N714AX

Part: PUMP — DAMAGED (OIL SCAVANGE) · airframe 90,152 hrs · 28,280 cycles

DESCENT THRU FL190, OIL PSI RT ENGINE DECREASING. ENG NEAR IDLE & SHUTDOWN BEFORE OIL WENT TO 0. SINGLE ENG APPR & LDG PROCEDURES COMPLIED WITH. DECLARED EMERGENCY. OIL PSI AT 6 PSI AT SHUTDOWN & #2 ENG WINDMILLED APROX 7 MIN. LANDING UNEVENTFUL. ACFT RFS. ENGINEERING REQUESTED DOWNLOAD OF DFDR. MX REQUESTED DFDR REVIEW OF NO OIL PSI DURATION OF OPS. NO OIL PSI IAW AMM 72-00-00, FOUND MANIFOLD OIL LINE DAMAGED, OIL LINE R & R. OPS & LEAK CHECKED GOOD. MX FOUND RT ENG MISSING A CLAMP FOR IDG WIRING & 1 IDG FEEDER CABLE CHAFED. NEW CLAMP INSTALLED & CABLE REPAIRED IAW AMM 20-11-00 & SWPM 20-30-13. CHECKED IDG IAW AMM 24-11-00, GOOD. ANALYSIS OF DFDR CONFIRMED OIL SYS OPS AT IDLE FOR 28 SEC BELOW 10 PSI. OIL PSI INSP IAW AMM 72-00-00. NO FAULTS. BORESCOPE INSP, GOOD. AIRCRAFT RELEASED TO SERVICE. ORIG SUB DATE: 11-01-2022.

Part: VENT — CRACKED (ZONE 400) · airframe 89,334 hrs · 27,843 cycles

CORE COWL VENT CRACKED

Part: THRUST REVERSER — CRACKED (ZONE 400) · airframe 89,334 hrs · 27,841 cycles

THRUST REVERSER TRAILING EDGE CRACKED

Part: THRUST REVERSER — CHAFED (ZONE 600) · airframe 89,334 hrs · 27,843 cycles

#2 ENGINE OUTBD THRUST REVERSER HAS A GOUGE AT THE 12 O'CLOCK POSITION

Part: THRUST REVERSER — GOUGED (ZONE 400) · airframe 89,334 hrs · 27,843 cycles

THRUST REVERSER HAS GOUGE ON INTERNAL FAIRING

Part: SUPPORT ANGLE — CRACKED (LT SLAT TRACK) · airframe 89,334 hrs · 27,843 cycles

#6 SLAT LOWER EDGE HAS A CRACKED SUPPORT ANGLE. LOCATED BETWEEN THE CENTER AND THE OUTBD AUX TRACK

Part: BRACKET — CRACKED (ZONE 400) · airframe 89,334 hrs · 27,843 cycles

BRACKET CRACKED ON SKIRT FAIRING

Part: COWL LATCH — WORN (ZONE 400) · airframe 89,334 hrs · 27,843 cycles

CORE COWL AFT LATCH HAS WEAR

Part: THRUST REVERSER — BENT (ZONE 400) · airframe 89,334 hrs · 27,843 cycles

THRUST REVERSER TRAILING EDGE BENT

Part: SLEEVE — WORN (ZONE 400) · airframe 89,334 hrs · 27,843 cycles

#1 ENGINE EXHAUST SLEEVE HAS A HOLE WORN ON THE LEADING EDGE AT 7 O'CLOCK POSITION

Part: SLEEVE — DETERIORATED (ZONE 400) · airframe 89,334 hrs · 27,843 cycles

#1 ENGINE EXHAUST SLEEVE LEADING EDGE WEAR COATING CHIPPED AND DETERIORATED.

