrs · 16,914 cycles

R4 &AMP; L4 DOOR INTERIOR THRESHOLD EMERGENCY LIGHTS INOP.(<P>REMOVED &AMP; REPLACED EMERGENCY POWER SUPPLY IAW B767 AMM 33-51-07, OPS CHECK GOOD. PART VERIFIED IAW B767 IPC 33-51-07-06.</P>)

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 84,307 hrs · 16,885 cycles

COCKPIT EMERGENCY EXIT SIGN INOP(<P>R/R FLIGHT DECK EMERGENCY EXIT LIGHT OPS CHECK GOOD AT THIS TIME WORK PERFORMED IN REF TO 767 AMM 33-51-01</P>)

Part: SEAL — LEAKING (EMERGENCY EXIT) · airframe 84,132 hrs · 16,843 cycles

OVERWING EMERGENCY EXIT DOOR MAKES NOISE ABOVE 10K FEET, REQUIRES REPOSITIONING(<P>FOUND DOOR SEAL DAMAGED. R/R RH FWD OVERWING EMERGENCY DOOR SEAL IAW AMM 52-09-03, OPS CHECK GOOD. PRESSURIZED A/C IAW AMM 5-51-24-782-001, NO LEAKAGE.</P>)

Part: RELAY — NO TEST (SLIDE) · airframe 84,073 hrs · 16,827 cycles

DURING SQUIB TEST #1 RH SIDE EMERGENCY SLIDE SQUIB LIGHT DOES NOT ILLUMINATE(<P>T/S WIRING FIM 25-65 FAULT TREE 818 STOPPED AT SHEET BLOCK 35. FOUND WIRE W786-102-16 WITH HIGH RESISTANCE, REPLACED WIRE W786-102-16 IAW WDM 25-65-12 AND SWPM 20-10. FOUND FAULTY TIME DELAY MODULE. REPLACED RELAY M1 IAW WDM 25-65-12. NO FURTHER DEFECTS NOTED.</P>)

Part: SLIDE — UNWANTED DEPLOY · airframe 84,073 hrs · 16,827 cycles

LH SLIDE COMPARTMENT DOOR DEPLOYED ACCIDENTLY WHILE T/S.(<P>REF LP 1787425 ITEM M13: R/R LH OVERRIDE SPOILER ACTUATOR IAW 25-65-2. OPS CHK GOOD. REF AIPC 25-65-20-01.</P> / <P>REF LP 1787425 ITEM M14: R/R INFLATOR CYLINDER IAW B767 AMM 25-65-02. OPS CHK GOOD. REF AIPC 25-65-02-01.</P> / <P>REF LP 1787425 ITEM M15: R/R FWD DOOR ACTUATOR IAW B767 SAMM 25-65-10-404-012-001. OPS CHK GOOD. NO FURTHER DEFECTS NOTED AT THIS TIME. REF AIPC 25-65-51-10.</P> / <P>REF LP 1787426 ITEM M16: R/R AFT DOOR ACTUATOR IAW B767 AMM 25-65-10-404-012-001. OPS CHK GOOD AT THIS TIME. NO DEFECTS NOTED. REF AIPC 25-65-51-10.</P> / <P>REF LP 1787426 ITEM M17: R/R LH ACTUATOR LATCH RELEASE IAW B767 AMM 25-65-11-404-012-001. OPS CHK GOOD. NO FURTHER DEFECTS NOTED. REF AIPC 25-65-11-02.</P> / <P>CLOSED SLIDE DOOR IAW B767 AMM 25-65-08.</P>)

Part: BATTERY — UNKNOWN (UNKNOWN) · airframe 83,524 hrs · 16,711 cycles

LH AFT EMERGENCY LIGHTS INOP(<P>R/R LH AFT EMERGENCY LIGHT BATTERY PACK IAW AMM 33-51-07 OPS CHECK GOOD</P>)

Part: LAMP — UNKNOWN (UNKNOWN) · airframe 83,524 hrs · 16,711 cycles

FOUND LH AFT MOST EMERGENCY EGRESS LIGHT INOP.(<P>RELAMPED LH AFT MOST EMERGENCY EGRESS LIGHT IAW AMM 33-51-06 OPS CHECK GOOD.</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 83,258 hrs · 16,652 cycles

FLIGHT ATTENDANT IN SECTION B REPORTS 25 LIFE VESTS REQUIRED BY FIM, ONLY 21 ON BOARD(<P>INSTALLED 4 MORE LIFEVESTS IN SEC 8 SPARES CABINET REF AMM 25-05-03</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 83,258 hrs · 16,652 cycles

R4 SLIDE PRESSURE GAUGE SHOWS HIGH(<P>PERFORMED R4 ESCAPE DOOR SLIDE INSPECTION WITH BUSTLE OFF PER AMM 25-66-01-206-001. NEEDLE IS IN GREEN ZONE. OK FOR SERVICE</P>)

Part: SLIDE — UNKNOWN (UNKNOWN) · airframe 83,019 hrs · 16,602 cycles

ON PREFLIGHT INSP FOUND L4 DOOR SLIDE ACCUMULATER  BOTTLE ON ZERO(<P>R/R L4 DOOR SLIDE IAW 767 AMM 25-66-01. OPS CHK GOOD</P>)

Part: AXLE — UNKNOWN (UNKNOWN) · airframe 82,882 hrs · 16,572 cycles

DURING TAXI PER ATC, REPORTED SMOKE FROM THE TIRE. WE NOTICED A "5" INDICATION FROM #3 BRAKE TEMP. CRASH AND FIRE RESPONDED AND SPRAYED THE BRAKES(<P>REMOVED AND REPLACED #2 AXLE PER B767 CMM 32-11-50 OEM REV 66 DATED 01MAR23 DAL 242382 A&AMP;P 2748903</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 82,882 hrs · 16,572 cycles

R1 EMERGENCY SIGN NOT ILLUMINATED (OVERHEAD)(<P>T/S R1 EMERGENCY LIGHT AISLE SIGN, FOUND WIRES DISCONNECTED AND TAPED. RE-TERMINATED WIRES, OPS CHECK NORMAL PER WDM 33-90-01.</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 82,850 hrs · 16,566 cycles

EMK INCOMPLETE AT L-1 POSITION.(<P>R/R EMK AT L1 POSITION IAW AMM 25-64-00. NO FURTHER DEFECTS NOTED. THIS CLEARS DMI 187646. PLACARDS REMOVED.</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 82,841 hrs · 16,564 cycles

PORTABLE OXYGEN BOTTLE USED AT L-4 LOCATION.(<P>TRANSFERRED TO MDDR 187645 PER MEL 35-31-01 CAT D, DUE DATE 16OCT2023</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 82,720 hrs · 16,540 cycles

AUTO LAND SYSTEM INOP(<P>REF MDDR 186226 FOR CORRECTIVE ACTION NR-00004. ACCOMPLISHED AFDS SYSTEM TEST PER AMM 22-10-00/501. ALL TESTS PASS. AIRCRAFT RETURNED TO CAT 3B STATUS. MDDR 186226 CLEARED. PLACARD&NBSP; REMOVED</P>)

Part: SWITCH — UNKNOWN (UNKNOWN) · airframe 82,720 hrs · 16,540 cycles

REMOVE APU "LOW OIL LEVEL SWITCH" AND REPLACE WITH APU "OIL QUANTITY TRANSMITTER"  P/N  8TJ99GGE1 AS PER TASK CARD 49-999-00-01(<P>REMOVED LOW OIL LEVEL SWITCH AND REPLACED WITH APU OIL QTY TRANSMITTER AS PER B767 AMM 49-94-04. OPS CHECK OK, NO LEAKS FOUND AT THIS TIME</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 82,720 hrs · 16,540 cycles

ROW 16 C/A EMERGENCY DOOR SURROUND DAMAGE (SPLINE  P/N  411T1205-2SP(<P>FOUND LOOSE TRIM LOCATED, CLEANED AND RESECURED LOOSE TRIM SPLINE AT MAIN CABIN ROW C/A EMERGENCY DOOR CUT OUT PER B767-300 AMM 20-30-01-992-001</P>)

Part: LAMP — UNKNOWN (UNKNOWN) · airframe 82,720 hrs · 16,540 cycles

FWD CARGO DOOR GREEN LIGHT IND IS INOP AND INTERMITTENT(<P>RELAMPED FWD CARGO DOOR GREEN LIGHT AS PER AMM 52-33-11. OPS CHECKS OK</P>)

Part: WINDSHIELD WIPER — UNKNOWN (UNKNOWN) · airframe 82,720 hrs · 16,540 cycles

F/O WIPER BLADE WORN(<P>REMOVED AND REPLACED F/O WIPER BLADE AS PER B767 AMM 30-42-03. OPS CHECK OK</P>)

Part: COMPUTER — UNKNOWN · airframe 82,720 hrs · 16,540 cycles

GPWS TERRAIN "TO LOW TERRAIN" ORAL SOUNDED BELOW 1000' AGL. WHEN STABILIZED ON ILS LOC AND G/S AND  ON SPEED(<P>REMOVED AND REPLACED EGPWS COMPUTER AS PER AMM 34-46-01. OPS CHECK OK PER 34-46-00/501. INSTALLED TERRAIN DATA BASE 996-109-633 PER AMM 34-46-00-472-001. MDDR 186478 CLEARED, PLACARD REMOVED, AUTOLAND TEST OK PER AMM 22-10-00/501</P>)

Part: PLUG — UNKNOWN (UNKNOWN) · airframe 82,720 hrs · 16,540 cycles

ENG #2 BORSCOPE, PLUG AP-9 DAMAGED(<P>REMOVED &AMP; REPLACED ENG #2 BORESCOPE PLUG AP-9 IAW 767-300 AMM 72-00-00. NO FURTHER DEFECTS NOTED.</P>)

Part: PAD — UNKNOWN (UNKNOWN) · airframe 82,720 hrs · 16,540 cycles

NLG W/W SNUBBERS PADS, WORN-OUT(<P>REMOVED WORN OUT SNUBBERS PADS, CLEANED AREA, DRILLED AND INSTALLED NEW SNUBBERS PAD AT NOSE LANDING GEAR WHEEL WELL PER B767-300 AMM 32-45-05-022-001 &AMP; AMM 32-45-05-422-007</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 82,564 hrs · 16,496 cycles

NO GREEN LIGHT ILLUMINATED FOR RH EMERGENCY ESCAPE SQUIB TEST LIGHT(<P>C/W FIM TASK 25-65 SHEET BLOCK #21. CLEANED ELECTRICAL CONNECTOR &AMP; RH WING ESCAPE SYS EMERGENCY BATTERY(M962) AND PERFORMED OPS CHECK OF WING ESCAPE SYSTEM SQUIB TEST PER AMM 25-65-00. OPS CHECKS GOOD</P>)

Part: MEDICAL KIT — UNKNOWN (UNKNOWN) · airframe 82,564 hrs · 16,496 cycles

EEMKS ARE BOTH MISSING ITEMS ( EMERGENCY MEDICAL EQUIPMENT, EMERGENCY MEDICAL KIT (EMK) AND/OR ASSOCIATED EQUIPMENT, REQUIRED BY FAR )(<P>R/R BOTH PARTS IAW AMM 25-64-03.&NBSP;</P>)

Part: FUEL FILTER — UNKNOWN · airframe 82,492 hrs · 16,479 cycles

EICAS MESSAGE: "L ENG FUEL FILTER"(<P>SEE ITEM 03 ON LOGPAGE 1615858.</P> / <P>LP 1615858 P3: R/R #1 ENG FUEL FILTER IAW AMM 73-11-02. LEAK CHECK GOOD. MSG CLEARED.</P>)

Part: FUEL FILTER — UNKNOWN · airframe 82,492 hrs · 16,479 cycles

STATUS MESSAGE: "L ENG FUEL FILT"(<P>REMOVED AND REPLACED #1 ENG FUEL FILTER IAW AMM 73-11-02. LEAK CHECK GOOD. MESSAGES CLEARED&NBSP;</P>)

Part: ACTUATOR — UNKNOWN (UNKNOWN) · airframe 82,449 hrs · 16,468 cycles

LH WING, INBOARD AILERON BOTH PCUS WITH LEAK HYDRAULIC(<P>R/R ACTUATOR ASSY - POWER CONTROL &AMP; OPS &AMP; LEAK CHECK GOOD IAW AMM 27-11-00</P>)

Part: PCA — UNKNOWN (UNKNOWN) · airframe 82,449 hrs · 16,468 cycles

VERTICAL STABILIZER REAR SPAR, UPPER PCA WITH EVIDENCE OF HYD LEAK(<P>VERTICAL STABILIZER REAR SPAR, UPPER PCA WAS REPLACED, OPERATIONAL TEST FOR LEAK WAS PERFORMED, NO LEAK FOUND IAW AMM 27-21-02-422-038 REV. 132 DATE 22 DEC 2022&NBSP;</P>)

Part: SERVO — UNKNOWN (UNKNOWN) · airframe 82,449 hrs · 16,468 cycles

VERTICAL STABILIZER REAR SPAR, LEFT YAW DAMPER SERVO WITH EVIDENCE OF HYD LEAK(<P>VERTICAL STABILIZER REAR SPAR, LEFT YAW DAMPER SERVO TORQUE WAS PERFORMED, THEN CHECK FOR LEAK, NO LEAK FOUND, THE TEST WAS PERFORMED OK FOR SERVICE IAW AMM 22-21-02-414-016 REV 138 22DEC2022.&NBSP;</P>)

Part: ACTUATOR — UNKNOWN (UNKNOWN) · airframe 82,449 hrs · 16,468 cycles

VERTICAL STABILIZER REAR SPAR, RUDDER RATIO CHANGER WITH EVIDENCE OF HYD LEAK(<P>R/R ACTUATOR ASSY - RUDDER RATIO CHANGER SERVO. OPS &AMP; LEAK CHECK GOOD IAW 27-20-00</P>)

Part: COMPUTER — UNKNOWN (UNKNOWN) · airframe 82,449 hrs · 16,468 cycles

SECTION 48, FEEL COMPUTER ELEVETOR WITH EVIDENCE OF HYD LEAK(<P>R/R COMPUTER ASSY - ELEV FEEL PN: 827 &AMP; PN:570. OPS &AMP; LEAK CHECK GOOD IAW AMM 27-30-00</P>)

Part: SEAL — UNKNOWN (UNKNOWN) · airframe 82,449 hrs · 16,468 cycles

LH WING, MAIN FUEL TANK ACCESS 542AB, 541XB, 541VB, 541UB AND 541TB WITH EVIDENCE OF LEAK(<P STYLE="MARGIN: 0CM;">LH WING, MAIN FUEL TANK ACCESS 542AB, 541XB, 541VB, 541UB AND 541TB, SEAL AND GASKET WERE REPLACED IAW AMM 28-11-00-796-111 REV 138 DEC 22, 2022</P>)

Part: PCU — UNKNOWN (UNKNOWN) · airframe 82,449 hrs · 16,468 cycles

LH WING, OUTBOARD AILERON, BOTH PCUS WITH LEAK HYDRAULIC(<P>R/R ACTUATOR - PWR CTRL OTBD AILERON &AMP; OPS &AMP; LEAK CHECK GOOD IAW AMM 27-11-00</P>)

Part: ACTUATOR — UNKNOWN (UNKNOWN) · airframe 82,449 hrs · 16,468 cycles

LH WING, SPOILER NO. 2 POWER CONTROL ACTUATOR WITH LEAK OF HIDRAULIC(<P>R/R ACTUATOR ASSY - PCA OTBD SPOILER &AMP; OPS &AMP; LEAK CHECK GOOD IAW AMM 27-61-00</P>)

Part: COMPENSATOR — UNKNOWN (UNKNOWN) · airframe 82,449 hrs · 16,468 cycles

SECTION 48, RETURN COMPENSATOR MODULE WITH EVIDENCE OF HYD LEAK(<P>R/R COMPSTR, COMPENSATOR SECTION 48 &AMP; OPS CHECK GOOD IAW AMM 27-00-00 &AMP; 29-22-02</P>)

Part: BUSHING — UNKNOWN · airframe 82,449 hrs · 16,468 cycles

RH MAIN LANDING GEAR, AFT TRUNNION BEARING, OUTER RACE WITH CORROSION(<P>RH MAIN LANDING GEAR, AFT TRUNNION BEARING, OUTER RACE, THE BUSHING WAS REPLACED IAW ENGINEERING ORDER A-32-045-01-2/001 &AMP; CMM 57-54-13. PN: 113T1108-17 &AMP; 113T1108-23</P>)

Part: PCA — UNKNOWN (UNKNOWN) · airframe 82,449 hrs · 16,468 cycles

DAMAGE - HYDRAULIC LEAK RH HORIZONTAL STABILIZER, MIDDLE PCA WITH EVIDENCE OF HYD LEAK(<P>PCA WAS REPLACED IAW AMM 27-31-05-424-027 REV 132. OPS CHECK GOOD</P>)

Part: ACTUATOR — UNKNOWN (UNKNOWN) · airframe 82,449 hrs · 16,468 cycles

ELEVATOR FEEL ACTUATOR WITH EVIDENCE OF HYD LEAK(<P>R/R ELEVATOR FEEL ACTUATOR. LEAK CHECK WAS PERFORMED, NO LEAKS FOUND. TEST AND ADJUSTMENT WERE GOOD IAW AMM 27-31-17-424-021 REV 138 DEC 22, 2022</P>)

Part: ACTUATOR — UNKNOWN (UNKNOWN) · airframe 82,449 hrs · 16,468 cycles

ENGINE 1, LH THRUST REVERSER, HYDRAULIC ACTUATOR WITH EVIDENCE OF LEAK(<P>R/R ACTUATOR - LOCKING &AMP; OPS &AMP; LEAK CHECK GOOD IAW AMM 71-80-00</P>)

Part: LCCA — UNKNOWN (UNKNOWN) · airframe 82,449 hrs · 16,468 cycles

LH WING, LATERAL CENTRAL CONTROL ACTUATOR ( M276 ) WITH LEAK HYDRAULIC.(<P>R/R ACTUATOR ASSY - CCA &AMP; OVERRIDE IAW AMM 22-13-03. OPS &AMP; LEAK CHECK GOOD</P>)

Part: BUSHING — UNKNOWN (UNKNOWN) · airframe 82,449 hrs · 16,468 cycles

LH MAIN LANDING GEAR, AFT TRUNNION BEARING, OUTER RACE WITH CORROSION(<P>THE BUSHING WAS REPLACED CORRECTLY IAW TRE 6757191 IAW SOPM 20-50-03 &AMP; CMM 57-54-13. OPS CHECK GOOD. PN: 113T1108-17 &AMP; 113T1108-23</P>)

Part: BRACKET — UNKNOWN · airframe 82,449 hrs · 16,468 cycles

RUDDER, UPPER PCA, UPPER TRANSFER BELLCRANK, FASTENER WITH FREE PLAY(<P>RUDDER, UPPER PCA UPPER TRANSFER BELLCRANK, BRACKET WAS REPLACED IAW SRM 51-10-02 PARAGRAPH 9 REV 121 DATE 15 DEC 2022. THE FASTENER OF BREACKET WAS INSTALLED AND TORQUE APPLIED 65 LB-IN.</P>)

Part: ACTUATOR — UNKNOWN (UNKNOWN) · airframe 82,449 hrs · 16,468 cycles

VERTICAL STABILIZER REAR SPAR, MIDDLE PCA WITH EVIDENCE OF HYD LEAK(<P>R/R ACTUATOR - RUDDER PWR CTRL &AMP; OPS &AMP; LEAK CHECK GOOD IAW 27-21-00</P>)

Part: PTU — UNKNOWN (UNKNOWN) · airframe 82,449 hrs · 16,468 cycles

SECTION 48, PTU AREA WITH EVIDENCE OF HYD LEAK(<P>SECTION 48, PTU WAS REPLACED, NO LEAK FOUND, OPERATIONAL CHECK SATISFACTORY IAW AMM 29-22-01-404-012 REV138 22DEC2022.</P>)

Part: GASKET — UNKNOWN (UNKNOWN) · airframe 82,449 hrs · 16,468 cycles

RH WING, MAIN FUEL TANK ACCESS 641AB, 641BB, 641DB, 641MB AND 641LB WITH EVIDENCE OF LEAK(<P>RH WING, MAIN FUEL TANK ACCESS 641AB, 641BB, 641DB, 641MB AND 641LB; SEAL AND GASKET WERE REPLACED IAW AMM 28-11-00-796-111 REV 138 DEC 22, 2022.</P> / <P>&NBSP;</P> / <P>P/N 65C33095-1 (GASKET); P/N 69-77023-1 9 (FUEL TANK)</P>)

