DPF-10-01-D
PROCEDURE DIRECTIVES IN-FLIGHT ACCEPTANCE OF PRODUCTION HELICOPTERS Warning:
Before using this document, make sure that this version is the one in force for the requirement to be met.
Author's summary: This document, directly resulting from DHP 1001 B, is in response to an immediate and daily need: - the servicing of production helicopters having to make optimization flights - presentation of these helicopters to the Aviation Authorities, and then to the Customer Modifications made by Version D Version D arises from the transfer of responsibility for weighing, checking of flight manuals, and flight training. The document has also been shortened.
Working group: J P Meunier (Flight Testing) R Bonnefous (Quality CAAC), B Re (Quality CAAC), E Lagneau (Production CAAC) F Guilherme (Production CAAC), T Janulewicz (Quality CAAC) T Moneclaey (Quality CAAC) Y Lescaudron (Production CAAC), Begani (Quality CAAC), Clerico (Quality CAAC) R Borlouoglou (Delivery CAAC) G Desvaux (Flight Testing)
Name:
Technical Leader: JP Meunier
For application: P Burtin
Signature:
Signed
Signed
Date:
9 December 1997
9 December 1997
1 "This document is the property of EUROCOPTER. It may not be communicated to third parties and/or reproduced without the prior written consent of EUROCOPTER and its contents may not be disclosed." © EUROCOPTER 11/1995
DPF-10-01-D HISTORY OF MODIFICATIONS
DATE
PART MODIFIED
PURPOSE OF MODIFICATION
28/10/88
Whole document
- DHP 1001 cancels and replaces DHN 018 with DHP 1003
07/04/89
Whole document
- Embodiment of DHP 1001 A
01/09/91
Whole document
- Embodiment of DHP 1001 B, following harmonization with Ecureuil and post Production approval operation
15/11/95
Whole document
- Transformation of DHP 1001 B to DPF 10-01-C
09/12/97
Whole document
- Updating: DPF 10-01-C becomes 10-01-D (transfer of responsibility for weighing, flight manuals and flight training, addition of VTP and shortening of document)
CONTENTS CHAPTER 0 – PURPOSE & KEY................................................................................................................................................4 CHAPTER 1 – GENERAL PRINCIPLES ...................................................................................................................................5 CHAPTER 2 – PROCEDURE........................................................................................................................................................6 § 2.1 BLOCK DIAGRAM ..........................................................................................................................................................6 § 2.2 FLIGHT LINE ACCESS INSPECTION – FLIGHT LINE TRANSFER INSPECTION......................................7 § 2.3 PREPARATION FOR FLIGHT – GENERAL..............................................................................................................7 § 2.4 PREPARATION FOR RUN-UPS.................................................................................................................................12 § 2.5 FLIGHT ACCEPTANCE................................................................................................................................................15 § 2.6 PRESENTATION OF AIRCRAFT TO AVIATION AUTHORITIES...................................................................16 § 2.7 CUSTOMER ACCEPTANCE/AIRCRAFT DELIVERY.........................................................................................18 CHAPTER 3 - RESPONSIBILITIES..........................................................................................................................................22 § 3.1 PRODUCTION CAAC....................................................................................................................................................22 § 3.2 QUALITY CAAC.............................................................................................................................................................22 § 3.3 FLIGHT TESTS................................................................................................................................................................22 § 3.4 DELIVERY CAAC..........................................................................................................................................................22 § 3.5 CUSTOMER SERVICE DEPARTMENT...................................................................................................................22 Appendix 1: WORK BOOK CT 113 Appendix 2: Page 2/2 of the document "APPENDIX II" Appendix 3: Pages 1 and 2 of the document "APPENDIX III" Appendix 4: AIRCRAFT DOCUMENTATION
2 "This document is the property of EUROCOPTER. It may not be communicated to third parties and/or reproduced without the prior written consent of EUROCOPTER and its contents may not be disclosed." © EUROCOPTER 11/1995
DPF-10-01-D DOCUMENTS QUOTED The documents quoted in this booklet are identified in the text by a figure in brackets (-) and are listed below. REFERENCE NUMBER
SUBJECT OF QUOTATION (DOCUMENT TITLE)
REFERENCE OF DOCUMENT QUOTED QAMA 10-33
1
Visite Entrée Piste (Flight Line Access Inspection)
2
Visite Sortie Montage (Assembly Roll-out Inspection)
QAMA 10-29
3
Pesée des Appareils (Weighing of Aircraft)
704 A 06 0001
4
Mise à jour des Manuels de Vol (Updating of Flight Manuals)
5
Gamme de travaux de la sortie chaîne à la livraison client des appareils (Aircraft Work Scheme from Production roll-out to Customer Delivery)
332 A 04 1515 365 A 04 0561 350 A 04 0026
6
Essais Pluie (Rain Tests)
332 A 04 0902 365 A 04 0409 350 A 04 0020
7
Balise de Détresse (Emergency Locator Transmitter)
DPF 06-03
8
Compensation des Systèmes de cap (Compensation of Heading Systems)
DHN 1-027
9
Visite avant Services Officiels (Inspection before Presentation to the Aviation Authorities)
QAMA 10-35
10
Documentation Appareils (Aircraft Documentation)
QAMA 10-11
11
Agrément de Production (Production Organization Approval)
12
Réception Constructeur / Acceptation DPM/SQ des Hélicoptères de Série (Manufacturer's Acceptance / DPM/SQ Acceptance of Production Helicopters)
13
Livraison Contrats Série (Production Contracts Delivery)
14
Stockage des Hélicoptères Eurocopter (Eurocopter Helicopter Storage)
15
Opérateurs ayant délégation d'inspection (Operators delegated for inspection)
QAF 05-04
P 02 QAMA 10-08
DPF 03-04 703 A 90 0015 QAMA 10-30 A75
3 "This document is the property of EUROCOPTER. It may not be communicated to third parties and/or reproduced without the prior written consent of EUROCOPTER and its contents may not be disclosed." © EUROCOPTER 11/1995
DPF-10-01-D
CHAPTER 0 – PURPOSE & KEY PURPOSE The purpose of this document is to define the sequence of operations concerning all Production Helicopters from production line roll-out to delivery. KEY AEMG CAAC CDN CEIRB CEV CI CLN CT 113
C of A
RC NAC CT 113
DCAc DEV DGAC DPM/SQ FC FME FT GSAC IPC LS MET MMA MRR MST NT PF 1 PFA PFS PRE SB SPAE STNA TSA TSS
CDS
VA1 VAD VC1 VEP VIV VSM VSO VTP
BFF ALF
TS IPC SL MET MMA MRR MST TN
MSR SB
TA
