N1013A

Part: FIRE LOOP — FALSE INDICATION (ZONE 100) · airframe 92,037 hrs · 15,176 cycles

AFTER LANDING STATUS MSG "MN CARGO LOOP 2" ILLUMINATED. ACCOMPLISHED FIM 26-14 FT 809 BLOCKS 1-2-3-4-5-6 AND 7 AFTER AFOLTS TEST, NO MN CARGO LOOP 2 PRESENT. CARGO SMOKE DETECTION SYSTEM OK. AIRCRAFT RETURNED TO SERVICE.

Part: PCB — DEFECTIVE (ZONE 100) · airframe 91,935 hrs · 15,141 cycles

RED MAIN DECK CARGO FIRE WARNING WITH ASSOCIATED LIGHTS AND MASTER CAUTION INTERMITTENTLY EVERY 5 MINS.MTX GROUNDED A/C .MTX REMOVED AND REPLACED PRINTED CIRCUIT CARD IN P54 M2026 IAW B767 AMM 26-10-01 & OPS CHECKS GOOD & NO FAULTS NOTED AT THIS TIME. AND RETURNED A/C TO SERVICE.

Part: OVERHEAT LOOP — FALSE INDICATION (ZONE 100) · airframe 91,932 hrs · 15,140 cycles

INTERMITENT MN CARGO LP 1 AND 2 STATUS MESSAGE W/FIRE WARNING.MTX GROUNDED A/C AND PERFORM MAIN CARGO/ENG/APU/FIRE/OVHT TEST. IAW AMM 26-14-00. OPS CHECKED NORMAL. NO MSG. RETURNED ACFT TO SERVICE.

Part: BATTERY — FAULTED (ZONE 100) · airframe 91,709 hrs · 15,058 cycles

DURING TAXI ,APU BATTERY, NO STBY STATUS MESSAGE DISPLAYED. ADVISED BY MTC TO RETURN TO PARKING (BTB). MTX GROUNDED ACFT AND REMOVED AND REPLACED APU BATTERY IAW AMM 24-31-04 AND REMOVED AND REPLACED APU BATTERY CHARGER IAW AMM 24-31-04. OPS CHECK GOOD. ACFT REMAINS NO ETOPS.AND RETURNED AC TO SERVICE.

Part: WARNING MESSAGE — ILLUMINATED (CARGO DOOR) · airframe 91,158 hrs · 14,847 cycles

PER MXC REQUEST VERIFY LOCK POSITION IN MCD , A/C RETURNED TO THE GATE AND GROUNDED BY MTX, MTX THEN VERIFIED LOCK RBL:33, LBL:33 +LBL:11 PREVIOUSLY INSTALLED IN STA.756.45, RELOCATED TO STA.755.45 IAW BCF CMM 25-51-70. ALL LOCKS SECURED. AND RETURNED A/C TO SERVICE.

Part: DIRECTOR — MALFUNCTIONED (ZONE 200) · airframe 90,961 hrs · 14,776 cycles

AFTER TAKE-OFF, RT FLIGHT DIRECTOR DISAPPEARED TROUBLE SHOT IT AFTER 18K AND COULDN'T GET RESOLUTION SWITCHED RIGHT SIDE TO CENTER AND SGL SOURCE FD TCAS MSG APPEARED. MX MADE CALL TO RETURN TO AFW, (ATB) DEFERRED RT FLIGHT DIRECTOR SYSTEM IAW MEL C ABX-34-22-4A. RETURNED AIRCRAFT TO SERVICE.

Part: PUMP — WARNING MESSAGE (ZONE 500) · airframe 90,551 hrs · 14,619 cycles

DURING TAXI, L FWD FUEL PUMP EICAS MSG DISPLAYED AFTER ENGINE START. A/C RECTURNED TO GATE. (BTB) DEFERRED L FWD FUEL PUMP FOR DEPARTURE IAW MEL ABX-28-22-1. MTX RETURNED A/C TO SERVICE.

Part: PUMP — INOPERATIVE (RT FUEL) · airframe 89,845 hrs · 14,354 cycles

DURING TAXI OUT THE RIGHT HAND AFT FUEL PIMP INOP MSG APPEARED AFTER ENGINE START A/C RETURNED TO GATE (BTB) AND MTX GROUNDED A/C . MTX FOUND INCORRECT BREAKER WAS LOCKED OUT FOR LH PUMP DEFERRAL . RESET RH BREAKER AND COLLARED CORRECT BREAKER.OPS CHECK GOOD RETURNED A/C TO SERVICE

Part: PUMP — WARNING MESSAGE (LT FUEL) · airframe 89,839 hrs · 14,351 cycles

DURING TAXIOUT THE L FWD FUEL PUMP EICAS MSG APPEARED AND AC RETURNED TO BLOCK (BTB) AND MAINTENANCE GROUNDED AC .MTX DEFERRED LH FWD FUEL PUMP IAW MEL ABX-28-22-1 . AND RETURNED AC TO SERVICE .

Part: FIRE WARNING — FALSE ACTIVATION (ZONE 200) · airframe 89,795 hrs · 14,336 cycles

DURING LOADING OF AIRCRAFT MAIN DECK CARO FIRE WARNING ACTIVATED MULTIPLE TIMES.FIRE DEPARTMENT CAME AND DECLARED NO SIGNS OF FIRE OR SMOKE IN MCD, OR LOWER CARGOS. MX PERFORMED TEST OF TAIM TEST BOXES PER B767 AMM 26-14-00, NO FAULTS NOTED. PERFORMED AFOLTS SYSTEM CHECK AND VISUALLY INSPECTED FIRE CARD M2026 IN P54 PANEL PER B767 AMM 26-10-00. NO FAULTS NOTED AIRCRAFT RELEASED NON ETOPS.AC REMAINS IN SERVICE

Part: WARNING MESSAGE — ILLUMINATED (LT FUEL PUMP) · airframe 89,571 hrs · 14,247 cycles

AFTER ENGINE START L FWD FUEL PUMP EICAS ILLUMINATED DURING TAXI.AC RETURNED TO BLOCK AND MTX GROUNDED AC , DEFERRED FOR DEPARTURE .IAW MEL ABX-28-22-1 AC WAS RETURNED TO SERVICE AND AC DEPARTED .

Part: FITTING — CORRODED (LT WING) · corrosion level 2 · airframe 89,176 hrs · 14,093 cycles

LH WING FWD LOAD PITCH FITTING, CORROSION DAMAGE ON INB FITTING.(<P>CORROSION ON INBD FITTING WAS REWORKED IAW TRE6757246, REV 1, MAY 20, 2024. LEVEL CORROSION 2. NO FURTHER DEFECTS NOTED.</P>)

Part: SHOE — WORN (NLG BRAKE) · airframe 89,176 hrs · 14,093 cycles

NOSE LANDING GEAR BOTH BRAKE SHOES OF WHEELS UPPER GEAR WITH WEAR(<P>NOSE LANDING GEAR BRAKE SHOES OF WHEELS WERE REPLACED I.A.W. AMM 32-45-05-022-001 REV. 142 DATE 22 APR 24 AND AMM 32-45-05-422-007.REV. 142 DATE 22 APR 24. TORQUE APPLIED 35 IN LB , S/N 1222912342 DATE.11 JUL 24 I.A.W. AMM 20-11-00-910-802 REV. 142 DATE 22 APR 24. NO FURTHER DEFECTS NOTED.</P>)

Part: SKIN — CORRODED (NR 1 NACELLE) · corrosion level 2 · airframe 89,176 hrs · 14,093 cycles

PYLON #1 UPPER SURFACE, CORROSION DAMAGE ON THE BUSHING OF THE INBD LUG OF FWD UPPER SPAR FITTING.(<P>REPAIR FOR CORROSION DAMAGE ON THE BUSHING OF THE INB LUG OF FWD UPPER SPAR FITTING WAS ACCOMPLISHED IAW TRE 6754190 ISSUED DATE MAY 16,2024. FAA FORM 8100-9 DATE 21-MAY-2024. CORROSION</P> / <P>LEVEL 2. NO FURTHER DEFECTS NOTED.</P>)

Part: BUSHING — EXCESS PLAY (NLG DOOR) · airframe 89,176 hrs · 14,093 cycles

NOSE LANDING GEAR AFT DOORS BOTH WITH EXCESSIVE PLAY IN THE PIVOT POINTS(<P>NOSE LANDING GEAR AFT DOORS BOTH WITH EXCESSIVE PLAY IN THE PIVOT POINTS, BUSHINGS WERE REPLACED AIW AMM 32-21-01-404-036 REV 142 22-APR-24 STEP H (29) TORQUE APPLIED 60 FT LB / SERIAL TORQUE: 722111529 / DATE EXP: 10-DEC-24. OPS CHK GOOD.</P>)

Part: SKIN — DENTED (RT WING TE FLAP) · airframe 89,176 hrs · 14,093 cycles

RH WING, INBOARD FLAP, MAIN FLAP, AT 2" FROM TRAILING EDGE AND 6" FROM INBOARD EDGE, DENT ON UPPER SKIN(<P>RH WING, INBOARD FLAP, MAIN FLAP WAS REPAIRED IAW SRM 57-53-01-2R-1 TABLE I FIG 201 SHEET 5 PAG.2,3,6 AND SRM 51-70-03-0G-0 PAR 5.A FIG.5 PAG 10,11,25 REV 49 APR 15/2024. NO FURTHER DEFECTS NOTED.</P>)

Part: VENT — MISINSTALLED (RT WING) · airframe 89,176 hrs · 14,093 cycles

RIGHT WING MAIN, TANK, BETWEEN RIB 19 AND RIB 18, FUEL DUCT VENT, LOCKWIRE MISSING ON BOTH NUT RETAINER(<P>RIGHT WING MAIN TANK, BETWEEN RIB 19 AND RIB 18, FUEL DUCT VENT, LOCKWIRE WAS INSTALLED CORRECTLY IAW AMM 20-10-23-420-801 REV 142, APR 22,2023; TORQUE APPLIED TO THE ACCESS DOOR 40 IN-LBS S/N 0823900243, DATE 15-NOV-2024. CHECK FOR LEAKS IAW TASK M6728451 CDCCL. NO FURTHER DEFECTS NOTED</P>)

Part: SKIN — DELAMINATED (RT AILERON) · airframe 89,176 hrs · 14,093 cycles

RH WING, INBOARD AILERON, TRAILING EDGE, RH SIDE WITH DELAMINATION(<P>RH WING, INBOARD AILERON, TRAILING EDGE, RH SIDE WAS REPAIRED IAW SRM 57-60-01-2R-1 REPAIR 1 TABLE II FIG 201 PAG 1-6 AND SRM 51-70-03-0G-0 PAR 5A(2) FIG 12 PAG 10,11, 36 REV 49 APR 15/2024. NO FURTHER DEFECTS NOTED.</P>)

Part: BONDING JUMPER — BROKEN (LT MLG) · airframe 89,176 hrs · 14,093 cycles

MAIN LANDING GEAR WELL LH PART AFT LOWER (STA 1065 ) WITH BROKEN BONDING BUMPER ON APU FUEL DRAIN LINE(<P>MAIN LANDING GEAR WELL, LEFT REAR LOWER STA 1065 BONDING BUMPER REPLACED ON APU FUEL DRAIN LINE I.A.W SWPM 20-20-10 REV. 85 DATE 15 FEB 24 BONDING APPLIED 1.1 MILLI-OHMS NS B0007830 DATE 13DIC2024. OPS CHK GOOD.</P>)

Part: CONTROL CABLE — ABNORMAL (LT ELEVATOR) · airframe 89,176 hrs · 14,093 cycles

SECTION 48 INTERNAL AREA, LH ELEVATOR CONTROL CABLE RUBBING WITH PULLEY BRACKET (DUE BAD INSTALLATION) LOCATED AT B. STA 1605.5 LH SIDE.(<P>SECTION 48 INTERNAL AREA, LH ELEVATOR CONTROL CABLE RUBBING WITH PULLEY BRACKET (DUE BAD INSTALLATION) LOCATED AT B. STA 1605.5 LH SIDE WAS REPLACED IAW B767 SRM 51-10-02-0G-0 REV. 49 15-APR-</P> / <P>24. OPS CHK GOOD.</P>)

Part: SKIN — PUNCTURED (LT ELEVATOR) · airframe 89,176 hrs · 14,093 cycles

LH INB ELEVATOR UPPER PANEL, PUNCTURE AT ELEV STA 104.2 APPROX. AND 28" FROM T.EDGE.(<P>LH INBOARD ELEVATOR, UPPER PANEL WAS REPAIRED IAW SRM 55-20-01-2R-1 REPAIR 1 FIG 201 TABLE I PAG 1-3, SRM 51-70-04-0G-0 PAR.5.B PAG.16 AND SRM 51-70-17-0G-0 PAR 4.B FIG.24 PAG.14,55 REV 49 APR 15/2024. NO FURTHER DEFECTS NOTED</P>)

Part: NONE — NONE (NONE) · airframe 89,176 hrs · 14,093 cycles

FAA AGING INSPECTION RH A/A PACK EXHAUST RAM AIR ACTUATOR BONDING LEAD WITH WIRES BROKEN.(<P>RH A/A PACK EXHAUST RAM AIR ACTUATOR BONDING LEAD WAS REPLACED IAW AMM TASK 21-53-03-404-012 REV. 142, APR 22, 2024. BONDING TEST WAS PERFORMED 0.003 MILLIOHMS. BONDING S/N: 2568 DATE NEXT: 14/FEB/2025. NO FURTHER DEFECTS NOTED.</P>)

Part: METERING VALVE — LEAKING (STEERING) · airframe 89,176 hrs · 14,093 cycles

NOSE LANDING GEAR STEERING VALVE WITH HYDRAULIC LEAK IN THE BODY(<P>NOSE LANDING GEAR STEERING METERING VALVE WAS REPLACED IAW AMM 32-51-04-404-013 REV. 142 22-APR-24. OPS CHK GOOD.</P>)

Part: SKIN — DELAMINATED (RT AILERON) · airframe 89,176 hrs · 14,093 cycles

RH WING, INBOARD AILERON, TRAILING EDGE, RH SIDE WITH DELAMINATION(<P>RH WING, INBOARD AILERON, TRAILING EDGE, RH SIDE WAS REPAIRED IAW SRM 57-60-01-2R-1 REPAIR 1 TABLE II FIG 201 PAG 1-6 AND SRM 51-70-03-0G-0 PAR 5A(2) FIG 12 PAG 10,11, 36 REV 49 APR 15/2024. NO FURTHER DEFECTS NOTED.</P>)

Part: SKIN — DENTED (LT WING TE FLAP) · airframe 89,176 hrs · 14,093 cycles

LH WING, INBOARD FLAP SURFACE LEADING EDGE AREA UPPER OUTSIDE CORNER WITH TWO DENTS.(<P>LH WING, INBOARD FLAP, MAIN FLAP WAS REPAIRED IAW SRM 57-53-01-2R-1 FIG 201 SHEET 5 PAG 2-6 AND SRM 51-70-17-0G-0 PAR 4.A FIG 10 PAG 13,14,34 REV 49 APR 15/-2024. NO FURTHER DEFECTS NOTED.</P>)

Part: SKIN — PUNCTURED (LT ELEVATOR) · airframe 89,176 hrs · 14,093 cycles

LH INB ELEVATOR UPPER PANEL, PUNCTURE AT ELEV STA 104.2 APPROX. AND 28" FROM T.EDGE.(<P>LH INBOARD ELEVATOR, UPPER PANEL WAS REPAIRED IAW SRM 55-20-01-2R-1 REPAIR 1 FIG 201 TABLE I PAG 1-3, SRM 51-70-04-0G-0 PAR.5.B PAG.16 AND SRM 51-70-17-0G-0 PAR 4.B FIG.24 PAG.14,55 REV 49 APR 15/2024. NO FURTHER DEFECTS NOTED.</P>)

Part: EVAS UNIT — UNKNOWN (UNKNOWN) · 13,414 cycles

CAPTAINS EVAS IS INOP(<P><SPAN>REMOVED AND REPLACED CAPTAINS EVAS AS PER 25-60-00 (AMM) OPS CHECKED NORMAL.</SPAN></P>)

Part: SMOKE GOGGLES — UNKNOWN (UNKNOWN) · airframe 87,099 hrs · 13,367 cycles

FIRST OBSERVERS SMOKE GOGGLES INOP(<P>TRANSFERRED TO MDDR 185104 PER MEL 25-11-02-01A CAT A DUE 17MAT23. PLACARDS INSTALLED. LOGPAGE 1773702 M3: REMOVED AND REPLACED FIRST OBSERVERS SMOKE GOGGLES IAW AMM 25-64-00. THIS ACTION CLEARS DMI 185109. MCC NOTIFIED. PLACARD REMOVED</P>)

Part: FIRST AID KIT — NONE · airframe 85,953 hrs · 12,976 cycles

FIRST AID KIT NEXT TO OVHEAD BIN COMPROMISED MISSING RED SEAL.(<P>REMOVED AND REPLACED FIRST AID KIT IW B767 AMM 25-64-03.</P>)

Part: NONE — NONE · airframe 85,949 hrs · 12,974 cycles

CORROSION DAMAGE ON RIGHT INBOARD TE FLAP TORQUE TUBE(<P>RIGHT INBOARD TE FLAP TORQUE TUBE WAS REPLACED IAW SB 767-57A0066</P>)

Part: NONE — NONE · airframe 85,949 hrs · 12,974 cycles

MANIFOLD WITH HYDRAULIC LEAKAGE EVIDENCE WAS FOUND IN VERTICAL STABILIZER BETWEEN REAR SPAR AND FIN STA 100 / FIN STA 125.(<P>TORQUE WAS CHECKED / CORRECTED ON THE AFFECTED MANIFOLD CONNECTIONS AS WELL AS TORQUE STRIPE APPLICATION WAS PERFORMED PER EO 6729A019.</P>)

Part: NONE — NONE · airframe 85,949 hrs · 12,974 cycles

EVIDENCE OF MICROBIAL GROWTH ON INTERNAL STRUCTURE OF CENTER AUXILIARY AND MAIN WING TANKS(<P>EVIDENCE OF MICROBIAL&NBSP;<SPAN>GROWTH </SPAN><SPAN>WAS ELIMINATED PER AMM 28-11-00-107-081</SPAN></P>)

Part: NONE — NONE · airframe 85,949 hrs · 12,974 cycles

FUEL LEAKAGE EVIDENCE IN INBOARD LEFT WING AT RIB 9, ACCESS PANEL 533AB(<P>FUEL LEAKAGE WAS REPAIRED PER AMM 28-11-00-308-013</P>)

