Airworthiness Review Checklist - Aircraft Survey Copy

Information

Airworthiness Review Check-list – Aircraft Survey.
VAA-ENG-114-CAME-6 AR Checklist.
AIRCRAFT Registration -
Aircraft Model-
Aircraft Serial-
Aircraft Line Number -
Conducted on
Prepared by
Location
Personnel

Aircraft Configuration Check

Configuration:

Configuration of the aircraft for the aircraft survey should consist of the following: - Engine Fan Cowls Open - APU Bay Doors Open and stand positioned for access - Cargo Bay Doors Open and stands positioned for access - Refuelling Panel Open - Power applied to aircraft - Interior Lighting On - Flaps and Slats extended (optional)

Aircraft Markings and Placards Audit

Markings and Placards (CASR 42.900(3)3

Markings (CASR 42.900(3)) Markings that are required, by or under CASA Regulations or by the aircraft’s type certification basis to be on the aircraft: -are correct; and -are in the correct position on the aircraft References – Aircraft TCDS / CASR Part 90 / CASR Part 45 / Aircraft AMM - IPC.
Do you want to expand and use the (CASR 45 Aircraft Registration Requirements) checklist?
45.040; Markings not to be obscured
45.045; Number and location of sets of markings — fixed-wing aircraft.
45.045(1); On a fixed-wing aircraft, 3 sets of the aircraft’s markings must be displayed, as follows:
45.045(1)(a); 1 set either on the under surface of the port wing or across the under surface of both wings, in each case as set out in subregulation (2);
45.045(2); A marking on the wing of an aircraft:
45.045(2)(a); must have its top towards the leading edge of the wing; and
45.045(2)(b); must be as nearly as possible parallel to the leading edge, and half way between the leading and the trailing edge, of the wing.
45.045(1)(b); the 2 other sets on:
45.045(1)(b)(i); the fuselage, as set out in subregulation (3);
45.045(3); If the markings are on the aircraft’s fuselage, there must be 1 set on each side of the fuselage:
45.045(3)(a); between the trailing edge of the wing and the leading edge of the tailplane;
45.065; Minimum height of characters:
for markings on other parts of the aircraft — 300 mm;
for markings on the aircraft’s wings — 500 mm;
45.070; Minimum width of characters.
45.070(1); The width of a character must be equal to 2/3 of its height, with the following exceptions:
45.070(1)(a); the letter ‘I’ and the digit ‘1’, whose width must be equal to 1/6 th of their height;
45.070(1)(b); the letters ‘M’ and ‘W’, whose width may be equal to their height.
45.070(2); A character must be made up of solid lines that are 1/6 th as thick as the character is high.
45.075; Size of hyphens.
45-075(1); A hyphen in a set of markings must be 1/6 th of the height of the characters in the set.
45-075(2); The width of a hyphen must be equal to 4 times its height.
45.080; Minimum spacing of characters.
45.080(1); The space between any 2 adjacent characters must be at least 1/6 th of their height.
45.080(2); The space between a hyphen and a character must be at least 1/6 th of the height of the character.
45.085; How markings to be marked on aircraft.
45.085(1); An Australian aircraft’s markings must be painted on it, or fixed to it in some other way that is at least as permanent as painting.
45.085(2); The markings:
45.085(2)(a); must be legible; and
45.085(2)(b); must have no ornamentation; and
45.085(2)(c); must be of a colour that clearly contrasts with their background.
45.090; No confusing markings to be on aircraft.
45.090(1); Subject to subregulation (3), a person must not, without the written approval of CASA, place on an Australian aircraft a design, mark or symbol that modifies, or creates confusion about, the marks displayed on the aircraft as its markings.
45.150; How and where aircraft registration identification plate is to be attached to aircraft (refer to 45.140 for description of registration ID plate) - Check that the registered owner on the ownership plate agrees with the registered owner on the respective Registration Certificate.
45.150(1); An aircraft’s registration identification plate must be attached to it in a way that ensures that the plate is not likely to be defaced or to become detached from the aircraft.
45.150(2); The plate must be attached:
45.150(2)(c)(i); near the aircraft’s entrance or main entrance; and
45.150(2)(c)(ii); where it is clearly visible.
Placards (CASR 42.900(3)) Placards that are required, by or under CASA Regulations or by the aircraft’s type certification basis, to be fitted to the aircraft are correctly fitted. References – Aircraft TCDS / CASR Part 90 / Aircraft AMM - IPC.
Do you want to expand and use the (CASR 90 Placard) checklist?
90.130(3); External Doors - The information on the doors must be clearly marked both internal and external as per (4) (a), (b) & (c).
