DOCUMENTO TECNICO TECHNICAL DOCUMENT

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DOCUMENTO TECNICO TECHNICAL DOCUMENT Documento nº/Document no. Avión/Aircraft DT-06-3009 CN-235-300 MP Título/title CN-235-300 MP AIRWORTHINESS LIMITATIONS Firma/Signature Realizado/Prepared Nombre/Name J. ANGOLOTI DEL MONTE Cargo/Position CONTINUOUS AIRWORTHINESS Firma/Signature Comprobado/Checked Nombre/Name J. VERDÚ JEREZ Cargo/Position CERTIFICATION CASA PLATFORMS DEPARTMENT HEAD Firma/Signature Aprobado/Approved Nombre/Name J.M. RUIZ BARRAGÁN Cargo/Position TYPE CERTIFICATION HEAD Fecha 1ª edición 1st. issue date Jan. 07 Class. acceso Access class. PROPIEDAD DE EADS-CASA, Sociedad Unipersonal. Este Documento no puede ser utilizado ni reproducido total o parcialmente sin la previa autorización escrita de la Dirección de Proyectos y Sistemas de EADS-CASA. EADS-CASA, Sociedad Unipersonal PROPERTY. This Document shall neither be used nor completely or partially reproduced without previous written authorizacion by EADS-CASA Engineering and Systems Directorate.

Transcript of DOCUMENTO TECNICO TECHNICAL DOCUMENT

Page 1: DOCUMENTO TECNICO TECHNICAL DOCUMENT

DOCUMENTO TECNICO TECHNICAL DOCUMENT

Documento nº/Document no. Avión/Aircraft

DT-06-3009 CN-235-300 MP

Título/title

CN-235-300 MP AIRWORTHINESS LIMITATIONS

Firma/Signature

Realizado/Prepared Nombre/Name J. ANGOLOTI DEL MONTE

Cargo/Position CONTINUOUS AIRWORTHINESS

Firma/Signature

Comprobado/Checked Nombre/Name J. VERDÚ JEREZ

Cargo/Position CERTIFICATION CASA PLATFORMS DEPARTMENT HEAD

Firma/Signature

Aprobado/Approved Nombre/Name J.M. RUIZ BARRAGÁN

Cargo/Position TYPE CERTIFICATION HEAD

Fecha 1ª edición 1st. issue date

Jan. 07

Class. acceso Access class.

PROPIEDAD DE EADS-CASA, Sociedad Unipersonal. Este Documento no puede ser utilizado ni reproducido total o parcialmente sin la previa autorización escrita de la Dirección de Proyectos y Sistemas de EADS-CASA. EADS-CASA, Sociedad Unipersonal PROPERTY. This Document shall neither be used nor completely or partially reproduced without previous written authorizacion by EADS-CASA Engineering and Systems Directorate.

bbb580
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DT-06-3009 Edic./Issue A Pag. I

Revisión Motivo de Modificación/Change reason Realiz./Prep. Aprobado/App.

Fecha/Date Capítulos, Secciones, Hojas afectadas/Chapters,Sections,Sheets affected Firma/Sign. Firma/Sign.

A First Issue.

January 2007 All pages. J. Angoloti

J.M. Ruiz Barragán

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DT-06-3009 Edic./Issue A Pag. II

EDICION ACTUAL DE PAGINAS/CURRENT PAGES ISSUE

Nº Pág. Edic. Nº Pág. Edic. Nº Pág. Edic. Nº Pág. Edic. Nº Pág. Edic. Nº Pág. Edic.

Cover A

I A

II A

1 A

1.1 A

1.2 A

1.3 A

1.4 A

1.5 A

1.6 A

1.7 A

1.8 A

1.9 A

1.10 A

1.11 A

1.12 A

1.13 A

1.14 A

1.15 A

1.16 A

1.17 A

1.18 A

1.19 A

1.20 A

Palabras clave/Key words

AIRWORTHINESS LIMITATIONS, MRBD, LIMITATIONS, TASK

Resumen/Summary

SEE PARAGRAPHS "INTRODUCTION" AND "SCOPE".

