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Allstar PZL Glider SZD-54-2 Perkoz Technical & Service Manual

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Allstar PZL Glider
Sp. z o.o.
TECHNICAL SERVICE
MANUAL
for a sailplane
SZD-54-2 „Perkoz"
Model:
Serial No.:
Registration:
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
THIS MANUAL IS TO BE ALWAYS AVAILABLE DURING ROUTINE MAINTENANCE OPERATION,
INSPECTION AND PERIODIC WORKS.
Doc No. 542.4.02
Issue II  April 2014
corrected

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  • Page 1 Allstar PZL Glider Sp. z o.o. TECHNICAL SERVICE MANUAL for a sailplane SZD-54-2 „Perkoz” Model: Serial No.: Registration: 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 THIS MANUAL IS TO BE ALWAYS AVAILABLE DURING ROUTINE MAINTENANCE OPERATION, INSPECTION AND PERIODIC WORKS.
  • Page 2 Note to English version, Issue II ‒ April 2014, corrected: By the way of the Revision No. 2 implementation, the whole Technical Service 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 15.1, 15.2, 15.3, 15.4, 16.1, 16.7, 16.9, 16.10 17.4, 17.10, 17.18, 17.20, 17.24, 17.28, 17.30 18.4, 18.10, 18.11, 18.12 Issue II April 2014 Allstar PZL Glider Sp. z o.o. page 0.1 Revision No. 2 May 2017 Doc No. 542.4.02 corrected...
  • Page 4 SECTION 0. TECHNICAL SERVICE MANUAL „Perkoz” ISSUANCES Rev. Affected Date of Insertion Affected Pages No. and Date of Approval Section Issue Date & Signature Allstar PZL Glider Sp. z o.o. Issue II April 2014 page 0.2 Doc No. 542.4.02 Revision corrected...
  • Page 5 SECTION 0. TECHNICAL SERVICE MANUAL „Perkoz” ISSUANCES Rev. Affected Date of Insertion Affected Pages No. and Date of Approval Section Issue Date & Signature Issue II April 2014 Allstar PZL Glider Sp. z o.o. page 0.3 Revision Doc No. 542.4.02 corrected...
  • Page 6 April 2014 2.21 April 2014 May 2017 2.22 May 2017 April 2014 2.23 April 2014 May 2017 2.24 April 2014 Allstar PZL Glider Sp. z o.o. Issue II April 2014 page 0.4 Doc No. 542.4.02 Revision No. 2 May 2017 corrected...
  • Page 7 19.2 April 2014 16.9 May 2017 16.10 May 2017 List of pages for Supplements is enclosed in page 19.2. Issue II April 2014 Allstar PZL Glider Sp. z o.o. page 0.5 Revision No. 2 May 2017 Doc No. 542.4.02 corrected...

  • Page 8: Table Of Contents

    Canopy ....................2.18 2.12. Rudder control system ................2.20 2.13. Elevator, aileron and longitudinal trimming control system ....2.22 2.14. Airbrake control system ................ 2.26 Allstar PZL Glider Sp. z o.o. Issue II April 2014 page 0.6 Doc No. 542.4.02 Revision corrected...
  • Page 9 Tire pumping end ................... 4.1 4.2. Wingtips mounting key ................4.1 4.3. Rear fitting assembly key ..............4.2 4.4. Mounting wrench ................... 4.2 Issue II April 2014 Allstar PZL Glider Sp. z o.o. page 0.7 Revision No. 2 May 2017 Doc No. 542.4.02 corrected...
  • Page 10 Service life of elements installed on sailplane ........10.1 10.2.1. Crew safety harness ..............10.1 10.2.2. Tow releases ................10.1 10.2.3. Board instruments ..............10.1 Allstar PZL Glider Sp. z o.o. Issue II April 2014 page 0.8 Doc No. 542.4.02 Revision No. 2 May 2017...
  • Page 11 Rules for operations of cables ............. 16.3 16.8. Inspection of non-accessible areas in control systems ......16.3 16.9. Inspection of main units subjected to fatigue loads ......16.4 Issue II April 2014 Allstar PZL Glider Sp. z o.o. page 0.9 Revision Doc No. 542.4.02 corrected...
  • Page 12 Parts replacement ..............17.27 17.7. Primary and secondary structure ............17.29 17.7.1. Primary structure ................ 17.29 17.7.2. Secondary structure ..............17.30 17.8. Assemblies interchangeability ............. 17.30 Allstar PZL Glider Sp. z o.o. Issue II April 2014 page 0.10 Doc No. 542.4.02 Revision corrected...
  • Page 13 SECTION 19. SUPPLEMENTS ................19.1 19.1. Introduction ..................19.1 19.2. List of inserted supplements ..............19.1 Supplements – List of actual pages ............. 19.2 19.3. Issue II April 2014 Allstar PZL Glider Sp. z o.o. page 0.11 Revision Doc No. 542.4.02 corrected...

  • Page 14: Table Of Figures

    Location of balancing weight in sailplane tail ........7.5 Fig. 7-4. Battery mounting in sailplane tail ............7.5 Fig. 9-1. Inspection of control surfaces balance ..........9.3 Allstar PZL Glider Sp. z o.o. Issue II April 2014 page 0.12 Doc No. 542.4.02 Revision No.
  • Page 15 Reaming of connecting spars main bolt sleeves and rear fittings ..17.25 Fig. 17-28. Way to avoid further cracking of perspex ........17.26 Issue II April 2014 Allstar PZL Glider Sp. z o.o. page 0.13 Revision Doc No. 542.4.02 corrected...
  • Page 16 SZD-54-2 SECTION 0. TECHNICAL SERVICE MANUAL „Perkoz” ISSUANCES Intentionally left blank Allstar PZL Glider Sp. z o.o. Issue II April 2014 page 0.14 Doc No. 542.4.02 Revision corrected...

  • Page 17: Section 1. Description And Technical Data

    Emergency jettison mechanism located on canopy frame, on the right hand side. The canopy equipped with “Röger hook”. Issue II April 2014 Allstar PZL Glider Sp. z o.o. page 1.1 Revision Doc No. 542.4.02 corrected...
  • Page 18  electrical turn indicator with bank indicator  bank indicator for inverted flight  variometer ±60 kn and other equipment listed in Section 8. of this Manual. Allstar PZL Glider Sp. z o.o. Issue II April 2014 page 1.2 Doc No. 542.4.02 Revision No.

  • Page 19: Sailplane Technical Data

    8.1. of this Manual, without balance weights and any load (crew, parachutes, baggage). Maximum in-flight mass In Category „U” 1356 [lb] In Category „A” 1301 [lb] Issue II April 2014 Allstar PZL Glider Sp. z o.o. page 1.3 Revision No. 2 May 2017 Doc No. 542.4.02 corrected...

