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Allstar PZL Glider SZD-54-2 Perkoz Flight Manual

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Allstar PZL Glider
Sp. z o.o.
FLIGHT MANUAL
for a sailplane
SZD-54-2 „Perkoz"
Model:
Serial No.:
Registration:
THIS FLIGHT MANUAL IS A DIRECT TRANSLATION FROM THE EASA APPROVED POLISH
VERSION
TRANSLATION OF THIS DOCUMENT AND CONVERSION OF TECHNICAL DATA HAVE BEEN
DONE BY BEST KNOWLEDGE AND JUDGMENT
IN ANY CASE OF DISCREPANCIES IN TRANSLATION THE POLISH VERSION SHOULD BE USED
T
HIS SAILPLANE IS TO BE OPERATED IN COMPLIANCE WITH INFORMATION AND LIMITATIONS
. T
.
CONTAINED HEREIN
HIS DOCUMENT SHOULD BE ALWAYS STORED ON BOARD
Doc No. 542.4.01
Issue II  April 2014
corrected

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  • Page 1 Allstar PZL Glider Sp. z o.o. FLIGHT MANUAL for a sailplane SZD-54-2 „Perkoz” Model: Serial No.: Registration: THIS FLIGHT MANUAL IS A DIRECT TRANSLATION FROM THE EASA APPROVED POLISH VERSION TRANSLATION OF THIS DOCUMENT AND CONVERSION OF TECHNICAL DATA HAVE BEEN...
  • Page 2 Note to English version, Issue II ‒ April 2014, corrected: By the way of the Revision No. 2 implementation, the whole Flight Manual in English was checked and corrected in order to eliminate mistakes found and to be in line with Polish version. The corrections are not indicated to achieve compatibility with Polish version, however all pages are marked with “corrected”...
  • Page 3 Record of revisions................... 0.2 0.2. List of effective pages ................0.4 0.3. Table of contents ..................0.5 0.4. Table of figures ..................0.6 Issue II April 2014 Allstar PZL Glider Sp. z o.o. page 0.1 Revision Doc No. 542.4.01 corrected...
  • Page 4 2.2, 2.3, 2.4, 2.5, 26.07.2017 2.6, 2.8, 2.9, 2.10 4.14, 4.15, 4.17 6.3, 6.8, 6.9 7.4, 7.8, 7.10, 7.11, 7.12, 7.13 Allstar PZL Glider Sp. z o.o. Issue II April 2014 page 0.2 Doc No. 542.4.01 Revision No. 2 May 2017...
  • Page 5 SECTION 0. FLIGHT MANUAL „Perkoz” ISSUANCES Rev. Affected Date of No. and Date of Insertion Affected Pages Section Issue Approval Date & Signature Issue II April 2014 Allstar PZL Glider Sp. z o.o. page 0.3 Revision Doc No. 542.4.01 corrected...
  • Page 6 April 2014 4.15 May 2017 April 2014 4.16 April 2014 List of pages for Supplements is enclosed in page 9.3 Allstar PZL Glider Sp. z o.o. Issue II April 2014 page 0.4 Doc No. 542.4.01 Revision No. 2 May 2017...
  • Page 7 SECTION 5. PERFORMANCE SECTION 6. MASS AND BALANCE SECTION 7. SAILPLANE AND SYSTEMS DESCRIPTION SECTION 8. SAILPLANE HANDLING, CARE AND MAINTENANCE SECTION 9. SUPPLEMENTS Issue II April 2014 Allstar PZL Glider Sp. z o.o. page 0.5 Revision Doc No. 542.4.01 corrected...
  • Page 8 Fig. 7-1. Cockpit equipment and controls..............7.3 Fig. 7-2. Instrument panel at front seat ..............7.6 Fig. 7-3. Instrument panel at rear seat ..............7.6 Fig. 7-4. Scheme of electric installation ..............7.8 Allstar PZL Glider Sp. z o.o. Issue II April 2014 page 0.6 Doc No.
  • Page 9 Certification basis ..................1.2 1.3. Warnings, cautions and notes ..............1.2 1.4. Description and technical data ..............1.3 1.5. Three-view drawing .................. 1.5 Issue II April 2014 Allstar PZL Glider Sp. z o.o. page 1.1 Revision Doc No. 542.4.01 corrected...
  • Page 10 NOTE : draws the attention on any special item not directly related to safety but which is important or unusual. Allstar PZL Glider Sp. z o.o. Issue II April 2014 page 1.2 Doc No. 542.4.01...
  • Page 11 Control systems for elevator, ailerons and airbrakes – pushrod type. Rudder control system mixed: cable/pushrod. Longitudinal trim control – spring type. Tow release control – cable type. Wheel brake operated with Bowden cable. Issue II April 2014 Allstar PZL Glider Sp. z o.o. page 1.3 Revision Doc No. 542.4.01 corrected...
  • Page 12 Category „U” 1356 1356 [lb] Maximum in-flight mass Category „A” 1301 ---- [lb] Maximum wing loading 7,70 7,28 [lb/ft Allstar PZL Glider Sp. z o.o. Issue II April 2014 page 1.4 Doc No. 542.4.01 Revision No. 2 May 2017 corrected...
  • Page 13 SZD-54-2 SECTION 1. FLIGHT MANUAL „Perkoz” GENERAL 1.5. Three-view drawing Fig. 1-1. 3-view drawing Issue II April 2014 Allstar PZL Glider Sp. z o.o. page 1.5 Revision Doc No. 542.4.01 corrected...
  • Page 14 SZD-54-2 SECTION 1. FLIGHT MANUAL „Perkoz” GENERAL Intentionally left blank Allstar PZL Glider Sp. z o.o. Issue II April 2014 page 1.6 Doc No. 542.4.01 Revision corrected...

