Open Orbit

Blunders and Accidents

[ aviation , caproni ]

[ en, sv ]

Nils was an airman that started in the Swedish Air Force as a conscript. During his career in the Air Force and later ABA / SAS he experienced several incidents, many in which his life was in jeopardy.

Datum Ändring

2022-10-27

First release of text

2023-10-14

Corrected errors after original text was discovered

2023-10-14

Added unpublished section: Effect Loss During Takeoff

2023-10-14

Added unpublished section: Eagle Hunt with Airplane

Translated by Mattias Holm.

Foreword by Mattias

This article was first published in Svensk Flyghistorisk Tidskrift 4/12. It is re-published here with a non-commercial clause.

The article is a number of short stories about different incidents during Nils' flying career. The article has been edited by Mattias Holm, adding links, and images to provide more context.

The translation was done by Mattias as well, and it should be stated that several terms are very hard to translate. Someone with better insight in aviation terms could help out here (e.g. by filing an issue report at GitHub or by contacting Mattias at Mastodon).

As an example of terms that I find uncertain, include:

Flöjla motorn

Feathering the propeller pitch

Upptagning

Flair (the pitch-up of an aircraft before landing)

Kupera motor

Turning off the engine

Flygplansmästare

Aircraft master

Magra motorn

Thinning the engine

Gå ut

Abort

Vikning

Wing drop

I have added distances, speed and elevation in some cases. Distance, speed and elevation added by me are given in nautical miles, knots and feet respectively (since this is what is used in international aviation). However, the original story had some elevations in meters and speeds in km/h, in those cases I have kept the original and added the converted amount in parenthesis.

One of the stories refers to a US lieutenant, Franklin D. Talcott. The story was told on occasion by Nils, and I remember him saying that Lt. Talcott was overconfident and killed in the crash (this not directly mentioned in the story) that was caused by reckless flying.

Research notes about Talcott are available here.

Talcott flew a P51 Mustang during a raid in Poland and was forced into an emergency landing in Sweden. That Mustang was repaired and flew up to F 8 Barkaby by a US Embassy flight officer. The aircraft was formally purchased by Sweden in 1945 and served in the air force until it was sold to the Dominican Republic in 1952. The fatal accident was with another Mustang that was supposed to be ferried up towards F 8 Barkaby. It seems that Talcott is the same person mentioned here and here.

Note
As far as I have been able to determine, all named individuals here are dead. Several for over 70 years. Hence the GDPR should normally not apply.

Blunders and Accidents

During my 40 years as a pilot there has naturally been several things that I am ashamed for. Here follows an account for some of them, without consideration for the chronological order.

With the Throttle in the Hand

On May 7, 1943, I was heading out on a reconnaissance mission in a fully fueled Caproni, three weeks after my first solo flight. As I after takeoff reduced the throttle to climb, the throttle fell off in my hand. Considering the high start weight and my lack of routine, I did not dare to feather the propeller pitch, that was running at 2000 RPM. I came in for landing, but was way to high and hand to go around. The next attempt had to be aborted during flaring as a truck was passing the runway (this was before the introduction of telephony). Despite full rudder and banking, I was unable to keep the course due to being near minimum control speed and the right engine’s power, and I got a significant course deviation to the left. The mechanic was quick with retracting the landing gear and after a while we got enough speed to climb to traffic speed height.

Ca.313
Figure 1. Caproni Ca.313. Probably 1944, Flygvapenmuseum / FVM.149864 / https://digitaltmuseum.se/021025518001/tavla / CC-BY 4.0.

The next landing went fine. The speed I regulated by in similarly to Tummelisa temporarily cutting the left engine.

I was called in for interrogation and the lieutenant was very critical of my escapades, until I showed him the throttle. It consisted of a chromed brass tube. The mounting was very simple. Only a drilled hole through the tube and then attached using a split cotter pin.

To my great surprise, the lieutenant changed his criticism to praise.