Part: NONE — NONE · airframe 85,949 hrs · 12,974 cycles

LEAKAGE EVIDENCE IN THE AFT LH ACMP HYDRAULIC LINE CONNECTION OF THE LH ENG STRUT NACELLE, 437BL ACCESS.(<P>AFFECTED HYDRAULIC LINE WAS CHECKED / CORRECTED AND FOR SUCH REASON THE LEAKAGE WAS ELIMINATED.</P>)

Part: NONE — NONE · airframe 85,949 hrs · 12,974 cycles

SEVERAL DENTS WERE FOUND BETWEEN 5:00 TO 8:00 HRS OF RH INLET COWL ACOUSTIC PANEL(<P>DENTS WERE REPAIRED IN ACCORDANCE WITH B767 SRM 54-15-01-2R-3 REPAIR 3 AND EO 1971A291</P>)

Part: NONE — NONE · airframe 85,949 hrs · 12,974 cycles

RIGHT WHEEL WELL ALTERNATING CURRET MOTOR PUMP C1 AND C2 WITH DRAIN LEAK(<P>PUMP ASSEMBLIES WERE REPLACED AND THE TEST LEAK WAS PERFORMED IN EACH PUMP ASSY (NIL FINDINGS). OFF PART SN MX629963 &AMP; MX540177 / PN 731966 &AMP; 731966</P>)

Part: NONE — NONE · airframe 85,949 hrs · 12,974 cycles

RH WING OUTBOARD FLAP ACCESS PANEL "666MT" WITH DENT AT 5 INCH FROM INTERNAL PANEL EDGE AND 25 INCH FROM FLAP TRAILING EDGE(<P>DENT WAS REPAIRED PER SRM 57-53-01-2R-1 AND 51-70-10-2R-0.</P>)

Part: NONE — NONE · airframe 85,949 hrs · 12,974 cycles

PRESSURIZATION LEAKAGE EVIDENCE ON EXTERNAL DOUBLERS INSTALLED IN UPPER FUSELAGE SKIN SURFACE AT BODY STA 434 / STA 654+22(<P>SEALANT WAS REPLACED AROUND OF EXTERNAL DOUBLERS&NBSP;<SPAN>INSTALLED IN UPPER FUSELAGE SKIN SURFACE AT BODY STA 434 / STA 654+22</SPAN></P>)

Part: NONE — NONE · airframe 85,949 hrs · 12,974 cycles

LEAKAGE EVIDENCE IN THE LINE CONNECTIONS OF THE LH ENG STRUT TRAILING EDGE FAIRING, 437DB ACCESS.(<P><SPAN>AFFECTED HYDRAULIC CONNECTIONS WERE CHECKED / CORRECTED AND FOR SUCH REASON THE LEAKAGE WAS ELIMINATED</SPAN></P>)

Part: NONE — NONE · airframe 85,949 hrs · 12,974 cycles

FUEL LEAKAGE EVIDENCE IN LH WING CENTER SECTION LOWER SURFACE AT SPLICE STRINGER L-6 AND WBL115(<P>FUEL LEAKAGE WAS REPAIRED PER AMM 28-11-00-308-013</P>)

Part: NONE — NONE · airframe 85,949 hrs · 12,974 cycles

LEAKAGE EVIDENCE IN AFT RH HYDRAULIC "T" CONNECTION OF THE LH ENG STRUT NACELLE, 437BR ACCESS.(<P>AFFECTED CONNECTION WAS CHECKED / CORRECTED AND FOR SUCH REASON THE LEAKAGE WAS ELIMINATED</P>)

Part: NONE — NONE · airframe 85,949 hrs · 12,974 cycles

HYDRAULIC LINES / CONNECTIONS WITH LEAK EVIDENCE WERE FOUND IN VERTICAL STABILIZER BETWEEN REAR SPAR AND FIN STA 58 / FIN STA 79.(<P>TORQUE WAS CHECKED / CORRECTED ON THE AFFECTED HIDRAULIC LINES / CONNECTIONS AS WELL AS TORQUE STRIPE APPLICATION WAS PERFORMED PER EO 6729A019.</P>)

Part: NONE — NONE · airframe 85,949 hrs · 12,974 cycles

THREE DENTS ON ENGINE #2 PRIMARY EXHAUST OUTER SKIN BETWEEN 6/8 O´CLOCK AND BETWEEN NAC STA 323.42/344.67(<P>WELD FILL REPAIR IAW BOEING MSG: CMA-TLS-22-0022-02B</P>)

Part: NONE — NONE · corrosion level 2 · airframe 85,949 hrs · 12,974 cycles

CORROSION ON ACCESS PANEL SUPPORT FOR KEEL BEAM BETWEEN STA 889 TO STA 915.5(<P>ACCESS PANEL SUPPORT P/N 145T8629-2 WAS REPLACED PER PRODUCTION DRAWING AND SRM 51-10-02</P>)

Part: NONE — NONE · airframe 85,949 hrs · 12,974 cycles

WEAR ON OUTBOARD CORNER AT OSS 682.74 OF SLAT #9, RH WING(<P>WEAR WAS REPAIRED IN ACCORDANCE WITH B767 SRM 51-70-10-2R-4.</P>)

Part: NONE — NONE · airframe 85,949 hrs · 12,974 cycles

SEVERAL DENTS WERE FOUND ON LH INLET COWL ACOUSTIC PANEL(<P>DENTS WERE REPAIRED IN ACCORDANCE WITH E.O 1971A291</P>)

Part: NONE — NONE · airframe 85,949 hrs · 12,974 cycles

PUNCTURE ON LH ELEVATOR LOWER SKIN AT 44 INCH OF THE INBOARD CLOUSURE RIB AND 26 INCH OF THE TRAILING EDGE.(<P>AFFECTED AREA WAS REPAIRED ON LH ELEVATOR LOWER SKIN IAW SRM 55-20-01-2R-1 &AMP; 51-70-17-0G-0</P>)

Part: NONE — NONE · airframe 85,949 hrs · 12,974 cycles

RH WING OUTBOARD FLAP ACCESS PANEL "666KT" WITH DENT AT 33 INCH FROM EXTERNAL PANEL EDGE &AMP; 25 INCH FROM FLAP TRAILING EDGE AND SECOND ONE AT 68 INCH FROM EXTERNAL PANEL EDGE &AMP; 25 INCH FROM FLAP TRAILING EDGE.(<P>DENTS WERE REPAIRED PER SRM 57-53-01-2R-1 AND 51-70-10-2R-0.</P>)

Part: NONE — NONE · airframe 85,499 hrs · 12,841 cycles

AP. 21939. FIRST OFFICERS PTT SWITCH INTERMITTENT.(<P>COMPLIED&NBSP; AP-21939. R/R PTT S551 &AMP; S552 IAW AMM 23-51-03. FLT INT. F/O SYS OPS CHECK OK PER AMM 23-51-00.&NBSP;</P>)

Part: NONE — NONE · airframe 85,499 hrs · 12,841 cycles

LOWER CARGO SMOKE DETECT LOOP 2 INOP ( LOWER CARGO COMPARTMENT FIRE DETECTION SYSTEMS ( FWD AND AFT ) DETECTOR LOOPS)(<P>T/S PER W/D&NBSP; &AMP; SSM&NBSP; 26-16-01; TAIM&NBSP; M12281 &AMP;&NBSP; TAIM&NBSP; M12273&NBSP; ARE&NBSP; NOT&NBSP; CONNECTED (NC)&NBSP; TO LOOP 2&NBSP; LWR FWD&NBSP; COMPARTMENT. TEST OF TAIM (6) OK = M12277, M12276, M12278, M12279, M12284 &AMP; M12285 PER AMM 26-14-00-865.</P> / <P>MDDR # 167808 CLEARED UP.</P>)

Part: TAPE — NONE · airframe 85,499 hrs · 12,841 cycles

MAIN DECK CARGO DOOR FORWARD AND AFT DOOR FRAME HAS LOOSE AND WORN TAPE.(<P><SPAN>REMOVED&NBSP; AND&NBSP; REPLACED&NBSP; LOOSE&NBSP; AND&NBSP; WORN&NBSP; TAPE&NBSP; AT&NBSP; MAIN DECK&NBSP; BY&NBSP; CARGO&NBSP; DOOR&NBSP; CUT OUT&NBSP; FWD&NBSP; &AMP;&NBSP; AFT&NBSP; PER&NBSP; B767-300&NBSP; &NBSP; AMM&NBSP; &NBSP; 25-52-10-308-159</SPAN></P>)

Part: NONE — NONE · airframe 85,499 hrs · 12,841 cycles

#2 ENG EXHAUST CASE ( CORE COWL ) RUB PADS HAS SEVERAL LOOSE/WORN PADS(<P><SPAN>REMOVED AND REPLACED LOOSE&NBSP; OR&NBSP; WORN OUT&NBSP; RUB PADS&NBSP; AT # 2 ENG.&NBSP; EXHAUST&NBSP; CORE&NBSP; COWL PER&NBSP; B767-300&NBSP; SRM 51-40-02-0G-0.</SPAN></P>)

Part: DRIVE SHAFT — NONE · airframe 85,499 hrs · 12,841 cycles

#2 ENGINE O/B T/REV FAILED MECHANICAL BRAKE TEST(<P>REMOVED AND REPLACED&NBSP; # 2 ENGINE&NBSP; O/B&NBSP; T/REV&NBSP; &NBSP;FLEXIBLE&NBSP; DRIVE SHAFT&NBSP; AS PER BOEING&NBSP; 767&NBSP; AMM 78-31-18.&NBSP; PERFORMED&NBSP; &NBSP;MECHANICAL&NBSP; BRAKE TEST.&NBSP; OPS CHECK&NBSP; NORMAL&NBSP; AT THIS TIME&NBSP; AS PER&NBSP; BOEING 767&NBSP; AMM 78-30-00.</P>)

Part: NONE — NONE · airframe 85,499 hrs · 12,841 cycles

#1 NACELLE STRUT REAR ACCESS PANEL BOTH HOLD OPEN RODS DAMAGED(<P><SPAN>REMOVED &AMP; REPLACED BOTH&NBSP; HOLD OPEN RODS FOR # 1&NBSP; NACELLE&NBSP; STRUT REAR ACCESS PANEL AS PER AMM 20-11-00.</SPAN></P>)

Part: NONE — NONE · airframe 85,499 hrs · 12,841 cycles

COCKPIT PORTABLE OXYGEN FULL FACE MASK LENS FRAME DAMAGED P/N 10800C15F(<P><SPAN>REMOVED&NBSP; AND&NBSP; REPLACED&NBSP; PORTABLE&NBSP; OXYGEN&NBSP; FULL&NBSP; FACE&NBSP; MASK&NBSP; AS&NBSP; PER&NBSP; &NBSP;B767-300&NBSP; &NBSP;AMM&NBSP; 35-31-00.</SPAN></P>)

Part: ROLLER — NONE · airframe 85,499 hrs · 12,841 cycles

LWR. FUSELAGE AVIONICS COMPTARTMENT ACCESS DOOR FWD ROLLER IS WORN - OUT(<P>REMOVED &AMP; REPLACED&NBSP; FWD ROLLER AT ELECTRONICS&NBSP; COMPARTMENT&NBSP; ACCESS DOOR&NBSP; IAW&NBSP; B767&NBSP; AMM 20-11-00.</P> / <P>OPERATIONAL CHECK&NBSP; IS NORMAL IAW B767&NBSP; AMM 52-48-04.</P>)

Part: SEALANT — DETERIORATED · airframe 85,499 hrs · 12,841 cycles

#1 ENG I/B T/REV INTERIOR SURFACE HAS DETERIORATED FIRE RESISTANT SEALANT (PREPARED&NBSP; CLEANED & NBSP; AND&NBSP; REPAIRED&NBSP; DETERIORATED&NBSP; FIRE&NBSP; RESISTANT SEALANT&NBSP; AT&NBSP; #&NBSP; 1 ENG ; T/REV&NBSP INNER&NBSP; SURFACE&NBSP; PER&NBSP; B767-300&NBSP; AMM&NBSP; &NBSP;78-31-00-308-H00</P>)

Part: SKIN — GOUGED · airframe 84,821 hrs

DURING AIRCRAFT TOUCH UP PAINT MX FOUND GOUGE IN LOWER AFT SECTION OF FUSELAGE AT APPROX FS 1632 IN THE NON PRESSURIZED AREA(<P ><SPAN>REPAIRED FUSELAGE IAW B767 SRM 53-00-01-2R-12 REPAIR 12. EO 6753A992</SPAN></P> / <P>&NBSP;</P>)

Part: MASK — INOPERATIVE · airframe 84,612 hrs · 12,561 cycles

LH SUPERNUMERARY OXYGEN MASK INOP(<P>TRANSFERRED TO MDDR #161209 PER MEL 35-11-02-03A, CAT C. DUE: 23FEB22. PLACARDS INSTALLED. MCC ADVISED.</P> / <P>DISP: TS@ 1003Z.</P> / <P><SPAN>REMOVED AND REPLACED O2 MASK IAW AMM 35-11-51. OPS CHECK GOOD IAW AMM 35-11-00. THIS CLEARS MDDR 161209.</SPAN></P>)

Part: NONE — NONE · airframe 84,348 hrs · 12,481 cycles

CREW OXYGEN PRESSURE READS 40PSI ON EICAS INDICATION INOP.(<P>TRANSFER TO MDDR 159293 IAW MEL 35-11-02-01, CAT B.</P> / <P>LP 1604090 -&NBSP; REMOVED AND REPLACED VOLTAGE AVERAGING UNIT IAW AMM 35-11-06. OPS CHECK GOOD AT THIS TIME. THIS CLEARS MDDR 159293.</P>)

Part: NONE — NONE · 12,372 cycles

EMERGENCY LIGHT SWITCH WIRE CLIP IS LOOSE AND DOES NOT FUNCTION PROPERLY(<P>SECURED EMERGENCY LIGHT SWITCH WIRE CLIP IAW AMM 33-51-08. PERFORMED LIGHT TEST IAW AMM 33-51-08. OPS CHECK GOOD.</P>)

Part: CIRCUIT BREAKER — TRIPPED (APU FIRE DETECT)

APU FIRE LP1 AFTER EXT POWER DISC(<P><SPAN>RESET FIRE LOOP BREAKER IAW B767 AMM 20-60-01</SPAN></P>)

Part: NONE — NONE

AFTER EXT POWER DISC DUCT PSI FALLS TO ABOUT 10PSI W/ PACKS ON(<P><SPAN>PLACED ON MDDR 156389 IAW MEL 49-11-01-01 CAT C DUE 17NOV21&NBSP;</SPAN></P> / <P><SPAN>EH 1155Z REFENCE LOG 1386918 ITEM M14 CVG 07NOV INSPECTED APU COMPARTMENT DUCTS AND PERFORMED BLEED AIR OPC IAW AMM 49-57-01. OPC NORMAL. ALSO PERFORMED ENGINE DRY MOTOR. N2 SPEED/29 PERCENT IAW AMM 71-00-00.THIS CLEARS DMI 156389, MCC NOTIFIED, PLACARD REMOVED</SPAN></P>)

Part: NONE — NONE

WHEN EXT PWR SELECTED ON AFTER BOCK IN APU SHUT DOWN WITH ASSOCIATED EICAS MESSAGE APU FAULT(<P><SPAN>PREFORMED APU BITE PROCEDURES IAW B767 FIM 49-11 FAULT TREE 987 NO FAULT S NOTED APU OPS CHECK GOOD NO FURTHER MX ACTION REQUIRED&NBSP;</SPAN></P>)

Part: EEC — NONE

WHILE DESCENDING THROUGH FL210 L/H N1 WAS 25% HIGHER THAN R/H N1. L/H N1 &AMP; ENG INDICATION WAS HIGHER THAN R/H IND SIGNIFICANTLY(<P><SPAN>PERFORMED L/H ENG PIMU BITE PROCEDURE PER FIM 71-01 FT 810, FOUND FAULT CODES 35220-A, 155/9-A, &AMP; 15519-B. INSPECTED PS3 LINE AND FOUND MOISTURE IN LINE AND L/H EEC PER FIM 71-01 TASK A &AMP; B, REMOVED&NBSP; AND&NBSP; REPLACED L/H EEC PER B767 AMM 73-2115. PERFORMED TEST NO 11 &AMP; 12 PER AMM 77-00-02. BOTH TEST WERE GOOD.&NBSP; OPS CHECK GOOD, NO FURTHER DEFECTS NOTED AT THIS TIME</SPAN></P>)

Part: NONE — NONE

ON DESCENT THRUST LEVER (LEFT) IN IDLE POSITION N1 57% VS RT N1 47% NO CHNAGE WITH ANTI-ICE ON. UPON MATCHING N1'S OIL PRESS 47PSI.(<P><SPAN>PERFORMED IDLE RUNS AND FOUND NO SPLIT AT THIS TIME. DONE IAW 71-00-00</SPAN></P>)

Part: NONE — NONE

EVENT RECORD @ 1900Z FL360 TAT- 28 SAT- 57: R ENG PARAMETERS HIGHER THAN L ENG CAUSING FUEL IMBALANCE LOW 1000LBS ON R TANK. RAN ENG ANTI-ICE FOR A FEW MINUTES AND R&AMP;L ENG MATCHED BACK UP.(<P>PARAMETERS WITHIN LIMITS IAW AMM 71-00-00. NO HISTORY OR DEFECTS NOTED AT THIS TIME.</P> / <P>LOGPAGE # 1373267 - RAN ENG ANTI ICE FOR A FEW MINUTES AND R AND L ENGINE MATCHED.</P>)

Part: SENSOR — NONE · 12,333 cycles

"FWD EQ SUP FAN 1" STATUS MSG.(<P>ITEM TRANSFERRED TO MDDR 155847 PER MEL 21-58-03-02-01. CAT C, DUE 07NOV21.&NBSP;</P> / <P>REF LOG 1373264 - C/W AP-20899, REMOVED AND REPLACED SUPPLY EXHAUST FAN CURRENT SENSOR IAW 21-58-11. OPS CKS GOOD. THIS CLEARS MDDR 155847.</P>)

Part: ECU — NONE

"R ENG EEC C1" STATUS MSG(<P>REMOVED AND REPLACED RH ENG EEC IAW B767 AMM 73-21-15. PERFORMED EEC STATIC TEST IAW B767 AMM 71-00-00. NO DEFECTS NOTED.</P>)

Part: NONE — NONE

AFTER T/O DURING CLIMB R ENG CONTROL STATUS MESSAGE DISPLAYED. R ENG CONTROL ADVISORY MESSAGE DISPLAYED AFTER LANDING.(<P>PERFORMED FIM TASK 73-21 FT 878, TOOK ABOVE 70% ENGINE RUN IAW AMM 71-00-00, OPS CHECK GOOD. ALSO PERFORMED BITE ON PIMU, NO FAULTS. IAW FIM 71-01-00.</P>)