Autorisation d'Exportation de Matériel de Guerre Centre d'Affaire Appareils Commercialisés Certificat de Navigabilité Certificat d'Exploitation de l'Installation Radio Électrique de Bord Centre d'essais en vol Certificat d'Immatriculation Certification de Limitation de Nuisance Carnet de travaux (ou "Forme 113" ou "cahier de Retouches") Direction des Constructions Aéronautiques Demande Essais en Vol Direction Générale de l'Aviation Civile Direction des Programmes des Méthodes d'acquisition et de la Qualité Fiche Client Fiche Matricule d'Équipement Fiche Technique Groupement pour la Sécurité Aviation Civile Catalogue Illustré des Pièces Lettre Service Manuel d'Entretien Manuel de Maintenance Aéronef Manuel de Réparation Manuel de Stockage Note Technique Premier Point Fixe Point Fixe avant 1er vol Point Fixe de Sortie Programme Recommandé d'Entretien Service Bulletin Service des Programmes Aéronautiques Service Technique de Navigation Aérienne Travaux systématiques avant vol Travaux systématiques après vols de mise au point ou travaux systématiques de sortie Visite avant 1er vol de la journée Visite après dernier vol de la journée Visite certificat 1er vol Visite entrée piste Visite inter-vol Visite Sortie Montage Visite avant Présentation aux Services Officiels Visite de Transfert Piste
Authorization to Export War Equipment Commercialized Aircraft Business Center Airworthiness Certificate Aircraft Radioelectric Installation Operating Certificate Flight Test Center Registration Certificate Noise Abatement Certificate Work Book (or "Form 113" or "Repair Book") Directorate of Aeronautical Constructions Flight Testing Request French Civil Aviation Authority Programs, Acquisition Methods and Quality Department Customer Data Sheet Equipment Log Card Technical Sheet Civil Aviation Safety Group Illustrated Parts Catalog Service Letter Maintenance Manual Aircraft Maintenance Manual Repair Manual Storage Manual Specification First Run-up Run-up before 1st Flight Roll-out Run-up Master Servicing Recommendations Service Bulletin Aeronautics Program Department Air Navigation Technical Department Routine Work Before Flight Routine Work after Optimization Flights or Routine Roll-out Work Check before 1st flight of day Check after last flight of day 1st flight certification inspection Flight Line Access Inspection Turnaround Check Assembly Roll-out Inspection Inspection before Presentation to Aviation Authorities Flight Line Transfer Inspection
4 "This document is the property of EUROCOPTER. It may not be communicated to third parties and/or reproduced without the prior written consent of EUROCOPTER and its contents may not be disclosed." © EUROCOPTER 11/1995
DPF-10-01-D CHAPTER 1 – GENERAL PRINCIPLES An analysis of the acceptance procedure for production helicopters defines the following key phases in aircraft acceptance: -
Flight Line Access Inspection or Flight Line Transfer Inspection which marks the end of manufacture and the start of tests.
-
1st Run-up: The aircraft runs for the first time.
-
1st Flight: The aircraft really begins its in-flight check
-
Presentation to the Aviation Authorities: The aircraft is completed.
-
Acceptance: This is the culmination of the manufacture and test process.
-
Delivery: The Customer takes possession of its aircraft.
This analysis also reveals the importance of certain documents which are preserved even after delivery: -
APPENDIX III, opened by Line Production, follows the aircraft until delivery and certifies correct completion of the major phases of acceptance.
-
The WORK BOOK is the record of all important work carried out from VEP to delivery.
5 "This document is the property of EUROCOPTER. It may not be communicated to third parties and/or reproduced without the prior written consent of EUROCOPTER and its contents may not be disclosed." © EUROCOPTER 11/1995
DPF-10-01-D
CHAPTER 2 – PROCEDURE § 2.1 - BLOCK DIAGRAM
Flight Line Access Inspection Flight Line Transfer Inspection
Preparation for Flights – General
Preparation for Run-ups
In-Flight Acceptance
Presentation to Aviation Authorities
Customer Acceptance – Aircraft Delivery
6 "This document is the property of EUROCOPTER. It may not be communicated to third parties and/or reproduced without the prior written consent of EUROCOPTER and its contents may not be disclosed." © EUROCOPTER 11/1995
DPF-10-01-D § 2.2 – FLIGHT LINE ACCESS INSPECTION & FLIGHT LINE TRANSFER INSPECTION The Flight Line Access Inspection or Flight Line Transfer Inspection defines the conditions for transfer of the helicopters to production flight tests. These inspections are the responsibility of the Quality CAAC. Their fields of application are defined by: QAMA 10-33 for the Flight Line Access Inspection (1) QAMA 10-29 for Flight Line Transfer Inspection included in VSM (2) These inspections are carried out by one or more VEP Quality representatives and involve functional verification of the different systems, testing of the "Safety" systems, recording of Quality defects, and checking aircraft conformity with the Customer Data Sheet and the Flight Manual. During these inspections, the VEP Quality representative checks flight manual conformity according to QAF 05-04 (4). § 2.3 – PREPARATION FOR FLIGHT – GENERAL 2.3.1
APPLICATION FOR PASS & REGISTRATION
According to the legislation in force, no aircraft may begin its run-ups and flights without registration and pass. For Manufacturer optimization flights, temporary registration is provided by the Production Flight Test Operations office. It has the following form: F-WW … for civil aircraft under GSAC supervision; it is accompanied by a pass with restricted use allowing Manufacturer's optimization. F-Z … for "GOVERNMENT" or "Export Military" aircraft under DPM/SQ control. A) Aircraft under GSAC supervision All aircraft under GSAC supervision must have an airworthiness document on board (pass or C of A). For production acceptance flight tests, the Production Flight Test Department applies to the GSAC for the pass. This pass application is initiated when the transfer authorization in Appendix III is signed by the VEP authorized personnel. For aircraft undergoing a specific test during an acceptance cycle (DEV), an exceptional pass must be requested from the DGAC. This DGAC pass must also be obtained for accepted aircraft intended for Customer flight training on French territory, or ferrying with Manufacturer's crew outside French territory. B) Aircraft under DPM/SQ control After transfer acceptance by VEP Quality, the flight line transfer authorization must be signed by the DPM/SQ, on page 1 of Appendix III. No pass is requested. The temporary registration assigned by Production Flight testing and the DPM/SQ signature on Appendix III are sufficient to authorize flight.
7 "This document is the property of EUROCOPTER. It may not be communicated to third parties and/or reproduced without the prior written consent of EUROCOPTER and its contents may not be disclosed." © EUROCOPTER 11/1995
DPF-10-01-D For aircraft accepted by the DPM/SQ which have to go to France or abroad, a registration certificate must be requested from the DCAc. This registration certificate replaces the pass. 2.3.2
WORK BOOK
A) DESCRIPTION This document records all work, anomalies, or missing items ascertained at the different stages between transfer of the aircraft to Production Flight testing and delivery to the Customer. It is the only document in which remarks and work requests are to be entered by authorized persons.
