N649UA

Part: ENGINE — FOD (LEFT) · airframe 131,018 hrs · 20,068 cycles

IN CLIMB WITH CLIMB POWER SET EXCESSIVE VIBRATION LEFT ENGINE. 5 .0 VIB WITH FEEL/SOUND.AFTER LANDING IT WAS FOUND AT THE ENGINE NR 1 SIGNALS OF BIRD STRIKE, WITH BLOOD AND STRONG SMELL OF BIRD. AFTER INSPECTION OF BIRD STRIKE REFER AMM 05-51-18-212-001, REMOVED THE INLET CONE REFER AMM 72-31-01-024-001-N00, RECORDED THE BLADES SEQUENCE AND IT WAS FOUND BLADES AT POSITIONS 18, 19, 20, 21, 22, 23, 34, 35 AND 36 DAMAGED, ONE OUTLET GUIDE VANE AT 1 O'CLOCK POSITION WITH MISSING MATERIAL AND PANEL NR 1 OF THE FAN EXIT LINER SEGMENT OUTTER PANEL WITH HOLE. FOR FURTHER EVALUATE IT'S IS NECESSARY TO REMOVE SPINNER FRONT CONE, SPINNER REAR CONE AND FAN BLADES DAMAGED FOR REFERENCE SEE AMM 72-31-02/401. IT WAS REMOVED SPINNER FRONT CONE, SPINNER REAR CONE IAW AMM 72-31-01-024-001-N00. IT WAS REMOVED ENGINE NR 1 FAN BLADES FULL SET AS PER AMM 72-31-02-004-012-N00. INITIATED BIRD STRIKE INSPECTION BY EC/RA 7200-07362, PERFORMED SHEET 1 BLOCKS 1 AND 10. FOUND SEVERAL DAMAGES AT ENGINE FAN BLADES NUMBER 18, 19, 20, 21, 22, 23, 34, 35 AND 36. NECESSARY TO CONTINUE BLOCK 11 BOROSCOPE INSPECTION. NECESSARY BOROSCOPE INSPECTION BY EC/RA 7200-07362 SHEET 1 BLOCK 11. IT WAS ACCOMPLISHED BORESCOPE INSPECTION AS PER EC/RA 7200-07362 SHEET 1 - BLOCK 11, NO ABNORMAL CONDITION FOUPERFORMED TASK 71-00-00-725-008-N00 TEST 8 VIBRATION SURVEY VIBRATION VALUES WITHIN LIMITS DETERMINED PER TASK ABOVE

Part: HANDLE — OUT OF ADJUST (ZONE 800) · airframe 130,701 hrs · 20,028 cycles

DOOR 1R YELLOW. EMERG EXIT. FLAG POPS UP BEHIND VICE IN FRONT OF RED. PULL. HANDLE ADJUSTED DOOR 1R YELLOW EMERGENCY FLAG SO THE FLAG GOES INTO ITS PROPPER POSITION ADD EMP: U376824

Part: LAMP — NO TEST (ZONE 200) · airframe 130,423 hrs · 19,995 cycles

OPERATIONAL TEST - EMERGENCY ESCAPE PATH LIGHTING (EEL) SYSTEM PERFORM OPERATIONAL CHECK - PATH LIGHT 6D DOESN'T WORK. REMOVED AND REPLACED LAMP ASSY REF 33-51-10-962-105, GOOD FOR SERVICE.

Part: CONTROL MODULE — FAULTED (ZONE 100) · airframe 130,359 hrs · 19,987 cycles

AFTER TO ALL FWD GALLEY OVENS AND CHILLERS INOP. AFT R COFFEPOT INOP OPERATED GALLEY OVENS/CHILLERS FOR APPROX 25 MIN AT HIGH PWR UNABLE TO DUP. PLEASE CHECK KVA SETTING OF FWD ELCU PER NAT DRAWING N0542-D73 WD 25-31-11, PINS 11 & 14 ARE JUMPERED. IF NO DEFECT CONT.. INSPECT GALLEY DISC D9066 FOR SECURITY AND INSPECT PINS FOR DAMAGE. ALSO INSPECT D378 OF FWD ELCU M225 AND MAIN FEEDER CABLES A1,A2,B1,B2,C1,C2, IF NO FAULTS REPLACE THE FWD ELCU M225 AND BPCU AS A PRECAUTION VERIFIED CORRECT KVA SETTING WITH PINS 11 AND 14 JUMPER OF D378, CONTINUITY CHECKED GOOD. REF NAT DRAWING N0542-D73. PERFORMED GVI OF D378 AND FEEDER CABLES A1,A2,B1,B2,C1,C2 AT M225 ELCU, NO ISSUES FOUND. REF AMM 25-31-03-404-009, NAT DRAWING N0542-D73. R & R BPCU REF AMM 24-41-03-404-008, OPS CHECKED OK. R & R ELC REF AMM 25-31-03-404-009 , OPS CHECKED OK. DURING ENGINE RUNS VERIFIED GALLEY POWER DID NOT SHED POWER WITH LOAD SUPPLIED. GALLEY POWER CHECKED GOOD.

Part: LIGHT — BROKEN (ZONE 200) · airframe 130,126 hrs · 19,959 cycles

EMERGENCY LIGHTS OPERATIONAL CHECK, EMERGENCY LIGHT ON SEATS 35F AND 48F ARE BROKEN. REMOVED AND REPLACED EMERGENCY LIGHT ON SEATS 35F AND 48F REF CMM 25-21-53. GOOD FOR SERVICE.

Part: SIGN — DAMAGED (ZONE 200) · airframe 128,189 hrs · 19,719 cycles

30R EXIT ROW PLASTIC NOT SECURED BRACKET FOR LENS COVER IS DAMAGED. INSTALLED TAPE TO SECURE IN PLACES WAITING ON ECRA FOR SIGN OFF. PICTURES ADDED COMPLIED WITH ECRA 3351-01489 PART 1 AND 2 INITIATED DIP TO COMPLY WITH PART 3 IN 3 FLIGHT CYCLES OK TO CARRY FOR PERMANENT REPAIR WITHIN 3 FLT CYCLES PER ECRA 3351-01489, WILL REQUIRE REPETITIVE INSPECTION PRIOR TO EACH DEPT. QC REVIEWED RECORDS REMOVED AND REPLACED EXIT SIGN AT ROW 30 RH SIDE REF AMM 33-51-01 OPS TEST GOOD.

Part: ENGINE — BIRD INGESTION (RIGHT) · airframe 128,066 hrs · 19,698 cycles

REJECTED T/O ENG SRG D2 PSBL BIRD INGEST RT ENG SPEED 160 HIGHE ST BTMS 9+ CREW DEBRIEF: 160 KTS, APPROACHING T/O SPEEDS, SAW BIRD FLY IN F RONT OF ACFT, HEARD A BANG ON E2, OBSERVED MOMENTARY DROP AND RE COVERY OF EPR. CAPT SIMULTANEOUSLY THROTTLED DOWN FOR RTO. TOWER REPORTED A FLASH AT E2 ALSO. INSP INLET/EXHAUST- NO EVIDENCE OF BIRD STRIKE. SMELL OF BURNT BIRD NOT PRESENT EITHER. SUSPECT CO MPRESSOR STALL. ALL BRAKE TEMPS WERE NORMAL WHEN ACFT BLOCKED IN , FUSE PLUGS ALL INTACT. LOCKED FOR FINDINGS REF AMM 05-51-14 FOR REQUIRED INSP PERFORMED HIGH ENERGY STOP INSPECTION REF AMM-TASK 05-51-14-212-089. FOUND NO DAMAGE, FUSE PLUGS NORMAL. F.I.M 71-08 FAULT TREE 804 HAS US CHECK THE PS3 AIR FILTER ELEMENT AND THE PNEUMATIC RELAY VALVE ON THE 2.9 BLEED VALVE. FOUND ELEMENT RESTRICTED( DIRTY) UNLOCKED FOR SIGN OFF F.I.M 71-05 TREE 803 FINISHED . SOME WORK DONE ON LOGPAGES 3590303, 3586644 AND 3590561. PROBLEM WAS CLOGGED PS3 FILTER ELEMENTS ON 2.8 BLEED VALVE. REMOVED AND REPLACED BOTH PS3 AIR FILTERS AND 1 PS3 AIR FILTER ASSEMBLY ON 2.8 BLEED VALVE I.A.W ADD EMP:U242424,U365605 A.M.M 75-33-05 . COMPLETED F.I.M 71-08 TREE 804 OPS CHECK GOOD. VALVE AND SOLENOID WORK AS DESIGNED

Part: TRIM SWITCH — FAULTED (STAB) · airframe 126,045 hrs · 19,441 cycles

STAB TRIM EICAS CAME ON ON INIT CLIMBOUT PERFORMED TROUBLESHOOTING PROCEDURE FOR STAB TRIM REF FIM 27-48 TASK 809, FAULTING LEFT HYDRAULIC BRAKE PRESSURE SWITCH STAB TRIM MESSAGE NO LONGER ACTIVE REFERENCE LOG PAGE 8475892 FOR ACTION TAKEN. LEFT HYDRAULIC BRAKE PRESSURE SWITCH FAULTED ON STAB TRIM BOX DURING TROUBLESHOOTING. SETTED LEFT AND CENTER STAB TRIM SHUTOFF VALVE SWITCHES TO CUTOFF. REF B767 AMM 27-41-07 STEP 2E(3) REMOVED AND REPLACED LEFT HYDRAULIC BRAKE PRESSURE SWITCH REF AMM 27-41-07. OPS CK GOOD, LEAK CK GOOD. NO DEFECTS NOTED. NO MESSAGES SHOWING PARTS USED: 75-2741-3-0088,QTY :1

Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 124,775 hrs · 19,293 cycles

CABIN LIGHTING OPERATIONAL CHECK {B767-33-3-7008} - DIRECT CELING LIGHT AT POSITION 10A, 10D, 10D INOPERATIVE REPLACED THE LAMP REF AMM TASK 33-22-00-962-036 NO HELP.MEL DIRECT CELING LIGHT AT POS ITION 10A, 10D, 10L(CORRECTION) 3321A NEED MORE TIME TO FURTHER TROUBLESHOOTING. PLACED ON MEL 3321A DDP C/W. APPROVED UNPLAGED AND REPLUGED BALLIST. LIGHTS OPERAT NORMALY NOW

Part: NONE — NONE (NONE) · airframe 124,017 hrs · 19,181 cycles

PASSENGER AT SEAT 9L LOST LAPTOP DOWN THE SIDEWALL. LAPTOP WAS POWERED UP AT THE TIME IT WAS LOST LAPTOP WAS FOUND AND RETURNED TO PAX AT. 9L.

Part: RELAY — DAMAGED (P19 PANEL) · airframe 122,443 hrs · 18,948 cycles

ELETRICAL BURNING ODOR FROM FWD GALLEY/FWD PORTION OF FIRST CLASS 10 MINUTES INTO FLIGHT. PERFORMED CONDITIONAL INSPECTION IAW AMM 05-51-56-940-801-C1. FOUND SIDEWALL LIGHT BALLAST AT SEAT 1A TO BE SOURCE OF ELEC ODOR. NEEDS BALLAST 76-3321-3-0013. R+R BALLAST M745, NO HELP. T/S FURTHER, FOUND PIN 7 AT CONNECTOR D5110P BURNED, SUSPECT RELAY K365 FAILURE, RESULTING IN BURNED PIN, REF WDM 33-21-31 SHEET 2B. R+R RELAY S365. ALSO FOUND HIGH RESISTANCE ACROSS TERMINALS OF SWITCH S9102. RETERMINATED WIRES, LIGHTS NOW OPS CHECK GOOD. STILL NEED CONNECTOR D5110P. UPDATING FOR ''SDR'' RPL CONNECTOR D5110P, NO DEFECTS FOUND ON PINS. REF WD 33-21-32-1A, 33-21-31 AND SWPM 20-61-11. FIRST CLASS LIGHTS OP NORMAL AND 1A SIDEWALL LIGHT OVERHEAD TOGGLE SWITCH OPS NORMAL. NO ABMORMAL SMELLS ABOVE FIRST CLASS CEILING AREA. CLOSED CEILING PANELS.

Part: PRESSURE SWITCH — NO TEST (HYD SYS C) · airframe 122,078 hrs · 18,896 cycles

RAT DID NOT PRESSURIZE CENTER HYDRAULIC SYSTEM. RAM AIR TURB MODULE PRESSURE SWITCH REPLACED AND TEST RESULT NORMAL AS PER AMM 29-21-11 AMD 29-21-00. WORK ACCOMP BY MECH V924756 INSP BY V924743. ADD EMP:V924743

Part: SKIN — CRACKED (DR 1L) · airframe 122,075 hrs · 18,895 cycles

SUPPORT TASK - EA3515-01152 OP001 - 1EA FASTENER HOLE FOUND CRACK AT 8O''CLOCK (COUNT FROM INBOARD) ON FUSELAGE SKIN LAYER TRANSFER REFER NON-ROUTINE WO.1843962 AND ORIGINATED BY EMP V924735 RII INSPECTED OKAY BY HX 310582 ADD EMP:V896895 FUSELAGE SKIN DOOR 1L CUTOUT AFT CORNER REMOVED AS PER ECRA 5315-01199 REV - PART 1 ITEM A INTERIM REPAIR ATTACH MAINTENANCE WORK SHEET FORM 44-0008 ITEM 1 TO ITEM 44 ACCOMPLISHED BY MECH V897473 AND INSPECTED BY V896919 ADD EMP:V896919 SFR 1032881 INSPCTED OKAY BY V896895 ADD EMP:V896895

Part: SKIN — CRACKED (DR 1R) · airframe 122,075 hrs · 18,895 cycles

SUPPORT TASK - EA5315-01152 OP 002 1EA FASTENER HOLE FOUND CRACK AT 2O''CLOCK AND 8O''CLOCK (COUNT FROM INBOARD) ON FUSELAGE SKIN LAYER- TRNAFER REFER NON-ROUTINE WO.1843964 AND ORIGINATED BY V924735 RII INSPECTED OKAY BY HX 310582 ADD EMP:V896895 FUSELAGE SKIN DOOR 1R CUTOUT AFT CORNER REPAIRED AS PER ECRA 5515-01200 REV - PART 1 ITEM A INTERIM REPAIR ATTACH MAINTENANCE WORK SHEET FORM 44-0008 ITEM 1 TO ITEM 44 ACCOMPLISHED BY MECH V897473 AND INSPECTED BY V896919 ADD EMP:V896919 SFR 1032882. RII INSPECTED BY HX310582 ADD EMP:V896895

Part: SKIN — CORRODED (RH FUEL TANK) · airframe 122,075 hrs · 18,895 cycles

B767-28-3-0067, RHW FUEL TANK OVERWING FILL PORT ATTACH UPPER SKIN FOUND CORROSION REF HX NR WO.1865480, ORIG BY V897897 RHW FUEL TANK OVERWING FILL PORT UPPER SKIN PANEL CORROSION REPAIRED AS PER ECRA 5725-01126 REV.- ATTACHED MAINTENANCE WORK SHEET FORM 44.0008 ITEM 1 TO ITEM 37 ACCOMPLISHED ACCOMPLISHED BY MECH V897537, INSP V897897 RII INSPECTED BY HX147141. ADD EMP:V897897