Part: YAW DAMPER — UNKNOWN (UNKNOWN) · airframe 82,449 hrs · 16,468 cycles

VERTICAL STABILIZER REAR SPAR, RIGHT YAW DAMPER SERVO WITH EVIDENCE OF HYD LEAK(<P>VERTICAL STABILIZER REAR SPAR, RIGHT YAW DAMPER WAS REPLACE , NO LEAK FOUND IAW AMM 22-21-02-014-001 REV. 132 DATE 22 DEC. 2022</P>)

Part: ACTUATOR — UNKNOWN (UNKNOWN) · airframe 82,449 hrs · 16,468 cycles

RH WING, T/E SUPPORT STRUCTURE ON OUTBOARD AILERON ACTUATOR WITH LEAK(<P>R/R ACTUATOR - PWR CTRL OTBD AILERON &AMP; OPS &AMP; LEAK CHECK GOOD IAW AMM 27-11-00</P>)

Part: MANIFOLD — UNKNOWN (UNKNOWN) · airframe 82,449 hrs · 16,468 cycles

LH ENG, VALVE RH AND LH SIDE WITH LEAK(<P>LH ENG VALVE RH WAS REPLACED IAW 78-31-00-002-001-N01. OPS CHECK GOOD.</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 82,449 hrs · 16,468 cycles

LOWER HALF FUSELAGE, EXTERNAL SKIN. LIGHTNING STRIKE ON RIVET HEAD BELLOW 11" FROM STG 21 LH AT STA172.5(<P>LOWER HALF FUSELAGE, EXTERNAL SKIN FROM STG 21 LH AT STA172.5 RIVET WAS REMOVED AND REPLACED. AREA WAS INSPECTED AND NOT FOUND DAMAGE NOTED SRM 51-40-02-0G-0 REV 121 15-DEC-22</P>)

Part: ACTUATOR — UNKNOWN · airframe 82,449 hrs · 16,468 cycles

LH WING, LATERAL CENTRAL CONTROL ACTUATOR ( M274 ) WITH LEAK HYDRAULIC(<P>REMOVED AND REPLACED LCCA. OPS AND LEACK CHECK SATIFACTORY IAW AMM 27-11-14-494-018.</P>)

Part: WINDOW — ARCED · airframe 81,397 hrs · 16,240 cycles

# 3RH WINDOW WITH SIGN OF ELECTRICAL ARC . REMOVED # 3RH WINDOW PER B767-300 AMM 56-11-10. OK TO INSTALL NEW 3RH WINDOW. INSTALLED NEW # 3RH WINDOW PER B767-300 AMM 56-11-10. PENDING LEAK CHECK. ACCOMPLISHED R3 WINDOW LEAK CHECK PER 767-300 MM 05-51-24-782-001. NO LEAKS NOTED

Part: PLUG — NONE · airframe 81,397 hrs · 16,240 cycles

ENG. # 1 BOTH IGNITER PLUG WERE INSPECTED AND REQUIRE REPLACEMENT . REMOVED & REPLACED BOTH # 1 ENG. LOWER & UPPER IGNITE PLUGS IAW B767-300 AMM 74-21-02, PENDING OPS CHK . PERFORMED ENGINE IGNITION SYSTEM AUDIBLE TEST IAW B767-300 AMM 74-00-00-705-012. FOUND OPERATING NORMAL .

Part: SCREW — MISSING · airframe 81,397 hrs · 16,240 cycles

ENG #2, INBOARD /SIDE NACELLE STRUT HAVE SEVERAL SCREWS MISSING IN DIFFERENT PANELS. INSTALLED SCREWS AT ENGINE # 2 INBOARD SIDE NACELLE STRUT IN DIFFERENT PANELS AS PER 767-300 SRM 51-40-02-0G-0.

Part: LIGHT — DAMAGED · airframe 81,397 hrs · 16,240 cycles

APU, FIRE WALL, LEFT SERVICE LIGHT DAMAGED. REMOVED REPLACED LEFT SERVICE LIGHT ASSY SHOCKMOUNT IN APU PER 767-300 AMM 20-11-00.

Part: VALVE — WARNING MESSAGE · airframe 81,397 hrs · 16,240 cycles

FAILURE L & R FAT Z DOES NOT COMMAND THE FAV CLOSE ( POST RUN - UP MESSAGED. PERFORMED BITE TEST FOR FAMV OR FATS FAULTS ON THE AIR SUPPLY BITE MODULE . TEST PASSED NO FAULTS NOTED. SYSTEM OK; AT THIS TIME

Part: OXYGEN BOTTLE — NONE · airframe 81,397 hrs · 16,240 cycles

FWD E&E SERVICE CREW OXYGEN TO FULL . SERVICED CREW OXYGEN CYLINDER AT FWD E E& COMPARTMENT AS PER B767-300 AMM 12-15-08-603-001, AMM 35-00-00-912-005, AMM 35-11-00-206-228, AMM 35-11-00-206-233. ADVISORY CIRCULAR AC 43.13-1B PGS 9-46 THRU 9-51 PGS 9-448 THRU 9-455. PENDING LEAK CHECK. NO LEAK CHECK FOUND .OXYGEN ;P/N 801307-00&/CYLINDER S/N&NBSP; P855622

Part: SWITCH — FAULT MESSAGE · airframe 81,397 hrs · 16,240 cycles

FAILURE L & R PRV OPEN & CLOSE SWITCHES DISAGREE ( POST RUN-UP MESSAGE. PERFORMED AIR SUPPLY CONTROL SYSTEM - BITE TEST IAW AMM 36-23-00. NO FAULTS NOTED, SYSTEM OK AT THIS TIME

Part: CONE — NONE · airframe 81,397 hrs · 16,240 cycles

REMOVE INLET CONE SPINNER PER CARD A-72-402-00-02 PER INSPECTION INSTALL INLET CONE AFTER INSPECTIONS COMPLIANCE .REMOVED FRONT SEGMENT OF THE INLET CONE PER B767-300 AMM 72-31-01.OK TO REINSTALL. REINSTALLED INLET CONE SPINNER @ RH ENGINE IAW B767 AMM 72-31-01.

Part: DOOR — NONE · airframe 81,397 hrs · 16,240 cycles

REMOVE EMERGENCY EXIT DOOR LEFT TO REFORM INSPECTION PER CARD A-53-406-00-01 INSTALL EMERGENCY EXIT DOOR LEFT AFTER INSPECTION COMPLIANCE .DISARMED THE;OFFWING ESCAPE SYSTEM PER MM 767-300 25-65-00-042-001 TO ACCOMODATED LH EMERGENCY EXIT INSPECTION. REMOVED OVERWING ESCAPE HATCH PER B767-300 AMM 52-21-01 FOR INSPECTION. INSPECTION COMPLETED OK TO REINSTALL. REINSTALLED OVERWING ESCAPE HATCH PER B767-300 AMM 52-21-01. ARMED THE OFFWING ESCAPE SYSTEM PER 767-300 MM 25-65-00-442-010.

Part: EXHAUST VALVE — NOT CLOSED · airframe 81,397 hrs · 16,240 cycles

CARGO GROUND EXHAUST VALVE STATUS MESSAGE IN FLIGHT T/S& FIM 21-26& &TASK 816; EXHAUST BACK UP VALVE;V384 FAILED TO CLOSE. REMOVED & REPLACED BACK UP EXH. VALVE V384 PER MM 767 21-28-01-004-001. LEAK & OPS CHECK GOOD .

Part: SEAL — LEAKING · airframe 81,397 hrs · 16,240 cycles

EVIDENCE OF OIL LEAK FROM FWD SEAL OF L.P.C ( OIL AT 6 O'CLOCK ) RUBSTRIP CLEANED INLET SECTION OF # 1 ENG. FWD OF LPC RUBSTRIP PER B767-300 AMM 12-25-01. PERFORMED ENG. RUN UP PER AMM 767-300 71-00-00 FOR LEAK CHECK. NO LEAKS NOTED.

Part: TAPE — BROKEN · airframe 81,397 hrs · 16,240 cycles

COCKPIT CAPTAIN'S EVAS TAMPER TAPE BROKEN-FOLLOW ACTIONS LISTED ON WORK CARD A-25-999-18-01 VERIFIED BLOWER BATTERY CHECK ON CAPT EVAS PER B767-300 AMM 25-60-99. TEST PASSED INSTALLED TAMPER TAPE PER B767-300

Part: FASTENER — LOOSE · airframe 81,397 hrs · 16,240 cycles

# 2 NACELLE I/B SIDE MID SECTION HAS 1EA FASTENER NOT TORQUED & PROTRUDING SECURED FASTENER AT # 2 NACELLE INBOARD SIDE MID SECTION AS PER 767-300 SRM 51-40-02-0G-0

Part: FASTENER — LOOSE · airframe 81,397 hrs · 16,240 cycles

COCKPIT VELCRO FASTENERS ON GLARE SHIELD LOOSE FOR FIRST OFFICER'S EVAS SECURED VELCRO FASTENERS ON GLARE SHIELD AT COCKPIT FIRST OFFICER'S EVAS AS PER B767-300 AMM 25-60-99-404-006

Part: BATTERY — FAULT MESSAGE · airframe 81,397 hrs · 16,240 cycles

MAIN BATTERY CHARGER MSG .REMOVED AND REPLACED MAIN BATTERY IAW B767-300 AMM 24-31-01. MSG CLEARED .

Part: SPINNER — NONE · airframe 81,397 hrs · 16,240 cycles

REMOVE #1 INLET CONE ( SPINNER ) FOR INTERNAL SURFACE INSPECTION PER W/C A-72-402-00-01 REMOVED FRONT SEGMENT OF THE INLET CONE PER B767-300 AMM 72-31-01.OK TO REINSTALL. REINSTALLED # 1 ENG. FRONT SEGMENT OF THE INLET CONE PER B767-300 AMM 72-31-01.

Part: WINDOW — ARCED · airframe 81,397 hrs · 16,240 cycles

# 3LH WINDOW WITH SIGN OF ELECTRICAL ARC . REMOVED 3LH WINDOW PER B767-300 AMM 56-11-10. OK TO INSTALL NEW 3LH WINDOW. INSTALLED NEW # 3LH WINDOW PER B767-300 AMM 56-11-10. PENDING LEAK CHECK . ACCOMPLISHED L3 WINDOW LEAK CHECK PER 767-300 05-51-24-782-001-. NO LEAKS NOTED .

Part: PLUG — WORN · airframe 81,397 hrs · 16,240 cycles

ENG # 2 BOTH IGNITERS PLUGS WORN OUT . REMOVED & REPLACED # 2 ENG. IGNITER PLUGS IAW B767-300 AMM 74-21-02. COMPLIED WITH IGNITION SYSTEM AUDIBLE TEST NO DISCREPANCIES NOTED IAW B767-300 AMM 74-00-00-705-012-N00.

Part: FASTENER — DAMAGED · airframe 81,397 hrs · 16,240 cycles

# 1 NACELLE O/B SIDE HAS ACCESS PANEL WITH 1EA DAMAGED FASTENER . REMOVED AND REPLACED DAMAGED FASTENERS AT # 1 NACELLE OUTBOARD SIDE ACCESS PANEL AS PER 767-300 SRM 51-40-02-0G-0.

Part: CARD — FAULT MESSAGE · airframe 81,397 hrs · 16,240 cycles

FAULT: WARNING L & R HPSOV CLOSED COMMAND WAS NOT DETECTED C POST RUN - UP MESSAGES. REMOVED/REPLACED RH BLEED AIR CARD M860 OPS CHECK OK; PER AMM 36-11-12; AS PER B767-300 MM

Part: DOOR — NONE · airframe 81,397 hrs · 16,240 cycles

REMOVE EMERGENCY EXIT DOOR RH DUE TO INSPECTION PER CARD A-53-406-00-01 INSTALL EMERGENCY EXIT DOOR RH AFTER INSPECTION COMPLIANCE .(DISARMED OFFWING ESCAPE SYSTEM PER MM 767 25-65-00-042-001TO ACCOMODATED RH EMERGENCY HATCH INSPECTION. REMOVED RH OVERWING ESCAPE HATCH; PER B767-300 AMM 52-21-01 FOR INSPECTION. INSPECTION COMPLETED OK TO REINSTALL. REINSTALLED RH OVERWING ESCAPE HATCH PER B767-300 AMM 52-21-01. ARMED THE OFFWING ESCAPE SYSTEM PER 767-300 MM 25-65-00-442-010.

Part: HOSE — DAMAGED · airframe 81,397 hrs · 16,240 cycles

APU FLEXIBLE HOSE DAMAGED IN EXHAUST DUCT COOLING . REMOVED & REPLACED APU FLEXIBLE HOSE AT COOLING EXHAUST DUCT IAW B767-300 AMM 49-51-01-404-006 NO LEAK.

Part: LIGHT — INOPERATIVE · airframe 81,041 hrs

FLIGHT ATTENDANT'S EMERGENCY LIGHT AT RH MID NOT WORKING.(<P>PERFORMED OPERATION CHECK IAW B767 AMM 33-51-05, OPS CHECK GOOD.</P>)

Part: MASK — INOPERATIVE · airframe 80,918 hrs

FIRST OBSERVER SEAT INOP (O2 MASK INOP)(<P>TRANSFERRED TO MDDR 162097 IAW MEL 25-11-02-01A, CAT A.</P> / <P>REPLACED OBS O2 MASK IAW AMM 35-11-51. THIS CLEARS MDDR 162097. ACL 2311Z</P>)

Part: NONE — NONE · airframe 80,680 hrs · 16,077 cycles

ENG. #1 FAN BLADES MARKED 36, 5,6,7,10 &AMP; 11 WERE FOUND WITH NICKS NEAR UPPER AREA .(<P><SPAN>BLENDED CUT # 1 ENG&NBSP; FAN BLADES&NBSP; WITH NICKS&NBSP; FOUND&NBSP; WITHIN&NBSP; LIMITS AND NOT&NBSP; OTHER&NBSP; DEFECTS&NBSP; NOTED&NBSP; AT THIS TIME&NBSP; PER&NBSP; B767-300&NBSP; &NBSP; AMM&NBSP; &NBSP; 12-31-02-308-003-Y00</SPAN></P> / <P><SPAN>PERFORMED&NBSP; &NBSP;NDT&NBSP; SPOT&NBSP; FPI&NBSP; AND&NBSP; EDDY CURRENT INSPECTION&NBSP; &NBSP; NO NICK&NBSP; ON CRACK&NBSP; IND&NBSP; NOTED&NBSP; AT THIS&NBSP; TIME</SPAN></P> / <P><SPAN>REF&NBSP; &NBSP;AMM&NBSP; 70-11-06&NBSP; &NBSP;AND&NBSP; &NBSP;72-31-02-404</SPAN></P>)

Part: NONE — NONE · airframe 80,680 hrs · 16,077 cycles

COCKPIT 2ND OBS SEAT LIFE VEST MISSING P/N RSS-301CP .(<P>INSTALLED LIFE VEST AT 2ND OBS SEAT LOCATION AS PER B767-300&NBSP; AMM 25-60-00</P>)

Part: NONE — NONE · airframe 80,680 hrs · 16,077 cycles

ENG . # 1 FAN BLADE MARKED # 13 HAS A NICK AT LOWER AREA .(<P><SPAN>BLENDED&NBSP; OUT&NBSP; #1&NBSP; &NBSP;ENG&NBSP; FAN&NBSP; BLADES&NBSP; WITH&NBSP; NICK&NBSP; &NBSP;FOUND WITHIN&NBSP; LIMITS&NBSP; AND&NBSP; NOT&NBSP; OTHER&NBSP; DEFECTS&NBSP; NOTED&NBSP; &NBSP;AT&NBSP; THIS&NBSP; TIME&NBSP; &NBSP; PER&NBSP; B767-300&NBSP; &NBSP; &NBSP; &NBSP;AMM&NBSP; &NBSP; 72-31-02-308-003-N00</SPAN></P> / <P><SPAN>PERFORMED&NBSP; NDT&NBSP; SPOT&NBSP; FPI&NBSP; &NBSP;AND&NBSP; EDDY&NBSP; CURRENT&NBSP; INSPECTION NO&NBSP; NICK&NBSP; ON&NBSP; CRACK&NBSP; IND.&NBSP; NOTED&NBSP; &NBSP; AT&NBSP; &NBSP;THIS&NBSP; TIME REF&NBSP; AMM&NBSP; 70-11-06&NBSP; &NBSP;AND&NBSP; AMM&NBSP; 72-31-02-404</SPAN></P>)

Part: ELT — NONE · airframe 80,680 hrs · 16,077 cycles

FWD VCC CLOSET ELT AUTO RELEASE SEAL DAMAGE P/N 1151324-1 S/N 1151324-08440(<P>REMOVED AND REPLACED ELT FROM FWD&NBSP; VCC CLOSET AS PER B767-300&NBSP; AMM 25-10-00</P>)

Part: NONE — NONE · airframe 80,680 hrs · 16,077 cycles

ENG. # 1 FAN BLADE MARKED # 19 HAS A DENT NEAR UPPER AREA .(<P><SPAN>NOT&NBSP; DENT&NBSP; FOUND&NBSP; AT&NBSP; THIS TIME&NBSP; &NBSP;FOUND NICK&NBSP; BLENDED&NBSP; OUT&NBSP; FAN&NBSP; BLADES&NBSP; AT&NBSP; #1&NBSP; ENG&NBSP; &NBSP;FOUND&NBSP; WITHIN&NBSP; LIMITS</SPAN></P> / <P><SPAN>AND NOT OTHER DEFECTS&NBSP; NOTED AT THIS TIME&NBSP; &NBSP;PER&NBSP; B767-300&NBSP; &NBSP;AMM&NBSP; 72-31-02-308-003-N00</SPAN></P> / <P><SPAN>PERFORMED&NBSP; NDT&NBSP; SPOT&NBSP; FPI&NBSP; AND&NBSP; EDDY&NBSP; CURRENT INSPECTION&NBSP; NO NICK ON&NBSP; CRACK&NBSP; INDICATION&NBSP; NOTED&NBSP; REF&NBSP; AMM</SPAN></P> / <P><SPAN>70-11-06&NBSP; &NBSP; AND&NBSP; 72-31-02-404</SPAN></P>)

Part: NONE — NONE · airframe 80,680 hrs · 16,077 cycles

ENG # 1 LOWER FAN BLADE AREA FOUND TO HAVE AN ACCUMULATION OF OIL .(<P>PERFORMED GVI OF ENGINE #1 LOWER FAN BLADE AREA &AMP; FOUND LEAK WITHIN ALLOWABLE LIMITS PER</P> / <P>AMM 72-00-00-206-231-N00 PAR 2 SEC F STEP&NBSP; 3 (D) .</P>)

Part: BRACKET — NONE · airframe 80,680 hrs · 16,077 cycles

FWD &AMP; AFT MEGAPHONE CLAMPS DAMAGE.(<P>REMOVED AND REPLACED 2EA BRACKET AT FWD &AMP; AFT MEGAPHONE PER B767-300. AMM 20-11-00-910-802</P>)

Part: PLUG — NONE · airframe 80,680 hrs · 16,077 cycles

ENG # 2 BORESCOPE PLUG AP-9 DAMAGED .(<P>REMOVED AND REPLACED ENG #2 BORESCOPE PLUG AP-9 IAW AMM 72-00-00-206-344</P>)

Part: DOOR — NONE · airframe 80,680 hrs · 16,077 cycles

LEFT ENG. T/R OTBD BLOCKER DOOR BETWEEN 10 &AMP; 11 O' CLOCK DELAMINATED .(<P>REMOVED AND REPLACED LH ENG T/R BLOCKER DOOR BETWEEN 10 &AMP; 11 O'CLOCK POSITION PER</P> / <P>AMM 78-31-14. OPS CHECK GOOD. NO DEFECTS NOTED.</P>)

Part: NONE — NONE · airframe 80,467 hrs · 16,018 cycles

L ENG HPSOV EICAS WITH ASSOCIATED STATUS MSG(<P>PERFORMED AIR SUPPLY CONTROL SYS BITE TEST IAW TASK 36-23-00-715-001. SYS CHK OK. A/C OK FOR DISPATCH.&NBSP;</P>)

Part: NONE — NONE

L ENG SPEED CARD STATUS MSG(<P>ACCOMPLISHED SYSTEM CHECK FOR FIM 73-22 FT 871. FOUND OK.</P>)

Part: HPC — UNRELIABLE · 15,925 cycles

LEFT ENGINE HPSOV CLOSED AND OPEN SWITCHES DISAGREE EICAS MSG.(<P>&NBSP;IT WAS REPLACED THE CONTROLLER ASSY - HIGH PRESSURE IAW AMM 36-11-08-004-050-008.</P>)

