N337AZ

Part: PROXIMITY SWITCH — INOPERATIVE (ZONE 800) · airframe 105,659 hrs · 20,347 cycles

"EMER DOOR" DESCRETE LIGHT COMES ON OCCASIONALY IN FLIGHT. NO EICAS MESSAGE DISPLAYED. PLACED ON DEFERRAL 68621 MINIMUM EQUIPMENT LIST ATI-52-71-01-01 CATEGORY C. DUE 18 DECEMBER 2025. SUPPLEMENTAL TO PREVIOUS REPORT IXXA20251207083 DATED 12/07/2025 AT KILN. ACCOMPLISHED WIRING DETAIL INSPECTION FROM A191 TO C191 THROUGH S219, A193 TO C193 THROUGH S199, A195 TO C195 THROUGH S218, A197 TO C197 THROUGH S198 IAW B767 AMM 20-60-03 AND IAI B767 SUPPLEMENTAL WDM 52-71-12. NO DEFECTS NOTED. REMOVED AND REPLACED PROXIMITY SENSOR ELECTRONICS UNIT IAW B767 AMM 32-09-04. OPERATIONAL CHECK GOOD IAW B767 AMM 33-16-00. DEFERRAL 68621 CLEARED.

Part: LIGHT — FALSE ACTIVATION (ZONE 800) · airframe 105,659 hrs · 20,347 cycles

EMERGENCY DOOR DESCRETE LIGHT COMES ON OCCASIONALY IN FLIGHT. NO EICAS MESSAGE DISPLAYED. PLACED ON DEFERRAL 68621 MINIMUM EQUIPMENT LIST ATI-52-71-01-01 CATEGORY C.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 105,408 hrs · 20,252 cycles

CORROSION WAS FOUND ON A FORWARD CARGO BALLMAT FLOOR SUPPORT FITTING AT APPROXIMATELY STA 566 COMMON TO THE FITTING OF NUTPLATE STRAP. LOCATED, DRILLED AND INSTALLED NEW FORWARD CARGO SUPPORT IN ACCORDANCE WITH B767 SRM 51-40-02 AND B767 SRM 51-40-05.

Part: SKIN — CRACKED (ZONE 600) · airframe 103,158 hrs · 19,299 cycles

CRACK INDICATION NOTED IN THE RIGHT WING SKIN COMMON TO THE INBOARD MOST HOLE AT WINGLET STRINGER L6.5 MODIFICATION

Part: SKIN — CRACKED (ZONE 600) · airframe 103,158 hrs · 19,299 cycles

CRACK INDICATION NOTED DURING THE ACCOMPLISHMENT OF EO# ATI-07-767-6236, WINGLET STRINGER MODIFICATION OF L 9.5 OUTBOARD SEGMENT.

Part: DOUBLER — CORRODED (ZONE 300) · corrosion level 2 · airframe 103,158 hrs · 19,299 cycles

EXISTING REPAIR DOUBLER ON UPPER SURFACE OF HORIZONTAL STAB CENTER SECTION IS CORRODED. INSIDE TAIL COMPARTMENT AT APPROX STA1735 ON RH SIDE.

Part: SEAL — GOUGED (SLIDING WINDOW) · airframe 103,158 hrs · 19,299 cycles

COCKPIT - #2 SLIDING WINDOW OPENING, LOWER FWD SEAL RETAINER TAB IS GOUGED

Part: STRINGER — CRACKED (ZONE 500) · airframe 103,158 hrs · 19,299 cycles

CRACK FOUND RUNNING FROM THE 11 TO 5 O'CLOCK POSITION COMMON TO STRINGER L-6.5 BETWEEN WSTA 990.20 AND WSTA 1018.20 INBOARD AFT FASTENER AS MARKED.

Part: BULKHEAD — CRACKED (ZONE 100) · airframe 103,158 hrs · 19,299 cycles

STA 1809.5 BULKHEAD RH FWD OUTER CHORD LOWER FWD FASTENER HAS CRACK EXTENDING FROM THE 3 O'CLOCK POSITION TO THE END OF THE PART AND UNDER ADJACENT STRUCTURE.