  • Page 20: Sailplane Three View Drawing

    SECTION 1. SZD-54-2 TECHNICAL SERVICE MANUAL DESCRIPTION AND „Perkoz” TECHNICAL DATA 1.3. Sailplane three view drawing Fig. 1-1. Sailplane 3-view drawing Allstar PZL Glider Sp. z o.o. Issue II April 2014 page 1.4 Doc No. 542.4.02 Revision corrected...

  • Page 21: Crew Mass Balancing

    Dismounting the weight consists in screwing out the screw and removing the weight from a sailplane. Intentionally left blank Issue II April 2014 Allstar PZL Glider Sp. z o.o. page 1.5 Revision Doc No. 542.4.02 corrected...
  • Page 22 SECTION 1. SZD-54-2 TECHNICAL SERVICE MANUAL DESCRIPTION AND „Perkoz” TECHNICAL DATA Intentionally left blank Allstar PZL Glider Sp. z o.o. Issue II April 2014 page 1.6 Doc No. 542.4.02 Revision corrected...

  • Page 23: Section 2. Assembling And Disassembling

     the main bolt (10) connects spar roots with the ball socket (9) mounted in the frame,  the safety pin (13) protects the main bolt. Issue II April 2014 Allstar PZL Glider Sp. z o.o. page 2.1 Revision No. 1 July 2015 Doc No. 542.4.02...
  • Page 24 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 2.2 Doc No. 542.4.02 Revision No. 1...
  • Page 25 SECTION 2. SZD-54-2 TECHNICAL SERVICE MANUAL ASSEMBLING & DISASSEMBLING, „Perkoz” SYSTEMS DESCRIPTION Fig. 2-1. Wings rigging Issue II April 2014 Allstar PZL Glider Sp. z o.o. page 2.3 Revision No. 1 July 2015 Doc No. 542.4.02 corrected...

  • Page 26: Wings Rigging

    De-rigging is to be made in reverse sequence. To remove the main bolt (10), move the wing tips up and down. Disconnection of controls at wing/fuselage junction occurs automatically. Allstar PZL Glider Sp. z o.o. Issue II April 2014 page 2.4 Doc No.

  • Page 27: Assembling And Disassembling Wingtips

    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 2.5 Revision Doc No. 542.4.02...
  • Page 28 1. Spar pin 2. Nest socket 3. Bolt 4. Pin 5. Sleeve 6. Wingtip mounting key (Fig. 4–2.) Fig. 2-2. Assembling wingtip: plane or winglet Allstar PZL Glider Sp. z o.o. Issue II April 2014 page 2.6 Doc No. 542.4.02 Revision corrected...

  • Page 29: 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 2.7 Revision Doc No. 542.4.02 corrected...
  • Page 30 6. Outer part of aileron clutch 7. Inner part of aileron clutch 8. Latch pin 9. Long wingtip aileron (outer) 10. Wingtip mounting key (Fig. 4‒2.) Allstar PZL Glider Sp. z o.o. Issue II April 2014 page 2.8 Doc No. 542.4.02...
  • Page 31 „Perkoz” SYSTEMS DESCRIPTION Fig. 2-4. Detail A of wing - long wingtip connection Fig. 2-5. Detail B of wing - long wingtip connection Issue II April 2014 Allstar PZL Glider Sp. z o.o. page 2.9 Revision Doc No. 542.4.02 corrected...

  • Page 32: Horizontal Tailplane Assembling And Disassembling

    Disassembling is to be accomplished in reverse sequence. Before pulling out stabilizer pins (4) from sleeves (5) slightly lift the tailplane to disconnect cone stabilizer fitting from fuselage fitting (3). Allstar PZL Glider Sp. z o.o. Issue II April 2014 page 2.10...
  • Page 33 13 - Rear web 14 - Elevator mass balance 15 - Screw 16 - Castellated nut 17 - Cotter pin Fig. 2-6. Horizontal tailplane assembling Issue II April 2014 Allstar PZL Glider Sp. z o.o. page 2.11 Revision Doc No. 542.4.02 corrected...

  • Page 34: Elevator Mounting And Dismounting

    2. Remove safety pin and unscrew castellated nut (7) out of hanging axle. 3. Deflect the aileron downwards and sidle out of hinges by moving it towards wing tip. Mounting to be accomplished in reverse sequence. Allstar PZL Glider Sp. z o.o. Issue II April 2014 page 2.12 Doc No.

  • Page 35: Long Wingtip Aileron Dismounting

    2 - Axle 3 - Distance sleeve 4 - Washer 5 - Cotter pin 6 - Nut 7 - Tire Fig. 2-7. Nose wheel mounting Issue II April 2014 Allstar PZL Glider Sp. z o.o. page 2.13 Revision Doc No. 542.4.02 corrected...

  • Page 36: Main Wheel Mounting And Dismounting

    26 - Axle screw 13 - Brake lever on control stick 27 - Front main former 14 - Mudguard 28 - Rear lower former Allstar PZL Glider Sp. z o.o. Issue II April 2014 page 2.14 Doc No. 542.4.02 Revision...
  • Page 37 SECTION 2. SZD-54-2 TECHNICAL SERVICE MANUAL ASSEMBLING & DISASSEMBLING, „Perkoz” SYSTEMS DESCRIPTION Fig. 2-8. Main landing gear Issue II April 2014 Allstar PZL Glider Sp. z o.o. page 2.15 Revision Doc No. 542.4.02 corrected...
  • Page 38 1 - Left half of the hub 2 - Right half of the hub 3 - Brake disk 4 - Connecting screw Fig. 2-9. Main landing wheel hub Allstar PZL Glider Sp. z o.o. Issue II April 2014 page 2.16 Doc No. 542.4.02...

  • Page 39: Main Landing Gear Mounting And Dismounting

    Mounting to be accomplished in reverse sequence. Issue II April 2014 Allstar PZL Glider Sp. z o.o. page 2.17 Revision Doc No. 542.4.02 corrected...

  • Page 40: Canopy

    10 - Canopy hinge fitting 5 - Canopy jettison pull rod 11 - Pin 6 - Lever bracket 12 - Lever 13 - Telescopic slide Allstar PZL Glider Sp. z o.o. Issue II April 2014 page 2.18 Doc No. 542.4.02 Revision...
  • Page 41 SECTION 2. SZD-54-2 TECHNICAL SERVICE MANUAL ASSEMBLING & DISASSEMBLING, „Perkoz” SYSTEMS DESCRIPTION Fig. 2-10. Canopy Issue II April 2014 Allstar PZL Glider Sp. z o.o. page 2.19 Revision Doc No. 542.4.02 corrected...

  • Page 42: Rudder Control System

    23 - Bolt 24 - Safety pin 25 - Connector CAUTION Bolts (23) must be inserted from the centre of cockpit towards fuselage shell. Allstar PZL Glider Sp. z o.o. Issue II April 2014 page 2.20 Doc No. 542.4.02 Revision...
  • Page 43 SECTION 2. SZD-54-2 TECHNICAL SERVICE MANUAL ASSEMBLING & DISASSEMBLING, „Perkoz” SYSTEMS DESCRIPTION Fig. 2-11. Rudder control system Issue II April 2014 Allstar PZL Glider Sp. z o.o. page 2.21 Revision Doc No. 542.4.02 corrected...

