N659UA

Part: ELEC CONNECTOR — BROKEN (ZONE 200) · airframe 127,471 hrs · 19,579 cycles

EMERGENCY CEILING LIGHT CONNECTER BROKEN AT RT CEILING PANEL AT SEAT ROWS 36, 37, 38. R & R CONNECTOR REF WDM 33-51-12, SWPM 20-61-28, N0542-D73, AMM 33-51-00. OPS CHECK GOOD.

Part: LIGHT SYS — NO DISCREPANCY (ZONE 200) · airframe 127,471 hrs · 19,579 cycles

DOOR 2R EMER EXIT LIGHT IS ON WHEN THE MASTER SWITCH IN FLIGHT DECK IS OFF WITH MASTER EMERGENCY LIGHT SWITCH OFF, DOOR 2R EMER EXIT LIGHT REMAINS OFF. EMERGENCY LIGHTING OPS CHECK REF AMM 33-51-00 PERFORMED SEVERAL TIMES; LIGHTS ARE FUNCTIONING AND EXTINGUISHING AS INTENDED.

Part: ACCESS PANEL — MISSING (ZONE 400) · airframe 127,143 hrs · 19,537 cycles

DURING WALK AROUND, NR 2 ENG PYLON OTBD PANEL 446AR FOUND MISSING.

Part: ACTUATOR — FAULTED (RIGHT) · airframe 126,644 hrs · 19,477 cycles

RIGHT OFF-WING ESCAPE SLIDE OPERATIONAL CHECK {B767-25-3-7036} - RIGHT OVERWING DOOR LATCH ACTUATOR REQUIRES REPLACEMENT. MARKED FOR RII REQUEST CLEARANCE TO INSTALL. IPC REFERENCE # MFG SN OFF NOT ON AC ACTUATOR, ASSY OFF 76-2565-9-0003 4625 ON 76-2565-9-0003 1288 VERIFED NO FOR DOOR LATCH ACT AND INSPECTED MOUNTING AREA PER AMM 5-6-11 AND IPC 25-65-11-02 NO DEFECTS NOTED OK TO INSTALL REPLACED R OVERWING SLIDE DOOR LATCH ACTUATOR REF AMM 25-65-11

Part: CABLE — OUT OF ADJUST (ZONE 800) · airframe 126,644 hrs · 19,477 cycles

RIGHT OVERWING SLIDE, NITROGEN BOTTLE ACTIVATION CABLE. REMOVED FOR REPLACEMENT PART NUMBER VERIFICATION PRIOR TO INSTALL VERIFIED RT OFFWING ESCAPE SYS INFLATION CABLE P/N REF IPC 25-65-02-01. INSTALLED THE NEW RIGHT HAND OFF WING SCAPE SYSTEM INFLATION CABLE AND PERFORMED ADJUSTMENT PER AMM 25 -65-04. VERIFIED RH OFFWING ESCAPE SYS INFLATION CABLE INSTALL & ADJUSTMENT REF AMM 25-65-04.

Part: CABLE — STRETCHED (ZONE 800) · airframe 126,644 hrs · 19,477 cycles

RIGHT OFF-WING ESCAPE SLIDE OPERATIONAL CHECK - SLIDE FAILS TO INFLATE. NR 7 SPOILER SQUIB, LATCH ACTUATOR AND BOTH DOOR ACTUATORS BLEW BUT BOTTLE FAILED TO PRESSURIZE SLIDE TO INFLATE AND DEPLOY. INSPECTED CAUSE OF SLIDE NON-INFLATION AND FOUND CROSS PIN TWISTED AND NOT SEATED IN BELLCRANK WHICH DID NOT PULL THE INFLATION CABLE ON THE BOTTLE. SEE PICTURE ATTACHED. PERFORMED AMM 25-65-00-842-021 UP TO STEP H 3 FOUND CABLE ASSY BETWEEN PRESSURIZATION BOTTLE AND RT OVERWING SLIDE DOOR BELLCRANK TWISTING DURING ACTUATION AT THE CROSS PIN ASSY. PART NIS AT IAD REFER LOG PAGE 5675791 FOR REPLACEMENT OF RHIGHT HAND OFFWING SCAPE SYSYEM INFLATION CABLE SDR UPDATED, AWAITING FURTHER INFORMATION TO COMPLETE AMM 25-65-00-842-021 STEP H3-END ACCOMPLISHED

Part: LIGHT — NO TEST (ZONE 200) · airframe 126,465 hrs · 19,454 cycles

EMERGENCY LIGHTS OPERATIONAL CHECK {B767-33-3-7000} - DURING OPERATIONAL CHECK WAS FOUND AFTER EXTERNAL LIGHT SIDE RIGHT DOOR 2RH INOP. IT WAS SLIDE AND OVERWING ESCAPE LIGHT LAMP REPLACEMENT AFTER DOOR RIGHT 2RH AS PER AMM-TASK 33-51-06-902-082, CHECKED OK.

Part: GUARD — DAMAGED (ZONE 200) · airframe 126,136 hrs · 19,416 cycles

FOUND FLT DECK EMERGENCY LIGHT SWITCH GUARD DAMAGED. REPLACED EMERGENCY LIGHT SWITCH GUARD ON FLTDE K PVERHEAD PANEL, OPS CHECKS GOOD.

Part: PANEL — MISSING (ZONE 400) · airframe 125,993 hrs · 19,399 cycles

PDA 2 REF LP 5040261, #1 ENGINE PANEL 436BR MISSING UPON ARRIVAL. REF LP 5039727, GOING TO APPLY CDL 54D INSTALLED INBOARD ACCESS DOOR ON #1 ENG PYLON IN REF TO AMM 54-53-00 PARTS USED: 76-5453-3-0063,QTY :1

Part: TRANSMITTER — FAULTED (HYD SYSTEM) · airframe 125,798 hrs · 19,376 cycles

L HYD QTY EICAS PRESSURE 3100 LEFT A/P DISCONNECTEDTECH SUPPORT UPDATE. REF WDM 29-33-11-2 TEST WIRING WITH A MEGGER FROM CONNECTOR D38 ON HYDRAULIC QUANTITY TRANSMITTER TO D4474P. SHAKE WIRES WHILE TESTING. BE SURE TO ISOLATE WIRING BEFORE TESTING. IADLM MACINNES REPLACED LEFT HYD QUANTITY TRANSMITTER REF AMM 29-33-02-404-014. LEAK CHECK AND OPERATIONAL CHECK STILL REQUIRED. CONNECTOR PLUG LEFT UNPLUGGED AND COVERED FOR WIRING CHECKS. CHECKED WIRING BETWEEN HYD QTY MONITOR UNIT BENCH PLUG D2704A PINS B2, C4, A4, AND B4 TO L HYD QTY XMITER CON D38 PINS 7, 5, 3, AND 4. RESISTANCE ON EACH WIRE WAS APROX 5 OHMS AND SOLID WITH NO HUNTING. APPLIED MEGGER TO CHECK FOR SHORTS, PIN TO GRD AND PIN TO PIN ON EACH WIRE. NO SHORTS FOUND. REMOVED UPPER WING PANEL ABOVE PYLON AND SHOOK OUT WIRING AND FOUND NO FAULTS. REMOVED FWD PIT FWD BULKHEAD PANEL AND CHECKED D5364 CON. CK'D OK. AFTER SECURING CON D5364 AND MOVING WIRING THE L HYD INDICATION ON EICAS SCROLLED DOWN TO ZERO AND THEN BACK TO .87 A COUPLE OF TIMES. KEPT MOVING WIRING BUT COULD NOT GET TO FAULT AGAIN. ALSO, CHECKED WIRING FROM HYD MON TO BOTH EICAS COMPUTERS. RESISTANCE WAS 1.5 OHMS AND NO SHORTS TO GRD. LH A/P DISCONNECT DURREMOVED WIRE W390-011-20 AND RAN NEW WIRE REFERENCE SWPM 20-25-00. REQUIRES NEW TERMINATION.

Part: CONTROLLER — FAILED (NR 2) · airframe 125,443 hrs · 19,331 cycles

STATUS CABIN ALT AUTO 1 PERFORMED CABIN PRESS CONTROLLER BITE PROCEDURE. AC MOTOR FAULT LIGHT CAME ON. REF FIM 21-31 FAULT TREE 803. CABIN ALT AUTO 1 INOP, VERIFIED MANUAL MODE WORK REQUESTING FOR DEFERRAL. STATUS CABIN ALT AUTO 1 CABIN PRESSURE CONTROL SYSTEM INOPERATIVE. DEFERRED REF MEL 2131A APPLIED MEL 2131A. *DM* ADDED ACTUATOR, REF FIM 21-31 FAULT TREE 803. ADDED IF NEEDED. CABIN PRE3SSURE CONTROLLERS 1AND 2 REPLACED AND OUTFLOW VALVE MOTORS 1 AND 2 REPLACED. OPS CKS COMPLETED.

Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 125,367 hrs · 19,321 cycles

EPL FROM SEAT 30 INOP REMOVED AND REPLACED EPL LIGHT FROM SEAT 30F OPS CHECK GOOD, SYSTEM OK FOR SERVICE. REF CMM 25-21-53.

Part: LENS — BROKEN (ZONE 200) · airframe 125,367 hrs · 19,321 cycles

EPL LENS BROKEN FROM SEAT 49F IT WAS REMOVED AND REPLACED EPL LIGHT ,OPERATINAL TEST GOOD. ITEM OK FOR SERVICE. REF CMM 25-21-53.

Part: LENS — BROKEN (ZONE 200) · airframe 125,367 hrs · 19,321 cycles

34F EPL LENS BROKEN REMOVED AND REPLACED EPL REF CMM 25-21-53 OPS CHECK GOOD SYSTEM OK FOR SERVICE.

Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 125,367 hrs · 19,321 cycles

EPL FROM SEAT 33F INOP REMOVED AND REPLACED EPL LIGHT REF CMM 25-21-53 OPS CHECK GOOD SYSTEM OK FOR SERVICE.

Part: GIRT BAR — FOD (ZONE 800) · airframe 124,383 hrs · 19,193 cycles

DOOR 1R SLIDE WILL NOT ARM FOLLOWING FIM 52-11-FAULT TREE 804 FOUND DEBRIS ON BOTTOM OF GIRT BAR, REMOVED DEBRIS, DOOR ARMED AND DISARMED WITH EASE

Part: LAMP — BURNED OUT (ZONE 200) · airframe 124,288 hrs · 19,180 cycles

EMERGENCY LIGHTS OPERATIONAL CHECK {B767-33-3-7000} - DURING THE EXTERNAL OPERATIONAL CHECK FOUND OF THE DOOR 2 RH INOP. REMOVED AND REPLACED THE SLIDE AND OVERWING ESCAPE LIGHT LAMP REPLACEMENT AS PER AMM-TASK 33-51-06-902-082, POSITION DOOR 2RH, CHECKED OK PARTS USED: 76-3301-3-0005,QTY :1

Part: CONTROL PANEL — UNSERVICEABLE (CABIN) · airframe 122,781 hrs · 18,996 cycles

SMOKE AND FUMES IN FD WHEN TAKING RWY. AIRCRAFT BACK TO STAND AS SMIKE IN THE COCKPIT NOTICED - FOUND C B N6 OVERHEAD PANEL POPPED, WITH STRONG ELECTRICAL SMELL IN THE COCKPIT.SMELL NOTICED COMING OUT THE L BOTTOM OVHD PANEL, NEAR L RUNWAY TURNOFF LIGHT CTL SWITCH. PANEL REMOVED, FOUND L RUNWAY CTL LIGHT S1 SWITCH BURNED OUT, SWITCH BROKEN IN OFF POS. FOUND WIRE BUDDLE AND TERMINAL BLOCKS CONTAMINATED ON OTHER COMPONENT S.ASSY PN 233N3214-31 REQUIREDOR ASSY PN 233T3100-308 REQUIRED SDR FLAGGED LEFT RUNWAY TURNOFF LIGHT CONDITION CHECKED SATIS WITH WIRE BUDDLE SATIS, NO TRACE OF BURN AMM 33-42-00 CB C1276 CONDITION CHECKED SATIS, NO TRACE OF BURN AND OVERHEAD PANEL AREA CHECKED ALSO SATIS WITH NO BURN MARKS TWO PICS ADDED LEFT LIGHTNING CONTROL PANEL M10056 REPLACED AS PER AMM 33-11-00 REV142 AND SSM 33-13-01 REV77 CONTROL PANEL INDIVIDUAL FUNCTIONS TESTED SATIS NON ROTABLE PART REPLACED REPAIRABLE ITEM AS FOLLOW:- PN: 233N3214-31 UNSERVICEABLE PART QUARANTINED IN GVA STORE PENDING STSB INVESTIGATION AIRCRAFT RETURNED TO SERVICE

Part: PCB — MALFUNCTIONED (EFIS) · airframe 121,854 hrs · 18,879 cycles

CREW REPORTS LOW SPEED AMBER BAND ON CAPTAINS SIDE EFIS AIRSPEED TAPE FLUCTUATING AND 30KT SPLIT WITH FO. ALL MACH AIRSPEED INDICATORS OPS NML. TO BE DEFERRED IAW MEL 3422BS DEFERRED IAW MEL 3422BS CAPT EFIS SPEED TAPE AIRSPEED INDICATION(S) INOPERATIVE. DUPLICATE, SEE LP 8033935 ST AND INDICATIONS ARE OK ROTABLE PARTS CHANGE WAS INDICATED - T T # 1461610 SN OFF 4335 CIRCUIT, PRINTE OFF 75-2730-9-9001 4335 ON 75-2730-9-9001 3669 STALL WARNING MODULE REMOVED AND INSTALLED IAW AMM 27-32-01-024- 001 / AMM 27-32-01-424-016. OPS TEST OF STALL WARNING SYS PERFOR MED SATIS IAW AMM 27-32-00-715-04-003. WARNING ELECTRONICS UNIT WEU CARD MODULE TEST C/OUT SATIS IAWAMM 31-51-04-724-154. ALL TE ADD EMP:V919249

Part: CONTROL VALVE — DAMAGED (A/C PACK TEMP) · airframe 121,801 hrs · 18,870 cycles

R PACK OFF IN FLT UNABLE TO RESET HAD BOTH EICAS AND OVHD PAN EL PACK OFF LIGHT LOCKED FOR POSITIVE FIX FOUND PACK TEMP VALVE BAD WHILE PERFORMING RT PACK TEMP CONTROLLER BITE PER AMM 21-51 CONTROL VALVE FAULTED AGAIN. FOUND DAMAGE ON THE POSITION CONTROLLER PER AMM 21-51-14/401 AS PERCAUTION. OPS CHECK GOOD FAULT TREE 803 FOUND TEMP CONTROL VALVE AT FAULT. RESET ALL INDICATOR ON TEMP CONTROL VALVE. REMOVED AND NO FAULTS.A/C OK TO CONTINUE. QTY CHECKS GOOD RAN RT PACK AGAIN AND FOUND ON ECS PAGE TEMP REPLACED RT TEMP CONTROL VALVE PER 21-51-12/401 OPS CHECK CONTROL VALVE POSITION BLANK. PERFORMED CONTROLLER BITE AND TEMP GOOD NO FAULTS ALL CHECKS GOOD ALSO REPLACED RIGHT PACK TEMP.

Part: SWITCH — FAULTY (ELEC PNL P36) · airframe 121,680 hrs · 18,856 cycles

CREW REPORTED ON APPROACH TO MUC, FLT HAD TO ACP GO-AROUND. DURING FLAP AND GEAR RETRACTION, CTR HYD DEMAND PUMP LOW PRESSURE LIGHT AND EICAS DISPLAYED. CREW SELECTED PUMP TO "ON" POSITION, LOW PRESS LIGHT AND EICAS REMAINED DISPLAYED. REQ TOMC APRVL TO DEF M PROCEDURE C/W MEL 2911G WORKING ITEM FIM TASK 29-11 FAULT TREE 841 FOLLOWED. ADP OPERATES CORRECTLY ADP PRESS LIGHT REMAINS ON WHEN ADP RUNNING UNDER NO LOAD. UPON INSPECT OF SWITCH S28 AND CONNECTOR D464 PER WDM UNDER LOAD VIA OPERATION OF FLAPS, FLIGHT CONTROLS AND CENTER SYSTEM PRESSURE SHOWS 2900PSI VIA ECS PAGE AND CENTER 29-11-32-1. CONNECTOR D464 FOUND HEAVILY CONTAMINATED WITH SPEEDBRAKE. PRESSURE REMAINED WITHIN OPERATING LIMITS THROUGH SYSTEM PRESSURE LIGHT REMAINS OFF. PER SSM 29-00-05-101 PAGE HYDRAULIC FLUID. WILL REQUIRE A NEW SWITCH, PACKING AND OPERARION AND DID NOT DROP BELOW 2500PSI UNDER HEAVY LOAD 101 SUSPECT SWITCH S28 (AIR HYD PUMP PRESS) IS FAULTY CONNECTOR AIR HYD PUMP PRESS SWITCH (S28) REPLACED REF AMM BOTH CENTER SYSTEM AND ADP PRESS LIGHTS REMAINED OFF THROUGHOUT :1 29-11-19-404-029 AND CONNECTOR D464 REPLACED WITH REF TO SWPM OPERATION. ADP AND ALL INDICATIONS OPERATE NORMALLY REF MAIN SECTION 20-61. SWITCH 28 LEAK CHECKED WITH NO FINDINGS AND ADP CENTER HYDRAULIC SYSTEM TEST AMM 29-11-00-735-116 PARTS USED: OPERATED UNDER LOAD WITH NO PRESSURE FLUCTUATIONS OR DROPS. 40-0595-3-1976,QTY :1 76-2911-3-0139,QTY :1 75-7834-3-0008,QTY

Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 121,392 hrs · 18,820 cycles

B767-53-3-7034 - CABIN - STA 852 L/H WING CENTER SECTION MOST O/B PRESSURE DECK SURFACE FOUND CORRODED AS RED MARK - TRANSFER REFER NON-ROUTINE WO.2885899 AND ORIGINATED BY CENTER SECTION WING UPPER SKIN AT STA 852 LH MOST O/B STR-U17 TO PART 2 BEFORE 22MAR2025 FORM 44-0008 ITEM 1 TO ITEM 81 ACCOMPLIS STR-U18 REPAIRED AS PER EC/RA5714-01212 REV- PART 1 INTERIM HED BY REPAIR, ACCOMPLISH INSPECTION OF WING CENTER SECTION FWD UPPER PANEL (NO.2) AND U-17, U-18 STRINGER REPAIR PER ECRA5714-01212

Part: SKIN — CRACKED (BS 342 S20R) · airframe 121,392 hrs · 18,820 cycles

SUPPORT TASK - EA5315-01152 OP 002 , 1EA FASTENER HOLE FOUND CRACK ON BEAR STRAP AND 1EA FASTENER HOLE FOUND CRACK ON FUSELAGE SKIN AND BEAR STRAP ON RH SERVICE DOOR - TRANSFER REFER NON-ROUTINE WO.2843280 FUSELAGE SKIN REPAIRED ON RH SERVICE DOOR AFT LOWER CUTOUT STA AND FORM 44-0008 ITEM 1-32. AND 342, STR -20R AS PER SRM53-10-01-2R-1 REPAIR 1 FIG 201 THIS REPAIR IS A CATEGORY B REPAIR, SUPPLEMENTAL INSPECTIONS REQUIREMENTS REFER SRM53-10-01-2R-1 REPAIR 1 FIG 202 TABLE 202.

Part: SKIN — CRACKED (BS 1214 S37L) · airframe 121,392 hrs · 18,820 cycles

FUSELAGE LWR EXT SKIN BS 1214 S37L FOUND CRACKED. PERFORM INTERNAL HIGH FREQUENCY EDDY CURRENT (HFEC) INSPECTI THE REPAIR REFERENCING ECRA FIGURE 9. PART 3: PERMANENT REPAIR: ON OF THE SKIN AT THE CRITICAL FASTENER ROW ALONG THE EDGE OF PAR THE REPAIR ACCOMPLISHED IN PART 1 IS APPROVED AS PERMANENT T 1 DOUBLER PER 767 NDT MANUAL PART 6, 51-00-01 REF ECRA FIGURE PROVIDED THE REQUIRED REPEAT INSPECTIONS ARE ACCOMPLISHED. 9.