Double Engine Failure on Caproni

We had been doing winter exercises at F 21 in Luleå and was flying home to F 11. We were given aircraft number 21 and had an estimated flying time of three hours. As usually the aircraft was fully loaded for this type of flying. We had to get as much of the field equipment along, including oil drums and engine covers. The crew consisted of the undersigned, spotter Wibom, radio operator Eriksson and aircraft master Helmer Larsson.

The takeoff and climb went normal to around 600 m (ca 2000 feet). Helmer Larsson came to the front and looked out towards the left engine. Suddenly, both motors stopped. We started sinking quickly and I picked a lake to make an emergency landing on. I quickly checked the fuel cock, the instruments and finally found the main magnet switch to be in the OFF position (the both individual magnet switches was in position "BOTH"). We had fallen down to around 200 m (around 650 feet) and started to deploy the flaps for landing when Helmer thought we should do a start attempt. A couple of years later when we met at his workplace "Teknis" he claimed that I said:

 — No, now we are landing, you should not change your mind at this late stage. It can end in a catastrophe.

According to Helmer my voice was supposed to have been absolutely calm and serious, which I doubt.

In any case we did a start attempt by putting the throttle to idle, turn on the magnets switch, and behold both engines started up. They were still warm and the speed wind was enough to keep the propellers spinning with a good RPM.

The cause for the flameout was that Helmer had when he turned his head, bumped into the magnet switch in the ceiling with his winter hat. As the lowest, we estimated our altitude to 70-80 m (230 - 260 feet).

We continued the flying to F 11 without any comments, I could not notice any special reaction or nervosity with anyone onboard. We did not even think it was worth to report.

Thoroughly Scolded

The problem of failed airspeed indicators was common on the S 16 Caproni. The cause was that the pitot tube heaters burned off and therefore subsequent icing. Not until we stopped having the heating on already from taxiing it got better. The cause was of course the lack of cooling at the low speed. The heat was turned on after takeoff and the problem went away almost completely.

I suffered the problem at least three times. One time the airspeed indicator stopped at 220 km/h. For an experienced flyer, this was no bigger problem. The last time it happened to me, I landed as usual at the given runway which happened to be F 11 runway 26.

After a day or so I got called into colonel Schyberg. Unaware of this honor I was very surprised to get a real scolding for my bad judgement with landing over the administrative building with a broken airspeed indicator and therefore risking both human life and buildings.

On the question about whether I understood the risks I answered that it was not a problem because you could determine the speed by the wind sound and the stick pressure. Easy-peasy. The colonel turned red in his face and shouted:

 — Out!!!

It should be noted that the colonel, despite many attempts, never got approved for solo flying. It was not just him that had a problem with the landings, one just had to remember that it wasn’t an Sk 14.

So easy it can be to to mindlessly step on someone’s toes. I was ashamed.

Two Landing Failures in One Hour

Note
This was initially suspected to be the crash that is documented here [1]. However, after having read the official crash investigation, it can be concluded that [1] refers to a different event.

During my time as flight instructor at the aspirant school in Ljungbyhed, I had an aspirant that had serious problems with completing the exercise "landing during wing gliding". The exercise was about managing to handle an emergency landing after a too high approach, especially with aircraft that did not have flaps. In this case an Sk 15 (Klemm).

Sk 15
Figure 2. Klemm 35 / Sk 15. 1 August 1976, CC-BY 3.0.

For the modern pilot it may be in place to explain how it went:

When you came in to high or to far, the air resistance should increase in order to increase the sink rate. So one could bank the plane and apply the opposite rudder to maintain a straight course. It was actually not a nice feeling as the noise increased and the wind was blowing the pilot in the face in the open cockpit, but the effect on the sink rate was impressive. If the landing space was very limited one kept on with the wing gliding even during the landing flare to just before the 3-point landing set the plane straight.

My aspirant was afraid of the last moment and could not be made to stay in the wing gliding when we approached the ground. It was thus a normal landing and the purpose of the exercise to shorten the landing length was not achieved.