  • Page 15: Table Of Contents

    2.11. Aero-tow and winch-launching ..............2.9 2.11.1. Aero-tow ................... 2.9 2.11.2. Winch-launched take-off ..............2.9 2.12. Other limitations ..................2.9 2.13. Limitation placards ................... 2.10 Issue II April 2014 Allstar PZL Glider Sp. z o.o. page 2.1 Revision Doc No. 542.4.01 corrected...

  • Page 16: Introduction

    (152) (144) (137) (129) (122) (115) (109) (102) IAS kn (mph) (167) (158) (150) (142) (135) (127) (120) (113) Allstar PZL Glider Sp. z o.o. Issue II April 2014 page 2.2 Doc No. 542.4.01 Revision No. 2 May 2017 corrected...

  • Page 17: Airspeed Indicator Markings

    Approach speed at maximum mass = sailplane stalling speed at given mass, with airbrakes retracted. Fig. 2-1 Airspeed indicator colour marking Issue II April 2014 Allstar PZL Glider Sp. z o.o. page 2.3 Revision No. 2 May 2017 Doc No. 542.4.01...

  • Page 18: Mass

    Observation of all limitations relating to sailplane load plan, as well as these relating to CG range limits of sailplane without pilots, ensures to maintain the sailplane CG within the range allowed for flight. Allstar PZL Glider Sp. z o.o. Issue II April 2014 page 2.4 Doc No.

  • Page 19: Approved Manoeuvres

    The recommended entry speed for particular manoeuvres is given in Section 4. (item 4.6.9.). Issue II April 2014 Allstar PZL Glider Sp. z o.o. page 2.5 Revision No. 2 May 2017 Doc No. 542.4.01 corrected...

  • Page 20: Manoeuvring Load Factors

    Accelerometer markings Marking Value Significance + 7,0 Allowable manoeuvring load factors Red line - 5,0 for Aerobatic Category sailplane Allstar PZL Glider Sp. z o.o. Issue II April 2014 page 2.6 Doc No. 542.4.01 Revision No. 2 May 2017 corrected...

  • Page 21: Flight Crew

    In solo flying – placed in the side pocket or on the rear seat and fixed with safety harness. Issue II April 2014 Allstar PZL Glider Sp. z o.o. page 2.7 Revision Doc No. 542.4.01...

  • Page 22: Kinds Of Operation

    “Equipment list”, the sample of which is enclosed in the item 18.1. of the Technical Service Manual. Additional equipment can be installed on the sailplane as described in items 8.2 and 8.3 of the Technical Service Manual. Allstar PZL Glider Sp. z o.o. Issue II April 2014 page 2.8 Doc No.