Part: SPLICE PLATE — LEAKING · 15,925 cycles

FUEL LEAK EVIDENCE ON CENTER WING AT BODY SPLICE PLATE AREA BETWEEN STRINGER L-6 AND LBL97.95(<P>FUEL LEAK WAS REPAIRED PER AMM 28-11-00-308-013.</P>)

Part: MARKER — MISSING · 15,925 cycles

PHOTOLUMINESCENT ESCAPE PATH MARKING AT STA 478 (RH SIDE) AND STA 933 (LH SIDE) WITH BLUE FILTER MISSING(<P>SECTIONS OF <SPAN>PHOTOLUMINESCENT ESCAPE PATH MARKING WERE REPLACED</SPAN></P>)

Part: SPLICE PLATE — LEAKING · airframe 80,042 hrs · 15,925 cycles

FUEL LEAK EVIDENCE ON CENTER WING AT BODY SPLICE PLATE AREA BETWEEN STRINGER L-15 AND LBL97.95(<P>FUEL LEAK WAS REPAIRED PER AMM 28-11-00-308-013</P>)

Part: PCA — LEAKING · airframe 80,042 hrs · 15,925 cycles

HYDRAULIC LEAK ON LEFT OUTBOARD AILERON POWER CONTROL ACTUATOR, INBOARD SIDE(<P>IT WAS REPLACED THE L<SPAN>EFT OUTBOARD AILERON POWER CONTROL ACTUATOR, INBOARD SIDE</SPAN></P>)

Part: INSERT — MISSING

PHOTOLUMINESCENT ESCAPE PATH INSERT MISSING (CLOSE TO EMERGENCY EXIT, FWD - RH SECTION)(<P><SPAN>PHOTOLUMINESCENT ESCAPE PATH INSERT WAS INSTALLED</SPAN></P>)

Part: PCA — LEAKING · airframe 80,042 hrs · 15,925 cycles

HYDRAULIC LEAK ON LEFT OUTBOARD AILERON POWER CONTROL ACTUATOR (PCA), OUTBOARD SIDE(<P>IT WAS REPLACED THE LEFT OUTBOARD AILERON POWER CONTROL ACTUATOR (PCA), OUTBOARD SIDE</P>)

Part: SPLICE PLATE — LEAKING · airframe 80,042 hrs · 15,925 cycles

FUEL LEAK EVIDENCE ON CENTER WING AT BODY SPLICE PLATE AREA BETWEEN STRINGER L-10 AND LBL97.95(<P>FUEL LEAK WAS REPAIRED PER AMM&NBSP;<SPAN> 28-11-00-308-013.</SPAN></P>)

Part: RELAY — FAULTED (WING ANTI-ICE) · 15,924 cycles

AFTER ENGINE START, EICAS MSG L WING ANTI-ICE. FOLLOWED QRH AND R WING ANTI-ICE APPEARED.(<P>PER 767 FIM TROUBLESHOT &AMP; FOUND FAULTY L/H ANTI ICE WING VALVE. REMOVED AND REPLACED ANTI ICE WING REG &AMP; S/O VALVE ON LEFT SIDE IAW 767 AMM 30-11-02-004-001. OPS CHECK BAD. OPS LEAK CHECK GOOD. NEEDS FURTHER TROUBLESHOOTING. S/N OFF: 0306, P/N OFF: 2870537-104.</P> / <P>LP 1315360, ITEM M3: REMOVED AND REPLACED RELAY K1156(L-WING TAI DISAGREE) IAW AMM FIM TASK 30-11 FAULT TREE 803 BLOCK 25, C/W L &AMP; R OPS CHECKED GOOD.</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (RT A/C PACK) · airframe 80,027 hrs

R PACK TEMP EICAS MSG DISPLAYED. PERFORMED QRH(<P>PERFORMED PACK TEMP CONTROLLER BITE TEST IAW FIM 21-51-FT103 NO FAULTS NOTED. OPS TEST OK.</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION · airframe 79,989 hrs

IDLE DISAGREE EICAS MESSAGE ON DESCENT(<P>CHECKED BOTH PIMUS FOR FAULTS ..NO FAULTS STORED ..ALL OK PER FIM 73-21 FAULT TREE 824 ALL TEST OK</P>)

Part: BLADE — ERODED (NR 1 ENG HPT)

ON BORESCOPE INSPECTION FOUND HPT 1 BLADES WITH L/E AND CONCAVES SIDE EROSION ON SEVERAL BLADES ENGINE #1 S/N P729132(<P>BLADES CAN CONTINUE IN SERVICE AT REDUCED INTERVAL INSEPCTIONS OF 125 CYCLES REF B767 AMM 72-00-00/601. TRANS TO ATLAS MCI # A-005&NBSP; FOR REINSEPCTIONS ATLAS POWER PLANT ENGINEERING ADVISED.</P>)

Part: HOSE — LEAKING (OXYGEN SYSTEM) · 15,844 cycles

FOUND O2 LEAK BEHIND 1ST OBS O2 MASK BOX(<P>REMOVED AND REPLACED HOSE ASSY ON 1ST OBS O2 MASK BOX. NO LEAK NOTED IAW MM 20-10-10 AND 35-11-51</P>)

Part: INDICATION SYS — MALFUNCTIONED (FUEL SYSTEM)

RH ENG FUEL ON COMMAND BUG NOT DISPLAYED WITH FUEL CTRL SWITCH ON DURING ENG START.(<P>TRANSFERRED TO MDDR 149589 PER MEL 77-12-02, CAT B, DUE 06JUL21.</P> / <P>07JUL21- LP 1311610- ITEM #13- MIA- PERFORMED ENGINE RUN IAW AMM 71-00-00. THIS CLEARS MDDR 149589.</P>)

Part: TRANSMITTER — FLUCTUATES (APU OIL) · airframe 79,620 hrs

DURING APU RUNNING, FOUND OIL IND FLUCTUATE(<P>R&AMP;R APU OIL TRANSMITTER REF AMM 49-94-04, OPS CK GOOD, LK CK GOOD, NO OTHER DEFECT NOTED</P>)

Part: INDICATION SYS — MALFUNCTIONED (RT ENG FULE)

RIGHT ENGINE FUEL ON COMMAND BUG DISAPPEARS WHEN IGNITION IS SELECTED TO GND(<P>PERFORMED OPS TEST RT ENGINE FUEL COMMAND BAR IAW AMM 77-12-00, NO DEFECTS NOTED, BUG IN PLACE WHEN GND SELECTED, CHECKED 3 TIMES&NBSP;</P>)

Part: BULB — INOPERATIVE (FUEL PUMP SWITCH) · airframe 79,512 hrs · 15,813 cycles

RH FWD FUEL PUMP INOP (ER-120 RESTRICTED))( MAIN TANK FUEL PUMPS (NOTIFY DISPATCH) )(<P>DEFERRED IAW MEL 28-22-01, MDDR 148854, CAT C, DUE 25JUN21, PLACARD INSTALLED.</P> / <P>20JUN21 - LP 1187279 - ITEM # 11 - BWI - RELAMPED RH FWD FUEL PUMP SWITCH IAW B767 AMM 33-16-02/201. RESET R FUEL BOOST PUMP C/B. OPS TEST NORMAL "ON" BACK LIGHT OPS TEST NORMAL. THIS CLEARS MDDR 148854. PLACARD REMOVED.</P>)

Part: SELECTOR PANEL — FAULTED (LT ENGINE START) · airframe 79,419 hrs · 15,794 cycles

L ENGINE START SELECTOR STICKS IN GND POSITION DURING START. NO ASSOCIATED EICAS MESSAGE SHOWS(<P>TRANSFERRED TO MDDR&NBSP;148258 IAW MEL&NBSP;80-11-02, CAT C.</P> / <P>15JUNE21 - 1484745 - ITEM# 14 - BWI - REPLACED ENGINE IGNITION AND STARTING PANEL PER AMM 80-11-51. OPS CHECK GOOD. THIS CLEARS MDDR 148258. PLACARDS REMOVED.</P>)

Part: WARNING MESSAGE — FALSE INDICATION (APU) · airframe 79,391 hrs · 15,788 cycles

APU FAULT EICAS(<P>PERFORMED ECU BITE TEST IAW AMM 49-61-05, OPERATIONAL TEST OK.</P>)

Part: WARNING LIGHT — INOPERATIVE (OIL PRESSURE) · airframe 79,151 hrs · 15,738 cycles

LEFT ENG. OIL PRESSURE LIGHT INOP ( LOW ENG OIL PRESS INDICATION SYSTEM (-200/-300), ALL EXCEPT JT9D WITHOUT SB767-78-8 INSTALLED, AND CF6-80A/A2 WITHOUT SB767-78-8 INSTALLED )(<P>TRANSFER TO MDDR# 146554 IAW DDG 79-33-01-01 CAT "C" DUE DATE 17MAY21. PLACARD INSTALLED. C/W DDG PROCEDURES.</P><P>LP 1475963: REMOVED AND REPLACED LH ENGINE OIL PRESS LIGHT ASSY PER SWPM 20-84 AND SWITCH FUNCTION OPS CHECK GOOD, THIS CLEARS MDDR 146554.</P>)

Part: RADAR — UNKNOWN (WX SYS) · airframe 79,142 hrs

NO RADAR OR TERRAIN DATA DISPLAY ON FIRST OFFICERS MAP DISPLAY(<P>PERFORMED WEATHER RADAR SYSTEM TEST IAW AMM 34-43-00. OPS CHK GOOD.<BR /></P>)

Part: APU — SHUTDOWN · airframe 78,768 hrs · 15,656 cycles

APU SHUTDOWN AFTER BLOCKING IN.(<P>PERFORMED APU ECU BITE TEST IAW AMM 49-11-00/501. SYS OK, APU OK FOR SERVICE.</P>)

Part: SWITCH — INOPERATIVE (APU GENERATOR) · airframe 78,812 hrs · 15,665 cycles

APU INOP.(<P>TRANSFER TO MDDR 143540 IAW DDG 49-11-01B CAT C DUE DATE 11MAR21 PLAC INSTALLED. DISPATCH NOTIFIED.</P><P>LP 1332457: T/S PER FIM 49-11-998 AND FOUND GEN FILER DELTA P SWITCH FAULTY. REMOVED AND REPLACED DIFF PRESS SWITCH PER AMM 49-27-15, OPS OK. MCC NOTIFIED. PLACARDS REMOVED.THIS CLEARS MDDR #143540.</P>)

Part: ECU — MALFUNCTIONED (APU) · airframe 78,789 hrs · 15,660 cycles

APU INOP(<P>TRANSFER TO MDDR 143411 IAW DDG 49-11-01A CAT C DUE DATE 16MAR.</P><P>LP 1334244: PERFORMED FIM 49-11 FT 869 FROM BLK 01 TO 27. REMOVED AND REPLACED APU ECU IAW AMM 49-61-05. SYSTEM OPERATIONAL. TEST OK. CLEARED MDDR 143411. PLACARD REMOVED. DISPATCH NOTIFIED.</P>)

Part: PANEL — MISSING (THRUST REVERSER) · airframe 78,776 hrs · 15,658 cycles

ON POST FLIGHT WALK AROUND FOUND #1 ENGINE INBOARD TR STRUT AT 3 O'CLOCK POSITION LOOKING FWD, PANEL MISSING (INTERMEDIATE CASE)(<P>TRANSFERRED TO NON-MEL 143363 LOWER INTERMEDIATE FAIRING INBOARD SIDE # 1 ENGINE 3 O'CLOCK POSITION FWD FROM AFT OF ENGINE MISSING, MUST BE REPLACED BEFORE 101 FLIGHT HOURS PER AMM 72-34-05 NON MEL # 143363 INSPECTED PER AMM 73-34-05. NO OTHER DAMAGE.</P><P>BWI, 13MAR, LP 1334270, ITEM M4: INSTALLED NEW FAN EXIT FAIRING ON LEFT ENGINE INBOARD STRUT 3 O'CLOCK IAW AMM 72-34-05-308-015-N00. OK FOR SERVICE. THIS CLEARS NONMEL 143363.</P>)

Part: FAIRING — MISSING (THRUST REVERSER) · airframe 78,706 hrs

LEFT ENGINE INBOARD THRUST REVERSER COWL INTERMEDIATE CASE STRUT FAIRING MISSING AT THE 5:30 O'CLOCK POSITION VIEWING AFT.&NBSP;&NBSP;(<P>INSTALLED NEW FAN EXIT FAIRING ON LEFT ENGINE INBD STRUT 5:30 O'CLOCK IAW AMM 72-34-05-308-015-N00. OK FOR SERVICE.<BR /></P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (GENERATOR FILTER) · airframe 78,687 hrs · 15,639 cycles

APU BITE SYS MSG REMOVED AND REPLACED GENERATOR SCAVENGE FILTER IAW AMM 49-27-03. NO CONTAMINANTS FOUND. OPS CKS AND LEAK CKS GOOD.

Part: MASK — MISSING (PORTABLE OXY SYS) · airframe 78,626 hrs · 15,628 cycles

1 MASK MISSING LEFT FWD O2 CYLINDER. PORTABLE OXYGEN DISPENSING UNITS, BOTTLE AND MASK. FWD TO MDDR 141745 IAW DDG 35-31-01, CAT D. PLACARD INSTALLED. 04FEB21 - 1193407 - M6 -& MIA - INSTALLED MISSING MASK AT THE LT FWD O2 CYLINDER AS PER AMM 35-31-01. THIS CLEARS MDDR 141745.

Part: WARNING MESSAGE — FALSE ACTIVATION (RT ENGINE) · airframe 78,520 hrs · 15,605 cycles

EICAS AND STATUS MESSAGE: "RT ENGINE CONTROL" AFTER LANDING, REF B767 FIM 73-21-00-815-825-N00. FIM STATES ACCOMPLISH PIMU BIT. ACCOMPLISHED BIT, PER B767 FIM 71-01 FAULT TREE 803, BIT TEST OK, NO CURRENT FAULTS. OK TO CONTINUE.

Part: FUEL CONTROL — MALFUNCTIONED (NR 1 ENGINE) · airframe 78,522 hrs · 15,606 cycles

ITEM NR 1 RIGHT ENGINE FUEL CONTROL EICAS MESSAGE ON LANDING. ACCOMPLISHED PIMU BIT, REF B767 FIM 71-01 FAULT TREE 803, NO FAULTS FOUND. PLACED EEC NORM MODE (BOTH ENGINES) ON DEFERRAL, PER MEL 73-21-01-02 DMI 141111, DUE DATE 29JAN21 CAT C, MCC AND DISPATCH NOTIFIED AND PLACARDS INSTALLED. BOTH ENGINES IN ALTN. FOUND "P0 LINE FAIL" ON PIMU, FOLLOWED FIM 71-01 TASK 866. CHECKED PAMB WATER TRAP & FOUND EXCESSIVE WATER DEBRIS, CLEARED TRAP, IAW AMM 73-21-04/601. PIMU BIT GOOD. NO FAULTS. THIS CLEARS MEL, PLACARD REMOVED & MX PROCEDURES C/W.

Part: WARNING MESSAGE — FALSE ACTIVATION (RT ENGINE) · airframe 78,500 hrs · 15,601 cycles

RT ENGINE CONTROL EICAS MESSAGE UPON LANDING. PERFORMED PIMU BITE TEST, IAW FIM 73-21 FT 826. SYSTEM TEST OK.

Part: LAMP — NO TEST (EMERGENCY LIGHTS) · airframe 78,429 hrs · 15,586 cycles

EXTERIOR DR R4 MOUNTED EMERGENCY LIGHT FAILED TO ILLUMINATE DURING TEST. REMOVED AND REPLACED EMERGENCY LIGHT LAMP. OPERATIONS CHECKS GOOD, IAW AMM 33-51-06.

Part: START VALVE — MALFUNCTIONED (LT ENGINE) · airframe 78,408 hrs · 15,583 cycles

DURING T/C "T2051" FOUND UPON IDLE ENGINE RUN UP (L) START VALVE LIGHT DOES NOT INDICATE. REMOVED AND REPLACED LT ENGINE START VALVE, PER AMM 80-11-02. OPERATIONS CHECK SUCCESSFUL.

Part: BULB — INOPERATIVE (IDICATOR) · airframe 78,387 hrs · 15,579 cycles

RT GEN DRIVE DISCONNECT INOPERABLE. TRANSFER TO MDDR NR 139399, IAW DDG 24-11-01-01A, CAT "B", DUE DATE 15DEC20. C/W DDG PROCEDURES. DISPATCH NOTIFIED 1012Z TS. PLACARD INSTALLED. RELAMPED RT GEN DRIVE DISCONNECT INDICATOR, IAW AMM 24-11-01. OPERATIONS CHECK GOOD. THIS CLEARS MDDR NR 139399. PLACARD REMOVED.

Part: RADAR — MALFUNCTIONED · airframe 78,236 hrs · 15,544 cycles

F/O (RIGHT SIDE) WEATHER AND TERRAIN MODES INOPERABLE. PERFORMED TCAS BITE TEST, IAW B767 FIM TASK 34-45 FT 811. OPERATIONS CHECK GOOD. SYSTEM WORKING PROPERLY, NO DEFECTS NOTED.

Part: CONTROL PANEL — MALFUNCTIONED (WX RADAR SYS) · airframe 78,160 hrs · 15,529 cycles

F/O WX RADAR SWITCH DID NOT TURN ON RADAR DISPLAY. REMOVED AND REPLACED F/O EFIS CONTROL PANEL, PER AMM 34-22-02/201. OPERATIONS CHECK GOOD, PER AMM 34-43-00/ 501.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 78,135 hrs · 15,524 cycles

COCKPIT EMERGENCY EXIT LIGHT ASSEMBLY INOPERABLE. REMOVED AND REPLACED COCKPIT EMERGENCY EXIT LIGHT ASSEMBLY, IAW AMM 33-51-00. OPERATIONAL CHECK OK.

Part: SENSOR — MALFUNCTIONED (FAN AIR TEMP) · airframe 77,960 hrs · 15,488 cycles

LT ENGINE BLEED OVERHEAT DURING DESCENT, WITH IDLE POWER AT APROXIMATELY FL 250. ENGINE BLEED RESET, PER QRH PROCEDURE. WITHOUT FURTHER INCIDENT. TRANSFERRED TO MEL 36-12-02-01, MDDR 135795, CAT C, MBCB 19OCT20. MAINT PROCEDURES C/W. PLACARDS INSTALLED DISPATCH NOTED LC AT 1808Z. REMOVED AND REPLACED FAN AIR TEMP SENSOR, PER 36-11-17. REQUIRES OPERATIONS TEST, NO FAULTS. THIS CLEARS MDDR 135795.

Part: CONTROLLER — MALFUNCTIONED (CABIN PRESSURE) · airframe 77,946 hrs · 15,484 cycles

CABIN ALT EICAS AT FL 39.0 OUTFLOW VALVE UNCONTROLLABLE. ITEM 1: FOUND UNDER WING FAIRING SUPPORT AIR CONDITIONING GROUND SEV CONNECTION DUCT SUPPORT BRACKET ASSEMBLY DAMAGE AND ATTACHED AIR CONDITIONING DUCT DISCONNECTED. ACCOMPLISHED REPAIR, PER EO NO 6753A884. LEAK CHECK GOOD. ITEM 2: REMOVED AND REPLACED BOTH CABIN ALT CONTROLLERS AUTO 1 & AUTO 2, IAW B767 AMM 21-31-02. NO DEFECTS NOTED, OPS CHECK OF AUTO 1 & AUTO 2 GOOD, IAW B767 FIM 21-31 FAULT TREE 803 AT THIS TIME. ITEM 3: REMOVED AND REPLACED CABIN ALT CONTROLLER ON P5 PANEL, IAW B767 AMM 21-31-01. OPS CHECK, IAW B767 AMM 21-31-01. NO DEFECTS NOTED AT THIS TIME. C/W SYSTEM TEST OF EQUIPMENT COOLING, IAW B767 AMM 21-58-00. NO DEFECTS NOTED AT THIS. C/W EXCESSIVE CABIN PRESSURE LEAKAGE TEST, IAW B767 AMM 05-51-24. OFF PARTS: P/N 2117388-6, SN 108-1547, PN 130502-7, SN 114-A0307.

Part: CONTROLLER — MALFUNCTIONED (PRIORITY VALVE) · airframe 77,919 hrs · 15,478 cycles

EICAS MSG: LT ENGINE BLEED OFF. REMOVED AND REPLACED LEFT ENGINE PRV CONTROLLER, IAW AMM 36-11-19. DRY MOTORED ENGINE AND FOUND NO LEAKS. PERFORMED ENGINE RUN, IAW AMM 71-00-00, OPERATIONS NORMAL. OBSERVED NORMAL DUCT PRESSURE. DUCT PRESSURE REMAINED STEADY THROUGH FULL PNEUMATIC LOAD. S/N OFF: 900350, P/N OFF: 792755-16. REMOVED AND REPLACED PRV, IAW AMM 36-11-10, NO LEAKS NOTED. OPERATIONS CHECK GOOD.

