N255CM

Part: LINK — DAMAGED (ZONE 700) · airframe 94,728 hrs · 25,535 cycles

ON APPROACH GEAR NOT DOWN EICAS & NO NLG GREEN LIGHT NOT ILLUMINATED, FOLLOWED BY GEAR DISAGREE CHKLIST. 2 LOW PASSES FROM TOWER INDICATED NLG GEAR APPEARED TO BE DOWN. EICAS CONFIG & DISAGREE CHKLISTS PERFORMED & GEAR COMPLETION OF 14:16 LANDING SUCCESSFUL & TAXI TO GATE. WAS ADVISED NLG PIN WOULD NOT SECURE IN NLG. CREW DECLARED EMERGENCY LANDING. ACFT LANDED WITHOUT INCIDENT. ACFT GROUNDED FOR INSP & MX. R & R DAMAGED NLG AFT LOCK LINK & LEAKING LOCK ACTUATOR IAW AMM 32-21-09 & AMM 32-34-02. REMOVED, REPLACED & ADJUSTED NLG LOCK PROXIMITY SWITCH SENSORS S255 & S233 IAW AMM 32-61-03. GREASED ALL FITTINGS ON NLG IAW AMM 12-21-12. OPS AND LEAK CHKD GOOD IAW AMM 32-34-00. NO FURHTER MAINTENANCE ACTION REQUIRED.

Part: SEAL — DIRTY (R SLIDING WINDOW) · airframe 92,349 hrs · 24,580 cycles

PREFLIGHT CREW REPORTED R2 WINDOW DIFFICULT TO CLOSE. R2 WINDOW SEAL CLEANED AND LUBRICATED IAW BOEING 767-300 AIRCRAFT MAINTENANCE MANUAL 56-11-02. OPERATIONAL CHECK GOOD.

Part: ESCAPE REEL — UNWANTED DEPLOY (NR 5) · airframe 92,335 hrs · 24,568 cycles

POST FLIGHT LINE MAINTENANCE REPORTED ESCAPE REEL POSITION 5 DEPLOYED. FAULT TRANSFERRED TO DEFERRAL MAINTENANCE ITEM 52790 PER ATI MINIMUM EQUIPMENT LIST 25-61-01-01. ESCAPE DESCENT DEVICE CERTIFIED INOPERATIVE. POSITION 5 ESCAPE DEVICE REMOVED AND REPLACED. DEFERRAL MAINTENANCE ITEM 52790 CLEARED.

Part: ESCAPE REEL — UNWANTED DEPLOY (CABIN) · airframe 92,335 hrs · 24,568 cycles

POST FLIGHT LINE MAINTENANCE REPORTED ESCAPE REEL POSITION 4 DEPLOYED. FAULT TRANSFERRED TO DEFERRAL MAINTENANCE ITEM 52789 PER ATI MINIMUM EQUIPMENT LIST 25-61-01-01. ESCAPE DESCENT DEVICE CERTIFIED INOPERATIVE. POSITION 4 ESCAPE DEVICE REMOVED AND REPLACED.

Part: FRAME ANGLE — CRACKED (BS 883) · airframe 92,247 hrs · 25,534 cycles

REPAIR, MAIN FRAME INNER CHORD TRANSITION RADIUS. STA 883.5 RBL 89

Part: SKIN PANEL — DELAMINATED (VERTICAL STAB) · airframe 92,247 hrs · 25,534 cycles

R/H VERTICAL STAB HAS AREA DELAMINATED ON SKIN PANEL

Part: BATTERY — INOPERATIVE (UNKNOWN) · airframe 91,876 hrs · 24,391 cycles

DURING DAILY CHECK FOUND FLASHLIGHT IN FLIGHT DECK INOPERATIVE. REMOVED AND REPLACED FLASHLIGHT IN ACCORDANCE WITH IAI SSM 25-60-00.

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 91,821 hrs · 24,381 cycles

DURING SERVICE CHECK FOUND FLASHLIGHT INOPERATIVE. REMOVED AND REPLACED FLASHLIGHT BATTERY PACK PER AMM 25-64-00. OPERATIONAL CHECK GOOD.

Part: BATTERY — INOPERATIVE (C/P FLASHLIGHT) · airframe 90,579 hrs · 23,825 cycles

DURING ROUTINE MAINTENANCE FLIGHT DECK'S FLASHLIGHT RED BATTERY INDICATOR INOPERATIVE. REMOVED AND REPLACED EMERGENCY FLIGHT DECK FLASHLIGHT BATTERY IN ACCORDANCE WITH B767 IAI 25-60-00. OPERATIONAL CHECK GOOD.

Part: PAD — WORN (ZONE 400) · airframe 90,166 hrs · 23,601 cycles

REMOVED AND REPLACED # 2 ENGINE LOUVRED DOOR , AFT LATCH STOP PAD SEE PARTIAL 1-4 FOR FAB OF STOP PAD IAW B767 SRM 51-40-02 PARA 4

Part: WEB — CORRODED (ZONE 100) · airframe 90,166 hrs · 23,601 cycles

ALC PRESSURE DECK WEB @ STA 1310 RBL6 CORRODED

Part: ROD — DAMAGED (ZONE 500) · airframe 90,166 hrs · 23,601 cycles

HOLD OPEN ROD CHAFED AND DAMAGED #1 ENGINE O/B HYDRAULICS' BAY DOOR

Part: STRAP — CORRODED (ZONE 100) · corrosion level 2 · airframe 90,166 hrs · 23,601 cycles

FAIL SAFE STRAP CORRODED STA 540-610 RBL 44

Part: PANEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 90,166 hrs · 23,601 cycles

AORROSION FLC STA 522 ,RBL47 IN POCKET AT CHORD

Part: BRACKET — CORRODED (ZONE 100) · corrosion level 2 · airframe 90,166 hrs · 23,601 cycles

CORROSION WASTE TANK BRACKET P/N 417T1310-23

Part: PRESSURE WEB — CORRODED (ZONE 300) · corrosion level 2 · airframe 90,166 hrs · 23,601 cycles

CORROSION ON FWD SIDE OF P-DOME

Part: SUPPORT WEB — CORRODED (ZONE 100) · airframe 90,166 hrs · 23,601 cycles

ALC PDU MOUNT STA 1346 LBL33 CORRODED

Part: SKIN — DAMAGED (ZONE 600) · airframe 90,166 hrs · 23,601 cycles

CRACK DAMAGE RIGHT WING FIXED LEADING EDGE SKIN

Part: BRACKET — CORRODED (ZONE 100) · airframe 90,166 hrs · 23,601 cycles

CANNON PLUG CONNECTOR BRACKET ON PDU PAN AT STA 621 CORRODED

Part: SUPPORT FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 90,166 hrs · 23,601 cycles

FUSELAGE FRAME CORRODED

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 90,166 hrs · 23,601 cycles

INNER CHORD CORRODED

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 90,166 hrs · 23,601 cycles

STRINGER CORRODED

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 90,166 hrs · 23,601 cycles

STRINGER 39 L CORRODED

Part: WEB — CORRODED (ZONE 200) · corrosion level 2 · airframe 90,166 hrs · 23,601 cycles

UPPER CARGO FRAME CORRODED.