Part: STRINGER — CORRODED (BS 1540-1562) · corrosion level 2 · airframe 121,392 hrs · 18,820 cycles

AFT OF BULK CGO COMPT STA1540-1562 S38R FOUND CORROSION TRANSFER REF NO - ROUTINE WO.2907940. AFT OF BULK CGO COMPT STA 1540-1562 STRINGER S-38R REPAIRED AS PER SRM53-00-03-2R-2 REPAIR 2 FIG 201 AND REPAIR FASTENER LOCATIONS INSTALLED AS PER EC/RA 5300-03077 REV.

Part: SKIN — CRACKED (FUSELAGE) · airframe 121,392 hrs · 18,820 cycles

SUPPORT TASK - EA5315-01152 OP001, 1EA FASTENER HOLE FOUND CRACK ON FUS SKIN AND BEAR STRAP ON LH ENTRY DR. TRANSFER REF NON - ROUTINE WO.2843296 AND ORIG PAIR 1. SCUFF PLATE REMOVAL REQUIRED AS NECESSARY FOR INSPECTION IVERY OR 6000 MAXIMUM FLIGHT CYCLES FROM THE REPAIR INSTALLATION DY CURRENT (LFEC) PER NDT PART 6, 53-00-06, EXTERNAL VISUAL . INSPECTION THRESHOLD IS 37500 FLIGHT CYCLES AFTER AIRPLANE DEL , WHICHEVER OCCURS LATER. METHOD OF INSPECTION: LOW FREQUENCY ED REPAIR ACCOMPLISHED IAW 767 SRM 53-10-01-2R-1 REPAIR 1. SUPPLEME NTAL INSPECTIONS ARE REQUIRED PER SRM 53-10-01-2R-1 TABLE 202/RE REF SRM 53-10-01-2R-1 RPR1 TABLE 202 CATEGORY B REPAIR TOMC-APPROVAL FROM SC1ELBYC COMMENT INSPECTION REQUIREMENTS. RPR 1 ACCOMPLISHED. SUPPLEMENTAL INSPECTION REQUIRED 37,500 FLT CYCLES AFTER AIRPLANE DELIVERY OR 6000 MAX FLT CYCLES FROM REPAIR INSTALLATION WHICHEVER COMES LATER. REPEAT INSPECTION EVERY 3000 FLT CYCLES. CURRENT ACFT FLT CYCLES 18820. , HIGH FREQUENCY EDDY CURRENT (HFEC) PER NDT PART 6, 51-00-01. APPROVED DIP ITEM ATA # CORRECTED TO REFLECT 53-DIP REF. FIG 202. INSPECTION REQUIREMENTS SHEETS 1, 2, 3 AND 4 FOR INSPECTION DETAILS. APPROVED INSPECTIONS CREATED BY AUTODIP PENDING AIRCRAFT RECORDS AUDIT & UPDATE.

Part: STRINGER — CORRODED (BS 1540-1562) · corrosion level 2 · airframe 121,392 hrs · 18,820 cycles

AFT OF BULK CGO COMPT STA1540-1562 S39R FOUND CORROSION TRANSFER REF NON - ROUTINE WO.2907957. AFT OF BULK CGO COMPT STA1540-1562 STRINGER S39R REPAIRED IAW SRM53-00-03-2R-2 REPAIR2 FIG201 AND REPAIR FASTENER LOCATIONS INSTALLED IAW ECRA5300-03077 REV.

Part: BEAM — CRACKED (BS 325 LBL 13) · airframe 121,392 hrs · 18,820 cycles

1EA CRACK FOUND AT STA325 LBL13 FLR BEAM WEB. STA325 FLR BEAM WEB LBL13" CRACK AREA REPAIRED IAW ECRA 5315-01207 REV.

Part: FLOORBEAM — CORRODED (BS 325 LBL33-55) · corrosion level 2 · airframe 121,392 hrs · 18,820 cycles

B767-53-3-7062 CABIN -FWD ZONE FLR PNL P27 STA 325 LBL 33-55 FLR SUPPORT SURFACE FOUND CORRODED. FWD ZONE FLR PNL P27 STA325 LBL2"-LBL62" FLR BEAM UPR CHORD REPAIRED IAW SRM53-00-51-2R-1 REPAIR1 FIG201.

Part: FLOORBEAM — CORRODED (BS 1582 LBL 50) · corrosion level 2 · airframe 121,392 hrs · 18,820 cycles

B767-53-3-7079 CABIN - AFT GAL AREA FLR PNL P136 FLR SUPPORT STA 1582 LBL 50 SCREW HOLE CORRODED AS RED MARK. TRANSFER REF NR HX WO.2894650 AND ORIGINATED BY EMP V927004. CAB - AFT GAL AREA FLR PNL P136 FLR BEAM REPAIRED IAW SRM53-00-51-2R-1 REPAIR1 FIG201 JUST AT STA1582 BTW LBL45 AND LH MOST O/B WORK ACCOMP BY MECH V897471 AND INSP BY V898054 RII APPROVED BY HX202044

Part: PRESSURE BLKHD — DENTED (BS 1583) · airframe 121,392 hrs · 18,820 cycles

AFT PRESSURE BULKHEAD BS 1586 S35L-S36L FOUND DENTED. TRANSFER REF NON - ROUTINE WO.2955261.

Part: FRAME — CRACKED (BS 1809 S7-8R) · airframe 121,392 hrs · 18,820 cycles

BS 1809 RT FWD OUTER CHORD BTW STR 7R-8R FOUND 1EA CRACKED.

Part: SHUTOFF VALVE — FAILED (LT ENGINE) · airframe 120,378 hrs · 18,666 cycles

AIR RETURN FOR L ENG BLEED OFF/L PACK OFF PER IDT REQUIREMENTS, VERIFIED PROPER INSTALL OF E1 EEC PER AMM 73-21-04-404-016-N00. SLAVED NEW EEC RAN ENGINE, NO FIX, REINSTALLED ORIGINAL SERVICABLE EEC REF AMM 73-21-04-404-016-N00. FOLLOWED FIM 36-10 TASK 868, SWAPPED BLEED AIR CONTROL CARDS IN P50 PANEL M859 AND M860, RAN BOTH ENGINES, NO HELP. RETURNED CARDS TO ORIGINAL POSITIONS. ORDERED OVERHEAD SWITCH S4 IN BLEED AIR SUPPLY MODULE. FOUND PIN 5 WIRE HANGING BY A COUPLE OF STRANDS ON THE L ENG BLEED SWITCH. REPLACED INNER COMPONENTS FOR THE LH ENG BLEED SWITCH ON THE OVERHEAD RAN ENGINE, NO BLEED AIR PRESENT BUT WITH COWL ANTI ICE TURNED ON WE HAD A RISE IN EGT, SUSPECT BAD PRSOV. T/S PER FIM 36-10 TREE 876, IN BLOCK 1 NO VOLTAGE NOTED ON PINS 6 TO 7, DUE TO PREVIOUS SWAP OF L & R BLEED AIR CONTROL CARDS MORE T/S''ING ACCOMPLISHED PNEUMATIC HEALTH CHECK FOR LEFT ENG PRSOV REF AMM 36-00-22-705-001 STEP L. PRSOV FAILS TO OPEN WITH SUPPLY PRESSURE. REMOVED LEFT ENG PRSOV REF AMM 36-11-09-002-133-008. INSTALLED PRSOV REF AMM 36-11-09-402-164-008 UP TO STEP F.(11). INSTALLED FLEXIBLE SENSE LINE REF STEP F(16) AMM 36-11-09-402-164-008. REQD. SEE PIC. VALVE, SHUTOFF, OFF 76-3612-9-0002 1117 ON 76-3612-9-0002 0310 VALVE, SHUTOFF, OFF 76-3612-9-0002 1117 ON 0000 FINISHED INSTALLING PRSOV TO COUPLING, OPS CHECK & LEAKED CHECK GOOD PER REF AMM 36-11-09, NO FURTHER DEFECTS NOTED AT THIS TIME

Part: SHUTOFF VALVE — FAULTY (NR 1 ENGINE) · airframe 120,367 hrs · 18,664 cycles

PIREP CLIMBING UP OUT OF FL210 AUDIBLE LOUD BANG. LT ENG ROLLBACK FROM CLIMB THRUST, ROLLOFF TO THE LEFT. COMPLETED COMPRESSOR STALL CHECKLIST. NO FAULT DURING CHECKLIST. PER POWERPLANT ENGINEERING, NEED TO PERFORM FIM 71-05 TREE 803. PERFORM #1 ENG HPC STAGE 5,6,10,HPT 1,2,LPT STAGE 3 AND 6 WITH NO LIMIT DEFECT NOTED REF AMM 72-00-00-216-011-N01,72-00-00-216- 2-00-00-216-017-N01,72-00-00-216-018-N01. BORESCOPE INSPECTION REF INFO AMM 72-00-00-216-011-N01, 72-00-00-216-014-N01, 72-00-00-216-015-N01, 72-00-00-216-017-N01, 72-00-00-216-018-N01. PERFORMED FIM 71-05 FAULT TREE 803. COMPLETED BLOCKS 1 (YES) 2 (NO) 3 (YES) 4 (NO) 5 (YES) 6 (NO) 7 (NO) 8 (NO) 9 (NO). PLEASE CONTINUE WITH BLOCK 10. REF LP 5964724 FOR LEFT PIMU MESSAGES. ADD EMP:U242424,U393544 REMOVED AND REPLACED #1 ENGINE HPSOV REF AMM 36-11-07-004-032-002 UP TO PARAGRAPH G(1) OF THE INSTALLATION AMM 36-11-07-424-014-002 OPERATIONAL CHECKS AND LEAK CHECKS NEED TO BE ACCOMPLISHED. PARTS USED: 76-3611-9-0001,QTY :1 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1508557 SN OFF 2184 REMOVED AND REPLACED ENG #1 PRESSURE REGULATING SHUTOFF VALVE (PRSOV) REFERENCE AMM 36-11-09-402-164-00 COMPLIED WITH FIM 71-05 FAULT TREE 803 BLOCK 11 , TEST 4 ENG POWER & ACCEL/DECEL TEST. ALL CKS WITHIN LIMITS.

Part: FUEL CAP — MISSING (LH WING) · airframe 120,203 hrs · 18,641 cycles

FUEL RECEPTACLE CAP LEFT MISSING. MEL 2821J REQUESTED. FUEL RECEPTACLE CAP LEFT PLACED ON MAL 2821J.DDP C/W. FUEL RECEPTACLE CAP LEFT MISSING. DEFERRED REF MEL 2821J FUEL CAP LANYARD ATTACHING BRACKET BROKEN. AIRPLANE ARRIVED WITH TWO RECTABLE CAPS. THIS CLEARS MEL 2821J.

Part: LAVATORY — INOPERATIVE (ALL LAVS) · airframe 117,996 hrs · 18,342 cycles

ALL LAVS WILL NOT FLUSH ON ARRIVAL DISCOVERED BOTH TANKS FULLL AND FOUL INDICATION FLAGGED. DUMPED THE TANKS LAVS CAME ONLINE IMMEDIATELY.

Part: HINGE — MISSING (LT FWD NG) · airframe 117,918 hrs · 18,331 cycles

PDA 3 LEFT FWD NOSEGEAR DOOR HINGE COVER MISSING OK, ITEM IS PREVIOUSLY DOCUMENTED SEECDL.

Part: CAP — MISSING (LT FUEL CELL) · airframe 117,521 hrs · 18,273 cycles

DURING PRE-FUELING, FOUND LEFT FUEL TANK CAP MISSING. INSTALLED FUELING PANEL LEFT FUEL TANK CAP.

Part: BRAKE — BROKEN (#5 BRAKE) · airframe 115,014 hrs · 17,946 cycles

PDA 2 DURING ETOPS CHECK FOUND #5 BRAKE DAMAGED. BOTH PINS MISSING AND PIN HOUSING BENT AND AT LEAST ONE ROTOR MISSING (DAMAGED). DUE TO PDA LOG PAGE, NOTIFIED LINE MX CONTROL THAT A SDR FLAG MUST BE SET AND ESFR NEEDS TO BE FILED..

Part: SKIN — DAMAGED (LOWER FUSELAGE) · airframe 114,603 hrs · 17,874 cycles

LOWER FUSELAGE STA 1488 AT STR34L DAMAGED BY CATERING TRUCK C/W HFEC REF. NDT PART 6-51-00-19. NO CRACKS NOTED. VERIFIED MATERIAL. OK TO CONTINUE. VERIFIED FILLER MATERIAL. OK TO CONTINUE. INCORRECT MATERIAL NOTED. REMOVED DAMAGED AREA IN REF TO SRM 53-00-01-2R-1 VERIFIED MATERIAL TO BE USED FOR DOUBLER AS .120 - 2024T3 VERIFIED MATERIAL TO BE USED FOR DOUBLER AS .100 - 2024T3 VERIFIED MATERIAL TO BE USED FOR DOUBLER AS .100 - 2024T3 VERIFIED FILLER MATERIAL AS .100-2024T3 PO#9495433 REF SRM PO#6498447 IN REF TO SRM 53-00-01-2R-1 PO#9495433 IN REF TO SRM 53-00-01-2R-1 PO#9495433 IN REF TO SRM 53-00-01-2R-14 53-00-01-2R-1 FABRICATED DOUBLER AND FILLER, TREATED AND PRIMED. INSTALLED C/W RII REQUIREMENTS REF GMM 09-25-05. REPAIR IS INSTALLED. OK REPAIR WASHERS. REF SRM 53-00-01-2R REPAIR 1. OK TO REPAIR TO CONTINUE. DOUBLER/ FILLER. FABRICATED DOUBLER AND FILLER, TREATED AND PRIMED. INSTALLED INSTALLED DOUBLER/FILLER REPAIR, SEALED FILLER AND CIC AREA. REF REPAIR WASHERS. REF SRM 53-00-01-2R REPAIR 1. OK TO REPAIR SRM 53-00-01-2R-1 REPAIR 1. STEP 12 THROUGH STEP 15. DOUBLER/ FILLER. COMPLETED INSTALLATION OF DOUBLER/ FILLER REPAIR AT LWR FUSELAGE STA. 1488, STR-34L REF SRM 53-00-2R-1 REPAIR 1. SEE LOG 8152752 FOR DIP. VERIFIED REPAIR IS COMPLETE REF. SRM 53-00-2R-1 REPAIR 1.

Part: SKIN — DAMAGED (SKIN) · airframe 114,603 hrs · 17,874 cycles

UPPER FUSELAGE STA1488 AT STR24L DAMAGE BY CATERING TRUCK C/W HFEC REF. NDT PART 6-51-00-19. NO CRACKS NOTED. VERIFIED MATERIAL. OK TO CONTINUE. VERIFIED FILLER MATERIAL. OK TO CONTINUE. INCORRECT MATERIAL NOTED. REMOVED DAMAGED AREA IN REF TO SRM 53-00-01-2R-14 VERIFIED MATERIAL TO BE USED FOR DOUBLER AS .120 - 2024T3 VERIFIED MATERIAL TO BE USED FOR DOUBLER AS .100 - 2024T3 VERIFIED FILLER MATERIAL AS .100-2024T3 PO# 9495433 IN REF TO PO#6498447 IN REF TO SRM 53-00-01-2R-14 PO#9495433 IN REF TO SRM 53-00-01-2R-1 SRM 53-00-01-2R-14 VERIFIED DOUBLER AND FILLER, OK TO TREAT, PRIME AND INSTALL. C/W RII REQUIREMENTS REF GMM 09-25-05. REPAIR IS INSTALLED. OK TO CONTINUE. FABRICATED DOUBLER AND FILLER, OK TO TREAT, PRIME AND INSTALL IN INSTALLED DOUBLER/FILLER, SEALLED FILLER AND CIC AREA. REF SRM REF TO SRM 53-00-01-2R-14 53-00-01-2R-14 REPAIR 14. STEP 12 THROUGH 15. COMPLETED INSTALLATION OF DOUBLER/ FILLER REPAIR AT UPPER FUSELAGE STA. 1488, STR-24L REF SRM 53-00-01-2R-14 REPAIR 14. SEE LOG 8152796 FOR DIP. VERIFIED REPAIR COMPLETE REF. SRM 53-00-01-2R-14 REPAIR 14.

Part: SMOKE DETECTOR — FAILED (FWD CARGO) · airframe 114,392 hrs · 17,830 cycles

CARGO DET AIR STATUS STATUS MESSAGE "CARGO DET AIR" WILL NOT ERASE. COMPLIED WITH MEL VERIFED FAULT "FWD DET FAN" SEE PHOTO. CARD 2616E NOC DESK: 767 NAME: DM DATE: 05-FEB-22- FWD DET FAN FAULTED.. FWD CARGO COMPARTMENT REMAIN EMPTY. SEE LOG PAGE 7944671. LMC TO REPLACE SWITCH AND RELAY, REF SSM26-16-01 AND FIM 26-16 TASK 814. REPLACED BOTH FWD CARGO SMOKE DETECTOR BLOWERS REF AMM 26-16-02. BREAKER IS PULLED, BUT WILL NOT TURN ON. CHECKED FOR POWER AND SUSPECT BAD BLOWER FROM STOCK. NO FIX, MESSAGE REMAINS. BLOWER #1 SHOULD TURN ON WHEN BLOWER #2 GROUND ON CANNON PLUG, AND FOUND NO DEFECTS. MORE T/S REQUIRED. REF LOG PAGE 7944671 FOR REMOVAL AND REPLACEMENT OF SMOKE DETECTOR PLENUM PRESSURE SWITCH, AND RELAY K331. REMOVED AND SAMPLE VACUUM TUBING BETWEEN SMOKE DETECTOR AND MULTIPLE TUBES VACUUM. THE OTHERS DID NOT. ALSO MAYBE THE GREEN CHAMBER BETWEEN ON THE CARGO CEILING. TWO TUBES IN FWD CARGO DID HAVE A LITTLE SMOKE DECTORS AND BLOWERS. O REMOVED AND REPLACED K333. ELECTRICAL CHECKED GOOD. WITH BLOWER 2 WORKING STILL HAVE MESSAGE, CARGO DET AIR. SUSPECT BLOCKAGE IN PERFORMED CLEANING OF SMOKE DETECTORS TUBING IN FWD CARGO REF 26-16-00. CONFIRMED BOTH SMOKE DETECTOR BLOWERS FUNCTION PER AMM 26-16-02. MESSAGE CLEARED, NO FURTHER DEFECTS.

Part: CIRCUIT CARD — POWER LOSS (NA) · airframe 114,364 hrs · 17,824 cycles

CARGO DET AIR STATUS POWER DROPPED CARGO DET AIR FWD MEL 2616E WILL CLEAR AFTER RESET RESET CBS ON P35 PANEL. RESET RELAY K331. MSG CLEARED. PER LP 7945651 ON MEL.

Part: FITTING — CRACKED (LH UNDERWING) · airframe 114,123 hrs · 17,775 cycles

AD 2012-15-12, EA 5710-02220 REV.D OP 003 LH UNDERWING LONGERON FITTING TENSION BOLT HOLE INSP FOUND 3EA CRACKS AT 1ST LAYER COUNT FROM AFT TRANSFER REF. NON-ROUTINE ZGY511880 & ORIGINATED BY EMP V924733 RII APPROVED LH UNDERWING LONGERON FITTING (BATHTUB FITTING) INTERIM REPAIRED PER ECRA 5710-02789 REV ORIG PART 1 ITEM 1 WORK ACCOMPLISHED BY MECHANIC V897532 INSPECTED BY V896375 ADD EMP:V897532 ACCOMPLISH A PERMANENT REPAIR AS PER LATEST REVISION OF ECRA 5710-02789 ON OR BEFORE 24DEC22. ALSO REF ELB 7704043 DUP W-U. PER ECRA 5710-02789, INITIATE A DTA DIP TO "ACCOMPLISH A TOMC-APPROVAL FROM SC1ELBYC COMMENT PERMANENT REPAIR AS PER LATEST REVISION OF EC5710-02789 PART 3 ON OR BEFORE DECEMBER 24, 2022." QC REVIEWED QC REVIEWED INSPECTIONS CREATED BY AUTODIP PENDING AIRCRAFT RECORDS AUDIT & UPDATE.

