- Registered owner
- Bank Of Utah Trustee
- Location
- Salt Lake City, UT
- Owner type
- Corporation
- Serial number
- 30283
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Certificate issued
- September 4, 2019
- Expires
- September 30, 2029
- Mode S code
- ADECB0
From the FAA registry file of October 22, 2026.
On this page
Airworthiness directives that may apply · 0
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
No ADs matched this aircraft’s modelsADs on appliances, propellers and installed equipment aren’t matched by model; check those separately.
Information bulletins that may apply
Advisory, not mandatory.
No bulletins matched this aircraft’s models
NTSB investigations
No NTSB investigations matched to N997AMMatched 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 737-76Q aircraft
FAA incident reports
No FAA accident or incident reports matched to N997AMMatched 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 737-76Q aircraft
Service difficulty reports · 61
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR ASMF202101023Skin · crackedDURING 8A-P CHECK AT MEX STATION, IT WAS DETECTED SEVERAL CRACKS AT BOTH HORIZONTAL STABILIZERS. MAINTENANCE PERSONNEL PERFORMED A REVISION, DETECTING A CRACK OF 3.5" LENGTH AT STAB STA 101.90 AND 0.5" DISTANCE FROM REAR SPAR; A CRACK OF 1.00" LENGTH AT STAB SSDR ASMF202101013Filter · leakingDURING TRANSIT CHECK, A HYDRAULIC LEAK WAS DETECTED IN THE HYDRAULIC SYSTEM B. MAINTENANCE PERSONNEL PERFORMED REVISION DETECTING HYDRAULIC LEAK AT IN ACOUSTIC FILTER. SO THE ACOUSTIC FILTER P/N 1013983-1, S/S, MANUFACTURER SUNDSTRAND WAS REPLACED, IAW AMM BSDR ASMF202011015Acoustic Panel · damagedDURING TRANSIT CHECK, IT WAS DETECTED SEVERAL NICKS ON RIGHT ENGINE INNER BARREL ACOUSTIC PANEL. MAINTENANCE PERSONNEL PERFORMED A REVISION, DETECTING A NICK OF 0.187 LENGTH, 0.046 WIDTH FROM 2.5" DISTANCE OF AFTER EDGE OF INNER BARREL ACOUSTIC PANEL AT 12 HR
See all 61 reportsSTCs that may be installed
No STCs matched this aircraft’s modelsSTCs are matched through the model’s type certificate data sheet, and this registry model isn’t matched to one.