Part: RELAY — NONE

EICAS MSG FWD EQ. SUP FAN(<P>TRANSFER TO MDDR 155529, CAT C. DUE 01NOV21, DDG 21-58-03-02-01. PLACARD INSTALLED&NBSP;</P> / <P>REF LOG 1386863 #4 CVG - REMOVED &AMP; REPLACED LEFT ECS FAN CONTROL CARD M861 IAW 21-58-42. NO HELP. OPS CHECK BAD. SEE LOGPAGE 1386863 ITEM M5 FOR FURTHER T/S. T/S PER FIM 21-58 FT 991. T/S UP TO STEP 25 ON SHEET 3 AND FOUND CONTINUITY BETWEEN PIN 5 AND PIN 6 OF THE FWD RACK SUPPLY FAN 1 (B10). NEXT STEP REQUIRES REPLACEMENT OF LEFT ECS FAN CONTROL CARD (M861).T/S IAW FIM 21-58 FT 991 BLOCK 25. REMOVED &AMP; REPLACED EQUIP COOLING SUPPLY FAN 1 RELAY K343 IAW B767 WDM 21-58-14, OPS CHECK GOOD. THIS CLEARS DMI 155529 AND W/O #87552. CARD P/N OFF 285T0078-15 S/N OFF D02220&NBSP;</P>)

Part: CONTROLLER — NONE

COCKPIT TEMP CONTROL ERRATIC IN AUTO. TRIM VALVE CYCLES FULL OPEN AND CLOSED. COCKPIT TEMP HOT. TEMPERATURE CONTROLLED IN MAN MODE ONLY.(<P>TRANSFER TO MDDR # 155413 CAT "C" PER DDG 21-61-02-03. DUE 29OCT21. PLACARDS INSTALLED.</P> / <P>LOG PAGE 1480331: REMOVED AND REPLACED CABIN ZONE TEMP CONTROLLER IAW 21-61-03. OPS CHECK GOOD. THIS CLOSES MDDR 155413.</P>)

Part: NONE — NONE

FORWARD EQUIPMENT COOLING FAN EICAS MESSAGE.(<P>TRANSFER TO MDDR # 155416 CAT "C" PER DDG 21-58-03-02-01. DUE 29OCT21. PLACARDS INSTALLED. MX ACTION COMPLIED WITH.</P> / <P>LP 1480327: OPS CHECKS PER AMM 21-58-06, NO DEFECTS NOTED, THIS CLEARS MDDR 155416.</P>)

Part: NONE — NONE · airframe 83,824 hrs · 12,299 cycles

LH PACK TEMP LIGHT.(<P>TRANSFERRED LH PACK TO MDDR 155285 PER MEL 21-51-01-01, CAT C. DUE DATE 27OCT21.</P> / <P>CVG MX- LP 1373294 - ITEM M3: PERFORMED GVI IAW AMM 21-51-00. FOR L/H PACK, FOUND AIR LEAK BETWEEN PACK CONTROLLER AND&NBSP; THE "T" DUCT, MDDR 155285 REMAINS OPEN.</P> / <P>21OCT21- CVG MX, LP 1480330, ITEM M3: REPLACED THE HOT AIR DUCT CABLE ASSY IAW B767-300 AMM 20-11-00. THIS ACTION CLEARS DMI# 155285. MCC JOHN NOTIFIED. ALL PLACARDS REMOVED.</P>)

Part: FAN — NONE

FWD EQUIPMENT COOLING SUPPLY FAN 1 STATUS MESSAGE.(<P>TRANSFERRED TO MDDR 154894 IAW MEL 21-58-03-02-01, CAT 'C'.</P> / <P>LOG PAGE 1373282: REMOVED AND REPLACED FORWARD RACK SUPPLY COOLING FAN IAW AMM 21-58-06. OPS CHECK GOOD. THIS CLEARS MDDR 154894.</P>)

Part: BOTTLE — NONE

O2 BOTTLE DAMAGED DURING REPLACEMENT FOR SERVICING(<P>REMOVED AND REPLACED O2 BOTTLE IAW 767 AMM 12-15-08. LEAK AND OPS CHECK GOOD IAW 767 AMM 35-11-00.</P>)

Part: NONE — NONE

FWD EQUIP COOLING SUPPLY FAN STATUS MESSAGE.(<P>TRANSFERRED TO MDDR 154436, CAT: C, MEL 21-58-03-02-01. DUE 11OCT21. MCC NOTIFIED. PLACARDS INSTALLED.</P>)

Part: CARD — INOPERATIVE

RT ENG BLD OFF EICAS DURING DECENT PERF FIM 36-10 FT 836. AIR SUPPLY BITE HAD NO FAULTS. CHECKED FOR ANY LEAKS , LEAK CHECK GOOD. REMOVED CONNECTOR D64 HELP PRSOV OPEN AND FOUND NO CONTUITY BETWEEN PIN 1 AND 2.R/R M860 R ENG BLEED CARD PE AMM 36-11-12. PERF R ENG RUN PER AMM 72-00-00 OPS CHECK GOOD.

Part: VALVE — INOPERATIVE · airframe 83,676 hrs · 12,257 cycles

R ENG BLEED OFF ADVISORY MSG WHEN STARTING DESCENT. AFTER LEVELING OFF AT LOWER ALTITUDE AND ADDING POWER, IT WENT AWAY. REMOVED AND REPLACED PRSOV IAW AMM 36-11-09. OPS CHECK GOOD IAW AMM 71-00-00.

Part: BLEED VALVE — FALSE INDICATION

RT ENG BLEED OFF CAUTION MSG WHEN DESCENDING THRU FL330. FOLLOWED QRH W/ NO FURTHER ISSUE.(<P>BITE TEST C/O IAW B767 FIM 36-20 FAULT TREE 804, BITE TEST SHOWS NO FAULTS, A/C OK FOR SERVICE.</P>)

Part: WIRE — DAMAGED (FUEL PUMP)

AFTER TURNING ON ALL LEFT AND RIGHT MAIN FUEL PUMPS, WE RECEIVED L AFT FUEL PUMP EICAS MESSAGE. PRESS LIGHT CAME ON LEFT AFT PUMP SWITCH ON. CB PULLED. REMOVED AND REPLACED WIRE W444-301 ,R,B,Y-18 FROM AFT SPAR SPLICE TO CONNECTOR D4408P IAW SWPM CHAP 20,WDM 28-22-11 AND EO #6728A011. PERFORMED OPS TEST IAW&NBSP; 28-22-00, NO DEFECT NOTED. THIS CLEARS DMI # 152756.</P>)

Part: PUMP — FAULTED (FUEL BOOST)

L AFT FUEL PUMP EICAS MESSAGE JUST PRIOR TO ENGINE START(<P>REFERENCE LOG PAGE 1302219: T/S IAW FIM 28-22 FT 819. FOUND K10705 RELAY TRIPPED, RESET RELAY AND CHECKED POWER AT BOOST PUMP CONNECTOR D1542, FOUND 115A AT PINS 246. REMOVED AND REPLACED L AFT BOOST FUEL PUMP IAW AMM 28-22-03. OPS &AMP; LEAK CHECK GOOD. THIS CLEARS DMI 152548&NBSP;</P>)

Part: VALVE — FAULTED (LT PNEUMATIC SYS)

L ENG BLD OVHT AT FL250, RAN QRH, MESSAGE CLEARED.(<P>REMOVED AND REPLACED FAN AIR VALVE ASSY PER MCC REQUEST IAW B767 AMM 36-11-16. OPS CHECK GOOD. LEAK CHECK GOOD AT THIS TIME.</P> / <P>ITEM M10: PERFORMED HIGH POWER ENGINE RUNS IAW AMM 71-00-00 TEST PROCEDURES. NO DEFECTS FOUND AT THIS TIME. AIRCRAFT OK FOR SERVICE.</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (LT ENG BLEED) · airframe 83,398 hrs · 12,163 cycles

INFO ONLY- "L ENG BLD OVHT" EICAS DURING DESCENT. IT RESET WITH QRH PROCEDURE. NO FURTHER PROBLEMS.(<P>TROUBLESHOT IAW B767 FIM 36-20 FAULT TREE 804. NO FAULTS NOTED ON AIR SUPPLY MODULE.</P>)

Part: STARTER — FAILED (NR 2 ENGINE) · airframe 83,362 hrs · 12,152 cycles

DURING COMP. WASH OF #2 ENG, STARTER FAILED.(<P>REMOVED AND REPLACED #2 ENG STARTER IAW AMM 80-11-01. OPS CHECK GOOD. NO FAULTS AT THIS TIME. PERFORMED ENGINE RUNS IAW 71-00-00 IAW AMM.</P>)

Part: SOLENOID VALVE — FAULTED (APU)

APU INOP / ( AUXILIARY POWER UNIT (APU), ER OPERATIONS NOT ALLOWED (NOTIFY DISPATCH) R60 )(<P>TRANS TO MDDR 151702 CAT "C" PER DDG 49-11-01.</P> / <P><SPAN>LP #1392425 ITEM #11: COMPLIED WITH WORK ORDER #84670 REV 1 IAW ALL JOB TASK CARDS. REMOVED AND REPLACED DE OIL SOLENOID VALVE PER W/O 84670. THIS CLEARS MDDR 151702.</SPAN></P>)

Part: ENGINE — LEAKING (RIGHT)

FO DISCOVERED SIGNS OF FLUID LEAKING FROM R ENGINE(<P>INSPECTED PER AMM 71-71-00-601 TABLE 601 AND DETERMINED TO BE WITHIN LIMITS (FUEL)</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (LT ENG BLEED)

L ENG BLD OVHT EICAS(<P><SPAN>PERFORMED BITE OF AIR SUPPLY MODULE PER AMM 36-23-00-715-001. NO FAULTS FOUND NO PRIOR HISTORY. OK TO CONTINUES.</SPAN></P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (PITOT HEAT) · airframe 83,032 hrs · 12,051 cycles

PROBE HEAT EICAS MESSAGE DISPLAYED ON GROUND WITH A ENG RUNNING DURING TAXI-IN TO PARKING.(<P>T/S IAW FIM TASK 30-31 FAULT TREE 808. FOUND NO FAULTS AT THIS TIME. OPERATIONAL TESTED PITOT STATIC PROBE ANTI-ICING SYSTEM IAW AMM 30-31-00. NO FAULTS AT THIS TIME. PERFORMED ENGINE RUNS IAW AMM 71-00-00.&NBSP;</P>)

Part: CLAMP — LOOSE (BLEED SYS) · airframe 83,017 hrs

L BLD DUCT LEAK ON EICAS WHILE RUNNING LEFT PACK ON GROUND(<P>PERFORMED GVI ON LT PACK SYSTEM FOUND SEVERAL CLAMPS LOOSE, TIGHTENED CLAMPS IAW 20-11-00. PERFORMED OPS CK IAW AMM 21-51-00, OPS CKS GOOD, MSG NOT PRESENT</P>)

Part: CONTROL VALVE — INOPERATIVE (RT A/C PACK) · airframe 83,017 hrs

R PACK INOP ( AIR CONDITIONING PACKS, -200/-300 (NOTIFY DISPATCH) (ER RESTICTIED R-60) ). REMOVED AND REPLACED RH PACK FLOW CONTROL VALVE ASSY FOR RH PACK. OPS CHECKS AND INDICATION NORMAL.

Part: WARNING MESSAGE — FALSE ACTIVATION (EXHAUST FAN) · airframe 82,953 hrs

STATUS MESSAGE/AFT EQ EXH FAN 2(<P>TRANSFERRED TO MDDR 148954 IAW 21-58-05, CAT C, DUE 01 JUL 2021.</P> / <P>21JUN21 - LP 1485615 - ITEM# 3 - PDX - T/S PER FIM 21-58-FT882. SYSTEM OPS CHECKS NORMAL. THIS CLEARS MDDR 148954.</P>)

Part: MODULE — FAULTED (FLOW SENSING) · airframe 82,935 hrs · 12,017 cycles

APU FAULT EICAS(<P>TRANSFERRED TO MDDR # 148782 IAW MEL # 49-11-01A, CAT "C", DUE DATE: 27JUN21. MX ACTION C/W. DISP: BM @ 2214Z.</P> / <P>LP 1392596 ITEM #3: PER AP-20218 REMOVED AND REPLACED FLOW SENSING MODULE AND GASKET IAW B767 AMM 49-53-08, OPS CHECK GOOD, NO FAULTS AT THIS TIME, CLEARED DMI 148782, PLACARD REMOVED, MCC NOTIFIED.</P> / <P>LP 1392598 ITEM #9 RE-OPENED MDDR # 148782. REPLACED APU.

Part: INDICATION SYS — FALSE INDICATION (APU DUCT) · airframe 82,910 hrs

LOW APU DUCT PRESSURE(<P>PERFORMED APU DUCT PRESSURE CHECK IAW AMM 36-00-00. APU DUCT PRESSURE NORMAL</P>)

Part: ACOUSTIC PANEL — DEBONDED (NR 2 ENGINE) · airframe 82,876 hrs · 11,999 cycles

FOUND ACOUSTICAL PANEL AFT OF THE FAN BLADES REPAIR DEBONDED #2 ENGINE.(<P>TRANSFERRED TO NON-MEL 148016, AMM 72-00-00-206-167-H00 TABLE 642 CAN CONTINUE IN OPERATION FOR 10 FLIGHT CYCLES OR 100 FLIGHT HOURS.</P><P>REMOVED AND REPLACED ACCUSTICAL LINER PANEL AT 4 OCLOCK ON ENG # 2IAW AMM 72-33-01. THIS CLEARS NON MEL 148016. MCC NOTIFIED.</P>)

Part: FIRE WARNING — FALSE ACTIVATION (MAIN CARGO) · airframe 82,780 hrs · 11,972 cycles

MAIN CARGO FIRE WARNING DURING LOADING.(<P>PERFORMED AUTOMATIC FIRE/OVERHEAT TEST IAW AMM 26-10-00-716-019. SYS OPS CHECK GOOD.</P>)

Part: FILTER — DIRTY (COCKPIT TEMP) · airframe 82,683 hrs · 11,946 cycles

IN CRUISE FLIGHT DECK TRIM AIR POSITION INDICATORSUDDENLY WENT FULL WARM AND COCKPIT TEMP. ROSE. FLIGHT DECK TEMP OK @ FULL COLD POSITION- OPERATIO9N ERRATIC(<P>PERF. ZONE TEMP CONTROL BITE PER FIM 21-61 F/T 912 FOUND NO FAULTS. FOUND FD TEMP FILTER FULL OF DEBRIS. CLEANED FILTER OPS CHECK FD TEMP CONTROL PER AMM 21-61-00. OPS CHECK GOOD .</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (RT ENGINE) · airframe 82,594 hrs · 11,920 cycles

EICAS R ENG BLEED OFF(<P>PERFORMED FIM 36-10 FAULT TREE 836. RAN RIGHT ENG IAW AMM 71-00-00, NO FAULTS NOTED, A/C OK FOR FURTHER SERVICE.</P>)

Part: IDG — FAULTED (LEFT) · airframe 82,555 hrs · 11,909 cycles

STATUS MSG, LT IDG VALVE. T/S LT IDG VALVE EICAS MESSAGE IAW FIM TASK 24-20 FAULT TREE 802. FOUND LT IDG/OIL OUT BULB WIRING MESSAGE ON BPCU. REMOVED AND REPLACED LT NR 1 IDG IAW AMM 24-11-01. OP'S CHECK GOOD.

Part: PUMP — MALFUNCTIONED (FUEL BOOST) · airframe 82,521 hrs

RIGHT FWD FUEL PUMP EICAS AT DECENT FROM 41.0 15500 LBS IN RIGHT TANK OUT AND NORMAL 90 SECS LATER(<P>REMOVED AND REPLACED RIGHT FWD FUEL BOOST PUMP 28-22-03. OPS NORMAL AT THIS TIME, ALSO BLED FUEL PRESS SENSE LINE PER AMM 28-42-01. NO DEFECTS NOTED.</P>)

Part: IDG — FAULTED (RT GENERATOR) · airframe 82,446 hrs · 11,883 cycles

R GEN OFF EICAS MESSAGE, ASSOCIATED R AND L UTIL BUS OFF, ALSO RAN CHECKLIST, WOULD NOT RESET&NBSP;(<P>PERFORMED FIM TASK 24-20 TASK 804 FIM. REPLACED DIODE R GEN PER CUSTOMER REQUEST REMOVED AND REPLACED R GEN IDG AMM 24-11-01, OPS CHECK GOOD.</P>)

Part: WARNING MESSAGE — FALSE INDICATION (RT ENG BLEED) · airframe 82,432 hrs · 11,878 cycles

RT ENG BLEED OFF EICAS(<P>PERFORMED OPERATIONAL TEST &AMP; AIR SUPPLY DISTRIBUTION SYSTEM IAW AMM 36-11-00. NO FAULTS NOTED AT THIS TIME. OPS CHECK GOOD.</P>)

Part: IDG — MALFUNCTIONED (RIGHT) · airframe 82,432 hrs · 11,878 cycles

R GEN OFF(<P>TRANSFERRED TO MDDR 144222 IAW MEL 24-00-01-01. MX ACTION C/W. PLACARDS INSTALLED. ACL 2332Z</P><P>LP&NBSP;<SPAN>1466048:&NBSP;</SPAN><SPAN>REMOVED AND REPLACED #2 ENG IDG IAW 24-11-01-404. PERFORMED LEAK CHECK, ALL OK. SERVICED IDG IAW 12-13-03/301. PERFORMED OPERATION TEST IAW 24-11-00-715-006. SYSTEM CHECKS GOOD. THIS CLEARS MDDR 144222, MCC NOTIFIED. PLACARD REMOVED.</SPAN></P>)

Part: WARNING MESSAGE — FALSE INDICATION (FUEL BOOST PUMP) · airframe 82,389 hrs · 11,864 cycles

ON TAXI OUT CTR L AND R FUEL PUMP MSG CAME ON WITH 2,000LBS FUEL IN CTR TANK(<P>4,000LBS OF FUEL ADDED TO CENTER TANK. PERFORMED OPS CHECK OF CTR L &AMP; CTR R FUEL PUMPS PER AMM 28-22-00. BOTH PUMPS OPS CHECKED GOOD.</P>)

Part: FILTER — WARNING MESSAGE (FUEL SYSTEM) · airframe 82,338 hrs · 11,848 cycles

