Registered owner
Martinaire Aviation LLC
Location
Addison, TX
Owner type
LLC
Serial number
208B0334
Year built
1993
Type
Fixed wing single engine
Engine
Turbo-prop
Airworthiness
Standard, normal
Airworthiness date
August 4, 1993
Certificate issued
March 23, 2026
Expires
March 31, 2033
Mode S code
A01333

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 · 3

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 2017FA0000560Mount Bolt · corrodedWHILE PERFORMING A FLEET CAMPAIGN DIRECTIVE CREATED TO INSPECT THE HORIZONTAL STABILIZER MOUNT BOLTS, IT WAS FOUND THAT ALL FOUR OF THEM WERE CORRODED.Jul 21, 2017 · N1037N · Cessna 208B · Horizontal Stabilizer, Attach FittingsSDR MT9A201304230001Mount · crackedDURING A RECENT SCHEDULED INSPECTION, CRACKS WERE FOUND IN THE SUPPORT DOUBLER EMANATING ACROSS THE LOWER LT MOUNT BOLT HOLE OF THE AFT ELEVATOR BELLCRANK MOUNT. ALSO SEVERAL ADJACENT RIVETS IN THIS DOUBLER WERE ALSO CRACKED ACROSS THEIR HOLES AND THE DOUBLERApr 23, 2013 · N1037N · Cessna 208B · Fuselage Main, Attach FittingsSDR M36R20120114001Switch · failedPILOT REPORTED THE NR 1 AVIONICS SWITCH WAS STUCK AND THE NR 2 AVIONICS SWITCH WAS ALSO REPORTED INOPERATIVE WHEN PLACED IN THE ON POSITION. ON INSPECTION, FOUND THAT BOTH AVIONICS SWITCHES HAD FAILED. IT WAS ALSO LATER DETERMINED THAT THE 2 SWITCHES WERE WJan 14, 2013 · N1037N · Cessna 208B · Electrical Power System WiringSDR M36R201302011001Buss · miswiredDURING REPLACEMENT OF NR 1 AND NR 2 AVIONICS MASTER SWITCHES IT WAS NOTED THAT THE AVIONICS BUSS TIE SWITCH WAS MISSED WIRED. THE BUSS TIE SWITCH IS TO BE WIRED FROM THE OUTPUT OF AV NR 1 BUSS MASTER TO OUTPUT OF THE AV NR 2 BUSS MASTER. THIS AIRCRAFT TIE SWNov 29, 2012 · N1037N · Cessna 208B · Electrical Power System WiringSDR 2013FA0000086Switch · failedTHE PILOT REPORTED THE NR1 AVIONICS SWITCH FOR ACFT WAS STUCK ON AND THE NR 2 AVIONICS SWITCH WAS INOPERATIVE. THE PILOT REPORTED THE CONDITION TO THE TOWER, SHUTDOWN ALL AVIONICS DUE TO OVERHEATING AND LANDED USING TOWER LIGHT SIGNALS. UPON INSPECTION IT WANov 29, 2012 · N1037N · Cessna 208B · Electrical Power SystemSDR MT9A00000031Bearing · corrodedTHE SEALED BEARING WAS CORRODED AND FROZEN. ALSO, THE BEARING WAS CORRODED TO THE BOLT. (K)May 12, 2008 · N1037N · Cessna 208B · Trailing Edge Flap Control SystemSDR MT9A00000032Bearing · corrodedTHE SEALED BEARING WAS CORRODED AND FROZEN, ALSO THE BEARING WAS CORRODED TO THE BOLT. (K)May 12, 2008 · N1037N · Cessna 208B · Trailing Edge Flap Control System

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 N1037N before the one registered now. The FAA can assign a mark to another aircraft once a registration is cancelled.