| EASA Safety Information Notice No.: 2007 ? 08 Issued: 13 April 2007 addresses the automatic double engine failure on takeoff in a Diesel-powered DA-42 if external power is used for start (see ASW 07 May 07 "Sudden Silences").Note that: "This Safety Information Notice is for information only. No AD action by National Airspace Authorities is required." See tinyurl.com/2xc2oq |
| Aircraft |
Effect |
| AD 2007-10-15 Cessna Caravan C208/C208B |
Requirement is the installation of a functional low airspeed awareness system to operate the airplane in known icing conditions. AD is to assure that the pilot has enough information and the necessary equipment to prevent loss of control of the airplane while in-flight during icing conditions. Supersedes AD 2006-06-06 Final rule eff 21 Jun |
| 2007-CE-035-AD BAe Jetstream (all series) |
In-service reports have been received by BAE of failed bolts fitted to frame 199 wing spigot post assembly. If left uncorrected, failure of these bolts will severely compromise the structural integrity of the wing to fuselage attachment? failure of which would lead to loss of the aircraft. NPRM comments by 18 Jun |
| 2006-SW-08-AD Eurocopter EC130 B4 |
To notify the flight crew of an overheated battery, and to prevent a thermal runaway of the battery, an in-flight fire, and subsequent loss of control of the helicopter. NPRM comments by 20 Jul |
| 2006-SW-23-AD Eurocopter EC130 B4 |
Prompted by incident in which the engine remained at idle speed although the twist grip had been turned to the flight position.To detect debonding between the twist grip drive tubes and the control pinions on the pilot's collective levers to prevent loss of throttle control of the engine, and subsequent loss of control. NPRM comments by 20 Jul |
| 2007-NE-04-AD PW4164, -4168 engines |
AD results from a report of improperly manufactured LPT stage 4 disks. AD is to prevent an uncontained engine failure due to low-cycle fatigue (LCF). NPRM comments by 20 Jul |
| AD 2007-10-12 Reinforced Flight Deck Doors |
Results from a report of smoke and fumes in the cockpit? to prevent inadvertent release of the decompression latch and consequent opening of the decompression panel in the flight deck door, or penetration of the flight deck door by smoke. Affects 737, 757, DC-10, MD-10, MD-11. Final rule eff 27 Jun |
| 2007-NM-034-AD 747-100/200 |
Results from a report of a 2" crack through the fuselage skin and internal bonded doubler at the cutout of the bulk cargo door light. ..to detect and correct cracks in the fuselage skin at the cutout of the bulk cargo door light, which could result in reduced structural integrity of the fuselage at the bulk cargo door and consequent rapid decompression. NPRM comments by 9 Jul |
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