N389AZ

Part: POUCH — TORN (ZONE 200) · airframe 116,919 hrs · 24,026 cycles

UPPER EMERGENCY ESCAPE HARNESS POUCH TORN. TIME LIMITED ITEM 67991 INITIATED. DUE 04 MARCH 2026. REMOVED AND REPLACED UPPER EMERGENCY ESCAPE HARNESS POUCH IAW SRM 51-40-02. DEFERRAL 67991 CLEARED.

Part: COVER — DELAMINATED (NR 2 NACELLE) · airframe 113,947 hrs · 22,812 cycles

FIBERGLASS COVER SEPARATING #2 ENGINE.

Part: SKIN — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 113,947 hrs · 22,812 cycles

RW OB FLAP CORRODED

Part: SKIN — CRACKED (ZONE 100) · airframe 113,947 hrs · 22,812 cycles

FUSELAGE SKIN AT L1 DOOR LOWER AFT CORNER IS CRACKED.

Part: WEB — CRACKED (CARGO) · airframe 113,947 hrs · 22,812 cycles

FLC CARGO ROLLER RAIL AUX WEB CRACKED

Part: INTERCOSTAL — CRACKED (RT WING LE) · airframe 113,947 hrs · 22,812 cycles

RW LEADING EDGE INTERCOSTAL CRACKED.

Part: SKIN — CRACKED (NR 1 NACELLE) · airframe 113,947 hrs · 22,812 cycles

#1 ENGINE INBOARD CORE COWL OUTER SKIN CRACKED.

Part: STRAP — CRACKED (NR 1 NACELLE) · airframe 113,947 hrs · 22,812 cycles

#1 ENGINE AFT PYLON ATTACH STRAP CORRODED.

Part: BEAM — CORRODED (AFT CARGO) · corrosion level 2 · airframe 113,947 hrs · 22,812 cycles

AFT LOWER CARGO DOOR BEAM CORRODED.

Part: STIFFENER — CRACKED (NLG WW) · airframe 113,947 hrs · 22,812 cycles

NOSE WHEEL WELL VERTICAL CHORD.

Part: SKIN PANEL — DELAMINATED (VERTICAL STAB) · airframe 113,947 hrs · 22,812 cycles

VERTICAL STAB. SKIN PANEL DELAMINATED.

Part: DOOR FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 113,947 hrs · 22,812 cycles

ALC DOOR FRAME HAS 4 EACH NUTPLATE HOLES WITH CORROSION

Part: FRAME — CORRODED (BS 1197 S33-34R) · corrosion level 2 · airframe 113,947 hrs · 22,812 cycles

ALC STATION 1197 FRAME CAP HAS CORROSION ON UNDERSIDE OF LIP STR 34R AND 33R

Part: FRAME — CORRODED (BS 1197) · corrosion level 2 · airframe 113,947 hrs · 22,812 cycles

ALC STATION 1197+88 FRAME CAP CORROSION UNDERSIDE OF LIP ABOVE STR 33R

Part: CHANNEL — CRACKED (HORIZONTAL STAB) · airframe 113,947 hrs · 22,812 cycles

RIGHT HAND HORZ STAB PANEL 347AR MOUNTING BRACKET CRACKED

Part: FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 113,947 hrs · 22,812 cycles

ALC STA 1153 RT SIDE FRAME CAP CORRODED

Part: TRAY — CRACKED · airframe 113,947 hrs · 22,812 cycles

FLC 10R PDU TRAY CRACKED

Part: STRINGER — CORRODED (BS 1219 S39R) · corrosion level 2 · airframe 113,947 hrs · 22,812 cycles

ALC STRINGER 39R CORRODED AT STA 1219

Part: SKIN — DELAMINATED (HORIZONTAL STAB) · airframe 113,947 hrs · 22,812 cycles

LEFT HORZ UPPER SKIN PANEL DELAMINATED ON INNER SURFACE

Part: SKIN — CRACKED (RT WING) · airframe 113,947 hrs · 22,812 cycles

RIGHT WING FIXED L/E CRACK ABOVE OUTBOARD END OF #8 SLAT

Part: SKIN — CRACKED (BS 335 S20R) · airframe 113,947 hrs · 22,812 cycles

R/H FUSELAGE SKIN AT R1 DOOR LOWER CORNER CUTOUT CRACK INDICATION STA 335, STR 20R

Part: SKIN — DELAMINATED (VERTICAL STAB) · corrosion level 2 · airframe 113,947 hrs · 22,812 cycles

VERTICAL STAB LEFT LEAFING EDGE DELAMINATED

Part: MICROPHONE — INOPERATIVE · airframe 110,356 hrs · 21,472 cycles

LEFT MIC CONTROL STUCK IN CURRENT POSITION. UNABLE TO TRANSMIT OR RECEIVE ON ANY RADIO AFTER AIRBORNE. AIR TURN BACK TO KILN WITH EMERGENCY DECLARATION. NO ADDITIONAL PRECAUTIONARY ACTIONS NOTED. ON ARRIVAL, AIRCRAFT GROUNDED FOR UNSCHEDULED MAINTENANCE. WORK IN PROGRESS.

