N651UA

Part: HEAT EXCHANGER — LEAKING (NR 2 ENGINE) · airframe 131,965 hrs · 20,201 cycles

RIGHT ENG LOST QTY AND PRESS. BOTH WENT TO ZERO. EICAS ENG OIL PRESS R CREW REPORTED QUICK DROP OF OIL QUANTITY ALONG WITH DECREASING OIL PRESSURE AND ENG WAS SHUTDOWN. ENG WINDMILL TIME APPROXIMATELY 25 MINUTES WITH ZERO PSI & ZERO QTY OBSERVED. INSPECT PER AMM 72-00-00-206-019-N01. RT ENG OIL SERVICING TO FULL DONE, 32 QTS ADDED THIS IS FOR RT ENG, ENG 2 FOUND LEAK ON AIR OIL HEAT EXCHANGER , REPLACED PER AMM 79-21-09 PB 401 , DRY MOTORING CARRIED OUT, ENG RUN GROUND IDLE TEST 3 PERFORMED IAW AMM 71-00-00-795-003-N00. NO LEAKS FOUND ON ENG 2 AIR OIL HEAT EXCHANGER. OIL QTY & PX STABLE AT IDLE, ALL INDICATION OK. ABNORMAL EVENT SNAPSHOTS SENT TO ESCPP. WINDMILL INSP CARRIED OUT, REF LP 6744430, NO FAULTS FOUND. WITH CONSULTATION WITH TOMC AND POWERPLANT AIRCRAFT SERVICEABLE.

Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 131,626 hrs · 20,160 cycles

OPERATIONAL TEST - EMERGENCY ESCAPE PATH LIGHTING (EEL) SYSTEM PERFORM OPERATIONAL CHECK - OBSERVED EMERGENCY LIGHT AT SEAT 37F AND 31D INOPERATIVE. REMOVED AND REPLACED REF CMM 25-21-53 OPS CHECK GOOD SYSTEM FOR SERVICE.

Part: TRANSMITTER — FAULTED (NR 1 OIL QTY) · airframe 131,596 hrs · 20,157 cycles

LEFT ENGINE AT ZERO OIL QTY AT TAKEOFF. REMOVED AND REPLACED NR 1 ENG OIL QUANTITY TRANSMITTER IAW AMM 79-31-01. PERFORMED IDLE RUN ON BOTH ENGINES. OPS CHECKED GOOD, OIL QUANTITY DISPLAYS AS NORMAL.

Part: AUTOTHROTTLE SYS — MALFUNCTIONED · airframe 131,519 hrs · 20,145 cycles

AUTOTHROTTLES WOULD NOT ENGAGE WHEN AUTOTHROTTLE SWITCH PUSHED ON TAKE-OFF RESET TMC SERVO, TMC AC, AND TMC DC CB'S F 14,15, 16 PER AMM 22-32-00. CREW TO ATTEMPT ANOTHER T/O USING AUTOTHROTLLES.

Part: ANTI-ICE VALVE — FAULTED (NR 2 ENGINE) · airframe 131,519 hrs · 20,145 cycles

R ENG AI LIGHT WHEN SELECTED ON R&R ENGINE INLET THERMAL ANTI-ICE PRESSURE SWITCH REF AMM 30-21-01 REMOVED AND REPLACED THE #2 ENGINE NOSE COWL ANTI ICE SHUT OFF VALVE. PER AMM REF. 30-21-03 ENGINE RUN WAS PERFORMED. RIGHT ENGINE ANTI ICE LIGHT CHECKED GOOD AT THIS TIME. OK FOR SERVICE.

Part: ENGINE — LEAKING (NR 1) · airframe 131,349 hrs · 20,123 cycles

OIL QTY WENT TO ZERO OIL PRESSURE TO RED LINE & ENG SHUTDOWN. ONLY LEFT SIDE OF NR 1 ENGINE COATED WITH OIL. INBD SIDE WAS DRY. AFTER SPEAKING WITH CREW WHEN ACFT WAS COMING INTO IAD AT AROUND 6000FT LT ENGINE OIL QTY DROPPED TO ZERO FOLLOWED BY OIL PRESSURE DROPPING TO ZERO. SHUTDOWN ENGINE FOR OIL PRESSURE IN RED, TROUBLESHOT IAW AMM 72-00-00-206-019-N01, ENGINE WINDMILLING INSPECTION CHECK, ADDED 34 QTS TO FILL SYSTEM. CHECKED ALL CHIP DETECTORS, ALL ARE CLEAN. SOURCS OF OIL LEAK IS FROM THE AIR OIL COOLER OR ATTACHING LINES, ENGINE REMOVED FROM ACFT. NEW ENGINE INSTALLED ON ACFT. OPS CHECKS OF ENGINE AFTER INSTALL, OK.

Part: GIRT BAR — FAULTED (ZONE 800) · airframe 131,084 hrs · 20,092 cycles

DOOR 1L DISARM BAR DOESNT STOW ALL THE WAY 52-11-00-862-001AND CLOSING THE ENTRY/SERVICE DOOR EXTERNALLY, TASK 52-11-00-862-002+OPENING THE ENTRY/SERVICE DOOR INTERNALLY, TASK 52-11-00-862-003 AND CLOSING THE ENTRY/SERVICE DOOR INTERNALLY, TASK 52-11-00-862-004 C/0 WITHOUT REMARK.CONFIRMED GIRT BAR ARMING AND DISARMING WITHOUT REMARK.

Part: HOSE — COLLAPSED (ZONE 800) · airframe 130,546 hrs · 20,028 cycles

RIGHT OVERWING DOOR SLIDE INFLATION HOSE IS COLLAPSED APPROX 4 FOOT SECTION AS VIEWED FROM PANEL 198CR ADDING PARTS DISARMED AND INSTALLED SAFETY PIN FOR THE RIGHT-HAND OVERWING DOOR INFLATION CYLINDER PER AMM 25-65-00-042-001 REACTIVATED RIGHT HAND OVERWING DOOR SLIDE PER TASK 25-65-00-442-010. RIGH HAND INFLATION CYLINDER SAFETY PIN HAS BEEN REMOVED. REMOVED AND REPLACED RIGHT HAND OVERWING DOOR SLIDE INFLATION HOSE PER AMM 25-65-02. INSPECTED THE REACTIVATED RIGHT HAND OVERWING DOOR SLIDE PER TASK 25-65-00-442-010.

Part: FRAME — CORRODED (BS 1810) · airframe 127,453 hrs · 19,635 cycles

DURING C-CK IN ILN (WILMINGTON, OH) AMES MAINTENANCE FOUND THE L WR CHORD CORRODED LOCATED AT STA 1809.5 BULKHEAD FRAME INSTALLATION(P/N-148T1150-1). CORROSION WAS COMMON TO THE VERTICAL & HORIZONTAL FLANGE AS SHOWN IN FIGURES. DAMAGE WAS RE MOVED BY BLENDING AND IT WAS FOUND TO BE BEYOND THE ALLOWABLE LI MITS PER B767-300 SRM 53-80-08,AD-3, DETAIL-II AN ULTRSONIC THIC KNESS (UT) INSP OF THE REWORKED AREA WAS PERFORMED PER B767. WERE ACCOMPLISHED WITH NO REPORTED DEFECTS.

Part: ACCESS DOOR — CORRODED (AFT) · airframe 127,453 hrs · 19,635 cycles

AFT FLIGHT CONTROLS BAY ACCESS DOOR 313AL IS CORRODED. REMOVED ALL CORRODED PARTS DEEMED OUT OF LIMITS AND INSTALLED NE W PARTS IAW B767 SRM 51-40-02 ALONG WITH BOEING DWG 148T6602. SE E NON-ROUTINE 170098-0300-0005 FOR DETAILS

Part: FITTING — WORN (NR 2 NACELLE) · airframe 127,453 hrs · 19,635 cycles

DURING C-CHECK, AMES MAINT DISCOVER ED 2 FASTENER HOLES ON NR 2 PYLON BULKHEAD FITTING WAS WORN & ELONGATED. BOTH INBD & OTBD FASTENER HOLES MEASURED 0.3125" DIA WITH DISTANCE BETWEEN HOLES MEASURING NG 0.250". ATTACHING ANGLE WAS CRACKED & REPLACED. AS TIME-LIMITED FOR 24 MONTHS PENDING THE RESULTS OF A DAMAGE TO REMOVE THE ACFT FROM SERVICE ON OR BEFORE JUNE-7-2026, UNLESS ANOTHER 8100-9 FORM IS RECEIVED FINDING APPROVAL FOR DAMA ECRA-5412-01015. TOLERANCE REQUIREMENTS. PART-1 INTERIM REPAIR C/W PER ECRA 5412-01015 & REQUIRES DIP, DUE TO REPAIR INCORPORATED VIA ECRA 5410-01015 IS APPROVED PER ECRA 5412-01015. SUBSEQENT HFEC SURFACE SCAN AN D HFEC OPEN HOLE INSP WERE ACCOMPLISHED REVEALING NO DEFECTS.

Part: BEAR STRAP — CRACKED (L-1 DOOR AREA) · airframe 127,453 hrs · 19,635 cycles

L-1 DOOR CUTOUT AFT LOWER CORNER HAS A CRACK INDICATION IN BEARS TRAP ONLY AT THE LOWEST HOLE OUT OF FIVE LOCATIONS. REPAIRED CRACK IN L1 DOOR BEARSTRAP AT THE LOWEST HOLE OUT OF FIVE LOCATIONS IAW B767-300 SRM 53-10-01-2R-1 REPAIR 1.

Part: BRACKET — CRACKED (NR 2 NACELLE) · airframe 127,453 hrs · 19,635 cycles

BRACKETS AT AFT UPPER SIDE OF LOWER SKIRT FAIRING WHERE THE STIN GER PANEL ATTACHES FOUND TO BE CRACKED #2 PYLON. REF AMES NR 170098-0600-0110 AND WORK SHEET 83 REMOVED AND REPLACED 2 BRACKET ON THE NO 2 PYLON AFT LOWER SKIRT FAIRING WITH NEWLY FABRICATED BRACKETS IAW B767 BOEING DOCUMENT # 313T3380 AND SRM 51-40-02 PG 7.

Part: FLOOR SUPPORT — CORRODED (BS 1329-1351) · airframe 127,453 hrs · 19,635 cycles

CORROSION UNDER THE NUTPLATES ON THE LOWER SURF ACE OF THE ALC FLOOR SUPPORT, FROM STA.1329 TO STA.1351, RBL17.# 3449 REF AMES NR 170098-0100-0133 51-31-01-392-034. REMOVED CORROSION IN FLOOR SUPPORT FOUND TO BE REF EC/RA 5360-01811 REMOVED AND REINSTALLED ROLLER TRAY, PALLET LOCK, AND CARGO LOCK OUT OF LIMITS IAW B767-300 SRM 53-00-51-1A-1 FIG 101 DETAIL II IAW B767-300 AMM 25-53-02/401, AMM 25-53-26/401, AND AMM 25-53- REMOVED AND INSTALLED NEW FLOOR SUPPORT PER B767 SRM 51-40-02 SE 14/401 AT STA 1357-1417 RBL19. SEALENT APPLIED IAW B767 AMM E PARTIAL WORK ACOMPLISHED PARTIAL WORK SHEET NO. 51, 1.

Part: FLOOR SUPPORT — CORRODED (BS 1153-1175) · airframe 127,453 hrs · 19,635 cycles

GEN ITEM: 63-5310-1-2512 (B767-53-3-7154) CORROSION ON THE LOWER SURFACE OF THE PANEL SUP PORTS/ INTERCOSTALS, IN THE "BOX" AREA, FROM STA.1153 TO STA.117 5, LBL24 TO RBL24, LOCATED JUST BELOW THE ALC FLOOR.#3422 FWD SUPPORT WAS REMOVED AND FOUND TO BE OUT OF LIMITS. NOMINAL T HICKNESS .071 REMOVED .020 REM .051 FWD SUPPORT SPLICE WAS REPLA CED NEW PART NO 146T5000-92 IAW B767-300 SRM 51-40-02 AND BOEING DWG NO 146T5000. SEE NONROUTINE 170098-0100-0081 FOR DETAILS

Part: FLOOR SUPPORT — LOOSE (BS 1053 LBL34) · airframe 127,453 hrs · 19,635 cycles

UPPER CABIN STA 1053 LBL 34 FLOOR SUPPORT LOOSE ON I/B SIDE, ATTACH HOLE IS ENLARGED.

Part: ANGLE — CRACKED (NR 1 NACELLE) · airframe 127,453 hrs · 19,635 cycles

NR 1 PYLON AFT OB INTERNAL "L" ANGLE CRACKED AT MOST UPPER FASTENER,

Part: FLOOR SUPPORT — CORRODED (BS 1329-1351) · airframe 127,453 hrs · 19,635 cycles

CORROSION UNDEER THE NUTPLATES ON THE LOWER SURFACE OF THE ALC FLOOR SUPPORT FROM STA 1329 TO STA 1351 LBL19 NO 3447. REF AMES NR 170098-0100-0131 BLENDED CORROSION FOUND TO BE OUT OF LIMITS HAD TO FABRICATE NEW FLOOR SUPPORT IAW 47613FAAB01. SEE PARTIAL WORK ACCOMPLISHED AN D PARTIAL WORK SHEET 121 FOR WORK DETAILS EC/RA 5322-01124

Part: ANGLE — CRACKED (NR 2 NACELLE) · airframe 127,453 hrs · 19,635 cycles

GEN ITEM: EA 5700-03285 REV F OP 010 #2 PYLON OB AFT HYDRAULIC BAY "L" ANGLE IS CRACKED

Part: SKIN — CRACKED (NR 1 NACELLE) · airframe 127,453 hrs · 19,635 cycles

GEN ITEM: 63-5410-1-2501 #1 PYLON O/B SIDE ACCESS 436BL PYLON SKIN CRACKED FWD UPPER CORN ER & AFT CHAFE STRIP IS LOOSE/DAMAGED UPPER & LWR

Part: WEB — CRACKED (BS 1153) · airframe 127,453 hrs · 19,635 cycles

AFTER REMOVING CAP (FLOOR SUPPORT ) AT STA 1153 FOUND WEB TO BE CRACKED AT HOLE JUST INBD OF FRAME FITTING ON LH SIDE. REPAIRED CRACKED WEB AT STA 1153 IAW B767-300 SRM 51-70-13-0G-0 DETAIL II. SEE NONROUTINE 170098-0100-0268 FOR DETAILS

Part: SHEAR TIE — CORRODED (BS 1562 S38R&L) · airframe 127,453 hrs · 19,635 cycles

GEN ITEM: 63-5310-1-2638 SHEAR TIE T-FITTING AT STA 1562 BTWN STRINGER 38R AND 38L IS COR RODED .REMOVED & REPLACED SHEAR TIE T-FITTING AT STA 1562 BTWN STR 38R AND 38L IAW B767 SRM 51-40-02 PARA 9. SEE NONROUTINE 170098-0100 -0084 FOR DETAILS

Part: FLOOR SUPPORT — CRACKED (BS 1417) · airframe 127,453 hrs · 19,635 cycles

GEN ITEM: 63-5310-1-2621 (B767-53-3-7055) NDT VERIFIED CRACK, IN BRACKET THAT ATTACHES TH E BULK CARGO FLOOR SUPPORT TO FRAME 1417, LOCATED ON THE FWD SID E OF FRAME 1417, AT RBL16.#3462

Part: FLOOR SUPPORT — CRACKED (BS 1417) · airframe 127,453 hrs · 19,635 cycles

GEN ITEM: 63-5310-1-2621 (B767-53-3-7055) NDT VERIFIED CRACK, IN BRACKET THAT ATTACHES TH E BULK CARGO FLOOR SUPPORT TO FRAME 1417, LOCATED ON THE FWD SID E OF FRAME 1417, AT RBL9.#3461

Part: DRIVE ASSY — FAILED (WX RADAR) · airframe 126,132 hrs · 19,422 cycles

WEATHER RADAR FAILED. TRIED WX RADAR TRANSCEIVER, NO HELP, INSTALLED ORIGINAL - SHOWS "WX FAIL ANT" DRIVE, SCANNER- OFF 75-3443-9-0001 8782 ON 75-3443-9-0001 8778 DRIVE, SCANNER- OFF 75-3443-9-0001 8782 ON 0000 REMOVED AND REPLACED WRX RADAR PEDESTAL DRIVE SCANNER ASSY REF AMM 34-43-00 OPS CHECK GOOD ALL TEST PASSED PARTS USED: 75-3443-9-0001,QTY :1 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1130698 SN OFF 8782.

Part: BUSS — INOPERATIVE (LH AND RH) · airframe 125,857 hrs · 19,380 cycles

BOTH UTILITY BUSSES INOP. RESET CIRCUIT BRAKES P11T4 AND P11T31(UTL BUS L&R), SYSTEM OPERATES NORMAL.REF SSM 24-51-02.

Part: DOOR — DAMAGED (THRUST REVERSER) · airframe 125,215 hrs · 19,291 cycles

BLOCKER DOOR HONEYCOMB MISSING. REPORTING PARTS DEPARTING AIRCRAFT ON FLT #2206 APPROXIMATELLY 12X12 HONEYCOMB BLOCKER DOOR WAS R & R ON CDL NO DAMAGE FOUND C DUCT OR ENGINE. BLOCKER DOOR. NR 1 ENGINE INBOARD THRUST REVERSER C SECTION 1 EACH BLOCKER DOOR DAMAGE. APPROXIMATELY 3 OCLOCK POSITION. REQUEST CDL78CB REMOVED BLOCKER DOOR WILL REQUIRED ALL NEW PARTS. UPDATING REQUIRED PARTS INSTALLED BLOCKER DOOR REF AMM 78-31-14-404-011-N00 INCLUDING UP TO STEP 3.D.(4) REQUIRING MANUALLY RETRACT OF TR. CANNOT BE ACCOMPLISHED DUE TO 2 BUMPER PADS UNDER BLOCKER DOOR NEEDING REPLACEMENT. BUMPER PAD REPLACED IAW SOPM 20-50-12. AND BLOCKER DOOR INSTALL CONTINUED AND COMPLETED PER AMM 78-31-14.

