N653GT

Part: FUSE — FAILED (EMERGENCY LIGHTS) · airframe 82,643 hrs · 24,507 cycles

CREW ENTRY DOOR EMERGENCY LIGHT INOP (NO VOLTAGE AT FIXTURE)(<P ><SPAN>FOUND ON THE BATTERY POWER / SUPPLY FUSE #2 WAS LOOSE, REINSTALLED FUSE IAW B767 SWPM 20-84-18. OPS CHECK / GOOD IAW B767 AMM 33-51-00.</SPAN></P>)

Part: TERMINAL BLOCK — ARCED (WINDOW) · airframe 82,130 hrs · 24,176 cycles

AT 15000 IN A CLIMB, THE CREW NOTICED AN ACRID/NOXIOUS FUME IN THE COCKPIT. THE CREW RETURNED TO IAH ON OXYGEN AND RAN "THE SMOKE FIRE OR FUMES" QRH CHECKLIST. ON RUNWAY EXIT, THE EVACUATION CHECKLIST WAS RUN. LANDING WEIGHT 243,000 LBS, BELOW 272,000 LBS MLW.(<P>THROUGH T/S FOUND WINDOW TERMINAL BLOCK ARCHED ON LOWER LEFT CORNER OF CAPT WINDOW. REMOVED AND REPLACED CAPT NUMBER 1 WINDOW PER B767-200 AMM 56-11-01. CHECKED GOOD, NO DEFECTS NOTED, OK FOR SERVICE.</P>)

Part: UNKNOWN — ODOR (COCKPIT) · airframe 82,130 hrs · 24,176 cycles

APPROX 10-15 MIN AFTER TAKEOFF IN CLIMB AT FL340, CAPT AND F/O NOTED AN ACRID SMELL IN THE COCKPIT. "SMOKE, FIRE OR FUMES" QRH RUN ON GROUND, EVACUATION CHECKLIST RUN.(<P>PERFORMED INSPECTION IAW AMM 05-51-56/201 AND 21-00-21. COULD NOT DUPLICATE SMELL. PERFORMED ENG RUNS W/PRESSURIZATION, CHECKED ALL C/B PANELS, BTBS, BAT CHARGERS, WINDOW HEAT, COCKPIT LRU MODULES, AND GCU'S. NO SMELL NOTED, CANNOT DUPLICATE. AIRCREW WAS AT A/C DURING ALL T/S. SUSPECTED HAZMAT IN CONTAINERIZED CARGO. </P><P>LP 1177154 ITEM M3: CARGO ON BOARD ALL REQUIRED AIRWORTHINESS VERIFICATION, DHL INSPECTED CARGO, OK FOR SVC.</P><P>LP 1177155, ITEM M6: C/W AP 16508 (WATER&NBSP;EXTRACTORS&NBSP;INSPECTION, NIL FINDINGS).</P><P>LP 1177156, ITEM M7: INSPECTED AND CLEANED HEPA FILTER PER AMM 21-58-30. M8: INSPECTED APU BLEED DUCT IN LEFT MAIN GEAR WHEEL, NO DEFECTS NOTED PER AMM 36-11-00. M9: INSPECTED FLT DECK TRIM AIR MODULE, NO DEFECT NOTED PER AMM 21-61-01.</P><P>LP 1177157, ITEM M10: INSPECTED BOTH SUPPLY AND EXHAUST E&AMP;E COOLING FANS, NO DEFECTS NOTED PER AMM 21-58-02. M11: PERFORMED HIGH POWER RUNS IAW AMM 71-00-00, PERFORMED CONTAMINATION REMOVAL IAW AMM 21-00-21-102-030. PERFORMED CABIN PRESSURIZATION IAW AMM 05-51-24, ENGINE SOURCE USED. NO ODOR/FUMES NOTED. NO DEFECTS NOTED. A/C OK FOR SVC.</P>)

Part: ESCAPE REEL — UNWANTED DEPLOY · airframe 81,880 hrs · 24,028 cycles

DESCENT DEVICE DEPLOYED IN CREW SERVICE AREA.(<P>TRANSFERRED TO MDDR 119657 PER MEL 25-61-01-01, CAT 'C', DUE DATE: 04-NOV-19.</P><P>LP 1083015 - M10:&NBSP;REMOVED AND REPLACED DESCENT DEVICE IAW MAINTENANCE MANUAL SUPPLEMENT 25-61-03. THIS CLEARS DMI #119657. MCC NOTIFIED AND PLACARDS REMOVED.&NBSP;</P>)