Maintenance operations Request Signature CREW
Type Unit hours REMARK – ANOMALY Brief description of fault – Suggestions – Signature
Order No.
CE CP
SPECIFIC MONITORING 1 2
M
CYCLES
R WORK TO BE DONE – DECISION – Signatures
Flight testing
Quality
Quality
Production control Delegated certified operators Design office
Design office
Unit Report
Hours
Flight of day Totals
Flight type Flight No. Start time
Aircraft Type Availabili ty Indispen sable?
EXECUTION REPORT and information for monitoring of components moved Description and position
Reference
Serial No
No. Page No. Date
Inspection signature and date TS No.
Valida tion
Flight testing Quality Delegated certified
Flight testing
?
AIR ACTIVITY
Authorizations according to columns:
All personnel
The WORK BOOK thus makes it possible: -
To order the work and certify the following: -
-
Work execution report Daily maintenance inspections Checking of all operations performed Flight-by-flight knowledge of equipment aging
To record and manage postponed work.
The WORK BOOK does not replace certificates in use elsewhere (in particular Appendix III). It remains in force until effective delivery of the aircraft, but must not be delivered with it. B) RULES FOR USE OF THE WORK BOOK After the aircraft has been handed over to Flight Testing, no major work or operation can be carried out on the Flight Line if not previously entered in this document. Minor defects will be noted in the Quality File. The WORK BOOK must be clearly written. A new entry must be made for each operation.
8 "This document is the property of EUROCOPTER. It may not be communicated to third parties and/or reproduced without the prior written consent of EUROCOPTER and its contents may not be disclosed." © EUROCOPTER 11/1995
DPF-10-01-D Entries are to be numbered from 1 to …n in the column "Order No. .." The number will be repeated opposite the execution note if the latter is not shown on the same page. The designation of each entry must be written clearly. For example, No. 100 – MOD embodiment No. 325 radome tightness". The remaining MODs and sketches to be embodied concerning flight acceptance, identified in a list, must be entered in a reminder entry in the WORK BOOK. No aircraft can be made available for a run-up or a flight until all the remarks in the WORK BOOK have been corrected or postponed. The WORK BOOK is a technical document which must not be used as a "correspondence book" between the different departments. After signature, the green and pink sheets are to be detached by Production Flight Testing during flights, and by Quality from the VSO onwards. The green sheets are for action and filing by the Flight Line Quality Department. The pink sheets are analyzed and filed by Production Flight Testing. C) POSTPONED WORK All corrective action that is not mandatory from the standpoint of safety or good flight operation (repair, MOD) may be postponed. Only Flight Testing is authorized to postpone a technical entry. This will be noted in the column "Execution Report," and a reminder will be written on the appropriate flap. The name, date and signature of the person postponing the work must be shown. However, anomalies or remarks (of an administrative nature) entered in the WORK BOOK by Quality may be postponed by the Quality Manager of the sector (e.g. Awaiting updating of a technical note). 2.3.3
DEFINITION AND CYCLE OF ROUTINE CHECKS
A) Definition of checks Routine checks are carried out daily. For each day of flight, the following inspections must be made: -
A check "before the first flight" of the day (called VA1) This check is performed on completion of all repair and maintenance operations immediately before the first flight of the day. This check must be preceded by the VAD (see below).
-
One or more "turnaround" checks These checks, which comprise a check after and before flight, are carried out at the request of the crew between different flights in the same day.
-
A check "after the last flight" of the day (VAD) This check is made after the last flight of the day.
B) Execution of checks -
The program of these checks is defined in the aircraft maintenance manual, or in specific documents issued by Quality or in the flight manual (turnaround check). It also includes the embodiment of Design Office directives. 9 "This document is the property of EUROCOPTER. It may not be communicated to third parties and/or reproduced without the prior written consent of EUROCOPTER and its contents may not be disclosed." © EUROCOPTER 11/1995
DPF-10-01-D -
VA1 and VAD type checks are carried out by the Flight Line Quality Department or by the "flight line engineer" personnel delegated for flight line quality inspection pursuant to QAMA 10-30 A 75 (15).
-
Turnaround checks are carried out under the responsibility of the crew.
-
All these checks are certified in the corresponding check boxes of the WORK BOOK.
NB: The checking of repairs made on line outside the workshop and resulting from a flight or a run-up is the responsibility of the crew or the Production Flight Testing personnel authorized for "run-ups". Flight Line Quality may intervene at the request of Production Flight Testing. This check is recorded by a signature next to the entry made in the WORK BOOK. During the VA1 type check which follows, the Flight Line Quality Department guarantees compliance with standard practice and continued compliance by the indications given in the entries marked "done on flight line". NB: In the case of major work, at the request of the crew or of authorized Production Flight Testing personnel, the above provisions may be suspended. C) Check validity -
VA1 type checks are valid for 1 day VAD type checks are valid for 7 days.
If an aircraft is grounded for more than one week, the aircraft is considered as "temporarily stored". In this case the Storage Manual (MST) and specifications in force must be followed. D) Special procedure for checks For aircraft in the process of acceptance carrying out external missions (ferrying, demonstrations) and very exceptionally at Marignane, the Flight Testing crews themselves are responsible for carrying out the checks described above. In this case, they must certify the corresponding checks in the WORK BOOK before flight.
2.3.4
PREPARATION FOR RUN-UPS AND FLIGHTS
A) Standard flight program Depending on the aircraft configuration, the Production Flight Test Department prepares the list of standard flights to be performed. This document, called "Appendix II" (see Appendix 2) also provides the weights and centers of gravity necessary to perform each type of flight, i.e.: -
quantity of fuel ballast weight and position
B) Optional equipment / Aircraft configuration When it leaves the production line, after acceptance, the aircraft is transferred to the flight line workshop as defined by the Customer Data Sheet. The Customer Data Sheet is used to distinguish the following: -
Optional equipment installed on the aircraft Optional equipment delivered to accompany the aircraft. These items are sent to the flight line start-up store (see note below). Optional equipment delivered separately (in a case), with shipment circuits different from the helicopter acceptance circuit.
10 "This document is the property of EUROCOPTER. It may not be communicated to third parties and/or reproduced without the prior written consent of EUROCOPTER and its contents may not be disclosed." © EUROCOPTER 11/1995
DPF-10-01-D Optional equipment installed on aircraft is tested in flight (e.g. de-icing). However, in equipment delivered to accompany the aircraft the following are distinguished: -
Items for which a simple ground presentation is made to check compatibility of fixed and mobile parts (e.g. troop seats, skis). This operation must be done on the assembly line. In the case of a proven impossibility, the presentation(s) will be done on the flight line. This will be requested by an entry in the WORK BOOK.
-
Items tested in flight on a routine basis, or occasionally (e.g. hoists or slings), in particular for first production aircraft at the request of Production Flight Testing or the Aviation Authorities.
