N664GT

Part: LAMP — INOPERATIVE (EXTERIOR) · airframe 113,422 hrs · 18,241 cycles

LEFT AFT EXTERIOR EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED SLIDE AND OVERWING ESCAPE LIGHT LAMPS IAW AMM 33-51-06-902-082, REV 146, 22 AUG 2025. OPERATIONAL WAS GOOD IAW AMM SUBTASK 33-51-06-862-083.

Part: OVEN — SMOKE (ZONE 900) · airframe 113,382 hrs · 18,231 cycles

OVEN NR 2 RIGHT GIVES A LOT OF SMOKE. OVEN OPS CHK OK IAW AMM 25-32-00</P>)

Part: SLIDE — INOPERATIVE (ZONE 800) · airframe 113,217 hrs · 18,197 cycles

FA OPENED ARMED L4 DOOR SLIDE DID NOT INFLATE. R & R L4 SLIDE IAW AMM 25-66-01. OPS CHECK NORMAL. THIS CLOSES MDDR 238866. PLACARD REMOVED.

Part: WINDOW SHADE — MALFUNCTIONED (ZONE 200) · airframe 113,098 hrs · 18,171 cycles

LEFT OVERWING EMERGENCY EXIT (SEAT 23) WINDOW SHADE DOES NOT STOW PROPERLY(<P>R/R SEAT 23 LH WINDOW SHADE IAW AMM 25-27-01. OPS CHK OK. DMI 237098 CLOSED.&NBSP;</P>)

Part: PUMP — FAULTED (FUEL BOOST) · airframe 113,072 hrs · 18,165 cycles

LH AFT FUEL PUMP EICAS MSG RAN QRH WHICH SAID TURN PUMP OFF, PUMP WENT OUT AT 12000. MX FOUND C/B POPPED. R & R LT AFT FUEL PUMP IAW AMM 28-22-03-404-074. OPS CHECK OK.

Part: PIN — DISLODGED (ZONE 200) · airframe 113,006 hrs · 18,151 cycles

COCKPIT FIRE EXTINGUISHER PIN FELL OUT. REINSTALLED PULL TIGHT SEAL PER AMM 26-26-02. NO FURTHER DEFECTS NOTED.

Part: MODULE — UNSECURE (ZONE 200) · airframe 112,807 hrs · 18,109 cycles

L1 FLIGHT ATTENDANT, EMERGENCY O2 MODULE ASSY NOT SECURED. RESECURED O2 MODULE AT L1 ATTENDANT SEAT REF AMM 35-21-12/201. OPS CHECK GOOD.

Part: FUEL FILTER — CONTAMINATED (RT ENGINE) · airframe 112,747 hrs · 18,094 cycles

R ENG FUEL FILT EICAS MESSAGE ILLUMINATED BRIEFLY TWICE ON CLIMB OUT.(<P>ITEM 1: FOUND CONTAMINATION. REMOVED AND REPLACED RH FUEL FILTER &AMP; LK CHECK OK REF AMM 73-11-02.</P> / <P>LP 1902792 ITEM 7: REMOVED AND REPLACED LH ENG FUEL FILTER &AMP; LEAK CHECK GOOD OK PER AMM 73-11-02. REPLACED FILTER PER INSPECTION IN ITEM 1. CONTAMINATION FOUND.</P>)

Part: ANTENNA — DAMAGED (DME) · airframe 112,699 hrs · 18,085 cycles

LEFT DME ANTENNA DAMAGE.(<P>REPLACED LEFT DME ANTENNA LOWER FUSELAGE &AMP; PERFORMED OPERATIONAL TEST, TEST OK IAW B767 AMM 34-55-02.</P>)

Part: EXHAUST CONE — DAMAGED (ZONE 400) · airframe 112,699 hrs · 18,085 cycles

#1 ENG OFF EXHAUST PLUG REQUIRE SHEET METAL SUPPORT TO REMOVE HARDWARE.(<P>REMOVED HARDWARE AT #1 ENG EXHAUST PLUG ON OFF UNIT IAW B767 SRM 51-40-02. NO FURTHER DEFECTS NOTED.</P>)

Part: ANTENNA — DAMAGED (DME) · airframe 112,699 hrs · 18,085 cycles

RIGHT DME ANTENNA DAMAGED.(<P>REPLACED RIGHT DME ANTENNA LOWER FUSELAGE &AMP; PERFORMED OPS TEST, TEST OK IAW B767 AMM 34-55-02.</P>)

Part: FUEL FILTER — NOT REPORTED (ZONE) · airframe 112,699 hrs · 18,085 cycles

APU REQUIRES REPLACEMENT OF FUEL FILTER AT OR BEFORE 450 FLIGHT HOURS PER AMM 28-11-00-582-342. REMOVED FILTER IAW 767 AMM 49-31-04-004-001. FILTER GOOD TO INSTALL. INSTALL FILTER IAW 767 AMM 49-31-04-404-006. CONDUCT LEAK AND OPS CHECK, NO LEAKS OBSERVED & OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 112,699 hrs · 18,085 cycles

CABIN READING LIGHTS AT 4D INOP.(<P>TRANSFER TO DMI 231105 PER MEL 25-20-01 CAT E DUE DATE 17SEP2025.</P>)

Part: BRACKET — DAMAGED (ZONE 200) · airframe 112,699 hrs · 18,085 cycles

MAIN PASSENGER CABIN FWD STORAGE CLOSET MEGAPHONE BRACKET DAMAGED.(<P>REMOVED AND REPLACED MEGAPHONE BRACKET AT MAIN DECK FWD STORAGE CLOSET IAW B767 SRM 51-40-02. NO FURTHER DEFECTS NOTED.</P>)

Part: LATCH — WORN (ZONE 400) · airframe 112,699 hrs · 18,085 cycles

#2 ENG PYLON STRUT TWO LATCH WORN OUT. NEED TO BE REPLACED R/H ACCESS PANEL.(<P>REMOVED DAMAGED LATCHED AT LHS ACCESS PANEL AT #2 ENGINE PYLON STRUT, LOCATED, CLEANED, PREPARED, SECURED AND INSTALLED NEW LATCHES AS REQUIRED AT #2 ENGINE PYLON STRUT ACCESS PANEL PER BOEING 767 SRM 51-40-02-0G-0. PERFORM OPS CHECK, OPS CHK OK. NO FURTHER DISCREPANCY NOTED.</P>)

Part: SATCOM — FAULTED (ZONE 100) · airframe 112,699 hrs · 18,085 cycles

SATCOM DATALINK INOP (SATELLITE COMMUNICATION ) SATCOM SYSTEMS.(<P>MDDR 230661 CONTINUE, OPEN TEST ACTION PLAN AP -31160. AFTER CALLING SATCOM TEAM, ACTIVATED N664GT IRIDIUM SATCOM SDU IAW AMM 23-25-00, TEST DATALINK OK. DMI 230661 CLOSED. PLACARD REMOVED.</P>)

Part: ROLLER — DAMAGED (ZONE 100) · airframe 112,699 hrs · 18,085 cycles

FWD CARGO PDU UNIT R/H STA 580 HAS DAMAGE ROLLER.(<P>REMOVED AND REPLACED FWD CARGO PDU UNIT R/H STA 580 IAW B767-300 AMM 25-53-01. OPERATION CHECK OK GOOD.</P>)

Part: LATCH — FAULTED (ZONE 400) · airframe 112,699 hrs · 18,085 cycles

#2 ENGINE NACELLE STRUT, TWO LATCHES CHECK FOR OPERATION ON WALL ARROUND, FOUND BOTH PARTIAL OPEN.(<P>REMOVED AND REPLACED 2EA DEFECTIVE LATCHES AT #2 ENG NACELLE STRUT IAW B767 SRM 51-40-02. OPS CHECK GOOD.</P>)

