Accident Details
On 12 February 2011, a CASA C212-100 aircraft, registered PK-ZAI, operated by Sabang Merauke Raya Air Charter (SMAC), departed from Hang Nadim Airport, Batam at 1318 LT (0618 UTC) for a test flight following replacement of engine number one. The test flight was conducted over the Tanjung Pinang Island area. On board were two pilots and three company engineers.
At 0628 UTC, the aircraft appeared on Tanjung Pinang Approach radar display and was flying toward Tanjung Pinang. The controller informed that the aircraft was flying over Tanjung Pinang at 2000 feet. At 0633 UTC, it received clearance to climb to 4000 feet. At 0644 UTC, the aircraft disappeared from the radar display. Its last radar position was on a 16-mile radial of 010° from Tanjung Pinang Airport. The controller could not communicate with PK-ZAI.
At 0705 UTC, the controller requested relay by another aircraft to search for PK-ZAI, but other aircraft could not communicate with it. At 0706 UTC, the controller received information from the Indonesian Air Force Base at Gunung Bintan that an aircraft had crashed at Gunung Kijang forest, Bintan Island. After receiving this information, Tanjung Pinang Airport staff coordinated with the SAR Bureau, local police, and the Indonesian Army for search and rescue. The aircraft was found at Gunung Kijang forest, Bintan Island at coordinates 1° 10’ 45” N; 104° 34’ 22” E, about 30 km north of Tanjung Pinang Airport. All five occupants were fatally injured. The aircraft was substantially damaged.
Investigation
The official investigation identified the following factors contributing to the accident:
- The flight test was not properly prepared; there was no flight test plan.
- The current and applicable CMM is dissimilar to the CASA 212-100 and Garrett TPE331-5 Maintenance Manuals related to flight test requirements after replacement of only one engine.
- The left engine was shut down using normal/ground shut down procedure: fuel shut off switches off, followed by pulling the Power Lever rearward to reverse, as indicated by propeller pitch.
- The right engine most likely shut down by windmilling prior to impact, indicated by propellers piston distance to cylinder at normal flight range position and no rotating impact on blades.
- Casa Service Bulletin No. 212-76-07 Revision 1 (Anti Reverse), dated 23 December 1991, applicable to Casa 212-100/200, was not incorporated into this aircraft.
- The pilot in command had paresis or paralysis of the vestibular organ or system, which could result in failure to respond normally to three-dimensional motion. This condition may increase sensitivity to Spatial Disorientation (SDO), where the pilot cannot correctly perceive position, motion, and attitude relative to the earth's horizontal or to the aircraft, creating a dangerous precondition for unsafe action.
- Director General of Civil Aviation (DGCA) Decree No. 30/II/2000, issued 20 February 2009, requires additional medical examination items for issuing a medical certificate for pilots after their 60th birthday, including Video Nystagmography examination (differing from ICAO Doc 8984).