N1229A

Part: TRANSDUCER — MALFUNCTIONED (ZONE 700) · airframe 82,983 hrs · 20,034 cycles

DURING TAKEOFF ANTI SKID EICAS MSG. AT 40 KNOTS, ABORTED TAKEOFF (ATO) AND RETURNED TO GATE (BTB) AND MTX GROUNDED A/C , PERFORMED FIM 32-423 FT 803 AND FOUND MESSAGE TRANSDUCER 6, UNABLE TO ERASE. R & R ANTISKID TRANSDUCER 6 IAW AMM 32-42-06. OP TESTED GOOD. NO MESSAGES IN VIEW. RETURNED AC TO SERVICE

Part: START VALVE — FAILED (LEFT) · airframe 82,268 hrs · 19,767 cycles

DURING TAXI OUT, LEFT ENGINE START VALVE FAILED TO OPEN. NO ROTATION, L ENG STARTER EICAS , VALVE LIGHT. AIRCRAFT RETURNED TO BLOCKS (BTB). MAINTENANCE DEFERRED IAW MEL C ABX-80-00-2-1. AIRCRAFT RETURNED TO SERVICE.

Part: GENERATOR — MALFUNCTIONED (LEFT) · airframe 80,965 hrs · 19,295 cycles

DURING TAXI AFTER STARTING LH ENG,GOT LEFT ENG. CONTROL AND LEFT GEN DRIVE DISSCONNECT LIGHT, A/C RETURNED TO GATE (BTB) AND MTX GROUNDED A/C ,MTX DEFERRED LH GEN IAW MEL ABX-24-00-1-1 .AND RETURNED A/C TO SERVICE.

Part: CONTROL PANEL — FAILED (ZONE 200) · airframe 80,653 hrs · 19,179 cycles

DURIING CRUISE BOTH FD BARS FAILED LATERAL GUIDANCE FD BAR APPEARED, BUT DID NOT GIVE PROPER GUIDANCE FROM MCP. AIRCRAFT DIVERTED TO SFO. MAINTENANCE GROUNDEDTHE AIRCRAFT. MAINTENANCE RPLEACED MODE CONTROL PANEL PER 767 AMM 22-11-02,, MCDP TEST 04 PASSED, AIRCRAFT RALM DOWNGRADED TO CATI PENDING MCDP 30/40 TEST. AIRCRAFT RETURNED TO SERVICE.

Part: TAT PROBE — FAILED (ZONE 100) · airframe 80,370 hrs · 19,074 cycles

CREW REPORTED EICAS MSG "TAT PROBE" INFO: NO A/T, NO L NAV, NO V NAV DURING CLIMB STAGE AND PERFORMED AN AIR TURNBACK. MTC GROUNDED THE AIRCRAFT , REMOVED AND REPLACED TAT PROBE IAW B767 AMM 34-12-02 OPS CHECK WAS GOOD. AIRCRAFT WAS RETURNED TO SERVICE.

Part: HYDRAULIC LINE — LEAKING (ZONE 700) · airframe 80,246 hrs · 19,026 cycles

DURING CRUISE, STARTED TO LOOSE CENTER HYD QTY , PILOT DECLARED EMERGENCY AND DIVERTED TO NEAREST AIRPORT( KMSY ) AND LANDED SAFELY. AC WAS .MTX GROUNDED AC AND BEGAN LOOKING FOR HYD LEAK PERFOMED TAIL SKID SYSTEM TEST PER AMM 32-71-00, DURING TEST AND GEAR HANDLE IN UP POSITION HYDRAULIC LEAK STARTING AT DRAINS JUST FWD OF PACK BAY DOORS. ISOLATED LEAK TO GEAR UP LINE AT APPROXIMATELY STA 785 JUST AFT OF THE FLC BELOW MDC FLOOR PANEL AT STA 785, FOUND B NUT LOOSE ON BOTH LINES FWD AND AFT OF UNION FITTING. TIGHTENED LINES PER AMM 20-10-09, REPERFORMED TAIL SKID OPS LEAK CK PER AMM 32-71-00, LEAK NO LONGER PRESENT, PERFORMED HYDRAULIC SYSTEM LEAK CK PER AMM 29-11-00, NO DEFECTS OR LEAKS FOUND. MTX RETURNED AC TO SERVICE REF LP 38622-98/1.

Part: FUEL CELL — LEAKING (RT WING) · airframe 80,222 hrs · 19,014 cycles

RH WING LOWER SURFACE, FUEL LEAK AT STRINGER 15R, BWTN WBL 97.95 AND 197.4(<P>RH WING LOWER SURFACE, FUEL LEAK AT STRINGER 15R, BWTN WBL 97.95 AND 197.4. FUEL LEAK WAS REPAIRED, IAW AMM 28-11-00-308-013 REV 142 22APR24. THE FUEL LEAK TEST SATISFACTORY.</P>)

Part: LANYARD — MISSING (FUEL CAP) · airframe 80,222 hrs · 19,014 cycles

LH WING, FIXED LEADING EDGE STRUCTURE AREA FUELING STATION (PANEL 521 QB) LANYARD OF CAP (COLOR RED) MISSING.(<P>THE LANYARD OF FUEL CAP ADAPTER WAS REPLACED IAW AMM 28-11-04-404-019 REV: 142 DATE: 22-APR-24</P>)

Part: DOOR — LEAKING (EMERGENCY EXIT) · airframe 80,222 hrs · 19,014 cycles

EXTERNAL FUSELAGE, LEAK ON LH EMERGENCY EXIT DOOR.(<P><SPAN>SEAL OF EXTERNAL FUSELAGE, LH </SPAN><SPAN>EMERGENCY EXIT DOOR WAS REPLACED IAW </SPAN><SPAN>AMM 52-09-06-404-003 REV 142, APR 22, 2024. </SPAN><SPAN>CHECK FOR LEAKS WAS PERFORMED, NO FOUND </SPAN><SPAN>LEAKS.</SPAN></P>)

Part: STIFFENER — CRACKED (BS 246) · airframe 80,222 hrs · 19,014 cycles

SECTION 41 FLOOR STRUCTURE, FLOOR BEAM B. STA 246 FWD FACE OF WEB WITH CRACK ON STIFFENER LBL 36.(<P>SECTION 41 FLOOR STRUCTURE, FLOOR BEAM B. STA 246 FWD FACE OF WEB WITH CRACK ON STIFFENER LBL 36 WAS FABRICATED IAW DRAWING 141T5170 AND ORDER M6753450 ISSUED DATE JUN 06, 2024.</P>)

Part: FLOOR PANEL — DAMAGED (FWD CARGO) · corrosion level 2 · airframe 80,222 hrs · 19,014 cycles

ZONE 100, LOWER HALF FUSELAGE, FORWARD CARGO COMPARTMENT FLOOR PANEL 124BXF CORROSION EVIDENCE ON UNDERFLOOR PLATE.(<P>ZONE 100, LOWER HALF FUSELAGE, FORWARD CARGO COMPARTMENT FLOOR PANEL 124BXF CORROSION EVIDENCE ON UNDERFLOOR PLATE WAS REPAIRED IAW SRM 53-00-53-1A-1 REV 125 15APR24 AND SRM 53-00-53-2R-2 REV 125 15APR24.</P>)

Part: FRAME — CRACKED (BS 456) · airframe 80,222 hrs · 19,014 cycles

CRACK INDICATION FOR PLUG PREVIOUSLY INSTALLED AT FRAME, STA 456 AND STGR 26L, SEE PICTURE.(<P>CRACK INDICATION FOR PLUG PREVIOUSLY INSTALLED AT FRAME, STA 456 AND STGR 26L, SEE PICTURE. WAS REPAIRED IAW TRE6753695 ISSUED DATE JUN 08/2024, FVCI CONTROL# 24088-1 REV. IR DATE 06/09/2024, FAA FORM 8110-3 DATE 06/17/2024. A NEW FAA FORM 8110-3 MUST ISSUED WITHIN 12 MONTHS FROM THE DATE OF THIS FORM FOR THIS REPAIR APPROVAL TO REMAIN VALID AFTER DATE TIME.</P>)

Part: FLOOR PANEL — DAMAGED (FWD CARGO) · airframe 80,222 hrs · 19,014 cycles

ZONE 100, LOWER HALF FUSELAGE, FORWARD CARGO COMPARTMENT FLOOR PANEL 124AXF, MISSING MATERIAL AFT RIGHT CORNER, CRACK ON RIGHT LATERAL EDGE (NEAR LOCK) AND MISSING MATERIAL FWD RIGHT CORNER(<P><SPAN>ZONE 100, LOWER HALF FUSELAGE, </SPAN><SPAN>FORWARD CARGO COMPARTMENT FLOOR </SPAN><SPAN>PANEL 124AXF, MISSING MATERIAL AFT RIGHT </SPAN><SPAN>CORNER, CRACK ON RIGHT LATERAL EDGE (NEAR </SPAN><SPAN>LOCK) AND MISSING MATERIAL FWD RIGHT</SPAN></P> / <P><SPAN>CORNER. DAMAGES WERE REPAIRED IAW </SPAN><SPAN>B767 SRM 53-00-53-2R-4 REV. 125 15-APR-2024.</SPAN></P>)

Part: ACCESS PANEL — DAMAGED (LT WING) · airframe 80,222 hrs · 19,014 cycles

LEFT WING, REAR SPAR, PANEL ACCESS 551UB, ABOVE MAIN LANDING GEAR RETRACT ACTUATOR, CLAMP OVER HYDRAULIC LINE DAMAGED(<P>LEFT WING, REAR SPAR, PANEL ACCESS 551UB, ABOVE MAIN LANDING GEAR RETRACT ACTUATOR, OVER HYDRAULIC LINE CLAMP WAS REPLACED IAW AMM 20-10-11-964-001 REV. 142 DATE 22 APR 24R24.</P>)

Part: HINGE — CRACKED (CARGO DOOR) · airframe 80,222 hrs · 19,014 cycles

EXTERNAL FUSELAGE, CRACK ON DOOR AND HINGE OF CARGO HANDLING PANNEL(<P>EXTERNAL FUSELAGE, CRACK ON DOOR AND HINGE OF CARGO HANDLING PANNEL. BROKEN HINGE IS REMOVED AND THE HINGE IS REPLACED WITH A NEW ONE IAW SRM 51-40-02-0G-0 REV 125 15APR24, SRM 51-10-02-0G-0 PAR9 REV 125 15APR25 &AMP; AMM 51-21-10-377-003 REV 142 22APR24.</P>)

Part: SUPPORT ANGLE — CORRODED (BS 1726) · corrosion level 2 · airframe 80,222 hrs · 19,014 cycles

AFT FUSELAGE SECTION 48, CORROSION ON INTERNAL SKIN, BSTA 1725.5, BETWEEN STRINGERS 7 RH AND 6 RH, BELOW APU INTAKE DOOR(<P>AFT FUSELAGE SECTION 48, BSTA 1725.5, BETWEEN STRINGERS 7 RH AND 6 RH, BELOW APU INTAKE DOOR SUPPORT ANGLE WAS REPLACED IAW SRM 51-10-02-0G-0 PARAGRAPH 9 REV 125 15-APR-24 DWG 148T3120 REV H AND MISCELLANEOUS CONSECUTIVE NUMBER M6753457 ISSUED DATE 13-JUN-24</P>)

Part: FLOOR PANEL — CRACKED (FWD CARGO) · airframe 80,222 hrs · 19,014 cycles

ZONE 100, LOWER HALF FUSELAGE, FORWARD CARGO COMPARTMENT FLOOR PANEL 123FXF, CRACK ON UNDERFLOOR SKIN PLATE.(<P>ZONE 100, LOWER HALF FUSELAGE, FORWARD CARGO COMPARTMENT FLOOR PANEL 123FXF, CRACK ON UNDERFLOOR SKIN PLATE.WAS PERFORMED REPAIRED IAW SRM 53-00-53-2R-4 REV 125 15APR24 AND SRM 53-</P> / <P>00-53-1A-1 AD1 REV 125 15APR24.</P>)

Part: SEAL — LEAKING (EMERGENCY EXIT) · airframe 80,222 hrs · 19,014 cycles

EXTERNAL FUSELAGE, LEAK ON RH EMERGENCY EXIT DOOR.(<P><SPAN>SEAL OF RH EMERGENCY EXIT DOOR </SPAN><SPAN>WAS REPLACED IAW AMM 52-09-06-404--</SPAN><SPAN>003 REV 142, APR 22, 2024; CHECK FOR LEAKS </SPAN><SPAN>WAS PERFORMED, NO LEAKS FOUND</SPAN></P>)

Part: STIFFENER — CRACKED (BS 246) · airframe 80,222 hrs · 19,014 cycles

SECTION 41 FLOOR STRUCTURE, FLOOR BEAM B. STA 246 REAR FACE OF WEB WITH CRACK ON STIFFENER LBL26.(<P><SPAN>SECTION 41 FLOOR STRUCTURE, </SPAN><SPAN>FLOOR BEAM B. STA 246 REAR FACE OF WEB </SPAN><SPAN>WITH CRACK ON STIFFENER LBL26. STIFFENER </SPAN><SPAN>WAS REPLACED IAW B767 SRM 51-10-02-</SPAN><SPAN>0G-0 REV. 125 15-APR-2024.</SPAN></P>)

Part: PANEL — UNKNOWN (MAIN CARGO) · airframe 80,222 hrs · 19,014 cycles

UPPER HALF FUSELAGE, MAIN DECK CARGO, CEILING PANELS FROM B.STA 800 TO B.STA 1400, SMOKE DETECTION SYSTEM, CEILING PANELS, OBSTRUCTED SEVERAL INTAKE ORIFICES, EVALUATION(<P>UPPER HALF FUSELAGE, MAIN DECK CARGO, CEILING PANELS FROM B.STA 800 TO B.STA 1400, SMOKE DETECTION SYSTEM CEILING PANELS, INTAKE ORIFICES AND HOSES WERE CLEANED AND REINSTALLED IAW AMM 26-19-01-400-801, REV 142, APR 22, 2024. TEST OF CARGO SMOKE DETECTION WAS PERFORMED, TEST OK.</P>)

Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 80,222 hrs · 19,014 cycles

LH WING, UPPER SURFACE SKIN BETWEEN WS.1046.2 AND WS.1075.2 SAFETY LINE ATTCH POINT WITH POINTS OF CORROSION.(<P>LH WING, UPPER SURFACE SKIN BETWEEN WS.1046.2 AND WS.1075.2 WAS REPAIRED IAW SRM 57-20-01-2R-7 FIG 201 SHEET 1 PAG 1-2 AND SRM 51-70-17-2R-4 REPAIR 4 FIG 201 SHEET 1 REV 125 APR 15/2024 LEVEL CORROSION 2</P>)

Part: DOOR — LEAKING (EMERGENCY EXIT) · airframe 80,222 hrs · 19,014 cycles

EXTERNAL FUSELAGE, LEAK ON LH EMERGENCY EXIT DOOR.(<P><SPAN>SEAL OF EXTERNAL FUSELAGE, LH </SPAN><SPAN>EMERGENCY EXIT DOOR WAS REPLACED IAW </SPAN><SPAN>AMM 52-09-06-404-003 REV 142, APR 22, 2024. </SPAN><SPAN>CHECK FOR LEAKS WAS PERFORMED, NO FOUND </SPAN><SPAN>LEAKS.</SPAN></P>)

Part: DOOR — PUNCTURED (FUEL DOOR) · airframe 80,222 hrs · 19,014 cycles

LH WING, FIXED LEADING EDGE STRUCTURE AREA INNER SIDE FUELING STATION DOOR WITH ONE PUNCTURED.(<P>LH WING, FIXED LEADING EDGE STRUCTURE AREA INNER SIDE FUELING STATION DOOR WAS REPAIRED IAW SRM 57-41-01-2R-1 FIG 201 SHEET 3 PAG 2-4 &AMP; SRM 51-70-17-0G-0 PAR 4B FIG 24 PAG 14,55 REV 125 APR 15/2024</P>)

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 80,222 hrs · 19,014 cycles

CABIN CREW ENTRY, LOWER PANEL LEFT SIDE, EMERGENCY SIGN LENS, BROKEN(<P>EMERGENCY SIGN LENS FROM CABIN CREW ENTRY WAS REPLACED IAW AMM 33-51-02-412-003 REV 142 DATE 22 APR 2024</P>)

Part: SKIN — CRACKED (RT NR 10 SLAT) · airframe 80,222 hrs · 19,014 cycles

RH WING, SLAT 10, CRACK ON UPPER AND LOWER SKIN OSS 723.94(<P>RH WING, SLAT 10, CRACK ON UPPER AND LOWER SKIN OSS 723.94. THE TEAR ON THE SKIN OF THE SLAT #10 WAS REPAIRED IAW 53-43-01-2R-2 REV 125 15APR24, AMM 30-11-06-404-009 REV 142 22APE24, AMM 27-81-02-424-099 REV 22APR24, SRM 51-40-02-0G-0 REV 15APR24 AND SRM 51-20-01-0G-0 REV 125 15APR24.</P>)

Part: STRINGER — DAMAGED (BS 456 S26L) · airframe 80,222 hrs · 19,014 cycles

SECTION 43, HIDDEN DAMAGE (NICK) IN STGR 26LH STA 456(<P>SECTION 43, HIDDEN DAMAGE (NICK) IN STGR 26LH STA 456. THE STRINGER SEGMEMT WAS REPLACED PER SRM 51-10-02-0G-0 PAR 9 REV 125 15APR24 AND SRM 51-40-02-0G-0 REV 125 15APR24.</P>)

Part: OXYGEN MASK — INOPERATIVE (CABIN) · airframe 79,787 hrs · 18,839 cycles

O2 MASK INOP SUPERNUMERARY, TRANSFERRED TO MDDR 204626 PER MEL 35-11-03-02A. O2 MASK FAILED TO TEST. FOUND STOWED INCORRECTLY. RESTOWED O2 MASK AT SUPERNUMARY SEAT CLOSEST TO LAV IAW AMM 35-11-51. OPS TEST GOOD IAW AMM 35-11-00. THIS CLEARS MDDR 204626, PLACARD REMOVED.

Part: BUTTON — STUCK (OXYGEN BOX) · airframe 79,769 hrs · 18,831 cycles

OBSERVER INTERCOM WILL NOT TRANSMIT USING HEADSET MIC.(<P>FOUND RESET TEST BUTTON STUCK ON OXYGEN MASK BOX. REMOVED AND REPLACED OBSERVER OXYGEN MASK BOX IAW AMM 35-11-51. PERFORMED HEADSET MIC OPS CHECK IAW AMM 23-51-00, OPS CHECK GOOD. NO DEFECTS NOTED AT THIS TIME. PART EFFECTIVE PER IPC 35-11-52-16.</P>)

Part: ELT — DAMAGED (CABIN) · airframe 79,681 hrs · 18,804 cycles

PORTABLE ELT BY L1 DOOR CORD IS RIPPED(<P>REMOVED AND REPLACED L1 DOOR POTABLE ELT IAW AMM 25-63-03. OPS CHK GOOD.</P>)

Part: ELT — DAMAGED (CABIN) · airframe 79,681 hrs · 18,804 cycles

PORTABLE ELT BY L1 DOOR CORD RIPPED..(<P>REMOVED AND REPLACED L1 DOOR PORTABLE ELT IAW AMM 25-63-03. NO FURTHER DEFECTS NOTED</P>)

Part: ALTIMETER — MALFUNCTIONED (CAPTAIN'S) · airframe 79,569 hrs · 18,756 cycles

CAPT ALTIMETER MOMENTARILY WENT A FEW THOUSAND FEET LOW THEN RAPIDLY RECOVERED PASSING FL 340 IN CLIMB AND DESCENT. VSI ANOMALY NOTED AS WELL(<P>PERFORMED OPS TEST OF AIR DATA COMPUTING SYS, OPS TEST GOOD IAW AMM 34-12-00, NO DEFECTS NOTED.</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 79,454 hrs · 18,711 cycles

DEMO ESCAPE HARNESS ASSY BAG OPEN AND FOUND UNSERVICEABLE(<P>TRANSFER TO MDDR 200998 PER DDG 25-20-01 CAT E 120 DAYS DUE 13MAY2024. LP 1716038 M4: REMOVED AND REPLACED ESCAPE HARNESS DEMO BAG IAW AMM 25-60-00. NO FURTHER DEFECTS NOTED. THIS CLEARS DMI 200998. MCC NOTIFIED. PLACARDS REMOVED</P>)

Part: RELIEF VALVE — OUT OF LIMITS (SURGE TANK) · airframe 77,151 hrs · 17,911 cycles

SURGE TANK PRESSURE RELIEF VALVE R, OUT OF LIMITS IAW TASK A-28-004-00-02(<P>SURGE TANK PRESSURE RELIEF VALVE R, WAS REPLACED PER AMM 28-13-04-002-002 REQUIREMENTS</P>)

Part: SKIN — CRACKED (LT NACELLE) · airframe 77,151 hrs · 17,911 cycles

CRACK ON LH STRUT OUTBD SKIN PANEL BETWEEN NAC STA 221.25 / NAC / STA 237.5 (CUTOUT FOR ACCESS PANEL 432AL).(<P>REPAIR WAS ACCOMPLISHED PER BOEING SR# 3-5510858364.</P>)

Part: PCA — LEAKING (ELEVATOR) · airframe 77,151 hrs · 17,911 cycles

ELEVATOR PCA LOCATED IN THE RH HORIZONTAL STABILIZER ACCESS PANEL 345GB WITH EVIDENCE OF HYDRAULIC LEAK. ELEVATOR PCA WAS REPLACED PER AMM REQUIREMENTS PER AMM 27-31-00.