Part: FAIRING — CORRODED (ZONE 400) · corrosion level 2 · airframe 110,025 hrs · 21,353 cycles

CORROSION RIGHT HAND SIDE AFT FAIRING #1 ENGINE PYLON.

Part: SKIN — DELAMINATED (ZONE 300) · airframe 110,025 hrs · 21,353 cycles

DELAMINATED AREA ON LEFT HAND VERTICAL STABILIZER LEADING EDGE AT FSS 245.0 INNER SKIN.

Part: VERTICAL BEAM — DELAMINATED (ZONE 300) · airframe 110,025 hrs · 21,353 cycles

DELAMINATED AREA ON RIGHT HAND SIDE OF VERTICAL STABILIZER AT APPROX FSS 270.784.

Part: VERTICAL BEAM — DELAMINATED (ZONE 300) · airframe 110,025 hrs · 21,353 cycles

DELAMINATED AREA ON RIFGT HAND VERTICAL STABILIZER LEADING EDGE AT APPROX FSS 195 INNER SKIN.

Part: VERTICAL BEAM — DELAMINATED (ZONE 300) · airframe 110,025 hrs · 21,353 cycles

DELAMINATED AREA ON LEFT HAND VERTICAL STABILIZER LEADING EDGE AT APPROX FSS 270 INNER SKIN.

Part: BRACKET — BROKEN (ZONE 700) · airframe 110,025 hrs · 21,353 cycles

R/H MAIN LANDING GEAR SUPPORT BEAM ACCESS PANEL SUPPORT BRACKET JUST ABOVE STRUT DOOR AFT SIDE IS BROKEN.

Part: VERTICAL BEAM — DELAMINATED (ZONE 300) · airframe 110,025 hrs · 21,353 cycles

DELAMINATED AREA ON RIGHT HAND VERTICAL STABILIZER LEADING EDGE AT APPROX FSS 245.0 INNER SKIN.

Part: SKIN PANEL — CORRODED (ZONE 500) · corrosion level 2 · airframe 110,025 hrs · 21,353 cycles

AREA OF BULGING SKIN ON LEFT HAND WING I/B FLAP LOWER SURFACE AROUND MID FLAP.

Part: TIE CLIP — CRACKED (ZONE 400) · airframe 110,025 hrs · 21,353 cycles

CRACKED ANGLE SUPPORT BETWEEN AFT AND MID TORQUE BOX #1 ENG.

Part: PYLON — CRACKED (ZONE 400) · airframe 110,025 hrs · 21,353 cycles

CRACK VERTICAL EXTRUSION UPPER SURFSCE IN MID TORQUE BOX #1 ENG PYLON LOOKING IN OUTBD MOON PANEL.

Part: TIE CLIP — CRACKED (ZONE 400) · airframe 110,025 hrs · 21,353 cycles

CRACKED ANGLE SUPPORT MID TORQUE BOX #1 ENG.

Part: BEAM — CORRODED (ZONE 500) · corrosion level 2 · airframe 110,025 hrs · 21,353 cycles

L WING UPPER SURFACE JUST FWD OF #6 SPOILER, BULGE AT SEAM BETWEEN 2 SKIN PANELS. FAS WO N389AZ-02-01 NON ROUTINE 00310

Part: BEAM — CORRODED (ZONE 600) · corrosion level 2 · airframe 110,025 hrs · 21,353 cycles

R WING UPPER SURFACE JUST FORWARD OF #7 SPOILER, BULGE AT SEAM BETWEEN 2 SKIN PANELS. FAS WO N289AZ-02-01 NON ROUTINE 00313

Part: WEB — CRACKED (ZONE 500) · airframe 110,025 hrs · 21,353 cycles

L/H WING FRONT SPAR TO FIXED L/E WEB IS CRACKED AT APPROX LES 525. FAS WO N389AZ-02-01 NON ROUTINE 00308

Part: FRAME — CRACKED (ZONE 400) · airframe 110,025 hrs · 21,353 cycles

CRACK VERTICAL EXTRUSION UPPER SURFACE IN MID TORQUEBOC #1 ENG PYLON LOOKING IN OTBD MOON PANEL. FAS WO N389AZ-02-01 NON ROUTINE 00062