Part: PANEL — CRACKED (ZONE 100) · airframe 90,166 hrs · 23,601 cycles

P-33 PANEL CRACKED

Part: PANEL SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 90,166 hrs · 23,601 cycles

LPANEL SUPPORT CHORD CHORD

Part: FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 90,166 hrs · 23,601 cycles

CORROSION ON LOWER SURFACE OF UPPER FRAME CHORD, FRAME 1395 AT THE ROLLER RAIL LBL42 TO RBL42

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 90,166 hrs · 23,601 cycles

CORROSION ON STR 39L, FROM STA1540 TO STA 1542

Part: FLOOR PANEL — CORRODED (ZONE 100) · airframe 90,166 hrs · 23,601 cycles

CORRODED FLOOR BEAM UPPER CHORD

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 90,166 hrs · 23,601 cycles

STRINGER 39R CORRODED

Part: FLOOR PANEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 90,166 hrs · 23,601 cycles

FLOOR WEB CORRODED

Part: ATTACH ANGLE — CORRODED (ZONE 200) · corrosion level 2 · airframe 90,166 hrs · 23,601 cycles

SEAL DEPRESSOR ATTACH ANGLE CORRODED

Part: STRINGER CLIP — CORRODED (ZONE 100) · corrosion level 2 · airframe 90,166 hrs · 23,601 cycles

STRINGER CLIP CORRODED

Part: SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 90,166 hrs · 23,601 cycles

ROLLER TRAY SUPPORT

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 90,166 hrs · 23,601 cycles

SEAR TIE CORRODED

Part: RUB STRIP — CRACKED (ZONE 400) · airframe 90,166 hrs · 23,601 cycles

RUB STRIP CRACKED

Part: SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 90,166 hrs · 23,601 cycles

CORROSION UNDER ALC PDU MOUNT

Part: ACCESS PANEL — CRACKED (ZONE 400) · airframe 90,166 hrs · 23,601 cycles

PYLON PANEL 436AL DAMAGED

Part: WEB — CORRODED (ZONE 100) · corrosion level 2 · airframe 90,166 hrs · 23,601 cycles

CORROSION ON INTERCOSTAL WEB

Part: SUPPORT FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 90,166 hrs · 23,601 cycles

WIRE SUPPORT CLIP CORRODED

Part: SEAL DEPRESSOR — CRACKED (ZONE 200) · airframe 90,166 hrs · 23,601 cycles

SEAL DEPRESSOR CRACKED

Part: PLATE — CORRODED (ZONE 100) · corrosion level 2 · airframe 90,166 hrs · 23,601 cycles

FLC SILL PLATE CORRODED.

Part: FLOOR SUPPORT — MISREPAIRED (ZONE 100) · airframe 90,166 hrs · 23,601 cycles

FLOOR SUPPORT STIFFENER HAS DOUBLE DRILLED HOLES

Part: PICKLE FORK — CORRODED (ZONE 100) · corrosion level 2 · airframe 90,166 hrs · 23,601 cycles

RIGHT REAR SPAR STA 955 CORROSION AT INBD SIDE OF PICKLE FORK AT TOP

Part: STRINGER FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 90,166 hrs · 23,601 cycles

STRINGER CHANNEL FITTING CORRODED

Part: LOCK — CORRODED (ZONE 200) · corrosion level 2 · airframe 90,166 hrs · 23,601 cycles

LOCK ASSY. CORRODED

Part: SEAL DEPRESSOR — CRACKED (ZONE 200) · airframe 90,166 hrs · 23,601 cycles

SEAL DEPRESSOR CRACKED

Part: FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 90,166 hrs · 23,601 cycles

FRAME CHORD CORRODED

Part: SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 90,166 hrs · 23,601 cycles

ROLLER TRAY SUPPORT CORRODED

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 90,166 hrs · 23,601 cycles

BULK CARGO FLOOR SUPPORT STRINGER CORRODED

Part: STRINGER FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 90,166 hrs · 23,601 cycles

S39L IB CORRODED @ STA 785.9 WHERE IT MEETS THE BULKHEAD

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 90,166 hrs · 23,601 cycles

CORROSION STA368 BETWEEN 39L-38L

Part: ROLLER TRAY — CORRODED (ZONE 100) · corrosion level 2 · airframe 90,166 hrs · 23,601 cycles

CORROSION ON SUPPORT BRACKET STA1175-1179 LBL2 WING LOCK TRAY

Part: INTERCOSTAL — CORRODED (ZONE 100) · corrosion level 2 · airframe 90,166 hrs · 23,601 cycles

FLC CORROSION ON INTERCOASTAL RBL21, STA610-632

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 90,166 hrs · 23,601 cycles

FLC STA 676 S30R-S31R SHEAR TIE CORROSION

Part: AILERON — DELAMINATED (ZONE 600) · airframe 90,166 hrs · 23,601 cycles

RT OUTBD AILERON IS DELAMINATED ON LOWER SURFACE

Part: FLOORBOARD — CORRODED (ZONE 200) · corrosion level 2 · airframe 90,166 hrs · 23,601 cycles

UPPER CARGO FLOORBOARD 232G CORROSION

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 90,166 hrs · 23,601 cycles

CORROSION STA1283, RBL28 BALLMAT SUPPORT

Part: PLATE — CORRODED (ZONE 100) · corrosion level 2 · airframe 90,166 hrs · 23,601 cycles

CORROSION ON PLATE ASSEMBLY P/N 143T8510-23

Part: ROLLER TRAY — CRACKED (ZONE 100) · corrosion level 2 · airframe 90,166 hrs · 23,601 cycles