After consultation with the head flight instructor, it was decided that I, because the pupil was promising, would get an extra session. To work without being disturbed by other planes, we got to practice at Kvidinge airfield.

The exercises did not go well. The pupil was too tense and kept on aborting the wing gliding way to early. Suddenly he said:

 — This time I will make it.

It looked to go well with a strong banking, but when I felt that the speed was running out I said:

 — Abort!

But nothing happened so I felt compelled intervene - but too late. He held the rudder in a stern grip that I in the speed was not able to countermand. The result was a landing with a low left wing and a large drift. In protest against the not so mild treatment, the left gear folded it self substantially, and prevented further practice.

A walk to a farm and a telephone call to with the traffic controller resulted in that two airplanes came with help and a few technicians. The technicians stayed while a lieutenant in one plane; and I and the aspirant in the other started in a closed formation towards F 5 and the looming lunch.

The landing was also done in closed formation - I was to the left of the lieutenant who apparently forgot I was at his wing tip. He suddenly braked hard and turned left to the neutral zone. The well known 1 second reaction time was not enough. We collided, with smaller damages on both of the aircrafts' wing tips as result.

During the afternoon session the first flight instructor A approached me and voiced his dissatisfaction with my recklessness, and explained that the result for my part meant military detention. When I expressed my doubt that it was only my fault, because we landed in closed formation, the instructor asked if that was really true. After my affirmative answer, he removed himself without a word.

I avoided detention but so did the lieutenant. It was a difference between how one judged sergeants and a lieutenants at that time.

Wrecked Wing Tip

The flight instructor course (FIC) 1944 was finished with with an advanced flying competition; including both a mandatory and a freely composed programme, navigation flying under time, and finished with precision landing using an Sk 14. It was during the last part I messed up.

Sk 14
Figure 3. North American NA-16 / Sk 14. Public Domain.

The grading was done by having specified a simulated ditch. Every meter beyond it resulted in minus points. Landing before the ditch was equivalent with a crash and disqualification.

I had found out that you could have a few extra km/h in excess speed during the flare; by yanking on the stick the aircraft would touch down nicely due to the increased wing load.

Absolutely sure to land only a few meters plus, I looked right at the mark and the official, and when it was time I yanked the stick. The result was plus 5 m, but as a bonus I got a smaller damage on the wing tip. Guess if I was surprised. The whole thing went so quick that I didn’t get that it actually was a regular wing drop. The cause must have been that when I looked straight down, I had unconsciously turned the plane a little bit and caused a stall on the right wing.

I got a thorough scolding which was the custom at that time. I had earned it - but I did not have to pay for the wing tip.

Elevator Mass Balance in the Bed

This happened on Saturday, October 7, 1944. I was tired after an orienteering run and lunch and was laying on the bed, resting in the Åsen barack next to the sports field at F 5, Ljungbyhed.

The American Lieutenant Talcott was test flying a Mustang before transfer to F 8 (see Svensk Flyghistorisk Tidskrift 1/05). When I heard the fabulous engine roar I got out of bed and went to the window to see what was going on. The good Talcott had apparently not gotten over the tree tops and damaged the machine badly in the tree crowns. In an involuntary roll he passed by upside down, at approximately 10 m (30 feet) hight and about 20 m (60 feet) in front of my window. I can still see the expression of his face from the effort with trying to rectify the situation.

With a loud bang and a shaking floor, I turned around and found a big hole in the wall and on the bed, that I luckily left a few minutes earlier, was the Mustang's heavy elevator mass balance. If I had not been so curious this article would never have been written.

Start Problems with DC-6

Takeoff from Damascus some time in the beginning of 1949 with a DC-6. Normally wi never had any problems with takeoff, which normally was during dark in the evening as it was cooler. Due to a technical issue we were delayed to around 14:00 when it was as warmest. We started towards North West in counterslope and high terrain in front of us. I was the first officer for captain Einar Tehfer that had control.

