Transport Canada Holdover Time Guidelines Winter

Transcription

1 TABLE 8-1 LIST I FLUIDS TESTED FOR ANTI-ICING PERFORMANCE AND AERODYNAMIC ACCEPTANCE 4,5 LOWEST OPERATIONAL USE TEMPERATURE 3 LOW SPEED C F C F ABAX Industries DE-950 PG / ABAX Industries DE-950 Colorless PG /40 Not tested 10 Not tested ADDCON EUROPE IceFree I.80 PG / AllClear Systems LLC Lift-Off P-88 PG / AllClear Systems LLC Lift-Off E-188 EG / Arcton Ltd. 11 Arctica DG ready-to-use DEG as supplied Arcton Ltd. 11 Arctica DG 91 Concentrate DEG / AVIAFLUID International Ltd. AVIAFLO EG EG / Aviation Shaanxi Hi-Tech Physical Chemical Co. Ltd. Cleanwing I PG /5 Not tested 10 Not tested Aviation Xi an High-Tech Physical Chemical Co. Ltd. KHF-1 PG /5 Not available 1 Not available Baltic Ground Services 11 DEFROSOL ADF NG / Beijing Phoenix Air Traffic Product Not 11 CBSX-I PG Development and Trading Co. available 1 Not available1 Not available 1 Not available 1 Not available 1 Beijing Wangye Aviation Chemical Product Co Ltd. 11 KLA-1 EG /40 Not available1 Not available Beijing Yadilite Aviation Advanced Materials Corporation YD-101 Type I PG /40 Not tested 10 Not tested CHEMCO Inc. CHEMR EG I EG / CHEMCO Inc. CHEMR REG I EG / EcoFlo Concentrate NG /35 Not tested 10 Not tested EcoFlo Concentrate NG /35 Not tested 10 Not tested Octaflo EF Concentrate PG / Octaflo EF-80 PG / Octaflo EG Concentrate EG / Octaflo LYOD EG / Safewing EG I 1996 EG / Safewing EG I 1996 (88) EG / Page 1 of 9 July 015

2 TABLE 8-1 (cont d) LIST I FLUIDS TESTED FOR ANTI-ICING PERFORMANCE AND AERODYNAMIC ACCEPTANCE 4,5 LOWEST OPERATIONAL USE TEMPERATURE 3 LOW SPEED C F C F Safewing MP I 1938 ECO PG / Safewing MP I 1938 ECO (80) PG / Safewing MP I 1938 ECO (80) Premix 55% i.g. ready-to-use PG as supplied Not tested 10 Not tested Safewing MP I ECO PLUS (80) PG / Cryotech Deicing Technology Polar Plus PG / Cryotech Deicing Technology Polar Plus LT PG / Cryotech Deicing Technology Polar Plus LT (80) PG / Cryotech Deicing Technology Polar Plus (80) PG / Deicing Solutions LLC Safetemp ES Plus (Multiple Location) PG / Dow Chemical Company UCAR ADF Concentrate EG / Dow Chemical Company UCAR ADF XL54 EG as supplied Dow Chemical Company UCAR PG ADF Concentrate PG / Dow Chemical Company UCAR PG ADF Dilute 55/45 PG as supplied Heilongjiang Hangjie Aero-chemical Technology Co. Ltd. HJF-1 EG /35 Not tested 10 Not tested Heilongjiang Hangjie Aero-chemical Technology Co. Ltd. HJF-1A EG /5 Not tested 10 Not tested HOC Industries SafeTemp ES Plus PG / Inland Technologies CANADA Inc. DuraGly-E Type I ADF Concentrate EG / Inland Technologies CANADA Inc. DuraGly-P Type I ADF Concentrate PG / Kilfrost Limited Kilfrost DF Plus PG / Kilfrost Limited Kilfrost DF Plus (80) PG / Kilfrost Limited Kilfrost DF Plus (88) PG / Kilfrost Limited Kilfrost DF Sustain PDO / LNT Solutions LNT E188 EG / LNT Solutions LNT P180 PG / LNT Solutions LNT P188 PG / Page of 9 July 015