Part: FLOORBEAM — CORRODED (STA325/LBL23) · airframe 124,107 hrs · 19,142 cycles

CABIN STA 325 LBL 23 FLOOR BEAM SURFACE FOUND CORROSION,ORIGINAT ED BY EMP V902610,REF TO HAECO NON ROUTINE NO.9454610 EA 2500-1 2983 OP 002. PERFORMED BY EMP V902610, RII BY V905036. CABIN STA325 LBL23 FLO OR BEAM UPPER SURFACE CORROSION AREA REPAIRED AS PER SRM 53-00-5 1-2R-4 REV 122 AND ECRA 5315-01193 REV -. RII BY TA447, V905036.

Part: BATTERY — DISCHARGED (M1210) · airframe 124,107 hrs · 19,142 cycles

REMOVE AND REINSTALL EMERGENCY LIGHT BATTERY PACK PREVENT ALL EM ERGENCY LIGHT BATTERY (P/N:AD2013-1A) LOW VOLTAGE REF HAECO NON- ROUTINE NO.9453799, EA 2500-13033 OP022 PERFORMED BY EMP V905488, IDT BY EMP V905449, REMOVED AND REINST AMM 33-51-07-612-056,AMM 33-51-07-402-010,AMM 33-51-07-422-012, ALLED EMERGENCY LIGHT BATTERY PACKS CHARGE ALL EMERGENCY LIGHT B AMM 33-51-07-002-006 REV.138 ATTERY AND TEST FOUND M1210 BATTERY OUT OF LIMIT,REPLACED M1210 BATTERY AND INSTALLATION TEST FOUND PASS AS PER

Part: CONNECTOR — DAMAGED (CEILING PANEL) · airframe 124,107 hrs · 19,142 cycles

CEILING EMERGENCY LIGHT CONNECTOR DAMAGE AT 20AB 23AB 35AB 38AB 41AB 44AB 47AB 49AB 2A 6L 4L 8L 23LK 30LK 33LK 35LK 38LK 44LK 47 LK 50LK - ORIGINATED BY EMP V905488 ON HAECO NR 9454640, RAISED FROM EA 4420-03294 REV D OP001. PERFORMED BY EMP V905488, IDT BY V905449, REPLACED CEILING EMERG 33-51-05-402-024 REV 139. ENCY LIGHT CONNECTORS AT 20AB 23AB 35AB 38AB 41AB 44AB 47AB 49AB 2A 6L 4L 8L 23LK 30LK 33LK 35LK 38LK 44LK 47LK 50LK AND INSTALL ATION TEST FOUND PASS,AS PER SWPM 20-61-28 REV 81 AND AMM

Part: CHARGER — OUT OF LIMITS (M737) · airframe 124,107 hrs · 19,142 cycles

L/H AISLE L323 AND L1049 EXIT SIGN LIGNT DIM REF HAECO NON-ROUTI NE NO.9454390,ORIGINATED BY EMP V905488, SPEC NO.B767-33-3-7004 PERFORMED BY EMP V905488,IDT BY EMP V905449, PERFORMED T/S AND AMM 33-51-07-402-010 REV.138 WIRING CHECK FOUND M737 POWER SUPPLY MALFUNCTION REPLACED M737 POWER SUPPLY AND TEST FOUND L323 AND L1049 EXIT SIGN WORK NORMAL AS PER DWG N0542-D73 REV.B FIM 33-51 FAULT TREE 812 REV.139

Part: FLOORBEAM — CORRODED (STA303/LBL35) · airframe 124,107 hrs · 19,142 cycles

CABIN STA 303 LBL 35 FLOOR BEAM SURFACE FOUND CORROSION,ORIGINAT ED BY EMP V902610,REF TO HAECO NON ROUTINE NO.9454611,EA 2500-12 983 OP 002. PERFORMED BY EMP V902610, RII BY V905036. CABIN STA 303 LBL35 FL OOR BEAM UPPER SURFACE CORROSION AREA REPAIRED AS PER SRM 53-00- 51-2R-1 REV 122 AND ECRA 5315-01194 REV -. RII BY TA447, V905036.

Part: FLOORBEAM — CORRODED (STA 303) · airframe 124,107 hrs · 19,142 cycles

CABIN STA 303 LBL 35 FLOORBEAM SURFACE FOUND CORROSION, CABIN STA 303 LBL35 FL OOR BEAM UPPER SURFACE CORROSION AREA REPAIRED AS PER SRM 53-00- 51-2R-1 REV 122 AND ECRA 5315-01194 REV -.

Part: FLOORBEAM — CORRODED (STA 325) · airframe 124,107 hrs · 19,142 cycles

CABIN STA 325 LBL 23 FLOOR BEAM SURFACE FOUND CORROSION, CABIN STA325 LBL23 FLO OR BEAM UPPER SURFACE CORROSION AREA REPAIRED AS PER SRM 53-00-5 1-2R-4 REV 122 AND ECRA 5315-01193 REV -.

Part: LAMP — UNKNOWN (R FWD WING) · airframe 124,107 hrs · 19,142 cycles

R/H FWD WING SLIDE LIGHT L391 INOP - ORIGINATED BY EMP V905488 O N HAECO NR 9453840, SPEC NO.B767-33-3-7004. PERFORMED BY EMP V905488, REPLACED R/H FWD WING SLIDE LIGHT L391 LAMP AND NEW LAMP TEST FOUND PASS, AS PER AMM 33-51-06-902-082 REV 138.

Part: LAMP — UNKNOWN (R FWD WING) · airframe 124,107 hrs · 19,142 cycles

R/H FWD OVERING EGRESS LIGHT L394 INOP - ORIGINATED BY EMP ON HAECO NR 9453843, SPEC NO.B767-33-3-7004. PERFORMED BY EMP REPLACED R/H FWD OVERWING EGRESS LIGHT L394 LAMPS AND NEW LAMPS TEST FOUND PASS, AS PER AMM 33-51-06-9 02-082 REV 138.

Part: CONNECTOR — UNKNOWN (CEILING PNL) · airframe 124,107 hrs · 19,142 cycles

CEILING PANEL EMERGENCY LIGHT CONNECTORS DAMAGE AT 2A, 5A, 7A, 9 A, 21AB, 30AB, 32AB, 2L, 4L, 6L, 8L 16LK, 21LK, 41LK - ORIGINATE D BY EMP V905488 ON HAECO NR 9454018, EA 4420-03294 REV D OP001 PERFORMED BY EMP V905488, REPLACED CEILING PANEL EMERGENCY LIGHT CONNECTORS AND INSTALLATION TEST FOUND PASS, AS PER SWPM 20-61- 28 REV 81, AMM 33-51-402-024 REV 138.

Part: LAMP — UNKNOWN (L AFT DOOR) · airframe 124,107 hrs · 19,142 cycles

L/H AFT DOOR ERMERGENCY SLIDE LIGHT L397 INOP - ORIGINATED BY EM P V905488 ON HAECO NR 9453836, SPEC NO.B767-33-3-7004. PERFORMED BY EMP V905488, REPLACED L/H AFT DOOR EMERGENCY SLIDE LIGHT L397 LAMP AND NEW LAMP TEST FOUND PASS, AS PER AMM 33-51-0 6-902-082 REV 138.

Part: LAMP — UNKNOWN (R FWD DOOR) · airframe 124,107 hrs · 19,142 cycles

R/H FWD DOOR SLIDE LIGHT L393 INOP - ORIGINATED BY EMP V905488 O N HAECO NR 9453842, SPEC NO.B767-33-3-7004. PERFORMED BY EMP V905488, REPLACED R/H FWD DOOR SLIDE LIGHT L393 LAMP AND NEW LAMP TEST FOUND PASS, AS PER AMM 33-51-06-902-082 REV 138.

Part: RIVET — MISSING (ENG 1) · airframe 122,016 hrs · 18,862 cycles

PDA 3 DURING WALKAROUND FOUND 1 MISSING RIVET AT #1 ENGINE AFT PYLON INBOARD AREA BY EXHAUST. PHOTO ADDED. REPLACED MISSING RIVET WITH NEW ONE PER SRM 51-40-02.

Part: RIVET — MISSING (ENG 2) · airframe 122,016 hrs · 18,862 cycles

PDA 3 DURING WALKAROUND FOUND 3 MISSING RIVETS AND 3 LOOSE RIVETS AT #2 ENGINE PYLON AFT AREA BY ENGINE EXHAUST. PHOTOS ADDED. REMOVED AND REPLACE LOOSE RIVETS ON AFT ENGINE. PYLON PER SRM 51-50-02.

Part: NONE — NONE · airframe 120,763 hrs · 18,694 cycles

THIS IS A SUPPLEMENTAL REPORT FOR THE SAME CONTROL NUMBER CALA2022051601236 SUBMITTED ON 05/16/22.CREW REPORTS LOUD BANG ON CLIMB AND #2 ENGINE SHUT ITSELF DOWN, ENGINES NUMBER WAS REMOVED AND REPLACED

Part: WINDOW — NONE (F/O SIDE) · airframe 120,714 hrs · 18,687 cycles

EECM MESSAGE INDEX BIRD STRIKE PROBLEM WAS ENCOUNTERED BY THE FL IGHT CREW WHICH WAS NOT COVERED IN THE FAULT CODE DIAGRAMS (REF FAULT CODE DIAGRAM FOR FLIGHT CREW ACTION) BIRDSTRIKE ON FO FRONT W INDSCREEN CLEANED F/O WINDOW IAW AMM TASK 12-25-04-102-001 AND INSPECTED WINDOWS ALSO THE ADJACENT STRUCTURE IAW TASK 05-51-18-212-001- STEEP INO DAMAGE FOUND ADD FAULT:BIRDSTRIKE ON FO FRONT W INDSCREEN

Part: PUMP — INDICATION (NA) · airframe 119,868 hrs · 18,540 cycles

LEFT AFT FUEL EICAS MSG AFTER PUSH/START PLACARED PER MEL 2822M NO TIME FOR T/S. CB LH AFT FUEL PUMP OUT CB P6-3 G15 COLLARED PER MEL 2822M. DDP ACCOMPLISHED. AND COLLARED PER MEL. DISPATCH DESK: 84 NAME: WR DATE: 17-JAN-22- NOC DESK: 767 NAME: DOUG DATE: 17-JAN-22- L AFT MAIN FUEL PUMP INOP. TAPED OVER LH AFT PUMP SWITCH. ADD EMP:U288719

Part: CONNECTOR — DAMAGED (TE FLAP SYSTEM) · airframe 119,638 hrs · 18,495 cycles

*EMERGENCY DECLARED*TE FLAP DISAGREE ON APPROACH MOVING FLAPS FROM 5 TO 15 REF FIM 27-51 TREE 809, FSEU BITE FOUND FAULT 27-51104, TE FLAP UPDATE CLARIFICATION FAULT TREES 105, 809, 810 WERE COMPLETED, CORRECTION COMPLETED BITE TEST REF FIM 27-51 TREE 809 FIG 104A, DISAGREE AND TE FLAP SHUTDOWN, REF FIG 105 AND 117 TREES 810 AND NEED TO CONTINUE WITH FAULT TREE 117. COMPLETED FIM 27-51 TREE 810 FIG 105. NEED TO CONTINUE WITH FIM 839 TO CONTINUE. 27-51 TREE 839 FIG 117. FOUND HEAVILY DAMAGED CONNECTOR D02310P AT TE BYPASS VALVE V105. RR CONNECTOR D2310P. REF WDM 27-51-11. PERFORMED TE FLAPS REF AMM 27-51-32-822-078. NO FAULTS.

Part: PANEL — MISSING (RT WING LE) · airframe 117,873 hrs · 18,128 cycles

PDA 3 DURING W/A FOUND SMALL WING PANEL MISSING, RT WING LEADING EDGE UNDER THE WING O/B OF #2 ENGINE. REFER TO ORIGINAL LOG PAGE 6343710. THIS LOG PAGE WAS CREATED TO INCLUDE PDA INFO. REPLACED PANEL 621CB REF IPC 57-41-10. TOMC HAS BEEN NOTIFIED.

Part: SKIN — CORRODED (S39L BS 1540) · airframe 117,366 hrs · 18,053 cycles

BULK CGO COMPT AT STA 1540 BILGE AREA S-39L DRAIN HOLE AREA FOUND CORROSION REFER NR LP 9131172 BULK CGO COMPT STA 1540 BTW S39L TO S39R WATER DRAIN VALVE AREA SKIN INTERIM REPAIRED AS PER ECRA 5361-01082 REV - ADD EMP:V897545 RII BY HX 102369

Part: SHEAR ANGLE — CORRODED (BS 1540 S38L) · airframe 117,366 hrs · 18,053 cycles

BULK CARGO STA 1540 BETWEEN S38L TO S39L SHEAR TIE FOUND CORROSION CRK REF NR LP 9131280 BULK CARGO STA 1540 BTW S38L TO S39L SHEAR TIE REPLACED AS PER SRM 51-10-02 AND NEW SHEAR TIE INSTALLED AS PER SRM 51-40-02 ADD EMP:V906027 RII OK BY HX 102369

Part: SHEAR ANGLE — CORRODED (BS 1540 S39L/R) · airframe 117,366 hrs · 18,053 cycles

BULK CARGO STA 1540 BETWEEN S39L TO S39R SHEAR TIE FOUND CORROSION REF NR LP 9131299 BULK CARGO STA 1540 BTW S39L TO S39R SHEAR TIE REPLACED AS PER SRM 51-10-02 AND NEW SHEAR TIE INSTALLED AS PER SRM 51-40-02 ADD EMP:V906027 RII OK BY HX 102369

Part: STRINGER — CORRODED (BS 1540-1546) · airframe 117,366 hrs · 18,053 cycles

BULK CGO COMPT BILGE AREA AT STA 1540 TO 1546 S39L STRINGER FOUND CORROSION AS MARKED REFER NR LP 9131240 BULK CGO COMPT STA 1540-1546 S39L STRINGER PERMANENT REPAIRED AS PER ECRA 5360-01594 REV - ADD EMP:V897545 RII BY HX 102369

Part: STRINGER — CORRODED (BS 1540-1546) · airframe 117,366 hrs · 18,053 cycles

BULK CGO COMPT BILGE AREA AT STA 1540 - 1546 S39R STRINGER AREA FOUND CORROSION AS MARKED REFER NR LP 9131241 BULK CGO COMPT STA 1540-1546 S39R STRINGER PERMANENT REPAIRED AS PER ECRA 5360-01594 REV - ADD EMP:V897545 RII BY HX 102369

Part: WHEEL — CRACKED (NR 5 MLG) · airframe 116,957 hrs · 17,987 cycles

NR 5 MLG WHEEL SPOKES APPEAR CRACKED. PICS ADDED REMOVED AND REPLACED NR 5 MLG TIRE WHEEL ASSEMBLY, REF AMM 32-45-01.

Part: BATTERY — FAILED (EMERGENCY LIGHTS) · airframe 115,467 hrs · 17,698 cycles

BATTERY PACK M9045 FAILD REMOVED AND REPLACED BATTERY PACK M9045 IAW AMM 33-51-07

Part: BATTERY PACK — FAILED (EMERGENCY LIGHT) · airframe 115,467 hrs · 17,698 cycles

POWER SUPPLY M1557 FAILD REMOVED AND REPLACED M1557 BATTERY PACK IAW AMM 33-51-07

Part: BATTERY — FAILED (EMERGENCY LIGHTS) · airframe 115,467 hrs · 17,698 cycles

POWER PACK M737 FAILD REMOVED AND REPLACE BATTERY PACK M737 IAW AMM 33-51-07

Part: HOUSING — GOUGED (CRGO DOOR HANDLE) · airframe 115,467 hrs · 17,698 cycles

CARGO DOOR EXTERNAL HANDLE HOUSING WAS GOUGED. REMOVED AND REPLACED THE HOUSING IAW AMM 52-36-07-002-013, AND SRM 51-40-02 PAR 7.

Part: SKIN — DENTED (FUSELAGE) · airframe 115,465 hrs · 17,697 cycles

FOUND DAMAGE ON LOWER FUSELAGE BETWEEN STATION 1241 AND 1263 FWD OF BULK CARGO DOOR DAMAGE LOCATION IS STA 1263 STR 34 L. DENT IS APPROX 9"L X 6" W AND DEPTH IS APPROX .241 DEEP. A/Y MEASURES 24.89. DENT OUT OF LIMITS REF SRM A/D 1 53-00-01. NOT THE BULK CARGO DOOR. THE DAMAGE IS CLOSER TO WING TO BODY FAIRING COMPLIED WITH STEPS 1-4 OF REPAIR 29 FUSELAGE SKIN- EXTERNAL REPAIR AT A FRAME REF SRM 53-00-01 REPAIR 29. C/W INSP. COMPLIED WITH STEPS 1-4 OF REPAIR 29 FUSELAGE SKIN- EXTERNAL REPAIR AT A FRAME REF SRM 53-00-01 REPAIR 29. C/W HFEC PART 6 51-00-19, NO CRACKS NOTED. PART 3 FILLER AS 0.071" 2024-T3 PO#9923810 REF SRM 53-00-01 NEED TO VERIFY PART 1 DOUBLER AS 0.080" 2024-T3 PO#8602184 AND REPAIR 29 TABLE 1 REPAIR 29 TABLE 1P. PART 3 FILLER AS 0.071" 2024-T3 PO#9923810 REF SRM 53-00-01 C/W INSP.VERIFIED. 1 DO

Part: ENGINE — DAMAGED (NR 1) · airframe 108,658 hrs · 16,791 cycles

LEFT ENGINE OVERHEATED AND VIBRATION. 711 DEGREE. SHUTDOWN AND LANDED IMMEDIATELY. NR 1 ENGINE WAS REPLACED IAW TC 63-7100-1-9800.

Part: ENGINE — DAMAGED (NR 1) · airframe 108,658 hrs · 16,791 cycles

LEFT ENGINE OVERHEAT AND VIBRATION. 711 DEGREE. SHUTDOWN AND LANDED IMMEDIATELY. THE NR 1 ENGINE WAS REPLACED IAW TASKCARD 63-7100-1-9800.

Part: SPAR — CRACKED (NR 2 PYLON) · airframe 108,655 hrs · 16,789 cycles

NR 2 PYLON, FWD, UPPER SPAR WEB WAS FOUND CRACKED NEAR THE CASE DRAIN TUBE, AND FUEL TUBE CUTOUTS. INSTALLED AN INTERIM REPAIR IAW ECRA 5410-01884.

Part: SKIN — CRACKED (NR 2 NACELLE) · airframe 108,655 hrs · 16,789 cycles

NR 2 PYLON RT SIDE SKIN WAS FOUND CRACKED. REPAIRED IAW EC/R A 5430-02164, REV-.

