N695GT

ATA 5551

Part: ATTACH FITTING — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 60,948 hrs · 43,501 cycles

LEFT HORIZ STAB. UPPER CHORD ATTACH FITTING UNDER PANEL 335AT HAS CORROSION UNDER NUT PLATES & ALSO CORRODED NUT PLATES.CORROSION BENEATH 335AT FOUND TO BE OUT OF LIMITS. REMOVED , FABRICATED & REPLACED CORRODED CHORD ( PN 182T7103-77) IAW BOEING DWG 182T7103

ATA 5510

Part: FLANGE — CORRODED · corrosion level 2 · airframe 60,948 hrs · 43,501 cycles

FLANGE UNDER PANEL 335AT HAS CORROSION ON UPPER SURFACE.REMOVED CORROSION IAW B767-200 55-10-09 ALLOWABLE DAMAGE FOUND TO BE OUT OF LIMITS OT ".090 R.T .077

ATA 5330

Part: SKIN — CRACKED (BS 1654.5) · airframe 60,948 hrs · 43,501 cycles

UPPER L/H FUSELAGE STA 1654.5 BETWEEN STRINGERS 4L-5L EXTERNAL SKIN IS CRACKED.REPAIRED L/H FUSELAGE SKIN STA: 1654.5 I.A.W. B767 SRM 53-80-01-2R-4 REPAIR 4.

ATA 5740

Part: ATTACH FITTING — CORRODED (WING) · corrosion level 2 · airframe 60,948 hrs · 43,501 cycles

UPPER TRAILING EDGE PANEL ATTACH CHORD AT WS.434 22 INCHES AFT OF REAR SPAR HAS CORROSION AROUND NUTPLATE. BLENDED CORROSION ON UPPER CORD ON AILERON RIB AT WS 434 TO A DEPTH OF 0.17", MAX DEPTH ALLOWED .008" IAW B767 SRM 57-51-02-1A-1 DETAIL 19. OUT OF LIMITS. MECHANICALLY MEASURED TAG# 2932. INSTALLED NEW UPPER CHORD ON AILERON RIB AT WS 434 IAW B767SRM 51-40-02 PAR 4 AND 7 BOEING DWG 113T1510

ATA 5711

Part: SPAR — CORRODED (LT WING) · corrosion level 2 · airframe 60,948 hrs · 43,501 cycles

FRONT SPAR UPPER CORD CORRODED AROUND RIVET .013" MATERIAL REMOVED , FOUND TO OUT OF LIMITS. REPAIRED PER AMES ENGINEERING DOCUMENT REA 47396REA01.

ATA 5710

Part: SPLICE PLATE — CORRODED (LT WING) · corrosion level 2 · airframe 60,948 hrs · 43,501 cycles

CORROSION AROUND GROUNDING JACK ON FRONT SPAR UPPER CHORD AFT OF NUMBER 3 SLAT OUTBOARD DRIVE ROD ACTUATOR.COMPLETED REPAIR IAW REA: 47396REA05 AND 47396REA06 SEE BACK AND PARTIAL WS 27 PGS 1 AND 2 FOR PARTIAL WORK ACCOMPLISHED. COMPLETED HOLE SCAN ON SPLICE PLATE L/W UPPER LES 745-807. DEFECT FOUND IN SPLICE PLATE ONLY. REMOVED AND REPLACED SPLICE PLATE L/W LES 745-807 IAW REA 47396REA05 & 47396REA06.

ATA 5314

Part: WEB — CORRODED (BS 1002 KEEL) · corrosion level 2 · airframe 60,948 hrs · 43,501 cycles

LWW - CORROSION ON KEEL WEB AT STA.1002 LBL 5. BLENDED CORROSION IAW B767 SRM 53-50-12-1A REPAIRED IAW ENGINEERING DOCUMENT 47396REA04 DUE TO BLEND BEING OUT OF LIMITS

ATA 5340

Part: ATTACH BRACKET — CRACKED (BS 492) · airframe 60,948 hrs · 43,501 cycles

ATTACHED BRACKET BEHIND AFT LOWER CORNER SEAL DEPRESSOR IS CRACKED ON UPPER CARGO DOOR. REMOVED AND REPLACED CORNER SEAL DEPRESSOR IAW B767 SRM 51-40-0

ATA 5340

Part: ATTACH BRACKET — CRACKED (BS 475-500) · airframe 60,948 hrs · 43,501 cycles

ATTACHED BRACKET BEHIND FWD LOWER CORNER SEAL DEPRESSOR IS CRACKED ON UPPER CARGO DOOR. REMOVED AND REPLACED CORNER SEAL DEPRESSOR IAW B767 SRM 51-40-0

ATA 5530

Part: ANGLE — CRACKED (VERITCAL STAB) · airframe 60,948 hrs · 43,501 cycles

CLOSE OUT ANGLE UNDER RUDDER HAS CRACK AT LEFT END OF ANGLE

ATA 5511

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 60,948 hrs · 43,501 cycles

LEFT HORIZONTAL STAB LEADING EDGE INBD RIB IS CRACKED

ATA 5314

Part: ANGLE — CORRODED (BS 997-999) · corrosion level 2 · airframe 60,948 hrs · 43,501 cycles

LWW - CORROSION ON ANGLE THAT ATTACHES FRAME AT STA.997 TO KEEL WEB.BLENDED CORROSION IAW B767 SRM 53-50-12 FIG 1001 DETAIL II FOUND TO BE OUT OF LIMITS COMPLIED WITH ENGINEERING DOCUMENT #47396REA07

ATA 5314

Part: WEB — CORRODED (BS 978 KEEL) · corrosion level 2 · airframe 60,948 hrs · 43,501 cycles

LWW - SMALL AREA OF CORROSION ON KEEL WEB AT STA.978 LBL 4. BLENDED CORROSION IAW B767 SRM 53-50-12 FIG DETAIL II FOUND TO BE OUT OF LLIMITS COMPLIED WITH ENGINEERING DOCUMENT #47396REA07