Part: FILTER — NOT REPORTED (ZONE 400) · airframe 112,699 hrs · 18,085 cycles

L/H ENGINE FUEL FILTERS REQUIRE REPLACEMENT AT OR BEFORE 450 FLIGHT HOURS(<P>REMOVED L/H FUEL FILTER REF 767 M/M 73-11-02-002-003-G00, OK TO INSTALL NEW FILTER.&NBSP;INSTALLED NEW FILTER ELEMENT REF 767 AMM 73-11-02-402-004-G00. LEAK CHECKED GOOD REF AMM 71-00-00-795-034-H03</P>)

Part: BRACKET — CRACKED (ZONE 400) · airframe 112,699 hrs · 18,085 cycles

#1 ENGINE PYLON I/B DOOR OPEN ROD DAMAGE &AMP; BRACKET CRACKED.(<P>LOCATED, DRILLED, AND INSTALLED NEW HOLD OPEN ROD SUPPORT BRACKET IAW B767 SRM 51-40-02 &AMP; 51-40-05. INSTALLED NEW HOLD OPEN ROD IAW B767 SRM 51-40-02. NO FURTHER DEFECTS NOTED.</P>)

Part: ANTENNA — DAMAGED (VHF) · airframe 112,699 hrs · 18,085 cycles

CENTER VHF COMM ANTENNA DAMAGE.(<P>REPLACED CENTER VHF COMM ANTENNA LOWER FUSELAGE. PERFORM OPS TEST, TEST OK IAW AMM 23-12-03 &AMP; AIPC 23-12-03-02B.</P>)

Part: FILTER — WARNING MESSAGE (FUEL SYS) · airframe 112,699 hrs · 18,085 cycles

ON CLIMB OUT, RH ENG FUEL FILTER EICAS MESSAGE APPEARED THEN DISAPPEARED TWICE. C/W WITH QRH.(<P>REMOVED AND REPLACED FUEL FILTER AT RH ENG AS PER B767-300 AMM 73-11-02 &AMP; FIM 73-11-803, NO LEAKS NOTED&NBSP;</P>)

Part: ROD — DAMAGED (ZONE 400) · airframe 112,699 hrs · 18,085 cycles

#1 ENGINE INBOARD, HOLD OPEN ROD, CORE COWL LH DAMAGE WON'T LOCK.(<P>REMOVED AND REPLACED #1 ENG INBOARD HOLD OPEN ROD COWL LH AS REQUIRED IAW B767 AMM 71-11-11 AND 20-11-00. NO FURTHER DEFECTS NOTED.</P>)

Part: OXYGEN BOX — FAULTED (ZONE 200) · airframe 112,699 hrs · 18,085 cycles

RIGHT OBSERVER OXYGEN REGULATOR STOWAGE BOX DOES NOT CLOSE.(<P>RESTOWED OBSERVER O2 MASK REGULATOR IN STOWAGE BOX IAW B767 AMM 35-11-51, OPS TEST NORMAL. NO FAULTS NOTED.</P>)

Part: FUEL FILTER — NOT REPORTED (ZONE 400) · airframe 112,699 hrs · 18,085 cycles

R/H ENGINE REQUIRES REPLACEMENT OF FUEL FILTER AT OR BEFORE 450 FLIGHT HOURS PER AMM 28-11-00-582-342.<BR>(<P>REMOVED AND REPLACED FUEL FILTER AT R/H ENG AS PER REF B767 AMM 73-11-02. NO LEAKS NOTED.</P>)

Part: PRESSURE SWITCH — MALFUNCTIONED (FUEL SYS) · airframe 112,337 hrs · 18,007 cycles

DURING CLIMB OUT AT 7 MINS AFTER DEPARTURE, WHILE BOTH ENGINES ARE AT 14.0 FF MOMENTARY. RH ENG FUEL FILTER EICAS MSG AND RH ENG FUEL FILTER REMAINS.(<P>REMOVED AND REPLACED PRESSURE SWITCH IAW AMM 73-34-01-024-001. OPS CHECK GOOD, LEAK CHECK GOOD AND MSG CLEARED.</P>)

Part: FUEL FILTER — CLOGGED (LT ENGINE) · airframe 112,280 hrs · 17,994 cycles

DURING CLIMBOUT EICAS MESSAGE "L ENG FUEL FILTER" SHOWED. DUE TO ETOPS RESTRICTION RETURNED TO OKO. LP1691828: ENG RUN DUE PER COMPANY REQUEST.(<P>REMOVED AND REPLACED LT ENG FUEL FILTER ELEMENT IAW B767 AMM 73-11-02. LEAK CHECK NORMAL IAW B767 AMM 71-00-00, NO DEFECTS NOTED. LP 1691828: PERFORMED LT ENGINE RUN IAW B767 AMM 71-00-00, ENGINE STARTED STABILIZED, NO FAULTS OR DEFECTS. "LT ENG FUEL FILTER" DID NOT REPEAT.</P>)

Part: FUEL FILTER — WARNING MESSAGE (LT ENGINE) · airframe 112,102 hrs · 17,947 cycles

"L" ENG FUEL FILTER EICAS MSG FOLLOWED BY STATUS MSG. COMPLIED WITH QRH, ENGINE OPS NORMAL.(<P>INSPECTION &AMP; REPLACEMENT OF LEFT ENG FILTER IN WORK (OPEN DISCREPANCY). R/R LH ENG, RH ENG AND APU FUEL FILTERS IAW B767 AMM 73-11-02 &AMP; 49-11-00. LEAK CHECK NORMAL IAW B767 AMM 71-00-00 &AMP; 49-11-00&NBSP;</P>)

Part: SOCKET — NO TEST (CARGO HEAT) · airframe 112,048 hrs · 17,935 cycles

DURING CHECK, AFT CARGO HEAT INHIBIT AFTER AFT ARMED SWITCH ACTIVATION, FUNCTIONAL TEST WAS NOT SATISFACTORY, IN REF TASK CARD A-26-010-00-01.(<P>SOCKETS WERE REPLACED IAW SWPM 20-61-00 REV 87. NO FURTHER DEFECTS NOTED. TEST STATISFACTORY.</P>)

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 112,048 hrs · 17,935 cycles

BULK CARGO COMPARTMENT CEILING AREA FLOOR BEAM STA 1502 BETWEEN LBL88.5 AND RBL 88.5 LOWER CHORD SOME EXFOLATION L=1.625" W=0.812"(<P>CORROSION WAS REPAIRED <SPAN>IAW FAA 8110-3, FVCI EO 24225-1. NO FURTHER DEFECTS NOTED.</SPAN></P>)

Part: SKIN — CORRODED (ZONE 600) · airframe 112,048 hrs · 17,935 cycles

RIGHT WING, UPPER SKIN CORROSION ON SETTLEMENT AREA OF CAP FILL, OUTER FACE.(<P>RIGHT WING, UPPER SKIN CORROSION ON SETTLEMENT AREA OF CAP FILL OUTER FACE WAS REWORKED AND EVALUATED. FOUND WITHIN ALLOWABLE LIMITS IAW SRM 57-20-01-1A-1 TABLE 1 REV. 127 15-DEC-2024.</P>)

Part: GASKET — LEAKING (NR 2 ENGINE) · airframe 112,048 hrs · 17,935 cycles

ENG 2, THRUST REVERSER INNER ZONE, EVIDENCE OF OIL LEAKEAGE AT 6 O'CLOCK.(<P>ENG. 2 CARBON SEAL AND GASKET OF OIL SCAVENGE TUBE WERE REPLACED IAW GE CF6-80C2 SERVICE BULLETIN 79-0044 R00 OIL-B-SUMP AND C-SUMP DRAIN LINES-NUTPLATES INSPECTION REV 31-MAR-1995. NO FURTHER DEFECTS NOTED.</P>)

Part: SHUTOFF VALVE — LEAKING (HYD SYSTEM) · airframe 112,048 hrs · 17,935 cycles

SECTION 48 AT STA 1702, PRES SOV LEFT (V150) WITH EVIDENCE OF HYDRAULIC LEAK.(<P>VALVE WAS REPLACED IAW AMM 29-11-08-404-013. TORQUE APPLIED 700LB-LN S/N: 0224902084 21 FEB 25. OPERATIONAL TEST - LEFT HYDRAULIC SYSTEM ISOLATION VALVE WAS PERFORMED IAW AMM 29-22-00-715-043</P> / <P>REV 143 22-AUG-24. OK FOR SERVICE, NO LEAKS WERE FOUND.</P>)

Part: SERVO — LEAKING (ZONE 300) · airframe 112,048 hrs · 17,935 cycles

VERTICAL STABILIZER, INBOARD YAW DAMPER WITH LEAK EVIDENCE.(<P>INBOARD YAW DAMPER WAS REPLACED IAW AMM 22-21-02414-016 REV. 143 DATE: 22 AUG 24 AND 22-21-02-014-001 REV. 143 DATE: 22 AUG 24 TORQUE APPLIED 140LB- IN /170 LB -IN /80LB-LN WITH TOOL SIN 0524121887 DATE 15 MAY 25 OPERATIONAL TEST WAS PERFORMED. NO LEAKS FOUND. BODING TEST WAS PERFORMED 0.91 MOHMS WITH TOOL SIN D0008326 DATE 17 JUN 25</P>)

Part: SKIN — CORRODED (ZONE 100) · airframe 112,048 hrs · 17,935 cycles

CORROSION ON ATTACHMENT POINTS OF ANTENNA SATCOM BETWEEN STA 977 AND STA 1043, STGR 1L AND STGR 1R.<BR>(<P>CORROSION ON ATTACHMENT POINTS OF ANTENNA SATCOM BETWEEN STA 977 AND STA 1043, STGR IL AND STGR IR WAS&NBSP;REWORKED AND EVALUATED. FOUND WITHIN ALLOWABLE LIMITS IAW SRM 53-00-01-IA-I FIG. 101 REV. 127 15-DEC-2024 CORROSION LEVEL 1.</P>)

Part: LAMP — INOPERATIVE (ZONE 200) · airframe 112,048 hrs · 17,935 cycles

INOP EMERGENCY LIGHTS L391, L644 AND L781.(<P>EMERGENCY LIGHTS L391, L644 AND L781 LA MPS OF L391, L644 AND L781 WERE REPLACED. TASK CARD A-33-001-OO-01/001 INOP EMERGENCY LIGHTS L391, L644 AND L781 LAMPS OF L391, L644 AND L781 WERE REPLACED I.A.W. AMM 33-51-06-902-082 DATE 22 AUG 2024 REV 143. TEST WAS PERFORMED WITH SATISFACTORY RESULTS I.A.W. AMM 33-51-06-862-083. DATE 22 AUG 2024 REV 143.</P>)

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 112,048 hrs · 17,935 cycles

BULK CARGO COMPARTMENT CEILING AREA FLOOR BEAM STA 1518 BETWEEN LBL 88.5 AND RBL 88.5 LOWER CHORD SOME EXFOLIATION L=1.437" W=0.875"(<P>CORROSION WAS REPAIRED IAW FAA 8110-3, FVCI EO 24225-2. NO FURTHER DEFECTS NOTED.</P>)

Part: SKIN — CORRODED (ZONE 500) · airframe 112,048 hrs · 17,935 cycles

LEFT WING, UPPER SKIN CORROSION ON SETTLEMENT AREA OF CAP FILL, OUTER FACE.(<P>LEFT WING, UPPER SKIN CORROSION ON SETTLEMENT AREA OF CAP FILL OUTER FACE WAS REWORKED AND EVALUATED. FOUND WITHIN ALLOWABLE LIMITS IAW SRM 57-20-01-1A-1 TABLE 1 REV. 127 15-DEC-2024</P>)

Part: CASE — CORRODED (ENG FAN) · airframe 112,048 hrs · 17,935 cycles

ENG 1, BTW 10-3 O'CLOCK, V-GROOVE WITH CORROSION.(<P>ENG 1, BTW 10-3 O'CLOCK, V-GROOVE WITH CORROSION. AREA WAS CLEANED. INITIALS MEASURES WERE PERFORMED. DAMAGES WERE BLEND OUT AND REWORKS WERE FOUND WITHIN ALLOWABLE LIMITS I.A.W. AMM TASK 72-33-00-206-001 REV 143 22AUG24 AND SRM 51-10-02-0G-0 REV 127 15DEC24. CORROSION WAS CLEAN OUT EVALUATED AND FOUND WITHIN ALLOWABLE DAMAGE LIMITS.</P>)

Part: FUEL TANK — LEAKING (ZONE 100) · airframe 112,048 hrs · 17,935 cycles

CENTER TANK,ABOVE OF LEFT AIR COND PACK,BETWEEN L-10 AND LBL 20,WITH FUEL LEAK(<P>CENTER TANK, ABOVE OF LEFT AIR COND PACK, BETWEEN L-IO AND LBL 20, WITH FUEL LEAK. DAMAGE SEALANT WAS REMOVED, AREA WAS CLEANED AND FUEL LEAK WAS REPAIRED IAW AMM 28-11-00-308-013 REV. 143 22-AUG-2024. NO FURTHER DEFECTS NOTED.</P>)

Part: FITTING — LEAKING (ZONE 100) · airframe 112,048 hrs · 17,935 cycles

RIGHT CENTER TANK, REAR SPAR BULKHEAD TERMINAL FITTING, LOWER SURFACE, STA 955 AND RBL92 WITH FUEL LEAK.(<P>FUEL LEAK WAS REPAIRED IAW AMM 28-11-00-308-013 REV 143. LEAK CHK GOOD. NO FURTHER DEFECTS NOTED.</P>)

Part: SKIN — DENTED (ZONE 500 FLAP) · airframe 112,048 hrs · 17,935 cycles

LH WING INBOARD AFT FLAP, DENTS ON LOWER SKIN. LH WING INBOARD AFT FLAP, DENT'S ON LOWER SKIN WERE REPAIRED IAW SRM 57-53-01-2R-1 FIG 201 SHEET 4 NOTE A PAG 1-5 AND SRM 51-70-03-OG-O PAR 5L FIG 16 PAG 15, -41 REV 127 15/DEC/24. NO FURTHER DEFECTS NOTED/

Part: MODULE — LEAKING (ZONE 700) · airframe 112,048 hrs · 17,935 cycles

LH MAIN LANDING GEAR W/W BRAKE MODULE WITH LEAK EVIDENCE AT CEILING AREA.(<P>LH MAIN LANDING GEAR W/W VALVE BRAKE MODULE WAS REPLACED IAW AMM TASK 32-41-02-424-002-003 REV 143 DATE 22-AUG-24, LEAK TEST WAS PERFORMED, NO LEAKS WERE FOUND.</P>)

Part: SKIN — DENTED (ZONE 600 FLAP) · airframe 112,048 hrs · 17,935 cycles

RH WING, AFT FLAP LOWER SKIN OUTER PLIES WITH DENT BETWEEN IFS 230 AND IFS 280.(<P>DENT WAS REPAIRED IAW SRM 57-53-01-2R-1 FIG 201 SHEET 4 PAGE 1-5. NO FURTHER DEFECTS NOTED</P>)

Part: RIB — CRACKED (ZONE 600) · airframe 112,048 hrs · 17,935 cycles

RH WINGLET, CRACK ON RIB INNER FACE WBL 929.1227. CRACK ON RH WINGLET STRUCTURE UPPER FLANGE OF RIB 1, AFT WAS REPAIRED IAW TRE6757273 ISSUED DATE: 21 DEC24 AND RDR NUMBER: CMA-TLS-24-0226-10B DATE 12 JAN 25. NO FURTHER DEFECTS NOTED.