ALC ROLLER PAN 1R CRACKED

Part: ROLLER TRAY — CORRODED (ZONE 100) · airframe 90,166 hrs · 23,601 cycles

ALC CORROSION ON WING LOCK TRAY STA 1373 LBL6-LBL20

Part: SKIN PANEL — CORRODED (ZONE 100) · airframe 90,166 hrs · 23,601 cycles

FLC PDU TRAY 2L CORRODED UPPER AND LOWER SURFACES

Part: FLOOR SUPPORT — DAMAGED (ZONE 100) · airframe 90,166 hrs · 23,601 cycles

TOOLING DANAGE ON WEB AT STA 522

Part: PRESSURE WEB — CORRODED (ZONE 300) · corrosion level 2 · airframe 90,166 hrs · 23,601 cycles

CORROSION ON FWD SIDE OF AFT PRESSURE DOME

Part: SUPPORT BEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 90,166 hrs · 23,601 cycles

CORROSION FOUND ON TRANSITION BEAM (FLOOR BOARD SUPPORT BEAM) AT STA 1413 LBL 42 TO RBL 42 AROUND NUT PLATE HOLES TOP AND BOTTOM.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 90,166 hrs · 23,601 cycles

STRINGER CORRODED

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 90,166 hrs · 23,601 cycles

CORROSION FLOOR SUPPORT FS 1439 AT LBL8

Part: TORQUE TUBE — CHAFED (ZONE 500) · airframe 90,166 hrs · 23,601 cycles

LW IB TE TORQUE TUBE HAS BARE METAL/WEAR MARKS

Part: TUBE — CORRODED (LT WING TE FLAP) · corrosion level 3

LEFT WING INBOARD FLAP INNER TUBE CORRODED AND PITTED

Part: TORQUE TUBE — DAMAGED (ZONE 600) · airframe 90,166 hrs · 23,601 cycles

R/W T/E I/B FLAP OUTER TORQUE TUBE PITTED

Part: TORQUE TUBE — DAMAGED (ZONE 600) · airframe 90,166 hrs · 23,601 cycles

R/W T/E I/B INNER TORQUE TUBE PITTED

Part: TORQUE TUBE — DAMAGED (ZONE 500) · airframe 90,166 hrs · 23,601 cycles

LEFT WING INBD FLAP TORQUE TUBE DAMAGED

Part: WEB — CORRODED (ZONE 100) · corrosion level 2 · airframe 90,166 hrs · 23,601 cycles

CORROSION ON WEB AT STA 530

Part: STIFFENER — CORRODED (ZONE 100) · corrosion level 2 · airframe 90,166 hrs · 23,601 cycles

STIFFENER CORRODED

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 90,166 hrs · 23,601 cycles

STRINGER CORRODED

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 90,166 hrs · 23,601 cycles

SHEAR TIE CORRODED

Part: FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 90,166 hrs · 23,601 cycles

FRAME UPPER CHORD CORRODED

Part: SUPPORT BEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 90,166 hrs · 23,601 cycles

SUPPORT BEAM CORRODED

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 90,166 hrs · 23,601 cycles

FLOOR SUPPORT CORRODED

Part: ROLLER TRAY — CORRODED (ZONE 100) · corrosion level 2 · airframe 90,166 hrs · 23,601 cycles

ROLLER TRAY CORRODED

Part: LOCK — CORRODED (ZONE 200) · airframe 90,166 hrs · 23,601 cycles

FLOOR LOCK CORRODED

Part: DOOR — CORRODED (ZONE 200) · airframe 90,166 hrs · 23,601 cycles

MDCD AFT SEAL DEPRESSOR ATTACH ANGLE CRACKED

Part: SUPPORT BEAM — CORRODED (ZONE 100) · airframe 89,334 hrs · 27,843 cycles

CORROSION ON THE LOWER AND UPPER SURFACES OF THE WING LOCK SUPPORT TRAY STA 1219 FROM LBL-6 - RBL- 20

Part: ROLLER TRAY — CORRODED (ZONE 100) · corrosion level 2 · airframe 90,166 hrs · 23,601 cycles

ROLLER TRAY CORRODED

Part: FAILSAFE — CORRODED (ZONE 100) · corrosion level 2 · airframe 90,166 hrs · 23,601 cycles

RH FAILSAFE STRAP CORRODED AT KICK LOAD FITTING

Part: WEB — CORRODED (ZONE 100) · corrosion level 2 · airframe 90,166 hrs · 23,601 cycles

CORROSION ON CARGO GUIDE SUPPORT BEAM

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 90,166 hrs · 23,601 cycles

FLOOR SUPPORTS CORRODED

Part: INTERCOSTAL — CORRODED (ZONE 100) · corrosion level 2 · airframe 90,166 hrs · 23,601 cycles

INTERCOSTAL FLOOR SUPPORT CORRODED

Part: NONE — CORRODED (ZONE 100) · corrosion level 2 · airframe 90,166 hrs · 23,601 cycles

FRAME CHORD CORRODED.

Part: FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 90,166 hrs · 23,601 cycles

FITTING CORRODED BEYOND LIMITS

Part: CRANK ASSY — CORRODED (ZONE 500) · corrosion level 2 · airframe 90,166 hrs · 23,601 cycles

FLAP SUPPORT CRANK ARM SHAFT CORRODED.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 90,166 hrs · 23,601 cycles

FLOOR SUPPORT CORRODED.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 90,166 hrs · 23,601 cycles

FLOOR SUPPORT CORRODED

Part: INTERCOSTAL — CORRODED (ZONE 100) · corrosion level 2 · airframe 90,166 hrs · 23,601 cycles

CORROSION AROUND NUTPLATES ON UNDERSIDE OF INTERCOSTAL AT RBL 21 BETWEEN STA 588-610

Part: TRAY — CORRODED (ZONE 100) · corrosion level 2 · airframe 90,166 hrs · 23,601 cycles

WING LOCK TRAY WEB CORRODED

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 90,166 hrs · 23,601 cycles

SHEAR TIE CORRODED

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 90,166 hrs · 23,601 cycles

FLOOR SUPPORT FS 1540 CORROSION LBL33-RBL33

Part: SHEAR TIE — CORRODED · corrosion level 2 · airframe 90,166 hrs · 23,601 cycles

FS 1373 CORROSION ON SHEAR TIE BETWEEN L30R AND L31R

Part: INTERCOSTAL — CORRODED (ZONE 100) · corrosion level 2 · airframe 90,166 hrs · 23,601 cycles

CORROSION AT B STA 574, BLO, UNDER THE CDU.FLC.

