N359AZ

Part: WINDOW — RATCHETING (ZONE 200) · airframe 130,568 hrs · 24,491 cycles

FIRST OFFICER'S WINDOW WILL NOT CLOSE. MAKES RACHETING NOISE. AIRCRAFT. MAINTENANCE IN PROGRESS. SUPPLEMENTAL TO PREVIOUS REPORT IXXA20251207081 DATED 12/07/2025 AT KILN. REMOVED AND REPLACED CARRIAGE ASSEMBLY AND BALLSCREW OPERATING MECHANISM FOR R2 WINDOW IN ACCORDANCE WITH B767 AIRCRAFT MAINTENANCE MANUAL 56-11-04 AND B767 ISRAEL AEROSPACE INDUSTRIES SUPPLEMENTAL MAINTENANCE MANUAL 56-11-04. REINSTALLED ORIGINAL R2 WINDOW ASSEMBLY IAW B767 AMM 56-11-02 AND IAI SUPP AMM 56-11-02. OPERATOINAL AND LEAK CHECK GOOD.

Part: TERMINAL — LOOSE (ZONE 200) · airframe 128,377 hrs · 23,580 cycles

SUBSEQUENT TO SERVICE CHECK, LINE MAINTENANCE REPORTED L1 EMERGENCY EXIT SIGN WILL NOT ILLUMINATE. TIGHTENED TERMINAL SCREW PER BOEING 767-300 AIRCRAFT MAINTENANCE MANUAL 33-51-01. OPERATIONAL CHECK GOOD. NO ADDITIONAL FAULTS NOTED.

Part: INTERCOSTAL — CORRODED · airframe 128,058 hrs · 23,451 cycles

INTERCOSTAL STA 476-486 RBL 30 IS CORRODED.

Part: SUPPORT — CORRODED (ZONE 100) · airframe 128,058 hrs · 23,451 cycles

ALC PDU 8R O/B SUPPORT BEAM EXFOLIATED AROUND FWD & AFT MOUNT BOLT NUT PLATES & 2" AFT OF AFT NUT PLATE

Part: WEB — CORRODED (ZONE 200) · airframe 128,058 hrs · 23,451 cycles

J CHORD FOUND CORROSION ON WEB AT STA 720 RBL 38

Part: STIFFENER — CORRODED (ZONE 100) · airframe 128,058 hrs · 23,451 cycles

ALC STIFFENER @ STA. 1329-1351 RBL 33 LABELED "ITEM 7 & 8" HAS 9 CORRODED NUTPLATES, 3 OF WHICH HAVE EVIDENCE OF CORROSION ON STIFFENER SURFACE

Part: PANEL — DEBONDED (ZONE 300) · airframe 128,058 hrs · 23,451 cycles

RH SIDE OF VERTICAL STAB BETWEEN FRONT SPAR AND AUX SPAR BONDED SKIN PANEL DELAMINATION VIEWED IN BETWEEN FSS 170.259 TO 220.251

Part: WEB — CORRODED (ZONE 100) · airframe 128,058 hrs · 23,451 cycles

CORROSION FOUND UNDER PDU 4R

Part: LOCK — CORRODED (ZONE 100) · airframe 128,058 hrs · 23,451 cycles

L/H SIDE HAS CORRODED LOCK AT APPROX. STA. 1197+43

Part: SEAL — WORN (ZONE 300) · airframe 128,058 hrs · 23,451 cycles

PANEL 345AFB SEAL IS WORN

Part: STRINGER SPLICE — CORRODED (ZONE 100) · airframe 128,058 hrs · 23,451 cycles

STRINGER SPLICE P/N 143T3224-1 ON STINGER 38L FOUND CORRODED BEYOND LIMITS

Part: PANEL — CORRODED (ZONE 100) · airframe 128,058 hrs · 23,451 cycles

FLC BILGE PANEL STA 632-654 LT BL 12 IS CORRODED

Part: SKIN — DAMAGED (ZONE 600) · airframe 128,058 hrs · 23,451 cycles

R/W TIP MOUNTING BOLT HOLES THROUGH RIB (3 EACH) ARE ELONGATED.