Part: FUEL TANK — LEAKING (ZONE 600) · airframe 112,048 hrs · 17,935 cycles

RH WING, INSIDE DRY BAY, BETWEEN RIBS 6 TO 7 FUEL LEAK.(<P>RH WING, INSIDE DRY BAY, BETWEEN RIBS 6 TO 7 FUEL LEAK WAS REPAIRED IAW AMM 28-11-00-308-013 REV. 143 22-AUG 2024.&NBSP;<SPAN>NO FURTHER DEFECTS NOTED.</SPAN></P>)

Part: SERVO — LEAKING (ZONE 300) · airframe 112,048 hrs · 17,935 cycles

VERTICAL STABILIZER, OUTBOARD YAW DAMPER WITH LEAK EVIDENCE.(<P>VERTICAL STABILIZER OUTBOARD YAW DAMPER WAS REPLACED, REMOVED I.A.W AMM 22-21-02-014-001 AND WAS INSTALLED I.A.W AMM 22-21-02-414-016 REV.143 DATE 22 AUG 22, TORQUE APPLIED 140 LB/LN, 170 LB/IN, 150 LB/IN TORQUE DATA (S/N:0522902549 D/D: 09 OCT 25), BONDING TEST OK (0.03 MILLIOHMS) BONDING METTER DATA (S/N:DC008326 D/D:17 JUN 25) AND LEAK CHECK TEST OK.</P>)

Part: BEAM — CORRODED (ZONE 800) · airframe 112,048 hrs · 17,935 cycles

AFTER CARGO DOOR, BEAM INNER CHORD WITH CORROSION (L: 2.750"; W: 1.000") BTW STA 1285 &AMP; STA 1329, STRG 23.(<P>CORROSION WAS REWORKED, EVALUATED AND FOUND WITHIN ALLOWABLE LIMITS IAW SRM 53-30-02-1A-1 FIG 101 DETAIL IV. REV 127 15DEC24, SRM 51-10-02-0G-0 REV 127 15DEC24. CORROSION LEVEL 1. NO FURTHER DEFECTS NOTED.</P>)

Part: CASE — CORRODED (ENG FAN) · airframe 112,048 hrs · 17,935 cycles

ENG1, FAN CASE, BTW 12-6 O'CLOCK, WITH SEVERAL POINTS OF CORROSION.(<P>ENG 1, FAN CASE, BTW 12-6 O'CLOCK, WITH SEVERAL POINTS OF CORROSION. CORROSION WAS EVALUATED IAW AMM 72-33-00-206-OOI-HOO REV 143 22AUG22, SUBTASK 72-33-00-216-011-HOO REV 143 22AUG24. CORROSION LEVEL 1. CORROSION WAS CLEAN OUT, EVALUATED AND FOUND WITHIN ALLOWABLE DAMAGE LIMITS.</P>)

Part: FUEL TANK — LEAKING (ZONE 100) · airframe 112,048 hrs · 17,935 cycles

RIGHT CENTER TANK, LOWER SKIN, STRG L-17 AND RBL 62 WITH FUEL LEAK.(<P>RIGHT CENTER TANK, LOWER SKIN, STRG L-17 AND RBL 62 FUEL LEAK WAS REPAIRED IAW AMM 28-11-00-308-013. NO LEAKS NOTED. NO FURTHER DEFECTS NOTED</P>)

Part: SPAR — CORRODED (ZONE 300) · corrosion level 2 · airframe 112,048 hrs · 17,935 cycles

HORIZONTAL STAB TORSION BOX REAR SPAR LOWER CHORD BTW LBL13.83 AND RBL 13.83, LOWER SKIN WITH CORROSION, DIMENSION ITEM 1 L=1'' W=0.680'', ITEM 2 L=2.5 '' W= 1.437 '' AND ITEM 3 L= 3'' W= 1.480 ''.(<P>HORIZONTAL STAB TORSION BOX REAR SPAR LOWER CHORD BTW LBL13.83 AND RBL 13.83, LOWER SKIN WITH CORROSION, DIMENSION ITEM 1 L=L" W=O.680", ITEM 2 W=2.5 " 1.437 " AND ITEM 3 3" W: 1.480. JOB REPAIR WAS PERFORMED I.A.W. TRE6755079 AND RDR NUMBER CMA-TLS-24-0224-OIC DATE 23-DEC-24 CORROSION LEVEL 1. NO FURTHER DEFECTS NOTED</P>)

Part: FRAME — CORRODED (NR 2 ENG) · corrosion level 2 · airframe 112,048 hrs · 17,935 cycles

DURING THE REMOVAL OF THE FWD ACOUSTIC PANEL, CORROSION WAS FOUND ON THE FAN FRAME, ENGINE 2, BETWEEN 8:00 AND 10:00 O'CLOCK POSITION.(<P>ON THE FAN FRAME, ENGINE 2, BETWEEN 8:00 AND 10:00 O'CLOCK POSITION. CORROSION LEVEL 2 WAS REPAIRED IAW ESM 72-22-01 REPAIR 010 PAGE 4. FIG 902 REV 98 12-JAN-18. NO FURTHER DEFECTS NOTED.</P>)

Part: SUPPORT RING — CORRODED (ZONE 400) · corrosion level 2 · airframe 112,048 hrs · 17,935 cycles

ENG 1, NAC STA 195.50, AROUND ENG SUPPORT RING WITH CORROSION.(<P>ENG 1 SUPPORT RINGS RH AND LH WERE REPLACED IAW ESM TASK 72-23-00 SUBSTASK 72-23-00-040-253 AND TASK 72-23-00 SUBSTASK 72-23-00-040-365 REV. 98 DATE 25-MAR-24. REF IPC 72-33-54-02. NO FURTHER DEFECTS NOTED</P>)

Part: PACKING — LEAKING (ZONE 100) · airframe 112,048 hrs · 17,935 cycles

FUEL LEAK AROUND PRESSURE SWITCHES LEFT OVERRIDE FUEL PUMP AT REAR SPAR WS250, WING LH.(<P>O-RINGS OF THE PRESSURE SWITCH LEFT OVERRIDE FUEL PUMP WERE REPLACED. I.A.W. AMM 28-42-01-004-001/28-42-01-404-008 REV.143 DATE: 22-AUG-24, TORQUE APPLIED: 100 LB-IN TORQUE DATA: S/N:1123126455 DATE: 18-NOV-25.&NBSP;<SPAN>NO FURTHER DEFECTS NOTED.</SPAN></P>)

Part: PLATE — CORRODED (ZONE 200) · corrosion level 2 · airframe 112,048 hrs · 17,935 cycles

