N491AZ

Part: THRUST REVERSER — GOUGED (NR 2 ENGINE) · airframe 90,150 hrs · 16,255 cycles

#2 ENGINE, OUTBOARD THRUST REVERSER, OUTER RING IS GOUGED AT THE 10 O'CLOCK POSITION.

Part: SKIN — GOUGED (ZONE 500 FLAP) · airframe 90,150 hrs · 16,255 cycles

LEFT WING OUTBOARD FLAP, LOWER SKIN IS GOUGED.

Part: FAN COWL — DENTED (ZONE 400) · airframe 90,150 hrs · 16,255 cycles

# ENGINE O/B FAN COWL OUTER SKIN IS DENTED

Part: STRUCTURE — DAMAGED (ZONE 300) · airframe 90,150 hrs · 16,255 cycles

LIGHTNING STRIKES ON VERTICAL STABILIZER DIVERTER STRIPS ALONG ENTIRE LENGTH

Part: FAN COWL — DELAMINATED (ZONE 400) · airframe 90,150 hrs · 16,255 cycles

#1 ENGINE OUTBOARD FAN COWL IS DENTED/DELAMINATED

Part: STRUCTURE — DAMAGED (ZONE 300) · airframe 90,150 hrs · 16,255 cycles

LIGHTNING STRIKES ON VERTICAL STABILIZER DIVERTER STRIPS ALONG ENTIRE LENGTH

Part: FAIRING — DAMAGED (ZONE 600) · airframe 90,150 hrs · 16,255 cycles

RH WINGLIT TIP, FAIRING SKIN HAS LIGHTNING STRIKE DAMAGE

Part: SEAL — PUNCTURED (ZONE 300) · airframe 90,150 hrs · 16,255 cycles

HORIZONTALSTABILIZER BANANA FAIRING 313CLX IS PUNCTURED.

Part: SKIN — WORN (ZONE 400) · airframe 90,150 hrs · 16,255 cycles

#2 PYLON, AFT FAIRING PANEL 447CR HAS 2EA OVERSIZED HOLES

Part: FAIRING — DAMAGED (ZONE 600) · airframe 90,150 hrs · 16,255 cycles

RIGHT WINGLET TIP, FAIRING SKIN HAS LIGHTNING STRIKE DAMAGE

Part: WEB — CORRODED (ZONE 100) · corrosion level 2 · airframe 90,150 hrs · 16,255 cycles

FWD CARGO COMPARTMENT LOWER WEB AT STA 566 TO 544 RBL 12 TO RBL 24 APPROX HAS CORROSION ON UPPER SURFACE THAT IS EXFOLIATED

Part: SKIN PANEL — CORRODED (ZONE 300) · corrosion level 2 · airframe 90,150 hrs · 16,255 cycles

HORIZONTAL STAB CENTER SECTION UNDER CENTER STRAP IS CORRODED BETWEEN STRINGER 7 AND STRINGER 8 ABOVE RIB 1 LEFT. HAECO WO 320008 NON ROUTINE 40691

Part: SUPPORT BEAM — CORRODED (ZONE 600) · corrosion level 2 · airframe 90,150 hrs · 16,255 cycles

RIGHT WING, UPPER TRAILING EDGE PANEL SUPPORT BEAM IS CORRODED. HAECO WO 320008 NON ROUTINE 40687

Part: DOUBLER — GOUGED (THRUST REVERSER) · airframe 90,150 hrs · 16,255 cycles

#2 IB TR IDG DOOR LANDING IS GOUGED IN SERVERAL PLACES ON TR. HAECO WO 320008 NON ROUTINE 40561

Part: FAN COWL — DELAMINATED (ZONE 400) · airframe 90,150 hrs · 16,255 cycles

#1 END INBD FAN COWL LOWER FWD LANDING HAS PAINT WORN OFF EXPOSING COMPOSITE. HAECO WO 320008 NON ROUTINE 40562

Part: FAN COWL — ERODED (ZONE 400) · airframe 90,150 hrs · 16,255 cycles

#2 ENG OB FAN COWL LEADING EDGE IS ERRODED. HAECO WO 320008 NON ROUTINE 40568

Part: DOUBLER — GOUGED (THRUST REVERSER) · airframe 90,150 hrs · 16,255 cycles

#1 ENGINE TRDGI OIL SERVICE DOOR LANDING HAS GOUGED AT PLACES. HAECO WO 320008 NON ROUTINE 40541

Part: SKIN — WORN (ZONE 400) · airframe 90,150 hrs · 16,255 cycles

#2 ENGINE PYLON UPPER SKIN IS WORN ON THE LH SIDE JUST ABOVE THE INBD FAN COWL UPPER AFT CORNER AT APPROX NAC STA 200. HAECO WO 320008 NON ROUTINE 40538