Part: STRINGER — CRACKED (STA 1629-1654) · airframe 114,123 hrs · 17,775 cycles

STA 1629-1654.5 STR 14AR FOUND 3 EA CRACKS WHILE ACCOMPLISHING EA 5380-01178 OPS 002. REF TABLE 202 REPAIR 7 AND FIG 202 REPAIR 7 DETAIL XIV FOR FLIGHT CYCLES FROM THE REPAIR INSTALLATION, WHICHEVER COME FIRST REINSPECT REQUIREMENTS. IQ THRESHOLD 37500 FLT CYCLES OR 7500 CURRENT PTT 114123 PTC 17775. REF LOG PAGE 7703883 FOR REPAIR DETAIL. REPAIRED IAW SRM 53-80-01-2R-7 REPAIR 7 DETAIL VII FIG 201. CAT B REPAIR. REF SRM 53-80-01-2R-7: INSPECTION THRESHOLD IS 37500 FLIGHT TOMC-APPROVAL FROM SC1ELBYC COMMENT CYCLES AFTER AIRPLANE DELIVERY OR WITHIN 7500 FLIGHT CYCLES FROM REPAIR INSTALLATION, WHICHEVER COMES LAST. REPEAT INSPECTIONS REQUIRED BEFORE EVERY 7500 FLIGHT CYCLES DUE TO CATEGORY B REPAIR PER SRM TABLE 202. QC REVIEWED QC REVIEWED INSPECTIONS CREATED BY AUTODIP PENDING AIRCRAFT RECORDS AUDIT & UPDATE.

Part: STRINGER — CRACKED (LH LONGERON FIT) · airframe 114,123 hrs · 17,775 cycles

AD 2012-15-12, SUPPORT TASK - EA 5710-02220 OP 01 - LH LONGERON FITTING FOUND 1EA CRACK RUNNING AFT APPROX 7/8" IN LENGTH TRANSFER REF. HX NON-ROUTINE LP 9130257 & ORIGINATED BY EMP V924 735 LH LONGERON FTG REPLACED PER EA 5710-02220 REV D OP3 AND OP7 ACCOMPLISHED WORK DETAIL REFER SEQ 1610 AND 1602.ATTACHED FORM 44-0008 ITEM 1 ACCOMPLISHED WORK ACCOMPLISHED BY MECHANIC V897470 INSPECTED BY V896375 ADD EMP:V896375 RII BY HX146276,APPROVED

Part: LIGHT — INOPERATIVE (FLIGHT DECK) · airframe 114,123 hrs · 17,775 cycles

B767-33-3-7000 FLT DECK EMER EXIT LT INOP TRANSFER REF. NON-ROUTINE ZGY512623 & ORIGINATED BY EMP V920570 FLT DECK EMER EXIT LT ASSY REPLACED AND CARRIED OUT INSTALLATION TEST RESULT NORMAL PER AMM 33-51-01 WORK ACCOMPLISHED BY MECHANIC V898127 INSPECTED BY V898561 ADD EMP:V898127 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1922752 SN OFF 8254 IPC REFERENCE # LIGHT, EMERGENC OFF 76-3350-9-9001 8254 ON 76-3350-9-9001 0108

Part: BATTERY — INOPERATIVE (SEAT 21-23) · airframe 114,123 hrs · 17,775 cycles

B767-33-3-7002 SEAT 21 TO 23 DEF EMER LIGHT FOUND DIM TRANSFER REF. NON-ROUTINE ZGY512680 & ORIGINATED BY EMP V920574 SEAT 21 TO 23 LK EMER POWER SUPPLY (M1209) REPLACED AS PER AMM 33-51-07 AND TEST NORMAL AS PER AMM 33-51-07 WORK ACCOMPLISHED BY MECHANIC V934246 INSPECTED BY V896985 ADD EMP:V896985

Part: BATTERY — FAILED (M9047) · airframe 114,123 hrs · 17,775 cycles

B767-33-3-7002 - EMERGENCY BATTERY PACK M9047 SELF TEST FAIL TRANSFER REF. NON-ROUTINE ZGY512672 & ORIGINATED BY EMP V897802 EMERGENCY POWER SUPPLY CHARGER REPLACED AND INSTALLATION TEST NORMAL IAW AMM 33-51-07 WORK ACCOMPLISHED BY MECHANIC V920595 INSPECTED BY V897802 ADD EMP:V897802

Part: CHARGER — INOPERATIVE (OFF-WING) · airframe 114,123 hrs · 17,775 cycles

TRANSFER REF. NON-ROUTINE ZGY502632 & ORIGINATED BY EMP V897815 B767-33-3-7000 CABIN OFF-WING SECTION EMER EXIT SIGN NOT ILLUMIN ATED BATTERY CHARGER M1209 REPLACED AND TEST FOUND NORMAL IAW AMM 33- 51-07

Part: ANGLE — CRACKED (STA1809) · airframe 114,123 hrs · 17,775 cycles

AD 2005-11-02 - SUPPORT TASK EA 5300-01600 REV.A OP 01, LH 1809 BHD 1EA HOLE FOUND CRACK ON FWD OUTER CHORD LAYER TRANSFER REF. HX NON-ROUTINE LP 9130608 & ORIGINATED BY EMP V913 608 LH STA1809 BHD FWD OUTER CHORD REPAIRED AS PER EA5300-01600 REV A OP2(SEQ 1616) WORK ACCOMPLISHED BY MECHANIC V897381 INSPECTED BY V896853 ADD EMP:V896853 RII BY HX 199407,APPROVED ADD EMP:V897381

Part: PANEL — CRACKED (LH 809) · airframe 114,123 hrs · 17,775 cycles

AD 2005-11-02 - SUPPORT TASK EA 5300-01600 REV.A OP 01, LH 1809 BHD 1EA HOLE FOUND CRACK ON FWD OUTER CHORD LAYER TRANSFER REF. HX NON-ROUTINE LP 9130608 & ORIGINATED BY EMP V913 608 LH STA1809 BHD FWD OUTER CHORD REPAIRED AS PER EA5300-01600 REV A OP2(SEQ 1616) WORK ACCOMPLISHED BY MECHANIC V897381 INSPECTED BY V896853 ADD EMP:V896853 RII BY HX 199407,APPROVED ADD EMP:V897381

Part: STATUS MESSAGE — FALSE ACTIVATION (LT SHUTOFF VALVE) · airframe 113,327 hrs · 17,596 cycles

L ENG HPSOV STATUS MSG MSG EVIDENT ONLY ON FINAL TAXI TO GATE. NO CURRENT MSG FAULT DISPLAYED.

Part: SHUTOFF VALVE — FAILED (BLEED SYSTEM) · airframe 113,324 hrs · 17,595 cycles

WITH #1 ENG AT IDLE AND LEFT BLEED SWITCH OFF, HAD L HPSOV EICAS MSG AND BLEED LIGHT ON. REPLACED #1 ENG HPSOV REF MM 36-11-07-424-014-002. ACCOMPLISHED POWER RUN, OPS CHECK OK. ADD EMP:U71932 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1066459 SN OFF 1139 IPC REFERENCE # IPC36-11-07-02 VALVE, SHUTOFF, OFF 76-3611-9-0001 1139 ON 76-3611-9-0001 2184

Part: SKIN — DAMAGED (FWD SERV DOOR) · airframe 112,580 hrs · 17,446 cycles

GENERATING ITEM: 63-0600-102109 /// 63-0600-1-2109 FWD SERVICE DOOR EXTERNAL SKIN HAS A BLEND OUT AT S16R MARKED. REF AMES NR 0231. BLEND OUT ON DOOR FOUND TO BE OUT OF LIMITS IAW B767 SRM 52-10-01 FIG 101 DETAIL III. REPAIRED DAMAGED AREA IAW B767 SRM 52-10-01 REPAIR G.INSPECTED BY INSP 51. ADD EMP:V921404

Part: COFFEEMAKER — ODOR (RT FWD GALLEY) · airframe 107,856 hrs · 16,785 cycles

CREW REPORTED FLT ATTD HEARD LOUD POP FROM AFT SIDE OF RIGHT FWD GALLEY, FOLLOWED BY A BURNT ELECTRICAL SMELL. NO VISIBLE SMOKE OBSERVED. NO CB''S FOUND POPPED. CAPT PULLED CB''S FOR COFFEE MAKERS AND WARMER. SMELL QUICKLY DISSIPATED. FORM FOR FLT CREW TO COMPLETE AND FAX BACK TO TOMC. UPDATED MAA CODE FIX USING VENDOR MAA SCREEN PLEASE CONTACT TOMC. MAINT MUST MEET ACFT WITH SMOKE ODOR MAC RELATED WORK ORDER 000000001670087 AND PRTR MAC METER INITIATED FOR REMOVED COFFEEMAKERS 208 AND 209,CHKD CONNECTORS, NO DMG FOUND. CKD AREA WIRING,NO DMG FOUND. COMPLETED CHECK OF AREA PER MM05-51-56. NOTHING ABNORMAL. UNABLE TO DETERMINE WHICH COFFEE MAKER WAS SUSPECT DUE TO CLOSE PROXIMITY, INOPED COFFEEMKRS 208/ 209 TO BE REPLACED REFMEL 2520NC REMOVED COFFEEMAKERS 208 AND 209,CHKD CONNECTORS, NO DMG FOUND. CKD AREA WIRING,NO DMG FOUND. COMPLETED CHECK OF AREA PER MM05-51-56. NOTHING ABNORMAL. UNABLE TO DETERMINE WHICH COFFEE MAKER WAS SUSPECT DUE TO CLOSE PROXIMITY, INOPED COFFEEMKRS 208 209 TO BE REPLACED REFMEL 2520NC . MEL DDP ACCOMPLISHED DEFERRED DIRECTLY BY TOMC REMOVED AND REPLACED FWD GALLEY C/M #208 REF TO LOG#8397662 AND REMOVED AND REPLACED C/M #209. OPS CHK GOOD. MEL REMOVED. ROTABLE PARTS CHANGE WAS INDICATED - TT # 1202919 SN OFF 0199 COFFEEMAKER, IN OFF 31-2534-9-0001 0199 ON 31-2534-9-0001 0338

Part: COFFEEMAKER — ODOR (RT FWD GALLEY) · airframe 107,856 hrs · 16,785 cycles

CREW REPORTED FLT ATTD HEARD LOUD POP FROM AFT SIDE OF RIGHT FWD GALLEY, FOLLOWED BY A BURNT ELECTRICAL SMELL. NO VISIBLE SMOKE OBSERVED. NO CB''S FOUND POPPED. CAPT PULLED CB''S FOR COFFEE MAKERS AND WARMER. SMELL QUICKLY DISSIPATED. FORM FOR FLT CREW TO COMPLETE AND FAX BACK TO TOMC. UPDATED MAA CODE FIX USING VENDOR MAA SCREEN PLEASE CONTACT TOMC. MAINT MUST MEET ACFT WITH SMOKE ODOR MAC RELATED WORK ORDER 000000001670087 AND PRTR MAC METER INITIATED FOR REMOVED COFFEEMAKERS 208 AND 209,CHKD CONNECTORS, NO DMG FOUND. CKD AREA WIRING,NO DMG FOUND. COMPLETED CHECK OF AREA PER MM05-51-56. NOTHING ABNORMAL. UNABLE TO DETERMINE WHICH COFFEE MAKER WAS SUSPECT DUE TO CLOSE PROXIMITY, INOPED COFFEEMKRS 208/ 209 TO BE REPLACED REFMEL 2520NC REMOVED COFFEEMAKERS 208 AND 209,CHKD CONNECTORS, NO DMG FOUND. CKD AREA WIRING,NO DMG FOUND. COMPLETED CHECK OF AREA PER MM05-51-56. NOTHING ABNORMAL. UNABLE TO DETERMINE WHICH COFFEE MAKER WAS SUSPECT DUE TO CLOSE PROXIMITY, INOPED COFFEEMKRS 208 209 TO BE REPLACED REFMEL 2520NC . MEL DDP ACCOMPLISHED DEFERRED DIRECTLY BY TOMC REMOVED AND REPLACED FWD GALLEY C/M #208 REF TO LOG#8397662 AND REMOVED AND REPLACED C/M #209. OPS CHK GOOD. MEL REMOVED. ROTABLE PARTS CHANGE WAS INDICATED - TT # 1202919 SN OFF 0199 COFFEEMAKER, IN OFF 31-2534-9-0001 0199 ON 31-2534-9-0001 0338

Part: CIRCUIT BREAKER — FAILED · airframe 106,510 hrs · 16,611 cycles

LOST SATCOM, LT & RT AUTOPILOTS, UPPER EICAS, SATCOM AND ACARS. WHILE ATTEMPTING TO RESTORE SYSTEMS IAW QRH 160.3, NOTICED THE CIRCUIT BREAKER 115V AC BUSS L SECT 2, ON THE P6-3 PANEL WAS TRIPPED. THE CIRCUIT BREAKER C308 AND ASSOCIATED WIRI IAW AMM 20-60-01-862-001, CIRCUIT BREAKER RESET, INSPECTION AND THE CIRCUIT BREAKER C308 WAS REMOVED AND REPLACED IAW SWPM 20-30-00. DUE TO POOR CONDITION AND DAMAGE TO THE CIRCUIT BREAKER. LEFT ENGINE RUNS CARRIED OUT TO CONFIRM COMMAND OF ASSOCIATED SYSTEMS. L, C, R, AUTOPILOTS ENGAGED, NO ISSUES AND FOLLOWED COMMANDS AS EXPECTED. AUTOPILOT INTERFACE CHECKED GOOD, NO FURTHER PROBLEMS NOTED WITH CB C308. GOOD FOR FURTHER SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 105,808 hrs · 16,520 cycles

CABIN LT STA 1506-1516 LBL 82 FLOOR SUPPORT BEAM CORROSION. ACCOMPLISHED AN INTERIM REPAIR PER ECRA 5315-01106.

Part: FRAME — CRACKED (BS 763) · airframe 105,808 hrs · 16,520 cycles

MAIN DECK, BS 763, STRINGER 2R, FRAME WAS FOUND CRACKED. THE FRAME WAS REPAIRED IAW ECRA 5311-01959, REV -.

Part: SKIN — CORRODED (BS 1197) · airframe 105,808 hrs · 16,520 cycles

BS 1197+133, STRINGER 20L, INTERIOR SKIN WAS FOUND CORRODED. THE SKIN WAS REPAIRED IAW SRM 53-00-01, REPAIR 29, FIG 201, DETAIL I.

Part: FLOORBEAM — CORRODED (BS 1562) · airframe 105,808 hrs · 16,520 cycles

BS 1562, LBL 55 - 77, FLOORBEAM UPPER TEE CORRODED. THE FLOORBEAM WAS REPAIRED IAW SRM 53-00-51, REPAIR 1, FIG 201, DETAIL I.

Part: FLOORBEAM — CORRODED (BS 304) · airframe 105,808 hrs · 16,520 cycles

BS 304 FLOORBEAM FOUND CORRODED BETWEEN LBL 16 TO LBL 45. THE FLOORBEAM WAS REPAIRED IAW SRM 53-00-01, REPAIR 1, FIG 201.

Part: SHEAR TIE — CORRODED (BS 1417) · airframe 105,808 hrs · 16,520 cycles

BS 1417 STRINGERS 19 - 20L SHEAR TIE WAS FOUND CORRODED. THE SHEAR TIE WAS REPLACED IAW SRM 51-10-02, AND SRM 51-40-02.

Part: FRAME — CORRODED (BS 1219) · airframe 105,808 hrs · 16,520 cycles

FRAME EDGE, BS 1219, WL 218 FOUND CORRODED THE FRAME WAS REPAIRED IAW SRM 53-00-07, REPAIR 1, FIG 201, DETAIL III.

Part: INDICATOR — FAULTY (COCKPIT) · airframe 105,334 hrs · 16,451 cycles

ACFT ABORTED TAKEOFF AT 110 KTS DUE TO NO AIRSPEED INDICATION ON CAPT SIDE. REPLACED CAPTS MACH A/S IND IAW AMM 34-13-02, OP CKS GOOD. ROTABLE PARTS CHANGE WAS INDICATED. TT 1304760 SN OFF 1611 INDICATOR, MACH OFF 75-3111-9-0001 1611 ON 75-3111-9-0001 4055.

Part: CHILLER — FAILED (FWD GALLEY) · airframe 102,915 hrs · 16,098 cycles

AN ELECTRICAL ODOR OCCURED SHORTLY AFTER HEARING A BANGING NOISE FROM BELOW THE FORWARD GALLEY FLOOR AREA. THE CABIN CREW ALSO DESCRIBED HEARING A NOISE SIMILIAR TO SOMETHING WINDING DOWN. AFTER DOWN POWERING THE FWD GALLEY EQUIPMENT, THE ODOR DISIPATED. THE ODOR SEEMS TO BE PRESENT INSIDE THE FWD GALLEY CARTS. SUSPECT A CHILLER FAILED AND CAUSED THE NOISE AND ODOR. R & R FWD GALLEY CHILLER IAW AMM 25-33-01-004-082, AND AMM 25-33-01-404-152. OPS CHECKED GOOD IAW AMM 25-33-00-206-001.

Part: OVEN — SPARKS (GALLEY) · airframe 102,446 hrs · 16,025 cycles

MID CABIN OVEN R12 HAD SMOKE AND SPARKS WHEN TURNED ON. REMOVED AND REPLACED OVEN R12, IAW MM 25-31-00, OPS CHECK GOOD.

Part: LENS — MISSING (CABIN) · airframe 101,587 hrs · 15,895 cycles

LENS IS MISSING FROM EMERGENCY LIGHT ON CEILING AT 32B. REPLACED LENS.

Part: LIGHT — NOT SEATED (COCKPIT) · airframe 100,969 hrs · 15,810 cycles

COCKPIT EMERGENCY LIGHT OVER FLIGHT DECK ENTRY DOOR STAY ON WITH POWER OFF. RESEATED LIGHT REF 33 51 00.

Part: STRUCTURE — CORRODED (BS 955) · airframe 100,195 hrs · 15,698 cycles

CORROSION AT BS 955 BL 0 . REPAIRED IAW ECRA 5310-07009 PER 5100-02100-3.

Part: DECK PLATE — CORRODED (FUSELAGE) · airframe 100,195 hrs · 15,698 cycles

CORROSION AT BS 955 FWD DECK BL0-RBL/LBL 2. REPAIRED BS 955 FWD DECK BL0-RBL/LBL 2 IAW ECRA 5710-0258

Part: SKIN — CRACKED (NR 2 PYLON) · airframe 100,195 hrs · 15,698 cycles

NR 2 PYLON LT SIDE ACCESS PANEL OPENING 446BL, SKIN CRACKED AT UPPER FWD CORNER. REPAIRED IAW SRM 54-53-01 FIG 201,

Part: SLIDE — DEPARTED (OVERWING EXIT) · airframe 97,602 hrs · 15,334 cycles

IMMEDIATELY AFTER TAKEOFF CREW REPORTED RT WING SLIDE DEPLOYED & DEPARTED AIRPLANE. DECLARED EMER & RETURNED. INSTALLED RT OVERWING SLIDE IAW AMM ECRA 5300-02305A CREATED FOR INSPECTION & ATTACHED TO TOCS LOG FOR DAMAGE EVALUATION.

Part: DOOR — OPEN (EVAC SLIDE) · airframe 97,602 hrs · 15,334 cycles

LEFT OFF WING SLIDE COMPARTMENT DOORS CAME OPEN DURING RE-ACTIVATION PROCEDURE. INSTALL LT OVERWING SLIDE IAW AMM & SLIDE COMPARTMENT DOORS.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 97,602 hrs · 15,334 cycles

SUPPORT TASK, EMER LIGHTS ASSOCIATED WITH BATTERY PACK M99082 ARE INOPERATIVE. R & R EMERGENCY BATTERY PACK M99082. TESTED NORMAL IAW AMM 33-51-07.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 95,442 hrs · 15,031 cycles

EICAS MSG LE SLAT ASYM DISPLAYED, LE LIGHT ILLUMINATED WITH THE FLAP LEVER IN 1. BOTH FLAP POINTERS ARE CORRECT. CREW REPORTED POSSIBLE WAKE TURBULENCE ENCOUNTER, SEE SERVICE TIP 27-88-01 PG 901. PSEU BITE SHOWED LE OTBD ASYM MSG 27-81021, PROX BITE FAILED RT SLAT NR 8 INBD SENSOR 304. RAISED SLATS IN ALT MODE, MSG CLEARED, OPERATED FLAPS UP & DOWN SEVERAL TIMES. ALL OPERATIONS GOOD, CHECKED 304 SENSOR ADJUSTMENT IAW 27-88-01 ALL GOOD.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 95,442 hrs · 15,031 cycles

ON SHORT FINAL, LE DISAGREE, MISSED APPROACH. EICAS LE SLAT ASYM DISPLAYED. CREW REPORTED POSSIBLE WAKE TURBULENCE ENCOUNTER. PSEU BITE SHOWED LE OTBD ASYM MSG 27-81021. PROX BITE FAILED RT SLAT NR 8 INBD SENSOR 304. RAISED SLATS IN ALT MODE, MSG CLEARED. OPERATED FLAPS UP & DOWN SEVERAL TIMES, ALL OPERATIONS GOOD. CHECKED 304 SENSOR ADJUSTMENT IAW 27-88-01, ALL GOOD.

