N910TA

No registry detail on file · not in current registry

Operators of this aircraft

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

OperatorRolePeriodBasis
Penobscot Island AirOperator2011-07-17 – 2011-07-17Operator named in NTSB report

Accident & incident history

Acc · 2011-07-17 Operator named in NTSB report
CESSNA U206G Serious injury Part 135Penobscot Island Air
Source: NTSB case ERA11LA405

Maintenance disclosures

O · 2011-05-27 Unresolved
ATA 8530

DURING A 100HR INSPECTION, DISCOVERED BLOWBY BETWEEN FINS ON THE INTAKE SIDE OF THE CYLINDER. THE CYLINDER WAS REMOVED AND FOUND TO BE CRACKED BETWEEN THE INTAKE VALVE SEAT AND THE SPARK PLUG HOLE. THIS IS THE 6TH CYLINDER THIS YEAR WITH ALMOST IDENTICAL CRACKS.

Source: SDR PNB2011F00003 · FAA SDRS
O · 2011-05-27 Unresolved
ATA 8530

DURING A 100 HR INSP, DISCOVERED BLOWBY BETWEEN FINS ON THE INTAKE SIDE OF THE CYLINDER. THE CYLINDER WAS REMOVED AND FOUND TO BE CRACKED BETWEEN THE INTAKE VALVE SEAT AND THE SPARK PLUG HOLE. THIS IS THE 5TH CYLINDER THIS YEAR WITH ALMOST IDENTICAL CRACKS.

Source: SDR PNB2011F00004 · FAA SDRS
O · 2011-05-03 Unresolved
ATA 8530

LOW COMPRESSION NR2 CYLINDER ON 100HR INSPECTION. FOUND BLOWBY COMING AROUND FINS IN THE HEAD. CYLINDER WAS CRACKED BETWEEN SPARK PLUG HOLE AND INTAKE VALVE. ALL PREVIOUS COMPRESSION CHECKS WERE IN THE 70/60 RANGE.

Source: SDR PNB2011F00005 · FAA SDRS
O · 2011-05-03 Matched by certificate designator
ATA 8530

LOW COMPRESSION NR2 CYLINDER ON 100 HR INSPECTION. FOUND BLOW-BY COMING AROUND FINS IN THE HEAD. CYLINDER WAS CRACKED BETWEEN SPARK PLUG HOLE AND INTAKE VALVE. ALL PREVIOUS COMPRESSION CHECKS WERE IN THE 70/60 RANGE.

Source: SDR O592011F00000 · FAA SDRS
O · 2010-05-19 Unresolved
ATA 3220

DURING A 100 HR INSP, FOUND NOSE GEAR HAD FORE AND AFT MOVEMENT WHERE THERE SHOULD BE NONE. REMOVED AFT DRAG LINK BOLT TO INVESTIGATE AND FOUND IT TO BE WORN AND DEFORMED AS IF GETTING READY TO SHEAR. THIS IS THE THIRD OR FOURTH FOUND. THE OTHER ACFT THAT WERE FOUND HAD SHEARED THE BOLT AND LUCKILY DIDN`T COLAPSE THE GEAR. RECOMEND EITHER A MODIFICATION TO A LARGER BOLT OR 1000 HR TIME REPLACEMENT ESCECIALLY IF THE ACFT IS BEING USED ON ROUGH, UNIMPROVED RUNWAYS. PART IS NR 6 ON FIG 38 IN MFG SRM. THIS ACFT HAS HAD A LANDING DOSE FORK INSTALLED SINCE 12/9/04 AND HAS 1384.2 HRS SINCE IT WAS INSTALLED.

Source: SDR 2010FA0000595 · FAA SDRS