  • Page 44: Elevator, Aileron And Longitudinal Trimming Control System

    Use the adjustment grip on a cockpit LH side board to accurate positioning. Locking of mechanism is accomplished automatically after releasing trigger on control stick. Allstar PZL Glider Sp. z o.o. Issue II April 2014 page 2.22 Doc No.
  • Page 45 SECTION 2. SZD-54-2 TECHNICAL SERVICE MANUAL ASSEMBLING & DISASSEMBLING, „Perkoz” SYSTEMS DESCRIPTION Fig. 2-12. Elevator, aileron and trimmer control system in fuselage Issue II April 2014 Allstar PZL Glider Sp. z o.o. page 2.23 Revision Doc No. 542.4.02 corrected...
  • Page 46 11 - Aileron driving lever fitted to rib No. 1 in right wing 12 - Aileron driving latch pins 13 - Outer aileron clutch 14 - Inner aileron clutch 15 - Circlip 16 - Washer Allstar PZL Glider Sp. z o.o. Issue II April 2014 page 2.24 Doc No. 542.4.02 Revision...
  • Page 47 SECTION 2. SZD-54-2 TECHNICAL SERVICE MANUAL ASSEMBLING & DISASSEMBLING, „Perkoz” SYSTEMS DESCRIPTION Fig. 2-13. Aileron control system in wings Issue II April 2014 Allstar PZL Glider Sp. z o.o. page 2.25 Revision Doc No. 542.4.02 corrected...

  • Page 48: Airbrake Control System

    1 - Airbrake driving pushrod in cockpit 2 - Airbrake driving short pushrod 3 - Airbrake driving torsional tube in fuselage 4 - Roller guide 5 - Open loop slider Allstar PZL Glider Sp. z o.o. Issue II April 2014 page 2.26 Doc No. 542.4.02 Revision No.
  • Page 49 SECTION 2. SZD-54-2 TECHNICAL SERVICE MANUAL ASSEMBLING & DISASSEMBLING, „Perkoz” SYSTEMS DESCRIPTION Fig. 2-14. Airbrake control system in fuselage Issue II April 2014 Allstar PZL Glider Sp. z o.o. page 2.27 Revision No. 2 May 2017 Doc No. 542.4.02 corrected...
  • Page 50 8 - Airbrake upper plate 9 - Airbrake lower plate 10 - Cover 11 - Spring tension adjustment screw 12 - Spring 13 - Wing root rib Allstar PZL Glider Sp. z o.o. Issue II April 2014 page 2.28 Doc No. 542.4.02 Revision...
  • Page 51 SECTION 2. SZD-54-2 TECHNICAL SERVICE MANUAL ASSEMBLING & DISASSEMBLING, „Perkoz” SYSTEMS DESCRIPTION Fig. 2-15. Airbrake control system in wing Issue II April 2014 Allstar PZL Glider Sp. z o.o. page 2.29 Revision Doc No. 542.4.02 corrected...

  • Page 52: Front Instrument Panel

    27 - Nut 28 - SP3 stall warning device switch 29 - Bank indicator 30 - Fuses 31 - Transceiver 32 - Reducing connector Allstar PZL Glider Sp. z o.o. Issue II April 2014 page 2.30 Doc No. 542.4.02 Revision...
  • Page 53 Fig. 2-16. Front instrument panel installation diagram C – Total pressure S – Static pressure W – Compensated pressure Issue II April 2014 Allstar PZL Glider Sp. z o.o. page 2.31 Revision No. 2 May 2017 Doc No. 542.4.02 corrected...

  • Page 54: Front Instrument Panel Mounting And Dismounting

    To achieve this unscrew nut (27), pull rod will slide of the lever opening while removing the instrument panel (ref. section A-A). 5. Unscrew four nuts and remove the instrument panel from suspension (17). Mounting is to be accomplished in reverse sequence. Allstar PZL Glider Sp. z o.o. Issue II April 2014 page 2.32 Doc No.

  • Page 55: Sp3 Stall Warning Device Installation

    6 - Reducing connector 7 - Dehydrator 8 - T-pipe in rear instrument panel 9 - T-pipe in front instrument panel Issue II April 2014 Allstar PZL Glider Sp. z o.o. page 2.33 Revision No. 2 May 2017 Doc No. 542.4.02 corrected...

  • Page 56: Rear Instrument Panel

    16 - Rear instrument panel casing fixing screws 17 - Washers 18 - Rear instrument panel fixing screws 19 - Pressure conduits connector 20 - T-pipe on total energy probe „K-1” conduit Allstar PZL Glider Sp. z o.o. Issue II April 2014 page 2.34 Doc No. 542.4.02...

  • Page 57: Rear Instrument Panel Mounting And Dismounting

    2. Unscrew fixing screws (18). 3. Remove instrument panel (1). Mounting is to be accomplished in reverse sequence. Issue II April 2014 Allstar PZL Glider Sp. z o.o. page 2.35 Revision No. 2 May 2017 Doc No. 542.4.02 corrected...

  • Page 58: Electric System

    Automatic fuse Battery 2 circuit AWG 16 0,004 A/cmil AKU 8A Automatic fuse Battery 3 circuit - optional AWG 16 0,004 A/cmil AKU 8A Allstar PZL Glider Sp. z o.o. Issue II April 2014 page 2.36 Doc No. 542.4.02 Revision corrected...

  • Page 59: Removing Rear Seat Pan

    4. In this position rotate seat pan - right side upwards, then move it forward and take it out from fuselage. Issue II April 2014 Allstar PZL Glider Sp. z o.o. page 2.37 Revision No. 2 May 2017 Doc No. 542.4.02...
  • Page 60 4 - Guide laminated to fuselage board 5 - Supporting bolt 6 - Guiding screw 7 - Backrest socket with seat pan position regulation openings Allstar PZL Glider Sp. z o.o. Issue II April 2014 page 2.38 Doc No. 542.4.02...

  • Page 61: Tow Releases Control System

    14 - Cables tubing 15 - Front tow release box 16 - CG tow release box 17 - Cable turnbuckle by CG tow release lever Issue II April 2014 Allstar PZL Glider Sp. z o.o. page 2.39 Revision Doc No. 542.4.02 corrected...
  • Page 62 SECTION 2. SZD-54-2 ASSEMBLING & DISASSEMBLING, TECHNICAL SERVICE MANUAL „Perkoz” SYSTEMS DESCRIPTION Fig. 2-21. Tow releases control system Allstar PZL Glider Sp. z o.o. Issue II April 2014 page 2.40 Doc No. 542.4.02 Revision corrected...

  • Page 63: Battery And Equipment Mounting In Luggage Compartment

    Prepared reinforcements may be loaded with weight distributed over several attachment points, a value of 2,2 lb at single point. Issue II April 2014 Allstar PZL Glider Sp. z o.o. page 2.41 Revision No. 2 May 2017 Doc No. 542.4.02...