90.130(4); External Doors - Door handle Instructions (Check the signs needed for the aircraft are in place, their location, legibility and suitable contrast)
90.130(4)(a); the location of the handle;
90.130(4)(b); the operating instructions for the handle; and
90.130(4)(c); the position of the handle when the door is properly locked, or another way of showing when the door is properly locked.
90.135(3); Emergency Exits - Each emergency exit/entrance door to be marked so a seated passenger can see the location of the nearest exit – ie, meets Type Design/AR Support Docs refer.
90.135(4); Emergency Exits - Each passenger compartment must have a sign showing the way to an Emergency exit that is not located in the passenger compartment – ie, meets Type Design/AR Support Docs refer.
90.135(5); Emergency Exits - Instructions showing how to open the exit must be located inside and outside of Emergency Exit (if able to be open from the outside)
90.135(6)(a); Emergency Exits - each emergency exit sign and the instructions for operating each emergency exit must be provided with lighting so that if the cabin is in darkness and the cabin lighting is not operating, the sign and instructions can be read by a person attempting to open the emergency exit.
90.220(1)(b); Emergency Exits Interior markings.
26; Passenger emergency exit marking and locating signs
26.1; Each passenger emergency exit and its means of access must be conspicuously marked on the interior of the aeroplane.
26.2; The marking to identify and locate each passenger emergency exit must be recognisable from a distance equal to the width of the cabin.
26.3; Each passenger emergency exit and access to it must be marked in a way that enables the occupants to locate the exit even if there is dense smoke in the cabin.
26.4; Each passenger emergency exit must be indicated by locating signs that are visible to occupants approaching along the main passenger aisle or aisles, so that there is a sign:
(a); either:
(i); above the aisle or aisles near each passenger emergency exit; or
(ii); if low headroom makes this impracticable — at another overhead location; and
(b); next to each passenger emergency exit; and
(c); if a bulkhead or divider prevents fore and aft vision along the passenger cabin, either:
(i); on each such bulkhead or divider, indicating that emergency exits are beyond the bulkhead or divider; or
(ii); if this is not possible — to the same effect at another appropriate location
26.5; For paragraphs 26.4(a) and (b), 1 sign may serve more than 1 exit if the sign is such that each exit can be easily identified and readily seen because of the sign.
28; Filed on, or after, 1 May 1972 — emergency exit marking and locating sign – transport category
28.1; If the application for the type certificate for a transport category aeroplane was filed on, or after, 1 May 1972, each passenger emergency exit marking and each locating sign must be manufactured to meet the interior emergency exit marking requirements under which the aircraft was type certificated.
28.2; A sign must not be continued in use if its brightness decreases below 0.8 cd/m². Refer TCDS A16WE meets FAR 25.812(b)(1)(i)
31; Emergency exit operating handle marking, illumination and instructions
31.1; For each passenger emergency exit, the following must be conspicuously marked on the interior of the aeroplane:
(a); the location of the operating handle for the exit; and
(b); the opening instructions for the handle, including, if covered, the handle-cover removal instructions.
31.2; The marking must be:
(a); on, or near, each passenger emergency exit; and
(b); readable from a distance of 762 mm.
31.3; Each passenger emergency exit operating handle must be:
(a); self-illuminated with a minimum brightness
(b); conspicuously located and illuminated by the aeroplane’s emergency lighting including in conditions of occupant crowding at the exit.
31.4; If the application for the type certificate for a transport category aeroplane was filed before 1 May 1972, for each Type II or larger passenger emergency exit with a locking mechanism released by rotary motion of a handle, the instructions for opening must be shown by:
(a); a red arrow with a shaft at least 19 mm wide and a head twice the width of the shaft, extending along at least 70 degrees of arc at a radius approximately equal to three quarters of the handle length; and
(b); the word OPEN in red capital letters at least 25 mm high on a contrasting background placed horizontally adjacent to the arrowhead to show the open position of the handle.
90.235; Exterior Emergency Exit Marking.
40; Exterior emergency exit marking — requirements
40.1; The following must be clearly marked on the outside of the aeroplane for each emergency exit that is capable of being opened from the outside in accordance with this Subdivision:
(a); the external means of opening the emergency exit; and
(b); on the side of the fuselage or on the exit itself — a 50 mm coloured band highlighting the exit.
40.2; Each marking, including the coloured band, must have colour contrast that readily distinguishes it from the surrounding fuselage surface.
40.3; For subsection 40.2, the contrast must be as follows:
(a); if the reflectance of the darker colour is 15% or less, the reflectance of the lighter colour must be at least 45%;
(b); if the reflectance of the darker colour is greater than 15%, there must be at least a 30% difference between the reflectance of the darker colour and the reflectance of the lighter colour.
90.270(2); Toilets - Both sides of the door of each toilet in the aeroplane must have, installed above the door knob or near the door, a placard showing.