Part: SENSOR — MALFUNCTIONED (FAN AIR TEMP) · airframe 77,917 hrs · 15,477 cycles

LEFT BLEED OFF EICAS MESSAGE. COMPLIED WITH QRH. REPLACED FAN AIR TEMP SENSOR WITH SERVICEABLE UNIT, IAW AMM 36-11-17-004-001. OPS CHECKS NORMAL.

Part: MODULATING VALVE — INOPERATIVE (CABIN TEMP) · airframe 77,905 hrs · 15,474 cycles

FWD CABIN TEMP HOT/ZONE TRIM AIR MODULATING VALVES, PASSENGER, INOPERATIVE VALVE CLOSED. TRANSFERRED TO MDDR 134780, IAW MEL & 21-61-04-01A, CAT C. R & R MODULATING VALVE ASSY (P/N 398786-5), IAW AMM 21-61-05. OPS CK GOOD, NO FAULTS NOTED. THIS CLEARS MEL 21-61-04-01A DMI 134780. PLACARD REMOVED. T/I 0270/DP.

Part: SELECTOR — FAILED (CABIN PRESSURE) · airframe 77,883 hrs · 15,469 cycles

CABIN ALTITUDE UNCONTROLLABLE AT FL 360, OUTFLOW VALVE UNCONTROLLABLE. CABIN ALT AUTO 2 STATUS MESSAGE, CABIN ALTITUDE EICAS MESSAGE. REMOVED AND REPLACED SELECTOR CBN PRESSURE, IAW AMM 21-31-01. OPS CHECK NORMAL.

Part: A/C PACK — MALFUNCTIONED (LEFT) · airframe 77,739 hrs · 15,441 cycles

LEFT AC PACK NOT COOLING PROPERLY VERY DIFFICULT TO MAINTAIN CABIN TEMP ON GROUND ,,REF PREV WRITE UP ON PAGE 1140366(<P>INSPECTED LEFT A/C PACK COMPONENT BITE IS DONE ON BOTH ZONE TEMP CONTROL UNIT AND LEFT PACK TEMP CONTROL,PACK AND TRIM VALVES OPERATIONAL CHECK PREFORMED NO FAULTS FOUND AT THIS TIME PER AMM 21-51-00</P>)

Part: INDICATOR — INOPERATIVE (FUEL SYS) · airframe 77,711 hrs · 15,435 cycles

UPON ENTERING COCKPIT NOTICED "RIGHT FUEL INDICATOR AND FUEL TOTAL INDICATOR" NOT DISPLAYED.(<P>PERFORMED ENG RUN. RESET FUEL SYSTEM PAGE ON FMC PER 71-00-00<BR /></P>)

Part: RADAR — MALFUNCTIONED (WEATHER) · airframe 77,599 hrs · 15,412 cycles

L RADAR SHOWS ALMOST SOLID GREEN &AMP; YELLOW WITH NO PRECIP AND TILT TO MAX HIGH(<P>TRANSFERRED TO MDDR 132837 PER MEL 34-43-01, CAT D, DUE 11DEC20.&NBSP;</P><P>BWI, 14AUG, LP 1288010, ITEM M11: ACCOMPLISHED OPERATIONAL CHECK OF WX SYS. NO DISCREPANCIES NOTED IAW AMM 34-43-00/501. THIS ACTION CLEARS DMI # 132837. PLACARD REMOVED. DISP. ST @ 23:40Z.</P>)

Part: WARNING LIGHT — FALSE ACTIVATION (RT GENERATOR) · airframe 77,474 hrs · 15,382 cycles

RIGHT GENERATOR FIELD OFF LIGHT ILLUMINATED. PERFORMED AN OPS CHECK OF THE RT IDG IAW AMM 24-11-00. OPS CHECKED GOOD, LIGHT EXTINGUISHED.

Part: CIRCUIT BREAKER — MALFUNCTIONED · airframe 77,361 hrs · 15,358 cycles

CREW DEBRIEF ON RT GENERATOR ISSUE, AFTER TAKE OFF, RT GENERATOR NEVER TRIPPED OFF, GENERATOR LIGHT AND ALL OVERHEAD LIGHTS AND CREW FLORESCENT LIGHTS WENT DIM, BRIGHT, AND DIM. EICAS MESSAGE FO TRANSFER MESSAGE CAME ON AND OFF WITH REGULAR CYCLES. 1 HOUR INTO FLIGHT SYSTEM WORKS NORMAL. TROUBLESHOT SYSTEM IAW WDM 24-21-21. CHECKED FEEDER WIRES FROM RT GCU TO IDG. FOUND OK. FOUND 300 OHMS AT NEUTRAL CABLE FROM IDG. TIGHTENED LOOSE GROUND TERMINAL AT G05218. IAW WDM 24-21-21. OPS CHECKED OK IAW AMM 24-22-00. REMOVED AND REPLACED THE RT C/B 6903 AND CARRIED OUT AN OPS CHECK, CHECKED OK IAW AMM 24-22-03.

Part: IDG — MALFUNCTIONED (RT ENGINE) · airframe 77,352 hrs · 15,356 cycles

R GEN OFF EICAS IN FLIGHT. REMOVED AND REPLACED RT ENG IDG. CHECKED FOR OPEN CIRCUIT BETWEEN IDG TERMINAL N AND GROUND, NO CIRCUIT OPEN IAW WDM 24-21-11 / 24-21-21. ACCOMPLISHED OPS CHECK OF IDG, LEAK CHECK GOOD IAW AMM 24-11-01/401. RAN ENGINE IAW AMM 71-00-00. SYS OPS CHECKS GOOD. REMOVED AND REPLACED RIGHT GCU (OFF PART: P/N 734284F, S/N 4502).

Part: GCU — WARNING MESSAGE (RIGHT) · airframe 77,344 hrs · 15,355 cycles

RIGHT GEN OFF ILLUMINATED IN FLIGHT, SERVICED THE RT ENGINE IDG IAW AMM 12-13-03A. ACCOMPLISHED BITE TEST OF BPCU. REPLACED THE RT GCU IAW AMM 24-22-02. OPS CHECKED GOOD. NO LEAKS NOTED FROM IDG IAW AMM 71-00-00.

Part: UNKNOWN — UNKNOWN (FUEL SYSTEM) · airframe 77,326 hrs · 15,351 cycles

WITH ZERO LBS ON CENTER TANK, LT CENTER PUMP REMAINED ON. NO EICAS MESSAGE OR PRESSURE LIGHT. TRANSFERRED 3.5K LBS OF FUEL FROM CTR TO RT TANK. PRESS LIGHT AND EICAS MESSAGE APPEAR IAW AMM 28-26-00 & 28-42-00.

Part: PROCESSING UNIT — MALFUNCTIONED (FUEL SYSTEM) · airframe 77,317 hrs · 15,350 cycles

DID AIR RETURN DUE TO 2.5 FUEL DIFFERENCE BETWEEN TOTALIZER CALCULATED AND INCREASING. REMOVED AND REPLACED FUEL QTY IND PROCESSOR UNIT. ACCOMPLISHED OPERATIONAL CHECK, NO DISCREPANCIES NOTED IAW AMM TASK 28-41-08-004-001, 28-41-08-404-009 AND 28-41-00-715-001-002.

Part: WARNING MESSAGE — FALSE ACTIVATION (LEFT FUEL PUMP) · airframe 77,317 hrs · 15,350 cycles

LEFT CENTER PRESSURE PUMP LOSING FUEL.. FUELED CTR TANK TO 33.5K LBS OF FUEL. INSPECTED AIRCRAFT FOR LEAKS, NO LEAKS NOTED ON LT CENTER FUEL TANK IAW AMM 28-42-00.

Part: CONNECTOR — DIRTY (BOOST PUMP) · airframe 77,302 hrs · 15,347 cycles

LT CENTER FUEL PUMP PRESSURE LIGHT DID NOT ILLUMINATE WHEN EMPTY, READING 00. INSPECTED AND CLEANED CONNECTOR ON LEFT CENTER BOOST PUMP IAW SWPM 20-60-01. TRANSFERRED 4000LBS INTO CENTER, OPS CHECKED GOOD. CENTER BOOST PUMP AND PRESSURE LIGHT ON. TRANSFERRED FUEL OUT OF CENTER WITH LEFT CENTER PUMP OK. LIGHT ILLUMINATED AS QUANTITY APPROACHED 2050. PERFORMED IAW AMM 28-26-00 AND 28-42-00 AND 28-42-01.

Part: PIN — BACKED OUT (PRESSURE SWITCH) · airframe 77,291 hrs · 15,345 cycles

INFLIGHT ONLY, WITH FUEL IN THE CENTER TANK INDICATING EMPTY, CTR L FUEL PUMP EICAS AND CTR L PRESS LIGHT WILL NOT DISPLAY. TROUBLE SHOT L CTR FUEL PUMP PRESS SWITCH, FOUND A PUSHED BACK PIN. REPOSITIONED PIN, OPS CHECK GOOD IAW AMM 28-42-00 / 28-42-01. THIS ACTION CLEARS DMI 130587. PLACARD REMOVED.

Part: GCU — FAULTY · airframe 77,280 hrs · 15,342 cycles

R GEN OFF, SERVICED RT ENG IDG IAW AMM 12-13-03. ACCOMPLISHED BPCU TEST, FOUND GCU FAULT. REMOVED AND REPLACED GCU IAW AMM 24-22-02. RAN ENGINE, OPS CHECK OK IAW AMM 71-00-00.

Part: OXYGEN MASK — MALFUNCTIONED (OBSERVERS) · airframe 77,271 hrs · 15,340 cycles

2ND OBSERVER O2 MASK WILL NOT STOP FREE FLOWING DURING TEST.(<P>REMOVED AND REPLACED 2ND OBSERVER O2 MASK PER AMM 35-11-51. OPS CHECK GOOD.</P>)

Part: HOLDER — DAMAGED (MEGAPHONE) · airframe 77,271 hrs · 15,340 cycles

FWD L/H CLOSET MEGAPHONE RETAINER STRAP DAMAGED. REMOVED AND REPLACED DAMAGED MEGAPHONE HOLDER AT FWD L/H CLOSET PER AMM 20-11-00-910-802.

Part: SEAT BELT — DAMAGED (OBSERVERS) · airframe 77,271 hrs · 15,340 cycles

1ST OBS L/H LAP BELT DAMAGED.(<P>REMOVED AND REPLACED 1ST OBS SEAT PER AMM 25-11-07. OPS CHECK GOOD.</P>)

Part: TRANSCEIVER — MALFUNCTIONED (WEATHER RADAR) · airframe 77,271 hrs · 15,340 cycles

RADAR SYS L PAINTS RADAR SPIKES AND LITTLE ELSE.(<P>REMOVED /REPLACED L WX RADAR RECEIVER M213, OPS CHECK WX RADAR SYSTEM OK PER AMM 34-43-01.</P>)

Part: RADAR — MALFUNCTIONED (WEATHER) · airframe 77,208 hrs · 15,326 cycles

INTERMITTENT RADIAL SPIKING ON EHSI RADAR DISPLAY ON BOTH CAPTAIN`S AND FIRST OFFICER`S EHSI IN BOTH LT & RT SYSTEMS. PERFORMED FIM 34-22 FT 806 AND AMM OPS TEST 34-43-00, LT AND RT WX RADAR SYSTEMS. NO FAULTS FOUND, BITE TESTS AND TEST PATTERNS DISPLAYED OK.

Part: FCU — FAULTY (APU) · airframe 77,091 hrs · 15,300 cycles

FUEL FILTER HOUSING BOLT ON HOUSING BRAKE REMOVED WILL NOT ACCEPT NEW BOLT REMOVED AND REPLACED APU FCU. LEAK CHECK GOOD IAW AMM 49-31-01.

Part: EEC — FAULTED (RT ENGINE) · airframe 77,063 hrs · 15,294 cycles

STATUS MSG RT ENG EEC C1. PERFORMED FIN PROG TASK 71-01. FAULT TREE 803. EICAS MSG CLEARED, NO FAULTS NOTED, UNABLE TO RUN ENGINE TO VERIFY FAULT. TRANSFERRED TO DMI 129093, MEL 73-21-01-04, CAT 'A'. DUE FAULT LEVEL B DUE 21JUNE 20. REMOVED AND REPLACED EEC PER AMM 73-21-04/401. OPS CHECKED GOOD IAW AMM 71-00-00-995.

Part: LIGHT — INOPERATIVE (WINDOW HEAT) · airframe 76,993 hrs · 15,276 cycles

WINDOW HEAT LT FWD LIGHT INOPERATIVE OK TO DEFER IAW MEL 30-41-02A MDDR 128806, CAT C DUE 04JUN20. RELAMPED IAW AMM 33-13-00. OPERATIONS CHECKED GOOD. THIS CLEARS MDDR128806. PLACARD REMOVED.

Part: SHUTOFF VALVE — MALFUNCTIONED (BLEED AIR SYS) · airframe 76,993 hrs · 15,276 cycles

RIGHT HAND ENGINE BLEED VALVE AFTER SHUT DOWN VALVE NOT CLOSING. REPLACED RT ENGINE PRSOV IAW AMM 36-11-09. LEAK/OPS CHECK GOOD.

Part: UNKNOWN — MALFUNCTIONED (BLEED VALVE) · airframe 77,028 hrs · 15,286 cycles

RIGHT ENG BLEED VALVE AFTER SHUTDOWN NOT CLOSING, INTERMITTENTLY. OPERATED RT ENG 3 TIMES, VALVE CLOSES OFF LIGHT ILLUMINATES PROPERLY, NO FAULTS FOUND IAW AMM 71-00-00.

Part: FILTER — NOT REPORTED (BLEED AIR SYS) · airframe 76,935 hrs · 15,263 cycles

RT ENG AFTER SHUTDOWN BLEED VALVE STICKS OPEN(<P>REPLACED R PRSOV FILTER IAW AMM 36-11-09. RAN ENG (RIGHT) TWICE PER MM 71-00-00. VALVE CLOSES OFF LIGHT ILLUMINATES OK.</P>)

Part: PBE — NOT REPORTED (CABIN) · airframe 76,855 hrs · 15,248 cycles

MID CABIN PBE SHOWING NOTE: 5 EA. SERVICEABLE PBE REMAINING IN THE AIRCRAFT.(<P>MDDR #128101 MEL 35-20-01 CAT 'D', DD 05SEP20, PLACARD INSTALLED. DISP: DP @ 13:26Z.</P><P>LP&NBSP;1140399&NBSP;- ITEM 5: REMOVED AND REPLACED MID CABIN PBE PER AMM 35-31-02. THIS CLEARS MDDR 128101. PLACARD REMOVED.</P>)

Part: PROBE — FAULTY (RT ENGINE) · airframe 76,885 hrs · 15,254 cycles

R ENG EEC MODE EICAS(<P>TRANS TO DMI #128110 MEL 73-21-01-02.</P><P>LOG PAGE 1140400 ITEM #7: REMOVED AND REPLACED PT2/PT7 PROBE IAW MM 73-21-03. RAN R ENG SEVERAL TIMES PER MM 71-00-00. NO EICAS STATUS MSG, NO ADVISORY MSG AND NO PIMU MSG. THIS CLEARS MDDR 128110.</P><P><BR /></P>)

Part: UNKNOWN — MALFUNCTIONED (WEATHER RADAR) · airframe 76,845 hrs · 15,246 cycles

INTERMITTENT RADIAL SPIKE SPIKING ON BOTH EHSI RADAR SYSTEMS.(<P>PERFORMED GROUND TEST OF RADAR SYSTEMS. ALL CHECKS GOOD PER AMM 34-43-00.</P>)

Part: STATUS MESSAGE — ACTIVATED (COCKPIT) · airframe 76,794 hrs · 15,235 cycles

R ENG EEC C1 STATUS MESSAGE UPON LANDING.(<P>TRANSFERRED TO MDDR 127726 PER MEL 73-21-01-04, CAT A, DUE DATE 1000 FH.</P>)

Part: PROBE — FAULTY (RT ENGINE) · airframe 76,794 hrs · 15,235 cycles

R ENG EEC C1 STATUS MESSAGE UPON LANDING.(<P>TRANSFERRED TO MDDR 127726 PER MEL 73-21-01-04, CAT A, DUE DATE 1000 FH.</P><P>LOG PAGE 1140400 ITEM #7: REMOVED AND REPLACED PT2/PT7 PROBE IAW MM 73-21-03. RAN R ENG / SEVERAL TIMES PER MM 71-00-00. NO EICAS STATUS MSG, NO ADVISORY MSG AND NO PIMU MSG. THIS / CLEARS MDDR 127726.<BR DATA-MCE-BOGUS="1" /></P>)

Part: UNKNOWN — MALFUNCTIONED (WEATHER RADAR) · airframe 76,754 hrs · 15,229 cycles

LEFT RADAR SYSTEM WASN'T PAINTING KNOWN WEATHER ACCURATELY.(<P>PERFORMED OPS TEST OF LEFT AND RIGHT WEATHER RADAR. SYSTEM OPS CHECK NORMAL IAW AMM 34-43-00.</P>)

Part: FILTER HOUSING — LEAKING (NR 1 ENGINE) · airframe 76,768 hrs · 15,231 cycles

#1 ENGINE FUEL PUMP FILTER LEAKING.(<P>REMOVED AND REPLACED #1 ENG FUEL PUMP FILTER HOUSING PACKING AS PER MM CHP 73-11-02. LEAK CHECK OK.</P>)

Part: VALVE — FAILED (IDG OIL COOLING) · airframe 76,690 hrs · 15,216 cycles

STATUS MESSAGE RIGHT IDG VALVE. REMOVED AND REPLACED THE NR 2 ENGINE IDG AIR OIL COOLING VALVE, PERFORMED MPA IAW AMM 71-00-00-725 NO DEFECTS NOTED.