Part: STRINGER — CORRODED (FUSELAGE) · airframe 81,677 hrs · 23,907 cycles

BS 415 STR 33R CORRODED. (<P>REPAIRED STR 33R AT STA 405 - STA 434 IAW SRM 53-00-03-2R-2.</P>)

Part: SKIN — DENTED (FUSELAGE) · airframe 81,677 hrs · 23,907 cycles

LOWER EMPENNAGE SKIN HAS A DENT BS 1800 BETWEEN STR 36L - 37L. (<P>INSPECTED, EVALUATED, AND REPAIRED DENT AT STA 1805 36L - 37L IAW SRM 53-00-01, IAI EA CS-22572-007.</P>)

Part: PANEL — CORRODED (LT WING) · airframe 81,677 hrs · 23,907 cycles

LT WING UPPER TE PNL. FWD EDGE BULGING, JUST FWD OF I/B END OF O/B AILERON.&NBSP;(<P>REMOVED CORROSION, REPAIRED, AND RESTORED PROTECTIVE FINISHES AT LT WING UPPER SURFACE PANEL. FWD OF O/B AIL I/B SIDE ON TE SKIN IAW FAS EA 19023 REV. 1R.&NBSP;</P>)

Part: STRINGER — CRACKED (FUSELAGE) · airframe 81,677 hrs · 23,907 cycles

STA 438 STR 36R IS CRACKED. (<P>REPAIRED STRINGER AT STA 434-480 STR 36 IAW SRM 53-00-03-2R-2.</P>)

Part: SKIN — CORRODED (TE FLAP) · airframe 81,677 hrs · 23,907 cycles

RT WING IB MAIN FLAP UPPER SURFACE HAS AREA OF CORROSION 14 INCHES FROM I/B END. (<P>COMPLIED WITH EA 19025 REV. 1R, RT WING I/B MAIN FLAP, UPPER SURFACE I/B SIDE.&NBSP;</P>)

Part: WINDOW — FAILED (L1) · airframe 81,644 hrs · 23,888 cycles

L1 WINDOW DURING CLIMB OUT CRACKING AND SMOKING FROM OUTER BOTTOM CORNER TURNED OFF WINDOW HEAT(<P>INSPECTED L1 WINDOW FOR DAMAGE IAW 767 AMM 56-11-00 NOTED NONE. FOUND L1 WINDOW ELECT CONNECTOR TERMINAL LOOSE AT LWR LH CORNER CLEANED AND SECURED TERMINAL END AND REPLACED PROTECTIVE COVER PERFORMED M191 WINDOW HEAT CONTROLLER TEST IAW 767 AMM 30-41-01 NO FAULTS NOTED ACCOMPLISHED WINDOW HEAT GROUND TEST PER 767AMM 30-41-00-715 NO DEFECTS NOTED WINDOW PANE SHOWS NO EVIDENCE OF ARCING OR OVERHEAT CONDITION</P>)

Part: SHUTOFF VALVE — MALFUNCTIONED (BLEED AIR SYS) · airframe 80,907 hrs · 23,457 cycles

DURING CRUISE RECEIVED EICAS RT ENG, QRH FOLLOWED, MESSAGE WENT AWAY HIGH STAGE. FOLLOWED IMMEDIATELY BY LT ENG HIGH STAGE. PERFORMED FIM 36-10 FAULT TREE 978 BLOCK 48. REMOVED AND REPLACED LT ENG HPSOV. OPS CHECK GOOD.

Part: ENGINE — MALFUNCTIONED (LEFT) · airframe 80,881 hrs · 23,433 cycles

AFTER TAKEOFF RED N2 EXCEEDANCE LT ENG AND NON-RESPONSIVE. THRUST LEVER WITH ENG SPEED STILL INCREASING. PRECAUTIONARY ENG SHUTDOWN. REPLACED LT ENGINE PER AMM 71-00-00. LEAK CK AND OPS CKS GOOD.

Part: FAILSAFE — DAMAGED (BS 955) · airframe 80,581 hrs · 23,232 cycles

RIGHT FAIL SAFE STRAP FAILED AN OPEN HOLE INSPECTION. REPAIRED THE FAIL SAFE STRAP IAW SB 53-A0100, REV 3.

