N331AZ
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
NUMBER 2 PYLON AFT SECTION V-WEB HAS OUTBOARD VERTICAL STIFFENER CRACKED
NUMBER 2 PYLON AFT SECTION V-WEB AREA HAS INBOARD VERTICAL STIFFENER CRACKED
VERTICAL STIFFENER ANGLE ON FORWARD SIDE OF BS 246 FLOORBEAM, LBL 43.0, LEFT TUNNEL OF MEC IS CRACKED REFERENCE AMES WO N331AZ-40 NR 194950-0100-0064
NUMBER 1 ENGINE PYLON AFT NACELL STRUT FAIRING 437DB (STRINGER) INTERNAL WEB CRACKED.
FIRST OFFICER'S RIGHT WINDOW OPENED AND IS NOT CLOSING OR MOVING OUT OF OPEN POSITION WHILE ON THE GROUND. CLEANED AND LUBED LOWER TRACK OF FIRST OFFICER'S #2 WINDOW IN ACCORDANCE WITH B767 AMM 56-11-02. WINDOW CLOSES WITH NO ISSUES.
EXTERIOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED EXTERIOR EMERGENCY LIGHT IAW AMM 33-51-16. OPS CHECKED GOOD.
INTERIOR EMERGENCY LIGHTING SYSTEM INOPERATIVE. EMERGENCY LIGHTING BATTERY REMOVED AND REPLACED PER B767 AMM 25-64-02. OPERATIONAL CHECK GOOD. DEFERRAL MAINTENANCE ITEM 52497 CLEARED.
CRACK ON #2 ENGINE PYLON I/B SIDE INNER SKIN FOR ACCESS PANEL 444AL
VERTICAL STAB LE PANEL 321E BLEND OUTS OUT OF LIMITS.
FLC ROLLER TRAY AT STATION 654-790 BL 7 RH HAS CRACKS AND A DENT
#2 OTBD CORE COWL PRECOOLER EXHAUST DUCT IS WORN MISSING MATERIAL ALONG THE L/E
LEFT WING TRAILING EDGE PANEL 551QB HAS A WORN SEAL
ALC ROLLER TRAY STA1275 LBL 21 IS CRACKED
DURING HFEC OPEN FASTENER HOLE ROTARY SCAN, DEFECT INDICATIONS WERE NOTED AT THE BOTTOM TWO FASTENER HOLES. LOCATED BETWEEN S-19R AND LWR MAIN SILL CHORD, B STA 332-339.
VERT STSB ACCESS PANEL 324AL, FWD SUPPORT ANGLE LH O/B & RH O/B CRACKED AT LWR FASTENERS.
LEFT WING FIXED LEADING EDGE INTERCOSTAL AT LWS 520 CRACKED.
ALC DOOR FWD SCUFF PLATE CRACKED STA 1277
ALC DOOR MID SCUFF PLATE CRACKED REF 47637REA04 IR
FORWARD LOWER CARGO AFT SECTION AT FLOOR SUPPORT INTERCOSTAL AT LBL 20 BETWEEN STATIONS 720-740 HAS CORROSION AROUND NUTPLATES,
ELEVATOR SEAL PANEL IS CHAFFED
1809 BULKHEAD HORIZONTAL CHORD IS CRACKED ON LH SIDE AT LBL28.5
FLC STA 575 RBL36 CORROSION ON INTERCOSTAL OUT OF LIMITS
AFT LOWER CARGO FLOOR SUPPORT CRACKED STA 1461-1480, ABOVE S35R
FLC FLOOR WEB CORRSION STA 566-588 LBL17-23
P-32 DRIP PAN CORNER DAMAGE AND CRACKED
FLC STATION 566 RBL 28-38 CORRODED BEYOND LIMITS
P32 GROUNDING STUD LOOSE/WORN
L-1 DOOR CUTOUT AFT LOWER CORNER CRACKED S19L BODY ARM 332-339
FLOOR SUPPORT STA 1087 LBL22 CRACKED
LEFT GENERATOR P31 PANEL PUNCTURED
CORROSION AT INTERCOSTAL STA 522-544, LBL 26
LEFT GENERATOR P31 PANEL GROUNDING STUD LOOSE/WORN
FLOOR SUPPORT CRACKED AT STA1087, RBL22
CORROSION STA 624-630, RBL 38-42
CORROSION LOWER CARGO AT 8L PDU NUTPLATE CORRODED
FIRST OFFICER'S FORWARD OUTBOARD SEAT TRACK IS CRACKED
CAPTAIN'S FORWARD INBOARD SEAT TRACK IS CRACKED.