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DT-06-3009 Edic./Issue A PAG. 1

INDEX 0. DOCUMENT APPROVALS 1. AIRWORTHINESS LIMITATIONS 1.1 INTRODUCTION 1.2 SCOPE 1.3 RULES APPLICABLE TO AIRWORTHINESS LIMITATIONS 1.4 AIRWORTHINESS LIMITATIONS LISTING

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DT-06-3009 Edic./Issue A PAG. 1.1

1.- AIRWORTHINESS LIMITATIONS 1.1 INTRODUCTION During the CN-235-300 MP (Maritime Patrol) certification program certain maintenance tasks have been

identified that must be performed on all aircraft at, or before, the required interval, in order to meet certification requirements. These task intervals must not be escalated without the approval of the EADS-CASA Engineering Division (División de Proyectos) and the Airworthiness Authorities.

1.2 SCOPE Three types of tasks are included in the Airworthiness Limitations: a) SYSTEMS related tasks where a limiting interval has been calculated in a safety assessment to

achieve compliance with certification regulations. For ease of identification, systems tasks are identified in the MRB CN-235 PV01 Document. In the event of conflicting information, the present (Airworthiness Limitations) Document will be the final authority.

b) STRUCTURES related tasks where inspections must be performed at, or before, the prescribed

thresholds/intervals in order to detect fatigue cracks before the critical crack length is reached. c) Discard tasks for safe life STRUCTURAL items. 1.3 RULES APPLICABLE TO THE AIRWORTHINESS LIMITATIONS LIST a) No task may be deleted, and no task interval may be escalated without the approval of the EADS-

CASA Engineering Division and Airworthiness Authorities. b) Systems Maintenance tasks and Fatigue Damage tasks identified in the Airworthiness Limitations

may only have the task deleted or the threshold/interval escalated with the approval of the EADS-CASA Engineering Division and Airworthiness Authorities.

c) Items that are life limited will be discarded according to the life limits published in the Airworthiness

Limitations. These limits may be revised per the manufacturers recommended guidelines with the approval of the regulatory authority.

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DT-06-3009 Edic./Issue A PAG. 1.2

1.4 AIRWORTHINESS LIMITATIONS LISTING 1.4.1 Aircraft systems limitations The following are systems operational tasks which must be performed in order to show compliance with the

regulation.

MRB CN-235-PV01 TASK REFERENCE

TASK TIME INTERVAL

Electrical Power

24.008 Operational check of Transformer Rectifier. 400 FH

Flight Controls

27.012 Operational check to verify AILERON forward and rear Electromechanical Detent Rod disconnecting.

300 FH

27.014 Operational check of Pilot, Copilot and Emergency AILERON Trim System.

300 FH

27.027/27.028 Operational check of Normal and Emergency RUDDER Trim System.

300 FH

27.041 Operational check to verify ELEVATOR forward and rear Electromechanical Detent Rod disconnecting.

300 FH

27.043/27.045 Operational check of Pilot, Copilot and Emergency ELEVATOR Trim System.

300 FH

27.048 Functional check of FLAPS BRAKES individually. 2400 FH

Rear Ramp Cargo Door

52.021 Operational check of Microswitches checking circuit. 300 FH

Engine Controls

76.004 Operational check of Beta Lockout System Flight Idle Override Switch.

300 FH

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DT-06-3009 Edic./Issue A PAG. 1.3

1.4.2 Structural Inspection Limitations

A Damage Tolerance Analysis (Fatigue, crack growth, and residual strength analyses) has been made in order to obtain for each SSE a particular threshold and interval for inspection that will assure the economic and safe operation of the aircraft.

Structures maintenance tasks and their associated inspection thresholds and intervals arising from damage tolerance evaluation (FAR 25.571) will be identified following review of the results of the relevant full scale fatigue testing. Values (thresholds and intervals) to be corfirmed when final analysis of test results is completed.

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DT-06-3009 Edic./Issue A PAG. 1.4

SSE Nº DESCRIPTION THRESHOLD INTERVAL EFFECTIVITY

FF01 Forward Fuselage - Skins

FF0101 Longitudinal skin splices 7500FC/23273FH TBD SM01

FF0102 Circumferential skin splices 7500FC/23273FH TBD SM01

FF0103 Typical basic longitudinal and transversal crack in skin 7500FC/23273FH TBD SM01

FF02 Forward Fuselage - Internal Structure Over the Floor

FF0201 Frames 7500FC/23273FH TBD SM01 FF0202 Skin riveted to stringers 7500FC/23273FH TBD SM01 FF0203 Pressure floor structure 7500FC/23273FH TBD SM01 FF03 Forward Fuselage - Internal Structure Under the Floor