Part: LINE — LOOSE (OIL COOLER) · airframe 76,681 hrs · 15,215 cycles

DURING WALKAROUND IN IAH RH ENG. EVIDENCE OF OIL LEAK.(<P>FOUND OIL COOLER LINE LOOSE. TIGHTENED LINE, LEAK CHECK GOOD IAW AMM 79-20-00.</P>)

Part: FAN — MALFUNCTIONED (E&E BAY) · airframe 76,673 hrs · 15,213 cycles

"AFT EQPT EXH FAN 2" STATUS MESSAGE(<P>TRANSFERRED TO MDDR 126537 IAW DDG 21-58-05, CAT C, DUE DATE 11 APR-20.</P><P>LP 1008502 (04APR20): REMOVED AND REPLACED AFT EQUIP. EXH FAN #2 PER AMM 21-26-01. OPS CHECK GOOD. THIS CLEARS MDDR 126537.</P>)

Part: EVAS UNIT — INOPERATIVE (COCKPIT) · airframe 76,673 hrs · 15,213 cycles

EVAS SYSTEM INOPERATIVE.(<P>TRANSFER TO MDDR 126536 IAW DDG 25-63-06, CAT D, DUE DATE 30 JUL-20.</P><P><SPAN>LP 1008503: INSTALLED VELCRO ON THE FO'S EVAS SYSTEM IAW EO 6725A222. THIS CLEARS DMI 126536 AND PLACARD REMOVED.</SPAN><BR DATA-MCE-BOGUS="1" /></P>)

Part: PRESSURE SWITCH — FAULTY (IDG) · airframe 76,652 hrs · 15,209 cycles

AFTER T/O, DURING CLIMBOUT, RECEIVED STATUS MESSAGE, R IDG VALVE.&NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP;(<P>TRANSFER TO MDDR 126431, MEL 75-21-01-03A, CAT C, 9APR20. PLACARD INSTALLED. C/W MAINT. PROCEDURES.</P><P> LP 1008505-34 - (06APR20) - REMOVED AND REPLACED TURBINE VANE AND BLADE COOLING AIR VLV &AMP; IDG AIR OIL HEAT EXCHANGER VALVE OVERRIDE SOLENOID. OPS CHECK GOOD IAW B767 AMM 75-24-15-004-046-N00. THIS ACTION CLEARS MDDR 126431 (OFF PARTS: PN&NBSP;<SPAN>1109V0300-2,</SPAN><SPAN>&NBSP;798850-1; SN 3348, F34547)</SPAN><SPAN>.</SPAN></P><P>(NOTE: ITEM 35 - ALSO REPLACED IDG AIR-OIL HEAT EX VLV OVERRIDE PRESS SWITCH IAW AMM 24-11-13-004-001 AND PS4 AIR FILTER IAW AMM 75-33-05-402-021-N00/001-N00. OPS CHK OK.)</P>)

Part: APU — MALFUNCTIONED (APU BAY) · airframe 76,652 hrs · 15,209 cycles

APU WON'T START.(<P>TRANSFER TO MDDR #126446, MEL 49-11-01B, CAT "C", DUE DATE 09APR20, PLACARD INSTALLED.</P><P>IAH 02APR20, LP 1120020: REMOVED AND REPLACED APU REF AMM 49-11-01, OPS CHECK GOOD. THIS CLEARS MDDR 126446.</P>)

Part: ECU — MALFUNCTIONED (APU) · airframe 76,644 hrs · 15,208 cycles

APU AUTO SHUTDOWN.(<P>REMOVED AND REPLACED APU ECU, OPS CHECK NORMAL IAW AMM 49-61-05.</P>)

Part: STARTER — MALFUNCTIONED (NR 2 ENGINE) · airframe 76,635 hrs · 15,206 cycles

DURING ENG START WHEN START VALVE OPENED MANUALLY, NO N2 ROTATION.(<P>REMOVED AND REPLACED STARTER ON #2 ENG IAW AMM 80-11-01, AND OPS CHECKED NORMAL IAW B767 AMM 71-00-00.</P>)

Part: RELAY — FAILED · airframe 76,626 hrs · 15,205 cycles

R IDG VALVE STATUS MSG.(<P>OK TO DEFER IAW DDG 75-21-01-03A MDDR 126212, CAT C, DUE 03APR20, MAINTENANCE PROCEDURES COMPLIED WITH, PLACARD INSTALLED. DISPATCH: YK @ 15:00Z.</P><P>LOG PAGE 1119994: T/S PER FIM 24-20 FT 802, REMOVED AND REPLACED RELAY K1032. RAN ENG. OPS CHECK OK AS PER SWPM 20-81-12 &AMP; AMM 71-00-00. NO FAULTS OR STATUS MSGS, MDDR #126212 CLOSED.</P>)

Part: START VALVE — MALFUNCTIONED (RT ENGINE) · airframe 76,625 hrs · 15,204 cycles

ON START "R ENG STARTER" EICAS MSG.(<P>TRANSFERRED TO MDDR 126176 PER DDG 80-00-02-01, CAT C, ITEM DUE 02APR20. TI: ST @ 21:49Z.</P><P>27MAR20, LP 1120049 ITEM M3: REMOVED AND REPLACED START VALVE ON #2 ENG IAW B767 AMM 80-11-04, OPS CHECKED NORMAL IAW B767 AMM 71-00-00, THIS CLEARS DMI # 126176, PLACARD REMOVED. DISPATCH LC @ 15:07Z, MCC AM 15:07Z.</P>)

Part: SHUTOFF VALVE — MALFUNCTIONED (BLEED AIR SYS) · airframe 76,625 hrs · 15,204 cycles

ON T/O EICAS MSG R ENG HPSOV. ABORTED TAKEOFF. STATUS MSG R ENG HPSOV.(<P>REMOVED AND REPLACED R ENG HPSOV IAW AMM 36-11-07. RUN ENG PER AMM 71-00-00 OK.<BR /></P>)

Part: IDG — FAULTY (RT ENGINE) · airframe 76,625 hrs · 15,204 cycles

AFTER ENGINE 2 WAS STARTED, FO'S ADI &AMP; HSI FLICKERED ON &AMP; OFF, ASSOCIATED W/ INTERMITTENT, FO INST XFER STATUS MESSAGE &AMP; FLICKERING COCKPIT LIGHTS.(<P>PERFORMED OPERATIONAL TEST OF RH IDG IAW AMM 24-11-00. NOTED AC VOLTAGE BETWEEN 116 AND 126 VOLTS AC, CYCLED RH GEN SWITCH AND RH GEN FIELD SWITCH, VOLTAGE STAYED AT 116 VOLTS A/C. NO FURTHER DEFECTS NOTED.</P><P>LP 1120040, ITEM M4: REMOVED AND REPLACED RH IDG IAW AMM 24-11-01. PERFORMED OPERATIONAL TEST OF RH IDG IAW AMM 24-11-00, OPS CHECK NORMAL.</P>)

Part: CONNECTOR — DIRTY (RT STARTER) · airframe 76,625 hrs · 15,204 cycles

BTB RT ENG STARTER EICAS.(<P>TRANSFERRED TO MDDR #126030 I.A.W MEL 80-00-02-01, CAT 'C'.</P><P>20MAR, BWI, LP 1120039, ITEM M3: REMOVED, INSPECTED, CLEANED AND RE-INSTALLED RH ENG START VALVE CANNON PLUG IAW SWPM AND WDM 80-11-21, CONNECTOR D10970. PERFORMED ENGINE START SYSTEM OPS TEST IAW AMM 80-11-00, NO DEFECT NOTED. THIS CLEARS DMI #126030.</P>)

Part: ENGINE — OIL CONSUMPTION (RIGHT) · airframe 76,625 hrs · 15,204 cycles

RIGHT ENG OIL QUANTITY CONTINUALLY DROPS IN OIL QUANTITY DURING FLIGHT, ENGINE QUANTITY AT START INDICATED 23 QTS OIL QUANTITY AT ELAPSE TIME 98:55 IS 4 QTS.(<P>REMOVED AND REPLACED ENGINE 2 I.A.W ATLAS W/C A-71-999-02-01.</P>)

Part: GCU — MALFUNCTIONED · airframe 76,613 hrs · 15,203 cycles

INFO ONLY, R GEN CAME OFFLINE BRIEFLY &AMP; RESET W/O ISSUE.(<P>ACCOMPLISHED BPCU BITE TEST. NO MESSAGES NOTED, REMOVED AND REPLACED GENERATOR CONTROL UNIT (GCU). OPS CHECK NORMAL I.A.W AMM 24-22-02 &AMP; I.A.W AMM 71-00-00. NOTE: ENG RUN C/BY CREW.</P>)

Part: OXYGEN BOTTLE — DISCHARGED (CABIN) · airframe 76,601 hrs · 15,201 cycles

RIGHT SIDE OVERWING PORTABLE O2 (UPPER) AND L-1 BOTTLES READING ZERO.(<P>TRANSFERRED TO MDDR 125739, MEL 35-31-01, CAT "D", DUE DATE 11JUL20, PLACARDS INSTALLED.</P><P>LP&NBSP;<SPAN>1120033:&NBSP;</SPAN><SPAN>REMOVED AND REPLACED PORTABLE OXYGEN CYLINDER IAW AMM 35-31-01 . MDDR 125739 CLEARED. PLACARDS REMOVED.</SPAN></P>)

Part: OXYGEN MASK — UNWANTED DEPLOY (CABIN) · airframe 76,613 hrs · 15,203 cycles

PAX O2 MASK DEPLOYED.(<P>STOWED PAX O2 MASK IAW&NBSP; B767&NBSP; AMM 35-21-15.<BR /></P>)

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 76,601 hrs · 15,201 cycles

INFO ONLY: R GEN OFF EICAS MESSAGE WHILE IN FLIGHT. PERFORMED QRH, NO FURTHER ISSUE DURING FLIGHT.(<P>ACCOMPLISHED BUS PWR CONT UNIT BITE TEST, NO MESSAGES NOTED. SER. RT IDG IAW AMM 24-22-00. NOTE: CREW RAN RT ENG. OPS CHECK NORMAL IAW AMM 71-00-00.</P>)

Part: UNKNOWN — MALFUNCTIONED (GENERATOR SYS) · airframe 76,592 hrs · 15,199 cycles

DURING BOTH RIGHT AND LEFT ENGINE STARTS, BOTH RIGHT AND LEFT GENERATORS FAILED TO COME ONLINE. ACCOMPANIED WITH EICAS R/L GEN OFF MESSAGES. EXECUTED QRH PROCEDURE FOR BOTH GENS. APU REMAINED ON FOR DURATION OF FLIGHT AS BACKUP GENERATOR SOURCE, DUE TO IRREGULARITIES. UNABLE APU COLD SOAK.(<P>PERFORMED BOTH LEFT &AMP; RIGHT ENGINE RUNS IAW AMM REF 71-00-00. POWER TRANSFERS NORMAL. NO EICAS MSG. BPCU BITE TEST SHOWS NO FAULTS, AMM REF 24-22-00.</P>)

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 76,590 hrs · 15,198 cycles

CORROSION WAS FOUND ON THE FUSELAGE SKIN BETWEEN STA 1562/1582 AND STRINGER S-24L / S-25L, AT THE VACUUM OUTLET NOZZLE.(<P ><SPAN>FUSELAGE SKIN REPAIRED / PER&NBSP;SRM 53-60-01-2R-3 REPAIR 3. SEE RAM FORM N662GT-20-02.</SPAN></P>)

Part: WIRE — DAMAGED (FUEL SYSTEM) · airframe 76,590 hrs · 15,198 cycles

RT AFT FUEL PUMP INOP EICAS; C/B NOT POPPED.(<P>TRANSFERRED TO MDDR #125671 I.A.W MEL 28-22-01, CAT 'C'.&NBSP;</P><P>REF LOG PAGE 1120033 ITEM M12: REMOVED AND REPLACED RIGHT AFT BOOST PUMP PRESSURE SWITCH IAW AMM 28-42-01, NO HELP (P/N OFF 21C1-3-21, S/N OFF X019905).</P><P>REF LOG PAGE 1120034 ITEM M14: REPAIRED WIRE BEHIND P61 PANEL IAW SWPM 20-10-13 AND WDM 28-22-11. RIGHT AFT BOOST PUMP CHECK GOOD IAW AMM 28-22-00. CLEARS MDDR 125671.</P>)

Part: CONNECTOR — LOOSE (FIRE LOOP) · airframe 76,601 hrs · 15,201 cycles

RH ENGINE FIRE LOOP 2 STATUS MESSAGE (ENGINE FIRE DETECTION SYSTEMS, DETECTION LOOPS (ER RESTRICTED 120)).(<P>TRANSFERRED TO MDDR #125715 IAW MEL 26-11-01-01, CAT "C", DUE DATE 23MARCH20. PLACARD&NBSP; INSTALLED. NOTE: RESTRICTED TO ETOPS 120, DISP : DD @ 0013Z.</P><P>LP&NBSP;<SPAN>1120032:&NBSP;</SPAN><SPAN>TIGHTENED LOOSE CONNECTOR ON RH ENG LEFT AFT SIDE. FIRE WARNING SYS TESTS OK PER AMM 26-11-00 . MDDR 125715 CLEARED.</SPAN></P>)

Part: SKIN — DENTED (TAILCONE) · airframe 76,590 hrs · 15,198 cycles

TWO DENTS ON FUSELAGE TAIL CONE SKIN BETWEEN STA 1873.40 / STA 1881.75 AND LBL 3.4 / LBL 7.5.(<DIV> / </DIV><P ><SPAN>ONE DENT WAS FOUND WITHIN / SRM LIMITS. THE OTHER DENT WAS REPAIRED PER&NBSP;B767-300 SRM 53-00-01-2R-10 / REPAIR 10. SEE RAM FORM N662GT-20-03.</SPAN></P>)

Part: SKIN — DENTED (FUSELAGE) · airframe 76,590 hrs · 15,198 cycles

AN EVIDENT DENT DAMAGE WAS FOUND DURING THE INITIAL INSPECTION ON FUSELAGE SKIN STA 1197+88 / STA 119+110, AND BETWEEN STRINGER S-22L / S-24L.(<P >THE DAMAGE WAS REPAIRED IN / ACCORDANCE WITH&NBSP;B767-300 SRM 53-00-01-2R-1 REPAIR 1. SEE RAM FORM / N662GT-20-01.</P>)

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 76,590 hrs · 15,198 cycles

CORROSION DAMAGE WAS FOUND PREVIOUSLY ON THE BULK CARGO FLOOR STRUCTURE, BETWEEN STA 1417 / STA 1540 AND BL. 0.0. THE CORROSION WAS TEMPORARILY REPAIRED ON A PREVIOUS MAINTENANCE VISIT.(<P >THE REPAIRED PART (FLOOR / BEAM P/N 146T5005-1) WAS REPLACED IN THIS MAINTENANCE VISIT IN ACCORDANCE WITH / ATLAS EO&NBSP;6753A757 PART 2.</P>)

Part: BEARING — DAMAGED (EVAC SLIDE) · airframe 76,590 hrs · 15,198 cycles

RH OFF WING SLIDE WAS FOUND WITH DAMAGE ON THE TUBE BEARINGS.(<P>RH OFF WING SLIDE WAS REPLACED IAW AMM 25-65-01-024-001-001 AND AMM 25-65-01-424-060-001.</P>)

Part: ANTI-ICE VALVE — STICKS (RT WING) · airframe 76,613 hrs · 15,203 cycles

RIGHT WING ANTI-ICE VALVE STICKING DURING GROUND TEST.(<P>RIGHT WING THERMAL ANTI-ICE VALVE TEST WAS PERFORMED IAW AMM 30-11-02-404-012.<BR /></P>)

Part: IGNITION UNIT — FAULTY (APU) · airframe 76,613 hrs · 15,203 cycles

APU DID NOT START, 5 ATTEMPTS, FL 400, FL 350, FL 300, FL 250 &AMP; FL 170. OIL LEAK OBSERVED AFTER FLIGHT.(<P>IGNITION UNIT WAS REPLACED AND TEST WAS PERFORMED IAW AMM 49-41-03-404-010. OPS CHK GOOD.<BR /></P>)

Part: CONTROLLER — MALFUNCTIONED (CABIN PRESSURE) · airframe 76,556 hrs · 15,188 cycles

EICAS STATUS MESSAGE CABIN ALT AUTO 2 DISPLAYED.(<P>ACCOMPLISHED OPERATIONAL CHECK OF CABIN ALT AUTO 2. RESET SYS @ PRESSURE CABIN ALT AUTO 2 CONTROLLER, OPS CHECK GOOD IAW B767 AMM 21-31-00</P>)

Part: SEAL — BROKEN (PBE) · airframe 76,492 hrs · 15,176 cycles

LEFT MID CABIN PBE SEAL BROKEN.(<P>PLACED ON MDDR 124029, MEL 35-20-01, CAT 'D', DUE 27MAY20. PLACARD INSTALLED.</P><P>LP 1226096: REPLACED PBE. CLOSED MDDR 124029 PER ATLAS LOPA. PLACARD REMOVED.</P>)

Part: UNKNOWN — MALFUNCTIONED (RT ENGINE) · airframe 76,320 hrs · 15,134 cycles

HUNG START ON RT ENG, TEMP (20) OIL WAS AMBER AT START INITIATION, IMMEDIATE ACTION ACCOMPLISHED WITH MX ON DECK, WE SWITCHED TO #2 IGNITOR, ATTEMPTED 2ND START, SAME HUNG START, OIL TEMP HIGH AS (54).&NBSP;(<P>RESET RT ENGINE BREAKERS, RT EEC AND FUEL VALVES, RAN ENGINE TWICE PER AMM 73-11-00 &AMP; 76-11-00. NO FAULTS. OK TO CONTINUE.</P>)

Part: ISOLATION VALVE — INTERMITTENT (BLEED AIR SYS) · airframe 76,320 hrs · 15,134 cycles

LT ISOLATION VALVE INTERMITTENT.(<P>REMOVED AND REPLACED LEFT ISO VALVE IAW AMM 36-11-04, OPS CHK OK, LEAK CHK OK.</P>)

Part: O2 GENERATOR — INOPERATIVE (CABIN) · airframe 76,293 hrs · 15,123 cycles

FOUND O2 GENERATOR INOP (REF MDDR 122622 SEATS 37G-F-D INOP)(<P>REMOVED AND REPLACED O2 GENERATOR. OPS CHECK GOOD IAW B767 AMM 35-21-15-002-179-001. THIS CLEARS MDDR 122622, PLACARD REMOVED.<BR /></P>)

Part: TERMINAL — BROKEN (FIRE LOOP) · airframe 76,253 hrs · 15,110 cycles

RIGHT ENGINE FIRE LOOP 1 STATUS MESSAGE. FOUND A BROKEN TERMINAL LOG ON RIGHT ENGINE LOWER FWD FIRE LOOP 1. REPAIRED IAW SWPM 20-30-00. OPS CHECKED GOOD IAW AMM 26-11-00,

Part: EXHAUST VALVE — MALFUNCTIONED · airframe 76,131 hrs · 15,075 cycles

STATUS MSG: CARGO GROUND EXHAUST VALVE.(<P>RESET CARGO GROUND EXHAUST VALVE, OPS CHECK NORMAL IAW AMM 21-43-00.</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (CABIN PRESSURE) · airframe 76,070 hrs · 15,061 cycles

"CABIN ALT AUTO 2"&NBSP; STATUS MSG DISPLAYED.(<P>PERFORMED BITE TEST ON CABIN PRESSURE CONTROLLER IAW B767 FIM 21-31-00.&NBSP; OPS CHECK NORMAL.</P>)

Part: VALVE — MALFUNCTIONED (EXHAUST) · airframe 76,038 hrs · 15,053 cycles

CGO GND EX VALVE STATUS MSG.&NBSP;(<P>OPS CHECKED PER AMM 21-28-00, RESET EX VALVE C/B IAW GMM 3.8.1.<BR /></P>)

Part: ACTUATOR — MALFUNCTIONED (SPOILER) · airframe 76,026 hrs · 15,051 cycles

AIRCRAFT DIVERSION TO SNN, DUE TO R/H HYD QUANTITY EICAS MESSAGE IN FLIGHT, QTY 0.35.(<P>REMOVED AND REPLACED L/H WING #2 SPOILER PCA IAW AMM 27-61-02-424-023. DUE LEAKING PCA, OPS AND LEAK CHECKS OK. RIGHT HAND SYSTEM FILLED TO FULL.&NBSP;</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (SPAR VALVE) · airframe 75,952 hrs · 15,034 cycles

L FUEL SPAR VALVE EICAS MSG INFLIGHT, ASSOCIATED C/B ON P6 OPEN.&NBSP;(<P>RESET CIRCUIT BREAKER, OPS CHECKED IAW AMM 28-22-11. INSPECTED CANNON PLUG, NO DEFECTS FOUND.&NBSP;</P>)

Part: OIL SYSTEM — LEAKING (RT ENGINE) · airframe 75,921 hrs · 15,027 cycles

OIL POOLED IN RIGHT ENGINE COWLING, AROUND N1 BLADES.&NBSP;(<P>CHECKED AND FOUND TO BE OK IAW B767 FIM 71-08 FAULT TREE 813.</P><P><BR /></P><P><BR /></P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (OUTFLOW VALVE) · airframe 75,867 hrs · 15,017 cycles

CGO GND EXHAUST VALVE STATUS MESSAGE PRESENT AFTER LANDING.&NBSP;&NBSP;(<P>PERFORMED SYSTEM TEST IAW AMM 21-26-00, OPS CHECK GOOD. MESSAGE CLEARED.&NBSP;</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (CABIN PRESSURE) · airframe 75,840 hrs · 15,011 cycles

CABIN ALT AUTO 2 STATUS MESSAGE. FOLLOWED FIM TASK 21-31 FAULT TREE 810. PERFORMED BIT TEST OF CABIN PRESS CONTROLLER, NO FAULTS NOTED. MESSAGE CLEARED.

Part: WARNING MESSAGE — FALSE ACTIVATION · airframe 75,822 hrs · 15,009 cycles

CARGO GROUND EXHAUST VALVE STATUS MESSAGE. PERFORMED SYSTEM TEST IAW AMM 21-26-00, MESSAGE CLEARED.

Part: DUCT — DAMAGED (AIR SURGE) · airframe 75,795 hrs · 15,004 cycles

APU FLEXIBLE DUCT BEHIND SURGE VALVE HAS HOLE IN IT.(<P>REMOVED AND REPLACED&NBSP;APU SURGE VALVE DUCT RUBBER SLEEVE REF AMM 49-52-00, LEAK CHECKS OK.&NBSP;<BR /></P>)

Part: RELAY — MALFUNCTIONED (FUEL PUMP) · airframe 75,737 hrs · 14,991 cycles

LEFT CENTER FUEL PUMP INOPERATIVE. RESET GFI RELAY K10697. RAN ENGINES, OPS CHECK NORMAL IAW FIM 28-22 FT 805 AND AMM 71-00-00.

Part: STATUS MESSAGE — FALSE ACTIVATION (COCKPIT) · airframe 75,694 hrs · 14,983 cycles

STATUS MESSAGES: L ENG ANALOG N2 &AMP; R ENG ANALOG N2.&NBSP;(<P>ACCOMPLISHED FIM 77-12 FT 806 AND FIM 71-01 FT 804, NO FAULTS OR DISCREPANCIES NOTED. RESET SYSTEM, OPS CHECK NORMAL.&NBSP;</P>)

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 75,609 hrs · 14,965 cycles

L-1 EMERGENCY FLASHLIGHT INOP. TRANSFERRED TO MDDR 118005 PER MEL 25-63-04A, CAT 'C', DUE DATE: 30SEP2019. PLACARD INSTALLED. LP 841020 - M3: REMOVED AND REPLACED L-1 FLASHLIGHT ASSY IAW AMM 25-60-00. THIS CLEARS DMI 118005. PLACARD REMOVED.

