Crash of a Fletcher FU-24-950 in Dannevirke

Date & Time: Feb 25, 1997 at 0926 LT
Type of aircraft:
Registration:
ZK-DZF
Flight Phase:
Survivors:
Yes
MSN:
206
YOM:
1975
Country:
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
The topdressing operation had resumed after a break caused by weather deterioration associated with a weakening frontal system in the immediate area. Mist and low cloud had cleared, and the wind had picked up. The pilot was sowing into a narrow, rising valley. It was the sixth run over the same terrain, after an increase in payload. The pilot initially encountered lift then heavy sink. Unable to reverse course within the confines of the narrow valley, and despite the application of full power, 20 degrees of flap and an attempt to dump the payload, he failed to establish a climb. The aircraft stalled in a lefthand turn and impacted the valley side. The aircraft struck left wing first, removing the outer wing section. It then hit the ground flat but turning anti-clockwise and skidded tail first to a halt. The hopper mouth was torn loose, and this and the nose leg disrupted the cockpit floor, trapping the pilot's legs within the cockpit area and inflicting serious injuries. The pilot was wearing full restraint harness and a protective helmet, which undoubtedly saved him from further injury. He suffered some post-impact disorientation, but fortunately there was no post-crash fire. The Police and Fire Services in attendance were unaware of the actions required to secure the aircraft fuel and electrical systems.

Crash of a Fletcher FU-24-954 near Taihape: 1 killed

Date & Time: Jan 22, 1997 at 0800 LT
Type of aircraft:
Operator:
Registration:
ZK-EHX
Flight Phase:
Survivors:
No
MSN:
262
YOM:
1979
Country:
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Circumstances:
The pilot was conducting a topdressing operation in hilly terrain in fine weather. He had stopped sowing and commenced a right hand turn. Considerable height was lost in the turn for reasons undetermined. The aircraft impacted with terrain under power in a 60° banked, 30° nose down attitude. The aircraft was totally destroyed in the impact and post crash fire, the pilot receiving fatal injuries. No technical deficiencies were revealed.
Probable cause:
The exact cause of the accident could not be determined.

Crash of a Fletcher FU-24-950 in New Zealand: 1 killed

Date & Time: Aug 23, 1996 at 1522 LT
Type of aircraft:
Operator:
Registration:
ZK-EGQ
Flight Phase:
Survivors:
No
MSN:
239
YOM:
1977
Country:
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Captain / Total flying hours:
14237
Captain / Total hours on type:
14000.00
Circumstances:
The pilot, sole on board, was completing a top dressing flight in the region of Motueka. While flying at low height, the aircraft struck with its left wing a pine, lost height and crashed on the northern face of a ridge. The pilot was killed.
Probable cause:
The lone pine tree which the aircraft struck was probably obscured due to the position of the sun and shadow, making it difficult for the pilot to detect. Damage to the aileron control system resulted from the collision, and prevented the pilot from turning away from the ridge he had been sowing. Due to the impaired controllability the pilot was unable to recover from a steep left-banked turn, and the aircraft stalled and collided heavily with the face of the ridge in a nose-down attitude.
Final Report:

Crash of a Cessna 208A Caravan I in Picton: 5 killed

Date & Time: Jan 29, 1996 at 1627 LT
Type of aircraft:
Operator:
Registration:
ZK-SFA
Survivors:
Yes
Schedule:
Wellington - Picton
MSN:
208-0051
YOM:
1985
Country:
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
5
Pax fatalities:
Other fatalities:
Total fatalities:
5
Captain / Total flying hours:
1937
Captain / Total hours on type:
322.00
Circumstances:
Following an uneventful flight from Wellington, the pilot started the descent to Picton-Koromiko Airport in good weather conditions. On final, at an altitude of 1,700 feet, the single engine aircraft entered clouds and struck the slope of Mt Robertson located 10 nm northeast of Blenheim. All five occupants were killed and the pilot was seriously injured.
Probable cause:
The following causal factors were reported:
- The decision by the pilot to descend beneath the cloud layer.
- Illusions, created by the conditions, producing misleading visual references.
- The pilot's misidentification of distant terrain features.
- An undetected heading error, and loss of "positional awareness".
- Insufficient forward visibility, during the later stages of the descent.
- The high speed of the aircraft.
- The decision making by the pilot: the delayed decision to descend beneath the cloud layer; continued flight into deteriorating conditions.
The following contributing factors were reported:
- The pilot's familiarity with the area, creating a false sense of security.
- Improved general weather conditions, causing the pilot to relax.
- A possible false horizon, created by a sloping cloud base.
- The absence of documented procedures to ensure pilots crossed the coast south of Rarangi.
Final Report:

Crash of a Fletcher FU-24-954 in Rongoio Station: 1 killed

Date & Time: Nov 1, 1995 at 1020 LT
Type of aircraft:
Operator:
Registration:
ZK-EUG
Flight Phase:
Survivors:
No
Schedule:
Rongoio Station - Rongoio Station
MSN:
284
YOM:
1982
Country:
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Captain / Total flying hours:
10000
Captain / Total hours on type:
8500.00
Circumstances:
The pilot was completing spraying mission in the region of Rongoio Station, about 18 nm north of Wairoa. In flight, control was lost and the aircraft crashed, bursting into flames. The pilot, sole on board, was killed.
Probable cause:
The following findings were reported:
- The pilot suffered an acute myocardial infarction while in flight,
- The effects of the myocardial infarction probably led initially to loss of situational awareness and loss of control of the aircraft,
- The pilot may have realised at a late stage that a collision with the ground was imminent, but was unable to recover from the situation in time to avoid it.
Final Report:

Crash of a De Havilland DHC-8-102 in Palmerston North: 4 killed

Date & Time: Jun 9, 1995 at 0925 LT
Operator:
Registration:
ZK-NEY
Survivors:
Yes
Schedule:
Auckland - Palmerston North
MSN:
055
YOM:
1986
Flight number:
AN703
Country:
Region:
Crew on board:
3
Crew fatalities:
Pax on board:
18
Pax fatalities:
Other fatalities:
Total fatalities:
4
Captain / Total flying hours:
7765
Captain / Total hours on type:
273.00
Copilot / Total flying hours:
6460
Copilot / Total hours on type:
341
Aircraft flight hours:
22154
Aircraft flight cycles:
24976
Circumstances:
At 08:17 Ansett New Zealand Flight 703 departed Auckland (AKL) as scheduled bound for Palmerston North (PMR). To the north of Palmerston North the pilots briefed themselves for a VOR/DME approach to runway 07 which was the approach they preferred. Subsequently Air Traffic Control specified the VOR/DME approach for runway 25, due to departing traffic, and the pilots re-briefed for that instrument approach. The IMC involved flying in and out of stratiform cloud, but continuous cloud prevailed during most of the approach. The aircraft was flown accurately to join the 14 nm DME arc and thence turned right and intercepted the final approach track of 250° M to the Palmerston North VOR. During the right turn, to intercept the inbound approach track, the aircraft’s power levers were retarded to 'flight idle' and shortly afterwards the first officer advised the captain ".... 12 DME looking for 4000 (feet)". The final approach track was intercepted at approximately 13 DME and 4700 feet, and the first officer advised Ohakea Control "Ansett 703" was "established inbound". Just prior to 12 miles DME the captain called "Gear down". The first officer asked him to repeat what he had said and then responded "OK selected and on profile, ten - sorry hang on 10 DME we’re looking for four thousand aren’t we so - a fraction low". The captain responded, "Check, and Flap 15". This was not acknowledged but the first officer said, "Actually no, we’re not, ten DME we’re..... (The captain whistled at this point) look at that". The captain had noticed that the right hand main gear had not locked down: "I don’t want that." and the first officer responded, "No, that’s not good is it, so she’s not locked, so Alternate Landing Gear...?" The captain acknowledged, "Alternate extension, you want to grab the QRH?" After the First Officer’s "Yes", the captain continued, "You want to whip through that one, see if we can get it out of the way before it’s too late." The captain then stated, "I’ll keep an eye on the airplane while you’re doing that." The first officer located the appropriate "Landing Gear Malfunction Alternate Gear Extension" checklist in Ansett New Zealand’s Quick Reference Handbook (QRH) and began reading it. He started with the first check on the list but the captain told him to skip through some checks. The first officer responded to this instruction and resumed reading and carrying out the necessary actions. It was the operator’s policy that all items on the QRH checklists be actioned, or proceeded through, as directed by the captain. The first officer started carrying out the checklist. The captain in between advised him to pull the Main Gear Release Handle. Then the GPWS’s audio alarm sounded. Almost five seconds later the aircraft collided with terrain. The Dash 8 collided with the upper slope of a low range of hills.
Probable cause:
The captain not ensuring the aircraft intercepted and maintained the approach profile during the conduct of the non-precision instrument approach, the captain's perseverance with his decision to get the undercarriage lowered without discontinuing the instrument approach, the captain's distraction from the primary task of flying the aircraft safely during the first officer's endeavours to correct an undercarriage malfunction, the first officer not executing a Quick Reference Handbook procedure in the correct sequence, and the shortness of the ground proximity warning system warning.
Final Report:

Crash of a Fletcher FU-24-954 in Lake Grassmere: 1 killed

Date & Time: Jun 7, 1995 at 1100 LT
Type of aircraft:
Operator:
Registration:
ZK-EMU
Flight Phase:
Survivors:
No
Site:
Schedule:
Lake Grassmere - Lake Grassmere
MSN:
274
YOM:
1980
Country:
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Captain / Total flying hours:
4930
Captain / Total hours on type:
235.00
Circumstances:
Shortly after takeoff from a field located in Lake Grassmere, while completing the 8th sortie of the morning, the pilot lost control of the airplane that crashed on hilly terrain. The aircraft was destroyed and the pilot was killed.
Probable cause:
Pilot incapacitation was the probable cause of this accident. The incapacitation of this pilot was an unusual event, and could not have been predicted or prevented by any reasonable or effective medical screening process.
Final Report:

Crash of a Fletcher FU-24-950 near Taupo

Date & Time: May 8, 1995 at 0720 LT
Type of aircraft:
Operator:
Registration:
ZK-EMB
Flight Phase:
Survivors:
Yes
MSN:
252
YOM:
1978
Country:
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
332
Captain / Total hours on type:
44.00
Circumstances:
Sole on board, the pilot was engaged in a crop spraying mission in the region of Taupo. Shortly after takeoff, while climbing at low height, the pilot initiated a right turn when the aircraft lost height and crashed in a pasture about 11 km northeast of Taupo. The aircraft was destroyed and the pilot was seriously injured.
Probable cause:
The following findings were reported:
- During a turning manoeuvre at a low height, the aircraft stalled and squashed onto the ground in a wing level attitude, at a high rate of descent,
- The height of the aircraft above the ground at the time afforded the pilot little opportunity for recovery,
- The pilot probably reverted to an unsafe flying practice he had adopted during his earlier training,
- The unsafe practice had been recognised by a previous instructor who, when not successful in correcting it, had discontinued the pilot's training,
- The final instructor had no reason to be concerned about the pilot's flying as he had exhibited no dangerous trends and flew as instructed,
- Had the final instructor been aware of a previous trait of the pilot to perform unsafe manoeuvres he might have been able to correct it,
- The causal factors in this accident were a lack of continuity in training records, pressure the pilot believed he was under to achieve maximum productivity in his flying with a minimum of delay, the pilot's apparent refusal to accept cautions in relation to his ability, and the Fletcher aircraft's performance during the execution of a limit manoeuvre too close to terrain.
Final Report:

Crash of a Beechcraft 65-A80-8800 Excalibur in Hamilton: 6 killed

Date & Time: Mar 29, 1995 at 1225 LT
Type of aircraft:
Operator:
Registration:
ZK-TIK
Flight Phase:
Survivors:
No
Schedule:
Hamilton – New Plymouth
MSN:
LD-249
YOM:
1965
Country:
Region:
Crew on board:
2
Crew fatalities:
Pax on board:
4
Pax fatalities:
Other fatalities:
Total fatalities:
6
Captain / Total flying hours:
1099
Captain / Total hours on type:
71.00
Copilot / Total flying hours:
587
Aircraft flight cycles:
10137
Circumstances:
The aircraft departed Hamilton Airport runway 36 on a scheduled service to New Plymouth on behalf of Eagle Airways. Six minutes after takeoff, while climbing to an altitude of 5,000 feet, the crew informed ATC about the failure of the left engine and was cleared to return for an emergency landing. Four minutes later, the right turn failed as well. The airplane lost height and crashed in an open field located 9 km from Hamilton Airport. All six occupants were killed.
Probable cause:
Failure of both engines after the crew failed to realize that the fuel selector was positioned on the wrong fuel tank. The following contributing factors were reported:
- After the second engine failure, the crew failed to plan effectively for a forced landing, and ultimately failed to maintain controlled flight,
- Probable factors contributing to these failures include: workload, time pressure, unfamiliarity with the situation in which they found themselves and inexperience on type.
Final Report:

Crash of a Fletcher FU-24-400 in Mangakino

Date & Time: Feb 9, 1995
Type of aircraft:
Operator:
Registration:
ZK-BIF
Flight Phase:
Survivors:
Yes
Schedule:
Mangakino - Mangakino
MSN:
33
YOM:
1956
Country:
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
Shortly after takeoff from Mangakino, while climbing, the single engine aircraft collided with power cables and crashed in a field. The pilot was injured.