FF0301 Riveted joint around avionics and access cover in skin 7500FC/23273FH TBD SM01

FF04 Forward Fuselage - Pressure Bulkhead at FR1

FF0401 Frame 1 7500FC/23273FH TBD SM01

FF0402 Riveted joint FR1 to fuselage skin 7500FC/23273FH TBD SM01

FF05 Forward Fuselage - Windshield Frame

FF0501 Windshield frame upper sill 7500FC/23273FH TBD SM01

FF0502 Windshield frame lower sill 7500FC/23273FH TBD SM01

FF0503 Windshield frame vertical members 7500FC/23273FH TBD SM01

FF06 Forward Fuselage - Door Access Areas

FF0601 FWD Crew door cutout 7500FC/23273FH TBD SM01

FF0602 FWD Crew door attachment in fuselage 7500FC/23273FH TBD SM01

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DT-06-3009 Edic./Issue A PAG. 1.5

SSE Nº DESCRIPTION THRESHOLD INTERVAL EFFECTIVITY

FF07 Forward Fuselage - NLG Bay and Backup Structure

FF0701 Splice NLG trunnion to diagonal bar 7500FC/23273FH TBD SM01

FF0702 Splice NLG fuse attachments 7500FC/23273FH TBD SM01

FF08 Forward Fuselage - Pressure Bulkhead FR10

FF0801 FR10 web under floor structure 7500FC/23273FH TBD SM01

FF0802 Riveted joint FR10 to fuselage skin 7500FC/23273FH TBD SM01

FF09 Forward Fuselage - Forward Fuselage cutouts

FF0902 WC drainage box 7500FC/23273FH TBD SM01

FC01 Center Fuselage - Skins

FC0101 Longitudinal skin splices 7500FC/23273FH TBD SM01

FC0102 Circumferential skin splices 7500FC/23273FH TBD SM01

FC0103 Typical basic longitudinal and transversal crack in skin 7500FC/23273FH TBD SM01

FC02 Center Fuselage - Internal Structure Over the Floor

FC0201 Frames 7500FC/23273FH TBD SM01

FC0202 Skin riveted to stringers 7500FC/23273FH TBD SM01

FC0203 Machined frames (FR21 and FR24) attachment to wing fittings 7500FC/23273FH TBD SM01

FC0204 Splice between upper and lower former 7500FC/23273FH TBD SM01

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DT-06-3009 Edic./Issue A PAG. 1.6

SSE Nº DESCRIPTION THRESHOLD INTERVAL EFFECTIVITY

FC03 Center Fuselage - Internal Structure Under the Floor

FC0301 Skin riveted to stringers 7500FC/23273FH TBD SM01

FC0302 Longitudinal beams formers 7500FC/23273FH TBD SM01

FC0303 Stringer P19 and P22 7500FC/23273FH TBD SM01

FC0304 Machined frames FR21, FR23 and FR24 7500FC/23273FH TBD SM01

FC04 Center Fuselage - Wing Fuselage Attachment Area

FC0401 Wing-fuselage attachment at FR21 7500FC/23273FH TBD SM01

FC0402 Wing-fuselage attachment at FR24 7500FC/23273FH TBD SM01

FC0403 Wing fuselage Center attach fitting at FR24 7500FC/23273FH TBD SM01

FC0404 Wing fuselage lateral attachment at FR24 7500FC/23273FH TBD SM01

FC05 Center Fuselage - Windows Area

FC0501 Window cutouts 7500FC/23273FH TBD SM01

FC0502 Observation window cutout 7500FC/23273FH TBD SM01

FC06 Center Fuselage - Doors Access Areas

FC0601 FWD Emergency exit door cutout 7500FC/23273FH TBD SM01

FC0602 FWD Emergency exit door attachment to fuselage 7500FC/23273FH TBD SM01

FC0603 AFT Emergency exit door cutouts 7500FC/23273FH TBD SM01

FC0604 AFT Emergency exit door attachment to fuselage 7500FC/23273FH TBD SM01

FC0605 AFT door cutout 7500FC/23273FH TBD SM01

FC0606 AFT door attachments to fuselage 7500FC/23273FH TBD SM01

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DT-06-3009 Edic./Issue A PAG. 1.7