Part: STRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 95,414 hrs · 15,025 cycles

FAILSAFE STRAP HAS CORROSION AT BS 1560, RBL 10 - LBL 10. REPLACED FAILSAFE STRAP IAW SRM 51-40-02.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 95,414 hrs · 15,025 cycles

FORWARD CARGO FLOORBEAM WEB CRACKED AT BS 676 & LBL 22. REMOVED DAMAGE, INSTALLED REINFORCING DOUBLER REPAIR IAW ECRA 5330-05251.

Part: SKIN — PUNCTURED (FUSELAGE) · airframe 95,414 hrs · 15,025 cycles

MAIN CABIN BS 1373, STRINGER 17L IS PUNCTURED. REMOVED DAMAGE & INSTALLED STRINGER SPLICE REPAIR IAW SRM 53-00-03 FIG 201 REPAIR 1 DETAIL II.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 95,414 hrs · 15,025 cycles

AFT CARGO COMPARTMENT BS 1550 -1555, STRINGER 39L CORRODED. REMOVED DAMAGE & INSTALLED STRINGER REPAIR IAW SRM 53-00-03 FIG 201 REPAIR 2.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 95,414 hrs · 15,025 cycles

MULTIPLE AREAS OF CORROSION ON SEAT TRACK STATION 1210 - 1439, RBL 88.5. CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52 DETAIL VII. R & R SEAT TRACK IAW SRM 51-40-02 PARA 7 FIG 12.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 95,414 hrs · 15,025 cycles

MULTIPLE AREAS OF CORROSION ON SEAT TRACK STATION 1210 - 1439, RBL 88.5. CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 53-00- 52 DETAIL VII. R & R SEAT TRACK IAW SRM 51-40-02 PA RA 7 FIG 12.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 95,414 hrs · 15,025 cycles

CORROSION IN AFT CARGO COMPARTMENT MULTIPLE AREAS UPPER & LOWER SURFACE ON FRAME UPPER T CAP BS 1197 - 132 RT & LT SIDES. R & R T CAP, INNER CORD, PN 146T1060-1 IN AFT CARGO COMP BS 1197 - 132 RBL 45 TO LBL45 IAW SRM 51-40-02 PAR 4 & 7. REMOVED CORROSION IN MULTIPLE AREAS IAW SRM 51-10-02 PAR 14. 100% MATERIAL LOSS AT RBL43 & LBL43.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 93,485 hrs · 14,758 cycles

EXTERIOR EMER LIGHT BY MOST AFT RT MAIN DOOR INOPERATIVE. REPLACED LAMP FOR RT DOOR EMER LIGHT IAW 33-51-06.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 93,485 hrs · 14,758 cycles

SECOND EMER LIGHT AFT OF LT WING INOPERATIVE. LIGHT OPERATES GOOD IAW 33-51-06.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 93,021 hrs · 14,688 cycles

OVERWING EXIT INTERIOR EMER LIGHT IS INOPERATIVE. RECONNECTED EMER LIGHT BATTERY CONNECTOR. CHECKED GOOD.

Part: POWER SUPPLY — FAULTY (WARNING SYSTEM) · airframe 91,523 hrs · 14,476 cycles

WEX WARNING ELECTRONICS IS INTERMITTENT CAUSING ENG FIREX & APU FIREX CHECKS TO FAIL AS WELL AS EGPWS FAILURES. REPLACED B POWER SUPPLY & M107 27 CARDS IAW MM31-51-04. MSG CLEARED, OPERATIONS TESTED NORMAL.

Part: ACM — MALFUNCTIONED (AC BAY) · airframe 91,243 hrs · 14,439 cycles

LT PACK TEMP EICAS MESSAGE. CARRIED OUT ACM RESET & ACCOMPLISHED TROUBLE SHOOTING PROCEDURE IAW MM 21-51-03 PG 101, ALL OPERATIONS RESTORED TO NORMAL.

Part: CONNECTOR — NOT SEATED (SMOKE DETECTOR) · airframe 91,192 hrs · 14,432 cycles

FWD CARGO DETECTION FAN MAINTENANCE MESSAGE ON LOWER EICAS. PULLED CB'S, RESEATED CONNECTOR ON BLOWER 1, CLOSED CB'S, OPERATIONS NORMAL.

Part: INDICATOR — MALFUNCTIONED (COCKPIT) · airframe 91,124 hrs · 14,422 cycles

LOST BOTH FLIGHT DIRECTOR GLIDE SLOPE INDICATORS ON FINAL.

Part: ACTUATOR — FAILED (AC BAY) · airframe 90,767 hrs · 14,376 cycles

RT PACK TEMP EICAS. COMPLETED CHECKLIST, OPERATING IN MANUAL, TEMP CONTROL DIFFICULT. FOUND RT PACK RAM AIR EXIT DOOR FAILED IN CLOSED MODE & ALSO FAULTED ON CONTROLLER BITE CHECK. REPLACED ACT WRT MM 21-53-04, ALSO CONTROLLER BITE CHECKED NORMAL.

Part: TRANSCEIVER — FAULTY (WEATHER RADAR) · airframe 90,778 hrs · 14,377 cycles

WX RADAR NOT PAINTING PRECIPITATION, UNABLE TO GET GND RETURNS. TROUBLE SHOT FOUND WX RADAR TRANSCEIVER NOT PAINTING RRD WX RADAR RT. OPERATIONS CHECKED OK AT THIS TIME.

Part: LIGHT — INOPERATIVE (HYDRAULIC SYS) · airframe 90,547 hrs · 14,344 cycles

C ELEC 2 LOW PRESS LIGHT NOT ILLUMINATED WHILE THE PUMP IS SHED.

Part: CONTROL UNIT — FAULTY (COCKPIT) · airframe 90,330 hrs · 14,314 cycles

FIRST OFFICER`S INST PANEL FLOOD LIGHTS WON'T LIGHT OR DIM WITH CONTROL KNOB. LIGHTS DO NOT ILLUMINATE BRIGHT WITH LIGHT OVERRIDE SWITCH ON. REPLACED LIGHT MODULE, NO HELP. REPLACED DIMMER CONTROL UNIT, ALL OPERATIONS NORMAL.

Part: CONNECTOR — DIRTY (HYDRAULIC SYS) · airframe 90,282 hrs · 14,308 cycles

C HYD 2 PUMP WILL NOT SHED FOR ENG START. C2 PUMP SWITCH CIRCUIT CARD. CLEANED C2 PUMP LOW PRESSURE SWITCH CANON PLUG. INSPECTED CONNECTIONS ON ELCU, CONNECTIONS SECURE. ALL INDICATIONS OPERATIONS NORMAL.

Part: UNKNOWN — MALFUNCTIONED (BLEED AIR SYS) · airframe 90,281 hrs · 14,307 cycles

CABIN ALTITUDE HORN SOUNDED AS CABIN ALT CLIMBED AFTER LOOSING BLEEDS. DUE TO RAPID DEPRESSURIZATION & EMERGENCY DESCENT, NEED TO ACP ECRA 2130-01302 WITHOUT DEVIATION. AIRCRAFT CANNOT BE RETURNED TO SERVICE WITHOUT TOMC & ENGINEERING CONCURRENCE. REPORT ALL FINDINGS TO TOMC AND ENGINEERING. ACCOMPLISHED LM7521 IN ACCORDANCE WITH ECRA 2130-01303 WITHOUT DEVIATION. ALL SYSTEMS AND OPS CHECKS GOOD WITH NO FINDINGS BY AMT. ACCOMPLISHED LM7521 AND ECRA 2130-01302 WHICH INCLUDED AMM 05-51-98 IN ITS ENTIRETY WITHOUT DEVIATION. STANDBY AIRSPEED AND ALTIMETER SYSTEM TESTS ACCOMPLISHED PER AMM, ALL TESTS PASSED WITH NO FINDINGS.

Part: VALVE — FAILED (BLEED AIR SYS) · airframe 90,281 hrs · 14,307 cycles

RT ENG OVERHEAT LIGHT ILLUMINATED & LOST RT BLEED. REPLACED FAN AIR VLV & PRV IAW AMM, DUE FAULTS OF AIR SUPPLY BITE MOD.

Part: SHUTOFF VALVE — FAILED (BLEED AIR SYS) · airframe 90,281 hrs · 14,307 cycles

LT ENG BLEED LIGHT CAME ON, UNABLE TO RESTORE. REPLACED HPSOV IAW AMM & AIR SUPPLY BITE MOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 90,280 hrs · 14,306 cycles

EMERGENCY LIGHTS INOPERATIVE OVERWING RT SIDE GREEN LIGHTS. R & R MID LAVATORY FLOOR MOUNTED EMERGENCY EXIT LIGHT IAW AMM 33-51-10 & REPLACED POWER SUPPLY M1554 IAW AMM 33-51-07 & OPERATIONS CHECKED GOOD IAW AMM 33-51- 00 ON NON-ROUTINE 35242.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 90,280 hrs · 14,306 cycles

LT WING AFT EMERGENCY SLIDE LIGHT JUST AFT OF WING TO BODY FAIRINGS INOPERATIVE. R & R LT WING AFT EMERGENCY LIGHT IAW AMM 33-51-06 & OPERATIONS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 90,280 hrs · 14,306 cycles

LT WING EMERGENCY SLIDE LIGHT AFT OF WING TO BODY FAIRINGS INOPERATIVE. R & R LIGHT IAW AMM, OPERATIONS CHECKED GOOD.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 90,280 hrs · 14,306 cycles

STATION 287 T-CAP CORRODED AT RBL 25 TO LBL 30. R & R T-CAP IAW SRM 51-40-0 2 & 53-00-51 REPAIR IS CAT A IAW 53-00-51.

Part: STOP FITTING — DAMAGED (CARGO DOOR) · airframe 90,280 hrs · 14,306 cycles

AFT CARGO DOOR AFT FRAME LOWER STOP FITTING NR 10 HAD INTERIM REPAIR ACCOMPLISHED DURING C-14 CHECK IN TPA IAW ECRA 5360-01181. R & R FRAME STOP FITTING AT AFT CARGO AFT FRAME NR 10 IAW B767 SRM 51-40-02. RIG CHECKED GOOD AT NR 10 STOP FITTING IAW B767 MM 52-35-00.

Part: PANEL — UNSECURE (LAVATORY) · airframe 90,156 hrs · 14,289 cycles

2R OTBD LAVATORY FRAME DETACHED. SECURED PANEL OK TO CONTINUE.

Part: EXCITER — FAULTY (NR 2) · airframe 90,063 hrs · 14,277 cycles

NR 2 ENGINE DID NOT START ON NR 2 IGNITION. STARTED OK ON BOTH. RT ENGINE NR 2 IGNITER & EXCITER BOX REPLACED. RAN ENGINE NO FAULTS NOTED.

Part: SOCKET — FAILED (VACUUM OUTLET) · airframe 89,969 hrs · 14,265 cycles

ON APPROACH VACUUM OUTLET AT DOOR L2 STARTED SMOKING & ARCING. REPLACED SOCKET OUTLET & SPLICED NEW WIRE TERMINALS IAW SWP 20-30-11. SYSTEM CHECKED OK. NO FURTHER EVIDENCE OF WIRE DAMAGE

Part: LIGHT — DEFECTIVE (COCKPIT) · airframe 89,857 hrs · 14,251 cycles

FOUND CIRCUIT BREAKER P32 TRIPPED. IAW WDM PAGE 33-14-31, BREAKER FOR FLT KIT LIGHTS. FOUND CAPT LIGHT KIT LIGHT ASSY DEFECTIVE. REPLACED LIGHT ASSY IAW MM. CIRCUIT BREAKER NOW HOLDS POWER. LIGHT KIT ASSY FUNCTIONAL.

Part: SEALANT — MISSING (LT WG FUEL CELL) · airframe 89,255 hrs · 14,173 cycles

LEFT WING LEAKING FUEL FROM DRY BAY DRAIN HOLE. FOUND & REPAIRED AREA OF MISSING SEALANT. NEEDS TO BE FUELED & LEAK CHECKED AFTER 2300 HOURS 7-3-2013. LEAK CHECKED LEFT WING FUEL PANELS. NO LEAKS FOUND, IAW GMM UAL 09-10-05.

Part: SEAL — DAMAGED (R2 WINDOW) · airframe 89,196 hrs · 14,162 cycles

R2 COCKPIT WINDOW SEAL DAMAGED. REPLACED SEAL.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 89,063 hrs · 14,143 cycles

DURING EMERGENCY LIGHT OPS CHECK, DISCOVERED LT OVERWING DOOR EXIT IDENTIFIERS FOR BOTH OVERWING HATCHES WERE INOPERATIVE. R & R BATTERY PACK. OPS CHECKED GOOD. REF WDM 33-51-14.

Part: VALVE — FAILED (MID CABIN TEMP) · airframe 88,747 hrs · 14,102 cycles

MID-CABIN TEMP EICAS AND INOPERATIVE LIGHT. AUX ZONE TEMP CONTROLLER FAULTS AUX MID CABIN TRIM AIR VALVE. REPLACED AUX MID CABIN TRIM AIR VALVE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 88,681 hrs · 14,094 cycles

EMERGENCY LIGHTS INOPERATIVE. REPLACED LAMPS, CHECKED OK.

Part: HOSE — DAMAGED (CABIN) · airframe 88,586 hrs · 14,082 cycles

WHEN WORKING DF748 FOUND SUPPLY HOSE REF IPC 21-24-01-004A ITEM 15 WITH SMALL HOLE. NEW ONE ON ORDER AOG Z5340. REMOVED GASPER AIR FAN REF AMM. WAITING FOR PARTS TO INSTALL FAN. REPAIRED GASPER FAN HOSE IAW ECRA 2124-01007. RE-INSTALLED GASPER FAN REF.

Part: FAN — FAILED (GASPERS) · airframe 88,570 hrs · 14,080 cycles

WITH GASPER SWITCH ON, INDICATES OFF. GASPER FAN INOPERATIVE & SWITCH IS OFF POSITION. REMOVED GASPER FAN IAW AMM. REPAIRED GASPER FAN HOSE IAW ECRA 2124-01007. REINSTALLED GASPER FAN. FOUND TORN RUBBER BOOT FOR GASPER FAN. REPLACED BOOT.

Part: HOSE — LEAKING (LAVATORY TANK) · airframe 88,426 hrs · 14,060 cycles

BLUE FLUID LEAKING FROM BELLY DRAIN JUST FWD OF SERVICE PANEL WHEN RINSING LAV TANKS. REPLACED FILL LINE HOSE PER AMM 38-00 AND LEAK CHECKED.

Part: UNKNOWN — MALFUNCTIONED (ENTERTAIN SYS) · airframe 88,207 hrs · 14,034 cycles

PAX VIDEO AND ENT SYSTEM WHOLE AIRCRAFT INOP ENTERTAINMENT SYSTEM SCREEN FROZEN AND SOMETIMES IT KEEPS REBOOTING. CB P11 T34 PULLED AND COLLARED REF MEL PROCEDURES FOR ENTERTAINMENT SYSTEM DEACTIVATION. RESTORED ACFT TO ORIGINAL CONFIG FOR MEL 2520HY (C-B T34 CLOSED, MASTER SWITCH ON) T/S SYSTEM FOUND FWD ATT CREW TERMINAL INOP, SYSTEM WORK NORMAL FROM AFT POSTION. CHANGED PLACARD TO 2520GU. PARTS NIS - IAH. INF- :NOTED MX MESSAGES 331-000 -0001(CMOD) 305-002-0001 (CT) 198-000-00001 (MCU) X2 333-010-0001 (PTR), SYSTEM OPERATES NORMAL FROM AFT CREW PANEL. PARTS: 583-0263 RD-FA1051-01 (TERMINAL)

Part: RELAY — WARNING LIGHT (THRUST REVERSER) · airframe 88,059 hrs · 14,016 cycles

ON CLIMBOUT, LT ENGINE REVERSER LIGHT CAME ON THREE TIMES. ACCOMPLISHED FIM78-34-00 PG 131, REPLACED NR 1 ENG THRUST REVERSER ISOLATION DETECTOR RELAY. OPS CHECKED ALL INDICATION NORMAL.

Part: WIRE — EXPOSED (SEAT 37C) · airframe 87,935 hrs · 13,999 cycles

SEAT 37C ARMREST WIRES EXPOSED. REINSTALLED ARMCAP SEAT 37J, OPS NORMAL.

Part: TRANSCEIVER — FAULTY (COCKPIT) · airframe 87,796 hrs · 13,979 cycles

F/O RA FLAG ON ADI. REPLACED RIGHT RA RCVR PER MM AND CAT 3 TEST PER MM. A/C RETURNED TO CAT 3 STATUS.

Part: WARNING SYSTEM — ACTIVATED (HYDRAULIC SYS) · airframe 87,665 hrs · 13,959 cycles

LEFT HYD QTY EICAS MSG.

Part: DUCT — WORN (NR 1 STARTER) · airframe 87,530 hrs · 13,941 cycles

NR 1 ENGINE STARTER DUCT HAS AN AREA WORN IN IT FROM THE CORE COWL THRU PIN RETAINER RUBBING ON IT. REMOVED DUCT. REPAIRED IAW GPM 1-0-2-002 SECURED NR 1 STARTER DUCT.

Part: STRUT — CRACKED (ENGINE) · airframe 86,999 hrs · 13,867 cycles

TURBINE EXHAUST STRUT AT 2 O'CLOCK HAS 1.5 INCH CRACK AT BASE. AXIAL CRACK FOUND, NO U-SHAPED CRACKS FOUND. CARRY FWD FOR 70T PER AMM. WELDED AS PER MM.

Part: STRUT — CRACKED (ENGINE) · airframe 87,021 hrs · 13,871 cycles

TURBINE EXHAUST STRUT AT 1 O'CLOCK HAS 1.5 INCH CRACK AT BASE. AXIAL CRACK FOUND, NO U-SHAPED CRACKS FOUND. CARRY FWD FOR 70T PER AMM. RPR- :WELDED AS PER MM 72-54-01.

Part: STRUT — DAMAGED (NR 1 ENGINE) · airframe 87,021 hrs · 13,871 cycles

TURBINE EXHAUST STRUT AT 11 O'CLOCK POSITION HAS 1.5 INCH CRACK AT BASE. STRUT REPAIRED PER GMM 72-54-01 PG 801 PROCEDURE 'A' AND 'B' ITEM 1-5, PERFORMED BY WELDER.

Part: INJECTOR — DRY (ENGINE) · airframe 86,999 hrs · 13,867 cycles

RAN ENGINE FOR FUEL DISTRIBUTION VALVE OPS CHECK. NEED TO REMOVE INGITOR PLUG TO VERIFY NR 13 FUEL INJECTOR VALVE IS DRY BY BOROSCOPING. REMOVED IGNITOR PLUG FOR BORO. INSPECTOR VERIFIED THAT FUEL INJECTOR WAS DRY NR 13 INJECTOR.

Part: VALVE — FAULTY (CABIN TEMP) · airframe 86,628 hrs · 13,813 cycles

FORWARD CABIN TEMP EICAS MSG SAMC TEXT: SEE PREVIOUS HISTORY, ZONE TEMP CTLR AND AUX ZONE TEMP CTLR PREVIOUSLY REPLACED. SUGGEST REPLACE FWD CABIN ZONE TEMP CTL VALVE. CREW (938-13) REFUSAL WITH MEL 2161YH. REPLACED FWD TRIM AIR VALVE AMM. REPLACED FWD CABIN TEMP LIGHT. CLEARED PACK & TEMP CONTROLLERS. SYS OPS CHECK GOOD.

