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Accidents · NTSB WPR13FA244 · Final report

Raytheon Aircraft Company A36 accident near Mountainaire, Arizona, May 28, 2013

On May 28, 2013 at about 6:43 pm local time, a 2001 Raytheon Aircraft Company A36, registered N999PK, was destroyed in an accident during initial climb near Mountainaire, Arizona (Flagstaff Pulliam Airport). It was a personal flight under general aviation rules (Part 91). 2 people were killed. The weather was visual conditions (good weather).

The NTSB's probable cause their words, unchanged

The pilot's inability to maintain a climb after departure in high-density altitude conditions, which resulted in a collision with trees and terrain. Contributing to the accident were the pilot's decision not to track the four-lane highway just beyond the departure runway, which he could have used as an alternate landing site; his premature rotation of the airplane; and degraded engine performance that affected the airplane's climb ability.

Source: NTSB aviation accident database, copy made November 2, 2026. Docket and reports at the NTSB.

What the record shows

Date
May 28, 2013 · about 6:43 pm local time · cases in 2013
Place
Mountainaire, Arizona · Flagstaff Pulliam Airport · cases near this airport · map
Type
Accident
Injuries
2 people were killed.
Weather
visual conditions (good weather)
Aircraft
Raytheon Aircraft Company A36, built 2001
Registration
N999PK · registry record · serial E-3380
Damage
Destroyed
Flight
Personal flight · general aviation rules (Part 91)

The NTSB's narrative final · quoted from the NTSB record

The pilot had purchased the Beechcraft airplane about 18 months before the accident and based it at his home airport, which was located at an elevation of about 80 ft mean sea level (msl). The pilot flew the Beechcraft to an airport that was at an elevation of about 7,100 ft msl. A few days after his arrival, he returned to the airport for his planned departure and spent about 15 minutes asking the fixed base operator owner, who was also a pilot, multiple questions about the route to his next planned destination. According to the owner, he was surprised by the nature of the pilot's questions, his lack of basic aeronautical information knowledge for area restrictions, and his lack of formal planning for his flight. No witnesses reported anything unusual about the engine start or taxi. At the time the pilot was cleared by the air traffic control tower controller for takeoff, the airport density altitude was about 9,000 ft. No ground witnesses reported observing anything unusual with the takeoff, but a Cessna 172 pilot who was behind the Beechcraft reported that the Beechcraft's climbout was slow. Shortly after his own takeoff, about 75 seconds after the Beechcraft, the Cessna pilot asked the tower controller about the Beechcraft's situation and intentions because the Cessna was already well above the Beechcraft. This prompted the controller to ask the Beechcraft pilot if he needed assistance, and the pilot responded that he was climbing "very slowly" and would remain near the airport. Shortly after that, the Cessna pilot saw the Beechcraft impact trees. The accident site was about 3 miles southeast of the airport at an elevation about 300 ft below that of the departure airport. A postimpact fire obscured or destroyed a significant amount of evidence. Review of the Beechcraft's published performance data revealed that, for the given conditions, the airplane should have been able to successfully depart the airport and climb at a rate of about 500 feet per minute. Most of the engine components and all of the propeller components that survived the accident, displayed no evidence of preimpact mechanical deficiencies. The engine cylinder conditions were indicative of a history of generally lean operation. In addition, the No. 5 cylinder exhaust valve's appearance was consistent with excessively lean operation for an undetermined period of time, and the fuel injector nozzle for that cylinder was found to be partially occluded. Excessively lean operation will reduce engine power output, and will manifest itself as abnormally high exhaust and cylinder head temperatures and possible engine roughness. Further, if the No. 5 cylinder's injector was occluded for the flight, it would have resulted in overly lean operation of and reduced power output from that cylinder, yielded higher exhaust and cylinder head temperatures, and likely manifested itself as engine roughness. (Some witnesses close to the impact site reported that the engine was making "popping" noises.) Although the airplane was equipped to monitor, display, and record temperatures for each cylinder, it could not be determined whether the pilot monitored that display, and fire damage prevented the recovery of that data from the engine monitor. Further, there was insufficient evidence to determine the source of the injector's occlusion, quantify its effects on engine power output, determine its relation to the condition of the exhaust valve, or determine if it was present for the takeoff or an artifact of the postimpact fire. Although the engine was developing power at impact, there was insufficient evidence to quantify the actual power output for the climb or at the time of impact. There was also insufficient evidence to determine whether the pilot ensured that the throttle and propeller controls were set to and remained in their appropriate positions for the departure or whether the pilot adjusted the mixture properly (not overly lean). It is likely that the pilot lifted off prematurely at a speed lower than the prescribed value and was unable to accelerate or climb the airplane once it exited the ground effect regime. Because the surrounding terrain and the impact point were lower than the elevation of the airport, the pilot was able to continue to fly the airplane before crashing. This scenario is at least partially corroborated by the pilot's reported lack of preparation for the flight, which could have included a lack of performance planning. This scenario is also partially corroborated by the observed repetitive minor banking of the airplane, which often occurs when an airplane is flying very slowly. A premature liftoff or a climb attempt at a speed significantly below the prescribed value would place the airplane in a situation where the power required for level flight was very near to or exceeded the available power. A recovery would require the pilot to lower the nose in order to accelerate the airplane to obtain a positive rate of climb. Such an action is counterintuitive when low to the ground and requires accurate problem recognition, knowledge of the correct solution, and sufficient terrain clearance to accomplish. During the departure, the pilot reduced his options by deciding to turn to the east instead of continuing straight ahead to the south. Review of topographic data revealed that a four-lane highway was located just beyond the south end of the runway, and was situated in a north-south valley that descended to the south. However, instead of tracking over that highway, which could have been used as an off-airport emergency landing site, and its descending valley, which provided increasing terrain clearance, the pilot opted to turn east, toward higher, wooded terrain. Although that turn was consistent with both a left traffic pattern (in order to remain close to the airport as the pilot reported to the air traffic controller), and toward the pilot's on-course heading, by making that turn, the pilot reduced the likelihood of a partially or fully successful outcome to the flight.

