N762CX

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 92,380 hrs · 41,718 cycles

CORROSION ON SHEAR TIE IN FLC STATION 632 BETWEEN STRINGER 33L AND 34L

Part: PRESSURE DECK — CORRODED · corrosion level 2 · airframe 92,380 hrs · 41,718 cycles

PRESSURE DECK AT FS 1263-1285 TO HAVE 2 SPOTS OF CORROSION.

Part: CHANNEL — CRACKED (ZONE 400) · airframe 92,380 hrs · 41,718 cycles

#1 PYLON AFT STRUT V FRAME FOUND INBOARD AFT J CHANNEL CRACKED.

Part: BEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 92,380 hrs · 41,718 cycles

47487REA29 CORROSION AT STRINGER 38L STATION 720

Part: STUB FRAME — CRACKED (ZONE 200) · airframe 92,380 hrs · 41,718 cycles

LOWER FRAME INNER CHORD CRACKED

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 92,380 hrs · 41,718 cycles

CORROSION ON STRINGER L37

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 92,380 hrs · 41,718 cycles

STRINGER 38L CORRODED

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 92,380 hrs · 41,718 cycles

STRINGER 36L CORRODED

Part: ANGLE — CHAFED (ZONE 100) · airframe 92,381 hrs · 41,718 cycles

CHAFED ANGLE

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 92,380 hrs · 41,718 cycles

SHEAR TIE CORRODED STA. 566

Part: STRINGER — CRACKED (ZONE 100) · airframe 92,380 hrs · 41,718 cycles

STRINGER 12L CRACKED

Part: STRINGER SPLICE — CORRODED (ZONE 100) · corrosion level 2 · airframe 92,380 hrs · 41,718 cycles

S35L SPLICE CORRODED

Part: CHANNEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 92,380 hrs · 41,718 cycles

CHANNEL FOUND TO BE CORRODED

Part: RIB — CRACKED (ZONE 400) · airframe 92,380 hrs · 41,718 cycles

CORE COWL FAIRING RIB CRACKED.

Part: RIB — CRACKED (ZONE 400) · airframe 92,380 hrs · 41,718 cycles

#1 PYLON RIB CRACKED

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 92,380 hrs · 41,718 cycles

SHEAR TIE CORRODED

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 92,380 hrs · 41,718 cycles

CORROSION ON SHEAR TIE.

Part: INTERCOSTAL — BENT (ZONE 100) · airframe 92,380 hrs · 41,718 cycles

INTERCOSTAL BENT

Part: BEAM — CHAFED (ZONE 600) · airframe 92,380 hrs · 41,718 cycles

OB FLAP IB SUPPORT 1 2 3 BEAM CHAFED AT IB AND OB ARMS ABOVE MID FAIRING SUPPORT AMES NR136876- 0600-0067

Part: STUB FRAME — CRACKED (ZONE 200) · airframe 92,380 hrs · 41,718 cycles

FRAME INNER CHORD CRACKED AND LOWER END.

Part: STRINGER — CORRODED (ZONE 100) · airframe 92,380 hrs · 41,718 cycles

CORROSION ON STRINGER 35L

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 92,380 hrs · 41,718 cycles

STRINGER 39R CORRODED STA. 1272-1276

Part: FRAME — CRACKED (ZONE 400) · airframe 92,380 hrs · 41,718 cycles

RUBSTRIP V-FRAME CRACKED

Part: SUPPORT STRAP — CRACKED (ZONE 100) · airframe 92,380 hrs · 41,718 cycles

GILINER SUPPORT FOR VERTICAL SIDEWALL TO CEILING, RH , STA 1263~1241, BENT AND CRACKED.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · airframe 92,380 hrs · 41,718 cycles

FLOOR SUPPORT PAN IS CORRODED

Part: STRINGER — CORRODED (ZONE 100) · airframe 92,380 hrs · 41,718 cycles

CORROSION FOUND CENTER OF STRINGER STA. 764 36R

Part: INTERCOSTAL — CORRODED (ZONE 100) · airframe 92,380 hrs · 41,718 cycles

INTERCOSTAL FOUND TO BE CORRODED

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 92,380 hrs · 41,718 cycles

CORROSION ON STRINGER 32R JUST AFT OF FRAME STATION 412 REPLACED STRINGER 32R CORRODED SECTION IAW 47487REA27 SEE PARTIAL WORK CORRODED LEVEL 2 PT NUMBER 143T3001-56 STRINGER EXACT FS/BS LOCATION FS 401 TO 434 STRINGER 32R

Part: STRINGER CLIP — CRACKED (ZONE 100) · airframe 92,380 hrs · 41,718 cycles

CRACK FOUND AT STATION 566, REMOVED AND REPLACED CRACKED STRINGER CLIP IAW B767 SRM 51-40-02 SECTION 7

Part: STRINGER CLIP — CRACKED (ZONE 100) · airframe 92,380 hrs · 41,718 cycles

REMOVED AND REPLACED CRACKED STRINGER CLIP IAW B767 SRM 51-40-02 SECTION 7. STA 566

Part: STRINGER CLIP — CRACKED (ZONE 100) · airframe 92,380 hrs · 41,718 cycles

STRINGER CLIP CRACKED AT STATION 566

Part: SUPPORT WEB — CORRODED (ZONE 100) · corrosion level 2 · airframe 92,380 hrs · 41,718 cycles

PRESSURE DECK IMMEDIATELY INSIDE OF ALC DOOR STA 1263~1285 IS CORRODED.

Part: PYLON — GOUGED (ZONE 400) · airframe 92,380 hrs · 41,718 cycles

DAMAGE TO THE INBOARD SIDE OF OUTBOARD LOAD FITTING #2 PYLON.

Part: BEAR STRAP — CORRODED (ZONE 100) · corrosion level 2 · airframe 92,380 hrs · 41,718 cycles

CORROSION NOTED ON ALC DOOR SURROUND, LWR LIP, UNDER SEAL DEPRESSOR INSIDE, STA 1273~1282.

Part: VERTICAL SUPPORT — ERODED (ZONE 400) · airframe 92,380 hrs · 41,718 cycles

NO. 2 PYLON INBOARD VERTICAL FLANGE EROSION NAS 410 TO NAS 411

Part: SHEAR TIE — CORRODED (ZONE 100)

CORRODED SHEAR TIE STA.1263

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 92,380 hrs · 41,718 cycles

FORWARD LOWER CARGO CORROSION FUS.. STA. 566 SHEAR TIE BETWEEN STR. 38L AND 39L

Part: SHEAR TIE — CORRODED (ZONE 100) · airframe 92,380 hrs · 41,718 cycles

SHEAR TIE CORRODED AT STA. 1241 IN AFT LOWER CARGO

Part: INTERCOSTAL — BENT (ZONE 200) · airframe 92,380 hrs · 41,718 cycles

INTERCOSTAL IN MCD AT RBL82 IS BENT

Part: RIB — NONE (ZONE 500) · airframe 92,380 hrs · 41,718 cycles

LW L/E AIR LOAD RIB FORMER AT LES 441 IS BENT AND HOLES ARE ELONGATED

Part: STRINGER — DAMAGED (ZONE 200) · airframe 92,380 hrs · 41,718 cycles

NR 0200-0090 R/H FRAME STA 859 THE FRAME INNER CHORD IS CRACKED ON LOWER END COMMON TO THE STUB BEAM. (VERIFIED WITH HFEC SURFACE SCAN.)