NB: For optional equipment delivered to accompany aircraft, in compliance with the Customer Data Sheet (FC), for example hoist, sling, etc, the line manager shall give a complete inventory of this equipment in the transfer book. This optional equipment delivered to accompany the aircraft must be presented to the DPM/SQ at time of acceptance. C) Availability of aircraft for run-up or flight When an aircraft is available for a run-up or a flight, the WORK BOOK is given to the Production Flight Operations office. From this time on, any work on this aircraft could hinder the check before run-up or flight. For this reason all work is subject to the prior approval of the workshop manager and especially of the crew. The suspension of the aircraft's availability will be indicated by taking the WORK BOOK back from the Production Flight Operations office. For persons not belonging to Flight Testing Personnel, the Flight Line workshop or Flight Line Quality, access to an aircraft ready for flight or run-up is subject to approval by the Flight Line Engineer responsible for the aircraft. For persons outside the Company (for example, outside contractors), access to the hangars or flight line is controlled by the facility's Security Department. 2.3.5
MAINTENANCE WORK REQUESTED IN THE WORK BOOK
Non-routine maintenance work will be requested in the WORK BOOK following anomalies, airworthiness recommendations, service bulletins, airworthiness directives, etc. Barring exceptional cases, which will be noted in a "postponed" entry by Production Flight Testing, this non-routine work must be carried out. General rules concerning this work -
For any replacement of parts or components, use the documentation appropriate for the work (Technical Sheet, specification, maintenance manual and work cards) which specifies the operating method, the values to be observed (dimensions, clearance, etc) and the check procedures. The documentation section of Customer Service is responsible for preparing and updating the documents used by Production Flight Line (MET, MMA, MRR, PRE, MST and IPC).
-
In some cases, however, at the request of the Design Office, Quality or Flight Testing, an operating check may be required during a run-up or a flight.
11 "This document is the property of EUROCOPTER. It may not be communicated to third parties and/or reproduced without the prior written consent of EUROCOPTER and its contents may not be disclosed." © EUROCOPTER 11/1995
DPF-10-01-D -
The values to be checked during these functional checks do not need to be recorded if they are within the tolerances defined by the documentation. The test reports issued during the initial functional production-line tests will consequently not be repeated.
-
In the WORK BOOK, write "replacements or operating tests carried out in accordance with document No. … or certified by …"
-
Any work concerning one of the four safety systems, or that may interfere with one of these systems (flight controls, auxiliary controls, transmission, rotor head and blade attachments) must be followed by a second check.
-
In the case of oil "leaks" in the Transmission Systems, follow the procedure defined in the documents in force (TNs, work cards).
These operations are to be carried out by personnel "authorized for Transmission Systems ". 2.3.6
WORK SCHEME ON PRODUCTION AIRCRAFT FROM LEAVING THE PRODUCTION LINE TO CUSTOMER DELIVERY
The work scheme on production aircraft from leaving the production line to Customer delivery covers all routine operations and checks to be carried out on all aircraft during the flight line cycle and delivery to Customer. This four-part document is prepared by the Preparation Department in agreement with the Design Office, Quality and Flight Testing, and constitutes a report of the execution and check of routine work. This sheet is specific to each type of aircraft (5) Super Puma: TN 332 A 04 1515 Dauphin: TN 365 A 04 0561 Ecureuil: TN 350 A 04 0026 § 2.4 – PREPARATION FOR RUN-UPS 2.4.1
This preparation is defined by the work scheme (§ 2.3.6) and concerns:
a) Installation of blades b) Installation of squibs (basic and optional) c) Oil levels and top-ups d) Provisional weighing This operation is the responsibility of Quality in accordance with document 704 A 06 0001 (3) e) Installation of test installations The measuring equipment is limited to the installations necessary for acceptance flights. It is defined by Production Flight Testing for each type of aircraft in standard flight reports. Any additional installation on a production aircraft, for a special check, must form the subject of a Flight Testing Request. f) Installation of dual controls For safety reasons during acceptance tests, all aircraft must be fitted with dual controls. No exemption from this rule is allowed unless approved by the Head of Flight Personnel. 12 "This document is the property of EUROCOPTER. It may not be communicated to third parties and/or reproduced without the prior written consent of EUROCOPTER and its contents may not be disclosed." © EUROCOPTER 11/1995
DPF-10-01-D g) Seats All aircraft must be fitted with seats having a high back and safety belt. The fitting of a third crew member seat may be requested by Production Flight Testing. h) Installation of shuttle radio equipment For aircraft having no radio equipment or only partial radio equipment according to the Customer Data Sheet definition, the following shuttle components at least must be assembled: Intercom system Transponder with alti-coder Artificial horizon Two VHFs or one VHF if the aircraft already has one i) Check and preparation of aircraft Make a standard check "before first flight" in accordance with the maintenance manual. Load the quantities of fuel and ballast in compliance with Appendix 2. 2.4.2
FIRST RUN-UP (PF1)
The date of the first aircraft run-up shown in Appendix III is the reference point for the start of the "Production Flight Testing cycle". The Run-up program is defined by Flight Testing. The purpose of the Run-up is as follows: -
to depreserve the engine and transmission systems
-
to check the adjustment of the engines and rotor head and blades (tracking and balance). As the engines are under Manufacturer's guarantee, the presence of a representative of the Manufacturer is desirable.
-
to make a general operating check of the aircraft, the electric power supplies, the radio and navigation equipment, and to detect any interference.
On completion of the first Run-up, the authorized Flight Testing Personnel enter in the WORK BOOK the repairs and adjustments carried out during the Run-up (even if these repairs do not need to be followed by work in the workshop). Once the Run-ups are finished, the aircraft goes to the check before first flight. 2.4.3
ROUTINE WORK AFTER 1ST RUN-UP (TSA)
These operations follow the flight line work schemes described in Chapter 2.3.6 (5) and are as follows: a) Spectrometric analysis of engine oils after run-up b) Inspection of magnetic plugs c) Fuel sampling d) Hot draining of transmission systems
e) Inspection of filters f) Return to flight configuration 13 "This document is the property of EUROCOPTER. It may not be communicated to third parties and/or reproduced without the prior written consent of EUROCOPTER and its contents may not be disclosed." © EUROCOPTER 11/1995
DPF-10-01-D g) Installation of safety equipment: emergency locator transmitter, emergency floatation gear, first-aid kit If these items of equipment are installed on an aircraft, they must be operative throughout the acceptance flights. For precautions of use and servicing of the emergency locator transmitters, see: - DPF 06-03 (7) A shuttle first-aid kit must be on board the aircraft during all the acceptance flights. The flight line engineers are responsible for ensuring that this kit is present and for overseeing it.. The alignment and its validity are the responsibility of Flight Testing. 2.4.4
1ST FLIGHT CERTIFICATION INSPECTION (VC1)
When the aircraft is finished and ready for its first flight, the Flight Line Quality Department certifies Appendix III and Inspection VC1 in the WORK BOOK. A test Run-up (PFA) is then performed before the first flight. 2.4.5
RUN-UP BEFORE 1ST FLIGHT (PFA)
This run-up consists of the following: -
A general check of the aircraft and of all repairs noted during the first Run-up.
