N457AZ
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
L1 DOOR LOCKING PAWL BROKEN. REMOVED AND REPLACED L1 DOOR INTERLOCK PAWL IAW B767 AMM 52-11-26. OPERATIONAL CHECK GOOD.
NR 1 PYLON UPPER SKIN IS CHAFED AT OTBD SIDE AT FAN COWL AND T/R SEAM.
RIGHT WING OTBD FLAP FAIRING 672BB T/E FRAME IS CHAFED
AREA 1 HAS CRACK INDICATION WHILE PERFORMING BS1809.5 HFEC OPEN HOLE SCANS PER ATI-EO-5300-767-07548, SB 767 53A0078 REV 6, FOUND DEFECTIVE HOLE AREA 1 THE LWR AFT HOLE WAS MISSING MATERIAL. REF 8100-9 202512125726-0004, TIN-TIN 25-0256-01C
FLC BILGE PANEL LOCATED UNDER PDU 5C IS CORRODED AT STA 510 RBL 5
INTERCOSTAL IN FLC RBL 7 STA 510 HAS A CRACK
REPAIR IS WORN AND GOUGED ON TOP OF THE NR 2 PYLON L/E JUST AFT OF THE INLET COWL AT THE 11 O'CLOCK POS. AFT LOOKING FWD.
RIGHT WING INBOARD AFT FLAP OUTBOARD EDGE SEAL RETAINER IS DAMAGED AND BULB SEAL IS MISSING.
HOLE IN MAIN CARGO DOOR OUTER SKIN
DURING PRE-FLIGHT NOTICABLE SMELL OF BURNT WIRE IN THE FIGHT DECK. PLACED ON DEFERRAL 67357 MINIMUM EQUIPMENT LIST 21-58-03-01 CATEGORY C. DUE 06 NOVEMBER 2025. FLIGHT CREW DEBRIEFED AND FOUND THAT FORWARD EQUIPMENT SUPPLY FAN 1 EICAS MESSAGE AND EQUIPMENT COOLING SUPPLY FAN 1 BREAKER WAS OUT. IN ACCORDANCE WITH B767 FAULT ISOLATION MANUAL 21-58 FAULT TREE 904 PUSHED IN BREAKER. REMOVED AND REPLACED FORWARD SUPPLY FAN IN ACCORDANCE WITH B767 AIRCRAFT MAINTENANCE MANUAL 21-58-06. OPERATIONAL CHECK GOOD. DEFERRAL 67357 CLEARED.
AT 2500 MAIN CARGO DOOR ILLUMINATED WITH NO PRESSURIZATION ABNORMAL INDICATION. MASTER WARNING INDICATION FOR MAIN CARGO DOOR DISPLAYED. CREW ELECTED AIR TURN BACK TO DEPARTURE STATION KABE WITH AN EMERGENCY DECLARATION. LANDING WAS UNEVENTFUL WITH NO ADDITIONAL PRECAUTIONARY ACTIONS. ON ARRIVAL AIRCRAFT GROUNDED FOR MAINTENANCE.
AT 2500 MAIN CARGO DOOR ILLUMINATED WITH NO PRESSURIZATION ABNORMAL INDICATION. CREW ELECTED AIR TURN BACK TO KABE WITH AN EMERGENCY DECLARATION. LANDING UNEVENTFUL. ON ARRIVAL AIRCRAFT GROUNDED FOR MAINTENANCE. IAW ATI 767 MEL 52-71-01-02 DEFERRAL 60152 FOR MAIN DECK CARGO DOOR (MDCD) INDICATION SYS INITIATED. MDCD SENSOR S9024 SEQUENCE INDICATION CIRCUIT TO LOCK ACTUATOR ADJUSTED. FOR 11 CONSECUTIVE FLT CYCLES, NO ADDITIONAL FAULTS NOTED. GENERAL VISUAL INSPECTION OF DOOR LOCK ACTUATOR SYSTEM & WIRE SHAKE DOWN CHECK IAW SMM 52-32-12 AND AMM 20-60-03 GOOD. CHECKS OF ALL ASSOCIATED MDCD SENSOR RIGS PER SMM 52-32-SATISFACTORY. NO FAULTS FOUND. DEFERRAL MAINTENANCE ITEM 60152 CLEARED.