Part: COWLING — CHAFED (ZONE 400) · airframe 89,334 hrs · 27,843 cycles

LOWER CLOSE OUT CHANNEL CHAFED IN MULTI AREAS WHERE STOP PADS MATE UP ON #1 ENGINE O/B CORE COWL LOWER END

Part: NONE — CRACKED (ZONE 400) · airframe 89,334 hrs · 27,843 cycles

#1 ENGINE I/B CORE COWL UPPER LOUVER EXHAUST ON AFT FLANGE CRACKED

Part: TORQUE TUBE — CORRODED (ZONE 600) · corrosion level 2 · airframe 89,344 hrs · 27,843 cycles

RH FLAP IB TORQUE TUBE PITTED

Part: PANEL — CORRODED (ZONE 100) · airframe 89,334 hrs · 27,843 cycles

ALC PANEL SUPPORT ON BILGE PANEL RBL16 AT STATION 1281 CORRODED

Part: FLOOR PANEL — CRACKED (ZONE 100) · airframe 89,344 hrs · 27,843 cycles

FLOOR PANEL 122C CRACKED

Part: SEAL BRACKET — CRACKED (ZONE 400) · airframe 89,334 hrs · 27,843 cycles

FAN COWL SEAL RETAINER BRACKET CRACKED

Part: BEAM — CORRODED (ZONE 600) · corrosion level 2 · airframe 89,334 hrs · 27,843 cycles

R/W TRAILING EDGE FLAP #8 SUPPORT 1-2-3 BEAM HAS TWO FASTENERS COMMON TO THE SIDE BRACE ATTACH FITTING WITH DEFECT INDICATION WITH HFEC HOLE SCAN

Part: SUPPORT BRACKET — CORRODED (ZONE 100) · corrosion level 2 · airframe 89,334 hrs · 27,843 cycles

L/H BILGE PANEL SUPPORT BRACKET (L-2) AT STA 1270 CORRODED

Part: TORQUE TUBE — WORN (ZONE 600) · corrosion level 2 · airframe 89,334 hrs · 27,843 cycles

RH I/B FLAP TORQUE TUBE REQUIRES REMOVAL FOR INSPECTION IAW J/C ATI-57-793-12-02 #5 TORQUE TUBE FOUND TO BE PITTED AND WORN

Part: TORQUE TUBE — WORN (ZONE 500) · corrosion level 2 · airframe 89,334 hrs · 27,843 cycles

L/H I/B FLAP #4 TORQUE TUBE FOUND PITTED AND WORN BEYOND LIMITS

Part: RETAINER SEAL — CRACKED (ZONE 600) · airframe 89,334 hrs · 27,843 cycles

I/B FLAP FAIRING 671FB INSIDE O/B SEAL RETAINER CRACKED

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 87,831 hrs · 27,112 cycles

MULTIPLE EMERGANCY EXIT SIGN LIGHTS INOPERATIVE. AIRCRAFT GROUNDED FOR UNSCHEDULED MAINTENANCE. REMOVED AND REPLACED BATTERY PACK IAW BOEING 767 AMM 33-51-07. OPERATIONAL CHECK SATISFACTORY. AIRCRAFT RELEASED TO SERVICE.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHT) · airframe 87,804 hrs · 27,100 cycles

DURING SERVICE CHECK, FOUND LEFT ENTRY DOOR EXIT SIGN LIGHT NOT ON WITH FLIGHT DECK EMERGENCY LIGHT SWITCH IN THE ON POSITION. TROUBLESHOT IAW B767 IAI WDM 33-51-11 & 33-51-13, IDENTIFIED CRACKED PIN IN FEMALE END CONNECTOR D1084 PIN 2 CAUSING INTERMITTENT FUNCTION OF SYSTEM. REMOVED AND REPLACED PIN 2 OF C/P D1084 PER BOEING SWPM 20-16-00 & 767 IAI WDM 33-51-11 & 33-51-13. OPERATIONAL CHECK SATISFACTORY. NO FURTHER DEFECTS NOTED.