Part: SKIN — CRACKED (ZONE 300) · airframe 92,380 hrs · 41,718 cycles

FUSELAGE SSTA 1654 HAS CRACK IN THE SKIN BETWEEN STR 4L-5L

Part: STRINGER SPLICE — CORRODED (ZONE 100) · corrosion level 2 · airframe 92,380 hrs · 41,718 cycles

STR 33L CORRODED AT STA 742

Part: CHANNEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 92,380 hrs · 41,718 cycles

CORROSION FOUND ON Z CHANNEL AT STATION 522-544/24LBL-40LBL

Part: STRINGER CLIP — CRACKED (ZONE 100) · airframe 92,380 hrs · 41,718 cycles

STRINGER H-CLIP ON STR 36L AT STA 632 IS CRACKED

Part: STRINGER SPLICE — CORRODED (ZONE 100) · corrosion level 2 · airframe 92,380 hrs · 41,718 cycles

FACTORY STRINGER SPLICE AT STA 1285, S39L IS CORRODED

Part: CHANNEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 92,380 hrs · 41,718 cycles

SUPPORT CHANNEL AT RBL65, TOP OF P39 BOX, RUNNING FWDTO AFT IS CORRODED IN FASTENER HOLE FOR STANCHION CONNECTION

Part: BALL MAT — CRACKED (ZONE 100) · airframe 92,380 hrs · 41,718 cycles

ALC CENTER BALL MATT CRACKED ON LOWER SURFACE AT BALL FITTING

Part: ANGLE — CORRODED (ZONE 100) · corrosion level 2 · airframe 92,380 hrs · 41,718 cycles

FORWARD LOWER CARGO BILGE PANEL STATION 522-544 RIGHT HAND HAS CORROSION AT 3 LOCATIONS

Part: WEB — CRACKED (ZONE 400) · airframe 92,380 hrs · 41,718 cycles

#1 PYLON LOWER PAN WEB CRACKED IN RADIUS AND BENT INWARD ON O/B AND I/B SIDE AT NAS. 410.50 WHERE BOTTOM OF 313T1380 SKIN PANEL AND V-FRAME ATTACH

Part: INTERCOSTAL — CORRODED (ZONE 100) · corrosion level 2 · airframe 92,380 hrs · 41,718 cycles

WHILE WORKING SOURCE CARD, INTERCOSTAL FROM STA1263 TO 1285 RBL 13 FOUND TO BE CORRODED. AMES NR 136876-0100-0371

Part: NONE — CRACKED (ZONE 200) · airframe 92,380 hrs · 41,718 cycles

CABIN FLOOR SUPPORT BRACKET IS CRACKED, ON THE AFT SIDE OF FLOOR BEAM AT STA.1562, AT RBL78

Part: NONE — CORRODED (ZONE 100) · corrosion level 2 · airframe 92,380 hrs · 41,718 cycles

CABIN FLOOR PANEL SUPPORT IS CORRODED, FROM STA.1480 RBL85, TO STA.1560 RBL78

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 92,380 hrs · 41,718 cycles

SHEAR TIE CORRODED AT B STA 500, BL 0 IN THE FWD CARGO

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 92,380 hrs · 41,718 cycles

FLC CORROSION F/S 610 SHEAR TIE BETWEEN STR 33L & 34L

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 92,380 hrs · 41,718 cycles

FLC CORROSION F/S 544 SHEAR TIE BETWEEN STR 39L & 39R

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 92,380 hrs · 41,718 cycles

FLC CORROSION F/S 434 SHEAR TIE BETWEEN STR 37L & 38L

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 92,380 hrs · 41,718 cycles

SHEAR TIE IS CORRODED AT B STA 588, S-36L

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 92,380 hrs · 41,718 cycles

SHEAR TIE IS CORRODED AT B STA 588 BETWEEN, S-36R AND S-37R

Part: SUPPORT STRAP — CRACKED (ZONE 100) · airframe 92,380 hrs · 41,718 cycles

FLC F/S 522 RBL 48 LWR SLANT PANEL SUPPORT STRAP CRACKED

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 92,380 hrs · 41,718 cycles

SHEAR TIE IS CORRODED AT B STA 610, BETWEEN S-39L AND S-39R

Part: BRACKET — CORRODED (ZONE 100) · corrosion level 2 · airframe 92,380 hrs · 41,718 cycles

VERTICAL STANCHION BASE IS CORRODED AT STA 1087 LBL 26. AMES NR 136876-0100-0258

Part: SUPPORT PLATE — CORRODED (ZONE 100) · corrosion level 2 · airframe 92,380 hrs · 41,718 cycles

THERE IS CORROSION UNDER THE NUTPLATES, ON THE LOWER SURFACE OF THE ALC PANEL SUPPORT, AT STA.1411, LBL24 TO LBL44.

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 92,380 hrs · 41,718 cycles

CORROSION ON SHEAR TIE IN FLC BILGE AREA @ STA 742 AFT SIDE OF FLOOR SUPPORT BETWEEN STR 30L - 31L

Part: STANCHION — CORRODED (ZONE 100) · corrosion level 2 · airframe 92,380 hrs · 41,718 cycles

STANCHION ON O/B L/H SIDE STA 287 AND FORWARD OF P-36 LOWER END HAS HEAVY CORROSION

Part: SPLICE — CORRODED (ZONE 100) · corrosion level 2 · airframe 92,380 hrs · 41,718 cycles

CORROSION ALC STA 1255 STR 30R END FITTING. AMES NR 136876-0100-0167

Part: RETAINER — CORRODED (ZONE 600) · corrosion level 2 · airframe 92,380 hrs · 41,718 cycles

CORROSION ON UPPER TE SEAL RETAINER AT STA790 OB OF #12 SPOILER PCA

Part: SUPPORT — CHAFED (ZONE 600) · airframe 92,380 hrs · 41,718 cycles

NR 0600-0066 OB FLAP OB SUPPORT 6-8-9 BEAM IS CHAFFED ON OB SIDE OF OB ARM MARKED REMOVED CHAFFED DAMAGE ON O/B FLAP O/B SUPPORT 6-8-9 BEAM ON O/B SIDE OF O/B ARM TO COMPLY WITH REA 47487REA34 REV IR