Part: DISPLAY — FAILED (COCKPIT) · airframe 86,537 hrs · 13,801 cycles

UPPER EICAS FLICKERS & CYCLES TO COMPACT MODE. REPLACED UPPER EICAS DISPLAY UNIT REF MM. ALL OPS NOW GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 86,046 hrs · 13,729 cycles

SEAT MOUNTED EMERGENCY LIGHT OUT SEAT 38J. REPLACED LIGHT ASSEMBLY REF IPC P/N BR9644-21, (565-1162). NON-RII INSPECTION OF ITEM# 0462012 INSTALLATION AND OPERATION.

Part: MODULE — LEAKING (HYDRAULIC SYS) · airframe 85,701 hrs · 13,680 cycles

RIGHT SYSTEM EDP PRESSURE CASE DRAIN FILTER MODULE, LEAKING FROM PRESSURE DIFFERENTIAL PRESS IND ON MODULE. REMOVED AND INSTALLED NEW IND ASSY-DIF PRESSURE REF AMM. NEEDS LEAK CHECK.

Part: O-RING — DETERIORATED (ANTI-SKID SYS) · airframe 85,701 hrs · 13,680 cycles

FOUND HYDRAULIC LEAK LEFT WHEEL WELL AREA. FOUND HYD LEAK LEFT ANTI-SKID 4 OUT. REPLACED DETERIORATED O-RING ON ANTI-SKID MODULE 4 OUT UNION FITTING.

Part: ACTUATOR — FAULTY (RT AILERON) · airframe 85,701 hrs · 13,680 cycles

REMOVE RIGHT INBOARD AILERON ACTUATOR FOR LOG 2 AND LOG 3 RIGHT AILERON FLOATING. REMOVED ACTUATOR PER AMM 27-11-48 STEP1 THROUGH 2F7. P/N 282800.1009 S/N 2121.

Part: ACTUATOR — FAULTY (RT AILERON) · airframe 85,701 hrs · 13,680 cycles

AT 15000 270KTS TAKES 6 DEG LEFT RUDDER TO HOLD 2 DEG RT BANK RT INBD AILERON SHOWS UP. FOUND RT INBD CTR SYSTEM ACT INTERMITTENTLY BEING ABLE TO BE MOVED BY HAND THEN HYDRAULICALLY POWERED BACK TO NEUTRAL. VISUAL CONFIRM RT INBD AILERON FLOATING UP APPX 15 DEG. ACP T/S OF RT INBD AILERON, REPLACING RT CTR INBD AILERON ACTUATOR.

Part: BATTERY — FAULTY (MAIN) · airframe 85,651 hrs · 13,673 cycles

MAIN BATTERY CHARGER NOT WORKING. REPLACED MAIN BATTERY.

Part: WARNING LIGHT — FALSE ACTIVATION (FIRE LOOP) · airframe 85,551 hrs · 13,660 cycles

EICAS MESSAGE "NR 1 ENG FIRE LP1" DISPLAYED. TESTED NR 1 ENG FIRE DETECTION SYS PER MM 26-11-00-501 AND 26-11-00-0101. ALL CHECKED GOOD ON GROUND. CANNOT DUPLICATE PROBLEM. INSPECTED NR 1 ENG FIRE LOOPS, ALL LOOKS GOOD. NO DEFECTS FOUND.

Part: CIRCUIT CARD — FAULTED (SMOKE DETECTION) · airframe 85,526 hrs · 13,657 cycles

FWD CARGO DET 1 STATUS MESSAGE, MESSAGE INTERM. FIRE AND OVERHEAT TESTED. MESSAGE NOT FOUND ON STATUS PAGE. TESTED SYSTEM SEVERAL TIMES ON GROUND. CHECKED GOOD. REPLACED FIRE OVERHEAT AND TEST CARD FOR DF548.

Part: SPEAKER — INOPERATIVE (HANDSET) · airframe 85,182 hrs · 13,608 cycles

SPEAKER IN COCKPIT PHONE SET INOPERATIVE. TRANSMITS OK. CANNOT HEAR THRU PHONE SPEAKER. REPLACED DOOR 1L HANDSET AND RESET CIRCUIT BREAKERS ON P11, PANEL ADJUSTED PA VOLUME ON AUDIO ACCESSORY UNIT.

Part: COMPUTER — MALFUNCTIONED (AUTOTHROTTLE) · airframe 85,167 hrs · 13,606 cycles

AUTOTHROTTLE DISCONNECT LIGHT ILLUMINATED, WILL NOT CLEAR (FWD INSTRUMENT PANEL). REPLACED THRUST MANAGEMENT UNIT, OPS CHECKED GOOD. CAT III CHECKED GOOD RE FMM22-10-00.

Part: ISOLATION VALVE — MALFUNCTIONED (BLEED AIR SYS) · airframe 84,975 hrs · 13,581 cycles

RIGHT BLEED ISOLATION VALVE ECAM ON VALVE LIGHT ILLUMINATED. REPLACED THE RIGHT BLEED ISOLATION VALVE.

Part: TRANSMITTER — MALFUNCTIONED (VHF SYSTEM) · airframe 84,524 hrs · 13,521 cycles

AFTER DEPARTURE LOST LEFT VHF. CAN RECEIVE BUT NOT TRANSMIT. NO WAY TO RESTORE IN FLIGHT. CONTINUING TO DESTINATION. GROUND CHECKED , OPS NORMAL.

Part: FEEDER CABLE — CHAFED (NR 1 IDG) · airframe 84,341 hrs · 13,494 cycles

NR 1 ENGINE IDG MAIN FEEDER CABLE IS CHAFED THRU THE INSULATION ABOUT 12 INCHES FROM THE IDG TERMINAL LUGS. THERE ARE SOME SIGNS OF ARCHING ON THE FASTENER THAT CAUSED THE CHAFING. INSPECTED AND FOUND DAMAGE WITHIN LIMITS PER SWPM 20. WRAPPED CABLE WITH CHAFE TAPE AND REPOSITION HARNESS AWAY FROM CHAFE POINT.

Part: HOSE — LEAKING (GASPERS) · airframe 83,931 hrs · 13,441 cycles

FOUND GASPER AIR VENT HOSE AT SEAT 23AB LOOSE & SQUEALING. RESEALED & SECURED GASPER AIR VENT. OPS GOOD.

Part: NUT PLATE — BROKEN (RT AILERON) · airframe 83,760 hrs · 13,418 cycles

RIGHT I/B AILERON HAS EVIDENCE OF HYD LEAK. REQ INSPECTOR VERIFY LEAK LIMITS REF A-CK JOB CARD. OPENED PANEL 661BB AT RT INBD AILERON AND CLEANED AREA. ACCOMPLISHED LEAK CHECK OF I/B AILERON ACTUATORS. NO LEAKS FOUND. OK TO CLOSE ACCESS PANEL. ONE NUT PLATE BROKEN (TAGGED) NEEDS REPAIR. INSTALLED 1 EA. NEW NUT PLATE AND CLOSED RT WING I/B AILERON LOWER ACCESS PNL.

Part: SCREW — LOOSE (LT WING) · airframe 83,760 hrs · 13,418 cycles

TIGHTEN AND REPAIR LOOSE AND PULLED THRU SCREWS LT WING LWR PANEL INBD OF NR 1 ENG PYLON. TIGHTENED SCREWS AND REPAIRED NUT PLATES.

Part: CONTROLLER — FAULTY (APU) · airframe 83,268 hrs · 13,354 cycles

APUC FAILED TO RESET OR TEST AFTER FIRE BOTTLE WAS ARMED AT NLG. REPLACED APUC.

Part: PCU — OUT OF ADJUST (RUDDER) · airframe 83,246 hrs · 13,349 cycles

5 UNITS LEFT RUDDER TRIM NEEDED IN CLIMBOUT. FOUND LEFT RUDDER PCU OUT OF ADJUSTMENT. ADJUSTED PER MM. CHECKED ADJ OF CENTER AND RIGHT PCU. CHECKS NORMAL.

Part: FILTER — LEAKING (OIL SYSTEM) · airframe 83,246 hrs · 13,349 cycles

MAIN OIL FILTER WAS REPLACED AND ENGINE WAS MOTORED, BUT ENGINE STILL NEEDS 5 MIN ENGINE RUN, UNABLE TO RUN ENGINE DUE TO LACK OF HYDS. RAN ENGINE FOR 5 MINUTES, NO LEAKS FOUND.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 83,244 hrs · 13,348 cycles

BS 1540 AT BL 0 AFT BULK CARGO COMPARTMENT INTERNAL FUSELAGE SKIN CORRODED AT DRAIN VALVE (N-R 4175N00498). MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGE, FABBED AND INSTALLED DOUBLER AND FILLER AND PART MARKED PER SRM AND GNMM 1-01-007 ON NR 4175N00498.

Part: STOP FITTING — DAMAGED (FUSELAGE) · airframe 83,244 hrs · 13,348 cycles

AFT CARGO DOOR AFT FRAME LWR STOP FITTING (NR 10) HAD INTERIM REPAIR ACCOMPLISHED DURING C-14 CHECK IN TPA PER EC-RA 5360-01181. DAMAGE CAREFULLY BLENDED REF EA PD67-53-065 & UAL EC-RA 5360-01181. PERFORMED HFEC INSPECTION OF BLENDED AREA. NO DEFECTS NOTED. FLAP PEENED BLEND & RESTORED SURFACE PROTECTION. THIS IS AN INTERIM REPAIR. CF0406 CREATED TO REPLACE FITTING BY 01 OCT 2013.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 83,244 hrs · 13,348 cycles

DAMAGE TO FUSELAGE SKIN BELOW FWD LWR CORNER OF BULK CARGO DOOR APROX 10" LONG X 4.5" WIDE LOCATED AT BS 1428 ABOVE & BELOW STRINGER S34L. MAJOR REPAIR ACCOMPLISHED. EVALUATED DENT & FOUND OUT OF LIMITS OF SRM. CUT OUT DAMAGE & ACP VISUAL & NDT INSP FOR CRACKS. ACP NDT OF OPEN HOLES COMMON TO REPAIR PER PEMCO EA PD67 -53-063 & UA EC-RA# 5360-01180. FABRICATED & INSTALLED EXTERNAL DOUBLER,TRIPLER & FILLER REPAIR PER EA PD67-53-063 & UA EC-RA 5360-01180.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 83,244 hrs · 13,348 cycles

EEL PATH LIGHT INOP AT FWD VIDEO CLOSET. REPLACED EEL LIGHT AT FWD VIDEO CLOSET, OPS CHECK GOOD PER AMM ON NR 4175N00542.

Part: NUT — LOOSE (NLG IDLER) · airframe 83,244 hrs · 13,348 cycles

LANDING GEAR MONITOR STATUS EICAS MSG REPORTED BY CREW AFTER GEAR RETRACTION. TIGHTENED LOOSE NUT RT FWD NLG IDLER HINGE, TORQUED NUT PER AMM. ACCMP'D GEAR SWING SEVERAL TIMES PER AMM. EICAS MSG WAS CLEAR ON NR 4175N00193.

Part: LENS — MISSING (CABIN) · airframe 83,244 hrs · 13,348 cycles

SEATS 32 AND 37 J-K EEL LIGHTS MISSING LENS, OPERATES PROPERLY. REPLACED SEATS 32 AND 37 J-K EEL LIGHTS, OPS CK GOOD PER AMM 33-51-00 ON NR 4175N00004.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 83,244 hrs · 13,348 cycles

SEAT ROW 32 LT SIDE BULLNOSE EMERGENCY EXIT LIGHT INOP. REPLACED SEAT 32 LEFT BULLNOSE EEL LIGHT, OPS CK GOOD PER AMM ON NR 4175N00005.

Part: REGULATOR — LEAKING (CREW O2) · airframe 83,172 hrs · 13,337 cycles

DURING OPS CK OF CREW O2 FOUND OXYGEN LEAK. ISOLATED EACH CREW MASK STOWAGE BOX. SYSTEM STILL LEAKS. REPLACED CREW BOTTLE O2 REGULATOR PER MM. LEAK CHECK GOOD.

Part: WIRE — BURNED (GALLEY CART) · airframe 83,026 hrs · 13,316 cycles

THERE WAS SMOKE, SPARKS AND SMALL FLAMES COMING OUT OF AFT GALLEY CART CONTROLLERS PANELS. ALL AFT GALLEY CART CONTROLLER POWER CIRCUIT BREAKERS ON AFT GALLEY POWER DISTRIBUTION WERE PULLED, POWER TO CART CONTROLLERS WERE REMOVED. CREW NOTICED DAMAGE ON PIGTAIL CART LOCATION 508 ALSO. REPORTED BY FLIGHT CREW. FOUND CART CONTROLLER N62 WITH EVIDENCE OF SMOKE, ALSO FOUND BURNT PIN ON PIGTAIL P62. REPLACED CART CONTROLLER AND PIGTAIL. ACP TEST WITH CART AND CART CONTROL TESTER, ALL CHECKS OK. NO OTHER DAMAGE.

Part: BLADE — NICKED (NR 2 ENGINE) · airframe 82,981 hrs · 13,311 cycles

NR 2 ENGINE HAS SMALL NICK IN FAN BLADE NR 28. BLENDED OUT NICK PER MM. VISUAL AND DYE PENETRANT INSPECTION ACCOMPLISHED. NO CRACKS NOTED. DAMAGE IS APPROX 2 INCH FROM TIP AND 0.0313 DEEP.

Part: SWITCH — STUCK (COCKPIT LIGHTS) · airframe 82,990 hrs · 13,312 cycles

FLIGHT DECK LIGHTS STUCK IN FULL BRIGHT, REPLACED SWITCH MODULE. CHECKED OKAY.

Part: LATCH — BROKEN (FLASHLIGHT BOX) · airframe 82,861 hrs · 13,297 cycles

EMERGENCY FLASHLIGHT COMPARTMENT DOOR BELOW JUMPSEAT 260, CENTRE SEAT AT MID CROSS AISLE,HAS RIGHT DOOR LATCH BROKEN. DOOR SECURED CLOSED. LATCH TIE ROD BROKEN.

Part: SELECTOR PANEL — INOPERATIVE (AUDIO) · airframe 82,829 hrs · 13,293 cycles

RADIOS INOPERATIVE. REPLACED SECOND OBS AUDIO SELECTOR PANEL PER MM.

Part: AUDIO PANEL — FAULTY (COCKPIT) · airframe 82,803 hrs · 13,289 cycles

FIRST OFFICERS VHF L SELECTOR BUTTON STICKS AND IS HARD TO DEPRESS. REPLACED F/O'S AUDIO SELECT PANEL, OP CHECKS NORMAL.

Part: PRESSURE SWITCH — FAULTY (APU) · airframe 82,423 hrs · 13,240 cycles

APU START FAULT X2. REPLACED OIL PRESSURE SWITCH, OPS CHECKS GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 82,223 hrs · 13,210 cycles

OVERWING EMERGENCY EXIT SIGNS INOPERATIVE. REPLACED BATTERY PACK PER MM, OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 82,223 hrs · 13,210 cycles

EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED LIGHT ASSY PER MM, OPS CHECKED GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 82,223 hrs · 13,210 cycles

EMERGENCY LIGHT INOPERATIVE AT SEAT 36H. RELAMPED, OPS CHECKED OKAY.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 82,223 hrs · 13,210 cycles

EMERGENCY EXIT SIGN AT MID GALLEY FWD OF RT LAV INOPERATIVE. RELAMPED, OPS CHECKED GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 82,223 hrs · 13,210 cycles

EMERGENCY LIGHT INOPERATIVE AT SEAT 9K. RELAMPED, OPS CHECKED OKAY.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 82,223 hrs · 13,210 cycles

EMERGENCY LIGHTS INOPERATIVE AT SEATS 19 THRU 22H. REPLACED BATTERY PACK M1209 PER MM, OPS CHECKED GOOD.

Part: CONTROL PANEL — FAULTY (COCKPIT) · airframe 82,188 hrs · 13,205 cycles

NEITHER HF RADIOS WILL TUNE. FOUND FIRST OBSERVERS AUDIO CONTROL PANEL PTT BUTTON STUCK. REPLACED OBSERVERS AUDIO CONTROL PANEL.

Part: AMU — FAULTY (INTERPHONE) · airframe 82,188 hrs · 13,205 cycles

CAPTAIN'S & FIRST OFFICER'S INTERPHONE HAS STATIC. FOUND NOSE GEAR INTERPHONE JACK BAD. FOUND NOSE GEAR JACK OKAY. REPLACED AMU.

Part: OVEN — CONTAMINATED (GALLEY) · airframe 82,080 hrs · 13,190 cycles

FLIGHT ATTENDANT STATED ODOR BEGAN COMING FROM WARMING OVEN RIGHT SIDE. FOUND BURNED PLASTIC INSIDE WARMING OVEN. CLEANED OUT OVEN AND OPERATED. ODOR CLEARED.

Part: CONTROL PANEL — FAILED (AFCS) · airframe 82,000 hrs · 13,179 cycles

ALTITUDE WON'T GO BELOW 80,000 FT. REPLACED MODE CONTROL PANEL PER MM, OPS NORMAL.

Part: CONTROL PANEL — MALFUNCTIONED (AFCS) · airframe 82,000 hrs · 13,179 cycles

MODE CONTROL PANEL, HEADING WINDOW DISPLAYS IS BLANK, DOES NOT RESPOND TO HEADING (SEL, HOLD). HEADING STICKS. REPLACED MAIN CONTROL PANEL PER MM. HEADING WINDOW DISPLAY OPS CHECKED NORMAL.

Part: COMPUTER — FAILED (AUTOTHROTTLES) · airframe 82,000 hrs · 13,179 cycles

THRUST MANAGEMENT COMPUTER FAILED AUTOTHROTTLE TEST 40. REPLACED TMC PER MM. FAILED TEST AUTOPILOT PORTION OF TEST.

Part: CONTROL PANEL — MALFUNCTIONED (AFCS) · airframe 82,000 hrs · 13,179 cycles

HEADING SELECT BUTTON ON MAIN CONTROL PANEL INTERMITTENT. REPLACED AFCS MODE CONTROL PANEL PER MM. AIRCRAFT RETURNED TO CAT III STATUS PER MM.

Part: INDICATOR — FAULTY (FUEL SYSTEM) · airframe 81,647 hrs · 13,131 cycles

FUEL TRANSFER TBS. DUE TO LEFT TO CENTER FUEL TRANSFER, ACCOMPLISH FIM28-26-00 P107 FIG 104A. PAY PARTICULAR ATTENTION TO THE LEFT DEFUEL VALVE POSITION. ACCOMPLISHED FOUND LEFT DEFUELING VALVE IN CLOSED POSITION. SELECTING LEFT DEFUEL VALVE TO OPEN POPS C/B L4 ON P34 PANEL (DEFUELING VALVES CB). SECURED CLOSED. CANNON PLUG REMOVED FROM VALVE AND CB DID NOT POP AGAIN. REPLACED DEFUELING VALVES C-B, OPS CKS NORMAL. RIGHT WING FUEL QTY UNDERWING GAUGE FLASHING. DEFERRED DUE TIME - SEE HISTORY. REPLACED FUEL QUANTITY PROCESSOR, NO HELP. CONFIRMED FAULTY INDICATOR. PART NOT IN STOCK AT IAD. NEEDS FUELING PANEL INDICATOR MR28603 (PCN 481-9228). RPLC'D INDICATOR. OPS CHECK NORMAL.

Part: OXYGEN MASK — FAULTY (COCKPIT) · airframe 81,408 hrs · 13,097 cycles

F/O'S O2 MASK MICROFONE INOPERATIVE. REPLACED F/O'S MASK, GROUND CHECK NORMAL.

Part: SHUTOFF VALVE — FAULTY (BLEED AIR SYS) · airframe 81,408 hrs · 13,097 cycles

RT ENG PRV EICAS. REPLACED NR 2 ENG PRV AND OVER PSI SWITCH. ACCOMPLISHED "ENG PRV AND "BLEED" LIGHT. ACCOMPLISHED NR 2 ENGINE IDLE RUN BLEED AIR OPERATIONAL CHECK.

Part: CDU — MALFUNCTIONED (COCKPIT) · airframe 81,237 hrs · 13,070 cycles

F/O FMC CDU BLANK RTFL, HAPPENED ON PREFLIGHT AND RESET CB E29. CDU WORKED OK UNTIL NOW. REPLACED F/O'S FMC CDU IAW MM 34-61-02. OPS CHECK NORMAL.

Part: BATTERY — FAILED (APU) · airframe 81,186 hrs · 13,062 cycles

APU WILL NOT CRANK. REPLACED BATTERY PER MM, OPS CHECKED NORMAL.