  • Page 23: Aero-Tow And Winch-Launching

    WARNING: Aerobatics in rough air are forbidden. NOTE: Flying in weather conditions conducive to lightning is to be avoided. Issue II April 2014 Allstar PZL Glider Sp. z o.o. page 2.9 Revision No. 2 May 2017 Doc No. 542.4.01 corrected...

  • Page 24: Limitation Placards

    – means: allowed, provided the maximum in-flight mass of the glider in a given category is not exceeded. NOTE: All placards and their location are presented in the item 7.10. Allstar PZL Glider Sp. z o.o. Issue II April 2014 page 2.10 Doc No.
  • Page 25 3.7.1. Transition from inverted to normal flight ..........3.5 3.7.2. Landing with ground loop ..............3.5 3.7.3. Break or inadvertent release of towing cable ........3.6 Issue II April 2014 Allstar PZL Glider Sp. z o.o. page 3.1 Revision Doc No. 542.4.01 corrected...

  • Page 26: Introduction

    (handles are coupled). NOTE: If the canopy cannot be jettisoned, break out the perspex starting at the side window. Use the leg force, if necessary. Allstar PZL Glider Sp. z o.o. Issue II April 2014 page 3.2 Doc No. 542.4.01...

  • Page 27: Stall Recovery

    The sailplane pitches symmetrically. Recovery ensues troubleless and reliably by pulling the control stick. In recovery from stall with pitch beyond 30º normal operation of controls is sufficient. Issue II April 2014 Allstar PZL Glider Sp. z o.o. page 3.3 Revision Doc No. 542.4.01 corrected...

  • Page 28: Spin Recovery

     move back the rudder to neutral and pull out sailplane from dive. Recovery ensues without delay. Altitude loss, between initiation of recovery and regaining level flight, is 984 ft. Allstar PZL Glider Sp. z o.o. Issue II April 2014 page 3.4...

  • Page 29: Recovery From Spiral Dive

     while turning, maintain with control stick longitudinal balance to keep the nose and tail wheels above the ground, and deflect rudder opposite to the turn. Issue II April 2014 Allstar PZL Glider Sp. z o.o. page 3.5 Revision No. 2 May 2017 Doc No.

  • Page 30: Break Or Inadvertent Release Of Towing Cable

     tighten shoulder belts,  select place for landing,  land off-field or - if at all possible – on the airfield. Intentionally left blank Allstar PZL Glider Sp. z o.o. Issue II April 2014 page 3.6 Doc No. 542.4.01...
  • Page 31 4.6.5. Approach ..................4.15 4.6.6. Landing ..................... 4.15 4.6.7. High altitude flight ................4.15 4.6.8. Flight in rain ..................4.15 4.6.9. Aerobatics ..................4.16 Issue II April 2014 Allstar PZL Glider Sp. z o.o. page 4.1 Revision Doc No. 542.4.01 corrected...

  • Page 32: Introduction

    7. Secure the main bolt (10), connecting the handle of main bolt (11) with fuselage frame by means of safety pin (13). 8. Secure the wing front pins (3) by means of cotter pins (20). Allstar PZL Glider Sp. z o.o. Issue II April 2014 page 4.2...

  • Page 33: Wings De-Rigging

    Pull down the bolt (3) onto stop, by means of screwed-in key (6), hold in the „unlocked” position and shove-out the wingtip from wing socket. Issue II April 2014 Allstar PZL Glider Sp. z o.o. page 4.3 Revision Doc No. 542.4.01...
  • Page 34 22. Spar fitting, 23. Socket nut, 24. Root rib, 25. Wing upper and lower skin shell, 26. Fuselage shell, 27. Wing spars. Allstar PZL Glider Sp. z o.o. Issue II April 2014 page 4.4 Doc No. 542.4.01 Revision No. 1...
  • Page 35 SZD-54-2 SECTION 4. FLIGHT MANUAL „Perkoz” NORMAL PROCEDURES Fig. 4-1. Wings rigging Issue II April 2014 Allstar PZL Glider Sp. z o.o. page 4.5 Revision No. 1 July 2015 Doc No. 542.4.01 corrected...
  • Page 36 2. Nest socket 3. Bolt 4. Pin 5. Sleeve 6. Wingtip mounting key (Fig. 4‒2. in TSM) Fig. 4-2. Assembling winglets or plane wingtips Allstar PZL Glider Sp. z o.o. Issue II April 2014 page 4.6 Doc No. 542.4.01 Revision corrected...

