- Serial number
- 750-0145
- Year built
- 2001
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- March 18, 2001
- Certificate issued
- August 2, 2024
- Expires
- August 31, 2031
- Mode S code
- AD445C
- Registered owner
- Citation X Parts LLC
- Location
- Liberty, NC
- Owner type
- LLC
From the FAA registry file of October 20, 2026. The registry lists only the engine series, so ADs for every Allison AE3007C model are included below.
On this page
Airworthiness directives that may apply · 24
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment. Not a compliance determination.
| 1998 | 3 |
|---|---|
| 1999 | 1 |
| 2000 | 4 |
| 2001 | 3 |
| 2002 | 2 |
| 2003 | 1 |
| 2005 | 1 |
| 2006 | 3 |
| 2007 | 1 |
| 2008 | 1 |
| 2009 | 1 |
| 2010 | 1 |
| 2011 | 1 |
| 2012 | 1 |
| 2013 | 1 |
| 2015 | 1 |
| 2017 | 1 |
| 2018 | 1 |
| 2023 | 1 |
| 2026 | 1 |
See all 30 ADs
Information bulletins that may apply · 6
Advisory, not mandatory. Matched the same way as ADs.
Airframe · Cessna 750
SAIB AIR-21-15R1Navigation SystemSAIB CE-10-49R1Equipment/Furnishings Drain Mast HeaterSAIB NM-10-45Landing Gear: Nose/Tail Landing Gear Attach SectionSAIB CE-10-29R1Lights Aft Side Ledger Divider LightSAIB NM-10-13Navigation: Flight Management SystemEngine · Allison AE3007C series
SAIB NE-11-22Engine ControlsNTSB investigations
No NTSB investigations matched to N954JSMatched by N-number and event date. Investigations from before this aircraft carried the mark are under Earlier aircraft. Investigations on Cessna 750 aircraft
FAA incident reports
No FAA accident or incident reports matched to N954JSMatched by N-number and event date. Reports from before this aircraft carried the mark are under Earlier aircraft. Reports on Cessna 750 aircraft
Service difficulty reports · 3
SDR 3EJA9202406250001Battery · over voltageWHILE IN FLIGHT THE WE HAD BATT OVERCURRENT 1&2 EICAS.SDR 3EJA2022081520022Control Lever · malfunctionedUNCOMMANDED SLAT EXTENSION DURING CRUSISE (SUCCESSIVE) FOLLOWED BY A FLAPS FAIL EICAS MESSAGE. REMOVED AND REPLACED FLAP/SLAT LEVER HANDLE.SDR 3EJA95402/17/22None · noneIN SPEEDS IN EXCESS OF 250KTS THE ACFT ROLLS NOTICEABLY LEFT WHEN SPEED BRAKES EXTENDING AND THE SAME AMOUNT RIGHT AS RETRACTED. AFTER FLIGHT IT APPEARS THE LEFT OUTER SB PANEL DOES NOT EXTEND ALL THE WAY UP AND SLOWER THEN THE INBOARD