Canadair Regional Jet CL-600-2B19 Structural Repair Manual Chapter 57 Wings (2006)

Description

Canadair Regional Jet CL-600-2B19 Structural Repair Manual – Chapter 57 Wings

This Canadair Regional Jet CL-600-2B19 Structural Repair Manual is the complete Chapter 57 – Wings section of the Bombardier CRJ Structural Repair Manual (SRM), current to March 2006 revision. It is written for the CL-600-2B19 airframe and gives structural identification, allowable damage limits, and approved repair instructions for every major wing zone, from the wing box out to the wingtip and winglet, and rearward through the trailing edge devices.

File Details

• Manual type: Structural Repair Manual (SRM), Chapter 57 – Wings
• Aircraft: Bombardier/Canadair Regional Jet, model CL-600-2B19
• Language: English
• Page count: 562 pages
• File format: PDF
• Document title: Structural Repair Manual, CSP-A-008 25
• Revision date: March 10, 2006

Chapters Covered

• 57-00-00 Wings – General, Structural Identification, Wing Stations
• 57-00-00 Wings – Allowable Damage
• 57-00-31 Wings Skin and Plating – Allowable Damage
• 57-20-00 Wing Main Structure – General, Structural Identification
• 57-21-00 Wing Box Structure – Structural Identification, Allowable Damage, Repairs
• 57-21-03 Wing-Plank Integral Stringers – Structural Identification, Allowable Damage
• 57-21-07 Wing Box Spars – Structural Identification, Allowable Damage, Repairs
• 57-21-12 Wing Box Ribs – Allowable Damage, Repairs
• 57-21-17 Wing Box Intercostals – Structural Identification, Allowable Damage
• 57-21-27 Wing Box Fittings – Structural Identification, Allowable Damage
• 57-21-31 Wing Box Skin and Plating – Structural Identification, Allowable Damage, Repairs
• 57-21-32 Wing-Box Access Doors – Structural Identification, Allowable Damage, Repairs
• 57-21-55 Flap Hinge Boxes – Structural Identification, Allowable Damage, Repairs
• 57-30-00 Wingtip – General, Allowable Damage
• 57-31-00 Winglet – Structural Identification, Allowable Damage
• 57-31-14 Winglet Framing Structures – Allowable Damage, Repairs
• 57-31-31 Skin and Plating, Wing Extension and Winglet – Structural Identification, Allowable Damage
• 57-31-51 Fillets and Fairings, Winglet – Structural Identification, Allowable Damage, Repairs
• 57-40-00 Leading Edge – General, Structural Identification
• 57-41-00 Leading Edge Structure – Structural Identification, Allowable Damage, Repairs
• 57-41-12 Ribs, Wing Leading Edge – Structural Identification, Allowable Damage
• 57-41-29 Leading Edge Shrouds and Frames – Structural Identification, Allowable Damage
• 57-41-31 Wing Leading Edge Skins – Structural Identification, Allowable Damage, Repairs
• 57-50-00 Trailing Edge and Edge Devices – General, Structural Identification
• 57-51-00 Trailing Edge Structure – Structural Identification, Allowable Damage
• 57-51-14 Framing Structure, Trailing Edge – Structural Identification, Allowable Damage, Repairs
• 57-51-31 Skin and Plating, Trailing Edge – Structural Identification, Allowable Damage, Repairs
• 57-52-00 Inboard Flap and Vane – Structural Identification, Allowable Damage, Repairs
• 57-53-00 Outboard Flap and Vane – Structural Identification, Allowable Damage, Repairs
• 57-54-00 Flap Hinge Arms – Structural Identification, Allowable Damage, Repairs
• 57-55-00 Flap Hinge Fairings – Structural Identification, Allowable Damage, Repairs
• 57-60-00 Aileron – Structural Identification, Allowable Damage, Repairs
• 57-70-00 Spoilers – Structural Identification
• 57-71-00 Inboard Ground Spoiler – Structural Identification, Allowable Damage, Repairs
• 57-72-00 Outboard Ground Spoiler – Structural Identification, Allowable Damage, Repairs
• 57-73-00 Flight Spoiler – Structural Identification, Allowable Damage, Repairs
• 57-74-00 Spoileron – Structural Identification, Allowable Damage, Repairs

Taken together, this Chapter 57 Wings section walks a technician from general wing station reference data through structural identification of every wing component, into allowable damage limits for skins, spars, ribs, fittings and intercostals, and finally into approved repair procedures – including specific repair numbers, repair materials, and continuing airworthiness inspection requirements for flap, aileron, and spoiler skin damage.

Why This Canadair Regional Jet Wings Manual Matters

This Canadair Regional Jet CL-600-2B19 Structural Repair Manual Chapter 57 Wings lets a technician correctly identify wing structure by zone, check reported damage against the applicable allowable damage figures for extruded, machined, and formed sheet metal parts, and apply the correct approved repair – such as flush and non-flush skin repairs on the flaps, ailerons, and wing leading edge – without guesswork. Because wing structure is classified as primary structure, working from the exact CL-600-2B19 SRM Chapter 57 Wings data rather than a generic reference is what keeps a repair airworthy and inspection-ready.

This Structural Repair Manual Chapter 57 Wings download is delivered instantly as a PDF after purchase – no shipping, no waiting. Open it on a laptop, tablet, or phone in the hangar, or print the pages you need at the bench.