TCDS A14EA

DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION TYPE CERTIFICATE DATA SHEET NO. A14EA This data sheet which is a part of Type Certificate No. A14EA, prescribes conditions and limitations under which the product for which the type certificate was issued meets the airworthiness requirements of the Federal Aviation Regulations. Type Certificate Holder Type Certificate Holder Record De Havilland Aircraft of Canada Limited 4100 Westwinds Drive NE Calgary, Alberta Canada T3J 4L2 Viking Air Limited transferred TC A14EA to De Havilland Aircraft of Canada Limited on August 1, 2024 Bombardier Inc. transferred TC A14EA to Viking Air Limited on October 1, 2016 Canadair Limited transferred Type Certificate A14EA to Bombardier Inc. On March 6, 1998 I. MODEL CL-215-1A10 Amphibious Flying Boat (Restricted Category) Approved May 15, 1969 by the FAA and March 7, 1969 by the Canadian Department of Transport. The CL-215-1A10 has been produced in five groups: Serial Numbers 1001 to 1030, 1031 to 1050, 1051 to 1065, 1066 to 1080, and 1081 and subsequent. Data in this Type Approval that contains no specific reference to any group of serial numbers applies to all groups. (See NOTE 4). Engines Two Pratt and Whitney Double Wasp CA3. Fuel Avgas Grade 100/130 minimum to CAN 2-3.25-M77 or MIL-G-5572. Avgas Grade 100 LL to ASTM Specification D910. Oil Engine: All dispersant oils listed in Pr att & Whitney Aircraft Service Bulletin No. 1183 P or subsequent issue. Engine Limits See AFM as list ed in Approved Publications. GPU-2 Type: Andover Motors, Model 204 Fuel same as Aircraft. Oil MIL-0-6082 grade 1065 or SAE 10W30 Automotive Oil Oil Quantity: U. S. gal. Imp. gal. 0.9 0.75 Propeller and Propeller Limits Ma nufacturer Hamilton Sundstrand On aircraft 1001 to 1030 and 1039 and subsequent: Intermix in any combination of four types listed below: Propeller Types 43E60-581 P1 43E60-581 P2 43E60-701 43E60-583 Page No. 1 2 3 4 5 6 7 8 9 10 11 12 13 Rev. No. 15 10 5 5 9 10 12 14 12 13 12 13 14 A14EA Revision No. 15 De Havilland CL-215-1A10 CL-215-6B11 (CL-215T Variant) CL-215-6B11 (CL-415 Variant) October 19, 2026 Blades - Number and Type Three 6093A-10S (for -581P1 or P2) or Three 6901S-10 (for -701) or Three 6903A-10 (for -583) On aircraft 1031 to 1038: Propeller Type 43E60-581 P3 Blades - Number and Type Three 6903B-10S (for -581 P3) Diameter Limits Maximum 14 ft. 3 in (4.34 m) Minimum 13 ft. 11 1/2 in. (4.25 m) Pitch setting at 72-inch station For Propeller Type 43E60-581P1, 43E 60-581P2, 43E60-581P3 or 43E60-701: Low pitch stop 9.5 degrees ( 0.2 degrees) Constant speed range 9.5 degrees to 30 degrees Feathered 81 degrees ( 0.5 degrees) For Propeller Type 43E60-583: Low pitch stop 9.0 degrees ( 0.2 degrees) Constant speed range 9.0 degrees to 30 degrees Feathered 81 degrees ( 0.5 degrees) Except for transients, propeller must not be operated in the 1550 to 1750 RPM range. Airspeed Limits IAS CAS knots m.p.h. km/h knots m.p.h. km/h VMO (Maximum Operating) S.L. to 12,000 ft. 188 216 348 190 219 352 12,000 ft to 20,000 158 182 293 160 184 296 VFE (Flaps Extended) 10 138 159 255 140 161 259 25 Land and Water Operation 110 127 204 112 129 207 *25 Water Operation 114 131 211 116 133 215 *Refers to aircraft 1056 & subsequent VA (Maneuvering Speed) Restricted Category A/C at 36000 lb. 16329 kg MTOW. Water operation only 126 145 234 127 146 235 **A/C at 37700 