N9304F

CESSNA 208 · 1985 · Fixed-wing single-engine · 1 engine · 10 seats · Valid Registration

Registered owner: SKYDIVE BALTIMORE LLC, DE (owner ≠ operator)

Operators of this aircraft

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

OperatorRolePeriodBasis
Peninsula Airways Inc.Operatoron 1997-10-20Operator named in NTSB report

Accident & incident history

Incident · 1997-10-20 Operator named in NTSB report
Cessna 208B No injuries Part 135Peninsula Airways Inc.

Operated by PENINSULA AIRWAYS INC. (per NTSB report)

Source: NTSB case ANC98IA004
HUGHES 269B Fatal injury Part 91operator not named in the NTSB record
Source: NTSB case MIA71AM016

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.

4 reports on file, 1997-10-18 – 2004-06-17.

FLT CONT AFFECTED · 2004-06-17 Unresolved
ATA 2720

Part: ROLL PIN — SHEARED (RUDDER PEDAL) · airframe 13,849 hrs

DURING TAXI LT RUDDER ROLL PIN PN NAS561C3-18 SHEARED CAUSING RUDDER PEDAL TO DISCONNECT AND CAUSE LOSS OF STEERING AND BRAKING ACTION ON LT SIDE.

Source: SDR PNSA040601
OTHER · 2000-06-21 Unresolved
ATA 5330

Part: SKIN — DAMAGED (FUSELAGE) · airframe 10,994 hrs · 30,446 cycles

DURING LOADING OF AIRCRAFT, TRUCK BUMPED FUSELAGE JUST AFT OF CARGO DOOR. FLIGHT WAS DELAYED WHILE MAINTENANCE INSPECTED DAMAGE. FOUND MINOR SCRATCH. AIRCRAFT RELEASED FOR SERVICE.

Source: SDR PNSA0601
F.O.D. · 1997-10-23 Unresolved
ATA 7200

Part: ENGINE — BIRDSTRIKE (WING)

ON SHORT FINAL, SUFFERED BIRD STRIKE TO ENGINE INLET AND PROP. LANDING UNEVENTFUL. AIRCRAFT INSPECTED AND RELEASED FOR SERVICE.

Source: SDR PNSA971004
FLT CONT AFFECTED · 1997-10-18 Unresolved
ATA 5751

Part: SCREWS — LOOSE (AILERON BAL WGT)

AILERON JAMMED IN LEFT TURN PILOT WAS ABLE TO FREE-UP CONTROLS AND LAND SAFELY. FURTHER INVESTIGATION REVEALED SCREWS THAT ATTACH AILERON BALANCE WEIGHT TO LEADING EDGE OF AILERON HAD BACKED OUT TO THE POINT OF CATCHING THE TRAILING EDGE OF THE WING GAP FAIRING. RESECURED SCREWS NO FURTHER DAMAGE WAS FOUND. INSPECTED THREE OTHER C- 208 AIRCRAFT IN THE FLEET FOUND EACH OF THEM HAD BALANCE WEIGHT ATTACH SCREWS REQUIRING 1/4 TO 1/2 TURN TO TIGHTEN THEM.

Source: SDR PNSA971001