SSE Nº DESCRIPTION THRESHOLD INTERVAL EFFECTIVITY

FC07 Center Fuselage - Main Landing Gear Backup Structure

FC0701 MLG structure in outer bulkhead 7500FC/23273FH TBD SM01

FC0702 MLG lower skin 7500FC/23273FH TBD SM01

FC08 Center Fuselage - Fuselage Cutouts

FC0801 Radar antenna skin hole 7500FC/23273FH TBD SM01

FC0802 Flare dispenser skin hole 7500FC/23273FH TBD SM01

FC0803 DF, LFS and Scanner cutout 7500FC/23273FH TBD SM01

FC0804 DF, LFS and Scanner reinforced structure 7500FC/23273FH TBD SM01

FC0805 Microwave Radiometer cutout 7500FC/23273FH TBD SM01

FC0806 Slar supports 7500FC/23273FH TBD SM01

FR01 Rear Fuselage - Skins

FR0101 Circumferential skin splice at frames 7500FC/23273FH TBD SM01

FR0102 Longitudinal skin riveted joints at stringers 7500FC/23273FH TBD SM01

FR0103 Typical basic longitudinal and transversal crack in skin 7500FC/23273FH TBD SM01

FR02 Rear Fuselage - Internal Structure

FR0201 Frame structure 7500FC/23273FH TBD SM01

FR0202 Longitudinal beam structure 7500FC/23273FH TBD SM01

FR0203 Bracket area structure 7500FC/23273FH TBD SM01

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DT-06-3009 Edic./Issue A PAG. 1.8

SSE Nº DESCRIPTION THRESHOLD INTERVAL EFFECTIVITY

FR03 Rear Fuselage - Pressure Bulkhead at FR46

FR0301 Frame 46 web and stiffeners 7500FC/23273FH TBD SM01

FR0302 Frame 46 in attachment to VSTAB 7500FC/23273FH TBD SM01

FR04 Rear Fuselage - Ramp Door Attachments

FR0401 Ramp door hinge attach fittings at FR30 7500FC/23273FH TBD SM01

FR0402 Ramp door attach fittings at FR31-FR38 7500FC/23273FH TBD SM01

FR05 Rear Fuselage - Ventral Door Attachments

FR0501 Ventral door hinge attach fittings FR46 7500FC/23273FH TBD SM01

FR0502 Ventral door attach fittings FR39-FR45 7500FC/23273FH TBD SM01

FR06 Rear Fuselage - Horizontal Tailplane Attachments

FR0601 Horizontal tailplane attachment FR48 to HTP 7500FC/23273FH TBD SM01

FR0602 Horizontal tailplane attachment FR50 to HTP 7500FC/23273FH TBD SM01

FR07 Rear Fuselage - Vertical Tailplane Attachments

FR0701 Vertical tailplane attachment FR46 to VTP 7500FC/23273FH TBD SM01

FR0702 Vertical tailplane attachment FR50 to VTP 7500FC/23273FH TBD SM01

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DT-06-3009 Edic./Issue A PAG. 1.9

SSE Nº DESCRIPTION THRESHOLD INTERVAL EFFECTIVITY

WC02 Center Wing - Lower Skin

WC0201 Center wing lower surface access holes 7500FC/23273FH TBD SM01

WC0202 Center wing engine fairing attachment holes 7500FC/23273FH TBD SM01

WC0203 Center wing fuel gauge hole 7500FC/23273FH TBD SM01

WC0204 Lower skin attachment to FS 7500FC/23273FH TBD SM01

WC0205 Lower skin attachment to RS 7500FC/23273FH TBD SM01

WC0206 Center wing lower surface stringer runout 7500FC/23273FH TBD SM01

WC03 Center Wing - Front Spar

WC0301 FS lower cap 7500FC/23273FH TBD SM01

WC0302 FS web hole 7500FC/23273FH TBD SM01

WC0303 FS lower cap under fitting at WS1100 7500FC/23273FH TBD SM01

WC0304 FS in area under engine mount fittings 7500FC/23273FH TBD SM01

WC04 Center Wing - Rear Spar

WC0401 RS lower cap 7500FC/23273FH TBD SM01

WC0402 RS web holes 7500FC/23273FH TBD SM01

WC0403 RS lower cap under flap attachments 7500FC/23273FH TBD SM01

WC0404 RS lower cap under fitting at WS1100 7500FC/23273FH TBD SM01

WC05 Center Wing - Internal Structure

WC0501 Fuel passing holes 7500FC/23273FH TBD SM01

WC0502 Lower surface skin attachment to ribs 7500FC/23273FH TBD SM01

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DT-06-3009 Edic./Issue A PAG. 1.10

