- Joined
- Oct 30, 2003
- Messages
- 18,445
- Location
- Santa Maria, California
- Aircraft
- Givens Predator
- Total Flight Time
- 2600+ in rotorcraft
I fly a narrow line between allowing the client to experience the consequences of their mistakes and preserving the aircraft in flying condition.
I am often surprised by the creative ways the aircraft is put in harm’s way.
Mishaps tend to be a chain of mistakes and the trick is to break the chain before becoming an accident report. I will call the primary student Bob to protect his anonymity.
I started Bob in the back seat because there is less to manage. After some successful flight experience (around eight hours of dual and many takeoffs and landings) I moved Bob to the front where he has to manage the magnetos for the magneto check, the rotor brake, the toe brakes for steering and the radio. I cannot see the engine instruments from the back. I have the basic flight instruments of altitude and indicated air speed in the back. There is a lot to see and often the client’s vision is already narrowed by learning to fly.
We had just filled up with fuel and are both well over two hundred ponds so we were flying near maximum takeoff weight (first link in the accident chain).
Bob had floated long on the landing so we were quite a ways down the 8,000 foot runway when Bob began his takeoff roll (second link).
Bob was slow to get to full throttle once the rotor began to accelerate using up more runway (third link).
Bob let the nose come up too far and lifted off early (about 25kts) well below the minimum power required speed so we weren’t going to climb very fast until he lowered the nose and built up some airspeed (forth link).
We flew over the end of the runway at about 50 feet above the ground and did not seem to be climbing despite being only slightly below minimum power required speed (46kts) (fifth link) and I took control in an attempt to break the chain.
I carefully lowered the nose for best rate of climb trying to break the accident chain and she still wasn’t climbing.
I asked Bob what the engine rpm was and it was 2,290. Anything below 2,300 rpm and the engine is not running correctly and the takeoff is supposed to be aborted (sixth link). Bob had not noticed the low engine RPM.
I was trying to diagnose the engine problem without engine instruments so I asked Bob if the fuel pressure light was on and what the various instruments read.
I felt we could lose all power at any moment so I continued to scan for landing spots. There was a nice dirt patch straight ahead that is crisscrossed with fences. As I turned left we were over some mature crops so it would be an interesting landing. There were a few dirt roads but they were littered with people and vehicles. There were several fences and lots of irrigation ditches.
I called the tower to let them know I had engines problems and would be returning and asked for runway two. They were in the process of launching an Aironca on runway three zero so I felt returning to runway three zero was not a viable option. The tower (ATC) was quick to respond runway two clear to land and canceled the Aironca’s takeoff clearance. There is a stand of eucalyptus trees that I needed to go around making very gentle turns. The landing was uneventful.
I had to remind Bob that he had the brakes and we did not cross runway three zero till I was sure the takeoff cancelation for the Aironca was successful.
Back at the hangar Bob worked his way down the shutdown list; rotor brake on below 100 rotor rpm, lights off, transponder off, radio off, intercom off, alternator off, lean cut off, mag switches on. Even with the intercom off; I could hear Bob’s expression of surprise and dismay as he discovered only one of the magneto switches was in the off (run) position.
We still haven’t figured out how Bob hit the switch or why he didn’t see the red light on the tachometer when a magneto is not working right. The magneto switches are well out of the way and off in the forward position so any bumping is likely to turn them off (run position).
I went for a solo maintenance flight and saw over 2,400 rpm on takeoff and saw just over 900 feet per minute of climb so I felt we had found the problem. I saw 2,650 rpm on down wind at around 90kts (103 mph) indicated air speed.
I checked the ATIS and winds were variable at 4kts. As we taxied down to the run up area on Alpha the new ATIS came out with winds 270 at 11kts gusting to 18kts. We both felt this was over Bob’s wind limit with his current level of experience so we headed back to the hangar and packed it up for the day.
Each of the links is not dangerous on its own but when linked together they may form an accident chan. With the help of ATC and some luck we were able to break the accident chain.
I am often surprised by the creative ways the aircraft is put in harm’s way.
Mishaps tend to be a chain of mistakes and the trick is to break the chain before becoming an accident report. I will call the primary student Bob to protect his anonymity.
I started Bob in the back seat because there is less to manage. After some successful flight experience (around eight hours of dual and many takeoffs and landings) I moved Bob to the front where he has to manage the magnetos for the magneto check, the rotor brake, the toe brakes for steering and the radio. I cannot see the engine instruments from the back. I have the basic flight instruments of altitude and indicated air speed in the back. There is a lot to see and often the client’s vision is already narrowed by learning to fly.
We had just filled up with fuel and are both well over two hundred ponds so we were flying near maximum takeoff weight (first link in the accident chain).
Bob had floated long on the landing so we were quite a ways down the 8,000 foot runway when Bob began his takeoff roll (second link).
Bob was slow to get to full throttle once the rotor began to accelerate using up more runway (third link).
Bob let the nose come up too far and lifted off early (about 25kts) well below the minimum power required speed so we weren’t going to climb very fast until he lowered the nose and built up some airspeed (forth link).
We flew over the end of the runway at about 50 feet above the ground and did not seem to be climbing despite being only slightly below minimum power required speed (46kts) (fifth link) and I took control in an attempt to break the chain.
I carefully lowered the nose for best rate of climb trying to break the accident chain and she still wasn’t climbing.
I asked Bob what the engine rpm was and it was 2,290. Anything below 2,300 rpm and the engine is not running correctly and the takeoff is supposed to be aborted (sixth link). Bob had not noticed the low engine RPM.
I was trying to diagnose the engine problem without engine instruments so I asked Bob if the fuel pressure light was on and what the various instruments read.
I felt we could lose all power at any moment so I continued to scan for landing spots. There was a nice dirt patch straight ahead that is crisscrossed with fences. As I turned left we were over some mature crops so it would be an interesting landing. There were a few dirt roads but they were littered with people and vehicles. There were several fences and lots of irrigation ditches.
I called the tower to let them know I had engines problems and would be returning and asked for runway two. They were in the process of launching an Aironca on runway three zero so I felt returning to runway three zero was not a viable option. The tower (ATC) was quick to respond runway two clear to land and canceled the Aironca’s takeoff clearance. There is a stand of eucalyptus trees that I needed to go around making very gentle turns. The landing was uneventful.
I had to remind Bob that he had the brakes and we did not cross runway three zero till I was sure the takeoff cancelation for the Aironca was successful.
Back at the hangar Bob worked his way down the shutdown list; rotor brake on below 100 rotor rpm, lights off, transponder off, radio off, intercom off, alternator off, lean cut off, mag switches on. Even with the intercom off; I could hear Bob’s expression of surprise and dismay as he discovered only one of the magneto switches was in the off (run) position.
We still haven’t figured out how Bob hit the switch or why he didn’t see the red light on the tachometer when a magneto is not working right. The magneto switches are well out of the way and off in the forward position so any bumping is likely to turn them off (run position).
I went for a solo maintenance flight and saw over 2,400 rpm on takeoff and saw just over 900 feet per minute of climb so I felt we had found the problem. I saw 2,650 rpm on down wind at around 90kts (103 mph) indicated air speed.
I checked the ATIS and winds were variable at 4kts. As we taxied down to the run up area on Alpha the new ATIS came out with winds 270 at 11kts gusting to 18kts. We both felt this was over Bob’s wind limit with his current level of experience so we headed back to the hangar and packed it up for the day.
Each of the links is not dangerous on its own but when linked together they may form an accident chan. With the help of ATC and some luck we were able to break the accident chain.