N78060

Part: LIGHT — BROKEN (ZONE 200) · airframe 92,462 hrs · 12,950 cycles

SEATS 46D, 50F, 38F EMERGENCY PATH LIGHTS INOP. LIGHT ASSEMBLIES REMOVED AND REPLACED PER WDM 33-00-11-1. CHECKS OK.PARTS USED: 29-3326-3-0013,QTY :3 INFO UPDATE REGARDING SDR.

Part: LIGHT — UNSECURE (ZONE 200) · airframe 92,008 hrs · 12,888 cycles

EMERGENCY PACK LIGHT 54F SEAT IS OFF AND UNDER SEAT RESECURED SEAT ESCAPE PATH LIGHT COVER. OPS CHECK GOOD.REF. AMM 35-51-10.

Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 91,492 hrs · 12,820 cycles

FOUND LEFT BS 654 EMERGENCY OVERWING ESCAPE LIGHT INOPERATIVE. R & R LT BS 654 EMERGENCY OVERWING ESCAPE LIGHT IAW AMM 33-51-06. OPS CHECKED GOOD.

Part: WINDOW — LEAKING (ZONE 200) · airframe 89,743 hrs · 12,587 cycles

EXTREME SQUEAL FROM CA NUM2 WINDOW AT APPX 7.6 PSI..SQUEAL LOUDE R A S PSI INCREASED TO MAX. DEBRIEFED FLIGHT CREW UPON ARRIVAL, THEY NOTICED EXTREME SQUEAL FROM CAPT L2 SLIDING WINDOW WHEN GOING APPROX 7.6 PSI DIFF.SQUEA L GOT LOUDER AS PSI INCREASED TO MAX.-, NOISE WAS SO LOUD CAPT W AS UNABLE TO COMMUNICATE WITH TOMC. THE SQUEAL REDUCED WHEN A/C WENT BELOW 28,000 FT.NO OTHER INDICATIONS/MSGS, ALL OTHER PARAME TERS NORMAL. CURRENT F.O.B 70.5. OVERWEIGHT LANDING DOCUMENTED O N SEPRERATE ITEM. NO EMERGENCY DECLARED. PERFORMED LEAK TEST ON LH NO.2 WINDOW AT 4 PSI IAW TASK 56-11-02-404-026 STEP 3. E. (23). NO LEAK NOTED. PERFORMED VISUAL INSPECTION NO OBSTRUCTION OR TORN SEALS NOTED. PER SENIOR MANAGER OF TOMC. AIRCRAFT DOES NOT REQUIRE EVALUATION FLIGHT. RETURNING AIRCRAFT BACK TO SERVICE BASED ON SATISFACTORY LEAK TEST.

Part: ACCESS PANEL — MISSING (ZONE 500) · airframe 89,428 hrs · 12,545 cycles

PDA 2 LEFT WING #5 SLAT, ANTI-ICE DUCT ACCESS PANEL MISSING ON SERVICE CHECK WALKAROUND. UPDATE TO INCLUDE PANEL SIZE AND PHOTOS. PANEL IS APPROX 5X12.5 INCHES, FALLING INTO CATEGORY 2 PDA PER GMM 02-30-95.

Part: TAT PROBE — MALFUNCTIONED (ZONE 100) · airframe 89,233 hrs · 12,519 cycles

R TAT PROBE EICAS MSG ITEM UPDATED IN ORDER TO FLAG SDR. AC RETURN TO GIG AS AN AIR R TAT PROBE WITH ASSOCIATED R TAT FAULT LIGHT ON. BOTH L AND R RETURN ON AN EMERGENCY CONDITION. TAT CB'S A28 AND A15 RE SET AT OVERHEAD PANEL. L TAT IS STILL AVAILABLE. REPLACED R TAT PROBE. SEALANT NOT APPLIED. NOT NECESSARY TO APPL TOMC-APPROVAL FROM SC1ELBYC COMMENT Y THE SEALANT IMMEDIATELY, REPLACED THE TAT PROBE RH REF AMM 33-26-05/401. APPLIED SEALANT TO RH TAT AS REQ PER AMM 34-26-05.

