Description
Airbus A318/A319/A320/A321 Chapter 05 Time Limits and Maintenance Checks Manual
This is the complete Chapter 05 – Time Limits and Maintenance Checks section of the Airbus A318/A319/A320/A321 Aircraft Maintenance Manual (AMM), identified by the reference code KNA, Revision 12, dated November 1, 2011. This Airbus A318 A319 A320 A321 Chapter 05 Time Limits Maintenance Checks Manual is delivered as an instant-download PDF running 698 pages, giving maintenance personnel the full zonal inspection program and event-driven inspection procedures for this aircraft family in one reference.
- Manual type: Aircraft Maintenance Manual (AMM) – Chapter 05
- Aircraft: Airbus A318, A319, A320, A321
- Document reference: KNA
- Revision: 12
- Revision date: November 1, 2011 (Nov 01/11)
- Language: English
- Page count: 698 pages
- File format: PDF
Chapters Covered
- 05-00-00 Time Limits – Maintenance Checks – General – Description and Operation
- 05-20-00 Scheduled Maintenance Checks – Description and Operation
- 05-21-00 Zonal Inspection: Lower Half of Fuselage
- 05-21-10 Zonal Inspection: Radome
- 05-21-20 Zonal Inspection: Avionics Compartment
- 05-21-30 Zonal Inspection: Forward Cargo Compartment
- 05-21-40 Zonal Inspection: Center Wing
- 05-21-50 Zonal Inspection: Aft Cargo Compartment
- 05-21-60 Zonal Inspection: Bulk Cargo Compartment
- 05-21-70 Zonal Inspection: Aft Cabin Underfloor Compartment
- 05-21-90 Zonal Inspection: Belly Fairing, Air Conditioning and Hydraulics Compartments
- 05-22-00 Zonal Inspection: Upper Half of Fuselage
- 05-22-10 Zonal Inspection: Cockpit
- 05-22-20 Zonal Inspection: Forward Cabin Utility Areas
- 05-22-30 Zonal Inspection: Forward Passenger Compartment
- 05-22-40 Zonal Inspection: Mid Passenger Compartment
- 05-22-50 Zonal Inspection: Aft Passenger Compartment
- 05-22-60 Zonal Inspection: Aft Cabin Utility Area
- 05-23-00 Zonal Inspection: Stabilizers and Cone/Rear Fuselage
- 05-23-10 Zonal Inspection: Fuselage Tail Section Aft of Aft Pressure Bulkhead
- 05-23-20 Zonal Inspection: Vertical Stabilizer and Rudder
- 05-23-30 Zonal Inspection: Trimmable Horizontal Stabilizer and Elevator
- 05-24-00 Zonal Inspection: Power Plant, Nacelles and Pylons
- 05-24-10 Zonal Inspection: Engine Pylon Box and Forward Fairing
- 05-24-30 Zonal Inspection: Engine Air Intake, Fan and Accessory Gearbox
- 05-24-50 Zonal Inspection: Engine Thrust Reverser and Exhaust Section
- 05-24-70 Zonal Inspection: Engine Aft Pylon
- 05-25-00 Zonal Inspection: Wing
- 05-25-20 Zonal Inspection: Wing Fixed Leading Edge
- 05-25-30 Zonal Inspection: Wing Flap Track Fairings and Wing Tip
- 05-25-40 Zonal Inspection: Wing Fuel Tank
- 05-25-50 Zonal Inspection: Wing Vent Surge Tank
- 05-25-60 Zonal Inspection: Wing Dry Bay (Outboard)
- 05-25-70 Zonal Inspection: Aft Section of Wing and Trailing Edge Fixed Structure
- 05-25-90 Zonal Inspection: Wing Aileron
- 05-27-00 Zonal Inspection: Landing Gear and Landing Gear Doors