Part: SKIN — CRACKED (NR 1 PYLON) · airframe 80,581 hrs · 23,232 cycles

NR 1 PYLON AT PANEL 416BR LANDING CRACKED THROUGH FASTENER HOLE. REPAIRED IAW EA 180129IR.

Part: BULKHEAD — CORRODED (BS 765) · airframe 80,581 hrs · 23,232 cycles

FWD CARGO BULKHEAD INNER ANGLE HAS COROSSION AT BS 765, STRINGER 38R. REPAIRED IAW EA 180131 1R.

Part: STRUCTURE — CRACKED (BS 287) · airframe 80,581 hrs · 23,232 cycles

NOSE WHEEL WELL BS 287. RBL 25 HAD A CRACK INDICATION IAW EA 6753A027. REPAIRED IAW IAW SRM 51-70-12, FIG 1, AND DWG 14179920.

Part: ESCAPE ROPE — MISROUTED (MAIN DECK) · airframe 80,581 hrs · 23,232 cycles

MAIN DECK EGRESS UNIT CABLES DISCONNECTED AND KINKED. ON REMOVAL, THE CABLE WAS FOUND TO BE ROUTED INCORRECTLY. ROUTED CABLE AND INSTALLED THE EGRESS UNIT. NO DEFECTS NOTED. IAW AMM 25-61-03, STEP 2, AND 3.

Part: FAILSAFE — DAMAGED (BS 955) · airframe 80,581 hrs · 23,232 cycles

LEFT FAIL SAFE STRAP FAILED AN OPEN HOLE INSPECTION. REPAIRED THE FAIL SAFE STRAP IAW IAW SB 53A0100, REV 3.

Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 80,581 hrs · 23,232 cycles

RH WING FUEL FILLER CAP OPENING ON THE WING CORRODED. REPAIRED THE WING UPPER SKIN AT FUEL FILLER OPENING IAW EA 180128.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 80,581 hrs · 23,232 cycles

EMERGENCY LIGHT ABOVE THE COCKPIT DOOR INOPERATIVE. REPLACED THE POWER SUPPLY M735 IAW AMM 33-51-07-402-010. OPS CHECKED IAW AMM 33-51-00-715-001, NO DEFECTS NOTED.

Part: STRUCTURE — CRACKED (BS 287) · airframe 80,581 hrs · 23,232 cycles

SECTION 41 NOSE WHEEL WELL BS 287, RBL 25 HAD A CRACK INDICATION. IAW PART 2 AND STEP 4 OF EA 6753A027. REPAIRED IAW SRM 51-70-12-06-0, AMM 05-51-28-782-001, & EO6753A683.

Part: SOCKET — DIRTY (EMERGENCY LIGHT) · airframe 80,581 hrs · 23,232 cycles

EMERGENCY EXIT LIGHT AT THE L1 DOOR INOPERATIVE. CLEANED THE SOCKET IAW SWPM 20-60-01, OPS CHECKED GOOD IAW AMM 33-51-00.

Part: ENGINE — ODOR (NR 1) · airframe 80,453 hrs · 23,128 cycles

STRONG BURNING ODOR FOR ABOUT 5 MINUTES, AT FL 400. REMOVED AND REPLACED THE NR 1 ENGINE IAW AMM 71-00-02, LEAK CHECKED AND ENGINE RUNS GOOD.

Part: STARTER — DEFECTIVE (APU) · airframe 80,388 hrs · 23,086 cycles

APU DOES NOT START. REMOVED AND REPLACED APU STARTER IAW AMM 49-41-01. OPS CHECK NORMAL.

Part: BLEED VALVE — DEFECTIVE (APU) · airframe 80,388 hrs · 23,086 cycles

AUTO SHUT DOWN APU SURGE BLEED DOES NOT RESPOND. REPLACED APU SURGE BLEED VALVE IAW AWW 49-53-01.

Part: INDICATOR — INOPERATIVE (FUELING PANEL) · airframe 80,388 hrs · 23,086 cycles

FUELING PANEL BACK LIGHTS ARE INOP. REMOVED AND REPLACED FUEL INDICATORS (3EA). OPS CHECK NORMAL IAW AMM 28-41-06.

