CIVIL AVIATION AUTHORITY – SAFETY AND AIRSPACE REGULATION GROUP MICROLIGHT TYPE APPROVAL DATA SHEET (TADS) NO: BM-83 ISSUE: 1 TADS BM-83 Issue 1 1 of 12 TYPE: Flight Design CTSL (1) MANUFACTURER: P & M Aviation Ltd, Unit B, Crawford St, Rochdale (UK type approval holder for Flight Design GMBH) (2) UK IMPORTER: P & M Aviation Ltd (3) CERTIFICATION: BCAR section S issue 6, CS-VLA Parts C & D (4) DEFINITION OF BASIC STANDARD: AE 0110 0001, revision 0, dated 25-Mar-14 (5) COMPLIANCE WITH THE MICROLIGHT DEFINITION: (a) MTOW 472.5 kg (b) No. Seats 2 (c) Maximum Wing Loading 47.2 kg/m² (d) Vso 34 kt CAS (e) Permitted range of pilot weights 55 – 100 kg per seat 180 kg total (f) Typical Empty Weight (ZFW) 288 kg (g) ZFW + 172 kg crew + 1 hr fuel (14 litres / 10 kg) 469 kg (h) ZFW + 86 kg pilot + full fuel (62 litres / 44.6 kg) 467.6kg (i) Max ZFW at initial permit issue 291 kg
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Flight Design CTSL - British Microlight Aircraft Association · 95 RON minimum unleaded to BS(EN) ... Rotax 912 engine (all versions) operators manual current issue . ... BM25 . Pegasus
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CIVIL AVIATION AUTHORITY – SAFETY AND AIRSPACE REGULATION GROUP
MICROLIGHT TYPE APPROVAL DATA SHEET (TADS)
NO: BM-83 ISSUE: 1
TADS BM-83 Issue 1 1 of 12
TYPE: Flight Design CTSL
(1) MANUFACTURER:
P & M Aviation Ltd, Unit B, Crawford St, Rochdale (UK type approval holder for Flight Design GMBH)
(2) UK IMPORTER: P & M Aviation Ltd
(3) CERTIFICATION: BCAR section S issue 6, CS-VLA Parts C & D
(4) DEFINITION OF BASIC STANDARD:
AE 0110 0001, revision 0, dated 25-Mar-14
(5) COMPLIANCE WITH THE MICROLIGHT DEFINITION:
(a) MTOW 472.5 kg
(b) No. Seats 2
(c) Maximum Wing Loading 47.2 kg/m²
(d) Vso 34 kt CAS
(e) Permitted range of pilot weights 55 – 100 kg per seat 180 kg total
(f) Typical Empty Weight (ZFW) 288 kg
(g) ZFW + 172 kg crew + 1 hr fuel (14 litres / 10 kg)
469 kg
(h) ZFW + 86 kg pilot + full fuel (62 litres / 44.6 kg)
467.6kg
(i) Max ZFW at initial permit issue 291 kg
CIVIL AVIATION AUTHORITY – SAFETY AND AIRSPACE REGULATION GROUP
MICROLIGHT TYPE APPROVAL DATA SHEET (TADS)
NO: BM-83 ISSUE: 1
TADS BM-83 Issue 1 2 of 12
(6) POWER PLANTS:
Designation Rotax 912 ULS Rotax 912 ULS
Engine Type 4 cylinder 4 stroke horizontally opposed
4 cylinder 4 stroke horizontally opposed
Reduction Gear 2.43:1 2.43:1
Exhaust System Rotax underslung muffler Rotax underslung muffler
10.1 Manuals approved for use with this aircraft (a) P&M Aviation Ltd manual ref : CTSL Man current issue (b) Rotax 912 engine (all versions) operators manual current issue
CIVIL AVIATION AUTHORITY – SAFETY AND AIRSPACE REGULATION GROUP
MICROLIGHT TYPE APPROVAL DATA SHEET (TADS)
NO: BM-83 ISSUE: 1
TADS BM-83 Issue 1 5 of 12
10.2 The following placards are to be fitted (see manual for full set)
Main Placard, LH window pillar by pilot’s head:
On main panel: At each filler cap:
LIMITATIONS: CTSL
P&M SERIAL NO EMPTY WEIGHT (MAX EMPTY WEIGHT 291.5KG) MAX AUW 472.5KG
TOTAL LOAD FUEL 55- KG 130L(FULL) KG 72L KG 31L 172 KG 13L
Vso FLAPS 35O 34KT VS1 FLAPS –12O 48KT VFe MAX FLAPS 66KT Va MANOEUVRE 89KT Vc CRUISE 118KT Vne 150KT MAX CONTIN RPM 4400 OIL PRESS (3500+ rpm) 2-5BAR OIL TEMP MAX 130OC CHT MAX 135 OC COOLANT (WATER/GLYCOL) 120 OC COOLANT (100% GLYCOL) 135 OC NON-AEROBATIC, NO INTENTIONAL SPINS. MANOEUVRE LIMITS +3.8G, -1.5G
CIVIL AVIATION AUTHORITY – SAFETY AND AIRSPACE REGULATION GROUP
MICROLIGHT TYPE APPROVAL DATA SHEET (TADS)
NO: BM-83 ISSUE: 1
TADS BM-83 Issue 1 6 of 12
At cowl hatch: At baggage door:
At throttle control console:
CIVIL AVIATION AUTHORITY – SAFETY AND AIRSPACE REGULATION GROUP
MICROLIGHT TYPE APPROVAL DATA SHEET (TADS)
NO: BM-83 ISSUE: 1
TADS BM-83 Issue 1 7 of 12
Flap, magnetos, fuel valve and circuit breakers on main panel lower section:
Adjacent to parachute handle between seats:
WARNING – EMERGENCY PARACHUTE REMOVE PIN BEFORE FLIGHT.
