- Registered owner
- Sunrise Asset Management LLC
- Location
- Las Vegas, NV
- Owner type
- LLC
- Serial number
- 4253
- Year built
- 2010
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- March 31, 2010
- Certificate issued
- August 26, 2022
- Expires
- August 31, 2029
- Mode S code
- A2C574
From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every CFM International CFM56-5B4 model are included below.
On this page
Airworthiness directives that may apply · 391
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1990 | 5 |
|---|---|
| 1991 | 1 |
| 1992 | 6 |
| 1993 | 10 |
| 1994 | 10 |
| 1995 | 4 |
| 1996 | 5 |
| 1997 | 10 |
| 1998 | 22 |
| 1999 | 14 |
| 2000 | 15 |
| 2001 | 9 |
| 2002 | 15 |
| 2003 | 3 |
| 2004 | 23 |
| 2005 | 20 |
| 2006 | 13 |
| 2007 | 16 |
| 2008 | 10 |
| 2009 | 13 |
| 2010 | 8 |
| 2011 | 12 |
| 2012 | 12 |
| 2013 | 17 |
| 2014 | 18 |
| 2015 | 23 |
| 2016 | 25 |
| 2017 | 24 |
| 2018 | 31 |
| 2019 | 24 |
| 2020 | 29 |
| 2021 | 17 |
| 2022 | 22 |
| 2023 | 19 |
| 2024 | 15 |
| 2025 | 21 |
| 2026 | 17 |
See all 558 ADs
Information bulletins that may apply · 8
Advisory, not mandatory.
Airframe · Airbus A320-214
SAIB NE-19-03Escape Slide Maintenance Tasks and Intervals - JASC 2565SAIB NM-15-02Cabin Equipment/FurnishingsSAIB NM-14-21Communications: Honeywell RTA 44D VHF TransceiversSAIB NM-13-24Air Conditioning System: Air Distribution FanSAIB NM-13-03Hydraulic Power System: Power Transfer UnitSAIB NM-06-57Reports of damage to airplanes and to property on the ground caused by blue or clear ice falling from airplanes.Engine · CFM International CFM56-5B4 series
SAIB NE-08-17R3Turbine Section - Propulsion Technology LLC Unapproved RepairSAIB NE-12-29Engine Fuel Distribution CFM56-5B LPTACC Fuel ManifoldHistorical bulletins · 1
NTSB investigations
No NTSB investigations matched to N278NVMatched 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 Airbus A320-214 aircraft
FAA incident reports
No FAA accident or incident reports matched to N278NVMatched 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 Airbus A320-214 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 WX0A2026080332913Epsu · no test(AIRCRAFT NOT GROUNDED) DURING EPSU SYSTEM TEST BAT/EPSU(10WL) FWD L FAULT. / FOLLOWING TSM 33-51-00-810-829-A, REMOVED AND REPLACED 10WL EPSU BATTERY IAW AMM 33-51-38-000-002-A AND AMM 33-51-38-400-002-A. OPS CHECK SATISFACTORY."SDR WX0A2026072432898Battery · inoperative(AIRCRAFT NOT GROUNDED) FLASHLIGHT BATTERY IN AFT JUMPSEAT INOP OR NOT CHARGING. REPLACED BATTERY IN AFT JUMPSEAT PER AMM 25-60-02"SDR WX0A2026021132729Horn · false activation(AIRCRAFT NOT GROUNDED) UNCOMMMANDED EVACUATION HORN ACTIVATION, RESET PER QRH, RESET SUCCESSFUL.. UNCOMMMANDED EVACUATION HORN ACTIVATION / RESET PER QRH/ RESET SUCCESSFUL. NOTED BY MOC."SDR WX0A2026012032706Unknown · odor(AIRCRAFT NOT GROUNDED) FROM APPROX 15000 FT TO 1000 FT DIRTY SOCK SMELL IN CABIN ON DESCENT. FLIGHT DECK FO NOTICED SMELL 4,000 TO 1,000 FT. COMPLIED WITH TC A32X-21-000-200. COMPLY WITH TASK CARD 21-000-003 WITHIN 10 CALENDAR DAYS. CW LVL 3 REF TC.SDR WX0A2025091732564Girt Bar · out of adjust(AIRCRAFT NOT GROUNDED) L1 DOOR SLIDE ARMING LEVER DOES NOT STAY FULLY IN ARMED POSITION / REF LP 2075758 FOR SLIDE REPLACMENT, LEVER WAS STILL NOT STAYING IN FULL ARM POSITION. REMVOED SLIDE, ADJUSTED GIRT BAR , AND INSTALLED SLIDE. L1 DOOR SLIDE LEVER STAYS SDR WX0A2024040532006Skin · cracked(MAJOR REPAIR - DISCREPANCY NOTED DURING HEAVY) LH WING LEADING EDGE , CRACK FOUND ON UP STOP #3 / L/H WING LEADING EDGE SKIN AT UP STOP #3 PERMANENTLY REPAIRED AS PER SRM 57-41-11-300-006 REV.148. REPAIR CATEGORY A. NO FURTHER ACTION REQUIRE. P/N: 2024T3 .063SDR WX0A1900010031976Flap System · faulted(EMERGENCY DECLARED) F/CTL FLAPS LOCKED WING TIP BRK ON GOING FROM FLAPS 1 TO 2 ON APPROACH / WHILE ACCMP TSM 27-51-00-810-819-A ON PAGE 2 STEP #4 SUBSTEP 4 PARA A, VISUALLY EXAMINED THE APPU (30VU) FOR SIGNS OF WATER THROUGH THE SIGHT GLASS, FOUND WATER DAMAGSDR WX0A2024031431976Appu · faulted(EMERGENCY DECLARED) F/CTL FLAPS LOCKED WING TIP BRK ON GOING FROM FLAPS 1 TO 2 ON APPROACH / WHILE ACCMP TSM 27-51-00-810-819-A ON PAGE 2 STEP #4 SUBSTEP 4 PARA A, VISUALLY EXAMINED THE APPU (30VU) FOR SIGNS OF WATER THROUGH THE SIGHT GLASS, FOUND WATER DAMAGSDR WX0A2023091031836Unknown · unknownFOUND AFT MEGAPHONE TO BE EXPIRED / REMOVED AND REPLACED AFT MEGAPHONE REF LOPA. OPS CHECK GOOD."SDR WX0A2023090531829Epsu · unknownBAT/EPSU FAULT WHILE PERFORMING EPSU TEST (10WL & 13WL) / REMOVED AND REPLACED EPSU BATTERY (10WL & 13WL) IAW AMM 33-51-38-000-002-A & 33-51-38-400-002-A."SDR WX0A2022112331657Power Supply · inoperativeRIGHT OVERWING EMEGENCY EXIT LIGHTS AND SIGN INOP / REMOVED AND REPLACED EMERGENCY BATTERY REF TSM 33-51-00-810-812-A OPS CHECK GOOD"SDR 1E1R2022102600419Hinge Arm · crackedTHE HINGE ARM BR1 AND ATTACH FORK FITTING OF THE VERTICAL STABILIZER WAS FOUND WITH A CRACK AT HOLES #5 AND #7 DURING INSPECTIONS. MAINTENANCE ATTEMPTED TO REMOVE THE CRACK DAMAGE BY OVERSIZING. THE CRACK STILL REMAINS AT EACH HOLE WITH A DIAMETER OF 0.279".
STCs that may be installed · 301
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
See all 301 STCs