Part: INTERCOSTAL — CORRODED (ZONE 100) · corrosion level 2 · airframe 128,058 hrs · 23,451 cycles

INTERCOASTAL CORRODED STA 544-566 RBL36

Part: HANDLE — DAMAGED (ZONE 800) · airframe 128,058 hrs · 23,451 cycles

FLC CARGO DOOR HANDLE DAMAGED

Part: NUT PLATE — CORRODED (ZONE 100) · corrosion level 2 · airframe 128,058 hrs · 23,451 cycles

NUT PLATE STRAP STA 544-566 BL 35L-34L CORRODED

Part: STRINGER — CORRODED (ZONE 100) · airframe 128,058 hrs · 23,451 cycles

ALC STR 37L CORRODED AT STA 1225

Part: INTERCOSTAL — CORRODED (ZONE 200) · airframe 128,058 hrs · 23,451 cycles

INTERCOSTAL STA588-610 RBL 25 CORRDODED AT NUTPLATES

Part: FLOORBEAM — CORRODED (ZONE 100) · airframe 128,058 hrs · 23,451 cycles

UNDERSIDE OF FLC FLOOR BEAM UPPER T CHORD IS HEAVILY CORRODED AROUND NUTPLATE AT LFS 720, LBL 43

Part: GROUND STUD — CORRODED (ZONE 100) · airframe 128,058 hrs · 23,451 cycles

GROUND LUG IN ALC BILGE PLATE @STA. 1280 RBL 29 IS CORRODED ON SURFACE & HARDWARE

Part: ROLLER TRAY — CORRODED (ZONE 100) · corrosion level 2 · airframe 128,058 hrs · 23,451 cycles

ROLLER TRAY STA 1159 RBL 8 CORRODED

Part: SKIN — DAMAGED (ZONE 100) · airframe 128,058 hrs · 23,451 cycles

THERE IS A DAMAGED FASTENER HOLE, IN THE EXTERIOR SURFACE OF THE FUSELAGE SKIN, WHERE THE LOWER SILL SCUFF PLATE HAS BEEN REMOVED FROM THE 4L DOOR LOCATION

Part: ROLLER TRAY — CORRODED (ZONE 100) · corrosion level 2 · airframe 128,058 hrs · 23,451 cycles

ROLLER TRAY RBL 20 STA 610-654+10 CORRODED

Part: FRAME — CORRODED (ZONE 100) · airframe 128,058 hrs · 23,451 cycles

FLC LT - RT FRAME @ F/S 498 RBL 33-43 IS CORRODED & SEPERATED

Part: PANEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 128,058 hrs · 23,451 cycles

BILGE PANEL STA 588 AT PDU CORRODED

Part: SHEAR WEB — CORRODED (ZONE 100) · airframe 128,058 hrs · 23,451 cycles

CENTER SHEAR WEB PANEL NUTPLATE ANGLE CORR AT LWR SIDE BETWEEN STA 1153 AND 1175

Part: INTERCOSTAL — CORRODED (ZONE 200) · airframe 128,058 hrs · 23,451 cycles

INTERCOSTAL & NUTPLATE ARE CORRODED @ F/S 566 RBL 26

Part: INTERCOSTAL — CORRODED (ZONE 100) · airframe 128,058 hrs · 23,451 cycles

UPON REMOVAL FOUND INTERCOSTAL STA 566-588 LBL 34 CORRODED AT NUTPLATES

Part: PANEL — CORRODED (ZONE 100) · airframe 128,058 hrs · 23,451 cycles

FLC BILGE PANEL STA 632-654 LT BL 12 IS CORRODED

Part: SEAT TRACK — CRACKED (COCKPIT) · airframe 128,058 hrs · 23,451 cycles

CAPT'S FWD OTBD SEAT TRACK IS CRACKED BETWEEN THE FWD STOP BOLT MOUNT HOLES. VERIFIED WITH HFEC

Part: ATTACH ANGLE — DAMAGED (ZONE 600) · airframe 128,058 hrs · 23,451 cycles

R/W FRONT SPAR ATTACH ANGLE P/N 112T2277-2 HAS ELONGATED HOLES

Part: ROLLER TRAY — CORRODED (ZONE 100) · corrosion level 2 · airframe 128,058 hrs · 23,451 cycles

ALC ROLLER TRAY STA 1197+24 1197+110 CORRODED

Part: STRINGER — CORRODED (ZONE 100) · airframe 128,058 hrs · 23,451 cycles

STR 38 LEFT AT HI-LOK IS CORRODED AT STA 654+128

Part: BRACKET — CORRODED (ZONE 200) · airframe 128,058 hrs · 23,451 cycles

FOUND DURING REMOVAL, WEB TO CHORD STIFFENER AT FLC STA 566 ELONGATED HOLE AND CORRODED.