lb. 17100 kg MTOW. Water operation only 128 147 237 129 148 239 3 A14EA IAS CAS knots m.p.h. km/h knots m.p.h. km/h A/C at 43500 lb. 19731 kg MTOW. Land operation only 149 171 276 150 173 278 A/C at 93500 lb. 19731 kg Lift-off and 15 flap Water operation only 131 151 243 133 153 246 VLE (Maximum Speed Landing Gear Extended) 129 148 239 130 150 241 VLO (Maximum Speed Landing Gear Operation) 129 148 239 130 150 241 VMCA (Minimum Control Speed with Automatic Propeller Feathering) 86 99 159 85 98 157 VLL (Maximum speed at which landing lights may be extended or used) Not applicable to aircraft 1081 and subsequent. 129 148 239 130 150 241 **Refers to Serial Numbers 1003, 1007, 1008, 1009, 1012, 1017, 1018, 1020, 1031 and subsequent, and aircraft Serial Number 1001 through 1030 fitted with additional buoyancy compartment in accordance with Canadair Service Bulletin Number CL215- 124. Restricted Category (water Bomber, including Chemical Foam, Configuration) IAS CAS knots m.p.h. km/h knots m.p.h. km/h VFE (Maximum speed with flaps extended) 15 138 159 255 140 161 259 VWD (Maximum airspeed at which water doors may be opened or operated in flight) 129 148 239 130 150 241 Maximum speed on water with probes extended (water speed) 80 92 148 *90 104 167 *Refers to aircraft 1051 and subsequent and aircraft which embody Service Bulletin CL215-203. Restricted Category, Liquid Sprayer Configuration Only IAS CAS knots m.p.h. km/h knots m.p.h. km/h VMO (Maximum Operating) S.L. to 20,000 ft 158 182 293 160 184 296 VJD (Maximum airspeed at which jettison doors may be opened or operated in flight) 158 182 293 160 184 296 Maximum Weight (Water or Chemical/Water Mix Tanks in use) (See NOTE 1) Lb. (Kg) Ramp 43500 (Land Operation) (19731) (Water Operation) 36300 (16465) *1* 38000 *1* (17236) Take-off 43500 (Land Operation) (19731) (Water Operation) 36000 (16329) *1* 37700 *1* (17100) Landing 34400 (Land Operation) (15604) *3* 37000 *3* (16783) Lb. (Kg) (Water Operation) 35500 (16103) *5* 37000 *5* (16783) Zero Fuel *4* 39000 (Land Operation) *4* (17690) 41000 (18597) (Water Operation) 41000 (18597) Water Bomber, including Chemical Foam, Configuration only Touch-down for water 33500 Pick-up (15195) *2* 35500 *2* (16103) Lift-off following 43500 Water Pick-up (19731) *1* Refers to Serial Numbers 1003, 1007, 1008, 1009, 1012, 1017, 1018, 1020, 1031 and subsequent, and aircraft Serial Number 1001 through 1030 fitted with additional buoyancy compartment in accordance with Canadair Service Bulletin Number CL215-124. *2* Refers to aircraft Serial Numbers 1051 and subsequent, and aircraft which incorporate New Probe System to Canadair Service Bulletin CL215-203. *3* Refers to aircraft 1056 to 1125 which incorporate Canadian Service Bulletin CL-215-376. *4* Refers to aircraft in the Liquid Sprayer Configuration. *5* Refers to aircraft 1056 and subsequent. 5 A14EA C.G. Limits See AFM as listed in Approved Publications. Maximum Occupants Ten (including two crew). Limite d by approved seating arrangements. In particular, see (See NOTE 2) Maximum Cargo General Cargo Load distribution must not exceed 150 lb./sq. ft. (732.36 kg/m2), nor 500 lbs. (226.8 kg) per running foot. For compartment limitations, refer to the following Canadair Reports: RAW-215-110 for S/N 1001 to 1030. RAW-215-144 for S/N 1001 to 1030 (Liquid Sprayer). RAW-215-146 for S/N 1031 to 1055. RAW-215-145 for SAR