90.270(2)(a); the words ‘NO SMOKING IN TOILET’ or ‘NO SMOKING’; or
90.270(2)(b); a symbol with the same meaning.
2.4; Cockpit door - Check that the door is in serviceable condition, with legible placards and that the locking mechanism is working.
5.10; Overhead Lockers - Check that the maximum weight signs are in place and their condition.
Flight Attendant Seats
1. Placards/Decals - Check that placards and fdecals are in place, their applicability to the aircraft, location, legibility and respective condition.
2. Placards/Decals - Check that placards and fdecals are in place, their applicability to the aircraft, location, legibility and respective condition.
3. Placards/Decals - Check that placards and fdecals are in place, their applicability to the aircraft, location, legibility and respective condition.
Toilets.
No smoking inside or outside the Toilets - Check that suitable signs are in place and correct operation (as applicable)
Toilet No 1
Toilet No 2
Toilet No 3
"Return to your seat" light in the Toilet and call button – Check operability
Toilet No 1
Toilet No 2
Toilet No 3
Placards/Decals – Check the placards and decals are in place and legible
Toilet No 1
Toilet No 2
Toilet No 3
Galley Placards/Decals –
- Check that the maximum weight placards/decals are in the respective compartments.
- Check that there are placards/decals in place noting passengers doors, tables and other items must be closed during take-off and landing
Forward
Aft

Aircraft External Audit

External Aircraft

Nose Landing Gear / Wheel Well Ensure Landing Gear data plate and aircraft records align. Inspect Nose Landing Gear and Wheel Well area paying attention to any obvious damage / leaks.
Do you want to expand and use the (CASR 45 Part 90 – External Aircraft Requirements) checklist?
Nose Landing Gear / Wheel Well
14.1 Check its general condition – - Check that it is clean enough to allow correct inspection - Check for damage, signs of corrosion, and the condition and suitability of placards/decals
14.2 Wheel well and doors - Check the blocking mechanism, proximity detectors, metalwork, gaps and painting.
14.3 Wheel rims - Check for damage, clamping of the nuts, state of the air-filling valve and temperature fuses ?
14.4 Tyres - Check for wear and tear, cuts and punctures.
14.5 Hydraulic tubes and cabling - Check that they are properly clamped and are complete.
14.6 Lubrication - Check for the correct lubrication.
14.7 Fluid leaks – Check for hydraulic fluid leaks.
14.8 Shock absorber (Oleo) - Check the condition of the shock absorber in relation to the correct extension and any leaks 50 cm ext.
E/E Bay Inspect E/E Bay area paying attention to any obvious damage.
Do you want to expand and use the (CASR 45 Part 90 – External Aircraft Requirements) checklist?
E&E Bays
8.1 Electronic equipment - Check the respective clamping and if there is any damage.
8.2 Command cables – - Check for wear and tear and corrosion - Check terminals and routing of the cables in pulleys or quadrants
8.3 Access doors - Check their general condition and that the lock mechanism is working
8.4 Visible electric cabling - Check the clamping and any friction or wear in the structure of the components.
Forward Cargo Bay Inspect Forward Cargo Bay paying particular attention to obvious damage. Ensure compliance to any parts of CASR Part 90 that affect the Forward Cargo Bay. References – CASR Part 90 / Aircraft AMM.
Do you want to expand and use the (CASR 45 Part 90 – External Aircraft Requirements) checklist?
Cargo Holds
9.1 General condition - Check the side panels, ceiling of the hold and depressurisation panels, especially their capacity to contain fire.
9.2 Structural damage - Check for internal structural damage in the hold.
9.3 Fire detection and extinguishing - Check that the fire detectors for general condition and that the respective evacuation exits are not obstructed.
9.4 Cargo transport and retention system: - Check the operation of the cargo system (where installed – AMO assistance will be required) - Check the cargo nets as regards their correct clamping and condition
9.5 Ceiling lights - Check the operation of the hold light system.
9.6 Placards/Decals linked to the operation of the hold door - Check that all the signs related to the operation of the cargo hold door are in place, legible and suitable and correct operation (as applicable)
9.7 Weight limit and pallet position Placards/Decals - Check that all the internal placards/decals related to the cargo position are in place, legible and suitable.
9.8 Cargo door – - Check that the door works properly and for hydraulic leaks next to the drivers or in the valve selection panel - Check for damage on the door seal, door block indicators/visors and damage in the respective frame
90.140(2)(a); Cargo and Baggage compartment lighting must be protected against the possibility of accidental damage
90.140(2)(b); Cargo and Baggage compartment lighting must be insulated so baggage placed adjacent to the lamp is not subject to excessive heat
Right Hand Engine Ensure engine data plate and aircraft records align. Inspect area paying attention to obvious damage / leaks.
Do you want to expand and use the (CASR 45 Part 90 – External Aircraft Requirements) checklist?
