Airbus A318 A319 A320 A321 Chapter 05 Time Limits & Maintenance Checks Manual PDF – Rev 40 2012

Description

Airbus A318 A319 A320 A321 Chapter 05 Time Limits & Maintenance Checks Manual PDF – Rev 40 2012

This 745-page Airbus A318/A319/A320/A321 Aircraft Maintenance Manual volume contains Chapter 05, Time Limits – Maintenance Checks. It brings together the scheduled zonal inspection instructions and the extensive unscheduled inspection procedures required after abnormal aircraft operation or reported events. The Airbus A318 A319 A320 A321 Chapter 05 Time Limits & Maintenance Checks Manual PDF – Rev 40 2012 is therefore a focused technical reference for maintenance personnel working with the inspection, evaluation and return-to-service requirements contained in ATA Chapter 05.

The scheduled portion of the chapter is organized around aircraft zones and gives accomplishment instructions for zonal inspection tasks. The unscheduled portion addresses conditions that can require immediate inspection or measurement after events such as hard landings, speed exceedances, bird or hail strikes, lightning strikes, tire or brake failures, runway excursions, engine events, high winds and other abnormal operating conditions. Procedures are supported throughout the manual by inspection tables, task references, aircraft-area drawings, component illustrations, definition diagrams and measurement figures.

File Details

• Manual type: Aircraft Maintenance Manual – Chapter 05, Time Limits – Maintenance Checks
• Brand / aircraft: Airbus A318, A319, A320 and A321
• Revision: 40
• Date: May 01/12
• Language: English
• Page count: 745 pages
• File format: PDF

Scheduled Zonal Maintenance Inspection Coverage

The scheduled-maintenance section provides accomplishment instructions for zonal inspections across the aircraft. Rather than treating inspection as one undifferentiated walk-around, the chapter divides the aircraft into clearly identified areas and gives the applicable inspection/check tasks for those zones. Many procedures specifically include Electrical Wiring Interconnection System (EWIS) general visual inspections as well as access information for panels, doors and compartment structures.

Coverage extends from the radome and avionics areas through the passenger and cargo compartments, center wing, landing-gear bays, powerplant installations, wing structure and tail. Inspection subjects include visible structure, wiring installations, access areas, fairings, doors, nacelles, pylons, control-surface areas and other equipment contained within the defined aircraft zones.

Unscheduled and Abnormal-Event Inspections

A major part of this Airbus A318/A319/A320/A321 Chapter 05 manual is devoted to inspections required after abnormal events. These procedures go well beyond a simple list of affected components. Depending on the event, the manual gives job setup information, inspection phases, specific aircraft areas to examine, damage criteria, task cross-references, follow-on actions and close-up requirements.

The hard and hard-overweight landing material, for example, includes landing classification information and inspection procedures for aircraft structure, landing gear, wings, engine and pylon interfaces and other critical areas. The manual distinguishes inspection requirements according to the reported event and available aircraft data, and contains supporting illustrations for critical structure and landing-gear components.

Other event-driven procedures address landing-gear limiting-speed exceedance, flap/slat overspeed, bird and hail strike, tire burst or tread throw, wheel failure, brake emergency application or overheat, excessive turbulence, VMO/MMO exceedance, lightning strike, engine bird strike or slush ingestion, tail runway impact, nose-landing-gear towing overload, steering-angle exceedance, runway or taxiway excursion, dust and volcanic-ash exposure, engine failure, impacts to engine cowls, fluid spillage, abnormal passenger/crew door movement, main-landing-gear vibration at touchdown, engine windmilling, wing-tip or fence impact, overweight taxiing, very high winds and high lateral loads.

Inspection Drawings and Technical References

The Chapter 05 procedures are accompanied by pictorial material that helps identify the areas and assemblies involved in inspection. Examples include aircraft-structure critical-area diagrams, engine-to-pylon and pylon-to-wing attachment illustrations, inlet cowl and fan-cowl details, thrust-reverser fittings, main and nose landing-gear illustrations, fuselage and center-section views, antenna and probe locations, engine nacelle drawings, wing-tip illustrations and measurement-point diagrams.

IMAGES PREVIEW

These figures are particularly useful where an abnormal event requires inspection of a defined structural region rather than a general external check. The manual also references related AMM tasks when additional opening, removal, system operation, testing, defueling, access or corrective work is required.

Aircraft Measurement, Leakage and Stability Procedures

Chapter 05 also includes procedures used when abnormal operation or repair makes structural verification necessary. Fuselage pressurization and leakage checks include tests in a repair area at differential pressures of 280 mbar (4.06 psi) and 550 mbar (7.97 psi), together with a procedure for measuring structural leakage.

The leveling and measurement material provides procedures for checking aircraft geometry after abnormal operation. It identifies datum lines and datum points and includes measurement references for the fuselage, wing, horizontal stabilizer, vertical stabilizer, engine pylons and landing gears. Figures include positions of measurement points, dimensional tables, checks of wing and fuselage point variation, vertical-stabilizer verticality, engine-pylon coordinates, landing-gear X/Y positions and main-gear symmetry.

An aircraft-stability section addresses the aircraft on its wheels under dry, wet and icy ground conditions as well as configurations involving jacks, a forward jack, a nose-wheel jack, a single main-gear wheel jack and wheel-change arrangements. The chapter additionally contains demagnetization maintenance practices for external parts of the windshield and sliding-window frames.

Chapters Covered

• 05-00-00 – Time Limits – Maintenance Checks – General
  • Description and operation
  • Scheduled and unscheduled maintenance-check structure
• 05-20-00 – Scheduled Maintenance Checks
  • Zonal inspection task numbering and accomplishment instructions
• 05-21-00 – Zonal Inspection: Lower Half of Fuselage
  • Radome; avionics compartment; forward, aft and bulk cargo compartments; center wing; aft cabin underfloor; belly fairing; air-conditioning and hydraulics compartments
• 05-22-00 – Zonal Inspection: Upper Half of Fuselage
  • Cockpit; forward cabin utility areas; forward, center and aft passenger compartments; aft cabin utility area
• 05-23-00 – Zonal Inspection: Stabilizers and Cone/Rear Fuselage
  • Aft fuselage tail section; vertical stabilizer and rudder; trimmable horizontal stabilizer and elevator
• 05-24-00 – Zonal Inspection: Power Plant, Nacelles and Pylons
  • Engine pylon box and forward fairing; air intake, fan and accessory gearbox; thrust reverser and exhaust section; aft pylon
• 05-25-00 – Zonal Inspection: Wing
  • Fixed leading edge; flap-track fairings and wing tip; fuel tank; vent surge tank; outboard dry bay; aft/trailing-edge structure; aileron
• 05-27-00 – Zonal Inspection: Landing Gear and Landing Gear Doors
  • Nose gear and doors; main landing gear and doors
• 05-28-00 – Zonal Inspection: Doors
  • Avionics doors; cargo doors; passenger/crew doors and emergency exits
• 05-50-00 – Unscheduled Maintenance Checks
  • Maintenance practices, fluid-leak measurement and quick-dispatch cross-references
  Complete PDF Bookmark Tree

  Complete Bookmarks

  The complete bookmarks in the “Airbus A318 A319 A320 A321 Chapter 05 Time Limits & Maintenance Checks Manual PDF – Rev 40 2012” are as follows:

  Manual Front Matter

  +Chapter 05 – TIME LIMITS – MAINTENANCE CHECKSp. 1

  Table of Contentsp. 1

  +05-00 – TIME LIMITS – MAINTENANCE CHECKS – GENERALp. 17

  +05-00-00 – TIME LIMITS – MAINTENANCE CHECKS – GENERALp. 17

  +05-00-00 PB 001 CONF 00 – TIME LIMITS – MAINTENANCE CHECKS – GENERAL – DESCRIPTION AND OPERATIONp. 17

  Generalp. 17

  Time Limits and Maintenance Checksp. 18

  +05-20 – SCHEDULED MAINTENANCE CHECKSp. 19

  +05-20-00 – SCHEDULED MAINTENANCE CHECKSp. 19

  +05-20-00 PB 001 CONF 00 – SCHEDULED MAINTENANCE CHECKS – DESCRIPTION AND OPERATIONp. 19

  Generalp. 19

  +05-21 – ZONAL INSPECTION : LOWER HALF OF FUSELAGEp. 20

  +05-21-00 – ZONAL INSPECTION : LOWER HALF OF FUSELAGEp. 20

  +05-21-00 PB 601 CONF 00 – ZONAL INSPECTION : LOWER HALF OF FUSELAGE – INSPECTION/CHECKp. 20

  05-21-00-200-001-A – Zonal Inspection as far as visible from the Ground of the Lower Half of the Fuselagep. 20

  05-21-00-200-002-A – Zonal Inspection of the Lower Half of the Fuselagep. 21

  +05-21-10 – ZONAL INSPECTION : RADOMEp. 22

  +05-21-10 PB 601 CONF 00 – ZONAL INSPECTION : RADOME – INSPECTION/CHECKp. 22

  05-21-10-200-001-A – GENERAL VISUAL INSPECTION OF RADOME (EWIS)p. 22

  +05-21-20 – ZONAL INSPECTION : AVIONICS COMPARTMENTp. 24

  +05-21-20 PB 601 CONF 00 – ZONAL INSPECTION : AVIONICS COMPARTMENT – INSPECTION/CHECKp. 24

  05-21-20-200-001-A – GENERAL VISUAL INSPECTION OF AVIONIC COMPARTMENT (EWIS)p. 24

  05-21-20-200-002-A – Zonal Inspection as far as Visible from the Ground of the Nose Gear Well (Zones 123)p. 25