Part: SUPPORT — CRACKED (ZONE 100) · airframe 92,380 hrs · 41,718 cycles

ALC STA 1260 RH SIDE WALL LWR CORNER GUSSET CRACKED. AMES NR 136876-0100-0169

Part: LINK — CHAFED (ZONE 500) · airframe 92,380 hrs · 41,718 cycles

OB FLAP OB FLAP SUPPORT 6-8-9 BEAM IS CHAFFED ON OB UPPER AFT ARM

Part: BRACKET — CRACKED (ZONE 100) · airframe 92,380 hrs · 41,718 cycles

FORWARD INBOARD ATTACH ANGLE FOR P33 PANEL IN MEC IS CRACKED AMES NR 136876-0100-0007

Part: GENERATOR — INOPERATIVE (NR 2)

ATN7451 ENROUTE KCVG TO KPHX, CREW REPORTS RIGHT ENGINE GENERATOR INOPERATIVE, APU FAILED ALL 3 START ATTEMPTS IN FLIGHT. ATI OPERATIONS QUICK READY HANDBOOK REQUIRES UNSCHEDULED LANDING AT NEAREST SUITABLE AIRPORT. DIVERSION TO KABQ WITH EMERGENCY DECLARATION. LANDING UNEVENTFUL. NO ADDITIONAL PRECAUTIONARY ACTIONS NOTED. AIRCRAFT GROUNDED FOR UNSCHEDULED MAINTENANCE.

Part: BEAR STRAP — CORRODED (BS 1346-1351) · airframe 87,688 hrs · 39,923 cycles

AIRBORNE/PEMCO NON-ROUTINE 2601N484 DISCREPANCY: C/R EVAL REPAIR-CORROSION ON BEAR STRAP BETWEEN STA1346-STA1351M STR34R - STR35R PER ATTACHED REA NO. B653-5510MR CORRECTIVE ACTION: REPAIR TO BE ACCOMPLISHED ON NR 2601N495 PER EO 19421 REV 1R AIRBORNE/PEMCO NON-ROUTINE 2601N495 DISCREPANCY: C/R: ACCOMPLISH E.O. #19421 CORRECTIVE ACTION: COMPLIED WITH EO# 19421

Part: STRINGER — CORRODED (BS 1300) · airframe 87,688 hrs · 39,923 cycles

DISCREPANCY: WHILE CLOSING AREA, CORROSION NOTED S37R STA 1300 IB OF AFT CARGO DOOR ENTRY CORRECTIVE ACTION: REMOVED AND REPLACE STRINGER SECTION S37R @ STA 1300 I/B OF AFT CARGO DOOR ENTRY. IAW B767 SRM 51-40-02

Part: STRAP — CRACKED (BS 1725 BULKHEAD) · airframe 87,688 hrs · 39,923 cycles

AIRBORNE/PEMCO NON-ROUTINE 2601N414 DISCREPANCY: STA 1725.50 INTERNAL UPPER BULKHEAD OUTER CHORD STRAP, HAS CRACK INDICATION AT FASTENER ABOVE STR 7R CORRECTIVE ACTION: PERFORMED REPAIR IAW B767-200 SRM 53-80-01 REPAIR 5 CRACK AT UPPER BULKHEAD OUTER CORD STRAP AT STRINGER 7R.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 86,682 hrs · 39,537 cycles

POST LANDING, L1 ENTRY DOOR EMERGENCY LIGHT INOPERATIVE. FAULT ISOLATED TO PIN 15 ON EMERGENCY POWER SUPPLY NO POWER. REMOVED AND REPLACED EMERGENCY BATTERY POWER SUPPLY IAW B767 AMM 33-51-07. SYSTEMS OPERATIONAL CHECK SATISFACTORY IAW B767 AMM 33-51-00. FAULT NOT DUPLICATED. ACFT RELEASED TO SERVICE.

Part: GENERATOR — INOPERATIVE (RIGHT) · airframe 83,997 hrs · 38,705 cycles

AT CRUISING ALTITUDE "R GEN DRIVE EICAS MSG DISPLAYED." IAW GEN DRIVE CHECKLIST COMPLIED WITH DISCONNECTING THE DRIVE AND STARTING APU. UPON STARTING THE APU, APU GEN OFF EICAS MSG DISPLAYED. RESET OF APU GEN NOT SUCCESSFUL. QRG DIRECTED LANDING AT NEAREST SUITABLE AIRPORT. DIVERSION TO KDFW WITH AN EMERGENCY DECLARATION. AIRCRAFT GROUNDED. APU START WITH RIGHT GENERATOR SUCCESSFUL. NO FAULTS NOTED ON BPCU. NO PREVIOUS FAULTS RECORDED. SHUTDOWN APU AND RESTARTED AGAIN. NO FAULTS NOTED. RH GEN DEFERRED IAW ATI MEL 24-00-01-01. CAT C NO FLY DATE 01/15/2018. MX PROCEDURES COMPLIED WITH. REMOVED AND REPLACED RH IDG. NO LEAKS NOTED. OPC SATISFACTORY. DMI CLEAR. ACFT RELEASED TO SERVICE.

Part: STRINGER — CRACKED (BS 676) · airframe 83,209 hrs · 38,399 cycles

STRINGER 13L CRACKED AT BS 676. REMOVED AND REPLACED THE STRINGER SECTION IAW SRM 53-00-03, REPAIR 1, AND SERVICE BULLETIN 368-53-041, REVISION 2.

Part: BEAM — CRACKED (NR 1 PYLON) · airframe 83,209 hrs · 38,399 cycles

NR 1 PYLON INBOUND HYD BAY DOOR LOWER BEAM CRACKED. REMOVED AND REPLACED THE BEAM IAW DRAWING 313T1380, SRM 51-40-02 AND SRM 51-40-05.

Part: BEAM — CORRODED (RWS 290) · corrosion level 2 · airframe 83,201 hrs · 38,389 cycles

RIGHT WING REAR SPAR TO TRAILING EDGE UPPER PANEL ATTACH BEAM UPPER STRUCTURE CORRODED AROUND NUTPLATES AT WS 290. BLENDED CORROSION. FOUND TO BE OUT OF LIMITS IAW SRM 57-51-02. REMOVED AND REPLACED BEAM UPPER STRUCTURE IAW DRAWING 113T1623, AND SRM 51-40-02.

Part: STRINGER — CRACKED (BS 676) · airframe 83,209 hrs · 38,399 cycles

STRINGER 10L CRACKED AT BS 676. REPAIRED IAW IAW SRM 53-00-03, AND SERVICE BULLETIN 368-53-041, REVISION 2.

Part: ATTACH ANGLE — CORRODED (WING) · corrosion level 2 · airframe 83,201 hrs · 38,389 cycles

PANEL 52CB AFT LOWER PANEL ATTACH ANGLE ON WING, CORRODED AT INBOARD END OF OPENING. REMOVED AND REPLACED LOWER ATTACH ANGLE IAW SRM 51-40-02.

Part: BEAM — CRACKED (NR 2 PYLON) · airframe 83,201 hrs · 38,389 cycles

THE NR 2 PYLON INBOUND HYD BAY DOOR LOWER BEAM CRACKED ON FORWARD END. REMOVED AND REPLACED INBOUND LOWER HYD BAY DOOR BEAM IAW SRM 51-40-05, AND 51-40-02.