Engine/Pylon
16.1 Condition of the hinges and clamps of the access doors - Check for damage, signs of corrosion, loose or missing screws, and the condition and suitability of placards/decals.
16.2 Condition of the air inlet - Check for damage, signs of corrosion and loose or missing screws
16.3 Sensors – Check for damage and obstructions.
16.4 Structural damage/repairs - Check on the list of repairs made for control and record of dents and damage, and the completeness of the repairs made.
16.5 Condition of Spinner and Fan blades – Check for damage and completeness of blendings (to match with approved data)
16.6 Condition of the thrust reverser and exhaust pipe - Check for damage, signs of corrosion, missing or damaged parts, repairs carried out, condition and suitability of placards/decals.
16.7 Condition of drains - Check for damage, obstruction and condition of placards/decals.
16.8 Fluid leaks - Check for hydraulic fluid or fuel leaks
16.9 Identification - Check the identification and ownership plates with regard to their availability, installation and the information complying with the respective documentation.
Right Hand Wing Inspect area paying attention to obvious damage / leaks. Ensure compliance to any parts of CASR Part 90 that affect the RH Wing area. References – CASR Part 90 / Aircraft AMM.
Do you want to expand and use the (CASR 45 Part 90 – External Aircraft Requirements) checklist?
Wings
12.1 General condition - Check for damage, cracks, signs of corrosion, state of repairs and any parts missing or damaged.
12.2 Flaps - Check for damage, cracks, signs of corrosion, state of repairs and any parts missing or damaged (device in extended position)
12.3 Slats - Check for damage, cracks, signs of corrosion, state of repairs and any parts missing or damaged (device in extended position)
12.4 Spoilers - Check for damage, cracks, signs of corrosion, state of repairs and any parts missing or damaged (device in extended position)
12.5 Fluid leaks – Check for hydraulic fluid or fuel leaks.
12.6 Static dischargers – Check that they are present, for general condition and at the respective location.
Right Hand Main Landing Gear / Wheel Well Ensure Landing Gear data plate and aircraft records align. Inspect RH Main Landing Gear and Wheel Well area paying attention to any obvious damage / leaks.
Do you want to expand and use the (CASR 45 Part 90 – External Aircraft Requirements) checklist?
Main Gears
15.1 Check its general condition – - Check that it is clean enough to allow correct inspection - Check for damage, signs of corrosion, and the condition and suitability of placards/decals
15.2 Wheel well and doors - Check the blocking mechanism, proximity detectors, metalwork, gaps and painting.
15.3 Wheel rims - Check for damage, clamping of the nuts, state of the air-filling valve and temperature fuses.
15.4 Tyres - Check for wear and tear, cuts and punctures.
15.5 Hydraulic tubes and cabling - Check that they are properly clamped and are complete.
15.6 Lubrication - Check for the correct lubrication.
15.7 Fluid leaks – Check for hydraulic fluid leaks.
15.8 Shock absorber (Oleo) - Check the condition of the shock absorber in relation to the correct extension and any leaks LH 6.5cm RH 7cm ext.
15.9 Brakes – Check for wear, tear and fractures.
AFT Cargo Bay Inspect AFT Cargo Bay paying particular attention to obvious damage. Ensure compliance to any parts of CASR Part 90 that affect the AFT Cargo Bay. References – CASR Part 90 / Aircraft AMM.
Do you want to expand and use the (CASR 45 Part 90 – External Aircraft Requirements) checklist?
Cargo Holds
9.1 General condition - Check the side panels, ceiling of the hold and depressurisation panels, especially their capacity to contain fire.
9.2 Structural damage - Check for internal structural damage in the hold.
9.3 Fire detection and extinguishing - Check that the fire detectors for general condition and that the respective evacuation exits are not obstructed.
9.4 Cargo transport and retention system - Check the operation of the cargo system (where installed – AMO assistance will be required) - Check the cargo nets as regards their correct clamping and condition
9.5 Ceiling lights - Check the operation of the hold light system.
9.6 Placards/Decals linked to the operation of the hold door - Check that all the signs related to the operation of the cargo hold door are in place, legible and suitable and correct operation (as applicable)
9.7 Weight limit and pallet position Placards/Decals - Check that all the internal placards/decals related to the cargo position are in place, legible and suitable.
9.8 Cargo door – - Check that the door works properly and for hydraulic leaks next to the drivers or in the valve selection panel - Check for damage on the door seal, door block indicators/visors and damage in the respective frame
90.140(2)(a) Cargo and Baggage compartment lighting must be protected against the possibility of accidental damage
90.140(2)(b) Cargo and Baggage compartment lighting must be insulated so baggage placed adjacent to the lamp is not subject to excessive heat
APU Ensure APU data plate and aircraft records align. Inspect area paying attention to obvious damage / leaks.