  • Page 64: Sailplane Drainage System

     Two  0,16” drainage holes in lower shell of every wing  Two  0,16” drainage holes in lower shell of horizontal stabilizer  One  0,16” drainage hole in lower shell of elevator Allstar PZL Glider Sp. z o.o. Issue II April 2014 page 2.42...

  • Page 65: Section 3. Technical Specification

    Canopy lock handle by front and rear seat 22,5 ÷ 29,2 Force required to actuate tow release by front or rear pilot, without towing line being tensed Issue II April 2014 Allstar PZL Glider Sp. z o.o. page 3.1 Revision Doc No. 542.4.02 corrected...

  • Page 66: Allowable Backlashes And Tolerances In Mounting Connections And Sailplane Control Systems

    (5) and (6) Fig. 2‒1., individually matching the dimension (a) Fig. 3‒1. with backlash +0,002” for every oversize. Fig. 3-1. Driver connection scheme Allstar PZL Glider Sp. z o.o. Issue II April 2014 page 3.2 Doc No.

  • Page 67: Maximum Allowable Backlashes On Sailplane Main Unit Connection Fittings

    “open” position. Lift manually the plate in top position within the scope of perceptible play and not pulling the cover from the plate. Issue II April 2014 Allstar PZL Glider Sp. z o.o. page 3.3 Revision Doc No. 542.4.02 corrected...

  • Page 68: Adjustment Of Sailplane Assemblies And Control Systems

    Control sticks’ neutral position in elevator control system is presented in Fig. 2‒12. Maximum elevator deflections are set using limiters – regulation screws (5) located at the front (1) and rear (2) flying control. Allstar PZL Glider Sp. z o.o. Issue II April 2014 page 3.4 Doc No.

  • Page 69: Adjustment Of Cables Tension In Rudder Control System

    - hung on the telescopic guide, whereas in the rear - connected to intermediate pushrod (2), and then this one to torsional tube lever (3). Adjustment can be done at pushrod (1) or (2). Issue II April 2014 Allstar PZL Glider Sp. z o.o. page 3.5 Revision Doc No. 542.4.02 corrected...

  • Page 70: Adjustment Of Trimmer Control System

    2. Set the seat pan in appropriate position. 3. Lock the seat pan by rotating knob (2) until bolts are slid out of tube. Allstar PZL Glider Sp. z o.o. Issue II April 2014 page 3.6...

  • Page 71: Section 4. Special Tools Specification

    Directions for use the key is presented in item 2.2. (Fig. 2‒2., pos. 6 and Fig. 2‒4., pos. 10) Fig. 4-2. Wingtips mounting key Issue II April 2014 Allstar PZL Glider Sp. z o.o. page 4.1 Revision Doc No. 542.4.02 corrected...

  • Page 72: Rear Fitting Assembly Key

    Directions for use the key is presented in item 2.1. (Fig. 2‒1., pos. 21). Fig. 4-3. Rear fitting assembly key 4.4. Mounting wrench This wrench and directions for use are presented in item 2.1. (Fig. 2‒1., pos. 12). Allstar PZL Glider Sp. z o.o. Issue II April 2014 page 4.2 Doc No.

  • Page 73: Section 5. Lubrication Instruction

    Bowden cables should be lubricated with cold-test machine oil. Its kinematic /s in temperature 104 °F and its acid value should viscosity should be about 0,09 in not exceed 0,20 mg KOH/g. Issue II April 2014 Allstar PZL Glider Sp. z o.o. page 5.1 Revision Doc No. 542.4.02 corrected...

  • Page 74: Elements Not Requiring Lubrication

    17 - Nose wheel bearings 18 - Tow releases 19 - Tail wheel bearings 20 - Wing-fuselage connecting assembly 21 - Wing-wingtip (plane or winglets) connection Allstar PZL Glider Sp. z o.o. Issue II April 2014 page 5.2 Doc No. 542.4.02 Revision No.
  • Page 75 SZD-54-2 SECTION 5. TECHNICAL SERVICE MANUAL „Perkoz” LUBRICATION INSTRUCTION Fig. 5-1. Lubrication scheme Issue II April 2014 Allstar PZL Glider Sp. z o.o. page 5.3 Revision Doc No. 542.4.02 corrected...
  • Page 76 SZD-54-2 SECTION 5. TECHNICAL SERVICE MANUAL „Perkoz” LUBRICATION INSTRUCTION Intentionally left blank Allstar PZL Glider Sp. z o.o. Issue II April 2014 page 5.4 Doc No. 542.4.02 Revision corrected...

  • Page 77: Section 6. Sailplane Alignment And Control Surfaces Deflection Inspection

    0,05” brass wires with painted red areola. Ways of control surfaces deflection adjusting are given in item 3.5. of this Manual. Issue II April 2014 Allstar PZL Glider Sp. z o.o. page 6.1 Revision Doc No. 542.4.02 corrected...
  • Page 78 SZD-54-2 TECHNICAL SERVICE MANUAL SAILPLANE ALIGNMENT AND CONTROL „Perkoz” SURFACES DEFLECTION INSPECTION Fig. 6-1. Sailplane alignment and control surfaces deflection Allstar PZL Glider Sp. z o.o. Issue II April 2014 page 6.2 Doc No. 542.4.02 Revision No. 2 May 2017...

  • Page 79: Section 7. Sailplane Weighing

    31,5” of trailing point of root aerofoil (Fig. 7‒1.). Level difference between ends of bar, for 27,6” long wedge, must not be greater than 0,04”. Issue II April 2014 Allstar PZL Glider Sp. z o.o. page 7.1 Revision Doc No. 542.4.02 corrected...
  • Page 80 Mass and CG position are derived from these formulas:        Allstar PZL Glider Sp. z o.o. Issue II April 2014 page 7.2 Doc No. 542.4.02 Revision corrected...

  • Page 81: Sailplane Without Pilots Mass And Cg Position

    CG position with calculation method (see item 7.3.). Issue II April 2014 Allstar PZL Glider Sp. z o.o. page 7.3 Revision No. 2 May 2017 Doc No.
  • Page 82 SZD-54-2 SECTION 7. TECHNICAL SERVICE MANUAL „Perkoz” SAILPLANE WEIGHING Fig. 7-2. CG range limits for a sailplane without pilots Allstar PZL Glider Sp. z o.o. Issue II April 2014 page 7.4 Doc No. 542.4.02 Revision No. 2 May 2017 corrected...
  • Page 83 3. Container cover 4. Four container mounting screws Fig. 7-3. Location of balancing weight in sailplane tail Fig. 7-4. Battery mounting in sailplane tail Issue II April 2014 Allstar PZL Glider Sp. z o.o. page 7.5 Revision Doc No. 542.4.02 corrected...