Part: SKIN PANEL — CRACKED (ZONE 200) · airframe 90,150 hrs · 16,255 cycles

FUSELAGE BS 180935 LH SIDE SKIN ABOVE HORIZ STAB, LOWER FWD HOLE SHOWS CRACK INDICATION NOTED AT 1 O'CLOCK POSITION AT BASE OF COUNTERSINK. HAECO WO 320008 NON ROUTINE 40582

Part: SKIN — WORN (ZONE 400) · airframe 90,150 hrs · 16,255 cycles

#2 ENGINE PYLON UPPER SKIN IS WORN IN SEVERAL SPOTS APPROX 9" AFT OF THE FWD EDGE. HAECO WO 320008 NON ROUTINE 40535

Part: SKIN PANEL — WORN (ZONE 600 FLAP) · airframe 90,150 hrs · 16,255 cycles

RH WING OTBD FLAP LOWER SURFACE SKIN IS WORN AT THE CONTACT POINT OF THE OTBD TRACK AFT FAIRING INBD BULB SEAL. HAECO WO 320008 NON ROUTINE 40490

Part: PANEL — GOUGED (ZONE 600 SPOILER) · airframe 90,150 hrs · 16,255 cycles

RH WING #8 SPOILER LOWER SURFACE IS GOUGE APPROX 10" INDS OF THE ACTUATOR. HAECO WO 320008 NON ROUTINE 40435

Part: FAIRING — PUNCTURED (ZONE 300) · airframe 90,150 hrs · 16,255 cycles

PARTS RACK ITEM, HORIZ STAB BANNANA FAIRING 313BRX IN PUNCTURED. HAECO WO 320008 NON ROUTINE 40478

Part: PANEL — WORN (ZONE 300) · airframe 90,150 hrs · 16,255 cycles

PARTS RACK ITEM HORIZ STAB BLADE SEAL PANEL 345AFB IS WORN. HAECO WO 320008 NON ROUTINE 40479

Part: SKIN PANEL — DENTED (ZONE 600 SLAP) · airframe 90,150 hrs · 16,255 cycles

RH WING SLAT NO. 8 INBD CORNER EDGE DENTED. HAECO WO 320008 NON ROUTINE 40386

Part: ACCESS PANEL — GOUGED (ZONE 100) · airframe 90,150 hrs · 16,255 cycles

P32 PANEL LH DOOR GOUGED

Part: RIB — GOUGED (ZON E600) · airframe 90,150 hrs · 16,255 cycles

RH WING FIXED LEADING EDGE RIB IS GOUGED, JUST OUTBD OF #2 PYLON AT APPROX OFSS 450. STREAMER ATTACHED. HAECO WO 320008 NON ROUTINE 40324

Part: FRAME SPLICE — CRACKED (ZONE 100) · airframe 90,150 hrs · 16,255 cycles

CRACK INDICATION FOUND 1 EA HOLE, AT R1 DOOR CUT OUT LOWER AFT CORNER, MARKED 4 O'CLOCK POSITION EXTERNALLY .500" DEEP TO .540" FROM SKIN SURFACE. HAECO WO 320008 NON ROUTINE 40323

Part: LIMITER — GOUGED (THRUST REVERSER) · airframe 90,150 hrs · 16,255 cycles

#1 ENGINE O/B T/R FWD DEFLECTION LIMITER FITTING HAS EDGE DAMAGED / GOUGED. HAECO WO 320008 NON ROUTINE 40292

Part: RETAINER — GOUGED (THRUST REVERSER) · airframe 90,150 hrs · 16,255 cycles

#1 ENGINE OB TR UPPER BIFURCATION FWD SEAL RETAINER CHANNEL IS WORN. HAECO WO 320008 NON ROUTINE 40293

Part: FAN COWL — WORN (ZONE 400) · airframe 90,150 hrs · 16,255 cycles

#1 ENGINE OB FAN COWL INNER SURFACE AFT UPPER WEAR PLATE HAS FRETTING DAMAGE AND BARE METAL

Part: FRAME — CRACKED (ZONE 100) · airframe 90,150 hrs · 16,255 cycles

MAIN CABIN FRAME AT STA 903.5 STR 19RH-20RH IS CRACKED

Part: SKIN — CORRODED (ZONE 300) · corrosion level 2 · airframe 90,150 hrs · 16,255 cycles