Part: NONE — DAMAGED (ZONE 600) · airframe 90,166 hrs · 23,601 cycles

PANEL 611FB HAS COMPOSITE DAMAGE FRONT SPAR RT HAND LOWER 318.33 TO 371.00.

Part: WEB — GOUGED (ZONE 100) · airframe 90,166 hrs · 23,601 cycles

GOUGE FOUND ON WEB AT STA 566 BL0

Part: NONE — CORRODED (ZONE 100) · corrosion level 2 · airframe 90,166 hrs · 23,601 cycles

CORROSION ON THE LOWER SURFACE OF THE FRAME UPPER CHORD (ALC FLOOR LEVEL FRAME STA 1153 FROM LBL42 TO RBL 42.

Part: SLAT — DAMAGED (ZONE 600) · airframe 90,166 hrs · 23,601 cycles

PANEL 611FB HAS COMPOSITE DAMAGE FRONT SPAR RT HAND LOWER 318.33 TO 371.00.

Part: NONE — DAMAGED (ZONE 200) · airframe 90,166 hrs · 23,601 cycles

AREA OF CORROSION UNDER BUBBLED UP PAINT AT FWD LOWER CORNER OF APU INLET DOOR FRAME DURING BLEND OUT REVEALED 3/4 INCH CRACK IN SIDE FAIRING SKIN.

Part: FLOOR PANEL — DAMAGED (ZONE 100) · airframe 90,166 hrs · 23,601 cycles

FLC FLOOR PANEL 122BF HAS COMPOSITE DAMAGE.

Part: NONE — CORRODED (ZONE 100) · corrosion level 2 · airframe 90,166 hrs · 23,601 cycles

CORROSION ON THE LOWER SURFACE OF THE UPPER FRAME CHORD, OF FRAME 1395 ( AT ALC FLOOR LEVEL ), AT THE ROLLER RAIL LOCATIONS FROM LBL42 TO RBL42.

Part: NONE — DAMAGED (ZONE 500) · airframe 90,166 hrs · 23,601 cycles

LEFT WING PANEL 511CB HAS SPEED TAPE REPAIR. COMPOSITE DAMAGE.

Part: NONE — DAMAGED (ZONE 600) · airframe 90,166 hrs · 23,601 cycles

RIGHT WING PANEL 611BB HAS COMPOSITE DAMAGE STA 197 TO STA 226.

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 90,166 hrs · 23,601 cycles

SHEAR TIE STA 1395 BETWEEN STRINGERS 37L - 38L CORRODED.

Part: FLOOR PANEL — DAMAGED (ZONE 100) · airframe 90,166 hrs · 23,601 cycles

FLC FLOOR PANEL 122DF HAS COMPOSITE DAMAGE 1 INCH X 1INCH HOLE.

Part: BRACKET — BROKEN (ZONE 100) · airframe 90,166 hrs · 23,601 cycles

STA 1562 - 1584 RBL 74 PART # 368-16-94490 FLOOR BOARD SUPPORT HAS BROKEN BRACKET ON FWD SIDE.

Part: STIFFENER — CORRODED (ZONE 100) · corrosion level 2 · airframe 90,166 hrs · 23,601 cycles

CORROSION FOUND ON WEB FLOOR SUPPORT STIFFENER AT STA 1480 RBL 9.

Part: NONE — CORRODED (ZONE 100) · corrosion level 2 · airframe 90,166 hrs · 23,601 cycles

ALC FLOOR PANEL SUPPORT IS CORRODED ON IT'S LOWER SURFACE AROUND THE NUTPLATE AT STA 1351 LBL18.

Part: CROSSMEMBER — CORRODED (ZONE 100) · corrosion level 2 · airframe 90,166 hrs · 23,601 cycles

CORROSION ON THE LOWER KEEL PANEL SUPPORT, CROSSMEMBER SUPPORT AT FS STA918.

Part: NONE — CORRODED (ZONE 100) · corrosion level 2 · airframe 90,166 hrs · 23,601 cycles

CORROSION ON THE LOWER KEEL PANEL SUPPORT, CROSSMEMBER SUPPORT, AT STA 1038.

Part: NONE — CORRODED (ZONE 100) · corrosion level 2 · airframe 90,166 hrs · 23,601 cycles

CORROSION ON THE LOWER SURFACE OF THE WING LOCK TRAY AT STA 1395 FROM LBL6 TO RBL20.

Part: NONE — GOUGED (ZONE 600) · airframe 90,166 hrs · 23,601 cycles

FLAP MITIGATION INSPECTION RIGHT FLAP 6 - 9 DRIVE BEAM ON THE # 8 FLAP SUPPORT HAS TOOLING MARKS/GOUGES.

Part: SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 89,334 hrs · 27,843 cycles

SUPPORT CORRODED

Part: FLOOR PANEL — DAMAGED (ZONE 100) · airframe 90,166 hrs · 23,601 cycles

FLC FLOOR PNL MID R/H @ STA 478 - 544 HAS COMPOSITE DAMAGE.

Part: SUPPORT PLATE — CORRODED (ZONE 100) · corrosion level 2 · airframe 90,166 hrs · 23,601 cycles

WING LOCK SUPPORT TRAY CORRODED

Part: SUPPORT FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 90,166 hrs · 23,601 cycles

CORROSION ON SUPPORT FITTING AT STA1179 BL0 ON WING LOCK TRAY ASSY

Part: SUPPORT BRACKET — CORRODED (ZONE 100) · corrosion level 2 · airframe 90,166 hrs · 23,601 cycles

CORROSION ON SUPPORT BRACKET

Part: SUPPORT FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 90,166 hrs · 23,601 cycles

CORROSION ON SUPPORT FITTING AT STA1179 RB16 ON WING LOCK TRAY ASSY

Part: NONE — CRACKED (ZONE 400) · corrosion level 2 · airframe 110,025 hrs · 21,353 cycles

CRACKED ANGLE SUPPORT BTWN AFT AND MID TOQRUE BOX #1 ENG PYLON. FAS WO N389AZ-02-01 NON ROUTINE 00065

Part: BEAM — GOUGED (ZONE 600) · corrosion level 2 · airframe 90,166 hrs · 23,601 cycles

(FLAP MITIGATION) RT WING #8 FLAP SUPPORT 1 2 3 BEAM HAS SMALL GOUGE INSIDE CENTER SECTION.