Part: VALVE — MALFUNCTIONED (APU) · airframe 75,594 hrs · 14,962 cycles

APU BLEED AIR INOP. REMOVED AND REPLACED APU BLEED AIR VALVE IAW AMM 36-11-10, OPS CHECK GOOD.

Part: CONNECTOR — DIRTY (APU) · airframe 75,570 hrs · 14,957 cycles

APU BLEED VALVE WOULD NOT OPEN FOR ENGINE START. CLEANED CONNECTOR. OPS CHECKED VALVE PER AMM 49-53-00, OPS CHECK GOOD.

Part: FAN — MALFUNCTIONED (CABIN) · airframe 75,581 hrs · 14,959 cycles

R RECIR FAN EICAS MESSAGE, ACCOMPANIED W/STRONG BURNING SMELL THROUGHOUT THE AIRCRAFT. TRANSFERRED TO MDDR # 117756 IAW MEL 21-25-01-01A, CAT 'C'. LP 841015 - M9: REMOVED AND REPLACED RT RECIRCULATING FAN IAW AMM 21-25-01, OPS CHECK GOOD. THIS CLOSES MDDR 117756. PLACARDS REMOVED AND MCC NOTIFIED.

Part: WIRE — BROKEN (RT ENGINE) · airframe 75,575 hrs · 14,958 cycles

RIGHT ENGINE FIRE LOOP #2 EICAS MESSAGE. TRANSFERRED TO MDDR 117744 IAW MEL 26-11-01-01, CAT 'C'. LP 841015 - M7: FOUND BROKEN WIRE AT TERMINAL TO FWD LOWER LOOP. REPLACED TERMINAL AS PER SWPM 20-30-00. OPS CHECK GOOD AS PER AMM 26-11-00. THIS CLEARS DMI #117744. PLACARDS REMOVED AND MCC NOTIFIED.

Part: STATUS MESSAGE — FALSE ACTIVATION (COCKPIT) · airframe 75,487 hrs · 14,939 cycles

R ENG ANALOG STATUS MESSAGE. L ENG ANALOG STATUS MESSAGE. ACCOMPLISHED FIM 77-12 FT 805, NO DISCREPANCIES NOTED. RESET EICAS MESSAGES.

Part: CLAMP — OUT OF ADJUST (FIRE LOOP) · airframe 75,479 hrs · 14,938 cycles

RIGHT ENGINE FIRE LOOP 2. TRANSFERRED TO MDDR 117246 PER MEL 26-11-01-01, CAT "C", DUE SEP 13, 2019. LP 1082219 - M8: PERFORMED FIM 26-11. INSPECTED TERMINALS AND LOOP, FOUND ELEMENT TOUCHING. RE-ADJUSTED CLAMP, PERFORMED SYSTEM TEST, AND ENGINE RUN IAW AMM 71-00-00. OPS CHECK GOOD, NO FAULTS NOTED. THIS CLEARS MDDR #117246. PLACARD REMOVED AND MCC NOTIFIED.

Part: FIRE LOOP — CONTAMINATED (RT ENGINE) · airframe 75,425 hrs · 14,926 cycles

RT ENG FIRE LOOP 2 STATUS MSG. CLEANED AND DRIED WATER FROM FWD LWR LOOP TERM RT ENG AND OPS CHECK PER AMM 26-11-02.

Part: FUEL FILTER — CLOGGED (RT ENGINE) · airframe 75,395 hrs · 14,921 cycles

AFTER TAKEOFF, R ENG FUEL FILT EICAS AND STATUS MESSAGE. REMOVED AND REPLACED THE FUEL FILTER ELEMENT REF AMM 73-11-03-404-001-H00. NO LEAKS NOTED.

Part: CONTROLLER — MALFUNCTIONED (A/C PACK) · airframe 75,354 hrs · 14,913 cycles

PACK TEMPERATURE EICAS MESSAGE AFTER LANDING. PERFORMED BITE PACK TEMP CONTROLLERS. NOTED RT PACK TEMP CONTROLLER RAM INLET FAULT. RESET CONTROLLER. PREFORMED BITE REF AMM 21-51-14. NO FAULTS NOTED. RAM AIR DOOR OPS CHECKS GOOD.

Part: SYMBOL GENERATOR — MALFUNCTIONED (WX RADAR) · airframe 75,354 hrs · 14,913 cycles

CAPT WX DOES NOT DISPLAY IN FLIGHT. SELECTING ALTN EFI DISPLAYS WX OK. SYSTEM TESTS OK ON GROUND, FAULT PRESENT ON LEFT AND RIGHT SYSTEM.&NBSP;(<P>REMOVED AND REPLACED LEFT SYMBOL GENERATOR REF AMM 34-22-01, OPS TEST GOOD.&NBSP;</P>)

Part: SEAL — WORN (ENGINE DRAIN) · airframe 75,207 hrs · 14,877 cycles

#2 ENG DRAIN MAST SEALANT WORN. (<P>REPLACED #2 ENGINE DRAIN MAST SEAL IAW AMM 71-71-00.</P>)

Part: CONE — ERODED (LT ENGINE) · airframe 75,207 hrs · 14,877 cycles

L ENG CONE FOUND WITH EROSION PEELING ALL OVER THE CONE.&NBSP; (<P>REMOVED AND REPLACED CONE SEGMENT PER AMM 72-31-01.</P>)

Part: CLAMP — LOOSE (START SYSTEM) · airframe 75,207 hrs · 14,877 cycles

LEFT ENGINE POOR N2 ACCELERATION DURING START WITH APU BLEED. LOW DUCT PRESSURE OBSERVED. (<P>FOUND 4 CLAMPS BEFORE PNEUMATIC STARTER LOOSE. RE-TIGHTENED 4 CLAMPS IAW AMM 80-11-01. NO LEAKS NOTED. DRY MOTOR DROP WAS 21 PSI VS 18 PSI BEFORE FINDING; AMM 71-00-00 AND VALVE STARTER CONTROL REF AMM 80-11-02.</P>)

Part: MONITOR — FAULTY (ENGINE) · airframe 75,207 hrs · 14,877 cycles

ENGINE VIB BITE WILL NOT CLEAR EICAS MAINTENANCE MESSAGES.&NBSP; (<P>REPLACED EVM IAW AMM 77-31-03. OPS CHECK NORMAL, NO EICAS MSG AT THIS TIME.&NBSP;</P>)

Part: MODULE — DEFECTIVE (APU) · airframe 75,206 hrs · 14,876 cycles

APU DUCT PRESSURE FLUCTUATING. (<P>REMOVED AND REPLACED APU FLOW CONTROL SENSOR MODULE IAW AMM 49-53-08.<BR /></P>)

Part: UNKNOWN — MALFUNCTIONED (LT ENGINE) · airframe 75,170 hrs · 14,869 cycles

"LEFT ENGINE POOR N2 ACCELERATION DURING START W/ APU BLEED. LOW DUCT PRESSURE OBSERVED. INFO ONLY."(<P><SPAN>PERFORMED DRY MOTOR OF ENGINE #1 IAW AMM 71-00-00.</SPAN><SPAN>OPS CHECK NORMAL AT THIS TIME.</SPAN></P><P><SPAN>ENGINE DRY MOTORED BY CREW</SPAN></P>)

Part: UNKNOWN — MALFUNCTIONED · airframe 75,046 hrs · 14,843 cycles

DURING #1 ENGINE START, N1 DISPLAY WENT BLANK.(<P>ACCOMPLISHED FIM TASK 77-12 FT 803. RESET SYSTEM, OPS CHECK NORMAL (EEC/PIMU).&NBSP;</P><P>NOTE: ENGINE RUN ACCOMPLISHED BY CREW, ALL NORMAL.&NBSP;</P>)

Part: ISOLATION VALVE — INOPERATIVE · airframe 74,990 hrs · 14,831 cycles

CTR ISOLATION VALVE INOPERATIVE. REMOVED AND REPLACED CTR ISOLATION VALVE. OPS AND LEAK CHECK GOOD IAW AMM 36-11-04.

Part: WARNING MESSAGE — FALSE ACTIVATION (BLEED SYSTEM) · airframe 74,985 hrs · 14,829 cycles

DURING CRUISE FLT AT FL 360, 2 HOURS INTO FLT, EICAS MESSAGE FOR LEFT BLEED ISOLATION VALVE, AND VALVE LIGHT IN SWITCH ILLUMINATED. ACCOMPLISHED BITE TEST OF AIR SUPPLY MODULE. RESET SYSTEM. PERFORMED OPERATIONAL CHECK OF BLEED SYSTEM. NO DISCREPANCIES NOTED IAW AMM 36-23-00.

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 74,967 hrs · 14,824 cycles

RH OVER WING EMERGENCY FLASHLIGHT IN F/A STATION NOT FLASHING.(<P>REMOVED AND REPLACED FLASHLIGHT BATTERY REF AMM 25-64-00.</P>)

Part: SPINNER — CRACKED (NR 1 ENGINE) · airframe 74,967 hrs · 14,824 cycles

FOUND THE NR 1 ENGINE FAN BLADE SPINNER CRACKED. R & R THE NR 1 ENG SPINNER DOME IAW AMM 72-31-01.

Part: DUCT — CRACKED (APU) · airframe 74,967 hrs · 14,824 cycles

LH WHEEL WELL APU DUCT CRACKED. R & R THE LT WHEEL WELL APU DUCT IAW AMM 36-11-01. LEAK CHECK GOOD.

Part: SPINNER — CRACKED (NR 1 ENGINE) · airframe 74,965 hrs · 14,823 cycles

FOUND # 1 FAN BLADE SPINER CRACKED&NBSP;(<P>REMOVED AND REPLACED&NBSP; #1 ENGINE SPINER&NBSP; DOME&NBSP; IAW AMM 72-31-01</P>)

Part: SLIDE — UNWANTED DEPLOY (R1 DOOR) · airframe 74,916 hrs · 14,810 cycles

R1 DOOR SLIDE DEPLOYED.(<P>REMOVED AND REPLACED R1 DOOR SLIDE ASSY REF AMM 25-66-01.</P>)

Part: UNKNOWN — MALFUNCTIONED (WEATHER RADAR) · airframe 74,834 hrs · 14,796 cycles

RADAR SPOKING/BOTH DISPLAYS, BOTH RADARS.(<P>PERFORMED FIM34-43 WXR BIT TEST OK. NO DEFECTS NOTED.</P>)

Part: SOFTWARE — FAULTY (COCKPIT) · airframe 74,810 hrs · 14,792 cycles

F/O RADAR POWER BUTTON REQUIRES 2 CYCLES TO POWER.&NBSP;(<P>TRANSFERRED TO MDDR # 111669 PER DDG 34-43-01. CAT 'D' DUE 12SEP19. PLACARD INSTALLED.&NBSP;</P><P>LP 1079085 - M5:&NBSP; INSTALLED&NBSP;EFIS SYM GENERATOR SOFTWARE UPDATE IAW AMM 34-22-00. OPS CKS GOOD, THIS CLEARS MDDR 111669.</P>)

Part: VALVE — MALFUNCTIONED (LT ENGINE) · airframe 74,781 hrs · 14,786 cycles

ON SHUTDOWN LEFT IDG VALVE STATUS MESSAGE&NBSP;(<P>&NBSP;TRANSFERRED TO MDDR 111509 CAT "C" IAW ATLAS MEL 75-21-01-03A. MAINTENANCE PROCEDURES C/W.</P><P>REMOVED AND REPLACED COOLER VALVE IAW AMM 24-11-12&NBSP;</P>)

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 74,774 hrs · 14,785 cycles

LEFT IDG VALVE STATUS MESSAGE ON APPROACH.&NBSP;(<P>PERFORMED BPCU BITE IAW FIM 24-20 FT 801. NO FAULTS NOTED. IDG RISE WAS PREVIOUS MESSAGE NOT CLEARED EICAS "AUTO EVENT" SHOWED "NO DATA" CLEARED MEMORY. SYSTEM NORMAL VALVE ORDERED, PRE-CAUTIONARY.&NBSP;</P>)

Part: DRIVE UNIT — MALFUNCTIONED (WEATHER RADAR) · airframe 74,774 hrs · 14,785 cycles

ITEM O1; CAPTAINS WEATHER RADAR FAIL AND ITEM 02; FO WEATHER RADAR FAIL.(<P>TRANSFERRED TO MDDR 111474 CAT "C" IAW ATLAS MEL 34-43-01-02 DUE DATE 21MAY19.&NBSP;</P><P>REF LOG PAGE 1055207 ITEM M3; REMOVED AND REPLACED ANTENNA DRIVE UNIT IAW AMM 34-43-05, SYSTEM OPS CHECK NORMAL. THIS CLEARS MDDR 111474.&NBSP;</P>)

Part: CONTROL VALVE — MALFUNCTIONED (AC BAY) · airframe 74,769 hrs · 14,783 cycles

RT PACK TEMP CTL VALVE EICAS MSG.(<P>REMOVED AND REPLACED R PACK CTL VALVE IAW AMM 21-51-12. OPS CHECK GOOD AND MSG CLEARED.&NBSP;</P>)

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 74,757 hrs · 14,780 cycles

RIGHT PACK TEMP EICAS MESSAGE ON APPROACH&NBSP;(<P>PERFORMED RT PACK TEMPERATURE CONTROLLER BITE TEST IAW AMM 21-51-14. TEST OK.&NBSP;</P>)

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 74,733 hrs · 14,776 cycles

LEFT IDG VALVE DISPLAYED.(<P>PERFORMED FIM 24-20 FT 802. NO FAULTS ON BPCU. CHECK CONTINUITY AT CONNECTOR D11 G45 IN IDG HEAT EXCHANGER VALVE. NO DISCREPANCIES NOTICED. CLEARED STATUS MSG IAW FIM 31-41-00/101, FIG 109. </P><P>LP 1009448 - M5: REMOVED K1033 RELAY AT P33, PRECAUTIONARY IAW FIM 24-20 FT 802.</P>)

Part: CONNECTOR — LOOSE (AC BAY) · airframe 74,715 hrs · 14,773 cycles

"RT PACK TEMP "EICAS MESSAGE " COMPLETED QRH CHECK LIST(<P>ACCOMPLISHED RH PACK BITE TEST, PACK TEMP CONTROL VALVE AT FAULT. FOUND CONNECTOR LOOSE, RESECURED CONNECTOR OPS CHECK NORMAL IAW AMM 21-60-00</P>)

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 74,694 hrs · 14,769 cycles

LT IDG VALVE STATUS MESSAGE(<P>PERFORMED FIM 24-20 FT 802 NO FAULTS FOUND ON BPCU. CLEARED STATUS MSG IAW FIM 31-41-00/101 FIG 109</P>)

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 74,702 hrs · 14,770 cycles

R PACK TEMP EICAS MSG IN FLIGHT OK IN STBY&NBSP;(<P>ACCOMPLISHED R 1 PACK BITE TEST NO FAULTS NOTED ACCOMPLISHED OPERATIONAL CHECK OF PACK SYSTEM NO DISCREPANCIES NOTED IAW AMM 21-60-00</P>)

Part: DRIVE UNIT — FAILED (WEATHER RADAR) · airframe 74,649 hrs · 14,761 cycles

LEFT AND RT WEATHER RADAR INOP(<P>REMOVED AND REPLACED WXR DRIVE UNIT IAW AMM 34-43-05. OPS CHECK NORMAL IAW AMM 34-43-00.</P>)

Part: CONTROL VALVE — MALFUNCTIONED (RT A/C PACK) · airframe 74,589 hrs · 14,746 cycles

RIGHT PACK OFF LIGHT ILLUMINATED IN DESCENT.(<P>REMOVED AND REPLACED FLOW CONTROL VALVE ASSY IAW AMM 21-51-01 AND RT PACK FLOW PRINTED CIRCUIT ASSY AS PER B767 AMM 21-51-09. OPS AND LEAK CHECK GOOD.</P><P><BR DATA-MCE-BOGUS="1" /></P><P>PRINTED CIRCUIT OFF P/N: 285T0093-11, S/N: D01158&NBSP;</P>)

Part: HORN — NO TEST (EQUIP COOLING) · airframe 74,589 hrs · 14,746 cycles

WHILE PERFORMING EQUIPMENT COOLING TEST, FOUND HORN INOP.&NBSP;(<P>REMOVED AND REPLACED GROUND CREW CALL HORN IAW AMM 23-43-01. OPS CHECK NORMAL.&NBSP;</P>)

Part: WARNING HORN — INOPERATIVE (APU FIRE) · airframe 74,589 hrs · 14,746 cycles

APU FIRE WARNING HORN INOP AT THE P-40 PANEL, APU REMOTE CONTROL PANEL.&NBSP;(<P>REMOVED AND REPLACED APU FIRE WARNING HORN AT P-40 PANEL. OPS CHECK NORMAL IAW AMM 23-43-01.</P>)

Part: CIRCUIT CARD — MALFUNCTIONED (MLG) · airframe 74,554 hrs · 14,739 cycles

UPON ROTATION, RECEIVED "GEAR NOT DOWN" WARNING MSG. A MASTER AURAL WARNING. RAN ASSOCIATED NON-NORMAL CHECKLIST. ADDITIONALLY, "AIR GND DISAGREE &AMP; LANDING GEAR MONITOR" STATUS MSG.(<P>REMOVED AND REPLACED WEU LANDING CONFIGURATION WARNING CARD MODULE (M983) IAW B767 AMM 31-51-04. OPS CHECK GOOD IAW B767 AMM 31-51-04. REMOVED AND REPLACED PROXIMITY SWITCH ELECTRONICS UNIT (PSEU) IAW AMM 32-09-04. PERFORMED OPS CHECK GOOD. ALSO, DURING TS, FOUND LH GEAR SYS 1 TILT SENSOR S245 EXTREMELY DIRTY AND FULL OF GREASE. CLEANED UP SENSOR AND PERFORMED TILT SENSOR TEST. TEST OK IAW AMM 32-09-07.&NBSP;</P>)

Part: STATUS MESSAGE — FALSE ACTIVATION (LT IDG) · airframe 74,522 hrs · 14,732 cycles

LEFT IDG VALVE STATUS MESSAGE.(<P>PERFORMED OPS CHECK IAW FIM 24-90-32-41, OPS CHECK GOOD.</P>)

Part: UNKNOWN — UNKNOWN (NR 2 ENGINE) · airframe 74,397 hrs · 14,706 cycles

# 2 ENG FUEL LEAK AFTER SHUTDOWN, FOLLOWED BY A STRONG ODOR INSIDE AFT CABIN (FUEL) ROWS 30-37.(<P>RAN # 2 ENG I.A.W AMM 71-00-00 NO LEAKS NOTED &AMP; ODOR NOTED.&NBSP;</P>)

Part: OVERHEAT LOOP — MALFUNCTIONED (LT ENGINE) · airframe 74,386 hrs · 14,705 cycles

LH ENG OVERHEAT LOOP 2 STATUS MESSAGE(<P>ITEM TRANSFER TO MDDR # 109583 - MEL 26-11-02-01 CAT C - DUE DATE 12APR19 / ACFT RESTRICTED ER 120.</P><P>LOG PAGE 1022046 - M13: REMOVED AND REPLACED FIRE LOOP I.A.W AMM 26-11-02. OPS CHECK GOOD, NO FAULTS NOTED &AMP; MSG CLEARED. THIS CLOSES MDDR # 109583.</P>)

Part: CIRCUIT CARD — MALFUNCTIONED (ENG OVERHEAT) · airframe 74,374 hrs · 14,702 cycles

PER MCC REQUEST REPLACE LH ENG OVHT LP2 CARD&NBSP; (DUE HISTORY)&NBSP;(<P>REMOVED AND REPLACED LH ENG. OVHT LP 2 CONTROL CARD IAW AMM 26-11-01 OPS CHECK GOOD.</P>)

Part: CONTROL CARD — MALFUNCTIONED (OVERHEAT SYS) · airframe 74,349 hrs · 14,698 cycles

LEFT ENG OH LP 2 INOPERATIVE. RESET L ENG OH LP 2 CONTROL CARD OPS CHECK GOOD IAW AMM 26-11-01 AND FIM 26-11-00 FIG 104.