The complete narrative as the NTSB published it. The NTSB's docket holds the report as a PDF and any photographs, statements and other documents from the investigation.

The factual record from the NTSB's investigation tables, in plain English

What happened, in order

  1. Low altitude operation/event during initial climb
  2. Collision during takeoff/land during initial climb defining event

The NTSB's findings

  • cause Aircraft › Aircraft oper/perf/capability › Performance/control parameters › Climb rate › Attain/maintain not possible
  • cause Environmental issues › Conditions/weather/phenomena › Temp/humidity/pressure › High density altitude › Effect on operation
  • factor Personnel issues › Action/decision › Info processing/decision › Decision making/judgment › Pilot
  • factor Personnel issues › Action/decision › Action › Incorrect action performance › Pilot
  • factor Aircraft › Aircraft power plant › Engine (reciprocating) › (general) › Damaged/degraded other cases naming the engine
  • Environmental issues › Physical environment › Object/animal/substance › Tree(s) › Not specified
  • Environmental issues › Physical environment › Terrain › Mountainous/hilly terrain › Not specified

Pilot

  • Certificate: private
  • Ratings: single-engine land
  • Flight time: 540 hours in all
  • Medical certificate: Class 3 (with waivers/limitations)
  • Seat: left
  • Injury: fatal

The aircraft

  • Airframe total time: 893 hours
  • Last inspection: annual inspection, June 1, 2012
  • Seats: 6
  • Landing gear: retractable
  • Engine: Cont Motor IO-550 SERIES (piston); 900 hours total
  • Fire on the ground

The flight

  • Departed from: FLG Flagstaff AZ at 1:42 am
  • Destination: BCE Bryce Canyon UT
  • Flight plan: none
  • Runway 21, 8,800 ft by 150 ft

Weather at the time

  • Light: daylight
  • Wind: from 210° at 17 knots, gusting 26
  • Visibility: 10 statute miles
  • Sky: clear
  • Temperature: 64°F (18°C), dew point 25°F (-4°C)
  • Altimeter: 29.95 inHg
  • Observation at 6:57 pm from FLG, 3 miles away

Injuries

FatalSeriousMinorNone
Flight crew1
Passengers1

Documents from the investigation the NTSB's docket: the evidence folder behind the report

45 documents, released by the NTSB on July 22, 2015. View them here, or download them; the NTSB redacts some personal details before release, and this site shows the NTSB's own titles rather than its file names.