Part: SKIN — DAMAGED (BS 232 S30L) · airframe 77,151 hrs · 17,911 cycles

LH FUSELAGE SKIN AT STA 232.5 AND 4" BELOW STGR 30 LH DAMAGED. REPAIRED IN ACCORDANCE WITH SRM 53-00-01-2R-8</P>)

Part: FUEL TANK — LEAKING (CENTER) · airframe 77,151 hrs · 17,911 cycles

LH FUEL LEAK AT CENTER TANK BETWEEN STGR L-10 AND LBL 75 / LBL 97(<P>LH FUEL LEAK AT CENTER TANK BETWEEN STGR L-10 AND LBL 75 / LBL97 WAS REPAIRED PER AMM 28-11-00-308-057 REQUIREMENTS</P>)

Part: SKIN — DAMAGED (BS 1647 S34L) · airframe 77,151 hrs · 17,911 cycles

LIGHTNING STRIKE ON LH FUSELAGE SKIN AT STA 1647.5 AND 3.5" BELOW STGR 34 LH.(<P>LIGHTNING STRIKE WAS REPAIRED IN ACCORDANCE WITH SRM 53-00-01-2R-8</P>)

Part: SUPPORT FITTING — CRACKED (NR 1 NACELLE) · airframe 77,151 hrs · 17,911 cycles

CRACK IN BASE OF OUTBOARD LUG, FITTING AT NAC STA 204.50 ON UPPER SPAR OF PYLON ENG. 1.(<P>REPLACEMENT OF FAN COWL SUPPORT BEAN FITTING OF LH ENG/STRUT WAS ACCOMPLISHED PER BOEING IN SERVICE ACTIVITIES 97-04-5456-00 (767) AND MXA EO TRE6754166</P>)

Part: SKIN — CORRODED (BS 654 S30L) · airframe 77,151 hrs · 17,911 cycles

BULGE ON LH FUSELAGE SKIN AT STA 654+57.5 AND 3" ABOVE STGR 30 LH.(<P>DAMAGE WAS REPAIRED PER SRM 53-00-01-2R-6 GUIDELINES</P>)

Part: HOSE — BROKEN (SMOKE DETECTOR) · airframe 77,151 hrs · 17,911 cycles

FUSELAGE INTERNAL AREA, STA808 TO STA999, WITH 4 BROKEN HOSES IN THE SMOKE DETECTION SYSTEM, UPPER FUSELAGE.(<P>THE 4 HOSES FROM SMOKE DETECTION SYSTEM WERE REPLACED PER AMM 26-10-00 REQUIREMENTS.</P>)

Part: FUEL TANK — LEAKING (CENTER) · airframe 77,151 hrs · 17,911 cycles

LH FUEL LEAK AT CENTER TANK BETWEEN STGR L-10 AND LBL 14(<P>LH FUEL LEAK AT CENTER TANK BETWEEN STGR L-10 AND LBL 14 WAS REPAIRED PER AMM 28-11-00-308-057 REQUIREMENTS</P>)

Part: ACTUATOR — LEAKING (STAB TRIM SYS) · airframe 77,151 hrs · 17,911 cycles

SECONDARY BRAKE FOR RH STABILIZER TRIM SYSTEM WAS FOUND WITH EVIDENCE OF HYDRAULIC LEAK. BRAKE ASSY - STAB TRIM ACTUATOR WAS REPLACED PER AMM 27-41-13-024-001

Part: HOSE — BROKEN (SMOKE DETECTOR) · airframe 77,151 hrs · 17,911 cycles

FUSELAGE INTERNAL AREA, STA478 TO STA654.22, WITH 3 BROKEN HOSES IN THE SMOKE DETECTION SYSTEM, UPPER FUSELAGE.(<P>THE 3 HOSES FROM SMOKE DETECTION SYSTEM WERE REPLACED PER AMM 26-10-00 REQUIREMENTS.</P>)

Part: FUEL TANK — LEAKING (CENTER) · airframe 77,151 hrs · 17,911 cycles

RH FUEL LEAK AT CENTER TANK BETWEEN STGR L-10 AND RBL 97(<P>RH FUEL LEAK AT CENTER TANK BETWEEN STGR L-10 AND RBL97 WAS REPAIRED PER AMM 28-11-00-308-057 REQUIREMENTS</P>)

Part: FUEL TANK — LEAKING (CENTER) · airframe 77,151 hrs · 17,911 cycles

RIGHT FUEL LEAK AT CENTER TANK BETWEEN STRINGER L6 AND RBL 97. FUEL LEAK REPAIRED IAW AMM 28-11-00-308-057.

Part: ACTUATOR — LEAKING (ELEVATOR CONTROL) · airframe 77,151 hrs · 17,911 cycles

INTERNAL ACCESS DOOR 313AL -- ELEVATOR CONTROL SYSTEM FEEL ACTUATOR WITH EVIDENCE OF HIDRAULYC LEAK(<P>ELEVATOR CONTROL SYSTEM FEEL ACTUATOR WAS REPLACED PER AMM 27-31-17-024-001 REQUIREMENTS</P>)

Part: RELIEF VALVE — FAULTED (SURGE TANK) · airframe 77,151 hrs · 17,911 cycles

SURGE TANK PRESSURE RELIEF VALVE FOR THE LT SIDE WAS FOUND OUT OF LIMITS PER TASK A-28-004-00-01. SURGE TANK PRESSURE RELIEF VALVE FOR THE LT SIDE WAS REPLACED PER AMM REQUIREMENTS. AMM 28-13-04-002-002.

Part: RELIEF VALVE — LEAKING (STAB TRIM) · airframe 77,151 hrs · 17,911 cycles

STABILIZER TRIM RELIEF VALVE HAD EVIDENCE OF A HYDRAULIC LEAK. LOCATED IN SECTION 48 AT BS 1725. THE RELIEF VALVE WAS REPLACED IAW AMM 27-41-19.

Part: VIEW PORT — CRACKED (FWD CARGO DOOR) · airframe 77,151 hrs · 17,911 cycles

CRACKS ON ALL VIEW PORTS LOCATED IN LOWER SURFACE OF FWD CARGO DOOR. VIEW PORTS WERE REPLACED IAW CMM 52-34-41.

Part: WINDOW — CRACKED (AFT PAX DOOR) · airframe 77,151 hrs · 17,911 cycles

FOUND A CRACK ON THE WINDOW OF AFT ENTRY DOOR. REPLACED THE WINDOW OF AFT ENTRY DOOR. AMM 56-31-01-004-001.

Part: HOSE — BROKEN (SMOKE DETECTOR) · airframe 77,151 hrs · 17,911 cycles

FUSELAGE INTERNAL AREA, STA1065 TO STA1540, WITH 9 BROKEN HOSES IN / THE SMOKE DETECTION SYSTEM, UPPER FUSELAGE.(<P>THE 9 HOSES FROM SMOKE DETECTION SYSTEM WERE REPLACED PER AMM 26-16-05-200-802-002 REQUIREMENTS.</P>)

Part: CONTROL MODULE — LEAKING (STAB TRIM) · airframe 77,151 hrs · 17,911 cycles

SECTION 48, AT STA 1725, STABILIZER TRIM CONTROL MODULE, LH SIDE WITH / EVIDENCE OF HYDRAULIC LEAK.(<P>STABILIZER TRIM CONTROL MODULE WAS REPLACED PER AMM 27-41-05 REQUIREMENTS.</P>)

Part: SEAL — LEAKING (PRESS BLKHD) · airframe 77,151 hrs · 17,911 cycles

SECTION48, PRESSURE DOME, CONTROL CABLES E1B AND E1A, AIR PRESSURE SEALS WITH EVIDENCE OF AIR LEAK(<P><SPAN DIR="LTR" ROLE="PRESENTATION">SECTION48, PRESSURE DOME, CO-</SPAN><SPAN DIR="LTR" ROLE="PRESENTATION">NTROL CABLES E1B AND E1A, AIR PRESSURE </SPAN><SPAN DIR="LTR" ROLE="PRESENTATION">SEALS WERE SEALED PER AMM 20-10-04-404-014</SPAN></P>)

Part: SEAL — DAMAGED (RT ACCESS PANEL) · airframe 77,151 hrs · 17,911 cycles

SEVERAL ACCESS FUEL PANELS FROM RH WING WITH DAMAGED RUBBER SEALS. DAMAGED RUBBER SEALS WERE REPLACED PER AMM 28-11-01-404-005 REQUIREMENTS.

Part: LIGHT — INOPERATIVE · airframe 76,544 hrs

FOUND FLIGHT DECK CEILING LEFT EMERGENCY LIGHT INOP(<P>RELAMPED, OPS CHECK NORMAL I/A/W AMM 33-51-00&NBSP;</P>)

Part: SLAT — DELAMINATED · airframe 76,449 hrs · 17,684 cycles

#1 SLTAT HAS DISBONDED METAL ON THE OUTBD END TOP SIDE(<P>THE PART HAS BEEN INSPECTED AND REPAIRED IAW APPROVED TECHNICAL DATA, WITH DUAL RELEASE CERTIFICATE, FAA8130-3 AND EASA AND TECHNICAL DATA SRM 51-70-10-2R-1 REPAIR 1 REV 120 DATE 15AUG22</P>)

Part: DOOR — CORRODED · airframe 76,449 hrs · 17,684 cycles

FWD LWR CARGO FWD RH BALL MAT FWD LATERAL LOCK HOUSING CORRODED(<P>REMOVED AND REPLACED FWD LATERAL LOCK HOUSING IAW SRM 51-40-05 &AMP; SRM 51-40-02</P>)

Part: BAND — BROKEN · airframe 76,074 hrs · 17,534 cycles

FLASH BAND ON ENTRY DOOR FLASHLIGHT ASSEMBLY BROKEN. REMOVED AND REPLACED PLASTIC BAND ON ENTRY DOOR FLASHLIGHT ASSEMBLY AMM 25-64-00</P>)

Part: MASK — NONE · airframe 75,585 hrs

FOUND L/H SUPERNUMERARY PARTIAL FACE OXYGEN MASK LEAKING.(<P>REMOVED AND REPLACED L/H SUPERNUMERARY PARTIAL FACE OXYGEN MASK ASSY IAW AMM 35-11-51. OPS CHECK GOOD.</P>)

Part: NONE — NONE · airframe 75,156 hrs · 17,179 cycles

APU DROPPED OFF LINE TWICE PRIOR TO BLOCK OUT(<P>TRANSFERRED TO MDDR 156768 IAW MEL 49-11-01A,&NBSP;<SPAN>CAT C&NBSP; DUE DATE 24NOV21. </SPAN></P> / <P><SPAN>APU ECU INDICATES " GEN FILTER" AS CAUSE FOR SHUT DOWN&NBSP;</SPAN></P> / <P>16NOV21 - LOG 1429853 - ITEM #10 - CVG - REMOVED AND REPLACED APU OIL FILTER DIFFERENTIAL PRESS SWITCH IAW AMM 49-27-15. OPS CKS AND LK&NBSP; CKS GOOD THIS CLEARS MDDR 1429853.</P>)

Part: NONE — NONE

LEFT WXR FAIL ILLUMINATED ON EHSI(<P>TRANSFERRED TO DMI # 156673 PER MEL 34-43-01 CAT D DUE DATE 12 MAR 22.</P> / <P>13NOV21 - LP 1476572 - ITEM #5 - ONT - PERF OPERATIONAL TEST WXR RADAR,&NBSP; L TRANSCEIVER FAILED. PER AMM 34-43-01 R/R L RADAR TRANSCEIVER PER AMM 34-43-01. OPS CHECK GOOD. NO FAULTS NOTED, THIS CLEARS DMI 156673.&NBSP;</P>)

Part: NONE — NONE

LEFT WEATHER SYSTEM FAIL.(<P>C/W OPS CHECK OF WXR SYSTEM OPS CHECK GOOD IAW AMM 34-43-00.</P>)

Part: NONE — NONE

APU INOP ( AUXILIARY POWER UNIT (APU), ER OPERATIONS NOT ALLOWED (NOTIFY DISPATCH) R60(<P>TRANSFERRED TO DMI 156541 MEL 49-11-01A CAT C&NBSP;</P> / <P>12NOV21 - LP 1476572 - ITEM #4 - ONT - PERFORMED APU BITE IAW FIM 49-11 FAULT TREE 987. LIGHT TEST FAULTED WITH LAMPS AND FAULTED GEN FILTER. REMOVED AND REPLACED APU ECU IAW AMM 49-61-05. OPS CHECK GOOD, NO FAULTS NOTED. THIS CLEARS MDDR 156541, PLACARDS REMOVED.&NBSP;</P>)

Part: NONE — NONE · 17,162 cycles

APU FAILED TWICE PRIOR TO AND DURING ENGINE START APU FAULT LIGHT ILLUM BOTH TIMES.(<P>TRANSFER TO MDDR 156494, DUE DATE 19NOV21, CAT C, PER DDG 49-11-01.</P> / <P>REF LOG 1362074 ITEM 6: FOUND WIRE W198226-22 TERMINATED TO PIN 24 ON CONNECTOR D5822J. MOVED WIRE TO PIN 27 ON D5822J. CHKD CONTINUITY BETWEEN D7 ON D4088 AN D1 ON D10268, CHECK GOOD. ALSO C/ W AP- 20593 REV D. PERFORMED APU SYS CK WITH ENGS AND APU IN MES MODE DURING STARTS IAW WDM 80-11-11 AND 80-11-21. THIS CLEARS MDDR 156494.</P>)

Part: NONE — NONE

APU BLEED INOP ( APU BLEED VALVE ) MX PROCEDURES FOLLOWED.(<P>TRANSFERRED TO MEL 36-11-04, MDDR 156131, CAT 'C'.</P> / <P>REF LOG 1362074 ITEM 6 AND LOG 1362077 ITEM 15: MOVED WIRE @24 TO POSITION 27 AND CONTINUITY AT D10266 TO D10268. ALL CKS GOOD. OPS CKS GOOD. THIS CLEARS MDDR 156131.</P>)

Part: MODULE — NONE · airframe 75,055 hrs · 17,139 cycles

CARGO A/C CONT EICAS MSG.(<P>T/S TO LEFT PACK ISSUE. TRANSFERRED TO MDDR # 155875, CAT C, DUE 07NOV21 IAW DDG 21-51-01-01, MX ACTION COMPLETE.&NBSP;</P> / <P>LOG PAGE 1134817: REMOVED AND REPLACE AIR SUPPLY BITE MODULE IAW AMM 36-23-01 OPS NORMAL THIS CLEARS MDDR 155875. PACK SYS TEST GOOD IAW AMM 21-51-00.</P>)

Part: NONE — NONE · airframe 75,053 hrs

APU AUTO SHUTDOWN(<P>TRANSFERRED TO DMI 155788 PER DDG 49-11-01A. CAT C DUE 06NOV21.</P> / <P>28OCT21 - LP 1424509 -&NBSP; T/S PER B767 FIM 49-11 FT 987 "APU BITE PROCEDURE". FOUND MINIFLAG #17 AND "FILTER SW" MESSAGE. CLEARED ECU AND PERFORMED VISUAL OF APU GEN DIFFERENTIAL PRESSURE INDICATOR REF B767 AMM 49-27-03. FOUND DIFFERENTIAL PRESSURE INDICATOR IN NORMAL POSITION. FOUND LOOSE CONNECTOR ON GEN FILTER SWITCH. RESECURED CONNECTOR ON GEN FILTER PRESSURE SWITCH AND OPERATED APU FOR ONE HOUR REF B767 AMM 49-11-00. APU OPERATED NORMAL AT THIS TIME WITH NO FAULTS. PERFORMED APU BITE PROCEDURE AFTER SHUTDOWN AND NO FAULTS/MESSAGES PRESENT. THIS CLEARS MDDR 155788, PLACARDS REMOVED.</P>)

Part: APU — WARNING MESSAGE

APU FAULT ON EICAS PERFORMED APU RUN NO FAULTS FOUND IAW B767 AMM 49-11-00.

Part: WARNING MESSAGE — FALSE INDICATION (CABIN PRESSURE)

CABIN ALT MASTER WARNING IN FLIGHT AT FL350.(<P>PERF FIM 21-31 FT 803 BOTH AUTO 1 &AMP; AUTO 2 SYSTEM OK. #2 NO DEFECTS NOTED IAW AMM 21-31-00, PERF CABIN PRESSURE LEAKAGE TEST PER AMM 05-51-24. NO DEFECTS LEAKS NOTED.</P>)

Part: MOTOR — FAULTED (APU STARTER) · 17,049 cycles

APU RELIABILITY COLD START ON FLT LEG RFD-SCK SAT -56C FL400: 3 START ATTEMPTS, ALL UNSUCCESSFUL.(<P>REMOVED AND REPLACED APU STARTER MOTOR IAW B767-300 AMM 49-41-01. OPS CHECK NO FAULTS AT THIS TIME</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (LT A/C PACK TEMP) · airframe 74,742 hrs

L PACK TEMP MSG(<P>TRANSFERRED TO MEL 21-51-01-01 MDDR 153165 CAT C DUE DATE 17SEP21.</P> / <P>CVG MX,&NBSP; 08SEP: LP 1440808, ITEM M4: PERF L/H TEMP CONTROLLER BITE IAW FIM 21-51-00. NO FAULTS FOUND. PERF OPS TEST OF PACKS IAW AMM 21-51-00, L/H PACK FULL COLD FOR 1 HOUR THEN TESTED BOTH PACKS FULL COLD IN "AUTO" &AMP; STBY FOR 10 MIN EACH. NO FAULTSW/MSGS NOTED. THIS CLEARS DMI 153165. PLACARDS RMVD. T.I.-JL @ 1658Z</P>)

Part: FILTER — FAULTED (SCAVANGE SYSTEM)

APU INOP ( AUXILIARY POWER UNIT (APU), ER OPERATIONS NOT ALLOWED (NOTIFY DISPATCH) R60 )(<P>REPLACE LUBE GEN SCAVAGE FILTER IAW AMM 49-27-03. APU START ON FIRST TIME. THIS CLEARS THIS DMI 152620.&NBSP; MCC NOTIFIED.</P>)

Part: RADAR — FAILED (WX SYSTEM)

L SYS "WXR RADAR FAIL" AMBER MSG ON LH MAP DISPLAY - UNABLE TO PAINT WX RETURNS. R SYS OK(<P>PERFORMED WXR BITE PROCEDURE IN ACCORDANCE WITH FIM 34-43 FT 805. SYSTEM OK</P>)

Part: FAN — FAULTED (FWD EQUP EXHST)

FWD EQPT EXH FAN STATUS MSG(<P>ITEM #1 - PERFORMED FIM 21-58 FT 905. REMOVED AND REPLACED C ECS FAN CONTROL CARD IAW AMM 21-65-04. NO HELP ISSUE REMAINS. SEE LP 1382436 FOR CONTINUATION. S/N OFF - D02125 P/N OFF - 285T0078-15.</P> / <P>23AUG21 - LP 1382436 - ITEM# 4 - CVG - REMOVED AND REPLACED FWD EQUIP COOLING EXHAUST FAN RELAY K345 IAW AMM 21-58-15. NO HELP, ISSUE REMAINS, SEE ITEM 5 FOR CONTINUED MTC ACTION. S/N OFF - 05920. P/N OFF - 10-61445-21.</P> / <P>LP&NBSP;1382436 M5: TRANSFERRED TO DMI 152376 IAW DDG 21-58-04-02-01. CAT C, DUE 02SEP21.</P> / <P>LP&NBSP;1382442: REMOVED AND REPLACED FWD EQUIPMENT EXHAUST FAN IAW AMM 21-58-06. OPS CHECKS GOOD. THIS CLEARS MDDR 152376. PLACARDS REMOVED. MCC NOTIFIED. NO OTHER MSG NOTED.</P>)

Part: SMOKE DETECTOR — FALSE ACTIVATION (CARGO BAY)

STATUS MSG CARGO DET AIR. PERFORMED FIM 26-16 FT 814. SYSTEM OPS NORMAL.

Part: WARNING MESSAGE — FALSE ACTIVATION (APU) · airframe 74,623 hrs · 16,998 cycles

AFTER BLOCK IN EICAS MSG "APU FAULT". PERFORMED APU OPS TEST IAW B767 AMM 49-11-00/201. OPS NORMAL.