  +05-21-20-200-003-A – GENERAL VISUAL INSPECTION OF LATERAL AVIONIC COMPARTMENT (EWIS)p. 26

  Figure 05-21-20-991-00200-A – Access Doors of the Avionics Compartment (Left Side)p. 28

  Figure 05-21-20-991-00700-A – Access Doors of the Avionics Compartment (Right Side)p. 29

  05-21-20-200-005-A – GENERAL VISUAL INSPECTION OF REAR AVIONIC COMPARTMENT (EWIS)p. 30

  05-21-20-200-007-A – GENERAL VISUAL INSPECTION OF AVIONIC COMPARTMENT (EWIS)p. 31

  05-21-20-200-008-A – GENERAL VISUAL INSPECTION OF LATERAL AVIONIC COMPARTMENT (EWIS)p. 33

  +05-21-20-200-010-A – GENERAL VISUAL INSPECTION OF REAR AVIONIC COMPARTMENT (EWIS)p. 35

  Figure 05-21-20-991-00600-A – Sidewall Panels of the Forward Cargo Compartmentp. 37

  05-21-20-200-012-A – GENERAL VISUAL INSPECTION OF NOSE GEAR WELL (EWIS)p. 38

  +05-21-30 – ZONAL INSPECTION : FORWARD CARGO COMPARTMENTp. 39

  +05-21-30 PB 601 CONF 00 – ZONAL INSPECTION : FORWARD CARGO COMPARTMENT – INSPECTION/CHECKp. 39

  05-21-30-200-001-A – GENERAL VISUAL INSPECTION OF FORWARD CARGO COMPARTMENT (AS FAR AS VISIBLE, IF ACT(S) INSTALLED) (EWIS)p. 39

  +05-21-30-200-002-A – GENERAL VISUAL INSPECTION OF UNDERFLOOR BAY OF FWD CARGO COMPARTMENT (EWIS)p. 41

  Figure 05-21-30-991-00300-A – Access Doors of the Lower Section of the Fuselage (Zone 130)p. 43

  05-21-30-200-003-A – GENERAL VISUAL INSPECTION OF BAY BEHIND FWD CARGO COMPARTMENT (EWIS)p. 44

  +05-21-30-200-004-A – GENERAL VISUAL INSPECTION OF FORWARD CARGO COMPARTMENT (EWIS)p. 46

  Figure 05-21-30-991-00200-A – Floor and Ceiling Panels of the Forward Cargo Compartmentp. 48

  Figure 05-21-30-991-00100-A – Sidewall Panels of the Forward Cargo Compartmentp. 49

  05-21-30-200-006-A – GENERAL VISUAL INSPECTION OF FORWARD CARGO COMPARTMENT (EWIS)p. 50

  +05-21-40 – ZONAL INSPECTION : CENTER WINGp. 52

  +05-21-40 PB 601 CONF 00 – ZONAL INSPECTION : CENTER WING – INSPECTION/CHECKp. 52

  05-21-40-200-001-A – GENERAL VISUAL INSPECTION OF CENTER WING BOX (EWIS)p. 52

  05-21-40-200-002-A – GENERAL VISUAL INSPECTION OF ZONE UNDER CABIN FLOOR (EWIS)p. 54

  05-21-40-200-003-A – Zonal Inspection as far as visible from the Ground of the Main Gear Well and the Hydraulics Compartment (Zones 147 and 148)p. 56

  05-21-40-200-004-A – GENERAL VISUAL INSPECTION OF MLG-WELL AND HYDRAULIC COMPARTMENT (EWIS)p. 57

  05-21-40-200-005-A – GENERAL VISUAL INSPECTION OF MLG-WELL AND HYDRAULIC COMPARTMENT (EWIS)p. 59

  +05-21-50 – ZONAL INSPECTION : AFT CARGO COMPARTMENTp. 61

  +05-21-50 PB 601 CONF 00 – ZONAL INSPECTION : AFT CARGO COMPARTMENT – INSPECTION/CHECKp. 61

  05-21-50-200-001-A – GENERAL VISUAL INSPECTION OF AFT CARGO COMPARTMENT (EWIS)p. 61

  05-21-50-200-002-A – GENERAL VISUAL INSPECTION OF UNDERFLOOR BAY OF AFT CARGO COMPARTMENT (EWIS)p. 63

  +05-21-50-200-003-A – Zonal Inspection of Aft Cargo Compartment (EWIS)p. 65

  Figure 05-21-50-991-00200-F – Floor and Ceiling Panels of the Aft Cargo Compartmentp. 67

  Figure 05-21-50-991-00100-A – Sidewall Panels of the Aft Cargo Compartmentp. 68

  05-21-50-200-004-A – GENERAL VISUAL INSPECTION OF AFT CARGO COMPARTMENT (EWIS)p. 69

  +05-21-60 – ZONAL INSPECTION : BULK CARGO COMPARTMENTp. 72

  +05-21-60 PB 601 CONF 00 – ZONAL INSPECTION : BULK CARGO COMPARTMENT – INSPECTION/CHECKp. 72

  05-21-60-200-001-A – GENERAL VISUAL INSPECTION OF BULK CARGO COMPARTMENT (AS FAR AS VISIBLE, IF ACT IS INSTALLED) (EWIS)p. 72

  05-21-60-200-002-A – GENERAL VISUAL INSPECTION OF UNDERFLOOR BAY OF BULK CARGO COMPARTMENT (EWIS)p. 74

  05-21-60-200-003-A – GENERAL VISUAL INSPECTION OF BULK CARGO COMPARTMENT (EWIS)p. 76

  +05-21-60-200-004-A – GENERAL VISUAL INSPECTION OF BULK CARGO COMPARTMENT (EWIS)p. 78

  Figure 05-21-60-991-00100-B – Floor and Ceiling Panels of the Bulk Cargo Compartmentp. 80

  Figure 05-21-60-991-00200-B – Sidewall Panels and Partition of the Bulk Cargo Compartmentp. 81

  +05-21-70 – ZONAL INSPECTION : AFT CABIN UNDERFLOOR COMPARTMENTp. 82

  +05-21-70 PB 601 CONF 00 – ZONAL INSPECTION : AFT CABIN UNDERFLOOR COMPARTMENT – INSPECTION/CHECKp. 82

  +05-21-70-200-001-A – GENERAL VISUAL INSPECTION OF AFT CABIN UNDERFLOOR COMPARTMENT (EWIS)p. 82

  Figure 05-21-70-991-00100-A – Access Doors of the Aft Fuselagep. 84

  05-21-70-200-002-A – GENERAL VISUAL INSPECTION OF AFT CABIN UNDERFLOOR COMPARTMENT (EWIS)p. 85

  +05-21-90 – ZONAL INSPECTION : BELLY FAIRING, AIR CONDITIONING AND HYDRAULICS COMPARTMENTSp. 87

  +05-21-90 PB 601 CONF 00 – ZONAL INSPECTION : BELLY FAIRING, AIR CONDITIONING AND HYDRAULICS COMPARTMENTS – INSPECTION/CHECKp. 87

  05-21-90-200-001-A – GENERAL VISUAL INSPECTION OF AIR CONDITIONING COMPARTMENT AND FAIRINGS (EWIS)p. 87

  05-21-90-200-003-A – GENERAL VISUAL INSPECTION OF OFFWING ESCAPE SLIDE STOWAGE AREA (EWIS)p. 89

  +05-21-90-200-005-A – GENERAL VISUAL INSPECTION OF HYDRAULIC COMPARTMENT AND FAIRINGS (EWIS)p. 91

  Figure 05-21-90-991-00400-A – Hydraulic Compartment Access Doors (195BB and 196BB)p. 92

  05-21-90-200-007-A – GENERAL VISUAL INSPECTION OF REAR FAIRING (EWIS)p. 93

  05-21-90-200-009-A – GENERAL VISUAL INSPECTION OF AIR CONDITIONING COMPARTMENT AND FAIRINGS (EWIS)p. 95

  +05-22 – ZONAL INSPECTION : UPPER HALF OF FUSELAGEp. 97

  +05-22-00 – ZONAL INSPECTION : UPPER HALF OF FUSELAGEp. 97

  +05-22-00 PB 601 CONF 00 – ZONAL INSPECTION : UPPER HALF OF FUSELAGE – INSPECTION/CHECKp. 97

  05-22-00-200-001-A – Zonal Inspection as far as Visible from the Ground of the Upper Half of the Fuselagep. 97

