Cirrus Design CORP SR22 and Robinson Helicopter Company R44 II mid-air collision near Frederick, Maryland, October 23, 2014
On October 23, 2014 at about 7:37 pm local time, 2 aircraft, Cirrus Design CORP SR22 (N122ES) and Robinson Helicopter Company R44 II (N7518Q), were involved in a mid-air collision near Frederick, Maryland (Frederick Municipal airport). 3 people were killed and 1 person had minor injuries; 1 other was unhurt. The weather was visual conditions (good weather).
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The NTSB's probable cause their words, unchanged
The failure of the helicopter pilots and the airplane pilot to maintain an adequate visual lookout for known traffic in the traffic pattern, which resulted in a midair collision. Contributing to the accident were the airplane pilot's descent below the published airplane traffic pattern altitude (TPA) and the helicopter pilot's climb above the proper helicopter TPA as prescribed in the Federal Aviation Administration's Aeronautical Information Manual for airports without published helicopter TPAs. Also contributing to the accident were the lack of a published helicopter TPA, the absence of radar equipment in the tower, and the controller's inadequate task prioritization.
The failure of the helicopter pilots and the airplane pilot to maintain an adequate visual lookout for known traffic in the traffic pattern, which resulted in a midair collision. Contributing to the accident were the airplane pilot's descent below the published airplane traffic pattern altitude (TPA) and the helicopter pilot's climb above the proper helicopter TPA as prescribed in the Federal Aviation Administration's Aeronautical Information Manual for airports without published helicopter TPAs. Also contributing to the accident were the lack of a published helicopter TPA, the absence of radar equipment in the tower, and the controller's inadequate task prioritization.
Source: NTSB aviation accident database, copy made October 4, 2026. Docket and reports at the NTSB.
What the record shows
- Date
- October 23, 2014 · about 7:37 pm local time
- Place
- Frederick, Maryland · Frederick Municipal · map
- Type
- Accident · mid-air collision
- Injuries
- 3 people were killed and 1 person had minor injuries; 1 other was unhurt.
- Weather
- visual conditions (good weather)
- Aircraft 1
- Cirrus Design CORP SR22 NO SERIES, built 2006
- Registration
- N122ES · registry record · serial 2008
- Damage
- Substantial damage
- Flight
- Personal flight · general aviation rules (Part 91)
- Aircraft 2
- Robinson Helicopter Company R44 II II, built 2004
- Registration
- N7518Q · registry record · serial 10281
- Damage
- Destroyed
- Flight
- Instructional flight · general aviation rules (Part 91)
The NTSB's narrative for the Cirrus Design CORP SR22 final · quoted from the NTSB record
The private airplane pilot was conducting a personal cross-country flight, and the commercial helicopter pilot and flight instructor were conducting a local instructional flight. A review of radar and voice communications revealed that the accident airplane pilot first contacted the nonradar-equipped tower when the airplane was 10 miles from the airport and that the local controller (LC) then acknowledged the pilot's transmission and instructed him to contact the tower when he was 3 miles from the airport. At this time, the LC was also handling two helicopters in the traffic pattern, one airplane conducting practice instrument approaches to a runway that intersected the runway assigned to the accident airplane, another airplane inbound from the southeast, and a business jet with its instrument flight rules (IFR) clearance on request. About 1 minute after the accident airplane pilot first contacted the LC, the LC began handling the accident helicopter and cleared it for takeoff. One minute later, the controller issued the business jet pilot an IFR clearance. When the accident airplane was 3 miles from the airport, the pilot reported the airplane's position to the controller, but the controller missed the call because she was preoccupied with the clearance read-back from the business jet pilot. About 1 minute later, the controller instructed the accident airplane pilot to enter the left downwind leg of the traffic pattern on a 45-degree angle and issued a landing clearance. She advised that there were three helicopters "below" the airplane in the traffic pattern, and the pilot replied that he had two of the helicopters in sight. Data downloaded from the airplane and witnesses on the ground and in the air indicated that, as the airplane entered the downwind leg of the traffic pattern, it flew through the accident helicopter's rotor system at the approximate point where the helicopter would have turned left from the crosswind to the downwind leg. Because of a specific advisory transmitted on the tower radio frequency advising of traffic on the downwind, the pilot of each accident aircraft was or should have been aware of the other. A witness in the helicopter directly behind the accident helicopter had a similar field of view as the accident helicopter, and he reported that he acquired both accident aircraft in his scan before the collision. Given this statement and that the accident helicopter had two commercial pilots in the cockpit, the pilots should have had the situational awareness to understand the conflict potential based on the airplane's position reports. Although the airplane was equipped with a traffic advisory system, its capabilities could have been limited by antenna/airframe obstruction or an inhibition of the audio alert by the airplane's flap position. The airplane's data indicated that the collision occurred at an altitude of about 1,100 ft mean sea level (msl). The published traffic pattern altitude (TPA) for light airplanes was 1,300 ft msl. Although several different helicopter TPAs were depicted in locally produced pamphlets and posters and reportedly discussed at various airport meetings, there was no published TPA for helicopters in the airport/facility directory or in the tower's standard operating procedures. According to the Federal Aviation Administration's Aeronautical Information Manual, in the absence of a published TPA, the TPA for helicopters was 500 ft above ground level; therefore, the appropriate TPA for helicopters at the accident airport was about 800 ft msl. The lack of an official helicopter TPA, which was published after the accident, significantly reduced the potential for positive traffic conflict resolution. Review of the airport procedures, tower capabilities, and the controller's actions revealed no specific departure from proper procedures. Because the tower was not equipped with radar equipment, all of the sequencing and obtaining of traffic information had to be done visually. This would have been especially difficult at the accident airport due to the local terrain and tree lines that extend above the pattern altitudes from the tower controllers' view, which can cause aircraft to easily blend in with the background. Further, the controller spent a lengthy amount of time on the task of issuing the IFR clearance to the business jet while handling multiple aircraft in the traffic pattern. It is likely that the lack of radar equipment in the tower and the controller's inadequate task management also significantly reduced the potential for positive traffic conflict resolution.