HORIZONTAL STAB CENTER SECTION UPPER SKIN HAS CORROSION BETWEEN RIB 1R AND 2R IN FRONT OF EXISTING REPAIR DOUBLER AT 2 EA PLACES. HAECO WO 320008 NON ROUTINE 40204

Part: RETAINER — GOUGED (ZONE 500 FLAP) · airframe 90,150 hrs · 16,255 cycles

L WING LFAP FAIRING 571AB SEAL RETAINER HAS EDGE DAMAGE. HAECO WO 320008 NON ROUTINE 40147

Part: SKIN — CRACKED (ZONE 200) · airframe 90,150 hrs · 16,255 cycles

CRACK FOUND IN 2ND HOLE FROM THE BOTTOM IN BOTH THE SKIN AND BEAR STRAP AT R1 DOOR LOWER AFT CORNER. HAECO WO 320008 NON ROUTINE 40152

Part: SKIN — CRACKED (ZONE 100) · airframe 90,150 hrs · 16,255 cycles

CRACK INDICATION IN THE 3RD HOLE FROM THE BOTTOM, SKIN ONLY AT THE L1 DOOR LOWER AFT CORNER. HAECO WO 320008 NON ROUTINE 40153

Part: LONGERON — WORN (ZONE 400) · airframe 90,150 hrs · 16,255 cycles

#1 PYLON PANEL 431AT 2 INNER LONGERONS ARE WORN. HAECO WO 320008 NON ROUTINE 40144

Part: TRANSMITTER — FAULTED (CENTER HYD IND) · airframe 89,886 hrs · 16,148 cycles

ENROUTE, CENTER HYD QTY EICAS & LIGHT ILLUM IN CRUISE. STATUS PAGE SHOWED 0 QTY & MAGENTA RF WITH 3000 PSI. DIVERTED, EMER DECLARED. LANDED WITHOUT INCIDENT. ACFT GROUNDED. CENTER HYD IND DEFERRED IAW MEL 29-33-02-01. HYD IND INOP. ACFT RELEASED TO SERVICE. IAW FIM 29-11 FAULT TREE 820 ACCOMP GVI OF HYD QTY XMITTER. REMOVED CONNECTOR & VERIFIED NO PINS BACKED OUT IAW AMM 29-33-02. RERACKED QTY MONTIOR IAW AMM 29-33-01. CREW DEBRIEFED, NO DEFECTS DURING ALL PHASES OF FLT. WIRE SHAKEDOWN & IND MONITOR UNABLE TO RECREATE FAULT IAW AMM 29-33-11. PULLED C/B 11L20. RESET C/B, DISCONNECT CONNECTOR AT D556, EICAS READS 0.00RF. RECONNECTED. R & R CENTER HYD QTY XMITTER IAW AMM 29-33-02. OPS CHECKED GOOD.

Part: SENSOR — BINDING (RT ENGINE TEMP) · airframe 89,151 hrs · 15,879 cycles

AT TOP OF DESCENT WITH RT THROTTLE MOVING TO IDLE, RT ENGINE COMPRESSOR STALLED MULTIPLE TIMES WITH A RISE IN EGT. AN ODOR WAS DETECTED IN CABIN. STALL & ODOR INCREASED EACH TIME THROTTLE REDUCED TO IDLE. CREW NOTIFIED DESTINATION STATION KILN, DECLARED EMERGENCY ON DESCENT. LANDED WITHOUT INCIDENT & NO ADDITIONAL PRECAUTIONARY ACTIONS. ON ARRIVAL, ACFT GROUNDED. IAW MM 72-00-00 PARA L SUBTASKS 1, 5, 6 & 11 & PARA M, FAN BLADE SHINGLING INSP, HP TURBINE BORESCOPE INSP, MAGNETIC CHIP DETECTOR CHECK, & CIT PRESSURE CHECK GOOD. NO FAULTS NOTED. IAW POWERPLANT ENGINEERING DFDR R & INTERROGATED & QAR DOWNLOADED FOR RELATIVE DATA PERTAINING TO ENG PARAMETERS. DURING ADDITIONAL TROUBLESHOOTING, LINE MAINT REPORTED, REVERSE FLOW BLEED CHECK FAILED. 8TH STAGE CHECK VALVE JAMMED OPEN & FAN AIR TEMP SENSOR WILL NOT CLOSE FULLY. INTERM AIR SUPPLY CHECK VALVE & FAN AIR TEMP SENSOR R & R. SECURITY & INTEGRITY OF ASSOCIATED DUCT CLAMPS VERIFIED. OPS AND LEAK CHECKED GOOD DURING FULL RUN-UP END TEST #8 WITH BLEED SHIFT CHECK IAW AMM 71-00-00. ENG ENGINEERING REVIEW OF DFDR & QAR DOWNLOADS CONCLUDED NO ADDITIONAL CORRECTIVE ACTIONS WARRANTED. AIRCRAFT RELEASED TO SERVICE.

