DENALI AIR INC

Part 135 operator · designator DLIA

Data confidence: Records are linked by certificate number, aircraft registration, or a name match that a reviewer has confirmed. Each record below shows how it was linked.

Also recorded as: DENALI AIR INC, Denali Air

Accident & enforcement record

Events that happened, regardless of the operator's own reporting. Each links to its public source.

NTSB accidents & incidents

Accident · 2012-09-13 Operator named in NTSB report
CESSNA A185F (N4786Q) No injuries Part 91

Operated by Denali Air (per NTSB report)

The pilot’s failure to maintain clearance from an electric transmission line during the approach to land because he was distracted by the airplane’s broken and deflected landing ski. Contributing to the accident was the in-flight failure of the right ski connecting bolt and the subsequent ski deflection.

Source: NTSB case ANC12LA106

FAA enforcement actions

Civil penalty ordered · 2017-05-17 Name match — reviewer confirmed
Drug & alcohol testing programAir carrier / commercial operator

Sanction: $2,100 · case closed 2017-09-15

Source: FAA case 2017WP910178

Maintenance disclosure history

Service Difficulty Reports are self-reported maintenance findings. The NUMBER of reports is not a measure of reliability — diligent operators file more, not fewer. These are shown for transparency, not as a negative signal. To verify a report, search its control number at the FAA SDRS site.

Reports span 1995–2012. Most-reported systems: Wings (57) — 2; Landing gear (32) — 1. Most-common natures of condition, as filed: OTHER — 3.

3 reports on file.

OTHER · 2012-09-13 Matched by certificate designator
N4786Q · ATA 3210

Part: BOLT — SHEARED (ACTUATOR)

AFT HYDRAULIC ACTUATOR BOLT WAS FOUND TO BE SHEARED IN HALF AND DISPLACED FROM ITS DESIGNED LOCATION. THE FAILURE OCCURRED DURING SKI ACTUATION WHILE AIRBORNE, FOLLOWING USE ON HARD/BREAKABLE CRUST SNOW SURFACES DURING PREVIOUS FLIGHTS. FURTHER INSPECTION OF THE BOLT REVEALED SIGNS OF A STRESS CRACK AND DISTORTION PRIOR TO SHEARING. RECOMMENDED REGULAR REMOVAL AND INSPECTION OF BOLT FOR FATIGUE AT REGULAR INTERVALS (100 HOUR/ANNUAL) OR MORE FREQUIENLY UNDER EXTREME USE CONDITIONS.

Source: SDR 2012FA0000684
OTHER · 1995-04-11 Matched by certificate designator
N6620L · ATA 5751

Part: RIB — CRACKED (RT AILERON)

REMOVED AND REPLACED SPAR AND RIB IN RT AILERON IAW SB 974. SPAR AND RIB BOTH CRACKED. TT OF ACFT 6772.4.

Source: SDR 95ZZZX2107
OTHER · 1995-04-11 Matched by certificate designator
N6620L · ATA 5751

Part: SPAR — CRACKED (RT AILERON)

REMOVED AND REPLACED SPAR AND RIB IN RT AILERON IAW SB 974. SPAR AND RIB BOTH CRACKED. TT OF ACFT 6772.4.

Source: SDR 95ZZZX2108

Linked aircraft

N-numberMake / modelYearStatusLink basis
N41101PIPER PA-31-350Valid RegistrationMatched by certificate designator
N47698PIPER PA-31-3101968Valid RegistrationMatched by certificate designator
N4786QCESSNA A185F1978Valid RegistrationMatched by certificate designatorOperator named in NTSB report
N555VSPIPER PA-31-3101971Valid RegistrationMatched by certificate designator
N6620LPIPER PA-31-3101969Valid RegistrationMatched by certificate designator
N974CSPIPER PA-31-3501976Valid RegistrationMatched by certificate designator