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Crash of a McDonnell Douglas MD-83 in Bandar-e Mahshahr

Date & Time: Jan 27, 2020 at 0736 LT
Type of aircraft:
Operator:
Registration:
EP-CPZ
Survivors:
Yes
Schedule:
Tehran - Bandar-e Mahshahr
MSN:
53464
YOM:
1994
Flight number:
RV6936
Country:
Region:
Crew on board:
8
Crew fatalities:
Pax on board:
136
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
18430
Captain / Total hours on type:
7840.00
Copilot / Total flying hours:
300
Copilot / Total hours on type:
124
Circumstances:
On Jan. 27, 2020, at 03:12 UTC Caspian Airlines (CPN) Flight 6936, an MD83, EP-CPZ took off from Mehrabad International Airport and climbed to FL320 as final cruising level. At about 03:45:37 UTC, the aircraft was flying according to the flight plan route on Airway B417 at an assigned FL320. Due to another traffic departing flight, an A320, IRA356 from Abadan Airport (OIAA) to destination Mashhad International Airport (OIMM), the ACC controller issued direct routing to the flight CPN 6936 position GODMO. At 03:49:34 UTC, CPN6936 requested descent clearance, so the flight was cleared to FL100. At 03:52:30 UTC, the pilot called Mahshahr AFISO and reported position 50 nm inbound GODMO and estimated time over GODMO at 03:59 UTC. At 03:52:51 UTC, Mahshahr AFISO reported necessary information as below: "RWY active is 31; wind is now 280/08kts, CAVOK, temperature +06, DP 04 and QNH 1023, expected VOR approach RWY 31 via GODMO 1E ARRIVAL" At 03:53: 33 UTC, the pilot requested RWY 13 and Mahshahr AFISO performed VOR/DME approach RWY 13, via GODMO 1F arrival. At 03:59:39 UTC, the pilot reported, “we are approaching position GODMO in contact with destination Mahshahr.” At 04:00:41UTC, the pilot reported his position “GODMO” to Mahshahr AFISO. At 04:02:46 UTC, the pilot reported leaving of IAF and received landing clearance for RWY13. Finally, at 04:06:11 UTC, the aircraft landed on RWY 13, passed two-thirds of RWY length and ran off the end of runway13 after landing at Mahshahr Airport at 04:06 UTC, Khuzestan province. The accident flight was being operated on an Instrument Flight Rules (IFR) flight plan in a Visual Meteorological Condition (VMC). The main door of the accident aircraft was opened in emergency condition, but the slide skid did not operate automatically. The cabin floor was just too close to the ground (grass surface) due to the impact of the nose and main landing gears strut which were broken after the runway overrun. The evacuation was performed from the main door, and all 136 passengers and 8 crew members disembarked.
Probable cause:
The Aircraft Accident Investigation Board determines that the probable causes of this accident were the pilots’ failures below, resulting in a runway overrun:
- Poor decision-making for acceptance of the risk of high-speed landing;
- Un-stabilized approach against the normal flight profile;
- Poor CRM in the cockpit; and
- Poor judgment and not accomplishing go-around while performing an unstabilized approach.

Contributing Factors:
- Loading of 5 tons of extra fuel, which increased the landing distance required.
- Decision to make a landing on RWY 13 with tailwind.
- Inability of the copilot (PM) to take control of the aircraft and proper action to execute goaround.
Final Report:

Crash of a Tupolev TU-154M near Qazvin: 168 killed

Date & Time: Jul 15, 2009 at 1133 LT
Type of aircraft:
Operator:
Registration:
EP-CPG
Flight Phase:
Survivors:
No
Schedule:
Tehran - Yerevan
MSN:
87A-748
YOM:
1987
Flight number:
RV7908
Location:
Country:
Region:
Crew on board:
12
Crew fatalities:
Pax on board:
156
Pax fatalities:
Other fatalities:
Total fatalities:
168
Aircraft flight hours:
26593
Aircraft flight cycles:
16248
Circumstances:
The three engine aircraft departed Tehran-Imam Khomeiny Airport at 1117LT on a regular schedule flight to Yerevan, carrying 158 passengers and 10 crew members. Sixteen minutes after takeoff, while cruising over Qazvin at FL340, the aircraft suddenly changed its heading to 270° and then entered a rapid descent, losing 20,000 feet in 90 seconds. In a near vertical attitude, the aircraft crashed in an open field, causing a large crater. The aircraft disintegrated on impact and all 168 occupants were killed.
Probable cause:
Failure of the first stage of the high compressor disk on the left engine while the aircraft was flying at FL340, due to fatigue cracks. Debris punctured the engine nacelle, and several hydraulic and fuel lines were cut while all control systems were unserviceable. A huge fire spread on the left side of the airplane and the airplane entered an uncontrolled descent until impact.
Final Report: