FAR Pts 119 and 135 Flashcards
FAR 119.33
Established specific requirements that part 121 and 135 air carriers follow to obtain air carrier certificate
– 121=larger aircraft
– 135=smaller aircraft generally
•All operators comply with part 91
– Both 121 and 135 will have ops specs
What is the purpose of OpSpecs?
They specify the authorizations, limitations, and certain procedures under which each type of operation must be conducted.
Do OpSpecs need to be available to crew members?
Yes.
Part 119 requires the operator to insert pertinent excerpts from the Ops Specs in the General Operations Manual (GOM) for ready use by their crewmembers and other employee personnel. The Ops Specs information in an operator’s manual must pertain only to that operator’s type of operation and be written in a manner that is directly applicable to the certificate holder or operator’s crewmembers and/or other employee personnel.
The regulations also require that when Ops Specs information is incorporated into the operator’s manual, the text will clearly identify each excerpt as part of the Ops Specs and state that compliance with each Ops Spec is mandatory.
What is the general layout of OpSpecs?
- Part A—General
- Part B—En Route Authorizations and Limitations
- Part C—Airplane Terminal Instrument Procedures and Airport Authorizations and Limitations
- Part D—Maintenance
What does FAR 119.49(a) list?
OpSpec requirements
119.69
•Required Positions under 135
– Directors of Operations
– Chief Pilot
– Director of Maintenance
What does 91.175 say about take off and landing under IFR?
A lot, in short though:
Your DA/MDA is the highest of the following:
–The DH or MDA prescribed by the approach procedure
–The DH or MDA prescribed for the pilot in command*
–The DH or MDA for which the aircraft is equipped
You can’t go below the DA/MDA unless:
-The approach is normal and stabilized
-Flight vis is at or above that perscribed on the approach
-At least one specified visual reference is visible (see the reg fof the complete list)
What are the IFR take off minimums for a pt 91 pilot? What about a Pt 135 pilot?
Pt 91, no mins. Use common sense
Pt. 135:
-Mins perscribed by the airport (ODP, SID, etc)
If no airport perscribed mins:
(1)For aircraft, other than helicopters, having two engines or less —1 statute mile visibility.
(2)For aircraft having more than two engines — 1/2 statute mile visibility
135.21
Must have manuals that tells the FAA your procedures
– Exception of 1 pilot
135.99(a)/.101/.105
Mandates 2 crew with 10 or more passenger seats, less than 10 you can fly 135 with 1 pilot if:
– Autopilot (op specs authorizes it)
– PIC must have 100 hrs in make/model
– Certificate holder applies for amendment to us autopilot and demonstrates safety
– Aircraft is not operated CAT II
135.100
Sterile Cockpit
Pilots may not perform any duties during a critical phase of flight except those required for the safe operation of the aircraft.
Pilots may not permit any activity during a critical phase of flight whichcould distract any pilot from or interfere with the performance ofhis/her duties.
For the purposes of this section, critical phases of flight includes all ground operations involving taxi, takeoff and landing, and all other flight operations conducted below 10,000 feet, except cruise flight.
135.107
A flight attendant is required if the aircraft has more than 19 seats.
Are 135 operators required to use FAA certified dispatchers?
No
135.159
Equipment requirements: Carrying passengers under VFR at night or under VFR over-the-top conditions
The Aircraft needs to have:
- An anti-collision light system
- Instrument lights to make all instruments, switches, and gauges easily readable, the direct rays of which are shielded from the pilots’ eyes; and
- A flashlight having at least two size “D” cell batteries
135.163
Equipment Requirements: Aircraft Carrying Passengers Under IFR
The Aircraft must have:
–A vertical speed indicator
–A free-air temperature indicator
–A heated pitot tube for each airspeed indicator;
–A power failure warning device or vacuum indicator to show the power available for gyroscopic instruments from each power source
–An alternate source of static pressure for the altimeter and the airspeed and vertical speed indicators
–Two independent sources of energy (with means of selecting either) of which at least one is an engine-driven pump or generator. Each energy source must be able to drive all required gyroscopic instruments powered by that particular source and installed, so that failure of one instrument or source, does not interfere with the energy supply to the remaining instruments or the other energy source.