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 NTSB's narrative for the Robinson Helicopter Company R44 II final · quoted from the NTSB record
The private airplane pilot was conducting a personal cross-country flight, and the commercial helicopter pilot and flight instructor were conducting a local instructional flight. A review of radar and voice communications revealed that the accident airplane pilot first contacted the nonradar-equipped tower when the airplane was 10 miles from the airport and that the local controller (LC) then acknowledged the pilot's transmission and instructed him to contact the tower when he was 3 miles from the airport. At this time, the LC was also handling two helicopters in the traffic pattern, one airplane conducting practice instrument approaches to a runway that intersected the runway assigned to the accident airplane, another airplane inbound from the southeast, and a business jet with its instrument flight rules (IFR) clearance on request. About 1 minute after the accident airplane pilot first contacted the LC, the LC began handling the accident helicopter and cleared it for takeoff. One minute later, the controller issued the business jet pilot an IFR clearance. When the accident airplane was 3 miles from the airport, the pilot reported the airplane's position to the controller, but the controller missed the call because she was preoccupied with the clearance read-back from the business jet pilot. About 1 minute later, the controller instructed the accident airplane pilot to enter the left downwind leg of the traffic pattern on a 45-degree angle and issued a landing clearance. She advised that there were three helicopters "below" the airplane in the traffic pattern, and the pilot replied that he had two of the helicopters in sight. Data downloaded from the airplane and witnesses on the ground and in the air indicated that, as the airplane entered the downwind leg of the traffic pattern, it flew through the accident helicopter's rotor system at the approximate point where the helicopter would have turned left from the crosswind to the downwind leg. Because of a specific advisory transmitted on the tower radio frequency advising of traffic on the downwind, the pilot of each accident aircraft was or should have been aware of the other. A witness in the helicopter directly behind the accident helicopter had a similar field of view as the accident helicopter, and he reported that he acquired both accident aircraft in his scan before the collision. Given this statement and that the accident helicopter had two commercial pilots in the cockpit, the pilots should have had the situational awareness to understand the conflict potential based on the airplane's position reports. Although the airplane was equipped with a traffic advisory system, its capabilities could have been limited by antenna/airframe obstruction or an inhibition of the audio alert by the airplane's flap position. The airplane's data indicated that the collision occurred at an altitude of about 1,100 ft mean sea level (msl). The published traffic pattern altitude (TPA) for light airplanes was 1,300 ft msl. Although several different helicopter TPAs were depicted in locally produced pamphlets and posters and reportedly discussed at various airport meetings, there was no published TPA for helicopters in the airport/facility directory or in the tower's standard operating procedures. According to the Federal Aviation Administration's Aeronautical Information Manual, in the absence of a published TPA, the TPA for helicopters was 500 ft above ground level; therefore, the appropriate TPA for helicopters at the accident airport was about 800 ft msl. The lack of an official helicopter TPA, which was published after the accident, significantly reduced the potential for positive traffic conflict resolution. Review of the airport procedures, tower capabilities, and the controller's actions revealed no specific departure from proper procedures. Because the tower was not equipped with radar equipment, all of the sequencing and obtaining of traffic information had to be done visually. This would have been especially difficult at the accident airport due to the local terrain and tree lines that extend above the pattern altitudes from the tower controllers' view, which can cause aircraft to easily blend in with the background. Further, the controller spent a lengthy amount of time on the task of issuing the IFR clearance to the business jet while handling multiple aircraft in the traffic pattern. It is likely that the lack of radar equipment in the tower and the controller's inadequate task management also significantly reduced the potential for positive traffic conflict resolution.