Part: FLANGE — CRACKED (ZONE 400) · airframe 90,166 hrs · 23,601 cycles

#1 ENG TR AFT METAL RUB STRIP CRACKED FLANGE ON UPPER AFT CORNER OF THE C-DUCT

Part: SUPPORT BRACKET — CORRODED (ZONE 100) · corrosion level 2 · airframe 90,166 hrs · 23,601 cycles

ALC PRESSURE WEB PANEL SUPPORT STRUCTURE AT STA 1324 CORRODED

Part: SUPPORT BRACKET — CORRODED (ZONE 100) · corrosion level 2 · airframe 90,166 hrs · 23,601 cycles

FLOOR SUPPORT STRUCTURE AT STA 1285 CORRODED

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 90,166 hrs · 23,601 cycles

ALC PRESSURE DECK WEB SUPPORT STRUCTURE CORRODED

Part: WEB — CRACKED (ZONE 400) · airframe 90,166 hrs · 23,601 cycles

#2 OB CORE COWL INNER WEB CRACKED

Part: INTERCOSTAL — CORRODED (ZONE 100) · airframe 90,166 hrs · 23,601 cycles

ALC INTERCOASTAL STATION 1087-1107 LBL42 HAS CORRODED NUTPLATES AND CORROSION ON SURFACE

Part: FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 90,166 hrs · 23,601 cycles

CORROSION ON STATION 1373 UPPER FRAME CHORD UPPER AND LOWER SURFACES, AT THE ALC FLOOR LEVEL LBL42 TO RBL20

Part: FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 90,166 hrs · 23,601 cycles

CORROSION ON THE UPPER AND LOWER SURFACE OF THE UPPER CHORD AT STATION 1197 ALC FLOOR LEVEL FROM LBL42 TO RBL42

Part: STIFFENER — CRACKED (ZONE 100) · airframe 90,166 hrs · 23,601 cycles

STA 676 AT 34L STIFFNER CRACKED

Part: SUPPORT FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 90,166 hrs · 23,601 cycles

CORROSION ON LOWER AND UPPER SURFACES OF THE UPPER CHORD STATION 1219, ALC FLOOR LBL 42 TO RBL42

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 90,166 hrs · 23,601 cycles

CORROSION ON FLOOR SUPPORT

Part: INTERCOSTAL — CORRODED (ZONE 100) · corrosion level 2 · airframe 90,166 hrs · 23,601 cycles

ALC INTERCOSTAL CORRODED

Part: ANGLE — CORRODED (ZONE 100) · corrosion level 2 · airframe 90,166 hrs · 23,601 cycles

ALC Z ANGLE CORRODED

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · airframe 90,166 hrs · 23,601 cycles

FLOOR SUPPORT CORRODED

Part: SPAR WEB — CORRODED (ZONE 100) · corrosion level 2 · airframe 90,166 hrs · 23,601 cycles

CORROSION FOUND ON AFT SPAR WEB OF WING CENTER BOX ON THE PAD UP AREA COMMON TO THE 22 BOLT HOLES THAT MOUNT THE PICKLE FORK.

Part: FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 90,166 hrs · 23,601 cycles

FLC CORROSION @ FLOOR FRAME UPPER CHORD STATION 676 RBL 17-22

Part: FRAME — CORRODED (ZONE 100) · airframe 90,166 hrs · 23,601 cycles

ZONE 100 CORROSION LBL 4 STATION 676 WEB

Part: FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 90,166 hrs · 23,601 cycles

FLC CORROSION @ STATION 676 RBL 45 UPPER CHORD

Part: SHEAR TIE — CORRODED (ZONE 100) · airframe 90,166 hrs · 23,601 cycles

SHEAR TIE CORRODED AT STATION 544, BL0

Part: FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 90,166 hrs · 23,601 cycles

FLC CORROSION @ STATION 676 RBL 5-8 FLOOR FRAME UPPER CHORD

Part: FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 90,166 hrs · 23,601 cycles

ALC CORROSION AT STA1109 RBL 6 FRAME UPPER CHORD

Part: SUPPORT — CORRODED (ZONE 100) · airframe 90,166 hrs · 23,601 cycles

CORROSION ON SUPPORT STATION 1417 BL0

Part: STRINGER — CORRODED (ZONE 100) · airframe 90,166 hrs · 23,601 cycles

CORROSION FLC STA 480, STR 36R

Part: THRUST REVERSER — CORRODED (ZONE 400) · corrosion level 2 · airframe 90,166 hrs · 23,601 cycles

CORROSION #2 ENGINE CASCADE SEGMENT

Part: ROLLER TRAY — CORRODED (ZONE 100) · corrosion level 2 · airframe 90,166 hrs · 23,601 cycles

ALC ROLLER TRAY LBL 10 STA 1087-1197 CORROSION

Part: STRINGER — CRACKED (ZONE 100) · airframe 90,166 hrs · 23,601 cycles

STRINGER 24 AT STA 676 CRACKED

Part: LOCK — CORRODED · corrosion level 2 · airframe 90,166 hrs · 23,601 cycles

CORROSION ON LOCK ASSEMBLY

Part: SHEAR TIE — CORRODED (ZONE 100) · airframe 90,166 hrs · 23,601 cycles

CORROSION FLC STA 412 SHEAR TIE BETWEEN STR 36R AND 37R

Part: FRAME — CORRODED (ZONE 100) · airframe 90,166 hrs · 23,601 cycles

CORROSION ON FRAME UPPER CHORD STA 742 AT LBL20-LBL42

Part: SUPPORT ANGLE — CORRODED (ZONE 100) · airframe 90,166 hrs · 23,601 cycles

CORROSION ON THE ALC CEILING PANEL SUPPORTS STA1351

Part: WEB — CORRODED (ZONE 100) · airframe 90,166 hrs · 23,601 cycles

CORROSION LOWER SURFACE WING LOCK SUPPORT TRAY

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · airframe 90,166 hrs · 23,601 cycles

CENTER FLOOR SUPPORT FS 1470-1414 CORROSION

Part: LOCK — CORRODED (ZONE 100) · corrosion level 2 · airframe 90,166 hrs · 23,601 cycles

CORROSION ON CARGO LOCK

Part: FLAP — CORRODED (ZONE 600) · corrosion level 2 · airframe 90,166 hrs · 23,601 cycles

RIGHT FLAP 6-6 PIN INNER AND OUTER HAS CORROSION

Part: TORQUE TUBE — WORN (ZONE 500) · corrosion level 2 · airframe 90,166 hrs · 23,601 cycles