Part: STABILIZER — WORN (ZONE 300) · airframe 103,158 hrs · 19,299 cycles

HORIZONTAL STAB FAIRING, 313BLX, HAS WEAR ON INNER SIDE.

Part: SKIN — DENTED (ZONE 100) · airframe 103,158 hrs · 19,299 cycles

AFT FUSELAGE, LOWER SKIN IS DENTED AT APPROX STA1790 BETWEEN STRINGERS 38R & 39R

Part: FAN COWL — WORN (ZONE 500) · airframe 103,158 hrs · 19,299 cycles

WEAR BEYOND LIMITS. LOWER FWD INNER EDGE WORN THROUGH EDGE PROTECTOR AND 1 PLY OF CARBON FIBER THAT MEASURED 16.75 INCHES X 1.2 INCHES.

Part: SKIN — DELAMINATED (ZONE 600) · airframe 103,158 hrs · 19,299 cycles

RIGHT WING, OUTBOARD FLAP, OUTBOARD LEADING EDGE SECTION IS DELAMINATED. POSSIBLE CAUSE UNDETERMINED

Part: SEAL DEPRESSOR — CRACKED (ZONE 200) · airframe 103,158 hrs · 19,299 cycles

MCD CUTOUT FWD LOWER SEAL DEPRESSOR ATTACH FITTING IS CRACKED

Part: RETAINER — GOUGED (ZONE 200) · airframe 103,158 hrs · 19,299 cycles

COCKPIT CAPTAIN L2 WINDOW OPENING LOWER SEAL RETAINER STRUCTURE TAB IS GOUGED

Part: SIDEWALL PANEL — DAMAGED (ZONE 200) · airframe 103,158 hrs · 19,299 cycles

MAIN CABIN SIDEWALL #L4 IS DAMAGED. REFER TO HAECO WO 320007 NON ROUTINE 38783

Part: RIB — CRACKED (ZONE 600) · airframe 103,158 hrs · 19,299 cycles

RIGHT WINGLET AFT ATTACH FRAME IS CRACKED INTERNAL JUST AFT OF UPPER AFT MOUNT BOLT. REF HAECO WO 320007 NON ROUTINE 38717

Part: RETAINER — GOUGED (ZONE 400) · airframe 103,158 hrs · 19,299 cycles

#2 ENG RH TR SEAL RETAINER FOUND GOUGED, CAUSE UNDETERMINED. ACCOMPLISHED BLENDOUT REPAIR MEASURING 0.750"W X 1.75"L X 0.018" DEEP

Part: MOUNT FITTING — GOUGED (ZONE 400) · airframe 103,158 hrs · 19,299 cycles

#2 ENG RH TR FWD DEFLECTION LIMITER GOUGED, CAUSE UNDETERMINEDBLEAND OUT MEASURES 1.6"L X 0.096" DEPTH

Part: MOUNT FITTING — GOUGED (ZONE 400) · airframe 103,158 hrs · 19,299 cycles

#1 ENGINE O/B T/R LOWER FWD DEFLECTION LIMITER FITTING WAS FOUND GOUGED

Part: BEAM — CHAFED (ZONE 400) · airframe 103,158 hrs · 19,299 cycles

#1 PYLON AFT FAIRING ASSY, INBD LATCH BEAM CHAFED EDGE DAMAGE DUE TO CONTACT WITH BROKEN HOLD OPEN ROD

Part: RIB — GOUGED (ZONE 500) · airframe 103,158 hrs · 19,299 cycles

LEADING EDGE RIB AT OSS 494 ON LEFT WING IS GOUGED ON INBOARD SIDE, BLENDED OUT AREA MEASURE 2" X 1"

Part: KEEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 103,158 hrs · 19,299 cycles

