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Herzlich Willkommen, Gast ( Login | Registrieren ) |
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Admin |
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#1
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![]() Administrator ![]() ![]() ![]() Gruppe: Admin Lizenzen und Qualifikation: CPL(H) Typerating(s): BO105, AS350 Beiträge: 541 seit: 07. Juni 03 Ort: Öhringen Mitglieder Nr.: 1 ![]() |
Ich habe im alten Forum schon einmal dieses Video online gestellt. Nachdem der Link in einem Newsletter (oder sonstwo) aufgetaucht war und demnach einigermaßen Traffic verursacht hat, mußte ich es leider vom Webserver entfernen.
Mittlerweile habe ich Vorkehrungen getroffen, daß es nicht mehr 'deep gelinkt' werden kann. Wenn ihr es ansehen möchtet, müßt ihr im Forum registriert und angemeldet sein: Bell 407 Looping und Rolle Ich muß nicht extra erwähnen, daß es (meines Wissens) keine Freigabe für derartige Manöver im FOM gibt, oder? Gruß, Marcus -------------------- |
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FabHud |
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#2
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Schnupperflieger ![]() Gruppe: Members Beiträge: 7 seit: 28. April 05 Mitglieder Nr.: 120 ![]() |
Hallo,
inzwischen ist das Video wohl weit verbreitet und die Last für dich wird eher gering bleiben. 2 Zitate dazu: QUOTE(clipboard) Rumour has it that the pilot flew the sequence during his "validation flight" on the Friday, and the Airshow Director and Safety Officer authorized the manouver based on information supplied to them by the pilot that Bell and the CAA had approved the manouvers, which we now know, was not the case. The fact that this pilot was trained in Germany by the factory pilots from MBB how to loop and roll a BK 117 and MBB 105, does not necessarily mean that he, as a "Professional pilot", is entitled to break the rules (and the law) by an act of such stupidity. Stupidity?? YES! The fact that Bell have withdrawn the warranties on the machine, theoretically renders it worthless. NO re-sale value! Zero. May just as well be dumped as scrap. The 407 handbook clearly states NO aerobatic manouvers permitted, and this SHOULD be respected. QUOTE(vince290) LETTER FROM BELL HELICOPTER SPECIAL INSPECTION PROCEDURES ATTACHMENT A to Letter August 30, 2004 The following actions will be required in order to evaluate the continued airworthiness of Model 407 Serial Number 53078 A. Permanent removal from service is required for the following components: a. All metal components of the main rotor hub assembly including the elastomeric components and blade bolts b. Main rotor mast assembly c. Boosted main rotor fixed and rotating controls, including the swashplate assembly and support. d. Main rotor control hydraulic actuators, and the support casting. e. Flight control bolts in the boosted control system. f. Drive system components to include tail rotor drive shafts, bearings, hangers, flex couplings and splined adapters. g. Input (Ka-Flex) drive shaft h. Transmission top case i. Transmission-mounted flight control bellcranks and support brackets. j. Tail rotor mast k. Tail boom and attach hardware l. Pylon support structure including the pylon side beams, corner mounts, longitudinal pitch restraints, stop fittings and associated attachment hardware. B. Components requiring complete inspection and overhaul at Bell Helicopter: a. Main and tail rotor blades b. Main rotor yoke assembly c. Tail rotor yoke assembly C. Components to be overhauled by a facility suitable to Bell (Bell Tennessee/CSR): a. Transmission assembly b. Freewheel assembly c. Tail rotor gearbox D. Airframe inspection by qualified personnel suitable to Bell: a. Fuselage structure for evidence of cracks or distortion b. Instrument panel console for evidence of distortion c. Battery and ballast weight supports d. Cabin roof beam assembly e. Roll-over bulkheads Page 2: f. Vertical control tunnel g. Engine deck for cracks, distortion evidence h. Tail boom attachment fittings and longerons i. Horizontal stabilizer j. Vertical and auxiliary fins In support of the above return to service action, the aircraft interior shall be removed and other systems and controls as necessary to permit close and rigid visual inspection of the entire fuselage structure as recommended above. Prior to release for return to service, items not listed above shall be inspected in accordance with the basic aircraft 300 hour / annual inspection. Any material abnormalities or discrepancies identified during the conditional inspection are to be reported to Product Support Engineering - Light Helicopters, for evaluation. Items listed above that are to be permanently removed from service are deemed unsuitable for use, and shall be destroyed, permanently marked or otherwise disfigured so as to prevent inadvertent installation on an operational helicopter. Grüsse, FabHud |
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Wassermaxe |
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#3
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Schnupperflieger ![]() Gruppe: Members Beiträge: 4 seit: 30. April 05 Mitglieder Nr.: 121 ![]() |
Hallo!
Der Link funktioniert leider bei mir nicht ![]() Grüße, Wassermaxe [edit von Admin]Wir klären das gerade per PN.[/edit] |
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