Part: PUMP — INOPERATIVE (FUEL SYSTEM)

RH CENTER FUEL PUMP INOP(<P>TRANSFERRED TO MDDR&NBSP;<SPAN>150252</SPAN><SPAN> IAW MEL 28-22-02A, CAT C.</SPAN></P> / <P>LOG PAGE 1453782 ITEM 4 - REMOVED AND REPLACED CENTER RT FUEL PUMP IAW 28-22-05. OPERATIONAL TEST GOOD NO FAULTS - AMM 28-22-05. THIS CLEARS MDDR 150252. ALL PLACARDS REMOVED.</P>)

Part: PRESSURE SWITCH — FAULTED (ANTI ICE SYSTEM)

R ENG TAI VALVE STATUS MESSAGE(<P>TRANSFERRED TO MDDR 150187 IAW MEL 30-21-01-04-02, CAT C.</P> / <P>LP 1453769: REMOVED AND REPLACED ENG. INLET TAI PRESSURE SWITCH IAW AMM 30-21-01. OPERATIONAL CHECK OK. NO EICAS MSG. A/C OK TO RELEASE. THIS CLEARS MDDR 150187.</P>)

Part: INDICATION SYS — FALSE INDICATION (ENG VIBRATION) · airframe 74,340 hrs

INDICATION ON RIGHT ENG FAN VIBRATION FLUCTUATING BETWEEN 1.0 &LT; 3.5 ON CLIMB OUT FOR A FEW MINS. NO ABNORMAL VIBRATION NOTED/ FELT.(<P>TRANSFERRED TO MDDR 149953 PER MEL 77-31-01-01, CAT "C", DUE DATE: 20JUL21. DISP: LC @ 17:25Z.</P> / <P>CVG MX, 13JUL, LP 1453765, ITEM M7: PER AMM 77-31-01, PER MCC REQUEST SWAP #1 BERING ACCELEROMETER TO ALT EXTERNAL ACC. PER FIM 77-31 FT 803. THIS CLEARS DMI 149953. PLACARD REMOVED. INI DP @ 17:05.</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (WX RADAR SYS) · airframe 74,292 hrs · 16,893 cycles

WXR SYS STATUS MESSAGE IN FLIGHT(<P>PERFORMED WEATHER RADAR OPERATIONAL CHECK PER AMM 34-43-00. NO FAULTS NOTED.</P>)

Part: WARNING MESSAGE — FALSE INDICATION (WX RADAR) · airframe 74,254 hrs · 16,882 cycles

STATUS MESSAGE WXR SYS DISPLAYED IN FLIGHT.(<P>PERF FIM 34-43 FT 805, NO FAULTS NOTED. FERF OPS TEST IAW AMM 34-43-00. OPS TEST GOOD. NO FEFECTS OR STATUS MSGS NOTED AT THIS TIME</P>)

Part: STATUS MESSAGE — FALSE ACTIVATION (WX RADAR SYS) · airframe 74,254 hrs

ITEM #1 STATUS MESSAGE WXR SYS DISPLAYED IN FLIGHT.(<P>PERF FIM 34-43 FT 805, NO FAULTS NOTED. PERF OPS TEST IAW AMM 34-43-00, OPS TEST GOOD, NO DEFECTS OR STATUS MSGS NOTED AT THIS TIME.</P>)

Part: UFI — FAULTED (RT FUEL PUMP) · airframe 74,100 hrs · 16,823 cycles

CTR R FUEL PUMP INOP(<P>TRANSFERRED TO MDDR 146974 IAW MEL 28-22-02A, CAT, C DUE 24MAY21.&NBSP;</P><P>LP 1465297: REMOVED AND REPLACED UFI PER AMM 28-31-90-404-001 AND 28-31-90-004-001. OPS CKS GOOD PER AMM 28-31-90-041. THIS CLEARS MDDR 146974. MCC NOTIFIED. PLACARDS REMOVED.</P>)

Part: TRANSCEIVER — MALFUNCTIONED (HF COMMS) · airframe 73,980 hrs · 16,784 cycles

BOTH HFS WILL NOT RECEIVE, ALSO NO SELCAL(<P>OPS CHECKED BOTH HF SYSTEMS IAW AMM 23-11-00. BOTH SIDES CAN XMIT BUT NOT RECIEVE. PERFORMED FIM TASK 23-11 FT TO SHEET 1 BLOCK 23. FOUND CONTROL INPUT FAIL LIGHT AT LH TRANSCEIVER. PER TABLE 101 IN FIM SUGGEST REPLACING RADIO COMMUNICATION PANEL. FURTHER TROUBLESHOOTING REQ, PART ON ORDER WITH MCC.&NBSP;</P>)

Part: PUMP — FAILED (FUEL SYS) · airframe 73,980 hrs · 16,784 cycles

RIGHT CENTER PUMP FAIL(<P>TRANSFERRED TO MDDR # 145831 PER MEL 28-22-02, EXP 04MAY21 CAT C. MCC NOTIFIED. PLACARDS INSTALLED. DISP. JL @ 2159Z</P><P>27APR21 - LP 1465506 ITEM 8 - ONT - PERFORMED OPERATIONAL CHECK OF PUMP AND UFI IAW AMM 28-31-90. THIS CLEARS MDDR 145831. TJ 1520</P>)

Part: OXYGEN MASK — MALFUNCTIONED (CAPTAIN'S) · airframe 73,842 hrs · 16,743 cycles

CAPT O2 MASK NEEDS TO BE REPLACED. EXTREMELY HARD TO BREATH WHEN CHECKED. O2 NOT FLOWING THRU PROPERLY(<P>REMOVED AND REPLACED CAPT 02 MASK IAW AMM 35-11-51. OPS CHECK GOOD, VERIFIED OXYGEN FLOW NORMAL.</P>)

Part: STARTER — MALFUNCTIONED (APU) · airframe 73,850 hrs · 16,745 cycles

APU FAULT EICAS MSG COMPIED WITH QRH 2ND AND 3RD START ATTEMPTS WERE UNSUCCESSFUL(<P>TRANSFERRED TO MDDR 1449.31 MEL 49-11-01A&NBSP;</P><P><SPAN>REMOVED AND REPLACED APU STARTER MOTOR. IAW AMM 49-41-01. PERFORMED 3 SUCCESSFUL APU STARTS. OPS CHECK NORMAL. NO DEFECTS NOTED. THIS CLEAR MDDR #144931. PLACARDS REMOVED.</SPAN></P><P><SPAN>JT@0244Z</SPAN></P>)

Part: PRESSURE SWITCH — MALFUNCTIONED (LT ENGINE) · airframe 73,632 hrs · 16,682 cycles

DURING PRE-FLIGHT CHECKLIST FOUND LH ENG PRESSURE WARNING LIGHT NOT EMITTING.(<P>REMOVED AND REPLACED LH ENG LOW OIL PRESSURE WARNING SWITCH IAW AMM 79-33-01. OPS CHECK GOOD. LIGHT EMITTS.</P>)

Part: SEAL — EXPOSED (NR 1 INLET PROBE) · airframe 73,602 hrs · 16,674 cycles

#1 ENGINE INLET PROBE SEAL EXPOSED (TRIMMED). TRIMMED #1 ENGINE INLET COWL SEAL IAW SRM 51-00-00 AND GMM 3.2.39. OPS CHECK GOOD AT THIS TIME AND PLACED ON NON MEL. REF GMM 3.2.39 AND 3.2.40. DATE 3 MAR 21- LP 1312700 ITEM 5 - SCK - ITEM TO BE REPLACED WITHIN 10 FC REF AMM 72-22-00-212-001-H00 FOR FINAL REPAIR. DMI 143236 TO REMAIN OPEN 9 FC REMAIN UNTIL FINAL REPAIR FOR THE NON MEL.

Part: RADAR — MALFUNCTIONED (WX SYSTEM) · airframe 73,390 hrs · 16,613 cycles

RADAR FAILED TO PAINT THUNDERSTORM, ALTHOUGH WE HAD VISUAL CONTACT WITH THE WX AS WE WERE FLYING OVER IT.(<P>PERF L AND R WXR RADAR OPERATIONAL TEST IAW AMM 34-43-00. BOTH SYSTEM ARE NORMAL. NO FAULTS IN VIEW.</P>)

Part: OXYGEN MASK — INOPERATIVE (1ST OBSERVER'S) · airframe 73,403 hrs · 16,618 cycles

1ST OBSERVER O2 MASK INOP(<P>TRANSFERRED TO MDDR 141972 IAW MEL 25-11-02-01A, CAT A.</P><P>06FEB21 - LP1316197 ITEM 6 - ONT - REMOVED AND REPLACED O2 MASK IAW AMM 35-11-51. OPS CHECK GOOD, NO FURTHER DEFECTS, DMI 141972 CLOSED.<BR /></P>)

Part: CONTROLLER — FAULT MESSAGE (CABIN) · airframe 73,354 hrs · 16,605 cycles

CABIN ALT AUTO 2 STATUS MSG. PERFORMED CABIN PRESSURE CONTROLLER BITE PROCEDURE IAW FIM 21-31-FT 803. NO FAULTS FOUND OPS NORMAL.

Part: CARD — WARNING MESSAGE (RT ENGINE SPEED) · airframe 73,330 hrs · 16,594 cycles

RT ENGINE SPEED CARD MESSAGE. PERFORMED ENG SPEED CARD TEST, PER FIM 73-21 FAULT TREE 871. OPERATIONS CHECK GOOD. PERFORMED ENGINE RUN ON NR 2 ENGINE, PER AMM 71-00-00-862-053-H03. OPERATIONS CHECK GOOD. VERIFIED NO FAULTS WERE FOUND DURING OPERATIONS CHECKS.

Part: SENSOR — FAILED (RT ENG N2 SPEED) · airframe 73,339 hrs · 16,599 cycles

RIGHT ENGINE SPEED CARD STS MSG. R & R RT ENGINE N2 SPEED CARD OFF PN 285T0458-303, SN D04761. OPS CHECK NORMAL IAW AMM 73-21-54. MSG CLEARED. 28JAN21 LOG PG 1271503 ITM 5 MIA; R & R RIGHT ENGINE N2 SPEED SENSOR. OPS CHECK NORMAL IAW AMM 77-12-02. PERFORMED ENGINE RUN IAW AMM 77-12-02. PERFORMED ENGINE RUN UP. OPS CHECK NORMAL. NO DEFECTS OR FAULTS NOTED IAW AMM 71-00-00.

Part: CARD — FAILED (SPEED IND SYSTEM) · airframe 73,328 hrs · 16,593 cycles

PROBE HEAT AFTER ENGINE START. PERFORMED FIM 30-31-FT-807. FOUND SPEED CARD BAD. REMOVED AND REPLACED SPEED CARD, IAW M/M 73-21-54. OPERATIONS CHECK GOOD.

Part: EEC — FAULT MESSAGE (COCKPIT) · airframe 73,328 hrs · 16,593 cycles

RT ENGINE EEC MSG AFTER START. RESET EEC (RT). OPERATIONS CHECK GOOD, IAW 71-00-00.

Part: MASK — LEAKING (COCKPIT) · airframe 73,324 hrs · 16,592 cycles

F/O MASK OXYGEN FOUND LEAKING. REMOVED AND REPLACED F/O MASK OXYGEN, IAW AMM 35-11-51. PERFORMED OXYGEN MASK MICROPHONE TEST, IAW AMM 35-11-01. OPERATIONS CHECK GOOD.

Part: LINE — LEAKING (RT ENG OIL SUMP) · airframe 73,324 hrs · 16,592 cycles

UPON ARRIVAL, RIGHT ENGINE OIL QUANTITY LOW. PERFORMED HI-POWER ENGINE RUN LEAK CHECK, PER MCC REQUEST IAW 767 AMM. TWO LEAKS NOTED ON D-SUMP SUPPLY LINE. REMOVED, INSPECTED, AND CLEANED SCAVENGE INLET SCREEN ASSEMBLYS, LUBE FILTER, AND MAGNETIC ISOLATOR PLUGS. NO SIGNIFICANT CONTAMINATION NOTED, REF AMM 79-21-06-002-002-H00. SERVICED RIGHT ENGINE OIL, IAW AMM 13-13-01. PERFORMED ENGINE IDLE RUN 10 MINUTES, IAW AMM 71-00-00. ALL INDICATIONS NORMAL. NO LEAKS NOTED. AFTER RE-TORQUING OF D-SUMP SUPPLY LINE AND HI-POWER RUN-UP.

Part: RADAR — UNKNOWN (WX SYSTEM) · airframe 73,165 hrs · 16,542 cycles

L WX RADAR FAIL. C/W WX RADAR OPERATIONS TEST, IAW AMM 34-43-00. OPERATIONS CHECK GOOD AT THIS TIME. NO FAULTS FOUND.

Part: CHARGER — UNKNOWN (APU) · airframe 73,140 hrs · 16,534 cycles

APU BATT CHARGER STATUS MESSAGE. R & R APU BATT CHARGER, PER AMM 24-31-05. OPERATIONS NORMAL AT THIS TIME, REF LP 1352703 ITEM 7 FOR APU COLD SOAK DMI.

Part: ACCELEROMETER — MALFUNCTIONED (ENGINES) · airframe 73,007 hrs · 16,492 cycles

DURING CLIMBOUT LPT VIB WAS ERRATIC, POINTER MOVED BETWEEN 0 AND 5.0 FOR APPROX ONE MINUTE. NO VIBRATION WAS FELT IN FLIGHT DECK VIBRATION IN CRUISE FAN 0.6 N2 0.9. ACCOMPLISHED ENGINE RUN OF BOTH ENGINES AND NO VIBRATIONS NOTED, REF AMM 71-00-00. OKAY FOR RETURN TO SERVICE. TRANSFERRED TO MDDR 138787, IAW MEL 77-31-01-01, CAT C. REMOVED & REPLACED NR 1 ENGINE CRF ACCELEROMETER & N2 (CORE) ENGINE VIB HARNESS, IAW AMM 77-31-02. PERFORMED NR 1 ENGINE RUN, PER AMM 71-00-00. OPERATIONS CHECK NORMAL AT THIS TIME.

Part: RELAY — MALFUNCTIONED (FUEL PUMP) · airframe 72,757 hrs · 16,410 cycles

RT CENTER FUEL PUMP EICAS AFTER PUSHBACK. TRANSFERRED TO MDDR 136873, IAW DDG 28-22-02A. CAT C DUE 07NOV20. VERIFIED RT BOOST PUMP INSTALLED IS 5006286F. PER FIM 28-22 FI 805 RT CENTER FUEL PUMP CB C370 IN CLOSED POSITION. VERIFIED RT GFI RELAY K10696 NOT OPEN. FOUND 28VDC AT RELAY K330 TERMINAL X1. FOUND 115V POWER ON CON. D2804 PINS 2, 4, 6. PLACED RT CENTER OVR PUMP ON ORDER WITH MCC P/N 5006286F. DMI REMAINS OPEN. REMOVED AND REPLACED CENTER FUEL PUMP, IAW AMM 28-22-05, NO HELP. RT CENTER FUEL PUMP INTERMINENT WILL WORK SOMETIMES. CHECKED RELAY K330 PIN X2, PER FIM 28-22 FI 805. FOUND NO 28 VDC AT TERMINAL X2. SUSPECT BAD K330 RELAY P/N MS27418-2B. PLACED ON ORDER WITH MCC. DMI REMAINS OPEN. P/N OFF 5006286F. S/N OFF 2757. REMOVED AND REPLACED K330 RELAY, IAW SWPM 20-81-22 (P/N MS27418-2B). OPERATIONS CHECK GOOD OF THE RT CENTER AUX PUMP, IAW AMM 28-22-00. THIS CLEARS DMI 136873. PLACARDS REMOVED.

Part: LOCK BOLT — OUT OF POSITION (PRIORITY VALVE) · airframe 72,751 hrs · 16,408 cycles

LT ENGINE BLEED OFF EICAS MESSAGE. COMPLETED QRH CHECK LIST. ICING ENGINE EICAS MESSAGE, RAN QRH CHECK LIST. FOUND PRV LOCKOUT BOLT TO BE OUT OF POSITION. RE-INSTALLED AND TORQUED. RAN ENGINE AND PERFORMED OPERATIONS CHECK. OPERATIONS CHECK GOOD. BLEED VALVE AND INDICATION GOOD AT THIS TIME. NO FURTHER DEFECTS NOTED, REF B767 AMM 36-11-18, 71-00-00 & 20-00-00. PERFORMED OPERATIONS CHECK OF ENGINE ANTI-ICING DURING ENGINE RUN, NO DEFECTS NOTED AT THIS TIME, REF THIS LP ITEM 1 AND B767 AMM 31-21-00.

Part: WARNING MESSAGE — FALSE ACTIVATION (FUEL PUMP) · airframe 72,636 hrs · 16,375 cycles

CENTER RT FUEL PUMP EICAS MESSAGE CENTER TANK FUEL PUMPS, ONE INOPERATIVE, CENTER TANK FUEL USED. NOTIFY DISPATCH. TRANSFERRED TO MDDR 136097, IAW MEL 28-22-02A, CAT C 10/17/2020. REVERSED DDG, PERFORM FIM 28-22 TASK 805, NO FAULTS NOTED AND SYSTEM TESTED GOOD, IAW AMM 28-22-00. THIS CLEARS MDDR 136097, PLACARD REMOVED, MCC NOTIFIED. (TI: LC 1552Z)

Part: O-RING — DAMAGED (NR 2 ENGINE) · airframe 75,598 hrs · 16,362 cycles

#2 ENGINE HAS OIL LEAK FROM HORIZONTAL DRIVE SHAFT. OIL LEAK IS WITH IN ALLOWABLE LIMITS. REF AMM TASK: 72-63-02-226-001-H00. ITEM TRANSFERRED TO NON-MEL NR 135433 FOR TRACKING PURPOSES AND PLANNED FURTHER ACTION. CVG STA, 13OCT20 LP 1250999, ITEM M8: SEE NR 69803-NR-00007 FOR CORRECTIVE ACTION. REMOVED HORIZONTAL DRIVE SHAFT COVER AND FOUND O RING CUT. REPLACED FWD AND AFT O RINGS IAW B767 AMM 72-63-01. WORK ACCOMPLISHED ON GE WORK ORDER 22043. LEAK CHECK GOOD.

Part: VALVE — MALFUNCTIONED (EQUIP COOLING) · airframe 72,571 hrs · 16,354 cycles

FWD EQUIP VALVE EICAS. TRANSFERRED TO DMI NR 135231, IAW MEL 21-58-07-02-01 CAT "C" DUE DATE 10OCT20. PLACARD INSTALLED. DEACTIVATED USING PROCEDURE NR 1. DISPATCH SP 00.13Z 30SEP20, CVG. VERIFIED VALVE TO BE FAULTING. REMOVED & REPLACED FWD EQUIPMENT VALVE. OPERATIONS CK GOOD, REF B767 AMM 21-58-05. THIS CLEARS DMI 135231. PLACARDS REMOVED. MCC NOTIFIED. DISPATCH EH @ 1740Z.

Part: RELAY — FAILED (ENG ANTI ICE) · airframe 72,571 hrs · 16,354 cycles

RT ENG ANTI-ICE DISCRETE LIGHT DOES NOT ILLUMINATE "VALVE" WHILE IN TRANSIT. "TAI" DOES ILLUMINATE ON EICAS. TRANSFER TO MDDR 135223, CAT C, PER DDG 30-21-02-01A DUE 09OCT20. MX ACTION COMPLIED WITH, PLACARD INSTALLED. 2219Z SP. REMOVED AND REPLACED RELAY K2108 RIGHT ENGINE AUTO DISAGREE RELAY, IAW AMM 30-21-11, OPERATIONS CHECK OK. THIS CLEARS MDDR 135223.

Part: WARNING MESSAGE — FALSE ACTIVATION · airframe 72,563 hrs · 16,350 cycles

FWD EQUIPMENT VALVE EICAS, QRH COMPLETED. RAN FIM 21-48 TASK, NO FAULTS NOTED AT THIS TIME.

Part: DUCT — DAMAGED (APU SURGE) · airframe 72,563 hrs · 16,350 cycles

APU SURGE DUCT HAS HOLE IN IT. REMOVED AND REPLACED APU DUCT, IAW B767 AMM 20-11-01. PERFORMED OPERATIONS CHECK, IAW AMM 49-11-00. OPERATIONS CHECK GOOD.

Part: WARNING MESSAGE — FALSE ACTIVATION · airframe 72,545 hrs · 16,344 cycles

"FWD EQUIPMENT VALVE" EICAS. PERFORMED OPERATIONS CHECK, IAW AMM 21-58-00. OPERATIONS CHECK GOOD. FIM TASK 21-58 TASK 805 STATES SHORT TERM POWER INTERRUPTIONS LIKE THE ONES THAT OCCUR DURING A POWER TRANSFER (GROUND-APU, APU-ENGINE, APU-GROUND ETC) CAN CAUSE THE EICAS MESSAGE, FWD EQUIPMENT VALVE TO SHOW AND VALVE LIGHT TO COME ON. NORMAL OPERATIONS.

Part: WARNING MESSAGE — FALSE ACTIVATION (ICE DETECTION) · airframe 72,549 hrs · 16,346 cycles

LT ICE DETECTOR EICAS MESSAGE. T/S PER FIM 30-81FT 805, SYSTEM OK, NO MESSAGE AT THIS AT TIME.

Part: DISPLAY — FAILED (EICAS) · airframe 72,511 hrs · 16,334 cycles

EICAS WARNING ON CLIMBOUT. "EICAS DISPLAY", LOWER EICAS DISPLAY FAILED ON CLIMBOUT. INTERMITTENT BLANKING 3X ON DESCENT AND RETURN TO STATION. REMOVED AND REPLACED LOWER EICAS DISPLAY UNIT. OPS CHECK OK, REF MM TASK 31-41-01-404-001 AND 31-41-01-404-002, 31-41-00-715-001. EQUIP COOLING OPS CHECK 21-58-00-710-806-015 FIM 31-90-12-00.

Part: WARNING MESSAGE — FALSE ACTIVATION · airframe 72,484 hrs · 16,324 cycles

FWD EQUIPMENT VALVE EICAS MSG. A/C RELEASED ON MEL 21-58-01-01, MDDR 134712, CAT 'C'.< : MIX MANIFOLD VALVE PREVIOUSLY CHANGED. PERFORMED OPS CHECK IAW AMM 21-58-00. NO FAULTS NOTED. PERFORMED ENGINE RUN OF BOTH ENGINES IAW AMM 71-00-00 AND CONFIRMED VALVE WAS IN COMMAND POSITION PER MEL 21-58-00.

Part: INDICATOR — MALFUNCTIONED (ENGINE) · airframe 72,502 hrs · 16,331 cycles

STANDBY ENGINE INDICATOR INOP. SYSTEM BITE GOOD, PER AMM 77-41-00. NO OTHER FAULTS, OPS CHECK GOOD.

Part: WARNING MESSAGE — FALSE ACTIVATION (FWD EQUIPMENT) · airframe 72,471 hrs · 16,319 cycles

EICAS FWD EQUIPMENT VAL AFTER PUSHBACK 2ND ENG START, COMPLIED WITH QRH FLOW CHART THAT LED TO CONTINUED NORMAL OPS. PERFORMED OPS CHECK, REF AMM 21-58 TASK 849. OPS CHECK GOOD.

Part: STATUS MESSAGE — FALSE ACTIVATION (EXHAUST FAN) · airframe 72,429 hrs · 16,306 cycles

AFT EQ EXH FAN 2 STATUS MSG. PERFORMED FIM 21-26 F/T 808 TO BOX 1, MSG CLEARED. NO FAULTS NOTED. OPS NORMAL AT THIS TIME.

Part: TRU — FAILED (APU) · airframe 72,429 hrs · 16,306 cycles

APU TRU INOP (APU TRU DEACTIVATED) TRANSF TO MDDR NR 134359 CAT "D" PER DDG 24-32-01B DUE 11 JAN 21. PLACARD INSTALLED, MX ACTION COMPLIED WITH DP 1315Z). R & R APU TRU, AS PER AMM 24-32-00. PERFORMED OPERATIONAL CHECK OF APU TRU START, PER AMM 24-32-04 AND FOUND OK. THIS CLEARS DMI NR 134359, PLACARDS REMOVED, MCC ADVICED T, ZH AT 2040Z.

Part: WARNING MESSAGE — FALSE ACTIVATION (RT WINDOW) · airframe 72,429 hrs · 16,306 cycles

RIGHT FWD WINDOW EICAS MESSAGE DISPLAYED LIGHT ILLUMINATED. PERFORMED RT FWD WINDOW BITE TEST, IAW AMM 30-41-00, NO FAULTS NOTED. PERFORMED OPS CHECK IAW AMM, OPS CHECK NORMAL. NO FAULT MSGS NOTED, NO INOP LIGHT ILLUMINATED, NO CUT WIRES ON RT FWD WINDOW HEAT HARNESS.

Part: APU — MALFUNCTIONED · airframe 72,406 hrs · 16,299 cycles

APU WILL NOT START, 3 ATTEMPTS MADE. TRANSFERRED TO MDDR 134284 IAW MEL 49-11-01A, CAT C. DUE DATE 22 SEP 20. PERF FIM 49-11 FT 991, BLOCK 11, FOUND 115 VAC AT TRU START RELAY PINS A2,B2, AND C2. APU TRU NEEDS TO BE REPLACED (P/N 28VS200Y-4B-2). CONFIRMED APU TRU AT FAULT, APU OPS CHECKED GOOD WITH TRU DEACTIVATED. THIS CLEARS MDDR 134284. PLACARD REMOVED. TRU PLACED ON MDDR 134359.

Part: CHARGER — INOPERATIVE (APU) · airframe 72,429 hrs · 16,306 cycles

AUXILIARY POWER UNIT INOPERABLE, ER OPERATIONS NOT ALLOWED (NOTIFY DISPATCH) R60. TRANSFERRED TO MDDR 134217 IAW MEL 49-11-01A, CAT C. REMOVED AND REPLACED APU BATTERY CHARGER, IAW B767 AMM 24-31-05. OPS CHECK GOOD, THIS CLEARS MDDR 134217. MCC EDGAR NOTIFIED. ALL PLACARDS REMOVED.

Part: ACOUSTIC PANEL — DAMAGED (ENGINE) · airframe 72,429 hrs · 16,306 cycles

AS PER AMM 72-00-00-206-167-H00,TABLE 642, FIGURE 628 CONDITION: DAMAGED ACOUSTICAL PANELS AFT OF THE FAN BLADES, CONTINUE IN-OPERATION LIMIT 10 FLIGHT CYCLES OR 100 FLIGHT HOURS. OPENED NON-MEL 134014. APPLIED RTV SEALANT TO ACOUSTIC PANEL DAMAGE AT 4 O'CLOCK POSITION AFT OF FAN BLADES ON NR 2 ENG, IAW B767 AMM 72-33-01. THIS CLEARS NON MEL 134014, MCC EDGAR NOTIFIED. ALL PLACARDS REMOVED.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 72,375 hrs · 16,287 cycles

ENTRY WAY LOCATED EMERGENCY LIGHT IS OUT. REMOVED AND REPLACED ENTRY WAY DOME MOUNTED EMERGENCY LIGHT LAMP. OPERATIONS CHECKS GOOD IAW AMM 33-51-00.

Part: VALVE — MALFUNCTIONED (LT IDG) · airframe 72,219 hrs · 16,241 cycles

LT IDG VALVE STATUS. REMOVED AND REPLACED IDG AIR COOLING VALVE IAW AMM 24-11-07. GROUND RAN #1 ENG IAW AMM 71-00-00. OPS CHECK GOOD. NO FURTHER DEFECTS NOTED.

Part: FIRE LOOP — INTERMITTENT (LT ENGINE) · airframe 72,123 hrs · 16,213 cycles

LEFT ENGINE FIRE LOOP NR 1, EICAS MESSAGE INTERMITTENT.

Part: WIRE — DAMAGED (FIRE LOOP) · airframe 72,123 hrs · 16,213 cycles

LH ENGINE FIRE LOOP 1 EICAS MSG INTERMITTENT (ENGINE FIRE DETECTION SYSTEMS , DETECTION LOOPS. REPLACED WIRES W5324-452R-16 AND W5324-454R-16 IAW SPM 20-10-11 AND WDM 26-11-11. OPS CKS GOOD IAW AMM 26-11-00.

Part: MODULATING VALVE — INOPERATIVE (CABIN TEMP) · airframe 72,071 hrs · 16,197 cycles

AFT CABIN TEMP CONTROL INOPERATIVE, PERFORMED A ZONE TEMP CONTROL BITE IAW FIM 21-60, FT 804. FOUND AFT TRIM VALVE INOPERATIVE. REMOVED AND REPLACED THE TRIM AIR MODULATING VALVE AFT CABIN IAW AMM 21-61-07. CHECKEDD GOOD.

Part: ACCELEROMETER — MALFUNCTIONED (LT ENGINE) · airframe 72,045 hrs · 16,189 cycles

LEFT ENGINE VIB INDICATION INOPERATIVE. R & R THE NR 1 ENGINE ACCELEROMETER IAW 77-31-02, AND PERFORMED ENGINE RUNS IAW 71-00-00, OPS CHECKED GOOD.

Part: CLAMP — LOOSE (FIRE DETECTOR) · airframe 71,984 hrs · 16,172 cycles

LEFT ENGINE FIRE LOOP 1 INOPERATIVE. PERFORMED A FIRE LOOP RESISTANCE MEASUREMENT IAW FIM 26-11 FAULT TREE 804 TABLE B, RESISTANCE FOUND WITHIN THE RANGE AND NO MESSAGE IS SHOWN. MCC NOTIFIED. PERFORMED TROUBLESHOOTING OF THE ENGINE FIRE DETECTION LOOP, RESISTANCE CHECK IAW FIM 26-11 FT 804, VERIFIED FIRE LOOPS ARE WITHIN LIMITS, NOTICED THE FIREWALL LOOP HAD A LOOSE CLAMP. SECURED THE CLAMP IAW AMM 26-11-02. TIGHTENED CONNECTOR D4230A .

Part: FIRE LOOP — MALFUNCTIONED (LT ENGINE) · airframe 71,984 hrs · 16,172 cycles

LEFT ENG FIRE LOOP 1 INOPERATIVE. PERFORMED A FIRE LOOP RESISTANCE MEASUREMENT IAW FIM 26-11, FAULT TREE 804, TABLE B, RESISTANCE FOUND WITHIN THE RANGE AND NO MESSAGE IS SHOWN.

Part: STATUS MESSAGE — INTERMITTENT (LT ENGINE FIRE) · airframe 71,980 hrs · 16,170 cycles

INTERMITTENT LEFT ENGINE FIRE LOOP 1 STATUS MESSAGE, IAW FIM TASK 26-11-00-815-805. INSPECTED THE FIRE DETECTOR LOOP, FOUND OK. RESEATED DETECTOR CARD, INSPECTED THE BLEED DUCT COUPLING, COMPLETED FIRE TEST, PASSED. NO CURRENT MESSAGES.

Part: UNKNOWN — MALFUNCTIONED (APU) · airframe 71,951 hrs · 16,161 cycles

APU FAILED DURING PUSH BACK. PERFORMED APU TEST IAW AMM 49-11-00. NO FAULTS FOUND AT THIS TIME.

Part: BUSS — MALFUNCTIONED (ELECTRICAL SYS) · airframe 71,936 hrs · 16,157 cycles

UPON ARRIVAL IN THE FLIGHT DECK, FOUND BOTH CAPTAIN AND FO SIDE PFD FAILED, UPPER EICAS SCREEN WAS FAILED AS WELL. RESET APU BUS IAW AMM 24-21-00, OPS CHECKED NORMAL AT THE PRESENT TIME.

Part: WARNING MESSAGE — FALSE ACTIVATION (LT ENG FIRE LOOP) · airframe 71,915 hrs · 16,149 cycles

LEFT ENGINE FIRE LOOP 2 STATUS MESSAGE. PERFORMED MULTIPLE OPS TESTS OF ENG FIRE DETECTION SYS. OPS CHECK GOOD. NO MSG SHOWN AT THIS TIME IAW AMM 26-11-00.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 71,915 hrs · 16,149 cycles

RT IDG VALVE STATUS MESSAGE SHOWING. PERF VISUAL INSPECTION OF IDG, CHECKED IDG OIL LEVEL IAW 24-17-00, OIL LEVEL OK, NO DEFECTS/MSGS NOTED. PERF ENGINE; RUN (RT) IAW 71-00-00, OPS CHECK NORMAL AT THIS TIME.

Part: TRANSCEIVER — MALFUNCTIONED (WEATHER RADAR) · airframe 71,896 hrs · 16,142 cycles

LEFT WEATHER RADAR STUCK IN TEST MODE. REPLACED WXR TRANSCEIVER IAW AMM 34-43-01. OPS GOOD.

Part: FIRE DETECTOR — UNSECURE (ENGINE BAY) · airframe 71,886 hrs · 16,139 cycles

DURING PRE-FLIGHT, FOUND THE NR 1 FIRE LOOP NR 2 STATUS MESSAGE. PERFORMED INSPECTION FOR THE ENG NR 2 FIRE LOOP IAW FIM 26-11 FT 804. FOUND HARDWARE MISSING ON UPPER AFT ENGINE FIRE WALL FIRE DETECTOR, INSTALLED MISSING HARDWARE IAW AMM 26-11-02. OPS CHECKED GOOD.

Part: FIRE LOOP — MALFUNCTIONED (RT ENGINE) · airframe 71,884 hrs · 16,138 cycles

R/H ENG FIRE LOOP 2. REMOVED AND REPLACED LP PRINTER CIRCUIT CARD IAW AMM 26-11-02. NO HELP. REMOVED AND REPLACED THE NR 2 ENG DETECTOR ASSY FIRE LOWER AFT NR 2 FIRE LOOP IAW AMM 26-11-02, OPS TESTED OK.

Part: LINE — FAILED (BLEED SYS) · airframe 71,892 hrs · 16,141 cycles

LEFT ENGINE RUN CHECKS FOR BLEED AIR NOT SUCCESSFUL. FOUND FLEX LINE AND UNION TO LT ENG PRV BAD. REPLACED IAW MM 20-10-10, RAN ENG IAW MM PNEUMATIC SYSTEM TESTED GOOD.

Part: LINE — DEFECTIVE (BLEED AIR SYS) · airframe 71,872 hrs · 16,134 cycles

LT ENG BLEED OFF MSG ON DESCENT AT 14,000'. FOUND MUSCLE AIR LINE TO PRV BAD. REPLACED PER AMM 36-10-10. RAN ENG PER AMM 71-00-00. SYS TEST GOOD.

Part: SHUTOFF VALVE — MALFUNCTIONED (BLEED AIR SYS) · airframe 71,871 hrs · 16,133 cycles

LT ENG BLEED OFF MSG. REMOVED AND REPLACED LEFT ENG PRESSURE SHUTOFF VALVE IAW AMM 36-11-18. OPS CHECK GOOD. ALSO REMOVED AND REPLACED BLEED AIR SUPPLY CONTROL CARD OFF PART: PN285T1115-15D01676 IAW AMM 36-11-12. OPS CHECKS GOOD.

Part: CONNECTOR — DEFECTIVE (BLEED AIR SYS) · airframe 71,871 hrs · 16,133 cycles

AFTER PUSH BACK AND ENGINE START LT ENG BLEED EICAS, NO DUCT PRESSURE ON LEFT SIDE. TRANSFERRED TO MDDR 129269 PER MEL 36-11-01-02A, CAT 'C', DUE 14JUN20. C/W MX ACTION, PRSOV SECURED CLOSED AND FAMV OPEN. PLACARD INSTALLED. REMOVED AND REPLACED NR 1 ENG PRSOV CONNECTOR D22 IAW SWPM 20-30-10. THIS CLEARS DMI 129269.

Part: CONNECTOR — NOT SEATED (BLEED AIR SYS) · airframe 71,852 hrs · 16,128 cycles

LEFT ENG BLEED OFF. PERFORMED AIR SUPPLY BITE PROCEDURE IAW FIM 36-20 FT 804 "PRV", "PRVC" FAULT. RESEATED CONNECTOR OF PRVC IAW AMM 36-11-19. PERFORMED OPS CHECK, OPS CHECK GOOD.

Part: UNKNOWN — MALFUNCTIONED (WEATHER RADAR) · airframe 71,813 hrs · 16,115 cycles

WEATHER MAP RANGE DISAGREE ON ALL MAP RANGES WHILE LT RADAR IN USE. OPERATIONS CHECK OF LT WX RADAR IAW FIM 34-43-00-809. NO FAULT NOTED.

Part: WIRE — DAMAGED (FIRE LOOP) · airframe 71,774 hrs · 16,102 cycles

RIGHT ENGINE LOOP 2 INOPERATIVE. REPAIRED DAMAGED WIRE INSULATION AT LOWER FORWARD LOOP 2 AND TESTED IAW SWPM 20-10-13 AND AMM 26-11-00.

Part: OXYGEN MASK — WORN (COCKPIT) · airframe 71,691 hrs · 16,073 cycles

FO O2 MASK WORN(<P>REMOVED AND REPLACED FO O2 MASK PER AMM 35-11-51, OPS AND LEAK CHECK GOOD.</P>)

Part: CONTROLLER — FAULTY (COCKPIT TEMP) · airframe 71,613 hrs · 16,047 cycles

FLT DECK TEMP CAUTION MESSAGE AND INOP LIGHT.(<P>PERFORMED BITE OF ZONE TEMPERATURE CONTROLLER IAW AMM 21-61-03. FOUND CONTROLLER FAULT. REMOVED AND REPLACED ZONE TEMP CONTROLLER IAW AMM 2-61-03, OPS CHECK GOOD. NO FAULTS FOUND. OK FOR SERVICE.<BR /></P>)

Part: ACM — INOPERATIVE (RIGHT) · airframe 71,609 hrs · 16,045 cycles

RIGHT PACK INOPERATIVE. REMOVED AND REPLACED THE RT ACM IAW AMM 21-51-03. OPS CHECKED GOOD.

Part: SKIN — GOUGED (CARGO DOOR) · airframe 7,156,348 hrs · 16,029 cycles

FOUND FOUR GOUGES ON FORWARD CARGO DOOR LOWER AFT SKIN.(<P>CUT-OUT DAMAGE ON FWD CARGO DOOR LOWER AFT SKIN, FABRICATED REPAIR DOUBLER &AMP; FILLER &AMP; INSTALLED REPAIR ON FWD CARGO DOOR AFT LOWER SKIN IAW B767 SRM 52-30-01-2R-6 REPAIR 6. DIM. DOUBLER.160 2024-T3, 20"X6". FILLER 9" X 1" .125 2024-T3.</P>)

Part: SENSOR — DEFECTIVE (APU) · airframe 71,560 hrs · 16,027 cycles

APU PNEUMATIC SYS INOP (APU BLEED VALVE)(<P>TRANSFERED TO DMI 125811 IAW MEL 36-11-04 CAT "C", EXP 25 MAR 20. PLACARD INSTALLED.</P><P>LP 1120068 - M6: REMOVED AND REPLACED APU PT2 SENSOR IAW AMM 49-61-04. TEST OK. THIS CLEARS MDDR 125811.</P>)

Part: BLEED AIR SYS — MALFUNCTIONED (APU) · airframe 71,546 hrs · 16,020 cycles

PRIOR TO BLOCKOUT APU BLEED PRESSURE DROPPED TO 5 PSI. UNABLE TO CLEAR AFTER RE-STARTING APU (SAME ISSUE EXISTS).(<P>PERFORMED AUX POWER CONTROL UNIT BITE TEST IAW AMM 49-61-05. RESTART OF APU OPS NORMAL WITH 30PSI WITH PACKS RUNNING.</P>)

Part: CONTROLLER — MALFUNCTIONED (AC BAY) · airframe 71,515 hrs · 16,008 cycles

STATUS MSG CARGO A/C CONTROLLER.(<P>BIT L/H PACK TEMP CONTROLLER, IAW B767 AMM 21-51-00. OPS GOOD.<BR /></P>)

Part: SENSOR — FAULTY (APU) · airframe 71,484 hrs · 15,995 cycles

APU INOP (PNUEMATICS P2 FAULT)(<P>TRANSFERRED TO DMI #125395 IAW MEL 49-11-01A, CAT 'C', DUE 15MAR20.</P><P>LP 1178078: REPLACED APU INLET P2 SENSOR. OPS CHK GOOD. CLOSED MDDR IAW AMM 49-61-04.</P>)

Part: SMOKE DETECTOR — FALSE ACTIVATION (CARGO BAY) · airframe 71,442 hrs · 15,979 cycles

STATUS CARGO DET AIR.(<P>REMOVED AND REPLACED SMOKE DETECTOR IAW AMM 26-11-02. OPS CHECK OK.</P>)

Part: OIL SYSTEM — LOW (RT IDG) · airframe 71,388 hrs · 15,960 cycles

R IDG VALVE STATUS MSG.(<P>PERFORMED BPCU BITE TEST IAW AMM 24-11-00, FOUND IDG HIGH RISE TEMP MSG ON R GEN POWER SYSTEM. PERFORMED R IDG OIL SERVICING IAW AMM 12-13-03. OPS CHECK GOOD. NO STATUS MSG PRESENT. NO BPCU STATUS MSG PRESENT.</P>)

Part: TRU — MALFUNCTIONED (APU) · airframe 71,388 hrs · 15,960 cycles

EICAS MSG APU FAULT.(<P>TRANSFERRED TO MEL 49-11-01A, MDDR 124554 CAT C, DUE 21FEB20. DOWNGRADED TO ETOPS 60.&NBSP;</P><P>REF LOG PAGE 1187675 ITEM M5; REMOVED AND REPLACED TRU AS PER AM 24-32-01. OPS CHECK NORMAL, MDDR 124554 CLEARED.</P>)

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 71,252 hrs · 15,902 cycles

CARGO DET AIR STATUS MESSAGE(<P>PLACED ON MDDR 123225 PER MEL 26-14-01, CAT 'C'.&NBSP;<BR /></P><P>LP 1213489 -&NBSP;PERFORMED OPS CHECK OF CARGO SMOKE DETECT SYSTEM IAW B767 AMM 26-11-00. OPS CHK GOOD AT THIS TIME. THIS CLEARS MDDR 123225.</P>)

Part: CONTROLLER — MALFUNCTIONED (PRESS REGULATOR) · airframe 71,182 hrs · 15,879 cycles

RIGHT ENG BLD OFF WOULD NOT CYCLE ON - NO DUCT PRESS WITH APU BLEED OFF.(<P>REMOVED AND REPLACED #2 ENG PRESSURE REGULATING VALVE CONTROLLER IAW AMM 36-11-18. OPS CHECK AND LEAK CHECK GOOD.</P>)

Part: WIRE — DISCONNECTED (RT ENGINE BLEED) · airframe 71,182 hrs · 15,879 cycles

RIGHT ENGINE BLEED EICAS MESSAGE AFTER ENGINE START. ACCOMPLISHED AIR SUPPLY BITE PROCEDURES IAW FIM 36-26 FT 102B. FOUND FAULT TO LRU FAV. OPENED NR 2 ENG AND DISCOVERED LOSE WIRE CONNECTION ON CENTER TERMINAL. SECURED THE WIRE IAW AMM 36-11-16. RAN NR 2 ENG, OPS CHECKED NORMAL, NO FAULTS.