Part: TAT PROBE — FAULTY (ZONE 100) · airframe 89,233 hrs · 12,519 cycles

RIGHT TAT PROBE EICAS MSG ITEM UPDATED IN ORDER TO FLAG SDR. AC RETURN TO GIG AS AN AIR RETURN ON AN EMERGENCY CONDITION. R TAT PROBE WITH ASSOCIATED R TAT FAULT LIGHT ON. BOTH L AND R TAT CB'S A28 AND A15 RE SET AT OVERHEAD PANEL. L TAT IS STILL AVAILABLE. REPLACED THE TAT PROBE RH REF AMM 33-26-05/401 ITEM OK PENDING SEALING PARTS USED: 64-3412-3-0001,QTY :1 99-3412-3-0007,QTY :1 ADD EMP:U411260,U411220 INSPECTED AND APPROVED REPLACEMENT OF TAT PROBE RH REF AMM 33-26-05/401 ITEM OK, PENDING SEALING. NECESSARY APLLY SEALANT, SEALANT NOT APPLYED DUE TO SHORT TIME TO RELEASE THE ACTO FLIGHT REPLACED R TAT PROBE. SEALANT NOT APPLIED. NOT NECESSARY TO APPL Y THE SEALANT IMMEDIATELY, IF THE CURE TIME WILL CAUSE AFLIGHT DELAY. BUT, YOU MUST APPLY THE SEALANT AS SOON AS POSSIBLE TO KE EP MOISTURE OUT OF THE AREA BETWEEN THE PROBE AND AIRPLANE SKIN. THE SEALANT DEFERRAL MUST NOT EXCEED A MAXIMUM OF EIGHT WEEKS. CARRIED FOR 2 FLIGHT CYCLES REF AMM 34-26-05-404-004.

Part: SKIN — GROUND DAMAGE (ZONE 300) · airframe 89,222 hrs · 12,517 cycles

DURING ACCOMPLISHMENT OF THE VERTICAL STABILIZER PAINT. THE GSE (LIFT) CRASHED ON THE INBOARD ELEVATOR RIGHT POSITION. UPDATED ATTRIBUTES TO MAJOR REPAIR, SDR AND ESFR.(YES). UPLOAD THE PICTURES THE RH INBOARD ELEVATOR WAS REPAIRED AS PER EC/RA: 5520-01160. ITEM OK TO SERVICE ALL APPLICABLE INSPECTION STEPS REQUESTED PER EC/RA: 5520-01160 WERE ACCOMPLISHED.

Part: ELEVATOR — DAMAGED (ZONE 300) · airframe 89,222 hrs · 12,517 cycles

THE RH INBOARD ELEVATOR WAS REPAIRED AS PER EC/RA: 5520-01160. ITEM OK TO SERVICE.

Part: ACM — FAULTED (RIGHT) · airframe 87,812 hrs · 12,337 cycles

ON GROUND DURING PUSH GND CREW REPORTED SPARKS FROM PACK BAY AREA AND CREW SMELLED SMOKE, AND NOTED A STATUS MESSAGE ''R ACM''.R ACM RMEOVED AND A TURBINE BLADE WAS MISSING, THE ACM SHAFT WAS SEIZED. INSPECTIONS OF PACK BAY AREA CARRIED OUT NIL FINDINGS. NEW ACM FITTED, TESTS CARRIED OUT - TESTS PASS. NO LEAKS, NO FUMES IN AIRCRAFT. R/H AIR CYCLE MACHINE REMOVED IAW AMM 21-51-03-004-001-001, ON INSPECTION TURBINE BLADE MISSING FROM ACM, NO FURTHER DAMAGE ADD EMP:U401977,U403720,U405168 FOUND IN FIDH OR OTHER COMPONENTS, REPLACEMENT ACM FITTED IAW AMM 22-51-03-404-031-001 PARA 3G EXCLUDING FITMENT OF T1 INLET DUCT & REINSTALL OF TURBINE BYPASS VALVE. APPLICABLE TESTS ON THE RIGHT CTC CARRIED OUT FOR ALL THE RIGHT PACK COMPONENTS THAT WERE REMOVED AND REFITTED (PACK TEST AND PNEUMATIC TEST). TEST SHOWS PASS ON THE CTC AND NO LEAKS WERE NOTED ON THE PACK AND APPLICABLE COMPONENTS. PACK OPERATION SHOWS NORMAL INDICATIONS ON THE MAINTENANCE PAGE, ''R ACM'' STATUS MSG NO LONGER PRESENT. MEL RESTORATION CARRIED OUT, AIRCRAFT SERVICEABLE.

Part: ACTUATOR — LEAKING (RT ELEVATOR) · airframe 85,838 hrs · 12,073 cycles

LOSING CTR HYD SYSTEM QTY DOWN TO .57. CREW FOLLOWED CHECK LIST. TOMC MO. FOUND RIGHT INBD ELEVATOR PCA LEAKING AT SHAFT. REMOVED ELEVATOR PCA PER AMM 27-31-05-024-001 PARTS USED: 76-2735-9-0001,QTY :1 C/W RII REQUIREMENTS FOR PCA INSTALLATION. ACTUATOR, ELEVA OFF 76-2735-9-0001 4479 ON 0000 ACTUATOR, ELEVA OFF 76-2735-9-0001 4479 ON 76-2735-9-0001 4888 INSTALLED RIGHT ELEVATOR INBOARD PCA AS PER AMM TASK 27-31-05-424-027. OPS AND LEAK CHECK GOOD.

