N78SA

CESSNA 208B · 1995 · Valid Registration

Registered owner: MARTINAIRE AVIATION LLC, TX (owner ≠ operator)

Operators of this aircraft

Who operated this tail, and how firmly we know it.

OperatorRolePeriodBasis
MARTINAIRE AVIATION L.L.C. (MT9A)Certificate holderMatched by certificate designator
MARTINAIRE AVIATION L.L.C. (MT9A)Operator2022-03-17 – 2022-03-17Operator named in NTSB report

Accident & incident history

Acc · 2022-03-17 Operator named in NTSB report
CESSNA 208B None injury Part 135MARTINAIRE AVIATION L.L.C.
Source: NTSB case CEN22LA149

Maintenance disclosures

O · 2019-11-18 Matched by certificate designator
ATA 7250

A STANDARD BORESCOPE INSPECTION OF THE COMPRESSOR TURBINE BLADES WAS CONDUCTED WITH NO DEFECTS NOTED IN ACCORDANCE WITH THE PRATT AND WHITNEY CANADA MAINTENANCE MANUAL. THE TECHNICIAN ELECTED TO DO AN ADDITIONAL INSPECTION OF THE BLADES THROUGH THE EXHAUST DUCT EVEN THOUGH IT IS NOT REQUIRED PER PWC MM 72-00-00 D(3)M NOTE 1. SEVERAL TIP TRAILING EDGES WERE FOUND TO BE DISCOLORED, CHIPPED AND/OR MISSING. THE ENGINE WAS OPENED AT “C” FLANGE AND THE CT DISC REMOVED. THE DISC WAS SENT TO AN APPROVED ENGINE FACILITY AND THE BLADES WERE REMOVED FOR ADDITIONAL INSPECTION. THIS INSPECTION NOTED HOT CORROSION PRESENT ON THE TIP OF EACH BLADE. THE ENGINE HAS RECEIVED REGULAR TURBINE AND COMPRESSOR WASH/RINSES AS DESCRIBED BY THE MAINTENANCE MANUAL. THE ENGINE SHOWED NO SIGNS OF CORROSION DURING THE PREVIOUS BORESCOPE OF THE CT BLADES THROUGH THE EXHAUST AND NOZZLE PORTS CONDUCTED 200 HRS. PRIOR TO THIS EVENT.

Source: SDR M36R201911260018 · FAA SDRS
O · 2017-07-21 Matched by certificate designator
ATA 5551

WHILE PERFORMING A FLEET CAMPAIGN DIRECTIVE CREATED TO INSPECT THE HORIZONTAL STABILIZER MOUNT BOLTS, IT WAS FOUND THAT ALL OF THEM WERE CORRODED.

Source: SDR 2017FA0000555 · FAA SDRS