Part: FLOORBEAM — CORRODED (BS 1518) · airframe 108,655 hrs · 16,789 cycles

BS 1518 FLOORBEAM FOUND CORRODED AT LBL 28. REPAIRED IAW SRM 53-00-51, REPAIR 1, FIG 201.

Part: FLOORBEAM — CORRODED (BS 1502) · airframe 108,655 hrs · 16,789 cycles

BS 1502, FLOORBEAM FOUND CORRODED, LBL 15 TO LBL 35. REPAIRED IAW SRM 53-00-51, REPAIR 1, FIG 201.

Part: LEAD — NOT REPORTED (EMERGENCY LIGHT) · airframe 107,331 hrs · 16,606 cycles

AFT GALLEY CROSS AISLE EEL LIGHT INOP RPL''D LEAD STRIP TO LIGHT ASSY. OPS NORMAL. REF: AMM33-51-00-201

Part: CONTROLLER — FAULTY (CABIN PRESSURE) · airframe 105,287 hrs · 16,296 cycles

PRESSURIZATION CONTROL AUTO INOPERATIVE LIGHT ILLUMINATED. OPERATION IN MANUAL MODE WAS OK. EMERGENCY DECLARED. FOLLOWED FIM 21-31-00-815-803. REMOVED AND REPLACED THE NR 2 AUTOMATIC PRESSURE CONTROLLER, OPS CHECKED GOOD IAW AMM 21-31-02.

Part: CABLE — MALFUNCTIONED (GALLEY) · airframe 104,631 hrs · 16,198 cycles

GALLEY HOT PLATE SMOKING, SPARKING ELECTRICALLY AT P51 OPS CHECKED HOT PLATE, WHICH SHOWED NO SIGN OF SPARKS OR SMOKING . HEATS OK HOTPLATE IS H51. P51 IS GALLEY CART NEW TECH CONTROLLER. FOUND TWO SOCKETS DISCOLORED. REPLACED P51 CABLE OPERATIONAL CHECK GOO D REF 25-32-95

Part: RELAY — LOOSE (AC SYSTEM) · airframe 104,347 hrs · 16,158 cycles

ENTIRE AIRCRAFT TOO HOT TRIED BOTH PACKS IN MAN COOL. TRIM AIR OFF. ONE PACK OFF AT A TIME EMERGENCY DECLARED. INSPECTED BOTH PACK COMP, NO PROBLEMS NOTED. BITE TEST SHOWS NO FAULTS, REF FIM 21-61 TASK 803, ALL TRIM AIR VALVES OPERATING NORMALLY. RAN ENGINES REF 71-00-00 OPERATED PACKS AND GOT 63F IN ALL CABINS. DURING INSPECTION ON ELECTRICAL SYSTEM FOUND LEAD A1 LOOSE ON K114 RELAY AT P34, REF WDM 24-41-11 PG 1A,RETIGHTENED.

Part: UNKNOWN — MALFUNCTIONED (CABIN) · airframe 104,102 hrs · 16,125 cycles

EMER LIGHTING STRIP IN F/C GALLEY AND EXIT LIGHT DOOR 1L FLASHING ON/OFF. INSP CONNECTIONS TO EMERGENCY LIGHT ALL OK. AS PRECAUTION REPLACED BATTERY AS PER AMM 33-51-07 AND PER FORMED OPS TEST ALL OK.

Part: SEAL — LEAKING (NR 1 ENGINE) · airframe 103,979 hrs · 16,109 cycles

NR 1 ENGINE OIL QTY SLOWLY DECREASED TO 0. OIL PRESS HELD STEADY FOR A WHILE. EMERGENCY DECLARED. ENGINE IDLE RUN TEST CONFIRMED OIL LEAK FROM OIL SEAL DRAIN FOR THE IDG DRIVE. REMOVED IDG, REPLACED IDG DRIVE OIL SEAL & ASSOCIATED PACKING GROOVE PER AMM 72-61-04/401. IDG REINSTALLED PER AM M 24-11-01/401. IDG LEAK CHECK AND OPS TEST PER AMM 24-11-01/501. OPS GOOD, NO LEAKS FOUND.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 103,844 hrs · 16,090 cycles

1L MED EMER LIGHT FLASHING CREW VERBAL REPORT: EMER LIGHT CAME ON AND WENT OFF ON ONE OCCASION AT DR 1L AREA. EMERGENCY LIGHTS OPERATIONAL TEST PERFORMED PER AMM 33-51-00. ALL LIGHT FUNCTIONS ARE NORMAL AND NIL DISCREPANCIES FOUND. AIRCRAFT RESTORED TO NORMAL CONDITION.

Part: LIGHT — INTERMITTENT (CABIN) · airframe 103,612 hrs · 16,061 cycles

EMERGENCY EXIT LIGHTS FLICKER ON/OFF INTERMITTENT AT FRONT GALLEY/CLOSET/DOOR 1L. ACCOMPLISHED EMERGENCY LIGHT CHECK PER AMM 33-51-00, TEST NORMAL NO SIGNS OF FLICKERING LIGHTS WHEN EITHER ON OR OFF.

Part: LIGHT — INTERMITTENT (CABIN) · airframe 103,579 hrs · 16,056 cycles

EMERGENCY EXIT LIGHTS ARE FLICKERING ON AND OFF WITH SWITCH IN ARMED POSITION. ACCOMPLISHED EMERGENCY LIGHT TEST REF MM33-51-00, NO FAULTS FOUND

Part: LIGHT — INTERMITTENT (CABIN) · airframe 103,531 hrs · 16,050 cycles

DOOR 1L EXIT PATH LIGHTS ILLUMINATE INTERMITTENT. CYCLED EMERGENCY LIGHTS AND NO FAULTS NOTED, TEST PASS. REF FIM 33-51-808.

Part: CONNECTOR — LOOSE (BATTERY PACK) · airframe 103,464 hrs · 16,040 cycles

EMERGENCY LIGHTING IS ON AND INTERMITENTLY FLASHING ON LEFT SIDE OF AC ONLY BY 1L GALLEY ON ARRIVAL CREW REPORTED FLOOR LIGHTS AT DOOR 1 LEFT AND EXIT SIGN LIGHT FLICKERED 6 TIMES IN 20 MINUTES. CYCLED EMERGENCY LIG TS ON AND ALL LIGHTS ILLUMINATED WITHOUT ANY FLICKERING IAW FIM 33-51-808 ALL OPS FOUND NORMAL UNABLE TO FAULT. FOR FURTHER TS WE LOCATED BATTERY PACK M1557 AND FOUND A LOOSE CONNECTION OPS CHECKED AGAIN ALL OPS NORMAL

Part: SENSOR — FAULTY (NR 1 BLEED SYS) · airframe 103,433 hrs · 16,036 cycles

LT ENGINE BLEED OVERHEAT, FOLLOWED BY LT PACK OFF AND LT BLEED OFF, FOLLOWED CHECK LIST. EMERGENCY DECLARED. REPLACED THE NR 1 ENGINE FAN AIR TEMP SENSOR IAW AMM 36-11-17. RAN HIGH POWER RUN AND PERFORMED AMM 36-00-3 NO LEAKS NOTED NO FAULTS NOTED IN THE AIR SUPPLY SYSTEM..

Part: POWER SUPPLY — FAULTY (EMERGENCY LIGHTS) · airframe 103,400 hrs · 16,029 cycles

EMERGENCY LIGHTS FLICKERING INTERMITTENTLY. REPLACED THE POWER SUPPLY IAW AMM 33-51-07, ALL OPS NORMAL.

Part: LIGHT — INTERMITTENT (CABIN) · airframe 103,390 hrs · 16,028 cycles

EMERGENCY EXIT LIGHTS FLICKER ON AND OFF INTERMITTENTLY WITH ALL SWITCHES SET CORRECT EMERGENCY LIGHTS OPS NORMAL ON GROUND NO FLICKERING ON AND OFF INTERMITTENT . COULD NOT DUPLICATE FAULT AT THIS TIME.

Part: LIGHT — UNKNOWN (CABIN) · airframe 103,295 hrs · 16,016 cycles

TWO EMERGENCY LIGHTS FLASHING ON AND OFF NEAR L2 LAVATORY. CARRIED OUT EMERGENCY LIGHT TEST, ALL GOOD.

Part: LIGHT — FAULTY (CABIN) · airframe 103,206 hrs · 16,003 cycles

MID LAV EMERG LIGHT IS FLASHING. EMERGENCY LIGHTS OPS TEST C/O IAW AMM 33-51-00 SATIS.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 103,206 hrs · 16,003 cycles

FLOOR EMERG LIGHTING IN FRONT OF EMERG EXITS STAYS ILLUMINATED AT ALL TIMES. ACCOMPLISHED EMERG LIGHT TEST REF MM33-51-00, ALL TEST PASSED, NO FAULTS FOUND.

Part: LIGHT — INTERFERENCE (CABIN) · airframe 103,097 hrs · 15,989 cycles

EMERGENCY EXIT LIGHTS WERE FLASHING INTERMITTENTLY BY SEAT 19A AT LAV. OVERWING EXIT NO FAULT NOTED, OPS CHK NORMAL.

Part: LIGHT — INTERMITTENT (CABIN) · airframe 102,940 hrs · 15,967 cycles

EXIT SIGN AND FLOOR TRACK LIGHT IN FRONT OF MID LAV AND ROWS 19 TO 20 BLINK ON AND OFF ACP EMER LIGHTS TEST, REF AMM 33-51-00. LIGHTS OPS NORMAL WITH NO FLICKERING.

Part: LIGHT — INTERMITTENT (CABIN) · airframe 102,940 hrs · 15,967 cycles

EMERG EXIT LIGHTS FLASH AT LEFT WINDOW EXIT INSPECTED LIGHT ASSY 2 EA. ALL LOOKS NORMAL, OPS CK NORMAL AMM 33-51-00.

Part: LIGHT — INTERMITTENT (CABIN) · airframe 102,926 hrs · 15,965 cycles

EMERG LIGHTS ABOVE MID LAVS FLICKER OFF/ON. OPERATED EMERGENCY LIGHTS WRT AMM 33-51-00 A FEW TIMES AND NO PROBLEMS APPARENT.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 102,616 hrs · 15,923 cycles

FLOOR ESCAPE PATH LIGHTS AND DOOR LOWER EMERG EXIT LIGHTS FLICKER ALL OVER CABIN ACCOMPLISHED OPERATIONAL TEST FOR EMERGENCY LIGHT REF AMM 33-51-00 PAGE 501. ALL OPERATION AND INDICATION NORMAL.

Part: ANGLE — CORRODED · airframe 102,303 hrs · 15,881 cycles

CENTER WING UPPER REAR SPAR ATTACH ANGLE CORROSION INTERIM REPAIR.

Part: ACTUATOR — UNSERVICEABLE (NR 2 ENGINE) · airframe 100,740 hrs · 15,667 cycles

CREW REPORTS SURGE ON RT ENG, FLAGGING SDR DUE TO RETURN TO FIELD. SVA FAILED IN CLOSED POSITION. R & R NR 2 ENG VARIABLE STATOR VANE ACTUATOR. BORESCOPE COMPLETED WITH NO DAMAGE FOUND.

Part: BATTERY — DISCHARGED (CABIN) · airframe 97,751 hrs · 15,254 cycles

EMERGENCY PATHWAY LIGHTS AT 1A TO 14A, 21AB TO 26AB & 19JK TO 34JK FAILED OPERATIONS TEST. R & R M732, M737 & M99080 BATTERIES IAW AMM 33-51-07. CHARGED THE EMER LIGHT BATTERIES IAW AMM 33-51-07. PERFORMED EMER PATH LIGHTS OPERATIONAL TEST IAW AMM 33-51-00. FOUND NORMAL CONDITION, ALL EMER PATH LIGHTS ON.

Part: SKIN PANEL — CRACKED (PYLON) · airframe 97,556 hrs · 15,227 cycles

SUSPECT CRACK IN PYLON SKIN AT PANEL CUT OUT UPPER LT CORNER THRU RIVET. NEED QC DEPARTMENT TO ACCOMPLISH HFEC TO CONFIRM. PERFORMED HFEC INSPECTION TO SUSPECTED CRACK LOCATION IAW NDT PART 6 51-00-19. VERIFIED THE LENGTH OF CRACK MARKED WHERE CRACK STOPS PAST FASTENER HOLE. REMOVED FASTENERS COMMON TO DOUBLER REPAIR IAW SRM 54-53-01 REPAIR 7. MANUFACTURED, PARTIAL, COMPLETED REPAIR 7 IAW SRM 54-53-01.

Part: CONNECTOR — UNSECURE (CABIN) · airframe 97,269 hrs · 15,190 cycles

SEAT MOUNTED EMER EXIT LIGHT INOPERATIVE. AT 33 LT, SECURED UNDER SEAT CONNECTOR. OPERATIONS CHECKS NORMAL.

Part: CIRCUIT CARD — FAULTY (FIRE DETECTION) · airframe 96,792 hrs

EICAS MSG RT STRUT DUCT LEAK. RT PACK OFF RT ENG BLEED OFF FIM 26-18-00 PAGE 107 BLOCK 8, 28 & 65 INDICATED DUCT LEAK & WW FIRE CARD M691 FAULTY. REPLACED CARD M691 IAW AMM 26-10-01. TEST IS OK & AFTER RUN UP NO MSG APPEARED. OK TO SERVICE.

Part: SKIN — DENTED (FUSELAGE) · airframe 96,738 hrs · 15,116 cycles

DENT IN FUSELAGE SKIN BS 1303.5 & 1 INCHES BELOW STRINGER 37L. REPAIRED DENT IN FUSELAGE SKIN IAW ECRA 5330-04977.

Part: DOUBLER — GOUGED (FUSELAGE) · airframe 96,738 hrs · 15,116 cycles

DEEP GOUGE ON DOUBLER AT BS 1819 WHERE PANEL 313CLX ATTACHES UNDER LT HORIZONTAL. R & R DOUBLER IAW SRM 53-80-01 FIG 201 REPAIR 3.

Part: DOUBLER — GOUGED (FUSELAGE) · airframe 96,738 hrs · 15,116 cycles

DEEP GOUGE ON DOUBLER AT BS 1819 WHERE PANEL 314CRX ATTACHES UNDER RT HORIZONTAL. R & R -1 DOUBLER IAW SRM 53-80-01 FIG 201 REPAIR 3.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 96,738 hrs · 15,116 cycles

CORROSION ON FLOORBEAM AT STATION 347, RBL 40 - 51. REPAIRED FLOORBEAM AT BS 347, RBL 14 TO SIDE OF BODY IAW SRM 53-00-51 REPAIR 1.

Part: DOOR — DENTED (CABIN) · airframe 96,738 hrs · 15,116 cycles

LEFT FWD ENTRY DOOR HAS 2 DENTS, ONE 18 INCHES FROM BOTTOM EDGE & 4 INCHES FROM AFT EDGE. ONE 20 INCHES FROM BOTTOM EDGE & 2 INCHES FROM AFT EDGE. FOUND OUT OF LIMITS. REPAIRED IAW SRM 52-10-01 FIG 201 REPAIR 6 CAT B REPAIR.

Part: SKIN — CRACKED (FUSELAGE) · airframe 96,738 hrs · 15,116 cycles

AD-2006-09-09 POPPED RIVET HEAD & EXTERNAL SKIN CRACKED LOWER CORNER APU INLET OPENING BS 1725, STRINGER 7R. REPAIRED IAW SRM 53-80-01 FIG 201 DET III RPR 5.

Part: CREASE BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 96,738 hrs · 15,116 cycles

CORROSION ON GUARD AT CREASE BEAM STATION 287.0, RBL 81. R & R CREASE BEAM AT BS 287.0, RBL 81 IAW SRM 51-40-02, PAR 7 FIG 1 DUE TO 100% MATERIAL LOSS PN 14 1T8310-410.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 96,738 hrs · 15,116 cycles

CORROSION ON FLOORBEAM AT STATION 325, RBL 22 - 52. REPAIRED CABIN FLOORBEAM AT STATION 325, RBL 10 - 52 IAW SRM 53-00-51, REPAIR 1 FIG 201.

Part: STRUCTURE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 96,738 hrs · 15,116 cycles

CORROSION ON TOP SURFACE OF MAIN FRAME, AFT CARGO COMPARTMENT FLOOR STRUCTURE BS 1197 RBL 22, LBL 42 & RBL 5.5. FLOOR STRUCTURE WAS FOUND TO BE OUT OF LIMITS IAW SRM 53-60-07 & 53-00-07 FIG 10 1 DET III. R & R UPPER CHORD IAW SRM 51-40-02 PAR A 4 FIG 3 & 8, SRM 53-60-07 & DWG 146T1206.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 96,738 hrs · 15,116 cycles

CORROSION ON FLOORBEAM AT STATION 287 RBL 19 MAIN CABIN. REPAIRED FLOORBEAM AT BS 287 IAW SRM 53-00-51 FIG 201 REPAIR 1. THIS IS A CATEGORY A REPAIR.

Part: STRUCTURE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 96,738 hrs · 15,116 cycles

CORROSION TWO EACH AREAS ON TOP SURFACE OF MAIN FRAME, AFT CGO COMPARTMENT FLOOR STRUCTURE BS 1219 LBL 10 & LBL 47. CORROSION WAS FOUND TO BE 100% MATERIAL LOSS & OUT OF LIMITS IAW SRM 53-00 -07 FIG 101. R & R CHORD IAW SRM 51-40-0 2 PARA 4 FIG 3, 4 & 8.

Part: CONNECTOR — LOOSE (CABIN) · airframe 95,551 hrs · 14,949 cycles

EMERGENCY LIGHTS ON SEATS 36B & 33J INOPERATIVE. TROUBLE SHOT & FOUND EMER EXIT LIGHTING CONNECTORS LOOSE AT SEAT ROWS 36AB & 33JK. SECURED & OPERATIONS CHECKED IAW AMM 33-51-00.

Part: STATUS MESSAGE — ACTIVATED (COCKPIT) · airframe 93,989 hrs · 14,745 cycles

STATUS MESSAGE RT REV ISLN VLV CAME ON UPON LANDING.

Part: HINGE — WORN (AC BAY) · airframe 93,987 hrs · 14,744 cycles

LT PACK RAM AIR INLET DOOR HINGE PIN IS MIGRATED OUT & RUBBING ON PLENUM. REMOVED LT PACK INLET DOOR. FWD & AFT DOOR HINGES WORN & AFT BLOCKS ARE WORN. ACCOMPLISHED INSTALLED INLET DOOR IAW AMM 21-53-01.

