N311AZ
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
LEADING EDGE SLAT DISAGREE EICAS MESSAGE IN THE AIR AFTER MOVING FLAP LEVER TO 1. AIR TRAFFIC CONTROL DECLARED EMERGENCY ON BEHALF OF THE FLIGHT CREW. AIRCRAFT LANDED WITHOUT INCIDENT AND WAS GROUNDED FOR INSPECTION AND MAINTENANCE. COMPLIED WITH B767 FIM 27-81-00-990-806 AND B767 FIM 27-51-00-990-808. SYSTEM CHECK GOOD NO FAULTS NOTED. GENERAL VISUAL INSPECTION AND OPERATIONAL CHECK OF FLAPS AND SLATS NOTED NO FAULTS.
LEFT WING #4 FLAP SUPPORT 6-6 OUTER PIN IS CORRODED AROUND THE SPLINES
FUSELAGE INTERCOSTAL ANGLE AT STA 1351 S17R IS CRACKED
L1 DOOR ESCAPE SLIDE DISARM LEVER COVER ATTACH BRACKET DAMAGED. NON-ESSENTIAL FURNISHINGS 68075 INITIATED. DUE 20 MARCH 2026. SUPPLEMENTAL TO PREVIOUS REPORT IXXA20251120077 DATED 20 NOVEMBER 2025 AT KILN. REMOVED DAMAGE ON THREE AREAS ON L1 DOOR ESCAPE SLIDE DISARM LEVER COVER AND REPAIRED UNDER VACUUM USING BM & 9-3T4H3 CL7 AND T7781, RC-0995746 AND EPOCAST 50-AI/9816, RC-1149439 IN ACCORDANCE WITH B767 AMM 25-00-00. DEFERRAL 68075 CLEARED.
RH WING LE 3 NOSE FORMERS FOUND CRACKED AT OSS446, OSS499 AND OSS550. P/N 114T2512U14, 114T2511U14, AND 114T2202-22.
FOLLOWING SERVICE CHECK INSPECTIONS, LINE MAINTENANCE REPORTED EMERGENCY DOOR INDICATION LIGHT ILLUMINATES INTERMITTENTLY. FAULT TRANSFERRED TO DEFERRED MAINTENANCE ITEM 58202 PER ATI MINIMUM EQUIPMENT LIST 52-71-01-01 MEL CAT C. PER BOEING 767-300 WIRING DIAGRAM MANUAL 52-71-12 AND IAI MAINTENANCE MANUAL 52-71-12, FAULT ISOLATED TO CHOKE S903. INTEGRITY CHECK OF S192-S193 AND S9013-S9016 SATISFACTORY. ALL VALUES READ AS REQUIRED. CHOKE 9031 READS OPEN CAUSING EMERGENCY DOOR LIGHT INTERMITTENT INDICATIONS. ELEC DOOR CHOKE REMOVED AND REPLACED IAW BOEING 767-300 SWPM 20-90-11. OPERATIONAL CHECK GOOD PER BOEING 767-300 52-71-00. NO ADDITIONAL FAULTS NOTED.
FOLLOWING SERVICE CHECK, LINE MAINTENANCE REPORTED LH OVERHEAD AND ENTRY DOOR EMERGENCY LIGHTS INOPERATIVE. BATTERY POWER SUPPLY REMOVED AND REPLACED IAW BOEING 767-300 MAINTENANCE MANUAL 33-51-00/0001. OPERATIONAL CHECK GOOD. DEFERRAL MAINTENANCE ITEM 52802 CLEARED.
FLC R/H SIDE ROLLER TRAY STA. 434-478 HAS CORROSION ON TRAY AROUND THE CONTAINER LOCK. INSTALL STRUCTURAL PROVISIONS FOR ELT MOD
CARGO COMPARTMENT STA. 1197+44 TO 1263 LT ROLLER TRAY CRACKED
CARGO COMPARTMENT STA. 1197+44 TO 1263 RT ROLLER TRAY CRACKED
#2 PYLON CLOSE OUT WEB CRACKED
#4 SLAT CORRODED LOWER SIDE OF WEDGE.
FLOOR SUPPORT BRACKET CRACKED IN HALF AT STA 1562 RBL-79 IAW B767 SRM 51-40-02-8, RBL79, STR 21R
FLOOR SUPPORT BRACKET IS CRACKED IN HALF, AT STA.1562, LBL79, JUST BELOW THE CABIN FLOOR, CLOSE TO STR 20L
L1 DOOR LOWER AFT CORNER CRACKED.
LINE MAINTENANCE REPORTED, #3 DESCENT RAIL DEPLOYED ON ENTRY DOOR #1. REMOVED AND REPLACED #3 DEVICE DESCENT IAW B767 IAI SMM 26-61-03.