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APU
17.1 Check its general condition – - Check that it is clean enough to allow correct inspection - Check for damage, signs of corrosion, and the condition of placards/decals
17.2 Condition of the air inlet - Check for damage, corrosion and loose or missing screws.
17.3 Condition of the exhaust pipe - Check for damage, signs of corrosion, missing or damaged parts, repairs carried out and condition.
17.4 Condition of drains - Check for damage, obstruction and condition.
17.5 Fluid leaks - Check for fuel leaks.
Empennage
13.1 LH horizontal stabiliser - Check for damage, cracks, signs of corrosion, completeness of repairs and any parts missing or damaged
13.2 LH elevator - Check for damage, cracks, signs of corrosion, completeness of repairs and any parts missing or damaged.
13.3 RH horizontal stabiliser - Check for damage, cracks, signs of corrosion, completeness of repairs and any parts missing or damaged.
13.4 RH elevator - Check for damage, cracks, signs of corrosion, completeness of repairs and any parts missing or damaged.
13.5 Vertical stabiliser - Check for damage, cracks, signs of corrosion, completeness of repairs and any parts missing or damaged.
13.6 Rudder - Check for damage, cracks, signs of corrosion, completeness of repairs and any parts missing or damaged
13.7 Fluid leaks – Check for hydraulic fluid leaks.
13.8 Static dischargers – Check that they are present, for general condition and at the respective location (GVI from ground level).
Left Hand Main Landing Gear / Wheel Well Ensure Landing Gear data plate and aircraft records align. Inspect LH Main Landing Gear and Wheel Well area paying attention to any obvious damage / leaks.
Do you want to expand and use the (CASR 45 Part 90 – External Aircraft Requirements) checklist?
Main Gears
15.1 Check its general condition – - Check that it is clean enough to allow correct inspection - Check for damage, signs of corrosion, and the condition and suitability of placards/decals
15.2 Wheel well and doors - Check the blocking mechanism, proximity detectors, metalwork, gaps and painting.
15.3 Wheel rims - Check for damage, clamping of the nuts, state of the air-filling valve and temperature fuses.
15.4 Tyres - Check for wear and tear, cuts and punctures.
15.5 Hydraulic tubes and cabling - Check that they are properly clamped and are complete.
15.6 Lubrication - Check for the correct lubrication.
15.7 Fluid leaks – Check for hydraulic fluid leaks.
15.8 Shock absorber (Oleo) - Check the condition of the shock absorber in relation to the correct extension and any leaks LH 6.5cm RH 7cm ext.
15.9 Brakes – Check for wear, tear and fractures.
Left Hand Wing Inspect area paying attention to obvious damage / leaks. Ensure compliance to any parts of CASR Part 90 that affect the LH Wing area. References – CASR Part 90 / Aircraft AMM.
Do you want to expand and use the (CASR 45 Part 90 – External Aircraft Requirements) checklist?
Wings
12.1 General condition - Check for damage, cracks, signs of corrosion, state of repairs and any parts missing or damaged.
12.2 Flaps - Check for damage, cracks, signs of corrosion, state of repairs and any parts missing or damaged (device in extended position)
12.3 Slats - Check for damage, cracks, signs of corrosion, state of repairs and any parts missing or damaged (device in extended position)
12.4 Spoilers - Check for damage, cracks, signs of corrosion, state of repairs and any parts missing or damaged (device in extended position)
12.5 Fluid leaks – Check for hydraulic fluid or fuel leaks.
12.6 Static dischargers – Check that they are present, for general condition and at the respective location.
Left Hand Engine Ensure engine data plate and aircraft records align. Inspect area paying attention to obvious damage / leaks.
Do you want to expand and use the (CASR 45 Part 90 – External Aircraft Requirements) checklist?
Engine/Pylon
16.1 Condition of the hinges and clamps of the access doors - Check for damage, signs of corrosion, loose or missing screws, and the condition and suitability of placards/decals.
16.2 Condition of the air inlet - Check for damage, signs of corrosion and loose or missing screws
16.3 Sensors – Check for damage and obstructions.
16.4 Structural damage/repairs - Check on the list of repairs made for control and record of dents and damage, and the completeness of the repairs made.
16.5 Condition of Spinner and Fan blades – Check for damage and completeness of blendings (to match with approved data)
16.6 Condition of the thrust reverser and exhaust pipe - Check for damage, signs of corrosion, missing or damaged parts, repairs carried out, condition and suitability of placards/decals.
16.7 Condition of drains - Check for damage, obstruction and condition of placards/decals.
16.8 Fluid leaks - Check for hydraulic fluid or fuel leaks
16.9 Identification - Check the identification and ownership plates with regard to their availability, installation and the information complying with the respective documentation.