Part: INTERCOSTAL — CORRODED (STA595) · airframe 122,075 hrs · 18,895 cycles

B767-53-3-7025 - FWD CARGO COMPT STA595 RH PDU LH AND RH MOUNT NUTS SUPPORT BEAMS FOUND CORROSION TRANSFER REF HXWO 1858999 AND ORIGINATED BY EMP V896810 FWD CARGO COMPT STA588-610 RBL33 SUPPORT BEAM (143T0019-11) (MINOR REPAIR) ATTACH MAINTENANCE WORK SHEET FORM 44-0008 REPLACED AS PER SRM51-10-02 AND FASTENER INSTALLED AS PER ITEM 1 TO ITEM 30 ACCOMPLISHED SRM51-40-02 (PSE REPLACED) AND STA588 TO STA600 RBL33 WORK ACCOMPLISHED BY MECHANIC V897467 INSPECTED BY V896375 SUPPORT BEAM (143T5019-2) REPAIRED AS PER ECRA 5330-07097 REV- RII INSPECTED BY HX156019 ADD EMP:V897897

Part: CHANNEL — CORRODED (STA 478-500) · airframe 122,075 hrs · 18,895 cycles

B767-53-3-7023, FWD CGO COMPT- STA 478 TO 500, RBL 33" LONGITUDINAL FLR SUPPORT LWR SURFACE FOUND CORROSION CRACK TRANSFER REF HXWO 1883016 AND ORIGINATED BY EMP V930061 FWD CARGO COMPT STA470 TO STA498 RBL30" LONGITUDINAL FLOOR WORK ACCOMPLISHED BY MECHANIC V897549 INSPECTED BY V896375 SUPPORT REPLACED AS PER SRM51-10-02 AND FASTENER INSTALLED AS PER SRM 51-40-02 ATTACH MAINTENANCE WORK SHEET FORM 44-0008 ITEM 1 TO ITEM 14 ACCOMPLISHED RII INSPECTED BY HX169509 ADD EMP:V898550

Part: INTERCOSTAL — CORRODED (STA 527-544) · airframe 122,075 hrs · 18,895 cycles

B767-53-3-7025 FWD CGO BTW STA 527 - STA 544 UNDER GR PDU INTERNAL 2EA WEB SUPPORT BEAM FOUND CORROSION TRANSFER REF HXWO 1858981 AND ORIGINATED BY EMP V896375 FWD CARGO STA524-541 RBL33.08 FLOOR SUPPORT BEAM REPLACED WORK ACCOMPLISHED BY MECHANIC V897467 INSPECTED BY V896375 AS PER SRM51-10-02 AND FASTENER INSTALLED AS PER SRM51-40-02 ATTACH MAINTENANCE WORK SHEET FORM 44-0008 ITEM 1 TO ITEM 18 ACCOMPLISHED RII INSPECTED BY HX169509 ADD EMP:V898550

Part: UNKNOWN — CORRODED (STA 583) · airframe 122,075 hrs · 18,895 cycles

B767-53-3-7025 FWD CGO COMPT STA 583 RH PDU LH MOUNT NUT SUPPORT BEAM FOUND CORROSION TRANSFER REF HXWO 1858982 AND ORIGINATED BY EMP V896810 FWD CARGO COMPT STA583 RBL30-RBL40 SUPPORT BEAM REPLACED WORK ACCOMPLISHED BY MECHANIC V897467 INSPECTED BY V896375 AS PER SRM51-10-02 AND FASTENER INSTALLED AS PER SRM51-40-02 ATTACH MAINTENANCE WORKSHEET FORM 44-0008 ITEM 1 TO ITEM 13 ACCOMPLISHED RII INSPECTED BY HX169509 ADD EMP:V898550

Part: UNKNOWN — CORRODED (STA 500 - 522) · airframe 122,075 hrs · 18,895 cycles

B767-53-3-7025 FWD CGO BTW STA 500 - 522 R/H TORQUE BOX WEB FOUND CORROSION TRANSFER REF HXWO 1858980 AND ORIGINATED BY EMP V896375 FWD CARGO STA497 TO STA541 RBL25 TO RBL40 TORQUE BOX WEB WORK ACCOMPLISHED BY MECHANIC V897549 INSPECTED BY V898550 REPLACED AS PER SRM51-10-02 AND FASTENER INSTALLED AS PER SRM51-40-02 ATTACH MAINTENANCE WORK SHEET FORM 44-0008 ITEM 1 TO ITEM 9 ACCOMPLISHED RII INSPECTED BY HX185167 ADD EMP:V897008

Part: INTERCOSTAL — CORRODED (STA502-512) · airframe 122,075 hrs · 18,895 cycles

B767-53-3-7025 - FWD CARGO FLOOR STA502-512 RBL36.88 SUPPORT BEAM FOUND CORROSION TRANSFER REF HXWO 1877224 AND ORIGINATED BY EMP V896810 FWD CARGO FLOOR STA502 TO STA512 RBL36.88 FLOOR SUPPORT BEAM WORK ACCOMPLISHED BY MECHANIC V897549 INSPECTED BY V896375 REPLACED AS PER SRM51-10-02 AND FASTENR INSTALLED AS PER SRM51-40-02 ATTACH MAINTENANCE WORK SHEET FORM 44-0008 ITEM 1 TO ITEM 9 ACCOMPLISHED RII INSPECTED BY HX169509 ADD EMP:V898550

Part: FLOOR SUPPORT — CORRODED (STA 498) · airframe 122,075 hrs · 18,895 cycles

B767-53-3-7023, FWD CGO COMPT- STA 498 RBL 39" LATERAL TORQUE BOX PNL SUPPORT CHORD LWR SURFACE FOUND CORROSION TRANSFER REF HXWO 1883060 AND ORIGINATED BY EMP V930061 FWD CARGO COMPT STA498 RBL30 TO RBL40 LATERAL TORQUE BOX WORK ACCOMPLISHED BY MECHANIC V897549 INSPECTED BY V896375 PANEL SUPPORT CHORD REPLACED AS PER SRM51-10-02 AND FASTENER INSTALLED AS PER SRM51-40-02 , ATTACH MAINTENANCE WORKSHEET FORM 44-0008 ITEM 1 TO ITEM 9 ACCOMPLISHED RII INSPECTED BY V898550 ADD EMP:V898550

Part: INTERCOSTAL — CORRODED (STA 550) · airframe 122,075 hrs · 18,895 cycles

B767-53-3-7025 FWD CGO COMPT STA 550 TR PDU LH MOUNT NUT SUPPORT BEAM FOUND CORROSION TRANSFER REF HXWO 1858966 AND ORIGINATED BY EMP V896510 FWD CARGO COMPT STA544-566 RBL25 AND RBL33.08 SUPPORT WORK ACCOMPLISHED BY MECHANIC V897549 INSPECTED BY V896375 BEAM REPLACED AS PER SRM51-10-02 AND FASTENER INSTALLED AS PER SRM51-40-02 ATTACH MAINTENANCE WORK SHEET FORM 44-0008 ITEM 1 TO ITEM 14 ACCOMPLISHED RII INSPECTED BY HX169509 ADD EMP:V898550

Part: UNKNOWN — CORRODED (STA512 RBL30-34) · airframe 122,075 hrs · 18,895 cycles

B767-53-3-7025 - FWD CARGO FLOOR STA512 RBL30-34 SUPPORT BEAM FOUND CORROSION TRANSFER REF HXWO 1877229 AND ORIGINATED BY EMP V896810 FWD CARGO FLOOR STA512 RBL30-40 SUPPORT BEAM REPLACED AS WORK ACCOMPLISHED BY MECHANIC V897549 INSPECTED BY V896375 PER SRM51-10-02 AND FASTENER INSTALLED AS PER SRM51-40-02 ATTACH MAINTENANCE WORK SHEET FORM 44-0008 ITEM 1 TO ITEM 9 ACCOMPLISHED RII INSPECTED BY HX169509 ADD EMP:V898550

Part: WEB — CORRODED (FWD CRGO COMPT) · airframe 122,075 hrs · 18,895 cycles

B767-06-3-7050, FWD CGO COMPT STA 592 "9R" PDU BELOW MOUNTING SUPPORT BRACKET SHEAR WEB AREA FOUND CORROSION TRANSFER REF HXWO 1878888 AND ORIGINATED BY EMP V930061 FWD CARGO COMPT STA541-STA600 RBL25 TO RBL40 FLOOR BEAM WEB WORK ACCOMPLISHED BY MECHANIC V897549 INSPECTED BY V896375 REPLACED AS PER SRM51-10-02 AND FASTENER INSTALLED AS PER SRM51-40-02 ATTACH MAINTENANCE WORKSHEET FORM 44-0008 ITEM 1 TO ITEM 8 ACCOMPLISHED RII INSPECTED BY HX169509 ADD EMP:V898550

Part: FASTENER — DAMAGED (FWD CRGO DR) · airframe 122,075 hrs · 18,895 cycles

SUPPORT TASK FWD CARGO COMPT DOOR EXTERIOR FASTENER HAS LIGHTNING STRIKE 65" FROM AFT & 46" FROM LOWER EDGE TRANSFER REF HXWO 1857673 AND ORIGINATED BY EMP V896888 FWD CARGO COMPT DOOR EXTERIOR SKIN STA552 INTERIM REPAIRED AS PER ECRA 5232-01174 REV - PART 1 ATTACH FORM 44-0008 ITEM 1 TO ITEM 26 WORK ACCOMPLISHED WORK ACCOMPLISHED BY MECHANIC V920531 INSPECTED BY V896375 RII INSPECTED BY HX169509 ADD EMP:V898550

Part: SKIN — DAMAGED (STR22R-23R) · airframe 122,075 hrs · 18,895 cycles

B767-06-3-7083 - FUSELAGE SKIN HAS LIGHTNING STRIKE AT BS654+44-BS654+66 BTW S22R / S23R TRANSFER REF HXWO 1839295 AND ORIGINATED BY EMP V896888 FUSELAGE SKIN AT STA654+44 TO STA654+66 BETWEEN STR22R-23R WORK ACCOMPLISHED BY MECHANIC V897549 INSPECTED BY V896375 SKIN REPAIRED AS PER SRM53-00-01-2R-6 REPAIR 6 FIG.201 (CATEGORY A REPAIR) ATTACH MANITENANCE WORKSHEET FORM 44-0008 ITEM 1 TO ITEM 22 ACCOMPLISHED RII INSPECTED BY HX169509 ADD EMP:V898550

Part: INTERCOSTAL — CORRODED (STA 478 - 500) · airframe 122,075 hrs · 18,895 cycles

B767-53-3-7023, FWD CGO COMPT- STA 478 TO 500 RBL 39" LONGITUDINAL FLR SUPPORT LWR SURFACE FOUND CORROSION AS MARK TRANSFER REF HXWO 1883040 AND ORIGINATED BY EMP V930061 FWD CARGO COMPT STA478 TO 497 RBL39" LONGITUDINAL FLOOR WORK ACCOMPLISHED BY MECHANIC V897549 INSPECTED BY V896375 SUPPORT REPLACED AS PER SRM51-10-02 AND FASTENER INSTALLED AS PER SRM51-40-02 ATTACH MAINTENANCE WORK SHEET FORM 44-0008 ITEM 1 TO ITEM 9 ACCOMPLISHED RII INSPECTED BY HX169509 ADD EMP:V898550

Part: UNKNOWN — CORRODED (STA 502 RBL 39) · airframe 122,075 hrs · 18,895 cycles

B767-53-3-7023, FWD CGO COMPT STA 502 RBL 39" LATERAL TORQUE BOX PNL SUPPORT CHORD LWR SURFACE FOUND CORROSION TRANSFER REF HXWO 1883048 AND ORIGINATED BY EMP V930061 FWD CARGO COMPT STA502 RBL30 TO RBL40 LATERAL TORQUE BOX PANEL SUPPORT CHORD REPLACED AS PER SRM51-10-02 AND FASTENER INSTALLED AS PER SRM51-40-02 ATTACH MAINTENANCE WORKSHEET FORM 44-0008 ITEM 1 TO ITEM 9 ACCOMPLISHED RII INSPECTED BY HX169509 ADD EMP:V898550 WORK ACCOMPLISHED BY MECHANIC V897549 INSPECTED BY V896375 ADD EMP:V896375

Part: STRINGER — CORRODED (STA 1540) · airframe 122,075 hrs · 18,895 cycles

B767-53-3-7058 AFT OF BULK CGO BILGE STA 1540 S38L STRINGER FOUND CORROSION TRANSFER REF HXWO 1856266 AND ORIGINATED BY EMP V896810 BULK CARGO COMPT BILGE AREA STA1540 STRINGER 38L INTERIM REPAIRED AS PER ECRA 5361-01114 REV - PART 1 ATTCH FORM 44-0008 ITEM 1 TO ITEM 28 ACCOMPLISHED , WORK ACCOMPLISHED BY MECHANIC V897381 INSPECTED BY V896375 RII INSPECTED BY HX169517 ADD EMP:V898549

Part: SKIN — CORRODED (STA 1540) · airframe 122,075 hrs · 18,895 cycles

B767-53-3-7058 AFT OF BULK CGO BILGE STA 1540 S39 POS INNER SKIN FOUND CORROSION TRANSFER REF HXWO 1856087 AND ORIGINATED BY EMP V896810 FUSELAGE STA1540-STA1562 BETWEEN STR39L AND STR39R SKIN INTERIM REPAIRED AS PER ECRA5361-01114 REV - PART 1 ATTACH FORM 44-0008 ITEM 1 TO ITEM 35 ACCOMPLISHED WORK ACCOMPLISHED BY MECHANIC V897381 INSPECTED BY V896375 RII INSPECTED BY HX169517 ADD EMP:V898549

Part: STRINGER — CORRODED (STA 1540 - 1562) · airframe 122,075 hrs · 18,895 cycles

B767-53-3-7058 AFT OF BULK CGO BILGE STA1540 TO STA1562 S39L STRINGER FOUND CORROSION TRANSFER REF HXWO 1856237 AND ORIGINATED BY EMP V896810 BULK CARGO COMPT BILGE AREA STA1540 TO STA1562 STRINGER 39L INTERIM REPAIRED AS PER ECRA 5361-01114 REV - PART 1 ATTACH FORM 44-0008 ITEM 1 TO 28 ACCOMPLISHED WORK ACCOMPLISHED BY MECHANIC V897381 INSPECTED BY V896375 RII INSPECTED BY HX169517 ADD EMP:V898549

Part: DOOR FRAME — CRACKED (STA542) · airframe 122,075 hrs · 18,895 cycles

B767-06-3-7011 FWD CARGO : FWD CARGO DOOR AT STA 542 FRAME LOWER PORTION FOUND CRACKED TRANSFER REF HXWO 1851416 AND ORIGINATED BY EMP V898555 FWD CARGO DOOR STA542.4 FRAME INNER CHORD REPAIRED AS PER ECRA5234-01095 REV - ATTACH FORM 44.0008 ITEM 1 TO ITEM 19 ACCOMPLISHED , WORK ACCOMPLISHED BY MECHANIC V897381 INSPECTED BY V896888 RII INSPECTED BY HX169509 ADD EMP:V898550

Part: FLOOR SUPPORT — CORRODED (STA303/LBL40-55) · airframe 122,075 hrs · 18,895 cycles

CABIN STA 303 LBL 40"-55" FLR SUPPORT CORRDED TRANSFER REF. NON-ROUTINE HX NRC WO.1843972 AND ORIGINATED BY EMP NO. V927576 CABIN STA 303 FLOOR BEAM LBL 40" - LBL 55" UPPER CHORD REPAIRED AS PER SRM 53-00-51-2R-1 REPAIR 1 FIG 201. ATTACHED FORM 44-0008 ITEM 1-31 ACCOMPLISHED. WORK ACCOMPLISHED BY MECHANIC V897381 INSPECTED BY V896919 RII INSPECT IS OKAY. APPROVED BY HX 341008.