Part: SUPPORT — DAMAGED (RT WING TE FLAP) · airframe 83,209 hrs · 38,399 cycles

RIGHT WING TRAILING EDGE FLAP SUPPORT HAS A DAMAGED FASTENER HOLES. SPOT FACED.

Part: BEAM — CRACKED (NR 2 NACELLE) · airframe 83,201 hrs · 38,389 cycles

NR 2 PYLON OUTBOUND HYD BAY DOOR LOWER BEAM IS CRACKED AT THE FORWARD END AND FORWARD BRACKET IS MISSING FASTENERS. REMOVED AND REPLACED LOWER BEAM IAW SRM 51-40-02.

Part: SKIN — CRACKED (BS 287) · airframe 83,201 hrs · 38,389 cycles

FUSELAGE EXTERNAL SKIN CRACKED AT THE R1 DOOR CUTOUT BS 287, STRINGER 11R. REPAIRED THE SKIN IAW SRM 53-10-01, FIG 201, DETAIL III, AND ENGINEERING DOCUMENT 47288REA01.

Part: SKIN — CRACKED (BS 1654) · airframe 83,209 hrs · 38,399 cycles

FOUND A 2 INCH CRACK ON THE EXTERIOR SKIN LEFT SIDE OF SEC 48, BS 1654, STRINGER 13L. REPAIRED IAW SRM 53-80-01.

Part: WEB — CORRODED (LT WING LE) · corrosion level 2 · airframe 83,201 hrs · 38,389 cycles

LEFT WING LEADING EDGE STRINGER 885 WEB CORRODED ON FIXED LEADING EDGE. FABRICATED A NEW WEB IAW SRM 57-41-13, ITEM 2. INSTALLED THE WEB AND RIB IAW IAW SRM 51-40-02.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 80,794 hrs · 37,532 cycles

THE FOLLOWING WORK WAS ACCOMPLISHED DURING VISIT BY MX & ENGINEERING SERVICES. FUSELAGE SKIN, PN 146T3531-3, CORRODED AT STATION 1414, STRINGER 35R INBD OF AFT DRAIN MAST AT SKIN LAP. THE FUSELAGE SKIN WAS REPAIRED IAW SRM 53-00-01 REPAIR 12 FIGURE 201 & 46971REA27 REVISION A DATED 4 16 16 WITH MINOR DEVIATION TO EXTEND DOUBLER FOR UPPER SKIN TO ONE ROW ABOVE STRINGER 35R & TO ONE ROW AFT OF FRAME AT STATION 1417. IAW SRM, THIS IS A ZONE A CATEGORY B REPAIR WITH RE-INSPECT REQUIRED EVERY 3,000 CYCLES. STRINGER 36R, PN 146T3003-12, WAS FOUND TO BE CORRODED AT STATION 1405 DURING FUSELAGE SKIN REPAIR. REPAIRED STRINGER WITH STRINGER SPLICE IAW SRM 53-00-03 REPAIR 2.

Part: HOSE — BLOWN (HYD SYSTEM) · airframe 80,760 hrs · 37,519 cycles

EICAS MESSAGE "C HYD QTY", LOSS OF ALL QTY LEADING TO C HYD FAILURE. FOUND HOSE BLOWN.

Part: FAULTY · airframe 80,486 hrs · 37,340 cycles

EMERGENCY LIGHT UNARMED. R & R DRAWER ASSEMBLY & BULBS. OPERATIONAL CHECKED SATISFACTORY IAW AMM 33-13-01.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 79,416 hrs · 36,963 cycles

EMERGENCY LIGHT ASSEMBLY AT L1 DOOR IS INOPERABLE. RELAMPED EMER LIGHT JUST OUTSIDE L1 DOOR AREA. OPERATIONAL CHECKED SATISFACTORY IAW AMM 33-51-06. ACFT RELEASED TO SERVICE.

Part: FAILSAFE — CRACKED (FUSELAGE) · airframe 79,359 hrs · 36,945 cycles

LEFT FAILSAFE IS CRACKED .250 AT STATION 955, LBL 90. REPAIRED LT FAILSAFE STRAP IAW ENGINEERING DOCUMENTS 46725ORD01,47008ORD01,47008ORD03 & 47008ORD13.

Part: SUPPORT FITTING — CRACKED (TE FLAP) · airframe 79,359 hrs · 36,945 cycles

NUMBER 8 FLAP SUPPORT FITTING NUMBERED FROM INBD TO OTBD 1 - 4. NR 1 FLAP SUPPORT BOLT SHOWS CRACK INDICATION. REAMED HOLE NR 1 IN THE NR 8 FLAP SUPPORT FITTING COMMON TO THE REAR SPAR TO A FINAL HOLE DIAMETER OF .7495" IAW REA 47158REA03 & SRM 51-40-05.

Part: LONGERON — CORRODED (BS 970) · corrosion level 2 · airframe 79,358 hrs · 36,944 cycles

LONGERON AT BS 970 IN THE LEFT MLG WW CORRODED. BLENDED, HFEC INSPECTED & ROTO PEENED IAW ED 47158REA11 & SRM 51-10-00.

Part: SUPPORT FITTING — CRACKED (TE FLAP) · airframe 79,359 hrs · 36,945 cycles

NUMBER 8 FLAP SUPPORT FITTING HOLES NUMBERED FROM INBD TO OTBD 1 - 4. NUMBER 4 HOLE HAS A CRACK INDICATION. REAMED HOLE NR 4 IN THE NR 8 FLAP SUPPORT FITTING COMMON TO THE REAR SPAR TO A FINAL HOLE DIAMETER OF .8745" & 8755" IAW REA 47158REA03 & SRM 51-40-05.

Part: STRAP — CRACKED (FUSELAGE) · airframe 79,359 hrs · 36,945 cycles

RIGHT FAILSAFE STRAP IS CRACKED .250 AT STATION 955, RBL 90. REPAIRED RT FAILSAFE STRAP IAW ENGINEERING DOCUMENTS 42765ORD01, 47008ORD02,47008ORD04 & 47008ORD14.

Part: SUPPORT FITTING — CRACKED (TE FLAP) · airframe 79,359 hrs · 36,945 cycles

DURING INSPECTION, NR 2HOLE IS PITTED & SHOWS CRACK INDICATION. NR 2 FLAP SUPPORT FITTING NUMBERED FROM LT TO RT. REAMED HOLE NR 2 IN THE NR 2 FLAP SUPPORT FITTING COMMON TO THE REAR SPAR TO A FINAL HOLE DIAMETER OF .8745" & .8755" IAW REA 47158REA03 & SRM 51-40-05.