Part: BATTERY PACK — DISCHARGED (M1208) · airframe 84,979 hrs · 11,960 cycles

CABIN - DR1 CUTOUT EXIT SIGN LT COME ON LESS THAN 15 MINS (BAT EQ#M1208) TRANSFER REF. NON-ROUTINE HX NRC WO.2709089 AND ORIGINATED BY EMP NO. V897815 EMER LT BAT PACK EQ NO.M1208 REPLACED AND BAT PACK EQ NO.M1208 ATTACHED FORM 44-0008 ITEM 1-3 ACCOMPLISHED. CHARGER REPLACED AND INSTALLATION TEST CARRIED OUT NORMAL. WORK ACCOMPLISHED BY MECHANIC V897815 INSPECTED BY V898561 CABIN DR1 CUTOUT EXIT SIGN LT TEST CARRIED OUT NORMAL AS PER AMM 33-51-07, 33-51-00.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 84,979 hrs · 11,960 cycles

LH AISLE CLG PNL EMER LT ABOVE SEAT 7A TO 11A LT COME ON LESS THAN 15 MINS (BAT EQ#M7235) TRANSFER REF. NON-ROUTINE HX NRC WO.2709037 AND EMER LT BAT PACK EQ#M7235 REPLACED AND INSTALLATION TEST CARRIED OUT NORMAL AS PER AMM 33-51-07, CABIN LH AISLE CLG EMER LT ABOVE SEAT 7A TO 11A EMER LT TESTED NORMAL AS PER AMM 33-51-00, ATTACHED FORM 44.0008 ITEM 1-2 ACCOMPLISHED.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 84,979 hrs · 11,960 cycles

CTR PAX SEAT 1 TO 6 FLOOR PROXIMITY EMER LT COME ON LESS THAN 15 MINS (BAT EQ#M6756) TRANSFER REF. NON-ROUTINE HX NRC WO.2709064 AND EMER LT BAT PACK EQ#M6756 REPLACED AND INSTALLATION TEST CARRIED OUT RESULT NORMAL, CTR PAX SEAT 1 TO 6 FLOOR PROXIMITY EMER LT TESTED NORMAL AS PER AMM 33-51-07, 33-51-00, ATTACHED FORM 44.0008 ITEM 1-2 ACCOMPLISHED.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 84,979 hrs · 11,960 cycles

CTR PAX SEAT 30 TO 37 FLOOR PROXIMITY EMER LT FOUND DIM (BAT EQ#M732) TRANSFER REF. NON-ROUTINE HX NRC WO.2709101 AND CABIN EMER LT BAT PACK EQ#M732 REPLACED AND INSTALLATION TEST ATTACHED FORM 44.0008 ITEM 1-2 ACCOMPLISHED WORK ACCOMPLISHED CARRIED OUT RESULT NORMAL, CTR PAX SEAT 30 TO 37 FLOOR PROXIMITY EMER LT TESTED NORMAL AS PER AMM 33-51-00, 33-51-07, IDT INSPECT IS OKAY.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 84,979 hrs · 11,960 cycles

CTR PAX SEAT 45 TO 54 FLOOR PROXIMITY EMER LT FOUND DIM (BAT EQ#M734) TRANSFER REF. NON-ROUTINE HX NRC WO.2709112 AND CABIN CTR PAX SEAT 45 TO 54 FLOOR PROXIMITY EMER LT BAT PACK 33-51-07,33-51-10 ATTACHED FORM 44.0008 ITEM 1-6 ACCOMPLISHED EQ#M734 REPLACED AND SEAT 48DEF EMER LT ASSY REPLACED AND EMER LT TESTED CARRIED OUT RESULT NORMAL AS PER AMM 33-51-00, IDT INSPECT IS OKAY.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 84,979 hrs · 11,960 cycles

RH AISLE CLG PNL EMER LT ABOVE SEAT 40 TO 50 LT COME ON LESS THAN 15 MINS (BAT EQ#M6760) TRANSFER REF. NON-ROUTINE HX NRC WO.2709012 AND EMER LT BAT PACK EQ#M6760 REPLACED AND BAT INSTALLATION TEST CARRIED OUT NORMAL, CABIN RH AISLE CLG EMER LT ABOVE SEAT 40 TO 50 TESTED NORMAL AS PER AMM 33-51-00,33-51-07 ATTACHED FORM 44.0008 ITEM 1-2 ACCOMPLISHED.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 84,979 hrs · 11,960 cycles

RH AISLE CLG PNL EMER LT ABOVE SEAT 1 TO 2 LT COME ON LESS THAN 15 MINS (BAT EQ#M730) TRANSFER REF. NON-ROUTINE HX NRC WO.2709084 AND EMER LT BAT PACK EQ#M730 REPLACED AND INSTALLATION TEST CARRIED OUT NORMAL, CABIN RH AISLE CLG PNL EMER LT TESTED NORMAL AS PER AMM 33-51-07,33-51-00 ATTACHED FORM 44.0008 ITEM 1-2.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 84,979 hrs · 11,960 cycles

CTR PAX SEAT 38 TO 44 FLOOR PROXIMITY EMER LT FOUND DIM (BAT EQ#M6760) TRANSFER REF. NON-ROUTINE HX NRC WO.2709094 AND EMER LT BAT PACK EQ#M6760 REPLACED AND INSTALLATION TEST FORM 44.0008 ITEM 1-2 ACCOMPLISHED. WORK ACCOMPLISHED BY CARRIED OUT NORMAL, CTR PAX SEAT 38 TO 44 FLOOR PROXIMITY EMER LT TESTED NORMAL AS PER AMM 33-51-00,33-51-07 ATTACHED IDT INSPECT IS OKAY.

