- Registered owner
- Umb Bank Na Trustee
- Location
- Salt Lake City, UT
- Owner type
- Corporation
- Serial number
- 35830
- Year built
- 2009
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- December 17, 2022
- Certificate issued
- November 2, 2022
- Expires
- November 30, 2029
- Mode S code
- AAFDC4
From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every CFM International CFM56-7B26/3 model are included below.
On this page
Airworthiness directives that may apply · 10
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 2007 | 1 |
|---|---|
| 2009 | 1 |
| 2010 | 2 |
| 2014 | 1 |
| 2015 | 2 |
| 2018 | 4 |
| 2019 | 1 |
| 2021 | 1 |
| 2022 | 1 |
| 2023 | 1 |
Engine · CFM International CFM56-7B26/3 series
AD 2023-05-05Turbine Engine Compressor SectionAD 2022-02-03Turbine Engine Accessory DriveAD 2018-26-01Turbine Engine Compressor SectionAD 2018-09-51EngineEmergency ADAD 2015-18-0473-tooth gearshaft located in the engine accessory gearbox (AGB)AD 2015-04-02Dual engine thrust instability eventAD 2010-13-09Stage 3 low-pressure turbine (LPT)AD 2010-01-05LP turbine rear framesAD 2009-11-02HPC 4-9 spoolsAD 2006-26-01Fuel filtersSuperseded and historical ADs · 5
Information bulletins that may apply · 1
Advisory, not mandatory.
Engine · CFM International CFM56-7B26/3 series
SAIB NE-08-17R3Turbine Section - Propulsion Technology LLC Unapproved RepairNTSB investigations
No NTSB investigations matched to N807VLMatched 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 737-8EH aircraft
FAA incident reports
No FAA accident or incident reports matched to N807VLMatched 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 737-8EH aircraft
Service difficulty reports · 6
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR BJNA202608240001Power Supply · faultedEMERGENCY EXIT ISLE LIGHT OUT BETWEEN ROWS 3 AND 15. IAW WDM 33-51-13 AND WDM 33-51-21 FOUND BAD POWER SUPPLY PACKS M2335, M1695, AND M1676. NOTED SHORTS FROM ISLE EMERGENCY LIGHTS. CORRECTED SORTS IAW WDM 33-51-13 AND WDM 33-51-21. R & R EMERGEMNCY ISLE HOUSDR BJNA202601150001Bleed Valve · leakingON DESCENT THROUGH LOWER ALTITUDES BELOW 12,000 FT CABIN HAS STRONG ENGINE OIL/ WET SOCK SMELL. PERFORMED FIM FOR SMOKE/FUMES IN CABIN IAW FIM 21-00 TASK 806 UP TO STEP F. (F). OIL SMELL ON HAPPENS WHEN RIGHT ENGINE BLEED IS THE SUPPLY FOR PNEUMATIC/PACK SYSTSDR BJNA20250503001Battery Pack · inoperativeDURING SERVICE CHECK FOUND EMREGENCY AISLE LIGHTS ROW 9 ABC AND ROW 12 ABC INOP. R/R EMERGENCY POWER SUPPLY/BATTERY PACK IAW AMM 33-51-06/201 A/C OK FOR SERVICE POS M2335SDR BJNA202501250001Lamp · burned outFOUND EMERGENCY, AREA LIGHT LAMP INOP. AT SEAT 5DEF. R/R EMERGENCY AREA LIGHT LAMP IAW AMM 33-51-03-960-801. OPS CHECK GOOD. A/C OK FOR SERVICE. LIGHT AT SEAT LOCATION 5 DEF.SDR BJNA202410170001Charger · inoperativeFOUND M1671 BATTERY POWER SUPPLY INOP. UNABLE TO CHARGE BATTERY. REMOVED & REPLACED POWER SUPPLY IAW AMM 33-51-06-960-806. OPS CHECK GOOD.SDR BJNA20230823001Packing · failedLOST B HYD SYS QTY ON TAXI OUT. FOUND PACKING PN: NAS1612-4 ON FRONT PLUG. REMOVED AND REPLACED FAILED (BLOWN) PACKING IAW AMM 20-10-17. OPS CHECK GOOD AFTER SERVICING IAW AMM 12-12-00. AC OK FOR SERVICE. NO LEAKS DETECTED AT THIS TIME.
STCs that may be installed · 2
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Engine · CFM International CFM56-7B26/3 series
STC SE04840NYInstallation of HarcoSemco Exhaust Gas Temperature (EGT) Electrical Harnesses in CFM56-7 engineSTC SE03036CHApplication of a deep compressive stress layer using a Low Plasticity Burnishing (LPB) process on CFM56-7 Series Engines Stage 1 High Pressure Compressor (HPC) Blade Dovetails in accordance with Delta Air Lines Inc. Drawing No. 72-0396, Revision B, dated November 3, 2011, or later FAA Approved revision.