Part: COUPLING — LOOSE (BLEED AIR SYS) · airframe 74,347 hrs · 14,697 cycles

L ENG OH LP 2 STATUS MSG(<P>ACCOMPLISHED L EG DETECTION SYSTEM BITE PROCEDURE FOUND A BLEED DUCT COUPLING&NBSP; LOOSE TIGHTENED CONNECTION COUPLING&NBSP; NO OTHER&NBSP; DISCREPANCIES NOTED&NBSP; IAW FIM 26-11-00&NBSP; FIG 104&NBSP;&NBSP;</P>)

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 74,232 hrs · 14,670 cycles

HI FLOW INHIBIT MESSAGE ON EICAS(<P>PLACED ON MDDR 108804 PER MEL 21-51-01.&NBSP;</P><P>LOG PAGE 1026220: MESSAGE ERASED, OPERATIONAL TEST NORMAL IAW AMM 21-51-00. MDDR # 108804&NBSP;</P><P>CLOSED.&NBSP;</P>)

Part: CONTROL UNIT — FAULTY (APU) · airframe 74,240 hrs · 14,671 cycles

APU UNABLE TO REMAIN RUNNING (<P>TRANSFERRED TO MDDR 108863</P><P>LP 1026219: REMOVED AND REPLACED APU CONTROL UNIT IAW B767 AMM 49-61-25/401. OPS CHECK NORMAL. THIS CLEARS MDDR 108683 AND PLACARD REMOVED.<BR /></P>)

Part: APU — FAULTY (APU BAY) · airframe 74,068 hrs · 14,633 cycles

APU DUCT PRESSURE OSCILATES BETWEEN 15 AND 5 PSI.(<P>TRANSFERRED TO MDDR # 107924 AS PER MEL 49-11-01-01 CAT C&NBSP;</P><P>LOG PAGE 1042631: REMOVED AND REPLACED A/C APU IAW AMM 49-11-01, LEAK AND OP CHECK GOOD. APU OIL SERVICED &AMP; CHK IAW AMM 12-13-04.<BR /></P>)

Part: GASKET — FAILED (FLOW SENS MODULE) · airframe 74,048 hrs · 14,628 cycles

APU INOP.(<P>TRANSFER TO MDDR # 107814 IAW DDG&NBSP; 49-11-01A CAT C.REPLACED FLOW SENSING MODULE GASKET IAW B767 AMM 49-53-08/401. OPS CHECK NORMAL. NO MORE / LEAKS FOUND.&NBSP;</P>)

Part: MODULE — LOOSE (PNEUMATIC SYSTEM) · airframe 73,986 hrs · 14,614 cycles

PNEUMATIC DUCT PRESSURE DROPS TO 5 PSI DURING ENGINE START.(<P>FOUND FLOW SENSING MODULE LOOSE: RE-SECURED FLOW SENSING MODULE IAW B767 AMM 49-53-08. PERFORMED OPS CHECK IAW B767 AMM 71-00-00-862. OPS CHECK GOOD.<BR /></P>)

Part: FILTER — NOT REPORTED (APU AIR) · airframe 73,955 hrs · 14,607 cycles

APU AIR INOP.(<P>TRANSFERRED TO MDDR #107318 PER&NBSP;49-11-1-1<BR /></P><P>REMOVED AND REPLACED APU SURGE VALVE FILTER IAW B767 AMM 49-53-06 OPS CHECKED NORMAL, NO LEAKS FOUND. APU AIR PARAMETERS NORMAL DURING ENGINE START/RUN. THIS CLEARS MDDR 107318, PLACARD REMOVED.<BR /></P>)

Part: STARTER — MALFUNCTIONED (RT ENGINE) · airframe 73,955 hrs · 14,607 cycles

EICAS R ENG STARTER&NBSP;(<P>RESET AIR SUPPLY MODULE I.A.W AMM 36-23-00. REMOVED STARTER, INSPECTED, AND FOUND TO BE SERVICEABLE AND REINSTALLED I.A.W AMM 80-11-01. PERFORMED DRY MOTOR USING GROUND AIR START, OPS CHECK GOOD I.A.W AMM 71-00-00</P>)

Part: START VALVE — MALFUNCTIONED (LT ENGINE) · airframe 73,955 hrs · 14,607 cycles

LEFT ENGINE EICAS MESSAGE. VLV START FLUCTUATION AIR FLOW ON START.(<P>FOR COMPANY CONVENIENCE REMOVED AND REPLACED AIR SUPPLY VALVE ASSY ON LEFT ENGINE IAW B767 AMM 36-11-16 / 401. OPS CHECK NORMAL.<BR /></P>)

Part: NOT REPORTED — MALFUNCTIONED (RT ENGINE) · airframe 73,871 hrs · 14,587 cycles

ABORTED RIGHT ENGINE START IAW QRH. NOT ENOUGH BLEED PRESSURE. ACCOMPLISHED OPERATIONAL CHECK OF ENG (RIGHT) DUCT PRESSURE 25 PSI, N2 FUEL, FLOW 0.7 AT ENG START. NO DISCREPANCIES NOTED OPS CHECK GOOD IAW AMM 71-00-00.

Part: BLADE — NICKED (NR 1 ENG FAN) · airframe 73,871 hrs · 14,587 cycles

#1 ENGINE 1ST STAGE FAN ROTOR HAS !EA BLADE WITH A NICK IN THE LE APPROX. 7" FROM TIP.(<P>BLENDED AND PERFORMED DPI OF DAMAGED AREA IAW B767 AMM 72-31-02 AND B767 SOPM 20-20-02,PERFORMED TEST #8 IAW B767 AMM 71-00-00,NO DEFECTS NOTED AT THIS TIME.</P>)

Part: CABLE — WORN (IGNITION SYSTEM) · airframe 73,871 hrs · 14,587 cycles

#2 ENGINE EXCITER TO IGNITER PLUG CABLE "B" IGNITER END IS WORN AND "C" CLIP IS FALLING OFF.(<P>REMOVED AND REPLACED #2 ENGINE IGNITER TO EXCITER CABLES CHANNELS "A" + "B" IAW AMM 74-21-01,PERFORMED ENGINE IGNITION AUDIBLE TEST IAW B767 AMM 74-00-00,NO DEFECTS NOTED AT THIS TIME.P/N ON AND S/N OFF FOR CABLE "A" ARE 10-609660-9,CSGCCD2558.</P>)

Part: BLADE — NICKED (NR 2 ENG FAN) · airframe 73,871 hrs · 14,587 cycles

#2 ENGINE #4 BLADE HAS NICK.(<P>BLENDED AND PERFORMED DPI OF DAMAGED AREA IAW B767 AMM 72-31-02 AND B767 SOPM 20-20-02,PERFORMED TEST #8 IAW B767 AMM 71-00-00,NO DEFECTS NOTED AT THIS TIME.</P>)

Part: SKIN — GOUGED (NR 2 ENG CASE) · airframe 73,871 hrs · 14,587 cycles

#2 ENGINE NOSE COWL HAS GOUGE 4 O'CLOCK POSITION.(<P>REPAIRED AT FAN CASE RING SEGMENT.</P>)

Part: UNKNOWN — LEAKING (NR 2 ENGINE) · airframe 73,871 hrs · 14,587 cycles

#2 ENGINE HAS OIL PUDDLING AFT OF FAN BLADES.(<P>CLEANED #2 ENGINE OIL PUDDLE AFT OF FAN BLADES,FOUND TO BE WITHIN LIMITS IAW B767 FIM 71-08 FAULT TREE 813,NO DEFECTS NOTED.</P>)

Part: BLADE — NICKED (NR 1 ENG FAN) · airframe 73,871 hrs · 14,587 cycles

#1 ENGINE 1ST STAGE FAN ROTOR HAS 1EA BLADE WITH A NICK IN THE LE APROX 5" FROM THE ROOT SECTION.(<P>BLENDED AND PERFORMED DPI OF DAMAGED AREA IAW B767 AMM 72-31-02 AND B767 SOPM 20-02-02,PERFORMED TEST #8 IAW B767 AMM 71-00-00,NO DEFECTS NOTED AT THIS TIME.</P>)

Part: UNKNOWN — LEAKING (NR 2 ENGINE) · airframe 73,871 hrs · 14,587 cycles

#2 ENGINE HAS SIGNS OF OIL LEAK IN AREA OF THE LOWER HALF O/B SIDE OF IDG.(<P>CLEANED AREA IAW B767 AMM 20-10-22,LEAK CHECK ACCOMLPISHED ON TASK CARD A-24-017-01-02.</P>)

Part: BLADE — DAMAGED (NR 1 ENG FAN) · airframe 73,871 hrs · 14,587 cycles

#1 ENGINE 1ST STAGE FAN ROTOR LAS 1EA BLADE WITH A NICJ=K IN THE LE APPROX 12" FROM TIP.(<P>BLENDED AND PERFORMED DPI IAW B767 AMM 72-31-02 AND B767 SOPM 20-2-02,PERFORMED TEST #8 IAW B767 AMM 71-00-00,NO DEFECTS NOTED AT THIS TIME.</P>)

Part: SAFETY WIRE — NONE (B-NUT) · airframe 73,871 hrs · 14,587 cycles

#2 ENG O/B OIL COOLER HAS 2 EA. B NUT THAT REQUIRE SAFETY AND HAS SIGNS OF LEAK.(<P>TORQUED AND SAFETIED #2 ENGINE O/B AIR/OIL HEAT EXCHANGER SUPPLY/RETURN LINES IAW B767 AMM 79-21-09, PERFORMED TEST #3 IAW B767 AMM 71-00-00, NO DEFECTS NOTED AT THIS TIME.</P>)

Part: BLADE — NICKED (NR 2 ENG FAN) · airframe 73,871 hrs · 14,587 cycles

#2 ENGINE #13 BLADE HAS NICK.(<P>BLENDED AND PERFORMED DPI OF DAMAGED AREA IAW B767 AMM,72-31-02 AND B767 SOPM 20-20-02,PERFORMED TEST #8 IAW AMM 71-00-00,NO DEFECTS NOTED AT THIS TIME.</P>)

Part: RELAY — FAULTY (ELECTRICAL SYS) · airframe 73,766 hrs · 14,567 cycles

STBY POWER LIGHT CYCLING ON OVERHEAD PANEL. ASSOCIATED EICAS WARNING ALSO(<DIV>R&AMP;R RELAY&NBSP; K110 PERFORMED OPS CHECK REF AMM 24-33-00 WAS NORMAL</DIV>)

Part: UNKNOWN — MALFUNCTIONED (IGNITION SYSTEM) · airframe 73,766 hrs · 14,567 cycles

IGNITION NR 1 INOP ON LEFT AND RIGHT ENGINES (ER 60)(<P>TRANSFERRED TO MDDR #105980.<BR /></P><P>LP 1033930-M3: PERFORMED OPERATIONAL CHECK IAW AMM 74-00-00-705-012-000, OPS CHECK GOOD. THIS ACTION CLEARS MDDR 105980 AND PLACARD IS REMOVED.&NBSP;</P>)

Part: SELECTOR SWITCH — FAILED (CARGO TEMP) · airframe 73,620 hrs · 14,534 cycles

FWD CARGO A/C INOP(<P>TRANSFER TO MDDR 105007 IAW DDG 21-28-01 CAT D DUE DATE 22 APR-19</P><P>LOG PAGE 1046802 REMOVED AND REPLACED FWD CARGO A/C TEMP SELECTOR SWITCH I.A.W AMM 21-61-04 OPS CHECK GOOD,

Part: START VALVE — NOT REPORTED (RT STARTER) · airframe 73,616 hrs · 14,532 cycles

R STARTER CUTOUT EICAS MSG&NBSP;(<P>TRANSFERRED TO MDDR # 104951 AS PER MEL 80-00-02-01 CAT C&NBSP;</P><P>LOG PAGE 1046792 REMOVED AND REPLACED START VALVE OPS CHECK OK I.A.W AMM 80-11-01 &AMP; 71-00-00 , MDDR # 104951 CLOSED&NBSP;</P>)

Part: STARTER — ABNORMAL (RIGHT) · airframe 73,616 hrs · 14,532 cycles

R STARTER CUTOUT EICAS&NBSP;(<P>MAX MOTOR RIGHT ENGINE N2&NBSP; 26% FOR ONE MINUTE NO EICAS MSG NOTED I.A.W AMM 80-11-00</P>)

Part: SWITCH — DIRTY (WX RADAR SYS) · airframe 73,611 hrs · 14,530 cycles

WX RADAR DOES NOT DISPLAY ON F/O ADI ,TERRAIN DOES NOT DISPLAY ON F/O ADI&NBSP;(<P>CLEANED WXR KORRY SWITCH OF F/O HSI CONTROL PANEL , OPS CHECK WX RADAR SYSTEM ON BOTH SIDES I.A.W AMM 34-43-00 TEST GOOD&NBSP;</P>)

Part: SMOKE DETECTOR — INOPERATIVE (LAVATORY) · airframe 73,572 hrs · 14,518 cycles

SMOKE DETECTOR INOP AT MID LT LAV. LAV LOCKED. REMOVED AND REPLACED DETECTOR AT MID LT LAV IAW AMM 26-13-01. OPS CHECK OK.

Part: BPCU — FAULTY (ELECTRICAL SYS) · airframe 73,572 hrs · 14,518 cycles

UTILITY BUS LOSES POWER DURING POWER SWITCH. T/S AND FOUND BPCU FAULTING. R&R BPCU REF AMM 24-41-03, OPS CKS GOOD.

Part: OXYGEN BOX — FAULTY (COCKPIT) · airframe 73,572 hrs · 14,518 cycles

SECOND OBSERVER SEAT INOP. R&R SECOND OBSERVER O2 MASK BOX ASSY AS PER AMM 35-11-051. LEAK CHECK GOOD.

Part: UNKNOWN — MALFUNCTIONED (EXTERNAL POWER) · airframe 73,541 hrs · 14,511 cycles

GPU INTERMITTENTLY WOULD NOT CONNECT. REMOVED AND REPLACED AUX POWER BREAKER C905 AS PRECAUTIONARY PER 24-20-03.

Part: ANTI-ICE VALVE — MALFUNCTIONED (LT ENGINE) · airframe 73,532 hrs · 14,506 cycles

STATUS MSG L ENG TAI VALVE&NBSP;(<P>REMOVED AND REPLACED L ENG TAI VALVE I.A.W AMM 30-21-03 SYS OPS AND LK CHECK NORMAL&NBSP;</P>)

Part: SWITCH — OUT OF ADJUST (ELECTRICAL SYS) · airframe 73,536 hrs · 14,510 cycles

UTILITY BUSES WILL NOT COME ON LINE AFTER LANDING ENGINE SHUT DOWN ON APU POWER BUT WILL NOT RESET. ADJUSTED S17 LOAD SHED SWITCH IAW MM 22-32-04. LT AND RT UTILITY BUS OK PER LOAD SHED FUCTION CHECK 22-32-04.

Part: SWITCH — ABNORMAL (UTILITY BUSS) · airframe 73,504 hrs · 14,501 cycles

UTILITY BUS WILL NOT COME ON LINE(<P>RESET LEFT AND RIGHT UTILITY BUS SHEDDING SWITCHES NO OTHER FAULTS NOTED MM REF 24-22-00 AND 24-11-00</P>)

Part: OUTFLOW VALVE — WARNING MESSAGE (CABIN PRESSURE) · airframe 73,501 hrs · 14,499 cycles

OUTFLOW VALVE EICAS MSG(<P><SPAN>REMOVED / AND REPLACED OUTFLOW VALVE IAW AMM 21-31-03 OPS NORMAL</SPAN><BR DATA-MCE-BOGUS="1" /></P>)

Part: WARNING SYSTEM — ACTIVATED (CABIN PRESSURE) · airframe 73,454 hrs · 14,487 cycles

CABIN ALT AUTO NR 1 STATUS MSG. PERFORMED CABIN PRESS CONTROLLER BITE TEST AS PER FIM PROCEDURE 21-31-00 FIG 103 TEST PASS MSG CLEARED.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 73,453 hrs · 14,486 cycles

STATUS MSG CABIN ALT AUTO 2 (OUTFLOW VALVE DID NOT OPEN ON LANDING). PERFORMED BITE ON CABIN PRESSURE CONTROLLER AS PER AMM 21-31-02, TEST PASSED NO MESSAGES.

Part: IDG — LEAKING (LEFT) · airframe 73,428 hrs · 14,481 cycles

LEFT IDG LEAKING INTERNALLY. R & R LT IDG IAW AMM 24-11-01-404-001-006, OPS NORMAL.

Part: WARNING MESSAGE — FALSE ACTIVATION · airframe 73,396 hrs · 14,474 cycles

STATUS MESSAGE IN FLIGHT FOR THE CABIN ALTITUDE AUTO 2. THE CABIN PRESSURE CONTROLLER 2 BITE TEST CARRIED OUT IAW AMM 21-31-02, TEST PASSED , NO ACTIVE MESSAGE.

Part: ACTUATOR — MALFUNCTIONED (TE FLAP) · airframe 73,356 hrs · 14,465 cycles

TRAILING EDGE FLAP DISAGREE EICAS ON CLIMB OUT AT INITIAL FLAP RETRACTION MOVEMENT. REMOVED AND REPLACED FLAP LOAD ACTUATOR IAW AMM 27-51-30 OPS CHECK SATISFACTORY.

Part: CONTROLLER — MALFUNCTIONED (CABIN TEMP) · airframe 73,381 hrs · 14,471 cycles

MID CABIN TEMP INOPERATIVE. REMOVED AND REPLACED THE CABIN ZONE TEMP CONTROLLER IAW AMM 21-61-03, OPS CHECKED GOOD. REMOVED AND REPLACED THE MID ZONE VALVE ASSY IAW AMM 21-43-01, OPS CHECK NORMAL. REMOVED AND REPLACED THE MID CABIN AUX ZONE DUCT OVERHEAT SWITCH IAW AMM 21-61-01. OPS CHECKED GOOD.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 73,345 hrs · 14,463 cycles

EICAS MSG MID CABIN TEMP QRH PROCEDURE PERFORMED. MID CABIN TEMP MSG SELF ERASED ON GROUND ALL SATISFACTORY AS PER AMM 21-61-00. OPS CHECK SATISFACTORY.

Part: CONTROL VALVE — INOPERATIVE (LT A/C PACK) · airframe 73,339 hrs · 14,462 cycles

LEFT PACK INOPERATIVE IN AUTO. REMOVED AND REPLACED THE LT PACK TEMPERATURE CONTROL VALVE IAW AMM 21-31-00. OPS CHECKED GOOD.

Part: CONTROL UNIT — MALFUNCTIONED (CABIN PRESSURE) · airframe 73,334 hrs · 14,461 cycles

CABIN ALTITUDE AUTO 1 STATUS MESSAGE. REMOVED AND REPLACED THE NR 1 AUTO PRESSURE UNIT IAW AMM 23-31-00. OPS CHECKED OK

Part: RELAY — MALFUNCTIONED (CABIN TEMP) · airframe 73,334 hrs · 14,461 cycles

TWICE DURING CRUISE, MID CABIN TEMP EICAS ILLUMINATED AND WENT OUT BY ITSELF, ON FOR APPROXIMATED 1 MINUTE EACH TIME. REMOVED AND REPLACED K2063 AUX MID ZONE AUTO/OFF RELAY. MID CABIN TEMP CONTROL OPERATED NORMAL IAW AMM 21-61-00.

Part: FILTER — DIRTY (RT ENGINE) · airframe 73,269 hrs · 14,449 cycles

RT ENGINE FUEL FILTER STATUS MESSAGE. REMOVED AND REPLACED RT ENGINE FUEL FILTER IAW AMM 73-11-02, LEAK CHECK OK.

Part: SWITCH — FAULTY (CABIN TEMP) · airframe 73,253 hrs · 14,445 cycles

AS WE ADDED POWER FOR TAKE OFF "MID CABIN TEMP" MESSAGE APPEARED. REJECTED TO. REMOVED AND REPLACED MID CABIN OVHT TEMP SWITCH S635, LT PACK TEMP CONTROLLER, MODULATING VALVE, & CABIN ZONE CONTROLLER PER AMM 21-61-03.

Part: FILTER — CONTAMINATED (RT ENGINE) · airframe 73,173 hrs · 14,427 cycles

RIGHT ENG FUEL FILTER MESSAGE. REPLACED ENG FUEL FILTER PER AMM 73-11-02 FOUND CONTAMINATION INSP FUEL STRAINER CKS OK. RAN ENG PER AMM 71-00-00 CKS GOOD.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 73,158 hrs · 14,421 cycles

MAIN CABIN SEAT TRACK AT STA 654+39 RBL 11 HAS CORROSION. R&R SEAT TRACK AT STA 654 TO STA 782 PER SRM 53-00-52-2R-1 REPAIR 1.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 73,158 hrs · 14,421 cycles

AFT MAIN CABIN SEAT TRACK HAS CORROSION BETWEEN STA 1412 AND STA 1439 LBL 54.75. R&R SEAT TRACK AT STA 1412-1439 LBL 54.75 PER DWG 146T5200.