External Aircraft Inspect external part of the aircraft paying particular attention to any obvious damage / leaks. Ensure compliance to any parts of CASR Part 90 that affect the exterior of the aircraft. References – CASR Part 90 / Aircraft AMM.
Do you want to expand and use the (CASR 45 Part 90 – External Aircraft Requirements) checklist?
Fuselage
90.130(2); External Doors - Door to be of a kind that can be opened from both inside and outside – ie, meets Type Design/AR Support Docs refer
10.1 General condition - Check the painting and for any hydraulic and fuel leaks, damaged and/or missing parts, wrinkles or surface alterations.
10.2 Structural damage/repairs - Check on the list of repairs made in the aircraft, control and record of dents and damage, and the completeness of the repairs made.
10.3 Radome - Check the painting, for any damage and the completeness of the electric discharge strips.
10.4 Outdoor lights (taxi, approach, navigation, strobe and beacon) - Check that they are working properly.
10.5 Static Ports - Check that the fuselage surface is unobstructed and in good condition in the critical zones.
10.6 Sensors – Check for damage and obstructions

Aircraft Internal Audit

Aircraft Data Plate Ensure aircraft data plate is installed and aircraft records align.
Aircraft Registration Plate Ensure aircraft registration plate is installed and aircraft records align.
Flight Deck (42.900(3)(e)) Inspect Flight Deck for obvious damage. Ensure correct FCOM inclusive of QRH and CDL is installed to the aircraft. This is in lieu of the AFM as this document is not carried on board by VAA. References – CASR Part 90 / Aircraft AMM / Emergency Equipment Drawing.
Do you want to expand and use the (CASR 45 Part 90 – Internal Aircraft Requirements) checklist?
Cockpit
90.285 (3) Pitot Heat Indication Systems - The aeroplane must have an indication system to indicate to the flight crew if the flight instrument pitot heating system is not operating. Check probe condition, non-obstruction and heating operability.
90.285 (4) The indication system must comply with the following requirements:
(a) the indication system must incorporate an amber light that is in clear view of a flight crew member;
(b) the indication system must be designed to alert the flight crew if either of the following conditions exists: -
(i) the flight instrument pitot heating system is switched off – ie, meets Type Design/AR Support Docs refer;
(ii) the flight instrument pitot heating system is switched on and any pitot tube heating element is inoperative – ie, meets Type Design/AR Support Docs refer
2.1 Circuit Breaker - Check if there are any intentional deactivations and the respective document support. 6 inop collared
2.2 Compass Calibration - Check that the calibration label has been affixed confirming the calibration intervals in compliance with the applicable requirements Last Swing Record:
2.5 Emergency exits (removable windows or hatches) - Check that they are working properly and it is possible to access them.
2.6 Emergency exit ropes - Check that they are properly clamped and in serviceable condition.
2.7 Minimum Equipment List - Check that the MEL/DDG manual is in good order, properly stored, up to date and duly applicable.
2.8 Validate emergency equipment list - Check the quantity, validity, location, storage and clamping, when necessary, of all the emergency equipment in line with the emergency equipment list. Record LOPA / Emergency Equip drawing used for inspection and retain copy with check sheets.
2.10 Axe - Check the respective condition and clamping.
2.11 Windows/Windscreens - Check that there are no cracks or delamination outside the limits and zones with signs of overheating and blockages to visibility.
2.12 Windscreen wipers – Check the general visual condition for serviceability.
2.13 On-board Certificates – Check that any on-board certificates are up to date:- CofA, CofR, Radio Licence.
Passenger Cabin Ensure Passenger Lay out and Emergency Equipment is as per approved documentation. Ensure compliance to any parts of CASR Part 90 that affect the passenger cabin of the aircraft. Inspect Passenger Cabin for obvious damage. Ensure PA systems and Megaphones operate correctly. Ensure the Emergency Lighting System operates correctly. References – CASR Part 90 / Aircraft AMM / LOPA / Emergency Equipment Drawing.
Do you want to expand and use the (CASR 45 Part 90 – Internal Aircraft Requirements) checklist?