  • Page 37: Assembling And Disassembling Long Wingtips

    1. Pull down the bolt (3) onto stop, by means of screwed-in key (10), hold in the “unlocked” position; 2. Shove-out the wingtip from wing socket. Issue II April 2014 Allstar PZL Glider Sp. z o.o. page 4.7 Revision Doc No. 542.4.01 corrected...
  • Page 38 6. Outer part of aileron clutch 7. Inner part of aileron clutch 8. Latch pin 9. Long wingtip aileron (outer) 10. Wingtip mounting key (Section 4. in TSM) Allstar PZL Glider Sp. z o.o. Issue II April 2014 page 4.8 Doc No. 542.4.01...
  • Page 39 NORMAL PROCEDURES Fig. 4-4. Detail A of the wing – long wingtip connection Fig. 4-5. Detail B of the wing – long wingtip connection Issue II April 2014 Allstar PZL Glider Sp. z o.o. page 4.9 Revision Doc No. 542.4.01 corrected...

  • Page 40: Horizontal Tailplane Assembling

    14 - Elevator mass balance 7 - Rudder 15 - Screw 8 - End lever 16 - Castellated nut 17 - Cotter pin Allstar PZL Glider Sp. z o.o. Issue II April 2014 page 4.10 Doc No. 542.4.01 Revision corrected...
  • Page 41 SZD-54-2 SECTION 4. FLIGHT MANUAL „Perkoz” NORMAL PROCEDURES Fig. 4-6. Horizontal tailplane assembling Issue II April 2014 Allstar PZL Glider Sp. z o.o. page 4.11 Revision Doc No. 542.4.01 corrected...

  • Page 42: Daily Inspection

    – placard on RH cockpit side), in necessity calculate the resultant CG position (item 6.3.).  Correct installation of balancing weights (if installed).  Back rest correct installation and securing. Allstar PZL Glider Sp. z o.o. Issue II April 2014 page 4.12 Doc No.

  • Page 43: Procedure Before Take-Off

     in steep, stabilized climb the control stick forces can be trimmed. 54 ÷ 62 kn (59÷68 mph). Recommended winch-launching speed: Issue II April 2014 Allstar PZL Glider Sp. z o.o. page 4.13 Revision Doc No. 542.4.01 corrected...

  • Page 44: Aero-Towed Take-Off And Climb

    Complete service by the pilot for SP3 stall warning device is described in document “Stall Warning Device ANTI-STALL SP3, Flight Manual, Issue 1, dated 23.03.1995”, to be provided together with Fight Manual, in case of installation of anti- stall device. Allstar PZL Glider Sp. z o.o. Issue II April 2014 page 4.14 Doc No.

  • Page 45: Side-Slip

    It is recommended to dry the rain-soaked sailplane after flight, and before take-off – when soaked in standstill. Issue II April 2014 Allstar PZL Glider Sp. z o.o. page 4.15 Revision No. 2 May 2017 Doc No. 542.4.01...

  • Page 46: Aerobatics

    65 ÷ 81 kn (75÷93 mph) airspeed. WARNING: Remember on limitations to sailplane mass in Aerobatic Category. WARNING: Advanced and competition aerobatics in calm air only. Allstar PZL Glider Sp. z o.o. Issue II April 2014 page 4.16 Doc No. 542.4.01 Revision...
  • Page 47 - 2 / + 3,5 tail slide + 4 / - 2 eight 108 (124) barrel roll 97 (112) Issue II April 2014 Allstar PZL Glider Sp. z o.o. page 4.17 Revision No. 2 May 2017 Doc No. 542.4.01 corrected...
  • Page 48 SZD-54-2 SECTION 4. FLIGHT MANUAL „Perkoz” NORMAL PROCEDURES Intentionally left blank Allstar PZL Glider Sp. z o.o. Issue II April 2014 page 4.18 Doc No. 542.4.01 Revision corrected...
  • Page 49 5.2.1. Airspeed indicator system calibration ..........5.2 5.2.2. Stall speeds ..................5.5 5.3. Additional, non-approved information ............5.5 5.3.1. Demonstrated cross-wind performance ..........5.5 5.3.2. Speed polar ..................5.6 Issue II April 2014 Allstar PZL Glider Sp. z o.o. page 5.1 Revision Doc No. 542.4.01 corrected...