Part: SHUTOFF VALVE — DEFECTIVE (FUEL SYSTEM) · airframe 80,388 hrs · 23,086 cycles

REFUELING PANEL FILL VALVES WILL NOT OPEN UNLESS THE OVERFILL RESET SWITCH IS HELD. REMOVED AND REPLACED RIGHT TANK O/B FUELING SHUT OFF VALVE. OPS CHECK NORMAL IAW AMM 28-21-00.

Part: WEB — CRACKED (LT WING TE) · airframe 80,017 hrs · 22,836 cycles

LEFT WING TE WEB CRACKED BETWEEN WS 226.3 AND 255.4. FABRICATED A DOUBLER AND FILLER. INSTALLED IAW EO 6757A134.

Part: WARNING LIGHT — ILLUMINATED (LT ENG EEC) · airframe 79,881 hrs · 22,737 cycles

LEFT ENGINE EEC ILLUMINATED ON TAKEOFF ROLL AT 40 KNOTS.

Part: ESCAPE REEL — DAMAGED (COCKPIT) · airframe 796,886 hrs · 2,261 cycles

FOUND COCKPIT DESCENT DEVICE DAMAGED DURING EQUIPMENT INSPECTION. REPLACED THE DESCENT DEVICE IAW AMM 25-61-03.

Part: AILERON — OSCILLATES (WING) · airframe 79,427 hrs · 22,441 cycles

MULTIPLE ITEMS: AILERON OSCILLATED UNCONTROLLABLY WITH AUTOPILOT ENGAGED IN FLIGHT. EFIS DISPLAY BLACKED OUT INTERMITTENTLY WHILE IN HOLDING WITH AUTOPILOT ON AND AILERONS WOULD JERK LT THEN RT UNCOMMANDED. GLARE SHIELD LIGHTS FLICKERED ALSO. TCAS RA COMMANDED A DESCENT WITHOUT ANY TRAFFIC IN THE AREA. ATC NOTIFIED AND THEY ADVISED US OF NO TRAFFIC CONFLICT. WE DESCENDED FROM 12,000 TO 10,000 FT. THERE WAS A TRAFFIC INDICATION OF CO ALTITUDE TRAFFIC LESS THAN A MILE AT THE 12 O'CLOCK POSITION ON CA. F/O TRAFFIC DISPLAYS. PERFORMED AILERON SERVO TEST IAW MM 22-00-02 MCDP NR 7, OPS CHECKED GOOD AT THIS TIME. FOUND LT IDG TO BE AT FAULT. TRANSFERRED TO MDDR 70068 IAW 24-00-01-03, LT IDG DISCONNECTED, MCC NOTIFIED. ITEM 11: PERFORMED OPS CHECK OF TCAS SYSTEM IAW AMM 34-45-00, OPS CHECK GOOD, NO DEFECT NOTED AT THIS TIME.

Part: FRAME — CRACKED (FUSELAGE) · airframe 79,399 hrs · 22,423 cycles

POSSIBLE CRACK AT RT STA 859.5 FRAME INNER CHORD TRANSITION RADIUS. REMOVED AND INSTALLED FASTENERS STA 750-850, RBL 11. REMOVED AND INSTALLED FASTENERS INNER CHORD FRAME 859.5. REPAIR ANGLE SRM 51-40-02, 51-40-019, BSB 767 53-A0209, EO 0675A038, NDT PART 6 51-00-16, 51-00-14.

Part: FRAME — CRACKED (FUSELAGE) · airframe 79,399 hrs · 22,423 cycles

POSSIBLE CRACK AT STA 859.5 FRAME INNER CHORD TRANSITION RADIUS LT SIDE. REMOVED DAMAGE, HFEC INSPECTED 13 HOLES, MADE 0.040 INSURANCE CUT, LOCATED AND DRILLED REPAIR ANGLE, FABRICATED REPAIR WASHER, TREATED PRIME REPAIR ANGLES, COLD WORKED HOLE, INSTALLED IAW SRM 51-40-02, B-SB-761-53A0209, EO 753A038, NDT PART G, 51-00-16.

Part: ACTUATOR — CORRODED (TE FLAP) · corrosion level 2 · airframe 79,399 hrs · 22,423 cycles

NR 7 ROTARY ACTUATOR ASSY FIXED RING GEAR IS CORRODED. NR 7 REACTION RING SPLINES ARE CORRODED. R & R NR 7 FLAP ACTUATOR IAW AMM 27-51-22, R & R NR 7 REACTION RING IAW SB 767-27A0229.