DC-6
Figure 4. SAS DC-6. Public Domain.

The acceleration was unusually slow and we soon understood it was too late to abort the takeoff, but would we take off before the end of the runway? Doubtful!

Then Einar shouted: "This will not go, but whether we are airborne or not, you retract the gear when you cannot see the end of the runway". The end of the runway disappeared under the nose and it was with great discomfort I moved the landing gear leaver to UP.

With high nose and light shaking of the plane we left the field, but we still hade the mountains in front of us. When we had reach control speed, Einar started a light left turn at around 10 m (30 feet) altitude. We climbed together with the terrain and it really did not feel good, it was a few critical minutes. In addition, we had turbulence at this altitude in the strong sunlight. The engines held, despite we considerably exceeded the time for maximum start power.

We arrived home and consulted Hans Walther who was head of the newly established performance department. He contacted the Douglas factory that handed out graphs for the correction of start weight, temperature, air pressure, wind strength, elevation over the sea etc. It turned out that it was not possible to take off from Damascus under the given environmental conditions, but we managed anyway.

The result of our takeoff was additional instructions and better education of the pilots. We should remember that this was during the infancy of aviation.

Flameout on Four Engines

During the Korean war, there was a shortage of high octane aviation fuel. To solve the problem, they added, if I recall correctly, a substance that we called TCP. DC-7C was especially sensitive with its high compression. They had taken out as much effect as possible in the aircraft. The gas pressure at start was not 62 inches but 62.5!

DC-7C
Figure 5. SAS DC-7C. Public Domain.

The TCP had the disadvantage that you got a coating on the spark plugs. This often resulted in large delays due to spark plug changes. 36 plugs in every engine!

Normally we "thinned" the engine when we got up to cruising altitude. However, an instruction was issued that we should wait 5 minutes before doing the "thinning", so that the engine temperature had stabilized.

We started from Beirut towards Rome. The cruising altitude we reached over Cyprus where whe entered strong CB clouds. We served from Rome via Damascus to Teheran and back through Beirut to Rome.

Rome Teheran Map
Figure 6. Rome-Damascus-Teheran-Beirut-Rome Round Trip. Distance is around 3950 NM (7320 km).

The distance was too long for normal work so the crew was reenforced with a captain, telegraph operator and a mechanic. We had three beds at our disposal. This leg it was my turn to sleep and i quickly laid down after takeoff and fell asleep immediately, but was woken by the aircraft going dead quiet, with the exception of the patter of the hail. Out of the bed and to the guys in the cockpit that were a bit chocked. All four engines had flamed out. I understood that there was icing in the carburetors so i forced my self over the mechanic and turned down the throttle, and turned the pre-heater knobs all the way up, and it did not take many seconds before the engines were spinning again. I stayed and checked that the engines were running fine after the "thinning" with 8 BMEP.

After 5 minutes I was sleeping well in my bed again.

The cause for the icing was that the carburetors was cooled down by excess fuel that caused the moisture in the air to turn to ice. During 14 days, another three flameouts happened at the same place and we pilots decided internally to "thin the engines" as soon as we reached cruising altitude and the problem was away.

Violent Flight Training

We had flight training at Bromma. It was the PFT (Pilots Flight Training) a torturous exercise that was carried out 2 times per year. This was probably 1949. The instructor was the gruff captain Carls, pupils Steinmark and the undersigned.

Steinmark was first to be grilled. Everything went fine until we were supposed to land without number one engine (left outer engine) at runway 13. Just as we were about to touch down Carls yelled: "Obstacles on the runway. Throttle up!"

Tehier shoveled gas on the remaining engines, but could naturally not get the speed up with full flaps. In addition the plane started turning left, despite full right rudder and corresponding bank.

"I need to get number one on or we are doomed" Steinmark shouted. "No it should go" Carls responded. But it didn’t and after a couple of excruciatingly long seconds Carls surrendered and number one spun up.