Aircraft S/N 1031 to 1038. RAW-215-172 for SAR Aircraft S/N 1058 to 1059. RAW-215-174 for S/N 1062 and 1063. RAW-215-190 for S/N 1056 and subsequent. Jettisonable Liquid Cargo: Water Bomber Configuration: Two tanks at Station 403.8, maximum water load of 6000 lb. (2722 kg) each. Volume 706 gallons (588 Imp. gallons) each. Liquid Sprayer Configuration: Five cabin installed tanks with total maximum chemical/water load of 10,500 lb. (4763 kg). Volume 1400 gallons (1166 Imp. gallons). Chemical Foam Configuration: Two tanks at Station 403.8, maximum load, water or chemical/water mix, of 6000 lb. (2722 kg) each. Volume 706 gallons (588 Imp. gallons) each. Non Jettisonable Liquid Cargo Chemical concentrate for Chemical Foam operations. Four cabin installed storage tanks with total maximum chemical load of 1,566 lb. (710 kg). Volume 158 US gallons (132 Imp). Additional Cargo Limitations (a) Carriage of general cargo in the cabin is prohibited when the water or chemical concentrate or chemical/water mix tanks are in use. (b) Landing with jettisonable water or chemical/water load in the tanks is prohibited. (c) All chemicals to be used in Liquid Spraying Operations must be approved by the local environmental authorities prior to commencement of spraying. (d) All chemicals to be used in Chemical Foam operations must comply with Canadair Material Specification CMS560-01 and be approved by the local environmental authorities prior to commencement of foam fire fighting operations. Fuel Capacity Usable Fuel U.S. gal. Imp. gal. S/N 1001 to 1030 1146 954 S/N 1031 and Sub. 1562 1301 Oil Capacity Engines: (eac h) U.S. gal. Imp. gal. Total 36.0 30.0 Usable* 30.7 25.6 * Excluding propeller feathering reserve of 2.0 gallons (1.7 Imp. gal.) each engine. Control Surface Movements Controls to be rigged in accordance with the following Canadair Drawings: (a) P215-90014 Diagram Aileron Controls. (b) P215-90015 Diagram Elevator Controls. (c) P215-90016 Diagram Rudder Controls. Maximum Operating Altitude Take-off and landing 8000 feet (Pressure Altitude) Enroute 20,000 feet Maximum altitude for water pick-up 5000 feet* * 8000 feet for water pick-up on A/C S/N 1051 and subsequent and aircraft incorporating Canadair Service Bulletin CL215-203. Additional Limitations Dispatch into known icing condit ions is prohibited unless aircraft is modified in accordance with Canadair Modification Summary SC-21002 and operated in accordance with Supplement II of the DOT Approved Flight Manual PSP 291. Serial Numbers Eligible Serial Number 1001 to 1125. (See NOTE 4). Placards Placards are listed in the following Canadair Drawings: 215-40053, 215-40440, 215-40443, 215-51004, 215-51137, 215-51311, 215-51312, 215-51314, 215-51317, 215-51387, 215-51402, 215-66000, (See NOTE 3). Approved Publications D.O.T. Approve d Airplane Flight Manual, Canadair Product Support Publication No. 191 for S/N 1001 to 1030 and Publication No. 291 for S/N 1031 and subsequent. D.O.T. Approved Maintenance Specification, Canadair Product Support Publication No. 295. D.O.T. Approved Drawing List, Canadair Report No. RAL-215-101. D.O.T. Approved Loading Instructions. (See NOTE 6). Life Limited Parts Required retirement times for life- limited components are as prescribed in the D.O.T. Approved Maintenance Specification, Canadair Product Support Publication No. 295. II. Model CL-215-6B11 (CL-215T Variant), Restricted