- 05-27-10 Zonal Inspection: Nose Gear and Doors
- 05-27-30 Zonal Inspection: Main Landing Gear and Doors
- 05-28-00 Zonal Inspection: Doors
- 05-28-10 Zonal Inspection: Avionics Compartment Doors (Forward and Lateral)
- 05-28-20 Zonal Inspection: Avionics/Cargo Compartment Doors (Right Side)
- 05-28-30 Zonal Inspection: Passenger/Crew Doors and Emergency Exits
- 05-50-00 Unscheduled Maintenance Checks – Description and Operation, Fluid Leak Measurement, Quick Dispatch Guide and Cross-References
- 05-51-00 Inspections – Description and Operation, Inspection Form
- 05-51-11 Inspection After Hard/Overweight Landing
- 05-51-12 Inspection After Landing Gear Down Limiting Speed Exceeded
- 05-51-13 Inspection After Flap/Slat Limiting Speed Exceeded
- 05-51-14 Inspection of Airframe After Bird or Hail Strike
- 05-51-15 Inspection After a Tire Burst or Tread Throw or Wheel Failure
- 05-51-16 Inspection After Brake Emergency Application or Overheat
- 05-51-17 Inspection After Flight in Excessive Turbulence or in Excess of VMO/MMO
- 05-51-18 Inspection After Lightning Strike
- 05-51-19 Inspection After Engine Bird Strike or Slush Ingestion
- 05-51-21 Inspection After Tail Runway Impact
- 05-51-22 Inspection After NLG Towing Overload or Overrun
- 05-51-23 Inspection After NLG Steering Angle Exceeded
- 05-51-24 Inspection After Leaving Runway or Taxiway
- 05-51-25 Inspection After Dust Storm/Volcanic Ash Conditions
- 05-51-26 Inspection After Engine Failure
- 05-51-27 Inspection After Impact on Engine Cowls
- 05-51-28 Procedure After Fluid Spillage
- 05-51-29 Inspection After Abnormal Pax/Crew Door Movement
- 05-51-31 Inspection After Significant MLG Vibration at Touch-Down
- 05-51-34 Inspection After Engine Windmilling
- 05-51-35 Inspection After Impact on Wing Tip/Fence
- 05-51-41 Inspection After Overweight Taxiing
- 05-51-42 Inspection After Very High Winds on Ground
- 05-51-43 Inspections After Work on System Electrical Installation
- 05-51-44 Inspection After Flight With High Lateral Loads
- 05-51-45 Inspection After Flight in Severe Icing Conditions
- 05-53-00 Pressurization Test of Fuselage (Leakage Checks) After Abnormal Operation or Repair
- 05-54-00 Demagnetization
- 05-56-00 Leveling and Measurement After A/C Abnormal Operation
- 05-57-00 Aircraft Stability
- 05-59-00/32 Non-Revenue Flight Requirements, Ferry Flight With Gear Down
Complete PDF Bookmark Tree
Complete Bookmarks
The complete bookmarks in the “Airbus A318 A319 A320 A321 Chapter 05 Time Limits Maintenance Checks Manual” 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
+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-D – Access Panels and Doors of the Left Nacelle (Left Side)p. 175
Figure 05-24-10-991-00200-D – Access Panels and Doors of the Left Nacelle (Right Side)p. 176
Figure 05-24-10-991-00300-D – Access Panels and Doors of the Right Nacelle (Left Side)p. 177