Part: NIPPLE — MISSING (LAV SERVICE) · airframe 120,720 hrs · 18,701 cycles

PDA 3 VERBAL LAV SERVICE REPORT -- NIPPLE MISSING FOR LAV SERVICE -- SEE PHOTO PHOTO ADDED INSTALLED NEW LAV SERVICE NIPPLE. OK FOR SERVICE. CALLED LAV SERVICE TRUCK. REFERENCE 38-32-03-50.

Part: EGT INDICATION — WARNING MESSAGE (RT ENG) · airframe 119,045 hrs · 18,480 cycles

RT ENG HIGH EGT ON TAKE OFF. MAX EGT 737 SECONDS DURATION. DUE TO PREVIOUS HISTORY OF EGT FAULTS A POSITIVE FIX IS UNLOCKED FOR UPDATE. REQUIRED. PER CREW WHEN THROTTLES WERE PULLED BACK RIGHT ENGINE EGT DEBRIEF CREW, CAPTAIN STATED THAT ONCE THROTTLES BACK TO IDLE, INDICATION WENT BLANK ON EICAS AND STAND BY DISPLAYS. THE #2 ENGINE EGT INDICATION ON BOTH THE UPPER EICAS DISPLAY TOMC-MEREDITH AND STBY ENGINE INDICATION WERE BLANK. INSPECTED INLET AND EXHAUST NO OBVIOUS DEFECTS NOTED. REPLACED W6 HARNESS AND 4 EGT PROBES AT ENGINE #2. RAN ENGINES, TOOK #2 ENGINE TO 90% N1 WITH EGT 528 TWICE WITH NO FAULTS NOTED WITH EGT INDICATION.

Part: AUTOTHROTTLE SYS — FAILED · airframe 117,203 hrs · 18,197 cycles

AUTO THROTTLES FAILED TO ENGAGE ON TAKEOFF THRUST MANAGEMENT SYS (INCLUDING A/T SYS) PLACED ON MEL. MEL STICKER AND C/B COLLARED F16 ON THE P11. DOWNGRADED A/C TO "AUTOLAND LIMIT-LAND 2". DISPATCH DESK: 82 NAME: JERRY DATE: 02-JAN-22- NOC DESK: 76 NAME: DOUG DATE: 02-JAN-22- OK TO DEFER AUTOTHROTTLE SERVO INOP T/S REF. B767-3 FIM 22-03-00 MCDP AUTO FLIGHT BITE. NO FLT. IAW AMM 22-03-00-818, ALL TESTS PASSED. ACFT. UPGRADED TO FULL FAULTS DISPLAYED. PERFORMED MCDP TESTS 02, 10, & 12 IAW FIM CAT CAPABILITY. " AUTO LAND CAT II" PLACARD REMOVED FROM FLIGHT 22-03-00-803, 810, & 812. AUTO THROTTLE SERVOS & DISCONNECT OPS DECK. CHECK NORMAL. UNABLE TO DUPLICATE FAULT. ACCOMP. MCDP TEST 30 ADD EMP:U107527

Part: NONE — NONE (NA) · airframe 116,695 hrs · 18,074 cycles

AUTO THOTTLES WILL NOT ENGAGE. CREW DEBRIEFED, STATED NO FMA ON EADI. TRIED IN MULTIPLE MODES LOCKED FOR T/S. PER LP 7341532 R IDG STATUS MESSAGE. FURTHER DETAILS AWAITED

Part: SENSOR — FAULTED (LT SLAT SYS) · airframe 115,274 hrs · 17,797 cycles

ON APP ICAS LE SLAT ASSY MESSAGE ON ICAS COMPLIED WITH QRH AND L ANDED BIT THE FSEU AND FOUND THE FOLLOWING FAULT: LE OUTBD ASYM MSG NO. 27-81021. FDE LE ASYM LATCHED. PRIMARY A/S <90 A-A02 FR PSEU, IB SLAT +1.21V, OB SLAT +5.54V, LRV POS -2.33V. INTERROGATED PSEU AND GOT 302 FAULT, (R SLAT #10 INBD). RETRACTED FLAPS ELECTRICALLY AND HAVE SAME FAULT ON FSEU. AND MESSAGE WENT AWAY. LOWERED FLAPS AND MESSAGE CAME BACK. LE WILL NOT RETRACT HYDRAULICALLY. RETRACTED LE ELECTRICALLY REMOVED AND REPACED #10 SLAT INBOARD S302 SENSOR, ADJUSTED SCENSOR SWITCH AND RETRACT TARGET PER AMM 27-88-01-902-001.

Part: HYDRAULIC LINE — LEAKING · airframe 115,209 hrs · 17,786 cycles

DURING CHECK NO 2 SERVICE HMG BLOCK 8 OPRATIONAL CHECK FOUND HYDRAULIC LEAK THRU BODY OF HMG. PERFORMED INTERIM REPAIR PER ECRA 2420-01623 PART 1. HYD LINES PLUGGED ,UNIONS REMOVED NO LEAKS NOTED FROM HYDRAULIC LINES PRESSURIZED.INITIATE A DIP TO PERFORM PERMANENT REPAIR AS PER ADD EMP:U288719,U235671 ECRA PART 3. HMG WILL BE DEFFERED LOG PAGE 6259714. OK TO DIP HMG DEACTIVATED WITH LINES REMOVED AND CAPPED AND REPAIR HMG WITHIN TWO FLIGHT CYCLES PER ECRA 2420-01623 TOMC-APPROVAL FROM SC1ELBYC COMMENT QC REVIEWED SDR FLAGGED. RECORDS UPDATE - AP QC REVIEWED T/A : 2 FC.......AP/U366012 REPLACED HMG AS PER AMM 24-25-01. OPS CHECK NORMAL AND NO LEAK NOTED. ADD EMP:U288719 TOMCQC REV PERFORMED ROTABLE PARTS UPDATE ADD EMP:U288719 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1119064 SN OFF 1444 IPC REFERENCE # IPC 24-25-01-01

Part: HYDRAULIC SYSTEM — LEAKING · airframe 115,199 hrs · 17,785 cycles

IN REFERENCE LOG PAGE 625880 HMG INOP. IN REFERENCE LOG PAGE 6258880 HMG INOP DEFERRED PER MEL 2425A. ADD EMP:U288719,U235671 DISPATCH DESK: 76 HMG CAPPED DUE TO HYD LEAK PER ECRA 2420-01623 LOG PAGE 6258880 . NO LEAKS WITH LINES AND HMG CAPPED 64-2425-9-0001. HMG INOP DEFERRED PER MEL 2425A. NO PARTS AT GIG. M&E

Part: SKIN — CHAFED (FUSELAGE) · airframe 115,185 hrs · 17,782 cycles

B767-53-3-7093 FUSELAGE SKIN ON SEC 48 BELOW PANELS 321BL, 322AL , 323AL, 324AL, IS CHAFFED FROM THE PANEL BLADE SEAL REPAIRED BLENDED AREA IAW EC/RA 5381-01012. SEE BACK OF R25U FOR PARTIAL WORK. REF AMES NR 0446 AND UAL JOB CARD 63-5330-1-2602 ADD EMP:V929553

Part: SKIN — CHAFED (FUSELAGE) · airframe 115,185 hrs · 17,782 cycles

REF AMES NR 0448 AND UAL JOB CARD 63-5330-1-2602. B767-53-3-7093 AFT FUSELAGE SKIN ON SEC 48 BELOW PANELS 321BR, 322AR, 323AR, 3 24AR IS CHAGGED FROM PANEL BLADE SEAL REPAIRED BLENDED AREA IAW EC/RA 5381-01012. SEE BACK OF R25U FOR PARTIAL WORK. ADD EMP:V929553

Part: LENS — MISSING (CABIN) · airframe 115,004 hrs · 17,754 cycles

FWD GALLEY COMPT #216 LOWER PATH LIGHT LENS MISSING. INSTALLED FWD GALLEY COMPT #216 LOWER PATH LIGHT LENS PER AMM 33-51-10, OPS CHECK GOOD.

Part: SKIN — DENTED (BS 420-440) · airframe 112,751 hrs · 17,437 cycles

PREVIOUS REPAIR DOUBLER ON EXTERNAL FUSELAGE SKIN APPROXIMATE BS 420 TO 440 HAS DENT ABOVE STRINGER 34L. REF. AAR N/R: 9463825. REMOVED AND FABRICATED NEW REPAIR DOUBLER AND INSTALLED ON EXTERNAL FUSELAGE SKIN APPROXIMATE BS420 TO 440 IAW B767-300 SRM 53-00-01 AND SRM 51-40-08 AND PERM RES-WI 2015143-11 P-1 AND IR AND EC/RA#5310-06002. DATA WAS TRANSCRIBED FROM PAPER DOCUMENT :AAR N/R 9463825. WORK ACCOMPLISHED BY MECHANIC, INSPECTED BY Q.C., RII INSPECTION ACCOMPLISHED BY AAR MIAMI INSPECTOR.

Part: CONNECTOR — LOOSE (CABIN) · airframe 107,078 hrs · 16,681 cycles

EMERG LIGHT INOP. SEAT 18F SECURED CONNECTOR, OPS CHKS NORMAL.

Part: INDICATOR — READS HIGH (COCKPIT) · airframe 106,577 hrs · 16,613 cycles

AT FL360 STANDBY ALTIMETER WAS 500 FEET HIGH AT 36500 FEET. FOUND VIBRATOR INOP. REPLACED STBY ALT INDICATOR. OPS CHECKS GOOD. REF AMM 34-13-06.

Part: FLOOR SUPPORT — DAMAGED (FUSELAGE) · airframe 106,052 hrs · 16,541 cycles

M/D STA 256 RBL 59 FLOOR SUPPORT FOUND OVAL SCREW HOLE. M/D STA 256 RBL 59 FLOOR SUPPORT SCREW HOLE OVAL AREA REPAIRED A S PER RI-53-00-12222 REV A AND REF ECRA 5310-07300 REV.

Part: FLOORBEAM — CORRODED (BS 368) · airframe 106,052 hrs · 16,541 cycles

MAIN DECK, BS 368, RBL 54 FLOORBEAM CORRODED. THE FLOORBEAM WAS REPAIRED IAW ECRA 5310-07288, REV -.

Part: WEB — CORRODED (BS 1241-1373) · airframe 106,052 hrs · 16,541 cycles

MAIN DECK BS 1241 - 1373, RBL 90 - 94 AFT CARGO DOOR UPPER AREA WEB FOUND CORRODED. THE WEB WAS REPLACED IAW SRM 51-10-02.

Part: FLOOR SUPPORT — CORRODED (BS 852) · airframe 106,052 hrs · 16,541 cycles

BS 852 RBL 55 FLOOR SUPPORT UPPER SURFACE CORRODED. FLOOR SUPPORT BS 784 TO 883 REPAIRED IAW 53- 00-51, REPAIR 3, FIG 201.

Part: STRUCTURE — CRACKED (BS 1809) · airframe 106,052 hrs · 16,541 cycles

TAIL COMPARTMENT BS 1809, RT FORWARD OUTER STRUCTURE FOUND CRACKED. REPAIRED IAW EA 53-00-01-600, REV A, OP 005.

Part: FLOORBEAM — CORRODED (BS 287) · airframe 106,052 hrs · 16,541 cycles

FLOORBEAM CORRODED BS 287, RBL 11 TO 34. THE FLOORBEAM WAS REPAIRED IAW SRM 53-00-51, REPAIR 1, FIG 201.

Part: FLOORBEAM — CORRODED (BS 303) · airframe 106,052 hrs · 16,541 cycles

FLOORBEAM CORRODED BS 303, RBL 12 TO 46. THE FLOORBEAM REPAIRED IAW SRM 53-00-51, REPAIR 1, FIG 201.

Part: FLOORBEAM — CORRODED (BS 325) · airframe 106,052 hrs · 16,541 cycles

BS 325, LBL 12 - 16 FLOORBEAM UPPER SURFACE FOUND CORRODED. REPAIRED IAW SRM 53-00-51, REPAIR 1, FIG 201.

Part: CONNECTOR — LOOSE (CABIN) · airframe 103,576 hrs · 16,159 cycles

EMERGENCY PATH LIGHT AT LT MID LAV AND CROSS AISLE IS INOP. FOUND CONNECTION AT LEFT MID LAV AT SIDE WALL DISCONNECTED, SECURED, OPS TEST GOOD REF AMM 33-99-99.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 103,576 hrs · 16,159 cycles

RT EMERGENCY EXIT SLIDE PATH AFT LIGHT IS INOP. RELAMPED, OPERATIONAL CHECK GOOD REF AMM 33-51-06

Part: SKIN — DENTED (FUSELAGE) · airframe 99,523 hrs · 15,582 cycles

DENT ON FUSELAGE AT STRINGER 37 RT & BS 654+44, JUST AFT OF FWD CARGO DOOR. REPAIRED FUSELAGE SKIN IAW SRM 53-00-01 FIG 201 REPAIR 12.

Part: CAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 99,523 hrs · 15,582 cycles

CORROSION ON LOWER SURFACE OF T CAP IN AFT CARGO PIT, STATION 1131, LBL 36. T CAP IN AFT CARGO HAD 100% MATERIAL LOSS. R & R IAW SRM 51-40-02.

Part: CAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 99,523 hrs · 15,582 cycles

CORROSION ON LOWER SURFACE OF T CAP IN AFT CARGO PIT, STATION 1197+88 & RBL 36. UPON EVALUATION FOUND T CAP TO HAVE 100% MATERIAL LOSS. OUT OF LIMITS IAW SRM 53-00-07 FIG 101. R & R T CAP 146T1060-01 IAW SRM 51-40-05 & 51-40-02.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 99,523 hrs · 15,582 cycles

CORROSION ON LOWER SURFACE OF T CAP IN AFT CARGO PIT STATION 1219, LBL 36. R & R AFT CARGO COMPARTMENT, T CAP AT STATION 1219 IAW SRM 51-40-02 & DWG 146T0250.

Part: PIN — MIGRATED (BYPASS VALVE) · airframe 97,023 hrs · 15,248 cycles

TRAILING EDGE FLAPS WILL NOT MOVE ELEC OR WITH HYD. FOUND PIN MIGRATING OUT OF VLV INDICATOR LEVER PROHIBITING FULL VLV MOVEMENT. REPLACED FLAP PDU BYPASS VLV & ROTARY ACTUATOR.

Part: SLIDE — DEPLOYED (L1 DOOR) · airframe 95,632 hrs · 15,055 cycles

DOOR 1L SLIDE WAS DEPLOYED ON ARRIVAL. SLIDE ASSEMBLY MR25708-739 DETACHED FROM ACFT & IS LOCATED IN BAY 1 OF THE SERVICE CTR IAW AMM 25-66-00. COMPLETED MM 25-66-00 FROM PG 203 STEP 18 TO END. REPLACED 1L SLIDE ASSEMBLY IAW MM 25-66-01. CONTINUE WITH PROCEDURE FOR RE ACTIVATION OF ENTRY DOOR AMM 25-66-00 PG 203 STEP 18.

Part: CONNECTOR — CONTAMINATED (CABIN) · airframe 94,989 hrs · 14,969 cycles

EEL BETWEEN DOOR 1L & SEAT 1A INOPERATIVE. CLEANED & REMOVED MOISTURE FROM POWER STRIP CRIMPS & CONNECTIONS. ACCOMPLISHED EMER OPERATIONS CHECKED OK.

Part: CONTACT — CONTAMINATED (CABIN) · airframe 94,989 hrs · 14,969 cycles

EEL BETWEEN DOOR 1L & 1R INOPERATIVE. CLEANED & REMOVED MOISTURE FROM POWER STRIP CRIMPS & EEL CONTACTS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 94,989 hrs · 14,969 cycles

EMERGENCY EXIT LIGHT FWD LOWER BY DOOR 1 LT INOPERATIVE. REPLACED LOWER EMER EXIT LIGHT ASSEMBLY OPERATIONS TEST PASS IAW MM 33-51-00.

