N251AZ
Registered owner: CARGO AIRCRAFT MANAGEMENT INC, OH (owner ≠ operator)
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
REJECTED TAKE OFF DUE TO LOW SPEED REJECT 60 AND 65 KNOTS. LOST BOTH EICAS SCREENS. STANDBY ENG BACKUP DID NOT WORK. ENG OIL PRESSURE ON LT SIDE REACHED RED LINE. ENGINE OIL TEMP ON LT SIDE REACHED 83 AND RT SIDE -16. EICAS MESSAGE DISAGREE STANDBY INVERTER OIL TEMP INDICATOR ON RT SIDE TEMPORARILY BLANKED. CREW DID NOT DECLARE EMERGENCY. ACFT WAS GROUNDED FOR INSPECTION AND MAINT. FOUND ALL INDICATIONS TO BE IN NORMAL CONFIGURATION AT BLOCK IN. LT EICAS FOUND EICAS DISAGREE & STANDBY INVERTER. RT EICAS HAD EICAS DISAGREE ONLY. CLEARED MESSAGES AND BIT BOTH EICAS NO CODES DISPLAYED. CLEANED WATER FOUND IN GALLEY AND IN E&E BAY. CLEANED ALL WATER IN GALLEY & TRAY. TIGHTENED LOOSENED SCREW IN TRAY ALLOWING WATER TO SEEP DOWN. WATER FOUND UNDER LT EICAS COMPUTER. CLEANED WATER & CONDENSATION. R & R LT EICAS COMPUTER. OPS CHKD GOOD. HIGH POWER ENG RUN NOTED NO FAULTS. ALL WORK ACCOMPLISHED IAW FIM 31-41 FAULT TREE 808, AMM 31-41-02, AMM 24-33-03, AMM 20-60-07, B767 AMM 20-60-06
ONE INERTIAL ESCAPE REEL FELL FROM STORED POSITION. PLACED ON DEFERRAL 71291 MINIMUM EQUIPMENT LIST ATI-25-61-01-01. DUE 18 MARCH 2026. INSTALLED NEW DESCENT DEVICE IN ACCORDNACE WITH IAI B767 AMM 25-61-03. DEFERRAL 71291 CLEARED.
1 CRACK FOUND ON THE R1 DOOR CUTOUT AFT CORNER 2ND FASTENER HOLE FROM THE BOTTOM, .CRACK TO BE IN EXTERNAL SKIN ONLY.
FRAME INNER CHORD IS CRACKED IN THE TRANSITION RADIUS STUB BEAM STA 903.5 RIGHT SIDE
BONDED PANEL ON RIGHT SIDE OF VERTICAL STAB DELAMINTED AT FSS.295
WING L/E HAS CRACK AT SLAT TRACK CUT OUT AFT OF #4 SLAT
LARGE BONDED PANEL ON L/H SIDE OF VERTICAL HAS DELAMINATION AT FSS 295
WING L/E HAS CRACK AT SLAT TRACK CUT OUT AFT OF #4 SLAT
#2 PYLON INTERNAL I/B UPPER ANGLE CRACKED, SEEN THRU ACCESS HOLE 446AL..
MAINTENANCE FOUND INTERIAL ESCAPE REEL, THIRD FROM FORWARD AT L1 DOOR FELL OUT. SYSTEM DEFERRED 64323, MEL CATEGORY C INITIATED. SYSTEM DEFERRED 64323, MEL CATEGORY C INITIATED. INSTALLED L1 DOOR INERTIA ESCAPE REEL IAW B767 AMM 25-61-05. NO OTHER DEFECTS NOTED. DEFERRAL 64323 CLEARED.
ENROUTE FROM KBWI TO KSBD, CREW REPORTED LT ENG FILTER EICAS MESSAGE. CREW ELECTED A LT ENG SHUTDOWN FOLLOWED BY A DIVERSION WITH AN EMERGENCY DECLARATION TO KDEN. LANDING WAS WITHOUT INCIDENT & NO ADDITIONAL PRECAUTIONARY ACTIONS TAKEN. ON ARRIVAL, ACFT WAS GROUNDED FOR MAINTENANCE. LINE MAINTENANCE NOTED DEBRIS IN B SUMP & SCAVENGER FILTER. INDEPENDENT, EXTERNAL ANALYSIS OF OIL SAMPLES ADVISED HIGH LEVELS/ADVANCED WARNINGS OF WEAR METALS ATI POWERPLANT ENGINEERING CONCLUDED ENGINE SERIAL NR 690323 COULD NOT CONTINUE IN SERVICE. LT ENG R & R IAW TASK CARDS ATI-24-003-00-01, ATI-26-000-01-01, ATI-36-005-00-05, ATI-71-602-00-03, & ATI-71-999-04-01. OPS CHECKED SAT. NO FAULTS NOTED, ACFT RELEASED TO SERVICE.