CORROSION FOUND ON RBL 9.50 KEEL CHORD UPPER SURFDACE , APPROXIMATELY AT BS 786

Part: SKIN — CRACKED (ZONE 200) · airframe 103,158 hrs · 19,299 cycles

CRACK FOUND IN FORWARD ENTRY DOOR AFT LOWER CORNER FUSELAGE SKIN EXTENDING FROM FASTENER IN 10 O'CLOCK POSITION

Part: SUPPORT BEAM — CHAFED (ZONE 600) · airframe 103,158 hrs · 19,299 cycles

R/H AFT MLG SUPPORT BEAM FWD EDGE OF THE LOWER FREE FLANGE HAS CHAFING DAMAGE DUE TO CONTACT WITH LOWER BULB SEAL ATTACH ANGLE APPROX 30" OTBD OF THE INBD END OF BEAM

Part: LONGERON — CHAFED (ZONE 400) · airframe 103,158 hrs · 19,299 cycles

#1 PYLON PANEL 431AT INNER FWD STRUCTURAL CHANNELS (PN 313T2100-86 AND 313T2100-82) ARE CHAFED ON THE FWD ENDS

Part: FAIRING — DAMAGED (ZONE 300) · airframe 103,158 hrs · 19,299 cycles

R/H STAB FAIRING #314CRX FOUND TO HAVE 2EA PUNCTURES IN INNER SKIN

Part: SKIN — CRACKED (ZONE 200) · airframe 103,158 hrs · 19,299 cycles

CRACK FOUND IN SKIN OF FORWARD SERVICE DOOR AFT LOWER CORNER EXTENDING OUT FROM FASTENER IN 2 O'CLOCK AND 8 O'CLOCK POSITION

Part: PANEL — ERODED (ZONE 500) · airframe 103,158 hrs · 19,299 cycles

L.WING L/E PANEL 511CB ERRODED ON THE ERROSION STRIP EDGE

Part: PANEL — CRACKED (ZONE 500) · airframe 103,158 hrs · 19,299 cycles

L.WING L/E PANEL 511BB CRACKED AT FASTENER HOLE ON AFT SURFACE AND DELAMINATION ON FWD EDGE

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 101,418 hrs · 18,643 cycles

LINE MAINTENANCE REPORTED, DESCENT DEVICE HARNESS BAG TORN. REMOVED AND REPLACED EMERGENCY EQUIPMENT BAG. NO ADDITIONAL FAULTS NOTED.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 101,284 hrs · 18,575 cycles

