N229AZ
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
CENTER AISLE STAND EMERGENCY FLASHLIGHT HOLDER BOTTOM BROKEN. PLACED ON DEFERRAL 74109 MINIMUM EQUIPMENT LIST CATEGORY C PER ATI-25-63-04-01. DUE 23 JUNE 2026. REMOVED AND REPLACED CENTER AISLE STAND EMERGENCY FLASHLIGHT HOLDER IN ACCORDANCE WITH B767 SRM 51-40-02. OPERATIONAL CHECK GOOD. DEFERRAL 74109 CLEARED.
NUMBER 6 EMERGENCY INERTIAL REEL REQUIRES REPLACEMENT. PLACED ON DEFERRAL 67545 MINIMUM EQUIPMENT LIST 25-61-01-01 CATEGORY C. DUE 12 NOVEMBER 2025. REMOVED AND REPLACED #6 INERTIA DESCENT DEVICE IN ACCORDANCE WITH AIRCRAFT MAINTENANCE MANUAL 25-61-05. NO OTHER DEFECTS NOTED DEFERRAL 67545 CLEARED.
CENTER PEDESTAL EMERGENCY FLASHLIGHT HOLDER BROKEN. MAINTENANCE PLACED ON DEFERRAL 65656 MINIMUM EQUIPMENT LIST 25-63-04-01 CATEGORY C. DUE 07 SEPTEMBER 2025. IN ACCORDANCE WITH B767 FIM 52-71 FAULT TREE 816 AND B767 WDM 52-71-12 BITE PROCEDURE FOR PROXIMITY SENSOR ELECTRONIC UNIT AND FAULTED CODE 005, 007, AND 219. INSPECTED AND CLEANED SENSOR S219. FAULT CLEARED. REMOVED AND REPLACED DEACTIVATION CHOKE S9013 ON TB101F (A191-C191) IAW B767 SWPM 20-90-15 AND IAI SUPPLEMENTAL WDM 52-71-12. OPERATIONAL CHECK GOOD. DEFERRAL 65652 CLEARED.
MULTIPLE EICAS MESSAGE WITH STANDBY POWER AUTO DURING DESCENT FL290. EMERGENCY DECLARED TO KCVG. AIRCRAFT LANDED WITHOUT INCIDENT NO OTHER PRECAUTIONARY ACTIONS TAKEN. AIRCRAFT WAS GROUNDED FOR INSPECTION AND MAINTENANCE. LINE MAINTENANCE REMOVED AND REPLACED MAIN BATTERY TRANSFER RELAY IN ACCORDANCE WITH BOEING 767 AIRCRAFT MAINTENANCE MANUAL 24-33-02. OPERATIONAL CHECK GOOD. AIRCRAFT WAS RELEASED FOR SERVICE.
AIR TURN BACK INITIATED DUE TO MULITPLE ENGINE INDICATION FLUCTUATIONS FOR EXHAUST GAS TEMPERATURE, OIL PRESSURE, OIL TEMPERATURE AND OIL QUANTITY. STATUS MESSAGE EICAS DISAGREE ON THE GROUND AFTER LANDING. NO EMERGENCY DELCARED. SYSTEM DEFERRED 64215, MEL CATEGORY A. REMOVED AND REPLACED EICAS COMPUTER IAW MM 31-41-02. OPERATIONAL CHECK GOOD. DEFERRAL 64215 CLEARED.
EXTERIOR FUSELAGE SHIN HAS SEVERAL OUTWARDLY PROTUDING DENTS BETWEEN STA 654+44 - STA 654+68, AT STRINGERS S-R1 THOUGH S-4L. 8110-3 ISSUED.