SSE Nº DESCRIPTION THRESHOLD INTERVAL EFFECTIVITY

WC06 Center Wing - Longitudinal Spanwise Splices

WC0601 Center panels spanwise AFT splice at WS1100 7500FC/23273FH TBD SM01

WC0602 Center panels spanwise FWD splice 7500FC/23273FH TBD SM01

WC07 Center Wing - Center / Outer Wing Joint

WC0701 Lower surface joint to center - outer wing WS4250 7500FC/23273FH TBD SM01

WC0702 RS joint center – outer wing WS4250 7500FC/23273FH TBD SM01

WC0703 FS joint center – outer wing WS4250 7500FC/23273FH TBD SM01

WC0704 Center to outer wing joint bolts WS4250 7500FC/23273FH TBD SM01

WC08 Center Wing - Wing Fuselage Attachment Fittings

WC0801 Wing to fuselage AFT fitting WS1100 7500FC/23273FH TBD SM01

WC0802 Wing to fuselage FWD fitting WS1100 7500FC/23273FH TBD SM01

WC0803 Wing to fuselage attachment bars fitting WS1100 7500FC/23273FH TBD SM01

WC09 Center Wing - Inner Flap Attachments

WC0901 Inner flap attachment 7500FC/23273FH TBD CGO1

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DT-06-3009 Edic./Issue A PAG. 1.11

SSE Nº DESCRIPTION THRESHOLD INTERVAL EFFECTIVITY

WO02 Outer Wing - Lower Skin

WO0201 Outer wing lower surface access holes 7500FC/23273FH TBD SM01

WO0202 Outer wing flap attachment area 7500FC/23273FH TBD SM01

WO0203 Outer wing fuel gauge hole 7500FC/23273FH TBD SM01

WO0204 Outer wing lower skin splice to FS 7500FC/23273FH TBD SM01

WO0205 Outer wing lower skin splice to RS 7500FC/23273FH TBD SM01

WO0206 Outer wing lower surface stringers runout 7500FC/23273FH TBD SM01

WO03 Outer Wing - Front Spar

WO0301 FS lower cap 7500FC/23273FH TBD SM01

WO0302 FS web 7500FC/23273FH TBD SM01

WO04 Outer Wing - Rear Spar

WO0401 RS lower cap 7500FC/23273FH TBD SM01

WO0402 RS web 7500FC/23273FH TBD SM01

WO0403 RS attachment to outer flap 7500FC/23273FH TBD SM01

WO0404 RS attachment to aileron 7500FC/23273FH TBD SM01

WO05 Outer Wing - Internal Structure

WO0501 Fuel passing holes in stringers 7500FC/23273FH TBD SM01

WO06 Outer Wing - Longitudinal Spanwise Splice

WO0601 Low surface panels spanwise splice 7500FC/23273FH TBD SM01

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DT-06-3009 Edic./Issue A PAG. 1.12

SSE Nº DESCRIPTION THRESHOLD INTERVAL EFFECTIVITY

WO07 Outer Wing - Center / Outer Wing Joint

WO0701 Lower surface splice to center wing at WS4250 7500FC/23273FH TBD SM01

WO0702 FS cap splice to center wing at WS4250 7500FC/23273FH TBD SM01

WO0703 RS cap splice to center wing at WS4250 7500FC/23273FH TBD SM01

WO0704 Splice bolts 7500FC/23273FH TBD SM01

WO08 Outer Wing - Internal / External Outer Wing Joint

WO0801 Lower surface splice to external wing at WS8110 7500FC/23273FH TBD SM01

WO0802 FS cap splice to external wing at WS8110 7500FC/23273FH TBD SM01

WO0803 RS cap splice to external wing at WS8110 7500FC/23273FH TBD SM01

WO09 Outer Wing - Outer Flap Attachment

WO0901 Outer flap attachments 7500FC/23273FH TBD SM01

EM01 Engine Mounts - Front Engine Mount

EM0101 Welded structure 7500FC/23273FH TBD SM01

EM0102 Firewall structure 7500FC/23273FH TBD SM01

EM02 Engine Mounts - Rear Engine Mount

EM0201 Welded structure 7500FC/23273FH TBD SM01

EM0202 Attachment to forward spar 7500FC/23273FH TBD SM01

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DT-06-3009 Edic./Issue A PAG. 1.13

