N379AZ

Part: INDICATOR — MALFUNCTIONED (ZONE 200) · airframe 113,815 hrs · 21,134 cycles

CREW REPORTED ON TAXI OUT BOTH EICAS SCREENS BLANK FOLLOWED BY COMPACT MODE. UPPER EICAS BLANK THEN HOT ELECTRICAL SMOKE NOTED. CREW ELECTED A BLOCK RETURN FOR FAULT ISOLATION AND CORRECTIVE ACTIONS. AIRCRAFT GROUNDED FOR MAINTENANCE. GENERAL VISUAL INSPECTION VERIFIED UPPER DISPLAY UNIT HAD DISTORTED COLOR AND INDICATION. INTEGRITY AND SECURITY OF EQUIPMENT COOLING SOURCE TO DISPLAY UNIT GOOD. EHSI & EICAS INDICATOR ASSEMBLY REMOVED AND REPLACED. LEFT AND RIGHT EICAS COMPUTERS OPERATIONAL CHECKS GOOD PER BOEING 767-300 AIRCRAFT MAINTENANCE MANUAL 31-41-01 AND 31-41-02. NO ADDITIONAL FAULTS NOTED, AIRCRAFT RELEASED TO SERVICE.

Part: PANEL — CRACKED (ZONE 100) · airframe 112,706 hrs · 20,716 cycles

P33 REAR PANEL CRACKED STA 303 LBL11.

Part: BRACKET — CRACKED (ZONE 500) · airframe 112,706 hrs · 20,716 cycles

LEFT WING LE BRACKET LES 475 CRACKED.

Part: PANEL — WORN (ZONE 200) · airframe 112,706 hrs · 20,716 cycles

THE FOOTREST PANELS LOCATED WHERE THE PILOT PLACES HIS FEET IS WORN

Part: SLEEVE — DELAMINATED (THRUST REVERSER) · airframe 112,706 hrs · 20,716 cycles

#1 ENGINE OUTBOARD T/R SLEEVE AFT UPPER EDGE COMPOSITE DELAMINATED.

Part: DOOR SILL — CORRODED (ZONE 100) · corrosion level 2 · airframe 112,706 hrs · 20,716 cycles

CORROSION AT THE UPPER CHORD AT LOWER SILL FOR THE CUTOUT FOR THE BULK CARGO DOOR STA 1426, S33L

Part: SKIN — DAMAGED (ZONE 500) · airframe 112,706 hrs · 20,716 cycles

HOLE INBD OF STRINGER 6.5 IS OVERSIZED

Part: SKIN — DAMAGED (ZONE 500 SLAT) · airframe 102,706 hrs · 20,716 cycles

#5 SLAT HAS COMPOSITE REPAIR @ I/B END

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 112,706 hrs · 20,716 cycles

ALC STRINGER 36R STA 1197+72 TO 1197+74 CORROSION

Part: SKIN — CORRODED (ZONE 100) · corrosion level 2 · airframe 112,706 hrs · 20,716 cycles

LAP SEAM AT S36R BETWEEN STA. 1197+66 AND 1197+88 CORROSION

Part: DIFFUSER — DETERIORATED (ZONE 200) · airframe 112,706 hrs · 20,716 cycles

THE FOOTREST DIFFUSER ASSMBLIES ARE WORE, LOCATED WHERE THE F/O PLACES HIS/HER FEET ON THE FLOOR BELOW THE RUDDER PEDALS. PART NUMBERS 214T1119-10 AND -11

Part: SKIN — CRACKED (ZONE 200) · airframe 112,706 hrs · 20,716 cycles

RI LOWERR AFT DOOR CORNER CUTOUT CRACKED

Part: SLIDING WINDOW — OUT OF ADJUST (ZONE 200) · airframe 112,607 hrs · 20,677 cycles

PRE-DEPARTURE, CREW REPORTED FO WINDOW NOT FULLY CLOSING. STOPS AT "CLOSED" HANDLE 1 SHY OF FULLY CLOSED. SUBSEQUENT TO GENERAL VISUAL INSPECTION, LINE MAINTENANCE IDENTIFIED #2 WINDOW OUT OF ADJUSTMENT. WINDOW READJUSTED PER B767 AMM 56-11-02. OPERATIONAL CHECK GOOD. NO ADDITIONAL FAULTS NOTED.

Part: CARRIAGE — CRACKED (SLIDING WINDOW) · airframe 112,525 hrs · 20,640 cycles

FOLLOWING ROUTINE MAINTENANCE, FIRST OFFICER'S OPENABLE WINDOW SLIDING TRACK BRACKET CRACKED IN TWO PLACES. REMOVED AND REPLACED FIRST OFFICER'S #2 OPENABLE WINDOW SLIDING TRACK BRACKET IN ACCORDANCE WITH AIRCRAFT MAINTENANCE MANUAL 56-11-04. OPERATIONAL CHECK GOOD.

