- Registered owner
- Bank Of Utah Trustee
- Location
- Salt Lake City, UT
- Owner type
- Corporation
- Serial number
- 43337
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Certificate issued
- September 27, 2021
- Expires
- September 30, 2028
- Mode S code
- ACC1EB
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 39
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 2018 | 3 |
|---|---|
| 2019 | 3 |
| 2020 | 6 |
| 2021 | 9 |
| 2022 | 2 |
| 2023 | 8 |
| 2024 | 5 |
| 2025 | 2 |
| 2026 | 8 |
See all 46 ADs
Information bulletins that may apply · 4
Advisory, not mandatory.
NTSB investigations
No NTSB investigations matched to N921AKMatched 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 737-9 aircraft
FAA incident reports
No FAA accident or incident reports matched to N921AKMatched 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 737-9 aircraft
Service difficulty reports · 64
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR ASAA2026080867883Lamp · inoperativeROW 17ABC LOWER EMERGENCY EXIT LIGHT ASSY HAS BULBS INOP. GROUNDED - YES. RELAMPED 17ABC LWR EMERY EXIT LIGHT ASSY, OPS CHECK GOOD REF B737 AMM 33-51-04.SDR ASAA2026072367850Transition Panel · corrodedAFT CARGO COMPT RIGHT SIDE TRANSITION PANEL UPPER AND LOWER SURFACE HAS CORROSION NUMEROUS PLACE BETWEEN BS767 AND BS727J+13. GROUNDED - YES. BLENDED AWAY CORROSION. ORIGINAL THICKNESS .040, MAT LOSS IN VARIOUS LOCATIONS AT .009, NEW THICKNESS IN VARIOUS LOCATSDR ASAA2026072367849Transition Panel · corrodedAFT CARGO COMPT RIGHT SIDE TRANSITION PANEL UPPER AND LOWER SURFACE HAS CORROSION NUMEROUS PLACE BETWEEN BS727J+13 AND BS727+4. GROUNDED - YES. BLENDED AWAY CORROSION ORIGINAL THICKNESS .040 MAT LOSS AT GREATEST .006 IN VARIOUS PLACES, NEW THICKNESS .034 AREA
See all 64 reportsSTCs that may be installed · 105
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
See all 105 STCs