Figure 05-24-10-991-00400-D – 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-A – Access Doors of the Left Nacelle (Left Side)p. 183
Figure 05-24-30-991-00200-A – Access Doors of the Left Nacelle (Right Side)p. 184
Figure 05-24-30-991-00300-A – Access Doors of the Right Nacelle (Right Side)p. 185
Figure 05-24-30-991-00400-A – 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-A – Access Doors of the Left Nacelle (Left Side)p. 193
Figure 05-24-50-991-00200-A – Access Doors of the Left Nacelle (Right Side)p. 194
Figure 05-24-50-991-00300-A – Access Doors of the Right Nacelle (Left Side)p. 195
Figure 05-24-50-991-00400-A – Access Doors of the Right Nacelle (Right Side)p. 196
05-24-50-200-002-A – GENERAL VISUAL INSPECTION OF HOT SECTION (EWIS)p. 197
+05-24-70 – ZONAL INSPECTION : ENGINE AFT PYLONp. 199
+05-24-70 PB 601 CONF 00 – ZONAL INSPECTION : ENGINE AFT PYLON – INSPECTION/CHECKp. 199
+05-24-70-200-001-A – GENERAL VISUAL INSPECTION OF PYLON LEADING EDGE AND LOWER FAIRING (EWIS)p. 199
Figure 05-24-70-991-00100-E – Location of the Access Panels of the Left Nacelle (Left Side)p. 202
Figure 05-24-70-991-00200-E – Location of the Access Panels of the Left Nacelle (Right Side)p. 203
Figure 05-24-70-991-00500-E – Location of the Access Panels of the Right Nacelle (Left Side)p. 204
Figure 05-24-70-991-00600-E – Location of the Access Panels of the Right Nacelle (Right Side)p. 205
+05-25 – ZONAL INSPECTION : WINGp. 206
+05-25-00 – ZONAL INSPECTION : WINGp. 206
+05-25-00 PB 601 CONF 00 – ZONAL INSPECTION : WING – INSPECTION/CHECKp. 206
05-25-00-200-001-A – Zonal Inspection of the Wings as far as visible from the groundp. 206
05-25-00-200-002-A – GENERAL VISUAL INSPECTION OF WING LOWER SURFACE INCLUDING UPPER AND LOWER SURFACES OF SLATS AND FLAPS (EWIS)p. 207
05-25-00-200-003-A – GENERAL VISUAL INSPECTION OF WING UPPER SURFACE INCLUDING SLATS, FLAPS AND SPOILERS (EWIS)p. 209
+05-25-20 – ZONAL INSPECTION : WING FIXED LEADING EDGEp. 211
+05-25-20 PB 601 CONF 00 – ZONAL INSPECTION : WING FIXED LEADING EDGE – INSPECTION/CHECKp. 211
+05-25-20-200-001-A – GENERAL VISUAL INSPECTION OF INBOARD FIXED LEADING EDGE STRUCTURE (EWIS)p. 211
Figure 05-25-20-991-00100-A – Access Panels of the Upper Leading Edge of the Wingp. 213
Figure 05-25-20-991-00200-A – Access Panels of the Lower Surface of the Wingp. 214
05-25-20-200-002-A – GENERAL VISUAL INSPECTION OF OUTBOARD FIXED LEADING EDGE STRUCTURE (EWIS)p. 215
+05-25-30 – ZONAL INSPECTION : WING FLAP TRACK FAIRINGS AND WING TIPp. 217
+05-25-30 PB 601 CONF 00 – ZONAL INSPECTION : WING FLAP TRACK FAIRINGS AND WING TIP – INSPECTION/CHECKp. 217
+05-25-30-200-001-A – GENERAL VISUAL INSPECTION OF FLAP TRACK NO 2 AND FAIRING (EWIS)p. 217
Figure 05-25-30-991-00100-A – Access Panels of the Flap Track Fairingsp. 219
05-25-30-200-002-A – GENERAL VISUAL INSPECTION OF FLAP TRACK NO 3 AND FAIRING (EWIS)p. 220
05-25-30-200-003-A – GENERAL VISUAL INSPECTION OF FLAP TRACK NO 4 AND FAIRING (EWIS)p. 222
