AIRBUS

Customer Acceptance Test Report • H145
SIM
1 · General
2 · Init Chk
3 · EPC
4 · Systems
5 · Flt Report
Personnel
Flight Info
Weather
Weight Data & Remarks
Configuration
Signatures

Test Pilot

Customer Pilot

Preflight Checks
Subject / Test Requirement Result Requirement
Exterior Check Acc. Flight Manual
COMPLETE
Interior Check Acc. Flight Manual
COMPLETE
Check "Power Up Test"
PWR-UP TST OK
Check HC Controls (H145 Only)
FREE MOVEMENT
After Startup Tests
Subject / Test Requirement Result Requirement
After Both Engines Running
START-UP TST OK
Nav and Radios
AVIONIC MASTER ON
AFCS / Avionics Self Test Acc. Flight Manual
P-FLT TST OK
Qualitative Assessment of AFCS & GNSS Approach
Subject / Test Requirement Result Requirement
Basic Modes
SATISFACTORY
Upper Modes
SATISFACTORY
Backup SAS
SATISFACTORY
GPS Approach IAS = 120kt Engaged (if weather permits)
SATISFACTORY
Level Flight Data at 2×70% TRQ (H145)
ZP
[ft] OAT
[°C] Pilot IAS
[kt] Gross Mass
[kg] Endurance
[HH:MN] IAS Red.
[kt]
Automatic Inflight Power Check
ENG 1ENG 2
N1 [%]
TOT [°C]
TRQ ISO-TOT
TRQ ISO-N1
TOT AND/OR N1 MARGIN ENG1 MARGIN > 0%
TOT AND/OR N1 MARGIN ENG2 MARGIN > 0%
Final Functional Checks

Brief functional check of the following items if installed

Subject / Test Requirement Result Requirement
Ventilation System Incl. Cabin Outlets
Heating System Incl. Cabin Outlets
IBF Check On/Off Indication for Both Systems
Internal Lighting
VHF Radios
DMAP
WXR
HTAWS
TCAS
Rear Camera
After Landing Check
Rotor Braking
Subject / Test Requirement Result Requirement
Apply Rotor Brake at 50% NRO
SEC
H145 ≤ 50 SEC
Verify Flight Report
Block Time:
h mn
Flight Time:
h mn
Landings (Local Reference)
Engine Cycles
CUM — ENG 1 Cycles CUM — ENG 2
N1
N2
Creep Life (H145 Only)
CUM — ENG 1 Creep Life CUM — ENG 2