NUMBER 1 ENGINE PYLON I/B AFT FAIRING (STINGER) PANEL SUPPORT CRACKED
R2 WINDOW WILL NOT CLOSE. FAULT ISOLATED TO HANDLE ASSEMBLY. AIRCRAFT GROUNDED FOR MAINTENANCE. REMOVED AND REPLACED RIGHT NO. 2 WINDOW MECHANISM SCREW ASSEMBLY IAW B767 AMM 56-11-04. OPERATIONAL CHECK GOOD. AIRCRAFT RELEASED TO SERVICE.
FIRST OFFICER'S R2 WINDOW STUCK IN OPEN POSITION. OPERATED WINDOW IN ACCORDANCE WITH AIRCRAFT MAINTENANCE MANUAL 56-11-02. WINDOW FULLY CLOSED AND SEALED.
FIRST OFFICER'S #2 WINDOW WILL NOT CLOSE AND SECURE. VERIFIED SECURITY AND INTEGRITY OF OPENABLE MECHANISM AND CLOSED WINDOW IAW B767 AMM 56-11-00. COMPLIED WITH ADJUSTMENT OF THE FIRST OFFICER'S OPENABLE WINDOW AND OPERATIONAL CHECK GOOD PER B767 AMM 56-11-02.
POSITION #3 RAPID DESCENT DEVICE IS DEPLOYED UPON LANDING. SYSTEM DEFERRED 38167, MEL CAT C. INSTALLED POSITION #3 RAPID DESCENT DEVICE IAW B767 MAINTENANCE MANUAL 25-61-03. DEFERRAL 38167 CLEARED.
TAILCONE UPR SKIN PUNCTURED APPROX STA 1905 LBL 10
#2 ENG PYLON TO WING FAIRING 447DB HAS A CRACKED BULKHEAD. REF FAS WO FS220060 NON ROUTINE 00174
MAIN FRAME STA 903 LBL89 INNER CHORD IS CRACKED.
L/H WING O/B FLAP I/B #2 SUPPORT 1-2-3 BEAM HAS (1) HOLE MARKED IN RED SHARPIE. THAT HAS SEVERAL OPEN HOLE INDICATIONS OF DEFECTS NOTED AT THE 6 OCLOCK POSITION. VISSUAL DAMAGE NOTED ON THE I/B SIDE OF HOLE. REF FAS WO FS220060 NON ROUTINE 00586
(2) FASTENER HOLES WITH CRACK INDICATIONS ON REAR SPAR FITTING OF FLAP SUPPORT # 1 ON THE OUTER HALF OF THE O/B FITTING. REF FAS WO FS220060 NON ROUTINE 00580
RH HORIZONTAL STABILIZER FWD #1 FITTING CORRODED. REF FAS WO FS220060 NON ROUTINE 00451
SLAT #8 HAS A DENT AND POSSIBLE CRACK LEADING EDGE UPPER EXTERNAL SURFACE INBD END. REF FAS WO FS220060 NON ROUTINE 00518
RH HORIZONTAL STABILIZER FWD #6 FITTING CORRODED. REF FAS WO FS220060 NON ROUTINE 00455
RH HORIZONTAL STABILIZER FWD #4 FITTING CORRODED. REF FAS WO FS220060 NON ROUTINE 00454
RH HORIZONTAL STABILIZER FWD #3 FITTING CORRODED. REF FAS WO FS220060 NON ROUTINE 00453
RH HORIZONTAL STABILIZER FWD #2 FITTING CORRODED. REF FAS WO FS220060 NON ROUTINE 00452
CORROSION AREA ON BEAM PN 113T1911-40 BETWEEN WS841.20 & WS811.20 APPROX IN LENGTH 30".