Part: SUPPORT FITTING — CORRODED (TE FLAP) · corrosion level 2 · airframe 79,359 hrs · 36,945 cycles

DURING HFEC INSPECTION, NR 4 HOLE IS PITTED & SHOWS CRACK INDICATION. NR 2 FLAP SUPPORT FITTING NUMBERED FROM LT TO RT. REAMED HOLE NR 4 IN THE NR 2 FLAP SUPPORT FITTING COMMON TO THE REAR SPAR TO A FINAL HOLE DIAMETER OF .8745" & .8755" IAW REA 47158REA03 & SRM 51-40-05.

Part: SUPPORT FITTING — CRACKED (TE FLAP) · airframe 79,359 hrs · 36,945 cycles

NUMBER 1 FLAP FITTING, NR 3 HOLE SHOWS CRACK INDICATION DURING HFEC INSPECTION. NR 1 FLAP SUPPORT FITTING, NUMBERING IS FROM LT TO RT. REAMED HOLE NR 3 IN THE NR 1 FLAP SUPPORT FITTING COMMON TO THE REAR SPAR TO A FINAL HOLE DIAMETER OF .07495" & .07505" IAW REA 47158REA03 & SRM 51-40-05.

Part: SUPPORT FITTING — CRACKED (TE FLAP) · airframe 79,359 hrs · 36,945 cycles

DURING INSPECTION, NR 2 FLAP SUPPORT FITTING, NR 1 HOLE IS PITTED & SHOWS CRACK INDICATION. NR 2 FLAP SUPPORT FITTING NUMBERED FROM LT TO RT. REAMED HOLE NR 1 IN THE NR 2 FLAP SUPPORT FITTING COMMON TO THE REAR SPAR TO A FINAL HOLE DIAMETER OF .8750" IAW REA 47158REA03 & SRM 51-40-05.

Part: SUPPORT FITTING — CRACKED (TE FLAP) · airframe 79,359 hrs · 36,945 cycles

NUMBER 8 FLAP SUPPORT FITTING HOLES NUMBERED FROM INBD TO OTBD 1 - 4. NR 2 HOLE HAS A CRACK INDICATION. REAMED HOLE NR 2 IN THE NR 8 FLAP SUPPORT FITTING COMMON TO THE REAR SPAR TO A FINAL HOLE DIAMETER OF .7495" IAW REA 47158REA03 & SRM 51-40-05.

Part: SUPPORT FITTING — CRACKED (TE FLAP) · airframe 79,359 hrs · 36,945 cycles

NUMBER 8 FLAP SUPPORT FITTING HOLES NUMBERED FROM INBD TO OTBD 1 - 4. NR 3 HOLE HAS A CRACK INDICATION. REAMED HOLE NR 3 IN THE NR 8 FLAP SUPPORT FITTING COMMON TO THE REAR SPAR TO A FINAL HOLE DIAMETER OF .8745" & 8755" IAW REA 47158REA03 & SRM 51-40-05.

Part: SKIN — CRACKED (FUSELAGE) · airframe 79,359 hrs · 36,945 cycles

AFT FUSELAGE EXTERNAL SKIN HAS CRACKED PAINT, POSSIBLE SKIN CRACK, AT STATION 1654, STRINGER 13R. REPAIRED IAW SRM 53-80-01 REPAIR 7. VERTICAL CRACK & MARKED CRACK LOCATION IAW NDT MANUAL PART 6 PROCEDURE 51-00-19.

Part: PRESSURE DECK — CRACKED (FUSELAGE) · airframe 79,359 hrs · 36,945 cycles

PRESSURE DECK WEB FROM STATION 917 TO 972, LBL 97.42 TO 74.78 HAS A CRACK ON THE OTBD AFT CORNER. SERVICEABLE PRESS DECK FABRICATED & INSTALLED IAW DWG 145T8752 & ENGINEERING DOCUMENT 47008ORD03.

Part: SUPPORT — CORRODED (TE FLAP) · corrosion level 2 · airframe 79,359 hrs · 36,945 cycles

NUMBER 1 FLAP SUPPORT 1, 2 & 3 BEAM HAS A HOLE WITH A DEFECT INDICATION WITH ROTARY SCAN, HOLE HAS CORROSION IN IT. HOLE REPAIRED IAW ENGINEERING DOCUMENT REA47158REA09.

Part: BUSHING — CORRODED (LT WING) · corrosion level 2 · airframe 79,359 hrs · 36,945 cycles

NUMBER 1 SUPPORT 1, 2 & 3 BEAM HAS 3 BUSHINGS WITH DAMAGE AT THE NR 3 JOINT. REPLACED 3 BUSHINGS IAW ENGINEERING DOCUMENT 47158REA09.

Part: SUPPORT BEAM — DAMAGED (WING) · airframe 79,359 hrs · 36,945 cycles

NUMBER 7 SUPPORT 1, 2 & 3 BEAM HAS A HOLE WITH A DEFECT INDICATION WITH ROTARY SCAN, POSSIBLE SCORING. REAMED HOLE CLEAN & ROUND TO .470" IAW SRM 51-10-02 & ENGINEERING DOCUMENT 47158REA07. PERFORMED HFEC IAW NDT MANUAL 51-00-16 PART 6 WITH NO DEFECTS NOTED.

Part: LINK — WORN (TE FLAP) · airframe 79,359 hrs · 36,945 cycles

NUMBER 5 FLAP SUPPORT OTBD REACTION LINK HAS GROOVE WORN IN SEAL CAVITY & BEARING IS SCORED. R & R ROLLER BEARING IN REPAIRED REACTION LINK IAW CMM 27-51-84 & ENGINEERING DOCUMENT 47158REA05.

Part: SUPPORT FITTING — CRACKED (TE FLAP) · airframe 79,359 hrs · 36,945 cycles

NUMBER 7 FLAP SUPPORT FITTING HOLES. NUMBERED FROM INBD TO OTBD 1 - 4 NR 4 HOLE CRACK INDICATION. REAMED HOLE NR 4 IN THE NR 7 FLAP SUPPORT FITTING COMMON TO THE REAR SPAR TO A FINAL HOLE DIAMETER OF .8745" & .8755" IAW ENGINEERING DOCUMENT REA47158REA03 & SRM 51-40-05.

Part: SUPPORT FITTING — CRACKED (TE FLAP) · airframe 79,359 hrs · 36,945 cycles

NUMBER 7 FLAP SUPPORT FITTING HOLES. NUMBERED FROM INBD TO OTBD 1 - 4. NR 3 HOLE CRACK INDICATION. REAMED HOLE NR 3 IN THE NR 7 FLAP SUPPORT FITTING COMMON TO THE REAR SPAR TO A FINAL HOLE DIAMETER OF .8745" & .8755" IAW ENGINEERING DOCUMENT REA47158REA03 & SRM 51-40-05.

Part: SEAL — DAMAGED (TE FALP) · airframe 79,359 hrs · 36,945 cycles

NUMBER 5 FLAP SUPPORT OUTBOUND, REACTION LINK LOWER BEARING GREASE SEAL DAMAGED. R & R ROLLER BEARINGS IN REPAIRED REACTION LINK IAW CMM 27-51-84 & ENGINEERING DOCUMENT 47158REA05.

