DOCUMENTO TECNICO TECHNICAL DOCUMENT
Transcript of 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.
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
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".
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
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.
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
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.
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
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
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
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
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
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
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
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
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
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
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
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
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
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
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
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
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).