Part: SEAL — MISSING (OVEN) · airframe 94,276 hrs · 14,869 cycles

OVEN 41 RUBBER SEAL MISSING, BUS GALLEY. REQUIRES DOOR SEAL OR OVEN REPLACEMENT AT POS R41. REPLACED OVEN, OPERATIONS CHECKED OK.

Part: ACCESS DOOR — MISSING (EXTERNAL POWER) · airframe 94,164 hrs · 14,851 cycles

EXTERNAL POWER ACCESS DOOR FOUND MISSING ON ARRIVAL.

Part: RIB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 93,399 hrs · 14,742 cycles

CORROSION FOUND ON FWD CARGO COMPARTMENT DOOR SILL INTERNAL RIB. LOWER SURFACE BS 576 STRINGER 45R - STRINGER 48R.

Part: SKIN — DENTED (FUSELAGE) · airframe 93,399 hrs · 14,742 cycles

LT FUSELAGE SKIN DENTED AT APPROXIMATELY BS 396 BETWEEN STRINGER. 33L & 34L. FOUND DENT TO BE PREVIOUS OUT OF LIMITS BLEND REPAIR.

Part: SKIN — DENTED (FUSELAGE) · airframe 93,399 hrs · 14,742 cycles

DENT IN FUSELAGE SKIN AT APPROXIMATELY BS 409 BETWEEN STRINGER 33L & 34L. FOUND DENT TO BE A PREVIOUS OUT OF LIMITS BLEND. REPAIRED.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 93,399 hrs · 14,742 cycles

FWD CARGO COMPARTMENT BILGE FRAME TIE CLIP AT AFT SIDE CORRODED BS 742, RBL 8. LOCATED, DRILLED, PAINTED & INSTALLED NEW SHEAR TIE IAW B767-300 SRM51-40-02 & DRAWING 143T1214 REV E.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 93,399 hrs · 14,742 cycles

MAIN CABIN FLOOR STRUCTURE FOUND CORRODED BEYOND LIMITS BS 790, LBL 32. REMOVED DAMAGE & REPAIRED FLOOR BEAM LOCATED BETWEEN STATION 808 - 788, LBL 32 IAW SRM53-00-51 REPAIR 3 FIG 201 IAW TIMCO NR24938.

Part: B-NUT — LEAKING (ELEVATOR) · airframe 93,378 hrs · 14,739 cycles

SUSPECT HYD LEAK AFT TAIL CONE AREA. FOUND SEVERAL B NUTS LEAKING AT THE ELEVATOR AP ACTUATORS. TIGHTENED, NO LEAKS NOTED.

Part: LIFE VEST — MISSING (CABIN) · airframe 93,371 hrs · 14,737 cycles

LIFE VEST MISSING SEAT 35A. INSTALLED LIFE VEST AT SEAT 35A, OK TO CONTINUE.

Part: BALLAST — DEFECTIVE (CABIN) · airframe 93,345 hrs · 14,733 cycles

VERY VERY LOUD SQUEAL IN OVERHEAD MID COACH CABIN. PLACED CEILING LIGHT AT ROW 30-31L ON MEL. BALLAST CONNECTOR D11218 DISCONNECTED & STOWED. BALLAST WAS THE CAUSE OF LOUD HUMMING NOISE, WILL REQUIRE BALLAST PCN 563-0055 & 05814-16 BALLAST.

Part: B-NUT — LOOSE (RT ELEVATOR) · airframe 93,327 hrs · 14,731 cycles

HYD FLUID STREAM IS VISIBLE COMING FROM APU ACCESS DOOR. FOUND B NUT LOOSE ON RT ELEVATOR PCA. TIGHTENED B NUT, OPERATED ELEVATOR NUMEROUS TIMES WITH NO LEAKS. CLEANED AREA. HYD QTY GOOD.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 93,140 hrs · 14,707 cycles

AFTER TAKEOFF, RT REVERSER ISOLATION VLV STATUS MESSAGE DISPLAYED. ALSO, REVERSER ISOLATION LIGHT IS ON. NO EICAS MESSAGE DISPLAYED.

Part: WEB — CRACKED (LT PYLON) · airframe 92,498 hrs · 14,626 cycles

LT PYLON AFT WEB 313T3355-233 CRACKED AT OTBD AFT FASTENER HOLE. INSTALLED NEW WEB IAW DRAWING 313T3355.

Part: FUEL LINE — LEAKING (LT ENGINE) · airframe 92,498 hrs · 14,626 cycles

FUEL LEAK LT ENGINE BOTTOM CORE. FOUND FUEL OIL COOLER OUTLET LINE LEAKING & BULGING IAW IPC 73-11- 06-20 PAGE 18 ITEM 68 K P/N 280-4427. REMOVED FM11 TUBE & HOSE ASSEMBLY NEED TO COMPLETE FROM STEP 3 PAGE 402 TO END. REPLACED FM11 FUEL TUBE IAW AMM 73-11-99.

Part: APU — SHUTDOWN (APU BAY) · airframe 92,406 hrs · 14,613 cycles

APU SHUTDOWN ON PUSH BACK.

Part: BLOWER — FAILED (SMOKE DETECTOR) · airframe 92,208 hrs · 14,588 cycles

LOWER EICAS MESSAGE FWD & AFT DET FAN. TROUBLESHOT EICAS MESSAGE IAW FIM 26-16 -00 PG 109. SWAPPED CONNECTOR AT FWD BLOWER & MESSAGE CLEARED. SUSPECT FWD & AFT NR 1 BLOWERS IAW WD 26-16-21. REPLACED FWD & AFT NR 1 SMOKE DETECTOR BLOWERS IAW AMM. OPS CHECKED OK, NO MESSAGES.

Part: SMOKE DETECTOR — FAULTY (CARGO BAY) · airframe 92,208 hrs · 14,588 cycles

AMSITM 6449 2086025 MAINT ITEM DISPLAY-STATUS MESSAGE "AFT CARGO DET 2" BY- 118014. REPLACED SMOKE DETECTOR NR 2 AFT IAW MM26-16-01. OPERATIONS CHECKED NORMAL.

Part: GARLOCK SEAL — LEAKING (BLEED AIR SYS) · airframe 92,208 hrs · 14,588 cycles

ON TAXI OUT RT BLEED DUCT LEAK EICAS MESSAGE. ALSO HAVE "DUCT LEAK" LIGHT ON OVERHEAD PANEL. LIGHT & EICAS MESSAGE OUT APPROXIMATELY FIVE MINUTES AFTER SHUTTING OFF RIGHT BLEED & ISOLATING RIGHT SYSTEM. REPLACED GARLOCK SEALS ON RT BLEED DUCT, IAW IPC 36-11-04 ITEM R. OPERATIONS CHECKED WITH APU, ENGINE NR 2 RUN. NO LEAKS OR MESSAGES.

Part: CONTROL VALVE — INOPERATIVE (A/C PACK) · airframe 92,008 hrs · 14,562 cycles

AFT CABIN TEMP CONTROL FAILED TO CONTROL DESIRED TEMP. VERY WEAK AIRFLOW IN AFT CABIN, COULD NOT COOL UNTIL 2 HOURS INTO FLT. FOUND RT PACK VALVE INOPERATIVE. AMS FOUND FCV STUCK IN ALMOST FULL CLOSED POSITION. VALVE MR21290, PCN 643-9118. FOUND PACK CPRSR OUT TEMP AT FAULT R & R REF MM.

Part: CONTROL VALVE — FAILED (AFT CABIN) · airframe 92,000 hrs · 14,561 cycles

AFT CABIN TEMP CONTROL FAILED TO CONTROL DESIRED TEMP. VERY WEAK AIRFLOW IN AFT CABIN, COULD NOT COOL UNTIL 2 HRS INTO FLT. FOUND RT PACK VALVE INOPERATIVE. REPLACE THE VALVE. FOUND FCV STUCK IN ALMOST FULL CLOSED POSITION. VALVE MR21290, PCN 643-9118, REF AMM 21-51-01-401 FOR R & I.

Part: ACTUATOR — FAULTY (TURBINE COOLING) · airframe 91,930 hrs · 14,552 cycles

RT ENG PIMU FAULT MESSAGES EEC CHANNEL A FAULT CAT 2, EEC CHANNEL A TCC FD-BK FAIL, EEC CHANNEL B FAULT CAT 2 AND EEC CHANNEL B TCC FD-BK FAIL FOUND. REPLACED NR 2 ENG TURBINE CASE COOLING AIR VALVE ACTUATOR IAW AMM. PERFORMED PARTIAL RIG.

Part: ANTENNA — FAILED (WX RADAR) · airframe 91,883 hrs · 14,546 cycles

WEATHER RADAR ANTENNA FAILED, RETURNED TO FIELD.

Part: PRESSURE SWITCH — FAULTY (HYD SYSTEM) · airframe 91,542 hrs · 14,501 cycles

C SYS HYD PRESSURE INDICATES 20 BUT NO SYS PRESSURE LIGHT AND NO EICAS EITHER LIGHTS CHECKED OK. R & R CENTER HYD SYS PRESSURE SWITCH IAW AMM. OPS AND LEAK CHECKED GOOD.

Part: B-NUT — LOOSE (HYD SYSTEM) · airframe 91,435 hrs · 14,487 cycles

EVIDENCE OF HYD FLUID ON RT OTBD AILERON. FOUND LOOSE B-NUT ON PRESSURE LINE TO RT OTBD AILERON. TIGHTENED AND LEAK CHECKED. OPS CHECKED GOOD, NO LEAKS NOTED.

Part: SELECTOR PANEL — FAULTED (AUDIO SYS) · airframe 91,420 hrs · 14,485 cycles

NR 2 AUDIO SELECTOR PANEL VOLUME CONTROL DEFECTIVE. REMOVED AND REPLACED FIRST OBSERVER`S AUDIO SELECTOR PANEL.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 91,359 hrs · 14,477 cycles

EMERGENCY LIGHTS INOPERATIVE SEAT ROWS 24 LT THRU 33 LT. REPLACED BATTERY AND CHARGER M99082 IAW MM, SEATS OPS CHECKED NORMAL.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 91,359 hrs · 14,477 cycles

EMERGENCY LIGHT INOPERATIVE AT R1 DOOR. REPLACED LAMP, OPS NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 91,359 hrs · 14,477 cycles

EMERGENCY LIGHT INOPERATIVE AT AFT RT INBD LAVATORY. REPLACED EMERGENCY LIGHT. SYS OK.

Part: FAN — FAILED (EXHAUST) · airframe 91,262 hrs · 14,465 cycles

FWD EQUIP EXHAUST FAN STATUS MESSAGE. REPLACED FORWARD EXHAUST FAN.

Part: ACTUATOR — MALFUNCTIONED (RT AILERON) · airframe 90,832 hrs · 14,410 cycles

DURING CRUISE, NO RT INBD AILERON INDICATION MOVEMENT. DISCONNECTED AUTOPILOT AND ACCOMPLISHED SERIES OF TURNS. CONFIRMED RT INBD AILERON WOULD NOT MOVE DOWN DURING TURNS. AILERON ALSO NOT FAIRED IN NEUTRAL POSITION AND REQUIRED LT AILERON TRIM TO MAINTAIN STRAIGHT AND LEVEL FLIGHT. REPLACED BOTH RIGHT INBOARD AILERON PCA'S PER AMM.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 90,586 hrs · 14,379 cycles

EMERGENCY LIGHTS INOPERATIVE AT SEATS 1AB TO 9AB. REPLACED EMERGENCY LIGHT CHARGER PER AMM.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 90,586 hrs · 14,379 cycles

R2 DOOR EMERGENCY LIGHT BATTERY INOPERATIVE. BATTERY REPLACED AND OPS TESTED NORMAL IAW MM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 90,242 hrs · 14,329 cycles

EMERGENCY LIGHTS ARE INOPERATIVE ON SEATS FROM 1ST CLASS THROUGH BUSINESS CLASS ON LEFT SIDE. REPLACED BATTERY. EMERGENCY LIGHT CHECKED OKAY.

Part: BATTERY — DISCHARGED (CABIN) · airframe 90,242 hrs · 14,329 cycles

EMERGENCY LIGHTS ARE INOP ON SEATS FROM 24 AB TO 33AB. BATTERY LOCATED BEHIND DADO PANEL AT SEAT 29A. REPLACED BATTERY CHARGER UNIT AND BATTERY AND TEST PER MM, CHECKS NORMAL.

Part: CONNECTOR — UNSECURE (CABIN) · airframe 90,242 hrs · 14,329 cycles

EMERGENCY LIGHT AT SEAT 19JK IS INOP. SECURED CONNECTOR FOR EMERGENCY SEAT LAMP, OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 90,242 hrs · 14,329 cycles

EMERGENCY LIGHTS ARE INOP ON SEATS FROM 24 AB TO 33AB.

Part: CONTROL PANEL — FAULTY (HF COMM) · airframe 90,117 hrs · 14,313 cycles

UNABLE TO TRANSMIT OUT ON LT HF RADIO. NO RECEPTION FROM LT HF EITHER. ESTABLISHED HF COMMUNICATION AND SELCALL CHEC. OPS NORMAL.

Part: CONNECTOR — DIRTY (BLEED SYS) · airframe 89,728 hrs · 14,256 cycles

CENTER BLEED ISOLATION WILL NOT OPEN. CLEANED CONNECTOR ON CENTER ISOLATION VALVE, OPS CHECKED OKAY.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 89,665 hrs · 14,247 cycles

EMERGENCY LIGHTS INOPERATIVE ON SEATS 1A TO 2A AND 6AB THRU 14AB. EMERGENCY LIGHT BECAME VERY DIM. REPLACED BATTERY AT ROW 8A.

Part: NUT — CRACKED (NR 4 WHEEL) · airframe 89,498 hrs · 14,225 cycles

NR 4 FWD MAIN WHEEL HAS 1 EA TIE BOLT NUT CRACKED AND BOLT IS LOOSE IN WHEEL HALVES. REPLACED NR 4 FWD WHEEL TIRE ASSY PER MM.

Part: FSEU — FAULTY (TE FLAP) · airframe 88,731 hrs · 14,122 cycles

FLAP O-SPEED WARNING AT CRUISE AT 320 370 AND CLIMBING THRU 32.7.5 TIMES. M545 FAULT REPLACED FSCU PER AMM.

Part: TIMER — OUT OF ADJUST (LAVATORY) · airframe 88,679 hrs · 14,112 cycles

MID RIGHT LAV SINK WATER WON'T SHUTOFF. WATER SHUTOFF VALVE FAILED. REPLACED WATER SHUTOFF VALVE TO ENABLE DEFFERAL. REQUIRES NEW FAUCET VALVE OR TIMER, NO TIME TO TROUBLESHOOT. PER MEL DEACTIVATED WATER HEATER AND BOARDED HAND SANITIZER. ADJUSTED HYDRAULIC TIMER PER MM 38-11-06 TASK 824-804. FAUCET OPERATES NORMALLY, CYCLED NUMEROUS TIMES.

Part: STEERING UNIT — MALFUNCTIONED (SATCOM) · airframe 88,415 hrs · 14,073 cycles

LOW GAIN ON SATCOM WITH BITE FAIL & T-P BSU FAULT. CANNOT PLACE CALL BUT SAT WORKS FOR ACARS. REPLACED PORT BEAM STEERING UNIT PER MM 23-25-17 PER MM 23-25-17 AND ACCOMPLISHED INSTALLATION TEST PER MM 23-25-00, OPS CHECKS GOOD.