Part: PRESSURE SWITCH — FAILED (RT ENGINE TAI) · airframe 71,166 hrs · 15,873 cycles

R ENG TAI VALVE STATUS DISPLAYED. REMOVED AND REPLACED THE RT ENG TAI VALVE IAW AMM 30-21-03. OPS CHECKED NORMAL. REMOVED AND REPLACED THE PRESSURE SW IAW AMM 30-21-01. OPS CHECKED NORMAL.

Part: OXYGEN MASK — PULLED (COCKPIT) · airframe 71,165 hrs · 15,871 cycles

CAPTAIN'S OXYGEN MASK PULLED OUT. STOWED THE OXYGEN MASK IAW AMM 35-11-00. OPS CHECKED GOOD.

Part: DOOR — BROKEN (OXYGEN BOX) · airframe 70,943 hrs · 15,797 cycles

CENTER SUPERNUMERARY O2 STORAGE BOX LEFT DOOR IS BROKEN.(<P>SECURED FASTENERS AND RE-POSITIONED DOOR @ CENTER SUPERNUMERARY O2 MASK IAW AMM 35-21-05.<BR /></P>)

Part: MANIFOLD — DISCONNECTED (VACUUM SYS) · airframe 70,889 hrs · 15,776 cycles

IN CRUISE FLIGHT, CARGO DET AIR STATUS MESSAGE DISPLAYED.(<P>T/S USING FIM 26-16 FAULT TREE 813. REPLACED PRESSURE SWITCH S454 AND PROBLEM REMAINS. OFF PART (PN: 32V92, SN: NSN). RE-RAN FIM TO STEP 31. SUSPECT FAULTY BLOWER MOTOR M716. SEE ITEM M9 FOR DISCREPANCY IAW B767 AMM 26-16-02. BLOWER HAS 115V AT PIN 1 &AMP; 2&NBSP; WITH U35 C/B PULLED.<BR /></P><P>LP 1111641 - M9:&NBSP;REMOVED &AMP; REPLACED SMOKE DETECTOR BLOWER #1 FWD, OPS CHECK GOOD, MESSAGE CLEARED. OFF PART (PN: 033638, SN: A04563)</P><P>LP 1111643 - M14:&NBSP;PLACED CARGO DET AIR ON MEL 26-14-01, DMI 120576. (M) PROCEDURES C/W. INOP PLACARDS INSTALLED. NO OTHER DEFECTS NOTED AT THIS TIME.&NBSP;</P><P>LP 1111645 - ITEM 2:&NBSP;VERIFIED POWER AT BLOWERS 1&AMP;2&NBSP; (M718/M719) PER WDM 26-16-21. CHECKED PLUMBING FROM SMOKE EJECTOR VALVE. FOUND VACUUM MANIFOLD DISCONNECTED, RESECURED IAW AMM 26-19-04. SMOKE DETECTION SYSTEM OPS NORMAL. THIS CLEARS MDDR 120576. PLACARDS REMOVED.</P>)

Part: BLEED AIR SYS — UNKNOWN (APU) · airframe 70,860 hrs · 15,765 cycles

APU BLEED AIR LOW PRESSURE WITH BOTH PACKS ON.(<P>TRANSFERRED APU TO DMI 120377 IAW DDG 49-11-01A, CAT 'C', DUE: 19-NOV-19.</P><P>LP 1232397 - M5: ACCOMPLISHED B767 FIM 49-11 FAULT TREE A08, NO FAULTS NOTED. THIS CLEARS DMI 120377. PLACARDS REMOVED AND MCC NOTIFIED.</P>)

Part: UNKNOWN — MALFUNCTIONED (APU) · airframe 70,830 hrs · 15,752 cycles

APU AUTO SHUTDOWN PRIOR TO BLOCK OUT.(<P>PERFORMED BITE TEST ICU IAW AMM 49-11 FAULT 3 958, OPS TEST OK.<BR /></P>)

Part: MODULE — FAULTY (FLIGHT CONTROL) · airframe 70,824 hrs · 15,749 cycles

AFTER TAKEOFF, RUDDER RATIO/AILERON LOCKOUT EICAS.&NBSP;(<P>REMOVED AND REPLACED STAB/LOCK OUT MODULE, BOTH LEFT AND RIGHT. PERFORMED OPERATIONAL TEST, OPS CHECK GOOD. RUDDER RATIO EICAS, PERFORMED FIM TASK 27-21 FT 804, NO FAULT FOUND. RUDDER RATIO EICAS MESSAGE&NBSP;NOT DUPLICATED&NBSP;AT THIS TIME IAW AMM 27-21-23.&NBSP;</P><P><BR /></P><P>OFF PART (LEFT): PN:&NBSP;285T0015-116, SN:&NBSP;D00088&NBSP;</P>)

Part: BLEED AIR SYS — MALFUNCTIONED (APU) · airframe 70,824 hrs · 15,749 cycles

APU DOES NOT MAKE ADEQUATE PRESSURE FOR ENGINE START.&NBSP;&NBSP;(<P>PERFORMED POWERPLANT NORMAL OPERATION PROCEDURE PER AMM 71-00-00-862 AND FOUND NORMAL APU BLEED PRESSURE (30PSI) UPON ENGINE START. APU OPS TEST GOOD PER AMM 49-00-00.&NBSP;</P>)

Part: UNKNOWN — UNKNOWN (APU) · airframe 70,807 hrs · 15,742 cycles

APU DUCT PRESSURE VERY LOW WITH AIR DRAW.(<P>PERFORMED BITE OF APU IAW FIM 49-11 F/T 987, NO FAULTS NOTED. STARTED APU AND PUT LOAD ON IT IAW AMM 49-11-00, OPS CHECK NORMAL AT THIS TIME.</P>)

Part: COVER — CRACKED (EMERGENCY LIGHT) · airframe 70,766 hrs · 15,724 cycles

EMER LIGHTS GUARDED COVER CRACKED&NBSP;(<P>REPLACED LIGHT SWITCH GUARD IAW AMM 33-51-00 OPS CKS NORMAL</P>)

Part: UNKNOWN — ODOR (COCKPIT) · airframe 70,760 hrs · 15,722 cycles

DIRTY SOCK SMELL NOTICED IN THE COCKPIT. POSSIBLY TCP(<P>CHECKED A/C BAY PNEUMATIC DUCTS AND COMPONENTS FOR OIL CONTAMINATION .OPERATED BOTH PACKS AND CONFIRMED NO CONTAMINATION NOTICED AT THIS TIME PER AMM 21-00-21-102-300 AND 05-51-56&NBSP;</P>)

Part: OXYGEN BOX — BROKEN (COCKPIT) · airframe 70,739 hrs · 15,714 cycles

CAPT O2 RESET TEST SWITCH IS BROKEN.(<P>REMOVED AND REPLACED CAPT O2 MASK BOX IAW AMM 35-11-00, OPS CHECK GOOD AND NO LEAKS NOTED. NO OTHER DEFECTS NOTED AT THIS TIME.&NBSP;</P>)

Part: VALVE — UNKNOWN (RT ENGINE) · airframe 70,689 hrs · 15,698 cycles

RIGHT ENGINE TAI VALVE LIGHT DOES NOT CYCLE WHEN TURNED ON FROM AUTO. LIGHT DOES TEST. COULD NOT DUPLICATE ON GROUND AT THIS TIME PER AMM 30-21-00, OPS CHECKS NORMAL.

Part: RETAINER — CRACKED (RT ENGINE) · airframe 70,414 hrs · 15,604 cycles

RT ENG 7 O'CLOCK POSITION SEAL RETAINER CRACKED AND A SECTION WAS MISSING. REMOVED & REPLACED SEAL RETAINER IAW AMM 71-00-00.

Part: SHUTOFF VALVE — FAULTY (AC BAY) · airframe 70,393 hrs · 15,599 cycles

FWD EQUIPMENT VALVE CAUTION MESSAGE ON TAXI OUT. DID NOT CLEAR IN 30 SECONDS, CLEARED AFTER 4:30 SECONDS. TRANSFERRED TO MDDR 117248 IAW MEL 21-58-07-02-01, CAT "C", DUE 13-SEP-2019. MX ACTION C/W, PROCEDURE #2. LP 1066756 - M2: PERFORMED FIM 21-58 FT 899, FOUND MANIFOLD INTERCONNECT VALVE TO BE FAULTING. REMOVED AND REPLACED MANIFOLD INTERCONNECT VALVE IAW 21-58-01. OPS CHECK NORMAL AT THIS TIME. THIS CLEARS MDDR #117248. PLACARDS REMOVED AND MCC NOTIFIED.

Part: CONTROL VALVE — MALFUNCTIONED (AC BAY) · airframe 70,383 hrs · 15,596 cycles

RT PACK TEMP EICAS MESSAGE, PACK WILL NOT RESET. TRANSFERRED TO MDDR # 117154 AS PER MEL 21-51-01-01, CAT C. M PROCEDURES COMPLIED WITH. PLACARDS INSTALLED AND MCC NOTIFIED. LP 1066746 - M3: T/S PER FIM 21-51 FT 807. FOUND CONTROLLER FAULT LIGHT ON. PER AMM 21-51-14 SWAPPED LT TEMP CONTROLLER WITH RT CONTROLLER. VERIFIED RT CONTROLLER FAULT LIGHT ON FOLLOWS CONTROLLER. MCC NOTIFIED P/N 1151864-1/625946-9 CVG BIN CAB0408. LP 1066748 - M2: REMOVED AND REPLACED RT PACK TEMP CONTROLLER IAW AMM 21-51-14. PERFORMED BITE TEST, TEMP CONTROL VALVE FAULTED. MDDR STILL OPEN. OFF PART (PN: 1151864-1, SN: 079C-0642) LP 1066748 - M3: REMOVED AND REPLACED RT TEMP CONTROL VALVE IAW AMM 21-61-07. OPS CHECK GOOD. THIS CLEARS MDDR 117154. PLACARDS REMOVED AND MCC NOTIFIED.

Part: IDG — FAILED (LT GENERATOR) · airframe 70,322 hrs · 15,579 cycles

L GEN FAILED IN CRUISE FLT (FL 360 SAT -47), ATTEMPTED THE RESET OF "GEN CONT" SW, FAILED RESET. APU WAS AVAILABLE.&NBSP;(<P>REMOVED AND REPLACED LEFT INTEGRATED DRIVE GENERATOR IAW B767 AMM 24-11-01, OPS CHECK GOOD.</P>)

Part: CARBON SEAL — LEAKING (NR 2 IDG) · airframe 70,297 hrs · 15,569 cycles

ACCOMPLISHED INSPECTION CHECK ON DRAIN LINES IAW AMM 71-71-00. FOUND IDG DRAIN LINE WITH MINOR LEAKAGE. REMOVED ALL CAPS AND PLUGS, AND RESTORED ENGINE TO NORMAL CONFIGURATION. NR 2 ENGINE IDG DRAIN LINE CAPPED PER AMM 71-71-00 FOR CARBON SEAL TO BE REPLACED. REMOVED RH ENG DRAIN LINE CAPS. REMOVED AND RH ENG IDG. REMOVED AND REPLACED RH ENG IDG CARBON SEAL IAW AMM 72-64-02. RE-INSTALLED RH ENG IDG IAW AMM 24-11-01. OPS CHECK GOOD AT THIS TIME.

Part: WARNING MESSAGE — FALSE ACTIVATION (FWD EQUIP VALVE) · airframe 70,295 hrs · 15,568 cycles

FWD EQPT VAL ADVISORY MSG AFTER ENGINE START. QRH COMPLETED, MSG CLEARED. T/S PER FIM 21-58 FT 898, SYSTEM IS OK.

Part: SWITCH — MALFUNCTIONED (FUEL PUMP) · airframe 70,271 hrs · 15,558 cycles

LT FWD FUEL PUMP WILL NOT TURN OFF. PRESS LIGHT TEST GOOD, NO EICAS MSG FOR L FWD FUEL PUMP (AT CRUISE).&NBSP;(<P>CYCLED FUEL PUMP SWITCH SEVERAL TIMES, OPS CHECK GOOD ON GROUND REF AMM 28-42-00.</P>)

Part: CONTROLLER — MALFUNCTIONED (AC BAY) · airframe 70,110 hrs · 15,497 cycles

RIGHT BLEED DUCT LEAK LIGHT ILLUMINATED. BOTH PACKS RUNNING, OUTSIDE TEMP 110 F, RIGHT BLEED ILL WHILE RIGHT PACK ON.(<P>TRANSFERRED TO MDDR 115141 IAW MEL 21-51-01-01, CAT C, CLEAR BY DATE 31-JUL-19. ACCOMPLISHED M PROCEDURES, WHEN R PACK TURNED OFF, LIGHT EXTINGUISH. ISOLATED TO RIGHT PACK.&NBSP;&NBSP;</P><P>LP 1094266 - M6: REPLACED RIGHT PACK TEMP CONTROLLER IAW AMM REF 21-51-00. RAN ENGINE #2 IAW AMM 71-00-00. OPS AND LEAK CHECK GOOD AT THIS TIME.&NBSP; MCC NOTIFIED AND PLACARDS REMOVED. THIS CLEARS DMI 115141.</P>)

Part: PLACARD — MISSING (FIRST AID KIT) · airframe 69,992 hrs · 15,450 cycles

COCKPIT FIRST AID KIT IN OVERHEAD BINS MISSING PLACARD, P/N 368-11-00-91615-429. (<P>LOCATED AND INSTALLED NEW PLACARD AT COCKPIT OVERHEAD BIN IAW AMM 20-10-13-964-001.</P>)

Part: IDG — MALFUNCTIONED (LEFT) · airframe 69,951 hrs · 15,434 cycles

LT GENERATOR DRIVE LIGHT AND EICAS MESSAGE AFTER ENGINE START. REACTIVATED IDG ON LT ENG IAW AMM 24-11-01. SERVICED IDG IAW AMM 12-13-03. RAN LH ENG. IDG OPS CHECK GOOD. PER MCC REQUEST. DEACTIVATED LT ENG IDG IAW DDG PROCEDURES. REMOVED AND REPLACED THE NR 1 ENG IDG IAW AMM 24-11-01. OPS CHECKED GOOD.

Part: SERVICE PORT — LOOSE (IDG) · airframe 69,940 hrs · 15,430 cycles

ON WALK AROUND, OIL NOTICED SEEPING UNDER LH ENGINE IDG SERVICE DOOR(<P>FOUND IDG SERVICE PORT NECK LOOSE AT IDG HOUSING. SECURED FITTING AND SERVICED IDG IAW AMM 12-13-03. PERFORMED ENGINE RUN IAW AMM 71-00-00-712-168-H03, NO LEAKS NOTED. OK FOR SERVICE&NBSP;</P>)

Part: IDG — FAILED (LEFT) · airframe 69,912 hrs · 15,421 cycles

DURING CRUISE FLIGHT, LEFT GEN OFF EICAS, AND LEFT GEN & LEFT DRIVE LIGHTS APPEARED. QRH WAS RUN, APU STARTED, FLT CONTINUED. T/S DISCREPANCY AND SWAPPED L/H & R/H GCUS AND PERFORMED ENGIEN RUN. NO VOLTS OR FREQUENCY ON LEFT ENGINE. CONFIRMED LEFT IDG TO BE BAD. SWAPPED GCUS TO ORIGINAL POSITIONS. ALSO FOUND MULTIPLE FAULTS FOR IDG ON BPCU IAW FIM 767-24-20 TREE 804. REMOVED AND REPLACED THE LT IDG AND PERFORMED OPS CHECK IAW AMM 24-11-01. OPS CHECKED GOOD.

Part: WARNING MESSAGE — FALSE ACTIVATION (LT GENERATOR) · airframe 69,898 hrs · 15,417 cycles

AT FL 400, L GEN OFF EICAS MSG WITH OTHER ASSOCIATED EICAS MSG. PERFORMED L GEN OFF QRH CHECKLIST AND ALL MSG CLEARED W/GEN RESET. PERFORMED BPCU BITE PROCEDURE IAW FIM 24-20 FT 801, NO FAULTS NOTED AT THIS TIME. VERIFIED LH IDG OIL LEVEL, LEVEL OK REF AMM 12-13-03. OK FOR SERVICE.

Part: FAN — INOPERATIVE (EXHAUST) · airframe 69,816 hrs · 15,393 cycles

FWD EQUIPMENT EXHAUST STATUS MESSAGE. PERFORMED FIM TASK 21-58 FAULT TREE 905 AND FOUND FWD EQ EXH FAN TO BE INOP. REMOVED AND REPLACED THE FORWARD RACK EXHAUST FAN. INSTALLATION CHECKED GOOD PER AMM 21-58-06.

Part: GCU — MALFUNCTIONED (APU) · airframe 69,773 hrs · 15,378 cycles

APU INOP. PERFORMED BITE PROCEDURE OF APU ECU IAW AMM 49-61-05, NO FAULTS FOUND AND APU OPERATES NORMALLY. MCC REQUESTS REPLACEMENT OF GCU. REMOVED AND REPLACED APU GCU IAW AMM 24-22-02. PERFORMED OPS CHECK OF APU GCU AND BITE CHECK. NO FAULTS FOUND, OPS CHECK GOOD.

Part: EXHAUST FAN — MALFUNCTIONED (E&E BAY) · airframe 69,623 hrs · 15,330 cycles

FWD EQUIP COOLING FAN EXHAUST EICAS MESSAGE DISPLAYED.(<P>MEL 21-58-04-02-01 APPLIED, TRANSFERRED TO MDDR 111661.</P><P>LP 1032150 - M2: PERFORMED FIM TASK 21-58 FT 905 TO #40. REMOVED AND REPLACED FWD RACK EXHAUST FAN IAW AMM 21-58-06. OPS CHK GOOD. THIS CLEARS MDDR #111661. MCC ADVISED AND PLACARDS REMOVED.</P>)

Part: UNKNOWN — ODOR · airframe 69,548 hrs · 15,308 cycles

DURING TO AND INITIAL CLIMB PACKS EMITTED A "WET SOCKS" ODOR. SUSPECT AEROSOLIZED&NBSP; ENGINE OIL INTO BLEED SYSTEM(<P>PERFORMED&NBSP; OPS CHECK OF PACK SYSTEM IN HOT AND COLD. NO SMELL NOTED AND OPS CHECK GOOD. REF AMM 21-51-00&NBSP;</P>)

Part: PANEL — MALFUNCTIONED (COCKPIT) · airframe 69,505 hrs · 15,293 cycles

NR 2 ENGINE START VALVE DID NOT CLOSE(<P>START VALVE PLACED ON MEL PER MEL 80-11-02. START SWITCH FOUND BAD, REF MDDR 110888.</P><P>R+R ENGINE IGNITION AND START PANEL IAW AMM 80-11-51. PERFORMED ENGINE DRY MOTOR AND OPS CHECK OF THE IGNITION SYSTEM. ALL OPS CHECKS NORMAL. NO DEFECTS NOTED AT THIS TIME. PLACARDS REMOVED. THIS CLEARS DMI # 110888.<BR DATA-MCE-BOGUS="1" /></P>)

Part: SEAL — LEAKING (PNEUMATIC SYSTEM) · airframe 69,438 hrs · 15,268 cycles

PNEUMATIC LEAK AT JOINT OF AFT AIR CONDITIONING SERVICE HOOK UP.(<P>REMOVED AND REPLACED PERI-SEALS PER AMM 36-11-01. NO LEAKS NOTED.</P>)

Part: BPCU — INOPERATIVE · airframe 69,438 hrs · 15,268 cycles

UTILITY BUSS WOULD NOT COME ON LINE, BPCU INOP.(<P>REMOVED AND REPLACED BPCU IAW 24-41-03. OPS CHECK OK.</P>)

Part: FAN — FAILED (SMOKE DETECTOR) · airframe 69,438 hrs · 15,268 cycles

FWD DET FAN MAINTENANCE MESSAGE.&NBSP;(<P>REMOVED AND REPLACED FWD COMPARTMENT SMOKE DETECTOR BLOWER. OPS CHECK NORMAL IAW B767 AMM 26-16-02.</P>)

Part: CONNECTOR — UNSECURE (RT A/C PACK) · airframe 69,411 hrs · 15,257 cycles

RIGHT PACK INOP. DURING DVI OF RT PACK ASSY, FOUND PACK TEMP SENSOR CANNON PLUG BACK SHELF TO BE LOOSE. TIGHTENED BACK SHELL IAW AMM 21-61-02. OPS CHECK GOOD. THIS CLEARS DMI 110042. NO OTHER DEFECT NOTED. DISPATCHER ZH 1422Z.</P>)

Part: BATTERY — INOPERATIVE (APU) · airframe 69,403 hrs · 15,255 cycles

APU BATTERY INOP ON APU START.(<P>REMOVED AND REPLACED&NBSP;APU BATTERY ASSY IAW AMM 24-31-04. OPS CHECK OK.<BR /></P>)

Part: CONTROL VALVE — MALFUNCTIONED (CABIN TEMP) · airframe 69,373 hrs · 15,245 cycles

AFT CABIN TEMP EICAS MSG(<P>TRANSFERRED TO MDDR # 109694 AS PER MEL 21-61-04-02 CAT C&NBSP;</P><P>LOG PAGE 1060879 - M3: PERFORMED FIM 21-60- FT 806 , FOUND TRIM AIR MOD. VALVE FAULT. REMOVED AND REPLACED TRIM AIR MOD. VALVE I.A.W AMM 21-61-07. OPS CHECK NORMAL AT THIS TIME. THIS CLEARS MDDR # 109694. PLACARDS REMOVED AND MCC NOTIFIED.</P>)