ON CLIMB AT 7,000 FT CREW REPORTED FLIGHT CONTROL MALFUNCTION. IN BOTH AUTOPILOT AND MANUAL MODE FLIGHT CONTROLS UNRESPONSIVE. CREW DIVERTED TO KRIV WITH AN EMERGENCY DECLARATION. LANDING WAS UNEVENTFUL AND NO ADDITIONAL PRECAUTIONARY ACTIONS. ON ARRIVAL THE AIRCRAFT WAS GROUNDED FOR UNSCHEDULED MAINTENANCE. SUPPLEMENTAL INFORMATION TO PREVIOUS SUBMITTAL IXXA202309011056 ON 11 SEPTEMBER 2023 AT KILN. IAW B767 FAULT ISOLATION MANUAL (FIM) 22-02-815 AND 22-04-811 THE FOLLOWING FLAGS WERE NOTED: NO INFC FCC L AUTO TRIM VLD ½ AND LEFT SAM FAULT BALL SAM. REMOVED AND REPLACED LEFT STAB TRIM AND AILERON MODULE ASSEMBLY IAW B767 AMM 27-09-00. OPERATIONAL TEST GOOD IAW B767 AMM 22-00-02 AND 27-11-00. FAULTS CLEARED. CYCLED ALL FLIGHT CONTROLS WITH ALL SYSTEMS/SINGLE HYDRAULIC SYSTEM, NO LEAKS OR ADDITIONAL FAULTS NOTED. MODE CONTROL PANEL TEST 30/40 GOOD. SYSTEM OPERATIONAL TEST SATISFACTORY. QAR/FDR DOWNLOADED FOR BOEING REVIEW. REMOVED AND REPLACED THRUST MANAGEMENT COMPUTER IAW B767 AMM 22-31-01 IAW B767 AMM 22-31-01. OPERATIONAL CHECK GOOD. DURING AUTOTHROTTLE TEST, CLUTCH PACK SLIPPING. REMOVED AND REPLACED CLUTCH PACK ASSEMBLY IAW B767 22-32-05. OPERATIONAL AND MCDP GROUND TESTS 10/30/40 SATISFACTORY. SUBSEQUENT TO FUNCTIONAL FLIGHT CHECK ATN337, CREW REPORTED AUTO PILOT AND FLIGHT CONTROL CHECKS GOOD, ALTERNATIVELY, 1 KNOB THROTTLE SPLIT AT 60% N1 AND LEFT INBOARD AILERON NOT EXTENDING FULLY ON FLAPS 25 APPROACH. 2 UNITS AILERON HELD IN TO COMPENSATE. WHILE ENSURING INTEGRITY OF THROTTLE RIGGING, LINE MAINTENANCE IDENTIFIED LEFT ENGINE PUSH/PULL CABLE OUT OF RIG. IAW B767 AMM 76-11-00 RERIGGED LEFT ENGINE PUSH/PULL CABLE BACKLASH. WITH ENGINE ENGAGED PER B767 AMM 71-00-00, NO THROTTLE SPLIT. OPERATIONAL CHECK GOOD. AILERON DROOP TEST AND AILERON POSITION INDICATING SYSTEM TEST IAW B767 FIM 27-11-807 AND AMM 27-18-00 SATISFACTORY. MCDP TESTS 7, 30, AND 67 GOOD. NO FAULTS FOUND. FOLLOWING BOEING REVIEW OF TELEMETRY QAR/FDR DOWNLOADS, NO ADDITIONAL CORRECTIVE ACTIONS WERE RECOMMENDED. AIRCRAFT RETURNED TO SERVICE.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 101,284 hrs · 18,575 cycles