LW INBD #4 SUPPORT TORQUE TUBE WORN AND PITTED

Part: SCUFF PLATE — CORRODED (ZONE 200) · corrosion level 2 · airframe 90,166 hrs · 23,601 cycles

R2 DOOR MAIN SCUFF PLATE CORRODED

Part: FLOOR PANEL — CRACKED (ZONE 200) · airframe 90,166 hrs · 23,601 cycles

UPPER CARGO FLOOR PANEL 241M DAMAGED HONEYCOMB

Part: LOCK FITTING — CORRODED (ZONE 200) · corrosion level 2 · airframe 90,166 hrs · 23,601 cycles

UPPER CARGO CENTER LOCK PAD STA 1417 BL0 HAS CORROSION

Part: SEAL PLATE — DELAMINATED (ZONE 800) · airframe 90,166 hrs · 23,601 cycles

RMLG DOOR AFT EDGE SEAL PLATES ARE COMING LOOSE AND HAS MULTIPLE AREAS OF DELAMINATION

Part: STRAP — CORRODED (ZONE 100) · corrosion level 2 · airframe 90,166 hrs · 23,601 cycles

FLC FWD DOOR FRAME UPPERSTRAP CORRODED

Part: LOCK FITTING — CORRODED (ZONE 200) · corrosion level 2 · airframe 90,166 hrs · 23,601 cycles

UPPER CARGO LOCK PAD STA 1502 RBL 66 HAS CORROSION.

Part: WEB — CORRODED (ZONE 100) · corrosion level 2 · airframe 90,166 hrs · 23,601 cycles

ALC PRESSURE WEB CORRODED

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 90,166 hrs · 23,601 cycles

SHEAR TIE AT STA 1395 BETWEEN STRINGERS 3R-38R CORRODED

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 90,166 hrs · 23,601 cycles

ALC BALLMAT SUPPORT STRUCTURE CORRODED

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 90,166 hrs · 23,601 cycles

STRINGER 33R STA 1540 IN ALC IS CORRODED

Part: PANEL — CRACKED (ZONE 600) · airframe 90,166 hrs · 23,601 cycles

PANEL 194NR INNER SURFACE DAMAGED.

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 90,166 hrs · 23,601 cycles

SHEAR TIE STA 1307 BETWEEN STRINGERS 35R-36R IS CORRODED.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 90,166 hrs · 23,601 cycles

CORROSION ON LOWER FLOOR SUPPORT STRUCTURE

Part: CEILING PANEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 90,166 hrs · 23,601 cycles

CORROSION ON 2 ALC CEILING SUPPORTS, FROM STA 1285 TO STA 1307 AT RBL80 LOCATED ABOVE ALC DOORWAY

Part: FRAME ANGLE — CORRODED (ZONE 100) · corrosion level 2 · airframe 90,166 hrs · 23,601 cycles

CORROSION ON THE UPPER CHORD OF FRAME 1562

Part: STIFFENER — CORRODED (ZONE 100) · corrosion level 2 · airframe 90,166 hrs · 23,601 cycles

CORROSION ON THE WASTE VALVE BOX, FROM STA 1567 TO STA 1575

Part: FLOOR PANEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 90,166 hrs · 23,601 cycles

ALC SUB-FLOOR CORRODED

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 90,166 hrs · 23,601 cycles

2 FLOOR SUPPORTS CORRODED P/N 143T5000-71 AND 143T5000-72

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 90,166 hrs · 23,601 cycles

STRINGER 33R STA 1085-1101

Part: BRACKET — CORRODED (ZONE 100) · corrosion level 2 · airframe 90,166 hrs · 23,601 cycles

CORROSION ON BRACKET AT STA 1087

Part: FLOOR PANEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 90,166 hrs · 23,601 cycles

CORROSION FLC STA 588 RBL 2.5-7.5 FLOOR WEB

Part: SUPPORT BRACKET — CORRODED (ZONE 100) · corrosion level 2 · airframe 90,166 hrs · 23,601 cycles

FLOOR BOARD BRACKET CORRODED

Part: WEB — CORRODED (ZONE 100) · corrosion level 2 · airframe 90,166 hrs · 23,601 cycles

FLOOR WEB CORRODED

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 90,166 hrs · 23,601 cycles

CORROSION FLC STA 434 SHEAR TIEBETWEEN STR 37R AND 38R

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 90,166 hrs · 23,601 cycles

RT HAND SLOPE PANEL TO FLOOR SUPPORT FS1540 TO FS1409 RBL40 CORROSION

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 90,166 hrs · 23,601 cycles

CORROSION FLC STA 434 SHEAR TIE BETWEEN STR 39L AND 39R

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 90,166 hrs · 23,601 cycles

STRINGER FLANGE CORRODED STA 434

Part: STRUCTURE — CORRODED (ZONE 100) · corrosion level 2 · airframe 90,166 hrs · 23,601 cycles

UPPER CHORD CORROSION

Part: FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 90,166 hrs · 23,601 cycles

CORROSION FLC STA 478 RBL 21 & RBL 28 FLOOR FRAME UPPER CHORD LWR SURFACE

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 90,166 hrs · 23,601 cycles

FLC SHEAR TIE CORRODED STA 566

Part: SUPPORT BRACKET — CORRODED (ZONE 100) · corrosion level 2 · airframe 90,166 hrs · 23,601 cycles

CORROSION ON THE BULK CARGO CEILING SUPPORT

Part: CEILING PANEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 90,166 hrs · 23,601 cycles

ALC CEILING PANEL SUPPORT CORRODED

Part: BEAM — CORRODED (ZONE 800) · corrosion level 2 · airframe 90,166 hrs · 23,601 cycles

FWD LOWER CARGO DOOR BEAM BELOW VENT DOORS CORROSION AT 4 PLACES ON BEAM

Part: MOUNT — CRACKED (ZONE 100) · airframe 90,166 hrs · 23,601 cycles

ALC 8R PDU MOUNT CRACKED

Part: FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 90,166 hrs · 23,601 cycles

CORROSION ON THE LOWER SURFACE OF THE UPPER FRAME CHORD, AT STA.1175 (ALC FLOOR LEVEL) FROM LBL42 TO RBL42

Part: LOCK FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 90,166 hrs · 23,601 cycles

CORROSION ON LOWER SURFACE WING LOCK TRAY

Part: ROLLER TRAY — CORRODED (ZONE 100) · corrosion level 2 · airframe 90,166 hrs · 23,601 cycles