+05-25-30-200-004-A – GENERAL VISUAL INSPECTION OF WING TIP (EWIS)p. 224
Figure 05-25-30-991-00200-B – Access Panels of the Wing Tipp. 225
05-25-30-200-005-A – GENERAL VISUAL INSPECTION OF FLAP TRACK NO 2 AND FAIRING (EWIS)p. 226
05-25-30-200-006-A – GENERAL VISUAL INSPECTION OF FLAP TRACK NO 3 AND FAIRING (EWIS)p. 228
05-25-30-200-007-A – GENERAL VISUAL INSPECTION OF FLAP TRACK NO 4 AND FAIRING (EWIS)p. 230
+05-25-40 – ZONAL INSPECTION : WING FUEL TANKp. 232
+05-25-40 PB 601 CONF 00 – ZONAL INSPECTION : WING FUEL TANK – INSPECTION/CHECKp. 232
05-25-40-200-005-A – GENERAL VISUAL INSPECTION OF WING FUEL TANK (EWIS)p. 232
05-25-40-200-004-A – GENERAL VISUAL INSPECTION OF WING FUEL TANK (EWIS)p. 234
+05-25-50 – ZONAL INSPECTION : WING VENT SURGE TANKp. 236
+05-25-50 PB 601 CONF 00 – ZONAL INSPECTION : WING VENT SURGE TANK – INSPECTION/CHECKp. 236
+05-25-50-200-001-A – GENERAL VISUAL INSPECTION OF VENT SURGE TANK (EWIS)p. 236
Figure 05-25-50-991-00100-A – Access Panels of the Vent Surge Tank of the Wingp. 238
+05-25-60 – ZONAL INSPECTION : WING DRY BAY (OUTBOARD)p. 239
+05-25-60 PB 601 CONF 00 – ZONAL INSPECTION : WING DRY BAY (OUTBOARD) – INSPECTION/CHECKp. 239
05-25-60-200-001-A – GENERAL VISUAL INSPECTION OF DRY BAY (OUTBOARD) (EWIS)p. 239
+05-25-70 – ZONAL INSPECTION : AFT SECTION OF WING AND TRAILING EDGE FIXED STRUCTUREp. 241
+05-25-70 PB 601 CONF 00 – ZONAL INSPECTION : AFT SECTION OF WING AND TRAILING EDGE FIXED STRUCTURE – INSPECTION/CHECKp. 241
05-25-70-200-001-A – Zonal Inspection as far as visible of the Main Landing Gear Bayp. 241
+05-25-70-200-002-A – GENERAL VISUAL INSPECTION OF SHROUD BOX (EWIS)p. 242
Figure 05-25-70-991-00100-B – Access Panels of the Left Wing Lower Trailing Edgep. 244
Figure 05-25-70-991-00300-B – Access Panels of the Right Wing Lower Trailing Edgep. 245
05-25-70-200-003-A – GENERAL VISUAL INSPECTION OF INBOARD FIXED TRAILING EDGE STRUCTURE FROM SHROUD BOX TO RIB 9 (EWIS)p. 246
05-25-70-200-004-A – GENERAL VISUAL INSPECTION OF FALSE SPAR BOX (EWIS)p. 248
05-25-70-200-005-A – GENERAL VISUAL INSPECTION OF OUTBOARD FIXED TRAILING EDGE STRUCTURE FROM RIB 9 TO RIB 27 (EWIS)p. 250
05-25-70-200-006-A – GENERAL VISUAL INSPECTION OF MLG BAY (EWIS)p. 252
+05-25-90 – ZONAL INSPECTION : WING AILERONp. 254
+05-25-90 PB 601 CONF 00 – ZONAL INSPECTION : WING AILERON – INSPECTION/CHECKp. 254
+05-25-90-200-001-A – GENERAL VISUAL INSPECTION OF AILERON (EWIS)p. 254
Figure 05-25-90-991-00100-A – Access Panels of the Wing Aileronp. 256
+05-27 – ZONAL INSPECTION : LANDING GEAR AND LANDING GEAR DOORSp. 257
+05-27-00 – ZONAL INSPECTION : LANDING GEAR AND LANDING GEAR DOORSp. 257
+05-27-00 PB 601 CONF 00 – ZONAL INSPECTION : LANDING GEAR AND LANDING GEAR DOORS – INSPECTION/CHECKp. 257
05-27-00-200-001-A – Zonal Inspection as far as Visible from the Ground of the Landing Gear and the Landing Gear Doorsp. 257
+05-27-10 – ZONAL INSPECTION : NOSE GEAR AND DOORSp. 258