Part: FRAME — CRACKED (FUSELAGE) · airframe 79,399 hrs · 22,423 cycles

POSSIBLE CRACK AT RT STA 883.5 FRAME CHORD TRANSITION RADIUS. MADE 0.040 CUTOUT, COLD WORKED HOLE, DRILLED DOUBLER, TREATED AND PRIMED DOUBLER, INSTALLED REPAIR ANGLE IAW 51-40-02, EO 6753A038, 53-A0209, NDT PART G 51-00-16.

Part: PRESSURE DECK — DENTED (FUSELAGE) · airframe 79,399 hrs · 22,423 cycles

DENT AT STA 996 AND LBL 18 ON SLOPING PRESSURE DECK, FLAGGED, UNDER FLOORBOARD 241GFF. REMOVED DAMAGED IAW SRM 53-50-51-2R-1, REPAIR 1. FABRICATED REPAIR PARTS IAW SRM 53-50-51-2R-1. INSTALLED REPAIR PARTS IAW SRM 51-40-02.

Part: RING GEAR — CORRODED (WING) · corrosion level 2 · airframe 79,399 hrs · 22,423 cycles

NRI 3295, NR 3 ROTARY ACTUATOR ASSY FIXED RING GEAR CORRODED. NR 3 REACTION RING SPLINES ARE CORRODED, NRI 3296 & NRI 3295. REMOVED AND INSTALLED NR 3 ROTARY ACTUATOR IAW AMM 27-51-11 UP TO STEP 3F, NRI 3296. R & R NR 3 REACTION RING IAW EO 6727A007.

Part: RING GEAR — CORRODED (TE FLAP) · corrosion level 2 · airframe 79,399 hrs · 22,423 cycles

NRI 3273, LT WING, NR 2 FLAP ACTUATOR RING TEETH ARE CORRODED, NRI 3274. LEFT WING NR 2 FLAP ACTUATOR REACTION RING HAS CORRODED TEETH. NRI 3273, R & R ROTARY ACTUATOR TO STEP 3, FC161 IAW AMM 27-51-22, WORK TO BE COMPLETED ON EO 6727A007, PT SUPPLEMENTAL 25. NRI 3274, R & R NR 2 FLAP ACTUATOR RING IAW 27A0229.

Part: RING GEAR — CORRODED (WING) · corrosion level 2 · airframe 79,399 hrs · 22,423 cycles

NR 5 ROTARY ACTUATOR HAS CORROSION ON FIXED RING GEAR, NRI 3334. NR 5 REACTION RING HAS CORROSION ON SPLINES, NRI 3333. R & R NR 5 ROTARY ACTUATOR UP TO STEP 3F IAW EO 6727A007 PT1, NRI 3334. R & R NR 5 REACTION RING IAW EO 6717A007.

Part: WEB — CORRODED (FAIRING) · corrosion level 2 · airframe 79,399 hrs · 22,423 cycles

NR 2 LOWER AFT FAIRING CORROSION, PITTING AND DOUBLE FLUSH HOLES. REMOVED, REPLACED AND FABRICATED NEW WEB FOR NR 2 LOWER AFT FAIRING FROM .063 2024-T3, BATCH 100341297 IAW SRM 51-40-02.

Part: SKIN — DENTED (LE SLAT) · airframe 79,044 hrs · 22,183 cycles

LEFT WING NR 6 SLAT, UPPER SKIN HAS A DENT IN MIDDLE OF SLAT, PN 114T3100-1A, SN 00094. ACCOMPLISHED TIME LIMITED REPAIR IAW SRM 57-43-02 FIG 101 & EO 6757A111 PART 1. INSPECT WITHIN 150 FLIGHT CYCLES.