Part: WARNING MESSAGE — ILLUMINATED (L1 DOOR) · airframe 87,072 hrs · 26,848 cycles

PRE-DEPARTURE: CREW REPORTS L1 DOOR INDICATION AFTER ENGINE START. AIRCRAFT GROUNDED FOR UNSCHEDULED MAINTENANCE, WORK IN PROGRESS.

Part: BRACKET — CRACKED (LT COWLING) · airframe 85,819 hrs · 26,355 cycles

L/H AFT PRECOOLER MOUNT BRACKET CRACKED VIEWED BENEATH #2 L/H CORE COWL. REMOVED AND REPLACED L/H AFT PRECOOLER MOUNT BRACKET IAW B767 SRM 51-40-02 PARA 9 AND IAW 47404FAB04.

Part: MOUNT BRACKET — GOUGED (NR 2 NACELLE) · airframe 85,834 hrs · 26,361 cycles

AIRCRAFT GROUNDED FOR C-CHECK-24. IN COMPLIANCE OF TASK CARD ATI-54-408-00-02 " GVI - EXTERNAL - NO. 2 NACELLE STRUT" LEFT AFT PRECOOLER MOUNT BRACKET CRACKED VIEWED BENEATH #2 LEFT CORE COWL. REMOVED AND REPLACED LEFT AFT PRECOOLER MOUNT BRACKET IAW B767 SRM 51-40-02

Part: TEE FITTING — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 85,819 hrs · 26,355 cycles

CORROSION ON INTERIOR "T" SECTION OF ALC DOOR 10" FROM AFT EDGE, 24" FROM TOP EDGE.REMOVED AND REPLACED INTERIOR "T" SECTION OF ALC 3RD FROM TOP USING 140T2604-3 IAW BOEING DWG# 140T2604.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 85,834 hrs · 26,361 cycles

AIRCRAFT GROUNDED FOR CHECK-C24. IN COMPLIANCE OF TASK CARD ATI-53-572-00-01 "GVI - INTERNAL - BULK CARGO COMPARTMENT BULK FLOOR SUPPORT" F.S. 1417 HAS CORROSION ALONG LENGTH OF THE SUPPORT TOP SIDE. REMOVED AND INSTALLED "Z" BEAM IAW BOEING DWG 452T3260 REV E AND B767 SRM 51-40-05.

Part: WEB — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 85,819 hrs · 26,355 cycles

ALC DOOR HAS LIGHT CORROSION AT INTERIOR PANEL MOUNTING SCREW LOCATIONS.REPLACED SKIN ON ALC DOOR IAW B767 51-40-02 PAR 4 BOEING DWG 140T2640 AND DOC 47404FAB02

Part: SKIN — CORRODED (DOOR) · corrosion level 2 · airframe 85,834 hrs · 26,361 cycles

AIRCRAFT GROUNDED FOR C-CHECK-24. IN COMPLIANCE OF TASK CARD ATI-20-073-00-01, ALC DOOR HAS LIGHT CORROSION AT INTERIOR PANEL MOUNTING SCREW LOCATIONS. REPLACED SKIN ON ALC DOOR IAW B767 51-40-02 PAR 4 BOEING DWG 140T2640 AND DOC 47404FAB02.

Part: WEB — BROKEN (NR 2 PYLON) · airframe 85,834 hrs · 26,361 cycles

AIRCRAFT GROUNDED FOR C-CHECK-24. IN COMPLIANCE OF TASK CARD ATI-20-105-00-01 "DET - FORWARD NACELLE STRUT FAIRING - NACELLE 2 (EZAP)" THE FOLLOWING FINDINGS WERE NOTED: NUMBER 2 PYLON - WEB AND BRACKET WHICH THE NOSE COWL ANTI-ICE DUCT ATTACHES TO AT FORWARD END OF PYLON AT PASS THRU ARE WORN/BROKEN. REMOVED/INSTALLED WORN BRACKET IAW B767 SRM 51-40-02. REMOVED/INSTALLED WEB AS DIRECTED REPAIR ENGINEERING ORDER-47404FAB01 ON #2 PYLON FWD END.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 85,819 hrs · 26,355 cycles

STRINGER SPLICE AT STA. 434 S31R CORRODED.REMOVED AND REPLACED CORRODED SPLICE AT STA 434 S31R IAW B767 SRM 51-40-02.