Category, Amphibious Flying Boat Restricted Category, Approved March 30, 1993 by the FAA and March 28, 1991 by the Canadian Department of Transport (DOT) III. Model CL-215-6B11 (CL-415 Variant), Restricted Category Approved October 14, 1994 by the FAA and June 24, 1994 by the Canadian Department of Transport (DOT) DATA PERTINENT TO CL-215-6B11 (CL-215T Variant) and CL-215-6B11 (CL-415 Variant) Engines Two Pratt & Whitney Canada (See NOTE 7) PW123AF (Turboprop) w ith P&WC SB 21211 incorporated. Fuel Fuels conforming to any of the follo wing specifications are approved for use. Mixing of fuels is permitted. TYPE SPECIFICATION Kerosene CANADA USA UK Jet A, A-1 CGSB 3.23 ASTM D1655 DERD 2494 JP8 3-GP-23 MIL-T-83133 DERD 2453 Wide Cut* Jet B CGSB 3.22 ASTM D1655 DERD 2486 JP4 CGSB 3.22 MIL-T-5624 DERD 2486 High Flash 3-GP-24 MIL-T-5624 DERD 2452 JP5 *NOTE: Refer to Flight Manual Limitations Section for operating limits for JP4/Jet B fuel. 7 A14EA Oil Engine: All MIL-L-23699, type II oils and Castrol 4000 Engine Limits See AFM as list ed in Approved Publications. Airspeed Limits IAS CAS knots m.p.h. km/h knots m.p.h. km/h VMO (maximum Operating) 187 215 347 190 219 260 S.L. to 20,000 feet VFE (Flaps Extended) 10 138 159 256 140 161 260 15 138 159 256 140 161 260 25 114 131 211 116 134 215 25* 116 134 215 117 135 217 25** 119 137 220 120 138 222 VA (Maneuvering Speed) See Flight Manual for variation of VA with aircraft weight. * For CL-215-6B11 (CL-215T Variant) Refer to A/C 1056 and subsequent incorporating Canadair S.B. 215-376 ** For CL-215-6B11 (CL-415 Variant). VLE (Maximum Speed-Landing Gear Extended) 129 148 239 130 150 241 VLO (Maximum Speed-Landing Gear Operation) 129 148 239 130 150 241 VMCA (Minimum Control Speed in the air with Automatic Propeller Feathering Operative) 84 97 155 84 97 155 VLL (Maximum speed at which Landing lights may be extended or used)** 129 148 239 130 150 241 ** not applicable to A/C 1081 and subsequent VWD (Maximum Speed at which water doors may be opened or operated in flight) 129 148 239 130 150 241 Maximum speed on Water with Probes 80 92 148 extended (water speed) *90 104 167 * Refers to aircraft 1051 and subsequent and aircraft which embody Service bulletin CL215-203. C.G. Limits See AFM as listed in Approved Publications. Maximum Cargo Additional Cargo Limitations (a) Carriage of general cargo in the cabin is prohibited when water tanks are in use. (b) Landing with jettisonable water load in the tanks is prohibited. Fuel Capacity Usable Fuel Pressure refueling: 1530 gallons (1275 Imperial Gallons) (Total Capacity) Gravity refueling: 1562 gallons (1301 Imperial Gallons) (Total Capacity) Maximum refuel pressure: 50 psig. Oil Capacity Engines: (Each) Total U.S. Gal. 5.1 Imp. Gal. 4.3 Usable 0.9 0.8 Control Surface Movements Rudder Elevator Aileron 30R 23L Up 22  Down 20  Up 20  Down 13.75   0.5   0.5   0.5   0.5   0.5   0.5  Neutral 2  TE up Additional Limitations Dispatch into kn own icing conditions is prohibited DATA PERTINENT TO CL-215-6B11 (CL215T Variant) The data in this Type Approval apply to Aircraft model CL-215-1A10 retrofitted with the Canadair Modification Kit described in: - Report RAD-215T-103 (Kit Specification for the Retrofit of CL-215-piston aircraft with turboprop engines) for A/C with S/Ns 1056, 1057, 1061, 1080, 1109, 1113, to 1122, 1124, 1125. - Report RAL-K215T-0001 Rev. A or later