D2X-X7 Rev.6 121203



CIVIL AVIATION REQUIREMENTS SECTION 2, AIRWORTHINESS SERIES 'X', PART VII 22ND AUGUST 1984 Rev.6 3rd December 2012


2. Requirement
2.1 No person in charge of any aircraft shall allow such aircraft to be flown unless
the following valid documents, as applicable (in original or attested copies), are
carried on board the aircraft:

xiv Aeroplane/ Helicopter search procedure checklist;
xv Maintenance Release/Certificate to release to service;
xvi LOPA (Layout of Passenger Arrangement);
xvii Emergency and Safety Equipment Layout;

 XXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXX
CAR D8O-OIV 11.1 Helicopter search procedures checklist
An operator shall ensure that there is on board a checklist of the procedures to be followed in searching for a bomb in case of suspected sabotage. The checklist shall be supported by guidance on the course of action to be taken should a bomb or suspicious object be found.

CAR D8O-O III  2.1.1.5 The pilot-in-command should have available on board the aeroplane the
essential information concerning the search and rescue services in the area over which the aeroplane will be flown.

2.4.2.3 Aeroplanes on all flights should be equipped as applicable with the ground-air signal codes for search and rescue purposes

2.4.5 Aeroplanes on flights over designated land areas Aeroplanes, when operated across land areas which have been designated by the Airports Authority of India (AAI) concerned as areas in which search and rescue would be especially difficult, shall be equipped with such
signaling devices and lifesaving equipment (including means of sustaining life) as may be appropriate to the area overflown.

3.3.1.4 An operator shall ensure that the pilot-in-command has available on board
the aeroplane all the essential information concerning the search and rescue services in the area over which the aeroplane will be flown

Layout of Passenger Accommodations (LOPA)
The LOPA is an engineering diagram of the aircraft’s cabin interior that includes, but is
not limited to, locations of passenger and flight attendant seats, emergency equipment,
exits, lavatories, and galleys. It leads the reviewer through the interior design/layout and
is the document that certifies the interior components and installation.

  SPSINGHAME.COM






Comments

Post a Comment

Popular posts from this blog

Cessna 152 Magneto Check

MAGNETO CHECK. NEVER ADVANCE TIMING BEYOND SPECIFICATIONS IN ORDER TO REDUCE RPM DROP. Too much importance is being attached to RPM drop in single ignition. RPM drop on single ignition is a natural characteristic of dual ignition design. The purpose of the following magneto check is to determine that all cylinders are firing. If all cylinders are not firing, the engine will run extremely rough and cause for investigation will be quite apparent. The amount of RPM drop is not necessarily significant and will be influenced by ambient air temperature, humidity, airport altitude, etc. In fact, absence of RPM drop should be cause for suspicion that the magneto timing has been bumped up and is set in advance of the setting specified. Magneto checks should be performed on a comparative basis between individual right and left magneto performance. a. Start and run engine until the oil and cylinder head temperatures are in normal operating ranges. b. Advance engine speed to 1700 RPM. c. Tu
Read more

Brake System Cessna 172

                             BRAKE SYSTEM -MAINTENANCE PRACTICES              1. Description and Operation A. The hydraulic brake system is comprised of two master cylinders, located immediately forward of the  pilot’s rudder pedals, brake lines and hoses, and single-disc, floating cylinder brake assemblies located at  each main landing gear wheel. B. The parking brake system is comprised of a pull-type handle and mechanical connections which are  linked to the rudder pedal assembly. Pulling aft on the brake handle applies mechanical pressure to the  rudder pedals, activating the brakes and locks the handle in place. Turning the handle 90 degrees will  release the parking brake and allow for normal operation through the rudder pedals. C. Brake operation is accomplished by pushing on the upper part of each rudder pedal. This motion is  mechanically transmitted to the respective brake master cylinder, and through fluid-carrying lines out to  the brake assembly where fluid pressure
Read more

McCauley Propeller Installation fixed pitch

Image
Propeller Installation for all fixed pitch propellers (except 1A162 model propellers).                   WARNING: MAKE SURE THE MAGNETO IS GROUNDED BEFORE INSTALLING  THE PROPELLER OR CONNECTING EXTERNAL POWER.                NOTE: McCauley recommends that propeller mounting nuts (if applicable) be replaced at each  propeller installation, whenever possible. However, nuts may be reused providing the threads are in good condition and the locking material prevents turning of the nut on the  stud by hand. Propeller mounting bolts must be magnetic particle inspected in accordance  with ASTM E-1444 or replaced whenever the propeller is removed from the engine.                NOTE: The aircraft maintenance manual or STC installation instructions should always be  consulted for any specialized procedures applicable to a specific aircraft. Various spinner arrangements not manufactured by McCauley may be used which require additional procedures. (1) Make sure the mating surfaces of t
Read more