Part: PANEL — CORRODED (ZONE 100) · airframe 128,058 hrs · 23,451 cycles

CENTER BILGE PANEL STA 544-566 CORRODED

Part: STRIKER — DAMAGED (ZONE 800) · airframe 128,058 hrs · 23,451 cycles

ALC DOOR STRIKER MISSING SKIN DAMAGE

Part: FRAME — CORRODED (ZONE 100) · airframe 128,058 hrs · 23,451 cycles

FRAME WEB STA 518-522 RBL 35 CORRODED

Part: INTERCOSTAL — CORRODED (ZONE 100) · airframe 128,058 hrs · 23,451 cycles

INTERCOSTAL STA 544-566 RBL 33 CORRODED AT NUTPLATES

Part: STRINGER — CORRODED (ZONE 100) · airframe 128,058 hrs · 23,451 cycles

ALC STR 37L CORRODED AT STA 1225

Part: BRACKET — CRACKED (ZONE 100) · airframe 128,058 hrs · 23,451 cycles

FLOOR SUPPORT BRACKET STA 544-566 RBL 38-37 IS CRACKED

Part: STRUCTURE — CORRODED (ZONE 100) · airframe 128,058 hrs · 23,451 cycles

FLC J CHORD STATION 566 RBL 26 IS CORRODED

Part: ROLLER TRAY — CRACKED (ZONE 100) · airframe 128,058 hrs · 23,451 cycles

FLC ROLLER TRAY 368-434 RBL20 CRACKED

Part: ROLLER TRAY — CRACKED (ZONE 100) · airframe 128,058 hrs · 23,451 cycles

ALC ROLLER TRAY STA 1197-1263 LBL21-LBL23 CRACK AT END OF TRAY

Part: ROLLER TRAY — CORRODED (ZONE 100) · corrosion level 2 · airframe 128,058 hrs · 23,451 cycles

ROLLER TRAY STA 1087-1197CORRODED RBL45-RBL43

Part: FITTING — DAMAGED (ZONE 100) · airframe 128,058 hrs · 23,451 cycles

FS 522 COMMON TO CORD & WEB IS DOUBLE DRILLED AND IS POTTED

Part: INTERCOSTAL — CORRODED (ZONE 100) · corrosion level 2 · airframe 128,058 hrs · 23,451 cycles

FOUND INTERCOSTAL T STA 544-549 RBL 37 CORRODED

Part: ROLLER TRAY — CORRODED (ZONE 100) · airframe 128,058 hrs · 23,451 cycles

ALC ROLLER TRAY ASSY. FOR STA. 1187 TO 1197+44 LBL-8 IS CORRODED ON LOWER SIDE OF TRAY.

Part: SKIN — CRACKED (ZONE 200) · airframe 128,058 hrs · 23,451 cycles

FUSELAGE SKIN AND BEAR STRAP IS CRACKED SINGLE FASTENER HOLE AT THE LOWER AFT CORNER OF THE R1 DOOR CUTOUT STA 335 JUST ABOVE S20R. (VERIFIED WITH HFEC HOLE SCAN)

Part: SKIN — CRACKED (ZONE 200) · airframe 128,058 hrs · 23,451 cycles

FUSELAGE SKIN AND BEAR STRAP IS CRACKED SINGLE FASTENER HOLE AT THE LOWER AFT CORNER OF THE R1 DOOR CUTOUT STA 335 JUST ABOVE S20R. (VERIFIED WITH HFEC HOLE SCAN)

