N714AX
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
PRE-FLIGHT CREW REPORTED L1 ENTRY DOOR CAME OFF TRACKS. ADJUSTED L1 ENTRY DOOR INTO CORRECT POSITION OF TRACK IAW B767 AMM 52-11-00.
CENTER HYDRAULIC PRESSURE EICAS ON APPROACH. QUANTITY IN CENTER REACHED 0.08. ALTERNATE FLAP AND GEAR EXTENSION ENGAGED. HYDRAULIC QTY WAS FULL AT TOP OF DESCENT AND EMPTY WHEN FLAPS 5 SELECTED. DUE TO IRREGULAR OPERATIONS CREW ELECTED AN EMERGENCY DESCENT. LANDING WAS WITHOUT INCIDENT AND NO ADDITIONAL PRECAUTIONARY ACTIONS. ON ARRIVAL, AIRCRAFT WAS GROUNDED FOR UNSCHEDULED MAINTENANCE. WORK IN PROGRESS
FOUND COCKPIT EMERGENCY FLASHLIGHT INOPERATIVE. REMOVED AND REPLACED FLASHLIGHT IAW B767 AMM 25-05-03. OPERATIONAL CHECK GOOD.
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.
CORE COWL VENT CRACKED
CORE COWL AFT LATCH HAS WEAR
BRACKET CRACKED ON SKIRT FAIRING
THRUST REVERSER TRAILING EDGE BENT
THRUST REVERSER HAS GOUGE ON INTERNAL FAIRING
#6 SLAT LOWER EDGE HAS A CRACKED SUPPORT ANGLE. LOCATED BETWEEN THE CENTER AND THE OUTBD AUX TRACK
#2 ENGINE OUTBD THRUST REVERSER HAS A GOUGE AT THE 12 O'CLOCK POSITION
THRUST REVERSER TRAILING EDGE CRACKED
#1 ENGINE EXHAUST SLEEVE LEADING EDGE WEAR COATING CHIPPED AND DETERIORATED.
#1 ENGINE I/B CORE COWL UPPER LOUVER EXHAUST ON AFT FLANGE CRACKED
#1 ENGINE EXHAUST SLEEVE HAS A HOLE WORN ON THE LEADING EDGE AT 7 O'CLOCK POSITION
LOWER CLOSE OUT CHANNEL CHAFED IN MULTI AREAS WHERE STOP PADS MATE UP ON #1 ENGINE O/B CORE COWL LOWER END
RH FLAP IB TORQUE TUBE PITTED
ALC PANEL SUPPORT ON BILGE PANEL RBL16 AT STATION 1281 CORRODED
FLOOR PANEL 122C CRACKED
FAN COWL SEAL RETAINER BRACKET CRACKED
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
L/H BILGE PANEL SUPPORT BRACKET (L-2) AT STA 1270 CORRODED
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
L/H I/B FLAP #4 TORQUE TUBE FOUND PITTED AND WORN BEYOND LIMITS
I/B FLAP FAIRING 671FB INSIDE O/B SEAL RETAINER CRACKED
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.
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.
PRE-DEPARTURE: CREW REPORTS L1 DOOR INDICATION AFTER ENGINE START. AIRCRAFT GROUNDED FOR UNSCHEDULED MAINTENANCE, WORK IN PROGRESS.
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
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.
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.
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
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.
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.
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.
STRINGER SPLICE AT STA. 434 S31R CORRODED.REMOVED AND REPLACED CORRODED SPLICE AT STA 434 S31R IAW B767 SRM 51-40-02.
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.
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.
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.
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
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.
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.
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
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.
AFT PRESSURE BULKHEAD WAS FOUND DENTED. REPAIRED THE BULKHEAD IAW REA 47317, REA 05, REV IR.
BULGING FUSELAGE SKIN BS 462, STRINGER 23R. REMOVED DAMAGE AND REPAIRED IAW SRM 53-00-01, REPAIR 1.
FIRST OFFICER'S RIGHT FORWARD SEAT TRACK WAS CRACKED. REMOVED AND REPLACED THE SEAT TRACK IAW IAW AMM 25-11-01-822-095-001
LT FAILSAFE STRAP LOWER HOLE COMMON TO THE TEE FITTING CRACKED. THE FAILSAFE WAS REPAIRED.
EMERGENCY DESCENT DEVICE NUMBER 5 PARTIALLY EXTENDED. REMOVED AND REPLACED THE EMERGENCY DESCENT DEVICE IAW MMS 25-61-03. AIRCRAFT RELEASED TO SERVICE.
EMERGENCY DESCENT DEVICE NUMBER 1 IN THE SUPERNUMERARY AREA WILL NOT EXTEND. REMOVED AND REPLACED EMERGENCY DESCENT DEVICE IAW MMS 25-61-03.
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.
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.
FLIGHT DECK EMER FLASH LIGHT INDICATOR LED DOES NOT FLASH. R & R EMER FLASHLIGHT BATTERY. OPERATIONAL CHECKED SATISFACTORY. FAULT NOT DUPLICATED.
LEFT FRAME 883.15 IS CRACKED ON AFT LOWER SIDE, AT STUD BEAM BELOW CARGO DECK. REPAIRED IAW EO 53-767-4907.
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.
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.
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.
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.
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.
STATION 752, STRINGER 34L, CORRODED AT DOME NUT. REPAIRED STRINGER 34L IAW SRM 53-00-03.
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.