- Registered owner
- Bering Air Inc
- Location
- Nome, AK
- Owner type
- Corporation
- Serial number
- 408-0018
- Year built
- 2023
- Type
- Fixed wing multi engine
- Engine
- Turbo-prop
- Airworthiness
- Standard, normal
- Airworthiness date
- July 31, 2023
- Certificate issued
- September 7, 2023
- Expires
- September 30, 2030
- Mode S code
- A4CE2A
From the FAA registry file of October 22, 2026.
On this page
Airworthiness directives that may apply · 2
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 2023 | 1 |
|---|---|
| 2026 | 1 |
Information bulletins that may apply
Advisory, not mandatory.
No bulletins matched this aircraft’s models
NTSB investigations
No NTSB investigations matched to N409BAMatched 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 Textron 408 aircraft
FAA incident reports
No FAA accident or incident reports matched to N409BAMatched 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 Textron 408 aircraft
Service difficulty reports · 13
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR FXTA20261016001Rib · cracked3 CRACKED RIBS RIGHT FLAP COVE. RIB P/N: 7822265-10 @ WS 100.5", RIB P/N: 7822265-12 @ WS 116.0", RIB P/N: 7822265-12 @ 131.5"SDR FXTA20260628002Flex Drive · failedRT OUTBOARD FLAP FLEX SHAFT RUBBER CASE FAILING AT THE CRIMP UNDER STAINLESS STEEL OUTER WRAP. THIS SEPARATION ALLOWS THE OUTER CASE TO LENGTHEN AND THE INNER DRIVE SHAFT CAN SLIDE LEFT AND RIGHT TO THE POINT THE DRIVE COMES OUT OF THE JACKSCREW CAUSING THE FLSDR FXTA20260628001Bolt · looseFLAP ACTUATOR ATTACHMENT HARDWARE FOUND LOOSESDR FXTA20251029001Cylinder · leakingPILOT FELT STRONG LEFT RUDDER PRESSURE ON TWO CONSECUTIVE TAKE OFFSSDR FXTA20240325003Exhaust Duct · crackedLEFT EXHAUST ON LEFT SIDE OF THE ENGINE CRACKED AROUND WELDED TUBE FOR THE HEATED INLET LIP.SDR FXTA20250408003Pressure Switch · looseFOUND LH ENGINE OIL LOW PRESSURE SWITCH LOOSE IN BOSS.SDR FXTA2020404000004Door · out of rigAFT CABIN DOOR CAS MESSAGE CONTINUOUSLY ON. AFT DOOR PROXIMITY SWITCH NEEDED RE-RIGGED.SDR 2024FA0000799Skin · crackedDURING AIRCRAFT WASH, 18-INCH CRACK FOUND ON LEFT VERTICAL STABILIZER SKIN AND TOP PANEL, BELOW RUDDER COUNTERBALANCE. FOUND LEFT FWD & AFT SKIN TO BE CRACKED AT BEND RADIUS.SDR FXTA20240729004Screw · looseCO-PILOTS YOKE SHAFT ATTACHMENT SCREWS LOOSE.SDR FXTA20240312001Cylinder · leakingRUDDER BIAS SYSTEM ALLOWING RUDDER TO FAVOR ONE SIDE INSTEAD OF BALANCING AS DESIGNED. MORE PILOT RUDDER INPUT REQUIRE TO COUNTER ACT.SDR FXTA2024032105001Cylinder · leakingRUDDER PEDAL HARDER TO PUSH WITH RUDDER BIAS ON. FOUND THE RUDDER BIAS AIR CYLINDER LEAKING AIR FROM ONE SIDE CAUSING THE RUDDER TO BIAS THE NON LEAKING SIDE.SDR FXTA2024032129001Support · crackedLH LOWER ENGINE COWLINGS HAVE STRUCTURE CRACKED UNDER THE ICE VANE DOOR LINKAGE CASTING ATTACHMENTS. P/N: 7852122-28 & 7852122-27 CRACKEDSDR FXTA2024032110001Duct · chafedLH & RH AFT ICE VANE DOOR FOUND CHAFING ON EXIT DUCT CAUSING A GROOVE TO BE WORN INTO THE SKIN WHEN THE ICE VANES WERE IN THE NORMAL CONFIGURATION.
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.
Earlier aircraft with this N-number · 1
This aircraft carried N409BA before the one registered now. The FAA can assign a mark to another aircraft once a registration is cancelled.