3 TABLE 8-1 (cont d) LIST I FLUIDS TESTED FOR ANTI-ICING PERFORMANCE AND AERODYNAMIC ACCEPTANCE 4,5 LOWEST OPERATIONAL USE TEMPERATURE 3 LOW SPEED C F C F Newave Aerochemical Co. Ltd. FCY-1A EG / Newave Aerochemical Co. Ltd. FCY-1Bio+ EG /5 Not tested 10 Not tested Oksayd Co. Ltd. DEFROST ECO 1 NG /30 Not tested 10 Not tested Shaanxi Cleanway Aviation Chemical Co., Ltd Cleansurface I EG / Shaanxi Cleanway Aviation Chemical Co., Ltd Cleansurface I-BIO EG /5 Not tested 10 Not tested Velvana a.s. AIRVEL OK 1 PG / Page 3 of 9 July 015

4 TABLE 8- LIST II FLUIDS TESTED FOR ANTI-ICING PERFORMANCE AND AERODYNAMIC ACCEPTANCE LOWEST OPERATIONAL USE TEMPERATURE 3 C F 7,8 LOWEST ON-WING VISCOSITY ABAX Industries Ecowing 6 PG Aviation Shaanxi Hi-Tech Physical Chemical Co. Ltd. Cleanwing II PG Safewing MP II FLIGHT PG Safewing MP II FLIGHT PLUS PG Cryotech Deicing Technology Polar Guard II PG Kilfrost Limited ABC-3 PG Kilfrost Limited ABC-Ice Clear II PG Kilfrost Limited ABC-K Plus PG / (h) (a) 75/ (a) 00 (a) 50/ (a) 50 (a) 100/ (f) (a) 75/ (f) (a) 50/ (f) (a) 100/ (a) (a) 75/ (c) (c) 50/ (a) (a) 100/ (o) (a) 75/ (o) (a) 50/ (o) (a) 100/ (g) (a) 75/ (g) (a) 50/ (a) 80 (a) 100/ (f) 500 (a) 75/ (f) 000 (a) 50/ (f) 400 (a) 100/ (a) 7 70 (a) 75/ (a) (a) 50/ (a) 558 (n) 100/ (f) 640 (a) 75/ (f) (c) 50/ (f) 5 60 (a) LNT Solutions LNT P50 PG Y-M-D 13 75/5 Not available 1 Not available (e) (a) 100/0 1 Not available Not available (e) 150 (a) Newave Aerochemical Co. Ltd. FCY- PG /50 Not available 1 Not available (e) (a) 100/ (f) 8 90 (a) 75/ (f) (f) 50/ (f) (a) Page 4 of 9 July 015

5 TABLE 8- (cont d) LIST II FLUIDS TESTED FOR ANTI-ICING PERFORMANCE AND AERODYNAMIC ACCEPTANCE Newave Aerochemical Co. Ltd. FCY- Bio+ PG LOWEST OPERATIONAL USE TEMPERATURE 3 C F 7,8 LOWEST ON-WING VISCOSITY 100/ (a) 7 10 (a) 75/ (c) (c) 50/ (a) (a) Page 5 of 9 July 015

6 TABLE 8-3 LIST III FLUIDS TESTED FOR ANTI-ICING PERFORMANCE AND AERODYNAMIC ACCEPTANCE LOWEST OPERATIONAL USE TEMPERATURE 3 LOW SPEED C F C F LOWEST ON-WING VISCOSITY7, / (m) Not Available AllClear Systems LLC AeroClear MAX EG /5 Dilution Not Applicable Dilution Not Applicable Dilution Not Applicable Dilution Not Applicable Clariant Produkte (Deutschland) Safewing MP III 031 ECO PG / (n) 10 (n) 75/ (n) 86 (n) 50/ (n) 16 (n) Page 6 of 9 July 015