Part: SKIN — DEBONDED (ZONE 300) · airframe 128,058 hrs · 23,451 cycles

VERTICAL STAB LEFT HAND SIDE LOWER BONDED PANEL REQUIRES COMPOSITE REPAIR

Part: SKIN — CRACKED (ZONE 200) · airframe 128,058 hrs · 23,451 cycles

AFT CORNOR OF L1 DOOR CUTOUT THE SKIN IS CRACKED AT THE LOWER FASTNER HOLE STA 335 JUST ABOVE FLOOR LEVEL (FOUND WITH HFEC OPEN HOLE SCAN)

Part: SHEAR WEB — CORRODED (ZONE 100) · airframe 128,058 hrs · 23,451 cycles

NUT PLATE HOLES CORR AT STA 1153 FWD SIDE CENTER AREA BY BILDGE SHEAR WEB

Part: ROLLER TRAY — CORRODED (ZONE 100) · corrosion level 2

ROLLER TRAY CORRODED

Part: INTERCOSTAL — CORRODED (ZONE 100) · airframe 128,058 hrs · 23,451 cycles

AT STA 1263 CORR ON INTERCOSTAL AT APPROX RBL36 BY CARGO DOOR CUT OUT TAG

Part: ANGLE — CRACKED (ZONE 200) · airframe 128,058 hrs · 23,451 cycles

CRACKED ANGLE AT O/B END OF FLOOR BEAM @STA 1562 80R

Part: WEB — DENTED (ZONE 100) · airframe 128,058 hrs · 23,451 cycles

ALC BILGE PNL STA 1329-1351, LBL6-LBL33 DENTED.

Part: SHEAR TIE — CORRODED (ZONE 100) · airframe 128,058 hrs · 23,451 cycles

CORROSION ON THE AFT AND FWD SIDES OF THE SHEAR-TIE, AT STA.1562, BETWEEN STR.38L AND STR.38R

Part: ANGLE — CRACKED (ZONE 200) · airframe 128,058 hrs · 23,451 cycles

CRACKED ANGLE O/B END OF FLOOR BEAM ON L/H FUSELAGE STA1562

Part: BRACKET — CRACKED (ZONE 100) · airframe 128,058 hrs · 23,451 cycles

ANGLE BRACKET CRACKED AT FLOOR BEAM STA1087 RBL 26

Part: BEAR STRAP — CORRODED (ZONE 100) · airframe 128,058 hrs · 23,451 cycles

CORROSION ON THE BEAR STRAP, FWD OF FRAME 1562, BETWEEN STR.39L AND STR.39R

Part: SUPPORT — CORRODED (ZONE 200) · airframe 128,058 hrs · 23,451 cycles

PDU SUPPORT 1241-1263 RBL 26 IS CORRODED

Part: SKIN — DENTED (ZONE 500 TE FLAP) · airframe 128,058 hrs · 23,451 cycles

LEFT WING TRAILING EDGE INBD AFT FLAP DENTED

Part: ACOUSTIC PANEL — DELAMINATED (ZONE 300) · airframe 128,058 hrs · 23,451 cycles

VERTICAL STAB LEFT UPPER BONDED PANEL REQUIRES REPAIR

Part: SKIN — CRACKED (ZONE 200) · airframe 128,058 hrs · 23,451 cycles

LOWER AFT CORNER OF R1 DOOR CUTOUT THE SKIN IS CRACKED @ 2 LOWER FASTENER HOLES

Part: SUPPORT BRACKET — CORRODED (ZONE 100) · airframe 128,058 hrs · 23,451 cycles

CORROSION ON THE UPPER SURFACE OF A SMALL SUPPORT BRACKET, JUST INSIDE THE THRESHOLD OF THE FLC DOOR CUTOUT, AT STA.504.

Part: SKIN — DENTED (ZONE 500) · airframe 128,058 hrs · 23,451 cycles

LEFT WING INBD AFT FLAP DENTS 16,17,18

Part: CARGO TRACK — CORRODED (ZONE 200) · airframe 128,058 hrs · 23,451 cycles

UPPER CARGO FLOOR PANEL 252P FOUND SEAT TRACK CORRODED AFT OF FS 1461 RBL 88.5.

