Registered owner
Pa1 208b-0319 LLC
Owner type
LLC
Serial number
208B0319
Year built
1992
Type
Fixed wing single engine
Engine
Turbo-prop
Airworthiness
Standard, normal
Airworthiness date
October 9, 1992
Certificate issued
September 12, 2026
Expires
September 30, 2033
Mode S code
A00F60

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

No NTSB investigations matched to N1026VMatched 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 N1026VMatched 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 · 10

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

SDR ENHA20191111618Wire · damagedPILOT LOG PAGE DISCREPANCY: "USE OF WINDSHIELD HEAT CAUSED ELECTRICAL SPARKS TO COME FROM L/H CIRCUIT BREAKER PANEL"Nov 8, 2019 · N1026V · Cessna 208B · Ice/Rain Protection System WiringSDR ENHA2019092600005Skin · crackedFROM FAA FORM 337: REPAIRED SMALL CRACK APPROXIMATELY 1" LENGTH ON RIGHT WING UPPER SKIN JUST FORWARD OF TRAILING EDGE AT RIGHT WING STATION 53. STOP DRILLED CRACK AND INSTALLED SMALL REPAIR PATCH IAW MODEL STRUCTURAL REPAIR MANUAL 51-78-00-8.Sep 26, 2019 · N1026V · Cessna 208B · Wing, Plate/SkinSDR ENHA2019092600004Skin · damagedFROM FAA FORM 337: REPAIRED SMALL HOLE APPROXIMATELY 1/8" DIAMETER ON RIGHT WING UPPER SKIN JUST FORWARD OF TRAILING EDGE AT RIGHT WING STATION 46. INSTALLED SMALL CIRCULAR PATCH IAW MODEL STRUCTURAL REPAIR MANUAL 51-78-00-8.Sep 26, 2019 · N1026V · Cessna 208B · Wing, Plate/SkinSDR EHNA2019092600003Skin · crackedFROM FAA FORM 337: FOUND RT UPPER FUSELAGE SKIN (P/N 2611001-2) CRACKED AT FS 186.45, RBL 25.40, AND WL 141.00. REPLACED SKIN P/N 2611001-2 WITH NEW PART IAW FIELD REPAIR #FR-208B0319-7011.Sep 26, 2019 · N1026V · Cessna 208B · Fuselage Main, Plate/SkinSDR ENHA2019092600002Skin · dentedFROM FAA FORM 337: LEFT OUTBOARD HORIZONTAL STABILIZER LEADING EDGE DENTED. REPLACED OUTBOARD LEADING EDGE SKIN P/N 2632000-3, LEADING EDGE RIB P/N 2632021-7 AND P/N 2632021-8 WITH NEW PARTS USING ORIGINAL RIVET SIZE AND SPACING IAW SRM 55-30-00.Sep 26, 2019 · N1026V · Cessna 208B · Horizontal Stabilizer, Plate/SkinSDR ENHA2019092600001Bulkhead · crackedFROM FAA FOR 337: REPAIRED SMALL CRACK IN FUSELAGE BULKHEAD @ FS 400. STOP DRILLED CRACK AND INSTALLED DOUBLER IAW MODEL SERIES STRUCTURAL REPAIR MANUAL 53-20-00.Sep 26, 2019 · N1026V · Cessna 208B · Fuselage Main, BulkheadSDR AJAA2014F00027Transponder · failedUPON TAKEOFF THE PILOT NOTICED A BURNED ODOR IN THE COCK-PIT. ALL CIRCUIT BREAKERS WERE IN, NOTHING TRIPPED. PILOT NOTICED THAT THE TRANSPONDER WAS DISPLAYING A "FAILURE" ON THE SCREEN. TURNED POWER OFF TO TRANSPONDER, AND CAME BACK AROUND FOR A SAFE LANDINNov 8, 2013 · N1026V · Cessna 208B · Navigation SystemSDR BSYA200600026Door · unsecureON TAKEOFF OUT OF BOS PILOT HAD A DOOR AJAR LIGHT COME ON. ABORTED TAKEOFF SECURED CARGO DOOR AND CONTINUED WITH FLIGHT.Sep 21, 2006 · N1026V · Cessna 208B · Door Warning SystemSDR BSY2004F00000Odor · detectedGOT A STRONG ODOR (ELECTRICAL) IN COCKPIT. HAD MAINTENANCE LOOK AT AIRCRAFT COULD NOT DUPLICATE PROBLEM.Oct 24, 2003 · N1026V · Cessna 208B · Air Distribution SystemSDR BSY2002F00020Wire · looseON TAKE OFF OUT OF BOSTON, SPARKS WERE FLYING OUT FROM UNDERNEATH PILOTS PANEL, RETURNED TO BASE. FOUND EXPOSED WIRE OUT OF CONNECTOR P160 ON WIRE NR HA20 ON PROPELLER DEICE CIRCUIT, SHORTED ON SIDE PANEL REPAIRED CONNECTOR, OPS GOOD.Aug 9, 2002 · N1026V · Cessna 208B · Propeller/Propulsor System Wiring

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

Earlier aircraft with this N-number · 1

This aircraft carried N1026V before the one registered now. The FAA can assign a mark to another aircraft once a registration is cancelled.