-
When this Run-up is satisfactory, the aircraft is declared ready for 1st flight by Production Flight Testing staff which then sign Appendix III.
This run-up will be followed by a turnaround check. 2.4.6
CORRECTION OF HEADING SYSTEMS
A) The correction method is defined in document DHN I-027 (8) A manual correction is made to adjust the standby compass or for a gyroscopic heading system that does not require great accuracy. It may be postponed depending on the servicing requirements. For aircraft equipped with a self-contained navigation system, this operation will be carried out with the rotor turning or directly in flight before the navigation flight. B) After correction, the following operations are to be carried out: -
The standby compass deviation record sheet is to be completed and displayed in the aircraft
-
For gyrocompass, the compensation curve is to be filed in the aircraft file.
-
The magnetic bearing of the radio-compass is to be checked and any tests of installations to be checked in a clear area.
14 "This document is the property of EUROCOPTER. It may not be communicated to third parties and/or reproduced without the prior written consent of EUROCOPTER and its contents may not be disclosed." © EUROCOPTER 11/1995
DPF-10-01-D § 2.5 – IN-FLIGHT ACCEPTANCE 2.5.1
AIRCRAFT ACCEPTANCE FLIGHTS
For production aircraft, "standard" flights have been defined by Flight Testing in agreement with the Aviation Authorities. The program of these flights is shown in the standard flight reports which are grouped in Flight Testing documents called "Appendix 6 and Appendix 6A". After each flight, the crew will analyze the defects and decide on the action to be taken with the Production FlightLine crew. For aircraft with a high level of complexity, the first flight may be followed by a debriefing meeting on the initiative of Production Flight Testing. The fuel and ballast are loaded on the flight line by the flight line engineer responsible for the aircraft, in compliance with the Flight Test document, Appendix II. This operation is under the responsibility of the flight engineer. The Flight Line Quality Department does not check it. The checks to be made during optimization flights are defined in Chapter 2.3.3. After each flight, check that all the repairs in the WORK BOOK have been executed, or postponed by Production Flight Testing. Once all the optimization flights are completed, the aircraft is ready to be transferred to the painting or VIP phase. Aircraft not requiring painting or trimming go directly to the TSS phase or to VSO preparation (see § 2.5.7). 2.5.2
AIRCRAFT PAINTING
This is generally carried out after the acceptance flights, to limit possible damage which may require repairs. This phase is presently carried out by a contractor outside Eurocopter under the responsibility of Eurocopter Quality CAAC. 2.5.3
VIP OR COMFORT INSTALLATION PHASE
This phase comprises the installation of trimmings, seats, etc, for so-called "VIP" versions or "Comfort" versions. It is also carried out after the flights to prevent any deterioration. 2.5.4
RAIN TESTS
These tests are carried out after the end of the optimization tests and the painting phase to check that no deterioration has occurred with respect to the tests and the waterproofing executed during the production line ground tests. They are described in the specifications (6): Super Puma: 332A 04 0902 Dauphin: 365 A 04 0349 Ecureuil: 350 A 04 0028 2.5.5
TEST RUN-UP AFTER PAINTING AND VIP PHASE
Once the aircraft is finished (repairs, Code 2 postponed operations, inspections and checks carried out), it is taken out for a run-up to check correct reinstallation before flight.
15 "This document is the property of EUROCOPTER. It may not be communicated to third parties and/or reproduced without the prior written consent of EUROCOPTER and its contents may not be disclosed." © EUROCOPTER 11/1995
DPF-10-01-D 2.5.6
TEST FLIGHT AFTER PAINTING, VIP AND RAIN TESTS
A test flight is carried out after painting operations and (or) VIP installation and rain tests. When the test run-up and flight are satisfactory, the flight engineer declares "aircraft fit for preparation for presentation to the Aviation Authorities" by entering this in the WORK BOOK. 2.5.7
ROUTINE WORK AFTER OPTIMIZATION FLIGHTS (TSS) AND PREPARATION FOR PRESENTATION TO THE AVIATION AUTHORITIES
This work includes the operations defined in the Flight Line Work Schemes (§ 2.3.6). For the Ecureuil family, no TSS is carried out but only VSO preparation which however includes certain phases of it. 2.5.8
ROLL-OUT RUN-UP (PFS )
The finished aircraft is taken out for the PFS. This Run-up allows checking of correct reinstallation and good final operation. If this aircraft is under DPM/SQ control, a representative from this organization may attend. 2.5.9
INSPECTION BEFORE PRESENTATION TO THE AVIATION AUTHORITIES (VSO)
This inspection is carried out by the Flight Line Quality Department in accordance with QAMA 10-35 (9) before DPM/SQ presentation and acceptance for military aircraft or Manufacturer acceptance for civil aircraft. 2.5.10
OFFICIAL WEIGHING
This is done under the responsibility of Quality when the aircraft is finished, in accordance with document 704 A 06 0001 (3). § 2.6 – PRESENTATION OF AIRCRAFT TO AVIATION AUTHORITIES The aircraft is presented to the Aviation Authorities by Quality in accordance with document QAMA 10-08 (12). This presentation marks the end of the Production Flight Testing Acceptance cycle. After having done the following: -
Completed Appendix III, page 2, by the signatures of: the crew which certifies favorable acceptance of the aircraft the Production CAAC manager who certifies the completion of the aircraft according to the Customer Data Sheet the head of Production Flight Testing Quality which certifies compliance of the aircraft with the Customer Data Sheet and the customized Flight Manual, by signing the Certificate of Conformity
-
Compiled the aircraft documentation in accordance with QAMA 10-11 (10),
-
Checked the presence of the AEMG for military aircraft,
The group leader of Flight Line Quality presents the aircraft to the Aviation Authorities.