+05-27-10 PB 601 CONF 00 – ZONAL INSPECTION : NOSE GEAR AND DOORS – INSPECTION/CHECKp. 258
05-27-10-200-001-A – GENERAL VISUAL INSPECTION OF NOSE GEAR AND NOSE GEAR DOORS (EWIS)p. 258
+05-27-30 – ZONAL INSPECTION : MAIN LANDING GEAR AND DOORSp. 260
+05-27-30 PB 601 CONF 00 – ZONAL INSPECTION : MAIN LANDING GEAR AND DOORS – INSPECTION/CHECKp. 260
05-27-30-200-001-A – GENERAL VISUAL INSPECTION OF LH/RH MAIN LANDING GEAR (EWIS)p. 260
+05-27-30-200-002-A – GENERAL VISUAL INSPECTION OF MAIN LANDING GEAR CYLINDER DOOR (EWIS)p. 261
Figure 05-27-30-991-00100-A – Main Landing Gear and Doorsp. 262
05-27-30-200-003-A – GENERAL VISUAL INSPECTION OF MAIN LANDING GEAR SECONDARY DOOR (EWIS)p. 263
05-27-30-200-004-A – GENERAL VISUAL INSPECTION OF MAIN LANDING GEAR MAIN DOORS (EWIS)p. 264
+05-28 – ZONAL INSPECTION : DOORSp. 265
+05-28-00 – ZONAL INSPECTION : DOORSp. 265
+05-28-00 PB 601 CONF 00 – ZONAL INSPECTION : DOORS – INSPECTION/CHECKp. 265
05-28-00-200-001-A – Zonal Inspection of the Doors as far as Visible from the Groundp. 265
+05-28-10 – ZONAL INSPECTION : AVIONICS COMPARTMENT DOORS (FORWARD AND LATERAL)p. 266
+05-28-10 PB 601 CONF 00 – ZONAL INSPECTION : AVIONICS COMPARTMENT DOORS (FORWARD AND LATERAL) – INSPECTION/CHECKp. 266
+05-28-10-200-001-A – GENERAL VISUAL INSPECTION OF FWD AVIONICS COMPARTMENT DOOR (EWIS) (INCLUDING EXTERNAL SURFACE)p. 266
Figure 05-28-10-991-00100-A – Avionics Compartment Left Side Door and Forward Doorp. 268
05-28-10-200-002-A – GENERAL VISUAL INSPECTION OF FWD AVIONICS COMPARTMENT DOOR (EWIS)p. 269
+05-28-10-200-003-A – GENERAL VISUAL INSPECTION OF LATERAL AVIONICS COMPARTMENT DOORS (EWIS) (INCLUDING EXTERNAL SURFACE)p. 271
Figure 05-28-10-991-00200-A – Avionics Compartment Right Side Doorp. 273
05-28-10-200-004-A – GENERAL VISUAL INSPECTION OF LATERAL AVIONICS COMPARTMENT DOORS (EWIS)p. 274
+05-28-20 – ZONAL INSPECTION : AVIONICS COMPARTMENT DOORS, CARGO COMPARTMENT DOORS (RIGHT SIDE)p. 276
+05-28-20 PB 601 CONF 00 – ZONAL INSPECTION : AVIONICS COMPARTMENT DOORS, CARGO COMPARTMENT DOORS (RIGHT SIDE) – INSPECTION/CHECKp. 276
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. 276
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. 278
05-28-20-200-003-A – GENERAL VISUAL INSPECTION OF BULK CARGO COMPARTMENT DOOR INCLUDING DOOR STOPS ON FUSELAGE DOOR FRAME (EWIS)p. 280
+05-28-20-200-004-A – GENERAL VISUAL INSPECTION OF FWD CARGO COMPARTMENT DOOR (EWIS)p. 281
Figure 05-28-20-991-00100-A – Access Panels of the Cargo Compartment Doorsp. 283
05-28-20-200-005-A – GENERAL VISUAL INSPECTION OF AFT CARGO COMPARTMENT DOOR (EWIS)p. 284
05-28-20-200-006-A – GENERAL VISUAL INSPECTION OF BULK CARGO COMPARTMENT DOOR INCLUDING DOOR STOPS ON FUSELAGE DOOR FRAME (EWIS)p. 286
+05-28-20-200-007-A – GENERAL VISUAL INSPECTION OF REAR AVIONIC COMPARTMENT DOOR (EWIS) (INCLUDING EXTERNAL SURFACE)p. 287
Figure 05-28-20-991-00200-A – Rear Avionics Compartment Doorp. 289