Part: LATCH — MISINSTALLED (OVERWING EXIT) · airframe 93,987 hrs · 14,744 cycles

FWD LATCH FOR LT OVERWING SLIDE PANEL DOES NOT ENGAGE. FOUND LATCH INSTALLED INCORRECTLY REINSTALLED LATCH IAW MM25-65-09 THRU STEP 3 D 1 D CONT OF AMIS ITEM 9872050. CONT IAW AMM 25-65-09 FROM 3 D 1 D THRU END OF 25-65-09, ALL CHECKED OK.

Part: A/C PACK — INOPERATIVE (AC BAY) · airframe 93,923 hrs · 14,736 cycles

RT PACK INOPERATIVE LT EICAS RT PACK TEMP. OPERATES IN STANDBY.

Part: HANDLE — DEFECTIVE (RUDDER PEDAL) · airframe 93,885 hrs · 14,731 cycles

CAPTAIN`S SIDE, RUDDER PEDAL ADJUST KNOB DOES NOT ENGAGE DETENTS, PEDALS CAN SLIP FWD. R & R CRANK HANDLE ON CRANK ASSEMBLY IAW AMM 27-21-06, OPERATIONS CHECKED NORMAL.

Part: OXYGEN MASK — UNSECURE (CABIN) · airframe 93,443 hrs · 14,676 cycles

O2 MASKS DOWN AT 24A. REPACKED MASKS IAW 35-21-14-532-268001 767-300 SUB UA AMM.

Part: TRANSCEIVER — FAULTY (VOR) · airframe 93,277 hrs · 14,655 cycles

CAPTAIN VOR INOPERATIVE. LT VOR TRANSCEIVER REPLACED IAW AMM. ALL CHECKED GOOD.

Part: SDU — FAILED (SATCOM) · airframe 93,088 hrs · 14,633 cycles

SATCOM FAILING SYSTEM TEST. FOUND SDU CH MOD 1 TX FAULT & SDU CH 1 RX FAULT. R&R M1780 SDU.

Part: LINE — DAMAGED (MLG BRAKE) · airframe 93,088 hrs · 14,633 cycles

BRAKE PRESSURE AT ZERO DURING COCKPIT PREFLIGHT CHECK. R & R HYDRAULIC BRAKE LINE FROM BRAKE METERING VALVE & THE AUTO BREAK SHUTTLE VALVE. LEAK CHECKED GOOD. BREAK PSI GOOD. HYD BRAKE ACC READS 0 PSI.

Part: VALVE — FAULTY (CABIN TEMP) · airframe 92,851 hrs · 14,600 cycles

AUX MID ZONE TEMP CONTROLLER FAULTING AUX MID TRIM VALVE. REPLACED AUX MIDTRIM VALVE, NO HELP, STILL FAULTS AUX TRIM VALVE ON CONTROLLER & UNABLE TO MOVE VALVE POSITION FROM FLIGHT DECK. SUSPECT BAD VALVE FROM STOCK PCN (643-9023). REPLACED AFT AUX TRIM VALVE IAW MM21-61-07.

Part: HEAT SHIELD — DAMAGED (ENGINE) · airframe 92,851 hrs · 14,600 cycles

HEAT SHIELD FOR HYD & FUEL LINES ON RT SIDE OF ENGINE DAMAGED. REPLACED HEAT SHIELD BLANKET.

Part: CONTROLLER — FAULTED (NR CABIN PRESS) · airframe 92,295 hrs · 14,531 cycles

CABIN ALTITUDE AUTO 2 NOT MAINTAINING. REACHED APPROX 8.5 DIFFERENTIAL PRESSURE CLIMBING AT 300 FT-MIN. SELECTED AUTO 1 AND SYS RESTORED. REPLACED NR 2 AUTO CABIN PRESSURE CONTROLLER.

Part: HARNESS — FAILED (EEC) · airframe 92,011 hrs · 14,495 cycles

NR 2 ENGINE T3 BLANK, REPLACED W6. 6451-2, STILL BLANK EVEN AFTER THE T3 PROBE WAS REPLACED. EEC HARNESS W6 REPLACED. RAN ENGINE CHECKED NORMAL.

Part: COVER — MISSING (SEAT ARMREST) · airframe 91,978 hrs · 14,491 cycles

ARMREST MISSING COVER, EXPOSED WIRES. REPLACED ARM COVER, NO EXPOSED WIRES.

Part: OXYGEN MASK — FAILED (FIRST OFFICER) · airframe 91,949 hrs · 11,487 cycles

FIRST OFFICER`S OXYGEN MASK LOUD SQUEAL WHEN AIR COMES OUT. R & R OXYGNE MASK IAW AMM 35-11-51. LEAK AND OPS CHECKED GOOD.

Part: CIRCUIT CARD — FAILED (PITOT HEAT) · airframe 91,683 hrs · 14,453 cycles

RIGHT AUX PITOT HEAT AND CAPTAIN`S PITOT HEAT MESSAGE ON LOWER EICAS. FOUND K514,K515, AND K516 STUCK IN AIR MODE. REPLACED M12 DRIVER CARD IN PSEU PER AMM. SYS OPS NORMAL PER AMM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 91,566 hrs · 14,439 cycles

FLOOR SPONGEY AND CLICKS LOUDLY IN AISLE FLOOR BY 7C-B AND 8C-B MADE INTERIM REPAIR IAW MM 53-21-99, .3" X 2" DELAMINATION IN FLOOR PANEL AT 7CB. REPAIR AT NEXT C CHECK.

Part: CONTROLLER — NO TEST (NR 2 ENGINE) · airframe 91,235 hrs · 14,398 cycles

NR 2 ENGINE HPC PNEUMATIC HEALTH CHECK TEST FAILED. NR 2 ENGINE HPC REPLACED AS PER AMM.

Part: SHUTOFF VALVE — SEIZED (NR 2 ENGINE) · airframe 91,235 hrs · 14,398 cycles

NR 2 ENGINE HPSOV TEST PORT FOUND SEIZED. NR 2 ENGINE HPSOV REPLACED AS PER AMM 36-11-07.

Part: LIGHT — DIM (COCKPIT DOOR) · airframe 91,235 hrs · 14,398 cycles

COCKPIT DOOR AREA OVERHEAD EMERGENCY LIGHT IS DIM. EMERGENCY LIGHT ASSY REPLACED AND OP TESTED NORMAL AMM.

Part: LIGHT — INOPERATIVE (SEAT 39B) · airframe 91,235 hrs · 14,398 cycles

SEAT 39B EMERGENCY LIGHT INOPERATIVE. EMERGENCY LIGHT ASSY REPLACED, OPS CHECKED NORMAL IAW MM.

Part: PUMP — FAULTY (HYDRAULIC SYS) · airframe 91,213 hrs · 14,395 cycles

RIGHT ELEC HYD PUMP PRESSURE IS LOW (2500 PSI) AS INDICATED ON HYD PAGE & BRAKE PRESSURE INDICATOR. REMOVED RIGHT HYD AC MOTOR PUMP. PUMP IS ON TABLE NEXT TO NR 2 ENGINE. INSTALLED RIGHT HYDRAULIC ACMP, LEAK CHECK GOOD.

Part: FITTING — LEAKING (HYD SYSTEM) · airframe 91,049 hrs · 14,375 cycles

ADP HAS A LEAKING HYD FITTING. TIGHTENED FITTING HALF A TURN. RAN ADP FOR 5 MIN NO LEAKAGE NOTED.

Part: SWITCH — DAMAGED (AUDIO PANEL) · airframe 91,016 hrs · 14,371 cycles

CAPTAIN`S AUDIO PANEL PTT SWITCH INTERMITTENT. REPLACED AUDIO CONTROL PANEL PER MM, GROUND CHECKED NORMAL.

Part: START VALVE — FAILED (LT ENGINE) · airframe 90,975 hrs · 14,364 cycles

LEFT ENGINE STARTER EICAS AND UNSUCCESSFUL START. PERFORMED MANUAL START AND CHECKED GOOD. REPLACED START VALVE.

Part: WHEEL — DAMAGED (NR 3 MLG) · airframe 90,923 hrs · 14,356 cycles

NR 3 TIRE HAS LUG NUTS SHEARED OFF AT 12 O'CLOCK POSITION. NR 3 WHEEL ASSY REPLACED AS PER AMM.

Part: RELAY — FAILED (FLAP/SLAT SYS) · airframe 90,796 hrs · 14,339 cycles

FLAP/SLAT ELECTRICAL STATUS MESSAGE ON EICAS. MESSAGE CLEARED AFTER RACKING M545 FSEU IAW FIM 27-51-00. MESSAGE COMES BACK AFTER CYCLE POWER. REPLACED FSEU M545 NO HELP, INSTALLED ORIGINAL FSEU. FOUND BAD FSEU FAULT RELAY K730, REPLACED K730 RELAY WDM 27-51-61 MESSAGE CLEARED. ACCOMPLISHED TEST PER AMM, OPS CHECKED GOOD.

Part: NUT PLATE — MISSING (LT WING SLAT) · airframe 90,796 hrs · 14,339 cycles

LEADING EDGE SLAT WING PANEL 500, LEFT WING. HAS FIVE FASTENERS DRILLED, NUT PLATES NEED TO BE REPLACED. REPLACED MISSING NUT PLATES AND SCREWS RE-INSTALLED PANEL.

Part: SWITCH — DIRTY (EMERGENCY LIGHTS) · airframe 90,380 hrs · 14,283 cycles

EMERGENCY LIGHTS SWITCH FROZEN IN ARMED POSITION. CLEANED SWITCH, OPS OKAY.

Part: CONNECTOR — UNSECURE (CENTER FUEL PUMP) · airframe 90,367 hrs · 14,281 cycles

CENTER AUXILLARY FUEL OVERRIDE PUMP LOW PRESSURE LIGHT ILLUMINATED. PUMP PREVIOUSLY REPLACED. SEATED CONNECTORS ON P-5 FUEL MANAGEMENT PANEL. FUELED CENTER TANK TO 5000 LBS. TRANSFERRED FUEL TO WING TANKS AND CENTER TANK. LOW PRESSURE LIGHTS GROUND CHECKED GOOD.

Part: SWITCH — FAULTY (EMERGENCY LIGHTS) · airframe 90,359 hrs · 14,280 cycles

EMERGENCY LIGHT SWITCH ON FLIGHT DECK WILL NOT MOVE OUT OF ARMED DETENT. REPAIRED EMERGENCY LIGHT SWITCH, OPS CHECKED NORMAL.

Part: TUBE — LEAKING (NR 5 SLAT TRACK) · airframe 90,229 hrs · 14,264 cycles

FOUND NR 5 SLAT TRACK DRAIN TUBE MISALIGNED AND LEAKING. DRAIN TUBE HAS DAMAGED END FITTING AND O-RINGS. REPLACED DRAIN TUBE IAW COA 618091. NO LEAKS NOTED.

Part: TUBE — LEAKING (RT WING) · airframe 90,220 hrs · 14,263 cycles

FUEL LEAK RIGHT WING. REPLACED NR 5 SLAT COVER DRAIN TUBE REF AD 767-57A0094 NO LEAKS NOTED REF COA 618091.

Part: SKIN — DAMAGED (BS 478-522) · airframe 90,126 hrs · 14,251 cycles

SCRATCH AND DENT FOUND BETWEEN BS 478- 522 S36-38R BELOW FWD CARGO DOOR. DENT DAMAGE EXCEEDS SRM 53-00-01 FIG 101 LIMITS. ECRA 5330-04380 FOLLOWED FOR INTERIM REPAIR. GOUGE BLENDED PER SRM 53-00-01 FIG 101 DETAIL II. HFEC INSPECTION PER NTM PART 6-51-00-01 AND NO CRACKS NOTED. CONFIRMED DENT IS SMOOTH, FREE FROM CRACKS AND GOUGES AND THERE IS NO OIL CANNING. ACCOMPLISHED PERMANENT REPAIR PER ECRA 5331-01676.

Part: FRAME — CORRODED (BS 977 S22R) · corrosion level 2 · airframe 90,126 hrs · 14,251 cycles

BS 977 FRAME CORRODED ON OUTER ANGLE AT S22R. CORROSION REMOVED PER SRM 53-00-01. BLEND OUT EXCEEDED MAX LIMITS, AND REPAIRED IAW ECRA 5352-01075. MAJOR REPAIR

Part: STRINGER — DAMAGED (BS 500 S37R) · airframe 90,126 hrs · 14,251 cycles

STRINGER 37R BS 500 DAMAGED. REPAIRED IAW ECRA 5331-01676.

Part: ACTUATOR — NO TEST (OVRWNG SLIDE) · airframe 90,126 hrs · 14,251 cycles

LEFT OVERWING ESCAPE SLIDE FAILED DEPLOYMENT CHECK, SPOILER ACTUATOR FIRED BUT DOOR DID NOT OPEN AND SLIDE DID NOT DEPLOY. REMOVED AND REPLACED FWD DOOR OPENING ACTUATOR CABLE. FOUR DOOR LATCHES REPLACED. SLIDE DEPLOYMENT BOTTLE REPLACED. REPLACED NR 6 SPOILER OVERRIDE ACTUATOR. REPLACED DOOR OPENING ACTUATORS.

Part: CHILLER — FAULTY (GALLEY) · airframe 93,829 hrs · 14,725 cycles

CHILLER C31 POPS CB WITH MEL 2520NB. PULLED & COLLARED CB. CHILLER IS MID GALLEY FWD SECTION. REPLACED MID GALLEY CHILLER POS C31 IAW AMM, OPERATIONS CHECKED NORMAL.

Part: WIRE — UNSECURE (CABIN) · airframe 90,030 hrs · 14,236 cycles

THE 24A WIRE HANGING OUT. CAPPED & STOWED EMERGENCY SEAT EXIT LIGHT FOR SEAT 23AB, STOWED WIRES UNDER SEAT IN THE OUTBOARD LEG SEAT BOX PANEL. REPINNED CAPPED WIRES AND INSTALLED CONNECTOR REF SWPM 20-64-17, SEAT 23AB EMERGENCY PATH LIGHT CHECK'S GOOD.

Part: STRUCTURE — DENTED (FUSELAGE) · airframe 89,990 hrs · 14,231 cycles

SCRATCH AND DENT FOUND BETWEEN STA 478- 522 S38-36R BELOW FWD CARGO DOOR SCRATCH 34.5" WAVE. WAVE FORM 6".DENT IS 10" LONG 3.5" WIDE DEPTH .147. FOUND ON ARRIVAL TO LHR. DENT DAMAGE EXCEEDS SRM 53-00-01 FIG 101 LIMITS. EC-RA 5330-04380 FOLLOWED FOR INTERIM REPAIR. ACCESS GAINED TO ADJACENT STRUCTURE, NO OTHER DAMAGE NOTED GOUGE BLENDED PER SRM 53-00-01 FIG 101 DETAIL II. DEEPEST AREA OF BLEND 6" AFT OF STN478 BLENDED OUT TO .010" 130252. ACP'D HFEC INSPECTION PER NTM PART 6-51-00-01 AND NO CRACKS NOTED. CONFIRMED DENT IS SMOOTH, FREE FROM CRACKS AND GOUGES, AND THERE IS NO OIL CANNING. ACP A PERMANENT REPAIR.

Part: HYDRAULIC SYSTEM — LOW (RIGHT) · airframe 89,612 hrs · 14,182 cycles

RIGHT HYD LOW NEEDS FLUID READS .66. SERVICING PERFORMED AS AMM TASK 12-12-01-703-062 OK. ADDED 5 QTS HYD OIL TO CTR AND 7 QUARTS IN THE RIGHT RESERVOIR.

Part: HOSE — LEAKING (BRAKE SYSTEM) · airframe 89,612 hrs · 14,182 cycles

LEFT GEAR BREAK LINE LEAKING. WORKING WITH LOCAL MECH TO ID WHICH LINES AND BRAKE, WORKING WITH ORDLE FOR AN ECRA TO DEF THE BRAKE. LOOKING FOR CAPS TO CAP LINES. FOUND NR 1 BRAKE FLEX HYD LINE ABOVE THE GEAR LEAKING HYD, REF IPC 32-41-62-005, ITEM 172(160-1560). BRAKE FLEX HOSE LINE RPL'D AS AMM TASK 20-10-10-404-002 LEAK TEST PERFORMED OK. CTR AND RIGHT HYD SYS SERVICED

Part: CLAMP — UNSECURE (HEAT VALVE) · airframe 89,101 hrs · 14,112 cycles

UNUSUAL HEAT BLOWING FROM FLOOR LEVEL SIDEWALL VENTS AT LEFT SIDE ROW 38. INSPECTED REAR AND BULK CARGO HEAT VALVES. FOUND ON BULK CARGO HEAT VALVE UPPER PIPING CLAMP CONNECTION SLIGHT HOT AIR ESCAPING. CHECK TIGHTENED CLAMP CONNECTION AND SUBSEQUENT LEAK CHECK NOW SATISFACTORY AND NO MORE WARM AIR FROM FLOOR PANELS AT REAR LEFT CABIN. RELEASED A-C FOR SERVICE.

Part: UNKNOWN — MALFUNCTIONED (CABIN) · airframe 89,012 hrs · 14,101 cycles

MID CABIN AUTO CONTROL INOPERATIVE.

Part: KNOB — LOOSE (RADAR) · airframe 88,486 hrs · 14,032 cycles

FIRST OFFICER'S RADAR AND HSI DIMMING KNOB LOOSE AND CAN BE LIFTED VERTICALLY OUT OF DETENT. REPLACED THE UNIT.

Part: STATOR — BROKEN (BRAKE) · airframe 88,335 hrs · 14,015 cycles

ON WALKAROUND, FOUND PARTS OF NR 7 BRAKE UNIT STATOR BROKEN. NR 7 MAIN WHEEL BRAKE ASSY REPLACED AS PER AMM. INSPECTED MAIN AXLE ASSY NO DAMAGE OR FAULTS FOUND MAIN WHEEL ASSY REMOVED AND REFITTED AS PER AMM. WHEEL INSPECTED, NO DAMAGE FOUND.

