Crash of a Boeing 737-2H6 in Managua

Date & Time: Jul 18, 1993 at 1930 LT
Type of aircraft:
Operator:
Registration:
N401SH
Survivors:
Yes
Schedule:
Tegucigalpa - Managua - San José
MSN:
20584
YOM:
1972
Flight number:
SH415
Country:
Crew on board:
6
Crew fatalities:
Pax on board:
88
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
The approach to Managua-Augusto Cesar Sandino Airport was completed in poor weather conditions with limited visibility due to thunderstorm activity and heavy rain falls. On short final, the captain got distracted by lightning striking the ground to the right of the airplane. Then the aircraft landed nose first, causing it to be partially torn off. The aircraft bounced, veered off runway to the right and came to rest 45 metres to the right of the runway. All 94 occupants evacuated safely, except a crew member who was seriously injured.

Crash of a Cessna 402C in Las Vegas: 3 killed

Date & Time: Jul 12, 1993 at 1440 LT
Type of aircraft:
Operator:
Registration:
N818AN
Flight Phase:
Survivors:
No
Schedule:
Las Vegas – Grand Canyon
MSN:
402C-0324
YOM:
1980
Crew on board:
1
Crew fatalities:
Pax on board:
2
Pax fatalities:
Other fatalities:
Total fatalities:
3
Captain / Total flying hours:
4120
Captain / Total hours on type:
568.00
Aircraft flight hours:
11513
Circumstances:
The pilot had a 25 minutes turnaround for the accident trip from the prior flight. No witnesses were found who observed the pilot preparing for the flight or performing a preflight inspection. Company procedures specify that the pilots are responsible for loading and unloading the baggage. The manifest for the prior flight showed 54 lbs of baggage in the nose compartment. Shortly after liftoff, the pilot told the local controller that the baggage door was open and he requested a 'go around.' The local controller told the pilot to make right traffic. Multiple witnesses saw the airplane in a nose high attitude during the initial climb after takeoff. They reported the pilot entered a right turn which continued until the airplane 'fell to the ground and hit nose first.' An airline pilot witness said that the airplane's actions were a 'classic VMC roll.' Other witnesses reported that the left nose baggage compartment door was open during the takeoff and initial climb. Evidence shows that the right eng was developing little or no power. All three occupants were killed.
Probable cause:
The pilot's failure to maintain adequate airspeed while maneuvering in the traffic pattern. A factor which contributed to the accident was the pilot's failure to assure that the nose baggage compartment door was secured.
Final Report:

Crash of a Fokker F28 Fellowship 3000 in Sorong: 41 killed

Date & Time: Jul 1, 1993
Type of aircraft:
Operator:
Registration:
PK-GFU
Survivors:
Yes
Schedule:
Jakarta - Surabaya - Ujung Pandang - Ambon - Sorong
MSN:
11131
YOM:
1978
Flight number:
MZ724
Country:
Region:
Crew on board:
4
Crew fatalities:
Pax on board:
39
Pax fatalities:
Other fatalities:
Total fatalities:
41
Circumstances:
Following an uneventful flight from Ambon, the crew was cleared to descend to Sorong-Jefman Airport. On final, the pilot encountered poor visibility due to heavy rain falls and failed to realize his altitude was insufficient. On short final, the aircraft struck a promontory located 3,000 feet short of runway 22. Upon impact, the left main gear was torn off and the aircraft crashed in shallow water. Two passengers were rescued while 41 other occupants were killed.
Probable cause:
For unknown reasons, the crew continued the approach at an insufficient altitude until the aircraft impacted a promontory and crashed.

Crash of a Britten-Norman BN-2A-21 Islander in Mitwaba

Date & Time: Jun 23, 1993
Type of aircraft:
Operator:
Registration:
9Q-CLW
Survivors:
Yes
Schedule:
Kisengwa - Mitwaba
MSN:
2030
YOM:
1981
Location:
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
3
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
On final approach to Mitwaba Airfield, the pilot was completing a last turn to join the approach path when the aircraft stalled and crashed on hilly terrain about 3 km short of runway. All four occupants were injured and the aircraft was destroyed.
Probable cause:
It is believed that the loss of control was the consequence of strong downdrafts and severe atmospheric turbulences specific to this region.