RH HORIZONTAL STABILIZER AFT #7 FITTING CORRODED. REF FAS WO FS220060 NON ROUTINE 00456
MAIN FRAME STA 903 LBL89 INNER CHORD IS CRACKED. FASWO FS220060 NON-ROUTINE 00116
RH HORIZ STAB UPPER SURFACE HAS AREA OF BARE METAL AND SURFACE CORROSION BETWEEN FRONT AND REAR SPARS JUST OB OF STAB TO BODY FAIRING. REF FAS WO FS220060 NON ROUTINE 00219
MAIN FRAME STA 903.5 RBL 89 INNER CHORD IS CRACKED. REF FAS WO FS220060 NON-ROUTINE 00115
PRIOR TO DEPARTURE, FIRST OFFICER'S R2 WINDOW DIFFICULT TO OPEN. UNLOCK HANDLE DOES NOT SEAT IN THE OPEN POSITION. SECURED ROLL PIN IN LOCK HANDLE AND SAFETIED PIN. OPERATIONAL CHECK SATISFACTORY IAW B767 AMM 56-11-00. NO ADDITIONAL FAULTS NOTED.
ENROUTE MAIN CARGO DECK A-2 SMOKE DETECTION AMBER LIGHT ON CENTER CONSOLE WITH NO INDICATION OF SMOKE, MASTER CAUTION OR EICAS INDICATIONS. CREW DECLARED EMERGENCY AND DIVERTED TO KMSP. UPON LANDING NO THERMAL HOT SPOTS DETECTED BY FIRE CREW. MAIN DECK CARGO FREIGHT WAS OFFLOADED TO FACILITATE INSPECTION. GENERAL VISUAL INSPECTION OF UPPER CARGO. NO DEFECTS NOTED. INITIATED DEFERRAL MAINTENANCE ITEM CAT C. AICRAFT RELEASED TO SERVICE. FLIGHT CONTINUED TO DESTINATION STATION KSMF WITH NO FAULTS PRESENT FOR DURATION OF FLIGHT. REMOVED AND REPLACED SMOKE DETECTOR 2A IAW B767 IAI MM 26-14-01. OPERATIONAL CHECK SATISFACTORY. DEFERRAL MAINTENANCE ITEM 21070 CLEAR.
VERTICAL STABILIZER LEFT SIDE SKIN PANEL WAS DELAMINATED BEYOND SRM LIMITS. REMOVED AND REPLACED CORE AND INNER SKIN AND REPAIRED PER AMES ENGINEERING DOCUMENT 47447REA02 REV IR AND APPROVED BY DERT-710167-SW ON 8110-3 DATED 1-19-21.
PERFORMED A CRACK TRIM OUT OF THE RIGHT SIDE FAIL STRAP PER AMES ENGINEERING DOCUMENT 472070RD04.RIGHT SIDE STA 955 REFERENCING BOEING SERVICE BULLETIN 767-53A0100 AND BOEING SERVICE BULLETIN 767-53-0116.
MAINTENANCE, DURING ROUTINE OPERATIONS AT CVG, DISCOVERED ON 331AZ A CRACK IN THE SECTION 46 FUSELAGE SKIN AT THE FORWARD JAMB OF THE RIGHT AFT LOWER CARGO DOOR, PN 146T3510, AT STA 1270, NEAR DOOR STOP NUMBER 10. THE SKIN IS MADE FROM 2024-T3 X 0.210 CLAD ALUMINUM, PER B767300 SRM 51-00-04, TABLE 3. THE SKIN IS CLASSIFIED AT PRIMARY STRUCTURE, FCBS, AND PSE PER B767-300 SRM 51-00-04, FIGURE 1. WORK IN PROGRESS.
VISUAL SMOKE EMITTING FROM CAPTAIN'S SPEAKER ON POWER TRANSFER TO GROUND POWER UNIT. DURING A DETAILED VISUAL INSPECTION OF CAPTAIN'S SIDE CONSOLE, DETERMINED THE SOURCE OF THE ODOR AND SMOKE COMING FROM CAPTAIN'S SPEAKER IAW AMM 20-60-01. REMOVED AND REPLACED THE SPEAKER IAW AMM 23-51-02. OPS CHECKED SATISFACTORY. NO FURTHER DEFECTS WERE NOTED. AIRCRAFT RELEASED FOR SERVICE.