Part 121 Flashcards

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1
Q

What type of aeroplane does this part consider?

A

An aeroplane having SEATING configuration of MORE than 30 SEATS, EXCLUDING any REQUIRED CREW member SEATS OR a PAYLOAD CAPACITY of MORE than 3410kg

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2
Q

What are the requirements for night operations VFR?

A

A person shall NOT PERFORM an operation at NIGHT under VFR

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3
Q

What are the requirements for extended over water operations?
What is an extended over water operation?

A

A person must NOT PERFORM an EXTENDED over WATER operation VFR;
Operation planned ROUTE that contains a POINT in EXCESS of 50nm from the SHORE

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4
Q

What are the requirements for operations under VRF above more than scattered cloud?

A

PIC must NOT perform AIR OPERATION ABOVE more than SCATTERED cloud UNLESS ME aeroplane:
Meets the requirements for IFR and the MINIMUM NUMBER of flight CREW required for IFR, holding CURRENT INSTRUMENT RATINGS are at CONTROLS:
EQUIPPED with OPERATIVE instruments and equipment, including radio navigation equipment, that are REQUIRED for IFR;
Capable, with 1 ENGINE INOPERATIVE, of maintaining a NET flight PATH that has a POSITIVE SLOPE at 1000ft ABOVE CLOUD;
Carries RADIO NAVIGATION EQUIPMENT enabling it to be NAVIGATED by IFR to an aerodrome where an INSTRUMENT APPROACH procedure may be carried out for landing;
Carries SUFFICIENT FUEL and RESERVES to proceed by IFR to an aerodrome where an INSTRUMENT APPROACH procedure may be carried out FOR LANDING

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5
Q

What are the meteorological requirements for IFR flight?

A

PIC must NOT COMMENCE operation under IFR UNLESS CURRENT meteorological REPORTS or a COMBINATION of REPORTS and FORECASTS indicate that CONDITIONS:
At ETA will be AT or ABOVE MINIMA published in AIP for INSTRUMENT APPROACH likely to be USED OR;
At ETA 1 or 2 ALTERNATE aerodrome MEETS the CEILING and VISIBILITY REQUIRED by 91.405;
PIC must NOT COMMENCE operation under IFR UNLESS AT LEAST 1 ALTERNATE aerodrome meets CEILING and VISIBILITY REQUIRED by 91.405 if:
The DEPARTURE or DESTINATION aerodrome is OUTSIDE NZ AND;
The DESTINATION aerodrome has LESS than 2 SEPARATE RUNWAYS suitable for use

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6
Q

What are the reduced take off minima requirements?

A

If the HOLDER ensures the operation is CONDUCTED in accordance with REDUCED takeoff MINIMA in EXPOSITION;
The PIC and SECOND in COMMAND are QUALIFIED for REDUCED MINIMA TAKE OFF;
The RUNWAY to be used has CENTRE LINE MARKING or LIGHTING;
REDUCED take-off MINIMA on the runway to be used are PUBLISHED in the applicable AIP;
If the aeroplane is a 2 ENGINE PROPELLER driven aeroplane, the aeroplane is EQUIPPED with an operative AUTO FEATHER or AUTO COARSE system;
The runway VISIBILITY is ESTABLISHED using RVR; and
The METHOD for OBSERVING and CONFIRMING that the required VISIBILITY exists for take-off is ACCEPTABLE to the Director

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7
Q

What are the enroute limitation requirements?

What types of aeroplanes can be exempt from this?

A

HOLDER must NOT operate a PISTON ENGINE aeroplane on a ROUTE that REQUIRES MORE than 60 MINUTES flight time with 1 ENGINE INOPERATIVE CRUISE speed in STILL AIR at ISA from an ADEQUATE aerodrome;
2 TURBINE POWERED ENGINE aeroplane 60 MINUTES;
MORE than 2 TURBINE POWERED ENGINE aeroplane 180 MINUTES

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8
Q

What are the take off distance requirements?

A

HOLDER must ensure TAKE OFF WEIGHT does NOT EXCEED MAX TAKE OFF WEIGHT specified in flight MANUAL;
When calculating MAX take off WEIGHT the HOLDER ensure assuming CRITICAL ENGINE FAILS at Vef and using SINGLE V1 that:
ACCELERATE STOP DISTANCE REQUIRED does NOT EXCEED the ACCELERATE STOP DISTANCE AVAILABLE;
TAKE OFF DISTANCE REQUIRED does NOT EXCEED TAKE OFF DISTANCE AVAILABLE;
Any CLEARWAY forming part of the take off TODR shall NOT EXCEED HALF the take off RUN AVAILABLE;
In case of WET or CONTAMINATED runway, take off DISTANCE is calculated to the POINT at which aircraft reaches HEIGHT of 15ft ABOVE take off SURFACE using REDUCED V1;
Take off RUN REQUIRED does NOT EXCEED the take off RUN AVAILABLE using V1 for REJECTED and CONTINUED take off;
On WET or CONTAMINATED runway, take off WEIGHT does NOT EXCEED that permitted for take off WEIGHT on DRY runway under SAME CONDITIONS

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9
Q

What specific considerations are taken into account when calculating maximum take off weight?

A

Aerodrome ELEVATION;
PRESSURE ALTITUDE of aerodrome when PRESSURE varies MORE than 1% from ISA;
Ambient TEMPERATURE of aerodrome;
TYPE of runway SURFACE and SURFACE CONDITION;
Runway SLOPE in DIRECTION of TAKE OFF;
NOT MORE than 50% of REPORTED HEADWIND component or NOT LESS than 150% of REPORTED TAILWIND component

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10
Q

What factors shall be taken into account when calculating landing weight?
What assumptions are made for the dispatch of an aeroplane to land at an aerodrome?