Part: PANEL — CRACKED (UNKNOWN) · airframe 110,508 hrs · 19,920 cycles

DURING REPAIRS OF DAMAGES TO THE #5 SLAT INBOARD SIDE, LINE MAINTENANCE REPORTED 15 INCH CRACK FOUND AT LEFT WING STATION 587 LEADING EDGE. AIRCRAFT GROUNDED. REMOVED AND REPAIRED DAMAGE ON LEFT WING FIXED LEADING EDGE AT STATION 587.15 IAW B767-300 SRM 51-70-01 PARAGRAPH 4E-4G AND 4I AS DIRECTED BY B767-300 SRM 57-41-01. GENERAL VISUAL INSPECTION OF WIRE BUNDLES UNDER REMOVED LEFT WING LEADING EDGE SKIN AT STATION 587 SATISACTORY. NO FAULTS FOUND.

Part: PANEL — CRACKED (UNKNOWN) · airframe 110,508 hrs · 19,920 cycles

DURING REPAIRS OF DAMAGES TO THE #5 SLAT INBOARD SIDE, LINE MAINTENANCE REPORTED 18 INCH CRACK FOUND AT LEFT WING STATION 464 LEADING EDGE. REMOVED AND REPAIRED DAMAGE ON LEFT WING FIXED LEADING EDGE SEGMENT BY WAY OF A COMPOSITE REPAIR UNDER VACUUM IAW B767 SRM 51-70-08 REPAIR 1. GENERAL VISUAL INSPECTION OF WIRE BUNDLES UNDER REMOVED LEFT WING LEADING EDGE SKIN AT STATION 464 SATISFACTORY. NO FAULTS FOUND.

Part: PANEL — CRACKED (UNKNOWN) · airframe 110,508 hrs · 19,920 cycles

DURING REPAIRS OF DAMAGES TO THE #5 SLAT INBOARD SIDE, LINE MAINTENANCE REPORTED 8 INCH CRACK FOUND AT LEFT WING STATION 571 LEADING EDGE. AIRCRAFT GROUNDED. REMOVED AND REPAIRED DAMAGE ON LEFT WING FIXED LEADING EDGE AT STATION 571.8 IAW B767-300 SRM 51-70-07 PARAGRAPH 4E-4G-4I AS DIRECTED BY B767-300 SRM 57-41-01. GENERAL VISUAL INSPECTION OF WIRE BUNDLES UNDER REMOVED LEFT WING LEADING EDGE SKIN AT STATION 571 SATISACTORY. NO FAULTS FOUND

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 110,467 hrs · 19,905 cycles

POST FLIGHT CREW REPORTED, AFTER ARRIVING AT GATE STRONG RUBBER ODOR WAS NOTED IN THE FLIGHT STATION. INITIATED DEFERRAL MAINTENANCE ITEM 44639 OF THE LEFT AIR CONDITIONING PACK IAW B767 200/300 MINIMUM EQUIPMENT LIST 21-51-01-01. COMPLIED WITH CONDITIONAL INSPECTION FOR SMOKE/FUMES IN THE CABIN IAW B767 AMM 05-51-56 AND B767 AMM 21-00-21. NO FAULTS FOUND. AIRCRAFT RELEASED TO SERVICE. DOWNLINE MAINTENANCE REACTIVATED LEFT PACK SYSTEM AND OPERATED WITH APU LEFT AND RIGHT ENGINES INDEPENDANTLY. NO BURNT SMELL AND OPERATIONAL CHECK GOOD IAW B767 AMM 21-51-00. DEFERRAL MAINTENANCE ITEM 44639 CLEARED.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 110,470 hrs · 19,906 cycles

ON DESCENT PASSING THROUGH 11000 UNTIL 9000, CREW REPORTED A HARSH RUBBER SMELL IN THE FLIGHT STATION. LANDING WAS WITHOUT INCIDENT AND NO PRECAUTIONARY ACTIONS. ON ARRIVAL, ODOR DISSIPATED. AIRCRAFT WAS GROUNDED FOR UNSCHEDULED MAINTENANCE. COMPLIED WITH A DETAILED VISUAL INSPECTION OF LEFT AND RIGHT ENGINES FOR FLUID LEAKS AND INSPECTED PNEUMATIC DUCTING IAW B767 AMM 75-00-00. NO DEFECTS NOTED. ADDITIONALLY, COMPLIED WITH CONDITIONAL INSPECTION SMOKE/FUMES IN THE CABIN IAW B767 AMM 05-51-56 AND REMOVAL OF OIL CONTAMINATION FROM AIR CONDITIONING AND PNEUMATIC SYSTEMS IAW B767 AMM 21-00-21. NO FAULTS FOUND.