Part: SLAT — SEPARATED (NR 1) · airframe 83,833 hrs · 11,811 cycles

PDA 2 REF LOG PAGE 5929189, SECTION OF CLOSURE PANEL APPROXIMATELY 20" BY 2" SEPARATED FROM #1 LEADING EDGE SLAT TRAILING EDGE. THIS LOG PAGE TO NOTE DAMAGE. REF GMM02-30-95. INFO NOTED. ENGINEERING CONTACTED. SEE LOG PAGE 5929189. INSPECTION FOR PART DEPARTED AIRCRAFT TO BE PERFORMED AND DOCUMENTED.

Part: BATTERY — DISCHARGED (M732) · airframe 82,502 hrs · 11,612 cycles

CABIN SEAT 16LK TO SEAT 27LK EMERGENCY LIGHT FOUND DIM FOR 15 MINUTES. TRANSFER REF NR HX WO.1711217 AND ORIGINATED BY EMP NO.V896965. M732 EMER LT POWER SUPPLY AND BATTERY PACK REPLACED AND OP TEST RESULT NORMAL REF AMM 33-51-07. WORK ACCOMPLISHED BY MECHANIC V907894 INSPECTED BY V896995.

Part: BATTERY — DISCHARGED (SEAT 5L) · airframe 82,502 hrs · 11,612 cycles

FWD ZONE R/H EMERGENCY LIGHT NOT ILLUMINATE. TRANSFER REF NR HX WO.1849197 AND ORIGINATED BY EMP NO.V896965. CABIN SEAT 5L EMERGENCY LIGHT POWER SUPPLY AND BATTERY PACK REPLACED AND INSTALLATION TEST NORMAL AS PER AMM 33-51-07. WORK ACCOMPLISHED BY MECHANIC V907892 INSPECTED BY V896995.

Part: BATTERY — DISCHARGED (37 DEF) · airframe 82,502 hrs · 11,612 cycles

CABIN SEAT #37DEF TO SEAT #44DEF EMERGENCY LIGHT FOUND DIM FOR 15 MINUTES. TRANSFER REF NR HX WO.1711248 AND ORIGINATED BY EMP NO.V896965. M734 EMER LT POWER SUPPLY AND BATTERY PACK REPLACED AND OP TEST RESULT NORMAL REF AMM 33-51-07. WORK ACCOMPLISHED BY MECHANIC V907894 INSPECTED BY V896995.

Part: BATTERY — DISCHARGED (SEAT 16 DEF) · airframe 82,502 hrs · 11,612 cycles

CABIN SEAT #16 DEF TO SEAT #27 DEF EMERGENCY LIGHT FOUND DIM FOR 15 MINUTES. TRANSFER REF NR HX WO.1711262 AND ORIGINATED BY EMP NO.V896965. CABIN EMER LT CHARGER AND BATTERY PACK (M6758) REPLACED AND INSTALLATION TEST NORMAL AS PER AMM 33-51-07. WORK ACCOMPLISHED BY MECHANIC V907892 INSPECTED BY V896995.

Part: LENS — UNKNOWN (PDA) · airframe 82,320 hrs · 11,586 cycles

EXTERIOR LIGHT OPERATIONAL CHECK {B767-33-3-0008} - RIGHT OUTBOARD LOGO LIGHT & BOTH LEFT LOGO LIGHTS ARE OUT. REQUEST ITEM TO BE PLACED ON MEL 3345A. ITEM PLACED ON MEL 3345A. LOGO LIGHTS INOP COVER. CLEANED OUTER LOGO LIGHT ASSEMBLY ON LEFT STABILIZER AND ASSEMBLIES REQUIRE NEW COVER GASKETS, CLEAN OLD SEALANT, REPLACED BULB AND REPLACED BULB ON INNER LOGO LIGHT. BOTH REINSTALL LENS COVER AND SEALANT APPLIED. RELAMPED OUTER LOGO LIGHT BULB ON RIGHT STABILIZER. REMOVED SEALANT AND PANEL NEEDS INSTALLATION WITH SEALANT AROUND LENS INSTALLED NEW LENSES AND GASKETS ON LH INBOARD, OUTBOARD, AND RH OUTBOARD LOGO LIGHTS IN REFERENCE TO AMM 33-45-00. OPS CHECK GOOD.