DURING INITIAL CLIMB OUT RECEIVED EICAS AND STATUS MSG: L ENG FUEL FILT.(<P>REMOVED AND REPLACED FUEL FILTER IAW 767 AMM 73-11-03. OPS CHECK GOOD AT THIS TIME. NO FURTHER MSGS. LEAK CHECK GOOD ON LEFT ENGINE.</P>)

Part: SKIN — CRACKED (FUSELAGE) · airframe 82,327 hrs · 11,845 cycles

UPPER FUSELAGE DURING HFEC FOUND CRACKS BETWEEN RIVETS ON I/B SIDE OF ELT ANTENNA CUT OUT. NOTE OUTER SKIN(<DIV> / </DIV><P STYLE="MARGIN:0IN;MARGIN-BOTTOM:.0001PT"><SPAN>COMPLIED WITH WORK INSTRUCTIONS / BELOW AND EO6753A923</SPAN></P><P CLASS="XXMSOLISTPARAGRAPH" STYLE="MARGIN: 0IN 0IN 0.0001PT;"><SPAN>1.&NBSP;&NBSP;&NBSP;&NBSP;&NBSP;REMOVE AND DISCARD THE EXISTING / ANTENNA DOUBLER FOUND BETWEEN DOOR FRAME STATION STA911 AND STA923.7,</SPAN></P><P CLASS="XXMSOLISTPARAGRAPH" STYLE="MARGIN: 0IN 0IN 0.0001PT;"><SPAN>2.&NBSP;&NBSP;&NBSP;&NBSP;&NBSP;REMOVE THE ELT TRAY (INTERCOSTAL) / BETWEEN BSTA 1540 TO 1562 ATTACH SERVICEABLE TAG AND ROUTE TO STORES</SPAN></P><P CLASS="XXMSOLISTPARAGRAPH" STYLE="MARGIN: 0IN 0IN 0.0001PT;"><SPAN>3.&NBSP;&NBSP;&NBSP;&NBSP;&NBSP;REMOVE ELT TRAY (INTERCOSTAL) / ATTACH BRACKET AT BSTA 1540 AND 1562 ATTACH SERVICEABLE TAG AND ROUTE TO STORES</SPAN></P><P CLASS="XXMSOLISTPARAGRAPH" STYLE="MARGIN: 0IN 0IN 0.0001PT;"><SPAN>4.&NBSP;&NBSP;&NBSP;&NBSP;&NBSP;AT BOTH REMOVED BRACKET LOCATION / OF THE FRAME AT BSTA 1540 AND 1562 ACCOMPLISH OPEN HOLE HFEC INSPECTION FOR NO / CRACK CONDITION &NBSP;</SPAN></P><P CLASS="XXMSOLISTPARAGRAPH" STYLE="MARGIN: 0IN 0IN 0.0001PT;"><SPAN>5.&NBSP;&NBSP;&NBSP;&NBSP;&NBSP;ON BOTH FRAMES BSTA 1540 AND 1562 / &NBSP;INSTALL PLUG RIVET AT THE OPEN HOLES AS PER B767-300 SRM 53-00-07-1A-1, / NOTE D</SPAN></P><P CLASS="XXMSOLISTPARAGRAPH" STYLE="MARGIN: 0IN 0IN 0.0001PT;"><SPAN>6.&NBSP;&NBSP;&NBSP;&NBSP;&NBSP;TRIM THE REPORTED DAMAGE AREA BY / INCLUDING THE EXISTING ANTENNA INSTALLATION FOOTPRINT IN RECTANGULAR PATTERN / &NBSP;BY MAINTAINING MINIMUM MATERIAL REMOVAL WITH 1 INCH MINIMUM CORNER RADIUS</SPAN></P><P CLASS="XXMSOLISTPARAGRAPH" STYLE="MARGIN: 0IN 0IN 0.0001PT;"><SPAN>7.&NBSP;&NBSP;&NBSP;&NBSP;&NBSP;INSTALL REPAIR AS PER B767-</SPAN><SPAN>300 SRM&NBSP;<A HREF="HTTP://" TARGET="_BLANK" TITLE="THIS EXTERNAL LINK WILL OPEN IN A NEW WINDOW"><SPAN STYLE="COLOR: WINDOWTEXT; TEXT-DECORATION-LINE: NONE;"><SPAN>53-00-01-2R-1 / REPAIR 1 - FUSELAGE SKIN - EXTERNAL REPAIR AT A STRINGER</SPAN></SPAN></A></SPAN></P><P CLASS="X_X_MSOLISTPARAGRAPH"><A HREF="HTTP:" TITLE="THIS EXTERNAL LINK WILL OPEN IN A NEW WINDOW" REL="NOOPENER NOREFERRER" TARGET="_BLANK" STYLE="COLOR: #0066CC; TEXT-DECORATION-LINE: NONE; OUTLINE: NONE;" DATA-MCE-HREF="HTTP:"><SPAN STYLE="COLOR: #1F497D;"></SPAN></A></P>)

Part: TRU — MALFUNCTIONED (APU) · airframe 82,298 hrs · 11,834 cycles

APU WON'T START(THIS BECOMES DMI NR 142640 IAW MEL 49-11-01A CAT C DDD 01MAR21 A/C DOWNGRADED TO NON ETOPS 19FEB21- LOG PG 1339208 ITM 4 - RIV - PERFORMED BITE OF ECU IAW FIM 49-11 FT958. FAULTED "A/C START CIRCUIT" PERFORMED FIM 49-11 F/T 991 UP TO SHEET 2 BLOCK 23. REMOVED AND REPLACED APU START TRU IAW AMM 24-32-04. OPS CHECK GOOD IAW AMM 49-11-00 PERFORMED 3 SUCCESSFUL START. NO DEFECTS NOTED AT THIS TIME. THIS CLEARS DMI 142640.)

Part: WIRE — DAMAGED (FIRE LOOP) · airframe 82,268 hrs · 11,826 cycles

STATUS MESSAGE R ENG FIRE LP 2(<P>ITEM PLACED ON DMI 142461 IAW MEL 26-11-01-01. AIRCRAFT RELEASED TO ETOPS 120.</P><P>15 FEB 21 LP 1339197 ITEM 7 - MIA - T/S AS PER FIM 26-11 FT 804, FOUND THE LOWER FWD FIRE LOOP WIRE WITH DAMAGED INSULATION. REPAIRED WIRE AS PER SWPM 20-10-11 AND REROUTED IT AS PER 20-10-12 OP'S TEST OF FIRE ENG SYS ON IAW AMM 26-11-00 THIS CLEARS MDDR 142461.</P><P><BR /></P>)

Part: CIRCUIT CARD — MALFUNCTIONED (FIRE DETECTION) · airframe 82,257 hrs · 11,823 cycles

STATUS MESSAGE R ENG FIRE LP 2(<P>TRANSFERRED TO MDDR 142353 IAW MEL 26-11-01-01, CAT C, DUE 22FEB21.</P><P>14FEB21 / LP 1339191 / ITEM# 5 / BWI - REMOVED AND REPLACED #2 ENGINE FIRE LOOP 2 CONTROL CARD IAW AMM 260-10-01. OPS TEST GOOD. DMI 142353 CLOSED. PLACARD REMOVED.</P>)

Part: PRESSURE SWITCH — MALFUNCTIONED (FUEL PUMP) · airframe 82,227 hrs · 11,815 cycles

RIGHT FWD FUEL PUMP EICAS MOMENTARILY&NBSP;(<P>REMOVED AND REPLACED&NBSP;RT FWD PRESSURE SWITCH S72 PER AMM 28-42-01. OPS CHECK GOOD.</P>)

Part: IDG — INOPERATIVE (LEFT) · airframe 82,180 hrs · 11,799 cycles

LEFT IDG INOP (C/W AP 18475 IAW AMM 24-11-01, FAILED STEP 2)(<P>TRANSFERRED TO MDDR 141992, CAT "B", DUE DATE 08FEB21. IAW MEL 24-00-01-01 MAINTENANCE ACTION COMPLIED WITH. MCC NOTIFIED. PLACARDS INSTALLED. L/H IDG. TJ 1754Z.</P><P>LP 1303726: REMOVED AND REPLACED LEFT IDG REF AMM 24-11-01. OPS CHECK PERFORMED REF AMM 24-11-00. OPS CHECK GOOD. THIS CLEARS DMI 141992.</P>)

Part: STATUS MESSAGE — FALSE INDICATION (NR 2 FIRE LOOP) · airframe 82,159 hrs · 11,793 cycles

RIGHT ENG FIRE LOOP 2 STATUS MSG ON DECENT. PERFORMED FIRE LOOP OPS CHECK PER AMM 26-10-00, OPS CHECK GOOD. NO FAULTS FOUND AT THIS TIME.

Part: EICAS — FAULT MESSAGE (WINDOW) · airframe 82,157 hrs · 11,792 cycles

RIGHT FWD WINDOW EICAS AFTER LANDING. PERFORMED WINDOW ANTI-ICING BITE IAW FIM 30-41 FAULT TREE 804. INDICATION CLEARED. NO FURTHER DEFECTS NOTED. OPS CHECK IAW AMM 30-41-00 OPS CHECK GOOD.

Part: FIRE DETECTOR — FALSE ACTIVATION (RT ENGINE) · airframe 82,144 hrs · 11,787 cycles

RIGHT ENG FIRE LP 2 STATUS MESSAGE. PERFORMED OPS CHECK OF ENG FIRE DETECTION SYS PER 26-11-00. OPS CHECK GOOD AT THIS TIME. LP 1236236 ITEM 4: PERFORMED INSPECTION ON FIRE DETECTION CARD FILES PER AMM 26-11-02. FOUND NO EVIDENCE OF WATER OR ANY OTHER DAMAGE. OPS CHECK GOOD AT THIS TIME PER AMM 26-11-00.

Part: EICAS — FALSE INDICATION (RT FWD WINDOW) · airframe 82,144 hrs · 11,787 cycles

RIGHT FWD WINDOW EICAS MESSAGE. PERFORMED OPS TEST FLIGHT COMPT. WINDOW ANTI-ICING SYSTEM, OPS CHECK NORMAL, NO DEFECTS NOTED, MESSAGE CLEARED IAW AMM 30-41-00.

Part: FILTER — FAILED (RT ENGINE) · airframe 82,119 hrs · 11,777 cycles

"RT ENGINE FUEL FILT" MESSAGE ON EICAS. REMOVED AND INSPECTED RT ENGINE FUEL FILTER, IAW B767 AMM 73-11-02, NO VISIBLE CONTAMINATION FOUND. INSTALLED NEW FILTER, IAW B767 AMM 73-11-02-404-008. LEAK CHECK GOOD, WET MOTOR NR 2 ENGINE PERFORMED, IAW AMM 71-00-00-712-168-H03.

Part: WARNING MESSAGE — FALSE ACTIVATION (RT FUEL PUMP) · airframe 81,957 hrs · 11,735 cycles

IN CRUISE AND AT TOP OF DESCENT INTERMITTENT EICAS MESSAGE "RT FWD FUEL PUMP". PERFORMED FIM 28-22 FT 8191 THROUGH BLOCK 49. BOOST PUMP OPERATES NORMALLY.

Part: RELAY — FAILED (RT PACK TEMP) · airframe 81,858 hrs · 11,710 cycles

RIGHT PACK SURGING, DUCT PRESSURE DROPS TO 5 PSI. TRANSFERED TO MDDR NR 139725 MEL 21-51-01-01 CAT "C" DUE DATE 28DEC20. PERFORMED RT PACK TEMP CONTROLL BITE, IAW FIM 21-51 FAULT TREE 845 FOUND FAULT LOW LIMIT VALVE. R & R K10318 RELAY, PER WDM 21-51-22 LOW LIMIT VALVE RELAY. OPERATIONS CHECKS GOOD. NO FURTHER DEFECTS NOTED.

Part: PRESSURE SWITCH — FAILED (FUEL PUMP) · airframe 81,823 hrs · 11,696 cycles

RT FWD FUEL PUMP EICAS MESSAGE ON DESCENT. REMOVED AND REPLACED RT FWD PRESSURE SWITCH S72, IAW AMM 28-42-01. OPERATIONS CHECK GOOD.

Part: START VALVE — SLOW (LT ENGINE) · airframe 81,808 hrs · 11,693 cycles

L START VALVE SLOW TO OPEN. PERFORMED ENGINE RUN OF LT ENGINE, IAW AMM 71-00-00 AND AMM 80-11-00/501 STARTER VALVE IN TRANSIT FOR APPROXIMATELY 4 SECONDS. ALL SYSTEM OPERATIONS NORMAL. NO DEFECTS NOTED AT THIS TIME.

Part: SKIN — DENTED (HORIZONTAL STAB) · airframe 81,671 hrs · 11,644 cycles

PRE-FLIGHT INSPECTION FOUND WHAT APPEARS TO BE TWO DENTS ON THE LEADING EDGE OF THE LEFT HORIZONTAL STABILIZER, APPROXIMENLY 5 AND 10 FEET FROM THE WING ROOT. INSPECTED LT LEADING EDGE INBOARD LEFT LEADING EDGE 5 FT FROM ROOT AND 10 FT FROM ROOT BOTH WITHIN LIMITS, PER SRM 55-10-01-1A-1. INBOARD D-01-20 STICKER 51160 & OUTBOARD D-02-20 STICKER 51159.

Part: CONTROL PANEL — MALFUNCTIONED (COCKPIT TEMP) · airframe 81,646 hrs · 11,633 cycles

FLIGHT DECK TEMP CONTROL SYSTEM INOPERABLE IN AUTO MODE (FLIGHT DECK COMPT TEMP CONTROL SYSTEM, AUTO MODE). TRANSFERRED TO DMI 137761, IAW MEL 21-61-02-03, CAT C. CLEANED FLIGHT DECK TEMP SENSOR FILTER, IAW B767 AMM 21-61-09. PERFORMED FIM TASK 21-61 TREE 912. NO FAULTS FOUND. REMOVED AND REPLACED RELAY K238 AND P37 PANEL. OPERATIONS CHECK GOOD. DMI CLEARED. PLACARD REMOVED. NO FURTHER DEFECTS NOTED BY MX DP 1755Z.

Part: SEAL — DEBONDED (ACOUSTIC PANEL) · airframe 81,621 hrs · 11,621 cycles

SEALANT DISBONDED ON NR 1 ENGINE FWD OUTER ACOUSTIC PANEL 2 O`CLOCK POSITION. TRANSFERRED TO NON MEL 137644, PER AMM 72-00-00 TABLE 640, GOOD FOR 10F/C. APPLIED SEALANT TO ACOUSTIC LINER SEGMENT ON NR 1 ENGINE 2 O`CLOCK POSITION, IAW AMM 72-33-01. THIS CLEARS NON-MEL 137644. MCC NOTIFIED.

Part: CONTROL SWITCH — FAILED (COCKPIT TEMP) · airframe 81,621 hrs · 11,621 cycles

FD TEMP CONTROL INOPERABLE IN AUTO MODE. TRANSFERRED TO MDDR 137649, PER DDG 21-61-02-03. REMOVED AND REPLACED FD TEMP CONTROL SWITCH 21-61-04, OPERATIONS NORMAL. THIS CLEARS MDDR 137649.

Part: UNKNOWN — UNKNOWN (COCKPIT TEMP) · airframe 81,621 hrs · 11,621 cycles

FD REMAINED FULL COLD, WOULD NOT ADJUST ABOVE 20 C WHEN OPERATED IN STANDBY FD INCREASED TO 24 C. PERFORMED FD TEMP MANUAL CONTROL TEST, IAW AMM 21-61-00 AND FOUND NO DEFECTS. OPERATIONS CHECK GOOD.

Part: CONNECTOR — LOOSE (COCKPIT TEMP) · airframe 81,621 hrs · 11,621 cycles

FD CONTROL TEMP UNCONTROLLABLE HEATING/COOLING WITHOUT ADJUSTING TEMP. T/S LT PACK, FOUND TEMP SENSOR CANNON PLUG LOOSE. TIGHTENED, OPERATIONS NORMAL, IAW AMM 21-52-02.

Part: ACOUSTIC LINER — DAMAGED (NR 1 ENGINE) · airframe 81,611 hrs · 11,616 cycles

FOUND DAMAGE ON ACOUSTIC LINER ON NR 1 ENGINE 2 O'CLOCK POSITION. CONTINUES OPERATIONS LIMIT, IAW 72-00-00. 10 FLT CYCLES. EXAMINED THE LINE SEGMENT AND FOUND MISSING PIECES. NO MISSING PIECES ARE PERMITTED, IAW AMM 72-32-00. TRANSFERED TO NON MEL 137410. REMOVED AND REPLACED ACOUSTIC PANEL ON NR 1 ENGINE, IAW AMM 72-33-01.

Part: FIRE BOTTLE — DISCHARGED (NR 1 APU) · airframe 81,559 hrs · 11,597 cycles

APU FIRE BOTTLE NR 1 DISCHARGED. TRANSFER TO MDDR NR 137012 IAW DDG NR 26-22-01-01, CAT C, DUE DATE 10NOV2020. ST 2248Z 04 NOV 20-BWI. REMOVED AND REPLACED NR 1 APU BOTTLE AND PERFORMED OPERATIONS CHECK, OPERATIONS CHECK GOOD. ALL WORK DONE IN ACCORDANCE WITH AMM 26-22-02. THIS CLEARS DMI NR 137012. PLACARD REMOVED. DL 0810.

Part: WARNING MESSAGE — FALSE ACTIVATION (FUEL PUMP) · airframe 81,520 hrs · 11,581 cycles

RT FWD FUEL PUMP EICAS ON INITIAL DESCENT. PERFORMED OPERATIONS CHECK OF RT FWD FUEL PUMP, PER B767 AMM 25-27-00. OPERATIONS CHECK OK, NO MESSAGE DISPLAYED.

Part: PRESSURE SWITCH — UNKNOWN (FUEL PUMP) · airframe 81,525 hrs · 11,582 cycles

RT FWD FUEL PUMP EICAS ON INITIAL DESCENT. PERFORMED OPERATIONS CHECK, IAW AMM 28-22-00 "RT FUEL SYSTEM PRESS" MESSAGE DISP. T/S PER FIM 28-22 T826. SUSPECT FUEL PRESS SW S71 TO BE AT FAULT, PN 60B92400-7 ON ORDER W/ MCC. TRANSFERED TO MDDR 136855, IAW DDG 28-22-01. MX ACTION COMPLIED WITH. PLACARD INSTALLED. MCC NOTIFIED.