Part: ACTUATOR — CRACKED (SPOILERS) · airframe 88,027 hrs · 13,975 cycles

HYD QTY DECREASED TO ZERO AND SYSTEM PRESS AND QTY LIGHT ILLUM EICAS MSG DISPLAYED (L,R) HYD SYS PRESSURE, (L,R) HYD QTY POS 1 (01=L,02=R). FRM CODE 29 11 12 --. ON INSPECTION FOUND LEFT WING INBOARD SPOILER ACTUATOR NR 6 HAS CRACKED CASE. REPLACED ACTUATOR AS PER MM. CARRIED OUT LEAK CHECK OF ALL THREE HYD SYSTEMS AND FUNCTION CHECK OF SPOILERS AND FLAP-SLAT SYSTEMS. SPOILER PANEL RIG CONFIRMED AS ACCEPTABLE AS PER MM. ALL SYSTEMS ARE FULL AND OPERATE NORMALLY. PLEASE NOTE THIS PART IS A BORROWED PART FROM BRITISH AIRWAYS, PART NR ON 252T1301-3; SERIAL NR ON 1252. PART NR OFF 252T1301-3 SERIAL NR OFF 2247A. CONTAINER IS PLACED IN BULK CARGO.

Part: LATCH — UNSECURE (RT NACELLE) · airframe 87,825 hrs · 13,947 cycles

THIRD FASTENER ABOVE RIGHT ENG OUTBOARD SIDE UNLATCHED. SECURED LATCH.

Part: POWER CABLE — DAMAGED (AFT GALLEY) · airframe 87,722 hrs · 13,932 cycles

AFT GALLEY, PIGTAIL P51 P52 P53 HAS EXPOSED WIRES. REPLACED P52 AND P53 PIGTAIL POWER CORDS. REPLACED P51 PIGTAIL. ALL PIGTAILS OPERATE NORMAL.

Part: SWITCH — NO TEST (BLEED AIR SYS) · airframe 87,066 hrs · 13,845 cycles

LEFT ENG BLEED LIGHT INOP AND WILL NOT TEST. RELAMPED LIGHT SW.

Part: AUDIO PANEL — MALFUNCTIONED · airframe 86,992 hrs · 13,835 cycles

SEAT AUDIO STATIC ROWS 19AB THROUGH 39AB.

Part: DUCT — BLOWN (CABIN AIR) · airframe 87,050 hrs · 13,843 cycles

ROW 19 AB BLOWN DUCT, SECURED WITH TYPE 44 ADHESIVE REF BAC DWG 214T4020.

Part: VALVE — FAULTY (FUEL SYSTEM) · airframe 86,736 hrs · 13,798 cycles

HAD TO X FEED TWICE DUE TO 1500LBS IMBALANCE. FMC SHOWED EVEN BURN ON BOTH ENGINES. DUE TO HISTORY OF UNWANTED FUEL TRANSFER, REPLACE THE FWD AND AFT FUEL CROSSFEED VALVES & ACTUATORS. REPLACED BOTH XFEED VLVS AND ACTUATORS, AND ALL TESTED NORMAL.

Part: STRUCTURE — DAMAGED (CARGO BAY) · airframe 86,736 hrs · 13,798 cycles

RAMP REPORTS SMALL HOLE IN AFT PIT FLOOR. RPR MADE PER GNMM 1- 0-1-102. HOLE LOCATED NEAR CARGO NET ATTACH IN MIDDLE OF BULK PIT. REPAIRED SMALL HOLE PER SRM 53-60-53.

Part: DISPLAY — FAULTY (COCKPIT) · airframe 86,620 hrs · 13,784 cycles

UPPER EICAS SCREEN SHOWING INCORRECT COLORS AND STATUS WON'T DIM AFTER SHUTDOWN. REPLACED UPPER EICAS DISPLAY PER AMM. OP CHECK OKAY.

Part: ENGINE — VIBRATION (NR 1) · airframe 86,454 hrs · 13,759 cycles

DUE TO REPEAT VIB IND HIGHER THAN NORMAL TO PREVENT IRREG OPS, ACCOMPLISH FAN BLADE ROOT LUBE. `WILL REQUIRE VIBRATION SURVEY (HIGH POWER RUN), TEST NR 8 PER AMM. ACP'D TEST NR 8 VIBRATION SURVEY. TEST FAILED, (N1 VIB) INDICATES 4.2 AT 78% N1 AND (BB VIB) WAS 2.3 AT 77% N1. ACCMP'D TRIM BALANCE REF SFOPD JIC R0931. ACCMP VIBRATION SURVEY REF MM. CHKS WITHIN LIMITS. MAX VIB 2.8 N1 AT 78% N1 ON DECEL.

Part: FITTING — WORN (LT MLG DOOR) · airframe 86,182 hrs · 13,722 cycles

LT MLG TRUNNION DOOR AFT HINGE HAS EXCESSIVE PLAY. FOUND AFT DOOR FITTING HAT BUSHINGS WORN AND PULLED OUT OF FITTING. NEW FITTING ASSY ON ORDER. WILL NEED FITTING 113T8313-6 AOG S5293. WORKING OUTSIDE. WILL REQUIRE GEAR SWING AFTER FITTING REPLACEMENT. PART ETA. REPLACED LT TRUNNION DOOR AFT ATTACH FITTING.

Part: SEAT — UNSECURE (ROW 37) · airframe 86,020 hrs · 13,702 cycles

ROW 37 MIDDLE SECTION OF SEATS COMING UNATTACHED FROM FLOOR ON RIGHT SIDE. SECURED SEAT ASSEMBLY IN TRACK.

Part: HOSE — CRACKED (ANTI-SKID MODULE) · airframe 85,589 hrs · 13,644 cycles

ONE HOSE TO THE ANTI SKID SHUT OFF VALVE MODULE IS CRACKED. BRAKE POS 6 HAS BEEN DEACTIVATED. REPAIRED, PRESSURIZED LINE TO 6K PSI, NO LEAKS NOTED. FOUND BAD UNION PACKING. REPLACED PACKING, OPS NORMAL.

Part: MODULE — MALFUNCTIONED (LEFT) · airframe 84,987 hrs · 13,567 cycles

ALTITUDE ALERT CHIME GOES OFF RANDOMLY THROUGHOUT FLIGHT IN CRUISE. REPLACED LEFT SIREN-OWL MODULE M999, REF MM.

Part: FILTER — DIRTY (APU) · airframe 84,238 hrs · 13,452 cycles

APU FAILED. APU FAILED AT DEP TIME. TROUBLE SHOT PER FAULT DISPLAY. ACCOMPLISHED BITE CHECK. FAULT DISPLAY SHOWED "GEN FILTER" FAULT. REPLACED GENERATOR SCAVENGE FILTER AND LUBE FILTER ASSY'S IAW MM. APU STARTS AND RUNS NORMAL.

Part: MODULATING VALVE — FAULTY (CABIN TEMP) · airframe 84,186 hrs · 13,446 cycles

AFT CABIN TEMP EICAS. PERFORMED BITE ZONE TEMP CONTROLLER, FOUND AFT TRIM AIR VALVE FAULT, DEFERRED AFT TRIM AIR VALVE PER MEL 2161BB, VALVE SHOWED CLOSED ON EICAS, SECURED CLOSE PER CB'S PULL OUT IAW MEL PROCEDURE 1. REPLACED AFT TRIM AIR VALVE, NO HELP. SUSPECT BAD VALVE FROM STOCK. CONNECTOR WAS DIFFICULT TO REMOVE AND INSTALL. RECOLLARED BREAKERS. REPLACED TRIM AIR MODULATING VALVE PER MM.

Part: B-NUT — LEAKING (RT MLG WW) · airframe 84,053 hrs · 13,420 cycles

FLAP SLAT HYDRAULIC SHUTOFF VALVE IN RT MAIN GEAR WHEEL WELL LEAKING 20 DROPS PER MINUTE FROM PRESSURE PORT B-NUT. ACCOMPLISHED RINGLOCK REPAIR TO PRESSURE PORT END OF TUBE PER GNMM. LEAK CHECK OKAY.

Part: SKIN — DENTED (FUSELAGE) · airframe 83,789 hrs · 13,382 cycles

DURING ACFT LOADING HAD IMPACT AT DOOR 2L. STATION IS 46 BETWEEN 1540 TO 1562 AND STRINGER LOC IS APPROX S22 TO S23. DIMENSIONS OF THE DENT ARE (INCHES): LENGTH 3.5 WIDTH 2.75 AND DEPTH 0.0858. THE DENT IS SMOOTH WITH NO SHARP EDGES CUTS OR CREASE, ADJACENT RIVETS APPEARS OK IAW SRM DENT IS WITHIN LIMITS. YELLOW DOT APPLIED. DENT IS JUST AFT AND BELOW DOOR 2LT CUTOUT NEAR REGISTRATION NUMBER. MARKED WITH YELLOW DOT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 83,712 hrs · 13,370 cycles

AFT SEAT MOUNTED EEL INOP AT SEAT 8AB. RELAMPED, OP NORMAL.

Part: CONNECTOR — UNSECURE (CABIN) · airframe 83,712 hrs · 13,370 cycles

EEL EXIT SIGNS AND OVERHEAD AISLE LIGHTS INOP AFT RT SECTION. SECURED CONNECTOR ON PWR SUPPLY ASSY M734, CHECKS OKAY.

Part: PUMP — MALFUNCTIONED (FUEL SYSTEM) · airframe 83,438 hrs · 13,331 cycles

CENTER R FUEL PUMP DISPLAYED, CB GRIB ON P6-4 F21 R FUEL OVERRIDE PUMP. REPLACED CENTER RT FUEL OVERRIDE PUMP PER MM, OPS CHECKS GOOD.

Part: CDU — FAULTY (COCKPIT) · airframe 83,423 hrs · 13,329 cycles

R CDU (F-O) BLANKED OUT, RTFL. REPLACED R CDU PER MM, OPS CHECKS OKAY.

Part: START VALVE — FAILED (RT ENGINE) · airframe 83,382 hrs · 13,323 cycles

RIGHT ENGINE START VALVE LIGHT DID NOT EXTINGUISH WHEN START VALVE CLOSED. CYCLED CIRCUIT BREAKER D20. DURING NEXT START ATTEMPT, VALVE LIGHT CAME ON BUT NO DUCT PRESSURE DROP. OBSERVED & N2 ROTATION. REPLACED NR 2 ENG STARTER AND START VALVE. OPERATION OF STARTER AND VALVE NORMAL.

Part: SEAL — LEAKING (PAX DOOR) · airframe 83,352 hrs · 13,319 cycles

DOOR PRESSURE LEAK, RTFL CAN SEE DAYLIGHT UNDER DOOR. FOUND LOOSE AND THRESHOLD FOUND INTACT AND IN GOOD CONDITION. LEAKED CHECKED DOOR PER MM, NO LEAKS FOUND.

Part: HANDSET — INOPERATIVE (CABIN) · airframe 83,318 hrs · 13,313 cycles

PURSER UNABLE TO CALL COCKPIT FROM DOOR 1L. REPLACED HANDSET AT 1L, OPS CHECK. GOOD.

Part: BOTTLE — UNSERVICEABLE (EVAC SLIDE) · airframe 82,947 hrs · 13,263 cycles

LEFT OFF WING EMERGENCY SLIDE BOTTLE NEEDS REPLACEMENT. REPLACED LT OVERWING SLIDE EMERGENCY BOTTLE. ACCOMPLISHED RII INSPECTION AS REQUIRED REF MM. ALL PINS REMOVED AND SYSTEM RE-ARMED.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 82,248 hrs · 13,165 cycles

EMERGENCY EXIT LIGHTS ON AFT OF CABIN. REPLACED AFT RT SIDE BATTERY PACKS PER MM.

Part: SLIDE — UNSECURE (R1 DOOR) · airframe 82,172 hrs · 13,154 cycles

DOOR 1R SLIDE HAS COVER LACING UNRAVELED ON THE AFT SIDE. REMOVED AND REPLACED DOOR 1 RIGHT SLIDE RAFT ASSY PER MM.

Part: FEEDER CABLE — BURNED (GENERATOR) · airframe 82,110 hrs · 13,146 cycles

APU GEN WILL NOT STAY ON LINE. APU RUNS AIR. APU ELECTRICAL INOP. APU PNEUMATIC FUNCTION IS OK. DEFERRED APU GENERATOR PER MEL. HMG TEST OK. GROUND CREW REPORTS THE 2ND AND 3RD FEEDER WIRES ARE BURNED AT THE GENERATOR TERMINAL BLOCK . THE FEEDER WIRES ARE SECURE. PERFORMED BPCU TEST. APU GEN SYS SHOWS DP TRIP, OVERLAP ZONE, GEN-FDR. CHECKED APU GEN FEEDER CABLES AND FOUND THAT 2 OF THE FEEDER CABLES SHOW BURN MARKS AT THE TERMINAL BLOCK. REPLACED GENERATOR AND FEEDER HARNESS FROM GEN TO FIREWALL. ALL OPS CK NORMAL ON GROUND.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 81,981 hrs · 13,127 cycles

EMERGENCY FLOOR PATH LIGHT RT AISLE FWD GALLEY (L901) AND EMERGENCY EXIT IDENTIFIER AT DOOR 1 RT (L972) ARE INOP. REPLACED LIGHT ASSY, TESTED OK.

Part: STAND OFF — BROKEN (E/E BAY) · airframe 81,903 hrs · 13,115 cycles

FOUND P33 PANEL EQUIPMENT SHELF STANDOFFS BROKEN. OPENED P33 PANEL REMOVED INSIDE RELAY BRACKET, REMOVED 2 UPPER BROKEN STAND OFFS STARTED TO FABRICATE LOWER CORNER STRAP REPAIR. NO ELECTRICAL COMPONENTS WERE DISTURBED INSIDE P-33 PANEL. ALSO REPLACED BROKEN STAND-OFFS. CLEANED AREA AND CLOSED PANEL.

Part: WIRE HARNESS — DAMAGED (WINDSHIELD) · airframe 81,222 hrs · 13,022 cycles

WINDSHIELD HEAT MESSAGE, RTFL. WINDOW L1 FOUND J5 WIRE HARNESS TERMINAL PROTECTOR CAP MELTED. DISCONNECTED TERMINAL BLOCK FROM WINDOW. REPLACED TERMINAL AND WIRE ASSY. OPS NORMAL.

Part: CONTROL UNIT — FAULTY (POSITION 1) · airframe 81,128 hrs · 13,009 cycles

RIGHT AND LEFT UTILITY BUSSES WILL NOT COME ON LINE AND A-C WILL NOT TAKE GROUND POWER. REPLACED BUSS POWER CONTROL UNIT IAW MM. OPS CKS NORMAL. BOTH UTILITY BUSSES ON LINE AND A-C WILL ACCEPT GROUND POWER.

Part: DIPLEXER — MALFUNCTIONED (SATCOMM) · airframe 80,660 hrs · 12,937 cycles

SATCOM FAILED TWICE DURING CALLS. INITIALLY COMMS ESTABLISHED BRIEFLY AND THEN DROPPED. REPLACED M1791, DUE TO A LGA HPA VSWR FAULT. OPS CK OK.

Part: ENGINE — COKED (NR 1) · airframe 80,654 hrs · 12,933 cycles

NR1 ENGINE HAS COAKING ON VSV AND COMPRESSOR CASE. REPLACED ENGINE.

Part: IDG — FAULTY (NR 2) · airframe 80,654 hrs · 12,933 cycles

LOAD SHED ISSUES. DUE TO REPORT OF RT HYD QTY INDICATION DROP TWO TIMES AND FWD AND RT AFT GALLEY POWER WENT OFF NEED TO PERFORM A VISUAL INSPECTION OF RT GEN BREAKER TERMINALS (3 PHASE) C903. REPLACED RELAY & REPLACED NR 2 ENG IDG PER MM.

Part: ACTUATOR — LEAKING (LT ENG VSV) · airframe 80,592 hrs · 12,923 cycles

AFTER ARRIVAL FOUND LT ENGINE FUEL LEAK FROM DRAIN TUBE NR5, VARIABLE STATOR VANE ACTUATOR. PERFORMED ENG RUN UP IAW AMM. LEAK WITHIN LIMIT IAW AMM. REPLACE THE VSV ACTUATOR NOT MORE THEN 50 F HOURS. INSPECT THE LEAK BEFORE EACH DEPARTURE. TO PREVENT IRREG OPS REPLACE LT ENG STATOR VANE ACTUATOR. REPLACED NR 1 ENG VSV ACTUATOR IAW MM, OPS CHECKED GOOD.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHT) · airframe 80,326 hrs · 12,890 cycles

SEAT 1A AFT EMERGENCY LIGHT INOP, REPLACED LIGHT ASSY, NO HELP. FOUND CONNECTOR INSIDE SEAT CONSOLE ASSY DISCONNECTED, RECONNECTED AND SECURED CONNECTOR. OP CHECK OF EEL LIGHT GOOD.

Part: TRANSCEIVER — FAULTY (HF SYSTEM) · airframe 80,251 hrs · 12,881 cycles

RIGHT HF TRANSMISSIONS ARE INOP IN ALL CREW POSITIONS. RECEPTION IS NORMAL REPLACED RT TRANSCEIVER PER MM. ACCOMPLISHED LAMP TEST ON FRONT PANEL. NO LIGHT CAME ON. CYCLED CB. NO HELP. REPLACED RT TRANSCEIVER PER MM. OPS NORMAL.

Part: OVEN — CONTAMINATED (GALLEY) · airframe 80,101 hrs · 12,865 cycles

CREW REPORTS BURNING ODOR IN CABIN. ACCOMPLISHED INSP OF MID GALLEY AREA. FOUND MELTED PLASTIC IN WARMING OVEN W41. CLEANED OVEN, OPS CHECK NORMAL.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHTS) · airframe 79,779 hrs · 12,824 cycles

SEAT MOUNTED EMERGENCY EXIT LIGHT ON SEAT 10J (FWD) INOP. SEAT MOUNTED EMERGENCY EXIT LIGHT ON SEAT 10J (FWD) INOP. FOUND LIGHT DISCONNECTED, SECURED CONNECTOR. OP NORMAL.

Part: LIGHT — WRONG PART (SEAT 19J) · airframe 79,779 hrs · 12,824 cycles

SEAT MOUNTED EMERGENCY EXIT LIGHT ON SEAT 19J IS THE WRONG COLOR, IT SHOULD BE RED. SEAT MOUNTED EMERGENCY EXIT LIGHT ON SEAT 19J IS THE WRONG COLOR, IT SHOULD BE RED.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 79,779 hrs · 12,824 cycles

SEAT MOUNTED EMERGENCY EXIT LIGHT ON SEAT 37B IS INOP. RELAMPED, OP NORMAL.