16 "This document is the property of EUROCOPTER. It may not be communicated to third parties and/or reproduced without the prior written consent of EUROCOPTER and its contents may not be disclosed." © EUROCOPTER 11/1995
DPF-10-01-D For aircraft under DPM/SQ control, the Quality Department presents the aircraft file for acceptance. For aircraft under GSAC supervision, Eurocopter Quality performs Manufacturer's acceptance, under the authority of DGAC Production Organization Approval No. P 02 (11), allowing the DGAC C of A to be claimed from the GSAC. 2.6.1
AIRCRAFT UNDER DPM/SQ CONTROL
This concerns GOVERNMENT aircraft or aircraft for which the Customer has asked this body to check it. An expert from the DPM/SQ may ask to take part in an optimization or test flight (except first flight). The DPM/SQ checks the aircraft file and consults the CEV for in-flight checking operations. On completion of the CEV flights, any remarks or anomalies specified by the CEV or by the DPM/SQ must be noted in the WORK BOOK. Production Flight Testing must be consulted for the action to be taken. The DPM/SQ then gives its opinion: Either this is favorable, and acceptance of the aircraft may be declared, Or it is unfavorable, and the aircraft is returned to the Manufacturer for additional optimization. In this case the aircraft is Adjourned. CE 102: After signature by the Manufacturer, this document allows the Aviation Authorities to declare acceptance. An aircraft under DPM/SQ control may be sampled as a batch aircraft when the contract specifies this. It is transferred to the CEV for special checks, performance checks, etc. During its stay with this organization, Eurocopter is required to supply any spare parts required. IDENTIFICATION PLATE Quality punches the identification plate which must be affixed to the aircraft. AIRCRAFT LOG BOOKS, ROUTE LOG BOOK These are certified by DPM/SQ after acceptance for government aircraft. ENGINE LOG BOOKS These are filled in by Quality (flight hours entered). 2.6.2
AIRCRAFT UNDER GSAC SUPERVISION
The Quality Department performs Manufacturer's acceptance of aircraft under GSAC supervision. This acceptance is indicated by the signing of the Certificate of Conformity by an authorized person from the Quality Department with reference to DGAC Production Organization Approval No. P02 (11). C of A/CLN Based on this Certificate of Conformity, the DGAC delivers the C of A/CLN, without routine work by the GSAC.
17 "This document is the property of EUROCOPTER. It may not be communicated to third parties and/or reproduced without the prior written consent of EUROCOPTER and its contents may not be disclosed." © EUROCOPTER 11/1995
DPF-10-01-D IDENTIFICATION PLATE The Quality Department completes the identification plate and stamps it with the reference of the Production Organization Approval (P02). It is then affixed to the aircraft. AIRCRAFT LOG BOOKS, ROUTE LOG BOOK AND ENGINE LOG BOOK These are updated and certified by Quality after Manufacturer's acceptance. AIRCRAFT RADIOELECTRIC INSTALLATION OPERATING CERTIFICATE (CEIRB) Aircraft registered in France must obtain the CEIRB; some export aircraft need a Certificate of Conformity for radio equipment, if the contract requires it. At the request of the Quality Department, the STNA prepares and signs these documents which are included in the aircraft file given to the Customer at delivery. French aircraft leave the factory with a temporary CEIRB and the Radio Book issued by the Quality Department. The final CEIRB is sent by the STNA directly to the Customer based on the Certificate of Conformity sanctioning the Manufacturer's acceptance. NB: 1: Throughout DPM/SQ acceptance or Manufacturer's acceptance, no work may be carried out on the aircraft without the approval of the authorities responsible for acceptance. § 2.7 – CUSTOMER ACCEPTANCE / AIRCRAFT DELIVERY 2.7.1
PREPARATION FOR TRANSFER TO THE HELICOPTER DELIVERY DEPARTMENT
The aircraft is restored to the configuration defined by the Customer data sheet. If appropriate, the shuttle radio installation is left on board (for Customer flight, flight training or ferrying). 2.7.2 TRANSFER OF AIRCRAFT TO THE HELICOPTER DELIVERY DEPARTMENT Transfer to the Helicopter Delivery Department takes place after a "transfer inspection" carried out by Quality in accordance with QAMA 10-08 (12). While the aircraft is at the Delivery Department, servicing, work, and VAD and VA1 checks are performed by Production and Production Flight Line Quality until the physical departure of the aircraft. The commercial aspect of the aircraft delivery process is covered in DPF 03-04 (13). 2.7.3
CUSTOMER WAITING TIME
Depending on the waiting time, renewal of the C of A and pass should be planned (to maintain airworthiness). A Run-up, maintenance flight or other operations will be necessary depending on the duration of grounding (comply with the maintenance documentation).
18 "This document is the property of EUROCOPTER. It may not be communicated to third parties and/or reproduced without the prior written consent of EUROCOPTER and its contents may not be disclosed." © EUROCOPTER 11/1995
DPF-10-01-D 2.7.4
PREPARATION OF CUSTOMER FLIGHTS
Except in special cases, a Run-up will be made before these flights if the aircraft has not flown for more than 7 days. If the aircraft has stayed for more than a month at the Helicopter Delivery Department, a test run-up and flight will be made. 2.7.5
CUSTOMER HAND-OVER / CUSTOMER FLIGHT
Hand-over can take place before or after the Customer flight. -
For GOVERNMENT aircraft (France), the aircraft is taken by the ferrying organization or the consignee unit before the "Customer" flight usually made by the military crew alone.
-
For CIVIL and EXPORT MILITARY aircraft, the "CUSTOMER" flight is usually made by a mixed crew of Eurocopter and Customer personnel. The Eurocopter pilot acts as flight commander.
Unless special instructions are given, the Eurocopter shuttle equipment will be removed after Customer hand-over (dual controls, shuttle radio, etc). 2.7.6
CUSTOMER REMARKS
The Customer's remarks are entered in a document of "Customer remarks" and followed up by the Helicopter Delivery Department. In-flight remarks giving rise to repairs are to be noted on the CT113 after agreement between F/EV.S and the Customer's crew. After the Customer has signed the hand-over, the aircraft undergoes transfer of ownership. 2.7.7
FINAL REGISTRATION OF FRENCH CIVIL AIRCRAFT
Depending on the contract specifications, the Sales Department, with the Customer, initiates the registration application at the Registration Office. This application includes the identity of the future owner, the home airport, the operator, and the reserved registration number. The reserved registration number must be forwarded to the Customer Data Sheet department of the Economic and Financial Department, for inclusion in the advance C of A application. Based on the Certificate of Conformity signed by Eurocopter Quality Department, the GSAC sends the C of A to Quality and sends a copy to the Registration Office. The Registration Office then issues the CI which is held available for the owner or for Eurocopter, or sent by mail. 2.7.8
"TRAINING" FLIGHTS
The aircraft must be handed over to the Customer (unless approval to the contrary is given by the Sales Department). Production CAAC and Flight Line Quality CAAC continue to provide support and maintenance in the context of Production Organization Approval P02. The use of the WORK BOOK remains in force during this phase. Once the flights are completed and repair and maintenance operations have been carried out, the aircraft will be prepared either for ferrying or for disassembly and shipment. REGISTRATION FOR "TRAINING" FLIGHTS A) French civil aircraft: Training flights may be carried out either under the Customer's registration or under temporary Eurocopter registration. In the latter case, an exceptional Pass for Flight Training must be requested from the DGAC. 19 "This document is the property of EUROCOPTER. It may not be communicated to third parties and/or reproduced without the prior written consent of EUROCOPTER and its contents may not be disclosed." © EUROCOPTER 11/1995
DPF-10-01-D B) Foreign civil aircraft: Training flights are carried out under temporary Eurocopter registration with an exceptional Pass for Flight Training which must be requested from the DGAC by Flight Testing. In addition, during the flight training, the aircraft must be made available to Eurocopter by the Customer; the aircraft is then insured by the Manufacturer. C) Military aircraft: Training flights are carried out under the same temporary registration as during acceptance flights. 2.7.9
DELIVERY & SHIPMENT
Checking that postponed work has been carried out. Removal of shuttle radio components (if appropriate). Removal of first-aid kit. Inventory, according to Customer Data Sheet, of the aircraft and optional items delivered to accompany the aircraft (see "Protocol for transfer of aircraft to Customer Delivery Department"). 2.7.10
AIR FERRYING BY EUROCOPTER CREW
The following must be placed in the helicopter: -
Standard aircraft tool kit (miscellaneous blanks).