Part: PRESSURE SWITCH — FAILED (FUEL SYSTEM) · airframe 81,448 hrs · 11,558 cycles

ON TAKEOFF ROLL WITH 7000 LBS IN CENTER TANK, CENTER RT FUEL PUMP EICAS MESSAGE. ITEM TRANSFERED TO MDDR 136106, PER MEL 28-22-02A CAT C DUE DATE 25-OCT-20. MX ACTION C/W CB COLLARED. TIME INITIALS GTCAT 0338. CVG MX, 17OCT. REMOVED AND REPLACED RIGHT CENTER FUEL PRESSURE SWITCH, IAW B767 AMM 28-42-01. OPERATIONS CHECK GOOD AT THIS TIME. MCC NOTIFIED. PLACARDS REMOVED CIRCUIT BREAKERS RESTORED. TIME INITIALS 1304 ZULU ZH.

Part: WARNING MESSAGE — FALSE ACTIVATION (CABIN PRESSURE) · airframe 81,261 hrs · 11,505 cycles

CABIN ALT AUTO 2 STATUS MESSAGE. OPERATIONS CHECK CABIN ALT AUTO 2 STATUS MESSAGE, IAW FIM 21-31 FT 803, NO DEFECT NOTED. SYSTEM OK.

Part: WARNING LIGHT — FALSE ACTIVATION (LT ENGINE) · airframe 81,054 hrs · 11,441 cycles

LEFT ENGINE VALVE DISCREET LIGHT ILLUMINATED. PERFORMED ENGINE RUN IAW 71-00-00 FOR OPERATIONS CHECK OF ENGINE SOLENOID VALVE IAW AMM 73-21-20. OPERATIONS CHECK GOOD. LIGHT EXTINGUISHED AND SYSTEM OPERATIONS NORMAL.

Part: OIL SYSTEM — LOW (APU) · airframe 80,945 hrs · 11,407 cycles

APU FAULTS AFTER LANDING, 2 ATTEMPTS FAILS APPROX 85% RPM. APU ECU INDICATED LOW OIL LEVEL. ADD 2 QTS TO APU IAW AMM 12-13-04. CLEARED MSG, RAN APU WITH HEAVY LOAD. NO LEAKS NOTED. 3 SUCCESSFUL APU STARTS, OPS CHECK NORMAL. APU HRS @ 4985.3.

Part: TRANSCEIVER — NOT SEATED (WEATHER RADAR) · airframe 80,848 hrs · 11,375 cycles

LEFT WEATHER RADAR INOPERATIVE. RERACKED THE WX RADAR LT TRANCEIVER IAW AMM 34-43-01. PERFORMED SYSTEM TEST OK.

Part: UNKNOWN — MALFUNCTIONED (BLEED AIR SYS) · airframe 80,724 hrs · 11,335 cycles

EICAS: R ENG BLEED OFF PERFORMED AIR SUPPLY BOX BITE TEST IAW FIM 36-20-00. PERFORMED ENGINE RUN UP. NO FAULTS AT THIS TIME.

Part: OIL SYSTEM — LOW (APU) · airframe 80,707 hrs · 11,328 cycles

APU FAULT LIGHT ILLUMINATED, 2 START ATTEMPTS, APU ECU INDICATION LOW OIL PRESSURE, OIL LEVEL. ADDED 3 QTS OF OIL TO APU IAW AMM 12-13-04, CLEARED FAULT AND RAN APU WITH PACKS FOR 5 MINUTES, NO FAULTS, OIL LEVEL GOOD. OPS CHECKED GOOD IAW AMM 49-00-00.

Part: WARNING LIGHT — FALSE ACTIVATION (CARGO FIRE) · airframe 80,698 hrs · 11,326 cycles

DURING INTERIOR INSPECTION, CARGO FIRE LIGHT ILLUMINATED. PERFORMED A BITE TEST IAW FIM 26-14 FT 809. OK FOR SERVICE.

Part: SENSOR — LOOSE (CARGO DOOR) · airframe 80,674 hrs · 11,317 cycles

IN CRUISE CARGO DOOR EICAS LT ILLUMINATED WITH MAIN CARGO DOOR EICAS MESSAGE. INSPECTED MAIN CARGO DOOR SEAL, LATCHES, AND PRESSURE SW IAW FIM 52-90-18-00. NO DEFECTS NOTED. PRESSURIZED A/C IAW AMM 05-51-24 AND OPS CKS GOOD AT THIS TIME. INSPECTED AND FOUND (S891) SENSOR LOOSE. TIGHTENED AND ADJUSTED PER REF AMM 52-71-09. PERFORMED OPS TEST AND PASSED. NO EICAS MSG IND ILLUMINATED WITH DOOR OPERATION.

Part: CAP — DEFECTIVE (FIRE HANDLE) · airframe 80,655 hrs · 11,310 cycles

APU INOP. REMOVED AND REPLACED APU FIRE HANDLE CAP ASSY, OPS CHECK OK IAW AMM 26-10-00. THIS CLEARS MDDR 130678.

Part: WARNING MESSAGE — FALSE ACTIVATION (FUEL PUMP) · airframe 80,494 hrs · 11,263 cycles

CTR R FUEL PUMP EICAS PRESSURE LGT WITH 8.6 FUEL IN CTR TANK INTERMITTENT. PERFORMED AN OPS CHECK PER AMM 28-22-05. OPS TESTED GOOD.

Part: CONTROL PANEL — DEFECTIVE (WEATHER RADAR) · airframe 80,329 hrs · 11,204 cycles

WX RADAR GAIN CONTROL LOOSE IN AUTO&NBSP;(<P>REPLACED WX RADAR PANEL, OPS NORMAL IAW AMM 34-43-02.</P>)

Part: PUMP — INOPERATIVE (FUEL SYSTEM) · airframe 80,324 hrs · 11,202 cycles

BOTH LH &AMP; RH CTR TANK FUEL PUMPS INOP(<P>PLACED ON MDDR 128515 PER MEL 28-22-02-01, CAT 'C'.</P>)

Part: BRAKE — FIRE (NR 5) · airframe 79,972 hrs · 11,094 cycles

#5 BRAKE FIRE INDICATED BY MARSHALLER WHEN TURNING INTO PARKING SPOT.(<P>REPLACED #5 MAIN TIRE AND BRAKE ASSY, REPLACED #6 MAIN TIRE IAW AMM 32-41-08. PERFORMED HIGH ENERGY STOP INSP IAW AMM 05-51-14, BRAKE SEIZURE INSP IAW AMM 05-51-15 AND DRY CHEMICAL EXTINGUISHER USED INSP IAW AMM 05-51-95 (#5 MAIN TIRE OFF PART: PN 2608811-5, SN B2772/B2772), (#6&NBSP;<SPAN>MAIN TIRE OFF PART: PN&NBSP;</SPAN><SPAN>2608811-5</SPAN><SPAN>, SN B8778/B8778).</SPAN></P><P>LP&NBSP;<SPAN>1160423:&NBSP;</SPAN><SPAN>PLACED #5 BRAKE ON MDDR 126644 PER MEL 32-41-01B DUE TO BRAKE HYD LINE DAMAGED.</SPAN></P><P>LP 1160424 - ITEM 2: REPLACED BRAKE LINE. CLOSED MDDR 126644 (LINE OFF P/N: AS112-061-0660, NSN).</P>)

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 79,878 hrs · 11,067 cycles

CTR R FUEL PUMP EICAS W/ 3.4 QTY PRIOR TO T/O. RAN QRH.(<P>PERFORMED CTR R FUEL PUMP OPS CHECK IAW AMM 28-22-00. NO EICAS MSG PRESENT. OPS CHECK NORMAL, NO FUEL IN CENTER.</P>)

Part: OIL SYSTEM — LOW (APU) · airframe 79,776 hrs · 11,036 cycles

APU FAULT, 3 ATTEMPTS TO START.(<P>PERFORMED BITE OF APU IAW FIM 49-11-FT 987, FOUND LOW OIL PRESS FAULT LIGHT. APU OIL FOUND TO BE LOW, SERVICED APU TO FULL IAW AMM 12-13-14, APU HOURS @4144.8; PERFORMED 03 SUCCESSFUL APU STARTS. PLACED LOAD ON APU, NO FAULTS/MSGS NOTED. APU OPS NORM AT THIS TIME. VISUAL INSPECTION OF APU AREA, NO OIL LEAKS NOTED.</P>)

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 79,761 hrs · 11,033 cycles

AT TAKE OFF EICAS MESSAGE "CTR R FUEL PUMP" WITH 5,000 LBS IN THE CTR TANK.(<P>PERFORMED OPS CHK ON CTR R FUEL PUMP REF B767 AMM 28-22-00. OPS CHK NORMAL. NO MESSAGES DISPLAYED. OK TO CONTINUE AT THIS TIME.</P>)

Part: OXYGEN MASK — INOPERATIVE (COCKPIT) · airframe 79,715 hrs · 11,016 cycles

LEFT SUPERNUMERARY SEAT OXYGEN MASK INOP.(<P>TRANSFER TO MDDR 125249 IAW DDG 35-11-02-03A, CAT C, DUE DATE 12 MAR-20.</P><P>REF LOG PAGE 1191109 ITEM 2: REMOVED AND REPLACED SUPERNUMERARY SEAT O2 MASK IAW 767 M/M 35-11-51. MASK OPERATES NORMAL. THIS CLEARS MDDR 125249. PLACARD REMOVED.</P>)

Part: PRESSURE SWITCH — FAILED (FUEL SYS) · airframe 79,680 hrs · 11,006 cycles

EICAS MSG RT FWD FUEL PUMP.(<P>TRANSFERRED TO MEL 28-22-01, MDDR 125137, CAT 'C'.</P><P>LP 1191092: REMOVED AND REPLACED RIGHT FWD FUEL PRESS SWITCH IAW AMM 28-42-01. OPS CHECKS GOOD. DMI 125137 CLEARED.</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (RT FUEL PUMP) · airframe 79,675 hrs · 11,005 cycles

R FWD FUEL PUMP EICAS CAME ON FOR DECENT 30 SECONDS ON INITIAL DECENT.(<P>PERFORMED OPS CHECK OF R FWD FUEL PUMP IAW B767 AMM 28-22-00. OPS CHECK NORMAL. NO MESSAGES DISPLAYED.<BR /></P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (RT FUEL PUMP) · airframe 79,680 hrs · 11,006 cycles

UPON COMMENCING INITIAL DESCENT, R FWD FUEL PUMP EICAS ILLUMINATED. THE ISSUE SELF-CORRECTED.(<P>PER SERVICE LETTER 28-026 BOEING SUGGESTS DAILY SUMPING FOR INTERMITTENT FUEL PUMP ISSUES DUE TO POSSIBLE MOISTURE CLOSING CHECK VALVE. SUMPED FUEL TANKS IAW AMM 12-11-03. OPS CHECK OF BOOST PUMPS NORMAL.<BR /></P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (FUEL VALVE) · airframe 79,656 hrs · 11,001 cycles

ON AIRCRAFT INBOUND, FOUND LEFT ENGINE FUEL VALVE MESSAGE APPEARED ON ENGINE SHUTDOWN.(<P>PERFORMED ENGINE RUN IAW 71-00-00. LIGHT AND MESSAGE CLEARED. OPS NORMAL. FOUND NO FAULTS. PLACED FUEL / IGNITION CONTROL RELAY ON ORDER WITH MCC.</P>)

Part: CONTROL VALVE — FAILED (RT A/C PACK) · airframe 79,587 hrs · 10,972 cycles

RIGHT PACK INOP.(<P>TRANSFERRED TO MDDR 124631 IAW DDG 21-51-01-01, CAT C, DUE DATE 23FEB2020.</P><P>LP&NBSP;1166631: REPLACED RIGHT PACK FLOW CONTROL AND SHUT OFF VALVE IAW AMM 21-51-01-004. OPS CHECK GOOD. THIS CLEARS MDDR 124631. PLACARD REMOVED.</P>)

Part: CONNECTOR — DIRTY (FLOW CNTRL VALVE) · airframe 79,575 hrs · 10,967 cycles

WITH R/H PACK OFF THERE IS NO PACK OFF LIGHT OR R PACK OFF EICAS MSG.(<P>CLEANED FLOW CONTROL VALVE CONNECTOR IAW AMM 21-51-01. OPS CHECK GOOD AT THIS TIME.</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (RT A/C PACK) · airframe 79,545 hrs · 10,956 cycles

CREW REPORTS R/H PACK OFF LIGHT AND R/H PACK OFF EICAS ADVISORY MESSAGE NOT ILLUMINATED WITH PACK SWITCH OFF.(<P>TRANSFERRED TO MDDR 124437 IAW DDG 21-51-01-01, CAT 'C', DUE 19FEB20, RESTRICTED TO WITHIN 60 MIN OF SUITABLE AIRPORT.</P><P>LP 1086889- M5 PACK CONTROL ( TEP ) VALVE CANNON PLUG SECURED -FLOW CONTROL VALVE&NBSP; CANNON PLUG SECURED&NBSP; OPS CHECK GOOD&NBSP; RIGHT PACK&NBSP; TEST OK&NBSP; IAW AMM 21-51-12 00</P>)

Part: FAN — VIBRATION (LT ENGINE) · airframe 79,492 hrs · 10,939 cycles

LEFT ENG FAN VIB AT 5.0 DURING CLIMB AT CRUISE ALT. LEFT FAN VIB 1.9.(<P>REMOVED 38EA SERVICEABLE FAN BLADE FROM ESN 706465 AND INSTALLED SERVICEABLE ON LEFT HAND ENGINE IAW AMM 72-31-02. PERFORMED VIBRATION SURVEY IAW AMM 71-00-00, TEST #6 OPS CHECK GOOD, WITHIN LIMITS.<BR /></P><P><SPAN>LP&NBSP;</SPAN><SPAN>1066856:&NBSP;</SPAN><SPAN>REMOVED FAN SPINNER FOR FAN BLADE REPLACEMENT IAW AMM 72-31-01. INSTALLED FAN SPINNER IAW AMM 72-31-01. RETORQUED FAN SPINNER AFTER ENGINE RUN IAW AMM 72-31-01.</SPAN></P>)

Part: ENGINE — VIBRATION (LEFT) · airframe 79,460 hrs · 10,924 cycles

LEFT ENGINE FAN VIB 4.7 ON CLIMB. PERFORMED GENERAL VISUAL INSPECTION ON INLETS & EXHAUST. 1ST STAGE FAN BLADE VISUAL INSPECTION IAW FIM 71-05 FT 856. PERFORMED ENGINE RUN, ALL PARAMETERS WITHIN LIMITS ON GROUND IAW AMM 71-00-00.</P>)

Part: CAM — BENT (THRUST REVERSER) · airframe 79,460 hrs · 10,924 cycles

LEFT ENGINE HIGH VIBRATION DURING CLIMB OUT, INDICATED 5.0. PERFORMED FIM TASK 71-05 FT 852, CHIP DETECTORS, CLEANED AVM CONNECTORS, O/T ENG, FOUND UPPER LATCH RING INBOARD THRUST REVERSER BENT, NOT ENGAGED. REPLACED LATCH CAM, STRAIGHTENED STOP BRACKET, IAW AMM 78-31-02, ADJUSTED LATCH RING IAW AMM 78-31-02, COMPLETED ENGINE RUN UP VIB WITHIN LIMITS.

Part: FIRE WARNING — FALSE ACTIVATION (MAIN DECK) · airframe 79,459 hrs · 10,923 cycles

MAIN CARGO DECK FIRE WARNING MESSAGE ILLUMINATED. PERFORMED INSPECTION OF ALL CARGO COMPARTMENTS, RAN ENGINES AND BITE IAW TASK 26-14-00-815-809-003. NO FAULTS NOTED. FIM TASK 05-51-56-202-001 C/W, NO FURTHER FAULTS NOTED.

Part: BLEED AIR SYS — MALFUNCTIONED (LEFT ENGINE) · airframe 79,422 hrs · 10,911 cycles

LEFT ENGINE BLEED WAS CYCLING ON AND OFF ON APPROACH. PERFORMED FIM TASK 36-20 FT 803. NO FAULTS FOUND. ACFT OK FOR SERVICE.

Part: UNKNOWN — MALFUNCTIONED (VIBE SYSTEM) · airframe 79,342 hrs · 10,883 cycles

DURING CLIMB OUT LEFT ENGINE VIB DISPLAYED 4.7 ON THE FAN, ENGINE SNAPSHOT TAKEN FL 31.1 AT 1010Z SAT -40 DURING CLIMB.(<P>LEFT ENGINE VIB BITE SELF TEST IS SATISFACTORY. NO MESSAGE AT THIS TIME. MAINTENANCE PAGE SHOWS 0+0 UNITS, WITHIN LIMITS I.A.W AMM 77-31-00.</P>)

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 79,325 hrs · 10,874 cycles

R FWD FUEL PUMP PRESS EICAS AT TOD. RAN CHECK LIST, EICAS CLEARED ON ITS OWN BEFORE COMPLETION OF CHECK LIST.(<P>PERFORMED OPS CHECK OF R/H FWD BOOST PUMP IAW AMM 28-22-00. NO FAULTS/MSGS NOTED, OPS CHK NORMAL AT THIS TIME.<BR /></P>)

Part: UNKNOWN — MALFUNCTIONED (LT ENGINE) · airframe 79,271 hrs · 10,859 cycles

LEFT FAN VIBRATION 4.5 DURING CLIMB TO LEVEL OFF. FAN VIB 1.2 DURING CRUISE.(<P>PERFORMED FIM 71-05 1852 UP TO SHORT 2 BLOCK 5. PERFORMED ENGINE RUN IAW B767 AMM 71-00-00. NO FAULTS NOTED. VIBRATION WITHIN LIMITS PER AMM 71-00-00.<BR /></P>)

Part: UNKNOWN — MALFUNCTIONED (LT ENGINE) · airframe 79,290 hrs · 10,866 cycles

L ENG FAN VIBRATION @ 4.3 DURING CLIMB - APPROXIMATELY 10 MINUTES FROM FL 200-FL 390.(<P>IAW AMM 71-00-00-862-020-803 PERFORMED FIM 71-05 FT 858 TO SHEET 2 BLOCK 3-25 AND SHEET 3 TO BLOCK 50. NO FAULTS NOTED. PERFORMED FIM 71-05 FT 852 UP TO SHEET 2 BLOCK 5 AND PERFORMED ENG RUN IAW AMM 71-00-00. NO FAULTS NOTED. ALL&NBSP; VIBRATION WITHIN LIMITS IAW AMM 71-00-00-00-862-020-803.</P>)

Part: DUCT — DAMAGED (RT WING TAI) · airframe 79,233 hrs · 10,844 cycles

FOUND TAI DUCT DAMAGED. DISCOVERED WHEN THE RT WING L/E PANEL WAS MISSING. REMOVED AND REPLACED THE NR 9 SLAT LE TAI DUCT PER AMM 30-11-06. LEAK CHECK GOOD PER AMM 30-11-00-790-801.