Part: SUPPORT ANGLE — CRACKED (ZONE 400) · airframe 110,025 hrs · 21,353 cycles

CRACKED ANGLE SUPPORT MID TORQUE BOX #1 ENG PYLON. FAS WO N389AZ-02-01 NON ROUTINE 00063

Part: BRACKET — CRACKED (ZONE 600) · airframe 110,025 hrs · 21,353 cycles

RH WING #7 SLAT INNER SURFACE SUPPORT ANGLE AT APPROX LES 320 IS CRACKED. FAS WO N389AZ-02-01 NON ROUTINE 00072

Part: SPAR — CRACKED (LT WING) · airframe 110,025 hrs · 21,353 cycles

L/H WING FRONT SPAR TO FIXED L/E T SUPPORT IS CRACKED AT APPROX LES 500.10. FAS WO N389AZ-02-01 NON ROUTINE 00050

Part: BULKHEAD — CRACKED (ZONE 400) · airframe 110,025 hrs · 21,353 cycles

#1 PYLON AFT FAIRING PANEL #437DB HAS CRACKED BLKHD ANGLE. FAS WO N389AZ-02-01 NON ROUTINE 00045

Part: SPAR — CRACKED (ZONE 500) · airframe 110,025 hrs · 21,353 cycles

L/H WING FRONT SPAR TO FIXED L/E T SUPPORT IS CRACKED AT APPROX LES 525. FAS WO N389AZ-02-01. N/R 00049.

Part: BRACKET — CRACKED (ZONE 500) · corrosion level 2 · airframe 110,025 hrs · 21,353 cycles

LH WING #6 SLAT INNER SUPPORT ANGLE AT APPROX LES 281.12 IS CRACKED. FAS WO N389AZ-02-01 NON ROUTINE 00061

Part: BRACKET — CRACKED (ZONE 600) · airframe 110,025 hrs · 21,353 cycles

RH WING #7 SLAT INNER SURFACE SUPPORT ANGLE AT APPROX LES 295 IS CRACKED. FAS WO N389AZ-02-01 NON ROUTINE 00071

Part: NONE — NONE · airframe 109,862 hrs · 21,290 cycles

ON 19 MARCH 2022 , 389AZ FLIGHT NUMBER (ATN3569) WHILE AT FL360 AND IN CRUISE, THE AUDIBLE MASTER WARNING AND THE MAIN CARGO DOOR LIGHT INDICATED. CREW CLEARED THE WARNING, REFERENCED ATI QUICK READY HANDBOOK, RAISED TO 9500 FL AND BEGAN DESCENT TO 16,000. NO PRESSURIZATION CHANGES OR ADVERSE CONDITIONS NOTED. ATI OPS VIA AIRINC ADVISED AIR TURN BACK TO DESTINATION STATION. AFTER INITIATING RETURN, WARNING EXTINGUISHED AT 16,000 AND REMAINED OFF. LANDING WAS UNEVENTFUL WITH NO ADDITIONAL PRECAUTIONARY ACTIONS NOTED. ON ARRIVAL AIRCRAFT GROUNDED FOR UNSCHEDULED MAINTENANCE. WORK IN PROGRESS.

Part: NONE — NONE · airframe 109,716 hrs · 21,255 cycles

MAIN CARGO DOOR WARNING INDICATION AT 340 FLIGHT LEVEL WITH NO LOSS OF PRESSURIZATION. AIR TURN BACK TO DEPARTURE STATION-KILN. EMERGENCY DESCENT WAS UNEVENTFUL WITH NO ADDITIONAL PRECAUTIONARY ACTIONS. ON ARRIVAL AIRCRAFT WAS GROUNDED FOR INSPECTION. GENERAL VISUAL INSPECTION OF THE MAIN CARGO DOOR SATISFACTORY. NO FAULTS NOTED. INITIATED DEFERRAL MAINTENANCE ITEM-29314 MEL CAT C. POST FLIGHT, CREW REPORTED NO SYSTEM FAULT INDICATIONS FOR REMAINDER OF FLIGHT. OPERATIONAL CHECK OF THE MAIN CARGO DOOR INDICATION AND CONTROL SWITCHES IAW IAI SMM 52-32-00 GOOD. FAULT NOT DUPLICATED. SECURITY AND INTEGRITY OF WIRING AND TARGETS AT EACH MOUNT AREA OF MAIN CARGO DOOR LOCK INDICATION AND HOOK LATCH SATISFACTORY. WITH PRESSURIZATION MAIN CARGO DOOR INDICATION SYSTEM TEST PER B767 AMM 52-71-09 SATISFACTORY. FAULT NOT DUPLICATED. DEFERRAL MAINTENANCE ITEM 29314 CLEARED.

Part: SPLICE PLATE — DAMAGED (LT WING LE) · airframe 64,104 hrs · 24,834 cycles

NON-ROUTINE 3018.0330 DISCREPANCY: LEFT WING LEADING EDGE LOWER STRUCTURE AT WS 416 BENT AND CRACKED. CORRECTIVE ACTION: REPAIRED LEFT WING LEADING EDGE LOWER STRUCTURE AT WS 416 IAW EO NR 20449-1 WITHOUT ANY DEVIATIONS.