- Registered owner
- Cargo Aircraft Management Inc
- Location
- Wilmington, OH
- Owner type
- Corporation
- Serial number
- 27908
- Year built
- 1995
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- April 16, 2012
- Certificate issued
- September 16, 2019
- Expires
- September 30, 2029
- Mode S code
- A3E89A
From the FAA registry file of October 22, 2026.
On this page
Airworthiness directives that may apply · 34
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1990 | 1 |
|---|---|
| 1991 | 4 |
| 1993 | 1 |
| 1994 | 2 |
| 1995 | 1 |
| 1996 | 1 |
| 1997 | 1 |
| 1998 | 1 |
| 1999 | 2 |
| 2000 | 4 |
| 2001 | 1 |
| 2002 | 2 |
| 2003 | 2 |
| 2004 | 2 |
| 2005 | 1 |
| 2006 | 1 |
| 2007 | 3 |
| 2008 | 1 |
| 2009 | 4 |
| 2012 | 2 |
| 2013 | 1 |
| 2014 | 1 |
| 2016 | 1 |
| 2018 | 1 |
| 2020 | 2 |
| 2021 | 2 |
| 2022 | 1 |
| 2023 | 1 |
See all 47 ADs
Information bulletins that may apply · 4
Advisory, not mandatory.
NTSB investigations · 1
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
FAA incident reports
No FAA accident or incident reports matched to N351AXMatched by N-number and event date, checked against the reported make and model. Reports from before this aircraft carried the mark are under Earlier aircraft. Reports on Boeing 767-33A aircraft
Service difficulty reports · 12
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR CNMA2026040004Pressure Valve · inoperativeL HPSOV EICAS MSG, AND L BLEED LIGHT ILLUMINATEDSDR CNMA2026030002Altimeter · inoperativeCA ALTIMETER INOP. FLAGGED OFF AT 25,000 FT.SDR CNMA2025050001Longeron · crackedDURING ACCOMPLISHMENT OF INSPECTION 76AD2012-15-12-G, A CRACK WAS FOUND IN THE LH UNDERWING LONGERON. PER SB 767-57A0126 INSTRUCTIONS, THIS REQUIRES FURTHER INSPECTION OF THE STRUCTURE AND AT MINIMUM REPLACEMENT OF THE UNDERWING LONGERON.SDR CNMA2023F00205Relay · inoperativeRAT DID NOT DEPLOY DURING AUTO DEPLOYMENT TEST ~ RAT DEPLOY RELAY K235 REPLACED RAT AUTO DEPLOY TESTED SERVICEABLE IAW B767-300 AMM 29-21-00-735-048 REV 139.SDR CNMA202209290375O-Ring · leakingR HYD QTY EICAS DURING CRUISE. QUANITY INDICATOR INDICATED HYDROLIC LEAK. CORRECTIVE ACTION: REMOVED AND REPLACED O-RING ON #11 SPOILER ACTUATOR IAW B767 AMM CHP 20-10. LEAK CHECKS GOOD.SDR 2022F00289Cylinder · emptyL/H OVERWING EXIT SLIDE INFLATION BOTTLE PRESSURE READS ZERO. CORRECTIVE ACTION: L/H OVERWING EXIT SLIDE BOTTLE REPLACE IAW B767-300 AMM 25-65-02-404-010 REV 136.SDR 2022FA0000293Pseu · defectivePRIOR TO CRUISE, IN CLB OUT, ALL CARGO / ENTRY DOORS CAUTION ILLUM. CORRECTIVE ACTION: REPLACED PSEU BOX IAW B767AMM 32-09SDR CNMA2021030001Sensor · defectiveAIR GROUND DISAGREE STATUS MESSAGE CORRECTIVE ACTION: R&R SENSOR S10598 PER SB76727A0160 AND ADJUSTED. OPS CK GOOD. TS IAW B767 FIM 3209 FAULT TREE 810 REPLACE RELAYS K199 & K293 IAW SB 76727 A0160SDR CNMA201911070001Pressure Switch · inoperativeR ENG FUEL FILT ICAS MESSAGE. CORRECTIVE ACTION: REMOVED AND REPLACED FUEL FILTER DIFFERENTIAL PRESSURE SWITCH PER AMM B767 73-34 LEAK CHECK GOOD MESSAGE CLEARED NO FURTHER DEFECTS NOTED AT THIS TIME. REF FIM 767 73-11 FAULT TREE 803SDR CNMA201902120002Outflow Valve · failedYELLOW CABIN AUTO INOP ICAS MESSAGE. WHITE CABIN ALT AUTO 2 AND AUTO 1 STATUS MESSAGES. MANUAL CONTROL INOP. CORRECTED ACTION: T/S TO OUTFLOW VALVE ACTUATOR. REMOVED AND REPLACED ACTUATOR IAW B763 AMM CH 21-31. OPS CHECK SATISFACTORY.SDR CNMA2018101090001Pca · failedEXCESSIVE RIGHT RUDDER TRIM (5 UNITS) REQ'D TO MAINTAIN LEVEL YOKE DURING CLIMB OR ON APPROACH WITH FLAPS OUT. ON GROUND DURING INITIAL FLAP EXTENSION, R INBD AILERON WAS NOTED SIGNIFICANTLY LOWER THAN L INBD AILERON, BUT FLT CONTROL CHECK FELT & LOOKED OK. ISDR CNMA20110008Radome · dentedBIRD STRIKE - AFTER BIRD STRIKE INSP FOUND RADOM DAMAGE INDENTED APPROX 2 FT ROUND SLIGHT LT OF CTR. R & R NOSE RADOME IAW AMM 53-12. LATCHED AND OK FOR SERVICE, RADOME WAS NOT PERFORATED AND RADAR ANTENNA AREA WAS INTACT.
STCs that may be installed · 5
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Engine · GE CF6-80C2B6F
STC SE01543CHReplace Hamilton Sundstrand P/N 778839-13, 778839-14, 778839-19, 778839-20, 778839-37, 778839-38, 816682-1, 840618-2, 880724 carbon bushings with Cook Airtomic P/N AIR22947 Slotted Entry Busing in the High Pressure Shutoff Valve.STC SE01478CHInstallation of Cook Airtomic alignment joint p/n AIR 22912.STC SE01471ATReplace right and left side Rohr, Inc. fire detection harness on GE CF6-80C2 engine.STC SE00463LAInstall fireproof blankets on the engine fan reverser intermediate fireseal, in lieu of fireproof intumescent coating. This STC is jointly by owned by Hi Temp Insulation and MRA Systems acting through Middle River Aircraft Systems, 103 Chesapeake Park Plaza, Baltimore, MD 21220STC SA2227SOInstallation of wiring and associated components for utilization of the Rolls Royce, Inc., ARINC, interface/readers UT1317 or UT1317/1, for the purpose of acquisition, recording, and analysis in real time of engine/aircraft/ systems. (767 SERIES POWERED BY RR RB-11-524 SERIES