Part: CIRCUIT CARD — FAULTY (TE FLAPS) · airframe 79,760 hrs · 12,821 cycles

FLAP DISAGREE MSG. CONFIG LGT ON & EICAS MSG FLAPS DISPLAY WITH FLAP IN TAKE OFF POSITION, ABORTED TAKEOFF AT 20 KNOTS IAW CREW. PERFORMED FIM TASK 31-51-00 VERIFIED WIRING FROM WEU TAKEOFF CONFIG CARD PIN 44 TO FSEU AND CHECKED DIODE R607. WIRING CHECKED GOOD. REPLACED TAKEOFF CONFIG CARD. TAKEOFF CONFIG, OPS CHECKS NORMAL.

Part: CONTROLLER — FAILED (POSITION 2) · airframe 79,685 hrs · 12,808 cycles

RIGHT HPSOV EICAS MESSAGE DURING TAXI. RT HPSOV INOP PER MEL. BIT AIR SUPPLY MODULE WITH 2 EA FAULTS SHOWN FOR HPC. REPLACED HPC PER AMM. RAN ENG AND APPLIED PNEUMATIC LOADS, NO FAULTS NOTED.

Part: SHUTOFF VALVE — FAULTY (POSITION 2) · airframe 79,670 hrs · 12,806 cycles

RT BLEED LGT AND HI STAGE (OVHT) LGT ILLUMINATED. CREW COMMENTS: RT BLEED LIGHT AND HPSOV EICAS ILLUMINATED AT TOD. RT BLEED VALVE WAS CLOSED. BITE CHECK OF BLEED CONTROLLER FAULTS HPSOV. HPSOV LOCKED OUT IAW IN CLOSED POSITION. PERFORMED HEALTH CHECK, FOUND BAD FAN AIR VALVE, INTERNAL ELECTRICAL SHORT. REPLACED FAN AIR MOD. VALVE IAW MM. RE-ACTIVATED RT ENGINE HPSOV. FOUND DAMAGED ELBOW FOR CONTROL PRESSURE LINE AT HPSOV. REPLACED ELBOW ASSY. RT BLEED CHECKS NORMAL DURING ENGINE RUN.

Part: SHUTOFF VALVE — MALFUNCTIONED (BLEED AIR SYS) · airframe 79,500 hrs · 12,784 cycles

RIGHT ENG BLEED LIGHT & RT ENG HPSOV EICAS MSG, ENG BLEED SW OFF & ENG RUNNING, LT & RT DUCT PRESS ARE ON. BLEED LIGHT ALSO ON PRESSURE ALMOST 0-3 PSI. HPSOV LOCKED CLOSED. REPLACED HPSOV AND HPSOV CONTROLLER, OPS CHECK GOOD.

Part: PACKING — FAULTY (FUEL SYSTEM) · airframe 79,339 hrs · 12,761 cycles

DURING PFC FOUND FUEL LEAK ENG 100. LEAK LOCATED BETWEEN FUEL PUMP AND VALVE-FUEL BYPASS ASSEMBLY. PACKING REPLACED. RUN UP PERFORMED BY COCKPIT CREW. LEAK NO LONGER PRESENT.

Part: VALVE — FAULTY (LT ACM) · airframe 79,312 hrs · 12,758 cycles

APU NOT COOLING WITH PACKS IN FULL COLD. FOUND LT PACK NOT COOLING. REPLACED LT COMPRESSOR OUTLET TEMP SENSOR, LT PACK CONTROL ASSY AND LT PACK LOW LIMIT VALVE. RAN PACK FOR 45 MINUTES. OPS CK OK.

Part: ACM — FAILED (LEFT) · airframe 79,291 hrs · 12,756 cycles

APU PUTTING OUT HOT AIR ONLY. CABIN ZONE TEMP CONTROLLER FAULT ON UNIT, REPLACED. NO HELP. CHANGED LEFT AIR CYCLE MACHINE. PACK OUTPUT NORMAL.

Part: CONNECTOR — INOPERATIVE (EMERGENCY LIGHTS) · airframe 79,219 hrs · 12,746 cycles

FLOOR EMERGENCY LIGHT ADJACENT TO DOOR 1R INOP. THIS IS AN EMERGENCY LIGHT STRIP ADJACENT TO GALLEY. THIS IS NOT A CROSS AISLE. DOOR 1R EMERGENCY LIGHT WORK NORMAL AND CROSS AISLE LIGHT WORKS NORMAL, JUST 1EA EMERGENCY STRIP INOP. CLEANED AND RE-SECURED EMERGENCY LIGHT STRIP CONNECTOR. OPS CHECKS GOOD.

Part: ACTUATOR — LEAKING (THRUST REVERSER) · airframe 79,211 hrs · 12,743 cycles

REVERSER ACTUATOR LEAKING. REMOVED NR 1 ENGINE RIGHT SIDE TOP UNLOCKING ACTUATOR. ACCOMPLISHED REMAINING INSTALLATION FROM MM STEP 6 ITEM D TO COMPLETION. ACTUATOR REPLACEMENT COMPLETED.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 78,993 hrs · 12,710 cycles

EMERGENCY FLASHLIGHT AT DOOR 2L HAS BAD BATTERY. REPLACED FLASHLIGHT BATTERY AND SEAL.

Part: RELAY — INTERMITTENT (APU FUEL) · airframe 78,922 hrs · 12,700 cycles

APU WILL NOT START. REPLACED FUEL CONTROL, NO HELP, FOUND APU FUEL VALVE INTERMITTENT, REPLACED, NO HELP. REPLACED RELAYS K175 AND K192. APU OPS CHECK GOOD.

Part: POWER SUPPLY — FAULTY (EMERGENCY LIGHT) · airframe 78,870 hrs · 12,693 cycles

DOOR 2L EMERGENCY EXIT LIGHT ON. REPLACED POWER SUPPLY AND OPS CK GOOD.

Part: SENSOR — FAULTY (PROBE HEAT LT) · airframe 78,821 hrs · 12,686 cycles

EICAS MSG PROBE HEAT DISPLAYED. TWO OR MORE PROBE HEAT LIGHTS REMAIN ILLUM DURING PROBE HEAT TEST WITH APL ON GRD AND ENGS OFF (FAULTY PROBES IDENTIFIED IN LOG). CREW COMMENTS: TAT F/O PITOT L AUX PITOT. REPLACED S268, NO HELP. REPLACED S10598, CHECKS NORMAL.

Part: HEAT EXCHANGER — DAMAGED (LT A/C PACK) · airframe 78,315 hrs · 12,618 cycles

LEFT PACK BAY DUCT BETWEEN HEAT EXCHANGER AND ACM DUCT HAS HOLE IN IT. REPLACED DAMAGE HEAT EXCHANGER AND ACM DUCT.

Part: ISOLATION VALVE — FAULTY (LEFT) · airframe 75,185 hrs · 12,319 cycles

LEFT ISOLATION VALVE LIGHT ON ISOLATION VALVE IS FAULTY. REPLACED LT ISOLATION VALVE, CKS OK.

Part: AUDIO PANEL — FAULTY (COCKPIT) · airframe 78,232 hrs · 12,605 cycles

COPILOT AUDIO CONTROL HAS AUDIBLE TONE WHEN ANY MIC SELECTOR IS PRESSED. SWAPPED PANEL WITH SECOND OBSERVERS PANEL. F/O PANEL, OPS NORMAL. SECOND OBSERVERS SEAT AUDIO PANEL WAS SWAPPED WITH FO AUDIO PANEL, AUDIO PANEL INOP. REPLACED ACP.

Part: LATCH — CRACKED (THRUST REVERSER) · airframe 78,124 hrs · 12,591 cycles

RT ENG T/R COWL V-BAND LATCH CRACKED. REPLACED RT ENG T/R COWL V-BAND, CKD OPS OK.

Part: LINE — LEAKING (HYD SYSTEM) · airframe 78,000 hrs · 12,571 cycles

C HYD SYS PRESS ON UPPER EICAS. FLUID LEVEL IS .14. FOUND CTR HYD LINE ON LT MAIN GEAR TRUCK POSITIONER LEAKING. REPLACE HYD LINE AND ACCOMPLISH TEST IAW MM. OPS CKS OK.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 78,000 hrs · 12,571 cycles

FLOOR EXIT PATH LIGHTS ON IN BACK THIRD OF AIRPLANE. PERFORMED EEL RESET TEST. EEL RESET AS NEEDED. NO DEFECTS NOTED.

Part: MODULE — FAULTY (TRIM SYSTEM) · airframe 76,993 hrs · 12,423 cycles

CTR SYS WILL NOT TRIM NOSE DOWN. ACFT WILL NOT TRIM NOSE DOWN WITH CTGTR SYS, NOSE UP OK. SINGLE CHANNEL CHECKS OK, LT SYS TRIMS NORMAL, ALT TRIMS NORMAL. OPS CHK INDICATES RT WILL NOT TRIM IN PRIMARY AND ALTERNATE. REPLACED RT STAB TRIM LOCKOUT MODULE. ACFT WILL NOT TRIM NOSE DOWN ON RT PRIMARY CHANNEL. NO CLICK AT SWITCH. REPLACED RT STAB TRIM LIMIT SWITCH AND POS TRANSMITTER.

Part: TANK — LEAKING (RT WING) · airframe 76,963 hrs · 12,418 cycles

RT WING ROOT FUEL LEAKING FROM SEAM INTO THE AC BAY. CTR TANK OPEN AND VENTED, RT TANK OPEN AND VENTED, IN TANK ACP BLOW BACK TO SOURCE LEAK. FUEL SEEP STOPPED, CLEANING AREA WHERE NEW SEALANT TO BE APPLIED. ACCOMPLISHED FUEL TANK SEALANT REPAIR OF AFFECTED LEAKING AREA ON INTERNAL AND EXTERNAL OF TANK.

Part: ACTUATOR — MALFUNCTIONED (CROSSFEED VALVE) · airframe 76,904 hrs · 12,409 cycles

AFT FUEL CROSSFEED VALVE LT-ON-& "FUEL CROSSFEED" EICAS MSG. ACTUATOR FOUND FAULTY. REPLACED AFT ENG CROSSFEED VALVE ACTUATOR. OPERATIONAL CHECK GOOD. NEXT SEGMENT AFT FUEL CROSSFEED VALVE LIGHT ON WITH SWITCH IN OFF POSITION. REPLACED VALVE ACTUATOR AGAIN. OP CHKS NORMAL.

Part: ASPIRATOR — LEAKING (OVERWING SLIDE) · airframe 76,628 hrs · 12,368 cycles

ASPIRATOR LEAKING FROM BARREL. EXTERNAL DAMAGE TO THE OUTSIDE OF ASPIRATOR. REPLACED ASPIRATOR.

Part: LIGHT — INOPERATIVE (INDICATOR) · airframe 76,668 hrs · 12,374 cycles

WHEEL WELL FIRE LIGHT ON ROLL OUT NO BELLS WITH IT. LIGHT ASSY (WHEEL WELL) LIGHT AT FAULT. NEEDS LIGHT ASSY REPLACED. WHEEL WELL FIRE TEST OK PCN FOR BASE ASSY.

Part: SHUTOFF VALVE — MALFUNCTIONED (RT ENGINE) · airframe 76,440 hrs · 12,334 cycles

AFTER ENG START R ENG HPSOV & ASSOCIATED BLEED VALVE ILLUMINATED. REPLACED HPSOV VALVE RT, RAN ENG; NO MESSAGES.

Part: GASPER FAN — OVERHEATED (MID GALLEY) · airframe 76,086 hrs · 12,284 cycles

ELECTRICAL BURNING ODOR AT MIDDLE GALLEY AREA. CHECKED MIDDLE GALLEY AREA ABOVE CEILING AND NOTHING ABNORMAL FOUND. NOTICED GASPER FAN MOTOR VERY HOT. DEACTIVATED GASPER FAN AND ODOR DISAPPEARED. SUGGEST GASPER FAN REPLACEMENT.

Part: ANTI-ICE VALVE — FAILED (LT ENGINE) · airframe 76,031 hrs · 12,275 cycles

L ENG A-I WILL NOT OPEN. ENGINE ANTI ICE VALVE WAS INTERNALLY FAILED. REPLACED AND OPS CHECKED VALVE. CHECKS OKAY.

Part: RESTRICTOR VALVE — FAULTY (THRUST REVERSER) · airframe 75,906 hrs · 12,260 cycles

NR 2 T-R ISO VALVE FAILED CHECK. RESTRICTOR REMOVED AND REPLACED BY REDUCER (MS21916D10-8) AND PACKING (NAS1612-10).

Part: TERMINAL — BROKEN (CABIN) · airframe 75,808 hrs · 12,242 cycles

EMERGENCY ESCAPE BATTERY PACK BEHIND SEAT 1K INOP. NEEDS MODULE REMOVED FOR ACCESS TO BATTERY. DOOR 1R EMERGENCY EXIT SIGN AND ONE F-C GALLEY FLOOR STRIP INOP. REQ MINIMUM 2 SHIFT SLOT FOR REPAIR. DOOR 1R UPPER EXIT SIGN OPERATES NORMAL. ONE (1) EA FLOOR MOUNTED STRIP ACROSS FROM INOP STRIP OPERATES NORMAL. ALL F-C SEAT MOUNTED LIGHTS OPERATES NORMAL. LOCATION NUMBERS OF INOP LIGHTS ARE L901 AND L972. DOOR 1R LIGHT STRIP AT FWD MOST CORNER IS INOP. ALL SIGNS THAT ILLUMINATE THE WORD EXIT OPERATES NORMAL. NO CROSS AISLE STRIPS INOP. FOUND DOOR 1L EXIT SIGN INOP. REPAIRED BROKEN TERMINAL AND REPLACED LIGHT ASSY, DUE TO DETERIORATION. ALL EMERGENCY LIGHTS OPERATE NORMAL.

Part: FMC — FAILED (COCKPIT) · airframe 75,684 hrs · 12,214 cycles

FMC FAILURE, RTFL. REPLACED NR 1 ADC & ACP TEST. FOUND CAPT PITOT DRAIN OPEN IN E&E & RESET. ACP LOW & HIGH RANGE PITOT STATIC LEAK TESTS & RVSM CHECKS. CHECKS OKAY.

Part: BATTERY — FAULTY (MAIN) · airframe 75,215 hrs · 12,142 cycles

MAIN BATTERY CHARGER STATUS MESSAGE. REPLACED MAIN BATTERY CHARGER, NO HELP. REPLACED MAIN BATTERY, OPS CHECK OKAY.

Part: OIL COOLER — FAULTY (APU) · airframe 75,061 hrs · 12,117 cycles

APU OIL COOLER NEEDS REPLACEMENT. REPLACED APU OIL COOLER.

Part: SLIDE — STUCK (OVERWING SLIDE) · airframe 75,061 hrs · 12,117 cycles

LH OVERWING EXIT SLIDE DOOR WILL NOT OPEN. OPENED SLIDE DOOR WITH GREAT DIFFICULTY. UPON OPENING DOOR, FOUND THE FWD AND AFT DOOR OPENING SQUIB ACTUATORS AND THE LATCH RELEASE SQUIB ACTUATOR FIRED. ALSO FOUND CONTROL ROD BROKEN, AND INTEGRATOR TORQUE TUBE NOT MOVING TO FULL OPEN. ALSO VERIFIED THAT SPOILERS NR & NR 7 SQUIBS NOT FIRED AND SLIDE RAFT NOT UNRAVELED. REPLACED CONTROL ROD. AFTER REPLACING ROD AND ATTEMPTING TO CLOSE ESCAPE SLIDE DOOR, SCREWS ON THE SLIDE PACK BOARD FOUND TO BE CATCHING ON TO THE SLIDE TARGET SWITCH BRACKET. SLIDE TO BE REPLACED. REPLACED SLIDE & REPLACED ALL DOOR LATCH ACTUATORS.

Part: LATCH — NO TEST (OVERWING SLIDE) · airframe 75,061 hrs · 12,117 cycles

LT OVERWING EXIT SLIDE DOOR LATCHES FAILED TORQUE CHECK. REMOVED AND REPLACED ALL FOUR DOOR LATCHES, ADJUSTED AND CHECKED LATCH OPERATIONS, LATCH CHECK GOOD.

Part: CONTROL VALVE — FAULTY (AC PACK) · airframe 75,061 hrs · 12,117 cycles

LEFT PACK CLIMBS CABIN AT 300 FPM WHEN FED FROM RIGHT BLEED. LEFT BLEED FEED OK. REFLY T/S TO FAULTY FLOW CONTROL VALVE. REPLACED FLOW CONTROL VALVE, LEAK AND OPS CHECK GOOD. T/S TO FAULTY FLOW CONTROL VALVE. REPLACED FLOW CONTROL VALVE IAW MM 21-51-01, LEAK AND OPS CHECK GOOD.

Part: FLOORBEAM — CRACKED (BS 246 LBL 17) · airframe 75,061 hrs · 12,117 cycles

FLOOR BEAM AT STA 246, MID-CHORD CRACKED AT LBL 17 INBOARD OF CABLE RUN AGE2B, BEST VIEWED FROM AFT SIDE. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGED CHORD AND FABRICATED A NEW MID CHORD SECTION AND REPAIR ANGLES AND INSTALLED.

Part: STRUCTURE — DAMAGED (BS 246) · airframe 75,061 hrs · 12,117 cycles

STA 246 CABIN FLOORBEAM MID CHORD FASTENER HOLE AT LBL 11 FOUND PREVIOUSLY DAMAGED AND FILLED WITH SEALANT. MAJOR REPAIR ACCOMPLISHED: INSTALLED FREEZE PLUG REPAIR.

Part: PIN — BROKEN (ESCAPE SLIDE) · airframe 75,061 hrs · 12,117 cycles

LT OVERWING SLIDE DOOR HAS BROKEN SLIDE ALIGNMENT PIN, FWD POSITION. REMOVED AND REPLACED ALIGNMENT PIN.

Part: PANEL — WORN (NR 1 PYLON) · airframe 69,461 hrs · 11,272 cycles

NR 1 PYLON INBOARD PANEL 437ERX HAS 3 EACH WORN FASTENER HOLES. REPAIRED PANEL PER REO G12256, REV A. ACCOMPLISHED TAP TEST. TAP TEST GOOD. REPAIR IS NOW CONSIDERED PERMANENT.

Part: HOUSING — DEFECTIVE (EVAC SLIDE) · airframe 75,061 hrs · 12,117 cycles

RIGHT OVERWING SLIDE, INTEGRATOR FAILS OPS CHECK AND DOES NOT RETURN TO VERTICAL POSITION. REPLACED DISCONNECT HOUSING. REPLACED & ADJUSTED NR 4 LATCH. LATCH OPS CHECKS GOOD AT 25" LB.

