N659GT

Part: SKIN PANEL — DELAMINATED (VERTICAL STAB) · airframe 61,764 hrs · 44,180 cycles

RIGHT SIDE VERTICAL STAB SKIN DELAMINATED. REMOVED AND REPAIRED SKIN PANEL AND INSTALLED STAB SKIN WITH INTERIM FASTENERS.

Part: KEELBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,947 hrs · 43,501 cycles

LLW - CORROSION ON KEEL WEB AT STA 1002 LBL 5.&NBSP;(<P><SPAN>BLENDED CORROSION IAW B767 SRM 53-50-12-1A, REPAIRED IAW ENGINEERING DOCUMENT 47396REA04 DUE TO BLEND BEING OUT OF LIMITS.</SPAN><BR /></P>)

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 60,947 hrs · 43,501 cycles

L HORIZONTAL LEADING EDGE INBD END RIB IS CRACKED.(<P>CUT OUT DAMAGE AND REPAIRED IAW B767 SRM 55-10-09 REPAIR 1.</P>)

Part: ATTACH BRACKET — CRACKED (FUSELAGE) · airframe 60,947 hrs · 43,501 cycles

ATTACH BRACKET BEHIND FWD LOWER CORNER SEAL DEPRESSOR IS CRACKED.(<P>REMOVED AND REPLACED ATTACH BRACKET BEHIND FWD LOWER CORNER SEAL DEPRESSOR IAW B767 SRM 51-40-02.</P>)

Part: STRUCTURE — CORRODED (HORIZ STAB) · corrosion level 2 · airframe 60,947 hrs · 43,501 cycles

FLANGE UNDER PANEL 335AT HAS CORROSION ON UPPER SURFACE.(<P>REMOVED CORROSION IAW B767 SRM 55-10-09. FOUND TO BE OUT OF LIMITS OT .090" R.T .077. INSTALLED UPPER CHORD IAW B767 SRM 51-40-02.</P>)

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,947 hrs · 43,501 cycles

UPPER L/H FUSELAGE STA 1654.5 BETWEEN STRINGERS 4L-5L EXTERNAL SKIN IS CRACKED.(<P>REPAIRED L/H FUSELAGE SKIN AT STA 1654.5 IAW B767 SRM 53-80-01-2R-4 REPAIR 4.</P>)

Part: ANGLE — CRACKED (RUDDER) · airframe 60,947 hrs · 43,501 cycles

CLOSE OUT ANGLE UNDER RUDDER HAS CRACK AT LEFT END OF ANGLE.(<P>REMOVED AND REPLACED CRACKED CLOSE OUT ANGLE UNDER RUDDER IAW BOEING DOCUMENT #173T1215 AND B767-200 SRM 51-40-02.</P>)

Part: RIB — CORRODED (AILERON) · corrosion level 2 · airframe 60,947 hrs · 43,501 cycles

UPPER TRAILING EDGE PANEL ATTACH CHORD AT WS 434, 22 INCHES AFT OF REAR SPAR HAS CORROSION AROUND NUTPLATE.(<P>BLENDED CORROSION ON UPPER CHORD ON AILERON RIB AT WS 434 TO DEPTH OF .017", MAX DEPTH ALLOWED.008" IAW B767 SRM 57-51-02-1A-1 DETAIL 19. OUT OF LIMITS.&NBSP;INSTALLED NEW AILERON UPPER CHORD RIB IAW B767 SRM 51-40-02 AND BOEING DWG 113T1510.</P>)

Part: ATTACH BRACKET — CRACKED (FUSELAGE) · airframe 60,947 hrs · 43,501 cycles

ATTACHED BRACKET BEHIND AFT LOWER CORNER SEAL DEPRESSOR IS CRACKED ON UPPER CARGO DOOR.(<P>REMOVED AND REPLACED CORNER SEAL DEPRESSOR IAW B767 SRM 51-40-02.</P>)

Part: STRUCTURE — CORRODED (LT HORIZ STAB) · corrosion level 2 · airframe 60,947 hrs · 43,501 cycles

L HORIZ STAB UPPER CHORD ATTACH FITTING UNDER PANEL 335AT HAS CORROSION UNDER NUT PLATES, AND ALSO CORRODED NUT PLATES.&NBSP;(<P><SPAN>CORROSION BENEATH 335AT FOUND TO BE OUT OF LIMITS. REMOVED, FABRICATED, AND REPLACED CORRODED CHORD IAW BOEING DWG 182T7103.</SPAN></P>)

Part: SPAR — CORRODED (WING) · corrosion level 2 · airframe 60,947 hrs · 43,501 cycles

CORROSION AROUND RIVET ON FRONT SPAR UPPER CHORD AT LES 730.(<P>BLENDED CORROSION. 0.013" MATERIAL REMOVED. BEYOND LIMITS. REPAIRED IAW AMES DOCUMENT 47396REA01.</P>)

