Registered owner
Pa1 208b-0672 LLC
Owner type
LLC
Serial number
208B0672
Year built
1998
Type
Fixed wing single engine
Engine
Turbo-prop
Airworthiness
Standard, normal
Airworthiness date
May 1, 1998
Certificate issued
September 13, 2026
Expires
September 30, 2033
Mode S code
A4D881

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 · 7

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

SDR ENHA 202410040001Tube · looseBLEED AIR HEAT INOP, NO AIRFLOW AND HOT SMELL WHEN BLEED AIR HEAT IS TURNED ON. MECHANICS FOUND SCAT TUBE AT CABIN AIR VALVE HAD COME LOOSE. RE-SECURED IAW 208MM 21-41-00, OPS CHECK GOOD.Sep 30, 2024 · N411GV · Cessna 208B · Air Distribution SystemSDR ENHA2024040800088Unknown · odorHOT ELECTRICAL SMELL. SMELL DISAPEARED ON TAXI BACK TO RAMP. SUSPECTED THAT DEICE FLUID WAS SPRAYED ON EXHAUST, MECHANICS INSPECTEDT ENGINE BAY, JUNCTION BOX, CIRCUIT BREAKER PANELS AND ALL WIRES BEHIND INSTRUMEENT PANEL, NO DEFECTS DETECTED.. PERFORMED RUNUApr 5, 2024 · N411GV · Cessna 208B · Air Distribution SystemSDR EPUA20170926001Fire Warning · false activationFIRE ALARM ACTIVATED WITH AUDIBLE PORTION ONLY , (NO LIGHT ILLUMINATED ON INSTRUMENT PANEL). FIRE DETECT WARNING HORN DEFERRED. NO FURTHER INFORMATION AVAILABLE AT THIS TIME.Sep 24, 2017 · N411GV · Cessna 208B · Fire DetectionSDR EPUA20170102001Bolt · brokenLEFT BRAKE ASSEMBLY BROKEN AND PARTIALLY DRAGGING. MAINTENANCE INSPECTED BRAKE ASSEMBLY AND DETERMINED THAT THE BOLT(PIN) HAD BROKEN AND CAUSED THE BRAKE ASSEMBLY TO CONTACT TIRE ASSEMBLY AND CAUSED IT TO START DRAGGING. DUE TO THIS EVENT THE FOLLOWING ITEMS WJan 2, 2017 · N411GV · Cessna 208B · BrakeSDR EPUA2015042215001Bolt · brokenLEFT TIRE ASSEMBLY STOPPED ROTATING UPON LANDING. INSPECTED & DETERMINED THAT ONE OF THE TWO ANCHOR BOLTS, PIN, ON THE BRAKE ASSEMBLY HAD BROKEN & CAUSED THE BRAKE ASSEMBLY TO JAM AGAINST THE TIRE ASSEMBLY THUS PREVENTING THE TIRE ASSEMBLY FROM ROTATING. REApr 22, 2015 · N411GV · Cessna 208B · BrakeSDR EPUA2012050101Bulkhead · crackedAFT CANTED BULKHEAD AT BS 474.4 CRACKED AT ELEVATOR PUSH PULL TUBE OPENING. DURING REMOVAL AFT VERTICAL SPAR WEB (2631021-12) WAS FOUND TO HAVE EXCESSIVE FRETTING, VERTICAL SPAR WEB ALSO REPLACED.Apr 27, 2012 · N411GV · Cessna 208B · Fuselage Main, BulkheadSDR EPUA032808Attach Bracket · crackedDURING ENGINE MAINTENANCE, 2 CRACKS APPROX .5 INCH LONG WERE DISCOVERED ON THE UPPER ENGINE MOUNT BRACKET ASSY-COWL ATTACH EMANATING FROM THE BOLT HOLE. A NEW BRACKET AND BOLT WERE INSTALLED AND AIRCRAFT WAS RETURNED TO SERVICE.Mar 27, 2008 · N411GV · Cessna 208B · Engine Mount Section

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