Part: SEAT TRACK — CRACKED (ZONE 200) · airframe 128,058 hrs · 23,451 cycles

FO'S FWD OTBD SEAT TRACK IS CRACKED AT FWD STOP MOUNT HOLES. VERIFIED WITH HFEC

Part: SHEAR TIE — CORRODED (ZONE 200) · airframe 128,058 hrs · 23,451 cycles

FLC FLOOR BEAM AFT SHEAR TIE IS CORRODED AT FS 720, BL O

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 128,058 hrs · 23,451 cycles

CORROSION ON SHEAR-TIE STA1395,39L-39R

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 128,058 hrs · 23,451 cycles

FLC FLOOR PANEL SUPPORT ANGLE CORRODED STA 737 LBL 45

Part: SKIN — DENTED (ZONE 500 TE FLAP) · airframe 128,058 hrs · 23,451 cycles

LW AFT FLAP DENTED

Part: CAP — CRACKED (ZONE 500) · airframe 128,058 hrs · 23,451 cycles

# 1 END CAP CRACKED

Part: CAP — CORRODED (ZONE 200) · corrosion level 2 · airframe 128,058 hrs · 23,451 cycles

ALC FLOOR SUPPORT CAP UNDERSIDE CORRODED STA 1350 @ RBL-28

Part: KEELBEAM — CORRODED (ZONE 100) · airframe 128,058 hrs · 23,451 cycles

CENTER AREA OF KEEL BEAM FS1040 CORROSION UNDER NUT PLATE CROSS "T" EXCRUSION.

Part: BRACKET — CORRODED · airframe 128,058 hrs · 23,451 cycles

CORROSION ON THE BRACKET UNDER THE FWD END OF THE RIGHT BULK CARGO SLOPING SIDEWALL PANEL SUPPORT, LOCATED ON THE FWD SIDE OF FRAME 1417, RBL48.

Part: NUT PLATE — CORRODED (ZONE 200) · airframe 128,058 hrs · 23,451 cycles

CENTER SHEAR WEB PANEL NUTPLATE STRIP CORRODED TOP AND BOTTOM STA 1153

Part: SUPPORT — CORRODED · airframe 128,058 hrs · 23,451 cycles

ALC PDU 8R I/B SUPPORT BEAM EXFOLIATED AROUND FWD & AFT MOUNT BOLT NUT PLATES

Part: FLOOR PANEL — CORRODED (ZONE 200) · airframe 128,058 hrs · 23,451 cycles

CORROSION ON THE UPPER SURFACE OF THE SUBFLOOR, FROM STA.276 TO 340, LBL85, UNDER THE COMPSITE FLOOR PANEL LOCATED JUST INSIDE OF THE L1 DOOR

Part: SKIN — CHAFED (ZONE 400) · airframe 128,058 hrs · 23,451 cycles

#1 PYLON FWD NACELLE STRUT FAIRING UPPER SKIN IS CHAFED IN 4EA SPOTS LOCATED JUST AFT OF THE INLET AT THE 12:00 POSITION

Part: SKIN — DELAMINATED (ZONE 500) · corrosion level 2 · airframe 128,058 hrs · 23,451 cycles

LW OUTBD FLAP UPPER SURFACE AREA OF DELAMINATION.

Part: SKIN — CHAFED (ZONE 400) · airframe 128,058 hrs · 23,451 cycles

SEVERAL CHAFFE MARKS IN THE UPPER SURFACE OF THE PANEL, ON TOP OF THE RIGHT PYLON, WHERE THE FWD FAIRING 441AT (DOGHOUSE PANEL)

Part: SUPPORT — CORRODED (ZONE 200) · airframe 128,058 hrs · 23,451 cycles

CORROSION ON THE UPPER AND LOWER SURFACES OF THE LOWER PANEL SUPPORT COMMON TO THE LEFT BULK CARGO SLOPING SIDEWALL

Part: FRAME — CORRODED (ZONE 200) · airframe 128,058 hrs · 23,451 cycles

ALC HAS SURFACE CORROSION AT STA. 1197+66 RBL-8.

Part: DOOR SILL — CORRODED (BULK CARGO) · airframe 128,058 hrs · 23,451 cycles

CORROSION ON THE LOWER SURFACE OF THE LOWER SILL, AT THE BULK CARGO DOOR FUSELAGE CUTOUT, UNDER THE AFT I/B NUTPLATE, AS VIEWED INSIDE OF THE FWD LIGHTENING, AT STA.1426.