Part: PUMP — MALFUNCTIONED (FUEL BOOST) · airframe 80,957 hrs · 11,375 cycles

R AFT FUEL PUMP CAS MSG HEADED TO HNL.SPEAKING TO TOMC NOW R AFT BOOST PUMP CIRCUIT BREAKERS (C371) OPENED (PULLED) & AT AFT FUEL PUMP SWITCH AT P5 PANEL. WHEN CLEARING DEFERRED COMPLIED WITH MEL COLLERED AT P6-4 PER MEL 2822N. INOP LIGHT LENS COVER INSTALLED ITEM, REMOVE COVER AND RETURN TO SPARE BULB CONTAINER. APPROVED MEL 2822N RIGHT AFT FUEL BOOST PUMP INOP. TS PER FIM 28-22 FAULT TREE 801 D1540 AT M335 RIGHT AFT FUEL BOOST PUMP AND PUMP ACCESS PANEL & SSM28-22-01-102.1 & WDM 28-22-11-1.1 PG1.1. NO PWR (115VAC)AT SECURED. 16 HOURS TO ISOLATE FAULTS. PIN #2 ON CONNECTOR D1540 (R AFT BOOST PUMP). NEEDS BOOST PUMP OPS TEST/INSULATION RESISTANCE TEST REF 28-22-00/501. FOUND K10702 R/AFT PUMP GFI CONT RELAY TRIPPED. PERFORMED FIM TASK 28-22 FAULT TREE 831. ALL CHECKS NORMAL UP TO BLOCK 5. PERFORMED AC FUEL PUMPS-INSPECTION RESISTANCE TEST PER AMM TASK OVERHEAD PUSH SWITCH. OK FOR SERVICE. 28-22-00-760-801 FOR RIGHT AFT BOOST PUMP. THE TEST IA PASSED. RUN THE PUMP AND HEARED THE PUMP IS WORKING. REMOVED MEL STICKER. MAKE SURE C/B IS PUSHED IN AND RELAMPED RIGHT AFT VERIFIED ACCOMPLISHMENT OF CDCCL STEPS RELATED TO RIGHT AFT FUEL PUMP AC INSULATION RESISTANCE TEST REF AMM TASK 28-22-00-760-801, IDT C/W. OK TO CONTINUE.

Part: COOLING FAN — FAILED (FWD IFE) · airframe 80,395 hrs · 11,294 cycles

FWD IFE COOLING EICAS S QUOT;FORWARD COOLING SYSTEM FAN FAILURE, ACTUAL SMOKE DETECTED, IFE CARD FAILURE, OR INBOARD SHUTOFF VALVE FAILED CLOSED." PER DEBRIEF OF CREW, CREW REPORTS ONLY RECVD STATUS MSG, NO OTHER FLT DECK EFFECTS NOTED, IFE SYS WORKED NORMAL. RESET SYS OPCK GOOD

Part: ACTUATOR — INOPERATIVE (RIGHT PACK) · airframe 79,747 hrs · 11,199 cycles

RIGHT PACK OFF ON CLIMB OUT THIS IS A SUPPLEMENTAL REPORT FOR THE SAME CONTROL NUMBER SUBMITTED ON 7/29/22. RIGHT PACK OFF ON CLIMB OUT. REMOVED & REPLACED R/H RAM AIR INLET ACTUATOR. OPS CHECKS NORMAL AT THIS TIME.

Part: FAILSAFE — CRACKED (STA 955) · airframe 78,800 hrs · 11,061 cycles

SUPPORT TASK - EA5340-01385 OP002, AD2012-09-04, 2EA CRACK INDICATIONS FOUND ON FAIL SAFE STRAP RUNNING FWD AND AFT OF THE FASTENER HOLE ON RH STA955 REAR SPAR BULK HEAD FAIL SAFE STRAP. TRANSFER REF. NON - ROUTINE WO.637883 AND ORIGINATED BY EMP V925917 FX RH SIDE STA 955 REAR SPAR BULKHEAD FAILSAFE STRAP PERMANENT R EPAIRED AS PER EA 5340-01385 REV ORIG OP 004 ACCOMPLISHED BY MECH V897490, INSP V906449 INSPECTED AND APPROVED BY HX170267

Part: FAILSAFE — CRACKED (STA 955) · airframe 78,800 hrs · 11,061 cycles

SUPPORT TASK - EA5340-01385 OP001, AD2012-09-04, 2EA CRACK INDICATION: FOUND ON FAIL SAFE STRAP RUNNING FWD AND AFT OF THE FASTENER HOLE ON LH STA955 REAR SPAR BULK HEAD FAIL SAFE STRAP. TRANSFER REF. NON - ROUTINE WO.637932 AND ORIGINATED BY EMP V925917 FUSELAGE LH SIDE STA 955 REAR SPAR BULKHEAD FAILSAFE STRAP PERMA NENT REPAIRED AS PER EA 5340-01385 REV ORIG OP 003 ACCOMPLISHED BY MECH V897381, INSP V906449 INSPECTED AND APPROVED BY HX170267