7 TABLE 8-4 LIST IV FLUIDS TESTED FOR ANTI-ICING PERFORMANCE AND AERODYNAMIC ACCEPTANCE ABAX Industries Ecowing AD-49 PG Max Flight 04 PG Max Flight SNEG PG Safewing MP IV LAUNCH Safewing MP IV LAUNCH PLUS PG PG LOWEST OPERATIONAL USE TEMPERATURE 3 C F 7,8 LOWEST ON-WING VISCOSITY 100/ (i) (a) 75/ (i) (c) 50/ (i) (c) 100/ (b) (a) 75/5 Dilution Not Applicable Dilution Not Applicable 100/ (p) (a) 75/ (q) (c) 50/ (q) (c) 100/ (a) (a) 75/ (a) (a) 50/ (a) (a) 100/ (p) (a) 75/ (q) (c) 50/ (p) (a) Cryotech Deicing Technology Polar Guard PG / (k) (c) 100/ (k) (c) 50/ (k) (a) 100/ (g) (a) Cryotech Deicing Technology Polar Guard Advance PG / (g) (a) 50/ (a) 80 (a) 100/ (a) (a) Deicing Solutions LLC ECO-SHIELD PG /5 Dilution Not Applicable Dilution Not Applicable Dow Chemical Company Dow Chemical Company UCAR Endurance EG106 De/Anti-Icing Fluid UCAR FlightGuard AD-480 EG / (j) 30 (a) 75/5 Dilution Not Applicable Dilution Not Applicable PG / (h) (d) 100/ (h) (d) 50/ (h) (a) Page 7 of 9 July 015

8 Dow Chemical Company TABLE 8-4 (cont d) LIST IV FLUIDS TESTED FOR ANTI-ICING PERFORMANCE AND AERODYNAMIC ACCEPTANCE UCAR FlightGuard AD-49 PG LOWEST OPERATIONAL USE TEMPERATURE 3 C F 7,8 LOWEST ON-WING VISCOSITY 100/ (i) (a) 75/ (i) (c) 50/ (i) (c) Kilfrost Limited ABC-S Plus PG / (f) (c) 100/ (f) (c) 50/ (f) (a) 1 100/0 Not available Not available (l) Not Available 16 LNT Solutions LNT E450 EG Y-M-D 13 75/5 Dilution Not Applicable Dilution Not Applicable Newave Aerochemical Co. Ltd. FCY 9311 PG / (c) (c) 75/5 Dilution Not Applicable Dilution Not Applicable Page 8 of 9 July 015