  05-22-00-200-002-A – Zonal Inspection of the Upper Half of the Fuselagep. 98

  +05-22-10 – ZONAL INSPECTION : COCKPITp. 99

  +05-22-10 PB 601 CONF 00 – ZONAL INSPECTION : COCKPIT – INSPECTION/CHECKp. 99

  +05-22-10-200-001-A – GENERAL VISUAL INSPECTION OF COCKPIT (EWIS)p. 99

  Figure 05-22-10-991-00100-A – Access Panels of the Cockpitp. 101

  05-22-10-200-002-A – GENERAL VISUAL INSPECTION OF COCKPIT (EWIS)p. 102

  +05-22-20 – ZONAL INSPECTION : FORWARD CABIN UTILITY AREASp. 104

  +05-22-20 PB 601 CONF 00 – ZONAL INSPECTION : FORWARD CABIN UTILITY AREAS – INSPECTION/CHECKp. 104

  05-22-20-200-006-A – GENERAL VISUAL INSPECTION OF FWD CABIN UTILITY AREAS INCLUDING FLOOR STRUCTURE (EWIS)p. 104

  05-22-20-200-003-A – GENERAL VISUAL INSPECTION OF FWD CABIN UTILITY AREA OVERHEAD COMPARTMENT (EWIS)p. 107

  +05-22-30 – ZONAL INSPECTION : FORWARD PASSENGER COMPARTMENTp. 109

  +05-22-30 PB 601 CONF 00 – ZONAL INSPECTION : FORWARD PASSENGER COMPARTMENT – INSPECTION/CHECKp. 109

  +05-22-30-200-001-A – GENERAL VISUAL INSPECTION OF FWD PASSENGER COMPARTMENT (EWIS) (INCLUDING FLOOR STRUCTURE)p. 109

  Figure 05-22-30-991-00100-A – Sidewall and Ceiling Panels of the Passenger Compartment (Zones 231-232)p. 112

  Figure 05-22-30-991-00200-A – Sidewall Panels of the Passenger Compartment (Zone 232)p. 113

  05-22-30-200-003-A – GENERAL VISUAL INSPECTION OF FWD PASSENGER OVERHEAD COMPARTMENT (EWIS)p. 114

  +05-22-40 – ZONAL INSPECTION : MID PASSENGER COMPARTMENTp. 116

  +05-22-40 PB 601 CONF 00 – ZONAL INSPECTION : MID PASSENGER COMPARTMENT – INSPECTION/CHECKp. 116

  +05-22-40-200-001-A – GENERAL VISUAL INSPECTION OF CENTER PASSENGER COMPARTMENT (EWIS) (INCLUDING FLOOR STRUCTURE)p. 116

  Figure 05-22-40-991-00100-A – Sidewall and Ceiling Panels of the Center Passenger Compartmentp. 119

  Figure 05-22-40-991-00200-A – Sidewall Panels of the Passenger Compartment (Zone 242)p. 120

  05-22-40-200-003-A – GENERAL VISUAL INSPECTION OF CENTER PASSENGER OVERHEAD COMPARTMENT (EWIS)p. 121

  +05-22-50 – ZONAL INSPECTION : AFT PASSENGER COMPARTMENTp. 123

  +05-22-50 PB 601 CONF 00 – ZONAL INSPECTION : AFT PASSENGER COMPARTMENT – INSPECTION/CHECKp. 123

  +05-22-50-200-001-A – GENERAL VISUAL INSPECTION OF AFT PASSENGER COMPARTMENT (EWIS) (INCLUDING FLOOR STRUCTURE)p. 123

  Figure 05-22-50-991-00100-A – Sidewall and Ceiling Panels of the Aft Passenger Compartment (Zone 251)p. 126

  Figure 05-22-50-991-00200-A – Sidewall Panels of the Passenger Compartment (Zone 252)p. 127

  05-22-50-200-003-A – GENERAL VISUAL INSPECTION OF AFT PASSENGER OVERHEAD COMPARTMENT (EWIS)p. 128

  +05-22-60 – ZONAL INSPECTION : AFT CABIN UTILITY AREAp. 130

  +05-22-60 PB 601 CONF 00 – ZONAL INSPECTION : AFT CABIN UTILITY AREA – INSPECTION/CHECKp. 130

  05-22-60-200-003-A – Zonal Inspection of the Overhead Compartment of the Aft Cabin (EWIS) (Zones 263 and 264)p. 130

  05-22-60-200-004-A – GENERAL VISUAL INSPECTION OF AFT CABIN UTILITY AREAS INCLUDING FLOOR STRUCTURE (EWIS)p. 132

  +05-23 – ZONAL INSPECTION : STABILIZERS AND CONE/REAR FUSELAGEp. 135

  +05-23-00 – ZONAL INSPECTION : STABILIZERS AND CONE/REAR FUSELAGEp. 135

  +05-23-00 PB 601 CONF 00 – ZONAL INSPECTION : STABILIZERS AND CONE/REAR FUSELAGE – INSPECTION/CHECKp. 135

  05-23-00-200-001-A – Zonal Inspection as far as visible from the ground of the Stabilizers and the Cone/Rear Fuselagep. 135

  05-23-00-200-002-A – Zonal Inspection of Stabilizers and Cone/Rear Fuselagep. 136

  +05-23-10 – ZONAL INSPECTION : FUSELAGE TAIL SECTION AFT OF AFT PRESSURE BULKHEADp. 137

  +05-23-10 PB 601 CONF 00 – ZONAL INSPECTION : FUSELAGE TAIL SECTION AFT OF AFT PRESSURE BULKHEAD – INSPECTION/CHECKp. 137

  +05-23-10-200-001-A – GENERAL VISUAL INSPECTION OF AFT FUSELAGE TAIL SECTION (EWIS)p. 137

  Figure 05-23-10-991-00100-A – Access Provision of the Aft Fuselage Tail Sectionp. 139

  05-23-10-200-002-A – GENERAL VISUAL INSPECTION OF TAIL CONE APU AIR INTAKE AREA (EWIS)p. 140

  05-23-10-200-003-A – GENERAL VISUAL INSPECTION OF TAIL CONE APU AND ACCESSORY COMPARTMENT (EWIS)p. 141

  05-23-10-200-004-A – GENERAL VISUAL INSPECTION OF TAIL CONE APU EXHAUST AREA (EWIS)p. 143

  +05-23-20 – ZONAL INSPECTION : VERTICAL STABILIZER AND RUDDERp. 144

  +05-23-20 PB 601 CONF 00 – ZONAL INSPECTION : VERTICAL STABILIZER AND RUDDER – INSPECTION/CHECKp. 144

  05-23-20-200-001-A – GENERAL VISUAL INSPECTION OF DORSAL FIN (EWIS)p. 144

  05-23-20-200-002-A – GENERAL VISUAL INSPECTION OF VERTICAL STABILIZER LEADING EDGE (EWIS)p. 146

  05-23-20-200-003-A – GENERAL VISUAL INSPECTION OF VERTICAL STABILIZER SPAR BOX (EWIS)p. 148

  05-23-20-200-004-A – GENERAL VISUAL INSPECTION OF VERTICAL STABILIZER TIP (EWIS)p. 150

  05-23-20-200-005-A – GENERAL VISUAL INSPECTION OF VERTICAL STABILIZER TRAILING EDGE (EWIS)p. 151

  05-23-20-200-006-A – GENERAL VISUAL INSPECTION OF RUDDER (EWIS)p. 153

  05-23-20-200-007-A – GENERAL VISUAL INSPECTION OF VERTICAL STABILIZER TRAILING EDGE (EWIS)p. 155

  05-23-20-200-008-A – GENERAL VISUAL INSPECTION OF RUDDER (EWIS)p. 157

  +05-23-30 – ZONAL INSPECTION : TRIMMABLE HORIZONTAL STABILIZER AND ELEVATORp. 159

  +05-23-30 PB 601 CONF 00 – ZONAL INSPECTION : TRIMMABLE HORIZONTAL STABILIZER AND ELEVATOR – INSPECTION/CHECKp. 159

  05-23-30-200-001-A – GENERAL VISUAL INSPECTION OF TRIMMABLE HORIZONTAL STABILIZER LEADING EDGE (EWIS)p. 159

  05-23-30-200-002-A – GENERAL VISUAL INSPECTION OF TRIMMABLE HORIZONTAL STABILIZER TIP (EWIS)p. 161

  +05-23-30-200-003-A – GENERAL VISUAL INSPECTION OF TRIMMABLE HORIZONTAL STABILIZER SPAR BOX (EWIS)p. 162

  Figure 05-23-30-991-00700-A – Access provision of the Aft Fuselage Tail Sectionp. 164

  05-23-30-200-004-A – GENERAL VISUAL INSPECTION OF TRIMMABLE HORIZONTAL STABILIZER TRAILING EDGE (EWIS)p. 165

  05-23-30-200-005-A – GENERAL VISUAL INSPECTION OF ELEVATOR (EWIS)p. 167

  05-23-30-200-007-A – GENERAL VISUAL INSPECTION OF TRIMMABLE HORIZONTAL STABILIZER TRAILING EDGE (EWIS)p. 169

  +05-24 – ZONAL INSPECTION : POWER PLANT, NACELLES AND PYLONSp. 171

  +05-24-00 – ZONAL INSPECTION : POWER PLANT, NACELLES AND PYLONSp. 171

  +05-24-00 PB 601 CONF 00 – ZONAL INSPECTION : POWER PLANT, NACELLES AND PYLONS – INSPECTION/CHECKp. 171

  05-24-00-200-001-A – Zonal Inspection as far as Visible from the Ground of the Power Plant, the Nacelles and the Pylonsp. 171