Part: CHECK VALVE — STUCK (ENGINE) · airframe 89,151 hrs · 15,879 cycles

AT TOP OF DESCENT WITH RT THROTTLE MOVING TO IDLE, RT ENGINE COMPRESSOR STALLED MULTIPLE TIMES WITH A RISE IN EGT. AN ODOR WAS DETECTED IN CABIN. STALL & ODOR INCREASED EACH TIME THROTTLE REDUCED TO IDLE. CREW NOTIFIED DESTINATION STATION KILN, DECLARED EMERGENCY ON DESCENT. LANDED WITHOUT INCIDENT & NO ADDITIONAL PRECAUTIONARY ACTIONS. ON ARRIVAL, ACFT GROUNDED. IAW MM 72-00-00 PARA L SUBTASKS 1, 5, 6 & 11 & PARA M, FAN BLADE SHINGLING INSP, HP TURBINE BORESCOPE INSP, MAGNETIC CHIP DETECTOR CHECK, & CIT PRESSURE CHECK GOOD. NO FAULTS NOTED. IAW POWERPLANT ENGINEERING DFDR R & INTERROGATED & QAR DOWNLOADED FOR RELATIVE DATA PERTAINING TO ENG PARAMETERS. DURING ADDITIONAL TROUBLESHOOTING, LINE MAINT REPORTED, REVERSE FLOW BLEED CHECK FAILED. 8TH STAGE CHECK VALVE JAMMED OPEN & FAN AIR TEMP SENSOR WILL NOT CLOSE FULLY. INTERM AIR SUPPLY CHECK VALVE & FAN AIR TEMP SENSOR R & R. SECURITY & INTEGRITY OF ASSOCIATED DUCT CLAMPS VERIFIED. OPS AND LEAK CHECKED GOOD DURING FULL RUN-UP END TEST #8 WITH BLEED SHIFT CHECK IAW AMM 71-00-00. ENG ENGINEERING REVIEW OF DFDR & QAR DOWNLOADS CONCLUDED NO ADDITIONAL CORRECTIVE ACTIONS WARRANTED. AIRCRAFT RELEASED TO SERVICE.

Part: UNKNOWN — UNKNOWN (MLG) · airframe 89,149 hrs · 15,876 cycles

CREW REPORTED ON APPROACH, UNUSUAL BUMP FROM NOSE GEAR AFTER EXTENDED AND LOCK INDICATIONS. CAPTAIN ELECTED TO DECLARE AN EMERGENCY WITH DESTINATION STATION (KBWI) AIR TRAFFIC CONTROL. LANDING WAS WITHOUT INCIDENT AND NO ADDITIONAL PRECAUTIONARY ACTIONS NOTED. ON ARRIVAL, AIRCRAFT GROUNDED FOR INSPECTIONS. PER B767 AIRCRAFT MAINTENANCE MANUAL 05-51-30 PHASE 1A AND 1B, 05-41-07 AND 05-51-18 NO FAULTS FOUND IN NOSE LANDING GEAR, MAIN LANDING GEAR E & E BAY AND FORWARD E &E. NO EXTERNAL DAMAGES NOTED. AIRCRAFT REMAINS OUT OF SERVICE PENDING FUNCTIONAL FLIGHT CHECK. FUNCTIONAL FLIGHT CHECK ATN491 VERIFIED OPERATIONAL CHECK OF NOSE LANDING GEAR DURING EXTENSION AND RETRACTION WITH NO FAULTS NOTED. AIRCRAFT RELEASED TO SERVICE.

