- Registered owner
- Ryan Air Inc
- Location
- Anchorage, AK
- Owner type
- Corporation
- Serial number
- 208B5120
- Year built
- 2014
- Type
- Fixed wing single engine
- Engine
- Turbo-prop
- Airworthiness
- Standard, normal
- Airworthiness date
- June 7, 2014
- Certificate issued
- July 1, 2014
- Expires
- July 31, 2027
- Mode S code
- A97007
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 21
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1988 | 1 |
|---|---|
| 1990 | 2 |
| 1996 | 1 |
| 1997 | 1 |
| 1998 | 2 |
| 2001 | 1 |
| 2002 | 1 |
| 2003 | 1 |
| 2004 | 2 |
| 2005 | 2 |
| 2006 | 3 |
| 2007 | 1 |
| 2008 | 3 |
| 2009 | 3 |
| 2021 | 1 |
| 2023 | 1 |
See all 26 ADs
Information bulletins that may apply · 3
Advisory, not mandatory.
NTSB investigations
No NTSB investigations matched to N707RAMatched 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 Cessna 208B aircraft
FAA incident reports
No FAA accident or incident reports matched to N707RAMatched 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 Cessna 208B aircraft
Service difficulty reports · 8
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR UATA5120929265701Flap Track · crackedFOUND CRACK IN OUTBOARD FLAP TRACK ON RH WING., TRACK WAS REMOVED AND REPLACED WITH NEW TRACK (PN: MC2622075-6, SN: J079924-020) AND BACK DRILLED TO PRE-EXISTING RIVET SIZES. TRACK WAS INSTALLED WITH MS20470AD RIVETS, AND HL18PB HI-LOKS OF VARYING LENGTHS. ALLSDR UATA5120205265301Attach Fitting · corrodedRIGHT FUSELAGE STRUT FITTINGS FAILED SID 53-20-07-250. LIFT STRUT FITTINGS. REMOVED FLOOR PANELS 2611127-18, 2611127-22 AND PULLY BRACKET 2612112-2 REMOVED FOR ACCESS. CAP ASSEMBLY 2611011-66 RIVETS REMOVED TO OUTBOARD SEAT RAIL FOR ACCESS. REMOVED LIFT STRUT SDR UATA5120710252101Unknown · smoke"WHEN BLEED AIR IS TURNED ON, SMOKE ENTERS COCKPIT." "INSPECTED, NO SMOKE WAS OBSERVED COMING FROM THE ENGINE COMPARTMENT." CAUSE SUSPECTED TO BE DIRT/DUST IN BLEED AIR HEAT/VENT DISTRIBUTION.SDR UATA7071031245702Flap Track · corrodedRIGHT FLAP MIDDLE FLAP TRACK HAS SEVERE CORROSION INBOARD SIDE. REMOVED AND REPLACED RIGHT FLAP MIDDLE FLAP TRACK IN REFERENCE TO C208 SRM 51-40-00.SDR UATA7071031245301Fitting · corrodedL/H AIRFRAME LOWER STRUT FITTING FOUND TO BE CORRODED/PITTED. REPLACED BOTH LH LOWER STRUT FITTINGS WITH NEW 2611113-5 AND 2611113-6. SEE 337 DATED 10/29/2024 FOR FURTHER DETAIL.SDR UATA202106227078Static Wick · crackedDURING THE SCHEDULED 100HR INSPECTION, A 0.75" CRACK WAS DISCOVERED, EMANATING FROM THE OUTBD STATIC WICK BASE ON THE L/H ELEVATOR. THE STATIC WICK WAS REMOVED AND THE CRACK WAS STOP DRILLED USING A #40 DRILL BIT. A REINFORCING DOUBLER OF 2024T3, 0.025" THICK,SDR UATA202007155307Attach Bracket · crackedDURING AN INSPECTION, THE TWO VERTICAL BRACKETS ON EITHER SIDE OF THE FLAP ACTUATOR, BETWEEN FS 201.5 AND 215.813 WERE FOUND TO HAVE CRACKS IN THE RADIUS OF THE BOTTOM FLANGE.SDR UATA202007157107Support Bracket · crackedLT ENGINE COWL INERTIAL SEPARATOR INLET SUPPORT BRACKET FOUND CRACKED UPON ROUTINE ENGINE INSPECTION.
STCs that may be installed · 300
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Cessna 208B
Earlier aircraft with this N-number · 1
This aircraft carried N707RA before the one registered now. The FAA can assign a mark to another aircraft once a registration is cancelled.