AS 332 L SITUATION DES REVISIONS DU MANUEL DE …€¦ · flight manual revisions status...

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Page 1 / 1 Edition du : 25/07/2017 Issue Dated : AS 332 L SITUATION DES REVISIONS DU MANUEL DE VOL FLIGHT MANUAL REVISIONS STATUS CERTIFICATION EASA EASA CERTIFICATION Ce manuel doit contenir la révision normale (RN) et les révisions rapides (RR) référencées dans l'édition (EDIT) considérée. This manual must contain the normal revision (RN) and rush revisions (RR) listed under the relevant issue (EDIT). PARTIE REGLEMENTAIRE PRESCRIBED SECTION Volume 1 SECT. / SUP. . . EDIT . . DATE 0 => 5.1 RN12 17-25 R SUP.0 RN6 04-21 SUP.10.1 RN1 03-04 SUP.10.2 RN2 14-43 SUP.10.3 RN2 01-06 SUP.10.4 RN2 00-41 SUP.10.5 RN0 95-50 SUP.10.6 RN5 15-18 SUP.10.7 RN2 01-06 SUP.10.8 RN0 95-50 SUP.10.9 RN1 00-41 SUP.10.10 RN3 15-26 SUP.10.11 RN5 08-04 SUP.10.12 RN1 00-30 SUP.10.13 RN3 16-37 SUP.10.14 RN2 01-06 SUP.10.15 RN0 95-50 SUP.10.16 RN5 08-04 SUP.10.17 RN1 03-07 SUP.10.18 RN3 11-27 SUP.10.19 RN1 01-08 PARTIE REGLEMENTAIRE PRESCRIBED SECTION Volume 1 SECT. / SUP. . . EDIT . . DATE SUP.10.20 RN0 95-50 SUP.10.21 RN6 07-42 SUP.10.22 RN0 95-50 SUP.10.25 RN1 05-07 SUP.10.27 RN2 14-43 SUP.10.51 RN0 03-26 SUP.10.53 RN1 11-27 SUP.10.56 RN7 15-50 SUP.10.65 RN3 14-43 SUP.11.1 RN3 15-26 SUP.11.3 RN0 95-50 SUP.11.4 RN1 03-39 PARTIE COMPLEMENTAIRE COMPLEMENTARY SECTION Volume 2 SECT. EDIT DATE 0, 5.2 => 9 RN9 12-42

Transcript of AS 332 L SITUATION DES REVISIONS DU MANUEL DE …€¦ · flight manual revisions status...

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Edition du : 25/07/2017 Issue Dated :

AS 332 L SITUATION DES REVISIONS DU MANUEL DE VOL

FLIGHT MANUAL REVISIONS STATUS CERTIFICATION EASA EASA CERTIFICATION

Ce manuel doit contenir la révision normale (RN) et les révisions rapides (RR) référencées dans l'édition (EDIT) considérée.

This manual must contain the normal revision (RN) and rush revisions (RR) listed under the relevant issue (EDIT).

PARTIE REGLEMENTAIRE

PRESCRIBED SECTION Volume 1

SECT. /

SUP.

. .

EDIT .

. DATE

0 => 5.1 RN12 17-25 R

SUP.0 RN6 04-21

SUP.10.1 RN1 03-04

SUP.10.2 RN2 14-43

SUP.10.3 RN2 01-06

SUP.10.4 RN2 00-41

SUP.10.5 RN0 95-50

SUP.10.6 RN5 15-18

SUP.10.7 RN2 01-06

SUP.10.8 RN0 95-50

SUP.10.9 RN1 00-41

SUP.10.10 RN3 15-26

SUP.10.11 RN5 08-04

SUP.10.12 RN1 00-30

SUP.10.13 RN3 16-37

SUP.10.14 RN2 01-06

SUP.10.15 RN0 95-50

SUP.10.16 RN5 08-04

SUP.10.17 RN1 03-07

SUP.10.18 RN3 11-27

SUP.10.19 RN1 01-08

PARTIE REGLEMENTAIRE PRESCRIBED SECTION

Volume 1 SECT.

/ SUP.

. .

EDIT .