IAW B767-200/300 MAINTENANCE EQUIPMENT LIST 33-51-02-01 SYSTEM FAULT TRANSFERRED TO DEFERRAL MAINTENANCE ITEM 44877. AIRCRAFT RELEASED TO SERVICE. SUPPLEMENTAL INFORMATION TO PREVIOUS SUBMITTAL IXXA20230911058 ON 11 SEPTEMBER 2023 AT KILN. DOWNLINE MAINTENANCE REMOVED AND INSTALLED L1 EMERGENCY LIGHT SOCKET IAW IAI AMM 33-51-06. OPERATIONAL CHECK GOOD. DEFERRAL MAINTENANCE ITEM 44877 CLEARED.
FORWARD LOWER CARGO PIT PDU TRAY 14R HAS PUNCTURE
FLIGHT COMPARTMENT EMERGENCY FLASHLIGHT TEST LIGHT NO ILLUMINATING. REMOVED AND REPLACED BATTERY IN ACCORDANCE WITH B767 AMM 25-64-02. OPERATIONAL CHECK GOOD.
FIRST OFFICER'S R2 WINDOW LOCKING HANDLE JAMMED. UNABLE TO UNLOCK SLIDE WINDOW BACK. R2 WINDOW INSPECTION CHECK PER B767 AMM 56-11-00 SATISFACTORY. NO FAULTS FOUND.
CREW REPORTED, DURING TAKEOFF ONE DESCENT DEVICE DEPLOYED. FLIGHT CONTINUED UNAFFECTED. REMOVED AND REPLACED L1 DOOR ESCAPE REEL PER IAI AMM 25-61-03.
#2 ENGINE OUTBOARD CORE COWL PRECOOLER EXHAUST BYPASS DUCT INNER RIM CHAFFED WITH MEASURABLE DEPTH>
WHILE PERFORMING INSPECTION OF HORIZONTAL STABILIZER JACKSCREW FOUND THREADS IN SOME AREAS TO BE WORN AND WATER RUNNING FROM LOWER GIMBALL.
FS 1702 FRAME TO STRINGER 3R CLIP CRACKED.
CORROSION ON HORIZONTAL STABILIZER UPPER SKIN AT RIB 1R.
MAIN CARGO DOOR SEAL DEPRESSOR GAUGED AND BENT ON AFT LOWER CORNER.
#1 INBD ARROWHEAD PANEL CRACKED AND SEPARATED AT LEADING EDGE FASTENERS.
FS 1678 FRAME TO STRINGER 3R CLIP CRACKED.
AFT UPPER SEAL DEPRESSOR ON MDCD IS BENT AND GAUGED.
SEVERE CHAFING AND MISSING MATERIAL ON THE PRE-COOLER EXIT DUCT SKIN.
FORWARD INTERCOSTAL/FRAME IS BENT AND CRACKED ON BOTH ENDS.
#2 ENG INBOARD CORE COWL UPPER AFT EDGE BENT AND SEPARATING FROM OUTER SKIN.
#2 PYLON HYDRAULIC BAY INBD SIDE HYDRAULIC VENT YUBE CLAMP STANDOFF CRACKED.
INBOARD FLANGE OF STINGER ATTACH FLANGE.IS BROKEN.
CRACKS FOUND EXTERNAL SKIN
SEAL DEPRESSOR BENT AND GOUGED
RIGHT HAND HORIZONTAL UPPER SKIN CORRODED.
#1 SLAT OUTBOARD ACTUATOR DOOR CRACKED.
PANEL 621DB IS CRACKED.
STRINGER CLIP CRACKED
MAIN DECK CARGO DOOR SEAL DEPRESSOR BENT AND GOUGED.
PYLON STINGER ATTACH ANGLE CRACKED
PYLON PANEL ATTACH ANGLES CRACKED.
PANEL ATTACH ANGLES CRACKED.
LW LES 504 L/E AIR LOAD RIB UPPER CHORD CRACKED AFT
L/W L/E UPPER FWD SURFACE CRACKED AT #1 SLAT O/B MAIN TRACK CUTOUT
ENROUTE FROM PHLI TO KONT AND PRIOR TO ETOPS SEGMENT, LEFT EICAS COMPUTER FAILED. FLIGHT CANNOT CONTINUE AS SCHEDULED DUE TO ETOPS REQUIREMENTS. DIVERSION TO PHNL. LANDING WAS UNEVENTFUL WITH NO ADDITIONAL PRECAUTIONARY ACTIONS NOTED. REMOVED AND REPLACED LEFT EICAS COMPUTER IAW B767 AMM 31-41-02. OPERATIONAL CHECK GOOD. NO ADDITIONAL FAULTS NOTED. AIRCRAFT RELEASED TO SERVICE.
AIRCRAFT GROUNDED FOR HEAVY MAINTENANCE SCHEDULED VISIT. IN COMPLIANCE OF TASK CARD 71-834-00-01, "GVI - ZONAL - CORE COWL PANELS - ENGINE 1" THE FOLLOWING DISCREPANCY WAS NOTED: #1 OUTBD CORE COWL EXTERNAL SKIN CRACKED. CONFIRMED BY EDDY CURRENT. REMOVED AND REPLACED AREA OF CRACK ON EXTERNAL SKIN OF #1 OUTBOARD CORE COWL IN ACCORDANCE WITH REA 47414REA07
AIRCRAFT GROUNDED FOR HEAVY MAINTENANCE SCHEDULED VISIT. NR 1 OUTBOARD PYLON EXTERNAL SKIN IS CRACKED AT AFT UPPER CORNER OF PANEL 432AL CUTOUT. FABRICATED, LOCATED, DRILLED AND INSTALLED A DOUBLER, TRIPLER, FILLERS AND RUB STRIP IAW REA 42414REA08.