9 CAUTIONS AND NOTES FOR TABLES 8-1, 8-, 8-3, 8-4 CAUTIONS This table lists fluids that have been tested with respect to anti-icing performance and aerodynamic acceptance (Type I: SAE AMS and 3.5.3; Type II, III, IV: SAE AMS and 3..5) only. These tests were conducted by Anti-icing Materials International Laboratory: The end user is responsible for contacting the fluid manufacturer to confirm all other SAE AMS144/148 technical requirement tests, such as fluid stability, toxicity, materials compatibility, etc. have been conducted. LOUT data provided in these tables is based strictly on the manufacturer s data, the end user is responsible for verifying the validity of this data. Type I fluids supplied in concentrated form must not be used in that form and must be diluted. NOTES 1 PG = propylene glycol; PDO = propylene glycol (propane-1, 3-diol); EG = ethylene glycol; DEG = diethylene glycol; NG = non-glycol. Expiry date is the earlier expiry date of the Aerodynamic Test(s) or Water Spray Endurance Test. Fluids that are tested after the issuance of this list will appear in a later update. 3 The values in this table were determined using test results from pre-production fluid samples when available. In some cases, the fluid manufacturer requested the publication of a more conservative value than the pre-production test value. The lowest operational use temperature (LOUT) for a given fluid is the higher of: a) The lowest temperature at which the fluid meets the aerodynamic acceptance test for a given aircraft type; b) The actual freezing point of the fluid plus its freezing point buffer (Type I = 10 C/18 F; Type II/III/IV = 7 C/13 F); or c) For diluted Type II/III/IV fluids, the coldest temperature for which holdover times are published. 4 The LOUT for Type I fluids that are intended to be diluted is derived from a dilution that provides the lowest operational use temperature. For other Type I dilutions, determine the freezing point of the fluid and add a 10 C freezing point buffer, as a dilution will usually yield a higher and more restrictive operational use temperature. Consult the fluid manufacturer or fluid documentation for further clarification and guidance on establishing the appropriate operational use temperature of a diluted fluid. 5 Type I concentrate fluids have also been tested at 50/50 (glycol/water) dilution. 6 If uncertain whether the aircraft to be treated conforms to the low speed or the high speed aerodynamic test, consult the aircraft manufacturer. The aerodynamic test is defined in SAE AS5900 (latest version). 7 The viscosity values in this table are those of the fluids provided by the manufacturers for holdover time testing. For the holdover times to be valid, the viscosity of the fluid on the wing shall not be lower than that in this table. The user should periodically ensure that the viscosity of a fluid sample taken from the wing surface is not lower than that listed. 8 The SAE AS9968 viscosity method should only be used for field verification and auditing purposes; when in doubt as to which method is appropriate, use the manufacturer method. Viscosity measurement methods are indicated as letters (in parentheses) beside each viscosity value. Details of each measurement method are shown in the table below. The exact measurement method (spindle, container, fluid volume, temperature, speed, duration) must be used to compare the viscosity of a sample to a viscosity given in this table. Method Brookfield Spindle Container Fluid Volume Temp. Speed Duration a LV1 (with guard leg) 600 ml low form (Griffin) beaker 575 ml* 0 C 0.3 rpm 10.0 minutes b LV1 (with guard leg) 600 ml low form (Griffin) beaker 575 ml* 0 C 0.3 rpm 33.3 minutes c LV-disc (with guard leg) 600 ml low form (Griffin) beaker 45 ml* 0 C 0.3 rpm 10.0 minutes d LV-disc (with guard leg) 50 ml tall form (Berzelius) beaker 00 ml* 0 C 0.3 rpm 10.0 minutes e LV-disc (with guard leg) 00 ml tall form (Berzelius) beaker 155 ml* 0 C 0.3 rpm 10.0 minutes f LV-disc (with guard leg) 150 ml tall form (Berzelius) beaker 135 ml* 0 C 0.3 rpm 10.0 minutes g SC4-34/13R small sample adapter 10 ml 0 C 0.3 rpm 10.0 minutes h SC4-34/13R small sample adapter 10 ml 0 C 0.3 rpm 30.0 minutes i SC4-31/13R small sample adapter 10 ml 0 C 0.3 rpm 10.0 minutes j SC4-31/13R small sample adapter 10 ml 0 C 0.3 rpm 10.0 minutes k SC4-31/13R small sample adapter 9 ml 0 C 0.3 rpm 10.0 minutes l SC4-31/13R small sample adapter 9 ml 0 C 0.3 rpm 10.0 minutes m SC4-31/13R small sample adapter 9 ml 0 C 0.3 rpm 30.0 minutes n LV0 UL adapter 16 ml 0 C 0.3 rpm 10.0 minutes o LV1 big sample adapter 50 ml 0 C 0.3 rpm 10.0 minutes p LV1 big sample adapter 55 ml 0 C 0.3 rpm 10.0 minutes q LV-disc big sample adapter 60 ml 0 C 0.3 rpm 10.0 minutes *If necessary, adjust fluid volume to ensure fluid is level with notch on the spindle shaft 9 Fluids listed in italics have expired and will be removed from this listing four years after expiry. 10 Manufacturer has indicated fluid was not tested. 11 Manufacturer has not provided fluid information as required in SAE ARP5718A; fluid may be removed from this listing in subsequent revisions. 1 Manufacturer had not provided LOUT information at the time of publication. 13 Currently in the test/re-retest process. 14 Fluid was not retested for low speed aerodynamics. This data will be removed four years after the expiry of the last low speed test. 15 Fluid did not meet the minimum Water Spray Endurance Test requirement in SAE AMS148G; a change to this requirement is being considered. 16 Measurements using the SAE AS9968 method do not provide stable, reliable results. Use the manufacturer method to evaluate viscosity. Page 9 of 9 July 015