N208SD

No registry detail on file · not in current registry

Operators of this aircraft

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

OperatorRolePeriodBasis
Hageland Aviation Services, Inc.Operatoron 2016-10-02Operator named in NTSB report

Accident & incident history

Accident · 2016-10-02 Operator named in NTSB report
CESSNA 208B Fatal injury Part 135Hageland Aviation Services, Inc.

Operated by HAGELAND AVIATION SERVICES INC (per NTSB report)

Source: NTSB case ANC17MA001

Maintenance disclosures

Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.

5 reports on file, 2010-02-01 – 2013-01-13.

OTHER · 2013-01-13 Unresolved
ATA 5553

Part: MOUNT — DAMAGED (VERTICAL STAB) · airframe 16,394 hrs · 29,785 cycles

VERTICAL STABILIZER BOLT MOUNTING HOLES WORN. REPAIRED VERTICAL STABILIZER HOLES IAW FORM 8110-3 DATED 1-12-2013. REPLACED AN176 TAIL ATTACH HARDWARE WITH INCREASED DIAMETER AN177 HARDWARE.

Source: SDR EPUA20130124002
OTHER · 2013-01-10 Unresolved
ATA 5730

Part: SKIN — LOOSE (RT WING) · airframe 16,394 hrs · 29,785 cycles

RIGHT WING TOP SKIN NEAR L/E HAS LOOSE RIVETS. REPAIRED RT WING IAW SRM 57-23-01, PARA 4 A-C, REV 4.

Source: SDR EPUA20130124003
OTHER · 2013-01-08 Unresolved
ATA 5330

Part: SKIN — WORN (BS 187) · airframe 16,394 hrs · 29,785 cycles

RT FUSELAGE SKIN AREA AT STA 187.00 AT WING STRUT ATTACH POINT HAS PREVIOUS REPAIR WORN BEYOND LIMITS. INSTALLED FUSELAGE SKIN REPAIR IAW FAA FORM 8110-3 DATED 1-13-13 AND DWG HAS-208-53-02.

Source: SDR EPUA20130124001
SMOKE/FUMES/ODORS/SPARKS · 2012-03-27 Unresolved
ATA 2120

Part: UNKNOWN — ODOR (CABIN) · airframe 15,550 hrs · 27,862 cycles

A BURNING ODOR WAS REPORTED IN ACFT. MX COULD NOT DUPLICATE ANY BURNING ODOR ON THE GROUND. SUBSEQUENT FLIGHT CHECK SHOWED NORMAL CONDITIONS, NO BURNING ODOR WAS PRESENT.

Source: SDR EPUA2012032901
OTHER · 2010-02-01 Unresolved
ATA 5730

Part: SKIN — CHAFED (LT WING) · airframe 12,798 hrs · 22,504 cycles

ABRASION ON LT INBOARD WING SKIN CAUSED FROM LT INBOARD WING/FUSELAGE FAIRING. LOCATED LEFT WING STATION 35 TO 35.5 INCHES FROM TRAILING EDGE, EXTENDING FORWARD 11 INCHES.

Source: SDR EPUA1553692