1) TURN IGNITION OFF 2) PULL HANDLE
CIVIL AVIATION AUTHORITY – SAFETY AND AIRSPACE REGULATION GROUP
MICROLIGHT TYPE APPROVAL DATA SHEET (TADS)
NO: BM-83 ISSUE: 1
TADS BM-83 Issue 1 8 of 12
On fuselage top, behind wing on the parachute panel:
CIVIL AVIATION AUTHORITY – SAFETY AND AIRSPACE REGULATION GROUP
MICROLIGHT TYPE APPROVAL DATA SHEET (TADS)
NO: BM-83 ISSUE: 1
TADS BM-83 Issue 1 9 of 12
(11) MANDATORY MODIFICATIONS / SERVICE BULLETINS / AIRWORTHINESS DIRECTIVES ETC: Nil (12) MINIMUM PERFORMANCE AT MAX TAKE-OFF WEIGHT
Rate of Climb: 1000 fpm at 60kt IAS Stall or Minimum Flying Speed: 34kt IAS at MTOW / idle
CIVIL AVIATION AUTHORITY – SAFETY AND AIRSPACE REGULATION GROUP
MICROLIGHT TYPE APPROVAL DATA SHEET (TADS)
NO: BM-83 ISSUE: 1
TADS BM-83 Issue 1 10 of 12
Issue History
Issue No. Reason and signatory
1 05 Jan 2015 Initial Issue A C Love
CIVIL AVIATION AUTHORITY – SAFETY AND AIRSPACE REGULATION GROUP
MICROLIGHT TYPE APPROVAL DATA SHEET (TADS)
NO: BM-83 ISSUE: 1
TADS BM-83 Issue 1 11 of 12
ANNEX A – MANDATORY MODIFICATIONS
None
ANNEX B - APPROVED OPTIONAL MODIFICATIONS
The installation of all optional modifications is to be inspected by a BMAA inspector and an entry made in the appropriate logbook(s). Note that other approved modifications may exist which are not listed here.
Mod ref Description Notes Issued
BMAA AAN 1018 Manual trim option As per CTSW 22/06/06
ANNEX C - WEIGHING INFORMATION
1. CG Datum: Leading edge of wing at any point (except stall strips)
In accordance with Article 41(1) of The Air Navigation Order 2016, as amended, the following action required by this Mandatory Permit Directive (MPD) is mandatory for applicable aircraft registered in the United Kingdom operating on a UK CAA Permit to Fly.
Applicability: All Microlights where P & M Aviation Ltd is the Type Approval Holder: TADS No. Aircraft Type TADS No. Aircraft Type BM2 Gemini Sprint BM43 Mainair Mercury BM3 Tri-Flyer Sprint BM44 Pegasus Quasar 2 TC BM4 Gemini Flash BM45 Cyclone AX3//503 BM5
Reason: Following maintenance, a clevis pin came out of the RP-4 roll trim system pulley on a QuikR causing a left turn. The split ring securing the clevis pin had come out. It is not known if the ring was disturbed during the maintenance. The split ring which came out was the same “spiral start” pattern as that which has caused trouble before (see Service Bulletin 139). This pattern of ring has no positive stop, so that simple rotation of the ring (e.g. caused by it getting caught on something) will cause it to disengage. Disengagement of the split ring and subsequent clevis pin departure could affect the control of the aircraft.
Effective Date: 24 November 2016
Compliance/Action: Compliance is required as follows, unless previously accomplished:
1. Before further flight, from the effective date of this MPD, inspect all clevis pin / split ring installations on the aircraft in accordance with paragraph 2 of P & M Aviation Ltd Service Bulletin 144.
2. If the inspection in paragraph 1 reveals any spiral start pattern split rings they must be replaced in accordance with paragraph 2 of P & M Aviation Ltd Service Bulletin 144 before further flight.
3. Record the inspection from paragraph 1 and any necessary rectification action from paragraph 2 in the aircraft technical log in accordance with paragraph 3 of P & M Aviation Ltd Service Bulletin 144.
4. Repeat the actions in paragraphs 1, 2 and 3 at each Permit to Fly revalidation.
ENSURE COMPLIANCE WITH THIS MPD IS RECORDED IN THE AIRCRAFT LOGBOOK
Reference Publications:
P & M Aviation Ltd Service Bulletin Number 144, Issue 3, dated 27 October 2016.
Remarks: 1. This MPD was not posted for consultation because of the urgency of the requirement.
2. Enquiries regarding this Mandatory Permit Directive should be referred
to: GA Unit, Civil Aviation Authority, Safety and Airspace Regulation Group, Aviation House, Gatwick Airport South, West Sussex, RH6 0YR.