  • Page 50: Introduction

    CAS - Calibrated Airspeed - instrument reading corrected for instrument error and aerodynamic calibration error. IAS - Indicated Airspeed – instrument reading corrected for instrument error only. IAS values presented in this Manual are given assuming zero instrument error. Allstar PZL Glider Sp. z o.o. Issue II April 2014 page 5.2 Doc No.
  • Page 51 SZD-54-2 SECTION 5. FLIGHT MANUAL „Perkoz” PERFORMANCE Fig. 5-1. AIS calibration – normal flight Issue II April 2014 Allstar PZL Glider Sp. z o.o. page 5.3 Revision Doc No. 542.4.01 corrected...
  • Page 52 SZD-54-2 SECTION 5. FLIGHT MANUAL „Perkoz” PERFORMANCE Fig. 5-2. AIS calibration – inverted flight Allstar PZL Glider Sp. z o.o. Issue II April 2014 page 5.4 Doc No. 542.4.01 Revision corrected...

  • Page 53: Stall Speeds

    ........ 8 kn (9,3 mph), in winch-launched take-off ......8 kn (9,3 mph), in landing ........... 8 kn (9,3 mph). Issue II April 2014 Allstar PZL Glider Sp. z o.o. page 5.5 Revision No. 2 May 2017 Doc No. 542.4.01...

  • Page 54: Speed Polar

    SZD-54-2 SECTION 5. FLIGHT MANUAL „Perkoz” PERFORMANCE 5.3.2. Speed polar Fig. 5-3. Speed polar without winglet Allstar PZL Glider Sp. z o.o. Issue II April 2014 page 5.6 Doc No. 542.4.01 Revision corrected...
  • Page 55 SZD-54-2 SECTION 5. FLIGHT MANUAL „Perkoz” PERFORMANCE Fig. 5-4. Speed polar with winglet Issue II April 2014 Allstar PZL Glider Sp. z o.o. page 5.7 Revision Doc No. 542.4.01 corrected...
  • Page 56 SZD-54-2 SECTION 5. FLIGHT MANUAL „Perkoz” PERFORMANCE Fig. 5-5. Speed polar with long wingtips (65,62 ft wing span) Allstar PZL Glider Sp. z o.o. Issue II April 2014 page 5.8 Doc No. 542.4.01 Revision corrected...
  • Page 57 6.3. Method for calculation of sailplane CG position ........6.4 6.4. Weight and balance record ..............6.6 6.5. Individual loading plan ................6.8 Issue II April 2014 Allstar PZL Glider Sp. z o.o. page 6.1 Revision Doc No. 542.4.01 corrected...
  • Page 58 Allowed range of mass (m ) and CG position (X ) of sailplane without pilots is given in a diagram (Fig. 6‒1.) – dashed area. Allstar PZL Glider Sp. z o.o. Issue II April 2014 page 6.2 Doc No. 542.4.01...
  • Page 59 SZD-54-2 SECTION 6. FLIGHT MANUAL „Perkoz” MASS AND BALANCE Fig. 6-1. CG range limits for a sailplane without pilots Issue II April 2014 Allstar PZL Glider Sp. z o.o. page 6.3 Revision No. 2 May 2017 Doc No. 542.4.01 corrected...
  • Page 60 4,33 3,35 When using back cushion for a short pilot, the cushion thickness must be value – respectively. added to the X or X Allstar PZL Glider Sp. z o.o. Issue II April 2014 page 6.4 Doc No. 542.4.01 Revision...
  • Page 61  For 65,62 ft wing span version: SCO = 37,756 in – length of MSC – = 1,969 in distance of MSC leading edge point from reference datum. Issue II April 2014 Allstar PZL Glider Sp. z o.o. page 6.5 Revision Doc No. 542.4.01 corrected...
  • Page 62 57,42 ft wing span Weighing or CG calculation record mass CG position made by [lb] [in] name / signature Document type Date Allstar PZL Glider Sp. z o.o. Issue II April 2014 page 6.6 Doc No. 542.4.01 Revision corrected...
  • Page 63 65,62 ft wing span Weighing or CG calculation record mass CG position made by [lb] [in] name / signature Document type Date Issue II April 2014 Allstar PZL Glider Sp. z o.o. page 6.7 Revision Doc No. 542.4.01 corrected...
  • Page 64 (you can use the file “Individual loading plan.xlsx” available at producer). Fig. 6-3. Table of individual loading plan with sample values Allstar PZL Glider Sp. z o.o. Issue II April 2014 page 6.8 Doc No.
  • Page 65 242 must be used). The results are to be entered in corresponding box of the table (yellow or pink). Fig. 6-4. Sample of individual loading plan table Issue II April 2014 Allstar PZL Glider Sp. z o.o. page 6.9 Revision No. 2 May 2017 Doc No. 542.4.01...
  • Page 66 SZD-54-2 SECTION 6. FLIGHT MANUAL „Perkoz” MASS AND BALANCE Intentionally left blank Allstar PZL Glider Sp. z o.o. Issue II April 2014 page 6.10 Doc No. 542.4.01 Revision corrected...
  • Page 67 ..7.13 7.10.7. Table „Individual loading plan” ............7.13 7.10.8. Compass deviation table ..............7.14 7.10.9. Table „Pre-flight checklist” ..............7.14 Issue II April 2014 Allstar PZL Glider Sp. z o.o. page 7.1 Revision Doc No. 542.4.01 corrected...