  05-24-00-200-002-A – Zonal Inspection of the Power Plant, the Nacelles and the Pylonsp. 172

  +05-24-10 – ZONAL INSPECTION : ENGINE PYLON BOX AND FORWARD FAIRINGp. 173

  +05-24-10 PB 601 CONF 00 – ZONAL INSPECTION : ENGINE PYLON BOX AND FORWARD FAIRING – INSPECTION/CHECKp. 173

  +05-24-10-200-001-A – GENERAL VISUAL INSPECTION OF UPPER FWD PYLON (EWIS)p. 173

  Figure 05-24-10-991-00100-B – Access Panels and Doors of the Left Nacelle (Left Side)p. 175

  Figure 05-24-10-991-00200-B – Access Panels and Doors of the Left Nacelle (Right Side)p. 176

  Figure 05-24-10-991-00300-B – Access Panels and Doors of the Right Nacelle (Left Side)p. 177

  Figure 05-24-10-991-00400-B – Access Panels and Doors of the Right Nacelle (Right Side)p. 178

  05-24-10-200-002-A – GENERAL VISUAL INSPECTION OF LOWER PYLON (EWIS)p. 179

  +05-24-30 – ZONAL INSPECTION : ENGINE AIR INTAKE, FAN AND ACCESSORY GEARBOXp. 181

  +05-24-30 PB 601 CONF 00 – ZONAL INSPECTION : ENGINE AIR INTAKE, FAN AND ACCESSORY GEARBOX – INSPECTION/CHECKp. 181

  +05-24-30-200-001-A – GENERAL VISUAL INSPECTION OF AIR INTAKE LIP (EWIS)p. 181

  Figure 05-24-30-991-00100-C – Access Doors of the Left Nacelle (Left Side)p. 183

  Figure 05-24-30-991-00200-C – Access Doors of the Left Nacelle (Right Side)p. 184

  Figure 05-24-30-991-00300-B – Access Doors of the Right Nacelle (Right Side)p. 185

  Figure 05-24-30-991-00400-B – Access Doors of the Right Nacelle (Left Side)p. 186

  05-24-30-200-002-A – GENERAL VISUAL INSPECTION OF FAN AND ACCESSORY GEAR BOX (EWIS)p. 187

  05-24-30-200-003-A – GENERAL VISUAL INSPECTION OF FAN COWL (EWIS)p. 189

  +05-24-50 – ZONAL INSPECTION : ENGINE THRUST REVERSER AND EXHAUST SECTIONp. 191

  +05-24-50 PB 601 CONF 00 – ZONAL INSPECTION : ENGINE THRUST REVERSER AND EXHAUST SECTION – INSPECTION/CHECKp. 191

  +05-24-50-200-001-A – GENERAL VISUAL INSPECTION OF THRUST REVERSER (EWIS)p. 191

  Figure 05-24-50-991-00100-B – Access Doors of the Left Nacelle (Left Side)p. 194

  Figure 05-24-50-991-00200-B – Access Doors of the Left Nacelle (Right Side)p. 195

  Figure 05-24-50-991-00300-B – Access Doors of the Right Nacelle (Left Side)p. 196

  Figure 05-24-50-991-00400-B – Access Doors of the Right Nacelle (Right Side)p. 197

  +05-24-50-200-002-A – GENERAL VISUAL INSPECTION OF HOT SECTION (EWIS)p. 198

  Figure 05-24-50-991-00500-A – HPT Case Flange Locationp. 200

  +05-24-70 – ZONAL INSPECTION : ENGINE AFT PYLONp. 201

  +05-24-70 PB 601 CONF 00 – ZONAL INSPECTION : ENGINE AFT PYLON – INSPECTION/CHECKp. 201

  +05-24-70-200-001-A – GENERAL VISUAL INSPECTION OF PYLON LEADING EDGE AND LOWER FAIRING (EWIS)p. 201

  Figure 05-24-70-991-00100-C – Location of the Access Panels of the Left Nacelle (Left Side)p. 204

  Figure 05-24-70-991-00200-C – Location of the Access Panels of the Left Nacelle (Right Side)p. 205

  Figure 05-24-70-991-00500-C – Location of the Access Panels of the Right Nacelle (Left Side)p. 206

  Figure 05-24-70-991-00600-C – Location of the Access Panels of the Right Nacelle (Right Side)p. 207

  +05-25 – ZONAL INSPECTION : WINGp. 208

  +05-25-00 – ZONAL INSPECTION : WINGp. 208

  +05-25-00 PB 601 CONF 00 – ZONAL INSPECTION : WING – INSPECTION/CHECKp. 208

  05-25-00-200-001-A – Zonal Inspection of the Wings as far as visible from the groundp. 208

  05-25-00-200-002-A – GENERAL VISUAL INSPECTION OF WING LOWER SURFACE INCLUDING UPPER AND LOWER SURFACES OF SLATS AND FLAPS (EWIS)p. 209

  05-25-00-200-003-A – GENERAL VISUAL INSPECTION OF WING UPPER SURFACE INCLUDING SLATS, FLAPS AND SPOILERS (EWIS)p. 211

  +05-25-20 – ZONAL INSPECTION : WING FIXED LEADING EDGEp. 213

  +05-25-20 PB 601 CONF 00 – ZONAL INSPECTION : WING FIXED LEADING EDGE – INSPECTION/CHECKp. 213

  +05-25-20-200-001-A – GENERAL VISUAL INSPECTION OF INBOARD FIXED LEADING EDGE STRUCTURE (EWIS)p. 213

  Figure 05-25-20-991-00100-A – Access Panels of the Upper Leading Edge of the Wingp. 216

  Figure 05-25-20-991-00200-A – Access Panels of the Lower Surface of the Wingp. 217

  05-25-20-200-002-A – GENERAL VISUAL INSPECTION OF OUTBOARD FIXED LEADING EDGE STRUCTURE (EWIS)p. 218

  +05-25-30 – ZONAL INSPECTION : WING FLAP TRACK FAIRINGS AND WING TIPp. 221

  +05-25-30 PB 601 CONF 00 – ZONAL INSPECTION : WING FLAP TRACK FAIRINGS AND WING TIP – INSPECTION/CHECKp. 221

  +05-25-30-200-001-A – GENERAL VISUAL INSPECTION OF FLAP TRACK NO 2 AND FAIRING (EWIS)p. 221

  Figure 05-25-30-991-00100-A – Access Panels of the Flap Track Fairingsp. 223

  05-25-30-200-002-A – GENERAL VISUAL INSPECTION OF FLAP TRACK NO 3 AND FAIRING (EWIS)p. 224

  05-25-30-200-003-A – GENERAL VISUAL INSPECTION OF FLAP TRACK NO 4 AND FAIRING (EWIS)p. 226

  +05-25-30-200-004-A – GENERAL VISUAL INSPECTION OF WING TIP (EWIS)p. 228

  Figure 05-25-30-991-00200-B – Access Panels of the Wing Tipp. 229

  05-25-30-200-005-A – GENERAL VISUAL INSPECTION OF FLAP TRACK NO 2 AND FAIRING (EWIS)p. 230

  05-25-30-200-006-A – GENERAL VISUAL INSPECTION OF FLAP TRACK NO 3 AND FAIRING (EWIS)p. 232

  05-25-30-200-007-A – GENERAL VISUAL INSPECTION OF FLAP TRACK NO 4 AND FAIRING (EWIS)p. 234

  +05-25-40 – ZONAL INSPECTION : WING FUEL TANKp. 236

  +05-25-40 PB 601 CONF 00 – ZONAL INSPECTION : WING FUEL TANK – INSPECTION/CHECKp. 236

  05-25-40-200-005-A – GENERAL VISUAL INSPECTION OF WING FUEL TANK (EWIS)p. 236

  05-25-40-200-004-A – GENERAL VISUAL INSPECTION OF WING FUEL TANK (EWIS)p. 238

  +05-25-50 – ZONAL INSPECTION : WING VENT SURGE TANKp. 241

  +05-25-50 PB 601 CONF 00 – ZONAL INSPECTION : WING VENT SURGE TANK – INSPECTION/CHECKp. 241

  +05-25-50-200-001-A – GENERAL VISUAL INSPECTION OF VENT SURGE TANK (EWIS)p. 241

  Figure 05-25-50-991-00100-A – Access Panels of the Vent Surge Tank of the Wingp. 243

  +05-25-60 – ZONAL INSPECTION : WING DRY BAY (OUTBOARD)p. 244

  +05-25-60 PB 601 CONF 00 – ZONAL INSPECTION : WING DRY BAY (OUTBOARD) – INSPECTION/CHECKp. 244

  05-25-60-200-001-A – GENERAL VISUAL INSPECTION OF DRY BAY (OUTBOARD) (EWIS)p. 244

  +05-25-70 – ZONAL INSPECTION : AFT SECTION OF WING AND TRAILING EDGE FIXED STRUCTUREp. 246

  +05-25-70 PB 601 CONF 00 – ZONAL INSPECTION : AFT SECTION OF WING AND TRAILING EDGE FIXED STRUCTURE – INSPECTION/CHECKp. 246

  05-25-70-200-001-A – Zonal Inspection as far as visible of the Main Landing Gear Bayp. 246