SSE Nº DESCRIPTION THRESHOLD INTERVAL EFFECTIVITY

FI02 Inner Flap - Spar

FI0201 Spar web 7500FC/23273FH TBD SM01

FI0202 Spar attachment to upper and lower skin 7500FC/23273FH TBD SM01

FI03 Inner Flap - Internal Structure

FI0301 Internal structure 7500FC/23273FH TBD SM01

FI04 Inner Flap - Flap Track Attachment Fittings

FI0401 Flap track attachment fitting 7500FC/23273FH TBD SM01

FI0402 Actuator flap attachment fitting 7500FC/23273FH TBD SM01

FI0403 Flap track structure 7500FC/23273FH TBD SM01

FO02 Outer Flap - Spar

FO0201 Spar web 7500FC/23273FH TBD SM01

FO0202 Spar attachment to upper and lower skin 7500FC/23273FH TBD SM01

FO03 Flap Outer - Internal Structure

FO0301 Internal structure 7500FC/23273FH TBD SM01

FO04 Outer Flap – Flap Track Attachment Fittings

FO0401 Flap track attachment fittings 7500FC/23273FH TBD SM01

FO0402 Actuator flap attachment fitting 7500FC/23273FH TBD SM01

FO0403 Flap track structure 7500FC/23273FH TBD SM01

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DT-06-3009 Edic./Issue A PAG. 1.14

SSE Nº DESCRIPTION THRESHOLD INTERVAL EFFECTIVITY

AI02 Aileron - Spar

AI0201 Spar web 7500FC/23273FH TBD SM01

AI0202 Spar splice to upper and lower skin 7500FC/23273FH TBD SM01

AI03 Aileron - Internal Structure

AI0301 Internal structure 7500FC/23273FH TBD SM01

AI04 Aileron - Hinge and Actuator Fittings

AI0401 Hinge fittings 7500FC/23273FH TBD SM01

AI0402 Actuator fitting 7500FC/23273FH TBD SM01

HT01 Horizontal Stabilizer - Upper Skin

HT0101 Upper skin at chordwise splice 7500FC/23273FH TBD SM01

HT0102 Upper skin splice to FS 7500FC/23273FH TBD SM01

HT0103 Upper skin splice to RS 7500FC/23273FH TBD SM01

HT0104 Upper skin in area of attach fitting to fuselage 7500FC/23273FH TBD SM01

HT03 Horizontal Stabilizer - Front Spar

HT0301 FS attach fitting to fuselage 7500FC/23273FH TBD SM01

HT0302 Front spar web 7500FC/23273FH TBD SM01

HT0303 Front spar upper cap 7500FC/23273FH TBD SM01

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DT-06-3009 Edic./Issue A PAG. 1.15

SSE Nº DESCRIPTION THRESHOLD INTERVAL EFFECTIVITY

HT04 Horizontal Stabilizer - Rear Spar

HT0401 RS attach fitting to fuselage 7500FC/23273FH TBD SM01

HT0402 Rear spar web 7500FC/23273FH TBD SM01

HT0403 Rear spar upper cap 7500FC/23273FH TBD SM01

HT0404 Attachment to elevator 7500FC/23273FH TBD SM01

HT05 Horizontal Stabilizer - Internal Structure

HT0501 Internal structure 7500FC/23273FH TBD SM01

VT01 Vertical Stabilizer - Skin

VT0101 Skin 7500FC/23273FH TBD SM01

VT0102 Skin splice to FS 7500FC/23273FH TBD SM01

VT0103 Skin splice to RS 7500FC/23273FH TBD SM01

VT0104 Skin in area of attach fitting to fuselage 7500FC/23273FH TBD SM01

VT02 Vertical Stabilizer - Front Spar

VT0201 FS attach fitting to fuselage 7500FC/23273FH TBD SM01

VT0202 Front spar web 7500FC/23273FH TBD SM01

VT0203 Front spar cap 7500FC/23273FH TBD SM01

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DT-06-3009 Edic./Issue A PAG. 1.16