AT FL340, CREW REPORTED LOSS OF CABIN PRESSURE, EICAS MSG AND AURAL WARNINGS-MASTER CAUTION-ILLUMINATED. CREW COMPLIED WITH ATI QUICK REFERENCE HANDBOOK PROCEDURES, AND ELECTED AIR RETURN TO DEPARTURE STATION KRFD WITH AN EMERGENCY DECLARATION DUE TO OVERWEIGHT LANDING. LANDING WAS WITHOUT INCIDENT AND ON ARRIVAL THE AIRCRAFT WAS GROUNDED FOR INSPECTIONS AND MAINTENANCE. SUBSEQUENT TO COMPLIANCE OF TROUBLSHOOTING PROCEDURES PER BOEING 767 FAULT ISOLATION MANUAL 21-31-FT 803 AND BOEING 767 AIRCRAFT MAINTENANCE MANUAL 21-31-03, LINE MAINTENANCE REPORTED OUTFLOW VALVE WILL NOT ALLOW AIRCRAFT TO PROPERLY PRESSURIZE. AIR OUTFLOW VALVE ASSEMBLY REMOVED AND REPLACED. OPERATIONAL CHECK SATISFACTORY AMM 21-31-03 / 21-31-00. OVERWEIGHT LANDING CONDITIONAL INSPECTIONS GOOD PER BOEING 767-300 AIRCRAFT MAINTENANCE MANUAL 05-51-35. NO FAULTS FOUND. 19 JULY 2024, FUNCTIONAL FLIGHT CHECK ATN457 SATISFACTORY. NO FAULTS NOTED. AIRCRAFT RELEASED TO SERVICE.
ON CLIMB OUT CREW REPORTED, MAIN CARGO DOOR LIGHT ILLUMINATED AT FL280. PRESSURIZATION OK. CREW ELECTED AIR TURN BACK TO KLAL WITH AN EMERGENCY DECLARATION. LANDING WAS WITHOUT INCIDENT AND NO ADDITIONAL PRECAUTIONARY ACTIONS NOTED. POST FLIGHT LINE MAINTENANCE VERIFIED OPERATIONAL CHECK OF MAIN CARGO DOOR GOOD. FAULT TRANSFERRED TO DEFERRAL MAINTENANCE ITEM 52639 PER ATI MINIMUM EQUIPMENT LIST 52-71-01-02. MAIN DECK CARGO DOOR FORWARD INSTRUMENT PANEL CERTIFIED INOPERATIVE. AIRCRAFT RESUMED SERVICE. MAIN CARGO DOOR OPERATIONAL CHECK PER IAI SUPPLEMENTAL MAINTENANCE MANUAL 52-32-00 SATISFACTORY. NO FAULTS NOTED.
ON CLIMB OUT CREW REPORTED, MAIN CARGO DOOR LIGHT ILLUMINATED AT FL280. PRESSURIZATION OK. CREW ELECTED AIR TURN BACK TO KLAL WITH AN EMERGENCY DECLARATION. LANDING WAS WITHOUT INCIDENT AND NO ADDITIONAL PRECAUTIONARY ACTIONS NOTED. FAULT TRANSFERRED TO DEFERRAL MAINTENANCE ITEM 52639 PER ATI MINIMUM EQUIPMENT LIST 52-71-01-02. CORRECTIVE ACTION DUE 26 JUNE 2024. AIRCRAFT RESUMED SERVICE.
MAIN CABIN - INSTALL STRUCTURAL PROVISIONS FOR ELT MOD
RIGHT WING, FIXED LEADING EDGE , ALIGNMENT RIB AT OSS 607.247 IS CRACKED AT THE LEADING EDGE NOSE SECTION.
RH MLG DOOR AFT EDGE PANEL DISPLACED, FIBER GLASS CLOSURE PLIES FOUND DELAMINATED. UNKNOWN ON HOW DAMAGE OCCURED. AREA OF DAMAGE WAS 34" LONG.
SUBSEQUENT TO SERVICE CHECK, LINE MAINTENANCE REPORTED AFT FD EMERGENCY FLASHLIGHT BATTERY REQS REPLACEMENT EMERGENCY LIGHTING FLASHLIGHT BATTERY REMOVED AND REPLACED PER BOEING 767-300 AIRCRAFT MAINTENANCE MANUAL 25-64-00. OPERATIONAL CHECK GOOD. NO ADDITIONAL FAULTS NOTED.
LEFT WING LE PANEL 521AMB HAS WORN HOLES
FWD CARGO DOOR, FWD LATCH CAM HAS EDGE DAMAGE.
CRACK FOUND ON THE RIGHT SIDE OF THE FORWARD OUTER VERTICAL CHORD ON THE TOP LEFT FASTENER LOOKING AFT. CRACK EXTENDS FROM THE END PART THROUGH THE FASTENER AND UNDER THE OVERLAPPING STRUCTURE.
ACCOMPLISH PERMANENT REPAIR OF LIGHTNING STRIKE AT STA 387 STR 33L
ACCOMPLISH PERMANENT REPAIR OF LIGHTNING STRIKE AT STA 412, STR 30R
LEFT WINGLET, AFT POSITION LIGHT, HOUSING IS DENTED AND GOUGED
AFT CARGO PIT STRINGER S35L STA 1490 LBL29 HAS CORROSION
#2 ENGINE, RH THRUST REVERSER, TORQUE BOX OUTER RING HAS FRETTING DAMAGE ON THE INNER SURFACE.
