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Atlas / NTSB / GAA16CA378

NTSB CAROL · Event

Event GAA16CA378

2016-07-14 Denver, Colorado, United States Airport · FTG None 1 aircraft Status: Completed

Registry · N465BP

FAA Aircraft Registry record.

Make / Model

PIPER PA46R-350T

Year of manufacture

2008 · 8 years old at event

Engine

LYCOMING TIO-540-AE2A (350 hp)

Seats / Engines

6 seats · 1 engine

Last airworthiness date

20080504

ADS-B equipped

Yes — Mode-S A5AC55

Registrant of record

CLEAR BLUE AVIATION LLC

Source: FAA Aircraft Registry (releasable master file).

Aircraft involved

Probable cause & findings

The pilot's improper nose down pitch attitude during touchdown resulting in a propeller strike, hard bounced landing, and nose landing gear collapse.

Factual narrative

The pilot reported that following an instrument flight rules (IFR) cross country flight, he canceled his IFR clearance, and made a visual approach to runway 26. He recalled that Tower told him that his airplane would be the last to land on runway 26, and he recalled that the inbound airplane behind him was vectored for an approach to runway 08. He reported that after landing, the nose gear collapsed and the airplane slid to the right side of the runway, and partially exited the runway before coming to rest. The airplane sustained substantial damage to the engine mounts, firewall and fuselage bulkheads. The Federal Aviation Administration Aviation Safety Inspector that examined the airplane and the accident scene, reported that during the landing the propeller struck the runway, the airplane bounced and settled back to the runway about 100 feet further down the runway where a second set of propeller blade strike markings were identified. The Inspector reported that the propeller blade strike markings were accompanied by black rubber skid marks that extended from the runway centerline and veered to the right edge of the runway. The Inspector reported that, the nose gear collapsed backwards as evidenced by white paint marks and metallic material scarring the asphalt. The airplane continued to veer to the right where it eventually departed the paved runway coming to a rest in the dirt. The Inspector confirmed that the distance from the initial propeller strike to the wreckage was about 735 feet. The meteorological aerodrome report at the accident airport reported that the wind direction and distance about the time of the accident was 010 degrees true at 4 knots. The pilot reported that following an instrument flight rules (IFR) cross country flight, he canceled his IFR clearance, and made a visual approach to runway 26. He recalled that Tower told him that his airplane would be the last to land on runway 26, and he recalled that the inbound airplane behind him was vectored for an approach to runway 08. He reported that after landing, the nose gear collapsed and the airplane slid to the right side of the runway, and partially exited the runway before coming to rest. The airplane sustained substantial damage to the engine mounts, firewall and fuselage bulkheads. The Federal Aviation Administration Aviation Safety Inspector that examined the airplane and the accident scene, reported that during the landing the propeller struck the runway, the airplane bounced and settled back to the runway about 100 feet further down the runway where a second set of propeller blade strike markings were identified. The Inspector reported that the propeller blade strike markings were accompanied by black rubber skid marks that extended from the runway centerline and veered to the right edge of the runway. The Inspector reported that, the nose gear collapsed backwards as evidenced by white paint marks and metallic material scarring the asphalt. The airplane continued to veer to the right where it eventually departed the paved runway coming to a rest in the dirt. The Inspector confirmed that the distance from the initial propeller strike to the wreckage was about 735 feet. The meteorological aerodrome report at the accident airport reported that the wind direction and distance about the time of the accident was 010 degrees true at 4 knots. Source: NTSB Aviation Accident Database Retrieved: 2026-02-12

NTSB Findings

Hierarchical cause / factor breakdown from the FAA bulk avdata database. Each finding tagged C (Cause) or F (Factor).

  • C Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Pitch control-Not attained/maintained - C
  • C Personnel issues-Task performance-Use of equip/info-Aircraft control-Pilot - C

Verbatim from NTSB's published report. Source file NTSB_2016_GAA16CA378.txt. Findings + structured fields enriched from FAA avall.mdb. Full investigation docket on data.ntsb.gov ↗.