Passenger Cabin
90.105(2); Flight Crew Restraints - Large Aircraft Certified on or after 1 Jan 1958 require, for each seat in Flight Compartment, an approved symmetrical type harness or a single shoulder strap harness that was approved and installed before 6 March 1980. The safety harness must:
90.105 (b) (i)&(ii); when not in use, be able to be secured so it does not: prevent the proper operation of the aircraft or hinder a person in the aircraft if he or she must leave the aircraft in an emergency
90.125(1)(b); Cabin Crew Seats
4; Cabin crew seats:- A cabin crew member’s seat must:
(a); be located in the passenger cabin near prescribed floor level emergency exits; and
(b); provide a direct view of the cabin area for which the cabin crew member is individually responsible; and
(c); be facing forward or rearward, and have an energy absorbing rest that is designed to support the arms, shoulders, head, and spine of the occupant; and
(d); be designed and positioned so that when not in use it will not interfere with the use of passageways and exits; and
(e); be located to minimise the probability of the occupant suffering injury from being struck by any item that is likely to be used in, and capable of being dislodged from, a galley, stowage compartment or serving cart; and
(f); be equipped with a restraint system that:
(i); consists of a combined safety belt and symmetric shoulder harness unit with a single point release; and
(ii); is capable of being safely secured when not in use to prevent interference with rapid egress in an emergency; and
(iii); is designed to the inertia load factors established under the certification basis of the aircraft
5; Cabin crew seats — alternative standards
5.1; In spite of paragraph 4 (b), for an aeroplane with a certification basis before FAR 25.785 as in force on 6 March 1980, or equivalent, the cabin crew member seats need not be relocated to meet the requirement of paragraph 4 (b), if a mirror gives an indirect view of the cabin area to the relevant cabin crew member
90.130(2); External Doors - Door to be of a kind that can be opened from both inside and outside – ie, meets Type Design/AR Support Docs refer ?
CASR90.410(2)(b); Emergency exits — Requirements
63.2; Each emergency exit from the aeroplane must be identified by an approved sign that:
(a) shows:
(i) the word “EXIT” in white letters 25 mm high on a red background 50 mm high, or in red letters 25 mm high on a white background 50 mm high; or
(ii) a universal exit symbol complying with the means of compliance set out in EASA AMC 25.812 (b) (1) and (2) as in force 19 September 2007; and
(b) is self-illuminated or electrically illuminated independently of the normal cabin lighting system; and
(c) has a luminance of at least 0.5 cd/m² at all times
90.135(2); Emergency Exits - Each passenger and crew member must have unobstructed access to at least 1 emergency exit.
90.205; Escape Devices - If: the aeroplane has an emergency exit higher than 1.83 m above the ground when the L/G is extended; and is not over the wing; the aeroplane must be equipped with an escape device to help passengers and members of the crew reach the ground.
90.205(3); Escape devices
10; Escape devices — requirements
10.1; For an aeroplane whose type certificate application was filed before 1 May 1972 — the escape device for a passenger emergency exit must be a self-supporting slide, or equivalent, designed so that:
(a); subject to subsection 10.2, it automatically:
(i); deploys simultaneously with the opening of the exit; and
(ii); erects within 10 seconds; and
(b); its lower end is self-supporting on the ground, including if 1 or more of the landing gear legs collapses.
10.2; For paragraph 10.1 (a), if the escape device is installed at a service door, or passenger door that qualifies as an emergency exit, means must be provided to prevent automatic deployment of the device when the door is opened from the inside or the outside of the aeroplane in non-emergency conditions.
10.3; For an aeroplane whose type certificate application was filed before 1 May 1972 — the escape device for the flight crew emergency exit must be a rope or other equivalent device, demonstrably suitable for the purpose, that is:
(a); able with its attachment to withstand a static load of 181.6 kg; and
(b); either:
(i); attached to the fuselage structure at, or above, the top of the emergency exit opening; or
(ii); for a device at a pilot’s emergency exit window — at another approved location if the stowed device or its attachment would otherwise reduce the pilot’s view in flight
90.215(1)(b); Access to Emergency Exits.
14; Passageways— Type I and Type II exits
14.1; Each passageway between individual passenger areas, or leading to a Type I or Type II emergency exit, must be:
(a); at least 508 mm wide; and
(b); unobstructed.
14.2; There must be enough space around each Type I or Type II emergency exit to allow a crew member to assist in the evacuation of passengers without reducing the unobstructed width of the passageway to below 508 mm:
15; Passageways— Type III and Type IV exits There must be access from the main aisle to each Type III or Type IV emergency exit and this access must not be obstructed by seats, berths, or other protrusions in a manner that would reduce the effectiveness of the exit.
21; Filed on, or after, 3 June 1992 — emergency exit access For an aeroplane:
(a); whose type certificate application was filed on, or after, 3 June 1992; or
(b); whose certification basis includes FAR 25.813 as in force on, or after, 3 June 1992; access to each emergency exit must meet the emergency exit access requirements under which the aeroplane was certificated
23; Passenger compartment obstructions, curtains and doorways
23.2; If, to reach an emergency exit from a seat in the passenger cabin, it is necessary to pass through a passageway between passenger compartments, the passageway must be unobstructed
23.3; For subsection 23.2, curtains are an obstruction unless they allow free and unimpeded passage through the passageway.
23.4; A door must not be installed in any partition between passenger compartments.