ON CLIMB AT 7,000 FT CREW REPORTED FLIGHT CONTROL MALFUNCTION. IN BOTH AUTOPILOT AND MANUAL MODE FLIGHT CONTROLS UNRESPONSIVE. CREW DIVERTED TO KRIV WITH AN EMERGENCY DECLARATION. LANDING WAS UNEVENTFUL AND NO ADDITIONAL PRECAUTIONARY ACTIONS. ON ARRIVAL, THE AIRCRAFT WAS GROUNDED FOR UNSCHEDULED MAINTENANCE. SUPPLEMENTAL INFORMATION TO PREVIOUS SUBMITTAL IXXA202309011056 ON 11 SEPTEMBER 2023 AT KILN. IAW B767 FAULT ISOLATION MANUAL (FIM) 22-02-815 AND 22-04-811 THE FOLLOWING FLAGS WERE NOTED: NO INFC FCC L AUTO TRIM VLD ½ AND LEFT SAM FAULT BALL SAM. REMOVED AND REPLACED LEFT STAB TRIM AND AILERON MODULE ASSEMBLY IAW B767 AMM 27-09-00. OPERATIONAL TEST GOOD IAW B767 AMM 22-00-02 AND 27-11-00. FAULTS CLEARED. CYCLED ALL FLIGHT CONTROLS WITH ALL SYSTEMS/SINGLE HYDRAULIC SYSTEM, NO LEAKS OR ADDITIONAL FAULTS NOTED. MODE CONTROL PANEL TEST 30/40 GOOD. SYSTEM OPERATIONAL TEST SATISFACTORY. QAR/FDR DOWNLOADED FOR BOEING REVIEW. REMOVED AND REPLACED THRUST MANAGEMENT COMPUTER IAW B767 AMM 22-31-01 IAW B767 AMM 22-31-01. OPERATIONAL CHECK GOOD. DURING AUTOTHROTTLE TEST, CLUTCH PACK SLIPPING. REMOVED AND REPLACED CLUTCH PACK ASSEMBLY IAW B767 22-32-05. OPERATIONAL AND MCDP GROUND TESTS 10/30/40 SATISFACTORY. SUBSEQUENT TO FUNCTIONAL FLIGHT CHECK ATN337, CREW REPORTED AUTO PILOT AND FLIGHT CONTROL CHECKS GOOD, ALTERNATIVELY, 1 KNOB THROTTLE SPLIT AT 60% N1 AND LEFT INBOARD AILERON NOT EXTENDING FULLY ON FLAPS 25 APPROACH. 2 UNITS AILERON HELD IN TO COMPENSATE. WHILE ENSURING INTEGRITY OF THROTTLE RIGGING, LINE MAINTENANCE IDENTIFIED LEFT ENGINE PUSH/PULL CABLE OUT OF RIG. PER B767 AMM 76-11-00 RERIGGED LEFT ENGINE PUSH/PULL CABLE BACKLASH. WITH ENGINE ENGAGED IAW B767 AMM 71-00-00, NO THROTTLE SPLIT. OPERATIONAL CHECK GOOD. AILERON DROOP TEST AND AILERON POSITION INDICATING SYSTEM TEST IAW B767 FIM 27-11-807 AND AMM 27-18-00 SATISFACTORY. MCDP TESTS 7, 30, AND 67 GOOD. NO FAULTS FOUND. FOLLOWING BOEING REVIEW OF TELEMETRY QAR/FDR DOWNLOADS, NO ADDITIONAL CORRECTIVE ACTIONS WERE RECOMMENDED. AIRCRAFT RETURNED TO SERVICE. ORIG SUBMISSION DATE: 09-11-2023