Part: PRESSURE SWITCH — FAILED (FUEL PUMP) · airframe 79,162 hrs · 10,818 cycles

L FWD FUEL PUMP INOP. PERFORMED TROUBLESHOOTING IAW FIM 28-22 FT 819 AND OPERATIONAL CHECKED OK. REMOVED AND REPLACED THE LT FWD BOOST PUMP PRESSURE SWITCH IAW AMM 28-42-01. SWITCH OPS CHECKED OK.

Part: WARNING LIGHT — NO INDICATION (LT ENGINE VALVE) · airframe 78,971 hrs · 10,763 cycles

L ENG VALVE DID NOT ILLUMINATE DURING ENG SHUTDOWN.(<P>PERFORMED BITE TEST OF L/H ENG PIMU, NO FAULTS FOUND AT THIS TIME. A/C OK FOR SERVICE IAW AMM 77-21-00.</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (FUEL PRESSURE) · airframe 78,963 hrs · 10,761 cycles

R CENTER FUEL PUMP PRESS EICAS WITH 4000 LBS IN TANK.(<P>TRANSFERRED 4000 LBS OF FUEL INTO CENTER TANK, COULD NOT DUPLICATE FAULT. OPERATIONS NORMAL, NO FAULTS NOTED. NO MESSAGES NOTED.TRANSFERRED FUEL BACK TO RIGHT TANKS. REF AMM 28-22-00. A/C OK FOR SERVICE.<BR /></P>)

Part: ISOLATION VALVE — INOPERATIVE (BLEED SYSTEM) · airframe 78,892 hrs · 10,734 cycles

L ISOLATION VALVE PB IS INOP.(<P>REMOVED AND REPLACED L ISLN VLV PB IAW B767 SWPM 20-84-14. PERFORMED SATISFACTORY L ISLN VLV OPS CHK IAW B767 AMM 36-11-04.<BR /></P>)

Part: OXYGEN MASK — BROKEN · airframe 78,892 hrs · 10,734 cycles

SUPERNUMERARY O/B R/H O2 MASK BELLOW BROKEN.(<P>REMOVED AND REPLACED R/H O2 MASK IAW B767 AMM 35-11-51. PERFORMED SATISFACTORY MASK OPS&NBSP; CHECK IAW B767 AMM 35-11-00.<BR /></P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (FIRE DETECTOR) · airframe 78,869 hrs · 10,725 cycles

AFT CARGO DET 1 STATUS MESSAGE.(<P>PERFORMED FIRE/OVHT TEST IAW B767 AMM 26-10-00, STATUS MSG CLEARED.

Part: OIL SYSTEM — LOW (APU) · airframe 78,849 hrs · 10,718 cycles

APU WILL NOT START X3.(<P>APU OIL FOUND TO BE LOW, SERVICED TO FULL IAW AMM 12-13-01. PERFORMED APU BITE IAW FIM 49-11 F/T 987. LRU "LOW OIL PRESS" MSG NOTED, CLEARED FAULT. PERFORMED 3 APU STARTS IAW AMM 49-11-00. NO FAULTS OR MSG NOTED, OPS CHECKS NORMAL AT THIS TIME.<BR /></P>)

Part: ELEMENT — OUT OF POSITION (NR 2 FIRE LOOP) · airframe 78,823 hrs · 10,709 cycles

STATUS MESSAGE IN FLIGHT, LT ENG FIRE LOOP 2. INSPECTED THE LEFT ENGINE FIRE LOOP 2. FOUND LOOP AT 1 O'CLOCK POSITION TO BE CURLED UPWARD, TOO CLOSE TO CORE COWL. REPOSITIONED THE ELEMENT, SYSTEM OPS CHECKED GOOD ON GROUND IAW AMM 2611-02.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 78,701 hrs · 10,672 cycles

AT TOP OF DESCENT, EICAS MSG "R FWD FUEL PUMP" FOR ABOUT 10 SEC. PERFORMED OPERATIONAL TEST OF R FWD FUEL PUMP IAW AMM 28-22-00. NO MESSAGES SHOWN OR FAULTS NOTED. OPS CHECK NORMAL AT THIS TIME.

Part: BATTERY — DEFECTIVE (APU) · airframe 78,701 hrs · 10,672 cycles

DURING DAILY CHECKLIST, A/C STANDBY POWER SYSTEM OPS TEST, "APU BAT DISCH" LIGHT WOULD NOT ILLUMINATE. R/R BATTERY CHARGER (APU) IAW AMM 24-31-05, NO HELP. REINSTALLED ORIGINAL BAT CHARGER IAW AMM 24-31-05. NEED FURTHER T/S ON APU BAT DISCH NO ILLUMINATION. LP 1215997 - M11: T/S PER FIM 24-31 FT 805 BOX 22. R/R APU BATTERY CURRENT MONITOR IAW AMM 24-31-08, NO HELP. FURTHER T/S REQ'D, LP 1215997 - M12: PER MCC REQUEST, T/S IAW WDM 24-31-41. CHECKED FOR CONTINUITY FROM K790 PIN A3 TO D10216 PIN 38 AND FROM K790 PIN A2 TO D10562 PIN 11. FOUND CONTINUITY, T/S M1172 PIN 11 TO D10216 PIN 2 FOUND CONTINUITY, FURTHER T/S REQ. LP 1215998 - M14: TRANSFERRED TO MDDR #117867 IAW DDG 24-31-01-02, CAT 'C', DUE: 27SEP19. MCC NOTIFIED. LP 1216001 - M3: REMOVED AND REPLACED STATIC INVERTER IAW AMM 24-33-03. NO FIX. MDDR # 117867 REMAINS OPEN. LP 1216007 - M5: PERFORMED T/S APU DISCHARGE LIGHT. REPLACED RELAY K790 ON P-49 APU PANEL, NO HELP. DMI 117867 REMAINS OPEN IAW WDM 24-31-41. LP 1216011 - M3: REMOVED AND REPLACED APU BATTERY IAW AMM 24-31-04. OPS CHECK NORMAL AT THIS TIME. THIS CLEARS DMI 117867.

Part: RELAY — FAILED (APU) · airframe 78,701 hrs · 10,672 cycles

APU INOP DUE TO APU BATTERY. TRANSFERRED TO MDDR #117866 IAW AMM 49-11-01A, CAT 'C', DUE 27SEP19. MCC NOTIFIED. LP 1216012 - M4: REMOVED AND REPLACED RELAY K791 IAW SWPM 20-81-12. OPS CHECK NORMAL AT THIS TIME. THIS CLEARS DMI #117866. PLACARDS REMOVED AND MCC NOTIFIED.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 78,696 hrs · 10,671 cycles

CTR R FUEL PUMP EICAS MESSAGE, BEFORE T/O. OPS CHECK CTR R FUEL PUMP IAW AMM 28-22-00, OPS CHECK GOOD.

Part: FIRE WARNING — FALSE ACTIVATION (COCKPIT) · airframe 78,670 hrs · 10,663 cycles

EICAS: MAIN CARGO FIRE, CARGO FIRE LIGHT ILLUMINATED. PERFORMED FIM 26-14-00, MESSAGE CLEARED. NO FAULT MESSAGES AT THIS TIME.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 78,661 hrs · 10,661 cycles

RIGHT FWD FUEL PUMP INTERMITTENTLY FLASHES "PRESS" LIGHT IN DESCENT. PERFORMED OPS TEST OF RT FWD FUEL PUMP IAW AMM 28-22-00, OPS NORMAL AT THIS TIME. NO MSG OR LIGHTS NOTED.

Part: INLET SCREEN — DIRTY (HSI) · airframe 78,640 hrs · 10,655 cycles

LEFT HSI SCREEN WENT BLACK FOR A LONG PERIOD, WITH A SMELL OF BURNING. THE SCREEN CAME BACK UP WITH NO CREW ACTION. REMOVED CAPTAINS EHSI AND CLEANED INLET SCREENS. REINSTALLED CAPTAINS EHSI. OPS CK NORMAL. REF TO FIM 34-22 FT 806 FLAG NOTE 2.

Part: RESISTOR — DEFECTIVE (DOOR WARNING) · airframe 78,601 hrs · 10,643 cycles

IN CRUISE FLIGHT, AT FL 370, RECEIVED A MASTER CAUTION AND EICAS MESSAGE "MAIN CARGO DOOR". PER CHECK LIST, DESCENDED TO 10,000' WITH LDG ALT SELECTOR AT 9,500'. MESSAGE CLEARED DURING DESCENT. PERFORMED MCD LOCKED SENSOR ADJUSTMENT IAW AMM 52-71-09. ADJUSTMENT CHECK OK. FOUND CONTROL PANEL "LOCKED" LIGHT ILLUMINATED BEFORE EICAS AND COCKPIT ANNUNCIATOR EXTINGUISHED. LP 1073386 - M4; STOWED IN KNOW GOOD CONTROL PANEL IAW AMM 52-32-20. OPS CHECK GOOD. REINSTALLED OLD PANEL IAW AMM 52-32-20. 1073386 M5; REMOVED AND REPLACED AUTO TRANSFORMER T235 (S/N OFF: NSN, P/N OFF 310-19717-01) NO HELP. DISCREPANCY REMAINS OPEN. WORK DONE IAW SWPM 20-40-00 AND INSTALLED CONTROLLER PANEL IAW AMM 52-32-20. LP 1073387 - M7; REMOVED AND REPLACED R731 IAW SWPM 20-01-11. MCD EICAS MESSAGE GOES AWAY WHEN LIGHT IS ON. BUT STILL A 1 SECOND DELAY WITH LATCHING BEFORE FULLY LATCHED. LP 1073387-&NBSP; M8; PERFORMED OPERATIONAL TEST OF MAIN DECK CARGO DOOR IAW AMM 52-32-00. SYSTEM OPERATES AS IT SHOULD.

Part: PRESSURE SWITCH — FAILED (OIL PRESSURE) · airframe 78,475 hrs · 10,599 cycles

LT ENG LOW OIL PRESSURE LIGHTS INOP. REMOVED AND REPLACED L/H LOW OIL PRESSURE SWITCH IAW AMM 79-33-01. PERFORMED ENGINE RUN IAW AMM 71-00-00. NO FAULTS NOTED. THIS CLEARS MDDR #116023. PLACARD REMOVED.</P>)

Part: WARNING LIGHT — FALSE ACTIVATION (APU FIRE) · airframe 78,432 hrs · 10,585 cycles

APU FAULT. PERFORMED A BITE TEST ON APU ECU. APU FIRE LIGHT ILLUMINATED IAW FIM 26-15 FT 803, NO FAULTS FOUND. FIRE TEST PASSED, NO FIRE DAMAGE NOTED, OPS CHECK GOOD IAW AMM 49-11-00.

Part: CIRCUIT CARD — UNKNOWN (APU FIRE LOOP) · airframe 78,441 hrs · 10,588 cycles

CREW CALL BACK FOR APU FIRE LOOP 1. PERFORMED A BITE IAW FIM 26-15 FT 803, FOUND NO FAULTS. REMOVED AND REPLACED THE APU FIRE DETECTION LOOP 1 CARD ASSY IAW AMM 26-10-01.

Part: WARNING MESSAGE — NO INDICATION (SPAR VALVE) · airframe 78,426 hrs · 10,582 cycles

RT SPAR VALVE DID NOT ILLUMINATE. TEST LIGHT OK BEFORE SHUT DOWN. PERFORMED FUNCTIONAL CHECK OF BOTH LEFT AND RIGHT SPAR VALVES IAW AMM 28-22-00, FUNCTIONAL TEST NORMAL. ALSO, PERFORMED RT ENGINE IDLE RUN AND OPS CHECK OF SPAR VALVE IS NORMAL.</P>)

Part: FIRE WARNING — FALSE ACTIVATION (COCKPIT) · airframe 78,408 hrs · 10,573 cycles

"MAIN CARGO FIRE" EICAS MSG W/WARNING BELL, AIRCRAFT AT GATE. (<P>INSPECTED ALL AREAS IN MAIN CARGO, NO SMOKE DETECTED. PERFORMED FIRE LOOP TEST IAW 26-14-00, OPS CHECK GOOD.&NBSP;</P>)

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 78,317 hrs · 10,549 cycles

MAIN CARGO DOOR EICAS RTB PHNL. NOTE: INDICATION WENT OUT APROX. 12000 FEET MSL.&NBSP;(<P>PERFORM BITE/FAULT ON SPESU PER AMM 32-09-11, NO FAULTS FOUND. PERFORM MEASUREMENTS OF TARGETS AND ADJUST IAW AMM 52-71-09, MEASUREMENT 2.35 MM FROM TOP LEVER TARGET S891 1.54 MM BETWEEN STOP LEVER AND STOP BOLT, ALL MEASUREMENTS WITHIN LIMITS PER AMM 52-21-07.</P><P>LP 1065679 - M3: PERFORMED PRESSURIZATION CHECK PER AMM 05-51-24 TO TEST PROX SWITCHES OF MAIN CARGO DOOR, TEST OK, NO DOOR MESSAGES OR LIGHTS.&NBSP;</P>)

Part: FIRST AID KIT — UNSERVICEABLE (CABIN) · airframe 78,292 hrs · 10,541 cycles

FIRST AID KIT SEAL BROKEN (EMERGENCY MEDICAL EQUIPMENT).(<P>MED KIT FIRST AID KIT TRANSFERRED TO MDDR 114705, CAT 'D', DUE DATE 10-NOV-19.</P><P>LP 1065665 - M6:&NBSP;REMOVED AND REPLACED&NBSP;FIRST AID KIT IAW AMM 25-64-03. PLACARDS REMOVED AND MCC NOTIFIED. THIS CLEARS DMI #114705.&NBSP;<BR /></P>)

Part: UNKNOWN — MALFUNCTIONED (WEATHER RADAR) · airframe 78,292 hrs · 10,541 cycles

LEFT WX RADAR DOES NOT CLEARLY ID WEATHER.(<P>PERFORMED MULTIPLE OPERATIONAL TEST, AND SYSTEM TEST OF BOTH LEFT AND RIGHT WEATHER RADAR SYSTEMS IAW AMM 34-43-00, NO FAULTS NOTED.&NBSP;</P>)

Part: UNKNOWN — MALFUNCTIONED (WEATHER RADAR) · airframe 78,260 hrs · 10,531 cycles

WEATHER RADAR DID NOT PAINT CELLS @ 75 MIL.&NBSP;(<P>PERFORMED RT UNIT ON GROUND IAW AMM 34-43-00 OPS TEST SATISFACTORY&NBSP;</P>)

Part: FIRE WARNING — FALSE ACTIVATION (COCKPIT) · airframe 78,215 hrs · 10,515 cycles

MASTER WARNING, MAIN CARGO FIRE AT THE GATE (PRE-FLT).&NBSP;(<P>PERFORMED T/S PER FIM 26-14 FT 809. NO FAULTS FOUND. CYCLED FIRE LOOP 1, LOOP 2. TURNED ON BOTH PACKS, NO FURTHER FAULTS NOTED.&NBSP;</P>)

Part: FIRE DETECTOR — CONTAMINATED (MAIN CARGO) · airframe 78,173 hrs · 10,501 cycles

MAIN CARGO FIRE INDICATION. PERFORMED VISUAL INSPECT OF CARGO COMPARTMENT, NO SIGNS OF FIRE. DETECTOR WENT OFF DUE TO EXCESSIVE POLLEN AT RIV AIRPORT. PERFORMED MAIN CARGO SYSTEM CHECK, NO DEFECTS NOTED IAW AMM 26-14-00.

Part: CIRCUIT BREAKER — TRIPPED (COOLING FAN) · airframe 78,142 hrs · 10,492 cycles

DURING POST-FLIGHT, HORN SOUNDED AND RETURNING TO THE COCKPIT, FWD EQPT OVHT MESSAGE . RAN QRH AND LEFT EQUIP COOLING SELECTOR IN STBY.(<P>FOUND FWD EQPT FAN #1 CB OPEN. RESET AND SELECTED AUTO. EQUIPMENT COOLING OPERATIONAL TESTS GOOD PER AMM 21-58-00.&NBSP;</P>)

Part: CIRCUIT CARD — MALFUNCTIONED (RT A/C PACK) · airframe 78,072 hrs · 10,468 cycles

RIGHT PACK OFF LIGHT INOPERATIVE, BUT WORKS IN TEST. REMOVED AND REPLACED CIRCUIT CARD MODULE IN THE RT PACK OFF SWITCH IAW B767 SWPM 20-84-00. OPS CHECK GOOD AT THIS TIME.