. DATE

SUP.10.20 RN0 95-50

SUP.10.21 RN6 07-42

SUP.10.22 RN0 95-50

SUP.10.25 RN1 05-07

SUP.10.27 RN2 14-43

SUP.10.51 RN0 03-26

SUP.10.53 RN1 11-27

SUP.10.56 RN7 15-50

SUP.10.65 RN3 14-43

SUP.11.1 RN3 15-26

SUP.11.3 RN0 95-50

SUP.11.4 RN1 03-39

PARTIE COMPLEMENTAIRE

COMPLEMENTARY SECTION

Volume 2

SECT. EDIT DATE

0, 5.2 => 9 RN9 12-42

UPDATE GUIDE 17-30 Page 1 / 1

REVISION TO AIRCRAFT PUBLICATION : AS 332 L

PUBLICATION CONCERNED : REGULATORY PART

CUSTOMIZATION AIRCRAFT S/N : -

VOL.1 REVISION No. : 12 DATE CODE: 17-25 CERTIFICATION CODE: A

- The outline of the revision is given below : . Sections or supplements affected (added or modified), . Major points of the revision.

- Check that pages in each section are those specified in the list of effective pages.

- Withdraw old and insert new pages affected by this revision.

- Return the acknowledgement card.

- This list of amended pages may be filed (apart from the manual).

DELETED PAGES INSERTED PAGES

SECTIONS PAGES DATE CODE SECTIONS PAGES DATE CODE

SRD - 1 23/03/2017 - 1 25/07/2017

NORMAL REVISIONS

0.0.P5 1 to 7 17-10 0.0.P5 1 to 7 17-25

2.2 1 95-50 2.2 1 95-50

2.2 2 16-18 2.2 2 17-25

DESCRIPTION OF THE REVISION SECTIONS PAGE

NR45 17-25

Update 0.0.P5 -

Deletion of "Post-MOD 07.28352" and addition of "if crashworthy seats are installed" 2.2 2

FLIGHT MANUAL

Approved 330 L 0.0.P5 A 17-25 Page 1

LIST OF APPROVED EFFECTIVE PAGES - EASA CERTIFICATION (1) EFFECTIVITY: - Without indication ...... Applicable to all aircraft. - |A | .................... Specific to EASA. - Clear text definition ... Self-explanatory (2) VARIANT OF STANDARD DEFINITION EFFECTIVITY: - Without indication ...... Applicable to all aircraft. - XXX ..................... Specific to aircraft equipped with XXX. (3) GROUP OF AIRCRAFT EFFECTIVITY: - Without indication ...... Applicable to all aircraft. - YYY ..................... Specific to S/N nnnn | | | | | | | SECTION, PAGE | DATE | (1) | (2) | (3) | | SUP or APP | CODE | | | | | | | | | | | 0.0.P1 1 | 15-09 | | | | | 0.0.P1 2 | 95-50 | | | | | 0.0.P1 3 | 05-21 | | | | | 0.0.P2 1 | 95-50 | | | | | 0.0.P3 1 | 05-21 | | | | | 0.0.P4 1 | 05-21 | | | | | 0.0.P5 1/07 | 17-25 | |A | | | | | 1.0.P1 1 | 15-09 | | | | | 1.0.P6 1 | 15-09 | | | | | 1.1 1 | 12-42 | | | | | 1.1 2 | 15-09 | | | | | 1.1 3 | 12-42 | | | | | 1.2 1 | 05-21 | | | | | 1.2 2 | 05-21 | | | | | 1.3 1 | 05-21 | | | | | 1.3 2 | 05-21 | | | | | 1.3 3 | 05-21 | | | | | 1.3 4 | 05-21 | | | | | 1.3 5 | 05-21 | | | | | 1.4 1 | 05-21 | | | | | 1.4 2 | 05-21 | | | | | 2.0.P1 1 | 15-09 | | | | | 2.0.P6 1 | 00-38 | | | | | 2.1 1 | 00-38 | | | | | 2.1 2 | 05-21 | | | | | 2.1 3 | 95-50 | | | | | 2.1 4 | 00-38 | | | | | 2.1 5 | 00-38 | | | | | 2.1 6 | 05-21 | | | | | 2.1 7 | 00-38 | | | | | 2.1 8 | 00-38 | | | | | 2.1 9 | 00-38 | | | | | | | | | |