R WING INTERNAL STRINGER L10 HAS 1 FASTENER HOLE AT APPROX WS 850 RIB 26 WITH GOUGE DAMAGE AT FASTENER HOLE
L WING WINGLET L/E PANEL HAS 1 FASTENER HOLE THAT IS OVER SIZED
MAIN CABIN LONGITUDINAL STIFFENER ABOVE CANTED BULKHEAD AT APPROX BS 1043+14 RBL 23 HAS DENT/GOUGE ON TOP AREA
MAIN CABIN LONGITUDINAL STIFFER ABOVE CANTED BULKHEAD AT APPROX STA 1021 HAS 3 EACH DENTS AT APPROX RBL30
APPROX 8" AFT OF AFT ENTRY DOOR L2 FLOOR STRUCTURE HAS GOUGE
#1 PYLON UNDER PANEL 431AT SKIN HAS CHAFFING MARK AT NAC STA 155 APPROX AS MARKED
FLOOR PANEL AT L2 DOORWAY STA 1461-1582 LBL 60-80 HAS PUNCTURE. HAECO WO 32011 NR 35279
R/H WING L/E AREA NOSE FORMER ANGLE IS CRACKED AT APPROX LES490. REF HAECO WO 320011 NR 34425
#2 ENG I/B CORE COWL HAS GOUGE ON 2ND FRAME FROM FWD
#2 ENG I/B CORE COWL HAS GOUGE ON 4TH FRAME FROM FWD
RIGHT UPPER WING TO BODY PANEL 196DR PANEL LANDING ATTACH BRACKET IS CRACKED. REF HAECO WO 320011 NON ROUTINE 35368
#2 ENG I/B CORE COWL HAS GOUGE ON 3RD FRAME FROM FWD
RH WING NOSE FORMER IS BROKEN AT OSS 429. REF HAECO WO 320011 NR 35357
RIGHT WING LEADING EDGE NOSE FORMER IS BROKEN AT OSS 456. HAECO WO 320011 AND NR 35356
5 SLAT O/B L/E PANEL NOSE FORMER BRACKET CRACKED AND FASTENER PULLING THROUGH
FWD CARGO COMPT, FLOOR BEAM SPLICE HAS SMALL GOUGES STA 654+110, LBL 32, WL 196
FWD CARGO COMPT, FLOOR BEAM SPLICE HAS SMALL GOUGES, STA 654+88, RBL 11 WL 196
RIGHT WING LOWER ACCESS PANEL 632AB IS WORN AND CORRODED
MAIN CABIN WINDOW FRAME AT STA 808-828 HAS THREAD DAMAGE
FORWARD CARGO FLOOR STRUCTURE INTERCOSTAL CORRODED TO EXFOLIATION @ STA 478 TO STA 500, APPROX. RBL 34 REF HAECO WO 320011 NR35320
#2 ENG FAN COWL DOOR I/B INSIDE SURFACE AFT REPAIR PLATES HAS A GOUGE AND WEAR
FABRICATE RIGHT WING LEADING EDGE RIB USING ALTERNATE FINISH. HAECO W.O. 320011 AND NR 35297
#1 PYLON UNDER DOOR #437BL HYDRAULIC VENT LINE SUPPORT BRACKET IS CRACK.
RIGHT WING LEADING EDGE BULL NOSE BEAM IS CRACKED AT OSS 664.58. REF HAECO WO 320011 NR 35285
MAIN CARGO DOOR CUTOUT AFT FRAME HAS 1EA HOLE WITH EVIDENCE OF CORROSION BETWEEN STR 20L AND 21L
FLOORBOARD RBL 73 TO RBL 88 FROM STA 388 TO 522 HAS LARGE DENT. REF WO HAECO 320011 NR 35259
MAIN CARGO DOOR CUTOUT AFT FRAME IS GOUGED BETWEEN STR 20L AND 21L. HAECO W.O. 320011 AND NR 35218
RH WING INTERNAL RIB 23 WEB IS DENTED AND GOUGED AT THE SAME LOCATION ON THE INBD SIDE BETWEEN STRINGERS L-5 AND L-6. REF HAECO WO 320011 NR 34976
FLIGHT DECK L2 SLIDING WINDOW CUTOUT FWD LOWER SEAL RETAINER DAMAGE
RH WING INTERNAL LOWER STRINGER L-10 FWD SKIN ATTACH FLANGE HAS MILTIPLE GOUGES AT THE ATTACH FASTENERS BETWEEN RIB 30 AND RIB 31 SPORADICALLY THROUGHOUT. REF HAECO WO 320011 NR 35010