#DocumentWhat it is
1 Engine Data Monitor - Specialist's Factual Report PDF, 4 pages View Download
2 NTSB Amended Flg Ground Control Transcripts PDF, 2 pages View Download
3 Flg Local Control Transcripts PDF, 7 pages View Download
4 ATC Recording PDF, 1 page View Download
5 Flg Controller Statements PDF, 2 pages View Download
6 911 Call Log PDF, 7 pages View Download
7 Coconino County Sheriff’s Office Report Excerpts PDF, 3 pages View Download
8 Coconino County Sheriff’s Office Witness Statements PDF, 5 pages View Download
9 Record of Conversation - Witness James Patton PDF, 2 pages View Download
10 Record of Conversation - Witness John Patton PDF, 1 page View Download
11 Record of Conversation - Witness K Patton PDF, 2 pages View Download
12 Record of Conversation - Witness J Stapley PDF, 1 page View Download
13 Record of Conversation - Witness A Taloye PDF, 1 page View Download
14 Records of Communication - Witness Airborne Pilot PDF, 5 pages View Download
15 Highlands Fire Department Report PDF, 18 pages View Download
16 Record of Conversation – Proprietor of B&b PDF, 1 page View Download
17 Records of Conversation - FBO Owner PDF, 3 pages View Download
18 Record of Conversation - Ramp Agent PDF, 1 page View Download
19 Record of Conversation - Baggage Transport PDF, 1 page View Download
20 Record of Conversation - Airplane Fueler PDF, 1 page View Download
21 Record of Conversation - Maintenance Facility PDF, 1 page View Download
22 Record of Communication - NTSB Materials Laboratory PDF, 1 page View Download
23 Record of Conversation - Pilot’s Son PDF, 2 pages View Download
24 Record of Conversation - Pilot’s Nephew PDF, 1 page View Download
25 Record of Conversation - FAA Bonanza CFI PDF, 1 page View Download
26 Records of Conversation - FAA Hasslacher PDF, 3 pages View Download
27 Record of Conversation - Flight Instructor Robarts PDF, 2 pages View Download
28 Fuel Slip PDF, 1 page View Download
29 FBO Receipts PDF, 3 pages View Download
30 On Scene and Post Recovery Information PDF, 55 pages View Download
31 Cylinder Field Examination PDF, 7 pages View Download
32 Continental Motors Cylinder 5 Exam Report PDF, 4 pages View Download
33 Cylinder 5 Dimensions PDF, 1 page View Download
34 Continental Motors Fuel System Component Report PDF, 5 pages View Download
35 Engine Driven Fuel Pump Information PDF, 19 pages View Download
36 Continental Motors Ignition System Report PDF, 9 pages View Download
37 Hartzell Propeller Report 130528 Rev 1 PDF, 11 pages View Download
38 Propeller Part Number Email PDF, 4 pages View Download
39 Partial Maintenance Records PDF, 2 pages View Download
40 Fuel Injection Article PDF, 3 pages View Download
41 Operational and Performance Information PDF, 20 pages View Download
42 Flagstaff Airport Information PDF, 2 pages View Download
43 Toxicological Reports PDF, 2 pages View Download
44 Statement of Party Representatives to NTSB Investigation PDF, 4 pages View Download
45 Release of Aircraft Wreckage, NTSB Form 6120.15 PDF, 1 page View Download

The same docket at the NTSB · documents without a copy here are fetched from the NTSB when you open them.

Connections how this case links to the rest of the register

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The whole map of how records connect · these connections as data: /graph/accident/WPR13FA244.json.

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Everything on this page comes from the NTSB's public records. The narrative, probable cause and findings are the NTSB's own words; the coded tables behind the report are written out in plain English, with pilots' ages, home towns and medical details left out. The documents and photographs are the NTSB's docket, shown as the NTSB released them. This site's own text does not name anyone involved, its policy at this time. A preliminary report can change; the final report usually follows one to two years later, and the page is refreshed when it does.