Part: SUPPORT FITTING — DAMAGED (TE FLAP) · airframe 79,359 hrs · 36,945 cycles

NUMBER 8 OTBD ROTARY ACT SUPPORT FITTING HAS 1 EACH DEFECTIVE HOLE AT APPROX THE 3:00 O CLOCK POSITION. HOLE REAMED TO .453", FREEZE PLUG INSTALLED IAW ENGINEERING DOCUMENT 47158REA04.

Part: SUPPORT FITTING — CORRODED (TE FLAP) · corrosion level 2 · airframe 79,359 hrs · 36,945 cycles

NUMBER 7 OTBD ROTARY ACT SUPPORT FITTING HAS 1 EACH DEFECTIVE HOLE APPROX AT THE 12:00 POSITION. HOLE REAMED TO .393", FREEZE PLUG INSTALLED IAW ENGINEERING DOCUMENT 47158REA04.

Part: SCUFF PLATE — CRACKED (FUSELAGE) · airframe 78,899 hrs · 36,660 cycles

4.5 INCHES CRACK IN THE AFT LOWER HALF BULK CARGO DOOR SILL SCUFF PLATE. INTERIM REPAIR 0.187 DIAMETER HOLE STOP DRILL. THREE LAYERS OF SPEED TAPE TAPERED EVERY TWO INCHES FWD & AFT OF THE CRACK ENDS. ACCESS AREA RESTORED & ACFT RESTORED TO SERVICE. PERMANENT REPAIR TO BE ACCOMPLISHED ON OR BEFORE THE NEXT TEN FLIGHT CYCLES.

Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 78,328 hrs · 36,383 cycles

DURING A2H CHECK FOUND R1 & L1 DOOR EMERGENCY LIGHTS INOPERATIVE. R & R EMERGENCY LIGHT POWER SUPPLY M735 & M786 IAW 767 WDM 33-51-11. OPERATIONS CHECKED NORMAL, ACFT WAS GNDED.

Part: ANGLE — CORRODED (ZONE 500) · corrosion level 2 · airframe 78,193 hrs · 36,336 cycles

LEFT WING T/E LOWER MOUNTING ANGLE FWD OF PANEL 552JB APPROXIMATE WS 390 IS CORRODED. R & R LT WING T/E LOWER PANEL MOUNTING ANGLE IAW SRM 51-40-02, ACFT WAS GROUNDED.

Part: ANGLE — CORRODED (BS 546-549) · airframe 78,193 hrs · 36,336 cycles

DURING HEAVY MX VISIT, MX AND ENGINEERING DISCOVERED MINOR CORROSION ON THE OUTER ANGLE OF THE LOWER DOOR JAMB FORWARD CORNER OF THE FORWARD LOWER CARGO DOOR. CORROSION REMOVED, BLENDED AREA WAS HFEC INSPECTED. SPOTFACED ALL OPEN FASTENER LOCATIONS IN BLENDED AREA AS REQUIRED TO OBTAIN A FLAT SURFACE PERPENDICULAR TO THE HOLE. FLAP ROTO-PEENED BLENDED AREA IAW SRM 51-20-06. REFINISH SURFACE AS REQUIRED IAW SRM 51-20-01.

Part: FLOORBEAM — CORRODED (BS 1395) · airframe 78,193 hrs · 36,336 cycles

DURING HEAVY MX VISIT, MX AND ENGINEERING DISCOVERED THAT THE UPPER CAP OF THE FLOORBEAM HAS CORROSION AT BS 1395, LBL 42. R & R FLOORBEAM CAP IAW DWG 146T1215 AND SRM 51-40-02.

Part: SUPPORT BRACKET — CRACKED (LT WING) · airframe 78,193 hrs · 36,336 cycles

DURING HEAVY MX VISIT, MX AND ENGINEERING DISCOVERED THE SUPPORT BRACKET FOR THE LT WING UPPER BONDED PANEL IS CRACKED AT WING STA 798.2. R & R THE SUPPORT BRACKET IAW SRM 51-40-02.

Part: RIB — CRACKED (VERTICAL STAB) · airframe 78,193 hrs · 36,336 cycles

VERTICAL STABILIZER ACCESS 324CLX, LOWER BOX INTERNAL LT FWD LOWER RIB CRACKED. R & R FWD LOWER RIB IAW SRM 51-40-02.

Part: FAILSAFE — CORRODED (BS 1348) · airframe 78,193 hrs · 36,336 cycles

DURING HEAVY MX VISIT, MX AND ENGINEERING REPORTED AN AREA OF CORROSION ON THE FAILSAFE STRAP, BS 1348 FRAME S21-22R. CORROSION REMOVED. HFEC OPEN-HOLE INSPECTION AND SURFACE SCAN INSPECTIONS WERE ACCOMPLISHED AND CRACK INDICATIONS WERE DISCOVERED IN THREE EXISTING FASTENER LOCATIONS. DISCREPANT HOLES WERE REWORKED FROM 0.250" IN .0156" INCREMENTS TO 0.277". HFEC OPEN-HOLE INSPECTION VERIFIED CRACK FREE CONDITIONS AT ALL EXISTING FASTENER LOCATIONS. MX CONFIRMS ALL CORROSION HAS BEEN REMOVED.

Part: STRINGER SPLICE — CRACKED (BS 1530-1562) · airframe 78,193 hrs · 36,336 cycles

STRINGER SPLICE IN AFT LOWER COMPARTMENT AT FS1535 S39L CRACKED. R & R STRINGER 39L IAW SRM 51-40-02 AND 53-00, FIG 201, SHEET 4.

Part: SUPPORT BRACKET — CRACKED (LT WING) · airframe 78,193 hrs · 36,336 cycles

LT WING FWD SPAR RIB SUPPORT BRACKET AT WBL 103 CRACKED. R & R BRACKET IAW DWG 114T1305 AND SRM 51-40-02.

Part: STRINGER — CORRODED (BS 1225) · airframe 78,193 hrs · 36,336 cycles

AFT LOWER COMPARTMENT STRINGER 36R AT BS 1225, CORRODED. R & R STRINGER 36R IAW SRM 53-00-03, REPAIR 2.

Part: ANGLE — CRACKED (NLG WW) · airframe 78,193 hrs · 36,336 cycles

DURING HEAVY MX VISIT, MX AND ENGINEERING DISCOVERED VERTICAL ANGLE AT BS 287, LBL 25 IN NOSE WHEEL WELL CRACKED. REPAIRED VERTICLE ANGLE IAW SRM 53-10-14, FIG NR 2 AND SRM 51-70-12, FIG NR 1.

Part: SKIN — CORRODED (LT WING) · airframe 78,193 hrs · 36,336 cycles

DURING HEAVY MX VISIT, MX AND ENGINEERING DISCOVERED AN ISOLATED AREA OF CORROSION ON LT WING UPPER SKIN PANEL CORROSION WAS REMOVED BY BLENDING. HFEC INSPECTED IAW NDT MANUAL, PART 6, 51-00-19. NO ADDITIONAL DEFECTS NOTED. REWORKED AREA WAS ROTO-PEENED AND REFINISHED IAW SRM 51-20-01. WORK ACCOMPLISHED IAW 47067REA07.

