No fatalities

Cessna 402C Hydraulic Failure Results in Landing Incident Near Boston (N18VV)

Boston, MA, United States

On September 17, 2024, a CESSNA 402 C (registration N18VV) operated by Cape Air was involved in an aviation accident near Boston, MA. No fatalities were reported. Investigators recorded the probable cause as: The failure of a solid hydraulic fluid line, which resulted in a loss of hydraulic fluid that prevented the landing gear extension process from completing normally. This summary draws on records from NTSB; 17 related events involving the same aircraft type or operator are linked below.

SourcesNTSBPrimary reportUpdated 1785761257Data APIEditorial standards

A Cape Air Cessna 402C sustained substantial damage after a hydraulic system failure caused landing gear malfunction; pilot and passengers uninjured.

Accident Summary

On September 17, 2024, at about 1730 eastern daylight time, a Cessna 402C, registration N18VV, operated by Cape Air as a Title 14 Code of Federal Regulations Part 135 scheduled passenger flight, was substantially damaged during a landing incident near Boston, Massachusetts. The pilot and two passengers were not injured.

Pilot's Account

According to the pilot, during climb out, both the left and right hydraulic flow lights flickered. Suspecting a loss of hydraulic pressure, the pilot attempted to extend the landing gear before all pressure was lost, but only the left main landing gear green position light illuminated. The hydraulic flow lights then illuminated steadily. The pilot decided to return to the departure airport, notified air traffic control, and requested delaying vectors to perform checklists. Following the "Landing Gear Will Not Extend Hydraulically" checklist, the pilot verified that the landing gear position indicating lights functioned normally with the "press to test" feature, as they had on the ground before takeoff. With the landing gear switch already down, the pilot slowed the airplane to under 130 knots, pulled the "GEAR HYD" circuit breaker, and pulled the emergency landing gear extension handle. There was no change in the position indicator lights nor any indication or noise that the gear had extended.

Landing and Damage

The pilot subsequently landed on the left main landing gear and began lowering the airplane’s nose. During the landing roll, the right wing contacted a runway light, after which a fuel leak began. The airplane came to rest upright on the right side of the runway at an intersection of the runway and taxiway.

Post-Accident Examination

Examination of the hydraulic system by the operator’s maintenance department revealed a fractured solid hydraulic line connected to the hydraulic system filter, with all hydraulic fluid drained from the system. Maintenance personnel then performed the emergency landing gear extension procedure by pulling the emergency extension handle fully out, observing all three landing gear come down and lock. A review of the airplane’s maintenance records could not determine the age of the hydraulic line or whether any maintenance had been performed on it.

Operator Response

Following the accident, the operator issued a Technical Notice to all maintenance personnel emphasizing the importance of general inspection criteria during maintenance on the airplanes.

Contributing factors

Gear extension and retract sys — FailurePilotIncorrect use/operation