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these operations specifications.
a. The certificate holder shall not takeoff an airplane for flight within airspace where RVSM is
applied unless the Administrator has approved the following aircraft systems for RVSM
operations and they are available and operational :
(1) Two independent altitude measurement systems comprised of the following elements:
(i) Cross-coupled static source system provided with ice protection, if located on the
aircraft in areas subject to ice accretion;
(ii) Equipment for measuring static pressure sensed by the static source, converting it to
pressure altitude and displaying pressure altitude to the flightcrew;
(iii) Equipment for providing a digitally-coded signal corresponding to the displayed
pressure altitude for automatic altitude reporting purposes;
(iv) Static source error correction (SSEC), if required to meet RVSM altimetry system error
requirements;
(v) Equipment to provide reference signals for automatic altitude control and alerting
systems
(2) One Secondary Surveillance Radar (SSR) altitude reporting transponder
(3) One altitude alert system
(4) One automatic altitude control system capable of automatically controlling the aircraft to a
referenced pressure altitude
b. Except when under the supervision of an appropriately trained check airman, the flightcrew must
have completed an approved training program on RVSM operating practices and procedures.
c. The integrity of design features necessary to ensure that altitude-keeping systems continue to
meet RVSM standards must be verified by scheduled tests and/or inspections in conjunction with
an approved continued airworthiness maintenance program.
d. The certificate holder is authorized to conduct operations in designated RVSM Airspace with the
airplanes listed in paragraph D0003 of these operations specifications.
e. The Administrator may authorize an operator to deviate from RVSM requirements for a specific
individual flight in RVSM airspace if:
(1) The operator submits an appropriate request with the air traffic control center controlling the
airspace in advance of the operation.
CIVIL AVIATION
ADMINISTRATION
OF CHINA CCAR-121 / 135 OPERATIONS SPECIFICATIONS
CAAC DOCUMENT
APPROVAL NO
AC-121-001R1
(Company Name) B0035-2 Certificate No:
Effective Date: Y M D
(2) At the time of filing the flight plan for the flight, Air Traffic Control (ATC) determines that the
aircraft may be provided appropriate separation and the flight will not interfere with, or impose
a burden on other operators.
1. Issued by (Branch Name) ,Regional Administration of CAAC
2. These Operations Specifications are approved by direction of CAAC
Principal Operations Inspector: (Name & Signature of POI)
3. Date Approval is effective (Y/M/D) Amendment Number:
4. The certificate holder hereby accepts and receives the Operations Specifications in this
paragraph.
Certificate Holder Representative: (Name & Signature)
Position: Date(Y/M/D):
CIVIL AVIATION
ADMINISTRATION
OF CHINA CCAR-121 / 135 OPERATIONS SPECIFICATIONS
CAAC DOCUMENT
APPROVAL NO
AC-121-001R1
(Company Name) B0037-1 Certificate No:
Effective Date: Y M D
B0037 AUTHORIZED TO CONDUCT CLASS II NAVIGATION USING A FLIGHT NAVIGATOR
The certificate holder is authorized to conduct Class II navigation using a flight navigator only within
the areas of en route operation where this paragraph is referenced in paragraph B0039 of these
operations specifications. Unless specifically authorized elsewhere in these operations specifications,
the certificate holder shall not conduct Class II navigation operations within Central East Pacific
Composite Airspace, North Pacific Airspace North Atlantic Minimum Navigation Performance
Specifications Airspace NAT/MNPS, or Areas of Magnetic Unreliability. The certificate holder shall
conduct all Class II navigation operations using a flight navigator in accordance with the provisions of
this paragraph.
a. Unless a flight navigator is used, in lieu of the pilots, to operate the long-range navigation
systems approved in accordance with paragraph B0015 of these operations specifications, a
periscope sextant with mount and at least one of the following additional navigation equipment
combinations must be installed and operational for any Class II navigation operation using a flight
navigator.
(1) An approved Inertial navigation system, or an approved Global Position Satellite Navigation
System.
(2) An approved Loran "C" receiver and a reliable drift and ground speed indication from either an
approved Doppler radar sensor, an approved Inertial navigation sensor, an approved Global
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CCAR121_135 Operations Specifications(43)
