NTSB CAROL · Event
Event SEA03LA037
Registry · N912LB
FAA Aircraft Registry record.
Make / Model
CESSNA 172S
Year of manufacture
2000 · 3 years old at event
Engine
LYCOMING I0360 SER (180 hp)
Seats / Engines
4 seats · 1 engine
Last airworthiness date
20001009
ADS-B equipped
Yes — Mode-S AC9F15
Registrant of record
ARIZONA FLYERS CLUB INC
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The pilot's failure to maintain adequate airspeed and the instructor's inadequate supervision of the flight. Contributing factors were the rime icing conditions, and the soft terrain encountered on the off runway rollout.
Factual narrative
On February 9, 2003, at 1540 Pacific standard time, a Cessna 172S, N912LB, registered to and being operated/flown by a private pilot, accompanied by a flight instructor, sustained substantial damage during a hard landing on flare/touchdown at the Snohomish County airport (PAE), Everett, Washington. Both pilots were uninjured. Instrument meteorological conditions (IMC) existed and an instrument flight rules (IFR) flight plan was in effect. The local flight, which was instructional, was operated under 14CFR91, and had originated from Boeing Field, Seattle, Washington, at 1440. The private pilot under instruction (PUI) reported that he was engaged in training towards an instrument rating with his flight instructor pilot (IP). He reported that he had acquired surface observations and terminal area forecast information for the area of the intended flight and had obtained an abbreviated weather briefing from Seattle Flight Service, and there was no reference to icing conditions. After their departure from Boeing Field and approaching the area of Paine Field both pilots overheard a radio report from another aircraft (location unknown) of icing conditions and the IP noted the formation of light rime ice on the non-icing certified aircraft's wings. The PUI initiated the VOR-B approach and broke out about 500-600 feet above ground after which a missed approach was executed. During the missed approach maneuver, approximately 1,000 feet altitude and in IMC, both pilots noted that the aircraft had begun picking up ice. The IP chose to terminate the flight and requested an "abbreviated" approach with radar vectors to the instrument landing system (ILS) runway 16R approach to a full stop landing on the 9,010 foot long runway. The aircraft was cleared for the approach and the IP briefed the PUI on the procedures for the approach i.e., "...higher speeds than normal at all times, no flaps, and fly the airplane onto the runway/no flare...." On short final, about 10-15 feet above ground, the left wing dropped and the aircraft landed hard on the left main gear and bounced. The pilot added power in an attempt to stabilize the aircraft and the flight instructor then took control of the aircraft but was unable to regain directional control. The aircraft continued off the left side of the runway and into soft terrain, during which the nose gear dug into soft terrain and the aircraft nosed over. The aircraft broke out about 500-600 feet above ground and the PUI reported that about 150-200 feet above ground approaching the threshold he began to slow his approach speed to 80-85 knots. As he crossed the threshold and 10-15 feet above the runway he "...pulled the power out and slowed up to about 70-75 knots..." at which time the IP felt the airframe shudder, the left wing "stalled," and the aircraft began a left roll/yaw. The aircraft's left wheel contacted the runway and the aircraft bounced. The IP took control of the aircraft, ensured that the power was cut and attempted to maintain directional control as the aircraft departed the left side of the runway rolling onto soft, wet grass during which it nosed over. The PUI remarked, "...after impact, I noted there was ice along most of the leading edges of both wings. I picked up one piece about 8-10 inches long, which had fallen off, and noted it had wrapped around the shape of the leading edge to form a flat face, perpendicular to the direction of the airflow. In its thickest part, it was about 0.75 - 1" thick, and about 0.25 - 0.5" in its thinnest part...." The private pilot under instruction (PUI) was engaged in training towards an instrument rating with a flight instructor pilot (IP) and had just executed a missed approach. During the missed approach maneuver, following his first instrument approach in IMC, the aircraft began picking up rime ice. The IP chose to terminate the flight and the aircraft was cleared via radar vectors for the ILS Runway 16R approach to the 9,010 foot long runway. The IP briefed the PUI on the procedures for the approach, specifically the need to maintain higher than normal airspeeds down to touchdown. On short final, about 10-15 feet above ground, and as the PUI retarded power and began decelerating to 70-75 knots, the left wing dropped and the aircraft landed hard on the left main gear and bounced. The IP then took control of the aircraft but was unable to regain directional control. The aircraft continued off the left side of the runway and into soft terrain, during which the nose gear dug in and the aircraft nosed over. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2003_SEA03LA037.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
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Related research
What the literature says.
Academic papers and agency reports matching this event's aircraft type or causal vocabulary (icing, stall, imc). Sourced from NASA NTRS, NTSB Safety Studies, FAA CAMI, AOPA Air Safety Institute, Embry-Riddle Scholarly Commons, arXiv, and the Semantic Scholar academic graph.
- arXiv 2023 · arXiv preprint
Variation of Critical Crystallization Pressure for the Formation of Square Ice in Graphene Nanocapillaries
Two-dimensional square ice in graphene nanocapillaries at room temperature is a fascinating phenomenon and has been confirmed experimentally.
- arXiv 2022 · arXiv preprint
Enhanced Prediction of Three-dimensional Finite Iced Wing Separated Flow Near Stall
Icing on three-dimensional wings causes severe flow separation near stall. Standard improved delayed detached eddy simulation (IDDES) is unable to correctly predict the separating reattaching flow due…
- NASA NTRS 2019 · Contractor Report (CR)
An Evaluation of an Analytical Simulation of an Airplane with Tailplane Icing by Comparison to Flight Data
This report presents the assessment of an analytical tool developed as part of the NASA/FAA Tailplane Icing Program. The analytical tool is a specialized simulation program called TAILSM4 which was de…
- NASA NTRS 2019 · Technical Publication (TP)
NASA/FAA Tailplane Icing Program: Flight Test Report
This report presents results from research flights that explored the characteristics of an ice-contaminated tailplane using various simulated ice shapes attached to the leading edge of the horizontal …
- NASA NTRS 2019 · Other
[Tail Plane Icing]
The Aviation Safety Program initiated by NASA in 1997 has put greater emphasis in safety related research activities. Ice-contaminated-tailplane stall (ICTS) has been identified by the NASA Lewis Icin…
- Embry-Riddle Scholarly Commons 2019 · Journal article (IJAAA)
Airport Policing in Pakistan: Structure, Training, and Issue
Airports are strategically and economically important installations of any country. Airports are the gateway of any country and any incidents at these gateways may harm the very aspects of a country i…
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