MAIN CABIN TEE ANGLE ATTACH CLIP FOR INTERCOSTAL AT STA 1043 S18L IS GOUGED ON THE LOWER ATTACH FLANGE COMMON TO THE FRAME.
MAIN CABIN TEE ANGLE ATTACH CLIP FOR INTERCOSTAL AT STA 1043 S18L IS GOUGED ON THE LOWER ATTACH FLANGE COMMON TO THE FRAME.
UNABLE TO COMPLY WITH WINGLET STRINGER MOD ATI-57-767-06242, DUE TO MISALIGNMENT ISSUE OF 767-3421-9 AND 767-3421-11 STRAPS WITH EXISTING FASTENER LOCATIONS PER THE DRAWING REQUIREMENTS
RIGHT WING TRAILING EDGE RIB AT WSTA 534.27 HAS AN ELONGATED HOLE
SRM 53-60-71-2R, REPAIR 2 REQUIRES ACCOMPLISHMENT TO FACILITATE RMLG SWIVEL FITTING SUPPORT REPLACEMENT
RIGHT WING, OUTBOARD FLAP, UPPER SURFACE, 36 INCHES+- FROM INBOARD EDGE AND 28 INCHES FROM TRAILING EDGE IS AN AREA OF DELAMINATION
FRAME AT STA 883 STR 19L-20L CRACKED
FWD CARGO LOWER DOORSILL ATTACH ANGLE IS CORRODED AT NUTPLATES STA 566 RBL 35 - 37. REF HAECO WO 320005 NON ROUTINE 34777
NUMBER 2 ENGINE OUTBOARD THRUST REVERSER INNER SURFACE FORWARD DOWNSTOP BASE IS GOUGED. REF HAECO WO 320005 NON ROUTINE 34756
#1 ENG R/H T/R INNER SIDE LOWER SECTION AFT OF BUMPER MOUNT BRACKET STRUCTURE HAS CHAFING DAMAGE
#1 ENG R/H T/R INNER SIDE FWD RIB MIDDLE SECTION HAS AREA THAT IS CHAFED. REF HAECO WO 320005 NON ROUTINE 34704
#1 ENGINE NACELLE ACCESS PANEL 431AT FORWARD INBOARD MATING AREA IS GOUGED. REF HAECO WO 320005 NON ROUTINE 34693
MAIN CABIN FRAME AT STA 1021 INNER CHORD HAS MULTIPLE GOUGES IN THE RADIUS BETWEEN STR 18L AND 20L. REF HAECO WO 320005 NON ROUTINE 34670
#1 ENGINE, RH THRUST REVERSER FWD CORE COWL RIB IS GOUGED. REF HAECO WO 320005 NON ROUTINE 34703
#1 ENG R/H T/R INNER SIDE FWD BUMPER BRACKET GOUGED. REF HAECO WO 320005 NR 34706
TOP PORTION OF #2 ENGINE STRUT FAIRING SUPPORT STRUCTURE FRAME -136 GOUGED
RIGHT WING UPPER SKIN IS CORRODED AT WING ROOT JUST AFT OF AFT OVERWING EXIT DOOR STEP
#1 PYLON, HYDRAULIC BAY, BILGE AREA, 2EA WEB STIFFENERS ARE GOUGED
#1 ENGINE, INBOARD ACCESS PANEL 437AR, AFT ATTACHMENT FLANGE FOUND WORN WITH A MATERIAL LOSS OF 0.026
FWD LOWER CARGO DOOR SILL ATTACH ANGLE IS CORRODED AT NUTPLATES BS 566, RBS 36-BL 38
LH SIDE LOWER STRINGER S-37L AT FWD AND AFT SIDE OF STATION 1562 HAS CORROSION
RW IB AILERON OB CLOSEOUT RIB UPPER LEADING EDGE IS CHAFFED
RH WING FIXED L.E. FRAME SUPPORT STRUCTURE JUST O/B OF W.S.651 IS CRACKED
FUSELAGE EXTERIOR, ZONE 100, STA 1390 +/- BETWEEN S34L - S35L, 27 +/- INCHES FORWARD OF BULK CARGO DOOR FORWARD EDGE, IS DENTED
CRACK FOUND ON THE LEFT SIDE OF HORIZONTAL INNER CHORD LOOKING AFT, R/H HORIZONTAL INNER CHORD AT STA 1809.5 RBL 28. CRACK LOCATED AT THE 7 OCLOCK POSITION ON THE LOWER ROW MOST INBOARD FASTENER EXTENDING TO THE END OF THE PART.