#2 PYLON OTBD STRUT ATTACH ACCESS PANEL LANDING (A/C SIDE) HAS PITTING. REF HAECO WO 320011 NR 34926
FWD CARGO COMPARTMENT LEFT SIDEWALL SUPPORT CRACKED AT STA 654+33, WL 158. REF HAECO WO 320011 AND NR 34720
#2 PYLON INBD ACCESS HYDRAULIC BAY AFT OTBD STRUCTURE CLIP CRACKED. REF HAECO WO 320011 NON ROUTINE 34843
FWD CARGO COMPARTMENT STA 500 TOP OF FLOOR BEAM CORRODED AND SPLITTING BELOW LOWER SILL OF CARGO DOOR. REF HAECO WO 320011 NON ROUTINE 34724
FWD CARGO COMPARTMENT STA 514 ATTACH ANGLE BELOW RH PDU CORRODED AROUND NUT PLATES. REF HAECO WO 320011 NR 34725
FWD CARGO COMPARTMENT STA 520 ATTACH ANGLE BELOW R/H PDU CORRODED O/B NUTPLATE. REF HAECO WO 320011 NR 34726
#2 ENGINE OUTBOARD THRUST REVERSER INNER FRAME HAS A GOUGE. HAECO W.O. 320011 AND NR 34816
AFT KEEL BEAM FITTING FWD OF 149BL ACCESS HAS CORROSION. REF HAECO WO 320011 NR 34676
LEFT WING LOWER ACCESS PANEL 532AB IS WORN AND CORRODED
R/H WING #12 L/E SLAT T/E WEDGE LOWER SURFACE IS CORRODED APPROX 11" INBOARD OF THE OUTBOARD END OF THE SLAT
LEFT WING LOWER ACCESS PANEL 531AB IS WORN AND CORRODED, HAECO WO 320011 AND NR 34514
RIGHT WING LOWER PANEL 631AB IS WORN AND CORRODED. HAECO W.O. 320011 AND NR 34518
RH WING OTBD LE AREA BULL NOSE WEB EXISTING REPAIR IS CRACKED IN THE RADIUS AT APPROV LES 680. REF HAECO WO 320011 NR 34436
RIGHT WING LEADING EDGE FORMER IS CRACKED AT APPROX OSS 560
RH WING OTBD LE AREA BULL NOSE WEB EXISTING REPAIR IS GOUGED IN THE RADIUS AT APPROX LES 690. REF HAECO WO 320011 NR 34437
RH WING OTBD LE AREA LE RIB ASSEMBLY LOWER CHORD ANGLE IS CRACKED JUST FWD OF THE FWD SPAR AT THE ATTACH BRACKET AT APPROX LES 813 REF HAECO WO 320011 NR 34440
RIGHT WING LEADING EDGE RIB AT OSS 499 IS GOUGED IN THE RADIUS AT APPROX LES 490. HAECO WO 320011 AND NR 34427
RIGHT WING #7 LEADING EDGE SLAT COVER AREA HAS ONE EACH CRACKED ATTACH BRACKET
RIGHT WING #7 LEADING EDGE SLAT COVER AREA HAS ONE EACH CRACKED ATTACH BRACKET
#2 PYLON FARING HAS A GOUGED FWD LONGERON
RMLG WHEEL WELL CANTED PRESSURE DECK WEB IS CRACKED APPROX 3" AFT OF STA 955.1 BULKHEAD AT APPROX RBL13. HAECO W.O. 320011 AND NR 34179
LMLG WW BULB SEAL REATINER IS CRACKED APPROX 76" OTBD OF THE INBD END OF THE MLG SUPPORT BEAM ON THE TE OF THE CUTOUT. REF HAECO WO 320011 NR 34164
PRE-DEPARTURE CREW REPORTED OVHD PNL "EMER DR" INDICATION LIGHT INTERMITTENT. FAULT TRANSFERRED TO DEFERRAL MAINTENANCE ITEM 57542 PER ATI B767-200/300 MINIMUM EQUIPMENT LIST 52-71-01-01 CATEGORY C. CORRECTIVE ACTION DUE 14 DECEMBER 2024. FAULT ISOLATED TO INDUCTANCE CHOKE S9031 DAMAGED. S9031 AND S9032 REMOVED AND REPLACED. OPERATIONAL CHECK PER IAI SUPPLEMENTAL MAINTENANCE MANUAL AND IAI WIRING DIAGRAM MANUAL 52-71-12 SATISFACTORY. NO SYSTEM FAULTS NOTED. DEFERRAL MAINTENANCE ITEM 57542 CLEARED.
