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Crash of a Raytheon Premier in Udaipur

Date & Time: Mar 19, 2008 at 1507 LT
Type of aircraft:
Registration:
VT-RAL
Survivors:
Yes
Schedule:
Jodhpur - Udaipur
MSN:
RB-23
YOM:
2001
Country:
Region:
Crew on board:
2
Crew fatalities:
Pax on board:
5
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
2900
Captain / Total hours on type:
40.00
Copilot / Total flying hours:
896
Copilot / Total hours on type:
58
Aircraft flight hours:
989
Aircraft flight cycles:
812
Circumstances:
The aircraft, after necessary met and ATC briefing took off at 0940 UTC from Jodhpur on direct route W58 at cruise FL 100 and sector EET 20 minutes as per Flight Plan. No abnormality was reported / recorded by the pilot during take off from Jodhpur. The crewmember of the aircraft while operating Jodhpur–Udaipur were the same who operated flight Delhi-Jodhpur on 18.3.2008. There were five passengers also on board the aircraft. The aircraft climbed to the assigned level where the pilot was experiencing continuous turbulence at FL100. The pilot communicated the same to the ATC Jodhpur and requested for higher level which was not granted and advised to continue at same level and contact ATC Udaipur for level change. It came in contact with Udaipur at 0944 UTC, approx 50 NM from Udaipur. At 0948 the weather passed by ATC was winds 180/07 kts. Vis 6 km. Temp 34, QNH 1006 Hpa and advised for ILS approach on runway 26. Consequently the pilot requested to make right base Rwy 26 visual approach, which was approved by the ATC. Aircraft did not report any defect/snag. Pilot further stated that during approach to land at Udaipur when flap 10 degree was selected, the flap didn’t respond and ‘Flaps-Fail’ message flashed. Thereafter he carried out the check list for flapless landing. At 1004 UTC when the aircraft reported on final the ATC cleared the aircraft to land on runway 26 with prevailing wind 230/10 Kts. The same was acknowledged by the crew and initiated landing. At about 20 to 30 feet above ground the pilot stated to have experienced sudden down-draft thereby the aircraft touched down heavily on the runway. The touch-down was on the centerline, at just before the touchdown Zone (TDZ), on the paved runway, after the threshold point. Consequent to the heavy impact both the main wheel tyre got burst; first to burst was right tyre. The aircraft rolled on the runway centerline for a length of about 1,000 feet in the same condition. Thereafter it gradually veered to the right of the runway 26 at distance of approx 2,200 feet runway length from the threshold of the runway. The aircraft left the runway shoulder and after rolling almost straight for another 90 ft it stopped after impact with the airport boundary wall.
Probable cause:
The approach speed for flapless landing was about 149 knots against the calculated speed 130-135 knots approx. Incident occurred as the aircraft impacted runway with higher speed while carrying out flapless approach and landing.
Final Report:

Crash of a De Havilland DH.89A Dragon Rapide near Jodhpur: 2 killed

Date & Time: Jun 15, 1954
Operator:
Registration:
G-AKLA
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Jodhpur – Hanoi
MSN:
6764
YOM:
1947
Country:
Region:
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
2
Circumstances:
Few minutes after takeoff from Jodhpur Airport, the twin engine aircraft crashed in unknown circumstances about 60 km east of the city. Both pilots were killed. They were in charge to deliver the airplane in Hanoi.

Crash of a Douglas C-47B-30-DK Dakota C.4 in Jodhpur

Date & Time: Oct 3, 1945
Operator:
Registration:
KN526
Flight Phase:
Flight Type:
Survivors:
Yes
MSN:
16325/33073
YOM:
1945
Country:
Region:
Crew on board:
4
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
An engine failed just after liftoff. The aircraft stalled and belly landed and slid for several yards before coming to rest. There were no casualties but the aircraft was written off.
Probable cause:
Engine failure.

Crash of a Potez 62.1 in Datia: 7 killed

Date & Time: Mar 7, 1938
Type of aircraft:
Operator:
Registration:
F-ANQR
Flight Phase:
Survivors:
No
Schedule:
Saigon – Calcutta – Jodhpur – Damascus - Marseille – Paris
MSN:
4031/12
YOM:
1936
Country:
Region:
Crew on board:
3
Crew fatalities:
Pax on board:
4
Pax fatalities:
Other fatalities:
Total fatalities:
7
Circumstances:
The aircraft departed Calcutta-Dum Dum Airport in the morning bound for Jodhpur. While flying over Madhya Pradesh, it went out of control and crashed in a field located near Datia. All seven occupants were killed.
Crew:
Hubert Robin, pilot,
Fernand Paujol, radio navigator,
Émile Schwager, engineer.
Probable cause:
Engine failure suspected.