Registered owner
Martinaire Aviation LLC
Location
Addison, TX
Owner type
LLC
Serial number
208B0102
Year built
1988
Type
Fixed wing single engine
Engine
Turbo-prop
Airworthiness
Standard, normal
Airworthiness date
July 1, 1988
Certificate issued
October 26, 2006
Expires
October 31, 2028
Mode S code
AD9C49

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.

On this page

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 N9760BMatched 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 · 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 · 5

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

SDR 2017FA0000572Mount 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 · N9760B · Cessna 208B · Horizontal Stabilizer, Attach FittingsSDR 2016F00196Circuit Breaker · failedWHILE ON APPROACH TO HHW AND DESCENDING PRE-LANDING CHECK FOUND THE FLAPS WERE NOT COMPLETELY IN THE FULL UP POSITION. PILOT MOVED THE FLAP HANDLE TO THE UP POSITION WITH NO MOVEMENT OF THE INDICATOR NEEDLE. SUBSEQUENTLY SWITCHED OVER TO THE STANDBY FLAP SYSep 29, 2016 · N9760B · Cessna 208B · Trailing Edge Flap Control SystemSDR MT9A00000018Bellcrank · damagedTHE BOLT WAS FROZEN TO THE BUSHING SLEEVE. THIS PREVENTED THE BOLT FROM ROTATING INSIDE THE BUSHINGS AND ELONGATED THE BOLT HOLE THROUGH THE MOUNTING BRACKET. ALSO, THE SLEEVE CORRODED TO THE BELLCRANK. (K)May 8, 2008 · N9760B · Cessna 208B · Trailing Edge Flap Control SystemSDR MT9A00000017Bellcrank · corrodedTHE BOLT WAS FROZEN TO THE BUSHING SLEEVE. THIS PREVENTED THE BOLT FROM ROTATING INSIDE THE BUSHINGS AND ELONGATED THE BOLT HOLE THROUGH THE MOUNTING BRACKET, ALSO, THE SLEEVE HAD CORRODED TO THE BELLCRANK. (K)May 8, 2008 · N9760B · Cessna 208B · Trailing Edge Flap Control SystemSDR MT9A00000016Bellcrank · damagedTHE BOLT WAS FROZEN TO THE BUSHING SLEEVE. THIS PREVENTED THE BOLT FROM ROTATING INSIDE THE BUSHINGS AND ELONGATED THE BOLT HOLE THROUGH THE MOUNTING BRACKET. (K)May 5, 2008 · N9760B · 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 N9760B before the one registered now. The FAA can assign a mark to another aircraft once a registration is cancelled.