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AT46 /
ATR ATR-42-600
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AT46 / Revision as of 15:03, 29 December 2016 by Integrator2 (talk | contribs)
Revision as of 15:03, 29 December 2016 by Integrator2 (talk | contribs)
| Aircraft | |||
|---|---|---|---|
| Name | ATR-42-600 | ||
| Manufacturer | ATR | ||
| Body | Narrow | ||
| Wing | Fixed Wing | ||
| Position | High wing | ||
| Tail | T-tail | ||
| WTC | Medium | ||
| Type code | L2T | ||
| Engine | Turboprop | ||
| Engine count | Multi | ||
| Position | (Front) Wing leading mounted | ||
| Landing gear | Tricycle retractable | ||
| Mass group | 3 | ||
|
| |||
ATR ATR-42-600
Description
Turboprop regional airliner. In service since 2010. An improved version of the ATR-42-500 with glass cockpit.
Technical Data
| Wing span | 24.57 m80.61 ft <br /> |
|---|---|
| Length | 22.67 m74.377 ft <br /> |
| Height | 7.59 m24.902 ft <br /> |
| Powerplant | 2 x PWC PW127M turboprops (2.400 SHP) with 6 blade propellers |
| Engine model | Pratt & Whitney Canada PW100 |
Performance Data
| Take-Off | Initial Climb (to 5000 ft) |
Initial Climb (to FL150) |
Initial Climb (to FL240) |
MACH Climb | Cruise | Initial Descent (to FL240) |
Descent (to FL100) |
Descent (FL100 & below) |
Approach | ||||||||||
| V2 (IAS) | 120 kts | IAS | 160 kts | IAS | kts | IAS | kts | MACH | TAS | 300 kts | MACH | IAS | kts | IAS | kts | Vapp (IAS) | 104 kts | ||
| Distance | 1165 m | ROC | 1355 ft/min | ROC | ft/min | ROC | ft/min | ROC | ft/min | MACH | ROD | ft/min | ROD | ft/min | MCS | kts | Distance | 1124 m | |
| MTOW | 1860018,600 kg <br />18.6 tonnes <br /> kg | Ceiling | FL260 | ROD | ft/min | APC | |||||||||||||
| WTC | M | Range | 716716 nm <br />1,326,032 m <br />1,326.032 km <br />4,350,498.691 ft <br /> NM | ||||||||||||||||
Accidents & Serious Incidents involving AT46
- B738 / AT46, Jakarta Halim Indonesia, 2016 (On 4 April 2016, a Boeing 737-800 crew taking off in normal night visibility from Jakarta Halim were unable to avoid an ATR 42-600 under tow which had entered their runway after ambiguity in its clearance. Both aircraft sustained substantial damage and caught fire but all those involved escaped uninjured. The Investigation concluded that contributory to the accident had been failure to use a single runway occupancy frequency, towing of a poorly lit aircraft, the potential effect on pilot detection of an obstruction of embedded approach lighting ahead of the displaced landing threshold and issues affecting controller traffic monitoring effectiveness.)