Part: SOLENOID VALVE — INOPERATIVE (APU) · airframe 69,335 hrs · 15,230 cycles

APU RELIABILITY COLD START ATTEMPTED ON FLT LEG CVG SCK SAT-50, FL 380 FAILED TO START ON 3 ATTEMPTS. APU INOP.(<P>TRANSFERRED TO MDDR 109396.<BR /></P><P>LP 1024068 - M3:&NBSP;TROUBLE SHOT APU IAW 49-11 FAULT TREE 991 UP TO BLOCK 11 SHEET 2. NO HELP. DMI # 109396 REMAINS OPEN.</P><P>LP 1024075 - M3:&NBSP;REMOVED AND REPLACED APU EXCITER BOX AND REMOVED AND REPLACED APU ELEC. IGNITION LEAD P/N 3888076-3 IAW AMM 49-41-03 AND AMM 49-41-04. DMI # 109396 REMAINS OPEN.&NBSP;</P><P>LP 1024079 - M3:&NBSP;REMOVED AND REPLACED APU IGNITER PLUG IAW AMM 49-41-02-404-006. MDDR # 109396 REMAINS OPEN.&NBSP;</P><P>LP 1060868-M3 ACCOMPLISHED ACTION PLAN. REMOVED AND REPLACED DE-OIL SOLENOID VALVE IAW AMM 49-27-08. LEAK AND OPS CHECK GOOD. THIS CLOSES DMI 109396. MCC NOTIFIED. PLACARDS REMOVED.&NBSP;</P>)

Part: ECU — MALFUNCTIONED (APU) · airframe 69,322 hrs · 15,225 cycles

APU FAULT ON LANDING TWO START ATTEMPTS, NO ROTATION OBSERVED(<P>REPLACED APU ECU IAW AMM 49-61-05. OPS CHECK NORMAL&NBSP;</P>)

Part: ECU — MALFUNCTIONED (APU) · airframe 69,335 hrs · 15,230 cycles

APU RELIABILITY COLD START FAILED 3 ATTEMPTS ON FLT LEG RFD-SCK SAT-64, FL 380 *APU FAULT EICAS ILLUMINATED.(<P>PER FIM 49-11 F/T 993 BIT ECU ON ARRIVAL HAD NO LIGHT OFF RE-SET ECU APU OPERATES OK 0 FAULTS NOTES. THIS DMI REMAINS OPEN FOR RE-EVALUATION AND RE-START DMI 109273 FOR VERIFICATION.&NBSP;<BR /></P>)

Part: RELAY — FAILED (APU) · airframe 69,234 hrs · 15,196 cycles

APU RELIABILITY COLD START ACCOMPLISHED ON THIS LEG ONT-RFD SAT -38 FL370 - START UNSUCCESSFUL.(<P>TRANSFERRED TO MDDR 108673 MEL 49-11-01, DUE DATE 24 MAR MAR 19 PLACARD INSTALLED<BR /></P><P>LOGPAGE 1069059: PERFORMED FIM 49-11 F/T 991. REMOVED AND REPLACED APU START/TRU SEL RELAY PER STEP 26 IAW AMM 20-81-00.</P><P>LOGPAGE 1069061: PERFORMED OPS CHECK OF APU IAW AMM 49-11-00. NO DEFECTS NOTED AT THIS TIME. THIS CLEARS DMI# 108673, PLACARD REMOVED. REF LOGPAGE 1069059 FOR CORRECTIVE ACTION&NBSP;<BR DATA-MCE-BOGUS="1" /></P>)

Part: MODULE — FAULTY (APU) · airframe 69,227 hrs · 15,193 cycles

APU RELIABILITY COLD SOAK START ATTEMPTED LEG CVG - ONT SAT -33C FL 360 , UNSUCCESSFUL AFTER 3 ATTEMPTS&NBSP;(<P>NOTED BY MX , REF LOG PAGE 1069052 ITEM 3 TRANSFERRED TO MDDR # 108569 AS PER MEL 49-11-01A CAT C&NBSP;</P><P>LOG PAGE 1069053 PERFORMED APU BITE TEST IAW FIM 49-11 FT 987 , ECU SHOWING MINIFLAG 15 , REMOVED AND REPLACED FLOW SENSOR MODULE IAW AMM 49-53-08 OPS CHECK NORMAL AT THIS TIME , MDDR # 108569 CLOSED&NBSP;</P>)

Part: CONTROL UNIT — FAULTY (APU) · airframe 69,211 hrs · 15,189 cycles

APU RELIABILITY COLD START ATTEMPIED ON FLIGHT LEG SCK -BDL SAT -58&NBSP; FL 370&NBSP; 3 ATTEMPTS UNSUCCESSFUL&NBSP;(<P>APU TRANSFERED TO MDDR 108569 IAW MEL 49-11-01A CAT C DUE 22MAR19&NBSP;</P><P>REF LOG PAGE 1058279 REMOVED AND REPLACED APU CONTROL UNIT IAW AMM 49-61-05 AND OPS CHECK IS GOOD AT THIS TIME , MDDR # 108569 CLOSED&NBSP;</P>)

Part: UNKNOWN — MALFUNCTIONED (WEATHER RADAR) · airframe 69,159 hrs · 15,173 cycles

LEFT RADAR SYSTEM INTERMITTENT RADIAL SPIKES DISPLAYED DISPLAYED WHILE IN ROUTE.&NBSP;(<P>PERFORMED SYSTEM TEST AND THE OPS TEST OF THE WEATHER RADAR SYSTEM IAW AMM 34-43-00. OPS CHECK TESTED OK WITHOUT ANY FAULTS.</P>)

Part: IGNITER — DAMAGED (APU) · airframe 69,025 hrs · 15,134 cycles

APU FAULT. APU FAILED TO START @ FL 270 SAT&NBSP; -24(<P>NO FAULTS FOUND, APU OPS CHECK GOOD IAW AMM 49-00-00.</P><P>LP 1054556-M4: R/R APU IGNITER IAW B767 AMM 49-41-02. OPS CHECK TESTED OK.&NBSP;</P>)

Part: ANTI-ICE VALVE — INOPERATIVE (RT ENGINE) · airframe 69,002 hrs · 15,127 cycles

RIGHT ENGINE ANTI ICE VALVE INOP(<P>TRANSFERRED TO MDDR 107375.<BR /></P><P>LOG PAGE 1054551: R&AMP;R ENGINE INLET TAI VALVE RH ENG (#2) IAW AMM 30-21-03. OPS CHECK GOOD. THIS CLEARS DMI 107375. MX PROCEDURES REVERSED.<BR /></P>)

Part: WARNING LIGHT — FALSE INDICATION (ANTI-ICE VALVE) · airframe 68,984 hrs · 15,121 cycles

R ENG ANTI ICE VALVE LIGHT ILLUMINATED.(<P>MX REQUESTED CREW TO START #2 ENGINE PERFORMED OPS TEST OF RIGHT ANTI ICE VALVE OPS CHECK OK NO FAULTS AMM 30-21-03.<BR /></P>)

Part: ANTI-ICE VALVE — MALFUNCTIONED (RT ENGINE) · airframe 68,977 hrs · 15,118 cycles

RT ENG ANTIICE "VALVE" LIGHT ILLUMINATED IN OVERHEAD PANEL, WITH ENG SHUTDOWN. CYCLED ANTI ICE VALVE IAW AMM 30-21-00 SYSTEM OPS CHECKS GOOD AT THIS TIME.

Part: OIL SYSTEM — LOW (APU) · airframe 68,937 hrs · 15,106 cycles

APU "FAULT" MSG AFTER ATTEMPTED APU START WHILE ON DESCENT.(<P>FOUND APU OIL TO BE LOW. SERVICED TO FULL AND PERFORMED 3 SUCCESSFUL STARTS. NO DEFECTS NOTED. REF B767 AMM 12-13-04.</P><P ><SPAN><BR /></SPAN></P>)

Part: SENSOR — FAULTY · airframe 68,839 hrs · 15,074 cycles

TAT READS 44DEG C (FLUCTUATES BTWN 42 AND 46 DEG C -WHILE PARKED WITH ENG SHUTDOWN - CAPT PITOT OVHEAD LT EXTINGUISHED. ACTUAL OUTSIDE AIR TEMP 03DEG PER CVG ATIS(<P>SWAPPED RELAY K552 NO HELP, REPLACED K644 AND K10446 NO HELP . CHECK GND AT RELAY K644 PIN X2 NO GND FOUND&NBSP; FROM BOTH SPEED CARDS. NEEDS FURTHER TS&NBSP; / TS TO TAT FAULT,&NBSP; FOUND GRND MISSING AT K516; TS TO SENSOR RT GEAR TILT S10598 - (PN 8-527-03 ) .&NBSP;REMOVED AND REPLACED SENSOR S10598 IAW WDM 27-62-11 OPS CHECK OK&NBSP; IAW 30-31-00 OPS CHECK OK&NBSP;</P>)

Part: SEAL — MISSING (FIRST AID KIT) · airframe 68,822 hrs · 15,067 cycles

SEAL MISSING 1ST AID KIT BY ENTRY DOOR(<P>TRANSFERRED TO MDDR 105927 PER MEL 25-64-01-01B.REPLACED MISSING SEAL ON FIRST AID KIT IAW GMM 3-28-1.THIS CLEARS DMI 105927.PLACARD REMOVED</P>)

Part: UNKNOWN — MALFUNCTIONED (FUEL SYSTEM) · airframe 68,822 hrs · 15,067 cycles

LEFT AFT FUEL BOOST PUMP INOP(<P>TRANSFERRED TO MDDR 105826 IAW MEL 28-22-01.</P><P>PERFORMED OPS CHECK OF FUEL BOOST PUMP IAW AMM 28-22-00, NO DEFECT NOTED AT THIS TIME. PLACARDS REMOVED AND DMI 105826 CLOSED. MAINT ACTION REVERSED.&NBSP;&NBSP;</P><P><BR DATA-MCE-BOGUS="1" /></P>)

Part: UNKNOWN — MALFUNCTIONED (FUEL SYSTEM) · airframe 68,822 hrs · 15,067 cycles

LEFT AFT FUEL PUMP INOP.(<P>PERFORMED OPERATION CHECK OF FUEL BOOST PUMP IAW 28-22-00, NO DEFECTS NOTED AT THIS TIME PLACARD REMOVED MAINT ACTION REVERSED.<BR DATA-MCE-BOGUS="1" /></P>)

Part: ADC — MALFUNCTIONED (COCKPIT) · airframe 68,822 hrs · 15,067 cycles

TEMP ON TAT BLANKS ON INDICATION VERY HIGH TEMP(<P>REMOVED AND REPLACED TOTAL AIR TEMPERATURE PROBE (P/N&NBSP;<SPAN>102LA2AG, S/N&NBSP;</SPAN><SPAN>86030)</SPAN><SPAN>&NBSP;</SPAN><SPAN>IAW AMM 34-12-02, NO FIX, PROBLEM STILL PERSIST. R/R AIR GROUND RELAY, NO HELP.</SPAN></P><P><BR DATA-MCE-BOGUS="1" /></P><P>LP 1032937: REMOVED AND REPLACED AIR DATA COMPUTER&NBSP;</P>)

Part: CARBON SEAL — NOT REPORTED (NR 2 ENGINE) · airframe 68,799 hrs · 15,060 cycles

PERFORM STEP 11 OF ECM #2018P-803 PER COMPANY REQUEST DUE TO HIGH OIL CONSUMPTION OF NR 2 ENGINE(<P>SEAL AND RING ASSEMBLED (CARBON SEAL) REMOVED IAW 72-64-02 AND NEW ONE INSTALLED. OPS CHECK GOOD AT THIS TIME. NO LEAKS FOUND THIS CLEARS DMI # 105333 <BR /></P>)

Part: GCU — FAULTED (APU GENERATOR) · airframe 68,738 hrs · 15,034 cycles

APU AC GENERATOR FAULTS WHEN LOAD EXCEEDS .70(<P>PERFORMED FIM 24-21 , FOUND GCU FAULT , REMOVED AND INSTALLED SERVICEABLE APU GCU I.A.W AMM 24-22-02 OPS CHECK GOOD&NBSP;</P>)

Part: WARNING LIGHT — ILLUMINATED (APU GENERATOR) · airframe 68,717 hrs · 15,026 cycles

APU GEN OFF EICAS AFTER APU WAS SHUT DOWN ON THE GROUND AFTER ENGINE START,&NBSP;(<P>PERFORMED APU GEN TEST IAW AMM 24-21-00, OPS CHECK NORMAL&NBSP;</P>)

Part: MODULE — WARNING MESSAGE (RT ENGINE) · airframe 68,726 hrs · 15,030 cycles

R ENGINE BLEED OFF MESSAGE&NBSP;(<P>PERFORMED BITE &AMP; CLEAR OF AIR SUPPLY MODULE I.A.W AMM 36-23-00 OPS CHECK GOOD , MSG CLEARED&NBSP;</P>)

Part: LIGHT — DEFECTIVE · airframe 68,651 hrs · 15,002 cycles

APU BOTTLE DISCHARGE LIGHT ILLUMINATED. FOUND APU REMOTE PANEL C/B POPPED DISCONNECTED P5936 TO BOX C/B OK, SUSPECT BAD BOX. REMOVED AND REPLACED LIGHT ASSY IAW 26-15-01. OPS CHECKS OK.

Part: CONTROLLER — INOPERATIVE (WINDOW HEAT) · airframe 68,591 hrs · 14,979 cycles

LEFT NR 2 WINDOW HEAT INOP. REMOVED AND REPLACED WINDOW HEAT CONTROLLER IAW AMM 30-40-01. OPS CHECK.

Part: CONTROLLER — MALFUNCTIONED (RT ENGINE PRV) · airframe 68,565 hrs · 14,968 cycles

R ENGINE PRV STATUS MSG. REMOVED AND REPLACED RH ENGINE PRV CONTROLLER IAW AMM 36-11-19&NBSP;</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (PRV) · airframe 68,561 hrs · 14,966 cycles

RIGHT ENGINE PRV STATUS&NBSP;(<P>PERFORMED BITE TEST. NO FAULTS NOTED AT THIS TIME AS PER AMM 36-23-00</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (RT PRV) · airframe 68,545 hrs · 14,958 cycles

RIGHT ENGINE PRV STATUS MESSAGE&NBSP;(<P>PERFORMED BITE TEST ON AIR FLOW BITE MODULE. NO FAULT NOTED, MESSAGE CLEARED PER FIM 36-10 FAULT TREE 847 BITE 36-20 FAULT TREE 804</P>)

Part: CHIP DETECTOR — NOT REPORTED (NR 2 STARTER) · airframe 68,524 hrs · 14,950 cycles

DURING #2 ENGINE STARTER OIL CHANGE. CHIP DETECTOR HOUSING&NBSP;(<P>REMOVED AND REPLACED PLUG IAW AMM ATLAS WO A-80-301-00-0. NO LEAKS NOTED&NBSP;</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (RT ENG PRV) · airframe 68,524 hrs · 14,950 cycles

R ENG PRV STATUS MSG(<P>PERFORMED R ENG PRV OPS CHECK I/A/W 36-11-18 OPS CHECK GOOD AT THIS TIME. MSG IS CLEARED<BR /></P>)

Part: WARNING MESSAGE — FALSE ACTIVATION · airframe 68,403 hrs · 14,907 cycles

HIGH FLOW INHIBIT STATUS MESSAGE. COMPLIED WITH FIM 21-51, FAULT TREE 813. FOUND NO FAULTS. RACKED THE PACK FLOW CONTROL CARD. HIGH FLOW INHIBIT STATUS MESSAGE REMAINED CLEAR. NO CORROSION NOTICED ON THE PACK FLOW CONTROL CARD.

Part: WARNING MESSAGE — FALSE ACTIVATION (HIGH FLOW) · airframe 68,395 hrs · 14,905 cycles

HIGH FLOW INHIBIT STATUS MESSAGE. TROUBLESHOT THE PACK SYSTEMS IAW FIM 21-51 FAULT TREE 813. FOUND SYSTEM TO BE OPERATING NORMALLY. MESSAGE CLEARED. NO DEFECTS NOTED AT THIS TIME.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 68,257 hrs · 14,850 cycles

RT ENG PRV STATUS MSG EICAS MSG CAME ON MONENTARY AFTER T/O & WENT OUT. CLEARED WITH NO HARD FAULT IAW AMM 36-11-09, OPS NML.

Part: SMOKE DETECTOR — FAULTY (CARGO BAY) · airframe 68,237 hrs · 14,843 cycles

ON PREFLIGHT FOUND "AFT CARGO DET 1" STATUS MESSAGE ON EICAS. R&R AFT CARGO SMOKE DETECTOR IAW AMM 26-97-01, OPS CHECKS GOOD.

Part: STATUS MESSAGE — ACTIVATED (COCKPIT) · airframe 68,232 hrs · 14,841 cycles

ON PREFLIGHT FOUND AFT CARGO DET 1 STATUS MESSAGE ON EICAS. TRANSFERRED TO MDDR 100326 AS PER DDG 26-16-01-01 CAT C.

Part: MOTOR — INOPERATIVE (WINDSHIELD WIPER) · airframe 68,216 hrs · 14,835 cycles

LEFT WINDSHIELD WIPER INOP. R&R LEFT WINDSHIELD WIPER MOTOR IAW 30-42-02.

Part: UNKNOWN — MALFUNCTIONED (APU) · airframe 68,216 hrs · 14,835 cycles

AFTER APU START UP, ENGINE SHUTDOWN NO APU BLEED PRESSURE. PERFORMED APU BITE, OPERATIONAL CHECK IS NORMAL. NO FURTHER DEFECT NOTED IAW AMM 49-61-05.

Part: BLEED AIR SYS — MALFUNCTIONED (APU) · airframe 68,216 hrs · 14,835 cycles

AFTER APU START UP, ENGINE SHUTDOWN NO APU BLEED PRESSURE.

Part: SWITCH — INOPERATIVE (COCKPIT) · airframe 68,174 hrs · 14,821 cycles

RT AUX PITOT PROBE HEAT LIGHT INOP. REMOVED AND REPLACED RT AUX PITOT HEAT LIGHT SWITCH IAW SWPM 20-81-14. OPS CHECK OK.

Part: DOUBLER — GOUGED (LT COWLING) · airframe 68,177 hrs · 14,822 cycles

LT ENGINE OB CORE COWL DOOR AFT FRAME ON REPAIR DOUBLER GOUGED. REMOVED EXISTING REPAIR FROM LT ENGINE OB CORE COWL DOOR AFT FRAME IAW SRM 51-10-02. ACCOMPLISHED REPAIR ON AFT FRAME IN LT ENGINE OB CORE COWL IAW SRM 54-45-01 REPAIR 14.

Part: SKIN — GOUGED (LE SLAT) · airframe 68,177 hrs · 14,822 cycles

SLAT NR 10 T/E WEDGE COVE HAS GOUGE THROUGH SKIN APPROX 1.5" LONG AT 11" O/B OF I/B EDGE. ACCOMPLISHED REPAIR ON SLAT NR 10 T/E WEDGE COVE SKIN IAW SRM 51-70-10 REPAIR.

Part: SKIN — PUNCTURED (FUSELAGE) · airframe 68,177 hrs · 14,822 cycles

FUSELAGE, SECTION 43 SKIN (P/N 143T3562-2) PUNCTURE AND STRINGER 5-34R (143T3001) DEFORMATION STA 654 TO STA 654+22. ACCOMPLISHED EO 6753A727 REV O PART 1 THRU 4.

Part: ENGINE — CHAFED (LEFT) · airframe 68,179 hrs · 14,823 cycles

LT ENGINE BEHIND GEAR BOX EWIS CHAFING. NR 1 REMOVED AND REPLACED ON T/C E1029-1, FAS W/O N1229-01-01.

Part: START VALVE — FAILED (RT ENGINE) · airframe 68,146 hrs · 14,806 cycles

RT START VALVE FAILED TO OPEN. REMOVED AND REPLACED RT ENG STARTER VALVE IAW AMM 80-11-02, OPS CHECK LEAK GOOD.

Part: RELAY — FAILED (START SYSTEM) · airframe 68,140 hrs · 14,804 cycles

AFTER BOTH ENGINE STARTED AND IGNITION SELECTED IN AUTO RECEIVED " LEFT START CUTOUT MESSAGE WITH NO LIGHT. COMPLIED WITH QRH CHECK. LEFT ENGINE ISOLATION VALVE MESSAGE EXTINGUISHED. REMOVED AND REPLACED NR 1 ENGINE START CONTROL RELAY IN REFERENCE TO SWPM 20-81. (K665). OPS CHECK GOOD AT THIS TIME.

Part: UNKNOWN — MALFUNCTIONED (WEATHER RADAR) · airframe 68,126 hrs · 14,800 cycles

WX RANGER DISAGREE ON CAPT'S HSI DISPLAY ALL RANGES INTERMITTENT. CAPT SIDE ONLY LT SYS REPEAT WRITE UP. PERFORMED FAULT ISOLATION PROCEDURES AS PER FIM 34-43 FT 104 AND EFIS BITE TEST IAW FIM 34-22 FIG 108, FOUND OK.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 68,122 hrs · 14,799 cycles

STATUS ANNUNCIATION " WXR RANGE DISAGREE" ON CAPTAINS HSI DISPLAYED WHEN RANGE SELECTED OUTSIDE OF 80NM (LT SYS). PERFORMED FIM 34-43 FT 809. NO FAULTS OR MESSAGES NOTED AT THIS TIME. OPS NORMAL.