Part: DOOR — OPEN (VENT) · airframe 86,236 hrs · 14,757 cycles

CABIN ALTITUDE EICAS WARNING (CABIN WOULD NOT HOLD PRESSURIZATION). CABIN AUTO INOPERATIVE EICAS CAUTION MESSAGE WITH INTERMITTENT MASTER AURAL WITH NO ASSOCIATED DISCRETE LIGHT EICAS ALERT. AIR TURN BACK TO DEPARTURE STATION. EMERGENCY DECLARATION WITH NO ADDITIONAL PRECAUTIONARY ACTIONS. AIRCRAFT GROUNDED FOR UNSCHEDULED MAINTENANCE ON ARRIVAL. POST FLIGHT, LINE MAINTENANCE IDENTIFED MAIN DECK CARGO DOOR VENT DOORS OPEN. ENSURED SECURITY AND INTEGRITY OF MDCD VENT DOOR IAW B767 AMM 52-30-00. CONDITIONAL INSPECTION AND CABIN PRESSURE LEAK CHECK GOOD IAW B767 AMM 05-51-24 AND 21-31-00. NO FAULTS FOUND. AIRCRAFT RELEASED TO SERVICE.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 86,134 hrs · 14,721 cycles

DURING PRE-DEPARTURE CHECK FOUND CENTER CONSOLE FLASHLIGHT INOPERATIVE. REMOVED AND REPLACED EMERGENCY FLASHLIGHT BATTERY IN ACCORDANCE WITH MAINTENANCE MANUAL 25-64-02. OPERATIONAL CHECK GOOD.

Part: MOUNT — DAMAGED (ZONE 100) · airframe 86,126 hrs · 14,718 cycles

UPON REMOVAL OF DAMAGED 13R PDU FOUND PDU MOUNT STRUCTURE DAMAGED. FAS WO FS220047 NON ROUTINE 00354

Part: SKIN — DENTED (LT NR 2 SLAT) · airframe 86,126 hrs · 14,718 cycles

L WING #2 SLAT UPPER SURFACE HAS SEVERAL DENTS

Part: SKIN — CRACKED (LT WING) · airframe 86,126 hrs · 14,718 cycles

3 EA CRACKES NOTED ON LH WING LOWER SKIN STR L9.5 BETWEEN STA 79 AND 990.2. 2EA CRACKS AT MOST OUTBOARD FASTENER #1 AT 12 AND 6 O CLOCK LOOKING UP/FWD A[[RPX .25" LONG EACH. 1 EA CRACK AT MOST INBOARD FASTENER #6 AT 12 O CLOCK LOOK UP/FWD APPROX 1/8" LONG

Part: SKIN — DENTED (RT NR 12 SLAT) · airframe 86,126 hrs · 14,718 cycles

RH WING #12 SLAT PN 114T4101-52G SN 00800 UPPER SURFACE OF T/E WEDGE HAS NUMEROUS DENTS. FAS WO FS220047 NON ROUTINE 00204

Part: DOOR — DENTED (MAIN CARGBO) · airframe 86,126 hrs · 14,718 cycles

MAIN CARGO COMPARTMENT UNDER RIGID BARRIER DOOR CARGO GUIDE DAMAGED ALONG ENTIRE LENGTH AND STRUCTURE DENTED BETWEEN GUIDES. FAS WO FS220047 NON ROUTINE 00021

Part: BRAKE ASSY — CRACKED (ZONE 700) · airframe 85,896 hrs · 14,621 cycles

NUMBER 5 MAIN WHEEL BRAKE ASSEMBLY FOUND DAMAGED DURING POST FLIGHT WALK AROUND, MISSING PIECES OF PRESSURE PLATE AND ROTORS, CRACKED PISTON HOUSING CAUSING FLUID LEAKAGE. BRAKE SEPARATION CAUSED DAMAGE TO THE WHEEL HEAT SHIELD AND PUNCTURED WING TO BODY FAIRING. BRAKE AND WHEEL ASSEMBLY WAS REMOVED AND REPLACED AS PER B767 AMM 32-41-08 AND 32-45-01. WING TO BODY FAIRING WAS TEMPORARILY REPAIRED IN ACCORDANCE WITH AIR TRANSPORT INTERNATIONAL ENGINEERING ORDER 53-767-8485 REV. IR.

Part: BATTERY PACK — INOPERATIVE (AFT FLASHLIGHT) · airframe 103,372 hrs · 22,421 cycles

POST FLIGHT, FLASHLIGHT AFT OF P-61 PANEL INOPERATIVE. INITIATED DEFERRAL MAINTENANCE ITEM 21097 IAW MEL 25-63-04-01 CAT C NO FLY DATE 03/12/2021. REMOVED AND REPLACED BATTERY IN EMERGENCY FLASHLIGHT NEXT TO P-61 IAW AMM 25-60-00. OPERATIONAL CHCECK SATISFACTORY. DEFERRAL MAINTENANCE ITEM CLEAR.