ROLLER TRAY SUPPORT IS CORRODED

Part: SUPPORT CHANNEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 90,166 hrs · 23,601 cycles

THE ROLLER TRAY SUPPORT IS CORRODED ON THE LOWER SURFACE, AT RBL20 FROM STA 1395 TO STA 1417

Part: SUPPORT CHANNEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 90,166 hrs · 23,601 cycles

THE ROLLER TRY SUPPORT IS CORRODED ON THE LOWER SURFACE AT RBL6 FROM STA 1395 TO STA 1417

Part: WEB — CORRODED (ZONE 100) · corrosion level 2 · airframe 90,166 hrs · 23,601 cycles

CORROSION ON LOWER SURFACE OF THE WING LOCK SUPPORT TRAY AT STA 1241 FROM LBL6 TO RBL20

Part: COWLING — CRACKED (ZONE 400) · airframe 90,166 hrs · 23,601 cycles

#1 ENGINE OB CORE COWL CRACKED AT LOWER CORNER OF VENT PANEL

Part: STRINGER — CORRODED (ZONE 300) · corrosion level 2 · airframe 90,166 hrs · 23,601 cycles

CORROSION LH HORZ STAB INTERNAL 6" OB SID OF RIB 2L LWR #9 STRINGER

Part: COWLING — DENTED (ZONE 400) · airframe 90,166 hrs · 23,601 cycles

N0 1 ENGINE INBD TR UPPER SECTION AROUND BLOCKER DOOR HAS PUNCTURES AND DENTS

Part: PANEL — CRACKED (ZONE 100) · airframe 90,166 hrs · 23,601 cycles

L/H FILLET PNL 195FL HAS COMPOSITE DAMAGE

Part: TEE ANGLE — CORRODED (ZONE 100) · corrosion level 2 · airframe 90,166 hrs · 23,601 cycles

CORROSION ON THE LOWER KEEL PANEL SUPPORT, CROSSMEMBER SUPPORT, AT STA.873.

Part: INTERCOSTAL — CORRODED (ZONE 800) · corrosion level 2 · airframe 90,166 hrs · 23,601 cycles

AFT CARGO DOOR HAS CORROSION ON #2,3,4 BEAM ASSY. FROM TOP OF DOOR AND ON INTERCOSTAL ON #4 BEAM ASSY. (INTERNAL SIDE)

Part: SKIN — CRACKED (ZONE 500) · airframe 90,166 hrs · 23,601 cycles

W LES 948 LWR L/E CRACKED

Part: PANEL — CRACKED (ZONE 300) · airframe 90,166 hrs · 23,601 cycles

VERT STAB REMOVABLE L/E PANEL 321E MOST UPPER L/E COMPOSITE ERODED & CRACKED

Part: SHROUD — CORRODED (ZONE 200) · corrosion level 2 · airframe 90,166 hrs · 23,601 cycles

CORROSION ON FIRE EXTINGUISHER SHOURD

Part: NOT REPORTED — NOT REPORTED (NOT REPORTED) · airframe 88,086 hrs · 22,731 cycles

IN THE ACCOMPLISHMENT OF EO 53-767-767-7487, STRUCTURAL FINDINGS WERE NOTED. AIRCRAFT GROUNDED FOR PAINT WORK IN PROGRESS.

Part: KEELBEAM — CORRODED (BS 999) · corrosion level 2 · airframe 86,325 hrs · 22,035 cycles

DURING KEEL BEAM INSPECTION PER ATI TASK S53-052-02, EXFOLIATION CORROSION IDENTIFIED AT PANEL 149BL, SEC 45, FS 999. AIRCRAFT GROUNDED FOR REPAIR. DAMAGE MEASURED AT 1.5 X 9/16. TOTAL BLEND OUT MEASURED 2.375 (L) X 1.125 (W) AND DEEPEST BLEND POINT MEASURED 0.0625. (D). BLEND OUT/INTERIM REAIR ACCOMPLISHED IAW B767-200 SRMP 53-50-12 AND ATI ENGINEERING ORDER 53-767-6968. PERMANENT REPAIR TO INCLUDE SHOT PEEN REWORK TO AFFECTED KEEL BEEM NO LATER THAN NEXT SCHEDULED HEAVY MAINTENANCE CHECK SCHEDULED MARCH 2020. AIRCRAFT RELEASED TO SERVICE

Part: CONNECTOR — DIRTY (COCKPIT) · airframe 81,334 hrs · 20,147 cycles

PREDEPARTURE CHECK: FLIGHT COMPARTMENT EMERGENCY EXIT SINGLE LIGHT INOPERATIVE. GENERAL VISUAL INSPECTION. CLEANED AND SECURED CONNECTOR. OPERATIONAL CHECK SATISFACTORY IAW B767 AMM 33-51-01. FAULT NOT DUPLICATED. NO FURTHER DEFECTS NOTED. NO PREVIOUS HISTORY OF DISCREPANCIES FOR SYS. ACFT RELEASED TO SERVICE.

Part: AUTOPILOT SYS — MALFUNCTIONED · airframe 83,421 hrs · 20,868 cycles

AT FL 370, CRUISE FLIGHT AUTOPILOT EICAS OFF. RE-ENGAGED THE AUTOPILOT EICAS OFF AGAIN. TRIED LEFT AND RIGHT AUTOPILOT, AUTOPILOT OFF QUICKER. CENTER ON AGAIN STAYED ON UNTIL DESCENT, H/S USED AUTOPILOT OFF, DESCENT TO FL 280, NON RVSM HAND ROLL DIFFICULT, FLOWN APPROACH. ROLL BECAME LOOSER WHILE DESCENDING, FLAPS 20 LANDING. EMERGENCY DECLARED AND LANDING WAS GUSTY BUT NORMAL. MAX AUTO BRAKE SELECTED EARLY ON APPROACH. COMPLETE STOP WITH NO INCIDENTS. AIRCRAFT GROUNDED. COMPLIED WITH FAULT ISOLATION MANUAL 27-11 FT 808, BLOCK 1 TO 41. FAULT NOT DUPLICATED ON GROUND. PERFORMED MCDP TEST 7-30-40-67, ALL PASSED, NO FAULTS IN PREVIOUS OR RESENT FLIGHT FAULTS IAW AMM 22-00-02. PERFORMED A DETAILED VISUAL INSPECTION OF AILERON FLIGHT CONTROL SYSTEM. EXAMINED ALL BEARINGS IN WW, FEEL MEC, TORQUE TUBES, CONTROL RODS, AILERON LOCKOUT MEC, AILERON OVERIDE QUANDRANT SUPPORT, SHAFT BEARINGS, LOST MOTION, AILERON CONTROL QUANDRANT, LCCA OUT PUT QUADRANT, LCCA HYD, LCCA TORQUE TUBES IAW AMM 27-11-16 FREE OF BINDING, DRUM ASSY, CONTROL WHEEL, CABLES-A1A-A1B-A2A-A2B-AB3A-AB3B. NO DAMAGE, MISSING PARTS, CORRODED PARTS, JAMBED, STIFF, OR SEIZED FOUND. NO FAULT BALLS ON CSEU BOX. AIRCRAFT IS OPERATING AS INTENDED IAW AMM 27-11-00. AILERON & AILERON TRIM CONTROL SYSTEM DESCRIPTION & OPERATIONS. MX-CONTROL AND OPS NOTED. ACCEPTANCE FLIGHT SATISFACTORY. NO DEFECTES NOTED. AIRCRAFT RELEASED TO SERVICE.

