No.
3868-S-20
             SAFETY INFORMATION NOTICE
SUBJECT: STANDARD PRACTICES
                  De-icing and anti-icing products
  For the attention of
   AIRCRAFT                                                              Version(s)
  CONCERNED                                  Civil                                                     Military
     EC120                                     B
     AS350                         B, BA, BB, B1, B2, B3, D                                               L1
     AS550                                                                                          A2, C2, C3, U2
     AS355                            E, F, F1, F2, N, NP
     AS555                                                                                     AF, AN, SN, UF, UN, AP
     EC130                                  B4, T2
  SA365 / AS365                   C1, C2, C3, N, N1, N2, N3                                         F, Fs, Fi, K, K2
     AS565                                                                                    MA, MB, SA, SB, UB, MBe
     SA366                                                                                                GA
     EC155                                   B, B1
     SA330                                     J                                                      Ba, L, Sm
     SA341                                     G                                                    B, C, D, E, F, H
     SA342                                     J                                                   L, L1, M, M1, Ma
   ALOUETTE II                  313B, 3130, 318B, 318C, 3180
  ALOUETTE III                     316B, 316C, 3160, 319B
     LAMA                                    315B
     EC225                                    LP
     EC725                                                                                                AP
     AS332                             C, C1, L, L1, L2                                            B, B1, F1, M, M1
     AS532                                                                                   A2, U2, AC, AL, SC, UE, UL
     EC175                                     B
      H160                                     B
     EC339                                                                                           KUH/Surion
                     C (C23, CB, CB-4, CB-5), D (DB, DBS, DB-4, DBS-4,
     BO105                                                                                         CBS-5 KLH, E-4
                         DBS-5), S (CS, CBS, CBS-4, CBS-5), LS A-3
                    A-1, A-3, A-4, B-1, B-2, C-1, C-2, C-2e, D-2, D-2m, D-3,
   MBB-BK117                                                                                         D-2m, D-3m
                                              D-3m
                   T1, T2, T2+, T3, P1, P2, P2+, P3, EC635 T1, EC635 T2+,
     EC135                    EC635 T3, EC635 P2+, EC635 P3,
                             T3H, P3H, EC635 T3H, EC635 P3H
Revision 0   2023-02-22                                                                                                       Page 1/2
                                                            This document is available on the Internet: www.airbushelicopters.com/techpub/
                                                       No. 3868-S-20
Airbus Helicopters has participated in an investigation conducted by the Canadian Transport Safety Board (TSB),
following an accident with an Ecureuil helicopter that occurred at the beginning of 2022 in Quebec.
The reported circumstances of this accident were that a helicopter collided with the frozen surface of a river
(accident of the “Controlled Flight into Terrain” (CFIT) type).
The precise description and analysis of this accident, which did not result in injury, are given in Air transportation
safety investigation report No. A22Q0029, which is available via the following link:
http://www.tsb.gc.ca/eng/enquetes-investigations/aviation/2022/A22Q0029/A22Q0029.html
You will find a summary of the circumstances of this accident and its analysis below:
- Before the flight during which the accident occurred, the helicopter was parked outside, at temperatures below
  zero. The external surface of the windshield was not protected and was covered in a layer of white frost.
- After starting the engine, the pilot applied a significant quantity of automobile windshield washer fluid to the
  entire windshield surface until all the frost was eliminated. He then removed the excess product by hand.
- A few moments after take-off, the outside surface of the windshield suddenly became covered with frost again.
- The pilot decided to perform a precautionary landing during which he was not able to judge the distance to the
  ground.
- The helicopter impacted the frozen and snow-covered surface of the river and then became immobilized on its
  left side.
The analysis performed by the TSB shows that the product used to de-ice the windshield was not the one
recommended by Airbus Helicopters. The use of a methanol & water-based product, instead of an ethylene glycol
& water-based product as recommended by Airbus Helicopters, led to the sudden icing (methanol being much
more volatile than water, as opposed to ethylene glycol). When a methanol & water-based windshield washer fluid
is used, the methanol will quickly evaporate and the remaining water will freeze as soon as the temperature drops
below zero.
This event leads Airbus Helicopters to remind you that only the products recommended in the Work Cards of the
Maintenance Manuals or Standard Practices Manual (MTC) must be used on our helicopters.
As regards de-icing or anti-icing protection, the applicable methods and products for our helicopters are described
in Work Cards 20-07-02-205 and 20-07-03-409 (MTC).
Revision 0   2023-02-22                                                                                               Page 2/2
                                                    This document is available on the Internet: www.airbushelicopters.com/techpub/