Part: FLOORBEAM — DAMAGED (FUSELAGE) · airframe 75,061 hrs · 12,117 cycles

MAIN CABIN FLOORBEAM STA 246 WEB CRACKED AT LBL 11.5. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGED SECTION OF WEB. FABRICATED FILLER AND 2 EA DOUBLERS AND INSTALLED.

Part: CABLE — DEFECTIVE (GALLEY) · airframe 73,091 hrs · 11,838 cycles

AFTER T/O AFT GALLEY PIGTAIL SPARKING AND POPPING NOISE. AFT GALLEY LOST PWR2 OF 5 PNL'S. FWD GALLEY ALSO LOST PWR. RT HYD QUANTITY WENT TO ZERO AND RETURNED TO NORM TWICE, STABILIZED AT 0.93. RT FUEL QUANTITY BLANKED AND RETURNED TO NORM. PULLED C/B N52 IN AFT GALLEY AND U34, P11 (R AFT GALLEY). RESET C/B U34, P11 AND PWR RETURNED TO FWD GALLEY, AND AFT GALLEY EXCEPT CART CONTROL N51, N52, N53. PULLED C/B'S N51, N52, N53<>104881 SAMC TEXT: PULLED C/B'S N51, N52, N53 AS PRECAUTION. C/B N52 FOR ASSOCIATED PIGTAIL DID NOT TRIP ON INITIAL SHORT. REPLACED CABLES P51, 52 AND 53, TESTS OKAY.

Part: CABLE — DEFECTIVE (GALLEY) · airframe 73,091 hrs · 11,838 cycles

AFTER T/O AFT GALLEY PIGTAIL SPARKING AND POPPING NOISE. AFT GALLEY LOST PWR 2 OF 5 PNL'S. FWD GALLEY ALSO LOST PWR. R HYD Q WENT TO ZERO AND RETURNED TO NORM TWICE, STABILIZED AT 0.93. RT FUEL Q BLANKED AND RETURNED TO NORM. PULLED CB N52 IN AFT GALLEY AND U34, P11 (R AFT GALLEY). RESET CB U34, P11 AND PWR RETURNED TO FWD GALLEY, AND AFT GALLEY EXCEPT CART CONTROL N51, N52, N53. PULLED CB'S N51, N52, N53<>104881. PULLED CB'S N51, N52, N53 AS PRECAUTION. CB N52 FOR ASSOCIATED PIGTAIL DID NOT TRIP ON INITIAL SHORT. REPLACED CABLES P51, 52 AND 53, TESTS OKAY.

Part: RELAY — FAULTY (FUEL SYSTEM) · airframe 72,457 hrs · 11,747 cycles

UNABLE TO FUEL ACFT, FUELING VALVES (ALL) DO NOT OPEN AUTOMATICALLY. RPL RELAYS K357 FUELING PWR TRANS ON THE P36 AND K181 OVERFILL CONT ON THE P36. ALSO RPL THE ASSY FUEL LEVEL SENSOR CARD. RPL RELAY K180. REPLACED FUEL QTY PROCESSOR. FUELER WAS ABLE TO PRESSURE FUEL ALL 3 TANKS.

Part: EEC — OUT OF ADJUST (NR 1 ENGINE) · airframe 72,100 hrs · 11,686 cycles

NR 1 ENG 'ENG EEC MODE' MESSAGE APPEARED ON EICAS ALONG WITH ALTN LIGHT. NR 1 ENG EEC REPLACED. ENGINE REPLACED DUE TO REPEATED EEC HITS. NO FAULT FOUND WITH ENGINE. PROBLEM PERSISTED ON THE AIRPLANE AFTER THE ENGINE WAS REPLACED.

Part: CONTROL SWITCH — MALFUNCTIONED (LT EEC) · airframe 72,072 hrs · 11,679 cycles

THE 'L ENG EEC MODE' EICAS MSG DISPLAYED. NOW OPERATING IN N1 MODE. REPLACED NR 1 EEC IAW MM 73- 21-04 FOR TS (L ENG EEC MODE) CAUTION MSG DISPLAYED ON UPPER EICAS. REPLACED LEFT DADC, LEFT ENG EEC CONTROL SWITCH, RAN BOTH ENGINES. COULD NOT DUPLICATE PROBLEM OR GET ANY STATUS MESSAGES.

Part: ANTI-ICE VALVE — FAULTY (LT ENGINE) · airframe 72,067 hrs · 11,677 cycles

THE L ENG ANTI-ICE VALVE HAS TO BE CYCLED EVERY TIME THE SWITCH IS TURNED OFF.

Part: ENGINE — STALLED · airframe 71,800 hrs · 11,636 cycles

TWO ENGINES STALLED AT FL380.

Part: ENGINE — STALLED (NR 2) · airframe 71,800 hrs · 11,636 cycles

TWO ENGINES STALLED AT FL380. DFDR INVESTIGATION REVEALED THAT ONLY THE NUMBER 2 ENGINE STALLED. AIRPLANE ENCOUNTERED AN ATMOSPHERIC WAVE AT .80 MACH CAUSING AUDIBLE COMPRESSOR STALLS AND A FLUCTUATION IN THE MACH METER FROM .75 TO .84 RETURNING TO .80. CREW REPORTS ALL ENGINE PARAMETERS NORMAL. ALL AMM CHECKS WERE WITHIN LIMITS.

Part: INLET BULLET — DAMAGED (RT ENGINE) · airframe 71,361 hrs · 11,577 cycles

CRACK AND DELAMINATION FOUND ON INLET CONE (SPINNER) ON RT ENGINE. SPINNER FOUND CRACKED/DELAMINATED. ASSY SENT TO SHOP. REPLACED INLET CONE. NO FAN BLADE DAMAGE FOUND. AFTER VERIFICATION FLIGHT, A/C DETERMINED OK FOR SERVICE.

Part: FMU — MALFUNCTIONED (RT ENGINE) · airframe 71,230 hrs · 11,557 cycles

RIGHT ENGINE START AT 51% N2 AFTER STARTER CUTOUT RIGHT OIL P EICAS CAME ON. ELECTED TO SHUT DOWN. FOUND FAULTY FUEL METERING UNIT. REMOVED AND REPLACED FMU AND RAN. ENG START NORMAL ALL INDICATIONS & OIL PRESSURE NORMAL.

Part: PUMP — FAULTY (FUEL SYSTEM) · airframe 71,191 hrs · 11,545 cycles

BOTH MAIN TANKS FED WHILE THERE WAS 12000LBS IN CENTER TANKS. RIGHT MAIN TANK FED FASTER, IMBALANCE OF 2000LBS. SUSPECT BAD OVERRIDE PUMPS. FOUND PUMP LEAKING DURING OPS CHECK. REMOVED PUMP TO REPLACE O-RINGS. DURING INSTALLATION SHOULDER SCREW BROKE. NEEDS NEW SHOULDER SCREW AND REINSTALL PUMP. CHANGED BOTH RT AND LT OJ PUMPS. OP CHECKS & LEAK CHECK GOOD.

Part: UNKNOWN — UNKNOWN (FUEL SYSTEM) · airframe 71,191 hrs · 11,545 cycles

BOTH MAIN TANKS FED WHILE THERE WAS 12000 LBS IN CENTER TANKS. RIGHT MAIN TANK FED FASTER, IMBALANCE OF 2000 LBS.

Part: CONNECTOR — LOOSE (CARGO DOOR) · airframe 70,801 hrs · 11,493 cycles

FWD CARGO DOOR EICAS ALONG WITH OVERHEAD CARGO DOOR LIGHT. RTFL. FOUND LOOSE CONNECTOR ON FWD CARGO DOOR WIRE HARNESS. SECURED CONNECTOR & DOOR INDICATION OPS NORMAL.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 70,433 hrs · 11,433 cycles

UPON REMOVAL OF GALLEY TIE ROD ATTACH PLATE THE L-ANGLE STRINGER WAS DAMAGED, FASTNER REMOVAL CAUSED END OF ANGLE TO CRACK OFF. REPAIRED IAW SRM 51-20-01 AND SRM 51-40-02.

Part: SWITCH — FAULTY (HYD SYS) · airframe 65,110 hrs · 10,687 cycles

LEFT HYDRAULIC SYSTEM FAILURE. RTFL. FOUND FAULTY SWITCH. REPLACED S30 SWITCH OP CHECKED GOOD. AC OK FOR SERVICE.

Part: CONTROLLER — ILLUMINATED (LT ENGINE) · airframe 70,401 hrs · 11,428 cycles

LEFT ENG BLEED LGT & L ENG HPSOV EICAS MSG DURING DESCENT WITH ENG BLEED SW ON, & ENG RUNNING. FOUND FAULTY HIGH PRESSURE CONTROLLER. REPLACED HIGH PRESSURE CONTROLLER IAW 36-11-19 OP CHECKED GOOD. AC OK FOR SERVICE.

Part: BATTERY — FAULTY (E&E BAY) · airframe 70,258 hrs · 11,403 cycles

THE 'MAIN BAT CHGR' EICAS MSG DISPLAYED. CYCLED STBY POWER THROUGH OFF-BATT, NO HELP. FOUND BATTERY TO BE FAULTY. REPLACED BATTERY PER MM 24-31-01, OPS CHECKED OK. AC OK FOR SERVICE.

Part: CONNECTOR — CHAFED (RT GENERATOR) · airframe 70,034 hrs · 11,371 cycles

RIGHT GENERATOR OFF LINE. RTFL ORD. REPLACED CONNECTOR. WIRES FROM CONNECTOR WERE CHAFED AND SHORTED AGAINST THE BACKSHELL.

Part: LIGHT — BROKEN (GALLEY) · airframe 69,867 hrs · 11,345 cycles

EMERGENCY EXIT PATH LIGHT STRIP BROKEN BY LEFT MID GALLEY.

Part: OXYGEN MASK — LEAKING (1ST OFFICER'S) · airframe 69,597 hrs · 11,299 cycles

F/O OXYGEN MASK LEAKS FROM THE HEADBAND.

Part: LIGHT — INOPERATIVE (RT OVERWING) · airframe 69,557 hrs · 11,291 cycles

EMERGENCY FLOOR LIGHTS BY RIGHT OVERWING INOPERATIVE.

Part: BULB — INOPERATIVE (EXTERIOR) · airframe 69,461 hrs · 11,272 cycles

DOOR 2 LEFT EXTERIOR EMERGENCY EXIT LIGHT INOP. SUSPECT BURNED OUT BULB. REPLACED LAMP OPS CHECKED GOOD. AC OK FOR SERVICE

Part: SKIN — CORRODED (FUSELAGE) · airframe 69,461 hrs · 11,272 cycles

AFT PIT STA 1088 BETWEEN STR 39L AND STR 39R, SKIN IS CORRODED. MAJOR REPAIR ACCOMPLISHED @ GSO: REMOVED DAMAGED AREA FABRICATED REPAIR AND INSTALLED.

Part: LIGHT — DAMAGED (CABIN) · airframe 69,461 hrs · 11,272 cycles

EMERGENCY LIGHT BAR AT AFT GALLEY AREA LEFT SIDE IS DAMAGED. REPLACED EEL STRIP OPS CHECKED GOOD. AC OK FOR SERVICE.

Part: LIGHT — DAMAGED (CABIN) · airframe 69,461 hrs · 11,272 cycles

EMERGENCY LIGHT BARS AT FWD RIGHT LAV, MID LEFT LAV, AND BOTH AFT LAVS ARE DAMAGED. REPAIRED AND REPLACED LIGHT BARS OPS CHECKED GOOD. ACFT OK FOR SERVICE.

Part: LIGHT — DAMAGED (CABIN) · airframe 69,461 hrs · 11,272 cycles

EMERGENCY LIGHT BAR AT MID RIGHT LAV IS DAMAGED. REPAIRED LIGHT STRIP OPS CHECK GOOD. ACFT OK FOR SERVICE.

Part: LIGHT — DAMAGED (CABIN) · airframe 69,461 hrs · 11,272 cycles

EMERGENCY LIGHT BARS AT FWD AND MID CROSSAISLE ARE DAMAGED. REPAIRED AND REPLACED LIGHT BARS OPS CHECKED GOOD. AC OK FOR SERVICE.

Part: WIRE — MISINSTALLED (NR 2 IDG) · airframe 69,461 hrs · 11,272 cycles

NR 2 ENGINE IDG WIRE LUGS ARE IMPROPERLY CRIMPED, MULTIPLE WIRE STRANDS BROKEN AT CRIMP POINT. REMOVED AND REPLACED IDG FEEDERS FROM PRODUCTION SPLICE AND REPLACED TERMINALS. OPS CHECK PERFORMED & INSPECTED.

Part: TERMINAL BLOCK — DAMAGED (NR 1 IDG) · airframe 69,461 hrs · 11,272 cycles

NR 1 ENG IDG FEEDERS SHOW SIGNS OF HEAT DAMAGE AT TERMINALS. FOUND DAMAGED TERMINALS AT IDG TERMINAL BLOCK. REPLACED TERMINALS. AC OK FOR SERVICE.

Part: FEEDER CABLE — BROKEN (CABIN) · airframe 69,461 hrs · 11,272 cycles

EEL FEEDER AT STA 1000L IS BROKEN. REPLACED EEL FEEDER OPS CK GOOD. AC OK FOR SERVICE.

Part: BRACKET — DEBONDED (EXIT LIGHT) · airframe 69,461 hrs · 11,272 cycles

AFT OVERWING EMERGENCY LIGHT BRACKET DISBONDED.

Part: CONNECTOR — DAMAGED (LEFT HYD SUPPLY) · airframe 69,461 hrs · 11,272 cycles

LEFT HYDRAULIC SUPPLY SHUTOFF VALVE DOES NOT CYCLE (MOVE) WHEN ENGINE FIRE HANDLE IS PULLED. FOUND CONNECTOR D44045 DAMAGED SUSPECT IMPROPERLY INSTALLED. REPLACED CONNECTOR OPS CHECKED GOOD IAW MM 29-11-06. AC OK FOR SERVICE.

Part: FIRE LOOP — NO TEST (CARGO BAY) · airframe 69,461 hrs · 11,272 cycles

FOUND CARGO FIRE TEST FAILED CARGO FWD HEAT INHIBIT.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHTS) · airframe 69,461 hrs · 11,272 cycles

DOOR 2 LEFT EXTERIOR EMERGENCY EXIT LIGHT INOP. RESECURED CONNECTOR.

Part: FRAME — CRACKED (BS 456) · airframe 69,461 hrs · 11,272 cycles

FWD PIT FRAME WEB CRACKED AT BS 456 LBL 28. MAJOR REPAIR ACCOMPLISHED: FABRICATED & INSTALLED NEW WEB.

Part: SKIN — CORRODED (BS 965) · airframe 69,461 hrs · 11,272 cycles

FOUND CORROSION ON CENTER WING UPPER SURFACE AT BS 965, BL0. MAJOR REPAIR ACCOMPLISHED: REMOVED CORROSION. FABRICATED & INSTALLED REPAIR SHIMS. ACCMP HFEC OF HOLES, NO DEFECT NOTED OVER SIZED HOLES.

Part: STRUCTURE — CHAFED (NR 2 PYLON) · airframe 69,461 hrs · 11,272 cycles

NR 2 PYLON RIGHT SIDE IS CHAFED IN 5 SPOTS AT NAC 195. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGED AREA, FABRICATED & INSTALLED DOUBLER REPAIR.

Part: CONNECTOR — DAMAGED (NR 2 NACELLE) · airframe 69,461 hrs · 11,272 cycles

NR 2 PYLON J BOX CONNECTOR D4236J IS DAMAGED BY HEAT. REPLACED CONNECTOR D4236J REF BSWPM 20-63-13. OPS CHECK ACCOMP.

Part: FRAME — CORRODED (BS 1197) · airframe 69,461 hrs · 11,272 cycles

AFT CARGO PIT AT BS 1197 +22 LBL 38 TO LBL 44 FRAME T-CAP HAS CORROSION UNDER SIDE OF CAP. FOUND TO BE OUT OF LIMITS. REMOVED ENTIRE "T" CORD. INSTALLED NEW "T" CORD REF SRM 51-40-02.

Part: FRAME — GOUGED (BS 1351 S24-25R) · airframe 69,461 hrs · 11,272 cycles

AFT PIT FRAME WEB GOUGED, STA 1351, STR 24R - 25R.

Part: FLOORBEAM — CRACKED (BS 266) · airframe 69,461 hrs · 11,272 cycles

MAIN CABIN AT STA 266.5 FLOORBEAM AT RBL 70.5 IS CRACKED ON UPPER FLANGE. REMOVED DAMAGE SECTION OF "T" CAP, INSTALLED "T" CORD AND 2 EA REPAIR ANGLE PER SRM 53-00-5 1, RPR 6. DAMAGE REMOVED STA 266.5, RBL 71 TO 49.

Part: CONNECTOR — DAMAGED (NR 2 NACELLE) · airframe 69,461 hrs · 11,272 cycles

NR 2 PYLON J BOX CONNECTOR D4256J IS DAMAGED BY HEAT. REPLACED CONNECTOR D4256J PER BSWPM 20-63-13. OPS CHECK ACCOMP.

Part: FRAME — CORRODED (BS 1197) · airframe 69,461 hrs · 11,272 cycles

AFT CARGO PIT AT BS 1197 +44 LBL 22 TO RBL 9 FRAME T-CAP HAS CORROSION UNDER NUT PLATE ATTACH FASTENER HOLES.

Part: CONNECTOR — DAMAGED (NR 2 NACELLE) · airframe 69,461 hrs · 11,272 cycles

NR 2 PYLON J BOX CONNECTOR D4240J IS DAMAGED BY HEAT. REPLACED CONNECTOR D4266J PER BSWPM 20-63-13. OPS CHECK ACCOMP.

Part: CONNECTOR — DAMAGED (NR 2 NACELLE) · airframe 69,461 hrs · 11,272 cycles

NR 2 PYLON J BOX CONNECTOR D4148J IS DAMAGED BY HEAT. REPLACED CONNECTOR D4148J PER BSWPM 20-63-13. OPS CHECK ACCOMP.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 69,461 hrs · 11,272 cycles

MAIN CABIN FLOORBEAM STA 287, RBL 70.5 UPPER FLANGE IS CORRODED.