05-28-20-200-008-A – GENERAL VISUAL INSPECTION OF REAR AVIONIC COMPARTMENT DOOR (EWIS)p. 290
+05-28-30 – ZONAL INSPECTION : PASSENGER/CREW DOORS AND EMERGENCY EXITSp. 292
+05-28-30 PB 601 CONF 00 – ZONAL INSPECTION : PASSENGER/CREW DOORS AND EMERGENCY EXITS – INSPECTION/CHECKp. 292
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. 292
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. 294
05-28-30-200-005-A – GENERAL VISUAL INSPECTION OF FWD AND AFT PASSENGER/CREW DOORS (EWIS)p. 296
05-28-30-200-007-A – GENERAL VISUAL INSPECTION OF FWD AND AFT EMERGENCY EXITS (EWIS)p. 298
+05-50 – UNSCHEDULED MAINTENANCE CHECKSp. 300
+05-50-00 – UNSCHEDULED MAINTENANCE CHECKSp. 300
+05-50-00 PB 001 CONF 00 – UNSCHEDULED MAINTENANCE CHECKS – DESCRIPTION AND OPERATIONp. 300
+05-50-00 PB 201 CONF 00 – UNSCHEDULED MAINTENANCE CHECKS – MAINTENANCE PRACTICESp. 301
05-50-00-790-001-A – Fluid Leak Measurement – Maintenance Practicesp. 301
+05-50-00-040-002-A – Quick Dispatch Guide and Cross-Referencesp. 302
Figure 05-50-00-991-00200-A – Location of the Antennas, Probes and sensors and Exterior lightsp. 310
+05-51 – INSPECTIONSp. 312
+05-51-00 – INSPECTIONSp. 312
+05-51-00 PB 001 CONF 00 – INSPECTIONS – DESCRIPTION AND OPERATIONp. 312
Generalp. 312
Figure 05-51-00-12100-A – Inspection Formp. 314
+05-51-11 – INSPECTIONS AFTER HARD/OVERWEIGHT LANDINGp. 315
+05-51-11 PB 601 CONF 00 – INSPECTIONS AFTER HARD/OVERWEIGHT LANDING – INSPECTION/CHECKp. 315
+05-51-11-200-004-B – Inspection After Hard/Hard Overweight Landing for Aircraft with Enhanced DMU/FDIMU Load Report 15p. 315
Figure 05-51-11-991-01500-A – Hard/Hard Overweight landing criteria for Enhanced DMU/FDIMU Load Report 15p. 345
Figure 05-51-11-991-01600-A – Inspection Flow Chartp. 346
Figure 05-51-11-991-01000-A – Nose Landing Gearp. 347
Figure 05-51-11-991-02300-A – Main Landing Gear Legp. 348
Figure 05-51-11-991-02400-A – Illustration of the Main Landing Gearp. 349
Figure 05-51-11-991-02500-A – Inlet Cowl: Engine Interface and Rear Bulkheadp. 350
Figure 05-51-11-991-02600-A – Fan Cowl Doors: Hinge and Latch Fittingsp. 351
Figure 05-51-11-991-02700-A – Thrust Reverser: Hinge Fittingsp. 352
Figure 05-51-11-991-02800-A – Thrust Reverser: Latch Fittingsp. 353
Figure 05-51-11-991-02900-A – Exhaust Nozzle: Engine Interfacep. 356
Figure 05-51-11-991-00700-A – Primary Structure – Materials and Protections Descriptionp. 357
Figure 05-51-11-991-00800-A – Engine-to-Pylon Attach Fittingsp. 358
Figure 05-51-11-991-00900-A – Pylon-to-Wing Attach Fittingsp. 359
Figure 05-51-11-991-01200-A – Lower Part of the Center Fuselagep. 360
Figure 05-51-11-991-01300-A – Center Sectionp. 361
Figure 05-51-11-991-01400-A – Component Location in the Belly Fairing Structurep. 362
Figure 05-51-11-991-01100-A – Main Structure of the Cone/Rear Fuselagep. 363
+05-51-12 – INSPECTION AFTER LANDING GEAR DOWN LIMITING SPEED EXCEEDEDp. 364
+05-51-12 PB 601 CONF 00 – INSPECTION AFTER LANDING GEAR DOWN LIMITING SPEED EXCEEDED – INSPECTION/CHECKp. 364