Part: NOT REPORTED — MALFUNCTIONED (APU) · airframe 68,109 hrs · 14,794 cycles

APU INOP WILL NOT SUPPLY BLEED AIR. TRANSFERRED TO MDDR 96746 IAW MEL 49-11-01A CAT C DUE DATE 29JUL18 PLACARD INSTALLED.

Part: CONTROL PANEL — DEFECTIVE (COCKPIT) · airframe 68,080 hrs · 14,785 cycles

LT ENG START SW DID NOT STAY IN GND POSITION ON 1ST ATTEMPT. ON 2ND ETTEMPT, SWITCH OPERATED NORMAL. REMOVED AND REPLACED GROUND START CONTROL PANEL IAW AMM 80-11-51. RAT NEEDS TO BE CYCLED. PERFORMED RAT OPS CHECK IAW AMM 29-21-00. OPS CHECK GOOD - EXTENDED & RETRACTED NORMALLY.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 68,051 hrs · 14,772 cycles

STATUS MSG AFT EQ EXH FAN 2. PERFORMED FIM 21-26 FAULT TREE 808 SYS NORMAL, CLEARED.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 68,051 hrs · 14,772 cycles

STATUS MSG, AFT EQ EXH FAN 2. PERFORMED FIM 21-26 FT 808 SYSTEM NORMAL, MSG CLEARED.

Part: CONTROL UNIT — MALFUNCTIONED (APU) · airframe 68,029 hrs · 14,764 cycles

APU INOP. REMOVED AND REPLACED APU CONTROL UNIT IAW MM 49-61-05. APU PNEUMATIC CHECK GOOD.

Part: PCA — LEAKING (SPOILER) · airframe 68,004 hrs · 14,756 cycles

CLIMBING OUT OF FL210 RT HYD QTY WENT TO 0.21 LOSS OF RT HYD SYSTEM. SYSTEM REQUIRES FLUID SERVICE. REMOVED AND REPLACED NR 11 SPOILER PCA IAW AMM 27-61-02, OPERATIONAL TEST AND LEAK TEST GOOD. REMOVED AND REPLACED ACMP FILTER MODULE OPERATIONAL TEST AND LEAK CK GOOD. REMOVED AND REPLACED FILTER MODULE FOR EDP IAW AMM 29-11-17, OPERATIONAL TEST AND LEAK TEST GOOD NO EVIDENCE OF CONTAMINATION FOUND.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 67,991 hrs · 14,749 cycles

CABIN ALT AUTO 2 STATUS MSG. PERFORMED BITE CK OF CABIN PRESS CONTROLLER 2, NO FAULTS NOTED IAW FIM 23-31-FT 803.

Part: BLEED AIR SYS — MALFUNCTIONED (APU) · airframe 67,993 hrs · 14,750 cycles

NO APU BLEED AIR PRESSURE. COMPLIED WITH ACTION PLAN FOR APU AIR. APU OPS CHECKS GOOD IAW AMM 49-00-00.

Part: APU — SHUTDOWN (APU BAY) · airframe 67,968 hrs · 14,742 cycles

APU SHUTDOWN IN THE BLOCKS UPON PARKING AND DECENT. UPON FURTHER INVESTIGATION AND OPERATION PER AMM 49-21-00/01 OPS CHECK GOOD.

Part: NOT REPORTED — MALFUNCTIONED (APU) · airframe 67,973 hrs · 14,744 cycles

APU BLEED VALVE INOP. PERFORMED FIM TASK 49-11 FT A04 ALL CHECKS GOOD. RUN APU WITH DUCT PRESSURE NO FAULTS. LEAK CHECKS ALL GOOD.

Part: NOT REPORTED — MALFUNCTIONED (APU) · airframe 67,968 hrs · 14,742 cycles

NO DUCT PRESSURE ON THE GROUND WITH APU RUNNING AND ALL ASSOCIATED VALVES OPEN. TRANSFERRED TO MDDR 95360 IAW MEL 49-11-01-01 CAT C EXPIRE 29JUN18.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 67,968 hrs · 14,742 cycles

DIRTY / WET SOAK SMELL IN COCKPIT LIFT OFF UNTIL APPROX 17,000FT APPROACH TO BE COMING FROM GASPER FANS. INSPECTED AND RAN RECIRCULATION FAN AND FOUND NO FAULTS OR SMEELL IAW AMM 21-25-00, OPS CHECK GOOD.

Part: STARTER — FAULTY (APU) · airframe 67,964 hrs · 14,741 cycles

APU INOP. REMOVED AND REPLACED STARTER APU PER AMM 49-41-01 OPS CHECK GOOD.

Part: CONTROLLER — FAULTY (BLEED AIR SYS) · airframe 67,946 hrs · 14,735 cycles

PER MCC REQUEST LOCK OUT R ENG HPSOV DUE TO HISTORY OF EICAS MESSAGE. REMOVED AND REPLACED HIGH T PRES CONTROLLER IAW AMM 36-11-08. OPS CHECK NORMAL AT THIS TIME NO FAULTS NOTED THIS TIME.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 67,926 hrs · 14,727 cycles

STATUS MSG R ENG PRV. MESSAGE CLEARED PER AMM 31-4-00. ACCOMPLISHED AIR SUPPLY BITE PER FIM NO CURRENT FAULTS RAN RIGHT ENGINE PER AMM 71-00-00 RIGHT ENGINE BLEED OPS CHECK NORMAL PER AMM 36-10-00.

Part: WARNING MESSAGE — FALSE ACTIVATION (COCKPIT) · airframe 67,921 hrs · 14,725 cycles

R ENG HPSOV STATUS MSG. PERFORMED BITE TEST TASK 36-23-00 AND FIM 36-20FT 804 BITE CHECK GOOD NO DEFECTS NOTED IAW AMM 36-23-00-715-001.

Part: SHUTOFF VALVE — MALFUNCTIONED (BLEED AIR SYS) · airframe 67,915 hrs · 14,721 cycles

R ENG HPSOV EICAS MESSAGE IN FLIGHT. CIRCUIT BREAKERS PULLED AND COLLARED. REMOVED AND REPLACED R ENGINE HPSOV REF AMM 36-11-07. OPS CHECK GOOD. THIS CLEARS MDDR 94821.

Part: CHARGER — MALFUNCTIONED (APU BATTERY) · airframe 67,894 hrs · 14,714 cycles

APU BATTERY CHARGER STATUS MESSAGE. REPLACED THE APU BATTERY CHARGER IAW AMM 24-31-05. OPS CHECKED NORMAL.

Part: CONTROLLER — FAULTY (BLEED AIR SYS) · airframe 67,894 hrs · 14,714 cycles

REPEAT WRITE, EICAS R ENG PRV ON TAKEOFF ROLL AND CLIMB INTERMITTENTLY STATUS MSG. RT ENG PRV BITE CARRIED OUT ON AIR SUPPLY MODULE WAS SHOWING PRVC FAULT. REPLACED PRV CONTROLLER PER AMM 36-11-19 OPS CHECK NORMAL.

Part: SHUTOFF VALVE — MALFUNCTIONED (RT ENGINE) · airframe 67,885 hrs · 14,711 cycles

RIGHT ENGINE EICAS DURING DEPARTURE. RT ENGINE PRV STATUS IN FLIGHT. REMOVED AND REPLACED THE HPSOV IAW AMM 36-11-07, TESTED OK.

Part: WARNING MESSAGE — FALSE ACTIVATION (RT ENGINE) · airframe 67,887 hrs · 14,712 cycles

RIGHT ENGINE PRV CAUTION MESSAGE, CLIMBING THROUGH 15,000FT, THE MESSAGE CLEARED, RT ENG STATUS REMAINED OF THE FLIGHT. PERFORMED A BITE TEST ON THE AIR SUPPLY MODULE, NO FAULTS DISPLAYED, MESSAGE CLEARED IAW AMM 36-33-0.

Part: PRIORITY VALVE — MALFUNCTIONED (RT ENGINE) · airframe 67,880 hrs · 14,710 cycles

MOMENTARY RT ENGINE PRV ADVISORY MESSAGE DISPLAYED DURING CLIMB OUT. THE ADVISORY CLEARED, BUT THE RT ENG PRV STATUS MESSAGE REMAINED. REMOVED AND REPLACED THE RT ENGINE PRV IAW AMM 36-11-18, OPS CHECKED NORMAL.

Part: BLADE — NICKED (ENGINE) · airframe 67,877 hrs · 14,709 cycles

DURING A PREFLIGHT INSPECTION, PILOT REPORTED A SMALL NICK ON THE LEDING EDGE SMALL NICK ON LEDING EDGE OF THE NR 8 FAN BLADE, ON THE LT ENGINE. PERFORMED AN INSPECTION IAW AMM 72-31-02-226-012-H00, AND FOUND TO BE WITHIN LIMITS, NO SHARPS EDGES OR CRACKS NOTED.

Part: SENSOR — LOOSE (APU INLET TEMP) · airframe 67,877 hrs · 14,709 cycles

APU INOPERATIVE. REMOVED AND REPLACED THE FLOW SENSING MODULE IAW AMM 49-53-08. OPS CHECKED OK. PERFORMED ECU BITE, TESTED OK. REPLACED SURGE VALVE, NO HELP IAW AMM 49-53-01. TIGHTENED THE APU INLET TEMP SENSOR IAW AMM 49-6103&, OPS CHECKED OK.

Part: WARNING MESSAGE — FALSE ACTIVATION (RT ENGINE) · airframe 67,877 hrs · 14,709 cycles

STATUS MESSAGE FOR THE RT ENGINE PRV. PERFORMED AN AIR SUPPLY BITE TEST IAW AMM 36-33-00. MESSAGES CLEARED. PERFORMED AN ENGINE RUN IAW AMM 71-00-00. NO MESSAGES ILLUMINATED.

Part: CIRCUIT CARD — MALFUNCTIONED (RT ENGINE) · airframe 67,868 hrs · 14,706 cycles

MOMENTARY RT ENGINE PRV ADVISORY MESSAGE DISPLAYED AFTER TAKEOFF. REPLACED THE BLEED AIR CONTROL CARD IAW AMM 36-11-16.

Part: VALVE — INOPERATIVE (RT ENGINE) · airframe 67,858 hrs · 14,703 cycles

DURING DESCENT AT APPROX 5000 FT MSL WITH THRUST REDUCED TO IDLE, RT ENGINE PRV ADVISORY MESSAGE DISPLAYED. REMOVED AND REPLACED RT ENGINE PRV IAW AMM 36-11-18, OPS CHECKED GOOD.

Part: VALVE — DEFECTIVE (BLEED AIR SYS) · airframe 67,858 hrs · 14,703 cycles

NR 2 PRV NOT HOLDING PRESSURE. R&R NR 2 ENGINE PRV IAW AMM 36-11-18.

Part: VALVE — DEFECTIVE (BLEED AIR SYS) · airframe 67,858 hrs · 14,703 cycles

NR 1 PRV NOT HOLDING PRESSURE. R&R NR 1 ENGINE PRV AND PRV CONTROLLER IAW AMM 36-11-19, 36-11-18. NO LEAKS FOUND.

Part: CONTROLLER — FAULTED (SHUTOFF VALVE) · airframe 67,858 hrs · 14,703 cycles

NR 1 ENGINE HPSOV SHOWS CONTROLLER FAULT. R & R THE NR 1 ENGINE HPSOV CONTROLLER IAW AMM 36-11-08. LEAK AND BITE CHECKED GOOD.

Part: VALVE — FAULTY (BLEED AIR SYS) · airframe 67,858 hrs · 14,703 cycles

NR 1 FAN AIR VALVE CONTROLLER FAULT. R&R NR 1 FAN AIR VALVE IAW AMM 36-11-17.

Part: TRANSMITTER — FAILED (LT ENGINE) · airframe 67,821 hrs · 14,690 cycles

NR 2 ENGINE LOW OIL PRESSURE LIGHT DOES NOT ILLUMINATE. R & R THE NR 2 ENGINE OIL PRESSURE TRANSMITTER IAW AMM 79-32-01. OPS CHECKED GOOD.

Part: LIGHT — NO INDICATION (NR 2 ENGINE) · airframe 67,807 hrs · 14,685 cycles

NR 2 ENGINE OIL PRESSURE LOW LIGHT DOES NOT ILLUMINATE. REMOVED AND REPLACED RT OIL PRESSURE LIGHT IAW AMM 33-13-00, OPS CHECKED GOOD.

Part: WARNING MESSAGE — FALSE ACTIVATION (EXHAUST FAN) · airframe 67,712 hrs · 14,653 cycles

AFT EQUIPMENT EXHAUST FAN 2 STATUS MESSAGE. MESSAGE CLEARED IAW AMM 21-58-00.

Part: APU — INOPERATIVE · airframe 67,695 hrs · 14,645 cycles

APU INOPERATIVE.

Part: PRESSURE SWITCH — FAILED (ANTI-ICE SYSTEM) · airframe 67,579 hrs · 14,603 cycles

EICAS MESSAGE FOR THE LEFT WING ANTI-ICE. PULLED AND THE RESET THE CIRCUIT BREAKERS A31, T20, FOR THE ANTI-ICE SYSTEM, THEN REMOVED AND REPLACED THE LEFT WING TAI PRESSURE SWITCH IAW AMM 30-11-04, OPS CHECKED GOOD.

Part: WARNING MESSAGE — FALSE ACTIVATION (ANTI-ICE VALVE) · airframe 67,557 hrs · 14,592 cycles

LEFT WING ANTI-ICE VALVE EICAS MESSAGE WITH LT WING ANTI-ICE VALVE LIGHT ON. ACCOMPLISHED A WING ANTI-ICE OPERATIONAL CHECK IAW AMM 30-11-00, OPS CHECKED GOOD.

Part: TRANSCEIVER — MALFUNCTIONED (WEATHER RADAR) · airframe 67,470 hrs · 14,558 cycles

STATUS MESSAGE WXR SYSTEM RT SIDE. REPEAT SQUAWK. REMOVED AND REPLACED RT WEATHER RADAR TRANSCEIVER IAW AMM 34-43-01. OPS CHECK GOOD.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 67,460 hrs · 14,554 cycles

DURING T/O ROLL, CLIMB AND INTERMITTENTLY DURING FLIGHT WXR FAIL MESSAGE. PERFORMED WEATHER RADAR SYSTEM BITE PROCEDURE IAW FIM 34-43-00-810-801 FAULT TREE 805. NO FAULTS NOTED AT THIS TIME. PERFORMED MAINTENANCE MESSAGE ERASE PROCEDURE IAW AMM 31-41-00-912-009. AFTER PERFORMING WEATHER RADAR BITE PROCEDURE, NO MESSAGE NOTED AT THIS TIME.

Part: WARNING MESSAGE — FALSE ACTIVATION (WX RADAR SYS) · airframe 67,428 hrs · 14,542 cycles

WEATHER RADAR SYS STATUS MESSAGE AND WEATHER RADAR FAIL DISPLAYED ON HSI WHEN LT SYS SELECTED. ACCOMPLISHED FIM 34-43 FT 805 SYSTEM OK, OPS CHECK NORMAL.

Part: WARNING MESSAGE — FALSE ACTIVATION (WEATHER RADAR) · airframe 67,391 hrs · 14,526 cycles

WEATHER RADAR SYS STATUS MESSAGE. CARRIED OUT THE WEATHER RADAR BITE TEST IAW FIM 34-43 FT 805, TESTED OK. MESSAGE CLEARED.

Part: VALVE — MALFUNCTIONED (APU) · airframe 67,335 hrs · 14,507 cycles

APU INOPERATIVE. REMOVED AND REPLACED APU SURGE VALVE IAW AMM 49-53-01, PERFORMED ENG START & RUN USING APU IAW AMM 71-00-00. BOTH ENGINE STARTS GOOD WITH NO DEFECTS NOTED.

Part: ENGINE — UNKNOWN (LEFT) · airframe 67,332 hrs · 14,506 cycles

ONE UNSUCCESSFUL START ATTEMPT MINIMUM N1 NOT REACHED AT 30 SECOND, LEFT ENGINE

Part: WARNING MESSAGE — FALSE ACTIVATION (WX RADAR SYS) · airframe 67,290 hrs · 14,490 cycles

LEFT WEATHER RADAR FAILED ON THE NAVIGATIONAL DISPLAY. WXR SYS STATUS MESSAGE. PERFORMED AN OPS CHECK IAW AMM 34-43-00, OPS CHECKED NORMAL.

Part: OIL FILTER — WARNING LIGHT (LEFT) · airframe 67,282 hrs · 14,487 cycles

LEFT OIL FILTER STATUS MESSAGE. REMOVED AND REPLACED THE OIL FILTER IAW 79-21-08. LEAK & CHECKED OK.

Part: WARNING LIGHT — MALFUNCTIONED (FIRE DETECTOR) · airframe 67,270 hrs · 14,482 cycles

YELLOW FAIL P-RESER DOES NOT COME ON DURING THE FIRE DETECTOR, SYSTEM FAILED. RESET FIRE DETECTION SYSTEM AFTER 10 SECONDS, FAIL P.RESET LIGHT AND EICAS MESSAGE CAME ON. AFTER RESET IT WENT AWAY IAW AMM 26-10-00.

Part: HEAT EXCHANGER — LEAKING (LEFT) · airframe 67,270 hrs · 14,482 cycles

LEFT HEAT EXCHANGER LEAKING AT FRONT. INSPECTED AND TIGHTENED THE CLAMPS. LEAK CHECKED GOOD IAW AMM 21-51-02.

Part: CONTROLLER — NO TEST (LT ENGINE) · airframe 67,270 hrs · 14,482 cycles

LEFT ENGINE PRESSURE CONTROLLER OPEN & CLOSE FAILED TO TEST. REMOVED AND REPLACED THE CONTROLLER ASSY IAW AMM 36-11-08, OPS CHECKED NORMAL.

Part: LINE — CRACKED (WATER EXTRACT) · airframe 67,270 hrs · 14,482 cycles

WATER EXTRACTOR BOTTOM LINE IS CRACKED IN TWO PLACES. REMOVED AND REPLACED THE WATER EXTRACTOR LINE. OPS CHECKED GOOD, NO LEAKS IAW AMM 21-51-04.

Part: CONNECTOR — BROKEN (FLOW CONTROL) · airframe 67,270 hrs · 14,482 cycles

LEFT ATC BAY FLOW CONTROL CONNECTOR BROKEN. REMOVED AND REPLACED THE CONNECTOR, OPS CHECKED NORMAL IAW AMM 20-62-12.

Part: CONNECTOR — DIRTY (OIL FILTER) · airframe 67,270 hrs · 14,482 cycles

EICAS STATUS MESSAGE FOR THE LEFT OIL FILTER DISPLAYED. CLEANED THE LEFT ENGINE DIFFERENTIAL OIL PRESSURE SWITCH CONNECTOR. OPS CHECKED NORMAL IAW AMM 79-21-08.

Part: SEAL — LEAKING (RT A/C PACK) · airframe 67,270 hrs · 14,482 cycles

RIGHT PACK LEAKING AT THE PRIMARY HEAT EXCHANGER UPPER CLAMP. REMOVED AND REPLACED THE SEALS, OPS CHECKED NORMAL, NO LEAKS IAW AMM 21-51-02.

Part: NOZZLE — OBSTRUCTED (LT A/C PACK) · airframe 67,270 hrs · 14,482 cycles

LEFT PACK WATER SPRAY NOZZLE COMPLETELY BLOCKED. REMOVED THE BLOCKAGE, OPS CHECKED NORMAL IAW AMM 21-53-05.

Part: START VALVE — DEFECTIVE (RT ENGINE) · airframe 67,232 hrs · 14,466 cycles

RT ENGINE START EICAS MESSAGE START VALVE NOT OPENING, SECOND GATE RETURN, RT ENGINE STARTER EICAS MESSAGE, X2 START VALVE LIGHT REMAINS ILLUMINATED. MANUALLY CYCLED START VALVE, OPS CHECKED THE START VALVE IAW AMM 80-71-02, AND 71-00-00. OPS CHECKED GOOD. REMOVED AND REPLACED THE RT ENGINE START VALVE IAW AMM 80-11-02. OPS CHECKED GOOD.

Part: WARNING LIGHT — FALSE ACTIVATION (OIL FILTER) · airframe 67,233 hrs · 14,467 cycles

LEFT OIL FILTER EICAS. PERFORMED AN ENGINE RUN IAW AMM 71-00-00. MESSAGE CLEARED, NO DEFECTS NOTED.

Part: SEAL — LEAKING (APU BEARING) · airframe 67,223 hrs · 14,462 cycles

OIL LIKE SUBSTANCE DRIPPING FROM APU AREA OF AIRCRAFT. PERFORMED AN APU LEAK CHECK IAW AMM 49-16-00-206-012, FOUND A LEAK FROM THE BEARING SEAL AREAS.

