Registered owner
Pa1 208b-0410 LLC
Owner type
LLC
Serial number
208B0410
Year built
1994
Type
Fixed wing single engine
Engine
Turbo-prop
Airworthiness
Standard, normal
Airworthiness date
January 25, 2001
Certificate issued
September 12, 2026
Expires
September 30, 2033
Mode S code
ADB4F0

From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every Pratt & Whitney PT6A model are included below.

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Airworthiness directives that may apply · 47

Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.

1968In forceSuperseded2026
ADs by the year they took effect: 53 ADs
19681
19691
19701
19751
19771
19782
19802
19861
19881
19903
19921
19941
19951
19961
19972
19982
20012
20022
20031
20042
20053
20063
20071
20083
20093
20112
20121
20142
20151
20161
20211
20221
20231
20241
See all 54 ADs

Information bulletins that may apply · 8

Advisory, not mandatory.

NTSB investigations · 1

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

FAA incident reports · 1

FAA accident and incident reports matched to this aircraft by N-number and event date, checked against the reported make and model.

Service difficulty reports · 13

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

SDR 2019FA0000274Flap Track · wornFLAP TRACKS WORNApr 23, 2019 · N9820F · Cessna 208B · Trailing Edge FlapsSDR 2019FA0000273Flap Track · wornFLAP TRACKS WORNApr 23, 2019 · N9820F · Cessna 208B · Trailing Edge FlapsSDR 2019FA0000272Torque Tube · corrodedRUDDER TORQUE TUBE REQUIRES REPLACEMENTApr 23, 2019 · N9820F · Cessna 208B · Rudder Control SystemSDR 2019FA0000271Structure · dentedDENTED ELEVATORApr 23, 2019 · N9820F · Cessna 208B · Elevator, Plate/SkinSDR 2019FA0000270Support Bracket · chafedFLAP LEADING EDGE CHAFING AND SUPPORT BRACKET WEARApr 23, 2019 · N9820F · Cessna 208B · Trailing Edge FlapsSDR 2019FA0000269Skin · chafedCHAFE DAMAGE ON LOWER COWLINGApr 23, 2019 · N9820F · Cessna 208B · Fuselage Main, Plate/SkinSDR 2019FA0000268Door Frame · corrodedLOWER CARGO DOOR THRESHOLD AIRFRAME SKIN CORRODEDApr 23, 2019 · N9820F · Cessna 208B · Fuselage Main, StructureSDR 2017F00194Bolt · shearedTWO AN5-40A BOLTS SHEARED UPON LANDING. TORQUES WASH VERIFIED TO BE CORRECT AND WHEN WHEEL WAS BUILT UP TORQUE SEAL WAS USED. THREADED PORTION OF THE BOLT SHEARED CLEAN THIS IS THE SECOND AIRCRAFT IN THE FLEET TO HAVE THIS ISSUE. WHEEL WAS REMOVED AND A NEW WHOct 11, 2017 · N9820F · Cessna 208B · Wheel/Ski/FloatSDR PNSA111101AAnnunciator · smokeSMOKE COMING FROM TOP OF PANEL IMMEDIATELY BELOW GLARE SHIELD.Nov 2, 2011 · N9820F · Cessna 208B · Central WarningSDR PNSA060807Alternator · failedDURING CRUISE FROM DLG TO TOG, STANDBY ALTERNATOR WARNING LIGHT ILLUMINATED. PILOT RETURNED TO DLG WHERE MAINTENANCE REPLACED STANDBY ALTERNATOR AND RETURNED AIRCRAFT TO SERVICE.Aug 15, 2006 · N9820F · Cessna 208B · AC Generator-AlternatorSDR PNSA050804Caliper · shearedON LANDING AT KCQ RIGHT BRAKE FAILED. MX FOUND TOP ANCHOR PIN OF RT BRAKE CALIBER SHEARED. BRAKE CAUSED DAMAGE TO WHEEL ASSY AND BRAKE TORQUE PLATE. REPLACED BRAKE TORQUE PLATE, ANCHOR PINS, WHEEL ASSY AND BRAKE PADS. AIRCRAFT RETURNED TO SERVICE.Aug 30, 2005 · N9820F · Cessna 208B · Master Cylinder/Brake ValveSDR PNSA040604Hub · damagedSLUGGISH RESPONSE TO TAKEOFF POWER AND RPM/TORQUE DROPPED OFF AT FLIGHT IDLE POWER SETTINGS. AIRCRAFT MADE NORMAL LANDING WITH POWER LEVER FURTHER FORWARD THAN NORMAL. MAINTENANCE FOUND PROPELLER BLADE ANGLE IN HUB 2 DEGREES OFF AND BETA RING BENT. AT TEARDOWJun 28, 2004 · N9820F · Cessna 208B · Propeller Hub SectionSDR 20000328SH006Inverter · failedWHILE ON A DATA GATHERING NIGHT FLIGHT. THE EQUIPMENT POWERED BY THE INVERTER LOST POWER. WHILE REACHING FOR THE POWER DISCONNECT SWITCH, A FLASH WAS NOTICED IN THE AREA IN WHICH THE INVERTER WAS INSTALLED. POWER TO THE INVERTER WAS CUT OFF AND THE AIRCRAFTFeb 24, 2000 · N9820F · Cessna 208B · AC Inverter

STCs that may be installed · 357

Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.

See all 357 STCs