Part: WEB — CRACKED (NR 2 PYLON) · airframe 85,819 hrs · 26,355 cycles

NUMBER 2 PYLON - WEB AND BRACKET THAT NOSE COWL ANTI-ICE DUCT ATTACHES TO AT FORWARD END OF PYLON AT PASS THRU ARE WORN/BROKEN.REPLACE WORE BRACKET IAW B767 SRM 51-40-02, NEW WEB REPLACEMENT DONE ON AMES REA 47404FAB01 ON #2 PYLON FWD END.

Part: SKIN — CRACKED (FUSELAGE) · airframe 85,834 hrs · 26,361 cycles

AIRCRAGT GROUNDED FOR C-CHECK-24. IN COMPLIANCE OF TASK CARD ATI-53-730-00-02 "GVI - EXTERNAL - EXTERIOR SECTION 48 - RIGHT SIDE", THE FOLLOWING FINDINGS WERE NOTED: AFT RIGHT EXTERIOR FUSELAGE SKIN IS CRACKED STA 1654.5 BETWEEN STRINGERS 4R-5R. REPAIRED EXTERIOR FUSELAGE SKIN STA 1654.5 S3R-S8R IAW B767 SRM 53-80-01.

Part: SKIN — CRACKED (FUSELAGE) · airframe 85,819 hrs · 26,355 cycles

AFT R/H EXTERIOR FUSELAGE SKIN IS CRACKED STA 1654.5 BETWEEN STRINGERS 4R-5R. (VERIFIED WITH HFEC SURFACE SCAN).REPAIRED EXTERIOR FUSELAGE SKIN STA 1654.5 S3R-S8R IAW B767 SRM 53-80-01 REPAIR 4.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 85,834 hrs · 26,361 cycles

AIRCRAFT GROUNDED FOR CHECK-C-24.IN COMPLIANCE OF TASK CARD ATI-53-454-00-01,"GVI - INTERNAL - BULK CARGO COMPARTMENT" FLC - CORROSION ON STRINGER 31R AT STA.412. REPAIRED STRINGER 31R STA 412-434 IAW B767 SRM 53-00-03 REPAIR 2.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 85,834 hrs · 26,361 cycles

AIRCRAFT GROUNDED FOR CHECK-C24. IN COMPLIANCE OF TASK CARD ATI-53-454-00-01, "GVI - INTERNAL - BULK CARGO COMPARTMENT" THE FOLLOWING FINDINGS WERE NOTED: FLC - CORROSION ON STRINGER 32R JUST FORWARD OF STA.434. REPAIRED STRINGER 32R STA. 412-434 IAW B767 SRM 53-00-03 REPAIR 2

Part: SLAT — BULGED (WING) · airframe 85,834 hrs · 26,361 cycles

AIRCRAFT GROUNDED FOR C-CHECK 24. IN COMPLIANCE OF TASK CARD ATI-57-806-00-02, "GVI - ZONAL - INBOARD SLAT NO. 7" THE FOLLOWING FINDINGS WERE NOTED: 7 SLAT - LOWER LEADING EDGE HAS BULGE 93 INCHES FROM OUTBOARD END AND 7 INCHES FROM TRAILING EDGE.