Part: TRANSCEIVER — MALFUNCTIONED (WEATHER RADAR) · airframe 77,998 hrs · 10,442 cycles

L WXR SYS FAIL MESSAGE. (<P>TRANSFERRED TO MDDR 112432 PER MEL 34-43-01 CAT 'D'. </P><P>LP 1050877 - REMOVED AND REPLACED&NBSP;WEATHER RADAR TRANSCEIVER&NBSP;PER AMM 34-43-01. OPS CKS GOOD. THIS CLOSES MDDR 112432.</P>)

Part: INDICATOR — INOPERATIVE (CABIN TEMP) · airframe 77,963 hrs · 10,428 cycles

AFT CABIN COMPARTMENT TEMP DISPLAY INOP (COMPT TEMP INDICATIONS).(<P>PLACED ON MDDR 111955</P><P>LP 1055284 - M2:&NBSP;&NBSP; REMOVED AND REPLACED COMPARTMENT TEMP INDICATOR IAW AMM 21-61-01, OPS CHECK GOOD. PLACARDS AND STICKER REMOVED. THIS CLEARS DMI 111955.<BR /></P>)

Part: STATUS MESSAGE — FALSE ACTIVATION (COCKPIT) · airframe 77,897 hrs · 10,409 cycles

STATUS MSG R ENG TAI VALVE.(<P>PERFORMED #2 ENG RUN AND TAI OPERATIONAL TEST. OPS CHECK GOOD. NO MESSAGE OR FAULT DISPLAYED. REF AMM 30-21-00.</P>)

Part: BULB — FAULTY (AC BAY) · airframe 77,825 hrs · 10,386 cycles

APPROX 30 MIN INTO FLIGHT, AT FL 380, FLT DECK TEMP RAPIDLY INCREASED TEMP TO 27°C IN MANUAL MODE. WITH SELECTOR NEAR 3RD DOT, COLD TEMP AGAIN RAPIDLY RISES.(<P><SPAN>PERFORMED BITE TEST OF TEMP ZONE BOX AND LEFT/RIGHT PACK BOXES. FOUND NOT FAULTS AT THIS TIME. CLEANED TEMP SENSOR IAW AMM 21-61-01. NO FIX. NEEDS MORE T/S.</SPAN></P><P><SPAN>LP 1050501 - M1: REMOVED AND REPLACED L PACK OUT TEMP BULB IAW 21-52-06. PACK TEMPS NORMAL AT THIS TIME.&NBSP;</SPAN></P><P><SPAN><BR DATA-MCE-BOGUS="1" /></SPAN></P>)

Part: TRU — MALFUNCTIONED (APU) · airframe 77,821 hrs · 10,385 cycles

APU FAIL TO START.(<P>REMOVED AND REPLACED APU TRANSFORMER RECTIFIER UNIT (TRU) IAW AMM 24-32-04.</P>)

Part: UNKNOWN — MALFUNCTIONED (APU) · airframe 77,819 hrs · 10,384 cycles

APU WON'T START. (<P>PERFORMED APU ECU BITE TEST IAW 49-11.00.&NBSP; OPS CHECKED GOOD&NBSP;AT THIS TIME.</P>)

Part: PUMP — MALFUNCTIONED (FUEL SYSTEM) · airframe 77,801 hrs · 10,377 cycles

ON BEGINNING OF DESCENT, CAUTION MESSAGE " RT FWD FUEL PUMP " DISPLAYED, AS WELL AS PRESSURE LIGHT. THESE EXTINGUISHED IN LESS THAN 1 MINUTE.(<P>TRANSFERRED TO MDDR # 110907 AS PER MEL 28-22-01 CAT C.</P><P>LP 1050498 - M5/M6:&NBSP;REMOVED AND REPLACED RELAY, K10704 IAW WDM 28-22-11 AND REMOVED AND REPLACED BOOST PUMP IAW AMM 28-22-03. OPS CK NORMAL. THIS CLEARS MDDR 110907. PLACARD REMOVED AND MCC NOTIFIED.</P><P><BR /></P><P>RELAY OFF PART (P/N: 9342G-10675 , S/N: 01084)</P>)

Part: SELECTOR — FAULTY (CABIN TEMP) · airframe 77,811 hrs · 10,380 cycles

30&NBSP; MINUTES INTO FLIGHT, COCKPIT AND FWD CABIN TEMP WENT UP 7 DEGREES IN 10 MINUTES. UNABLE TO ADJUST UNTIL TRIM AIR WAS CYCLED AND CABIN TEMP SET TO MANUAL.&NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; FLIGHT DECK TEMP INOP IN AUTO, OK IN MANUAL.&NBSP;&NBSP;(<P>PERFORMED OPS CHECK IAW AMM 21-61-00, FOUND FLT DECK TEMP INDICATION TO NOT MATCH SELECTOR SETTING. FWD CABIN TEMP, OPS CHECK GOOD. PERFORMED FIM 21-62 FT 912 BITE PROCEDURE, NO CURRENT OR PREVIOUS FLIGHT FAULTS. SUSPECT FAULTY FLT DECK TEMP SELECTOR SWITCH. P/N 625868-1 ON ORDER WITH MCC. TRANSFERRED TO MDDR 110938 IAW DDG 21-61-02-03 CAT 'C'.</P><P>LP 1050494 - M4:&NBSP;REMOVED AND REPLACED&NBSP;FLT DECK TEMP ZONE SELECTOR IAW AMM 21-61-04. FLT DECK TEMP ZONE STILL INOP, FURTHER T/S REQUIRED. DMI 110938 REMAINS OPEN&NBSP;</P><P>LP 1050495-7 PERFORMED BITE TEST ON ZONE TEMP CONTROLLER IAW AMM 21-61-04. OPS CHECK OK. THIS CLEARS MDDR 110938 AND PLACARDS REMOVED.</P>)

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 77,796 hrs · 10,376 cycles

RT FWD FUEL PUMP EICAS AND RT FWD PUMP PRESS LIGHT. THIS OCCURRED AT THE TOP OF DESCENT WHEN ENGINE THRUST WAS REDUCED. MSG AND LIGHT EXTINGUISHED ABOUT 30 SECONDS LATER.(<P>PERFORMED OPERATIONAL CHECK OF RT FWD FUEL PUMP PER AMM 28-42-00. OPS CHECK GOOD. PRESSURE INDICATION NORMAL AT THIS TIME.</P><P><BR DATA-MCE-BOGUS="1" /></P><P>NOTE: ITEM PLACED ON DEFERRAL AT NEXT STA "ONT" LP 1050485&NBSP;</P>)

Part: CONTROLLER — MALFUNCTIONED (LT BLEED) · airframe 77,784 hrs · 10,372 cycles

L ENG BLEED OFF MSG. RESET BITE ON CONTROLLER. ALL CHECKS GOOD AT THIS TIME IAW AMM 36-11-00.

Part: FIRE WARNING — FALSE ACTIVATION (MAIN CARGO) · airframe 77,784 hrs · 10,372 cycles

DURING PREFLIGHT MAIN CARGO FIRE WARNING INDICATIONS (5-10 SECONDS)(<P>OPS CHECKED FIRE WARNING DETECTION SYSTEM IAW AMM 26-14-00. NO DEFECTS NOTED AT THIS TIME. OPS NORMAL.</P>)

Part: ENGINE — VIBRATION (LEFT) · airframe 77,771 hrs · 10,367 cycles

LEFT ENGINE FAN VIBES REACHED 4.3 DURING CLIMB OUT.(<P>PERFORMED ENGINE RUN&NBSP; AND VIBE INDICATIONS NML PER AMM 71-00-00 PER FIM 71-05 FT 805. NOTE: VIB LEVELS CAN SUDDENLY SPIKE AT TRANSIENT LEVELS OF ENGINE SPEEDS.</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (RT FUEL PUMP) · airframe 77,762 hrs · 10,365 cycles

RIGHT FWD FUEL PUMP EICAS.&NBSP;(<P>PERFORMED OPS CHECK OF FUEL PUMP PER B767 AMM 28-42-00. OPS CHECK GOOD. PRESSURE INDICATION NORMAL.</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (LT EEC) · airframe 77,771 hrs · 10,367 cycles

15 MIN PRIOR TO DESCENT, FL400, L ENG EEC MODE R ENG EEC MODE CAUTION MSG. CONTINUED FLIGHT IN ALTN MODE.(<P>PERFORMED IDLE RUN #1 AND #2 ENG EEC. OPS CHECK GOOD IAW AMM 71-00-00.</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (FUEL PUMP) · airframe 77,700 hrs · 10,346 cycles

R FWD FUEL PUMP CAUTION MSG AND R FWD PRESS LIGHT DISPLAYED. DURING DECENT WITH THRUST AT IDLE. MSG CLEARED AFTER APPROX ONE MINUTE. PERFORMED OPERATIONAL CHECK OF THE FUEL BOOST PUMP IAW FIM 28-22-FT 826. OPS CHECK NORMAL AT THIS TIME.

Part: LIGHT — INOPERATIVE (CONTROL PANEL) · airframe 77,718 hrs · 10,353 cycles

TEMP CONTROL PANEL BACKGROUND LIGHT INOP.(<P>TRANSFERRED TO MDDR 110279.&NBSP;</P><P>LP 1055132: REMOVED AND REPLACED INDICATION ASSY CONT TEMP IAW B767 AMM 21-61-04. OPS CHECK GOOD. AIRCRAFT RETURNED TO NORMAL CONFIGURATION. THIS CLEARS MDDR #110279. MCC NOTIFIED AND PLACARDS REMOVED. RS @ 14:13Z.<BR /></P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (FUEL PUMP) · airframe 77,680 hrs · 10,341 cycles

RIGHT FWD FUEL PUMP EICAS.(<P>PERFORMED GROUND OPS CHECK, OPS NORMAL I.A.W AMM 28-22-00.</P>)

Part: CONTROLLER — MALFUNCTIONED (RT A/C PACK) · airframe 77,607 hrs · 10,323 cycles

RT PACK OFF LIGHT NOT ILLUMINATED AND RT PACK OFF EICAS MESSAGE NOT DISPLAYED WHEN RIGHT PACK SELECTED OFF. RESET PACK TEMP CONTROLLER. OPERATED RT AND LT PACK SEVERAL CYCLES. SYS OPS CK NORMAL PER AMM 21-61-00.

Part: FIRE WARNING — FALSE ACTIVATION (CARGO) · airframe 77,597 hrs · 10,320 cycles

MAIN CARGO COMPARTMENT FIRE INDICATIONS INTERMITTENT.(<P>RESET CARD PN 285N0028-136 @ P54 PANEL IAW AMM 26-16-00. NO DEFECTS NOTED AT THIS TIME, OPS &AMP; TEST NORMAL.<BR /></P>)

Part: STARTER — DEFECTIVE (APU) · airframe 77,475 hrs · 10,283 cycles

APU FAILED TO START.&NBSP;(<P>FOUND APU STARTER NOT MAKING CORRECT RPM. REMOVED AND REPLACED APU STARTER AS PER AMM 49-41-01. APU START SUCCESSFUL, OPS CHECK GOOD AT THIS TIME.&NBSP;</P>)

Part: UNKNOWN — MALFUNCTIONED (WEATHER RADAR) · airframe 77,421 hrs · 10,267 cycles

IN CRUISE AT FL370 L RADAR WOULD ONLY PAINT ON COUNTER CLOCK WISE SWEEP AND THEN WENT TO MXK FAIL.(<P>PERFORMED AN OPERATIONAL CK OF LEFT RADAR IAW 34-43-00. OPS CK'S OK AT THIS TIME AND NO FAULTS NOTED. ALSO CHECKED RADAR RT TIGHT IN RACK OK.</P>)

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 77,435 hrs · 10,270 cycles

R FWD FUEL PUMP MESSAGE ON EICAS JUST AFTER DESCENT.(<P>PERFORMED FIM 2822 F/T 819, NO DEFECTS FOUND, OPS CHECK IAW 28-22-00. OPS CHECK NORMAL AT THIS TIME.&NBSP;</P>)

Part: TRANSCEIVER — MALFUNCTIONED (WEATHER RADAR) · airframe 77,361 hrs · 10,251 cycles

WINDSHEAR FAIL MSG ON EICAS, WX FAIL ON MFD WHEN WXR SYS TOGGLE SW POSITIONED TO RIGHT.&NBSP;(<P>PERFORMED BITE IAW FIM 34-43 FT 805, FOUND RT FAIL ON BITE. REMOVED AND REPLACED WXR TRANSCEIVER IAW AMM 34-43-01, OPS CK NORMAL AT THIS TIME.</P>)

Part: IGNITER — WORN (APU) · airframe 77,345 hrs · 10,246 cycles

APU IGNITER PLUG WORN OUT.(<P>REMOVED AND REPLACED APU IGNITER PLUGS OPS CHECK NORMAL REF: AMM 49-41-02</P>)

Part: BLADE — NICKED (NR 2 ENGINE) · airframe 77,345 hrs · 10,246 cycles

NR 2 ENGINE HAS FAN BLADE WITH NICK BLADE MARKED.(<P>LOCATED AND BLENDED OUT NR 2 ENGINE FAN BLADE MARKED PER AMM 72-31-02-308-055-1-00.</P>)

Part: IGNITER — DAMAGED (NR 2 ENGINE) · airframe 77,345 hrs · 10,246 cycles

ENG NR 2 BOTH IGNITER PLUGS ARE DAMAGED.(<P>REMOVED AND INSTALLED ENGINE NR 2 BOTH IGNITERS IAW AMM 74-21-02. OPS CHECK NORMAL.</P>)

Part: BLADE — NICKED (NR 1 ENGINE) · airframe 77,345 hrs · 10,246 cycles

ENGINE NR 1 SEVERAL FIRST STAGE FAN ROTOR BLADES HAVE NICKS ON THE LEADING EDGES.(<P>BLENDED OUT ENG NR 1 SEVERAL FIRST STAGE FAN ROTOR BLADES LEADING EDGES IAW AMM 72-31-02-308-045-H00. PERFORMED NDT SPOT FLOURESCENT PENETRANT INSPECTION ON THE BLENDED AREAS. NO CRACK INDICATIONS NOTED AT THIS TIME REF 70-11-00 P1B 201</P>)

Part: WINDOW — DELAMINATED (COCKPIT) · airframe 77,345 hrs · 10,246 cycles

REPLACE 3L WINDOW DUE TO DELAMINATION.(<P>REMOVED AND REPLACED NR 3L WINDOW IAW AMM 56-11-10 OPEEATIONAL TEST NORMAL IAW AMM 30-41-00.&NBSP;</P>)

Part: IGNITER — DAMAGED (NR 1 ENGINE) · airframe 77,345 hrs · 10,246 cycles

ENGINE NR 1 BOTH IGNITER PLUGS ARE DAMAGED.(<P>REMOVED AND REPLACED NR 1 ENGINE IGNITER PLUGS IAW AMM 74-21-02. OPS CHECK NORMAL</P>)

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 77,345 hrs · 10,246 cycles

APU FIRE LP1 STATUS MESSAGE(<P><SPAN>NSPECTED FOR CONDITION /SECURE/ CLEANUP APU FIRE DETECTION SYSTEM PER AMM 26-15-00. PERFORMED APU FIRE DETECTION TEST IAW AMM 26-15-00. OPS CHECK NORMAL.</SPAN></P>)

Part: WIRE HARNESS — CHAFED (NR 1 ENGINE) · airframe 77,345 hrs · 10,246 cycles

ENGINE NR 1 WIRE HARNESS RUBBING ON HPSOV SUPPORT BRACKET(<P>REROUTED ENG NR 1 WIRE HARNESS PER W/D 71-51-52 AND SWPM 20-10-06</P>)

Part: ECU — MALFUNCTIONED (APU) · airframe 77,325 hrs · 10,238 cycles

APU INOP. NO DUCT PRESSURE.(<P>TRANSFERRED TO MDDR 107850</P><P>LP 1034331-M3 REMOVED AND REPLACED ECU IAW AMM 49-61-01 OPS CHECK AT THIS TIME&NBSP; DUCT PRESSURE&NBSP; AT 30 PSI&NBSP; TEST OK CLEARED MDDR 107850.</P>)

Part: BLADE — NICKED (COMPRESSOR) · airframe 77,324 hrs · 10,237 cycles

FOUND COMPRESSOR BLADE ON THE NR 1 ENGINE WAS FOUND DAMAGED. FOUND THE NR 1 BLADE NICKED, MEASURED .064 DEEP. BLENDED NICK DOWN TO .094 IAW AMM 72-31-02-308-045-1400. PERFORMED FLOURESCENT PENETRATION INSPECTION IAW AMM 72-31-02 & NDT 70-11-06, NO DEFECTS NOTED.

Part: SENSOR — MALFUNCTIONED (APU) · airframe 77,294 hrs · 10,226 cycles

APU INOPERATIVE. R & R THE INLET PRESSURE SENSOR IAW AMM 49-61-04. OPS CHECKED NORMAL.

Part: OXYGEN MASK — INOPERATIVE · airframe 77,294 hrs · 10,226 cycles

SUPERNUMERY SEAT O2 MASK INOP.(<P>TRANSFERRED TO MDDR 107537.<BR /></P><P>LP 1052836: REMOVED AND REPLACED OXYGEN MASK IAW AMM 35-11-01. OPS&NBSP;CHECK GOOD AT THIS TIME. THIS ACTION CLEARS DMI 107537. MCC NOTIFIED AND PLACARDS REMOVED.<BR /></P>)

Part: APU — SHUTDOWN · airframe 77,289 hrs · 10,225 cycles

APU SHUTDOWN DURING BEFORE START CHECKLIST(<P>BITE CHECK APU ECU CHECK NORMAL, NO FAULTS NOTED. RESTART OF APU SUCCESSFUL 1ST ATTEMPT PER AMM B767 49-61-05</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (FUEL PUMP) · airframe 77,263 hrs · 10,219 cycles

ON DESCENT RECEIVED R FWD FUEL PUMP EICAS MESSAGE, COMPLIED W/ QRH PROCEDURE, FUEL TANK INDICATING 15.2 LBS X 1000 IN THE RIGHT TANK&NBSP;(<P>PERFORMED OPERATIONAL CHECK ON RH FWD FUEL PUMP I.A.W AMM 28-22-00. COULD NOT DUPLICATE FAULT, NO MSG NOTED AT THIS TIME&NBSP;</P>)

Part: WARNING MESSAGE — FALSE INDICATION (FUEL PUMP) · airframe 77,259 hrs · 10,218 cycles

CTR R FUEL PRESS CAUTION MSG ON CLIMB OUT, COMPLIED WITH QRH.&NBSP;(<P>OPS CHECK OF CTR R FUEL PUMP SYS PER AMM 28-22-00, OPS CHECK GOOD</P><P><BR /></P>)

Part: FIRE WARNING — FALSE ACTIVATION (CARGO BAY) · airframe 77,099 hrs · 10,170 cycles

UPON POWER TRANSFER EICAS MESSAGE CARGO FIRE DETECTOR SHOWS ON EICAS AND RECEIVE ALERTS. COMPLIED WITH BITE TEST CHECK OF CARGO FIRE DETECTION SYSTEM AFTER POWER TRANSFER. ALL MESSAGES WENT AWAY NO FAULTS NOTED. SUSPECTED BAD HAND POWER CART ALL SYSTEM NORMAL.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 76,999 hrs · 10,145 cycles

ON STARTING LEFT ENGINE&NBSP; STATUS MESSAGES LEFT ENGINE OIL FILTER&NBSP;(<P>PERFORMED VISUAL INSPECTION OF LEFT&NBSP; ENGINE OIL FILTER NO DEFECTS NOTED IAW AMM 79-21-04 COULD NO DUPLICATED STATUS MESSAGES&NBSP;&NBSP;</P>)

Part: CONTROL PANEL — MALFUNCTIONED (COCKPIT) · airframe 76,995 hrs · 10,143 cycles

WHEN DESELECTING L FWD FUEL PUMP " PRESS" DOES NOT ILLUMINATE IN THE SWITCH AND ASSOCIATED EICAS MSG DOES NOT APPEAR, CANNOT TURN OFF&NBSP;(<P>RE-RACK FUEL PUMP / X-FEED PANEL REF AMM 28-22-00 OPS CHECK GOOD , OK FOR SERVICE&NBSP;</P>)

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 76,847 hrs · 10,097 cycles

STATUS MSG MAIN CARGO LOOP 2 (<P>PERFORMED FIM 26-10 FT 803, CHECKED ALL AFOLTS CARDS NO FAULTS FOUND AT THIS TIME, OPS CHECKS GOOD.</P>)

Part: PUMP — MALFUNCTIONED (FUEL BOOST) · airframe 76,767 hrs · 10,073 cycles

AT TOP OF DESCENT RT FWD FUEL PUMP INTERMITTENTLY FAILED&NBSP;(<P>PERFORMED OPS CHECK OF ALL FUEL BOOST PUMPS I.A.W AMM 28-22-00 RECEIVED NO ADVISORY MSG , CHECKED FUEL BOOST PUMP CIRCUIT BREAKERS AND FOUND NO TRIPPED BREAKERS OPS CHECK GOOD AT THIS TIME&NBSP;</P>)

Part: PRESSURE SWITCH — FAULTY (FUEL SYSTEM) · airframe 76,713 hrs · 10,051 cycles

LT FWD FUEL PUMP EICAS COMPLIED WITH QRH. REMOVED AND REPLACED LT FWD FUEL PUMP PRESSURE SWITCH. OPS CHECK GOOD, NO DEFECTS NOTED AT THIS TIME IAW AMM 28-42-01.

