DASH 7 CORROSION PREVENTION AND CONTROL MANUAL : PSM 1-7-5
Bok Engelsk 1992
| Utgitt | Ontario : de Havilland Inc. , 1992
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| Opplysninger | Published May 13, 1997. However, the copyright date is 1992, and it refers to the initial version of this binder. Through-out the binder the date refered to is May 13, 1997 exept for the list of effective pages wich are dated November 1/96. Temporary Revision No. 5-98, Revision Date 13 August 1997. - TABLE OF CONTENTS: INTRODUCTION General Arrangement of Manual Applicability of Data Revisions to Manual List of Effective Pages How to Use the Manual in Conjunction with PSM1-GEN-5 Publications Change Requests PART 1 GENERAL INFORMATION General Information Aircraft Stations General Aircraft Coordinate System General Major Assembly Datum Points Fuselage Vertical Stabilizer Horizontal Stabilizer Wings Nacelles Aircraft Zones General Major Zones Major Sub-zones Zones Access Panaels and Doors Access Panaels and Doors - Internal General Access Panaels and Doors - External General PART 2 SPECIFIC CORROSION INSPECTIONS Specific Corrosion Inspection Items Corrosion Inspection Area Identification If Corrosion Is Detected Relationship Of This Document To Maintenance Manual PSM 1-7-2 Selection of Corrosion Inspection Areas Definition of Corrosion Inspection Areas General Note on DHC-7 Corrosion Experience LANDING GEAR Nose Landing Gear - Zone 711 C32-711-01 Nose Landing Gear Primary Structure Including Structural, Retraction and Steering Components and Associated Hardware Main Landing Gear - Zones 721 and 731 C32-721-01 Main Landing Gear Primary Structure Including Structural, Retraction Mechanisum Components and Associated Hardware C32-721-01-01 Major Joints, Rod/Eye Ends, Bushings, Bolts/Pins and Retaining Hardware DOORS (Main Events) Zones 811, 821, 822, 823, 824, 825, 826, 827 and 828 FUSELAGE (Main Events) External - Zones 110, 120 and 210 Internal - Zones 111 and 112 Internal - Zones 121, 122 and 123 Internal - Zone 211 External - Zones 130 and 220 Internal - Zones 131, 132, 133, 134 and 135 Internal - Zones 221 and 222 External - Zones 140, 230, 240, 250, 260 and 270 Internal - Zones 141, 142, 143, 144, 145 and 146 Internal - Zones 231, 232, 233, 234, 241, 251, 261 and 271 External Surfaces and Internal Structure Zones - 310, 311 and 312 Internal Structure - Zones 281, 282, 283, 284 and 285 NACELLE (Main Events) Zones 420 and 430 Zones 410 and 440 EMPENNAGE - VERTICAL (Main Events) External Surface and Internal Structure (Fin Box) - Zones 320, 321 and 322 EMPENNAGE - HORIZONTAL (Main Events) Tailplane Box and Elevators - External Surface and Internal Structure (T/P Box) - Zones 330, 332, 333, 334, 335, 340, 342, 343, 344 and 345 WINGS (Main Events) Wing Box - Aircraft Center Line to Tip (Sta Yw0 to Yw542) External - Zones 520 to 620 Wing Box - Aircraft Center Line to Inner Nacelle Outer Rib (Sta Yw0 to Yw153) Internal Structure - Zones 521 and 621 Wing Box - Inner Nacelle Outer Rib to Fuel (Sta Yw153 to Yw364) Internal Structure - Zones 522, 523, 622 and 623 Wing Box - Fuel Bay Outer Rib to Tip (Sta Yw364 to Yw542) Internal Structure - Zones 524 and 624 Leading Edges - (Sta Yw47 to Yw542) Zones - 510, 511, 512, 513, 514, 610, 611, 612, 613 and 614 Fixed Trailing Edge, Flap Tracks/Screws (Sta Yw47 to Yw542) Zones 525, 526, 531, 532, 625, 626, 631 and 632 PART 3 ACCEPTANCE PAGE LOG OF REVISION RECOMMENDED CORROSION INSPECTION PROGRAM Recommended Corrosion Inspection Program Threshold Age and Intervals Integration of Corrosion Inspections into existing Maintenance Programs Contents of the Recommended Corrosion Inspection Program If Corrosion is Detected Reporting System Corrosion Detection Report DESCRIPTION OF AIRCRAFT AREA 32 Landing Gear 52 Doors 53 Fuselage, Forward 53 Fuselage, Center 53 Fuselage, Rear 53 Fuselage, Aft 53 Fuselage, Wing to Fuselage Fairings 54 Nacelle 55 Empennage, Vertical Stabilizer 55 Empennage, Horizontal Stabilizer 57 Wings, Wing Box 57 Wings, Leading Edges 57 Wings
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