-
Additional aircraft tool kit, included in the aircraft contract and taken from Customer Stores (see Customer Data Sheet).
-
Ferrying kit defined by Flight Testing depending on planned route.
-
If necessary, shuttle radio and radio-navigation equipment at the request of Flight Testing according to the aircraft's basic equipment
Reserve tanks (if requested) -
A test flight will be carried out before ferrying. The tightness and flow tests must be performed during this flight. After this flight, the fuel filters are to be checked and changed if necessary.
Nationality markings According to Flight Testing or Sales Department instructions, the Customer's emblems may be masked for ferrying. REGISTRATION FOR FERRYING Temporary registration for ferrying will be provided by Flight Testing operations. 2.7.11
AIR TRANSPORT
The aircraft will be preserved in accordance with the sheet, specification and work cards. In all cases, fuel tanks are to be emptied and neutralized. Transmission systems are also to be preserved, unless instructions to the contrary are mentioned on the Customer Data Sheet or in the Work Book CT 113 by a representative of the Customer Service or Delivery Department. 20 "This document is the property of EUROCOPTER. It may not be communicated to third parties and/or reproduced without the prior written consent of EUROCOPTER and its contents may not be disclosed." © EUROCOPTER 11/1995
DPF-10-01-D Inventory: same procedure as for air ferrying operations as concerns optional items, aircraft tool kits, etc. Disassembly and packaging will be carried out by the Dispatch Department. 2.7.12
SEA TRANSPORT
In Cases or Containers Preservation must be in accordance with the process sheet Disassembly must be in accordance with existing specification. Roll On/Roll Off or in ship's hold The aircraft may fly to the embarkation point. It will then be stored according to the process sheet and disassembled according to the documents.
21 "This document is the property of EUROCOPTER. It may not be communicated to third parties and/or reproduced without the prior written consent of EUROCOPTER and its contents may not be disclosed." © EUROCOPTER 11/1995
DPF-10-01-D
CHAPTER 3 - RESPONSIBILITIES § 3.1 – PRODUCTION CAAC The Production CAAC is responsible for the following: -
installation of test installations servicing of aircraft up to delivery servicing of aircraft during flight training checks, for personnel authorized by Quality
§ 3.2 – QUALITY CAAC The Quality CAAC is responsible for the following: -
carrying out the VEP or VTP and authorizing transfer of the aircraft to Flight Testing, checking aircraft documentation, carrying out and validating aircraft inspections up to effective delivery, managing authorizations and supervision of certified or delegated operators, carrying out provisional and official weighing operations, carrying out the VSO inspection, updating Flight Manuals, preparing documentation for presentation to the Aviation Authorities, presenting the aircraft to the Aviation Authorities.
§ 3.3 – FLIGHT TESTING The Flight Testing Dept. is responsible for the following: -
defining the program of acceptance tests, defining the test installations necessary for acceptance flights, optimizing the aircraft in flight.
§ 3.4 – DELIVERY CAAC The Delivery CAAC is responsible for the following: -
presenting the aircraft to the Customer and providing assistance up to delivery, providing the interface between the Customer and the various Eurocopter departments.
§ 3.5 – CUSTOMER SUPPORT DEPARTMENT The Customer Support Department is responsible for the following: -
updating the working documents it publishes (IPC, MET, PRE, MRR, etc), providing Quality with a Flight Manual in compliance with the aircraft delivered.
22 "This document is the property of EUROCOPTER. It may not be communicated to third parties and/or reproduced without the prior written consent of EUROCOPTER and its contents may not be disclosed." © EUROCOPTER 11/1995
DPF-10-01-D APPENDIX 1
FORM 113
BOOK
WORK BOOK Aircraft
Type
No.
1-
This work book is opened just before the production roll-out inspection.
2-
It is the only document in which remarks and requests for repairs issued by H/EV authorized personnel and by the inspectors should be noted (except for the repair card specially intended for minor anomalies that are standard practice).
3-
This document is the support for
4-
Once its columns have been filled in and signed, this document is also the only reference for: - certifying the availability or non-availability of an aircraft, - certifying readiness for a determined flight, - flight-by-flight knowledge of equipment aging (the times mentioned are those which substantiate this). - monitoring fuel, lubricant and hydraulic consumption.
5-
This document does not replace certificates in use elsewhere (in particular Appendix 3).
6-
The work book remains in force until effective delivery of the aircraft.
7-
It is an internal industrial document; its publication is prohibited outside the helicopter department or its licensees.
- the work order, after signing by the two leaders authorized to make the decision, - the work execution report, completed by the workshop, and the inspection certificate.
23 "This document is the property of EUROCOPTER. It may not be communicated to third parties and/or reproduced without the prior written consent of EUROCOPTER and its contents may not be disclosed." © EUROCOPTER 11/1995
DPF-10-01-D APPENDIX 1 Maintenance operations REQ Signa UEST ture Type
Crew
Unit hours
CE CP
SPECIFIC MONITORING 1 2
M
CYCL ES
AIR ACTI VITY
Flight of day Totals
R
REMARK – ANOMALY Brief description of fault – Suggestions – Signature
Order No.
Flight Testing
WORK TO BE DONE – DECISION – Signatures
?
Flight Testing
Quality
Quality
Production control Delegated certified operators Design office
Design office
Unit Report
Hours
Standar d flight Flight No. Start time
Aircraft Type
No.
Availabi Page lity No Indispe Date nsable? EXECUTION REPORT Inspection and information for monitoring of components moved signature and date Description and Reference Serial Valida TS No. position No tion Flight tests Quality Delegated certified operators All personnel
Enter here all work postponed during optimization, identified by their order number and subject (in one word). For work dependent on an outside event (procurement, availability of tools), specify the foreseeable date of execution. Always code the application phase with a number from 0 to 5 as follows: 0: Refused exceptionally to be corrected before first PF flight 1: To be corrected before 1st flight 2: To be corrected before a flight (also specify the type of flight before which the work must be done) 3: To be corrected before presentation to Authorities, 4: To be corrected before delivery 5: Deliverable in present condition. Delete the line once the work has been carried out. NB: This list does not constitute "Flight Reservations". These are only indicated by the word "postponed" entered in the column "Work to be done". The acceptance of these reservations is implicitly acquired by the Flight Commander's signature in the box "Accepted for flight". Date
Order No.
