- Registered owner
- Valmont Industries Inc
- Location
- Omaha, NE
- Owner type
- Corporation
- Serial number
- 5349
- Year built
- 1997
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- September 9, 1997
- Certificate issued
- February 24, 2009
- Expires
- July 31, 2029
- Mode S code
- A40817
From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every GE CF34 model are included below.
On this page
Airworthiness directives that may apply · 162
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1981 | 1 |
|---|---|
| 1982 | 6 |
| 1984 | 1 |
| 1988 | 2 |
| 1990 | 1 |
| 1991 | 2 |
| 1992 | 2 |
| 1993 | 1 |
| 1994 | 5 |
| 1995 | 5 |
| 1996 | 1 |
| 1997 | 3 |
| 1998 | 1 |
| 1999 | 4 |
| 2000 | 6 |
| 2001 | 8 |
| 2002 | 4 |
| 2003 | 5 |
| 2004 | 6 |
| 2005 | 8 |
| 2006 | 7 |
| 2007 | 8 |
| 2008 | 4 |
| 2009 | 6 |
| 2010 | 9 |
| 2011 | 4 |
| 2012 | 5 |
| 2013 | 4 |
| 2014 | 7 |
| 2015 | 4 |
| 2016 | 5 |
| 2017 | 11 |
| 2018 | 6 |
| 2019 | 6 |
| 2020 | 2 |
| 2021 | 6 |
| 2022 | 12 |
| 2023 | 9 |
| 2024 | 6 |
| 2025 | 6 |
| 2026 | 5 |
Airframe · Canadair CL-600-2B16
AD 2026-14-09Time Limits/Maintenance ChecksAD 2026-13-02NavigationAD 2026-07-01Landing gearInformation bulletins that may apply · 5
Advisory, not mandatory.
Airframe · Canadair CL-600-2B16
SAIB AIR-21-15R1Navigation SystemSAIB NM-11-51Ice and Rain Protection: Wing Anti-Ice SystemSAIB NM-10-13Navigation: Flight Management SystemSAIB NE-03-28Engine · GE CF34 series
SAIB NE-04-77Historical bulletins · 1
NTSB investigations
No NTSB investigations matched to N359VMatched 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 Canadair CL-600-2B16 aircraft
FAA incident reports
No FAA accident or incident reports matched to N359VMatched 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 Canadair CL-600-2B16 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 9JLA2022051323840Flight Recorder · inoperativeTHE FLIGHT CREW REPORTED OF RECEIVING A CAS MESSAGE INDICATING THE FLIGHT DATA RECORDER CIRCUIT BREAKER HAD TRIPPED. THE MAINTENANCE TEAM FOUND THE FLIGHT DATA RECORDER UNIT TO BE CAUSING THE FDR CIRCUIT BREAKER TO TRIP. REMOVED AND REPLACED FDR WITH AN INSPECSDR 9JLA2022042523838None · failedFLIGHT CREW REPORTED THE ICE DETECTOR 2 FAILED. OPERATIONS WERE CONTINUED ON MEL 30-80-1. THE MAINTENANCE TEAM TROUBLESHOT AND FOUND THE #2 ICE DETECTOR INOP. THE DETECTOR WAS REMOVED AND REPLACED WITH AN INSPECTED UNIT. OPS CHECKS WERE SATISFACTORY AND THE AISDR 9JLA2021120123821Selector Valve · defectiveTHE FLIGHT CREW REPORTED THAT THEY DIVERTED BACK TO KICT AFTER THE ILLUMINATION OF A #3 HYDRAULIC OVERHEAT INDICATION. THE LANDING WAS UNEVENTFUL. THE MAINTENANCE VENDOR TROUBLESHOT AND DETERMINED THAT THE LANDING GEAR SELECTOR VALVE WAS DEFECTIVE. THE VALVE WSDR 9JLA2021111023816Servo · faultedTHE FLIGHT CREW REPORTED THE AIRCRAFT PITCH NOSE UP/NOSE DOWN ERRATICALLY WITH AUTO-PILOT CONNECTED. AUTO-PILOT TRIM NOSE UP/ NOSE DOWN MESSAGE ILLUMINATED. OPERATIONS WERE CONTINUED PER MEL. THE MAINTENANCE VENDOR DETERMINED AN AUTOPILOT SERVO WAS AT FAULT ANSDR 9JLA2021072723805Ecu · failedDURING AIRCRAFT OPERATIONS THE FLIGHT CREW REPORTED THE APU WAS INOP. THE APU FAULT WAS DEFERRED BY MEL AND THE FLIGHT CONTINUED. THE MAINTENANCE VENDOR TROUBLESHOT AND DETERMINED THAT THE APU CONTROL UNIT HAD FAILED. THE DEFECTIVE ECU WAS REMOVED AND A TESTEDSDR 9JLA2021060323801Fire Bottle · low pressureTHE FLIGHT CREW REPORTED THE APU BOTTLE LO CAUTION MESSAGE ILLUMINATED, THE MAINTENANCE DISCREPANCY WAS DEFERRED. THE MAINTENANCE TEAM COULD NOT DETERMINE THE CAUSE OF THE LOW BOTTLE PRESSURE. THE APU FIRE BOTTLE WAS REMOVED AND AN OVERHAULED UNIT WAS INSTALLESDR 9JLA2021040620042Actuator · leakingTHE FLIGHT CREW REPORTED THAT DURING POST-FLIGHT CHECKS FLUID LEAKING FROM OUT OF THE RIGHT MAIN LANDING GEAR ACTUATOR. THE MAINTENANCE VENDOR FOUND THE RIGHT MLG ACTUATOR LEAKAGE WAS OUT OF LIMITS. THE RIGHT MLG ACTUATOR WAS REMOVED AND A TESTED ACTUATOR WAS SDR 9JLA2021020420033Computer · faultedTHE FLIGHT CREW REPORTED THAT IN FLIGHT THE "TAIL TANK HEAVY AND TAIL XFER SHUTOFF VALVE CLOSED" ANNUNCIATOR ILLUMINATED. THE MAINTENANCE VENDOR TROUBLESHOT COMPLETED TROUBLESHOOTING AND DETERMINED THAT THE FUEL COMPUTER P/N 736847-4 S/N 0247 WAS FAULTY. THE MSDR 9JLA2019021316338Cable Assy · frayedDURING A MAINTENANCE CHECK IT WAS FOUND THAT THE MAIN CABIN DOOR POWER ASSIST CABLE WAS SHOWING SIGNS OF FRAYING AND BROKEN STRANDS. THE CABLE WAS REPLACED. P/N 2R49573001-1SDR 9JLA2019021316336Relay · defectiveTHE FLIGHT CREW REPORTED THAT DURING FLIGHT THE AC ESS BUS CAUTION MESSAGE ILLUMINATED IN FLIGHT. TROUBLESHOOTING DETERMINED THE CENTRAL BUS RELAY P/N HA4A039 AND VOLTAGE SENSOR RELAY B0804074-001 TO BE DEFECTIVE. INSTALLED NEW RELAYS. FUNCTIONAL CHECKS SATISFSDR 9JLA2019021316333Switch · defectiveTHE MAINTENANCE TEAM REPORTED THAT THE APU FIRE WARNING DISCHARGE BUTTON WILL NOT ILLUMINATE DURING LAMP TEST TROUBLESHOOTING DETERMINED THAT THE PUSH BUTTON SWITCH P/N 13740-002 WAS DEFECTIVE. THE SWITCH WAS REPLACED WITH NEW. OPS CHECKS WERE SATISFACTORY.SDR 9JLA2019021316330Control Valve · intermittentTHE FLIGHT CREW REPORTED THAT DURING PREFLIGHT CHECKS IT WAS NOTED THAT THE APU LOAD CONTROL VALVE (LCV) OPERATIONS WERE INTERMITTENT. TROUBLESHOOTING DETERMINED THAT THE APU BLEED-AIR LCV. THE VALVE WAS REMOVED AND REPLACED WITH A REPAIRED CONTROL VALVE. OPS
STCs that may be installed · 858
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Canadair CL-600-2B16
STC ST01305WI-DModification of a Collins ALT-50A or ALT-55B Radio Altimeter system installation to a Collins ALT-1000 or ALT-4000 Radio Altimeter system installation in accordance with Collins Drawing Index as listed on AML No. ST01305WI-D, Revision -, or later FAA approved revision.STC ST12461IBInstallation of Cockpit Voice Recorder with optional RIPS UpgradeSTC ST00885LAInstallation of fire extinguisher cartridges as replacements for Pacific Scientific fire extinguisher cartridges in fire extinguisher bottles.
Earlier aircraft with this N-number · 1
This aircraft carried N359V before the one registered now. The FAA can assign a mark to another aircraft once a registration is cancelled.