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 for the Cirrus Design CORP SR22 from the NTSB's investigation tables, in plain English
What happened, in order
- Midair collision during approach (VFR pattern base) defining event
The NTSB's findings
- factor Organizational issues › Management › Policy/procedure › Availability of policy/proc › Not specified
- factor Environmental issues › Operating environment › Radar services/coverage › Approach/departure › Availability of related info
- factor Personnel issues › Task performance › Workload management › Task allocation › ATC personnel
- factor Personnel issues › Action/decision › Action › Incorrect action performance › Pilot of other aircraft
- factor Personnel issues › Action/decision › Action › Incorrect action performance › Pilot
- cause Personnel issues › Psychological › Attention/monitoring › Monitoring other aircraft › Pilot
- cause Personnel issues › Psychological › Attention/monitoring › Monitoring other aircraft › Pilot of other aircraft
Pilot
- Certificate: private
- Ratings: single-engine land; instrument: airplane
- Flight time: 959 hours in all; 804 in this make and model; 38 in the last 90 days; 23 in the last 30 days; 720 as pilot in command
- Last flight review: October 24, 2013
- Medical certificate: Class 3 (with waivers/limitations)
- Seat: left
- Injury: no injuries
The aircraft
- Airframe total time: 1,320 hours
- Last inspection: annual inspection, June 13, 2014; 30 hours since
- Maximum gross weight: 3,400 lb
- Seats: 4
- Landing gear: fixed
- Engine: Cont Motor IO-550-N (piston); 1,320 hours total
- Operator: Graeves Auto & Appliance INC
The flight
- Departed from: RZR Cleveland TN at 4:47 pm
- Destination: FDK Frederick MD
- Flight plan: IFR
- Runway 30, 3,600 ft by 75 ft
Weather at the time
- Light: daylight
- Wind: from 330° at 16 knots, gusting 21
- Visibility: 10 statute miles
- Sky: scat at 4,800 ft
- Temperature: 66°F (19°C), dew point 45°F (7°C)
- Altimeter: 29.90 inHg
- Observation at 7:53 pm from KFDK
Injuries
| Fatal | Serious | Minor | None | |
|---|---|---|---|---|
| Flight crew | 1 | |||
| Passengers | 1 |
The factual record for the Robinson Helicopter Company R44 II from the NTSB's investigation tables, in plain English
What happened, in order
- Midair collision during approach (VFR pattern downwind) defining event
The NTSB's findings
- factor Personnel issues › Action/decision › Action › Incorrect action performance › Pilot
- factor Organizational issues › Management › Policy/procedure › Availability of policy/proc › Not specified
- factor Environmental issues › Operating environment › Radar services/coverage › Approach/departure › Availability of related info
- factor Personnel issues › Action/decision › Action › Incorrect action performance › Pilot of other aircraft
- factor Personnel issues › Task performance › Workload management › Task allocation › ATC personnel
- cause Personnel issues › Psychological › Attention/monitoring › Monitoring other aircraft › Flight crew
- cause Personnel issues › Psychological › Attention/monitoring › Monitoring other aircraft › Pilot of other aircraft
Flight instructor
- Certificate: flight instructor, commercial pilot
- Ratings: instructor: helicopter; instrument: helicopter; rotorcraft: helicopter
- Flight time: 832 hours in all; 116 in this make and model; 57 in the last 30 days; 779 as pilot in command; 527 on instruments
- Medical certificate: Class 2 (without waivers/limitations)
- Seat: left
- Injury: fatal
Pilot
- Certificate: flight instructor, commercial pilot
- Ratings: instructor: airplane multi-engine; instructor: airplane single-engine; instructor: helicopter; instrument: helicopter; rotorcraft: helicopter
- Flight time: 2,850 hours in all; 7.3 in the last 30 days
- Medical certificate: Class 2 (without waivers/limitations)
- Seat: rgt
- Injury: fatal
The aircraft
- Airframe total time: 1,758 hours
- Last inspection: 100-hour inspection, October 2, 2014; 20 hours since
- Seats: 4
- Landing gear: fixed
- Engine: Lycoming IO-540 SER (piston); 1,758 hours total
- Operator: Advanced Helicopter Concepts, Inc
The flight
- Departed from: FDK Frederick MD at 7:35 pm
- Destination: FDK Frederick MD
- Flight plan: none
- Runway 30, 3,600 ft by 75 ft
- A second pilot was aboard
Injuries
| Fatal | Serious | Minor | None | |
|---|---|---|---|---|
| Flight crew | 2 | |||
| Passengers | 1 |
Documents from the investigation the NTSB's docket: the evidence folder behind the report
The docket, the folder of records gathered during an investigation (maintenance records, photographs, witness statements, examinations), has not been read from the NTSB for this case yet; the list appears here once it has. Open the docket at the NTSB.
About this page
Everything above comes from the NTSB's public accident database: the narrative, probable cause and findings are the NTSB's own words, and the coded tables behind its report (pilot, aircraft, flight, weather, injuries, sequence of events) are written out in plain English. Pilots' ages, home towns and medical details are left out on purpose. The documents and photographs are the NTSB's docket, the folder of records gathered during the investigation, shown as the NTSB released them (the NTSB redacts some personal details first) and listed under the NTSB's own titles. This site's own text never names pilots, passengers or anyone else involved. A preliminary report describes what is known soon after the event and can change; the final report, with the probable cause, usually follows one to two years later and this page is refreshed when it does. Case number ERA15FA025.