Part: OIL CAP — OPEN (RT ENGINE) · airframe 76,693 hrs · 10,045 cycles

RT ENG OIL PRESSURE BELOW AMBER BAND AT 26 FL 340, INCREASED TO ABOVE AMBER BAND 29 AT FL 360, ALL OTHER INDICATIONS NORMAL. COMPLIED WITH FIM 71-05 FT 865 FOUND THE OIL CAP IN OPEN POSITION, SERVICED OIL IAW AMM 12-13-01, PERFORMED ENGINE RUN UP TO 40% N1 FOR 8 MINS, NO OIL LEAKS FOUND AT THIS TIME, ENGINE RUN PERFORMED PER AMM 71-00-00.

Part: CONNECTOR — DIRTY (FUEL SYSTEM) · airframe 76,709 hrs · 10,050 cycles

"LT FWD FUEL PUMP" EICAS. GFI SYSTEM CB NOT TRIPPED, CLEANED CONNECTOR AT "L FWD PUMP LOW PRESS SW S70, SYSTEM OPS CK GOOD PER AMM 28-42-01.

Part: CONTROLLER — NOT REPORTED (BLEED AIR SYS) · airframe 76,671 hrs · 10,038 cycles

PER MCC REPLACE LEFT ENGINE PRVC. REMOVED AND REPLACED LEFT ENGINE PRVC IAW AMM 36-11-19. OPS CHECK GOOD AT THIS TIME.

Part: CONNECTOR — DIRTY (BLEED AIR SYS) · airframe 76,670 hrs · 10,037 cycles

LT ENG PRV EICAS MESSAGE ON DEPARTURE QRH COMPLETE. TROUBLE SHOOTING AND CLEAND CONNECTOR TO PRV ON LEFT ENGINE. PERFORMED BITE TEST AND PERFORMED OPS CHECK NORMAL IAW AMM 36-11-18 AND OPS CHECK GOOD AT THIS TIME.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 76,666 hrs · 10,036 cycles

STATUS MSG L ENG PRV. PERFORMED FIM 36-20 FT 806, PERFORMED ENGINE RUN FROM IDLE TO 50% N1 ENG NR 1, DUCT PRESSURE SWITCHING NORMAL, MAX PRESS UP TO 50 PSI. PERFORMED BITE PER FIM 36-20 FT 804 NO FAULTS NOTED L ENG PRV MSG CLEARED AMM 71-00-00.

Part: RADAR — MALFUNCTIONED · airframe 76,641 hrs · 10,029 cycles

RADAR ON LEFT AND RIGHT TILT CONTROL KNOB AT + 1 DEGREE UP, READS 1 DEGREE DOWN ON ND DISPLAY(<P>PER FIM 34-43-00 PERFORMED WX RADAR BITE CHECK IAW AMM REF 34-43-00. BITE CHECK PASS SYS NORMAL</P>)

Part: PUMP — MALFUNCTIONED (FUEL SYSTEM) · airframe 76,621 hrs · 10,023 cycles

FWD LEFT FUEL PUMP WON’T SHUT OFF. PERFORMED OPS TEST OF LEFT FWD FUEL PUMP IAW AMM 28-22-00.

Part: CONTROLLER — MALFUNCTIONED (COCKPIT TEMP) · airframe 76,603 hrs · 10,018 cycles

FLT DECK COMP TEMP AUTO MODE INOP(<P>TRANSF'D TO MDDR 103353</P><P><BR /></P><P>PER FIM 21-61 FT 912 ZONE TEMP CONTROLLER NO FAULTS FOUND DURING BITE TEST; MDDR 103353 CLOSED.</P>)

Part: UNKNOWN — UNKNOWN (CABIN TEMP) · airframe 76,603 hrs · 10,018 cycles

TEMP CONTROL SWINGS FROM VERY WARM TO VERY COLD IN COCKPIT(<P>PERFORMED OPS CK OF PACK TEMP IAW AMM 21-61-05 NO FAULT FOUND</P>)

Part: APU — SHUTDOWN (APU BAY) · airframe 76,287 hrs · 9,907 cycles

JUST PRIOR TO PUSHBACK APU SHUTDOWN. RESTART WAS SUCCESSFUL AND SUBSEQUENT ENGINE STARTS ACCOMPLISHED WITHOUT APU SHUTDOWN. ACCOMPLISHED APU FIM 49-11 FT 958. NO ECU FAULTS MINI FAULTS FOUND, 1 PREVIOUS RUN FAULT CLEARED, APU RUN CHECKS NORMAL AT THIS TIME OK FOR SERVICE.

Part: APU — SHUTDOWN (APU BAY) · airframe 76,287 hrs · 9,907 cycles

JUST PRIOR TO PUSHBACK APU SHUTDOWN. RESTART WAS SUCCESSFUL AND SUBSEQUENT ENGINE STARTS ACCOMPLISHED WITHOUT APU SHUTDOWN. ACCOMPLISHED APU FIM 49-11 FT 958. NO ECU FAULTS MINI FAULTS FOUND, 1 PREVIOUS RUN FAULT CLEARED, APU RUN CHECKS NORMAL AT THIS TIME OK FOR SERVICE.

Part: A/C PACK — SURGES (AC BAY) · airframe 76,249 hrs · 9,891 cycles

LEFT PACK SURGES WITH RIGHT PACK OFF. PREVIOUS WRITE UP. PERFORMED BITE TEST OF LEFT PACK CONTROL AND AIR SUPPLY BOX FOUND NO FAULT AT THIS TIME, OPS CHECK GOOD IAW AMM 21-21-00.

Part: GASKET — NOT REPORTED (APU) · airframe 76,227 hrs · 9,883 cycles

APU SURGE WITH 1 PACK. REMOVED AND REPLACED FLOW SENSE GASKET IAW AMM 49-53-08.

Part: FILTER — DEFECTIVE (APU) · airframe 76,217 hrs · 9,879 cycles

APU BLEED CYCLING WITH 1 OR 2 PACKS ON. REMOVED AND REPLACED APU SURGE VALVE FILTER IN REF AMM 49-53-06. OPS CHECK NORMAL.

Part: START VALVE — MALFUNCTIONED (LT ENGINE) · airframe 76,199 hrs · 9,873 cycles

L ENG STARTER. REMOVED AND REPLACED NR 1 ENG START VALVE IAW AMM 80-11-02 OPERATIONAL CHECK IS NORMAL, NO FURTHER DEFECTS NOTED AT THIS TIME.

Part: SENSOR — DEFECTIVE (APU) · airframe 76,183 hrs · 9,868 cycles

APU AUTO SHUT DOWN. REMOVED AND REPLACED INLET COMPRESSOR SENSOR IAW AMM 49-61-03. OPS CHECK NORMAL.

Part: ECU — FAULTY (APU) · airframe 76,174 hrs · 9,865 cycles

APU SHUTDOWN PAC SENSOR MESSAGE NO DUCT PRESSURE. REMOVED AND REPLACED APU ECU IAW AMM 49-60-01, TEST OK.

Part: MODULE — FAULTY (APU) · airframe 76,173 hrs · 9,864 cycles

NO APU DUCT PRESSURE. REMOVED AND REPLACED FLOW SENSE MODULE. OPS CHECK GOOD IAW AMM 49-53-08.

Part: MODULE — FAULTY (APU) · airframe 76,144 hrs · 9,853 cycles

APU NO DUCT PRESSURE. REMOVED AND REPLACED FLOW SENSING MODULE AS PER AMM 49-53-08. OPS CHECK GOOD, P/N OFF 3885081-1 S/N DCN219490. REMOVED AND REPLACED SURGE CONTROL VALVE AS PER AMM 49-53-01, OPS CHECK GOOD.

Part: RELAY — MALFUNCTIONED (FUEL SYSTEM) · airframe 76,088 hrs · 9,833 cycles

RT ENG FUEL VALVE EICAS MESSAGE. PERFORMED FIM TASK 76-11 FT 808, FOUND NO RT ENG FUEL VALVE EICAS SHOWING. REMOVED AND REPLACED RT ENG FUEL CONTROL RELAY K1252 IAW SWPM 20-81-00. PERFORMED WET MOTOR IAW AMM 71-00-00 NO DEFECTS NOTED.

Part: BLADE — LACK OF LUBE (LT ENGINE) · airframe 75,921 hrs · 9,775 cycles

DURING CLIMB LT ENGINE VIB (FAN ) REACH 4.7 AT CRUISE VARIED FROM 1.4 TO 1.7 EVENT RECORD AT 1705Z REPAT WRITE UP. REFERENCES ITEM M9 FOR FAN BLADE RELUBE AND REMAPPING PERFORMED VIBRATION SURVEY TEST NR 6 IAW AMM 71-00-00 ENG VIBRATION WITHIN LIMITS ACCEPTANCES A/C OK FOR SVC AT THIS TIME. REMOVED & RE LUBE AND RE INSTALLED FAN BLADES FOR REMAPPING IAW AMM 72-31-02 C/W STEP 3A J(1) FOR TORQUE PROCEDURRES FOR FAN BLADES SEE LP 128-M10 FOR SPINNER CAP INSTALLED & LP 1006428 M10 RE INSTALLED SPINNER IAW AMM 72-32-01 OPS CHECK GOOD.

Part: CONNECTOR — LOOSE (VIBRATION SYS) · airframe 75,903 hrs · 9,769 cycles

DURING CLIMB LT ENGINE FAN VIB REACHED 4.1 NO INDICATION OF NOISE, HOWEVER AT CRZ VIB SUSTAINED AT 1.2 TO 1.9. PERFORMED TASK 71-05 FT 856, FOUND CONNECTOR LOOSE AT FWD ACCELEROMETER. RESECURED CONNECTOR IAW AMM 77-31-01. GROUND RAN NR 2 ENGINE IAW AMM 71-000-00, ENGINE VIBRATION FOUND IN LIMITS. OK FOR SERVICE.

Part: EXCITER — FAULTY (APU) · airframe 75,886 hrs · 9,762 cycles

APU FAULT DURING START UP. REMOVED AND REPLACED APU IGNITION EXCITER IAW AMM 49-41-03. OPS GOOD.

Part: MODULE — FAULTY (APU) · airframe 75,881 hrs · 9,759 cycles

APU INOP. REMOVED AND REPLACED APU FLOW SENSING MODULE IAW AMM 49-53-08. OPS CHECK OK AT THIS TIME.

Part: IGNITER — DEFECTIVE (APU) · airframe 75,857 hrs · 9,752 cycles

APU FAULT WHEN ATTEMPTING TO START AT FL 390. REPLACED IGNITOR PLUG. CKS GOOD.

Part: ANTI-ICE VALVE — MALFUNCTIONED (RT ENGINE) · airframe 75,719 hrs · 9,702 cycles

RT ENG ANTI-ICE INDICATION INOP. REMOVED AND REPLACED RT ENGINE INLET ANTI-ICE VALVE AS PER AMM 30-21-03. OPERATION AND LEAK CHECK GOOD.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 75,684 hrs · 9,690 cycles

EICAS MSG: RT ENG ANTI-ICE FOLLOWED QRH, ON SAT COMM W/ MX CONTROL CONDITION DISSAPEARED. CONTINUED NORMAL OPS. PERFORMED OPS CHECK OF RIGHT ENGINE ANTI ICE IAW AMM 30-21-03. OPS CHECKED GOOD.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 75,673 hrs · 9,687 cycles

RT ENGINE ANTI-ICE EICAS MSG. PERFORMED OPS CHECK OF RT ENG TAI SYS PER AMM 30-21-03. NO DEFECTS NOTED AT THIS TIME.

Part: BOLT — BROKEN (FUEL CONTROL) · airframe 75,645 hrs · 9,675 cycles

APU FUEL CONTROL ASSY. FUEL FILTER BOWL BOLT BROKEN OFF. REMOVED AND REPLACED FUEL CONTROL ASSY AS PER AMM 49-31-01. LEAK & OPS CHECK OK AS PER AMM 49-31-01 & 49-11-00.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 75,639 hrs · 9,671 cycles

RT BLD ISOL VALVE EICAS MSG. CYCLED RT BLD ISLN VALVE, NORMAL. T/S PER FIM 36-10-837 NO FAULTS NOTED REF AMM 36-11-04.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 75,599 hrs · 9,657 cycles

LT WEATHER RADAR FAILED AT CRUISE " WXR SYS" STATUS MESSAGE. PERFORMED FIM TASK 34-43 FAULT TREE 805. LEFT WEATHER RADAR SYSTEM OPS CHECKS GOOD AT THIS TIME.

Part: RELAY — FAILED (ANTI-ICE SYSTEM) · airframe 75,566 hrs · 9,648 cycles

RIGHT ENGINE ANTI-ICE INOP. REMOVED AND REPLACED TD RELAY K469 IAW SWPM 20-80-00, RIGHT ENGINE ANTI-ICE OPS CHECK DURING ENGINE RUN UP PER AMM 30-21-00 & 71-00-00 OPS NORMAL.

Part: UNKNOWN — MALFUNCTIONED (ANTI-ICE SYSTEM) · airframe 75,566 hrs · 9,648 cycles

RIGHT ENGINE ANTI-ICE INOP. PERFORMED RT ENG TAI SYS TEST IAW AMM 30-21-00. OPS CHECK GOOD NO DEFECTS NOTED.

Part: CONTROLLER — MALFUNCTIONED (AC BAY) · airframe 75,548 hrs · 9,643 cycles

RIGHT PACK TEMP EICAS DURING FLIGHT, SWITCHED TO STANDBY N PER QRH. REMOVED AND REPLACED RIGHT PACK TEMP CONTROLLER IAW AMM 21-51-14. OPS CHECK IS GOOD AT THIS TIME. PERFORMED OPS CHECK IAW AMM 21-51-00.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 75,545 hrs · 9,642 cycles

WEATHER SYSTEM STATUS MESSAGE. PERFORMED FIM 34-43- FAULT TREE 805 ON WEATHER RADAR. BITE PROCEDURE PASS. NO MESSAGE.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 75,518 hrs · 9,635 cycles

STATUS MSG AFT EQ EXH FAN 2 DURING FLIGHT. PERFORMED FIM 31-41-00/101 FIG 109 CLEARED MSG , MSG DID NOT RETURN.

Part: CHECK VALVE — FAULTED (APU) · airframe 75,514 hrs · 9,634 cycles

APU SHUTDOWN WITH A FAULT LIGHT DURING PREFLIGHT. PERFORMED AN INSPECTION OF THE APU AIR SUPPLY VALVE IAW AMM 36-11-11, FOUND IT FAULTY, REMOVED AND REPLACED THE CHECK VALVE IAW AMM 36-11-11. RAN APU WILL FULL LOAD FOR 30 MINUTES NO FAULTS NOTED.

Part: PRESSURE SWITCH — UNKNOWN (FUEL PUMP) · airframe 75,502 hrs · 9,630 cycles

DC PUMP MESSAGE NOT DISPLAYED. REMOVED AND REPLACED THE FUEL PRESSURE SWITCH IAW AMM 28-25-03, OPS AND LEAK CHECKED GOOD.

Part: CONTROL VALVE — FAILED (APU SURGE) · airframe 75,502 hrs · 9,630 cycles

APU SHUTDOWN DURING PRE FLIGHT WITH A FAULT LIGHT. RESTARTED, ALL OTHER OPS NORMAL, INCLUDING APU USE IN FLIGHT. REMOVED AND REPLACED THE SURGE CONTROL VALVE IAW AMM 49-53-01.

Part: RELAY — FAULTY (FUEL SYSTEM) · airframe 75,521 hrs · 9,636 cycles

DC PUMP ON MX MESSAGE NOT DISPLAYED DURING TEST. REPLACED APU FUEL PUMP TRANSFER RELAY "K 505" IAW SWPM CH 20-81-11. SYSTEM C'S GOOD IAW MM 28-25-00-715-264.

Part: WARNING MESSAGE — FALSE ACTIVATION (RT EEC) · airframe 75,502 hrs · 9,630 cycles

RIGHT EEC STATUS MESSAGE DISPLAYED. OPS CHECKED THE RIGHT EEC IAW FIM 73-21 FT 874, NO DEFECTS NOTED.

Part: CONTROL UNIT — MALFUNCTIONED (APU) · airframe 75,499 hrs · 9,628 cycles

APU AUTO SHUTDOWN AFTER A SURGE, WITH ONLY ONE PACK RUNNING. REMOVED AND REPLACED THE APU CONTROL UNIT, OPS TESTED GOOD IAW AMM 49-61-05.

Part: CIRCUIT CARD — MALFUNCTIONED (LT BLEED SYS) · airframe 75,499 hrs · 9,628 cycles

LEFT AND RIGHT BLEED CAUTION AT LOW - IDLE POWER. OCCURED WITH PACK ON AND OFF. RECEIVED LEFT BLEED CAUTION AFTER TAKEOFF ROLL. REMOVED AND REPLACED THE LT ENGINE BLEED CARD IAW AMM 36-11-12, OPS CHECKED GOOD.

Part: TRANSMITTER — MALFUNCTIONED · airframe 75,499 hrs · 9,628 cycles

LEFT ENGINE OIL QUANTITY DECREASED TO 10 IN FLIGHT. SHOWS A DIFFERENCE OF .5 FROM LT AND RT. RT ENGINES QUANTITY WAS THE SAME ON PRE-FLIGHT. REMOVED AND REPLACED THE LEFT ENGINE OIL QUANTITY TRANSMITTER IAW AMM 79-31-01.

Part: RELAY — DEFORMED (RT ENGINE) · airframe 75,477 hrs · 9,625 cycles

RIGHT ENGINE RESET CHANNEL A RELAY SURFACE FOUND DEFORMED. THE RELAY REMOVED AND REPLACED AS PER SWPM 20-81-00, REV. 67, ENGINE PIMU SYSTEM OPERATIONAL TEST CARRIED OUT IAW AMM 77-35-00, REV. 124. FOUND SATISFACTORY.