  • Page 68: Introduction

    15 - lock trigger of longitudinal trim device 16 - lever of wheel brake 17 - microphone 18 - push to talk button 19 - document pocket 20 - telescopic slide Allstar PZL Glider Sp. z o.o. Issue II April 2014 page 7.2 Doc No. 542.4.01 Revision...
  • Page 69 SECTION 7. SZD-54-2 FLIGHT MANUAL SAILPLANE AND „Perkoz” SYSTEMS DESCRIPTION Fig. 7-1. Cockpit equipment and controls Issue II April 2014 Allstar PZL Glider Sp. z o.o. page 7.3 Revision Doc No. 542.4.01 corrected...

  • Page 70: Cockpit Controls

    Setting up the longitudinal trim is done by moving the lever forward or backward. Locking of mechanism is accomplished in desired position after releasing lever which returns to the original position influenced by the spring. Allstar PZL Glider Sp. z o.o. Issue II April 2014 page 7.4...

  • Page 71: Airbrakes Control

    Do not actuate wheel brake during inverted flight and aerobatics with negative loads – this may cause air to enter the brake and therefore brake failure. Issue II April 2014 Allstar PZL Glider Sp. z o.o. page 7.5 Revision Doc No. 542.4.01 corrected...

  • Page 72: Instrument Panels

    V - variometer S - switch of SP3 stall warning device Fig. 7-2. Instrument panel at front seat Fig. 7-3. Instrument panel at rear seat Allstar PZL Glider Sp. z o.o. Issue II April 2014 page 7.6 Doc No. 542.4.01...

  • Page 73: Board Instrument System

    Using a back cushion for low height pilot is acceptable. Sailplane standard equipment includes 5-point safety harness for both crew members, with optionally, 2nd lap belt. Issue II April 2014 Allstar PZL Glider Sp. z o.o. page 7.7 Revision Doc No. 542.4.01 corrected...

  • Page 74: Baggage Compartment

    In installation with at least two batteries, power switching should occur after voltage drop to 10,5 V. Observe the voltage indicator on VHF panel and – if installed – the stall warning device diode. Allstar PZL Glider Sp. z o.o. Issue II April 2014 page 7.8...