FLIGHT MANUAL

Approved 330 L 0.0.P5 A 17-25 Page 2

| | | | | | | SECTION, PAGE | DATE | (1) | (2) | (3) | | SUP or APP | CODE | | | | | | | | | | | 2.1 10 | 00-38 | | | | | 2.1 11 | 11-47 | | | | | 2.1 12 | 00-38 | | | | | 2.1 13 | 00-38 | | | | | 2.1 14 | 05-21 | | | | | 2.1 15 | 05-21 | | | | | 2.1 16 | 00-38 | | | | | 2.1 17 | 95-50 | | | | | 2.1 18 | 08-42 | | | | | 2.1 19 | 07-42 | | | | | 2.1 20 | 17-10 | | | | | 2.2 1 | 95-50 | | | | | 2.2 2 | 17-25 | | | | | 2.2 3 | 00-38 | | | | | 2.2 4 | 00-38 | | | | | 2.2 5 | 95-50 | | | | | 2.2 6 | 12-42 | | | | | 2.2 7 | 95-50 | | | | | 2.2 8 | 95-50 | | | | | 3.0.P1 1 | 15-09 | | | | | 3.0.P6 1 | 05-21 | | | | | 3.0.P6 2 | 97-40 | | | | | 3.1 1 | 97-40 | | | | | 3.1 2 | 97-40 | | | | | 3.1 3 | 00-38 | | | | | 3.1 4 | 00-38 | | | | | 3.1 5 | 08-42 | | | | | 3.1 6 | 07-42 | | | | | 3.1 7 | 07-42 | | | | | 3.1 8 | 07-42 | | | | | 3.1 9 | 07-42 | | | | | 3.1 10 | 07-42 | | | | | 3.1 11 | 15-09 | | | | | 3.1 12 | 09-51 | | | | | 3.1 13 | 05-21 | | | | | 3.1 14 | 05-21 | | | | | 3.1 15 | 05-21 | | | | | 3.1 16 | 05-21 | | | | | 3.1 17 | 15-09 | | | | | 3.1 18 | 05-21 | | | | | 3.2 1 | 95-50 | | | | | 3.2 2 | 95-50 | | | | | 3.2 3 | 07-42 | | | | | 3.2 4 | 95-50 | | | | | 3.2 5 | 12-42 | | | | | 3.2 6 | 12-42 | | | | | 3.2 7 | 95-50 | | | | | 3.2 8 | 97-40 | | | | | 3.2 9 | 97-40 | | | | | | | | | |

FLIGHT MANUAL

Approved 330 L 0.0.P5 A 17-25 Page 3

| | | | | | | SECTION, PAGE | DATE | (1) | (2) | (3) | | SUP or APP | CODE | | | | | | | | | | | 3.2 10 | 07-42 | | | | | 3.2 11 | 97-40 | | | | | 3.2 12 | 00-38 | | | | | 3.2 13 | 07-42 | | | | | 3.2 14 | 05-21 | | | | | 3.2 15 | 00-38 | | | | | 3.2 16 | 95-50 | | | | | 3.2 17 | 05-21 | | | | | 3.2 18 | 05-21 | | | | | 3.2 19 | 05-21 | | | | | 3.2 20 | 95-50 | | | | | 3.2 21 | 95-50 | | | | | 3.2 22 | 97-40 | | | | | 3.2 23 | 00-38 | | | | | 3.2 24 | 95-50 | | | | | 3.2 25 | 97-40 | | | | | 3.2 26 | 97-40 | | | | | 3.2 27 | 08-42 | | | | | 3.2 28 | 15-09 | | | | | 3.2 29 | 15-09 | | | | | 3.2 30 | 97-40 | | | | | 3.2 31 | 97-40 | | | | | 3.2 32 | 00-38 | | | | | 3.2 33 | 97-40 | | | | | 3.2 34 | 97-40 | | | | | 3.2 35 | 97-40 | | | | | 3.2 36 | 97-40 | | | | | 3.2 37 | 97-40 | | | | | 3.2 38 | 12-42 | | | | | 3.2 39 | 97-40 | | | | | 3.2 40 | 97-40 | | | | | 3.2 41 | 00-38 | | | | | 3.2 42 | 97-40 | | | | | 3.2 43 | 97-40 | | | | | 3.2 44 | 97-40 | | | | | 3.2 45 | 97-40 | | | | | 3.2 46 | 00-38 | | | | | 3.2 47 | 97-40 | | | | | 3.2 48 | 97-40 | | | | | 3.2 49 | 07-42 | | | | | 3.3 1 | 00-38 | | | | | 3.3 2 | 95-50 | | | | | 3.3 3 | 07-42 | | | | | 3.3 4 | 07-42 | | | | | 3.3 5 | 07-42 | | | | | 3.3 6 | 97-40 | | | | | 3.3 7 | 07-42 | | | | | 3.3 8 | 00-38 | | | | | 4.0.P1 1 | 15-09 | | | | | | | | | |