  • Page 84: Calculation Of Sailplane Without Pilots Cg Position

    31,5 - additional equipment CG position in luggage compartment m - battery mass increment in tail mass m 189,37 - position Allstar PZL Glider Sp. z o.o. Issue II April 2014 page 7.6 Doc No. 542.4.02 Revision No. 2 May 2017...
  • Page 85   with ballast   These values should be recorded in sailplane without pilots Weighing Table in item 6.4. in Flight Manual. Issue II April 2014 Allstar PZL Glider Sp. z o.o. page 7.7 Revision Doc No. 542.4.02 corrected...
  • Page 86  199,21 Final values entered in record are as follows: = 860+3,6 = 863,6 lb = (X = 31 in Allstar PZL Glider Sp. z o.o. Issue II April 2014 page 7.8 Doc No. 542.4.02 Revision No. 2 May 2017...

  • Page 87: Section 8. Equipment

    Section 16. Below are listed the minimum equipment types, that have been approved by the sailplane Type Certificate Holder. Issue II April 2014 Allstar PZL Glider Sp. z o.o. page 8.1 Revision No. 2 May 2017 Doc No. 542.4.02...

  • Page 88: Airspeed Indicators

    TS 10.220/47 Ø2,24”, 4 FGH 40 TS 10.220/48 8.1.3. Accelerometers Manufacturer Type Certificate / Approval 2,24”, GM510-2 Falcon Gauge MIL-A-5885 C 3,15”, GM510-3 Allstar PZL Glider Sp. z o.o. Issue II April 2014 page 8.2 Doc No. 542.4.02 Revision corrected...

  • Page 89: Stall Warning Unit

    Richard Tost front  TOST E TCDS 60.230/1 Fluggeratebau 8000 Munchen – CG  TOST G TCDS 60.230/2 Germany Issue II April 2014 Allstar PZL Glider Sp. z o.o. page 8.3 Revision No. 2 May 2017 Doc No. 542.4.02 corrected...

  • Page 90: Additional Equipment

    Additional equipment types, that have been approved by the sailplane Type Certificate Holder, are listed below. Equipment maintenance should be carried out in accordance with guidelines specified in Section 16. Allstar PZL Glider Sp. z o.o. Issue II April 2014 page 8.4...

  • Page 91: Variometers And Related Accessories

    All compasses are subject to compensation in sailplane ready to flight configuration. Deviation chart must be placed in a conspicuous position in sailplane cockpit, near the compass. Issue II April 2014 Allstar PZL Glider Sp. z o.o. page 8.5 Revision No. 2 May 2017 Doc No. 542.4.02...

  • Page 92: Turn And Bank Indicators

    12 V, maintenance-free, gel, Europower DIN 43534, BS 6290p.4, min. capacity 5 [Ah], recommended 6,5 ÷ 7,2 [Ah] EUROBAT and/or UL 1989. Allstar PZL Glider Sp. z o.o. Issue II April 2014 page 8.6 Doc No. 542.4.02 Revision No. 2...

  • Page 93: Transceiver

    Dittel FSG-40-System TCDS 10.911/45 Messtechnik EASA.21O.1305 GmbH Ø2,24”, FSG 90 LBA.0.10.911/98 JTSO (Funkwerk) EASA.21O.1304, Ø2,24”, FSG 2T LBA.0.10.911/103 JTSO Issue II April 2014 Allstar PZL Glider Sp. z o.o. page 8.7 Revision No. 2 May 2017 Doc No. 542.4.02 corrected...

  • Page 94: Emergency Locator Transmitter

    Mounting requires from Type Certificate Holder to develop supplements to TSM and FM, containing installation and maintenance instructions, and to approve it by Aviation Authority. Allstar PZL Glider Sp. z o.o. Issue II April 2014 page 8.8...

  • Page 95: Section 9. Inspection Of Control Surfaces Balance

    6. Measured force value „P ” compare with calculated according to formulas in ZM-i item 3. value „P ” . Issue II April 2014 Allstar PZL Glider Sp. z o.o. page 9.1 Revision No. 2 May 2017 Doc No. 542.4.02 corrected...
  • Page 96  weight of main aileron, wingtip aileron rudder, × g) elevator (G ,  measured balance force of main aileron, ZM-A-C ZM-A-E ZM-R ZM-E wingtip aileron, rudder, elevator Allstar PZL Glider Sp. z o.o. Issue II April 2014 page 9.2 Doc No. 542.4.02 Revision corrected...
  • Page 97 SECTION 9. SZD-54-2 TECHNICAL SERVICE MANUAL INSPECTION OF CONTROL „Perkoz” SURFACES BALANCE Fig. 9-1. Inspection of control surfaces balance Issue II April 2014 Allstar PZL Glider Sp. z o.o. page 9.3 Revision Doc No. 542.4.02 corrected...
  • Page 98 SECTION 9. SZD-54-2 TECHNICAL SERVICE MANUAL INSPECTION OF CONTROL „Perkoz” SURFACES BALANCE Intentionally left blank Allstar PZL Glider Sp. z o.o. Issue II April 2014 page 9.4 Doc No. 542.4.02 Revision corrected...

  • Page 99: Section 10. Airwothiness Limitations

    The periodic maintenance according to guidelines in Section 16. Service life and periodic maintenance for board instruments from other manufacturers – according to instrument certificates and instructions from instrument manufacturer. Issue II April 2014 Allstar PZL Glider Sp. z o.o. page 10.1 Revision Doc No. 542.4.02 corrected...
  • Page 100 SZD-54-2 SECTION 10. TECHNICAL SERVICE MANUAL „Perkoz” AIRWORTHINESS LIMITATIONS Intentionally left blank Allstar PZL Glider Sp. z o.o. Issue II April 2014 page 10.2 Doc No. 542.4.02 Revision corrected...

  • Page 101: Section 11. List Of Maintenance Documents Of Assemblies Approved Regardless Of Sailplane

    4. Stall warning device ANTI-STALL SP3. Technical Service Manual, Issue I 23.03.1995 - optional equipment. Instructions for equipment mounted on particular aircraft are delivered with sailplane. Issue II April 2014 Allstar PZL Glider Sp. z o.o. page 11.1 Revision No. 2 May 2017 Doc No. 542.4.02 corrected...
  • Page 102 SECTION 11. SZD-54-2 LIST OF MAINTENANCE DOCUMENTS TECHNICAL SERVICE MANUAL „Perkoz” OF ASSEMBLIES APPROVED REGARDLESS OF SAILPLANE Intentionally left blank Allstar PZL Glider Sp. z o.o. Issue II April 2014 page 11.2 Doc No. 542.4.02 Revision corrected...

  • Page 103: Section 12. Cleaning And Maintenance

    (not flooded) total and static pressure ports placed in sailplane nose and on vertical stabilizer leading edge. Painted surface may be maintained with wax or silicone polishing paste. Issue II April 2014 Allstar PZL Glider Sp. z o.o. page 12.1 Revision Doc No. 542.4.02 corrected...
  • Page 104 SZD-54-2 SECTION 12. TECHNICAL SERVICE MANUAL „Perkoz” CLEANING AND MAINTENANCE Intentionally left blank Allstar PZL Glider Sp. z o.o. Issue II April 2014 page 12.2 Doc No. 542.4.02 Revision corrected...