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,947 hrs · 43,501 cycles

CORROSION ON ANGLE THAT ATTACHES FRAME AT STR 997 TO KEEL WEB.(<P>BLENDED CORROSION IAW B767 SRM 53-50-12 FIG 1001 DETAIL&NBSP; II. FOUND TO BE OUT OF LIMITS, COMPLIED WITH ENGINEERING DOC #47396REA07.</P>)

Part: SPLICE PLATE — CORRODED (LT WING) · corrosion level 2 · airframe 60,947 hrs · 43,501 cycles

CORROSION AROUND GROUNDING JACK ON FRONT SPAR UPPER CHORD AFT OF NUMBER 3 SLAT OUTBOARD DRIVE ROD ACTUATOR.(<P>COMPLETED REPAIR IAW REA: 47396REA05 AND 47396REA06. REMOVED AND REPLACED SLICE PLATE L/W LES 745-807 IAW REA 47396REA05 &AMP; 47396REA06.&NBSP;</P>)

Part: ESCAPE REEL — UNWANTED DEPLOY · airframe 60,896 hrs · 43,467 cycles

4 EACH GALLEY DESCENT DEVICES DEPLOYED; 3 EACH AVAILABLE.(<P>TRANSFERRED TO DMI 122134 IAW MEL 25-61-01-01, CAT 'C'.</P><P>LP 1084472 - M5: REMOVED AND REPLACED 4 EACH EMERGENCY DESCENT DEVICES IAW AMM 25-61-03. NO DISCREPANCIES NOTED AT THIS TIME.&NBSP;THIS CLEARS DMI 122134, PLACARDS REMOVED.</P>)

Part: ESCAPE REEL — UNWANTED DEPLOY (GALLEY) · airframe 60,894 hrs · 43,465 cycles

4EA GALLEY DESCENT DEVICES DEPLOY; 3EA AVAILABLE.(<P>TRANSFERRED TO MDDR 122134 IAW MEL 25-61-01-01, CAT 'C'.</P>)

Part: CONTROL PANEL — SMOKE (COCKPIT) · airframe 60,053 hrs · 43,014 cycles

AIR TURN BACK ELECTRICAL SMELL MCP STOPPED WORKING(<P>REPLACED MCP PER AMM 22-11-02. INSTALLATION CHECKS GOOD' OPS CHECKS GOOD IAW 22-00-00. A/C STILL REMAINS CAT 3 B<BR /></P>)

Part: SWITCH — FAULTY (NLG) · airframe 59,630 hrs · 42,801 cycles

RED "CONFIG" LIGHT ILLUMINATED IN FLIGHT ACCOMPANIED BY EICAS "FLAPS" WARNING. WARNING SIREN. UNABLE TO CANCEL. PERFORMED FIM 31-51 FT 808 PER BLOCK 3 PSEU BITE FAULTS S266 NOSE GEAR NOT COMPRESSED SWITCH. R&R S266 IAW AMM 32-09-08, ADJUSTMENT AND OPS CHECKS OK. R&R PSEU IAW AMM 32-09-04 P/N OFF: 8-468-02, S/N OFF: 162.

Part: TERMINAL — ARCED (WINDOW HEAT) · airframe 58,331 hrs · 42,157 cycles

VERY STRONG ODOR OF ELECTRICAL FUMES AFTER TAKEOFF, TURNED OFF RIGHT FORWARD WINDOW HEAT , ODOR DISSIPATED IMMEDIATELY. FOUND THE LOWER RIGHT TERMINAL LOOSE AND ARCING, CLEANED THE TERMINAL AND REINSTALLED. OPS CHECKED GOOD IAW AMM 56-11-00.

Part: ENGINE — ODOR (NR 2) · airframe 58,280 hrs · 42,130 cycles

STRONG ELECTRICAL ODOR DETECTED WHIILE CLIMBING THROUGH FL 320 AND UNTIL A RETURN LANDING, THE ODOR DISSIPATED AT 4000 FT, NO SMOKE OR OTHER ABNORMALLY OBSERVED. REMOVED AND REPLACED THE NR 2 ENGINE IAW 71-00-00, PERFORMED REQUIRED TEST 1, 3, 4, 7, AND 12. OPS NORMAL.

Part: STRUCTURE — CRACKED (BS 859) · airframe 57,659 hrs · 41,748 cycles

BS 859.5, LBL 89, BELOW WL 200 STRUCTURE BETWEEN BOTTOM TWO FASTENERS CRACKED. REPAIRED IAW BULLETIN 76753A0209, REV 2, FIGURE 7.

Part: SKIN — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 57,659 hrs · 41,748 cycles

FORWARD CARGO DOOR, INTERIOR SIDE, 82 INCHES FROM LEADING EDGE AT LOWER DOOR FRAME WEB GAS SURFACE CORRODED. REMOVED AND REPLACED THE FWD CARDO DOOR LOWER SKIN PANEL IAW SRM 51-40-02-0G-0, AND DWG 140T2340, SHEET 2, REV.

Part: FLOOR PANEL — GOUGED (MAIN CARGO) · airframe 57,569 hrs · 41,748 cycles

MAIN CARGO DECK FLOOR PANEL 2420 IS GOUGE ON TOP. REPAIRED THE FLOOR PANEL IAW EA 170084, REV A, AND EO 6753A414.