  +05-25-70-200-002-A – GENERAL VISUAL INSPECTION OF SHROUD BOX (EWIS)p. 247

  Figure 05-25-70-991-00100-A – Access Panels of the Left Wing Lower Trailing Edgep. 250

  Figure 05-25-70-991-00300-A – Access Panels of the Right Wing Lower Trailing Edgep. 251

  Figure 05-25-70-991-00100-B – Access Panels of the Left Wing Lower Trailing Edgep. 252

  Figure 05-25-70-991-00300-B – Access Panels of the Right Wing Lower Trailing Edgep. 253

  05-25-70-200-003-A – GENERAL VISUAL INSPECTION OF INBOARD FIXED TRAILING EDGE STRUCTURE FROM SHROUD BOX TO RIB 9 (EWIS)p. 254

  05-25-70-200-004-A – GENERAL VISUAL INSPECTION OF FALSE SPAR BOX (EWIS)p. 256

  05-25-70-200-005-A – GENERAL VISUAL INSPECTION OF OUTBOARD FIXED TRAILING EDGE STRUCTURE FROM RIB 9 TO RIB 27 (EWIS)p. 258

  05-25-70-200-006-A – GENERAL VISUAL INSPECTION OF MLG BAY (EWIS)p. 260

  +05-25-90 – ZONAL INSPECTION : WING AILERONp. 262

  +05-25-90 PB 601 CONF 00 – ZONAL INSPECTION : WING AILERON – INSPECTION/CHECKp. 262

  +05-25-90-200-001-A – GENERAL VISUAL INSPECTION OF AILERON (EWIS)p. 262

  Figure 05-25-90-991-00100-A – Access Panels of the Wing Aileronp. 264

  +05-27 – ZONAL INSPECTION : LANDING GEAR AND LANDING GEAR DOORSp. 265

  +05-27-00 – ZONAL INSPECTION : LANDING GEAR AND LANDING GEAR DOORSp. 265

  +05-27-00 PB 601 CONF 00 – ZONAL INSPECTION : LANDING GEAR AND LANDING GEAR DOORS – INSPECTION/CHECKp. 265

  05-27-00-200-001-A – Zonal Inspection as far as Visible from the Ground of the Landing Gear and the Landing Gear Doorsp. 265

  +05-27-10 – ZONAL INSPECTION : NOSE GEAR AND DOORSp. 266

  +05-27-10 PB 601 CONF 00 – ZONAL INSPECTION : NOSE GEAR AND DOORS – INSPECTION/CHECKp. 266

  05-27-10-200-001-A – GENERAL VISUAL INSPECTION OF NOSE GEAR AND NOSE GEAR DOORS (EWIS)p. 266

  +05-27-30 – ZONAL INSPECTION : MAIN LANDING GEAR AND DOORSp. 268

  +05-27-30 PB 601 CONF 00 – ZONAL INSPECTION : MAIN LANDING GEAR AND DOORS – INSPECTION/CHECKp. 268

  05-27-30-200-001-A – GENERAL VISUAL INSPECTION OF LH/RH MAIN LANDING GEAR (EWIS)p. 268

  +05-27-30-200-002-A – GENERAL VISUAL INSPECTION OF MAIN LANDING GEAR CYLINDER DOOR (EWIS)p. 269

  Figure 05-27-30-991-00100-A – Main Landing Gear and Doorsp. 270

  05-27-30-200-003-A – GENERAL VISUAL INSPECTION OF MAIN LANDING GEAR SECONDARY DOOR (EWIS)p. 271

  05-27-30-200-004-A – GENERAL VISUAL INSPECTION OF MAIN LANDING GEAR MAIN DOORS (EWIS)p. 272

  +05-28 – ZONAL INSPECTION : DOORSp. 273

  +05-28-00 – ZONAL INSPECTION : DOORSp. 273

  +05-28-00 PB 601 CONF 00 – ZONAL INSPECTION : DOORS – INSPECTION/CHECKp. 273

  05-28-00-200-001-A – Zonal Inspection of the Doors as far as Visible from the Groundp. 273

  +05-28-10 – ZONAL INSPECTION : AVIONICS COMPARTMENT DOORS (FORWARD AND LATERAL)p. 274

  +05-28-10 PB 601 CONF 00 – ZONAL INSPECTION : AVIONICS COMPARTMENT DOORS (FORWARD AND LATERAL) – INSPECTION/CHECKp. 274

  +05-28-10-200-001-A – GENERAL VISUAL INSPECTION OF FWD AVIONICS COMPARTMENT DOOR (EWIS) (INCLUDING EXTERNAL SURFACE)p. 274

  Figure 05-28-10-991-00100-A – Avionics Compartment Left Side Door and Forward Doorp. 276

  05-28-10-200-002-A – GENERAL VISUAL INSPECTION OF FWD AVIONICS COMPARTMENT DOOR (EWIS)p. 277

  +05-28-10-200-003-A – GENERAL VISUAL INSPECTION OF LATERAL AVIONICS COMPARTMENT DOORS (EWIS) (INCLUDING EXTERNAL SURFACE)p. 279

  Figure 05-28-10-991-00200-A – Avionics Compartment Right Side Doorp. 281

  05-28-10-200-004-A – GENERAL VISUAL INSPECTION OF LATERAL AVIONICS COMPARTMENT DOORS (EWIS)p. 282

  +05-28-20 – ZONAL INSPECTION : AVIONICS COMPARTMENT DOORS, CARGO COMPARTMENT DOORS (RIGHT SIDE)p. 284

  +05-28-20 PB 601 CONF 00 – ZONAL INSPECTION : AVIONICS COMPARTMENT DOORS, CARGO COMPARTMENT DOORS (RIGHT SIDE) – INSPECTION/CHECKp. 284

  05-28-20-200-001-A – GENERAL VISUAL INSPECTION OF FWD CARGO COMPARTMENT DOOR INCLUDING FUSELAGE DOOR SILL, DOOR SEAL AND LOCK FITTINGS, EXTERNAL SURFACE (EWIS)p. 284

  05-28-20-200-002-A – GENERAL VISUAL INSPECTION OF AFT CARGO COMPARTMENT DOOR INCLUDING FUSELAGE DOOR SILL, DOOR SEAL AND LOCK FITTINGS (EWIS)p. 286

  05-28-20-200-003-A – GENERAL VISUAL INSPECTION OF BULK CARGO COMPARTMENT DOOR INCLUDING DOOR STOPS ON FUSELAGE DOOR FRAME (EWIS)p. 288

  +05-28-20-200-004-A – GENERAL VISUAL INSPECTION OF FWD CARGO COMPARTMENT DOOR (EWIS)p. 289

  Figure 05-28-20-991-00100-A – Access Panels of the Cargo Compartment Doorsp. 291

  05-28-20-200-005-A – GENERAL VISUAL INSPECTION OF AFT CARGO COMPARTMENT DOOR (EWIS)p. 292

  05-28-20-200-006-A – GENERAL VISUAL INSPECTION OF BULK CARGO COMPARTMENT DOOR INCLUDING DOOR STOPS ON FUSELAGE DOOR FRAME (EWIS)p. 294

  +05-28-20-200-007-A – GENERAL VISUAL INSPECTION OF REAR AVIONIC COMPARTMENT DOOR (EWIS) (INCLUDING EXTERNAL SURFACE)p. 295

  Figure 05-28-20-991-00200-A – Rear Avionics Compartment Doorp. 297

  05-28-20-200-008-A – GENERAL VISUAL INSPECTION OF REAR AVIONIC COMPARTMENT DOOR (EWIS)p. 298

  +05-28-30 – ZONAL INSPECTION : PASSENGER/CREW DOORS AND EMERGENCY EXITSp. 300

  +05-28-30 PB 601 CONF 00 – ZONAL INSPECTION : PASSENGER/CREW DOORS AND EMERGENCY EXITS – INSPECTION/CHECKp. 300

  05-28-30-200-001-A – GENERAL VISUAL INSPECTION OF FWD AND AFT PASSENGER/CREW DOORS INCLUDING DOOR STOPS ON FUSELAGE DOOR FRAMES AND DOOR SEALS, EXTERNAL SURFACE (EWIS)p. 300

  05-28-30-200-003-A – GENERAL VISUAL INSPECTION OF FWD AND AFT EMERGENCY EXITS INCLUDING DOOR SURROUND ON FUSELAGE DOOR FRAMES AND DOOR SEALS, EXTERNAL SURFACE (EWIS)p. 302

  05-28-30-200-005-A – GENERAL VISUAL INSPECTION OF FWD AND AFT PASSENGER/CREW DOORS (EWIS)p. 304

  05-28-30-200-007-A – GENERAL VISUAL INSPECTION OF FWD AND AFT EMERGENCY EXITS (EWIS)p. 306

  +05-50 – UNSCHEDULED MAINTENANCE CHECKSp. 308

  +05-50-00 – UNSCHEDULED MAINTENANCE CHECKSp. 308

  +05-50-00 PB 001 CONF 00 – UNSCHEDULED MAINTENANCE CHECKS – DESCRIPTION AND OPERATIONp. 308

  Generalp. 308

  +05-50-00 PB 201 CONF 00 – UNSCHEDULED MAINTENANCE CHECKS – MAINTENANCE PRACTICESp. 309

  05-50-00-790-001-A – Fluid Leak Measurement – Maintenance Practicesp. 309

  +05-50-00-040-002-A – Quick Dispatch Guide and Cross-Referencesp. 310

  Figure 05-50-00-991-00200-A – Location of the Antennas, Probes and sensors and Exterior lightsp. 318