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 101,284 hrs · 18,575 cycles

ON CLIMB AT 7,000 FT CREW REPORTED FLIGHT CONTROL MALFUNCTION. IN BOTH AUTOPILOT AND MANUAL MODE FLIGHT CONTROLS UNRESPONSIVE. CREW DIVERTED TO KRIV WITH AN EMERGENCY DECLARATION. LANDING WAS UNEVENTFUL AND NO ADDITIONAL PRECAUTIONARY ACTIONS. ON ARRIVAL THE AIRCRAFT WAS GROUNDED FOR UNSCHEDULED MAINTENANCE. SUPPLEMENTAL INFORMATION TO PREVIOUS SUBMITTAL IXXA202309011056 ON 11 SEPTEMBER 2023 AT KILN. IAW B767 FAULT ISOLATION MANUAL (FIM) 22-02-815 AND 22-04-811 THE FOLLOWING FLAGS WERE NOTED: NO INFC FCC L AUTO TRIM VLD ½ AND LEFT SAM FAULT BALL SAM. REMOVED AND REPLACED LEFT STAB TRIM AND AILERON MODULE ASSEMBLY IAW B767 AMM 27-09-00. OPERATIONAL TEST GOOD IAW B767 AMM 22-00-02 AND 27-11-00. FAULTS CLEARED. CYCLED ALL FLIGHT CONTROLS WITH ALL SYSTEMS/SINGLE HYDRAULIC SYSTEM, NO LEAKS OR ADDITIONAL FAULTS NOTED. MODE CONTROL PANEL TEST 30/40 GOOD. SYSTEM OPERATIONAL TEST SATISFACTORY. QAR/FDR DOWNLOADED FOR BOEING REVIEW. REMOVED AND REPLACED THRUST MANAGEMENT COMPUTER IAW B767 AMM 22-31-01 IAW B767 AMM 22-31-01. OPERATIONAL CHECK GOOD. DURING AUTOTHROTTLE TEST, CLUTCH PACK SLIPPING. REMOVED AND REPLACED CLUTCH PACK ASSEMBLY IAW B767 22-32-05. OPERATIONAL AND MCDP GROUND TESTS 10/30/40 SATISFACTORY. SUBSEQUENT TO FUNCTIONAL FLIGHT CHECK ATN337, CREW REPORTED AUTO PILOT AND FLIGHT CONTROL CHECKS GOOD, ALTERNATIVELY, 1 KNOB THROTTLE SPLIT AT 60% N1 AND LEFT INBOARD AILERON NOT EXTENDING FULLY ON FLAPS 25 APPROACH. 2 UNITS AILERON HELD IN TO COMPENSATE. WHILE ENSURING INTEGRITY OF THROTTLE RIGGING, LINE MAINTENANCE IDENTIFIED LEFT ENGINE PUSH/PULL CABLE OUT OF RIG. IAW B767 AMM 76-11-00 RERIGGED LEFT ENGINE PUSH/PULL CABLE BACKLASH. WITH ENGINE ENGAGED PER B767 AMM 71-00-00, NO THROTTLE SPLIT. OPERATIONAL CHECK GOOD. AILERON DROOP TEST AND AILERON POSITION INDICATING SYSTEM TEST IAW B767 FIM 27-11-807 AND AMM 27-18-00 SATISFACTORY. MCDP TESTS 7, 30, AND 67 GOOD. NO FAULTS FOUND. FOLLOWING BOEING REVIEW OF TELEMETRY QAR/FDR DOWNLOADS, NO ADDITIONAL CORRECTIVE ACTIONS WERE RECOMMENDED. AIRCRAFT RETURNED TO SERVICE