Part: FEEDER CABLE — DAMAGED (APU) · airframe 87,952 hrs · 14,011 cycles

APU INOP ELECTRICAL. UNABLE TO LOAD GENERATOR. REFER TO MM. APU FIELD OFF LIGHT. DEFERRED PER TOMC AND SEE CF831 FOR PARTS INFO. REPLACED APU GEN FEEDER HARNESS, REFER TO CF0831.

Part: FEEDER CABLE — DAMAGED (APU) · airframe 87,947 hrs · 14,010 cycles

FOUND APU FEEDER CABLE T1 BURNT ON APU GENERATOR NEED TO REPLACE APU GENERATOR DUE TO BURNT FEEDER HARNESS LEADS. REPLACED APU GENERATOR IN ACCORDANCE WITH MM.

Part: ACTUATOR — BROKEN (NR 6 SPOILER) · airframe 87,731 hrs · 13,983 cycles

LEFT HYD SYS PRESSURE EICAS, RTFL. FOUND NR 6 SPOILER ACTUATOR HOUSING BROKEN. REPLACED ACTUATOR AND LT CASE RET FILTERS. SERVICED LT HYD FLUID. OPERATIONAL CHECKED OK.

Part: WINDSHIELD — DELAMINATED (COCKPIT) · airframe 87,521 hrs · 13,957 cycles

DELAMINATED WINDSHIELD 1L IN UPPER RIGHT CORNER. REPLACED WINDSHIELD PER AMM.

Part: WINDSHIELD — DELAMINATED (COCKPIT) · airframe 87,521 hrs · 13,957 cycles

DELAMINATED WINDSHIELD 1R IN UPPER RIGHT CORNER. REPLACED 1R WINDSHIELD PER AMM.

Part: OXYGEN MASK — UNLATCHED (CABIN) · airframe 87,412 hrs · 13,942 cycles

OXYGEN PANEL IN ECONOMY NEEDS TO BE RESTOWED. REPACKED O2 MASK PER AMM. ALL OPS CHECK GOOD.

Part: CONTROL VALVE — FAULTY (AC BAY) · airframe 87,066 hrs · 13,897 cycles

LEFT PACK INOP WILL NOT RESET. REPLACED LEFT FLOW CONTROL CARD IN P50 CARDFILE PER MM, ALSO LEFT FLOW CONTROL VALVE PER MM, PACK OPS NORMAL.

Part: CONTROL VALVE — STUCK (LT A/C PACK) · airframe 86,911 hrs · 13,876 cycles

FOUND LT PACK FLOW CONTROL VALVE STUCK CLOSED. REPLACED LEFT FLOW CONTROL VALVE, OPS CHECKED GOOD ON GROUND.

Part: VALVE — FAULTY (LT A/C PACK) · airframe 86,909 hrs · 13,875 cycles

'LT PACK INOPERATIVE' ILLUMINATED ON EICAS. OPERATED NORMAL AFTER 'STANDBY' SELECTED. REPLACED LOW LIMIT VALVE.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 86,739 hrs · 13,852 cycles

EMERGENCY LIGHT IN COCKPIT IS INOPERATIVE. REMOVED AND REPLACED BATTERIES IAW AMM 33-51-01. OPS CHECKED GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 86,739 hrs · 13,852 cycles

EMERGENCY EXIT LIGHT ABOVE SEAT 36AB IS INOPERATIVE. REPLACED LAMP AT SEAT 36AB. OPS CHECKED GOOD.

Part: ACTUATOR — INTERMITTENT (RUDDER TRIM) · airframe 85,656 hrs · 13,711 cycles

RUDDER TRIM INTERMITTENT, FLIGHT DIVERTED. REPLACED RUDDER TRIM ACTUATOR PER MM. REPLACED RUDDER TRIM CONTROL MODULE PER MM. OPS CHECKS GOOD.

Part: MONITOR — FAULTY (HYDRAULIC SYS) · airframe 85,557 hrs · 13,695 cycles

RT HYD SYSTEM QTY IS 0.02; R HYD QTY EICAS MSG DISPLAYED. SAMC TEXT: WITH RT QTY LOW LIGHT ALSO. TOMC MAINT TEXT: PER CREW, PUMP LOW PRESS LIGHTS DID NOT ILLUMINATE PRESSURE NORMAL. NO SIGNS OF EXTERNAL LEAKAGE. REPLACED HYD QTY MONITOR UNIT PER MM, QTY SYS CKS NORMAL.

Part: SELECTOR PANEL — FAULTY (COCKPIT) · airframe 85,500 hrs · 13,689 cycles

RT HF TRANSMISSIONS ARE INOP, WEAK, GARBLED, INTERMITTENT AT (1=CAPT,2=F-O,3=F-OB) STATION. OTHER STATIONS NORMAL. TRIED NEW TRANSCEIVER, NO HELP. REPLACED O/B AUDIO SEL PNL. OP CKS OK.

Part: RELAY — FAULTY (EXTERNAL POWER) · airframe 84,960 hrs · 13,619 cycles

DUE TO REPORT OF EXTERNAL POWER CONTACTOR NOT OPENING AFTER EXTERNAL POWER WAS DE-SELECTED AND EXTERNAL POWER WAS REMOVED REPLACED EXTERNAL POWER CONTACTOR K114 PER MM. RPL'D EXTERNAL PWR CONTACTOR, CKS OKAY PER MM TEST. RAN ENGINES TO DUPLICATE DF680, PWR WOULD NOT TRANSFER TO ENG GEN'S & UTILITY BUSSES WOULD NOT COME ON. BPCU SHOWS SIGNS ON BOTH LINES, RESET PWR, BPCU DEAD. RPL'D BUSS PWR CONTROL UNIT REF MM, CKS OK PER MM. ** NEED TO RUN ENGINES TO CONFIRM REF SMC4.

Part: TRANSCEIVER — DEFECTIVE (HF COMM) · airframe 84,936 hrs · 13,614 cycles

HF TRANSMISSION & RECEPTION ARE INOP, WEAK, GARBLED INTERMITTENT, ETC. AT ALL CREW STNS. (1 = L HF, 2 = R HF) CREW COMMENTS: UNABLE TO XMIT. CAN RECEIVE OK. LONG SIDE TONE WHEN TUNING. COMPLIED WITH MEL. REMOVED AND REPLACED RIGHT HF TRANSCEIVER.

Part: PRESSURE SWITCH — MALFUNCTIONED (HYD SYSTEM) · airframe 84,872 hrs · 13,606 cycles

CENTER HYDRAULIC SYSTEM LOW PRESSURE LIGHT ILLUMINATED WITH EICAS AND ADP LOW PRESSURE LIGHT. REPLACED CENTER HYD SYSTEM LOW PRESSURE SWITCH PER MM, OPS NORMAL.

Part: FITTING — LEAKING (T/R ACTUATOR) · airframe 84,691 hrs · 13,580 cycles

HYD LEAK ON NR 2 ENG FOUND DURING PREDEPARTURE WALKAROUND, FOUND LEAK FROM LT TOP THRUST REVERSER ACTUATOR. SECURED FITTING FOR INTERCONNECT CABLE HOUSING FOR LEFT TOP THRUST REVERSER ACTUATOR. NO LEAKS NOTED.

Part: ROD — WORN (NR 2 PYLON) · airframe 84,656 hrs · 13,575 cycles

NR 2 ENGINE PYLON STRUT PLENUM SUPPORT RODS ARE WORN OUT. REPLACED RODS.

Part: B-NUT — LEAKING (NR 2 PYLON) · airframe 84,656 hrs · 13,575 cycles

NR 2 PYLON, EVIDENCE OF HYDRAULIC LEAK, INBD SIDE. FOUND HYD PRESS LINE ABOVE NR 2 PYLON AT BULKHEAD FITTING LEAKING MARKED WITH TAPE. SECURED LOOSE 'B' NUT ON HYDRAULIC LINE. RAN HYDRAULICS AND MOTORED ENGINE, NO LEAKS FOUND.

Part: DUCT — SPLIT (RT WING) · airframe 84,656 hrs · 13,575 cycles

RIGHT WING OUTBD DUCT GOING TO ANTI-ICE VALVE ABOVE NR 2 PYLON IS SPLITTING OUTBD OF CLAMP (MKD WITH TAPE). REMOVED DUCT AND SENT TO WELDING SHOP. REPLACED DUCT.

Part: FITTING — LEAKING (NR 1 ENGINE) · airframe 84,656 hrs · 13,575 cycles

NR 1 ENG HAS HEAVY COAKING AT 12'O'CLOCK. REMOVED 2 EA DRAIN LINES FROM PYLON AND HYD LINE CLUSTER NO BLOCKAGE NOTED. REMOVED PYLON ACCESS PNL 416BR & FOUND NO EVIDENCE OF LEAKAGE. REINSTALLED PNL. REMOVED NR 1 ENG PYLON JUNCTION BOX INSULATION AND COVER FOR ACCESS TO HYDRAULIC 'B' NUTS. FOUND EVIDENCE OF LEAKAGE FROM CASE DRAIN FITTING. CLEANED AREA,TIGHTENED FITTING. MOTORED ENGINE 114813, NO LEAKS NOTED. RE-INSTALLED J-BOX PNL AND INSULATION BLANKETS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 84,656 hrs · 13,575 cycles

EEL LIGHT AT SEATS 35KJ INOPERATIVE. RELAMPED, OP CHECKS NORMAL PER MM.

Part: EEC — FAULTY (NR 2 ENGINE) · airframe 84,656 hrs · 13,575 cycles

WHILE ACCOMPLISHING PIMU BITE CHECK FOUND NR 2 ENG EEC CH A FAULT CAT 2 MESSAGE EEC CH A TCA SOL W-A FAIL. TROUBLESHOT REF FIM 71 PIMU MESSAGE INDEX PG64K,PG64L, MESSAGE 354-22 & REF WDM 71-51-14. COMPLETED TO ITEM G INDICATES NEED EEC. REF PTT # 6562008 FOR T-S (VERIFIED 62 OHMS AT TVBCA SOL), REPLACED R ENG EEC AND MADE W-U FOR R ENG EEC IDLE TEST NR 6.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 84,656 hrs · 13,575 cycles

LEFT OVERWING SLIDE EMERGENCY LIGHT AFT OF FLAPS (2ND TO LAST) INOPERATIVE. RELAMPED PER MM, OP CHECKS NORMAL.

Part: CAP — MISSING (WINDSHIELD) · airframe 84,599 hrs · 13,566 cycles

MISSING WINDSHIELD HEAT TERMINAL CAP F/O WINDSCREEN. REPLACED CAP.

Part: CONTROLLER — FAULTY (BLEED AIR SYS) · airframe 84,568 hrs · 13,562 cycles

LEFT ENG BLEED OFF EICAS. FOUND FAULTED NR 1 ENG PRVC. REPLACE PRVC. RAN ENG PER JRH. ALL BLEED INDICATIONS NORMAL.

Part: CONTROL PANEL — FAULTY (WEATHER RADAR) · airframe 84,527 hrs · 13,558 cycles

WX RADAR FAILURE, RTFL. MESSAGE DISPLAYED. FOLLOWED PROCEDURE IN FM, NO HELP. ATTEMPTED CB RESET, FAIL MESSAGE RETURNED. ACP'D SYSTEM CHECK OF THE WX RADAR, NO SCAN SWEEP AND FAILURE MESSAGE FAULTED THE ANTENNA. REPLACED THE DRIVE ASSY & ANTENNA PER MM. ALSO DUE TO INTERMITTENT INPUT REPLACED THE CONTROL PANEL PER MM. SYSTEM CHECKED OK REF FAULT ISOLATION CHECK. DRIVE ASSY MR43183, CONTROL PANEL MR43155 ANTENNA.

Part: WIRE HARNESS — DAMAGED (CABIN) · airframe 84,504 hrs · 13,555 cycles

SEAT 6B EEPL LIGHT INOP ACCOUNT WIRING DAMAGED. OK TO CONTINUE PER MEL. RDF-P :EEPL HARNESS ASSY PCN 160-0100 AND EXIT LIGHT P/N BR9644-1. -RDF-P :VERIFIED PART# NEED 566-1162 & POWER AT CONNECTOR. REPLACED LIGHT ASSY FOR EEPL LIGHT OPS CHECK OK.

Part: PCA — OUT OF ADJUST (RT ELEVATOR) · airframe 84,204 hrs · 13,516 cycles

RT ELEVATOR FAILED PCA BELLCRANK CHECK. FOUND RT ELEVATOR EXCEEDS 1 INCH LIMITS BETWEEN LEFT & CENTER HYD SOURCES. INSPECTED AND ADJUSTED ELEVATOR PCA IAW AMM. ELEVATOR CHECKED GOOD.

Part: HEAT SHIELD — COKED (NR 2 PYLON) · airframe 84,096 hrs · 13,500 cycles

NR 2 PYLON, HEAVY COKING AROUND INBD LOWER PYLON HEAT SHIELD AREA. REMOVED CLOG FROM AFT PYLON DRAIN TUBE OUTLET.

Part: CONTROL VALVE — FAULTY (NR 2 ENGINE) · airframe 83,679 hrs · 13,436 cycles

RIGHT ENG START VALVE LIGHT DID NOT EXTINGUISH AFTER ENG SWITCH MOVED TO GND. GOT AIR TO ENG. REPLACED STARTER CTR VALVE RT ENG PER MM. ACP CHECK OK. RAN NR 2 ENGINE PER JRH. ALL OPS AND INDICATION NORMAL.

Part: ANTI-ICE VALVE — FAILED (LT ENGINE) · airframe 83,478 hrs · 13,411 cycles

L ENG ANTI-ICE EICAS. REPLACED L ENG ANTI-ICE VALVE PER MM, OPS TEST OKAY.

Part: ANTI-ICE VALVE — FAILED (ENGINE) · airframe 83,464 hrs · 13,409 cycles

EICAS MSG ENG ANTI- ICE DISPLAYED AND ENG ANTI-ICE VALVE LIGHT REMAINED ILLUM WITH SW ON POSITION 1. TROUBLESHOOT PER MM, REPLACED IAW MM,OPS CHECKED NORMAL.

Part: WINDOW — DEFECTIVE (COCKPIT) · airframe 83,138 hrs · 13,359 cycles

1ST OFFICER'S FIXED SIDE-FORWARD WINDOW'S VISIBILITY IS AFFECTED BY DEFECTS. REPLACE FIRST AVAILABLE. CREW COMMENTS: IN SUN VISIBILITY IS AFFECTED. REPLACED NR 2 RIGHT OPENABLE WINDOW PER MM.

Part: WINDOW — UNSERVICEABLE (COCKPIT) · airframe 83,138 hrs · 13,359 cycles

CAPTAIN'S FIXED SIDE-AFT WINDOW'S VISIBILITY IS AFFECTED BY DEFECTS, REPLACE FIRST AVAILABLE. CREW COMMENTS: IN SUN VISIBILITY IS AFFECTED. NR 3 LT WINDOW NEEDS REPLACEMENT. WINDOW REPLACED.

Part: COOLING FAN — FAILED (EQUIP COOLING) · airframe 83,103 hrs · 13,351 cycles

FORWARD EQUIPMENT COOLING SUPPLY FAN ON EICAS. REPLACED COOLING FAN, CHECKED GOOD.

Part: CONTROLLER — FAULTY (AC PACK) · airframe 82,650 hrs · 13,276 cycles

RIGHT PACK 'AUTO' TEMPERATURE CONTROL SYSTEM(S) INOPERATIVE. DEFERRED PER SAMC. REPLACED RT PACK TEMP CONTROLLER PER MM. CLEANED ALL CABIN TEMP SENSOR SCREEN. RT PACKS OP NORMAL.