23.5; If, to reach an emergency exit from a seat in the passenger cabin, it is necessary to pass through a doorway separating the passenger cabin from other areas of the aeroplane, the door must have a means to latch it open.
23.6; For subsection 23.5, the means of latching must be able to withstand the loads imposed upon it when the door is subjected to the ultimate inertia forces relative to the surrounding structure, as prescribed in FAR 25.561 (b) or equivalent, as in force on the date specified in the aeroplane’s type certificate data sheet or equivalent document.
90.225(1)(b); Interior Emergency Lighting
34; Interior emergency lighting system — requirements
34.1; Subject to subsection 34.2, the aeroplane must have an interior emergency lighting system, including power supply, that is independent of the aeroplane’s main lighting system and its power supply.
34.2; Without otherwise affecting subsection 34.1, the sources of general cabin illumination may be common to both the interior emergency lighting and the main lighting system.
34.3; The interior emergency lighting system must include the following:
(a); illuminated emergency exit markings;
(b); illuminated emergency exit locating signs;
(c); interior lighting in emergency exit areas;
(d); sources of general cabin illumination
36; Interior emergency lighting system — further requirements
For this Subdivision, subject to section 37, the interior emergency lighting system must:
(a); be controlled manually from the flight crew station with a cockpit control device that has an “on”, “off”, and “armed” position (the cockpit station); and
(b); for aeroplanes on which a cabin crew member is required — be controlled manually from both of the following:
(i); the cockpit station;
(ii); a point in the passenger compartment readily accessible from a normal cabin crew member’s seat (the cabin crew station); and
(c); be designed to prevent inadvertent operation of the manual controls; and
(d); when turned on at either the cockpit station or the cabin crew station — ensure that the interior emergency lighting remains on in the event of interruption of the aeroplane’s normal electric power; and
(e); when armed at the cockpit station — ensure that the interior emergency lighting comes on in the event of interruption of the aeroplane’s normal electric power; and
(f); provide the level of illumination required under this MOS for at least 10 minutes at the critical ambient conditions after an emergency landing.
37; Interior emergency lighting system — if cannot be switched off An interior emergency lighting system that is designed to be continuously on and cannot be switched off need not meet the requirements in paragraphs 36 (a) to (e), but must meet the requirement in paragraph 36 (f). Note Photoluminescent and radioluminescent light sources are examples of lighting systems that cannot be turned off.
90.230(2)(b); Floor Proximity Emergency Escape Path.
35; Type certificated on, or after, 1 January 1958— floor proximity emergency escape path marking
35.1; For a large aeroplane that was type certificated after 1 January 1958, the interior emergency lighting system must include floor proximity emergency escape path marking (FPEEPM):
(a); on, and from, 1 December 2010 — for an aeroplane that has a passenger seating configuration of 31 or more; and
(b); on, and from, 1 March 2012 — for an aeroplane that has a passenger seating configuration of 20 or more.
35.2; The FPEEPM must provide emergency evacuation guidance for passengers when all sources of illumination more than 1.22 m above the cabin aisle floor are totally obscured.
35.3; In darkness equivalent to the dark of night, the FPEEPM must enable each passenger:
(a); after leaving his or her seat — to visually identify the emergency escape path along the cabin aisle floor to the first exit, or pair of exits, forward and aft of the seat; and
(b); to readily distinguish each exit from the emergency escape path by reference to markings and visual features that are not more than 1.22 m above the cabin aisle floor.
90.240; Exterior Emergency Lighting - an over-wing exit on the aeroplane, or an escape device fitted for regulation 90.205, must be fitted with an exterior emergency lighting system that meets the standard for exterior emergency lighting set out in the Part 90 MOS.
90.245; Over Wing Escape Route - an over-wing emergency exit on the aeroplane must have an over-wing escape route
90.270(3); Toilets - Each toilet in an aeroplane that has 31 or more passenger seats must be equipped with:
90.270(3)(a); An unobstructed smoke detector that gives a warning signal that can be seen or heard by a flight crew member or cabin crew member; and
90.270(3)(b); 1 or more built-in fire extinguishers that will, in the event of a fire in a waste receptacle in the toilet, discharge into the receptacle – ie, meets Type Design/AR Support Docs refer
5.5 Cabin communication and emergency lighting - Check the operation of the cabin communication system and emergency lighting
5.6 Cabin lighting - Check that the lighting is working properly.
5.8 Indoor and outdoor emergency lighting – Check operability (including floor path escape lighting)
Configuration (42.900(3)(c)) Ensure the configuration of the aircraft complies with the aircraft approved design.
Defects (42.900(3)(d)) Ensure any defect apparent to the ARE is correctly recorded in the aircraft’s maintenance log system.
Condition of Aircraft (42.900(3)(f)) Ensure the condition of the aircraft is consistent with the aircraft’s maintenance log system.