Part: SKIN — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 57,569 hrs · 41,748 cycles

FWD CARGO DOOR INSIDE UPPER AREA CORRODED, APPROXIMATELY 24 INCHES FROM AFT EDGE. REMOVED AND REPLACED FWD CARGO DOOR SKIN IAW SRM 51-40-02-0G-0, AND DRAWING 140T2640, SHEET 2, REV.

Part: KEELBEAM — CORRODED (BS 990-1015) · corrosion level 2 · airframe 57,569 hrs · 41,748 cycles

LEFT KEEL BEAM CORRODED ON LOWER SURFACE OF INBOARD LOWER FLANGE, BS 990 - 1015, LBL 10. REPAIRED THE KEEL BEAM IAW EA 170090, REV IR, AND EO 6753A408.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 56,733 hrs · 41,287 cycles

L1 DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. RELAMPED L1 DOOR EXTERIOR EMERGENCY LIGHT. OPS OK IAW AMM 33-51-00.

Part: ESCAPE ROPE — DAMAGED (MAIN DECK) · airframe 56,279 hrs · 41,059 cycles

MAIN DECK FWD CARGO, DESCENT DEVICE F UNRAVELED, PN 379103D-29. R & R MAIN DECK DESCENT DEVICE F IAW AMM 25-61-00.

Part: SUPPORT — CORRODED (TE FLAP) · airframe 55,712 hrs · 40,763 cycles

LEFT WING NR 1 FLAP SUPPORT 1, 2 & 3 BEAM, OTBD STUD HOLE HAS CORROSION. REAMED HOLE & COMPLIED WITH REA 47172 REA07 REV IR.

Part: RIB — DAMAGED (TE FLAP) · airframe 55,712 hrs · 40,763 cycles

NUMBER 1 FLAP SUPPORT OUTER RIB HAS 5 HOLES THAT SHOW DEFECTS. REPAIRED DEFECTIVE HOLES IN THE NR 1 FLAP SUPPORT OUTER RIB IAW REA 4717REA11.

Part: PANEL — CORRODED (TE FLAP) · airframe 55,712 hrs · 40,763 cycles

LEFT WING OTBD FLAP, LOWER STRESS PANEL LE CORRODED, REPLACED FLAP.

Part: STRUCTURE — CORRODED (HORIZ STAB) · corrosion level 2 · airframe 55,712 hrs · 40,763 cycles

CORROSION STAB CTR BOX INTERIOR, UPPER STRUCTURE NR 11, FWD VERTICAL LEG. BLENDED AREA, FOUND TO BE OUT OF LIMITS. REPAIRED IAW SRM 55-10-03 & FIG 201 DETAIL 1 REPAIR 1.

Part: SKIN — CORRODED (RT WING) · airframe 55,712 hrs · 40,763 cycles

RIGHT WING UPPER SKIN IS CORRODED AROUND THE OVERWING FILL PORT ADAPTER. REMOVED CORROSION IAW SRM 57-20-01. FOUND TO BE OUT OF LIMITS. REPAIRED AREA IAW REA 47172 REA 10 REV IR.

Part: SKIN PANEL — CORRODED (LT WING) · airframe 55,712 hrs · 40,763 cycles

LEFT WING UPPER SKIN CORRODED AROUND OVERWING FILL PART ADAPTER. REPAIRED IAW DOC 47172REA12 REV 1R & REA 47172REA08 REV 1R.

Part: SUPPORT — CORRODED (TE FLAP) · airframe 55,712 hrs · 40,763 cycles

LEFT WING NR 1 FLAP SUPPORT 1, 2 & 3 BEAM INBD HANGER LOCATION, AFT UPPER HOLE HAS CORROSION. REAMED HOLE & COMPLIED WITH REA 47172REA01 REV IR.

Part: RIB — DAMAGED (TE FLAP) · airframe 55,712 hrs · 40,763 cycles

LEFT WING NR 2 FLAP SUPPORT, NR 3 HOLE HAS HFEC DEFECT INDICATION. REAMED NR 2 FLAP SUPPORT, NR 3 & 4 HOLES IAW REA 47172REA09.

Part: RIB — DAMAGED (TE FLAP) · airframe 55,712 hrs · 40,763 cycles

NUMBER 8 FLAP SUPPORT, OTBD RIB NR 2 HOLE OF THE ROTARY ACTUATOR MOUNT, HAS A HFEC INDICATION. REPAIRED DEFECTIVE HOLE IN THE NR 8 FLAP SUPPORT OTBD RIB IAW REA 47172REA11.

Part: SPAR — CORRODED (RT WING) · corrosion level 2 · airframe 55,054 hrs · 40,375 cycles

CORROSION ON RT WING AFT SPAR AT WS 920. REPAIRED RT WING TE IAW REA 47142REA01. SEE REA NR 547810000 0151 & PARTIAL WORK SHEET NR 3, IN WORK ORDER 9607 FOR WORK PERFORMED.