+05-51-12-200-001-A – Inspection after Landing Gear Extension at more than the Geardown Limiting Speedp. 364
Figure 05-51-12-991-00100-A – Lower Part of the Center Fuselagep. 374
Figure 05-51-12-991-00200-A – Center Sectionp. 375
Figure 05-51-12-991-00300-A – Component Location in the Belly Fairing Structurep. 376
Figure 05-51-12-991-00400-A – Main Gear Assemblyp. 377
Figure 05-51-12-991-00500-A – Inspection on the Wingp. 378
Figure 05-51-12-991-00600-A – Inspection on the Wingp. 379
+05-51-13 – INSPECTION AFTER FLAP/SLAT LIMITING SPEED EXCEEDEDp. 380
+05-51-13 PB 601 CONF 00 – INSPECTION AFTER FLAP/SLAT LIMITING SPEED EXCEEDED – INSPECTION/CHECKp. 380
+05-51-13-200-001-A – Inspection after Flap/Slat Extension at more than the Flap/Slat Limiting Speedp. 380
Figure 05-51-13-991-00100-A – Component Location of the Flap Systemp. 388
Figure 05-51-13-991-00200-A – Flap Componentsp. 389
Figure 05-51-13-991-00500-A – Track No. 1 Actuatorp. 390
Figure 05-51-13-991-00600-A – Typical Installation of the Actuatorp. 391
Figure 05-51-13-991-00400-A – Component Location of the Slat Systemp. 392
Figure 05-51-13-991-00300-A – Slat Componentsp. 393
+05-51-14 – INSPECTION OF AIRFRAME AFTER BIRD OR HAIL STRIKEp. 394
+05-51-14 PB 601 CONF 00 – INSPECTION OF AIRFRAME AFTER BIRD OR HAIL STRIKE – INSPECTION/CHECKp. 394
05-51-14-200-001-A – Inspection of the Airframe after a Bird or Hail Strike in Flightp. 394
05-51-14-200-002-A – Inspection of the Airframe after a Hail Strike on Groundp. 405
+05-51-15 – INSPECTION AFTER A TIRE BURST OR TREAD THROW OR WHEEL FAILUREp. 414
+05-51-15 PB 601 CONF 00 – INSPECTION AFTER A TIRE BURST OR TREAD THROW OR WHEEL FAILURE – INSPECTION/CHECKp. 414
05-51-15-200-001-A – Inspection after a Tire Burst or Tread Throw or Wheel Failurep. 414
+05-51-16 – INSPECTION AFTER BRAKE EMERGENCY APPLICATION OR OVERHEATp. 423
+05-51-16 PB 601 CONF 00 – INSPECTION AFTER BRAKE EMERGENCY APPLICATION OR OVERHEAT – INSPECTION/CHECKp. 423
05-51-16-200-001-A – Inspection After Brake Emergency Application or Overheatp. 423
+05-51-17 – INSPECTION AFTER FLIGHT IN EXCESSIVE TURBULENCE OR IN EXCESS OF VMO/MMOp. 428
+05-51-17 PB 601 CONF 00 – INSPECTION AFTER FLIGHT IN EXCESSIVE TURBULENCE OR IN EXCESS OF VMO/MMO – INSPECTION/CHECKp. 428
+05-51-17-200-001-A – Inspection after in Flight Excessive Load Factor due to Turbulence or Maneuver or in Excess of VMO/MMOp. 428
Figure 05-51-17-991-00700-A – Flow chartp. 442
Figure 05-51-17-991-00100-A – Inlet Cowl: Engine Interface and Rear Bulkheadp. 444
Figure 05-51-17-991-00200-A – Fan Cowl Doors: Hinge and Latch Fittingsp. 445
Figure 05-51-17-991-00300-A – Thrust Reverser: Hinge Fittingsp. 446
Figure 05-51-17-991-00400-A – Thrust Reverser: Latch Fittingsp. 447
Figure 05-51-17-991-00500-A – Exhaust Nozzle: Engine Interfacep. 450
+05-51-18 – INSPECTION AFTER LIGHTNING STRIKEp. 451
+05-51-18 PB 601 CONF 00 – INSPECTION AFTER LIGHTNING STRIKE – INSPECTION/CHECKp. 451