CORROSION ON FRAME BTW STA 1459 AND 40 IN LBL APROX OF LOWER AFT CORNER AT BULK CARGO. MEASURES LONG: 0.43IN, WIDTH: 0.45IN.(<P>CORROSION ON FRAME BTW STA 1459 AND 40 IN LBL APROX OF LOWER AFT CORNER AT BULK CARGO- MEASURES LONG: 0.43IN, WIDTH: 0.45IN. DAMAGE WEB FRAME BTW STA 1459 AND 40 IN LBL APPROX OF LOWER AFT CORNER AT BULK CARGO, WAS REMOVED IAW SRM 51-40-02-0G-0 REV 127 15/DEC/24. NEW WEB DRILLED AND ADJUSTED, ALODINE AND PRIMER WERE APPLIED AT NEW WEB HOLES AND NEW WEB WAS INSTALLED IAW SRM 51-10-02-0G-0 REV 127 15/DEC/24. AND SRM 51-40-02-0G-0 REV 127 15/DEC/24.DWG 146T8211. CORROSION LEVEL II. NO FURTHER DEFECTS NOTED</P>)

Part: ANTENNA — CORRODED (TCAS) · corrosion level 2 · airframe 112,048 hrs · 17,935 cycles

UPPER TCAS ANTENNA WITH CORROSION ON THE BASE.(<P>6734A112/002 UPPER TCAS ANTENNA WITH CORROSION ON THE BASE. UPPER TCAS ANTENNA WAS REPLACED WITH SATISFACTORY TEST IAW AMM 34-45-02-344-158 AND 34-45-02 REV 143 DATE 22/AUG/24 TORQUE S/N 924401124 DATE 30/SEP/25 WRENCH 23 LB-IN BONDING S/N DC005293 DATE 04/JUL/25 METTER 1MOHM.</P>)

Part: MODULE — LEAKING (HYD SYSTEM) · airframe 112,048 hrs · 17,935 cycles

SECTION 48 AT STA 1702, RETURN COMPENSATOR MODULE WITH EVIDENCE OF HYDRAULIC LEAK.(<P>SECTION 48 AT STA 1702, RETURN COMPENSATOR MODULE WAS REPLACED IAW AMM 29-22-02-404-012 REV 143</P> / <P>22-AUG 24, NO LEAKS WERE FOUND. OPS CHECK GOOD.</P>)

Part: SKIN — DENTED (ZONE 600 FLAP) · airframe 112,048 hrs · 17,935 cycles

RH WING, AFT FLAP UPPER SKIN WITH DENT BETWEEN IFS 230. RH WING AFT FLAP UPPER SKIN WITH DENT BETWEEN IFS 230 WAS REPAIRED IAW SRM 57-53-01-2R-1 PAG 1-7 FIG 201 AND SRM 51-70-10-2R-4 PAG 8-22 FIG 202 SHEET 1 REV 127 15/DEC/24. NO FURTHER DEFECTS NOTED.

Part: FUEL TANK — LEAKING (ZONE 100) · airframe 112,048 hrs · 17,935 cycles

FUEL LEAK ON CENTER TANK L6 LWBL 97.(<P>FUEL LEAK ON CENTER TANK L6 LWBL 97 WAS REPAIRED IAW AMM 28-11-00-08-013 REV.143 22-AUG-2024.&NBSP;<SPAN>NO FURTHER DEFECTS NOTED.</SPAN></P>)

Part: FUEL TANK — LEAKING (ZONE 100) · airframe 112,048 hrs · 17,935 cycles

FUEL LEAK ON CENTER TANK L10 LWBL 97.(<P>FUEL LEAK ON CENTER TANK L10 LWBL 97 WAS REPAIRED IAW AMM 28-11-00-308-013 REV. 143 22-AUG-2024.</P>)

Part: FITTING — LEAKING (ZONE 100) · airframe 112,048 hrs · 17,935 cycles

RIGHT CENTER TANK, REAR SPAR BULKHEAD TERMINAL FITTING, UPPER SURFACE, STA 955 AND RBL87 WITH FUEL LEAK.(<P>FUEL LEAK WAS REPAIRED IAW AMM 28-11-00-308-013 REV 143 22 AUG 2024. NO LEAKS NOTED. NO FURTHER DEFECTS NOTED.</P>)

Part: FUEL FILTER — WARNING MESSAGE · airframe 111,539 hrs · 17,827 cycles

LEFT AND RIGHT FUEL FILTER EICAS MESSAGES. R & R LH, RH & APU FUEL FILTERS IAW AMM 73-11-02 &AMP; 49-11-02. T/S IAW FIM 73-11-803 &AMP; SUPP MANUAL 28-11-00. NO LEAKS NOTED OR FILTER MSG PRESENT. OPS &AMP; LEAK CHECK GOOD.

Part: COVER — MISSING (ZONE 200) · airframe 111,466 hrs · 17,811 cycles

RH AFT EMERGENCY EXIT NO SMOKING &AMP; SEATBELT LIGHTS MISSING COVER(<P>REMOVED AND REPLACED RH AFT EMERGENCY EXIT NO SMOKING / SEAT BELT ASSY &AMP; OPS TEST GOOD IAW AMM 33-24-00. NO FURTHER DEFECTS NOTED</P>)

Part: LIGHT — INOPERATIVE (SEAT 5CA) · airframe 111,357 hrs · 17,790 cycles

EMERGENCY LIGHT OVER SEAT 5CA INOP(<P>R/R EMERGENCY LIGHT OVER 5 CA PER AMM 33-50-00. OPS CHK GOOD.</P>)

Part: PBE — DAMAGED (CABIN) · airframe 111,176 hrs · 17,744 cycles

LT AFT PBE DAMAGED. ( PBE SMOKE HOODS )(<P>PLACED AFT LEFT BULKHEAD PBE TO DMI 209909 PER MEL 35-20-01 CAT D EXP 20SEP24. PBE PLACED IN MX CLOSET. REMOVED AND REPLACED PBE AT AFT LH FA STATION PER AMM 25-64-02. OPS CHECKS GOOD. THIS CLEARS MDDR 209909</P>)

Part: LIGHT — INOPERATIVE (EXTERIOR E LIGHT) · airframe 110,737 hrs · 17,639 cycles

THE RIGHT SIDE EXTERIOR EMERGENCY LIGHTS ( L391 AND L644 ) INOP(<P>&NBSP;SLIDE LIGHT LAMP (L391) WAS REPLACED IAW AMM 33-51-06-902-082 REV 141 DATED 22DEC23. OPS CHECK GOOD</P>)

Part: SKIN — DENTED (RT WING TE FLAP) · airframe 110,737 hrs · 17,639 cycles

RIGHT WING INBOARD AFT FLAP UPPER SKIN WITH TWO DENTS(<P>UPPER SKIN WAS REPAIRED SRM 57-53-01-2R-1. NO FURTHER DEFECTS NOTED</P>)

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 110,737 hrs · 17,639 cycles

THE FLIGHT DECK EMERGENCY EXIT LIGHT ( L286 ) INOP(<P>PART WAS REPLACED IAW AMM 33-51-06. OPS CHECK GOOD</P>)

Part: LAMP — INOPERATIVE (EXTERIOR E LIGHT) · airframe 110,737 hrs · 17,639 cycles

THE LEFT SIDE EXTERIOR EMERGENCY LIGHT ( L645 ) INOP(<P>SLIDE LIGHT LAMP (L645) WAS REPLACED IAW AMM 33-51-06-902-082 REV 141. OPS CHECK GOOD</P>)

Part: PRESSURE SWITCH — FAULTED (FUEL SYS) · airframe 110,482 hrs · 17,592 cycles