Part: FLOOR SUPPORT — CORRODED (BS 859) · corrosion level 2 · airframe 73,158 hrs · 14,421 cycles

MAIN CABIN FLOOR SUPPORT AT BS 859.5, RBL 59 HAD CORROSION. R & R THE FLOOR SUPPORT SECTION IAW SRM 51-40-02-0G-0, AND SRM 53-00-51-2R-3, FIG 201.

Part: STRAP — CHAFED (BS 859.5) · airframe 73,158 hrs · 14,421 cycles

FUSELAGE FRAME STRAP WAS CHAFED AT BS 859.5, STRINGER 18L. R & R THE FRAME STRAP IAW SRM 51-40-02-0G-0.

Part: STRINGER — CORRODED (BS 1241-1263) · corrosion level 2 · airframe 73,158 hrs · 14,421 cycles

STRINGER 39R BETWEEN BS 1241 AND 1263 WAS CORRODED. REPAIRED THE STRINGER IAW EA 767-5360-28-A7415.

Part: SEAT TRACK — CORRODED (BS 654-764) · corrosion level 2 · airframe 73,158 hrs · 14,421 cycles

MAIN CABIN SEAT TRACK BS 654 TO 764, RBL 54.5 HAD CORROSION. R & R THE SEAT TRACK IAW SRM 51-40-02-0G-0, AND SRM 53-00-52-2R-2, REPAIR 2.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 73,158 hrs · 14,421 cycles

MID CABIN FLOOR SUPPORT BETWEEN STA 859.5 AND STA 883.5 RBL 75 HAS CORROSION. REMOVED, FABRICATED, AND INSTALLED REPAIR FLOORBEAM SPLICE & 1EA UPPER CHORD PER SRM 53-00-51-2R-3 REPAIR 3.

Part: ANNUNCIATOR — MALFUNCTIONED (AOA) · airframe 73,158 hrs · 14,421 cycles

ON THE P5 OVERHEAD ANNUNCIATOR PANEL, THE RT AOA ANNUNCIATOR WAS INOPERATIVE. R & R THE RT AOA ANNUNCIATOR LIGHT ASSY IAW AMM 33-16-02. OPS CHECKED GOOD.

Part: SEAT TRACK — CORRODED (BS 654-764) · airframe 73,158 hrs · 14,421 cycles

MAIN CABIN SEAT TRACK BS 654 TO 764 HAS CORROSION. R & R THE SEAT TRACK SECTION IAW SRM 51-40-02-0G-0 AND SRM 53-00-52-2R-1, REPAIR 1.

Part: SKIN — DENTED (FUSELAGE) · airframe 73,158 hrs · 14,421 cycles

RE-EVALUATE PROTRUDING DENT ON FUSELAGE SKIN BETWEEN STA 1629 - STA 1654.5 BELOW STR 36L. REPAIRED DENT AT FUSELAGE STA 1629 TO 1654.5 AT STR 26L TO STR 36L PER EO 6753A751 REV O AND EA 767-5380-28-A7456. THIS REPAIR IS A CATEGORY B REPAIR.

Part: FLOOR SUPPORT — CORRODED (BS 1087-1109) · corrosion level 2 · airframe 73,158 hrs · 14,421 cycles

MAIN CABIN LT FLOOR SUPPORT HAD CORROSION BETWEEN BS 1087 & 1109. R & R THE FLOOR SUPPORT IAW SRM 51-40-02-0G-0.

Part: RADAR — INOPERATIVE (WEATHER RADAR) · airframe 73,158 hrs · 14,421 cycles

WX RADAR INOP. R&R WEATHER RADAR ASSY PER AMM 34-43-05-424-016-002. OPS CHECK GOOD.

Part: SEAT TRACK — GOUGED (BS 1043-1065) · airframe 73,158 hrs · 14,421 cycles

MAIN CABIN SEAT TRACK WAS GOUGED AT TWO AREAS, RBL 55 BETWEEN BS 1043 & 1065. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 53-10-52-01, & DWG 145T5214.

Part: SEAT TRACK — CORRODED (BS 1087-1197) · corrosion level 2 · airframe 73,158 hrs · 14,421 cycles

MAIN CABIN SEAT TRACK BS 1087 TO 1197, RBL 55 HAD CORROSION. R & R THE SEAT TRACK IAW SRM 53-00-52-2R-2, REPAIR 2.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 73,158 hrs · 14,421 cycles

BULK CARGO COMPT FLOORBEAM CORRODED AT STA 1417 AND 1439, BL 0. REPAIRED FLOORBEAM AT THE BULK CARGO COMPARTMENT AT STA 1417 AND STA 1540, BL 0 PER EO 6753A757 REV 0 AND EA 767-5360-028-A7424. THIS IS A CLASS C REPAIR.

Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 73,158 hrs · 14,421 cycles

MID CABIN SEAT TRACK BETWEEN STA 875.2 AND STA 999 RBL 55 HAS SEVERAL GOUGES. REMOVED, FABRICATED, AND INSTALLED SEAT TRACK AT STA 875.2 - STA 999 RBL 55 PER DWG 145T5212 7 AND EA 767-5301-28-A7429.

Part: TRUSS — CORRODED (FUSELAGE) · corrosion level 2 · airframe 73,158 hrs · 14,421 cycles

MAIN CABIN LT SIDE FLOOR TRUSS HAS CORROSION STA 1109 TO STA 1139. R&R MAIN CABIN LT FLOOR TRUSS AT STA 1109 TO STA 1139 PER SRM 51-40-02-0G-0 AND DWG 146T0050.

Part: FLOOR SUPPORT — CORRODED (BS 1395-1536) · corrosion level 2 · airframe 73,158 hrs · 14,421 cycles

BULK CARGO FLOOR SUPPORT CORRODED BETWEEN BS 1417 AND 1439, RBL 36. R & R THE FLOOR SUPPORT IAW SRM 51-40-02-0G-0, AND DWG 146T5002.

Part: FRAME — CORRODED (BS 1153) · corrosion level 2 · airframe 73,158 hrs · 14,421 cycles

AFT CARGO BAY FRAME WAS CORRODED, BS 1153, STRINGER 20L. R & R THE FRAME IAW SRM 51-40-02-0G-0.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 73,158 hrs · 14,421 cycles

MAIN DECK FLOORBEAM CORRODED AT STA 1502, LBL 50, LBL 15, AND RBL 59. ACCOMPLISHED PERMANENT REPAIR OF THE MAIN DECK FLOORBEAM AT STA 1502, LBL 50, LBL 15 TO RBL 59 PER EO 6753A755 & EA 767-5360-28-A7412. THIS IS A CLASS A REPAIR.

Part: TRUSS — CORRODED (FUSELAGE) · airframe 73,158 hrs · 14,421 cycles

CORROSION ON MAIN CABIN RT TRUSS BETWEEN STA 1098 AND STA 1120 AT STR 20R. R&R MAIN CABIN RT SIDE FLOOR TRUSS BETWEEN STA 1098 & STA 1120 AT STR 20R IAW SRM 51-40-02-0G-0.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 73,158 hrs · 14,421 cycles

AFT MAIN CABIN SEAT TRACK HAS CORROSION BETWEEN STA 1360-1480 LBL 11. REMOVED, FABRICATED, AND INSTALLED SEAT TRACK AT STA 1360-1480 LBL 11 PER DWG 146T5200 & EA 767-5301-28-A7424.

Part: RIB — CRACKED (LT WING) · airframe 73,158 hrs · 14,421 cycles

LEFT WING L/E RIB WAS CRACKED AT THE ATTACH POINT TO FRONT SPAR LFS 500.10 OTBD OF THE NR 5 SLAT OTBD DRIVE UNIT. R & R THE LT WING L/E WING RIB IAW SRM 51-40-05 & SRM 51-40-02-0G-0.

Part: RELAY — MALFUNCTIONED (SHUTOFF VALVE) · airframe 73,158 hrs · 14,421 cycles

LEFT NACELLE VENT VALVE EICAS MESSAGE WILL NOT ERASE. TROUBLESHOT AND FOUND THE VENT SHUTOFF VALVE IN THE OPEN POSITION. R & R THE RELAY K676 AT P36 IAW FIM 7523, WDM 75-23-11, AND SWPM 28-81-22. MESSAGE NO LONGER APPEARED.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 73,158 hrs · 14,421 cycles

MAIN CABIN SEAT TRACK FROM STA 1197+132 - STA 1360 LBL HAS SEVERAL AREAS OF CORROSION. REMOVED, FABRICATED, AND INSTALLED SEAT TRACK AT STA 1197 +132 - STA 1360 LBL 11 PER SRM 56-60-52-01-1. 51-40-05, AND EA 767-5301-28-A7426.

Part: BUSHING — CORRODED (NR 1 PYLON) · airframe 73,158 hrs · 14,421 cycles

AFTER REMOVAL OF THE NR 1 PYLON, THE DIAGONAL BRACE AFT ATTACHMENT ON FRONT SPAR HAS PITTING AND FRETTING CORROSION'S ON THE BUSHINGS. ACCOMPLISHED SB 767-57-053 HIGH INTERFERENCE FIT METHOD OF BUSHINGS.

Part: VALVE — FAULTY (CABIN TEMP) · airframe 73,158 hrs · 14,421 cycles

FWD CABIN TRIM AIR INOP LIGHT STAYED ON DURING ENGINE RUN. R&R TRIM AIR VALVE PER AMM 21-61-07-404-041. LEAK AND OPS CHECK GOOD.

Part: SEAT TRACK — CORRODED (BS 340) · corrosion level 2 · airframe 73,158 hrs · 14,421 cycles

MAIN CABIN SEAT TRACK AT BS 340, LBL 20 HAD CORROSION. R & R THE SEAT TRACK IAW SRM 51-40-02-06-0, AND DWG 141T5120.

Part: SEAT TRACK — CORRODED (BS 865-1065) · corrosion level 2 · airframe 73,158 hrs · 14,421 cycles

MAIN CABIN SEAT TRACK BS 870 TO 1065, RBL 88.5 HAD CORROSION. R & R THE SEAT TRACK IAW SRM 51-40-02-0G-0, SRM 53-00-52-2R-1, REPAIR 3, FIG 201, AND EA 767-5301-28-A7431.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 73,158 hrs · 14,421 cycles

MAIN CABIN SEAT TRACK FROM STA 1087 TO 1197 HAS SEVERAL AREAS OF CORROSION. R&R MAIN CABIN SEAT TRACK SECTION FROM STA 1087 TO STA 1197 RBL 88 PER SRM 51-40-02-0G-0.

Part: SEAT TRACK — GOUGED (BS 915.5) · airframe 73,158 hrs · 14,421 cycles

MAIN CABIN SEAT TRACK, BS 915.5, LBL 89 WAS GOUGED. R & R THE SEAT TRACK SECTION IAW SRM 51-40-02-0G-0, AND EA 767-5301-28-A7430 I/R.

Part: FITTING — CRACKED (RT WING) · airframe 73,158 hrs · 14,421 cycles

RT WING JACK FITTING IS CRACKED. R&R RT WING JACK PAD FITTING PER DWG 112T500 REV B.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 73,158 hrs · 14,421 cycles

MAIN CABIN FLOORBEAM IS CORRODED AT STA 1480 RBL 46 TO RBL 52. R&R MAIN T CHORD SECTION, 2EA STRAPS AND 9EA STIFFENERS FROM STA 1480 RBL 37.5 TO RBL 59 PER SRM 53-00-51-2R-1 REPAIR 1.

Part: SEAT TRACK — CORRODED (BS 1230-1362) · corrosion level 2 · airframe 73,158 hrs · 14,421 cycles

MAIN CABIN SEAT TRACK AT LBL 54.45 BETWEEN BS 1230 - 1362.45 HAD SEVERAL AREAS OF CORROSION ON INBD FLANGE. REMOVED, FABRICATED, AND INSTALLED A REPLACEMENT SEAT TRACK IAW SRM 53-60-52-01-0, AND DWG 146T5212.

Part: FLOORBEAM — CORRODED (BS 1518) · airframe 73,158 hrs · 14,421 cycles

FLOORBEAM LOWER TEE HAD CORROSION AT BS 1518, LBL 88.5 TO RBL 88.5. REMOVED CORROSION AND REPAIRED THE FLOORBEAM LWR TEE IAW EA 767-5360-28-A7393, REV I/R.

Part: FAN — INOPERATIVE · airframe 73,158 hrs · 14,421 cycles

RT RECIRC FAN INOP. R&R RT RECIRC FAN PER AMM 21-25-01. OPS CHECK GOOD.

Part: BRACKET — CRACKED (BS 317) · airframe 73,158 hrs · 14,421 cycles

FWD ENTRY DOOR CUTOUT LOWER SILL UPPER SURFACE HAD FOUR FLOOR SUPPORT BRACKETS CRACKED. REMOVED, FABRICATED, AND INSTALLED THE BRACKETS IAW DWG 141T8310, AND SRM 51-40-05-0G-0.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 73,158 hrs · 14,421 cycles

MAIN CABIN SEAT TRACK HAS CORROSION ON SEVERAL AREAS AT LBL 88.5 BETWEEN STA 1230-1360. REMOVED, FABRICATED, AND INSTALLED SEAT TRACK AT LBL 88.5 STA 1230-1360 PER DWG 146T5214 AND EA 767-5301-28-A7422.

Part: SEAT TRACK — CORRODED (BS 1263-1285) · corrosion level 2 · airframe 73,158 hrs · 14,421 cycles

MAIN CABIN SEAT TRACK BS 1263 TO 1285 RBL 11 HAD CORROSION. R & R THE SEAT TRACK IAW SRM 51-40-02-0G-0.

Part: ACM — MALFUNCTIONED (AC BAY) · airframe 73,158 hrs · 14,421 cycles

RT PACK OVERHEATED DURING ENGINE RUNS. R&R RT AIR CYCLE MACHINE PER AMM 21-51-03-404-016. OPS CHECK GOOD.

Part: TRUSS FITTING — CORRODED (BS 1197) · corrosion level 2 · airframe 73,158 hrs · 14,421 cycles

CORROSION ON THE MAIN CABIN FLOORBEAM TRUSS BS 1197+11 ATTACHED TO STRINGER 20R. R & R THE TRUSS IAW DWG 146T0050, REV C.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 73,158 hrs · 14,421 cycles

MAIN CABIN SEAT TRACK LT SIDE 1099 TO 1197+88 HAS CORROSION. R&R MAIN CABIN SEAT TRACK AT STA 1099 TO 1197 + 88 LBL 88.5 IAW SRM 51-40-02-OG-0 AND DWG 146T5200.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 73,158 hrs · 14,421 cycles

MID CABIN FLOOR SUPPORT BETWEEN STA 871 - 903 LBL 11 HAS CORROSION. R&R FLOORBEAM AT STA 871-903 LBL 11 PER SRM 53-00-51-2R-3 REPAIR 3.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 73,158 hrs · 14,421 cycles

MAIN CABIN LT SIDEWALL FRAME AT STA 1197 + 88 BETWEEN LONGERON 19/20 HAS CORROSION. R&R LT MAIN CABIN INNER CHORD FRAME AT STA 1197 +88 BETWEEN LONGERON 19/20 PER SRM 51-40-02-0G-0.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 73,158 hrs · 14,421 cycles

MAIN CABIN SEAT TRACK HAS CORROSION AT RBL 88.5 AND BETWEEN STA 588 & 620. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT SEAT TRACK AT RBL 88.5 STA 434-654 PER DWG 143T521-7Y27.

Part: STRAP — CHAFED (FUSELAGE) · airframe 73,158 hrs · 14,421 cycles

INTERNAL FUSELAGE STA 859.5 AND STR 14R FRAME HAS CHAFFING MARK & 1EA RIVET HEAD CHAFED. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT FRAME STRAP PER DWG 145T8002-14 REV B AT STA 859.9 STR 14R.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 73,158 hrs · 14,421 cycles

MAIN CABIN FLOORBEAM LOWER CHORD HAS CORROSION BETWEEN STA 1480 RBL 0 TO RBL 88. ACCOMPLISHED BLEND OUT REPAIR ON MAIN CABIN FLOORBEAM ASSY LOWER CHORD AT STA 1480 BETWEEN RBL 0 AND RBL 88.5 PER EA 767-5360-28-A7417 I/R.

Part: FLOOR SUPPORT — CORRODED (BS 859) · corrosion level 2 · airframe 73,158 hrs · 14,421 cycles

MAIN CABIN FLOOR SUPPORT AT BS 859.5, LBL 34 HAD CORROSION. R & R THE FLOOR SUPPORT BETWEEN BS 850 TO 900 IAW SRM 51-40-02-0G-0, AND SRM 53-00-51-2R-3, FIG 201.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 73,158 hrs · 14,421 cycles

MAIN CABIN SEAT TRACK FROM STA 1230-1329 RBL 55 HAS SEVERAL AREAS OF CORROSION. REMOVED, FABRICATED, AND INSTALLED MAIN CABIN SEAT TRACK AT STA 1230 - 1329 PER 146T5200 & EA767-5301-28-A7423.

Part: SEAT TRACK — CORRODED (BS 1100) · corrosion level 2 · airframe 73,158 hrs · 14,421 cycles

MAIN CABIN SEAT TRACK BS 1100 HAD CORROSION. R & R THE SEAT TRACK SECTION IAW SRM 51-40-02-0G-0, AND SRM 53-00-52-2R-1, REPAIR 1.

Part: STRAP — CRACKED (FUSELAGE) · airframe 73,158 hrs · 14,421 cycles

AFT CARGO COMPARTMENT FLOORBEAM STABILIZING STRAP IS CRACKED AT STA 1285 LBL 40. R&R AFT CARGO COMPARTMENT FLOORBEAM STABILIZING STRAP AT STA 1263 TO STA 1351 AT LBL 40 PER SRM 51-40-02-0G-0.

Part: FRAME — GOUGED (BULK CARGO) · airframe 73,158 hrs · 14,421 cycles

BULK CARGO DOOR LOWER MID FRAME WAS DEEPLY GOUGED, JUST BELOW STOP. R & R THE MID FRAME IAW SRM 51-40-02-0G-0, AND DWG 146T6322.

Part: SENSOR — MALFUNCTIONED (COCKPIT TEMP) · airframe 73,158 hrs · 14,421 cycles

DURING ENGINE RUNS WITH PACKS OPERATING, THE LEFT PACK OUT TEMP READS -12. TROUBLESHOT IAW FIM 21-61-FT, AND FIM 21-61-FT803. FOUND THE FLIGHT DECK ZONE TEMP SENSOR WITH A FAULT INDICATION. PERFORMED A BITE TEST & RESET THE CONTROLLER IAW AMM 21-51-14-705-035. PERFORMED A COOLING PACK TEST IAW AMM 21-51-03-404-016. OPS CHECKED GOOD.

Part: FLOOR SUPPORT — GOUGED (BS 303-323) · airframe 73,158 hrs · 14,421 cycles

FWD CABIN FLOOR SUPPORT HAD GOUGES BETWEEN BS 303 - 323, LBL 30. R & R THE FLOOR SUPPORT IAW SRM 51-40-05-0G-0.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 73,158 hrs · 14,421 cycles

MAIN CABIN SEAT TRACK IS CORRODED FROM STA 1087 TO STA 1230 RBL 11. R&R MAIN CABIN SEAT TRACK SECTION FROM STA 1070 TO 1230 RBL 11 PER SRM 53-00-52-2R-1 REPAIR 1.

Part: FLOOR SUPPORT — CORRODED (BS 852-910) · corrosion level 2 · airframe 73,158 hrs · 14,421 cycles

MAIN CABIN FLOOR SUPPORT BETWEEN BS 871 TO 903 HAD CORROSION. REPAIRED THE FLOOR SUPPORT IAW SRM 53-00-51-2R-3, REPAIR 3.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 73,158 hrs · 14,421 cycles

CORROSION ON MAIN CABIN RT TRUSS FLOOR SUPPORT BETWEEN STA 1120 AND STA 1142 AT STR 20R. R&R MAIN CABIN FLOOR RT TRUSS BETWEEN STA 1120 AND STA 1142 AT STR 20R PER SRM 51-40-02-0G-0 AND DWG 146T0050.

Part: SEAT TRACK — CORRODED (BS 654-720) · corrosion level 2 · airframe 73,158 hrs · 14,579 cycles

MAIN CABIN SEAT TRACK AT BS 654 + 129, RBL 88 WAS CORRODED. REMOVED, FABRICATED, AND INSTALLED A REPLACEMENT SEAT TRACK IAW DWG 143T5218.