  +05-51 – INSPECTIONSp. 320

  +05-51-00 – INSPECTIONSp. 320

  +05-51-00 PB 001 CONF 00 – INSPECTIONS – DESCRIPTION AND OPERATIONp. 320

  Generalp. 320

  Figure 05-51-00-12100-A – Inspection Formp. 322

  +05-51-11 – INSPECTIONS AFTER HARD/HARD OVERWEIGHT LANDINGp. 323

  +05-51-11 PB 601 CONF 00 – INSPECTIONS AFTER HARD/HARD OVERWEIGHT LANDING – INSPECTION/CHECKp. 323

  +05-51-11-200-004-A – Inspection After Hard/Hard Overweight Landing for Aircraft without Enhanced DMU/FDIMU Load Report 15p. 323

  Figure 05-51-11-991-01500-B – Inspection – Definition Diagram without Enhanced DMU/FDIMU Load Report 15p. 351

  Figure 05-51-11-991-00500-A – Aircraft Structure – Critical Areasp. 352

  Figure 05-51-11-991-00700-A – Primary Structure – Materials and Protections Descriptionp. 353

  Figure 05-51-11-991-00800-B – Engine-to-Pylon Attach Fittingsp. 354

  Figure 05-51-11-991-00900-B – Pylon-to-Wing Attach Fittingsp. 355

  Figure 05-51-11-991-02500-B – Inlet Cowl: Engine Interface and Rear Bulkheadp. 356

  Figure 05-51-11-991-02600-B – Fan Cowl Doors: Hinge and Latch Fittingsp. 357

  Figure 05-51-11-991-02700-B – Thrust Reverser: Hinge Fittingsp. 358

  Figure 05-51-11-991-02800-B – Thrust Reverser: Latch Fittingsp. 359

  Figure 05-51-11-991-03000-A – Common Nozzle Assembly: Engine Interfacep. 361

  Figure 05-51-11-991-01000-A – Nose Landing Gearp. 362

  Figure 05-51-11-991-02400-A – Illustration of the Main Landing Gearp. 363

  Figure 05-51-11-991-01100-A – Main Structure of the Cone/Rear Fuselagep. 364

  Figure 05-51-11-991-01200-A – Lower Part of the Center Fuselagep. 365

  Figure 05-51-11-991-01300-A – Center Sectionp. 366

  Figure 05-51-11-991-01400-A – Component Location in the Belly Fairing Structurep. 367

  +05-51-11-200-004-B – Inspection After Hard/Hard Overweight Landing for Aircraft with Enhanced DMU/FDIMU Load Report 15p. 368

  Figure 05-51-11-991-01500-A – Hard/Hard Overweight landing criteria for Enhanced DMU/FDIMU Load Report 15p. 399

  Figure 05-51-11-991-01600-A – Inspection Flow Chartp. 400

  Figure 05-51-11-991-02300-A – Main Landing Gear Legp. 401

  +05-51-12 – INSPECTION AFTER LANDING GEAR DOWN LIMITING SPEED EXCEEDEDp. 402

  +05-51-12 PB 601 CONF 00 – INSPECTION AFTER LANDING GEAR DOWN LIMITING SPEED EXCEEDED – INSPECTION/CHECKp. 402

  +05-51-12-200-001-A – Inspection after Landing Gear Extension at more than the Geardown Limiting Speedp. 402

  Figure 05-51-12-991-00100-A – Lower Part of the Center Fuselagep. 412

  Figure 05-51-12-991-00200-A – Center Sectionp. 413

  Figure 05-51-12-991-00300-A – Component Location in the Belly Fairing Structurep. 414

  Figure 05-51-12-991-00400-A – Main Gear Assemblyp. 415

  Figure 05-51-12-991-00500-A – Inspection on the Wingp. 416

  Figure 05-51-12-991-00600-A – Inspection on the Wingp. 417

  +05-51-13 – INSPECTION AFTER FLAP/SLAT LIMITING SPEED EXCEEDEDp. 418

  +05-51-13 PB 601 CONF 00 – INSPECTION AFTER FLAP/SLAT LIMITING SPEED EXCEEDED – INSPECTION/CHECKp. 418

  +05-51-13-200-001-A – Inspection after Flap/Slat Extension at more than the Flap/Slat Limiting Speedp. 418

  Figure 05-51-13-991-00100-A – Component Location of the Flap Systemp. 426

  Figure 05-51-13-991-00200-A – Flap Componentsp. 427

  Figure 05-51-13-991-00500-A – Track No. 1 Actuatorp. 428

  Figure 05-51-13-991-00600-A – Typical Installation of the Actuatorp. 429

  Figure 05-51-13-991-00400-A – Component Location of the Slat Systemp. 430

  Figure 05-51-13-991-00300-A – Slat Componentsp. 431

  +05-51-14 – INSPECTION OF AIRFRAME AFTER BIRD OR HAIL STRIKEp. 432

  +05-51-14 PB 601 CONF 00 – INSPECTION OF AIRFRAME AFTER BIRD OR HAIL STRIKE – INSPECTION/CHECKp. 432

  05-51-14-200-001-A – Inspection of the Airframe after a Bird or Hail Strike in Flightp. 432

  05-51-14-200-002-A – Inspection of the Airframe after a Hail Strike on Groundp. 443

  +05-51-15 – INSPECTION AFTER A TIRE BURST OR TREAD THROW OR WHEEL FAILUREp. 453

  +05-51-15 PB 601 CONF 00 – INSPECTION AFTER A TIRE BURST OR TREAD THROW OR WHEEL FAILURE – INSPECTION/CHECKp. 453

  05-51-15-200-001-A – Inspection after a Tire Burst or Tread Throw or Wheel Failurep. 453

  +05-51-16 – INSPECTION AFTER BRAKE EMERGENCY APPLICATION OR OVERHEATp. 462

  +05-51-16 PB 601 CONF 00 – INSPECTION AFTER BRAKE EMERGENCY APPLICATION OR OVERHEAT – INSPECTION/CHECKp. 462

  05-51-16-200-001-A – Inspection After Brake Emergency Application or Overheatp. 462

  +05-51-17 – INSPECTION AFTER FLIGHT IN EXCESSIVE TURBULENCE OR IN EXCESS OF VMO/MMOp. 468

  +05-51-17 PB 601 CONF 00 – INSPECTION AFTER FLIGHT IN EXCESSIVE TURBULENCE OR IN EXCESS OF VMO/MMO – INSPECTION/CHECKp. 468

  +05-51-17-200-001-A – Inspection after in Flight Excessive Load Factor due to Turbulence or Maneuver or in Excess of VMO/MMOp. 468

  Figure 05-51-17-991-00700-A – Flow chartp. 484

  Figure 05-51-17-991-00100-B – Inlet Cowl: Engine Interface and Rear Bulkheadp. 486

  Figure 05-51-17-991-00200-B – Fan Cowl Doors: Hinge and Latch Fittingsp. 487

  Figure 05-51-17-991-00300-B – Thrust Reverser: Hinge Fittingsp. 488

  Figure 05-51-17-991-00400-B – Thrust Reverser: Latch Fittingsp. 489

  Figure 05-51-17-991-00600-A – Common Nozzle Assembly: Engine Interfacep. 491

  +05-51-18 – INSPECTION AFTER LIGHTNING STRIKEp. 492

  +05-51-18 PB 601 CONF 00 – INSPECTION AFTER LIGHTNING STRIKE – INSPECTION/CHECKp. 492

  +05-51-18-200-001-A – Inspection after Lightning Strikep. 492

  Figure 05-51-18-991-00100-A – Lightning Strike Inspection Areasp. 521

  Figure 05-51-18-991-00200-A – Location of the Antennas, Probes and Sensors and Exterior Lightsp. 522

  +05-51-19 – INSPECTION AFTER ENGINE BIRD STRIKE OR SLUSH INGESTIONp. 524

  +05-51-19 PB 601 CONF 00 – INSPECTION AFTER ENGINE BIRD STRIKE OR SLUSH INGESTION – INSPECTION/CHECKp. 524

  05-51-19-200-001-A – Inspection of the Engine after a Bird Strike or Slush Ingestionp. 524

  +05-51-21 – INSPECTION AFTER TAIL RUNWAY IMPACTp. 525

  +05-51-21 PB 601 CONF 00 – INSPECTION AFTER TAIL RUNWAY IMPACT – INSPECTION/CHECKp. 525

  +05-51-21-200-001-A – Inspection after a Tail Runway Impactp. 525

  Figure 05-51-21-991-00100-A – Tailcone Equipment (L Side)p. 528

  Figure 05-51-21-991-00200-A – APU Installation (R side)p. 529

  +05-51-22 – INSPECTION AFTER NLG TOWING OVERLOAD OR OVERRUNp. 530

  +05-51-22 PB 601 CONF 00 – INSPECTION AFTER NLG TOWING OVERLOAD OR OVERRUN – INSPECTION/CHECKp. 530

  +05-51-22-200-001-A – Inspection After a NLG Towing Overload or Overrunp. 530

  Figure 05-51-22-991-00100-A – Nose Landing-Gear Wellp. 535

  Figure 05-51-22-991-00200-A – Inspection of the NLG Steering Systemp. 536

  +05-51-23 – INSPECTION AFTER NLG STEERING ANGLE EXCEEDEDp. 537

  +05-51-23 PB 601 CONF 00 – INSPECTION AFTER NLG STEERING ANGLE EXCEEDED – INSPECTION/CHECKp. 537

  +05-51-23-200-001-A – Inspection after NLG Steering Angle of more than 95 deg.p. 537