Part: STRINGER — CORRODED (HORIZONTAL STAB) · airframe 83,201 hrs · 22,789 cycles

HORIZONTAL STAB CONTROL BOX INTERNAL. CORROSION ON THE OTBD SIDE OF RIB 2L LOWER LT STRINGER 11, VERTICAL LEG FWD SIDE. INSTALLED A NEW HORIZONTAL STABILIZER STRINGER IAW SRM 31-40-02 & REA 47308 AB01. AIRCRAFT GROUNDED.

Part: BUSHING — CORRODED (LT MLG BLOCK) · corrosion level 2 · airframe 83,201 hrs · 20,789 cycles

LEFT LANDING GEAR H BLOCK DAMAGED BUSHINGS WITH CORROSION. REPAIRED L/H LANDING GEAR "H" BLOCK IAW REA 47308REA08 TO REMOVE CORROSION.

Part: STRUT — CORRODED (LT WING) · airframe 83,201 hrs · 20,789 cycles

LEFT WING LEADING EDGE STRUT AT INBOARD END OF THE NR 5 SLAT TAI TELESCOPING DUCT CORRODED AROUND END OF DUCT. THE STRUT WAS REMOVED AND REPLACED IAW DWG 114T2201. AIRCRAFT GROUNDED.

Part: KEELBEAM — CORRODED (BS 999) · corrosion level 2 · airframe 83,201 hrs · 20,789 cycles

LEFT KEEL LOWER FLANGE UPPER SURFACE CORRODED AT BS 999. REPAIRED LOWER INBOARD KEEL FLANGE IAW SRM 53-50-12, REPAIR 1. AIRCRAFT GROUNDED.

Part: BRACKET — DAMAGED (HORIZONTAL STAB) · airframe 81,967 hrs · 20,206 cycles

DURING COMPLIANCE OF AD 2008-06-06: DETAILED INSPECTION AND LUBRICATION FOR THE DRIVE MECHANISM OF THE HORIZONTAL STABILIZER, FOUND LEFT HORIZONTAL STAB UPPER BODY FAIRING DOOR, INCLUDING ATTACH BRACKETS, DAMAGED. LINKAGE FOR THE HORIZONTAL STABILIZER TO BODY SEAL DOOR HAD SHIFT OUT OF RIG RESULTING IN SIGNIFICANT DAMAGE TO THE UPPER HORIZONTAL STAB TO BODY SEAL DOOR LINKAGE, LEFT SEAL DOOR, AND AIRCRAFT STRUCTURE OF THE AIRPLANE. DAMAGE INCLUDED UPPER AND LOWER OUTBOARD CHORDS OF THE LONGERON SPANNING BETWEEN STATION 1725.50 AND STATION 1809.50 AT WATER LINE 258.44. THE DAMAGE WAS A DEFORMATION OF THE HORIZONTAL FLANGE OF EACH AFOREMENTIONED CHORD. AIRCRAFT WAS GROUNDED FOR STRUCTURAL REPAIRS. IN ACCORDANCE WITH ATI ENGINEERING ORDER 53-767-5811, TEMPORARY REPAIRS INCLUDED REMOVING AND REPLACING THE LEFT UPPER HORIZONTAL STABILIZER BODY FAIRING DOOR AS WELL AS THE DAMAGED ATTACHING BRACKETS.

Part: STRUCTURE — DAMAGED (HORIZONTAL STAB) · airframe 81,967 hrs · 20,206 cycles

FOUND THE LEFT HORIZONTAL STAB UPPER BODY FAIRING DOOR, INCLUDING ATTACH BRACKETS, DAMAGED. REPAIRED IAW EO 53-767-5811.

Part: TEE FITTING — CORRODED (BS 955) · corrosion level 2 · airframe 80,890 hrs · 19,821 cycles

RIGHT TEE FITTING IS CORRODED AT THE AFT LOWER BOLT HOLE. MATCH DRILLED NEW TEE FITTING IAW SRM 51-10-02. INSTALLED IAW ENGINEERING DOCUMENT 47008ORD04.

Part: FAILSAFE — CRACKED (BS 955) · airframe 80,890 hrs · 19,821 cycles

LEFT FAILSAFE STRAP HAS CRACK INDICATION IN LOWER BOLT HOLE OF TRIM OUT AREA. FAILSAFE STRAP TRIM OUT AND REPAIRED IAW ENGINEERING DOCUMENT 47008ORD03.

Part: STRAP — CRACKED (FUSELAGE) · airframe 80,890 hrs · 19,821 cycles

AIRCRAFT GROUNDED FOR HEAVY MAINTENANCE. RIGHT FAILSAFE STRAP LOWER HOLE HAS CRACKED AT 10:00 POSITION, VERIFIED WITH HFEC SURFACE SCAN AND ROTARY SCAN. FAILSAFE STRAP TRIM OUT AND REPAIR ACCOMPLISHED IAW EA 47008ORD04.

Part: TEE FITTING — CORRODED (BS 955) · corrosion level 2 · airframe 80,890 hrs · 19,821 cycles

LEFT TEE FITTING IS CORRODED AT THE AFT LOWER BOLT HOLE. A NEW TEE FITTING MATCH DRILLED IAW SRM 51-40-05. THE TEE FITTING WAS INSTALLED IAW ENGINEERING DOCUMENT 47008ORD03.