Part: FEEDER CABLE — DAMAGED (EMERGENCY LIGHTS) · airframe 82,472 hrs · 13,250 cycles

EMERGENCY LIGHTS INOP SEATS 3, 4, 5, 6. FOUND EEL POWER CABLE CUT FROM POWER SEAT UNDER SEAT 3. REPAIRED AND SECURED. OPS GOOD.

Part: SATCOM — MALFUNCTIONED · airframe 82,154 hrs · 13,205 cycles

UPON DEPARTURE FA REPORTED IFE SYS WOULD NOT WORK, FLIGHT WOULD NOT OPEN. INFORMED TO DEFER ITEM. INSTALLED SC-A. SYS OPS CHECK OK.

Part: WIRE — OUT OF POSITION (CABIN) · airframe 81,780 hrs · 13,143 cycles

EMERGENCY EXIT LIGHTS CONNECTED TO POWER SPLY M1209 DO NOT COME ON WHEN FWD & AFT ATTENDANT TEST SWITCH IS PUSHED, WORKS NORMAL WHEN FLT DECK SWITCH IS ON OR ARMED AND POWER IS OFF. FOUND WIRE W1222-106-22 MIS-PINNED, CORRECTED REF WDM. OP CHECKED OKAY.

Part: SELECTOR VALVE — FAULTY (LANDING GEAR) · airframe 81,776 hrs · 13,142 cycles

GEAR LEVER STIFF. SUGGEST REPLACING MAIN LANDING GEAR SELECTOR VALVE ACCT BINDING, SHUTTER FELT WHEN ISOLATED FROM NLG SEL VLV WHEN OPERATING GEAR HANDLE UP. VLV ON AOG E4252 PART NUMBER 1U1302-1. MAIN LANDING GEAR SELECTOR VLV PER MM.

Part: SHUTOFF VALVE — FAULTY (APU) · airframe 81,554 hrs · 13,106 cycles

CREW REPORTS AFTER ENG START, THE APU BLEED VALVE APPEARS TO BE STUCK CLOSED. WITH SW ON, NO DUCT PRESSURE AND APU BLD SW VALVE LIGHT IS ON, WITH SW CLOSED, NO DUCT PRESSURE AND APU BLEED SWITCH VALVE LIGHT STILL ON. CYCLED SWITCH NUMEROUS TIMES AND NO HELP. RETURN TO BLOCK. DEFERRED IN ACC, WITH MEL. REPLACED APU SHUTOFF VALVE PER MM, OPS OK.

Part: TRANSCEIVER — WEAK (WX RADAR SYS) · airframe 81,436 hrs · 13,086 cycles

WEATHER RADAR FAILED. WXR RT WEAK DISPLAYED. INOP PER MEL. REPLACED WXR TRANSCEIVER AS PER MM.

Part: CONTROL MODULE — FAULTY (LANDING GEAR) · airframe 81,440 hrs · 13,087 cycles

EXTREME EFFORT REQUIRED TO RAISE GEAR LEVER TO UP. MUST BE FIXED BEFORE REVENUE FLT. REPLACING LANDING GEAR CONTROL MODULE. NEED 8 BOLTS 926-0380 FOR NOSE JACK FIXTURE. LANDING GEAR CONTROL MODULE HAS BEEN REPLACED. GEAR NEEDS A GEAR SWING PER SFO STATION MANAGER TO VERIFY FIX. ACCOMPLISHED GEAR SWING. GEAR HANDLE IS SMOOTH IN OPERATION FOR EXTENSION AND RETRACTION. NO DEFECTS NOTED.

Part: SWITCH — INOPERATIVE (APU BLEED) · airframe 81,288 hrs · 13,065 cycles

APU BLEED WILL NOT OPEN TO START SECOND ENGINE. UNABLE TO DUPLICATE ON ENG INE RUN AFTER RETURN TO GATE. REPLACED K495 RT BLEED AIR ENGINE START RELAY AS PRECAUTION IAW FIM FAULT CODE. ALSO NOTED DEFECT WITH APU BLEED SWITCH ON 2ND ENGINE RUN. REPLACED SWITCH. RAN ENGINE. OPS NORMAL.

Part: CIRCUIT CARD — FAULTY (BLEED AIR SYS) · airframe 81,252 hrs · 13,060 cycles

APU VALVE DISAGREE LIGHT DISPLAYED. VALVE CLOSED NORMALLY AND CB PULLED AND COLLARED. APU BLEED WOULD NOT OPEN AFTER STARTING LT ENG. AFTER ACFT RETURNED TO GATE AND LT ENG SHUTDOWN, APU BLEED VALVE OPERATED NORMAL. CHECK APU SHUTOFF VALVE INTERLOCK CIRCUITRY. OTHER POSSIBLE CAUSE: APU BLEED CHECK VALVE. OPS CHECK THIS ITEM WHILE STARTING BOTH ENGS BEFORE CLEARING THIS DF ITEM. FOUND LT ENGINE INDICATION INTERMITTENT AT BLEED SWITCH AND UPPER EICAS ADVISORY MESSAGE, REPLACED THE LT BLEED AIR CONTROL CARD, OPS NORMAL.

Part: ACTUATOR — INOPERATIVE (THRUST REVERSER) · airframe 81,092 hrs · 13,036 cycles

LEFT THRUST REVERSER OPENING ACTUATOR INOP. REPLACED OPENING ACTUATOR REF AMM. OPS NORMAL.

Part: VALVE — FAULTY (POTABLE WATER) · airframe 80,930 hrs · 13,015 cycles

CREW REPORTS NO WATER PRESSURE THROUGHOUT ACFT. POTABLE WATER FILL VALVE LEAKING AIR IN CLOSED POSITION. CONTROL ROD DISCONNECTED FROM VALVE. REPLACED BORROWED WATER FILL VALVE IN AFT PIT, NO HELP. FOUND WATER SYS AIR COMPRESSOR INOP. REPLACED POTABLE WATER SYS AIR COMPRESSOR IAW MM. PRESSURIZE THE POTABLE WATER SYS, AIR COMPRESSOR WILL NOT STOP RUNNING. FOUND DAMAGED LINE ON AIR COMPRESSOR. REPLACED LINE, NO HELP. CB FOR COMPRESSOR PULLED AND COLLARED. AIR SUPPLY LINE AT TOP OF WATER TANK BLOCKED. TEMP LINE INSTALLED. REPLACED AIR SUPPLY LINE ON TOP OF AIR TANK. INSTALLED AIR LINE. WATER SYS OPS NORMAL.

Part: MOTOR — FAILED (TE FLAP) · airframe 80,909 hrs · 13,011 cycles

FLAPS WILL NOT DEPLOY IN THE ALTERNATE POSITION. REPLACED FLAP ELECTRIC MOTOR PER MM BUT FLAPS WILL STILL NOT DEPLOY. NO PWR ON CONN D2312. SECURED BACK CONN D2312. FOUND FLAP BYPASS VALVE MIGRATED, RESECURED PIN, OPS CHECKED NORMAL.

Part: ANTENNA — CORRODED (SATCOM) · airframe 80,646 hrs · 12,968 cycles

FOUND CORROSION AT SATCOM LEFT ANTENNA. REPLACED LT SATCOM HIGH GAIN ANTENNA AND FWD AND AFT ANTENNA CABLES ON RT AND LT ANTENNAS. ACCOMPLISHED SATCOM SYS TEST, CHECKED NORMAL.

Part: CONNECTOR — FAULTY (COMMS) · airframe 80,507 hrs · 12,945 cycles

ACARS NO COMM MOST OF FLIGHT. IAW FIM 23-25-00-101 PARA D(B)UP TO STEP 4 ITEM REPLACED. DID FIND CONNECTORS LOOSE FROM SHIELDS AT HIGH POWER RELAY D2673, D2675. HIGH GAIN SYS LOGS ON FOR APPROX 90 SECONDS THEN SEARCHES AGAIN. CYCLE RESTARTS. HIGH PWR RELAY, PORT BSU, PORT LNA-DIP REPLACED PRECAUTIONARY. LOW GAIN SYS OPS NORMAL. CONNECTORS KN59329M06 PLACED ON PRECAUTIONARY.

Part: SATCOM — INOPERATIVE (NR 1) · airframe 80,422 hrs · 12,932 cycles

SATCOM INOPERATIVE. RESET, NO HELP. SATCOM MENU NOT AVAILABLE ON CDU. HIGH AND LOW GAIN NOT AVAILABLE. REPLACED SATELLITE DATA UNIT PER MM. OPS CHECKED NORMAL.

Part: CHARGER — FAULTY (MASTER BATTERY) · airframe 79,694 hrs · 12,831 cycles

MAIN BATTERY CHARGER STATUS MESSAGE. REPLACED MAIN BATTERY AND MAIN BATTERY CHARGER, MESSAGE CLEARED AND OPS OK.

Part: CAP — LEAKING (WING FUEL CELL) · airframe 79,552 hrs · 12,813 cycles

LT OVER WING FUEL LEAK, FLIGHT DIVERTED. REPLACED LT OVERWING FUEL CAP.

Part: BATTERY — FAILED (MAIN) · airframe 79,202 hrs · 12,764 cycles

EICAS MESSAGE MAIN BATTERY CHARGER. BATTERY BAD. REPLACED MAIN BATTERY IAW MM.

Part: ACTUATOR — FAULTY (HYD SYSTEM) · airframe 79,118 hrs · 12,750 cycles

C HYD SYS MAINT STATUS MSG CAME ON SHORT FINAL. OPERATED C1 AND C2 PUMPS ONE AT A TIME. C2 ONLY PUTTING OUT 2510 PSI. SHOULD BE 2800-3200 PSI. DEFERRED FOR NO TIME. AIR DRIVEN PUMP & C1 PUMP OK. REPLACED C HYD SYS C2 ACMP, NO HELP. SUSPECT PRESS TRANSMITTER SWITCH. PERFORMED CTR SYS INTERNAL LEAKAGE CHECK FOUND INBD AILERON WITH HEAVY CURRENT DRAW, CAPPED LT INBD PCA AND HAD NORMAL CURRENT DRAW COMPARED WITH C-1. REMOVED LT INBD PCA. REPLACED LT IB AILERON ACTUATOR. OPS CHECK GOOD. NO LEAKS. CTR HYD PRESSURE CKS NORMAL

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 78,696 hrs · 12,689 cycles

COCKPIT EMERGENCY LIGHT INOPERATIVE. REPLACED LIGHT ASSY, OPS CKD OK.

Part: CONTROLLER — FAILED (BLEED SYSTEM) · airframe 77,961 hrs · 12,583 cycles

RT BLEED INOP NO PRESSURE CYCLED CB'S AND SW NO HELP. POWERED ENG UP TO 63 PERCENT N1, NO HELP. REPLACED NR 2 ENG PRSOV (773288-7-8-10 / 29) AND PRV. BITE TEST BLEED AIR CONT SHOWED PRV FAIL. RAN ENGINE, STILL NO BLEED PRESSURES. REPLACED PRV CONTROLLER. RAN ENG. DUCT PRESSURE NORMAL.

Part: ACTUATOR — FAULTY (RUDDER TRIM) · airframe 77,668 hrs · 12,539 cycles

RUDDER TRIM INOP, FLIGHT DIVERTED. ACTUATOR FOUND DEFECTIVE. REPLACED RUDDER TRIM ACTUATOR. ACCOMPLISHED RII INSPECTION OF RUDDER TRIM ACTUATOR INSTALLATION. VISUAL FLT CONTROL MOVEMENT CHKS ACCOMPLISHED. ALL OPS & INDICATIONS NORMAL.

Part: MODULE — DAMAGED (CONTROL LEVER) · airframe 77,381 hrs · 12,493 cycles

ON RETRACTION GEAR HANDLE WAS VERY DIFFICULT TO MOVE THROUGH TOP THIRD OF TRAVEL. REPLACED MLG CONTROL LEVER MODULE.

Part: LINE — LEAKING (APU BLEED AIR) · airframe 77,162 hrs · 12,459 cycles

ON WALK AROUND NOTED LOUD NOISE COMING FROM APU AREA SUSPECT AIR LEAK AT PNEUMATICS BLEED VALVE. SHUTOFF OFF APU BLEED NOISE STOPPED. SECURED CLAMP FURTHER TROUBLESHOOTING FOUND POTABLE WATER PRESSURIZATION LINE BROKEN FROM APU PNEU DUCT BULK PIT LT AFT SIDE. REMOVED APU BLEED DUCT SECTION IN AREA OF DAMAGED FITTING FOR REPAIR OR REPLACEMENT. (DUCT IS IN SHEETMETAL SHOP.) REPAIRED DUCT. WELDED FITTING IN. REINSTALLED ORIGINAL APU BLEED DUCT AFTER REPAIR AND LEAK CHECK. NO LEAK PRESENT.

Part: CIRCUIT CARD — FAULTY (LT A/C PACK) · airframe 77,026 hrs · 12,440 cycles

LT PACK OFF LIGHT WILL NOT COME ON WITH PACK OFF. CHECKED AND RESECURED LT PACK FLOW CONTROL CARD, PACK OPS NORMAL EICAS AND LIGHT INDICATION SHOWING WITH PACK SWITCH OFF.

Part: ROD — BROKEN (NR 2 COWLING) · airframe 76,105 hrs · 12,297 cycles

FAN COWL HOLD OPEN ROD ON ENG NR 2 O/B SIDE, IS BROKEN AND UNUSABLE. REPLACED NR 2 ENG O/B FAN COWL HOLD OPEN ROD ASSY.

Part: LENS — UNSECURE (EMERGENCY LIGHTS) · airframe 75,977 hrs · 12,277 cycles

EMERGENCY EXIT LENS COVER LOOSE AT 2R. SECURED LENS ON EMERGENCY LIGHT. OP CHECKED OKAY.

Part: VALVE — MALFUNCTIONED (HYDRAULIC SYS) · airframe 75,810 hrs · 12,245 cycles

CHRONIC HYD TXF RT & CTR. CONDITION SUGGESTS FLUID XFER VIA ANTISKID SHUTTLE VALVES. REPLACED RT INBOARD SHUTTLE VALVE. NO LEAKS NOTED.

Part: PUMP — MALFUNCTIONED (RT OVERIDE) · airframe 74,969 hrs · 12,124 cycles

AN 1800 LB FUEL IMBALANCE DURING CENTER TANK PUMP USAGE. AND 20.0 LB REMAINING IN CENTER TANK. REPLACED RIGHT CENTER OVERRIDE PUMP, LEAK CHECKED. NO LEAKS NOTED. OPS CHECKS GOOD.

Part: POWER SUPPLY — FAULTY (EMERGENCY LGIHTS) · airframe 74,765 hrs · 12,095 cycles

TWO (2EA) AISLE EEL LIGHTS ABOVE SEATS 2A & 6A ARE INOP. NO VOLTAGE AT LIGHT ASSY'S. WILL NEED SEAT 1A REMOVED TO ACCESS BATTERY CHARGER- POWER SUPPLY TO T-S. ESTIMATE 3 SHIFTS. POWER SUPPLY PCN 563- 1046, 2EA. ADJACENT (OPPOSITE SIDE) AISLE LIGHTS OPERATE NORMAL. REPLACED BATTERY CHARGER (POWER SUPPLY). ACP OP TEST.

Part: PRESSURE SWITCH — FAULTY (LEFT) · airframe 74,662 hrs · 12,080 cycles

RECEIVED MSG, L OIL FILTER STATUS AFT ENG START. NO CONTAMINATION IN C-D'S OR FILTERS. REPLACED MAIN OIL FILTER. RAN ENGINE, NO LEAKS DETECTED. CHIP DETECTORS CLEAN. NEED TO REPLACE DIFF PRESS SWITCH AT FIRST OPPORTUNITY. REPLACED DIFF PRESS SWITCH. NO DEFECTS NOTED.