Part: NONE — CRACKED (N1 PYLON) · airframe 78,800 hrs · 11,061 cycles

NO.1 PYLON FWD LOWER DISCONNECT BOX UPPER R/H CUTOUT FOUND CRACK AS MARK REF HX NR WO 668480, ORIG BY V896876 NO.1 PYLON FWD MID SPAR WEB PERMANENT REPAIRED (CATEGORY A) AS P ER SRM 54-55-01-2R-2 REPAIR 2 FIG 202 ACCOMPLISHED BY MECH V912875 INSP V896816 INSPECTED AND APPROVED BY HX203175 ADD EMP:V897013

Part: BATTERY PACK — NONE (NO.1 PYLON) · airframe 78,800 hrs · 11,061 cycles

NO.1 PYLON FWD LOWER DISCONNECT BOX UPPER R/H CUTOUT FOUND CRACK AS MARK REF HX NR WO 668480, ORIG BY V896876 NO.1 PYLON FWD MID SPAR WEB PERMANENT REPAIRED (CATEGORY A) AS P ER SRM 54-55-01-2R-2 REPAIR 2 FIG 202 ACCOMPLISHED BY MECH V912875 INSP V896816 INSPECTED AND APPROVED BY HX203175 ADD EMP:V897013

Part: STIFFENER — CRACKED (NOSE WHEEL) · airframe 78,800 hrs · 11,061 cycles

SUPPORT TASK - EA5310-07143 REV D OP001 - NOSE WHEEL WELL LH STA 287 WL159 TO WL185 STIFFENER FOUND 1EA CRACK. TRANSFER REF. NON - ROUTINE WO.639289 AND ORIGINATED BY EMP V914375 LH NOSE WHEEL WELL VERTICAL STIFFENER ON STA 287 BETWEEN WL 159 AND WL 185 REPAIRED AS PER EA 5310-07143 REV D OP 003 REF HX CR.639432 SEQ 1.2116 FOR DETAIL. ACCOMPLISHED BY MECH V897381, INSP V906449 INSPECTED AND APPROVED BY HX146276 ADD EMP:V896825

Part: TRANSMITTER — INOPERATIVE (NR 1 OIL PRESS) · airframe 77,614 hrs · 10,892 cycles

NUMBER 1 OIL PRESSURE INDICATOR SHOWS NO READING. ALL OTHER ENG INDICATIONS NORMAL LOCKED TO HAVE SFO CALL TOMC TO CONFIRM REPAIRS ARE SUFFICIENT UNLOCKED FOR SFO UPDATE REMOVED OIL PRESSURE TRANSMITTER #1 ENGINE REF AMM 79-32-01-004-071-HOO. INSTALLED OIL PRESSURE TRANSMITTER REF AMM 79-32-01-404-088-HOO COMPLETED UP THRU ITEM F (6) OF PAGE 6. NEED TO ACP IDLE LEAK CHECK TEST #3. ADD EMP:U123412,U063347 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1761451 SN OFF 6796 TRANSMITTER, OI OFF 64-7900-9-0001 6796 ON 64-7900-9-0001 8411 RELOCKED UNTIL DAMAGED WIRING IS IDENTIFIED NOT TO EFFECT THE OIL PRESS SYSTEM AND OR IS REPAIRED OR HARNESS REPALCED REMOVED LOCK ACCOMPLISHED OPERATIONAL TEST OF #1 ENG OIL PRESSURE INDICATION SYSTEM PER AMM79-32-00-715-001-H00, FOUND LOOSE CANNON PLUG AND RETOURQED, RE-OPS CHECKED GOOD. ACCOMPLISHED TEST 3 PER AMM71-00-00-995-229-03 AND IDLE RAN PER AMM71-00-00-862-053-H03, OPS CHECK GOOD.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 70,110 hrs · 9,853 cycles

TWO EMERGENCY LIGHT LENS FOUND BROKEN NEAR LAV K. REPLACED THE LIGHT ASSEMBLIES.

Part: LAMP — INOPERATIVE (SWITCH) · airframe 69,929 hrs · 9,830 cycles

EMERGENCY LIGHT DISARM LIGHT LAMP INOPERATIVE. REPLACED THE LAMP IN THE EMERGENCY LIGHT DISARM SWITCH IAW AMM, OPS CHECKED GOOD.

Part: LENS — MISSING (CABIN) · airframe 69,141 hrs · 9,718 cycles

GALLEY 2 MISSING 2EA LENS COVER FOR EMERGENCY LIGHTS. GALLEY 5 MISSING 2 EA LENS COVERS FOR EMERGENCY LIGHTS. GALLEY 9 MISSING 1 EA LENS COVER FOR EMERGENCY LIGHTS. REPLACED ALL 5 LENS COVERS FOR EMERGENCY LIGHTS IN GALLEY 2,5, AND 9.