approved revision (K215T Engineering Configuration Statement), as amended by Modification Summaries, for A/C with S/Ns 1081 to 1090, 1092 to 1108, 1110 to 1112, and 1123. After embodiment of the kit, affected A/C shall be redesignated as model CL-215-6B11 (CL-215T Variant). Propeller and Manufacturer: Hamilton Sundstrand Propeller Limits Propeller Type: Two 14SF-17 (four-bladed) or Two 14SF-19 (four-bladed) Diameter:13 feet, 1/4 inch (3.97m) Pitch setting at 42-inch station: Reverse: -10  1.17 (dynamic conditions) -13.6 to -15.6 reverse pitch stop position Feathered: 86.0   Maximum Weight Restricted Category (Mass) (See NOTE 1) Take-Off lb. kg Land Operation 43,500 19,731 Water Operation 37,850 17,168 (For other weights see AFM as listed in Approved Publications). Maximum Occupants (a) Ten (including two crew). Limited by approved seating arrangements. In particular, see NOTE 2. Maximum Cargo General Cargo Load distribution must not exceed 150 lb./sq.ft. (732.36 kg/m2), nor 500 lbs. (226.8 kg) per running foot. For compartment limitations, refer to the following Canadair Report: RAW-215T-102 9 A14EA Jettisonable Liquid Cargo: Water Bomber Configuration: Two tanks at Station 403.8, maximum water load of 6000 lb. (2722 kg) each. Volume 706 gallons (588 Imp. gallons) each. Maximum Operating Take-off and Landing: 10000 feet Altitude Enroute: 20000 feet (Pressure Altitude) Water Pick-up: 5000 feet 8000 feet (1) (1) A/C incorporating Canadair SB CL215-203 Serial Numbers Eligible Serial Numbers 1056, 1057, 106 1, 1080, 1109, 1113 to 1122, 1124, 1125 retrofitted per RAD-215T-103 and Serial Numbers 1081 to 1090, 1092 to 1108, 1110 to 1112 and 1123 in retrofit per RAL-K215T-0001. Placards Substitution and/or removal of existing placards on CL-215-1A10 in addition to new (See NOTE 3) placards, as specified in Canadair Report MBS-215T-111 required to achieve model CL-215-6B11 aircraft (refer to Approved Publications). Approved Publications CL-215-6B11 (S/N 1056, 1057, 1061, 1080, 1109, 1113 to 1122, 1124, 1125 D.O.T. Approved Airplane Flight Manual, Product Support Publication No. 391 D.O.T. Approved Airworthiness Limitations, scheduled inspections and maintenance intervals sections of D.O.T. Approved Standard Maintenance Specifications, Product Support Publication No. 395. D.O.T. Approved Drawing List, Canadair Report No. RAL-215-xxx (for each individual aircraft) (CL-215-1A10) in addition to the following Canadair Modification Summaries (to achieve model CL-215-6B11): 215T001A, 215T001B, 215T001C, 215T001D, 215T003, 215T004, 215T011, 215T012, 215T013, 215T016, 215T017, 215T020A, 215T020B, 215T020C, 215T020D, 215T021, 215T024, 215T025, 215T026. D.O.T. Approved Loading Instructions (see NOTE 6). CL-215-6B11 (S/N 1081 to 1090, 1092 to 1108, 1110 to 1112, 1123 D.O.T. Approved Airplane Flight Manual, Product Support Publication No. 391-1 D.O.T. Approved Airworthiness Limitations, scheduled inspections and maintenance intervals sections of D.O.T. Approved Standard Maintenance Specifications, Product Support Publication No. 395-1. D.O.T. Approved Drawing List, Canadair Report No. RAL-215-xxx (for each individual aircraft) (CL-215-1A10) in addition to th e following Canadair Modification Summary (to achieve model CL-215-6B11): 215T60010 D.O.T. Approved Loading Instructions (see NOTE 6). Airworthiness CL-215-6B11 (S/N 1056, 1057, 1061, 1080, 1109, 1113 to 