SSE Nº DESCRIPTION THRESHOLD INTERVAL EFFECTIVITY

VT03 Vertical Stabilizer - Rear Spar

VT0301 RS attach fitting to fuselage 7500FC/23273FH TBD SM01

VT0302 Rear spar web 7500FC/23273FH TBD SM01

VT0303 Rear spar cap 7500FC/23273FH TBD SM01

VT0304 Rear spar at attachment to rudder 7500FC/23273FH TBD SM01

VT04 Vertical Stabilizer - Internal Structure

VT0401 Internal structure 7500FC/23273FH TBD SM01

EL01 Elevator - Skins

EL0101 Upper skin 7500FC/23273FH TBD SM01

EL0102 Lower skin 7500FC/23273FH TBD SM01

EL02 Elevator - Spar

EL0201 Spar web 7500FC/23273FH TBD SM01

EL0202 Spar splice to upper and lower skin 7500FC/23273FH TBD SM01

EL03 Elevator - Internal Structure

EL0301 Internal structure 7500FC/23273FH TBD SM01

EL04 Elevator - Hinge and Actuator Fittings

EL0401 Hinge fittings 7500FC/23273FH TBD SM01

EL0402 Actuator fitting 7500FC/23273FH TBD SM01

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DT-06-3009 Edic./Issue A PAG. 1.17

SSE Nº DESCRIPTION THRESHOLD INTERVAL EFFECTIVITY

RU02 Rudder - Spar

RU0201 Spar web 7500FC/23273FH TBD SM01

RU0202 Spar attachment to skin 7500FC/23273FH TBD SM01

RU03 Rudder - Internal Structure

RU0301 Internal structure 7500FC/23273FH TBD SM01

RU04 Rudder - Hinge and Actuator Fittings

RU0401 Hinge fittings 7500FC/23273FH TBD SM01

RU0402 Actuator fitting 7500FC/23273FH TBD SM01

SV01 Servotab - Fittings

SV0101 Rudder servotab fittings 7500FC/23273FH TBD SM01

SV0102 Elevator servotab fittings 7500FC/23273FH TBD SM01

SV0103 Aileron servotab fittings 7500FC/23273FH TBD SM01

DF01 Crew Door – FWD Crew Door

DF0101 FWD crew door structure 7500FC/23273FH TBD SM01

DF0102 Crew door attachment fittings to fuselage 7500FC/23273FH TBD SM01

DP01 Rear Door - Rear Door Structure

DP0101 Rear door structure 7500FC/23273FH TBD SM01

DE01 Emergency Door - Emergency Door Structure

DE0101 Emergency door structure 7500FC/23273FH TBD SM01

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DT-06-3009 Edic./Issue A PAG. 1.18

SSE Nº DESCRIPTION THRESHOLD INTERVAL EFFECTIVITY

DR01 Ramp Door - Ramp Door Structure

DR0101 Ramp door skin and reinforcements 7500FC/23273FH TBD SM01

DR0102 Ramp door hinge attach fittings at FR30 7500FC/23273FH TBD SM01

DR0103 Ramp door attach fitting 7500FC/23273FH TBD SM01

DR0104 Ramp door - locking mechanism 7500FC/23273FH SM01

DR0105 Internal structure of the ramp 7500FC/23273FH TBD SM01

DV01 Ventral Door - Ventral Door Structure

DV0101 Ventral door skin and reinforcements 7500FC/23273FH TBD SM01

DV0102 Ventral door hinge attach fittings at FR46 7500FC/23273FH TBD SM01

DV0103 Ventral door fittings to fuselage 7500FC/23273FH TBD SM01

DV0104 Ventral door internal structure 7500FC/23273FH TBD SM01

DA01 Access Doors Structure

DA0101 Nose fuselage. Gear door hinge 7500FC/23273FH TBD SM01

DA0102 Center fuselage. MLG access door hinges and latches 7500FC/23273FH TBD SM01

DA0103 Engine cowling door supports 7500FC/23273FH TBD SM01

TBD

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DT-06-3009 Edic./Issue A PAG. 1.19

1.4.3 Discard Tasks for Safe Life Structural Items In the following table, Structural Items wich are life limited as well as their associated Discard Time are provided:

DISCARD TASK FOR SAFE LIFE STRUCTURAL ITEMS

ITEM PART NUMBER DISCARD TIME (FC)

Nose Landing Gear CA 94300-XX 15.440

Main Landing Gear 35-41050-XXXX 15.440

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DT-06-3009 Edic./Issue A PAG. 1.20

1.4.4 Other Aircraft Limitations for CN-235-300 MP.

Part Number

Description

Discard Time

CN-235-10-10 (AC-875047)

Observer Window

7.250 Flight Cycles (Landings).