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 100,825 hrs · 18,410 cycles

POST FLIGHT, LINE MAINTENANCE IDENTIFIED FLIGHT DECK LIGHT OVERHEAD LIGHT WILL NOT ILLUMINATE ON EMERGENCY LIGHT TEST. ALTERNATIVELY, LIGHT WILL ILLUMINATE ON OVERRIDE FUNCTION. IAW B767 AMM 33-51-03, REMOVED AND REPLACED EMERGENCY LIGHT OVERHEAD LIGHT. OPERATIONAL CHECK GOOD. NO ADDITIONAL FAULTS NOTED.

Part: UNKNOWN — SMOKE (COCKPIT) · airframe 99,539 hrs · 17,930 cycles

DURING GROUND LOADING, CREW REPORTED SMOKE IN FLIGHT DECK. WORK IN PROGRESS.

Part: NONE — WORN (ZONE 500) · airframe 99,213 hrs · 17,786 cycles

FLAP SPLINED BUSHINGS WORN

Part: SKIN — CRACKED (ZONE 500) · airframe 99,213 hrs · 17,786 cycles

LOWER LEFT WING SKIN CRACKED

Part: NONE — WORN (ZONE 600) · airframe 99,213 hrs · 17,786 cycles

RW FLAP COLLAR FITTING WORN

Part: NONE — WORN (ZONE 500) · airframe 99,213 hrs · 17,786 cycles

FLAP COLLAR FITTING WORN

Part: TORQUE TUBE — WORN (ZONE 600) · airframe 99,213 hrs · 27,060 cycles

RW MAIN TORQUE TUBE WORN

Part: NONE — WORN (ZONE 600) · airframe 99,213 hrs · 17,786 cycles

RW SHEAR TUBE WORN

Part: NONE — WORN (ZONE 500) · airframe 99,213 hrs · 17,786 cycles

FLAP SHEAR TUBE WORN

Part: NONE — BROKEN (ZONE 400) · airframe 99,213 hrs · 17,786 cycles

EXHAUST SHROUD FINGER SEAL IS BROKEN

Part: TORQUE TUBE — WORN (ZONE 500) · airframe 99,213 hrs · 17,786 cycles

FLAP MAIN TORQUE TUBE WORN

Part: NONE — WORN (ZONE 600) · airframe 99,213 hrs · 17,786 cycles

RW FLAP SPLINE BUSHING WORN

Part: WEB — CRACKED (ZONE 400) · airframe 99,213 hrs · 17,786 cycles

PANEL WEB CRACKED

Part: BRACKET — CHAFED (ZONE 400) · airframe 99,213 hrs · 17,786 cycles

BRACKET FOR MOUNTING CORE COWL FAIRING CHAFED THROUGH

Part: NONE — NONE (ZONE 400) · airframe 99,213 hrs · 17,786 cycles

#2 ENGINE OUTBOARD CORE COWL AFT LATCH HOUSING COVER HAS HOLE

Part: BRACKET — CRACKED (ZONE 400) · airframe 99,213 hrs · 17,786 cycles

#2 PYLON HYDRAULIC BAY DOOR HOLD OPEN ROD MOUNT BRACKET ELONGATED HOLE.

Part: AUTOPILOT SYS — FAULTED · airframe 98,235 hrs · 17,457 cycles

ENROUTE FROM KONT TO KPHI AND APPROACHING 8,000 AUTOPILOT WOULD NOT DISENGAGE. AIR TURN BACK TO KONT WITH EMERGENCY DESCENT. LANDING WAS UNEVENTFUL WITH NO ADDITIONAL PRECAUTIONARY ACTIONS. UPON ARRIVAL AIRCRAFT WAS GROUNDED FOR UNSCHEDULED MAINTENANCE. WORK IN PROGRESS

Part: BATTERY PACK — INOPERATIVE · airframe 97,903 hrs · 17,355 cycles

PRE-DEPARTURE INSPECTIONS, LINE MAINTENANCE IDENTIFIED TWO EMERGENCY LIGHTS HAVE NO POWER. REMOVED AND REPLACED BATTERY IAW B767 AMM 33-51-07. NO ADDITIONAL FAULTS NOTED.

Part: NONE — NONE · airframe 96,975 hrs · 17,079 cycles

ENROUTE KRFD TO KSMF, LEFT ENGINE HAD HIGH VIBRATION AT IDLE ON DESCENT (4.6 N2 ON THE VIB GAUGE) AUDIBLE INDICATIONS SIMILAR TO GRINDING. EMERGENCY DECLARATION WITH AIR TRAFFIC CONTROL FOR PRIORITY LANDING AT CONGESTED AIRPORT. AIRCRAFT LANDING UNEVENTFUL WITH NO ADDITIONAL PRECAUTIONARY ACTIONS TAKEN. AIRCRAFT GROUND ON LANDING FOR FAULT ISOLATION.

Part: APU — FAILED · airframe 96,235 hrs · 16,845 cycles

FLIGHT ATN107, ENROUTE FROM KCVG TO KHRL CREW REPORTS AUXILIARY POWER PLANT (APU) FAULT EICAS MESSAGE DISPLAYED. LEFT INTEGRATED DRIVE GENERATOR DEFERRED. IAW ATI QUICK REFERENCE HANDBOOK, TRIED TO RESTART AUXILIARY POWER PLANT, CONVERSELY, THE SYSTEM FAILED TO START. PER ATI QUICK REFERENCE HANDBOOK , DIVERSION TO CLOSEST SUITABLE AIRPORT REQUIRED. DIVERSION TO KBNA WITH EMERGENCY DECLARATION. LANDING WAS UNEVENTFUL WITH NO ADDITIONAL PRECAUTIONARY ACTIONS. AIRCRAFT GROUNDED FOR UNSCHEDULED MAINTENANCE. WORK IN PROGRESS.

Part: FLOORBEAM — DAMAGED (BS 246) · airframe 87,007 hrs · 14,003 cycles

DAMAGED FLOORBEAM, FWD MAIN DECK, SEC 41, BS 246, RBL 73

Part: FRAME — CRACKED (BS 903) · airframe 87,007 hrs · 14,003 cycles

CRACK IN BS 903.5 FRAME.

Part: FRAME — CRACKED (BS 903) · airframe 87,007 hrs · 14,003 cycles

CRACK IN THE BS 903.5 FRAME RBL 89.