Part: FLOORBEAM — CORRODED (BS 1175) · airframe 78,193 hrs · 36,336 cycles

CORROSION WAS FOUND AROUND THE NUT PLATE ON THE HORIZONTAL FLANGE OF THE FLOOR FRAME AT BS 1175, BL0 TO BL45. R & R THE UPPER CHORD IAW SRM 51-40-02.

Part: NUT PLATE — MISSING (BS 1153) · airframe 78,193 hrs · 36,336 cycles

AFT LOWER COMPARTMENT FLOOR NUTPLATE MISSING AT STATION 1153. REPLACED NUT PLATE IAW SRM 51-40-02.

Part: SKIN — CORRODED (RT WING) · airframe 78,193 hrs · 36,336 cycles

DURING HEAVY MX, MX AND ENGINEERING REPORTED AN AREA OF CORROSION LOCATED ON THE UPPER RT WING SKIN BETWEEN WS 1066 AND 1070. THE CORROSION WAS REMOVED AND EXCEEDED LIMITS IAW SRM 57-20-01. AN HFEC INSPECTION WAS ACCOMPLISHED IAW NDT PART 6, 51-00-19 AND 51-00-16 WITH NO DEFECTS NOTED. FABRICATED FILLER, DOUBLER AND REPAIR STRAP IAW 47067, REA 12. ALODINE AND PRIME ALL REPAIR COMPONENTS IAW SRM 51-20-01. INSTALLED REPAIR PARTS IAW SRM 51-40-04.

Part: ANGLE — CORRODED · airframe 78,193 hrs · 36,336 cycles

DURING HEAVY MX VISIT, MX AND ENGINEERING DISCOVERED CORROSION AROUND A FASTENER HOLE, BENEATH THE NUTPLATE ON THE FWD LOWER CARGO DOOR ON THE UPPER ANGLE OF THE THIRD HORIZONTAL BEAM FROM THE TOP OF THE DOOR JUST AFT OF THE ACTUATOR BRACKET. THE NUTPLATE WAS REMOVED AND THE CORROSION WAS BLENDED OUT. ACCOMPLISHED HFEC INSPECTION TO ENSURE NO ADDITIONAL DEFECTS EXIST. APPLY ALODINE AND TWO COATS OF PRIMER TO THE BLENDED AREA AND INSTALLED THE NUTPLATE. ALL WORK ACCOMPLISHED IAW EO 52-767-4955 APPROVED ON FAA FORM 8110-3, DATED 23, AUG 13.

Part: ANGLE — CORRODED (DOOR FRAME) · airframe 78,193 hrs · 36,336 cycles

DURING HEAVY MX VISIT, MX AND ENGINEERING DISCOVERED MINOR CORROSION ON THE OUTER ANGLE OF THE LOWER DOOR FRAME AFT CORNER OF THE FWD LOWER CARGO DOOR. CORROSION WAS REMOVED. AREA HFEC INSPECTED, NO ADDITIONAL DEFECTS WERE NOTED.

Part: FLOOR SUPPORT — CORRODED (BS 742) · airframe 78,193 hrs · 36,336 cycles

FORWARD LOWER COMPARTMENT FLOOR SUPPORT FWD OF AIR MIXER AT BS 742 CORRODED. R & R FLOOR SUPPORT IAW SRM 51-40-02.

Part: SUPPORT — CRACKED (NR 2 PYLON) · airframe 78,193 hrs · 36,336 cycles

NR 2 PYLON PANEL ACCESS PANEL 442FR, MID SUPPORT UPPER INBD RIB SUPPORT CRACKED. R & R RIB SUPPORT IAW SRM 51-40-02.

Part: RIB — CORRODED (RT WING) · airframe 78,193 hrs · 36,336 cycles

RIGHT WING L/E RIB ABOVE THE ANTI-ICE TUBE HAS CORROSION AT LES 456. R & R RIB ABOVE RT WING ANTI-ICE TUBE IAW SRM 51-40-02.

Part: SPAR — CORRODED (LT WING TE FLAP) · airframe 78,193 hrs · 36,336 cycles

DURING HEAVY MX VISIT, MX AND ENGINEERING REPORTED AN AREA OF CORROSION LOCATED ON THE UPPER INNER SURFACE OF THE LT WING OTBD FLAP REAR SPAR AT STA OTEF 84.725. CORROSION WAS REMOVED. BLEND OUT EXCEEDS LIMITS IAW SRM 57-53-02, FIG 101, DETAIL IX. A HFEC OPEN-HOLE INSPECTION AND SURFACE SCAN INSPECTIONS WERE ACCOMPLISHED AND VERIFIED CRACK FREE CONDITIONS AT THE REWORKED LOCATION IAW NDT PART 6, 51-00-19 AND 51-00-16. MX CONFIRMS ALL CORROSION HAS BEEN REMOVED AND NO OTHER DAMAGE.

Part: SKIN — WORN (VERTICAL STAB) · airframe 78,193 hrs · 36,336 cycles

VERTICAL STABILIZER ACCESS 324AL, FUSELAGE MOUNTED TRIANGLE PANEL UPPER MATING SURFACE WORN. R & R FORWARD FAIRING SKIN PANEL IAW SRM 51-40-02.

Part: NUT PLATE — MISSING (ROLLER TRACK) · airframe 78,193 hrs · 36,336 cycles

AFT LOWER COMPARTMENT NUT PLATE LT SIDE ROLLER TRACK MISSING AT BS 1197. REPLACED NUT PLATE, CORROSION WAS FOUND ON UPPER ANGLE. R & R UPPER ANGLE AND REPLACED NUT PLATE IAW SRM 51-40-02.

Part: BEAM — CRACKED (NR 1 PYLON) · airframe 78,193 hrs · 36,336 cycles

INBD BEAM INSIDE OF THE NR 1 PYLON HYD BAY DOOR IS CRACKED AT FWD END. R & R BEAM IAW SRM 51-40-02.

Part: COOLING FAN — SHORTED (FWD) · airframe 77,688 hrs · 36,089 cycles

FAULT CODE 21-90-48-44, CREW NOTICED A BURNING ODOR AFTER ENGINE START AND FWD EQUIPMENT COOLING SUPPLY FAN CIRCUIT BREAKER TRIPPED ALONG WITH ASSOCIATED EICAS MESSAGE FOR FORWARD COMPARTMENT OVERHEAT. R & R FORWARD SUPPLY COOLING FAN IAW AMM 21-58-06, OPS CHECKS GOOD. NO DEFECTS NOTED AT THIS TIME.