1122, 1124, 1125 Limitations The Airworthiness Limitations are prescribed in the D.O.T. Approved Standard Maintenance Specification, Product Support Publication No. 395, Airworthiness Limitation Section. CL-215-6B11 (S/N 1081 to 1090, 1092 to 1108, 1110 to 1112, 1123 The Airworthiness Limitations are prescribed in the D.O.T. Approved Standard Maintenance Specification, Product Support Publication No. 395-1, Airworthiness Limitation Section. DATA PERTINENT TO CL-215-6B11 (CL-415 Variant) The data in this Type Approval applies to Aircraft Model CL-215-6B11 described by Report RAL-415-101 Issue NC plus Mod. Sums. Propeller and Manufacturer: Hamilton Sun dstrand Propeller Limits Propeller Type: Two 14SF-19 (four-bladed) Diameter: Pitch setting at 42-inch station: 13 feet, 1/4 inch (3.97m) Reverse: -10  1.17 (dynamic conditions) -13.6 to -15.6 reverse pitch stop position Feathered: 86.0   Maximum Weight Take-Off Re stricted Category lb. kg (Mass) Land Operation 43,850 19,890 (See NOTE 1) Water Operation 37,850 17,169 (For other weights see AFM as listed in Approved Publications). Maximum Occupants (a) Ten (including two crew). Limited by approved seating arrangements. (See NOTE 2) Maximum Cargo General Cargo Load distribution must not exceed 150 lb./sq. ft. (732.36 kg/m2), nor 500 lbs. (226.8 kg) per running foot. For compartment limitations, refer to the following Canadair Report: RAW-415-102 Maximum Water Tank Capacity: (Water Bomber Configuration:) VOLUME WEIGHT Gallons Imp Gal lb. kg Inboard tanks (2) 838 698 6980 3167 Outboard tanks (2) 783 652 6520 2957 All tanks (4) 1621 1350 13500 6124 Maximum Operating Take-off and Landing: 10000 feet Altitude Enroute: 20000 feet (Pressure Altitude) Water Pick-up: 8000 feet Serial Numbers Eligible Serial Number 2001 to 2999 Placards Required placards are specified in Canadair report MBS-215T-105 Approved D.O.T. Approved Airplane Flight Ma nual Canadair Product Support Publication No. 491 Publications D.O.T. Approved Airworthiness limitations, scheduled inspections and maintenance intervals sections of Canadair Product Support Publication No. 495. D.O.T. Approved Drawing List and Modification Summary listed in Canadair Report No. RAL-415-101 which defines the build standard of the production CL-415. D.O.T. Approved Loading Instructions (See NOTE 6) Airworthiness The Airworthiness Limitations ar e prescribed in the Standard Maintenance Specification, Limitations Canadair Product Support Publication No. 495, Airworthiness Limitations Section. DATA PERTINENT TO ALL MODELS EXCEPT AS INDICATED Datum The reference datum is located 300 inches (762 cm) forward of the keyhole slot in the chine angle on both sides of the fuselage at station 300.0. Leveling Means Longitudinal: Lugs on left hand nose wheel well sidewall at stations 170.0 and 182.5. Lateral: Lugs on front face of nose wheel well rear bulkhead, station 222.50. 