Crash of a Douglas DC-9-32 in Denpasar

Date & Time: Jun 21, 1993 at 1125 LT
Type of aircraft:
Operator:
Registration:
PK-GNT
Survivors:
Yes
Schedule:
Yogyakarta - Denpasar
MSN:
47790/907
YOM:
1979
Flight number:
GA630
Country:
Region:
Crew on board:
7
Crew fatalities:
Pax on board:
72
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
On approach to Denpasar-I Gusti Ngurah Rai Airport, Bali, the aircraft was too high on the glide. The captain made an overcorrection, causing the aircraft to approach the runway with a high rate of descent. In a nose-up attitude, the aircraft struck the runway surface with a positive acceleration of 5 g. After landing, the crew completed the deceleration and braking procedure, vacated the runway and rolled to the gate where all occupants disembarked safely. A complete inspection of the aircraft by technicians revealed that it suffered major fuselage damages and was later declared as damaged beyond repair.
Probable cause:
Wrong approach configuration on part of the flying crew.

Crash of an Antonov AN-26B near Choporti: 33 killed

Date & Time: Jun 17, 1993 at 2215 LT
Type of aircraft:
Operator:
Registration:
EY-26035
Flight Phase:
Survivors:
No
Site:
Schedule:
Batumi - Baku - Shimkent
MSN:
106 04
YOM:
1981
Country:
Region:
Crew on board:
5
Crew fatalities:
Pax on board:
28
Pax fatalities:
Other fatalities:
Total fatalities:
33
Circumstances:
En route from Batumi to Baku, while cruising at the assigned altitude of 5,100 metres, the crew encountered poor weather conditions with thunderstorm activity and severe turbulences. Shortly later, the aircraft stalled, entered an uncontrolled descent and crashed on the slope of a mountain (690 metres high) located near Choporti. The aircraft disintegrated on impact and all 33 occupants were killed.
Probable cause:
Loss of control in flight following atmospheric turbulences in thunderstorm area.

Crash of a Dornier DO228-201 in Lyudao

Date & Time: Jun 14, 1993
Type of aircraft:
Operator:
Registration:
B-12298
Survivors:
Yes
Schedule:
Taitung – Lyudao
MSN:
8151
YOM:
1988
Country:
Region:
Crew on board:
2
Crew fatalities:
Pax on board:
20
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
On final approach to Lyudao Airport, the crew failed to realize his altitude was too low when the aircraft struck the ground few metres short of runway threshold. Upon impact, the right main gear was torn off and the aircraft crash landed and came to rest on the main runway. All 22 occupants escaped uninjured while the aircraft was damaged beyond repair.
Probable cause:
The crew continued the approach at a too low altitude until the aircraft impacted ground short of runway.