Part: LAMP — INOPERATIVE (ANNUNCIATOR) · airframe 67,150 hrs · 14,434 cycles

LEFT ENGINE VALVE DID NOT ILLUMINATE WHEN FUEL CONTROL MOVED FROM CUT OFF TO RUN. FOUND DEBRIS INSIDE OF THE LIGHT, CLEANED AND REPLACED THE LAMP, PRESS TO TEST OK,TESTED LEFT FUEL VALVE SOLENOID AND LIGHT IAW AMM 71-00-00, REMOVED AND REPLACED LT ENG VALVE ANNUNCIATOR LIGHT IAW AMM 33-16-02 AND OPS CHECKED OK IAW AMM 71-00-00.

Part: WARNING MESSAGE — FALSE ACTIVATION (LT OIL FILTER) · airframe 67,166 hrs · 14,440 cycles

AFTER ENGINE START, THE LT OIL FILTER ADVISORY MESSAGE APPEARED FOR ONE MINUTE. THEN IT CONVERTED INTO A STATUS MESSAGE. TEMP IN CVG AT ENGINE START WAS -14C 7 DEG 7. IAW AMM 71-00-00, CONFIG 3, PAGE 271. ENGINE OPS NORMAL. AIRCRAFT OK FOR SERVICE.

Part: PRESSURE SWITCH — FAILED (ENGINE OIL) · airframe 67,145 hrs · 14,432 cycles

STATUS MESSAGE FOR THE LT OIL FILTER. REPLACED THE OIL FILTER DIFFERENTIAL PRESSURE SWITCH ON THE NR 1 ENGINE IAW AMM 79-35-01, OPS CHECKED GOOD, NO LEAKS NOTED.

Part: LIGHT — MALFUNCTIONED (SPAR VALVE) · airframe 67,101 hrs · 14,412 cycles

LEFT ENGINE SPAR VALVE LIGHT. REPLACED THE NR 1 FUEL SPAR VALVE LIGHT DRAWER ASSY IAW AMM 33-13-00. OPS CHECKED NORMAL.

Part: WARNING MESSAGE — FALSE ACTIVATION (LT OIL FILTER) · airframe 67,106 hrs · 14,414 cycles

STATUS MESSAGE FOR THE LT OIL FILTER. CLEARED THE STATUS MESSAGE ,NO OTHER ISSUES NOTED IAW AMM 79-35-00.

Part: PRESSURE SWITCH — DIRTY (OIL SYSTEM) · airframe 67,068 hrs · 14,392 cycles

LEFT OIL FILTER STATUS MESSAGE DURING SHUTDOWN. CLEANED THE LT ENGINE DIFFERENTIAL PRESSURE OIL SWITCH. SYSTEM CHECKED GOOD IAW MM 79-35-00.

Part: WARNING MESSAGE — FALSE ACTIVATION (OIL FILTER) · airframe 67,053 hrs · 14,384 cycles

DURING LEFT ENGINE START, HAD A LT OIL FILTER EICAS MESSAGE DISPLAY. PERFORMED ENGINE RUN IAW AMM 71-00-00, MESSAGE CLEARED NO DEFECTS NOTED.

Part: A/C PACK — INOPERATIVE (LEFT) · airframe 67,032 hrs · 14,373 cycles

LEFT PACK INOPERATIVE IN ANY MODE.

Part: WARNING LIGHT — FALSE ACTIVATION (COCKPIT TEMP) · airframe 67,032 hrs · 14,373 cycles

FLIGHT DECK TEMPPERATURE LIGHT ILLUMINATED ON OVERHEAD PANEL. PERFORMED FIM 21-61-00 FT 815 FOUND ZONE TEMP CONTROLL OPERATING NORMAL BITE CHECK OK AND VALVE FOLLOWS SWITCH IN FLIGHT DECK AND ON EICAS ECS PAGE.

Part: WARNING MESSAGE — FALSE ACTIVATION (RT ENGINE) · airframe 66,914 hrs · 14,298 cycles

STATUS MESSAGE FOR THE RT ENGINE SPEED CARD. PERFORMED AN OPS CHECK OF THE NR 1 ENGINE SPEED CARD IAW FIM 73-21, FT 871 , MESSAGE CLEARED, OPS CHECKED NORMAL.

Part: SENSOR — INOPERATIVE (RT A/C PACK) · airframe 66,831 hrs · 14,254 cycles

RIGHT PACK INOPERATIVE IN AUTO AND STANDBY. REMOVED AND REPLACED RIGHT PACK CABIN AIR SENSOR IAW AMM 21-61-02.

Part: DUCT — DAMAGED (RT A/C PACK) · airframe 66,742 hrs · 14,225 cycles

FOUND A DAMAGE DUCT FOR THE RT PACK, THREADS ARE GONE AT SENSOR FOR THE RT COMPRESSOR OUTLET. REPLACED THE RT PACK OUTLET DUCT.

Part: SHUTOFF VALVE — MALFUNCTIONED (PNUEMATIC SYS) · airframe 66,680 hrs · 14,202 cycles

DURING CLIMB & DESCENT, LEFT PRESSURE VARIES & SURGES 10 PSI TO 40 PSI TO 10 PSI, OPERATES NORMALLY ON GROUND AND CRUISE. REMOVED AND REPLACED LG PRSOV IAW AMM 36-11-09, OPS CHECKED GOOD.

Part: VALVE — FAILED · airframe 66,663 hrs · 14,196 cycles

DURING CLIMB OUT, 5000 FT THRU 15000 FT, THE LEFT DUCT PRESSURE SURGED FROM AROUND 40 PSI TO 10 PSI CONSTANTLY. DURING DESCENT, LEFT DUCT PRESSURE FLUCTUATED BY 30 PSI FROM 40 TO 10 PSI CONSTANTLY. SHUT THE LEFT PACK OFF TO MITIGATE SURGE. R & R PRV IAW AMM 36-11-18, OPS CHECKED GOOD, NO DEFECT NOTED.

Part: VALVE — INOPERATIVE (LEFT) · airframe 66,650 hrs · 14,193 cycles

LEFT ENGINE DUCT PRESSURE FLUCTUATED DURING CLIMB. REMOVED AND REPLACED FAMV, VALVE HANGS UP. LT FAMV HAS OPEN CIRCUIT BETWEEN CONNECTORS D2378A PIN 8A AND V343 PIN 1 IAW AMM 36-11-16. FAMV REACTIVATED, CLEANED ELECTRICAL TERMINAL STRIPS. FAMV CHANGED. OPS AND LEAK CHECKED GOOD IAW AMM 36-11-16.

Part: WARNING SYSTEM — ACTIVATED (BLEED AIR SYS) · airframe 66,672 hrs · 14,199 cycles

LT ENGINE BLEED OFF LIGHT ILLUMINATED. REF MDDR 89004 DUPLICATE WRITE UP. CLEARS MDDR 83993. PLACARDS REMOVED. MCC NOTIFIED.

Part: VALVE — MALFUNCTIONED · airframe 66,640 hrs · 14,190 cycles

AFTER TAKEOFF, THE LEFT ENGINE BLEED STARTED SURGING BETWEEN 10 T0 30 PSI UNTIL FL 240, AND THEN STABILIZED. LEFT BLEED MATCHED WITH RIGHT IN CRUISE EACH WAYPOINT 35-40 PSI AT FL 360 NO EICAS MESSAGES OR STATUS MESSAGE. REPLACED FAMV AND CLEANED TERMINAL STRIPS. OPS CHECKED GOOD IAW AMM 76-11-16, & 36-11-09.

Part: MODULE — MALFUNCTIONED (APU) · airframe 66,634 hrs · 14,188 cycles

APU, NO BLEED AIR. REMOVED AND REPLACED FLOW SENSING MODULE, OPS CHECKED NORMAL IAW AMM 49-53-08.

Part: A/C PACK — SURGES (LEFT) · airframe 66,620 hrs · 14,182 cycles

DURING DESCENT, THE LEFT PACK SURGED CONTINUOUSLY BETWEEN 20 AND 40 PSI. PERFORMED AN OPS CHECK, NO DEFECTS NOTED IAW AMM 21-51-00.

Part: VALVE — FAULTED (CABIN TEMP) · airframe 66,586 hrs · 14,169 cycles

AFT CABIN TEMP EICAS DISPLAYED WITH AFT CABIN AUTO INOPERATIVE LIGHT ILLUMINATED DURING TAXI. REMOVED AND REPLACED THE AFT CABIN TRIM AIR VALVE ACTUATOR IAW AMM 21-61-07, OPS CHECKED GOOD.

Part: SWITCH — FAILED (BOOST PUMP) · airframe 66,570 hrs · 14,164 cycles

LEFT AFT BOOST PUMP INOPERATIVE. REMOVED AND REPLACED THE LEFT AFT BOOST PUMP PUSH BUTTON SWITCH IAW SWPM 20-84-18. SWITCH AND BOOST PUMP OPS CHECKED GOOD IAW AMM 28-00-00.

Part: WARNING MESSAGE — FALSE ACTIVATION (FUEL PUMP) · airframe 66,566 hrs · 14,163 cycles

LEFT AFT FUEL PUMP MESSAGE, AMBER STATUS WHEN PUMP IS OFF. PERFORMED AN OPS CHECK IAW AMM 28-22-00. OPS CHECKED NORMAL.

Part: SEAL — LEAKING (APU OIL SYS) · airframe 66,555 hrs · 14,160 cycles

DURING A DAILY INSPECTION, FOUND APU OIL LEAKING FROM THE OIL COOLER BYPASS VALVE. REMOVED AND REPLACED TWO SEALS IAW 49-27-10. NO LEAKS NOTED.

Part: UNKNOWN — VIBRATION (UNKNOWN ENGINE) · airframe 66,499 hrs · 14,141 cycles

DURING DESCENT, WHEN ACFT HAS LEVELED AND AUTOTHROTTLES ARE ADVANCED FROM IDLE, THE ACFT EXPERIENCES AN AIRFRAME SHAKING & BOOM. UNABLE TO CONFIRM WHICH ENGINE, HOWEVER IT HAPPENED 3 TIMES DURING DESCENT. PERFORMED TROUBLSHOOTING IAW FIM 71-05 F/T 808, NO DEFECTS NOTED. INSPECTED THE ENGINE, NO DEFECTS NOTED. PERFORMED AN AIRFRAME VIBRATION CONDITION INSPECTION. NO DEFECTS NOTED, RAN BOTH ENGINES TO 70 PERCENT N1, NO FAULTS NOTED.

Part: UNKNOWN — MALFUNCTIONED (WEATHER RADAR) · airframe 66,380 hrs · 14,103 cycles

RADAR SPIKING INTERMITTENTLY. OPS CHECKED WX RADAR IAW AMM 34-43-00, OPS CHECKED NML AT TIME.

Part: O-RING — LEAKING (ENGINE OIL CAP) · airframe 66,332 hrs · 14,089 cycles

RIGHT ENG OIL CAP O-RING LEAKING. REMOVED AND REPLACED THE RT ENGINE OIL TANK CAP O-RING IAW AMM 79-11-03, LEAK CHECKED OK.

Part: FASTENER — LOOSE (VIBE MONITOR) · airframe 66,320 hrs · 14,085 cycles

NR 1 ENG VIBE MONITOR ERRATIC. INSP FOUND LOOSE HARDWARE & CLAMPS FRO ENG FAN, ACCELEROMETER T677 TIGHTENED. SECURED HARDWARE, RAN ENG. NO LONGER ERRATIC & WITHIN LIMITS IAW AMM 71-00-00, OPS CK GOOD.

Part: VALVE — FAILED · airframe 66,277 hrs · 14,069 cycles

AFT CABIN TEMP EICAS MESSAGE DURING CRUISE. QRH COMPLIED WITH, ASSOCIATED AFT CABIN CONTROLLER INOPERATIVE. REMOVED AND REPLACED TRIM MODULATING VALVE IAW AMM 21-61-07, OPS CHECKED NORMAL.

Part: DETECTION SYS — INOPERATIVE (ICE) · airframe 66,256 hrs · 14,061 cycles

ICE DETECTION AUTO INOPERATIVE. ICE DETECTION ON EICAS SYSTEM SHOULD HAVE BEEN OFF (+13C). PERFORMED OPS CHECK OF THE ICE DETECTION SYSTEM IAW AMM 30-81-00-715-017, OPS CHECKED GOOD.

Part: SKIN — DENTED (NR 2 NACELLE) · airframe 66,241 hrs · 14,056 cycles

TWO DENTS FOUND ON THE OUTBOARD NR 2 ENGINE NACELLE DURING A PREFLIGHT, WALKAROUND. ACCOMPLISHED PART ONE IAW EO #1971A145, PART 2 DVI EVERY 25 FLT CYCLES. PART 3 PERMANENT REPAIR PRIOR TO 1,000 FLT HRS.

Part: SHUTOFF VALVE — MALFUNCTIONED (LT ENGINE) · airframe 66,202 hrs · 14,044 cycles

LEFT ENGINE HPSOV EICAS MESSAGE ON LANDING, FOLLOWED BY A LT ENG HPSOV STATUS MESSAGE. REMOVED AND REPLACED HPSOV IAW AMM 36-11-07, OPS CHECKED GOOD IAW AMM 36-11-07.

Part: WARNING LIGHT — ILLUMINATED (PUMP PRESSURE) · airframe 66,196 hrs · 14,042 cycles

LEFT FWD FUEL PUMP PRESSURE LIGHT STAYS ILLUMINATED.

Part: WARNING MESSAGE — FALSE ACTIVATION (SHUTOFF VALVE) · airframe 66,194 hrs · 14,041 cycles

LEFT ENGINE HPSOV STATUS MESSAGE. PERFORMED ENGINE RUN FOR OPS CHECK OF HPSOV NO DEFECTS NOTED AT THIS TIME IAW MM 36-11-07.

Part: FIRE WARNING — FALSE ACTIVATION (LEFT NACELLE) · airframe 66,191 hrs · 14,040 cycles

LT ENGINE FIRE LOOP 2 EICAS MESSAGE. ACCOMPLISHED FIM 26-11FT 805 AND TESTED IAW AMM 26-11-00-815-805. NO DEFECTS NOTED.

Part: ACTUATOR — FAILED (APU DOOR) · airframe 66,183 hrs · 14,037 cycles

APU INLET DOOR CIRCUIT BREAKER TRIPPED. REPLACED THE APU DOOR ACTUATOR IAW 49-15-60. OPS CHECKED GOOD.

Part: WARNING LIGHT — FALSE ACTIVATION · airframe 66,179 hrs · 14,036 cycles

STATUS FOR HIGH FLOW INHIBIT. OPS CHECKED IAW FIM 21-51 FAULT TREE 813. NO DEFECTS NOTED AT THIS TIME.

Part: WIRE — OPEN (WINDOW HEAT) · airframe 66,173 hrs · 14,034 cycles

LEFT WINDOW HEAT EICAS MESSAGE. PERFORMED CONTINUITY CHECK FROM D4294J TO D1922, FOUND OPEN WIRE, BSD SPLICE ON WIRE W624-209R-24. IAW WDM 30-41-12. SPLICED THE WIRE IAW SWPM 20-30-12. PERFORMED OPS CHECK OF L2 WINDOW HEAT IAW AMM 30-41-00, OPS CHECKED GOOD. NO DEFECTS NOTED.

Part: STARTER — INOPERATIVE (APU) · airframe 66,135 hrs · 14,021 cycles

APU WILL NOT START. REMOVED & REPLACED THE STARTER MOTOR IAW AMM 49-41-004. OPS NORMAL,

Part: CONTROL PANEL — MALFUNCTIONED (START VALVE) · airframe 66,115 hrs · 14,013 cycles

RIGHT ENGINE START VALVE LIGHT DID NOT CYCLE DURING START. ENGINE STARTED NORMALLY. REMOVED AND REPLACED THE IGNITION AND STARTING PANEL IAW AMM 80-11-51. OPS CHECKED NORMAL.

Part: GROUND WIRE — DISCONNECTED (START VALVE) · airframe 66,127 hrs · 14,017 cycles

RIGHT ENGINE START VALVE LIGHT DIDN'T CYCLE DURING ENGINE START. ENGINE STARTED NORMALLY. FOUND GROUND TERMINAL DISCONNECTED, CONNECTED THE TERMINAL IAW SWPM 20-30-11, PERFORMED TEST 3 IAW MM 71-00-00. OPS CHECKED GOOD.

Part: CIRCUIT CARD — FAILED (N2 SPEED) · airframe 66,113 hrs · 14,012 cycles

WHEN RT STARTER ENGAGED TO GROUND LEFT AND RIGHT UTILITY BUSS AND LEFT HYD SYSTEM PRESSURE EICAS MESSAGE APPEAR.WHEN THEY SHOULD BE INHIBITED REPEAT ITEM SEE LOG PAGE 830589(<P>TROUBLESHOOT PER F.I.M 71-01 TAK A08 AND AMM 80-11-00 SUSPECT N2 SPEED CARD AT FAULT. REMOVED AND REPLACED N2 SPEED CARD PER AMM 73-21-54 CHECKS GOOD.AND NOT PRESENT DURING ENGINE START.</P>)

Part: GENERATOR — UNKNOWN (APU) · airframe 66,113 hrs · 14,012 cycles

APU GENERATOR INOPERATIVE. OPS CHECK IAW AMM 49-11-00, OPS CHECK NORMAL.

Part: VALVE — MALFUNCTIONED (RT IDG) · airframe 66,092 hrs · 14,005 cycles

STATUS MESSAGE. RT IDG VALVE. REMOVED AND REPLACED IDG COOLING VALVE IAW AMM 24-11-07, OPS CHECKED NORMAL.

Part: SKIN — DELAMINATED (NR 2 NACELLE) · airframe 66,092 hrs · 14,005 cycles

DURING A WALK AROUND, THE NR 2 ENGINE FAN COWL HAS AN AREA OF DELAMINATION. REMOVED, AND REPAIRED IAW AMM 71-11-04-714-001-400. INSTALLED IAW AMM 71-11-04/401.

Part: ACTUATOR — FAILED (APU FUEL SHUTOFF) · airframe 66,092 hrs · 14,005 cycles

FUEL VALVE INDICATION TEST FAILED. REMOVED AND REPLACED THE APU FUEL SHUTOFF VALVE ACTUATOR IAW AMM 28-25-02, OPS CHECKED OK.

Part: WARNING MESSAGE — ILLUMINATED (HYD SYSTEM) · airframe 66,090 hrs · 14,004 cycles

AFTER ENGINE START, SWITCH SELECTED TO GROUND LT & RT UTILITY BUSS AND LT HYD SYSTEM PRESSURE EICAS MESSAGE. PERFORMED NR 2 ENGINE IDLE START PROCEDURES AND RUNS IAW AMM 72-00-00 OPS CHECKED GOOD, NO DEFECTS NOTED. REMOVED AND REPLACED C904 & BTB AS PRECAUTION. SYSTEM CHECKED NORMAL IAW MM 24-23-03.

Part: PUMP — MALFUNCTIONED · airframe 66,062 hrs · 13,996 cycles

LEFT AND RIGHT CENTER OVERRIDE PUMPS INOPERATIVE. PERFORMED A FUNCTIONAL TEST OF LEFT AND RIGHT CENTER TANK OVER RIDE, JETTISON FUEL PUMP. FAILED ON PROTECTION SYSTEM IAW AMM 28-22-00 POST SB 767-28A0085 TEST PASS ON BOTH PUMP, NO FAULTS NOTED. OPS NORMAL OK FOR SERVICE.

Part: BEAM — DAMAGED (NR 2 STRUT) · airframe 66,058 hrs · 13,995 cycles

ENG NR 2 STRUT AFT FAN COWL ATTACHING HINGE BEAM DAMAGE ON LT, ALSO BRACKET FORWARD OF BEAM AT LT DAMAGED. WORK ACCOMPLISHED PER REA MF02465R0211 AND RFTA 02465-0211 REV NEW DATE 23 APR 2017 APPROVAL REF FAA FORM 8100-9 PENDING. ADDITIONAL REF SR 3-3883259508 SRM 54-52-02 IDENTIFICATION 1.

Part: ACTUATOR — MALFUNCTIONED (RAM AIR DOOR) · airframe 66,058 hrs · 13,995 cycles

RT AIR CONDITION RAM AIR INLET DOOR STUCK DURING OPERATION. RT AIR CONDITION RAM AIR INLET DOOR ACTUATOR REPLACED PER MM 21-53-03.

Part: TRANSMITTER — MALFUNCTIONED (RT OIL TEMP) · airframe 66,058 hrs · 13,995 cycles

NO DISPLAY ON EICAS RIGHT OIL TEMP. OIL TRANSMITTER REPLACED IAW MM 29-32-01.

Part: CHECK VALVE — BROKEN (PNEUMATIC SYS) · airframe 66,058 hrs · 13,995 cycles

PNEUMATICS SYSTEM LT AFT WALL CHECK VALVE SPRING BROKEN. PNEUMATIC SYSTEM LT AFT AC WALL CHECK VALVE REPLACED PER AMM 36-11-05.

Part: SEAL — TORN (LT WING) · airframe 66,058 hrs · 13,995 cycles

LT WING LE NR 2 AND NR 5 SLAT ANTI ICE DUCTS TORN COUPLINGS SEALS. LT WING LE NR 2 AND NR 5 SLAT ANTI ICE DUCTS TORN COUPLING SEALS REPLACED PER MM 30-11-06.

Part: CONTROL UNIT — FAULTY (APU) · airframe 66,058 hrs · 13,995 cycles

APU BLEED AIR DOES NOT INCREASE. APU CONTROL UNIT REPLACED PER AMM 49-61-05.