Part: DRIVE SHAFT — GROOVED (ENGINE)

ENGINE WAS REMOVED DUE TO END OF LEASE AND TRANSPORTED TO ENGINE SERVICE FACILITY FOR OVERHAUL. ACCORDING TO THE ENGINE TEARDOWN REPORT A LINE INSPECTOR FOUND A BOLT BETWEEN THE RADIAL DRIVE SHAFT (RDS) AND THE FAN FRAME. THE BOLT HAS CAUSED MAJOR DAMAGE TO THE RDS DURING ENGINE OPERATION. THE DAMAGE IS A GROOVE, APPROX. 4,25 MM DEEP. THE INVESTIGATION IS ON-GOING, BUT IT IS APPEARS TO BE A DOD. PLEASE CONTACT JHUTTU@GATELESIS OR [email protected] FOR FURTHER INFORMATION.

Part: SKIN — CRACKED (ZONE 200) · airframe 124,072 hrs · 21,801 cycles

EXTERNAL SKIN FOUND CRACKED L! DOOR CUTOUT

Part: FRAME — NONE (ZONE 100) · airframe 108,207 hrs · 19,076 cycles

STATION 654 BETWEEN STRINGER 7R - 8R HAS ELONGATED HOLES.

Part: STRINGER SPLICE — NONE (ZONE 200) · airframe 108,207 hrs · 19,076 cycles

FLOOR BEAM STA 654 STR 3 HAS ELONGATED HOLES.

Part: STRINGER SPLICE — NONE (ZONE 200) · airframe 108,207 hrs · 19,076 cycles

FLOOR BEAM FUS STA 654 STR 5R STRINGER SPLICE HAS ELONGATED HOLES.

Part: SHEAR PLATE — CORRODED (ZONE 100) · corrosion level 2 · airframe 108,207 hrs · 19,076 cycles

FWD ENTRY SHEAR PLATE HAS CORROSION.

Part: STRINGER SPLICE — NONE (ZONE 200) · airframe 108,207 hrs · 19,076 cycles

FLOOR BEAM FUS 654 STR 6 HAS ELONGATED HOLES.

Part: SLAT — DENTED (ZONE 600) · airframe 102,207 hrs · 19,076 cycles

R/H WING #10 SLAT UPPER I/B T/E HAS DENT.

Part: THRUST REVERSER — SCRATCHED (ZONE 400) · airframe 108,207 hrs · 19,076 cycles

LH ENGINE IB T ON C DUCT EXTERNAL SKIN ABOUT MID SECTION LWR HAS DEEP SCRATCHES.

Part: NONE — CRACKED (ZONE 100) · airframe 108,207 hrs · 19,076 cycles

INSPECTION FUSELAGE AT BS. 1809.5 BULKHEAD OUTER CHORD, DETECTED CRACK IN R/H FORWARD OUTER CHORD

Part: NONE — DELAMINATED · airframe 108,207 hrs · 19,076 cycles

R/H WING #9 SLAT LOWER SURFACE OF T/E WEDGE HAS AMALL DELAMINATION AREA AT O/B UPPER CORNER OF WEDGE.

Part: NONE — CORRODED (ZONE 100) · airframe 102,207 hrs · 19,076 cycles

KEEL BEAM ON HYD GROUND SERVICE DISCONNECT DOUBLER CORRODED.

Part: CONNECTOR — DETACHED (PRESSURE SWITCH) · airframe 108,187 hrs · 19,070 cycles

ENROUTE, AUTOTHROTTLE DISCONNECTED ON CLIMBOUT AT 340. RT THROTTLE POPPED 1 DEGREE BACK. RT THROTTLE WOULD NOT RETARD BELOW 93.3, N1. THROTTLE WOULD MOVE BUT INDICATOR DIDN`T. RT ENG SHUTDOWN, EMERGENCY DECLARED. LANDED UNEVENTFUL. ACFT GROUNDED. RT ENG TAI PRESS SWITCH & CONNECTOR DAMAGED WHEN CONNECTOR DETACHED, LANDING ON TRB-3 CABLE & T1 IDG CABLE. PLUG D742 RUBBED THROUGH IDG CABLE SLEEVE. CREATING A SHORT TO GROUND THROUGH THROTTLE CABLE TRB-3, SEVERING CABLE RESULTING IN RT THROTTLE STAYING AT 93.3, N1. R & R CONNECTOR D742, RT ENG ANTI-ICE PRESS SWITCH, THROTTLE PUSH-PULL CABLE & IDGR CABLE. IDG & DISCONNECT GOOD, TAI VALVE GOOD, IDLE TO TAKEOFF PWR, OPS NORM IAW AMM 71-00-00.