To my horror I found that we with barely control speed were heading to the right part of the air traffic control tower. We were a bit to low to make it, but both pilots instinctively applied full ailerons to the right, and the wing passed with the minimum possible margin over the tower.

I who was behind the pilots saw how the air traffic controllers disappeared. After landing they confirmed that they had thrown themselves at the floor.

Well, we wiped the sweat of our foreheads, retracted the flaps and continued the flight training. Steinmark got to do the three engine approach again because he hadn’t completed the landing and after instrument flying with two engines and subsequent landing it was my turn. We had nerves of steel at that time!

The problem was that we were below minimum control speed. As with the start in Damascus, Hans Walter took on the problem, and after input from the factory we got to take a new course about performance.

On the Way Without Parachute

The Caproni was grounded and was being modified. As a replacement we at F 11 got to borrow B 3 from F 1. There was a lack of flight instructors so it was decided that we normal pilots would train instrument flying with each other.

B 3
Figure 7. Junkers Ju 86K / B 3. Public Domain.

The cadets Borg, Gustavsson and I was on December 11 1942 supposed to grill each other in B 3 number 8.

I was first under the hood with Borg as safety flyer on the right side. Because the visibility towards the left was practically zero, it was decided that the third pilot would sit in the rear gunner’s seat and watch for any planes in the dead sector.

When I was done with my training, Borg entered under the hood with Gustavsson as safety flyer. I crawled back towards the rear turret. Just as I stepped over the radio nest I took the cable and attached my headset. I took my place and was about to put on the front mounted parachute. Then I heard Gustavsson shout:

"No, you are climbing! This is what you should do." at the same time that he pushed the stick forward significantly.

The result was that I flew up like a cork, to come back to my starting position when the pilot pulled the stick back. But then the speed wind had folded me backwards, resulting in my upper body laying outside the fuselage. Luckily I had the throat microphone and I yelled loudly for help while holding myself with hands and feet braced against the edge.

The radio operator Stig Carlsson noticed my situation and came to my help, he simply pulled me forward and all of me was soon onboard again. Guess if I quickly buckled up or not after this.

Except for the edge causing a skinned back, I escaped the adventure with the sheer horror.

Effect Loss During Takeoff

I took off with an Sk 14 at Ljungbyhed. When i reduced the throttle from full to climb, the engine was excessively throttled down. Immediately realized that the mixture lever was in thin mixture. The cause whs that I during the throttle reduction, managed to get the flight suit’s arm strap caught in the lever. This lever was just left of the throttle. The thinning was done by pulling the lever backwards. At a couple of m height, I managed to get the arm loose from the lever that was returned to rich. So the only thing to do was to continue the exercise. Here I must commend the Swedish Air Force. Already a week after this, there were no more arm straps in the entire air force.

Eagle Hunt with Airplane

On the way to Tokyo with a Coronado, we had a stopover at Kloten Airport, Zurich. At 150 m elevation during the approach to runway 16 we catch sight of a large bird in front of us. Risk for collision! Birds can as known cause large damage, especially if they are ingested by the engines, or hit the front of the wings.

From when I saw the bird until we hit it, i was reminded about the training in San Diego where we got it demonstrated how strong the windshield were. They tested the reliability by using an air cannon, shooting deep frozen cylinder shaped ducks towards the windshield, at a speed of 160 MPH.

I decided to not duck if the bird hit the windshield. There was a head on collision on my windshield and despite my decision, I ducked when the bird passed away. The windshield held and we informed the traffic manager about the event.

When we after refueling was ready to board again an airport official approached me with a gigantic eagle that he offered me. He said with a glimmer in the eye: a perfect shot captain. Because we were on the way to Tokyo, I had to with a sorrow in my heart decline the offer. But it would surely have been great with a stuffed eagle in the recreation room.

Epilogue

It may seem that I had a lot of blunders, but considering the 40 years and almost 22000 hours flying time maybe it is not too alarming. It was over three years between the incidents and they were of course focused to the air force.