Part: SLAT — CORRODED (RT WING) · corrosion level 2 · airframe 85,819 hrs · 26,355 cycles

NUMBER 7 SLAT - LOWER LEADING EDGE HAS BULGE 93 INCHES FROM OUTBOARD END AND 7 INCHES FROM TRAILING EDGE.REPAIRED #7 SLAT LOWER LEADING EDGE IAW REA# 47404REA02

Part: FAILSAFE — CRACKED (BS 955) · airframe 81,544 hrs · 24,928 cycles

RIGHT WING FAILSAFE STRAP AT WS 955, REAMED HOLES IAW SRM 51-40-02. LOWER HOLE DAMAGE EXTENDED BEYOND ALLOWABLE LIMITS AND WAS REPAIRED IAW 47317REA01.

Part: BULKHEAD — DENTED (BS 1582) · airframe 81,544 hrs · 24,928 cycles

AFT PRESSURE BULKHEAD WAS FOUND DENTED. REPAIRED THE BULKHEAD IAW REA 47317, REA 05, REV IR.

Part: SKIN — BULGED (BS 462) · airframe 81,544 hrs · 24,928 cycles

BULGING FUSELAGE SKIN BS 462, STRINGER 23R. REMOVED DAMAGE AND REPAIRED IAW SRM 53-00-01, REPAIR 1.

Part: SEAT TRACK — CRACKED (BS 172-196) · airframe 81,544 hrs · 24,928 cycles

FIRST OFFICER'S RIGHT FORWARD SEAT TRACK WAS CRACKED. REMOVED AND REPLACED THE SEAT TRACK IAW IAW AMM 25-11-01-822-095-001

Part: FAILSAFE — CRACKED (BS 955) · airframe 81,544 hrs · 24,928 cycles

LT FAILSAFE STRAP LOWER HOLE COMMON TO THE TEE FITTING CRACKED. THE FAILSAFE WAS REPAIRED.

Part: ESCAPE REEL — INOPERATIVE (NR 7) · airframe 79,980 hrs · 24,353 cycles

EMERGENCY DESCENT DEVICE NUMBER 7 IN THE SUPERNUMERARY AREA WILL NOT EXTEND. REMOVED AND REPLACED THE EMERGENCY DESCENT DEVICE IAW 25-61-03. ACFT RELEASED TO SERVICE.

Part: ESCAPE REEL — FAILED (CABIN) · airframe 79,919 hrs · 24,331 cycles

EMERGENCY DESCENT DEVICE NUMBER 1 IN THE SUPERNUMERARY AREA WILL NOT EXTEND. REMOVED AND REPLACED EMERGENCY DESCENT DEVICE IAW MMS 25-61-03.

Part: ESCAPE REEL — FAILED (NR 5) · airframe 79,980 hrs · 24,353 cycles

EMERGENCY DESCENT DEVICE NUMBER 5 PARTIALLY EXTENDED. REMOVED AND REPLACED THE EMERGENCY DESCENT DEVICE IAW MMS 25-61-03. AIRCRAFT RELEASED TO SERVICE.

Part: PUMP — INOPERATIVE (HYDRAULIC SYS) · airframe 79,150 hrs · 24,003 cycles

ON APPROACH SELECTED FLAPS 1. FLAPS WENT TO 1, EICAS MESSAGE CENTER HYDRAULIC SYS PRESS ANNUNCIATED. ON STATUS PAGE C HYD QTY READ 0. DURING THE ALTERNATE FLAP EXTENSION THE CAUTION AURAL BEEPER SOUNDED AND EICAS MESSAGE APPEARED "L/E SLAT DISAGREE AND T/E FLAP DISAGREE." THE SITUATION COULD NOT BE CORRECTED WITH ACCEPTABLE RESULTS. "ALL FLAPS AND SLATS UP LANDING CHECKLIST" COMPLIED WITH. FLIGHT 3001 COMPLETED THE CHECKLIST AND LANDED WITH NO FURTHER DIFFICULTIES. CFR CHECKED THE AIRCRAFT OVER BEFORE THE ACFT WAS RELEASED TO GROUND HANDLERS AND MX. ACFT TOWED OFF THE RUNWAY AND TO THE RAMP. AIRCRAFT GROUNDED FOR UNSCHEDULED MAINTENANCE. FOUND RAM AIR TURBINE MODULE CHECK VALVE CAP BLOWN OFF. REMOVED AND REPLACED HYDRAULIC PUMP MODULE IAW AMM 29-21-11. OPERATIONAL AND LEAK CHECK SATISFACTORY IAW AMM 29-21-00. FLAP ALTERNATE POWER DRIVE TEST COMPLIED WITH IAW AMM 27-51-00. NO FURTHER DEFECTS NOTED. AIRCRAFT RELEASED TO SERVICE.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 77,822 hrs · 23,493 cycles