Part: FLOOR SUPPORT — CORRODED (BULK CARGO) · airframe 128,058 hrs · 23,451 cycles

CORROSION UNDER 8 NUTPLATES, ON THE LOWER SURFACES OF THE 4 GREEN PANEL SUPPORT CHANNEL REPAIRS, FOR THE BULK CARGO FLOOR SUPPORTS, FROM STA.1415 TO STA.1422, AT LBL23, LBL16, LBL9, AND RBL9.

Part: ANGLE — CORRODED (ZONE 100) · airframe 128,058 hrs · 23,451 cycles

UNDERSIDE OF FLC FLOOR SUPPORT LONGITUDINAL ANGLE IS CORRODED AROUND FWD ATTACH HI-LOK, LOCATED AT LFS 654+121, LBL 21

Part: SUPPORT ANGLE — CORRODED (ZONE 100) · corrosion level 2 · airframe 128,058 hrs · 23,451 cycles

ALC FLOORBOARD SUPPORT ANGLE CORRODED1263 I/B OF PDU 7L

Part: SKIN — CHAFED (NR 1 NACELLE) · airframe 128,058 hrs · 23,451 cycles

#1 PYLON FWD NACELLE STRUT FAIRING UPPER SKIN IS CHAFFED IN 4EA SPOTS LOCATED JUST AFT OF THE INLET AT THE 12:00 POSITION

Part: INTERCOSTAL — CORRODED (ZONE 100) · corrosion level 2 · airframe 128,058 hrs · 23,451 cycles

INTERCOASTAL STA 588-610 RBL33 CORRODED

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 126,606 hrs · 22,916 cycles

ON FINAL APPROACH AURAL WARNING "TO LOW GEAR" WITH GEAR HANDLE DOWN AND THREE GREEN LIGHTS. KILN AIR TRAFFIC CONTROL TOWER CONFIRMED THE GEAR WAS EXTENDED. CREW CONFERENCED MAINTENANCE OPERATIONS CONTROL, CPO AND MADE THE DECISION TO SHOOT THE APPROACH AND LAND INTO KILN. AN EMERGENCY DESCENT WAS DECLARED AND AIR RESCUE AND FIRE FIGHTING SUPPORT (ARFF) REQUESTED. LANDING WAS WITHOUT INCIDENT AND NO PRECAUTIONARY ARFF NTERVENTIONS. ON ARRIVAL, AIRCRAFT WAS GROUNDED FOR MAINTENANCE. UPON INSPECTION, LINE MAINTENANCE ISOLATED FAULT TO S4 MICROSWITCH IN THE LANDING GEAR LEVER MODULE INTERMITTENTLY STICKING IN THE GEAR UP POSITION WITH GEAR LEVER DOWN. IAW B767 AMM 32-31-01 AND WDM 32-61-14, REMOVED AND REPLACED GEAR LEVER MODULE ASSEMBLY. SYSTEM OPERATIONAL CHECK GOOD. NO ADDITIONAL FAULTS NOTED. AIRCRAFT RELEASED TO SERVICE.

Part: SKIN — DENTED (ZONE 500 TE FLAP) · airframe 128,058 hrs · 23,451 cycles

LEFT WING TRAILING EDGE INBD AFT FLAP DENTED

Part: WEB — CORRODED (ZONE 100) · corrosion level 2

ALC BILGE PANEL @ STA 1153-1175 RBL10-LBL10 CORRODED

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2

ALC FLOOR BEAM UPPER CORD CORRODED ON UNDERSIDE @ STA 1197+22

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 128,058 hrs · 23,451 cycles

ALC FLOORBEAM UPPER CORD AT STA 1175, STRINGER 38R-39R AND 37L-38L

Part: RACK — CRACKED (ZONE 100) · airframe 124,341 hrs · 22,069 cycles

FOUND CRACKS ON E5 INTAKE/EXHAUST PLENUMS

Part: CHANNEL — CORRODED (ZONE 300) · corrosion level 2 · airframe 124,341 hrs · 22,069 cycles

L/H HORZ STAB TIP FOUND AFT O/B "C" CHANNEL TO BE CRACKED WITH PIECES MISSING, AND AFT O/B UPPER AND LWR NUT PLATE CHANNEL CORRODED 100% MATERIAL LOSS