ENG FUEL FILTER PRESSURE LIGHT CAME ON IN FLIGHT(<P>REMOVED AND REPLACE FUEL FILTER DIFFERENTIAL PRESSURE&NBSP; SWITCH PER FIM 73-34-01 AND AMM 73-34-01 LEAK AND OPS CK C/W</P>)

Part: BATTERY — UNKNOWN (UNKNOWN) · airframe 110,421 hrs · 17,571 cycles

LH AND RH OVERWING EMERGENCY EXIT SIGNS INOP(<P>REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY M1209 PER AMM 33-51-07. OPS CHECKS GOOD</P>)

Part: LIFE VEST — MISSING (CABIN) · airframe 110,421 hrs · 17,571 cycles

MISSING 3 SPARE LIFE VEST MISSING ( NON-ESSENTIAL EQUIPMENT & FURNISHINGS (NEF) (120 DAYS) (NEF-CABIN GENERAL 5) )(<P>INSTALLED 3 MISSING SPARE LIFE VESTS ON AIRCRAFT IAW LOPA DWG 6725A197-EEL. DMI 199117 CLOSED. PLACARD REMOVED AND MCC NOTIFIED.</P>)

Part: FILTER — UNKNOWN (UNKNOWN) · airframe 110,114 hrs · 17,502 cycles

"L ENG FUEL FILT" EICAS MSG COMPLIED WITH QRH. EICAS MESSAGE WENT OUT AND STATUS MSG REMOVED(<P>R/R LH ENG MAIN FUEL FILTER IAW AMM 73-11-02. NO LEAKS NOTED. OK FOR SEVICE.</P>)

Part: DEFIBRILLATOR — UNKNOWN (UNKNOWN) · airframe 109,772 hrs · 17,424 cycles

EMERGENCY DEFIBRILLATOR IN FWD EMERGENCY EQUIPMENT CLOSET NEAR EXPIRATION DATE.(<P>REMOVED AND REPLACED DEFIBRILLATOR IN FWD EMERGENCY EQUIPMENT CLOSET REF AMM 25-64-03</P>)

Part: FILTER — UNKNOWN (UNKNOWN) · airframe 109,482 hrs · 17,361 cycles

ENG 1 FUEL FILTER REPLACEMENT AFTER POST OPS RUNS DUE TO FOAM REPLACEMENT.(<P>ENG 1 FUEL FILTER REPLACEMENT AFTER POST OPS RUNS DUE TO FOAM REPLACEMENT, FUEL FILTER ELEMENT WAS REPLACED IAW AMM 73-11-02-404-008-H00 REV 139 DATE 22 APR 23. NO LEAKS FOUND.</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 109,482 hrs · 17,361 cycles

SEVERAL DENTS ON ENG. #2 PRIMARY EXHAUST OUTER SKIN BOTH SIDES(<P>DENT WAS EVALUATED AND FOUND WITHIN ALLOWABLE LIMITS IAW B767-300 SRM 54-42-30-1A-1 A.D. 1 FIG 101 SHEET 3 NOTE N DETAIL VIII REV 122 15 APR 23. DENT WAS ADDED ON DENT LOG DAMAGE CHART AS PER ATLAS GMM 3.19.1&NBSP;</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 109,482 hrs · 17,361 cycles

WING CTR FUEL TANK WITH FOAM DEFORMED.(<P>WING CTR FUEL TANK WITH FOAM DEFORMED WERE REPLACED IAW INVICTA-FRS INSTALLATION, B767 SERIES REV 1 01 JUN 18. PN: FF-00405-6133, FF-00405-6032, FF00405-5132.</P>)

Part: FILTER — UNKNOWN (UNKNOWN) · airframe 109,482 hrs · 17,361 cycles

ENG 2 FUEL FILTER REPLACEMENT AFTER POST OPS RUNS DUE TO FOAM REPLACEMENT.(<P>ENG 2 FUEL FILTER REPLACEMENT AFTER POST OPS RUNS DUE TO FOAM REPLACEMENT, FUEL FILTER WAS REPLACED IAW AMM 73-11-02-404-008-H00 REV139 DATE 22 APR 23. NO LEAKS WAS FOUND.</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 109,482 hrs · 17,361 cycles

DENT ON ENG #1 PRIMARY EXHAUST OUTER SKIN AT NAC STA 341.67 BETWEEN 4/5 O'CLOCK(<P>DENT WAS EVALUATED AND FOUND WITHIN ALLOWABLE LIMITS IAW B767-300 SRM 54-42-30-1A-1 A.D. 1 FIG 101 SHEET 3 NOTE N DETAIL VIII REV 122 15 APR 23. DENT WAS ADDED ON DENT LOG DAMAGE CHART AS PER ATLAS GMM 3.19.1</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 109,482 hrs · 17,361 cycles

DURING ELECTRICAL POWER ON WITH EXTERNAL POWER AND SUPPLY THE UTILITY BUS FAIL(<P>FIM TASK 24-51 FAULT TREE 804 WAS PERFORMED AND TEST PASSED IAW AMM 24-51-05-864-014 REV 139 DATE 22-APR-2023. SATISFACTORY TEST</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 109,482 hrs · 17,361 cycles

DURING MEASURING OF THE ELECTRICAL BONDING RESISTANCE OF AC OVERRIDE PUMP LH, AC OVERRIDE PUMP RH AND APU DC FUEL PUMP ARE OUT OF LIMITS.(<P>MEASURE THE ELECTRICAL BONDING RESISTENCE OF AC OVERRIDE PUMP LH AND AC OVERRIDE PUMP RH AFTER IAW AMM 28-22-05-404-078-002 REV 139 APR 22 2023. PUMP RH 0.32 MILLIHOMS, PUMP LH 0.23 MILLIOHMS, BONDING METER S/N DC005829 - 19 DEC 23. MEASURE THE ELECTRICAL BONDING RESISTENCE OF APU DC FUEL PUMP 0.05 MILLIOHMS OK IAW AMM 28-25-01-404-029 REV 139 APR 22 202</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 109,482 hrs · 17,361 cycles

CENTRAL FUEL TANK WITH FOAM DEFORMED.(<P>FOAM CENTRAL FUEL TANK CAVITIES 3, 4 AND 125 WERE REPLACED IAW INVICTA-FRS INSTALLATION, B767 SERIES REV 1 01 JUN 18. PN: FF-00405-3079, FF-00405-3078, FF-00405-4012.</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 109,482 hrs · 17,361 cycles

CENTER SECTION TANK RH SIDE BETWEEN ROOT AND SPLICE STRINGER 6RH WITH FUEL LEAK(<P>CENTER TANK SEALANT WAS REPAIRED IAW AMM 28-11-00-308-013. OPS CHECK GOOD</P>)

Part: BOLT — UNKNOWN (UNKNOWN) · airframe 109,482 hrs · 17,361 cycles

DURING MEASURING OF THE ELECTRICAL BONDING RESISTAMCE OF AC OVERRIDE PUMP LH, AC OVERRIDE PUMP RH AND APU DC FUEL PUMP ARE OUT OF LIMITS.(<P>BOLTS AND O-RINGS WERE REPLACED AND MEASURED THE ELECTRICAL BONDING RESISTENCE OF AC OVERRIDE PUMP LH AND AC OVERRIDE PUMP RH AFTER IAW AMM 28-22-05-404-078-002 REV 139 APR 22 2023. PUMP</P> / <P>RH 0.32 MILLIHOMS, PUMP LH 0.23 MILLIOHMS, BONDING METER S/N DC005829 - 19DEC 23. MEASURE THE ELECTRICAL BONDING RESISTENCE OF APU DC FUEL PUM 0.05 MILLIOHMS OK IAW AMM 28-25-01-404-029 REV 139</P> / <P>APR 22 2023 BONDING METER S/N DC 005040 - 08NOV23</P>)