  • Page 105: Section 13. Sailplane Transport And Storage In A Hangar

    Anyway, if a sailplane equipped with winglets is transported indeed, it is unacceptable to hold winglet “under the arm” – this could lead to serious injury! Issue II April 2014 Allstar PZL Glider Sp. z o.o. page 13.1 Revision Doc No. 542.4.02...

  • Page 106: Storage In A Hangar

    Reduce air pressure in tires. 13.2.1. Sailplane lifting and moving Fig. 13-1. Sailplane lifting and moving Allstar PZL Glider Sp. z o.o. Issue II April 2014 page 13.2 Doc No. 542.4.02...

  • Page 107: Sailplane Hanging

    Fig. 13‒2. To prevent structure damages protect these sites with soft material, such as felt. Fig. 13-2. Sailplane hanging areas Issue II April 2014 Allstar PZL Glider Sp. z o.o. page 13.3 Revision Doc No. 542.4.02 corrected...
  • Page 108 SECTION 13. SZD-54-2 TECHNICAL SERVICE MANUAL SAILPLANE TRANSPORT „Perkoz” AND STORAGE IN A HANGAR Intentionally left blank Allstar PZL Glider Sp. z o.o. Issue II April 2014 page 13.4 Doc No. 542.4.02 Revision corrected...

  • Page 109: Section 14. Dismounted Sailplane Transport

    If sailplane is sent by railway transport or road transport, then loading and securing in the container must be made according to special documentation. Issue II April 2014 Allstar PZL Glider Sp. z o.o. page 14.1 Revision Doc No. 542.4.02...
  • Page 110 SECTION 14. SZD-54-2 TECHNICAL SERVICE MANUAL DISMOUNTED SAILPLANE „Perkoz” TRANSPORT Intentionally left blank Allstar PZL Glider Sp. z o.o. Issue II April 2014 page 14.2 Doc No. 542.4.02 Revision corrected...

  • Page 111: Section 15. Information Tables

    Removable balance RH cockpit board in front weights of front seat pan Wheel brake Front and rear control stick Issue II April 2014 Allstar PZL Glider Sp. z o.o. page 15.1 Revision No. 2 May 2017 Doc No. 542.4.02 corrected...

  • Page 112: Terms Of Use Tables

    58,0 psi 36,3 psi Nose 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 15.2 Doc No. 542.4.02 Revision No. 2 May 2017...
  • Page 113 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 15.3 Revision No. 2 May 2017 Doc No. 542.4.02 corrected...
  • Page 114 – using the sample showed below and method of filling given in item 6.5. of the FM. Location :  RH cockpit board by front and rear seat. Allstar PZL Glider Sp. z o.o. Issue II April 2014 page 15.4 Doc No.
  • Page 115 10. Transceiver CHECK 11. Stall warning device 12. Towing cable connection CHECK Location :  RH cockpit board by front and rear seat. Issue II April 2014 Allstar PZL Glider Sp. z o.o. page 15.5 Revision Doc No. 542.4.02 corrected...

  • Page 116: Compass Deviation Table

    TECHNICAL SERVICE MANUAL „Perkoz” INFORMATION TABLES 15.2.8. Compass deviation table Location :  Front and rear instrument panel, close to compass (if compass is installed). Allstar PZL Glider Sp. z o.o. Issue II April 2014 page 15.6 Doc No. 542.4.02 Revision corrected...

  • Page 117: Section 16. Periodic Maintenance

    1000 flying hours are to be made in accordance with Service Manual for SP3 stall warning device, if it is installed in the glider. Issue II April 2014 Allstar PZL Glider Sp. z o.o. page 16.1 Revision No. 2 May 2017 Doc No.

  • Page 118: Periodic Maintenance Of Board Instruments

    Service of TOST main wheel is to be done in accordance with Installation and service manual of TOST wheels. Service of nose and tail wheels performed according to item 16.10.7.16. Allstar PZL Glider Sp. z o.o. Issue II April 2014 page 16.2...

  • Page 119: Rules For Operations Of Cables

    As an option, borescope inspection might be acceptable. Issue II April 2014 Allstar PZL Glider Sp. z o.o. page 16.3 Revision Doc No. 542.4.02 corrected...

  • Page 120: Inspection Of Main Units Subjected To Fatigue Loads

    12 - fuselage fitting (3) installation area in rear web (13), Fig. 2‒6.  metal parts  surface peeling, cracks, shape deviations,  composite parts  white spots, delamination, debonding. Allstar PZL Glider Sp. z o.o. Issue II April 2014 page 16.4...

  • Page 121: Maintenance Work And Actions Carried Out On A Sailplane

    4 - Additional actions for instruments are to be completed in accordance with maintenance programme after 300 flying hours, contained in Manual for the concerned instrument Issue II April 2014 Allstar PZL Glider Sp. z o.o. page 16.5 Revision Doc No. 542.4.02 corrected...
  • Page 122 (item 3.3.). 15 - Verify backlash in aileron and stabilizer control system – this is accomplished by measurement of play on top of control stick grip (item 3.4.1.). Allstar PZL Glider Sp. z o.o. Issue II April 2014 page 16.6 Doc No.

  • Page 123: Inspection Of Instruments And Pneumatic Installation

    Check operation and correct fitting of additional installations Additional installations comprise e.g. radio equipment, as well as all other devices installed. Issue II April 2014 Allstar PZL Glider Sp. z o.o. page 16.7 Revision No. 2 May 2017 Doc No. 542.4.02 corrected...

  • Page 124: Verify Reliable De-Rigging And Rigging Of Sailplane Main Units

    Check bonding of rear web with wing skin. Aileron condition verification. Before re-assembling, lubricate aileron hinges and connection of pushrod with aileron driving lever (see Section 5). Allstar PZL Glider Sp. z o.o. Issue II April 2014 page 16.8 Doc No.
  • Page 125 15 - Inspect visually elements and assemblies in control systems – flying controls, pushrods, levers and pedals. In necessity lubricate movable joints between parts (see Section 5). Issue II April 2014 Allstar PZL Glider Sp. z o.o. page 16.9 Revision No. 2 May 2017 Doc No. 542.4.02 corrected...

  • Page 126: Verify Mass Balance Of Control Surfaces

    16.10.10. Perform test flight 16.10.11. Check the patency of all drainage holes (see item 2.21., Fig. 2‒23. Sailplane drainage holes layout scheme) Allstar PZL Glider Sp. z o.o. Issue II April 2014 page 16.10 Doc No. 542.4.02 Revision No. 2...

  • Page 127: Section 17. Sailplane Repairs

    „Individual loading plan” in accordance with item 6.5. in Flight Manual. This manual refers to the „Workshop manual of performing strength laminates” IW-76/412,4. Issue II April 2014 Allstar PZL Glider Sp. z o.o. page 17.1 Revision Doc No. 542.4.02 corrected...