FLIGHT DECK EMER FLASH LIGHT INDICATOR LED DOES NOT FLASH. R & R EMER FLASHLIGHT BATTERY. OPERATIONAL CHECKED SATISFACTORY. FAULT NOT DUPLICATED.

Part: FRAME — CORRODED (FUSELAGE) · airframe 77,815 hrs · 23,491 cycles

LEFT FRAME 883.15 IS CRACKED ON AFT LOWER SIDE, AT STUD BEAM BELOW CARGO DECK. REPAIRED IAW EO 53-767-4907.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 77,815 hrs · 23,491 cycles

CORROSION UNDER NUTPLATE ON LOWER FLOORBEAM CHORD, AT STATION 1263, RBL 26 IN AREA OF PDU ATTACH BOLT. R & R FLOORBEAM IAW AMM 25-53-01, SRM 51-40-02, 51-40-03 & 51-20-01. BEAM FABRICATED IAW REA 47206FAB01.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 77,815 hrs · 23,491 cycles

STATION 642, STRINGER 32R, DOOR SILL CHORD CORRODED. BLENDED CORROSION ON DOOR SILL CHORD IAW SRM 53-00-15. REPAIRED LOWER SILL OUTER CHORD IAW SRM 51-70-12.

Part: SUPPORT BEAM — CORRODED (RT WING) · corrosion level 2 · airframe 77,815 hrs · 23,491 cycles

RIGHT WING NR 7 FLAP SUPPORT, 1-2-3 BEAM HAS CORROSION IN ONE EACH FASTENER. REPAIRED RT WING NR 7 FLAP SUPPORT, 1-2-3 BEAM IAW REA 47206REA02.

Part: SUPPORT BEAM — CORRODED (RT WING) · corrosion level 2 · airframe 77,815 hrs · 23,491 cycles

RIGHT WING NR 8 FLAP SUPPORT, 1-2-3 BEAM HAS CORROSION IN TWO EA FASTENERS. REPAIRED RT WING NR 8 FLAP SUPPORT IAW REA 47206REA03.

Part: SUPPORT — CORRODED (RT WING) · corrosion level 2 · airframe 77,382 hrs · 18,660 cycles

RIGHT WING OTBD FLAP NR 8 SUPPORT, OTBD RIB ACTUATOR BORE HAS EDGE PITTING AT 3 LOCATIONS ON THE INBD BORE & 1 LOCATION ON THE OTBD BORE. RT WING OTBD FLAP NR 8 SUPPORT BORE REPAIRED IAW REQUEST FOR ENGINEERING DOCUMENT 47206REA04.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 77,815 hrs · 23,491 cycles

STATION 752, STRINGER 34L, CORRODED AT DOME NUT. REPAIRED STRINGER 34L IAW SRM 53-00-03.

Part: STRUCTURE — CRACKED (NR 1 PYLON) · airframe 77,815 hrs · 23,491 cycles

NUMBER 1 PYLON OTBD HYD BAY DOOR, ACCESS CUT OUT FWD LOWER CORNER STRUCTURE, INSIDE CRACKED & WORN. R & R NR 1 PYLON OTBD HYD BAY DOOR , ACCESS CUT OUT FWD LOWER CHORD IAW SRM 51-40-02 & DWG 313T1300.