RH WING OUTBD LE HAS A CRACKED BRACKET TO THE NO.8 INBD CURATIN SPRING APPROXIMATELY WS 465. HAECO WO 320005 NON ROUTINE 34217
FUSELAGE EXTERIOR, ZONE 100, STA 400+-, S37L - 38L +- HAS TWO (2EA) GOUGES. REF HAECO WO 320005 NON ROUTINE 34171
#1 PYLON PANEL 437CL IS WORN ON INNER SURFACE. REF HAECO WO 320005 NON ROUTINE 34046
#2 PYLON PANEL 447CR IS WORN ON INNER SURFACE. REF HAECO WO 320005 NR 34049
#2 PYLON PANEL 447CL IS WORN ON INNER SURFACE. REF HAECO WO 320005 NON ROUTINE 34048
R1 DOOR LOWER CORNER FUSELAGE SKIN AND BEARSTRAP CRACKED
#1 PYLON PANEL 437CR IS WORN ON INNER SURFACE. REF HAECO WO 320005 NON ROUTINE 34047
INTERIM REPAIR ON FUSELAGE SKIN, STA 408, S30L REQUIRES PERMANENT REPAIR
INTERIM REPAIR ON FUSELAGE SKIN, STA 654+34, STR 22L REQUIRES PERMANENT REPAIR
LH FUSELAGE LIGHTNING STRIKE DAMAGE AT STATION 387 STRINGER33L
LIGHTENING STRIKE DAMAGE AT STA 654+34 S22L
LIGHTENING STRIKE STA 742 S4R
LH FUSELAGE-LIGHTENING STRIKE AT STA 408 STR 30L
LIGHTNING STRIKE DAMAGE AT STA. 676 STRINGER 3R-4R
FO'S WINDOW HAS A LOCKING BRACKET ON THE ESCAPE HANDLE WINDOW. WORK IN PROGRESS.
ENGINE PRE-COOLER INLET DUCT CRACKED
#2 PYLON OB ARROW HEAD PANEL CRACKED.
#6 SLAT WEDGE DELAMINATED
#3 SLAT OB CLOSE OUT DOOR DAMAGED.
MAIN DECK CARGO DOOR UPPER SEAL DEPRESSOR.
# 10 SLAT ROD DOOR COVER IS CRACKED
#4 SLAT OB ROD COVER DOOR CRACKED
MDCD AFT MID UPPER SEAL DEPRESSOR GOUGED
#1 PYLON PANEL 436CL HAS DAMAGED FIRE SEAL
#1 ENGINE IB FAN COWL DELAMINATED 0.125
FO'S AFT IB SEAT TRACK HOLES ARE WORN
AFT LOWER CORNER SEAL DEPRESSOR
FWD LOWER SEAL DEPRESSOR DAMAGED
PANEL 194NR IS PUNCTURED
# 1 PYLON PANEL 437DB WEB CRACKED
VERT STAB AUX SPAR WEB CRACKED O/B L/S FSS127
PYLON PANEL 447DB CRACKED WEB
P-33 PANEL BRACKET CRACKED
PANEL 447AL CHAFFED
CAPTAINS AFT INBD SEAT TRACK, POSITION HOLES WORN / ELONGATED.
#1 PYLON PANEL 436CL HAS DAMAGED ALUMINUM
NO. 1 PYLON AFT MOST WEB IS CRACKED ON INBOARD SIDE OF STINGER FAIRING MOUNTING FLANGE NAC STA 407.34
PANEL 432AL IS CHAFED
VERTICAL STAB, RIGHT HAND VERTICAL PNL @ FSS 14.128 DELAMINATED
RW INBD L/E UPPER SLAT TORQUE TUBE SUPPORT BRACKET IS CRACKED LOCATED APPROX AT LES 292
LT HORZ PANEL 335AFB HAS WORN TORN SEAL
VIEW PORT INTERNAL WINDOW CRACKED ON R/H AFT SERVICE DOOR -R2-
VIEW PORT INTERNAL WINDOW CRACKED ON L/H AFT PASSENGER ENTRY DOOR -L2-
ON THE GROUND, FLIGHT DECK DOOR EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED AFT POSITION BATTERY PACK IAW B767 AMM 33-51-07. OPERATIONAL CHECK SATISFACTORY. NO ADDITIONAL FAULTS NOTED. AIRCRAFT RELEASED TO SERVICE.
PRE-DEPARTURE MAINTENANCE REPORTS INTERIOR EMERGENCY EXIT LIGHT IS INOPERATIVE. INITIATED DEFERRAL MAINTENANCE ITEM 23948, MEL CAT C. AIRCRAFT RELEASED TO SERVICE SYSTEMS OPERATIONAL CHECK IAW B767 AMM 33-51-00 SATISFACTORY. FAULT NOT DUPLICATED. DEFERRAL MAINTENANCE ITEM-23948 CLEAR.