![]() |
If this is your first visit, be sure to check out the FAQ by clicking the link above. You may have to register before you can post: click the register link above to proceed. To start viewing messages, select the forum that you want to visit from the selection below. |
|
|
Thread Tools | Display Modes |
#1
|
|||
|
|||
![]()
With the current discussion in another thread regarding the accident record
of the BD-5, I thought it might be interesting to do a little more in-depth look. I decided to examine the accidents between 1 January 1990 and 13 November 2003 and do a breakdown as to relative accident/fatality rate, pilot experience, and cause of accidents. To give a little depth to the situation, I also ran the same analysis for two other single-seat homebuilts. I selected the RV-3 as an airplane with a similar "mission" as the BD-5. And I use the Fly Baby because, well, I ALREADY had the downloaded NTSB files on it. :-) DATA SOURCE: I downloaded the accident reports from the NTSB web pages for these three aircraft. In all cases, I used several variants of the names to try to avoid missing any reports. I also ran a simple search for all amateur-built accidents and amateur-built accidents with fatalities over the same period. I do not have any data indicating how many of each type of aircraft existed in each year. Therefore, I used the number of each type registered in January 2003 for the basis for some of the percentages. I used the FAA/EAA practice of only counting those airplanes which are listed as having airworthiness certificates, even though the listings are somewhat inaccurate. Thus, the following fleet-size figures are used: Fly Baby: 265 BD-5: 81 RV-3: 170 Using the January 2003 fleet size numbers is only for comparison; remember, it does not reflect the number of a given aircraft in the fleet at the time of any particular accident. When running percentages based on this fleet size, I did *not* add back the crashed airplanes into the total fleet size. This is different from my earlier, BD-5-only report, so the percentages will be slightly different. ANALYSIS METHOD: Using the NTSB reports, I extracted key features and transferred them to a database. The database included items like the type of aircraft, date of accidents, number of fatalities and injuries, the ratings held by the pilot, whether the aircraft was on its first flight, a "test flight", or whether the pilot had newly purchased the plane, and 36 separate categories for the accident cause. I would enter the NTSB primary cause as a "1" in each category, and any related events as "2"s. However, when developing the cause statistics, I ignored the primary/secondary indications and just counted whether the categorized item was a factor. I did vary from the NTSB cause determination in one kind of case: When an accident occurred after a loss of power. Often, the NTSB assigns pilot error as a cause (either primary or contributing) if the pilot in not able to safely land the aircraft after an engine failure. In my analysis, I considered only the even that *caused* the emergency; if the pilot misjudged a deadstick landing approach, I did not flag that as an accident cause. Keep in mind that the statistical base is NOT high for any of these three aircraft. We're talking 15-20 accidents over a 13-year period, here. But things are easier to compare when presented in percentages. Finally, the data presented may appear better if you switch your newsreader to a fixed-spacing font rather than variable spacing. OK, on to the results! OVERALL ACCIDENTS: Here are the total number of accidents I extracted from the NTSB online database. Again, this is the period from 1 Jan 1990 to 13 November 2003. Type Accidents fatal All Homebuilts 2881 837 Fly Baby 15 5 BD-5 22 9 RV-3 14 5 OVERALL ACCIDENT RATE: Let's look at the overall accident rate for the homebuilt fleet and the individual types. The "Accidents" is the total number of accidents vs. the number of that type on the Jan 2003 register, and the "Fatals" column is the number of accidents in which the pilot was killed. Accidents Fatals All Homebuilts 11.1% 3.2% Fly Baby 5.7% 1.9% BD-5 27.2% 11.1% RV-3 8.2% 2.9% FATAL ACCIDENTS TO TOTAL ACCIDENTS These ratios show the relative number of fatal accidents vs. the total accidents for that type. Type Fatal Rate All Homebuilts 29.1% Fly Baby 33.3% BD-5 40.9% RV-3 35.7% The number of accidents involving fatalities is one indicator of the relative crash-worthiness of a design. However, these factors do not reflect the type of accident...a structural failure at altitude is generally not survivable, no matter the design of the aircraft. PILOT QUALIFICATIONS The NTSB reports, especially the older ones, did not always list the ratings held by the accident pilot. Less than half the reports contained the pilot rating information. For the purposes of this analysis, I have presumed that the pilots whose