Crash of a Piper PA-31-350 Navajo Chieftain in Young: 7 killed

Date & Time: Jun 11, 1993 at 1918 LT
Registration:
VH-NDU
Survivors:
No
Schedule:
Sydney – Cowra – Young – Cootamundra
MSN:
31-8152083
YOM:
1981
Flight number:
OB301
Country:
Region:
Crew on board:
2
Crew fatalities:
Pax on board:
5
Pax fatalities:
Other fatalities:
Total fatalities:
7
Captain / Total flying hours:
1822
Captain / Total hours on type:
337.00
Copilot / Total flying hours:
954
Copilot / Total hours on type:
43
Aircraft flight hours:
3936
Circumstances:
At about 1500 hours EST, 11 June 1993, a standard company flight plan held by the CAA at the Melbourne flight briefing facility was activated. The plan indicated that Piper PA-31-350 aircraft VH-NDU would be conducting flight OB 301, a regular public transport service from Sydney (Kingsford Smith) airport to Cootamundra NSW, with intermediate landings at Cowra and Young. The flight was planned to be operated in accordance with IFR procedures, with a scheduled departure time from Sydney of 1720. The aircraft was to be crewed by two pilots. Prior to departure, the company scheduled a second aircraft to operate the Sydney–Cowra sector. Consequently, VH-NDU was required to land only at Young and Cootamundra. At that time of the year, the 1720 departure time meant that the flight would be conducted entirely at night. VH-NDU departed Sydney at 1738 carrying five passengers, with a fuel endurance of about 253 minutes. The pilot-in-command occupied the left cockpit seat. The aircraft initially tracked via the direct Sydney to Cowra route and climbed to a cruising altitude of 8,000 feet. At 1801 the pilot reported to Sydney FIS that the aircraft was now tracking direct to Young, and would report at Riley, an en route reporting point located 62 NM from Young on the Katoomba– Young track. FIS advised the area QNH was 1003 hPa. At 1814 the pilot reported the aircraft was at Riley and estimated arrival at Young at 1835. By 1820 the pilot had reported on descent to Young, with in-flight conditions of cloud and heavy rain. Recorded radar data later showed that the aircraft passed 13.5 NM to the south-east of Riley, south of the direct Katoomba–Young track. At about 18.5 NM north-east of Rugby, the aircraft turned right and initially tracked about 280° before turning left to track direct to Young. When queried by FIS at 1836, the pilot amended the estimate for his arrival at Young to 1838. At 1842, after prompting from FIS, the pilot reported at Young that he was commencing an NDB approach, and would call again on the hour or in the circuit. Shortly after 1845 witnesses at Young aerodrome saw the lights of an aircraft, which they believed to be VH-NDU, pass low overhead after approaching from the east. Some minutes later the same aircraft was seen to pass over the aerodrome from the opposite direction and appear to climb away towards the east. On both occasions the runway and aerodrome lights were not illuminated, although the aerodrome was equipped with PAL and it was the responsibility of the pilot-in-command to activate it. At 1850 FIS advised VH-NDU of the proximity of Cessna 310 aircraft, VH-XMA, which was estimating arrival at Young at 1900. VH-XMA subsequently reported holding in visual conditions at about 8 NM north of Young. The pilot of VH-NDU reported at 1903 that he was on another overshoot at Young, about to commence another approach, and would report again at 1915. FIS provided additional traffic on Piper PA31 aircraft, VH-XML, which was also estimating Young at 1915. At about this time witnesses reported seeing the runway lights illuminate. VH-XMA then proceeded to Young and landed on runway 01 at about 1912. At 1916 VH-NDU reported in the Young circuit area and cancelled SARWATCH. A pilot witness said that the aircraft passed over the northern end of the aerodrome from a westerly direction before turning right and taking up a heading consistent with a right downwind leg for a landing on runway 01. The aircraft was then seen to turn right and pass to the south of the aerodrome before entering what appeared to be a right downwind leg for runway 19. When abeam the aerodrome the aircraft again turned right and overflew the aerodrome to enter a second right downwind leg for runway 01. Another witness thought the aircraft (VH-NDU) was significantly lower than another aircraft approaching from the east (VH-XML). Shortly after VH-NDU turned onto an apparent base leg the navigation lights were lost to sight. Almost immediately a fireball was observed, consistent with the final position of the aircraft (see figure 2). At 1918 the pilot of VH-XMA telephoned the 000 emergency services number and reported the accident to the Goulburn Ambulance Control Centre. By 1920 this information had been relayed to the Young Ambulance Service, the Young Police, and the Young SES. An off-duty Fire Brigade officer, who was waiting at the aerodrome, drove into Young and alerted the Fire Brigade at 1930. The emergency services initially travelled to Young Aerodrome but were unable to gain immediate access to the accident site, which was located on a hill some 2.2 km to the south-south-east of the aerodrome, in an area remote from roads and lighting. Access was finally gained from a road located south of the accident site. An ambulance reached the aircraft wreckage at 1952 and the crew were able to rescue and resuscitate the only survivor, who was critically injured, and transport her to the Young Hospital. She died at Camperdown Children’s Hospital at 0510 the next morning.
Probable cause:
Significant factors
1. The cloudbase in the Young circling area was below the minimum circling altitude, associated with dark night conditions and limited ground lighting.
2. The workload of the pilot-in-command was substantially increased by the effects of aircraft equipment deficiencies, with a possible consequent degrading of his performance as a result of skill fatigue.
3. The instrument approach and landing charts did not provide the flight crew with terrain information adequate for the assessment of obstacle clearance during a circling approach.
4. The Monarch operations manual did not provide the flight crew with guidance or procedures for the safe avoidance of terrain at Young during a night-circling approach.
5. The aircraft descended below the minimum circling altitude without adequate monitoring of obstacle clearance by the crew.
6. The visual cues available to the flight crew were insufficient as a sole source of height judgement.
7. There were organisational deficiencies in the management and operation of RPT services by Monarch.
8. There were organisational deficiencies in the safety regulation of Monarch RPT operations by the CAA.
Final Report:

Crash of a Britten-Norman BN-2A-20 Islander in Golgubip: 9 killed

Date & Time: Jun 9, 1993
Type of aircraft:
Operator:
Registration:
P2-SWA
Survivors:
Yes
Schedule:
Tabubil - Golgubip
MSN:
805
YOM:
1976
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
10
Pax fatalities:
Other fatalities:
Total fatalities:
9
Circumstances:
On short final to Golgubip Airstrip, the twin engine airplane banked left, causing the left wing to struck the ground and the aircraft crashed 100 metres short of runway threshold. The pilot and a passenger were seriously injured while nine other occupants were killed.
Probable cause:
It was reported that the aircraft stalled and rolled to the left on final approach because its speed was insufficient.

Crash of a Britten-Norman BN-2A-20 Islander on Kiriwina Island

Date & Time: Jun 3, 1993
Type of aircraft:
Operator:
Registration:
P2-ISC
Flight Phase:
Survivors:
Yes
MSN:
394
YOM:
1974
Region:
Crew on board:
0
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
Crashed following an engine failure. There were no casualties.
Probable cause:
Engine failure for unknown reasons.