Registered owner
Martinaire Aviation LLC
Location
Addison, TX
Owner type
LLC
Serial number
208B0085
Year built
1988
Type
Fixed wing single engine
Engine
Turbo-prop
Airworthiness
Standard, normal
Airworthiness date
April 12, 1988
Certificate issued
October 26, 2006
Expires
October 31, 2028
Mode S code
AD37B0

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 · 2

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

FAA incident reports · 2

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 2017FA0000569Mount 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 · N9505B · Cessna 208B · Horizontal Stabilizer, Attach FittingsSDR 2009FA0000043Shroud · gougedENG PERFORMANCE RUNS INDICATED ITT WAS EXCEEDING TARGET TEMP +20 DEGREES C. THE ENGINE WAS SPLIT AT THE C-FLANGE AND THE ENG SEPARATED TO INSPECT THE HOT SECTION. IT WAS FOUND THAT THE CT BLADE SEGMENTS HAD SHIFTED AND ALSO THERE WAS SEGMENT TIP CURL AT SEVERJan 12, 2009 · N9505B · Cessna 208B · Turbine SectionSDR MT9A00000020Housing · wornRT BRAKE CYLINDER HOUSING WORN AT THE ANCHOR BOLT PASS THROUGH HOLE ALLOWING THE ANCHOR BOLT TO BE PRESSED OUT BY HAND. THIS IS NORMALLY A CLOSE TOLERANCE FIT. THIS CONDITION IN THE PAST HAS CAUSED THE ANCHOR BOLT TO SHEER OFF CAUSING CATASTROPHIC DAMAGE TO TMay 12, 2008 · N9505B · Cessna 208B · Landing Gear Brake SystemSDR MT9A00000019Housing · wornLT BRAKE CYLINDER HOUSING WORN AT THE ANCHOR BOLT PASS THROUGH HOLE ALLOWING THE ANCHOR BOLT TO BE PRESSED OUT BY HAND. THIS IS NORMALLY A CLOSE TOLERANCE FIT. THIS CONDITION IN THE PAST HAS CAUSED THE ANCHOR BOLT TO SHEER OFF CAUSING CATASTROPHIC DAMAGE TO THMay 12, 2008 · N9505B · Cessna 208B · Landing Gear Brake SystemSDR MT9A00000007Bellcrank · frozenTHE BOLT WAS FROZEN TO THE BUSHING SLEEVE. THIS PREVENTED THE BOLT FROM ROTATING INSIDE THE BUSHINGS. (K)May 9, 2008 · N9505B · Cessna 208B · Trailing Edge Flap Control SystemSDR MT9A00000009Bearing · corrodedTHE SEALED BEARING WAS CORRODED AND FROZEN ALSO, THE BEARING WAS CORRODED TO THE BOLT. (K)Apr 10, 2008 · N9505B · Cessna 208B · Trailing Edge Flap Control SystemSDR MT9A00000008Bearing · frozenTHE BOLT WAS FROZEN TO THE BUSHING SLEEVE. THIS PREVENTED THE BOLT FROM ROTATING INSIDE THE BUSHINGS. (K)Apr 10, 2008 · N9505B · 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 N9505B before the one registered now. The FAA can assign a mark to another aircraft once a registration is cancelled.