Part: SEAL DEPRESSOR — DAMAGED (FUSELAGE) · airframe 78,816 hrs · 22,022 cycles

NON-MEL ITEM 60559 REFERENCE LOG PAGE 647791 ITEM 1. GND CREW REPORTS DAMAGE TO SEAL COMPRESSOR OR MAIN DECK CARGO DOOR. ACCOMPLISHED TIME LIMITED REPAIR TO SEAL DEPRESSOR, COMPRESSOR, IAW SRM 53-00-15 & EO 6753A272.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 78,715 hrs · 21,959 cycles

AIRCRAFT RETURNED, AIR TURN BACK DUE FOLLOWING ITEM, TE FLAP DISAGREE, NOTED FAULT AS REPORTED. ACCOMPLISHED FIM 27-51 FAULT TREE 810 & FIM 27-58 FT 804 BITE & RESET OF FSPM. RAN FLAPS & SLATS FULL UP & DOWN HYD & ELEC WITH NO FAULTS NOTED. VISUAL INSPECTION ACCOMPLISHED, NO FAULTS NOTED.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 78,373 hrs · 21,767 cycles

TAKEOFF CONFIG WARNING, STAB TRIM DURING TAKEOFF. REJECTED TAKEOFF AT 20 KTS, STAB TRIM SET AT 2.25, NO ADVERSE BRAKING. TROUBLE SHOT IAW FIM 27-48 FAULT TREE 806 & FIM 27-48 FAULT TREE 809, NO DEFECTS NOTED AT THIS TIME.

Part: CABLE — DEPLOYED (DESCENT DEVICE) · airframe 78,299 hrs · 21,723 cycles

CABLE FOUND DEPLOYED ON ONE TIME USE DESCENT DEVICE LOCATED NR 1 POSITION MAIN DECK. R & R EMER DESCENT DEVICE WITH SERVICEABLE EMER DEVICE. WORK DONE IAW AMM 25-61-03.

Part: FITTING — GOUGED (CARGO BAY) · airframe 78,303 hrs · 21,725 cycles

MAIN CARGO BARRIER NET LT 4TH ATTACH FITTING FROM FLOOR HAS GOUGE. DAMAGE AREA WAS REMOVED BY BLEND OUT. AREA OF BLEND IS ACCEPTABLE IAW IAI DOCUMENTATION. AREA WAS TREATED, PRIMED & TOP COATED IAW IAI 8110-3 WITH REPAIR INSTRUCTIONS CS 22572-005.

Part: TRANSCEIVER — MALFUNCTIONED (WX RADAR SYS) · airframe 77,130 hrs · 20,699 cycles

WEATHER RADAR DID NOT PAINT WEATHER ENROUTE AND THEREFORE UNABLE TO DEVIATE AROUND TS ACTIVITY INTERMIRAL AREA, NO CAHNGE WHEN USING GAIN. REPLACED WEATHER RADAR TRANSCEIVER IAW AMM 34-43-01, OPS CHECK GOOD REF AMM 34-43-00, OK FOR SERVICE.

Part: SKIN — DAMAGED (BS 139-169) · airframe 76,760 hrs · 20,457 cycles

LIGHTNING STRIKE WAS FOUND ON LT SIDE OF FUSELAGE SKIN, AFT OF THE NOSE RADOME. COMPLIED WITH EO 6753A097.

Part: STRUCTURE — DELAMINATED (RT AILERON TE) · airframe 76,134 hrs · 20,231 cycles

RT TRAILING OTBD AILERON EDGE DELAMINATED. REF E/O 6757A039, RT WING OTBD AILERON DELAMINATION: PART I, TIME LIMITED REPAIR ACCOMPLISHED. PART II, DVI EVERY FLT CYCLE. PART III, PERMANENT REPAIR PRIOR TO 750 FLT CYCLES.

Part: TARGET — OUT OF ADJUST (PROXIMITY SWITCH) · airframe 76,415 hrs · 20,324 cycles

LEADING EDGE SLAT ASYMETRY WARNING, AFTER TAKEOFF. BITE CHECK PSEU, FOUND OTBD SLAT PROXIMITY SWITCH OUT OF LIMITS. ADJUSTED NR 4 OTBD TARGET, IAW AMM 27-88-00/201. RESET FSDU. CYCLED FLAPS OPS CHECKS GOOD.

Part: RIB — CHAFED (ZONE 600) · airframe 76,169 hrs · 20,241 cycles

RT WING L/E CHAFED BY NR 7 SLAT OTBD END CAP. REPAIRED IAW EO 6757A033, REV A DATED 6/15/12. APPROVAL ON 8110-3 DATED 6/16/12 BY DERT-710167-SW, AND AMES NON-ROUTINE 0127 WO 30654.