ALASKA ISLAND AIR INC

Part 135 operator · designator K1IC

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: ALASKA ISLAND AIR, ALASKA ISLAND AIR INC

Accident & enforcement record

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

NTSB accidents & incidents

No NTSB accidents or incidents linked to this operator.

FAA enforcement actions

No FAA enforcement actions linked to this operator.

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 2004–2013. Most-reported systems: ATA 85 — 2; Instruments (31) — 1; Doors (52) — 1; Stabilizers (55) — 1. Most-common natures of condition, as filed: OTHER — 4; VIBRATION/BUFFET; ENGINE STOPPAGE — 1.

5 reports on file.

VIBRATION/BUFFET; ENGINE STOPPAGE · 2013-04-04 Matched by certificate designator
N8374T · ATA 8530

Part: NOZZLE — MISSING (PISTON) · airframe 13,379 hrs

DURING CRUISE FLIGHT, A LOUD NOISE WAS HEARD COMING FROM THE ENGINE COMPARTMENT. FOLLOWED BY AN AIRFRAME VIBRATION, WHICH WAS FOLLOWED BY AN ENGINE SHUT DOWN. AFTER LANDING A LARGE HOLE WAS FOUND IN THE ENGINE CRANKCASE ABOVE THE NR 5 CYLINDER. DURING THE TEARDOWN INSPECTION, IT WAS NOTED THAT THE PISTON COOLING NOZZLE ASSEMBLIES HAD NOT BEEN INSTALLED. IT APPEARS THAT SOMETIME DURING THE ASSY OF THE ENGINE, A STD-1339, PLUG WAS INSTALLED INSTEAD OF A COOLING NOZZLE. THE PLUG EFFECTIVELY BLOCKS OFF THE FLOW OF OIL TO THE BASE OF THE CYLINDERS PREVENTING THEM FROM GETTING ANY ADDITIONAL COOLING AND LUBRICATION.

Source: SDR CY4R201309050001
OTHER · 2009-05-15 Matched by certificate designator
N8374T · ATA 5210

Part: LOOP — LOOSE (UPPER SILL)

THE LOOP ASSEMBLY IN THE UPPER SILL PLATE OF THE FUSELAGE AFT CABIN DOOR BECAME LOOSE, ALLOWING THE UPPER LATCH AT THE TIP OF THE DOOR TO RELEASE DURING CRUISE FLIGHT. THE TOP PORTION OF THE DOOR INCLUDING THE WINDOW, SUBSEQUENTLY BROKE OFF, DENTING THE LT INBD LEADING EDGE STABILATOR SKIN BETWEEN THE 2 MOST INBD RIBS. NO FURTHER DAMAGE WAS NOTED, AND FLIGHT CHARACTERISTICS REMAINED UNAFFECTED. PRIOR TO FLIGHT THE DOOR APPEARED TO BE SECURELY LATCHED.

Source: SDR K1I2009F00000
OTHER · 2005-07-16 Matched by certificate designator
N9304K · ATA 5540

Part: DOUBLER — CRACKED (RUDDER HINGE)

CRACKS WERE FOUND AT THE TOP OF THE RUDDER SPAR HINGE DOUBLER. CRACKING WAS ON BOTH SIDES OF THE DOUBLER IN THE BEND RADIUS`S. ACCESS FOR INSPECTION NECCESSITATES REMOVING THE RUDDERS TIP/COUNTERWEIGHT. RECURRENCE MAY BE PREVENTED BY FABRICATING AND INSTALLING AN ADDITIONAL SIMILAR DOUBLER ON THE AFT SIDE OF THE SPAR OPPOSITE THE EXISTING DOUBLER. HOWEVER, THAT MAY EFFECT FLEXIBILITY AND CAUSE THE RUDDER SPAR TO RECEIVE EXTRA STRESS. (AL03200519295) (K)

Source: SDR 2005FA0001406
OTHER · 2005-04-28 Matched by certificate designator
N8374T · ATA 3160

Part: ANTENNA — INOPERATIVE (FUSELAGE)

FOUND LOWER UAT ANTENNA UNSERVICEABLE DURING UAT UPGRADE. (K)

Source: SDR 2005FA0001061
OTHER · 2004-07-14 Matched by certificate designator
N8374T · ATA 8520

Part: CRANKCASE — CRACKED (ENGINE)

CRANK IN CRANKCASE JUST BELOW CYLINDER NR 3 BETWEEN THE BOTTOM CYLINDER HOLD DOWN STUDS AND ROCKER DRAIN NIPPLES. CRACK IS APPROX 2.5 INCHES LONG. (AL03200418212)

Source: SDR 2004FA0000775

Linked aircraft

N-numberMake / modelYearStatusLink basis
N73FQPIPER PA-32-3011981Valid RegistrationMatched by certificate designator
N8374TPIPER PA-32-3011981Valid RegistrationMatched by certificate designator
N9304KMatched by certificate designatorOperator named in NTSB report