FLIGHT MANUAL

Approved 330 L 0.0.P5 A 17-25 Page 4

| | | | | | | SECTION, PAGE | DATE | (1) | (2) | (3) | | SUP or APP | CODE | | | | | | | | | | | 4.0.P6 1 | 95-50 | | | | | 4.1 1 | 95-50 | | | | | 4.1 2 | 00-38 | | | | | 4.1 3 | 17-10 | | | | | 4.1 4 | 07-42 | | | | | 4.1 5 | 95-50 | | | | | 4.1 6 | 15-09 | | | | | 4.1 7 | 05-21 | | | | | 4.1 8 | 15-09 | | | | | 4.1 9 | 15-09 | | | | | 4.1 10 | 15-09 | | | | | 4.1 11 | 05-21 | | | | | 4.1 12 | 05-21 | | | | | 4.1 13 | 00-38 | | | | | 4.1 14 | 95-50 | | | | | 4.1 15 | 00-38 | | | | | 4.1 16 | 05-21 | | | | | 4.1 17 | 97-40 | | | | | 4.1 18 | 97-40 | | | | | 4.1 19 | 05-21 | | | | | 4.1 20 | 07-42 | | | | | 4.1 21 | 97-40 | | | | | 4.1 22 | 05-21 | | | | | 4.1 23 | 95-50 | | | | | 4.1 24 | 00-38 | | | | | 4.1 25 | 11-47 | | | | | 4.1 26 | 11-47 | | | | | 4.1 27 | 11-47 | | | | | 4.1 28 | 95-50 | | | | | 4.1 29 | 00-38 | | | | | 4.1 30 | 95-50 | | | | | 4.2 1 | 00-38 | | | | | 4.2 2 | 12-42 | | | | | 4.2 3 | 95-50 | | | | | 4.2 4 | 05-21 | | | | | 4.2 5 | 00-38 | | | | | 4.2 6 | 95-50 | | | | | 5.1.P1 1 | 15-09 | | | | | 5.1.P6 1 | 00-38 | | | | | 5.1 1 | 97-40 | | | | | 5.1 2 | 11-47 | | | | | 5.1 3 | 95-50 | | | | | 5.1 4 | 95-50 | | | | | 5.1 5 | 95-50 | | | | | 5.1 6 | 95-50 | | | | | 5.1 7 | 00-38 | | | | | 5.1 8 | 00-38 | | | | | 5.1 9 | 95-50 | | | | | 5.1 10 | 95-50 | | | | | | | | | |

FLIGHT MANUAL

Approved 330 L 0.0.P5 A 17-25 Page 5

| | | | | | | SECTION, PAGE | DATE | (1) | (2) | (3) | | SUP or APP | CODE | | | | | | | | | | | 5.1 11 | 00-38 | | | | | 5.1 12 | 00-38 | | | | | 5.1 13 | 00-38 | | | | | | | | | |

FLIGHT MANUAL

Approved 330 L 0.0.P5 A 17-25 Page 6

LOG OF APPROVED NORMAL REVISIONS BASIC RFM REVISIONS - EFFECTIVITY (1) (2) EASA | | | | NORMAL REVISION 0 date code 95-50 | NOT ISSUED | | | | | NORMAL REVISION 1 date code 97-40 | | | | | | NORMAL REVISION 2 date code 00-38 | | | | | | NORMAL REVISION 3 date code 05-21 | | | | | | NORMAL REVISION 4 date code 07-42 | | | | | | NORMAL REVISION 5 date code 08-42 | | | | | | NORMAL REVISION 6 date code 09-51 | | | | | | NORMAL REVISION 7 date code 11-47 | | | | | | | | | NORMAL REVISION 8 date code 12-42 | EASA Approval No 10044273 | | | on April 02nd,2013 | | | | | | | | NORMAL REVISION 9 date code 15-09 | Approved on December 7, 2015 under the| | | authority of EASA D.O.A No.21J056 | | | | | Title | Normal revision for improvement | | | | | Revised | 0.0.P1 p1 - 0.0.P5 p1 to p6 - 1.0.P1 p1 - 1.0.P6 p1 -_1.1 p2 | |information| 1.5 p1 - 2.0.P1 p1 - 3.0.P1 p1 - 3.1 p11 - 3.1 p17 - 3.2 p28 | | | and p29 - 4.0.P1 p1 - 4.1 p3, p6, p8, p9 and p10 - 5.1.P1 p1 | | | | | Deleted | None | |information| | | | | | | | | NORMAL REVISION 10 date code 16-18 | EASA Approval No 10061096 | | | on February 23, 2017 | | | | | Title | Addition of MOD 07-28352 (Add new label for regulation request | | | in cockpit when seats ST102 and H140 are installed) in section | | | 2.2 (PLACARDS & INSTRUMENT MARKINGS). | | | | | Revised | 0.0.P5 pages 1 to 6 - 2.2 page 2. | |information| | | | | | Deleted | None | |information| | | | |