Part: NONE — NONE · airframe 109,136 hrs · 17,277 cycles

SEAT 12E HAS BURN HOLE FROM PASSENGER CELL PHONE.(<P>FOUND CONTAMINATED AREA TO BE LIMITED TO PASSENGER BAG AND CUSHION 12E. REMOVED SOILED ITEMS FROM A/C AND CLEANED AREA IAW AMM 05-51-15. NO FURTHER ACTION REQUIRED</P>)

Part: LIGHT — INOPERATIVE · airframe 108,992 hrs · 17,247 cycles

EMERGENCY LIGHT ON OUTSIDE RIGHT FUSELAGE OF WING INOP.(>RELAMPED LIGHT, OPS CHECK NORMAL I/A/W AMM 33-51-06)

Part: LIGHT — INOPERATIVE · airframe 108,992 hrs

EMERGENCY LIGHT ON OUTSIDE LEFT FUSELAGE AFT OF WING INOP(RELAMPED LIGHT OPS CHECK NORMAL I/A/W AMM 33-51-06)

Part: EXTINGUISHER — NONE · airframe 108,397 hrs

FIRE EXT. IN AFT GALLEY INOP MISSING PIN.(<P>REMOVED AND REPLACED FIRE EXTINGUISHER IN AFT GALLEY IAW AMM 26-26-00. OPS CHECKS GOOD.&NBSP;</P>)

Part: ROD — UNSERVICEABLE · airframe 108,284 hrs · 17,093 cycles

ENG # 2 O/B FAN COWL, AFT HOLD OPEN ROD DON'T RETRACT . REMOVED AND REPLACED # 2 ENG O/B CORE COWL HOLD OPEN ROD. OPS CHECK NORMAL IAW B767-300 AMM 71-11-11.

Part: O-RING — LEAKING · airframe 108,284 hrs · 17,093 cycles

FOUND PNEUMATIC LEAK AT PRVC AT PRVC ACTUATOR PRESSURE TUBE LOCATION "K" AS PER EO# 1936A088. REMOVED & REPLACED O' RING AT LOCATION "K". RECHECKED PER EO #1936A088. NO LEAK NOTED.

Part: HYDRAULIC LINE — CONTAMINATED · airframe 108,284 hrs · 17,093 cycles

ENG # 1 EVIDENCE OF HYDRAULIC LEAK O/B SIDE OF ENGINE CONTAMINATED WITH DRIED UP HYDRAULIC FLUID. CLEANED #1 ENG HYDRAULIC LEAK PER B767-300 AMM 12-25-01. PENDING LEAK CHECK. PERFORMED LEAK CHECK PER B767-300 AMM 71-00-00 FOR ENG #1 HYD SYSTEM AND AMM 24-11-00. NO LEAKS NOTE)

Part: DOOR — FAULTY · airframe 108,284 hrs · 17,093 cycles

OVER WING EMERGENCY EXIT DOORS CLOSE AND REACTIVATE LH & RH. AFTER INSPECTION COMPLETED. REINSTALLED BOTH LEFT & RIGHT OVER WING EXIT DOORS PER B767-300 AMM 52-21-01. PERFORMED OFF WING ESCAPE SYSTEM ON BOTH SIDES IAW B767-300 AMM 25-65-00. SQUIB TEST PASSED

Part: SLIDE RAFT — OUT OF POSITION · airframe 108,284 hrs · 17,093 cycles

RH O/WING OVHD BIN RAFT NOT SECURED WITH STRAPS RW 23. RESECURED RH OVERHEAD RAFT PER B767-300 AMM 25-62-00

Part: SEAT BELT — DAMAGED · airframe 108,284 hrs · 17,093 cycles

COCKPIT 2ND OBS SEAT BELTS LH & RH TSO TADS ILLEGIBLE & DAMAGE.REMOVED AND REPLACED OBS SEAT BELT PER B767-300 AMM 25-11-00. OPS CHECK; GOOD

Part: O-RING — LEAKING · airframe 108,284 hrs · 17,093 cycles

FOUND PNEUMATIC LEAK AT PRVC SENSE LINE LOCATION "E" AS PER EO #1936A088. REMOVED AND REPLACED O' RING AT LOCATION "E". RECHECKED PER EO# 1936A088. NO LEAKS NOTED.

Part: FUEL FILTER — INSTALLED · airframe 108,284 hrs · 17,093 cycles

LEFT & RIGHT ENGINE FUEL FILTERS REQUIRES REPLACEMENT AT APPROX. 150 FLT HOURS DUE TO FUEL TANK ENTRY TO BE REPLACE PRIOR TO 108387 FLT HOURS . REMOVED AND REPLACED #1 ENGINE FUEL FILTER PER 767 M/M 73-11-03-404-009-1100, REQUIRES LEAK CHECK. REMOVED & REPLACED #2 ENG FUEL FILTER PER B767-300 AMM 73-11-03. REQUIRED LEAKS CHECK. PERFORMED LEAK CHECK OF ENG 1 & 2 FUEL FILTERS PER B767-300 AMM 71-00-00, NO LEAKS

Part: FASTENER — MISSING · airframe 108,284 hrs · 17,093 cycles

ENGINE # 1 EXHAUST NOZZLE WEAR PAD AT THE 7 O' CLOCK POSITION MISSING FASTENER (1) .INSTALLED MISSING FASTENER AT ENGINE # 1 EXHAUST NOZZLE WEAR PAD AT THE 7 O' CLOCK POS AS PER B767-300 SRM 51-40-02-0G-0.)

Part: SEAL — MISSING · airframe 108,284 hrs · 17,093 cycles

BOTH RIGHT & FWD LEF OVER WING EMERGENCY EXIT DOOR CUT OUT SILLS MISSING CORNER SEALS . (INSTALLED CORNER SEALS IN BOTH LEFT & RIGHT OVERWING EMERGENCY EXIT DOORS PER B767-300 AMM 20-30-01

Part: CONNECTOR — LEAKING · airframe 108,284 hrs · 17,093 cycles

ENG # 2 EVIDENCE OF HYD LEAK IN PYLON CONNECTION. CLEANED AREA AS REQUIRED IAW B767-300 AMM 12-25-01. TIGHTENED #2 ENGINE PRESS LINE HYDRAULIC DRIVEN PUMP IAW B767-300 29-11-05. PENDING LEAK CHECK. PERFORMED LEAK CHECK PER B767-300 AMM 71-00-00 & 29-11-00. NO LEAKS NOTED.

Part: CLAMP — DAMAGED · airframe 108,284 hrs · 17,093 cycles

FWD, MID & AFT MEGAPHONE CLAMPS DAMAGE.(REMOVED AND REPLACED DAMAGED MEGAPHONE CLAMPS AT FWD, MID AND AFT MEGAPHONE AS PER 767-300 SRM 51-40-02-0G-0.</P>)

Part: SEALANT — DETERIORATED · airframe 108,284 hrs · 17,093 cycles

ALL FOUR ( 4 ) OVER WING EMERGENCY EXIT DOOR CUTOUT SEAL DEPRESSOR SURFACES HAVE CRACK .(<P>NO SEAL DEPRESSOR DAMAGED. FOUND SEALANT DETERIORATED. CLEANED AREA AND RESEALED ALL 4 OVER WING EMERGENCY EXIT DOOR CUTOUTS PER B767-300 AMM 20-30-01-992-001.</P>)

Part: SURGE VALVE — FAULTY · airframe 108,284 hrs · 17,093 cycles

APU BLEED VALVE INOP REMOVED AND REPLACED APU AIR SHUTOFF VALVE IAW B767 AMM 36-11-10. NO LEAKS FOUND PENDING OPS CHECK, OPS CHECK GOOD, BUT BLEED PRESSURE LOW. T/S PER FIM 49-11 FAULT TREE 979. FOUND SURGE CONTROL VALVE FAULTY. REMOVED & REPLACED APU SURGE CONTROL VALVE AS PER B767-300 AMM 49-53-01. NO LEAKS OPS CHECK GOOD</P>)

Part: SAFETY CLIP — DAMAGED · airframe 108,284 hrs · 17,093 cycles

LOWER FUSELAGE, BOTH SAFETY PINS TO DEACTIVATE CYLINDER OF OVER WING SLIDES WITH FLAGS MISSING / DAMAGE. REMOVED & REPLACED LWR& FUSELAGE INFLATION CYLINDER DEACTIVATION PINS PER B767-300 AMM& 25-65-02.