Part: INDICATOR — FAILED (FUEL SYSTEM) · airframe 81,126 hrs · 13,054 cycles

DURING FUELING LOST POWER TO UNDER WING FUEL STATION. AFTER RESET RIGHT TANK GAUGE FAULTED. DEFERRED RIGHT TANK UNDERWING FUEL GAUGE INOP PER MEL 2841G. REPLACED RIGHT UNDER WING GAUGE.

Part: DISPLAY — FAULTY (ACARS) · airframe 80,772 hrs · 13,006 cycles

CREW REPORTS ACARS INOPERATIVE. REPLACED ACARS MNG UNIT PER MM. REPLACED INTER DISPLAY UNIT FOR ACARS PER MM, OPS CK OKAY.

Part: CONTROL PANEL — FAULTY (INTERPHONE) · airframe 80,624 hrs · 12,975 cycles

CONSTANT STATIC SOUND ON CAPTS FLT INTERPHONE. REPLACED CAPT'S ASP AS PER REF MM 23-51-01. INSTALLATION TESTED OK.

Part: SEAL PLATE — DAMAGED (RUDDER) · airframe 80,202 hrs · 12,913 cycles

HYDRAULIC LEAK AT RUDDER. FOUND RUDDER RATIO CHANGER SERVO VALVE SEAL PLATE DAMAGED. REPLACED REF MM. ACP LEAK CHECK.

Part: CONTROL VALVE — FAULTY (AC BAY) · airframe 79,778 hrs · 12,853 cycles

LEFT PACK OFF LT. DEPARTURE TIME WHEN NOTED. NO PACK OFF EICAS MESSAGE WHEN TURNED OFF. REPLACED PACK FLOW CONTROL VALVE PER AMM.

Part: O-RING — LEAKING (HYD LINE) · airframe 79,239 hrs · 12,776 cycles

HYD LEAK AT LT WING GEAR AREA. REPLACED O-RING AT HYD LINE ON THE LT NORMAL ANTISKID MODULE. LEAK CHECKED NORMAL.

Part: PANEL — CRACKED (NR 1 NACELLE) · airframe 79,224 hrs · 12,774 cycles

ON WALKAROUND FOUND CRACKED PANEL ON PYLON PANEL 437AR ON INBD SIDE OF NR 1 ENG. CRACK MEASURES 3.250 LONG. REPLACED PYLON PANEL 437AR.

Part: SENSE LINE — LEAKING (RT ENGINE) · airframe 78,949 hrs · 12,735 cycles

RT DUCT PRESSURE SIGNIFICANTLY HIGHER THAN LT DUCT AT T/O AND CLIMB POWER (60-47 PSI). R & R RT PRSOV, RT DUCT PRESS TRANSDUCER, RT HPC, RT PRC REF MM, NO HELP. SUSPECT PRSOV SENSE LINE LEAKING. R & R LINE, RAN ENGINES AT HIGH POWER. DUCT PRESS NORMAL AT ALL PARAMETERS.

Part: BLADE — OUT OF TOLERANCE (ENGINE FAN) · airframe 78,949 hrs · 12,735 cycles

PROMINENT VIBRATION ON TAKEOFF UNTIL FIRST POWER REDUCTION. CREW TOLD LOCAL MECH VIBS ON ENG 2 WERE 2.8 AND ENG 1 WAS 2.4 AND THOUGHT VIB FELT WAS FROM RT ENG. CHECK INLET AND EXH AND MAIN CHIP DETECTORS OF BOTH ENG'S. CHECK FOR ANY LOOSE VIB SENSORS OR CONNECTIONS. RUN ENG'S AND REF JRH FOR VIB GUIDELINES FOR GROUND OPERATIONS. ACCOMPLISHED FAN BLADE LUBE ON NR2 ENG RAN ENG'S IAW JRH, BOTH ENG VIBS WITHIN LIMITS.

Part: VALVE — FAULTY (PNEUMATIC SYS) · airframe 78,949 hrs · 12,734 cycles

PNEUMATIC DUCT PRESSURE ON OVERHEAD ON RT SIDE VARIES BETWEEN 65-80PSI WITH INC+DEC IN PWR. CHECK AIR SUPPLY MONITOR FOR FAULTS. AIR SUPPLY BITE SHOWS FAS AND PRESSURE SENSOR FOR RT ENG BLEED SYS. DEFERRED IAW MEL AND RT ENG PRSOV DEACTIVATED IN CLOSED POSITION. CHECK AIR SUPPLY BITE MODULE FOR CURRENT AND PAST FAULTS IAW MM. BITE MODULE FAULTING RT ENG PRV EXIT PRESSURE SENSOR. CHECK SENSOR LINES, PRV CONT SENSE LINES & PRSOV SENSE LINE. CHECKED SENSE CONNECTION, SENSE LINES ON PRSOV OK. REACTIVATED PRSOV. SWAPPED PRV MR36213-403 WITH HPSOV MR36213-179. NOW MR36213-403 IN HPSOV POSITION AND MR36213-179 IN PRV POSITION. REMOVAL AND INSTALLATION IAW MM.

Part: BATTERY PACK — MALFUNCTIONED (EMERGENCY LIGHT) · airframe 78,912 hrs · 12,728 cycles

OVERHEAD EMERGENCY EXIT LIGHT ABOVE DOOR 2R TURNS ON & OFF BY ITSELF. EMERGENCY LIGHT 2R FLICKERING ON AND OFF. REPLACED BATTERY M1556 IAW MM AND ACCOMPLISHED BATTERY TEST IAW MM. OPS TEST IAW MM. EMERGENCY LIGHT SYS OK, NO FAULTS FOUND.

Part: STARTER — FROZEN (NR 1 ENGINE) · airframe 78,467 hrs · 12,660 cycles

NR1 ENG HUNG START, LT ENG STARTER AND LT ENG STARTER CUTOUT EICAS MSG. START VLV LIGHT STAYED ILLUM. EEC MAINT SW'S IN THE NORM POS. CYC'D D11, P11-4 AND START SW, NO HELP. REPLACED STARTER IAW AMM ( FOUND FROZEN) AND REPLACED STARTER CONTROL VALVE IAW AMM. MOTORED ENGINE. OP CHECKED NORMAL.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 78,341 hrs · 12,642 cycles

CEILING AISLE EMERGENCY LIGHT MISSING LENS AT LT ROW 37. FOUND AND REINSTALLED LENS.

Part: WIRE — BROKEN (SEATS 7AB) · airframe 78,341 hrs · 12,642 cycles

CEILING AISLE EMERGENCY LIGHTS INOP AT SEATS 7AB AND 8KJ. REPAIRED BROKEN WIRE AT SEATS 7AB AND RESEATED LOOSE PIN AT CONNECTOR AT SEAT 8KJ, OP CHECKS GOOD.

Part: WIRE HARNESS — DAMAGED (EMERGENCY LIGHT) · airframe 78,341 hrs · 12,642 cycles

EEL LIGHT INOP AT SEAT 6KJ. RELAMPED, BUT NO HELP. FOUND PIN PUSHED BACK AND RESECURED PIN BACK IN PLACE. OP CKD GOOD.

Part: OVEN — SMOKE (GALLEY) · airframe 77,996 hrs · 12,592 cycles

WARMING OVEN NR W13 SMOKES AND SMELLS. REPLACED WARMING OVEN R13. OPS NORMAL.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 78,039 hrs · 12,597 cycles

EXIT PATH LIGHTING ON RIGHT SIDE OF COACH ILLUMINATED. ACCOMPLISHED A TEST OF THE EMERGENCY LIGHTS, OPS CHECKED NORMAL ON GROUND.

Part: FITTING — LEAKING (HYD SYSTEM) · airframe 77,561 hrs · 12,527 cycles

NR2 HYD QTY READS XXRF. RT HYD QUAN AT .74RF AT 4.5 HOURS FLT TIME. FOUND FITTING LEAKING STEADY ON VALVE ASSY FUSE. JUST OTBD OF LT MAIN GEAR. SECURED FITTING NO LEAKS.

Part: CONNECTOR — DAMAGED (NR 1 WINDOW) · airframe 77,328 hrs · 12,498 cycles

CONNECTORS J1, J4 & J5 ON NR 1 LT WINDOW ARE DAMAGED. COVERS WILL NOT SECURE. SECURED COVERS WITH TAPE ON J1,J4,J5. CONNECTORS. REPLACED CONNECTORS. OPS CHECKS NORMAL.

Part: LENS — DISLODGED (EMERGENCY LIGHT) · airframe 76,886 hrs · 12,440 cycles

EMERGENCY LIGHT LENS AT SEAT 19JK IS FALLING OFF. REPAIRED LENS ASSY. OPS CHECKED GOOD.

Part: PUMP — INOPERATIVE (HYD SYSTEM) · airframe 76,886 hrs · 12,440 cycles

RT HYD PUMP WILL NOT OPERATE. PUMP & RELAYS NO HELP. CONT WITH TROUBLE SHOOTING. REPLACED RT ACMP AND ACMP ELCU. OPS AND LEAK CHECKED GOOD.

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 76,089 hrs · 12,325 cycles

FLIGHT DECK EMERGENCY EXIT LIGHT INOP. LIGHT ASSY FROM STOCK WAS BAD. TRIED KNOWN GOOD ASSY, OPS NORMAL. RETURNED GOOD UNIT TO AC 6671. ORDERED ANOTHER LIGHT ASSY FROM DEN. REPLACED LIGHT ASSY, FLIGHT DECK EMERGENCY LIGHT CHECK OK.

Part: COMPUTER — FAILED (THRUST MGMT) · airframe 75,817 hrs · 12,288 cycles

A-T FAILED TO ENGAGE. A-T MODE NOT DISPLAYED ON ADI. CREW COMMENTS: FAILED TO STAY ENGAGED DURING CRUISE. ACFT REMOVED FROM CAT III. AUTOTHROTTLES INOP AND DEACTIVATED. FAULTING A-T SERVO 1 TMC. REPLACED TMC.

Part: BATTERY PACK — FAULTY (CABIN) · airframe 75,805 hrs · 12,286 cycles

EMERGENCY LIGHTS FLICKING ON AND OFF. REPLACE BATTERY PACK M1208 AS PRECAUTION. REPLACED FLOOR MOUNTED EMERGENCY LIGHT BATTERY PACK. REMARKS-SHOULD READ M1557 IAW NEW CONFIG INSTEAD OF M1208. CHECK OPS OK.

Part: FUSE — FAILED (EMERGENCY LIGHTS) · airframe 75,805 hrs · 12,286 cycles

DURING CHECK OF EMERGENCY EXIT LIGHT NOTED THAT DOOR 1L AND 1R EXIT-THRESHOLD LIGHT INOP. FOUND M1208 POWER SUPPLY FUSE BURNED OUT ,REPLACED FUSE. OPS OKAY.

Part: GCU — MALFUNCTIONED (LEFT) · airframe 74,806 hrs · 12,137 cycles

L ENG GEN WILL NOT RESET FWD EQP SUP FAN 1. TR UNIT AND L ENG EEC C1 STATUS MSG. CARRIED OUT BITE CHK OF BPCU. INSPECTED LEFT ENG GENERATOR FEED CABLES AND GENERATOR HARNESS CONNECTOR. NO FAULTS FOUND. REPLACED GCU AND CARRIED OUT ENG RUN. OPERATES NORMALLY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 74,615 hrs · 12,112 cycles

EMERGENCY LIGHT STRIP BY G1B INOPERATIVE. REPLACED STRIP AND PERFORM OPS TEST.

Part: PRESSURE SWITCH — MALFUNCTIONED (BOOST PUMP) · airframe 74,615 hrs · 12,112 cycles

RT AFT FUEL PUMP EICAS MESSAGE IN VIEW. REPLACED RT FWD FUEL BOOST PUMP PRESS SWITCH S72. FUEL PUMPS OPS CK NORMAL AND EICAS MSG CLEARED.

Part: GCU — MALFUNCTIONED (NR 1 GENERATOR) · airframe 74,166 hrs · 12,052 cycles

LT ENG GEN DRIVE LIGHT OUT. UNIT FOUND DEFECTIVE. REPLACED GCU IN ON NR1 ENG SIDE. RAN ENG SEVERAL TIMES, NO LIGHT FAULTS. OPS CHECKS GOOD.

Part: ECU — FAULTY (APU ENGINE) · airframe 74,116 hrs · 12,046 cycles

APU AUTOSHUTSDOWN. FAULT LIGHT ON. NO ABNORMAL INDICATIONS. REPLACED APU ECU. CHECKED GEN SCAVENGE, GEARBOX, TURBINE & COMP BEARING CHIP DETECTORS. NO CONTAMINATION FOUND. SERVICED APU OIL TO FULL. REPLACED APU GEN OIL FILTER DELTA P SWITCH.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHTS) · airframe 73,870 hrs · 12,014 cycles

FLOOR EEL LIGHT INOP BETWEEN DOOR 1R AND SEAT 1K. UNABLE TO ACCESS TERMINAL ENDS TO T-S DUE TO CABIN MODIFICTION. WILL REQ AT LEAST 3 TO 4 SHIFTS TO PULL SEAT 1K TO ACCESS. SUGGEST SMB VISIT. OK TO DF, STRIP IS NOT CROSS AISLE OR NEAR ORANGE OVERLAY LIGHTS. ALL DR1L AND DR1R LIGHTS OPERATE NORMAL. RESEATED CONNECTOR ON LIGHT STR1P L290, RESECURED CARPET THEN TESTED. TEST PASSED.

Part: SWITCH — FAULTY (RT WING) · airframe 73,655 hrs · 11,984 cycles

RT WING ANTI ICE VALVE LIGHT AND EICAS ON WHEN WING ANTI ICE SELECTED. REPLACED RT WING TAI OVERHEAT SWITCH. REPLACED RT WING TAI VALVE. AFTER REPLACEMENT OPS TEST OKAY.

Part: STATOR — DEFECTIVE (EEC) · airframe 73,370 hrs · 11,939 cycles

UPON LANDING GOT 'L ENG CONTROL' EICAS MESSAGE. EICAS DISAPPEARS AFTER TOUCH DOWN BUT SHOWS ON STATUS MSG. LEFT ENGINE PMA STATOR REPLACED ACC. ALL TEST PASSED.

Part: ACCELEROMETER — MALFUNCTIONED (LT ENGINE) · airframe 72,549 hrs · 11,818 cycles

AT LEVEL OFF AFTER POWER SET AT 86 PERCENT N1. LT ENG VIB INCREASED .8 TO 3.3 THEN 2.0. VIBS FELT IN YOKE & FUSELAGE. ACCOMPLISHED BORO ON 1 AND 2ND HPT, AND 3RD STAGE LPT, NO DEFECTS FOUND. REPLACING ENG VIB PICK-UP LM2031 THAN CLOSE UP. REPLACED ACCELEROMETER. ALL CHECKS GOOD.

Part: ACTUATOR — MALFUNCTIONED (LEFT) · airframe 72,495 hrs · 11,807 cycles

CREW REPORTS UNABLE TO COOL AIRCRAFT. ON ECS PAGE RT PACK PUTTING OUT 19 DEGREE AIR WITH RAM DOOR FULL OPEN. LT PACK PUTTING OUT 70 DEGREE AIR BUT RAM DOOR IS ONLY HALFWAY OPEN. OPERATING ONLY RT PACK ON THE GROUND, AS WELL AS GOING BETWEEN AUTO-STANDBY MODES, AND TURNING MASTER TRIM AIR OFF, NO HELP. REPLACED LT RAM AIR INLET ACTUATOR AS INDICATED BY BITE TEST. IN ADDITION LT PACK CONT REPLACED. PACK OPS OK IN STBY. THE CONTROLLER STILL FAULTS THE INLET ACTUATOR. REPLACED LT PACK TEMP CONTROLLER. NO HELP, STILL HITS RAM INLET ACTUATOR. DUE LT PACK BITE ACCOMPLISHED AND CONFIRMED FAULT OF RAM AIR PACK ACTUATOR, REPLACED ACTUATOR A SECOND TIME, CHECK OPS OK.

Part: OXYGEN MASK — FAULTY (COCKPIT) · airframe 72,426 hrs · 11,794 cycles

CREW OXYGEN MASK PROBLEM. POSITION 1 (1=CAPT,2=FO, 3=1ST OBS, 4=2ND OBS). CREW COMMENTS: OPEN WIRE, REPLACED CAPTAIN'S O2 MASK.

Part: HOSE — LEAKING (NR 1 ENGINE FUEL) · airframe 72,017 hrs · 11,732 cycles

NR 1 ENG FUEL LEAK ON TOP OF ENGINE. MAIN FUEL SUPPLY HOSE ASSY LEAKING. NEED HOSE ASSY. REPLACED MAIN FUEL LINE. ACP'D INSTALLATION INSPECTION OF MAIN FUEL LINE. LEAK CHECK GOOD.

Part: GEARBOX — WORN (LT ENGINE) · airframe 71,968 hrs · 11,723 cycles

LEFT ENGINE ANGLE GEARBOX LT PIN FOUND MIGRATED EXPOSING APPROXIMATELY 0.428 IN TOTAL LENGTH MEASURED FROM PIN TIP TO BUSHING ON GEARBOX CASING APPROX 0.985 IN. AFTER LUBRICATION PIN WAS PUSHED BACK UNTIL ONLY APPROX 1-16 IN EXPOSED. PIN HAS BEEN PRESSED BACK INTO HOUSING AND RESEATED WITH APPROX 0.060 PROTRUSION. ANGLE GEARBOX TO BE REPLACED. REPLACED ANGLE GEARBOX, DRIVE SHAFT AND DRIVE SHAFT HOUSING.

Part: MODULE — FAILED (RT STAB TRIM) · airframe 71,641 hrs · 11,667 cycles

STAB TRIM LIGHT AND EICAS DISPLAYED. ABLE TO ISOLATE WITH THE CUTOUT SWITCHES, TO FAIL WITH THE RT STAB-TRIM AILERON MODULE. REPLACED RT STAB TRIM-AILERON LOCKOUT MODULE, CHECKS OKAY.

Part: ACTUATOR — FAULTY (AILERON) · airframe 71,585 hrs · 11,658 cycles

AILERON LOCKOUT MESSAGE. REMOVED & REPLACED RT OUTBOARD AILERON LOCKOUT ACTUATOR. OPS CHECK GOOD.

Part: FSEU — FAULTY (TE FLAP) · airframe 71,580 hrs · 11,657 cycles

AILERON LOCKOUT LIGHT ON DURING TAXI. REPLACED RIGHT STAB TRIM-AIL LOCKOUT MODULE M525 AS PRECAUTION AND REPLACED FLAP-SLAT ELECTRONICS UNIT (FSEU) BECAUSE FAULTED BY RT SAME ON INBOUND LEG. ALL UNITS CHECK OKAY.

Part: MODULE — FAULTY (RIGHT) · airframe 71,405 hrs · 11,631 cycles

AIL LOCK LT ON AT LOW SPEED. EICAS MSG AILERON LOCKOUT DISPLAYED. OTBD AILERONS INDICATED NORMAL, UNLOCKED. REPLACED RT STAB TRIM-AILERON LOCKOUT MODULE. OPS TEST NORMAL.

Part: DOOR — DAMAGED (LE SLAT) · airframe 71,330 hrs · 11,620 cycles

RT WING ANTI-ICE DUCT SEAL BONDED DOOR ASSY NEEDS TO HAVE INTERIM REPAIR ACCOMPLISHED REF UA-EVA-72571. ACCOMPLISHED INTERIM REPAIR TO RT WING ANT-ICE DUCT SEAL BONDED DOOR ASSY, PERFORMED OPS CHECK OF SLAT. ALL CHECKS OK. DOOR ASSY P-N 114T0201-28 PCN 161-0128 TO BE REPLACED WITHIN 100 HOURS NOT TO EXCEED PTT 71430. REPLACED PANEL. POS CHECKED SLATS AND ADJUSTED PANEL AND OK.

Part: ACTUATOR — FAULTY (RT AILERON) · airframe 71,304 hrs · 11,615 cycles

THE "AIL LOCK" LT ON AT LOW SPEED. EICAS MSG AILERON LOCKOUT DISPLAYED. OUTBOARD AILERONS DID NOT INDICATE NORMAL - LOCKED OUT - BOTH. LEFT SAM FAULTS RIGHT LOCK OUT ACTUATOR, CONFIRMED ACTUATOR AT FAULT. REPLACED RT LOCK OUT ACTUATOR. OP CHECK GOOD.