Part: HOLDER — FAULTY (EXTERIOR LIGHT) · airframe 69,141 hrs · 9,718 cycles

DOOR L3 EXT EMERGENCY LIGHT INOP. REMOVED AND REPLACED LAMP HOLDER ASSEMBLY IAW AMM 33-51-06-902-08. ALL OPS CHECKS GOOD AT THIS TIME. INSPECTED INSTALLATION AND OPERATIONAL CHECK OF L3 EMERGENCY LIGHT ASSY WITH NO DEFECTS.

Part: OVEN — MALFUNCTIONED (GALLEY) · airframe 67,707 hrs · 9,525 cycles

OVEN 107 WAS HOT EVEN THOUGH NOT IN USE ELECTRICAL ODOR COMING FROM AREA. PULLED THE CIRCUIT BREAKER AND RESET AND PERFORMED OPS CHECK NO ELECTRICAL ODOR AND OPS NORMAL.

Part: CHILLER — ODOR (RT AFT GALLEY) · airframe 67,593 hrs · 9,509 cycles

AFT GALLEY CHILLERS OVERHEATED. BURNING SMELL NOTED. R&R RIGHT AFT GALLEY CHILLER IAW AMM 25-33-02-01. OPS CHECK GOOD . NO DEFECTS NOTED.

Part: CONNECTOR — LOOSE (CABIN) · airframe 66,414 hrs · 9,346 cycles

FOUND EMERGENCY ESCAPE PATH LIGHTS IN ROW 26D, 26F, 27D, 27F INOP . FOUND CONNECTOR UNDER ROW 25 LOOSE. RESECURED AND OPS CHECK GOOD OF EMERGENCY PATH LIGHTS IN ROW 26 AND 27 DEF

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 65,992 hrs · 9,285 cycles

EMERGENCY LIGHT FAILED OPS TEST, TROUBLESHOOTING FOUND BATTERY PACK EQ M1208 CANNOT CHARGE. BATTERY PACK REPLACED AND OPS CHECKED NORMAL IAW AMM 33-51-07.

Part: LIGHT — NO TEST (CABIN) · airframe 65,992 hrs · 9,285 cycles

SEATS 25DEF AND 40DEF EMERGENCY LIGHT INOPERATIVE. THE EMERGENCY LIGHT WAS REPLACED AND INSTALLATION TEST NORMAL IAW AMM 33-51-10.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 65,992 hrs · 9,285 cycles

EMERGENCY LIGHT OP TEST TROUBLESHOOTING FOUND BATTERY PACK EQ M1210 CANNOT CHARGE. THE BATTERY PACK WAS REPLACED AND OP TEST RESULT NORMAL AS PER AMM 33-51-07.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 65,992 hrs · 9,285 cycles

EMERGENCY LIGHT FAILED OPS TEST. TROUBLESHOOTING FOUND BATTERY PACK EQ M1208 CANNOT CHARGE. THE BATTERY PACK WAS REPLACED AND OPS CHECKED NORMAL IAW AMM 33-51-07.

Part: SKIN — DENTED (BS 360) · airframe 65,992 hrs · 9,285 cycles

FOUND A DENT AT BS 360 BETWEEN STRINGERS 20 AND 21L. REPAIRED IAW ECRA 5330-0591, REV- PART 1.

Part: LIGHT — INOPERATIVE (SEAT 5D) · airframe 65,285 hrs · 9,181 cycles

RIGHT AISLE EMERGENCY LIGHT INOPERATIVE IN SEAT 5D. REMOVED AND REPLACED THE EMERGENCY LIGHT. OPS GOOD.

Part: SHUTOFF VALVE — INOPERATIVE (LT BLEED SYS) · airframe 51,427 hrs · 7,242 cycles

DURING ENGINE RUN FOUND LT BLEED AT 55 PSI AND RT AT 45 PSI AT TAKEOFF POWER SETTING WITH BLEEDS ON PACKS OFF, WITH PACKS ON LT BLEED OSSICILATES FROM 40-60 PSI LT SIDE. R & R NR 1 ENG PRSOV, REF MM 36-11-09. OPS CK GOOD. ROTABLE PARTS CHANGE WAS INDICATED - TT 1597264, SN OFF 02042 VALVE, SHUTOFF, OFF 64-3611-9-0008 2042 ON 64-3611-9-0008 9013.