FIRST OFFICER'S WINDOW NOT CLOSING PROPERLY. FIRST OFFICER'S WINDOW OPERATIONAL CHECK IAW ISRAEL AEROSPACE INDUSTRIES SUPPLEMENTAL MAINTENANCE MANUAL 56-11-02 SATISFACTORY.
IN THE PROCESS OF PRE-DEPARTURE CHECKS, CREW REPORTED RIGHT FLIGHT MANAGEMENT COMPUTER (FMC) CENTRAL DISPLAY UNIT (CDU) BLANKED OUT WITH A BURNING SMELL. FMC CDU CIRCUIT BREAKER TRIPPED. AIRCRAFT GROUNDED FOR MAINTENANCE. GENERAL VISUAL INSPECTIONS OF CAVITY HOUSING RH FMC CDU SATISFACTORY. NO ADDITIONAL DAMAGES NOTED TO CABLES. BURNT ODORS ISOLATED TO RH FMC CDU ONLY. RH FMC CDU REMOVED AND REPLACED IAW BOEING 767-300 AIRCRAFT MAINTENANCE MANUAL 34-61-01. SUPPLY OF PROPER COOLING AIRFLOW TO RH FMC CDU VERIFIED GOOD PER B767 AMM 34-61-02. NO ADDITIONAL FAULTS NOTED.
DURING SCHEDULED MAINTENANCE, NR 3 POSITION INERTIAL ESCAPE REEL DEPLOYED. PER ATI MINIMUM EQUIPMENT LIST 25-61-01-01. NR 3 POSITION DESCENT DEVICE REMOVED AND REPLACED.
POST FLIGHT CREW REPORTED DURING INTIAL CLIMB OUT INERTIAL REELS WERE DISPLACED FROM HOLDER. NO ADDITIONAL FAULTS NOTED. FLIGHT CONTINUED UNAFFECTED. INERTIAL ESCAPE REELS POSITIONS 6 AND 7 WERE TRANSFERRED TO AN INOPERATIVE STATUS AND DEFERRAL MAINTENANCE ITEM 50247 PER ATI B767 MINIMUM EQUIPMENT LIST 25-61-01-01 WAS INITIATED. CORRECTIVE ACTION DUE 27 MARCH 2024. DOWNLINE, INERTIAL REELS POSITIONS 6 AND 7 WERE REMOVED AND REPLACED. NO ADDITIONAL SYSTEM FAULTS NOTED. DEFERRAL MAINTENANCE ITEM 50247 CLEARED.
POST FLIGHT CREW REPORTED DURING INTIAL CLIMB OUT INERTIAL REELS WERE DISPLACED FROM HOLDER. NO ADDITIONAL FAULTS NOTED. FLIGHT CONTINUED UNAFFECTED. INERTIAL ESCAPE REELS POSITIONS 6 AND 7 WERE TRANSFERRED TO AN INOPERATIVE STATUS AND DEFERRAL MAINTENANCE ITEM 50247 PER ATI B767 MINIMUM EQUIPMENT LIST 25-61-01-01 WAS INITIATED. CORRECTIVE ACTION DUE 27 MARCH 2024. DOWNLINE, INERTIAL REELS POSITIONS 6 AND 7 WERE REMOVED AND REPLACED. NO ADDITIONAL SYSTEM FAULTS NOTED. DEFERRAL MAINTENANCE ITEM 50247 CLEARED.
DURING PRE- FLIGHT INSPECTIONS AND MAINTENANCE, LINE TECH REPORTED OVERHEAD EMERGENCY LIGHT SWITCH GUARD BROKEN. OVERHEAD PANEL SWITCH GUARD REMOVED AND REPLACED PER B767 AIRCRAFT MAINTENANCE MANUAL 33-13-00. OPERATIONAL CHECK GOOD. NO ADDITIONAL FAULTS NOTED.
L/H SIDE FRAME STA 955 THE FAILSAFE STRAP HAS DEFECT INDICATION AT THE FWD SIDE OF THE LOWER BOLT HOLE COMMON TO T-FITTING
10 INCH DIAMETER DELAMINATION FOUND ON R/H VERTICAL STABILIZER PANEL
DURING DAILY SERVICE CHECK, LINE MAINTENANCE IDENTIFIED EMERGENCY DOOR DISCRETE LIGHT FLICKERING. SYSTEM DEFERRED-MEL CAT C. REMOVED AND REPLACED PROX SWITCH ELECTRONIC UNIT IAW AMM 32-09-04. OPERATIONAL CHECK SATISFATORY. FAULT NOT DUPLICATED. DEFERRAL 27916 CLEAR