Part: ACTUATOR — FAULTY (RT AILERON TAB) · airframe 71,238 hrs · 11,605 cycles

AILERON LOCKOUT EICAS MESSAGE. REPLACED RIGHT AILERON LOCKOUT ACTUATOR AND FSEU.

Part: FAIRING — DAMAGED (NR 1 PYLON) · airframe 71,132 hrs · 11,589 cycles

NR 1 ENG PYLON TOP FWD FAIRING (SLIPPER COWL) DAMAGED DURING UNCONTROLLED REVERSER DEPLOYMENT WITH BOTH REVERSER COWLS OPEN FOR MX. ACCOMPLISHED REPAIRS IAW SRM AND UA-EVA-72462. NEEDS TO BE EXAMINED AT THE NEXT 4 CONSECUTIVE C-CKS FOR DAMAGE. REINSPECTED NR 1 PYLON TOP FWD FAIRING (SLIPPER COWL) IAW UAL EVA AT C13. NO DAMAGE OR DISCREPANCIES NOTED. OK TO CONTINUE FOR REINSPECTIONS AT NEXT 3 CONSEQUTIVE CKS TO C16. 085625 DOCUMENTED ON NON ROUTINE 23626.

Part: THRUST REVERSER — MALFUNCTIONED (NR 1 ENGINE) · airframe 71,132 hrs · 11,589 cycles

NR 1 ENG PYLON TOP FORWARD FAIRING (SLIPPER COWL) DAMAGED DURING UNCONTROLLED REVERSER DEPLOYMENT WITH BOTH REVERSER COWLS OPEN FOR MAINTENANCE. ACCOMPLISHED REPAIRS PER SRM 54-53-71 AND UA-EVA-72462. NEED TO BE EXAMINED AT THE NEXT 4 CONSECUTIVE C-CKS FOR DAMAGE.

Part: VALVE — FAULTY (THRUST REVERSER) · airframe 71,132 hrs · 11,589 cycles

NR 1 ENG THRUST REVERSER ACTIVATED WITH LOCK OUT PIN INSTALLED IN ISOLATION VALVE. FURTHER TESTING SHOWS AN INTERNAL FAILURE OF ISOLATION VALVE. REPLACED STOW VALVE PER MM 78-34-10.

Part: O-RING — LEAKING (EVAC SLIDE)

LOW PRESSURE. LEAKING AT GAUGE. REMOVED & REPLACED GAUGE O-RING.

Part: BARREL — DEFECTIVE (EVAC SLIDE)

LOW BOTTLE PRESSURE. BARREL NOT SEALING. REPLACED BARREL.

Part: BARREL — LEAKING (ASPIRATOR)

LOW BOTTLE PRESSURE. BARREL NOT SEALING. REPLACED BARREL.

Part: ACTUATOR — DISCONNECTED (NR 1) · airframe 69,874 hrs · 11,419 cycles

L ENG EEC C1 AND L ENG CONTROL STATUS MESSAGES ON THE WAY TO THE GATE. INSTALLED NEW SVA NR 1 ENG. INSTALLED NEW SVA NR 1 ENG.

Part: LIGHT — SHORTED (P40 PANEL) · airframe 69,680 hrs · 11,391 cycles

APU FIRE PROTECTION SYSTEM INOP. REPLACED APU FIRE BOTTLE. FOUND FIRE BOTTLE ARM LIGHT ASSY SHORTED ON P40 PANEL. REPLACED LIGHT ASSY L542, CHECKS NORMAL.

Part: ENGINE — FAULTY (NR 1) · airframe 69,627 hrs · 11,383 cycles

NR 1 ENG FAULTY.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 68,802 hrs · 11,268 cycles

THE 'L OIL FILTER' STATUS MSG DISPLAYED.

Part: WEB — CRACKED (NR 2 NACELLE) · airframe 68,486 hrs · 11,219 cycles

NR 2 PYLON NAC STA 180 (APPROX) RIGHT SIDE, UPPER WEB CRACKED INTO RIVET HOLE. MAJOR REPAIR ACCOMPLISHED. REMOVED OLD DOUBLER. INSTALLED NEW DOUBLER REPAIR.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 68,486 hrs · 11,219 cycles

BULK CARGO COMPARTMENT AT STA 1562 BETWEEN STR 39R AND 39L, SHEAR TIE HAS CORROSION AROUND DRAIN HOLE AFT SIDE. MAJOR REPAIR ACCOMPLISHED. REPLACED SHEAR TIE.

Part: TORQUE BOX — CORRODED (FUSELAGE) · airframe 68,486 hrs · 11,219 cycles

AFT PIT, PITTING CORROSION IN TOP SURFACE OF TORQUE BOX STA 1345, RBL 8. MAJOR REPAIR ACCOMPLISHED. REMOVED CORROSION & FOUND TO BE OUT OF LIMITS. REMOVED WEB. FABRICATED & INSTALLED NEW WEB.

Part: FRAME — DAMAGED (BS 1197) · airframe 68,486 hrs · 11,219 cycles

AFT PIT STA 1197+66 FRAME CAP HAS FLAKED PAINT AND LIGHT SURFACE CORROSION FROM LBL 48 - RBL 10. MAJOR REPAIR ACCOMPLISHED. INSTALLED NEW FRAME CAP.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 68,486 hrs · 11,219 cycles

AFT PIT, UPPER CHORD FOR WEB AT STR 33L CORRODED ON THE LOWER SURFACE. *S/D* MAJOR REPAIR ACCOMPLISHED. INSTALLED NEW ANGLE.

Part: CONNECTOR — DAMAGED (HYD PUMP) · airframe 68,486 hrs · 11,219 cycles

RIGHT ACMP CONNECTOR D486P, PIN 'B' IS BURNED, SHOWS SIGNS OF ARCING. REPLACED RIGHT ACMP CONNECTOR D486P PIN "B". OPS CHKS NORMAL.

Part: SEAT TRACK — CORRODED (BS 795 LBL 62) · airframe 68,486 hrs · 11,219 cycles

CORROSION ON SHORT SEAT TRACK AT BS 795, LBL 62. MAJOR REPAIR ACCOMPLISHED. INSTALLED NEW SEAT TRACK SECTION.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 68,486 hrs · 11,219 cycles

AFT RIGHT EMERGENCY EXIT LIGHT DOOR HANDLE IS INOP. RELAMPED. OPS CHECKS GOOD.

Part: SHEAR TIE — CORRODED (BS 1219) · airframe 68,486 hrs · 11,219 cycles

AFT PIT AT STA 1219, LBL 4 - RBL 4, CORROSION ON ANGLE AT FRAME ATTACH TO SKIN. *S/D* MAJOR REPAIR ACCOMPLISHED. FABRICATED & INSTALLED NEW SHEAR TIE.

Part: STRUCTURE — CORRODED (BS 1197 S33L) · airframe 68,486 hrs · 11,219 cycles

AFT PIT CORROSION ON FRAME CAP LOWER SURFACE AT BS 1197+110 AND STR 33L. *S/D* MAJOR REPAIR ACCOMPLISHED. REPLACED "T" CAP.

Part: ANGLE — CORRODED (BS 1394) · airframe 68,486 hrs · 11,219 cycles

AFT PIT STA 1394, BL 0, CORROSION ON ANGLE AT FRAME ATTACH TO SKIN. *S/D* MAJOR REPAIR ACCOMPLISHED. REPLACED SHEAR TIE.

Part: WEB — CRACKED (NR 1 PYLON) · airframe 68,486 hrs · 11,219 cycles

NR 1 PYLON STA 156 WEB AT OUTBOARD DRAIN HOLE IS CRACKED, MIGRATED BEYOND EXISTING STOP DRILL. MAJOR REPAIR ACCOMPLISHED. FOUND 2 CRACKS AT INBOARD DRAIN HOLE. STOP DRILLED CRACKS. FABRICATED & INSTALLED A DOUBLER REPAIR.

Part: FLOORBEAM — CORRODED (BS 1518) · airframe 68,486 hrs · 11,219 cycles

MAIN CABIN FLOORBEAM T-CAP CORRODED UNDER STEEL SUBFLOOR AT BS 1518 AT BL 0. MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGED T-CAP SECTION. FABRICATED AND INSTALLED A NEW T-CHORD, SPLICE ANGLES & SPLICE STRAPS.

Part: FLOORBEAM — CORRODED (BS 1502) · airframe 68,486 hrs · 11,219 cycles

MAIN CABIN FLOORBEAM T-CAP CORRODED AT BS 1502 AND LBL 28. *S/D* MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGED SECTION OF T-CAP. FABRICATED A-1 AND -2 REPAIR ANGLES, -3 STRAP AND 4 EACH SHIM AND INSTALLED.

Part: STIFFENER — CRACKED (STA 246) · airframe 68,486 hrs · 11,219 cycles

STA 246 FLOORBEAM FWD SIDE VERT STIFFENER CRACKED AT LBL 26. MAJOR REPAIR ACCOMPLISHED. REMOVED AND INSTALLED NEW STIFFENER.

Part: FLOORBEAM — CORRODED (BS 284) · airframe 68,486 hrs · 11,219 cycles

CABIN FLOORBEAM FRAME CORRODED STA 284 RBL 17. *S/D* MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGED SECTION OF FLOORBEAM TEE AND FABRICATED A NEW TEE REPAIR ANGLE. DAMAGED T-CAP REMOVED BETWEEN RBL 17 - RBL 22 AND WL 208.

Part: CONNECTOR — DAMAGED (CARGO BAY) · airframe 68,486 hrs · 11,219 cycles

FWD CARGO COMP BELOW FLOOR-EQUIP COOLING SUPPLY AIR OVERHEAT SWITCH CONNECTOR WIRE HAS INSULATOR DAMAGE AND BARE CONDUCTOR EXPOSED 19 INCHES UPSTREAM OF CONNECTOR D00644. REPAIRED WIRE IAW BSWPM 20 -30-12 AND OPS CHECKED GOOD.

Part: WIRE — DAMAGED (SWITCH CONNECTOR) · airframe 68,486 hrs · 11,219 cycles

FWD CARGO COMP BELOW FLOOR-EQUIP COOLING SUPPLY AIR OVERHEAT SWITCH CONNECTOR WIRE HAS INSULATOR DAMAGE AND BARE CONDUCTOR EXPOSED 19 INCHES UPSTREAM OF CONNECTOR D00644.

Part: GROUND WIRE — DAMAGED (HEATER TAPE) · airframe 68,486 hrs · 11,219 cycles

BARE WIRE EXPOSED AT TOP LEFT BURNDY BLOCK CONNECTION, HEATER TAPE GROUND, APPROX LOCATION AFT SIDE OF FLOORBEAM STA 266.5, LBL 68. REPLACED B97 HEATER TAPE GROUND WIRE.

Part: SPRING — WEAK (R1 DOOR) · airframe 68,486 hrs · 11,219 cycles

R-1 DOOR DEPLOYMENT BAR GAS SPRING WEAK. REPLACED SPRING. OPS OKAY FOR SERVICE.

Part: LATCH — GOUGED (RT O/W SLIDE) · airframe 68,486 hrs · 11,219 cycles

RIGHT OVERWING SLIDE COMPT DOOR LATCH NR 1 SLIDER GOUGED. FOUND NR 1 LATCH GOUGED. REPLACED LATCH. OPS CHECKS GOOD.

Part: CYLINDER — INOPERATIVE (L2 DOOR) · airframe 68,486 hrs · 11,219 cycles

L-2 DOOR MANUAL DEPLOY GAS CYLINDER INOP.

Part: SPRING — FAULTY (L2 DOOR) · airframe 68,486 hrs · 11,219 cycles

L-2 DOOR MANUAL DEPLOY GAS CYLINDER INOP. REPLACED GAS SPRING.

Part: LATCH — GOUGED (RT O/W SLIDE) · airframe 68,486 hrs · 11,219 cycles

RIGHT OVERWING SLIDE COMPARTMENT DOOR LATCH NR 3 SLIDER GOUGED. FOUND NR 3 LATCH GOUGED. REPLACED LATCH. OPS CHECKS GOOD.

Part: HOUSING — CRACKED (LT OWING SLIDE) · airframe 68,486 hrs · 11,219 cycles

LT OVERWING DISCONNECT HOUSING CRACKED. REMOVED & REPLACED DISCONNECT HOUSING.

Part: TRANSMITTER — MALFUNCTIONED (TE FLAPS) · airframe 67,946 hrs · 11,129 cycles

FLIGHT CREW REPORT SLIGHT SPLIT BETWEEN LEFT AND RIGHT T/E FLAP INDICATOR NEEDLES NORMAL AT 1 AND 25 BUT SLIGHT SPLIT AT UNITS 5, 10 & 15. REPLACED LEFT FLAP POSITION TRANSMITTER NR 1 PER AMM CH 27-51-45 OP CHECK NORMAL. AC OK FOR SERVICE.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHTS) · airframe 66,046 hrs · 10,849 cycles

EMERGENCY EEL LIGHT INOPERATIVE AT SEAT 5AB. SECURED CONNECTOR.

Part: SMOKE GOGGLES — CRACKED (COCKPIT) · airframe 66,031 hrs · 10,847 cycles

CAPTAIN'S SMOKE GOGGLES BROKEN AND CRACKED. REPLACED GOGGLES. ACFT OK FOR SERVICE.

Part: STRUCTURE — LEAKING (LT WING) · airframe 64,049 hrs · 10,515 cycles

LEFT MAIN FUEL QTY DECREASED WITH LT CENTER FUEL PUMP ON AND 30,000 LBS IN CENTER TANK. AFTER TROUBLESHOOTING, FOUND LT FUEL TANK DRY BAY HAS RUNNING FUEL LEAK. RESEALED LEAK AT BOTTOM STRINGER BETWEEN LEFT TANK AND OUTBOARD OF DRYBAY AT 1700. ACCOMPLISHED LEAK CHECK; NO LEAKS. FUEL BALANCED. ACCOMPLISHED ADDÕL TROUBLESHOOTING ON LAYOVER; NO FAULTS NOTED. CHANGED LEFT CENTER TANK OVERRIDE PUMP PRECAUTIONARY. NO FURTHER REPORT OF FUEL IMBALANCE PROBLEM.

Part: INDICATOR — FAULTY (COCKPIT) · airframe 64,012 hrs · 10,508 cycles

FLAP INDICATOR NEEDLES OUT OF LIMITS FOR FLAPS 5, 15 & 20. CHECKED FLAP POSITION TRANSMITTER NR 1 AND NR 8 RIGGING FOUND OK. CLEANED TRANSMITTER CANNON PLUGS. EXTENDED AND RETRACTED FLAPS SEVERAL TIMES USING NORMAL AND ALTERNATE MODES. BOTH IND. NEEDLES FOLLOWING THE RELATED FLAP LEVER DETENT POSITION WITHOUT DISAGREE. UNABLE TO DUPLICATE PROBLEM.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 63,864 hrs · 10,484 cycles

FWD CARGO PIT, FOUND CORROSION ON ANGLE FRAME INSIDE NEXT TO ROLLOUT STOP 3RD FROM MOST FORWARD POSITION AT STA 575. 08-31-07 REMOVED CORROSION VERIFIED MATERIAL LOSS WITHIN LIMIT. OK FOR SERVICE.

Part: HOUSING — LEAKING (NR 1 DRIP STICK) · airframe 63,864 hrs · 10,484 cycles

CREW REPORT: FUEL BALANCE EXCEEDED 1400 LBS DURING 4 HOUR FLIGHT. TURNED ON ALL FUEL PUMPS & CHECKED FUEL TANK QTY AFTER 1 HOUR. NO LEAKS OR UNWANTED FUEL TRANSFER NOTED. CHECKED PER MM 28-11-95. LOCATED LEAK NEAR RT CTR AUX FUEL DRIP STICK NR 1 HOUSING. REPLACED NR 1 STICK HOUSING. LEAK CHECKED OK. NO ADD'L UNWANTED FUEL X-FER REPORTED IN PAST 21 DAYS.

Part: WIRE HARNESS — DAMAGED (GALLEY) · airframe 63,647 hrs · 10,452 cycles

ELECTRICAL BURNING ODOR WITH SMOKE FROM MID GALLEY (416) AFT COUNTER HOTPLATE AREA. C/B FOR HOTPLATE H41 HAS BEEN PULLED AND BURNING ODOR AND SMOKE HAS DISSIPATED. HOTPLATE WAS NOT HOT BUT AREA AROUND HOTPLATE WAS HOT, POSSIBLE DAMAGED WIRING HARNESS. [08-17-07] REMOVED AND INSPECTED THE BACK OF HOTPLATE FOR ANY BURNED WIRING OR ODOR. NOTHING FOUND. RT PLATE HAD A LOT OF PLASTIC BURNED ON TOP OF IT. CLEANED IT. HOTPLATE INOPERATIVE FOR THREE DAYS. WHEN DOMESTIC AGAIN, OPERATED HOTPLATE. NO ADDITIONAL ODOR. HOT PLATE & AIRPLANE RETURNED TO SERVICE.

Part: HOSE — DAMAGED (ESCAPE SLIDE) · airframe 63,572 hrs · 10,437 cycles

RIGHT OFF WING ESCAPE SLIDE INFLATION HOSE FROM INFLATION CYLINDER IS CONTAMINATED WITH HYDRAULIC FLUID AND IS DETERIORATED. [08-08-07] HOSE IS DETERIORATED AND WALLS HAVE COLLAPSED FROM LONG TERM CONTACT WITH HYDRAULIC FLUID. REPLACED HOSE ASSY. SLIDE AND AIRCRAFT OK FOR SERVICE.

Part: LIGHT — DAMAGED (CABIN) · airframe 63,226 hrs · 10,375 cycles

EMERGENCY FLOOR LIGHTING IN 1ST CLASS HAS BEEN TORN OFF OF FLOOR BY CATERING. [07-03-07] REPLACED EMERGENCY FLOOR LIGHTING.

Part: PLACARD — LOOSE (CABIN) · airframe 63,200 hrs · 10,369 cycles

EMERGENCY EXIT SIGN RIGHT SIDE LOOSE BETWEEN FIRST AND BUSINESS CLASS. [07-03-07] REPOSITIONED PHOTO LUMINESCENT AISLE PATH REF TO MM 33-50-99, CKD OKAY.

Part: POWER SUPPLY — SHORTED (SEAT 5C) · airframe 62,849 hrs · 10,314 cycles

SEAT 5C ARMREST GETTING HOT. *S/D* TROUBLESHOOTING, DISCOVERED PAX HAD SPILLED GLASS OF CHAMPAGNE OVER ARM REST. CONDUCTIVE LIQUID CAUSED INTERNAL SHORTING. C/B`S POPPED. DISCONNECTED LUMBAR CONTROL & POWER TO SEAT. REPLACED LUMBAR SWITCH PCU PCN 560-4142 AND INSEAT POWER SUPPLY PCN 585-5187. OPS CHECK, OK.

Part: TAIL CONE — PUNCTURED (FUSELAGE) · airframe 62,758 hrs · 10,295 cycles

TAIL CONE 18 INCH PUNCTURE AT STA 1898. [SUP 05-16-07] MAJOR REPAIR ACCOMPLISHED: MANUFACTURED & INSTALLED STRUCTURAL FILLERS AND DOUBLER REPAIR.

Part: FEEDER CABLE — LOOSE (EMERGENCY LIGHTS) · airframe 61,968 hrs · 10,146 cycles

FOUND RT SEATS 29FG-35FG EEL LIGHTS INOP. FOUND FEEDER CABLE CONNECTING TO EEL TRACK LOOSE. RECONNECTED CABLE. OPS CHECKS NORMALLY.

Part: PIN — SHEARED (OVERWING SLIDE) · airframe 61,968 hrs · 10,146 cycles

RT OVERWING SLIDE PACK GUIDE PIN FOUND SHEARED WHEN SLIDE WAS REMOVED, AND REQUIRES A NEW INSERT. SUPPLEMENTAL DATA UPDATE, INSTALLED INSERT IN SLIDE PACK DOOR USING RMS5-28TY7, REF BOAC DRWG 416T2024. INSTALLED GUIDE PIN. AC RETURNED TO SERVICE STATUS.

Part: SLIDE — UNRELIABLE (LT OVERWING) · airframe 61,968 hrs · 10,146 cycles

FOUND PRESSURE LINE FOR LT OVERWING SLIDE AT BS 1153 IS KINKED AT BEND. REPLACED SLIDE. OK FOR SERVICE. SLIDE PROBLEM ROOT CAUSE: SUSPECT PRESSURE LINE MISROUTED DURING REFURBISHMENT & INSTALLATION RESULTING IN DOWNWARD LOAD ON LINE.