A

Landing weight:
Aerodrome ELEVATION;
Ambient TEMPERATURE at the aerodrome;
TYPE of runway SURFACE and the runway SURFACE CONDITION;
Runway SLOPE in DIRECTION of LANDING;
NOT MORE than 50% of reported HEADWIND component or NOT LESS than 150% of reported TAILWIND component;
Dispatch:
FORECAST METEOROLOGICAL conditions;
Surrounding TERRAIN;
APPROACH and LANDING AIDS;
OBSTACLES within the MISSED APPROACH flight PATH;
May be DISPATCHED if ALTERNATE complies with PREVIOUS CONDITIONS

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11
Q

What are the landing distance requirements for dry runway?

A

HOLDER ensures LANDING WEIGHT for ETA does NOT EXCESS LANDING WEIGHT in flight MANUAL;
HOLDER ensures LANDING WEIGHT for ETA at destination or alternate aerodrome allows a FULL STOP landing from 50ft ABOVE THRESHOLD within:
For TURBOJET or TURBOFAN POWERED aeroplane 60% of LDA;
For PROPELLER POWERED aeroplane 70% of LDA

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12
Q

What are the landing distance requirements for wet runway?

A

HOLDER ensures that:
When WEATHER REPORTS or FORECASTS or a COMBINATION indicate at ETA the runway may be wet, LDA is AT LEAST 115% of LDR by D1;
When WEATHER REPORTS or FORECASTS or a COMBINATION indicate at ETA of the runway may be contaminated the LDA is AT LEAST 115% of LDR by D1 OR distance DETERMINED IAW contaminated landing distance DATA;
Landing DISTANCE on WET runway may be SHORTER than REQUIRED by A1 but NOT LESS than REQUIRED by D1, may be USED if DATA SPECIFIES SHORTER DISTANCE on WET runways

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13
Q

What are the requirements for flights over water?

A

HOLDER must ensure EXTENDED over WATER OPERATIONS are EQUIPPED with sufficient LIFE RAFTS with BUOYANCY and OVERLOAD CAPACITY to accommodate EVERY OCCUPANT in the event of a LOSS of 1 LIFE RAFT of LARGEST rated CAPACITY

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14
Q

What additional emergency equipment is required compared to 125?
When is this required?

A

HOLDER must ensure flights MORE than 120 MINUTES DURATION are EQUIPPED with EMERGENCY MEDICAL KIT suitable for use by QUALIFIED MEDICAL PERSONNEL

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15
Q

What are the requirements for a GPWS?

A

A HOLDER must ensure that each TURBINE POWERED aeroplane is EQUIPPED with GPWS;
NOT REQUIRED to comply if aeroplane is EQUIPPED with TAWS CLASS A

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16
Q

What are the requirements for a TAWS?

A

A HOLDER must ensure that each TURBINE POWERED aeroplane manufactured AFTER APRIL 2002 is EQUIPPED with TAWS CLASS A;
A HOLDER must ensure that each PISTON POWERED aeroplane is EQUIPPED with TAWS CLASS B

17
Q

What are the requirements of a maintenance review?

A

HOLDER must ensure:
Aeroplane NOT operated UNLESS a MAINTENANCE REVIEW has been carried out within PREVIOUS 12 MONTHS;
Each MAINTENANCE REVIEW is carried out by a Part 145 APPROVED personnel;
A MAINTENANCE REVIEW is NOT CERTIFIED as having been carried out UNLESS, since the last maintenance review:
Due maintenance SPECIFIED in maintenance PROGRAMME has been COMPLETED within TIME PERIOD specified;
Every applicable AIRWORTHINESS DIRECTIVE has been COMPLIED with IAW REQUIREMENTS in Part 39;
Every DEFECT entered in TECH LOG has been RECTIFIED or PROPERLY DEFERRED IAW procedures in EXPOSITION;
Every applicable CERTIFICATION for RELEASE-TO-SERVICE has been made IAW Part 43

18
Q

What are the minimum flight attendants requirements?

A

HOLDER must ensure NOT operated UNLESS MINIMUM number of FA carried as CREW members:
Is as SPECIFIED by MANUFACTURERS recommended EMERGENCY EVACUATION procedures for aeroplane configuration used;
Is as SPECIFIED by CERTIFIED DESIGN CRITERIA of aeroplane;
Will ensure AT LEAST 1 FA is present in each OCCUPIED COMPARTMENT;
Is IAW MINIMUM number in table below
15 - 50 = 1
51 - 100 = 2
101 - 150 = 3
151 - 200 = 4
201 - 250 = 6
251 -300 = 7
301 - 350 = 9
351 - 400 = 10
401 - 450 = 11
451 - 500 = 12
MORE than 500 = 12 PLUS 1 for every ADDITIONAL 50 PAX or COMPONENT if 50 PAX in EXCESS of 500

19
Q

What are the requirements for flight attendant designation?

A

HOLDER must designate:
For each operation REQUIRING 2 or MORE FA, a SENIOR FA responsible to PIC for OPERATIONAL and SAFETY functions of each FA;
For each operation REQUIRING 6 or MORE FA, a DEPUTY SENIOR FA

20
Q

Can the minimum amount of flight attendants change?

What must the circumstances be?

A

Number of FA by TABLE may be REDUCED by 1 to allow operation to continue if FA becomes UNFIT because of SICKNESS or INJURY during DUTY PERIOD if:
REQUIREMENTS before TABLE are met;
Remaining FA are TRAINED and COMPETENT to operate SAFELY with 1 LESS FA IAW procedures in EXPOSITION;
A FA meeting FA experience REQUIREMENTS is AVAILABLE to REPLACE unfit FA at FIRST AERODROME or landing