Part: DISPLAY — FAILED (COCKPIT) · airframe 48,096 hrs · 6,794 cycles

F/O NAVIGATIONAL DISPLAY INOPERATIVE. REMOVED & REPLACED F/O DISPLAY UNIT IAW MM 31-63-03-404-00 5. SYS OPS CHECKED GOOD. ALSO PERFORMED TEST NR 30 IAW FIM 22-00- 02. NO FAULTS NOTED.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 46,422 hrs · 6,585 cycles

DOOR 2R AFT FACING JUMPSEAT FLASHLIGHT NOT FLASHING RED LIGHT. REMOVED AND REPLACED FLASHLIGHT BATTERY P/N-25-2500-3-0012 AT JUMPSEAT 2R PER GMM 05-20-10. OPS CHECK GOOD. FLASHLIGHT SAFETY STRAP OK.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 45,479 hrs · 6,465 cycles

CABIN FLOOR SUPPORT CORRODED AT STA 326 LBL 30 TO LBL 57. CABIN STA 326 LBL 10 LBL 68 FLOORBEAM UPPER CHORD REPAIRED AS PER SRM 53-00-51 REPAIR 1 AND HFEC NIL CRACK FOUND.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 37,270 hrs · 5,435 cycles

L1 DOOR EXTERIOR EMERGENCY SLIDE LIGHT IS INOPERATIVE. REMOVED AND REPLACED BULB IN EXTERIOR SLIDE LIGHT, OPS CHECK GOOD IAW AMM 33-51-06.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 33,395 hrs · 4,934 cycles

CABIN BODY STATION 303, LBL 30 FLOOR SUPPORT FOUND CORRODED. CABIN BODY STATION 303 FLOORBEAM LBL 9 - LBL 37 REPAIRED PER SRM 53-00-51, FIG 201, REPAIR 1 AND HFEC NO CRACK FOUND.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 22,274 hrs · 3,390 cycles

INSPECTION FOUND FLOORBEAM CORRODED AT BS 325, LBL 30-55. THE CORROSION WAS REMOVED AND THE FLOORBEAM WAS REPAIRED IAW SRM 53-00-51, REPAIR 1.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 22,274 hrs · 3,390 cycles

INSPECTION FOUND FLOORBEAM CORRODED AT BS 303, LBL 25-30. THE CORROSION WAS REMOVED AND A REPAIR WAS INSTALLED IAW SRM 53-00-51, REPAIR 1.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 22,274 hrs · 3,390 cycles

INSPECTION FOUND FLOOR SUPPORT CORRODED AT BS 303-325, LBL 30. THE FLOOR SUPPORT WAS REPLACED IAW SRM 51-40-02.

Part: CHARGER — INOPERATIVE (BS 401) · airframe 18,057 hrs · 2,799 cycles

THE EMERGENCY LIGHTS AT STA 401 WOULD NOT TEST. THE EMERGENCY LIGHT BATTERY CHARGER AT STA 401, WL 204, RBL 95 WAS REMOVED AND REPLACED IAW MM 33-51-07.

Part: CHARGER — INOPERATIVE (BS 841) · airframe 18,057 hrs · 2,799 cycles

THE EMERGENCY LIGHTS AT STA 841 WOULD NOT TEST. THE EMERGENCY LIGHT BATTERY CHARGER AT STA 841, WL 204, RBL 95 WAS REMOVED AND REPLACED IAW MM 33-51-07.

Part: ELECTRICAL BOX — SHORTED (ROW 26 DEF) · airframe 17,513 hrs · 2,721 cycles

THE FLIGHT CREW REPORTED SMOKE IN THE CABIN WHILE EN ROUTE FROM HNL TO GUM. THE SMOKE WAS COMING FROM THE DSEB UNDER ROW 26 DEF. THE IFE FOR THAT ZONE WAS TURNED OFF AND THE SMOKE DISSIPATED. THE FLIGHT WAS CONTINUED TO GUM WHERE IT LANDED WITHOUT FURTHER PROBLEM. MAINTENANCE REMOVED AND REPLACED THE DSEB PER MM 23-32-74. THE WIRE HARNESS WAS INSPECTED AND NO PROBLEMS WERE NOTED WITH THE HARNESS OR PINS. OPERATION OF THE IFE SYSTEM AT ROW 26 DEF CHECKED GOOD.

Part: MONITOR — INOPERATIVE (SEAT 27L) · airframe 15,456 hrs · 2,429 cycles

THE VIDEO LCD MONITOR AT THE SEAT BACK OF SEAT 27L BECAME HOT TO THE TOUCH AND BEGAN TO SMOKE WHILE EN ROUTE FROM EWR TO HNL. THE SEATS IN THE ZONE FROM ROW 23 TO ROW 27 WERE POWERED OFF AND THE SMOKE CEASED. THE FLIGHT WAS CONTINUED TO HNL WHERE IT LANDED WITHOUT FURTHER INCIDENT. THE AREA AND HARNESS WERE INSPECTED FOR DAMAGE AND NONE WAS FOUND. THE FAULT WAS ISOLATED TO THE MONITOR AND THE MONITOR WAS REPLACED IAW MM 23-32-83. OPERATIONAL CHECKS WERE NORMAL.