Part: SLIDE — UNRELIABLE (RH OVERWING EXIT) · airframe 61,968 hrs · 10,146 cycles

RT OVERWING EXIT SLIDE, FOUND TO BE UNLACED DURING THE FIRST OPENING OF OVERWING SLIDE DOOR FOR INTEGRATOR TEST. REPLACED SLIDE. READY FOR SERVICE. SLIDE PROBLEM ROOT CAUSE: SUSPECT IMPROPER CINCHING DURING SLIDE REFURBISHING & REINSTALLATION AGGRAVATED BY VIBRATION.

Part: FEEDER CABLE — BROKEN (EMERGENCY LIGHTS) · airframe 61,968 hrs · 10,146 cycles

FOUND LT 1ST CLASS EEL LIGHTS INOPERATIVE. REPAIRED BROKEN EEL CABLE. OPS CHECKS NORMALLY.

Part: LATCH — FAULTY (OVERWING DOOR) · airframe 61,968 hrs · 10,146 cycles

LT OVERWING COMPARTMENT DOOR LATCH FAILED INTEGRATOR TORQUE TEST AT 275 INCH-LBS. REPLACED 4 SLIDE LATCHES PER MM25-65-09. DOOR TORQUE CHECK GOOD. LATCHES CHATTER IN LOCKED POSITION AND A FRET CHANNEL DEVELOPS OVER TIME.

Part: CABLE — DISCONNECTED (DOOR 1R & 2R SLI) · airframe 61,968 hrs · 10,146 cycles

FOUND DOORS 1R AND 2R SLIDE AFT CABLES DISCONNECTED FROM PACK BOARD. DOOR 1R & DOOR 2R SLIDES, AFT CABLES DISCONNECTED FROM PACK BOARD. BY-093796. REINSTALLED CABLES ON BOTH. OK FOR SERVICE. SLIDE PROBLEM ROOT CAUSE: SUSPECT IMPROPERLY CONNECTED DURING REFURBISHMENT.

Part: O-RING — FAILED (LT SLIDE BOTTLE) · airframe 61,968 hrs · 10,146 cycles

LEFT OFF-WING SLIDE CYLINDER HAS LOW BOTTLE PRESSURE AND WHITE INDICATOR IS NOT IN THE ARM INDICATOR WINDOW. REPLACED CYLINDER PER MM 25-65-02. A/C READY FOR SERVICE. SUSPECT O'RINGS LEAKING DUE TO HARDENING.

Part: OXYGEN BOTTLE — UNDERSERVICED (CREW) · airframe 61,769 hrs · 10,114 cycles

FOUND CREW OXYGEN PRESSURE BELOW LIMITS. SERVICED CREW OXYGEN CYLINDER. HOLDS PRESSURE; OK FOR RETURN TO SERVICE. SUSPECT PERIODIC CHECKING BY CREW DEPLETES SUPPLY.

Part: OIL SYSTEM — LEAKING (LT ENGINE) · airframe 61,753 hrs · 10,112 cycles

DURING CLIMB TO FL 350 QTY DECREASED TO 0 CURRENTLY LEVEL AT FL350 SHOWING 0 OIL QTY L ENG.

Part: UNKNOWN — SMOKE (NR 2 ENGINE) · airframe 61,719 hrs · 10,108 cycles

AFTER NR 2 ENG START GROUND REPORTED SMOKE FROM BOTTOM OF ENG COWL. ENG SHUTDOWN BY CREW. SECOND START ATTEMPT NO ROTATION AND HAD R START VLV LT PER CREW. REPLACED STARTER & STARTER VALVE. SUSPECT BEARING DRAG.

Part: TOILET — MALFUNCTIONED (LAVATORY) · airframe 58,061 hrs · 9,512 cycles

RETURNED TO IAD DUE TO A WATER LEAK IN THE MAIN CABIN. TOILET OVERFLOWED AND WATER KEPT RUNNING UNTIL CREW CLOSED LAV WATER VALVE.

Part: SLIDE — UNSERVICEABLE (OVERWING) · airframe 56,487 hrs · 9,261 cycles

DAMAGED BEARINGS. THIS TYPE OF EVENT HAS HAPPENED BEFORE AND BOEING IS WORKING ON IMPROVED FABRICATION MATERIALS TO ADDRESS THIS CONDITION. SLIDE WAS REMOVED FROM THE AIRCRAFT AND SENT TO THE COMPONENT SHOP WHERE BEARINGS WERE REPLACED.

Part: ANGLE — CRACKED (NR 1 PYLON) · airframe 56,487 hrs · 9,261 cycles

NR 1 PYLON MID SPAR AT STA 233.120 RT SIDE, ANGLE IS CRACKED AT THE 2ND FROM INBOARD ATTACH FASTENER. NR 1 PYLON MID SPAR P/N 311T3157-1 AT STA 233.120 RT SIDE, ANGLE IS CRACKED AT THE 2ND FROM INBOARD ATTACH FASTENER, VERIFIED WITH HFEC. THIS IS THE CLOSE-OUT ANGLE ON THE PYLON INBOARD SIDE, OUTBOARD FASTENER LOOKING INSIDE OF PYLON. THE CRACK IS PROBABLY CAUSED BY FATIGUE AND IT WAS REPAIRED WITH FABRICATED PYLON ANGLE.

Part: WIRE — BURNED (APU) · airframe 56,487 hrs · 9,261 cycles

EMPENNAGE INSIDE AT BS 1809 RT SIDE BELOW CENTER HORIZONTAL STAB FEEDER WIRE BUNDLES, INSULATION NOT SECURE, LOOSE ON APU FEEDER SPLICES AND FEEDER WIRES FOUND BURNT. *S/D* THE FEEDER WIRE, SPLICE AND CONNECTOR WERE REPLACED.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 56,487 hrs

EEL OVERHEAD LIGHTS AT SEATS 8B, 6B, 5B, 1B AND FWD OF 1B PLUS FWD LAV EEL LIGHT BAR INOP. *S/D* RESEATED BATTERY ON THE POWER SUPPLY.

Part: LATCH — WORN (CABIN)

R/W, O/W SLIDE COMPARTMENT, NR 4 AND 3 LATCHES ARE WORN. REMOVE AND REPLACE LATCHES IAW B767 MM25-65-98.

Part: FITTING — CRACKED (TE FLAPS) · airframe 49,750 hrs · 8,200 cycles

RT WING INBOARD FLAP, MIDDLE T/E HINGE FITTING IS CRACKED AT SPAR. INSTALLED ANGLE REPAIR.

Part: FITTING — CRACKED (TE FLAPS) · airframe 49,750 hrs · 8,200 cycles

LEFT INBOARD T/E MAIN FLAP MIDDLE AFT FLAP HINGE FITTING CRACKED ON INBOARD SIDE NEAR FLAP AFT SPAR. INSTALLED ANGLE REPAIR.

Part: STIFFENER — CRACKED (FLOORBEAM) · airframe 49,750 hrs · 8,200 cycles

STA 246 FLOORBEAM RBL 46 FWD SIDE STIFFENER CRACKED (BUCKLED). MAJOR REPAIR ACCOMPLISHED. REPLACED STIFFENER.

Part: BULB — INCORRECT (SMOKE DETECTOR) · airframe 49,750 hrs · 8,200 cycles

E&E SMOKE DETECTOR FAILS TEST. REPLACED E&E SMOKE DETECTOR. INCORRECT BULB INSTALLED. FOUND BULB ML382 INSTALLED, SHOULD BE CM382AS10.

Part: CONNECTOR — LOOSE (RT ENGINE) · airframe 49,188 hrs · 8,101 cycles

EICAS MESSAGE, RIGHT ENGINE FUEL FILTER DISPLAYED DURING CLIMBOUT. FUEL FILTER DIFFERENTIAL PRESSURE SWITCH WAS REPLACED. THE SWITCH WAS TESTED IN THE SHOP, AND FOUND TO BE SLIGHTLY OUT OF CALIBRATION, BUT NOT ENOUGH TO CAUSE THE EVENT. AS A RESULT OF SHOP FINDINGS, THE MOST LIKELY CAUSE OF THIS EVENT IS A LOOSE CONNECTOR AT THE SWITCH (FIXED DURING SWITCH REPLACEMENT).

Part: SQUIB — BLOWN (EVAC SLIDE) · airframe 49,558 hrs · 8,160 cycles

RT OVERWING SLIDE DOOR SQUIB BLOWN. SQUIB BLOWN IN CONJUNCTION WITH INADVERTANT SLIDE DEPLOYMENT. SQUIB REPLACED.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 47,896 hrs · 7,882 cycles

EMERGENCY LIGHT INOP AT DR1 FWD CROSSAISLE. REPLACED BROKEN FEEDER CABLE. OPS CKD NORMAL.

Part: COMPRESSOR — STALLED (NR 1 ENGINE) · airframe 46,225 hrs · 7,611 cycles

ABORTED TAKEOFF DUE TO NR 1 ENGINE COMPRESSOR STALL. AIRCRAFT SURGED ON TAKE OFF AT EPR ABOVE 1.25. SURGE CHECKS FOUND NO DISCREPANCY. EVENT CLASSIFIED AS A GROUP 3 SURGE DUE TO TIP CLEARANCES IN THE HPC.

Part: FRAME — BENT · airframe 43,262 hrs · 7,096 cycles

FORWARD CARGO, LEFT HAND FRAME UPPER CHORD ANGLE IS BENT,STATION 500 AND STRINGER 31L. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED.REPLACED FRAME UPPER CHORD.

Part: STRINGER — DAMAGED · airframe 43,262 hrs · 7,096 cycles

FUSELAGE STRINGER 25L AT STATION 544 HAS A DAMAGED FASTENER HOLE DUE TO LIGHTNING STRIKE. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED.REPAIRED STRINGER WITH SPLICE.

Part: WEB — CRACKED · airframe 43,262 hrs · 7,096 cycles

#1 PYLON UPPER WEB AT ELECT. WIRE BUNDLE FEED-THROUGH HAS 2 EA. CRACKS AT NUTPLATES. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED.REPAIRED WEB WITH REPAIR DOUBLER.

Part: WEB — CRACKED · airframe 43,262 hrs · 7,096 cycles

#1 ENG PYLON AFT UPPER WEB AT PNEUMATIC DUCT FEED-THROUGH IS CRACKED IN RADIUS. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. REPAIRED WEB WITH REPAIR DOUBLER.

Part: STIFFENER — CRACKED · airframe 43,262 hrs · 7,096 cycles

LEFT HAND NOSE TUNNEL AT BODY STATION 246, LBL23, VERTICAL STIFFENER CRACKED FORWARD SIDE OF FLOOR BEAM. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED.REPLACED STIFFENER.

Part: WEB — CRACKED · airframe 43,262 hrs · 7,096 cycles

#1 PYLON UPPER WEB AT GENERATOR CABLE FEED-THROUGH HAS 2 EA CRACKS AT NUTPLATES. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. REPAIRED WEB WITH REPAIR DOUBLER.

Part: PYLON — CRACKED · airframe 43,262 hrs · 7,096 cycles

#2 PYLON STRUT UPPER TORQUE BOX WEB AT GENERATOR FEED CABLE CUT-OUT IS CRACKED IN CORNER RADIUS. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED.DOUBLER INSTALLED.

Part: SKIN — DAMAGED · airframe 43,262 hrs · 7,096 cycles

LEFT FUSELAGE SKIN STATION 544, STRINGER 25L DAMAGED AT FASTENER HOLE COMMON TO TEAR STRAP DUE TO LIGHTNING STRIKE. MAJOR REPAIR ACCOMPLISHED. DOUBLER AND FILLERS INSTALLED.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 43,262 hrs · 7,096 cycles

FLOORBEAM SEAT TRACK SPLICE CRACKED AT STATION 786, LBL 10. MAJOR REPAIR ACCOMPLISHED. REPAIRED FLOORBEAM WITH REPAIR SPLICES AND FILLERS.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 43,262 hrs · 7,096 cycles

MAIN CABIN FLOOR BEAM T-CAP CORRODED STATION 850-854, LBL 48 TO LBL 52. MAJOR REPAIR ACCOMPLISHED. REPAIR ANGLE SPLICES AND SHIMS.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 43,262 hrs · 7,096 cycles

MAIN CABIN FLOOR BEAM T-CAP CORRODED STATION 850-854, RBL 48-RBL 52. MAJOR REPAIR ACCOMPLISHED. REPAIRED ANGLE-DOUBLER AND SHIMS.

Part: PACKING · airframe 38,671 hrs · 6,237 cycles

RIGHT HYDRAULIC SYSTEM MSG AND LOW QTY LIGHT ILLUMINATED, QTY DOWN TO 0.4, PUMPS TURNED OFF AND HYD FLUID LOSS MINIMIZED. RETURN TO FIELD OVERWEIGHT LANDING. SUPPLEMENTAL DATA UPDATE REPLACED PACKING OF CASE DRAIN FILTER DIFFERENTIAL PRESSURE INDICATOR. OPS CHECK, NO MORE LEAKAGE FOUND.REFILLED RIGHT HYDRAULIC RESERVOIR.

Part: COVER — OUT OF ADJ (CABIN) · airframe 37,324 hrs · 6,014 cycles

EMERGENCY LIGHTS REMAIN DISARMED WITH COCKPIT CONTROL SWITCH IN ARMED POSITION. SUPPLEMENTAL DATA UPDATE ADJUSTED SWITCH COVER, OPS CHECK OKAY.

Part: MOTOR — FAILED (CABIN PRESSURE) · airframe 6,302,001 hrs · 5,897 cycles

BOTH PRESSURE CONTROLLERS FAILED. DESCENDED TO FL180. OPERATED NORMALLY IN MAN MODE. *S/D* 3/27/01 AT LHR, AUTO PRESS SYSTEM NR 2 WAS DEFERRED INOP. ACFT FLEW TO ORD WITH NO PRESSURIZATION FAULTS. DURING ORD-IAD LEG, FLIGHT CREW REPORTED FAILURE OF BOTH AUTO CABIN PRESSURE CONTROLLERS. REPLACED NR 2 AC MOTOR. 3/29/01: DF534 WAS CREATED FOR AUTO PRESS SYSTEM NR 2. BITE ON BOTH NR 1 & 2 CPC SHOWED NR 2 AC MOTOR FAULT. 4/5/01: REPLACED NR 2 AC MOTOR (MR21324-142 OFF, -80 ON). ENGINEERING CALLOUT (EG3456) ACCOMPLISHED ON 4/18/01, PERFORMED WIRE CHECKS BETWEEN AC MOTORS AND CABIN PRESS CONTROLLERS. NO DISCREPANCIES WERE FOUND.

Part: CENTERING CAM — MISINSTALLED (NLG) · airframe 32,867 hrs · 5,211 cycles

AFTER TAKEOFF FLIGHT EXPERIENCED A CONFIGURATION SYSTEM WARNING HORN. WOULD NOT RESET. AIRCRAFT RETURNED TO JFK. ON FIRST APPROACH WITH FLAPS AT 30 THE FLAPS MOVED TOWARD UP, UNCOMMANDED. *S/D* NOSE GEAR STRUT WAS SERVICED WITH NEW SEALS IN JFK. CENTERING CAM WAS INADVERTENTLY INSTALLED 180 OUT WHICH PREVENTED NOSE GEAR AIR/GROUND SIGNAL TO READ AIR MODE ON SUBSEQUENT FLIGHT. CENTERING CAM WAS REPOSITIONED IN MIAMI.

Part: CENTERING CAM — DAMAGED (NOSE GEAR) · airframe 32,870 hrs · 5,212 cycles

FLAP INDICATION EICAS. DIVERTED TO MIA. *S/D* AN IMPROPERLY INSTALLED NOSE LANDING GEAR CENTERING CAM DID NOT ALLOW PROPER NOSE GEAR COMPRESSION, CAUSING CONFIGURATION WARNING LIGHTS TO APPEAR ON EICAS. REPLACED THE NOSE LANDING GEAR CENTERING CAM WITH NEW CAM. NOTE THAT THERE WAS NO PART DEFECT. CAM WAS IMPROPERLY INSTALLED.

Part: UNKNOWN — ODOR (NR 2 ENGINE) · airframe 32,306 hrs · 5,100 cycles

NR 2 ENGINE REPLACEMENT REQUIRED DUE TO OIL SMELL IN THE CABIN. LAV SMOKE DETECTOR ACTIVATED. RTF, OVERWEIGHT LANDING. ACCOMPLISHED OIL SYSTEM VACUUM AND PRESSURE CHECKS AND EXTENSIVE TEST CELL RUNS WITH NOTHING FOUND. ENGINE WAS RETURNED TO SERVICE AND HAS OPERATED OVER 2500 HOURS ON ANOTHER AIRCRAFT WITH NO REPORTS OF OIL ODOR OR SMOKE IN THE CABIN.

Part: PSEU — MALFUNCTIONED (MLG) · airframe 31,954 hrs · 5,040 cycles

AIR-GND DISAGREE, NOSE AIR GND DISAGREE AND LDG GEAR MONITOR EICAS MSG''S DISPLAYED AFTER TAKEOFF. ALSO HAD AUTO THROTTLE DISCONNECT, TAIL SKID MSG, PROBE HEAT. ALL EICAS MSG''S CLEARED EXCEPT AIR-GND DISAGREE, NOSE AIR GND DISAGREE AND LDG GEAR MONITOR. DIVERTED TO ORD. *S/D* REPLACED PROXIMITY SWITCH ELECTRONIC UNIT.

Part: BATTERY — DAMAGED (BATTERY BAY) · airframe 30,547 hrs · 4,817 cycles

RTF WITH MAIN BATTERY EICAS MESSAGE. *S/D* REPLACED MAIN BATTERY, CHECK NORMAL.

Part: SENSOR — OUT OF ADJUST (E/E DOOR)

TAKEOFF ABORTED AT 110 KNOTS. *S/D* E AND E COMPARTMENT DOOR WARNING ILLUMINATED. REPLACED AND ADJUSTED E AND E DOOR CLOSED SENSOR S201 PER MM, GROUND OPS CHECKS OK.

Part: BATTERY — DISCHARGED (CABIN)

EMERGENCY EXIT FLOOR LIGHTING IN RIGHT SIDE OF CABIN ROWS 21 TO 29 COMES ON INTERMITTENTLY. *S/D* THE CAUSE OF THE INTERMITTENT EEL WAS FOUND TO BE A BAD BATTERY ASSEMBLY. UAL CORRECTED THE PROBLEM BY REPLACING THE BATTERY ASSEMBLY WITH AN OVERHAULED, RECHARGED UNIT. NO PROBLEMS HAVE OCCURED SINCE THE REPLACEMENT, SYSTEM OPERATES NORMALLY.

Part: FIRE CARD — FAILED (RT ENGINE)

RIGHT ENGINE NR 1 FIRE LOOP STATUS MESSAGE DISPLAYS CONTINUOUSLY. *S/D* PROBLEM CAUSED BY A FAULTY AUTOMATIC FAULT AND LOGIC TEST CARD (AFOLTS). REPLACED CARD, SYSTEM OPS CHECKS GOOD.

Part: BLEED VALVE — CORRODED (LT ENGINE)

ABORTED TAKEOFF DUE TO LEFT ENGINE OVERTEMP. *S/D* THE 2.95 BLEED SOLENOID VALVES REMAINED OPEN AT HIGH POWER DUE TO INTERNAL CORROSION IN THE 2.95 BLEED VALVES. THIS LED TO THE LEFT ENGINE OVER TEMP CONDITION. THESE VALVES ARE CURRENTLY UNDERGOING AN UPGRADE TO NON-CORROSIVE MATERIAL.

Part: STRIP — INOPERATIVE (CABIN)

EMERGENCY EVACUATION LIGHTING STRIP AT CLOSET INOPERABLE. REPAIRED EEL STRIP.

Part: BUSHING — FAILED (SHAFT HOUSING)

ABORTED TAKEOFF AT 70 KNOTS DUE TO BLEED VALVE EICAS MESSAGE. *S/D* A FAILED NITRONIC BUSHING CAUSED THE BLEED VALVE EICAS MESSAGE. THE LEFT HIGH PRESSURE SHUTOFF VALVE WAS REPLACED, OPERATIONS CHECK NORMAL.