Part: SKIN — DELAMINATED (RT NR 11 SLAT) · airframe 124,341 hrs · 22,069 cycles

# 11 SLAT HAS DELAM ON UPPER WEDGE. TAP TEST BAD.

Part: STRINGER CLIP — CRACKED (ZONE 200) · airframe 124,341 hrs · 22,069 cycles

STRINGER CLIP CRACKED

Part: FLOOR PANEL — CRACKED (ZONE 100) · airframe 124,341 hrs · 22,069 cycles

BILGE FLOOR PANEL CRACKED

Part: SKIN — DELAMINATED (LT NR 4 SLAT) · airframe 124,341 hrs · 22,069 cycles

#4 SLAT DELAMINATED

Part: ACCESS DOOR — CRACKED (ZONE 400) · airframe 124,341 hrs · 22,069 cycles

#2 PYLON OB HYDRAULIC BAY DOOR

Part: RETAINER — CORRODED (NLG DOOR SEAL) · corrosion level 2 · airframe 124,341 hrs · 22,069 cycles

NLG DOOR SEAL RETAINER IS CORRODED

Part: PANEL — CRACKED (ZONE 400) · airframe 124,341 hrs · 22,069 cycles

PYLON SKIN PANEL CRACKED

Part: FLOOR MAT — CRACKED (ZONE 100) · airframe 124,341 hrs · 22,069 cycles

FLC LEFT AFT BALL MAT HAS CRACKED AND RAISED SKIN

Part: SKIN — CRACKED (BS 1809 S12R) · airframe 124,341 hrs · 22,069 cycles

AFT EXTERIOR FUSELAGE SKIN STA 1809 STRINGER 12R IS CRACKED (FOUND WHILE PERFORMING AREA 1 INSPECTION CRACK VERIFIED USING HFEC SURFACE SCAN)

Part: NONE — NONE (ZONE 500) · airframe 124,341 hrs · 22,069 cycles

LW OB FLAP LEADING EDGE BULLNOSE DAMAGED

Part: PANEL — DELAMINATED (VERTICAL STAB) · airframe 124,341 hrs · 22,069 cycles

VERT STAB LH UPPER FWD BONDED PANEL DELAMINATED

Part: PANEL — DELAMINATED (VERTICAL STAB) · airframe 124,341 hrs · 22,069 cycles

VERT STAB LH LOWER FWD BONDED PANEL DELAMINATED

Part: SKIN — CORRODED (ZONE 500) · corrosion level 2 · airframe 124,341 hrs · 22,069 cycles

#2 SLAT OUTBOARD INTERSTITIAL DUCT PANEL HAS AREAS OF BUBBLING POSSIBLE CORROSION

Part: DUCT — CHAFED (ZONE 100) · corrosion level 2 · airframe 123,277 hrs · 23,601 cycles

#1 PYLON ANTI ICE DUCT CHAFED

Part: RUB STRIP — CRACKED (ZONE 400) · airframe 123,277 hrs · 21,694 cycles

REPAIR - CHAFE STRIP BEHIND ENGINE MOUNT ACCESS PANEL 436AL BROKEN OFF NAC 203-NAC 203

Part: NONE — CRACKED (ZONE 400) · airframe 123,277 hrs · 21,694 cycles

O/B UPPER ATTACH FITTING AFT OF PNL 446AR IS CRACKED

Part: NONE — CORRODED (ZONE 400) · corrosion level 2 · airframe 123,277 hrs · 21,694 cycles

#1 PYLON UPPER LINK UPPER BUSHING IS PITTED

Part: NONE — CORRODED (ZONE 400) · corrosion level 2 · airframe 123,277 hrs · 21,694 cycles

#2 PYLON UPPER LINK UPPER BUSHING IS PITTED

Part: BUSHING — CORRODED (ZONE 400) · corrosion level 2 · airframe 123,277 hrs · 21,694 cycles