Part: O-RING — FAILED (HYD SYSTEM) · airframe 77,180 hrs · 35,893 cycles

DURING CRUISE, CENTER HYD QUANTITY DECREASED TO ZERO AND SYS PRESSURE AND (RSVR,QTY) LIGHTS ON. EICAS MESSAGE: CENTER HYD SYS PRESSURE AND CENTER HYD QUANTITY DISPLAYED. INFLIGHT EMERGENCY WAS DECLARED PRIOR TO LANDING. UPON INSPECTION FOUND RT WING NR 2 SPOILER POWER CONTROL ACTUATOR FILTER CAP LEAKING. R & R O-RING ON FILTER CAP IAW AMM 27-61-02. SYS OPS CHECKS NORMAL. NO LEAKS NOTED. SERVICED HYD SYS IAW AMM 12-12-01.

Part: PROXIMITY SENSOR — OUT OF ADJUST (THRUST REVERSER) · airframe 76,926 hrs · 35,793 cycles

DURING TAKEOFF ROLL, RT ENGINE THRUST REVERSE AMBER LIGHT REMAINED ON AFTER FORWARD THRUST WAS SELECTED. THRUST LEVERS WERE ADVANCED AND CREW REJECTED TAKEOFF AT 30 KTS. PERFORMED HIGH ENERGY STOP INSPECTION IAW AMM 05-51-14. ADJUSTED LT CENTER THRUST REVERSER LOCK PROXIMITY SENSOR IAW FIM PROCEDURE 78-36 FAULT TREE 806 AND AMM 78-36-00. OPS CHECKS GOOD.

Part: WARNING LIGHT — FALSE ACTIVATION (THRUST REVERSER) · airframe 76,637 hrs · 35,674 cycles

REJECTED TAKEOFF, ENGINE THRUST REVERSE AMBER LIGHT DISPLAYED DURING FWD THRUST. FAULT CODE 78-36-04-02. TROUBLESHOT IAW FIM PROCEDURE 78-36 FAULT TREE 806 AND PSEU BITE CHECK 32-09-03. SYS CHECKED OK.

Part: SKIN — DAMAGED (ACCESS DOOR) · airframe 76,543 hrs · 35,645 cycles

FWD ACCESS DOOR 119AL EXTERIOR. SHOWS BLENDING OUT OF LIMITS. PERFORMED MAJOR REPAIR IAW SRM 52-40-01, FIG 1 AND IPI SEMAN NR 2012045, DATE 03-23-2012. REMOVED DAMAGED OUTER SKIN IAW SRM 51-40-02. FABRICATED NEW OUTER SKIN IAW SRM 52-40-01, FIG 1. CLEANED, TREATED, PRIMED AREA AND NEW OUTER SKIN IAW SRM 51-20-01. INSTALLED NEW OUTER SKIN IAW SRM 51-40-02, 51-40-01, 51-40-03 AND 51-20-05 PERFORMED HEAT TREATMENT TO RIVETS TYPE IAW BPS-R-131.

Part: FUEL TANK — LEAKING (ZONE 600)

DURING TAKEOFF, THE CREW SMELLED A STRONG FUEL ODOR, THE PACKS WERE TURNED ON AND FUEL ODOR WENT AWAY. THE CREW LANDED WITHOUT FURTHER INCIDENT. MX INSPECTED FUEL SYS AND FOUND FUEL LEAK COMMING FROM CRACKED FASTENER ON THE RT TANK AT PYLON. THEY REPLACED AND RESEALED FASTENER IAW SRM 51-40-00 AND 51-20-05. LEAK CHECKED GOOD ON BOTH RT MAIN TANK AND CENTER TANK IAW AMM 28-11-00. ACFT RETURNED TO SERVICE.

Part: FAIRING — CONTAMINATED (WING-BODY) · airframe 76,227 hrs · 35,500 cycles

DURING TAKEOFF, THE CREW SMELLED A STRONG FUEL ODOR, THE PACKS WERE TURNED ON AND FUEL ODOR WENT AWAY. THE CREW LANDED WITHOUT FURTHER INCIDENT. MX CLEANED RESIDUAL FUEL FROM RT WING TO BODY FAIRING IAW AMM 20-30-83/201. ACFT WAS RETURNED TO SERVICE.

Part: DOOR FRAME — CRACKED (NR 2 PYLON) · airframe 74,722 hrs · 34,783 cycles

DURING ROUTINE C-CHECK INSP FOUND NR 2 PYLON INBD LWR HYD BAY DOOR FRAME CRACKED. REMOVED CRACKED FRAME. INSTALLED NEW FRAME IAW SRM 51-40-02.

Part: ANGLE — CRACKED (ZONE 400) · airframe 74,722 hrs · 34,783 cycles

DURING ROUTINE C-INSP FOUND ANGLE CRACKED ON NR 2 ENGINE PYLON. REMOVED CRACKED ANGLE. WELDED CRACKED ANGLE. REINSTALLED ANGLE IAW AMES PSM CHAP 7 SECTION 03, REV 3 6-14-10, AND SRM 51-40-02.

Part: DOOR FRAME — CRACKED (NR 2 NACELLE) · airframe 74,722 hrs · 34,783 cycles

DURING ROUTINE C-CHECK INSP FOUND NR 2 PYLON OTBD LOWER HYD BAY DOOR FRAME CRACKED. REMOVED CRACKED FRAME. INSTALLED NEW FRAME IAW SRM 51-40-02.

Part: STRUCTURE — CRACKED (BS 287) · airframe 74,722 hrs · 34,783 cycles

DURING ROUTINE C-CHECK INSP FOUND CHORD CRACKED AT STA 287 RT BOTTOM LINE 25. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSP. NO DISCREPANCIES NOTED. FABRICATED DOUBLERS. HEAT TREATED REPAIR PARTS. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW SRM 51-70-12, 51-40-02, AND NDT 51-00-19, PART6,

Part: SKIN — CRACKED (APU INTAKE DOOR) · airframe 74,762 hrs · 34,783 cycles

DURING ROUTINE C-CHECK INSP FOUND UPPER END APU AIR INTAKE DOOR SKIN CRACKED AT STA FS 1725. REMOVED CRACKED SKIN. PERFORMED NDT INSP. NO DISCREPANCIES NOTED. FABRICATED NEW SKIN, INTERNAL AND EXTERNAL DOUBLERS. CLEANED, TREATED PRIMED AREA AND REPAIR PARTS. INSTALLED REPAIR PARTS IAW FIG 201, REPAIR NR 5. MM 51-21-01-7, SRM 51-40-02, NDT PART E 51-00-19, 51-21-04-7, AND 51-21-10-7.

Part: SUPPORT BRACKET — CRACKED (NR 11 SPOILER) · airframe 74,722 hrs · 34,783 cycles

DURING ROUTINE C-CHECK INSP FOUND NR 11 SPOILER INBD SUPPORT BRACKET CRACKED AT WS 700. REMOVED CRACKED SPOILER SUPPORT BRACKET. INSTALLED NEW SPOILER SUPPORT BRACKET IAW SRM 51-40-02.