SUBJECT
Time
Code
Standard flight
Postponed
24 "This document is the property of EUROCOPTER. It may not be communicated to third parties and/or reproduced without the prior written consent of EUROCOPTER and its contents may not be disclosed." © EUROCOPTER 11/1995
DPF-10-01-D APPENDIX 2 EUROCOPTER Flight Testing
AIRCRAFT: 332 Long Serial No. Type
FUEL Vol. T3: F34/JP8 REQUIRED from 30 Sept to 31 March
ACCEPTANCE FLIGHTS
Version Customer A/C S/N°
DESCRIPTION OF FLIGHTS
Weight
Weight Kg
Centering m
FUEL Weight
Capacity
BALLAST Weight
APPENDIX 2 Page 2/2 Issue Moment m.Kg Crew
Center ing
Remarks
Distance
Adjustment Run-up General Inspection Autopilot Flying Characteristics Perf Radio com/nav Flying Characteristics Perf Radio com/nav With additional ext. tanks Climb flight De-icing (with T3 if installed) Compensation with rotor spinning Navigation Coupler Hoist Sling (ground tests if installed) Radar VIP inspection Sonar FLIR
25 "This document is the property of EUROCOPTER. It may not be communicated to third parties and/or reproduced without the prior written consent of EUROCOPTER and its contents may not be disclosed." © EUROCOPTER 11/1995
DPF-10-01-D APPENDIX 3 EUROCOPTER Production Flight Testing
Appendix 3 Helicopter E/X.S No. 1486 Type Issue Version Page SERIAL No. Customer Data Sheet No Customer A/C S/N° MANAGER Remarks/ Date Name Signature/ Reservations stamp
FLIGHT TESTING PRESENTATION SHEET Contractual definition for optimization
Customer Successive frontier operations PRESENTATION OF HELICOPTER FOR FLIGHT LINE TRANSFER The above-mentioned helicopter is COMPLETE and FINISHED in accordance with: - the conditions required In Chapter 2 of DPF 10-01 - the CUSTOMER DATA SHEET, latest edition of: EXCEPT for anomalies and missing items listed in the transfer file. The sealed aircraft is declared ready and available for the VEP. INSPECTION AND ACCEPTANCE OF AIRCRAFT FOR FLIGHT LINE TRANSFER Acceptance of aircraft:
For VEP For VTP
PRODUCTION LINE E/CQ QUALITY LINE
E/CO VEP QUALITY
Acceptance of aircraft for transfer to flight line Authorization for flight line transfer for aircraft under DPM/SQ control Delivery of pass for aircraft under DGAC control: Delivery of GSAC pass for production aircraft Delivery of DGAC pass for development aircraft E.V. ACCEPTANCE FOR IN-FLIGHT OPTIMIZATION Run-ups preparatory to flights satisfactory according to standards in force and flight line work scheme for conformity at first flight
DPM/SQ E/X.S E/X.S
E/X.S
There are …. items in CT 113 Items refused: REGISTRATION No. REGISTRATION No. Pass No. Approved for PF1
E/CO FLIGHT LINE QUALITY E/X.S / Eng. E/X.S / Radio
CODE 0: Refused (exceptionally, to be corrected before 1st PF) CODE 3: To be corrected before presentation to Authorities
CODE 1: To be corrected before 1st flight CODE 4: To be corrected before delivery (approval of Authorities)
CODE 2: To be corrected before end of flights CODE 5: Deliverable as is (DO or Customer approval)
26 "This document is the property of EUROCOPTER. It may not be communicated to third parties and/or reproduced without the prior written consent of EUROCOPTER and its contents may not be disclosed." © EUROCOPTER 11/1995
DPF-10-01-D
EUROCOPTER Production Flight Testing
Appendix 3 Helicopter E/X.S No. 1486 Type Issue Version Page SERIAL No. Customer Data Sheet No Customer A/C S/N° MANAGER Remarks/ Date Name Signature/ Reservations stamp
ACCEPTANCE PRESENTATION SHEET Certificate of conformity
Customer Successive frontier operations CERTIFICATE OF SATISFACTORY IN-FLIGHT OPTIMIZATION The above-mentioned helicopter is COMPLETE in terms of in-flight optimization in accordance with the standards in force for Customer definition and the special technical clauses identified on the Customer Data Sheet. EXCEPT for anomalies listed in the optimization report quoted opposite. NB: All work subsequent to the last optimization flight liable to affect aircraft flight quality must be submitted to Flight Testing according to procedure of DPF 10/01. Certificate of correct result of PFS (or flight) on completion of routine and specific work Certificate of satisfactory flight result Certificate of final state of aircraft COMPLETE AND IN CONFORMITY with the latest edition of the FC FINISHED according to flight line work scheme EXCEPT for anomalies and missing items identified in CT 113 Certificate of conformity with Customer Data Sheet Documentation up to date and complete FINISHED including work subsequent to last optimization flight, notification of which is given to Flight Testing Check of customized Flight Manual Aircraft sealed. Ready for presentation for acceptance to Aviation Authorities SIAR ACCEPTANCE / MANUFACTURER'S ACCEPTANCE Presentation of file and aircraft Satisfactory flight Acceptance of aircraft and its documentation (Quality Department in the framework of DGAC approval) DELIVERY OF HELICOPTER Shipped by air transport or in case Ferrying (full load)
E/X.S Pilot Radio
E/X.S Engineer Head of E/X.S FLIGHT LINE PRODUCTION
Date of last FC issue
QUALITY E/CQ
Date of last FC issue
In case of adjournment, state reasons DPM/SQ OR E/CQ
L/H PRODUCTION E/X.S OPS
27 "This document is the property of EUROCOPTER. It may not be communicated to third parties and/or reproduced without the prior written consent of EUROCOPTER and its contents may not be disclosed." © EUROCOPTER 11/1995
DPF-10-01-D APPENDIX 4 List of documents WHICH MUST ACCOMPANY THE AIRCRAFT DURING TRANSFER FROM PRODUCTION LINE TO PRODUCTION FLIGHT LINE
Appendix III Work Book CT 113 Equipment log cards (FME) Engine log book(s) Monitoring sheets List of concessions MOD list - Embodied MODs - Remaining MODs to be embodied where applicable Test or acceptance reports Installation certificates Aircraft transfer file Quality file CE 102 (for aircraft under DPM/SQ control) BGE: Bordereau de Groupage Equipement (Equipment Schedule)
28 "This document is the property of EUROCOPTER. It may not be communicated to third parties and/or reproduced without the prior written consent of EUROCOPTER and its contents may not be disclosed." © EUROCOPTER 11/1995