  Figure 05-51-23-991-00100-A – Inspection of the Nose Landing Gearp. 541

  +05-51-24 – INSPECTION AFTER LEAVING RUNWAY OR TAXIWAYp. 542

  +05-51-24 PB 601 CONF 00 – INSPECTION AFTER LEAVING RUNWAY OR TAXIWAY – INSPECTION/CHECKp. 542

  +05-51-24-200-001-A – Inspection after Leaving Runway or Taxiwayp. 542

  Figure 05-51-24-991-00200-C – Engine Nacellep. 563

  Figure 05-51-24-991-00300-C – Engine Mountsp. 564

  Figure 05-51-24-991-00400-A – Access Doors of the Pylon Boxp. 565

  +05-51-25 – INSPECTION AFTER DUST STORM/VOLCANIC ASH CONDITIONS IN FLIGHT OR ON THE GROUNDp. 566

  +05-51-25 PB 601 CONF 00 – INSPECTION AFTER DUST STORM/VOLCANIC ASH CONDITIONS IN FLIGHT OR ON THE GROUND – INSPECTION/CHECKp. 566

  05-51-25-200-002-A – Inspection after Flight through Dust Storm or Dust Contamination on Groundp. 566

  05-51-25-200-003-A – Inspection after Flight through Volcanic Ash or Volcanic Ash Contamination on Groundp. 582

  +05-51-26 – INSPECTION AFTER ENGINE FAILUREp. 602

  +05-51-26 PB 601 CONF 00 – INSPECTION AFTER ENGINE FAILURE – INSPECTION/CHECKp. 602

  05-51-26-200-001-A – INSPECTION AFTER ENGINE FAILUREp. 602

  +05-51-27 – INSPECTION AFTER IMPACT ON ENGINE COWLSp. 607

  +05-51-27 PB 601 CONF 00 – INSPECTION AFTER IMPACT ON ENGINE COWLS – INSPECTION/CHECKp. 607

  05-51-27-200-001-A – Inspection after Impact on Engine Cowlsp. 607

  +05-51-28 – PROCEDURE AFTER FLUID SPILLAGEp. 610

  +05-51-28 PB 601 CONF 00 – PROCEDURE AFTER FLUID SPILLAGE – INSPECTION/CHECKp. 610

  05-51-28-200-002-A – Procedure after Fluid Spillagep. 610

  +05-51-29 – INSPECTION AFTER ABNORMAL PAX/CREW DOOR MOVEMENTp. 611

  +05-51-29 PB 601 CONF 00 – INSPECTION AFTER ABNORMAL PAX/CREW DOOR MOVEMENT – INSPECTION/CHECKp. 611

  +05-51-29-200-001-A – Inspection after Abnormal Movement of the Pax/Crew Doorp. 611

  Figure 05-51-29-991-00100-A – Passenger/Crew Doorsp. 617

  +05-51-31 – INSPECTION AFTER SIGNIFICANT MLG VIBRATION AT TOUCH-DOWNp. 618

  +05-51-31 PB 601 CONF 00 – INSPECTION AFTER SIGNIFICANT MLG VIBRATION AT TOUCH-DOWN – INSPECTION/CHECKp. 618

  +05-51-31-200-001-A – Inspection after Significant MLG Vibration at Touch-Downp. 618

  Figure 05-51-31-991-00100-A – Bottom Cardan Joint – Clearancesp. 624

  Figure 05-51-31-991-00200-A – Botton Cardan Joint- Clearencesp. 625

  +05-51-34 – INSPECTION AFTER ENGINE WINDMILLING (AFTER ENGINE IN-FLIGHT SHUT-DOWN)p. 626

  +05-51-34 PB 601 CONF 00 – INSPECTION AFTER ENGINE WINDMILLING (AFTER ENGINE IN-FLIGHT SHUT-DOWN) – INSPECTION/CHECKp. 626

  05-51-34-200-001-A – Inspection after Engine Windmilling (After Engine In-Flight Shut-Down)p. 626

  +05-51-35 – INSPECTION AFTER IMPACT ON WING TIP /FENCEp. 627

  +05-51-35 PB 601 CONF 00 – INSPECTION AFTER IMPACT ON WING TIP /FENCE – INSPECTION/CHECKp. 627

  +05-51-35-200-001-A – Inspection after Impact on Wing Tip/Fencep. 627

  Figure 05-51-35-991-00100-A – Wing Tip and Wing Tip Fencep. 631

  +05-51-41 – INSPECTION AFTER OVERWEIGHT TAXIINGp. 632

  +05-51-41 PB 601 CONF 00 – INSPECTION AFTER OVERWEIGHT TAXIING – INSPECTION/CHECKp. 632

  05-51-41-200-001-A – Inspection after Overweight Taxiingp. 632

  +05-51-42 – INSPECTION AFTER VERY HIGH WINDS ON GROUNDp. 639

  +05-51-42 PB 601 CONF 00 – INSPECTION AFTER VERY HIGH WINDS ON GROUND – INSPECTION/CHECKp. 639

  05-51-42-200-001-A – Inspection after Very High Winds on Groundp. 639

  +05-51-43 – INSPECTIONS AFTER WORK ON SYSTEM ELECTRICAL INSTALLATIONp. 644

  +05-51-43 PB 501 CONF 00 – INSPECTIONS AFTER WORK ON SYSTEM ELECTRICAL INSTALLATION – ADJUSTMENT/TESTp. 644

  05-51-43-700-001-A – Inspection after Work on System Electrical Installationp. 644

  +05-51-44 – INSPECTION AFTER FLIGHT WITH HIGH LATERAL LOADSp. 648

  +05-51-44 PB 601 CONF 00 – INSPECTION AFTER FLIGHT WITH HIGH LATERAL LOADS – INSPECTION/CHECKp. 648

  +05-51-44-200-001-A – Inspection after Aircraft Operation with High Lateral Accelerationp. 648

  Figure 05-51-44-991-00100-B – Inlet Cowl: Engine Interface and Rear Bulkheadp. 659

  Figure 05-51-44-991-00200-B – Fan Cowl Doors: Hinge and Latch Fittingsp. 660

  Figure 05-51-44-991-00300-B – Thrust Reverser: Hinge Fittingsp. 661

  Figure 05-51-44-991-00400-B – Thrust Reverser: Latch Fittingsp. 662

  Figure 05-51-44-991-00600-A – Common Nozzle Assembly: Engine Interfacep. 664

  +05-53 – PRESSURIZATION TEST OF FUSELAGE (LEAKAGE CHECKS) AFTER A/C ABNORMAL OPERATION OR REPAIRp. 665

  +05-53-00 – PRESSURIZATION TEST OF FUSELAGE (LEAKAGE CHECKS) AFTER A/C ABNORMAL OPERATION OR REPAIRp. 665

  +05-53-00 PB 501 CONF 00 – PRESSURIZATION TEST OF FUSELAGE (LEAKAGE CHECKS) AFTER A/C ABNORMAL OPERATION OR REPAIR – ADJUSTMENT/TESTp. 665

  05-53-00-780-001-A – Test for Leakage in the Repair Area at a Differential Pressure of 280 mbar (4.06 psi)p. 665

  05-53-00-780-001-A-01 – Test for Leakage in the Repair Area at a Differential Pressure of 280 mbar (4.06 psi) (with AIDS)p. 670

  05-53-00-780-002-A – Test for Leakage in the Repair Area at a Differential Pressure of 550 mbar (7.97 psi)p. 675

  05-53-00-780-002-A-01 – Test for Leakage in the Repair Area at a Differential Pressure of 550 mbar (7.97 psi) (with AIDS)p. 681

  05-53-00-780-003-A – Test to Measure the Structural Leakagep. 687

  05-53-00-780-003-A-01 – Test to Measure the Structural Leakage (with AIDS)p. 693

  +05-54 – DEMAGNETIZATIONp. 699

  +05-54-00 – DEMAGNETIZATIONp. 699

  +05-54-00 PB 201 CONF 00 – DEMAGNETIZATION – MAINTENANCE PRACTICESp. 699

  05-54-00-860-001-A – Demagnetization of the External Parts of the Frames of the Windshield and Sliding Windowsp. 699

  +05-56 – LEVELING AND MEASUREMENT AFTER A/C ABNORMAL OPERATIONp. 701

  +05-56-00 – LEVELING AND MEASUREMENT AFTER A/C ABNORMAL OPERATIONp. 701

  +05-56-00 PB 601 CONF 00 – LEVELING AND MEASUREMENT AFTER A/C ABNORMAL OPERATION – INSPECTION/CHECKp. 701

  +05-56-00-200-001-A – Inspection/Check of the Leveling and Measurement after Abnormal Operation of the Aircraftp. 701