  • Page 75: Miscellaneous Equipment

    Models of equipment allowed for installation on the SZD-54-2 „Perkoz” sailplane, together with requirements for such installation, are specified in the item 8.2. of the Technical Service Manual. Issue II April 2014 Allstar PZL Glider Sp. z o.o. page 7.9 Revision Doc No. 542.4.01 corrected...

  • Page 76: Information Tables

    Removable balance RH cockpit board in front weights of front seat pan Front and rear control Wheel brake stick Allstar PZL Glider Sp. z o.o. Issue II April 2014 page 7.10 Doc No 542.4.01 Revision No. 2 May 2017 corrected...

  • Page 77: Limitation Table " Maximum Allowed Airspeed

    Maximum total load on both seats and in baggage compartment – see Individual Loading Plan for this sailplane! Location:  LH cockpit board by front and rear seat Issue II April 2014 Allstar PZL Glider Sp. z o.o. page 7.11 Revision No. 2 May 2017 Doc No. 542.4.01 corrected...
  • Page 78 58,0 psi 36,3 psi Front Wheel Main Wheel Tail Wheel Location :  painted near particular wheels on sailplane fuselage. Allstar PZL Glider Sp. z o.o. Issue II April 2014 page 7.12 Doc No. 542.4.01 Revision No. 2 May 2017...

  • Page 79: Limitation Table „Allowed

    – using the sample showed below and method of filling given in the item 6.5. of the FM. Location :  RH cockpit board by front and rear seat. Issue II April 2014 Allstar PZL Glider Sp. z o.o. page 7.13 Revision No. 2 May 2017 Doc No. 542.4.01 corrected...

  • Page 80: Compass Deviation Table

    10. Transceiver CHECK 11. Stall warning device 12. Towing cable connection CHECK Location :  RH cockpit board by front and rear seat. Allstar PZL Glider Sp. z o.o. Issue II April 2014 page 7.14 Doc No. 542.4.01 Revision corrected...
  • Page 81 Ground handling / road transport ............. 8.2 8.4.1. Ground handling ................8.2 8.4.2. Road transport .................. 8.3 8.5. Cleaning and care ..................8.4 Issue II April 2014 Allstar PZL Glider Sp. z o.o. page 8.1 Revision Doc No. 542.4.01 corrected...
  • Page 82 NOTE: Leaving sailplane outside, without protection against environmental conditions and sunlight, harmfully affects durability of the lacquer coat. Allstar PZL Glider Sp. z o.o. Issue II April 2014 page 8.2 Doc No. 542.4.01 Revision corrected...
  • Page 83  airbrake handle in cockpit immobilized in „closed” position,  aileron and airbrake control system torsional tube ends immobilized in openings in fuselage shell, Issue II April 2014 Allstar PZL Glider Sp. z o.o. page 8.3 Revision Doc No. 542.4.01 corrected...
  • Page 84 The safety belts should be regularly inspected against evidence of tear, or wear, corroded fittings etc. Depending on belts model regularly check the correct functioning of belts fastener or lock. Allstar PZL Glider Sp. z o.o. Issue II April 2014 page 8.4...
  • Page 85 SECTION 9. SUPPLEMENTS 9.1. Introduction ....................9.2 9.2. List of inserted supplements ..............9.2 9.3. Supplements - List of actual pages ............9.3 Issue II April 2014 Allstar PZL Glider Sp. z o.o. page 9.1 Revision Doc No. 542.4.01 corrected...
  • Page 86 9.2. List of inserted supplements Supplement Confirmation of the Date of issue Supplement title application on S/N Allstar PZL Glider Sp. z o.o. Issue II April 2014 page 9.2 Doc No. 542.4.01 Revision corrected...
  • Page 87 SECTION 9. FLIGHT MANUAL „Perkoz” SUPPLEMENTS 9.3. Supplements – List of actual pages Supplement Supplement Page Date of issue Page Date of issue Issue II April 2014 Allstar PZL Glider Sp. z o.o. page 9.3 Revision Doc No. 542.4.01 corrected...
  • Page 88 SZD-54-2 SECTION 9. FLIGHT MANUAL „Perkoz” SUPPLEMENTS Intentionally left blank Allstar PZL Glider Sp. z o.o. Issue II April 2014 page 9.4 Doc No. 542.4.01 Revision corrected...

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