Part: COVER — BROKEN · airframe 108,284 hrs · 17,093 cycles

LEFT AFT OVER WING EMERGENCY EXIT DOOR COVER ASSEMBLY IS BROKEN. REMOVED AND REPLACED LH AFT EMERGENCY HATCH COVER PER 767 MM 52-21-02-402-001. OPS CHECK GOOD</P>)

Part: INERTIA REEL — UNSERVICEABLE · airframe 108,284 hrs · 17,093 cycles

COCKPIT F/O LH SEAT BELT TSO TAG ILLEGIBLE . REMOVED & REPLACED FO INERTIA REEL PER B767-300 AMM 25-11-04. OPS CHECK GOOD.

Part: DOOR — OPEN · airframe 108,284 hrs · 17,093 cycles

OVER WING EMERGENCY EXIT DOOR'S LH & RH DEACTIVATE AND OPEN DOORS FOR INSPECTION REQUIREMENTS .DISARMED THE L/H & R/H OFF WING ESCAPE SYSTEM, REF 767 M/M 25-65-00-042-001. REMOVED L/H & R/H OVERWING ESCAPE HATCHES (4EA) REF 767 M/M 52-21-01-002-201. REF NR 13 FOR CLOSING LH & RH OVERWING EXIT DOORS ARMING OF THE OFF-WING ESCAPE SYSTEM</P>)

Part: PRESSURE SENSOR — INOPERATIVE · airframe 108,284 hrs · 17,093 cycles

CENTER HYDRAULIC PRESSURE INDICATOR INOP. REMOVED AND REPLACED CENTER HYDRAULIC PRESSURE TRANSMITTER IAW AMM 29-31-01. OPS CHECK PASSED, SYSTEM OK AT THIS TIME.

Part: NONE — NONE · airframe 107,767 hrs

PASSENGER MASKS OBSERVED DEPLOYED ROW 8 SEATS H K(<P>INSPECTED AND CHECKED AND STOWED PASSENGER OXYGEN MASKS AT SEATS 8 H K AS PER AMM 35-21-05 AND OK FOR SERVICE.</P>)

Part: OVEN — FIRE (NR 7) · airframe 107,759 hrs

SMOKE AND SMALL FIRE IN OVEN #7 TRAYS APPEAR TO BE THE WRONG SIZE(<P><SPAN>FOUND OBSTRUCTION BEHIND #7 OVEN TRAYS. CLEANED OBSTRUCTION AND PERFORMED OPS CK PER CMM 25-36-34. OPS CK GOOD. C/W SMOKE IN CABIN INSPECTION REF AMM 05-51-56. NO DEFECTS NOTED.</SPAN></P>)

Part: BULB — NONE · airframe 107,670 hrs

CEILING EMERGENCY LIGHT AT SEAT 40H INOP.(<P><SPAN>RELAMPED IAW AMM 33-51-04 OPS CHECK GOOD.</SPAN></P>)

Part: NONE — NONE · airframe 107,664 hrs · 16,958 cycles

LH WING #5 INBD. SLAT CRACKED AT THE INBD. EDGE DUE TO CONTACT WITH #1 ENG. OBTD. THRUST REVERSER(<P>REPAIRED LH WING #5 INBD. SLAT INBD. EDGE PER BOEING MSG# EAC-TLS-21-0004 APPROVAL SOURCE FAA FORM 8100-9 DATED 20 OCT 2021 AND DWG 114T4105</P>)

Part: NONE — NONE · airframe 107,664 hrs · 16,958 cycles

DENT ON EXTERNAL UPPER SURFACE OF HORIZONTAL STAB CENTER SECTION BETWEEN RIB 1R AND 2R AT STA 1767(<P>REMOVED DAMAGE, INSTALLED REPAIR DOUBLER AND TRIPLER IAW BOEING MSG# EAC-TLS-21-0003, REFERENCE FAA FORM 8100-9, DATED OCT. 10, 2021.</P>)

Part: NONE — NONE · airframe 107,664 hrs · 16,958 cycles

BS 1329 FRAME AND WEB CUT BETWEEN S37L TO S39L FOR ACCESS TO S38L REPAIR ON PWO# HM499-20446.(<P>REPAIRED FRAME WEB AND FAIL-SAFE CHORD BS 1329 BETWEEN S37L TO S39L PER BOEING REPAIR SKETCH EAC-TLS-21-0002 AND FAA FORM 8100-9 DATED 18 NOV 2021.&NBSP;</P>)

Part: SHEAR TIE — NONE · airframe 107,664 hrs · 16,958 cycles

SHEAR TIE COMMON TO FRAME WEB AT BS 1329 STR 38L, INBD AND OTBD SHEAR TIES HAVE CORROSION.(<P>REMOVED AND REPLACED 2EA SHEAR TIES AT AFT CARGO PIT BS 1329, INBD AND OTBD OF STR 38L PER SRM 51-40-02-0G-0 PGS 2-3</P>)

Part: NONE — NONE · airframe 107,664 hrs · 16,958 cycles

S38L AND REPAIR SPLICES REQUIRED FOR REPAIR BETWEEN BS 1307 AND 1340 DUE TO CORROSION. REFERENCE ALSO PWO# HM499-20243, RAM N664GT-21-(<P>FABRICATED AND INSTALLED STRINGER SECTION AND REPAIR SPLICES AT S38L, BS 1307 TO 1340 PER B767-300 SRM 53-00-03-2R-2.</P>)

Part: NONE — NONE · airframe 107,664 hrs · 16,958 cycles

LH WING RIB 32 (WS 1018.2) DISCREPANT HOLES COMMON TO S10L, S9L AND S7L.(<P>REAMED DAMAGED FASTENER HOLES COMMON TO S10L, S9L AND S7L AND INSTALLED FREEZE PLUGS AND FASTENERS MESSAGE EAC-TLS-21-0005 AND FAA FORM 8100-9 DATED 21 NOV 2021.</P>)

Part: NONE — NONE · airframe 107,664 hrs · 16,958 cycles

STRINGER 38L CORRODED IN MULTIPLE SPOTS FROM BS 1219 TO 1351 AFT CARGO COMPARTMENT.(<P>REMOVED CORROSION FROM S38L, BS 1219 TO 1307 WITHIN LIMITS, BS 1329 TO 1351 OUT OF LIMITS PER B767-300 SRM 53-00-03-1A-1, FIG. 101. FABRICATED AND REPLACED STRINGER SECTION WITH 2 STRINGER SPLICES AS PER B767-300 SRM 53-00-03-2R-2 ON PWO# HM499-20446, RAM N664GT-21-10.</P> / <P>&NBSP;</P>)