  Figure 05-56-00-991-00100-A – Datump. 709

  Figure 05-56-00-991-00200-A – Position of the Datum Points on the Fuselagep. 710

  Figure 05-56-00-991-00300-A – Table 1 (Dimensions in Millimeters / Inches)p. 711

  Figure 05-56-00-991-00500-A – Table 2 (Dimensions in Millimeters / Inches)p. 712

  Figure 05-56-00-991-00700-A – Check of the Z Variations of the Bottom Wing Points and the Bottom Fuselage Pointsp. 713

  Figure 05-56-00-991-00800-A – Measurement of the X, Y and Z Position of the Bottom Fuselage Pointsp. 714

  Figure 05-56-00-991-00900-A – Z Values of the Horizontal Datum Points of the Fuselagep. 715

  Figure 05-56-00-991-01000-A – Measurement of the Wing Points and the Horizontal Stabilizer Pointsp. 716

  Figure 05-56-00-991-01100-A – Angular Values of the Wing Points and the Horizontal Stabilizer Pointsp. 717

  Figure 05-56-00-991-01200-B – Verticality Check of the Vertical Stabilizerp. 718

  Figure 05-56-00-991-01300-A – X Position of the Point 32Lp. 719

  Figure 05-56-00-991-01400-A – XY Values of the Engine Pylonsp. 720

  Figure 05-56-00-991-01500-D – X and Y Positions of the Landing Gearsp. 721

  Figure 05-56-00-991-01600-A – Symmetry of the Main Landing Gearsp. 722

  +05-56-00-200-002-A – Preparation for Measurement of the Aircraftp. 723

  Figure 05-56-00-991-02000-A – Location of the Measurement Points on the Wingsp. 726

  Figure 05-56-00-991-01700-A – Location of the Measurement Points on the Fuselagep. 727

  Figure 05-56-00-991-01800-A – Location of the Measurement Points on the Vertical Stabilizer and THSp. 728

  Figure 05-56-00-991-01900-A – Location of the Measurement Points on the Engine Pylonsp. 729

  Figure 05-56-00-991-02100-A – Location of the Measurement Points on the Landing Gearsp. 730

  +05-57 – AIRCRAFT STABILITYp. 731

  +05-57-00 – AIRCRAFT STABILITYp. 731

  +05-57-00 PB 201 CONF 00 – AIRCRAFT STABILITY – MAINTENANCE PRACTICESp. 731

  +05-57-00-200-001-A – Aircraft Stabilityp. 731

  Figure 05-57-00-991-02500-A – Aircraft on its Wheels (on Dry Ground) (Applicable to a parked or towed aircraft).p. 734

  Figure 05-57-00-991-02600-A – Aircraft on its Wheels (on Wet Ground) (applicable to a parked or towed aircraft)p. 735

  Figure 05-57-00-991-02700-A – Aircraft on Jacksp. 736

  Figure 05-57-00-991-02800-A – Aircraft on Forward Jack or on Nose Wheel Jackp. 737

  Figure 05-57-00-991-02900-A – Aircraft on one Main Gear Wheel Jackp. 738

  Figure 05-57-00-991-03000-A – Aircraft Jacked at Main and Nose Gears for Wheel Changep. 739

  Figure 05-57-00-991-03100-A – Aircraft on its Wheels (on Ice Ground)p. 740

  +05-59 – NON-REVENUE FLIGHT – REQUIREMENTS FOLLOWING MAINTENANCE ACTIONSp. 741

  +05-59-00 – NON-REVENUE FLIGHT – REQUIREMENTS FOLLOWING MAINTENANCE ACTIONSp. 741

  +05-59-00 PB 001 CONF 00 – NON-REVENUE FLIGHT – REQUIREMENTS FOLLOWING MAINTENANCE ACTIONS – DESCRIPTION AND OPERATIONp. 741

  Generalp. 741

  Engine Replacementp. 742

  +05-59-32 – FERRY FLIGHT WITH GEAR DOWNp. 743

  +05-59-32 PB 201 CONF 00 – FERRY FLIGHT WITH GEAR DOWN – MAINTENANCE PRACTICESp. 743

  05-59-32-869-001-A – Preparation for Flight with Gear Downp. 743

  05-59-32-869-002-A – Return to Normal Operation after a Flight with Gear Downp. 745

  Chapter 06 – DIMENSIONS AND AREAS

  Chapter 07 – LIFTING AND SHORING

  Chapter 08 – LEVELING AND WEIGHING

  Chapter 09 – TOWING AND TAXIING

  Chapter 10 – PARKING, MOORING, STORAGE & RETURN TO SERVICE

  Chapter 11 – PLACARDS AND MARKINGS

  Chapter 12 – SERVICING

  Chapter 20 – STANDARD PRACTICES – AIRFRAME

  Chapter 21 – AIR CONDITIONING

  Chapter 22 – AUTO FLIGHT

  Chapter 23 – COMMUNICATIONS

  Chapter 24 – ELECTRICAL POWER

  Chapter 25 – EQUIPMENT/FURNISHINGS

  Chapter 26 – FIRE PROTECTION

  Chapter 27 – FLIGHT CONTROLS

  Chapter 28 – FUEL

  Chapter 29 – HYDRAULIC POWER

  Chapter 30 – ICE AND RAIN PROTECTION

  Chapter 31 – INDICATING/RECORDING SYSTEMS

  Chapter 32 – LANDING GEAR

  Chapter 33 – LIGHTS

  Chapter 34 – NAVIGATION

  Chapter 35 – OXYGEN

  Chapter 36 – PNEUMATIC

  Chapter 38 – WATER/WASTE

  Chapter 46 – INFORMATION SYSTEMS

  Chapter 49 – AIRBORNE AUXILIARY POWER

  Chapter 51 – STANDARDS PRACTICES AND STRUCTURES

  Chapter 52 – DOORS

  Chapter 53 – FUSELAGE

  Chapter 54 – NACELLES/PYLONS

  Chapter 55 – STABILIZERS

  Chapter 56 – WINDOWS

  Chapter 57 – WINGS

  Chapter 70 – (IAE) – STANDARD PRACTICES – ENGINE

  Chapter 71 – (IAE) – POWER PLANT

  Chapter 72 – (IAE) – ENGINE

  Chapter 73 – (IAE) – ENGINE FUEL AND CONTROL

  Chapter 74 – (IAE) – IGNITION

  Chapter 75 – (IAE) – AIR

  Chapter 76 – (IAE) – ENGINE CONTROLS

  Chapter 77 – (IAE) – ENGINE INDICATING

  Chapter 78 – (IAE) – EXHAUST

  Chapter 79 – (IAE) – OIL

  Chapter 80 – (IAE) – STARTING

• 05-51-00 – Inspections
  • Hard/hard overweight landing
  • Landing-gear-down limiting-speed exceedance
  • Flap/slat limiting-speed exceedance
  • Bird or hail strike
  • Tire burst, tread throw or wheel failure
  • Brake emergency application or overheat
  • Excessive turbulence or VMO/MMO exceedance
  • Lightning strike
  • Engine bird strike or slush ingestion
  • Tail runway impact
  • NLG towing overload or overrun
  • NLG steering angle greater than 95 degrees
  • Leaving runway or taxiway
  • Dust storm or volcanic ash conditions
  • Engine failure
  • Impact on engine cowls
  • Fluid spillage
  • Abnormal passenger/crew door movement
  • Significant MLG vibration at touchdown
  • Engine windmilling after in-flight shutdown
  • Impact on wing tip/fence
  • Overweight taxiing
  • Very high winds on ground
  • Inspection after work on system electrical installation
  • Flight with high lateral loads
• 05-53-00 – Pressurization Test of Fuselage
  • Leakage checks after abnormal operation or repair
• 05-54-00 – Demagnetization
  • Windshield and sliding-window frame external parts
• 05-56-00 – Leveling and Measurement After Aircraft Abnormal Operation
  • Aircraft datum, fuselage, wing, stabilizer, pylon and landing-gear measurement points
• 05-57-00 – Aircraft Stability
  • Stability conditions on wheels and in multiple jacking configurations
• 05-59-00 – Non-Revenue Flight Requirements Following Maintenance Actions
  • Ferry flight with gear down; preparation and return to normal operation

Taken as a whole, the manual provides a detailed Chapter 05 reference for routine zonal inspection work and for the much less routine situations in which an aircraft must be evaluated after an abnormal operating event. It combines defined inspection areas with task-by-task procedures, phased inspection tables, damage checks, system references, supporting figures, measurement instructions and aircraft-restoration steps.

Use This Manual for Correct Chapter 05 Inspection Procedures

The Airbus A318 A319 A320 A321 Chapter 05 Time Limits & Maintenance Checks Manual PDF – Rev 40 2012 supports technicians carrying out scheduled zonal inspections, abnormal-event inspections, structural and landing-gear checks, leakage testing, aircraft leveling and measurement work, stability evaluation and maintenance-related ferry-flight preparation. Using the specified inspection sequence, criteria, figures and task references helps ensure that checks are performed against the procedures and values contained in this revision rather than relying on incomplete general guidance. The manual is supplied as an instant PDF download after purchase, with no physical shipping required. It can be opened on compatible computers, tablets and phones and printed when a paper working copy is preferred.