Part: SIGN — INOPERATIVE (LAVATORY) · airframe 74,569 hrs · 12,062 cycles

ELECTRICAL PROBLEMS IN THE CABIN. FOUND AFT CABIN LAV-OCC SIGN L403 BAD. WILL NEED A NEW ONE. ALSO FOUND BROKEN GROUND WIRE HANGING LOOSE IN LAV M1284 DOOR SWITCH. REPAIRED BROKEN GROUND FOR DOOR SWITCH. RELAMPED HANDICAPPED LIGHT SWITCH S11 FOR LAV M1284. FOUND LAV -OCC LIGHT ASSY L402 BAD, WILL NEED A NEW ONE. FOUND ABOUT A DOZEN STIR STICKS. REPLACED BAD LIGHT ASSY.

Part: OXYGEN BOTTLE — LOW PRESSURE (R2 DOOR) · airframe 74,091 hrs · 11,991 cycles

DOOR 2R O2 BOTTLE LOW PRESSURE. REPLACED O2 BOTTLE.

Part: PUMP — MALFUNCTIONED (HYDRAULIC SYS) · airframe 73,765 hrs · 11,937 cycles

ADP LOW PRESS LIGHT AND EICAS MSG ON TAKEOFF DURING GEAR RETRACTION & FLAPS 5 TO 1. REPORTED BY CREW. REMOVED AND REPLACED ADP. NO HELP. STILL NEED TO LEAK CHECK, NEEDS FURTHER TROUBLESHOOTING. REPLACED MOD. AIR DRIVEN PUMP AND ADP REG AND SHUTOFF VALVES (3214334-3-33). LEAK AND OPS CHECK NORMAL.

Part: DENSITOMETER — FAULTY (CENTER FUEL TANK) · airframe 73,582 hrs · 11,911 cycles

DURING CRUISE, CENTER FUEL TANK REFILLED ITSELF FROM 700 LBS TO 1400. FUEL CONFIG LIGHT LIT. ACCOMPLISHED FQ BITE, FOUND 'CT DENS RESISTOR UNREADABLE'. REPLACED CTR TANK DENSITOMETER.

Part: PANEL — DAMAGED (LE SLAT) · airframe 72,319 hrs · 11,731 cycles

RT WING NR 7 LEADING EDGE SLAT CLOSURE PANEL DAMAGED. REINSTALLED REPAIRED PANEL. OPS CHECK NORMAL, FAIR GOOD. REPAIRED PER GN-MM 1-0-1-24.

Part: ACOUSTIC LINER — DAMAGED (NR 2 NOSE COWL) · airframe 72,292 hrs · 11,727 cycles

NR 2 ENG ACOUSTIC LINER 8 O'CLOCK POS DAMAGED. NR 2 ENG INNER ACOUSTIC PANEL 8 O'CLOCK POSITION CRACKED 4.5 INCHES FORWARD OF LPC BLADES. REPLACED NR 2 ENG NOSE COWL.

Part: SLIDE — FAULTY (LT OVERWING) · airframe 72,185 hrs · 11,713 cycles

LT OVERWING INFLATION HOSE IS FLATTENED 12 INCHES AT THE SLIDE COMPARTMENT ELBOW. SLIDE REPLACED.

Part: HOSE — FAILED (LT OVRWING SLIDE) · airframe 72,185 hrs · 11,713 cycles

LT OVERWING INFLATION HOSE IS FLATTENED 12 INCHES AT THE SLIDE COMPARTMENT ELBOW. SLIDE REPLACED.

Part: SLIDE — UNSERVICEABLE (L1 DOOR) · airframe 72,185 hrs · 11,713 cycles

DOOR L1 SLIDE COMING UNLACED. INSTALLED NEW SLIDE AT DOOR L-1.

Part: HOUSING — BROKEN (EVAC SLIDE) · airframe 72,185 hrs · 11,713 cycles

LEFT OVERWING SLIDE COMPARTMENT, DISCONNECT HOUSING IS BROKEN. REPLACED DISCONNECT HOUSING. REINSTALLED LT DISCONNECT CAM ASSY. EXAMINED INFLATION CABLE FOR FREEDOM OF MOVEMENT, CHECKS GOOD.

Part: LATCH — DEFECTIVE (L3 DOOR) · airframe 72,185 hrs · 11,713 cycles

LEFT OVERWING SLIDE COMPARTMENT DOOR NR 3 LATCH FAILED EDGE MARGIN CHECK. INSTALLED NEW NR 3 LATCH, OPS CHECKS GOOD.

Part: LATCH — SCORED (L4 DOOR) · airframe 72,185 hrs · 11,713 cycles

LEFT OVERWING SLIDE COMPARTMENT DOOR LATCH NR 4 IS SCORED. INSTALLED NEW LATCH, OPS CHECKS GOOD.

Part: STRUCTURE — DAMAGED (FUSELAGE) · airframe 71,779 hrs · 11,644 cycles

RT SIDE FUSELAGE DAMAGE FROM STA 1131 TO 1175 STRINGERS 18R TO 20R. MAJOR REPAIR ACCOMPLISHED. MANUFACTURED REPAIR DOUBLER TRIPLER AND FILLER REPAIR.

Part: WIRE — EXPOSED (CABIN) · airframe 71,721 hrs · 11,636 cycles

WIRES EXPOSED ON EMERGENCY FLOOR LIGHTS.

Part: WIRE — EXPOSED (CABIN) · airframe 71,721 hrs · 11,636 cycles

WIRES EXPOSED ON EMERGENCY FLOOR LIGHTS. REPLACED EEL LIGHT STRIP AND COVER.

Part: WIRE — FRAYED (MASK MICROPHONE) · airframe 70,258 hrs · 11,417 cycles

SECOND OBSERVER O2 MASK MIC WIRE IS FRAYED. *S/D* FOUND MIC WIRE FRAYED. REPLACED 2ND OBS O2 MASK PER MM 35-11-51. AC OK FOR SERVICE.

Part: DUCT — CRACKED (LT A/C PACK) · airframe 69,869 hrs · 11,357 cycles

LT PACK INOPERATIVE - REHEATER INLET DUCT CRACKED. *S/D* SUSPECT IMPROPER INSTALLATION. REPLACED LT PACK REHEATER DUCT PER MM 21-51-21. OP CHECKS NORMAL. AC OK FOR SERVICE.

Part: REGULATOR VALVE — FAULTY (NR 1 ENGINE) · airframe 69,587 hrs · 11,307 cycles

LEFT ENG BLEED AIR VALVE WILL NOT OPEN. DUCT PRESSURE ON LEFT SIDE IS ZERO. ADVANCED ENG POWER AND STILL NO HELP. FOUND PRESSURE REGULATING VALVE TO BE FAULTY. REPLACED PRV, RAN ENGINE OP CHECKED GOOD. AC OK FOR SERVICE.

Part: LIGHT — BROKEN (CABIN) · airframe 69,587 hrs · 11,307 cycles

REF SMC001 ON EEL STRIP BROKEN, NEW STRIP IS IN PLACE AND WILL REQUIRE SPLICING AND RE-ASSEMBLY OF EEL STRIP CABLE PROTECTIVE COVERS AND CARPET. FOUND LIGHT ASSEMBLY BROKEN. SPLICED IN SECTION OF EEL LIGHT ASSEMBLY, OP CHECKED GOOD. AC OK FOR SERVICE.

Part: VALVE — MALFUNCTIONED · airframe 69,343 hrs · 11,272 cycles

FWD EQUIPMENT VALVE EICAS MSG ON LANDING. FOUND OVERBOARD VALVE AND COOLING CONTROL PANEL FAULTY. REPLACED FORWARD OVERBOARD VALVE, AND EQUIPMENT COOLING CONTROL PANEL. OP CHECKS NORMAL. AC OK FOR SERVICE.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 69,173 hrs · 11,244 cycles

EMERGENGY LIGHT L313 AT DOOR IL HAS BROKEN WIRE. LIGHT ASSY LOCATED AT FWD UPPER CORNER OF DOOR FRAME VISIBLE FROM OUTSIDE WITH DOOR OPEN. FOUND BROKEN WIRE AT LIGHT ASSEMBLY. REPAIRED WIRE AND OP CHECK GOOD. AC OK FOR SERVICE.

Part: LIGHT — MISSING (CABIN) · airframe 68,749 hrs · 11,180 cycles

EMERGENCY LIGHT ON FLOOR 1E PLASTIC IS MISSING.

Part: CHECK VALVE — FAULTY (BLEED AIR SYS) · airframe 68,402 hrs · 11,122 cycles

NR 1 ENGINE HAS THE L BLEED OFF EICAS MSG AND L-BLEED OFF LIGHT ON WITH BLEED SELECTED. REPLACED ISOLATION BYPASS CHECK VALVE. FOUND DIRECT SHORT AT PRSOV CONNECTOR. FOUND D22 CONNECTOR ON PRSOV BAD. REPLACED SAME. OPS CHECKED GOOD. REPLACED PRSOV. LEAK & OP CHECKS GOOD.

Part: ASPIRATOR — LEAKING (EVAC SLIDE) · airframe 67,046 hrs · 10,918 cycles

LEAKING ASPIRATOR.

Part: PUMP — UNKNOWN (HYD SYSTEM) · airframe 67,015 hrs · 10,910 cycles

RTFL DUE TO CENTER HYDRAULIC PUMP PROBLEM. REPLACED HYDRAULIC AIR DRIVEN PUMP. ALSO REPLACED HYD LINES & PUMP MOUNTS. PERFORMED SYSTEM CHKS. OK FOR SERVICE.

Part: UNKNOWN — ODOR (GALLEY) · airframe 66,809 hrs · 10,875 cycles

ELECTRICAL BURNING ODOR IN MID GALLEY AREA AND AIRCRAFT RETURNED TO BLOCKS. INSP GALLEY AREA AND OVERHEAD AREA FOR EVIDENCE OF BURNING NO OBVIOUS SIGHT OF SMOKE OR BURNING. FIRE BRIGADE PERFORMED HEAT DECTECTOR EQUIPMENT NO SIGN FOUND.NO HISTORY () INSP CHILLERS ALL OK.

Part: LAMP — INOPERATIVE (SMOKE DETECTOR) · airframe 66,697 hrs · 10,857 cycles

DURING EQUIP COOLING TEST, SMOKE LIGHT DOES NOT COME ON AND NO FWD EQUIPMENT SMOKE ADVISORY MESSAGE. RELAMPED SMOKE DETECTOR. OPS CK OK PER JC EQUIP COOLING TEST.

Part: OXYGEN MASK — DEFECTIVE (COCKPIT) · airframe 53,900 hrs · 19,729 cycles

OXYGEN MASK DEFECTIVE AT 2.(1=CAPT,2=1ST OFF,3=1ST OBS). CREW COMMENTS: O2 MASK INFLATABLE BAND BURST.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 66,237 hrs · 10,776 cycles

EEL LIGHT INOP LOCATED AT FIRST CLASS ZONE RIGHT AISLE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 66,237 hrs · 10,776 cycles

EEL LIGHT INOP LOCATED MID ZONE LAVATORY LEFT & RIGHT AISLES.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 66,237 hrs · 10,776 cycles

EEL LIGHT INOP LOCATED AT FIRST CLASS ZONE LEFT AISLE.

Part: BEZEL — MISSING (CABIN) · airframe 66,237 hrs · 10,776 cycles

BEZEL IS MISSING FROM EEL LIGHT AT ROW 18 BC.

Part: POWER SUPPLY — FAULTY (CABIN) · airframe 65,770 hrs · 10,701 cycles

RIGHT SIDE BUSINESS CLASS EXIT STRIP LIGHTING ON AND OFF INTERMITTENTLY. PER FLT ATTENDANT, THE RT SIDE IN FIRST CLASS ONLY & AROUND DOOR 1R HAD THE PROBLEM. REPLACED POWER SUPPLY M1552. CHECKS GOOD.

Part: FLOORBEAM — MISMANUFACTURED (BS 368) · airframe 65,764 hrs · 10,698 cycles

CABIN FLOORBEAM AT BS 368 AND RBL 58 HAS 2 EACH MISDRILLED HOLES, ONE THROUGH UPPER CHORD AND WEB AND THE OTHER IN THE UPPER CHORD RADIUS. CUTOUT DAMAGE IN WEB AND OVERSIZED THE 2 MISDRILLED HOLES. FABRICATED 1 REPAIR ANGLE FOR THE FWD AND AFT SIDE OF THE FLOORBEAM WEB. FABRICATED AND INSTALLED FILLERS.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 65,764 hrs · 10,698 cycles

EEL LEAD WIRE BROKEN. REMOVED AND REPLACED EEL LIGHT BARS PER MM 33-51-10 AND OPS CHECK GOOD PER MM 33-51-00 ON N-R 25692.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 65,764 hrs · 10,698 cycles

RIGHT SIDE EXTERNAL OVERWING EMERGENCY EXIT LIGHT IS INOPERATIVE. TROUBLESHOT AND FOUND BAD LAMP. REMOVED AND REPLACED LAMP. OPS CHECKS GOOD.

Part: STIFFENER — CRACKED (BS 246) · airframe 65,764 hrs · 10,698 cycles

CABIN FLOORBEAM STA 246 VERTICAL STIFFENER AT FWD FACE, RBL 11, CRACKED AT BEND RADIUS. [08-14-07] REMOVED AND REPLACED VERTICAL STIFFENER PER SRM 53-10-51, PARAGRAPH 3. AIRPLANE READY FOR SERVICE. SUSPECT FATIGUE EXACERBATED BY ASSEMBLY PRE-LOAD.

Part: FLOOR PANEL — GOUGED (FWD CARGO BAY) · airframe 65,764 hrs · 10,698 cycles

FWD CARGO PIT TORQUE FLOOR GOUGED FWD AND AFT OF PDU 8C, RBL 5, STA 560. [08-14-07] FOUND OUT OF LIMITS. FABRICATED NEW PANEL PER BAC DWR 451T2504. INSTALLED NEW PANEL PER SRM51-40-02. AIRPLANE RETURNED TO SERVICE READY.

Part: HOSE — DAMAGED (RT ESCAPE SLIDE) · airframe 65,764 hrs · 10,698 cycles

RIGHT OVERWING SLIDE CYLINDER LWR INFLATION HOSE IS KINKED AND COLLAPSED. [08-07-07] REPLACED HOSE IAW 20-10-10. SLIDE PROBLEM ROOT CAUSE: SLIDE & INFLATION HOSE ARE IN AN AREA CONTAINING MANY HYDRAULIC LINES & SERVICING ACCESS; SUSPECT HOSE DAMAGED BY SKYDROL CONTAMINATION. SLIDE & AIRCRAFT OK FOR SERVICE.

Part: LATCH — WORN (OVERWING SLIDE) · airframe 65,764 hrs · 10,698 cycles

RIGHTHAND OVERWING SLIDE COMPARTMENT DOOR NR 3 LATCH WORN. REMOVED & REPLACED LATCH AND KEEPER.

Part: LATCH — BINDING (OVERWING SLIDE) · airframe 65,764 hrs · 10,698 cycles

LEFT OVERWING SLIDE DOOR NR 2 LATCH BINDING. [08-08-07] REPLACED AND ADJUSTED LATCH PER MM25-65-98. DOOR 2 LATCH MOVES FREELY. SLIDE & AIRCRAFT OK FOR SERVICE. SLIDE PROBLEM ROOT CAUSE: SLIDE LATCHES EXPERIENCE FRETTING CAUSED BY VIBRATION & EXCESSIVE CLEARANCE CAUSED BY WEAR.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 65,764 hrs · 10,698 cycles

FWD GALLEY FLOOR AREA, STA 246 AT RBL 72 AREA, BULKHEAD WALL, LOWER FLOOR CHORD CORRODED UNDER SHEAR WEBBING, FWD EDGE. REMOVED DAMAGED SECTION OF CHORD, RBL 49 TO RBL 72. FABRICATED & INSTALLED SPLICE & REPAIR ANGLES.