#1 PYLON O/B SIDE LINK UPPER FWD BUSHING IS PITTED

Part: FRAME — CRACKED (ZONE 400) · airframe 123,277 hrs · 21,694 cycles

#2 PYLON INTERNAL FRAME IS CRACKED @ UPPER I/B FASTENER HOLE ON O/B SIDE OF PYLON AFT OF PNL 446AR

Part: FITTING — WORN (ZONE 400) · airframe 123,277 hrs · 21,694 cycles

NO.2 PYLON O/B T/R OPENING ACTUATOR, UPPER PYLON BRACKET DAMAGED AT ATTACH BUSHING

Part: STIFFENER — CRACKED (ZONE 400) · airframe 123,277 hrs · 21,694 cycles

BRACKET JUST UNDER FWD END OF HYD BAY DOOR SILL BEAM FOUND CRACKED

Part: FRAME — CRACKED (ZONE 400) · airframe 123,277 hrs · 21,694 cycles

O/B FRAME JUST AFT OF PNL 436AL DAMAGED, NAC 285.45 TO NAC 285.45

Part: NONE — CRACKED (ZONE 400) · airframe 123,277 hrs · 21,694 cycles

I/B UPPER ATTACH FITTING AFT OF PNL446AL CRACKED

Part: NONE — CRACKED (ZONE 400) · airframe 123,277 hrs · 21,694 cycles

O/B UPPER ATTACH ANGLE ABOVE DAMAGED FRAME AFT OF PNL 436AL CRACKED NAC 200

Part: STIFFENER — CRACKED (ZONE 200) · airframe 123,277 hrs · 21,694 cycles

O/B T-FITTING TOP FLANGE MISSING/DAMAGED JUST AFT OF PNL 436AL NAC 278 - NAC 288

Part: NONE — CRACKED (ZONE 400) · airframe 123,277 hrs · 21,694 cycles

I/B UPPER ATTACH FITTING AFT OF PNL 436AL DAMAGED NAC 200

Part: IDG — MALFUNCTIONED (RT ENGINE) · airframe 112,303 hrs · 18,303 cycles

CREW CALLED IN, IAW QUICK REACTION HANDBOOK, DIVERTED DUE TO A RIGHT AC BUSS FAILURE EICAS MESSAGE INDICATION, APU FAILED IN FLIGHT TO START. EMERGENCY DECLARED. LANDED WITH NO FURTHER ISSUES NOTED. THE AIRCRAFT WAS GROUNDED. TROUBLESHOT TO FAULTY RIGHT ENGINE IDG WHICH WILL NOT MAINTAIN CORRECT DC/AC POWER. REMOVED AND REPLACED THE RT BUSS POWER UNIT, AND IDG . OPS CHECKED SATISFACTORY. ACFT RELEASED TO SERVICE.

Part: COVER — MISLOCATED (RT ENGINE) · airframe 111,548 hrs · 18,066 cycles

CLIMBING THROUGH FL210 FOR FL230 YELLOW CAUTION AROUND RIGHT ENGINE OIL PRESSURE. QTY INDICATION WAS ZERO,BUT TEMPS WAS GOOD. REQUESTED TO ATC LEVEL OFF AT FL220. EICAS MESSAGE DISPLAYED RIGHT ENGINE OIL PRESSURE. RAN THROUGH CHECKLIST. RIGHT ENGINE SHUTDOWN AS INSTRUCTED IN CHECKLIST WITH AN EMERGENCY DECLARATION FOR DIRECT KILN. ATC DIRECTED KILN AND A DESCENT TO 11000. AIR TURN BACK TO KILN WITH ONLY LEFT ENGINE IN OPERATION. TAXI TO RUNWAY WITH NO EMERGENCY EQUIPMENT REQUIRED. AIRCRAFT GROUNDED FOR CORRECTIVE ACTION. UPON INSPECTION OF RIGHT ENGINE, MECHANIC OBSERVED GEAR BOX DRIVE PLATE NOT INSTALLED. PERFORMED WINDMILL INSPECTION IAW B767 AMM 72-00-00. NO DEFECTS NOTED. RIGHT ENGINE OIL WAS SERVICED AND GEARBOX DRIVE ADAPTER PLATE INSTALLED. INSPECTION AND LEAK CHECK IAW B767 AMM 72-00-00 SATISFACTORY. NO FURTHER DEFECTS NOTED. AIRCRAFT WAS RELEASED TO SERVICE.