  • Page 128: Composite Structures Repairing

    Performing composite repairs personnel must be authorized to perform the strength composites and have a workshop practice in the composite sailplanes construction or repair. Further given directions allow to make the correct repair. Allstar PZL Glider Sp. z o.o. Issue II April 2014 page 17.2 Doc No.

  • Page 129: Damages Classification

    4” – wings, ailerons and stabilizers debonding As 1 or 2 for zone I, White spots but around main fittings UNACCEPTABLE Trailing edge 8” debonding Damaged paint Issue II April 2014 Allstar PZL Glider Sp. z o.o. page 17.3 Revision Doc No. 542.4.02 corrected...
  • Page 130 Fig. 17-1. Zoning and material specification for fuselage repairs Allstar PZL Glider Sp. z o.o. Issue II April 2014 page 17.4...
  • Page 131 W 2 – applies to plane wingtip, W 3 – applies to long wingtip. Fig. 17-2. Zoning and material specification for wing repairs Issue II April 2014 Allstar PZL Glider Sp. z o.o. page 17.5 Revision Doc No. 542.4.02 corrected...
  • Page 132 SECTION 17. TECHNICAL SERVICE MANUAL „Perkoz” SAILPLANE REPAIRS Zone III – vertical stabilizer and rudder Fig. 17-3. Material specification for vertical stabilizer repairs Allstar PZL Glider Sp. z o.o. Issue II April 2014 page 17.6 Doc No. 542.4.02 Revision corrected...
  • Page 133 SZD-54-2 SECTION 17. TECHNICAL SERVICE MANUAL „Perkoz” SAILPLANE REPAIRS Fig. 17-4. Material specification for rudder repairs Issue II April 2014 Allstar PZL Glider Sp. z o.o. page 17.7 Revision Doc No. 542.4.02 corrected...
  • Page 134 SECTION 17. TECHNICAL SERVICE MANUAL „Perkoz” SAILPLANE REPAIRS Zone III – horizontal stabilizer and elevator Fig. 17-5. Material specification for horizontal stabilizer repairs Allstar PZL Glider Sp. z o.o. Issue II April 2014 page 17.8 Doc No. 542.4.02 Revision corrected...
  • Page 135 SZD-54-2 SECTION 17. TECHNICAL SERVICE MANUAL „Perkoz” SAILPLANE REPAIRS Fig. 17-6. Material specification for elevator repairs Issue II April 2014 Allstar PZL Glider Sp. z o.o. page 17.9 Revision Doc No. 542.4.02 corrected...

  • Page 136: Typical Composite Structures Repairs

    Damage to the sandwich outer layer (shallow dent, loss) Fig. 17-7. Damage to the sandwich outer layer Fig. 17-8. Repair of damaged sandwich outer layer Allstar PZL Glider Sp. z o.o. Issue II April 2014 page 17.10 Doc No. 542.4.02 Revision No.
  • Page 137  laminate outer layer according to fabrics specification in Fig. 17‒1. ÷ Fig. 17‒6.,  perform repair of paint coating according to item 17.4. Issue II April 2014 Allstar PZL Glider Sp. z o.o. page 17.11 Revision Doc No. 542.4.02...
  • Page 138 Inner layer is made from very thin fabric. If repairer fail to leave intact inner layer rim during cleaning of the hole in accordance with Fig. 17‒2. it is necessary to enlarge the hole and re-prepare the rim. Allstar PZL Glider Sp. z o.o. Issue II April 2014 page 17.12...

  • Page 139: Solid Laminate Shell

    Issue II April 2014 Allstar PZL Glider Sp. z o.o. page 17.13 Revision Doc No. 542.4.02...

  • Page 140: Fuselage Central Section Skin Repair - Zone Ii

     paste composite piece in fuselage shell and exert a pressure with bands (wrap fuselage),  laminate 1 × 92110 in gluing areas from inner and outer side. Allstar PZL Glider Sp. z o.o. Issue II April 2014 page 17.14 Doc No.

  • Page 141: Repair Of Rear (Sandwich) Fuselage Part - Zone Iii

    Damage to sandwich outer shell (shallow dent, loss) Fig. 17-17. Damage to sandwich outer shell Fig. 17-18. Repair of damage to sandwich outer shell Issue II April 2014 Allstar PZL Glider Sp. z o.o. page 17.15 Revision Doc No. 542.4.02 corrected...
  • Page 142 17.3.5.1.2. Damage to sandwich outer shell and foam Fig. 17-19. Damage to sandwich outer shell and foam Fig. 17-20. Repair of damage to sandwich outer shell and foam Allstar PZL Glider Sp. z o.o. Issue II April 2014 page 17.16 Doc No.
  • Page 143 - Further operations acc. to item 17.3.5.1.1. 17.3.5.1.3. Sandwich structure trough damage Fig. 17-21. Sandwich structure trough damage Fig. 17-22. Repair of sandwich structure trough damage Issue II April 2014 Allstar PZL Glider Sp. z o.o. page 17.17 Revision Doc No. 542.4.02 corrected...
  • Page 144 17.3.5.2. 17.3.5.2.1. Sandwich outer shell damage (shallow dent, shallow or deep foam damage) Fig. 17-23. Damage to sandwich outer shell, detail “A” Allstar PZL Glider Sp. z o.o. Issue II April 2014 page 17.18 Doc No. 542.4.02 Revision No. 2...
  • Page 145 - Perform further operations acc. to item 17.3.5.1.3 through inner shell rebuilt, (2x92145 fabrics), - Foam and connection layer rebuild perform acc. to item 17.3.5.2.1, - Further operations acc. to item 17.3.5.1.1. Issue II April 2014 Allstar PZL Glider Sp. z o.o. page 17.19 Revision Doc No. 542.4.02 corrected...

  • Page 146: Inner Structure Debonding

    I case II Fig. 17-25. Inner structure debonding case I case II Fig. 17-26. Repair of inner structure debonding Allstar PZL Glider Sp. z o.o. Issue II April 2014 page 17.20 Doc No. 542.4.02 Revision No. 2 May 2017...

  • Page 147: Painting

    It is not allowed to place on them any additional markings or patterns in different colours. It is acceptable to place competition starting markings on vertical stabilizer. Issue II April 2014 Allstar PZL Glider Sp. z o.o. page 17.21 Revision Doc No. 542.4.02 corrected...

  • Page 148: Materials For Typical Repairs Of Composite Structures

    92145 asymmetric 0,0110 (0,28) 6 × 7 98110 plain 0,0039 (0,10) 98130 plain 0,0098 (0,25) KDU-1001 unidirectional 0,0157 (0,40) Allstar PZL Glider Sp. z o.o. Issue II April 2014 page 17.22 Doc No. 542.4.02 Revision No. 2 May 2017 corrected...
  • Page 149  foam and trailing edges gluing with the addition of microballoon,  joints, fittings, etc. gluing with addition of cut fibreglass and colloidal silica (aerosil). Issue II April 2014 Allstar PZL Glider Sp. z o.o. page 17.23 Revision Doc No. 542.4.02...