11 A14EA Mean Aerodynamic The leading edge of the MAC is 366.57 inches (931.08 cm) aft of the reference datum. Chord (MAC) The length of the MAC is 139.4 inches (354.07 cm). Minimum Crew Two (Pilot and Co-Pilot) Certification Basis CL-215-1A10 S/N 1001 to 1030 FAR 21.29(a)(1)(ii), FAR Part 25, dated February 1, 1965 plus amendment 25-18 dated September 29, 1968 with the deviations recorded in the following documents. Canadair Report No. RAO-215-100, Issue 2, dated 15 January 1966, including Revision "A" dated 28 February, 1969, and Revision "B" dated 21 May, 1970, and modified by D.O.T. letter dated 26 February, 1971. CL-215-1A10 S/N 1031 to 1125* FAR 21.29(a)(1)(ii), FAR Part 25, dated February 1, 1965 plus amendment 25-18 dated September 29, 1968 with the deviations recorded in the following documents. Canadair Report No. RAO-215-100, Issue 2, dated 15 January 1966, including Revision "A" dated 28 February 1969, Revision "B" dated 21 May, 1970, Revision "C" dated 13 September, 1973 and Revision "C", Addendum 1 dated 27 May, 1974, modified by DOT letter dated 23 April 1974, and by DOT letter dated 9 December 1981. * For Aircraft S/N 1058, 1059, 1062 and 1063, see NOTE 4. CL-215-6B11 (CL-215T Variant), and CL-215-6B11 (CL-415 Variant) FAR 21.29(a)(1)(ii), FAR Part 25, dated February 1, 1965 plus amendment 25-18 dated September 29, 1968 and selected requirements of FAR Part 25 including amendments 25-1 through 25-61 and of Airworthiness Manual Chapters 525 and 516, as specified in, and including the deviations recorded in, the following document: Canadair Report RAO-215-100, Issue 2, Revision H, dated September 19, 1991 for CL-215-6B11 (CL-215T Variant) with S/N 1056, 1057, 1061, 1080, 1109, 1113 to 1122, 1124, 1125. Canadair Report RAO-215-100, Revision I-1, CL-215-6B11 (CL-215T Variant) with S/N 1081 to 1090, 1092 to 1108, 1110 to 1112, 1123. Canadair Report RAO-215-100, Issue 2 Revision I, for CL-215-6B11 (CL-415 Variant) Compliance with the following requirements has been established: SFAR 27-2, Environmental Protection Agency Final Venting and Exhaust Emission Requirements For Turbine Powered Aircraft. Noise requirements of FAR Part 36 with Amendments 36-1 through 36-17, change 22 Appendices A, B, and C. Findings of Equivalent Safety: a) FAR Part 25.901(b)(1)(i) Installation b) FAR Part 25.1045(e) Cooling Test Procedures CL-215-1A10, and CL-215-6B11 (CL-215T & CL-415 Variants) Compliance with the following requirements has been established: Ditching provisions of FAR Part 25.801(b) through (e), and 25.807(d). (The requirements of 25.1415(a) through (d) are not applicable, per Report RAO-215-100, Appendix 11, item RU.801). CL-215-6B11 (CL-215T Variant) with S/N 1081 to 1090, 1092 to 1108, 1110 to 1112, 1123 ELOS Memo Requirement Title AT09323NY- T-P-1 14 CFR 25.1549(a)(b)(c) Digital Only Display of the Turbine Engine Required Parameters CL-215-6B11 (CL-415 Variant) Transport Canada Special Conditions (Airworthiness) SCA 93-4 High Intensity Radiated Fields (HIRF) (Ref FAA Issue Paper SE-3) SCA 93-5 Lighting Protection (Ref FAA Issue Paper SE-2) Import requirements A Restricted U.S. Airworthiness Certificate may be issued for the aerial dispensing of liquids approved under the special purpose of forest and wildlife conservation on the basis of the Canadian Department of Transport "Certificate of Airworthiness for Export" signed by or for the Minister of Transport. This form must contain the following statement: "The aircraft covered by this certificate has been examined and found to comply with the provisions of the following: CL-215-1A10 Canadair Ltd. Report No. RAO-215-100, Issue 2 dated January 15, 1966, including Revision "A" dated February 28, 1969, and Revision "B" dated May 21, 1970, plus FAA's "additional requireme nts" presented in Attachment "A" to FAA's minutes of November 10, 1966 meeting, as amended by FAA's letter