Part: GENERATOR — UNKNOWN (LEFT) · airframe 64,919 hrs · 10,546 cycles

CREW REPORTS LOSS OF LEFT GENERATOR. [SUP 05-04-07] REPLACED LEFT ENGINE INTEGRATED DRIVE GENERATOR. RAN UP ENG PER JRH 2-6-1, IDG OPERATED NORMALLY. OUTBOUND TRIP DID VERIFICATION TEST AND IDG OPERATED OK. SUSPECT INTERNAL WEAR LED TO FAULTY HERTZ OUTPUT & MISMATCH WITH OTHER A/C GENERATOR.

Part: SLIDE — LOW PRESSURE (R1 DOOR) · airframe 64,510 hrs · 10,475 cycles

DOOR 1R SLIDE PRESSURE READS BELOW SERVICEABLE LIMIT. REPLACED R1 DOOR SLIDE PER MM 25-66-01. CAUSED BY SUSPECT SEAL LEAKAGE AT BOTTLE CONNECTION.

Part: CIRCUIT CARD — FAILED (MLG) · airframe 62,938 hrs · 10,180 cycles

EICAS MSG 'LDG GEAR MONITOR' DISPLAYED WITH LDG GEAR UP AND LOCKED. FOUND ALL EXCEPT 4 CIRCUIT CARDS DISLODGED IN PSEU. REMOVED AND REINSTALLED ALL CIRCUIT CARDS.

Part: SKIN — CRACKED (NR 1 ENG PYLON) · airframe 62,345 hrs · 10,088 cycles

NR 1 ENG PYLON INBOARD SIDE 2 INCH CRACK OUTER SKIN OUT OF INSPECTION PANEL CUTOUT.

Part: BATTERY PACK — FAILED (ESCAPE SLIDE) · airframe 61,765 hrs · 10,003 cycles

SQUIB TEST ON EMERGENCY ESCAPE SLIDES WILL NOT TEST. REPLACED RIGHT AND LEFT SQUIB BATTERY PACKS PER AMM 25-65-17. SQUIB TESTS GOOD.

Part: ODOR — DETECTED (COCKPIT) · airframe 60,961 hrs · 9,871 cycles

DIVERTED TO YBG DUE TO ELECTRICAL ODOR AND FUMES IN FLIGHT DECK. CHK'D FOR BURNED WIRING AND PROBLEMS WITHIN E&E COMPARTMENT. NO EICAS MESSAGE NOTED BY FLIGHT CREW. CLEANED DIRTY OVENS AT FWD GALLEY. CHECKED WIRING AND COMPONENTS IN AREA AND FOUND NO DISCREPANCIES. OP CHECKS OK FOR SERVICE.

Part: ASPIRATOR — MALFUNCTIONED (SLIDE) · airframe 60,517 hrs · 9,800 cycles

BOTH ASPIRATORS STAYED OPEN DURING SLIDE DEPLOYMENT.

Part: TRIGGER — BROKEN (LT OVRWG SLIDE) · airframe 60,517 hrs · 9,800 cycles

LEFT OVERWING SLIDE PACK TRIGGER BROKEN. REPLACED SLIDE. AIRCRAFT RELEASED TO SERVICE. ROOT CAUSE WAS SLIDE PACK TRIGGER BROKEN DURING INSTALLATION.

Part: HINGE FITTING — CRACKED (RH INBD TE FLAP) · airframe 60,517 hrs · 9,800 cycles

RIGHT INBOARD AFT FLAP, CENTER HINGE FITTING CRACKED ON OUTBOARD SIDE IN COVE AREA. *S/D* THE RIGHT INBOARD AFT FLAP, CENTER HINGE FITTING, WAS FOUND CRACKED ON THE OUTBOARD SIDE IN THE COVE AREA. REPAIRED FITTING PER 767 SRM 57-53-02.

Part: LATCH — WORN (CABIN)

NR 1 AND NR 2 LATCHES EDGE MARGIN BEYOND LIMITS. REMOVED AND REPLACED LATCHES.

Part: DOOR — SEPARATED (RAM AIR) · airframe 58,394 hrs · 9,441 cycles

DIVERTED TO YQX DUE TO AIRFRAME VIBRATION. RAM AIR INLET DOOR ASSY WAS FOUND WITH FORWARD INLET DOOR ASSY P/N 213T3010-1 MISSING. AFT HINGE ASSY P/N 213T3108-4 ATTACHING THE FORWARD AND AFT INLET DOOR ASSY WAS ALSO MISSING. FORWARD HINGE ASSY P/N 213T3109-4 WAS FOUND ATTACHED TO THE AIRCRAFT. THE FIVE FASTENERS ATTACHING FORWARD HINGE ASSY TO THE FORWARD INLET DOOR WERE SHEARED. AFT INLET DOOR ASSY P/N 213T3009-1 WAS FOUND WITH NO VISIBLE STRUCTURAL DAMAGE. THE EIGHT FASTENERS INCLUDING THE COLLARS, ATTACHING THE AFT INLET DOOR ASSY TO AFT HINGE ASSY P/N 213T3108-4 WERE MISSING. BLOCKS AND ATTACHING HARDWARE WERE STILL INSTALLED ON THE AFT INLET DOOR. ACTUATOR WAS REPORTED TO HAD BEEN REPLACED.

Part: WIRE — BURNED (TERMINAL BLOCK) · airframe 54,604 hrs · 8,855 cycles

FOUND WIRES W298-021-08, W1046-913-08, W1046 -012-10, W1046-028-12. BURNED AT TB 5132 TERMINAL BLOCK INSIDE P37. REPLACED TERMINAL STRIP TB5132 IN P37 PANEL.

Part: HINGE — CRACKED (RT WING) · airframe 54,320 hrs · 8,808 cycles

RIGHT WING INBOARD FLAP CENTER EXTERNAL HINGE IS CRACKED. MAJOR REPAIR ACCOMPLISHED. REPAIRED FLAP HINGE WITH REPAIR ANGLES AND FILLER.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 54,320 hrs · 8,808 cycles

MAIN CABIN SEAT TRACK LBL 88 AT BS 747.5 TO 808 BROKEN, CRACKED AND CORRODED. DAMAGED SEAT TRACK REPLACED.

Part: SPAR — CRACKED (NR 2 NACELLE) · airframe 54,320 hrs · 8,808 cycles

NR 2 NACELLE UPPER SPAR WEB IS CRACKED SEVERAL PLACES AS SEEN THROUGH ACCESS 446BL. REPAIRED UPPER SPAR WEB WITH DOUBLER AND FILLER JUST FWD OF PYLON AFT BLKHD PER SRM 54-53-01, FIG 208. PER SB 767-54-0092 R1 PROBABLE CAUSE OF CRACKING IS FLEXING OF PYLON MIDSPAR WEB.

Part: HINGE — CRACKED (LT WING FLAP) · airframe 54,320 hrs · 8,808 cycles

LEFT WING INBOARD FLAP CENTER EXTERNAL HINGE IS CRACKED. MAJOR REPAIR ACCOMPLISHED. REPAIRED HINGE WITH REPAIR ANGLES.

Part: CONTROL PANEL — FAILED (WX RADAR SYS) · airframe 53,841 hrs · 8,709 cycles

FLIGHT DIVERTED DUE TO WX RADAR FAILURE. CREW REPORTED WX RADAR INOP. DOES NOT PAINT AND GREEN ARC ON DISPLAY. ALSO, NO GROUND RETURNS. ( THE GREEN ARC IS A FLAT PLATE ANTENNA ANOMALY THAT DOES NOT AFFECT WX RADAR PERFORMANCE.) MAINTENANCE REPLACED THE WX RADAR CONTROL PANEL AND THE WX RADAR SCANNER. THERE HAVE BEEN NO RECURRING PROBLEMS INVOLVING WX RADAR PERFORMANCE.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 51,701 hrs · 8,338 cycles

EMERGENCY EXIT PATH LIGHTS ROW 15-17 BLINK ON AND OFF. REPLACED M737 BATTERY ASSEMBLY.

Part: SMOKE DETECTOR — MALFUNCTIONED (LAVATORY) · airframe 47,627 hrs · 7,637 cycles

SMOKE ALARM WENT OFF IN AFT LAV. NO SMOKE OBSERVED AND FLIGHT LANDED UNEVENTFULLY. SUPPLEMENTAL DATA UPDATE THE AFT CENTER LAV SMOKE DETECTOR WAS AT FAULT. THE UNIT WAS REPLACED WITH P/N PU90-461R3 (PCN 563-3542) . THE SYSTEM CHECKED FINE AFTERWARD.

Part: WIRE HARNESS — DAMAGED (CABIN) · airframe 45,800 hrs · 7,328 cycles

EEL LIGHTING DAMAGED AT RIGHT HAND BUSINESS CLASS GALLEY. REPLACED TWO DAMAGED EEL LIGHTING STRIPS. REPAIRED DAMAGED POWER LEAD AND INSTALLED NEW LIGHTING COVER STRIP.

Part: STRAP — CRACKED · airframe 42,822 hrs · 6,793 cycles

FORWARD PIT STATION 287 LEFT HAND SIDE, STRINGER 26L TO 29L TEAR STRAP CRACKED. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 42,822 hrs · 6,793 cycles

AFT PIT FLOORBEAM T-CAP CORRODED UNDER NUT PLATE STRINGER 33L STATION 1197 + 110. MAJOR REPAIR ACCOMPLISHED. T-CAP REPAIRED.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 42,822 hrs · 6,793 cycles

AFT PIT FLOORBEAM T-CAP CORRODED ABOVE STRINGER 36L, STATION 1153. MAJOR REPAIR ACCOMPLISHED. REPAIRED T-CAP.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 42,822 hrs · 6,793 cycles

AFT PIT FLOORBEAM T-CAP CORRODED RBL 8, STATION 1197.66. MAJOR REPAIR ACCOMPLISHED. T-CAP REPAIRED.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 42,822 hrs · 6,793 cycles

AFT PIT FLOORBEAM T-CAP LOWER SURFACE HAS CORROSION AT STATION 1197+132 AT STRINGER 33L. MAJOR REPAIR ACCOMPLISHED. REPAIRED FLOORBEAM T-CAP.

Part: BEAM — CORRODED (FUSELAGE) · airframe 42,822 hrs · 6,793 cycles

CABIN C-ZONE STATION 852, LBL 54, UPPER TRANSBEAM CORRODED. MAJOR REPAIR ACCOMPLISHED. REPAIRED FLOORBEAM TRANSBEAM SPLICE.

Part: STRINGER — DAMAGED (FUSELAGE) · airframe 42,822 hrs · 6,793 cycles

E+E BAY AT STATION 287, STATION 26R END FITTING NEEDS TO BE RE-FABRICATED TO FACILITATE STRINGER REPAIR. MAJOR REPAIR ACCOMPLISHED. FABRICATED NEW STRINGER END FITTING.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 42,822 hrs · 6,793 cycles

STATION 287 RT, FUSELAGE SKIN CREASED. MAJOR REPAIR ACCOMPLISHED. REPAIRED SKIN DAMAGE AND INTERNAL BULKHEAD CHORD ANGLE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 42,822 hrs · 6,793 cycles

BODY STATION 347 LBL 88 WL 200 FLOORBEAM T-CAP CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED T-CAP.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 42,822 hrs · 6,793 cycles

BODY STATION 1131 LBL 35 LOWER STRAP DOUBLER CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED STRAP.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 42,822 hrs · 6,793 cycles

BODY STATION 347 LBL 48-88 T-CAP IS CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED SECTION AND SPLICES.

Part: BEAM — CORRODED (FUSELAGE) · airframe 42,822 hrs · 6,793 cycles

BODY STATION 852 LBL 33 TRANSBEAM CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED NEW SECTION AND SPLICES.

Part: SPLICE — CRACKED · airframe 42,822 hrs · 6,793 cycles

PYLON SPAR ANGLE, LEFT AFT SPLICE CRACKED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED SPLICE PLATE.

Part: ENGINE — STALLED (RIGHT) · airframe 40,839 hrs · 6,454 cycles

RIGHT ENGINE SURGED AND STALLED, FLAMES WERE COMING FROM THE FRONT AND BACK AFTER TAKEOFF. REPLACED ENGINE.

Part: AUTOPILOT SYS — MALFUNCTIONED (COCKPIT) · airframe 40,600 hrs · 6,413 cycles

ON DESCENT OUT OF 8,000 FEET AUTOPILOT SPD 210, FLAPS 5-WHEN SPEED BRAKE DEPLOYED PAST 1-2 TOWARDS FULL. AC REMAINED WINGS LEVEL, BUT YOKE SHOWED 2 1-2 TO 3 DEG ON STATUS PG RT INBOARD AILERON ALMOST FULLY DEFLECTED DOWN. OK WITH NO SPEED BRAKE. UNEVENTFUL LANDING.

Part: ACTUATOR — LEAKING (MLG) · airframe 35,034 hrs · 5,450 cycles

SHORTLY AFTER LANDING GEAR HANDLE RAISED, SHUDDER FELT WITH LOUD ''BANG '' SOUND. *S/D* FOUND TR MLG TRUCK POSITION ACTUATOR HAD INTERNALLY FAILED ON GEAR RETRACTION. REPLACED ACTUATOR.

Part: COMPRESSOR — STALLED (ENGINE)

COMPRESSOR STALL AT 19,000 FEET, 2 ADDITIONAL MOMENTARY COMPRESSOR STALLS ON APPROACH.

Part: BATTERY — DISCHARGED (CABIN)

EMERGENCY FLASHLIGHT RT SIDE CROSS AISLE FWD OF 15CDE NOT FLASHING. *S/D* REPLACED BATTERY KIT AND TESTS OK.

Part: AIR DIST — ODOR (CABIN)

STRONG BURNING RUBBER SMELL IN FIRST FOUR ROWS OF BUSINESS CLASS. DIVERTED TO PHL. A DETAILED CHECK OF THE AREA WAS ACCOMPLISHED AND NO PROBLEMS WERE FOUND. A SEARCH OF THE AMIS DATABASE HAS BEEN ACCOMPLISHED AND NO FAULTS COULD BE ATTRIBUTED TO THIS EVENT. THE AIRCRAFT HAS CONTINUED TO OPERATE WITHOUT FURTHER INCIDENT.

Part: LIGHT — INOPERATIVE (CABIN)

FLOOR EMERGENCY LIGHT AT SEAT 11 ON RIGHT SIDE INOPERABLE. REPLACED FLOOR EMERGENCY LIGHT, OPERATIONS CHECK NORMAL.

Part: CHIP DETECTOR — FELL OUT (NR 2 ENGINE)

RETURNED TO FIELD WITH NR 2 ENGINE SHUTDOWN, DUE TO LOW OIL QUANTITY. FOUND CHIP DETECTOR LYING IN COWL. CHANGED PROCEDURES TO REQUIRE LOCKWIRE OF THESE CHIP DETECTORS.

Part: COMPRESSOR BLADE — FAILED (LT ENGINE)

SHUTDOWN LEFT ENGINE DUE TO COMPRESSOR STALLS AND LANDED UNDER AMBER ALERT. EIGHTH STAGE BLADE FAILED, DUE TO SEVENTH STAGE INNER SHROUD DOWL PIN LIBERATION.