- Registered owner
- Cargo Aircraft Management Inc
- Location
- Wilmington, OH
- Owner type
- Corporation
- Serial number
- 23016
- Year built
- 1984
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- June 10, 2010
- Certificate issued
- March 31, 2010
- Expires
- November 30, 2029
- Mode S code
- AA9BC1
From the FAA registry file of October 22, 2026.
On this page
Airworthiness directives that may apply · 385
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1983 | 6 |
|---|---|
| 1984 | 1 |
| 1985 | 9 |
| 1986 | 11 |
| 1987 | 7 |
| 1988 | 8 |
| 1989 | 10 |
| 1990 | 20 |
| 1991 | 16 |
| 1992 | 12 |
| 1993 | 11 |
| 1994 | 17 |
| 1995 | 7 |
| 1996 | 9 |
| 1997 | 4 |
| 1998 | 9 |
| 1999 | 9 |
| 2000 | 23 |
| 2001 | 23 |
| 2002 | 14 |
| 2003 | 16 |
| 2004 | 16 |
| 2005 | 13 |
| 2006 | 11 |
| 2007 | 12 |
| 2008 | 16 |
| 2009 | 13 |
| 2010 | 12 |
| 2011 | 9 |
| 2012 | 14 |
| 2013 | 8 |
| 2014 | 12 |
| 2015 | 8 |
| 2016 | 7 |
| 2017 | 9 |
| 2018 | 8 |
| 2019 | 2 |
| 2020 | 6 |
| 2021 | 6 |
| 2022 | 4 |
| 2023 | 4 |
| 2024 | 1 |
| 2025 | 5 |
| 2026 | 5 |
See all 445 ADs
Information bulletins that may apply · 13
Advisory, not mandatory.
Airframe · Boeing 767-281
SAIB NM-20-07Navigation - Glideslope SystemSAIB NE-19-03Escape Slide Maintenance Tasks and Intervals - JASC 2565SAIB NM-18-33Engine Fuel and ControlSAIB NM-17-17Oxygen SystemSAIB NM-17-10Maintenance PracticesSAIB NM-17-09Flight Control SystemSAIB NM-15-03Flight ControlsSAIB NM-15-02Cabin Equipment/FurnishingsSAIB NM-09-03Engine Fuel and Control - Implementing Fuel Tank System Airworthiness LimitationsSAIB NM-08-43Cabin Equipment/Furnishings - SeatsSAIB NM-06-57Reports of damage to airplanes and to property on the ground caused by blue or clear ice falling from airplanes.NTSB investigations
No NTSB investigations matched to N783AXMatched by N-number and event date, checked against the reported serial number, make and model. Investigations from before this aircraft carried the mark are under Earlier aircraft. Investigations on Boeing 767-281 aircraft
FAA incident reports
No FAA accident or incident reports matched to N783AXMatched 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 767-281 aircraft
Service difficulty reports · 119
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR ABXA20250813175Manifold · crackedON TAXI R ENG HAD VIBRATIONS FROM 2.8 TO 3.3. WHEN ADDING TAXI THRUST VIBRATION INDICTIONS UP NTO 4.9 AND STARTED BEING VARIABLE- VIBRATION FELT IN AIRFRAME. AIRCRAFT RETURNED TO BLOCKS. (BTB). PERFORMED D.V.I OF RT ENG & FOUND UPPER & LOWER LPT COOLING AIR SDR ABXA2025081167Warning Message · illuminatedDURING TAXI, LEFT INBOARD AILERON POSITION DISAGREEMENT WITH THE INDICATOR ON THE LOWER STATUS PAGE. AIRCRAFT RETURNED TO BLOCKS. (BTB). MAINTENANCE DEFERRED IAW MEL C ABX-27-08-1. AIRCRAFT RETURNED TO SERVICE.SDR ABXA20250512094Compressor · stalledDURING CLIMB, LT ENG COMPRESSOR STALL AT APPROX FL 310 WITH CLIMB AND THRUST. STOPPED WHEN APPROX BELOW 93% N1. NO EICAS EXCEEDANCES. NO FURTHER STALLS IN CRUISE OR DESCENT. CONDUCTED STALL INSPECTION PER AMM 72-00-00/601, THEN CONDUCTED T/S PER FIM 71-05 FT
See all 119 reportsReports on N783AX not matched to an aircraft · 4
They name N783AX, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.
SDR ABXR080173Longeron · crackedLONGERON 16 LEFT WAS CRACKED AT STA 801 FRAME UPPER ATTCH FASTENER. REMOVED AND REPLACE LONGERON IAW SRM 53-02, FIG 18, SHEET 1. (A)SDR ABXR080170Angle · crackedCENTER WING TO FUSELAGE ANGLE CRACKED AND SEPERATED ABOVE REPAIR STRAP FORWARD SPAR AREA AT APPROX. RIGHT BUTT LINE 48. REMOVED AND REPLACED FITTING IAW DC9 SRM. (A)SDR ABXR080169Support · crackedRIGHT WING OUTBOARD SPOILER HAD OUTBOARD ACTUATOR SUPPORT BRACE CRACKED, UPPER END. REMOVED AND REPLACED OUTBOARD ACTUATOR SUPPORT BRACE IAW DC0 SRM 51-30-1, 51-30-2 AND 51-30-5. (A)
STCs that may be installed · 512
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.