FLIGHT MANUAL

Approved 330 L 0.0.P5 A 17-25 Page 7

LOG OF APPROVED NORMAL REVISIONS BASIC RFM REVISIONS - EFFECTIVITY (1) (2) EASA | | | | NORMAL REVISION 11 date code 17-10 | Approved on March 21, 2017 under the | | | authority of EASA D.O.A No.21J700. | | | | | Title | Deletion of paragraph 2.2 in section 2.1 and addition of NOTE | | | in paragraph 3 of section 4.1. | | | | | Revised | 0.0.P5 pages 1 to 7 - 2.1 page 20 - 4.1 page 3. | |information| | | | | | Deleted | None | |information| | | | | | | | | NORMAL REVISION 12 date code 17-25 |EASA approval No. 10062608 | | |on July 13, 2017. | | | | | Title | Section 2.2 deletion of "Post-MOD 07.28352" and addition of "if | | | crashworthy seats are installed". | | | | | Revised | 2.2 page 2 | |information| | | | | | Deleted | None | |information| | | | |

FLIGHT MANUAL

Approved 332 L 2.2 A 95-50 Page 1

SECTION 2.2 PLACARDS & INSTRUMENT MARKINGS 1 PLACARDS The following placards are located within the pilot's field of view. 1.1 Operating Limitations Placard | | | THIS HELICOPTER MUST BE OPERATED IN COMPLIANCE | | WITH THE OPERATING LIMITATIONS SPECIFIED IN THE | | DGAC APPROVED ROTORCRAFT FLIGHT MANUAL - THE | | AIRWORTHINESS LIMITATIONS SECTION OF THE ROTOR- | | CRAFT MAINTENANCE MANUAL MUST BE COMPLIED WITH | 1.2 Emergency Static Pressure System Placard | | | OPERATION OF STATIC PRESSURE | | EMERGENCY SYSTEM | | | | SHUT OFF AIR CONDITIONING | | CLOSE DOORS AND WINDOWS | | TO OBTAIN CORRECTED AIRSPEED REDUCE INDICATED | | AIRSPEED BY 7 TO 8 KT (13 - 15 km/h). | | TO OBTAIN TRUE ALTITUDE REDUCE INDICATED | | ALTITUDE BY 75 FEET (23 m) | 1.3 VNE Limitation A placard located in the cockpit indicates VNE values. 1.4 Collective Pitch Refer to SECTION 3.2, paragraph 5.3. 1.5 Maximum Permissible Loading The following information is displayed in the cabin or in the cargo compartment. 1.5.1 Cabin Floor A placard in the cabin specifies the maximum load-carrying capacity. | | | C A B I N F L O O R | | LOADING 800 daN/m2 | or Post-MOD OP 22189 | | | C A B I N F L O O R | | | | LOADING 800 daN/m2 | | CABIN FLOOR | | (1.16 lb/in2) | |LOADING : 1500 daN/m2 | or | 2.17 lbf/in2| | | | C A B I N F L O O R | | LOADING 167 lb/ft2 | N

FLIGHT MANUAL

Approved 332 L 2.2A 17-25 Page 2

1.5.2 In the Cargo Bay

Three placards specify the maximum permissible load-carrying capacities per loading area :

* If installed

1.6 Miscellaneous information

Pilot and copilot, if crashworthy seats are installed, the following R placard is added : R

| | | DO NOT STOW ANYTHING UNDER ANY SEAT | | |

2 INSTRUMENT MARKINGS

Color code :

- Red radial line : Minimum or maximum safe limit - Yellow arc : Caution range - Green arc : Normal operating range - Red triangle : Transient limit values - White triangle : Equipment operating limit - Yellow hatched line : Intermediate contingency rating limit - Red hatched line : 2 min 30 s rating limit (maximum contingency)