CREW REPORTED, STANDBY INVERTER STATUS MESSAGE WHEEL WELL FIRE AT 90-100 KNOTS (EICAS-FIRE BELL) 3 SECONDS. LANDING WAS WITHOUT INCIDENT AND NO ADDITIONAL PRECAUTIONARY ACTIONS. WIRING CHECKS ON STANDBY POWER SYSTEM PER BOEING 767 WIRING DIAGRAM MANUAL 24-33-11 AND SUPPLEMENTAL MAINTENANCE MANUAL 24-54-04 SATISFACTORY. NO FAULTS FOUND. SUBSEQUENT TO AN INTEGRITY CHECK OF P5 PANEL, LINE MAINTENANCE REPORTED SHORT IN S1 SWITCH GOING FROM AUTO TO OFF CAUSING THE WHEEL WELL FIRE AND STANDBY INVERTER MESSAGE TO DISPLAY. STANDBY POWER OVERHEAD PANEL REMOVED AND REPLACED. OPERATIONAL CHECK GOOD.
CREW REPORTED, STANDBY INVERTER STATUS MESSAGE WHEEL WELL FIRE AT 90-100 KNOTS (EICAS-FIRE BELL) 3 SECONDS. STANDBY IND FAIL. AIRCRAFT RESCUE AND FIRE FIGHTING WAS REQUESTED. LANDING WAS WITHOUT INCIDENT AND NO ADDITIONAL PRECAUTIONARY ACTIONS. GENERAL VISUAL INSPECTION OF THE WHEEL WELL DETECT LOOPS SATISFACTORY. NO FAULTS FOUND. OPERATIONAL CHECK SATISFACTORY PER BOEING 767 AIRCRAFT MAINTENANCE MANUAL 26-17-00. STATIC INVERTER REMOVED AND REPLACED PER BOEING 767 AIRCRAFT MAINTENANCE MANUAL 24-33-03. OPERATIONAL CHECK GOOD. ESIS RESET AND OPERATIONAL CHECK SATISFACTORY PER ATI SUPPLEMENTAL MAINTENANCE MANUAL 34-06.
LH 1809 CHORD CRACKED
FORWARD R1 DOOR CUTOUT CRACK INDICATION
L1 DOOR LOWER AFT CORNER CUTOUT CRACK INDICATION
ENGINE COWL RUB STRIP
UPPER HORIZONTAL SKIN PANEL DELAMINATED BEHIND LEADING EDGE
#6 SLAT LEADING EDGE SUPPORT BRACKET CRACKED.
CREW UNABLE TO CONTROL CABIN ALTITUDE IN CABIN ALT AUTO 1. CABIN ALT AUTO 2 ON ACTIVE DEFERRAL-38148 MEL CAT C. AIR TURN BACK TO DEPARTURE STATION WITH EMERGENCY DECLARATION. LANDING UNEVENTFUL WITH NO ADDITIONAL PRECAUTIONARY ACTIONS. ON ARRIVAL AIRCRAFT GROUNDED FOR UNSCHEDULED MAINTENANCE. REMOVED AND REPLACED #1 CABIN PRESSURE CONTROLLER IAW AMM 21-31-02. OPERATIONAL CHECK GOOD. AIRCRAFT RELEASED TO SERVICE.
EMERGENCY FLASHLIGHT INOPERATIVE. WORK IN PROGRESS
CREW REPORTED AT FLIGHT CHECK ATN229, LE ASYM EICAS MESSAGE AND LE DISAGREE DISCRETE DISPLAYED FLAP AND SLAT LOCKOUT OCCURRED AT CRUISE POSITION. AIR TURN BACK TO DEPARTURE STATION KCVG WITH EMERGENCY DECLARATION. LANDING UNEVENTFUL WITH NO ADDITIONAL PRECAUTIONARY ACTIONS. IAW B767 FAULT ISOLATION MANUAL 32-09-803, 27-81-809 AND WDM 27-88-12 SECURED WIRING TO FSEU PIN K1 TO C14 PER B767 AMM 27-81-11/21 AND REMOVED AND REPLACED PROXIMITY SWITCH SENSOR S286 IAW B767 AMM 27-88-01. OPERATIONAL CHECK SATISFACTORY PER B767 AMM 27-88-00/501
DEFERRAL MAINTENANCE ITEM #21961 INITIATED. AIRCRAFT RELEASED TO SERVICE.REMOVED AND REPLACED THE FORWARD EMERGENCY FLASHLIGHT IAW B767 AMM 25-60-00. THIS CLEARS DEFERRAL MAINTENANCE ITEM 21961. NO FURTHER MAINTENANCE ACTION REQUIRED. AIRCRAFT RELEASED TO SERVICE.