qualifications were not listed had Private licenses. Private Comm ATP Fly Baby 80.0% 13.3% 0.0% (One unlicensed pilot) BD-5 63.6% 18.2% 18.2% RV-3 71.4% 21.4% 7.1% Again, keep in mind the small sample size here. The 7.1% for ATPs involved in RV-3 crashes represents *one* individual. AIRCRAFT TEST STATUS Occasionally, the NTSB reports indicate that the airplane was on its first flight, or was newly-purchased. Or, they may indicate that the airplane was on a "test flight." It is unknown whether other accidents actually occurred during these phases; the NTSB investigator may not have been aware of it or didn't consider that it was a significant contributor to the cause of the accident. "First flight": Aircraft specifically identified as never having flown before. "Test Phase": Aircraft identified as still in its FAA-specified test phase, or the NTSB report indicates the purpose was a test flight. "New Pilot": NTSB report says the owner had recently purchased the aircraft. First Flight Test Period New Pilot Fly Baby 0.0% 0.0% 13.3% BD-5 9.1% 22.7% 9.1% RV-3 0.0% 0.0% 21.4% For the Fly Baby, a single accident was 6.7% of the total, the BD-4 was about 4.5%, and the RV-3 was about 7.1%. ACCIDENT CAUSES As mentioned earlier, I include both the primary and any secondary causes in this list, with the exception of any pilot error occurring after a loss of power. The accident categories I use a "LOP - Non-Pilot": A loss of power that is not attributable to the pilot's actions. This could include blockage of a fuel line, magneto failure, etc. This category is also used for unexplained losses of power. "LOP - Pilot": A loss of power attributable to pilot actions...fuel exhaustion, carb ice, etc. "Pilot Judgement/ mishandling": The classic "Pilot Error" category. These factors include both cases of bad decision-making as well as those of losing control of the aircraft due to windy conditions. Keep in mind that this really isn't the only "pilot error" category..."LOP - Pilot," "Density altitude,", "Maneuvering at Low Altitude," etc. are cataloged individually and are NOT reflected here. "VFR to IFR": Basically, scud running. "Mechanical Failure - Airframe": Generally, structural failure of some sort, though not necessarily of critical structure. Includes door, canopy, panel, etc. failures. "Mechanical Failure - other": Generally failures of non-engine or fuel system accessories. Does include propeller and spinner failures. "Maneuvering Low Alt": Unnecessary low flying. Does not include cases of high-altitude flying where the terrain outclimbs the airplane. "Density Altitude": Hot/High conditions "Builder error:" Workmanship problems, deviation from instructions, etc. "Mechanical Failure - Maintenance": Failures due to mistakes while performing maintenance...leaving bolts out, etc. "Midair": Collision with another aircraft. "Inadequate Preflight": Failure to detect flawed conditions or plan the flight properly. "Inexperience": Lack of experience, either in total time or in the accident airplane. "Fire": Pre-crash fires. "Undetermined": No surviving witnesses and the wreckage is too damaged to show any potential mechanical flaws. Again, keep in mind that both primary and secondary causes are included here, so the columns won't add up to 100%. (FB is Fly Baby) FB BD-5 RV-3 LOP - Non-Pilot 20.0% 40.9% 14.3% LOP - Pilot 13.3% 0.0% 14.3% Pilot Judgment/ mishandling 13.3% 36.4% 28.6% VFR to IFR 6.7% 0.0% 7.1% Mechanical Failure - Airframe 13.3% 0.0% 21.4% Mechanical Failure - other 0.0% 0.0% 14.3% Maneuvering Low Alt 0.0% 0.0% 7.1% Density Altitude 0.0% 4.5% 0.0% Builder error 13.3% 4.5% 0.0% Mechanical Failure - Maint. 20.0% 9.1% 7.1% Midair 0.0% 0.0% 7.1% Inadequate Preflight 6.7% 0.0% 0.0% Inexperience 6.7% 18.2% 7.1% Fire 0.0% 0.0% 7.1% Undetermined 6.7% 0.0% 0.0% Percentage one accident represents: 6.7% 4.5% 7.1% The BD-5 has a loss of power accident rate twice that of the Fly Baby and almost three times of the RV-3, reflecting the design's long problems with finding a reliable powerplant. The Pilot Judgment/Mishandling categories are fairly close for the RV-3 and BD-5, but the BD-5 has trigear and the RV-3 is a taildragger. The Fly Baby, though, is half their rates, which probably reflects the BD-5/RV-3 high-performance status. The BD-5's "Inexperience" results are interesting, too. Anyway, that's what the statistics look like. Ron Wanttaja |
Thread Tools | |
Display Modes | |
|
|
![]() |
||||
Thread | Thread Starter | Forum | Replies | Last Post |
AOPA Stall/Spin Study -- Stowell's Review (8,000 words) | Rich Stowell | Aerobatics | 28 | January 2nd 09 03:26 PM |
Pitts Seat Mod | Martin Morgan | Aerobatics | 0 | November 21st 03 04:56 AM |
Seat cushion | Ernest Christley | Home Built | 14 | August 5th 03 07:16 PM |
Seat cushions | Big John | Home Built | 3 | July 31st 03 10:59 PM |
DK-1 All Metal single seat biplane | Michael | Home Built | 0 | July 28th 03 05:16 PM |