  • Page 150: Non-Composite Parts Repair

    In case of using bushing in accordance with ZN-73/L-383320 clamping should be done on whole length of bushing, diameter w/o fin should be: for 2,5 mm cable – 0,22+0,01”, and for 3,2 mm cable ‒ 0,27+0,01”. Allstar PZL Glider Sp. z o.o. Issue II April 2014 page 17.24...

  • Page 151: Reaming Of Main Bolt Sleeves And Rear Fittings

    During reaming lubrications should be done with machine oil. Rear fitting Main bolt sleeves with locking pin Fig. 17-27. Reaming of connecting spars main bolt sleeves and rear fittings Issue II April 2014 Allstar PZL Glider Sp. z o.o. page 17.25 Revision Doc No. 542.4.02 corrected...

  • Page 152: Canopy Perspex

    Fig. 17-28. Way to avoid further cracking of perspex Cracks or complementing parts are to be glued with the use of dedicated organic glass glue in accordance to glue manufacturer guidelines. Allstar PZL Glider Sp. z o.o. Issue II April 2014 page 17.26...

  • Page 153: Parts Replacement

    Canopy: a) perspex without frame b) perspex with frame Control surfaces: a) rudder b) elevator c) ailerons Issue II April 2014 Allstar PZL Glider Sp. z o.o. page 17.27 Revision Doc No. 542.4.02 corrected...
  • Page 154 Parts 11a and 12 can be replaced only by certified organization due to required fit and backlash between fuselage and wing and proper regulation of fuselage-wing controls connections. Allstar PZL Glider Sp. z o.o. Issue II April 2014 page 17.28 Doc No.

  • Page 155: Primary And Secondary Structure

    8. Fuselage rear pin (16) Fig. 2‒1. 9. Frame tube (15) Fig. 2‒1. 10. Stabilizer fastening vertical bolt (1) Fig. 2‒6. 11. Aileron clutch (6) Fig. 2‒5. Issue II April 2014 Allstar PZL Glider Sp. z o.o. page 17.29 Revision Doc No. 542.4.02 corrected...

  • Page 156: Secondary Structure

    Production interchangeability means possibility to correct mounting mating assemblies made at separate workplaces. In specific cases this might require mutual reaming of connecting fittings and matching contours. Allstar PZL Glider Sp. z o.o. Issue II April 2014 page 17.30 Doc No. 542.4.02 Revision No.

  • Page 157: Section 18. Annexes

    At the time of removal of the equipment enter the date in column “Dismantled”. Make new updated list at each equipment change (installing or removing). Intentionally left blank Issue II April 2014 Allstar PZL Glider Sp. z o.o. page 18.1 Revision Doc No. 542.4.02 corrected...
  • Page 158 Inverted flight bank indicator Total energy variometer of range ±10 kn Total energy compensator Compensating vessel Electric turn and bank indicator 10 Transceiver Allstar PZL Glider Sp. z o.o. Issue II April 2014 page 18.2 Doc No. 542.4.02 Revision corrected...
  • Page 159 Technical Service Manual with corresponding “Record of sailplane weighing and determining of CG” or (if done) “Calculation record of sailplane without pilots CG”. Issue II April 2014 Allstar PZL Glider Sp. z o.o. page 18.3 Revision Doc No. 542.4.02 corrected...

  • Page 160: Record Of Sailplane Weighing And Determining Of Cg

    SZD-54-2 SECTION 18. TECHNICAL SERVICE MANUAL „Perkoz” ANNEXES 18.2. Record of sailplane weighing and determining of CG Allstar PZL Glider Sp. z o.o. Issue II April 2014 page 18.4 Doc No. 542.4.02 Revision No. 2 May 2017 corrected...

  • Page 161: Elevator, Rudder And Ailerons Balance Records

    SZD-54-2 SECTION 18. TECHNICAL SERVICE MANUAL „Perkoz” ANNEXES 18.3. Elevator, rudder and ailerons balance records Issue II April 2014 Allstar PZL Glider Sp. z o.o. page 18.5 Revision Doc No. 542.4.02 corrected...
  • Page 162 SZD-54-2 SECTION 18. TECHNICAL SERVICE MANUAL „Perkoz” ANNEXES Allstar PZL Glider Sp. z o.o. Issue II April 2014 page 18.6 Doc No. 542.4.02 Revision corrected...
  • Page 163 SZD-54-2 SECTION 18. TECHNICAL SERVICE MANUAL „Perkoz” ANNEXES Issue II April 2014 Allstar PZL Glider Sp. z o.o. page 18.7 Revision Doc No. 542.4.02 corrected...

  • Page 164: Calculation Record Of Sailplane Without Pilots Cg

    SZD-54-2 SECTION 18. TECHNICAL SERVICE MANUAL „Perkoz” ANNEXES 18.4. Calculation record of sailplane without pilots CG Allstar PZL Glider Sp. z o.o. Issue II April 2014 page 18.8 Doc No. 542.4.02 Revision corrected...
  • Page 165 Mass sum in column Luggage compartment mass increment m = (-m ) + (+m -m +m Other equipment Battery in vertical stabilizer Prepared by: Date: Signature Issue II April 2014 Allstar PZL Glider Sp. z o.o. page 18.9 Revision Doc No. 542.4.02 corrected...

  • Page 166: Record Of Control Surfaces Movements

    SZD-54-2 SECTION 18. TECHNICAL SERVICE MANUAL „Perkoz” ANNEXES 18.5. Record of control surfaces movements Allstar PZL Glider Sp. z o.o. Issue II April 2014 page 18.10 Doc No. 542.4.02 Revision No. 2 May 2017 corrected...

  • Page 167: Glider Alignment Record

    SZD-54-2 SECTION 18. TECHNICAL SERVICE MANUAL „Perkoz” ANNEXES 18.6. Glider alignment record Issue II April 2014 Allstar PZL Glider Sp. z o.o. page 18.11 Revision No. 2 May 2017 Doc No. 542.4.02 corrected...

  • Page 168: Measurement Record For Glider Control Systems Friction And Activation Forces

    SZD-54-2 SECTION 18. TECHNICAL SERVICE MANUAL „Perkoz” ANNEXES 18.7. Measurement record for glider control systems friction and activation forces Allstar PZL Glider Sp. z o.o. Issue II April 2014 page 18.12 Doc No. 542.4.02 Revision No. 2 May 2017 corrected...

  • Page 169: Section 19. Supplements

    19.2. List of inserted supplements Supplement Confirmation of the Date of issue Supplement title application on S/N Issue II April 2014 Allstar PZL Glider Sp. z o.o. page 19.1 Revision Doc No. 542.4.02 corrected...
  • Page 170 SECTION 19. TECHNICAL SERVICE MANUAL „Perkoz” SUPPLEMENTS 19.3. Supplements – List of actual pages Supplement Supplement Page Date of issue Page Date of issue Allstar PZL Glider Sp. z o.o. Issue II April 2014 page 19.2 Doc No. 542.4.02 Revision corrected...

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