Part: STIFFENER — CRACKED (NLG WW) · airframe 69,461 hrs · 11,272 cycles

LEFT VERTICAL STIFFENER CHORD, NLG WW, STA 287 HAS 3" CRACK, INDICATION LOCATED 10.75" FROM THE NOSE WW TOP PANEL.

Part: INSERT — OUT OF POSITION (EVAC SLIDE) · airframe 69,461 hrs · 11,272 cycles

RIGHT OVERWING SLIDE INFLATION HOSE CLAMP INSERT PULLED OUT.

Part: HOUSING — CRACKED (EVAC SLIDE) · airframe 69,461 hrs · 11,272 cycles

RIGHT OVERWING SLIDE DISCONNECT HOUSING IS CRACKED.

Part: ASPIRATOR — LEAKING (EVAC SLIDE)

ASPIRATOR LEAKS. CAUSE UNKNOWN. REPLACED ASPIRATOR AND BARREL ASSEMBLY. AC OK FOR SERVICE.

Part: GENERATOR — TRIPPED (RT ENGINE) · airframe 69,250 hrs · 11,238 cycles

RTFL DUE TO RIGHT GENERATOR TRIPPING AT 5,000 FT, FIELD OFF LIGHT ILLUMINATED. R GEN OFF EICAS DISPLAYED.

Part: UNKNOWN — ODOR (CABIN) · airframe 69,250 hrs · 11,238 cycles

POSSIBLE ELECTRICAL ODOR FROM VENT IN AFT GALLEY LEFT SIDE. SAME ODOR REPORTED NEAR ROWS 5-6. REPLACED GEN CONTROL UNIT AS PER AMM 24 -22-02, ALSO INSP IDG WIRE BUNDLES, NO ABNORMALITIES OBSERVED& GALLEY FANS WORKING FINE. FOLLOWED SERVICE TIP 21-00-00 FOR ODORS/ SMOKE IN THE CABIN & NO PROBS FOUND, ALSO APU BLEED AIR NOT IN USE WHEN FLT ATTENDANTS SMELLED ODOR . COFFEEMAKERS WERE REMOVED FOR A COMPLETE CLEAN UP OF THE AFT GALLEY INCLUDING WARMING OVENS. SMC3 PROCEDURE FOLLOWED. THIS CONFIRMS NORMAL OPERATION OF THE A/C'S SYSTEMS.

Part: ALTERNATOR — MALFUNCTIONED (ENGINE) · airframe 69,229 hrs · 11,235 cycles

L ENG CONTROL EICAS ON DESCENT, CAME ON RIGHT AFTER TURNING OFF ENG ANTI ICE. REPLACED THE PERMANENT MAGNET ALTERNATOR FOR THE NR 1 ENGINE EEC.

Part: IDG — INOPERATIVE (RT GENERATOR) · airframe 69,150 hrs · 11,224 cycles

RT GENERATOR INOP. REPLACED RIGHT IDG. ACCOMPLISHED IDG PERFORMANCE CHECK . ALL NORMAL.. ACP BPCU BITE CHECK. ALL OK. VERIFICATION FLIGHT CONFIRMED NORMAL OPERATION. ACFT OK FOR SERVICE

Part: CONNECTOR — LOOSE (EMERGENCY LIGHTS) · airframe 65,261 hrs · 10,822 cycles

LEFT EEL INOP IN FIRST CLASS AT LAV. SECURED CONNECTOR.

Part: LIGHT — DAMAGED (CABIN) · airframe 69,092 hrs · 11,216 cycles

EEL LIGHT TORN UP FIRST CLASS RIGHT SIDE. REPAIR EEL LIGHT ASSY, OPS CHECKED OK.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 69,088 hrs · 11,215 cycles

EEL LIGHT ADJACENT TO DOOR 1R INOP. REPAIRED EEL STRIP. OPS CHECKS GOOD.

Part: ACTUATOR — FAULTY (RUDDER TRIM) · airframe 68,382 hrs · 11,108 cycles

AIRCRAFT REQUIRES 4 UNITS LEFT RUDDER TRIM DURING CRUISE. L & R FUEL TANKS BALANCED. SUSPECT RUDDER TRIM ACTUATOR. REPLACED RUDDER TRIM ACTUATOR. ALL SYSTEMS CHECK NORMAL. PERFORM SINGLE HYDRAULIC SYSTEM CHECK OF EACH RUDDER POWER CONTROL ACTUATOR USING EACH HYDRAULIC SYSTEM IN SEQUENCE. TESTED FIVE MORE TIMES BEFORE HMV NO DISCREPANCIES.

Part: PUMP — LEAKING (HYD SYSTEM) · airframe 68,349 hrs · 11,104 cycles

CTR ADP HAS HYDRAULIC LEAK. REPLACED AIR DRIVEN PUMP PER MM29-11-03. DURING OPS CHECK OF ADP FOUND PRESSURE REGULATOR VALVE FAILED. OPS CHECK NORMAL. ACFT OK FOR SERVICE.

Part: WARNING LIGHT — ILLUMINATED (APU GENERATOR) · airframe 67,983 hrs · 11,044 cycles

APU GENERATOR "OFF" LIGHT ILLUMINATES AFTER RIGHT ENGINE STARTS.

Part: VALVE — FAULTY (CABIN TEMP) · airframe 67,983 hrs · 11,044 cycles

FWD CABIN TEMP CONTROL FAILED TO CONTROL DESIRED TEMP. CREW COMMENTS: FWD AND MID CABINS EXTREMELY COLD. AFTER EXTENSIVE TROUBLE SHOOTING FOUND FAULTY FWD TRIM AIR VALVE AND LOW LIMIT CONTROL VALVE. REPLACED BOTH VALVES OP CHECKED GOOD. AC OK FOR SERVICE.

Part: DRIVE UNIT — FAILED (WEATHER RADAR) · airframe 67,854 hrs · 11,021 cycles

RECEIVED "WXR FAIL ANT" ON EHSI. *S/D* REPLACED WEATHER RADAR ANTENNA DRIVE UNIT AS PER MM 34-43-05-401, TEST PASSED.

Part: WIRE — DAMAGED (EMERGENCY LIGHTS) · airframe 67,664 hrs · 10,988 cycles

FWD GALLEY EEL LIGHT INOPERATIVE. 10-11-07 REPLACED LIGHT AND REPAIRED WIRING. EEL OP CHECKED OK FOR SERVICE.

Part: WARNING LIGHT — ILLUMINATED (LT GENERATOR) · airframe 66,974 hrs · 10,867 cycles

LEFT GEN DRIVE LIGHT ILLUMINATED WITH ASSOCIATED EICAS L GEN DRIVE DISC MSG. [08-07-07] REPLACED LT IDG AS PER MM 24-11-01, FINAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: ENGINE — OIL CONSUMPTION (NR 1) · airframe 65,712 hrs · 10,643 cycles

NR 1 ENG HIGH OIL CONSUMPTION EXCEEDS LIMIT. [SUP 05-08-07] PRECAUTIONARY REPORT. NO OIL LEAKS DISCOVERED. SUSPECT OVER SERVICING.

Part: SCANNER — FAILED (WX RADAR SYS) · airframe 65,431 hrs · 10,594 cycles

FLIGHT DIVERTED DUE TO WEATHER RADAR FAILURE. REPLACED SCANNER ASSY PER MM34-43-05. PERFORMED OPERATIONAL TEST OF WEATHER RADAR. TEST SUCCESSFUL PER MM 34-43-00

Part: WIRE — DAMAGED (FUEL QTY) · airframe 63,382 hrs · 10,255 cycles

RIGHT WING T/E, WS 410, RIGHT MAIN FUEL QUANTITY WIRE BUNDLE FOR CONNECTOR, AFT SHELL CORRODED. FURTHER INSPECTION FOUND THE CORROSION WAS LIMITED TO THE CN1156 -4 CONNECTOR, HOWEVER, WHILE REMOVING THE CONNECTOR BACK SHELL, THE BACKSHELL BROKE APART INTO SEVERAL PIECES DUE CORRS DAMAGE. REMOVED DAMAGED CONNECTOR AND REPAIRED USING CINCH KIT CN1156-KB1 IAW CINCH SB CN1156-28- 02 AND UA-EVA-60584. INSTALLED CONNECTOR PER BAC CHAPTER 20. OPS CHECK GOOD PER MM

Part: LATCH — WORN (ESCAPE SLIDE) · airframe 63,382 hrs · 10,255 cycles

LT OVERWING SLIDE INTEGRATOR TORQUE CHECK FAILED. SLIDE DOOR LATCHES SHOW DEEP WEAR GROOVES ON LATCH SLIDERS PREVENTING PROPER LATCH MOVEMENT. REPLACED 4 LEFT OVERWING SLIDE DOOR LATCHES.

Part: FLOORBEAM — CRACKED (BS 246) · airframe 63,382 hrs · 10,255 cycles

FOUND STA 246 FLOORBEAM ATTACH ANGLE AT RBL 11 IS CRACKED. REPLACED SUPPORT ANGLE 141T5146-5 PER SRM 51-40-2.

Part: SWITCH — FAULTY (ESCAPE SLIDE) · airframe 63,382 hrs · 10,255 cycles

RT WING SLIDE DOOR SENSOR S219 IS OUT OF LIMITS. REPLACED THE S219 PROXIMITY SENSOR.

Part: DISPLAY — UNKNOWN (COCKPIT) · airframe 61,646 hrs · 9,985 cycles

DIVERTED TO LHR DUE TO LEFT CENTRAL DISPLAY UNIT PROBLEM. LEFT CDU FAILED. REPLACED LEFT CDU. OPS CHECK NORMAL.

Part: BLOCK — OUT OF POSITION (CABIN)

LT OVERWING STOP BLOCK IS RUBBING AGAINST RELEASE TRIGGER. REPLACE LOCATOR PIN IAW 767 SRM 51-40-02.

Part: SPACER — BURNED (APU GEN) · airframe 59,748 hrs · 9,685 cycles

BURNED SPACER BLOCKS BETWEEN APU GENERATOR 3 CABLES. FAILING SPLICE INSTALLATIONS REVEALED A MISMATCH BETWEEN THE SPLICE AND CRIMPER USED. MANUFACTURERS' SPLICES AND CRIMPER DIES MUST BE USED AS A MATCHED SET; IF NOT, AN INCOMPLETE SWAGE WILL RESULT IN HEAT GENERATION FROM GAPS BETWEEN CABLE AND SPLICE SURFACES. UA DEVELOPING A CHANGE ORDER TO REPLACE OLD AL SPLICES WITH NEWER "COPALUM" VERSION, P/N AMP277161-1 IN THE APU GEN POWER FEEDER CABLES.

Part: COMPUTER — FAILED (FLT MANAGE) · airframe 55,198 hrs · 8,974 cycles

RIGHT FMC CDU FAILED. RIGHT CDU WAS REPLACED. SHOP COULD NOT DUPLICATE CDU BLANKING DURING HOT, COLD AND VIBRATION OPERATION ON BENCH. AS A PRECAUTION, SHOP REPLACED COMPONENTS A6A2Q7, A6A2Q8, A6A2U16, A2A2U45, A2A2U48 IN CDU. THE CDU (MR40219-185) WAS REMOVED AND RETURNED TO THE SHOP. SHOP FOUND THE DISPLAY WAS DIM BUT NOT BLANK AND REPLACED THE CRT AND YOKE ASSEMBLY.

Part: SLIDE — UNSERVICEABLE (L1 DOOR) · airframe 52,409 hrs · 8,527 cycles

DOOR 1 LEFT SLIDE RAFT PRESSURE AT 2500 PSI. REPLACED 1L DOOR ESCAPE SLIDE.

Part: SKIN — DENTED (FUSELAGE) · airframe 50,075 hrs · 8,162 cycles

SKIN DENTED AT STATION 1241 STRINGER 39L. MAJOR REPAIR ACCOMPLISHED. FABRICATED & INSTALLED REPAIR DOUBLER.

Part: CONTROLLER — MALFUNCTIONED (RT PACK TEMP) · airframe 48,615 hrs · 7,910 cycles

RIGHT PAC TEMP EICAS MESSAGE ILLUMINATED. THE PACK TEMP CONTROLLER WAS REPLACED AND THE AIRCRAFT RETURNED TO SERVICE. SHOP FOUND NO FAULTS WITH THE CONTROLLER.

Part: WINDSHIELD — CRACKED (COCKPIT)

ELECTRICAL ARC OCCURRED AT THE BOTTOM OF THE LEFT FORWARD WINDOW DURING CRUISE. CREW TURNED OFF WINDOW HEAT. SUBSEQUENTLY WINDOW SHATTERED REMAINING IN ONE PIECE. REPLACED NUMBER 1 LEFT WINDSHIELD ASSEMBLY AS OUTLINED IN MM 56-11-01. ADDITIONALLY DUE TO WINDOW FAILURE AND SUBSEQUENT REPLACEMENT, REPLACED LEFT FORWARD WINDOW HEAT CONTROLLER M191 AS OUTLINED IN MM 30-41-01.

Part: FRAME — DENTED (FUSELAGE) · airframe 43,646 hrs · 7,045 cycles

FORWARD PIT FRAME LOWER CHORD AT BODY STATION 500 LEFT HAND IS DENTED BETWEEN STRINGER 29L AND 30L. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND REPLACED FRAME CHORD.

Part: SKIN — CHAFED (FUSELAGE) · airframe 43,646 hrs · 7,045 cycles

FUSELAGE SKIN AT RIGHT HAND AFT HORIZ SEAL IS CHAFED. MAJOR REPAIR ACCOMPLISHED. SKIN REPAIRED WITH DOUBLER.

Part: SKIN — CHAFED (FUSELAGE) · airframe 43,646 hrs · 7,045 cycles

BODY STATION 1809 LEFT HAND FUSELAGE SKIN CHAFED UNDER LOWER BANANA FAIRING. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED DOUBLER.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 43,646 hrs · 7,045 cycles

BODY STATION 852-870 LBL 55 FLOORBEAM T-CAP IS CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED FLOORBEAM T-CAP.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 43,646 hrs · 7,045 cycles

BODY STATION 1284 RBL 17 INTERCOSTAL CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED INTERCOSTAL.

Part: SPAR — CRACKED (NR 1 PLYON) · airframe 43,646 hrs · 7,045 cycles

NR 1 ENGINE PYLON UPPER SPAR WEB CRACKED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED REPAIR DOUBLER.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 43,646 hrs · 7,045 cycles

BODY STATION 790 RBL 12-14 FLOORBEAM CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED FLOORBEAM SPLICE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 43,646 hrs · 7,045 cycles

BODY STATION 1197+88 LBL 40-41 FLOORBEAM UPPER CHORD CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED UPPER CHORD T-CAP.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 43,646 hrs · 7,045 cycles

BODY STATION 850-855 RBL 33 FLOORBEAM T-CAP CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED FLOORBEAM T-CAP.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 43,646 hrs · 7,045 cycles

BODY STATION 790 LBL 12-14 FLOOR SUPPORT CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED REPAIR PARTS.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 43,646 hrs · 7,045 cycles

BODY STATION 1562 LBL 58 FLOORBEAM CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED REPAIR PARTS AND BEAM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,646 hrs · 7,045 cycles

LEFT NOSE TUNNEL AT BODY STATION 246, LBL 35, UPPER CHORD CRACKED AFT SIDE. MAJOR REPAIR ACCOMPLISHED. FABRICATED REPAIR PARTS.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 43,646 hrs · 7,045 cycles

FLOORBEAM T-CAP CORRODED UNDER NUT PLATE BODY STATION 153, LBL 10. MAJOR REPAIR ACCOMPLISHED. REPAIRED T-CAP WITH FABRICATED NEW SECTION AND SPLICE.

Part: INDICATOR — FAILED (COCKPIT) · airframe 41,019 hrs · 6,594 cycles

RTO AT 85 KTS. COPILOT MACH AIRSPEED INDICATOR (MASI) SHOWED ZERO KTS AND A-S WARNING FLAGD 80 KTS DURING TAKEOFF. TAKEOFF ABORTED WITH RTO ENGAGED FOR 3-5 SECONDS. REPLACED THE COPILOT MASI.

Part: WARNING SYSTEM — ACTIVATED (LT ENGINE) · airframe 2,782,003 hrs · 6,128 cycles

RTF GSO WITH LEFT ENGINE FUEL FILTER INDICATION. NORMAL LANDING. NO EMERGENCY DECLARED.

Part: WARNING LIGHT — ILLUMINATED (SLAT ASYMMETRY) · airframe 2,852,002 hrs

ON APPROACH, CREW GOT A LEADING EDGE SLAT ASYMMETRY INDICATOR LIGHT. DID GO-AROUND. AMBER ALERT. LANDED WITHOUT INCIDENT.

Part: TRANSCEIVER — FAILED (RADAR) · airframe 34,967 hrs · 5,499 cycles

AIRCRAFT RETURNED TO EZE DUE TO RADAR PROBLEMS. *S/D* THE WEATHER RADAR RECEIVER/TRANSMITTER AND ANTENNA DRIVE UNIT WERE REPLACED AND THE SYSTEM OPERATION RETURNED TO NORMAL. SHOP CHECKOUT OF THE REMOVED UNITS FOUND THAT THERE WERE NO FAULTS WITH THE RECEIVER TRANSMITTER BUT THE ANTENNA DRIVE UNIT (P/N 622-5125-001), WAS FOUND TO HAVE THE AZIMUTH FAILED AND LOCKED AND THEREFORE WAS THE CAUSE OF THE RADAR SYSTEM FAILURE ON AIRCRAFT 6651.

Part: ROTOR — CRACKED (NR 2 REAR BRAKE)

NR 2 REAR BRAKE CARBON ROTOR IS CRACKED AND DAMAGED. FOUND DURING MISSING TIE-BOLT INSPECTION. *S/D* THE CARBON ROTOR WAS FOUND DAMAGED. THE ROTOR ASSEMBLY WAS REPLACED, OPERATIONS CHECK NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN)

EMERGENCY FLOOR LIGHTING AT ROWS 15AB-28AB FLASHES INTERMITTENTLY. REPLACED BATTERY PACK (ROW 26 AB) AND GROUND CHECKED NORMAL.

Part: FAN BLADES — DAMAGED (NR 1 ENGINE)

BIRD STRIKE NR 1 ENGINE, ACCOMPANIED BY VIBRATION. AIRCRAFT RETURNED TO FIELD. EXTENSIVE FAN BLADE DAMAGE OCCURRED FROM BIRD STRIKE. THE COMPLETE SET OF FAN BLADES WERE REPLACED.