AIRCRAFT GROUNDED FOR HEAVY MAINTENANCE SCHEDULED VISIT. IN COMPLIANCE OF TASK CARD 53-872-00-01, EXTERNAL FUSELAGE SKIN CRACKED AT THE LOWER AFT CORNER OF THE R1 DOOR CUTOUT. CRACK IN R1 DOOR LOWER AFT CORNER FOUND TO BE OUT LIMITS. REPAIRS ACCOMPLISHED IN ACCORDANCE WITH BOEING 767 SRM 53-10-01 REPAIR 1. CATEGORY B REPAIR INSPECTION 6,000CY THRESHOLD, 3000CY INTERVAL.
AIRCRAFT GROUNDED FOR HEAVY MAINTENANCE SCHEDULED VISIT.SKIN CRACK AT NCC STA 211.75-237.5. REPAIRED SKIN CRACK AT NCC STA 211.75-237.5 COMMON TO THE NUMBER ONE STRUT OUTBOARD SKIN PANEL, USING AMES REPAIR DOCUMENT 47414REA08 REV 1R DATED 6-30-2020. APPROVED ON 8110-3 DATED 7-3-2020 BY DERT 701067-SW.
AIRCRAFT GROUNDED FOR HEAVY MAINTENANCE SCHEDULED VISIT. IN COMPLIANCE OF TASK CARD 54-822-00-01 "GVI - ZONAL - AFT NACELLE STRUT FAIRINGS - STRUT 1", THE FOLLOWING DISCREPANCY WAS NOTED: #1 PYLON INBD HYD BAY LOWER LONGERON IS CRACKED AFT OF #4 LATCH FITTING. REMOVED AND REPLACED AFT SECTION OF I'B BEAM IAW DOCUMENT #47414REA04
AIRCRAFT GROUNDED FOR HEAVY MAINTENANCE SCHEDULED VISIT. IN COMPLIANCE OF TASK CARD 54-822-00-01. "GVI - ZONAL - AFT NACELLE STRUT FAIRINGS - STRUT 1", THE FOLLOWING DISCREPANCY WAS NOTED: #1 PYLON OUTBD HYD BAY LOWER LONGERON CRACKED AT 3RD LATCH FITTING. #1 PYLON O/B HYD BAY LOWER LONGERON REMOVED AND REPLACED REPAIR PART DRILLED UP FABBED REPAIR SPLICE AND INSTALLED PARTS IN ACCORDANCE WITH BOEING 767 ATI SRM 51-40-02 AND AIRBORNE EO DOC #47414REA03
AIRCRAFT GROUNDED FOR HEAVY MAINTENANCE SCHEDULED VISIT. IN COMPLIANCE OF TASK CARD 54-408-00-02 "GVI - EXTERNAL - NO. 2 NACELLE STRUT", THE FOLLOWING DISCREPANCY WAS NOTED: #2 PYLON INBOUND STRUT SKIN IS CRACKED IN THE UPPER AFT CORNER OF THE CUTOUT FOR PANEL 442AL. (VERIFIED WITH HFEC SURFACE SCAN. REPAIRED DAMAGE AREA IN UPPER AFT CORNER OF CUTOUT FOR PANEL 442AL IN ACCORDANCE WITH AMES DOCUMENT 47414REA02.
AIRCRAFT GROUNDED FOR HEAVY MAINTENANCE SCHEDULED VISIT. PER CUSTOMER REQUEST, PLEASE REVIEW AND VERIFY N311AZ DENT AND BUCKLE REPORT ITEM #8 CONFORMS TO B767 SRM 53-00-01 REPAIR 12. REVIEWED DENT AND BUCKLE REPORT ITEM #8, PERFORMED CONFORMITY OF REPAIR IN ACCORDANCE WITH REA DOCUMENT #47414REA06. REPAIR DOUBLER AT STRINGER 12L BETWEEN STA 243 TO STA 265.
RIGHT SIDE WINDOW HANDLE LATCH SLIP BROKEN. HANDLE GOES TO 90 PERPENDICULAR TO WINDOW WITH ALMOST ZERO PRESSURE. ADJUSTED THE WINDOW STRIKE BRACKET ON THE FIRST OFFICER'S SIDE IAW IAI 56-11-02. OPS CHECKED GOOD.
EMERGENCY LOCATOR TRANSMITTER TESTED AND FAILED TO FUNCTION. REMOVED AND REPLACED EMERGENCY LOCATOR TRANSMITTER. OPERATIONAL CHECKED SATISFACTORY. AIRCRAFT RELEASED TO SERVICE.