+05-51-18-200-001-A – Inspection after Lightning Strikep. 451
Figure 05-51-18-991-00100-A – Lightning Strike Inspection Areasp. 477
Figure 05-51-18-991-00200-A – Location of the Antennas, Probes and Sensors and Exterior Lightsp. 478
+05-51-19 – INSPECTION AFTER ENGINE BIRD STRIKE OR SLUSH INGESTIONp. 480
+05-51-19 PB 601 CONF 00 – INSPECTION AFTER ENGINE BIRD STRIKE OR SLUSH INGESTION – INSPECTION/CHECKp. 480
05-51-19-200-001-A – Inspection of the Engine after a Bird Strike or Slush Ingestionp. 480
+05-51-21 – INSPECTION AFTER TAIL RUNWAY IMPACTp. 481
+05-51-21 PB 601 CONF 00 – INSPECTION AFTER TAIL RUNWAY IMPACT – INSPECTION/CHECKp. 481
+05-51-21-200-001-A – Inspection after a Tail Runway Impactp. 481
Figure 05-51-21-991-00100-A – Tailcone Equipment (L Side)p. 484
Figure 05-51-21-991-00200-A – APU Installation (R side)p. 485
+05-51-22 – INSPECTION AFTER NLG TOWING OVERLOAD OR OVERRUNp. 486
+05-51-22 PB 601 CONF 00 – INSPECTION AFTER NLG TOWING OVERLOAD OR OVERRUN – INSPECTION/CHECKp. 486
+05-51-22-200-001-A – Inspection After a NLG Towing Overload or Overrunp. 486
Figure 05-51-22-991-00100-A – Nose Landing-Gear Wellp. 491
Figure 05-51-22-991-00200-A – Inspection of the NLG Steering Systemp. 492
+05-51-23 – INSPECTION AFTER NLG STEERING ANGLE EXCEEDEDp. 493
+05-51-23 PB 601 CONF 00 – INSPECTION AFTER NLG STEERING ANGLE EXCEEDED – INSPECTION/CHECKp. 493
+05-51-23-200-001-A – Inspection after NLG Steering Angle of more than 95 deg.p. 493
Figure 05-51-23-991-00100-A – Inspection of the Nose Landing Gearp. 497
+05-51-24 – INSPECTION AFTER LEAVING RUNWAY OR TAXIWAYp. 498
+05-51-24 PB 601 CONF 00 – INSPECTION AFTER LEAVING RUNWAY OR TAXIWAY – INSPECTION/CHECKp. 498
+05-51-24-200-001-A – Inspection after Leaving Runway or Taxiwayp. 498
Figure 05-51-24-991-00200-B – Engine Nacellep. 519
Figure 05-51-24-991-00300-B – Engine Mountsp. 520
Figure 05-51-24-991-00400-A – Access Doors of the Pylon Boxp. 521
+05-51-25 – INSPECTION AFTER DUST STORM/VOLCANIC ASH CONDITIONS IN FLIGHT OR ON THE GROUNDp. 522
+05-51-25 PB 601 CONF 00 – INSPECTION AFTER DUST STORM/VOLCANIC ASH CONDITIONS IN FLIGHT OR ON THE GROUND – INSPECTION/CHECKp. 522
05-51-25-200-002-A – Inspection after Flight through Dust Storm or Dust Contamination on Groundp. 522
05-51-25-200-003-A – Inspection after Flight through Volcanic Ash or Volcanic Ash Contamination on Groundp. 538
+05-51-26 – INSPECTION AFTER ENGINE FAILUREp. 557
+05-51-26 PB 601 CONF 00 – INSPECTION AFTER ENGINE FAILURE – INSPECTION/CHECKp. 557
05-51-26-200-001-A – INSPECTION AFTER ENGINE FAILUREp. 557
+05-51-27 – INSPECTION AFTER IMPACT ON ENGINE COWLSp. 562
+05-51-27 PB 601 CONF 00 – INSPECTION AFTER IMPACT ON ENGINE COWLS – INSPECTION/CHECKp. 562
05-51-27-200-001-A – Inspection after Impact on Engine Cowlsp. 562
+05-51-28 – PROCEDURE AFTER FLUID SPILLAGEp. 565
+05-51-28 PB 601 CONF 00 – PROCEDURE AFTER FLUID SPILLAGE – INSPECTION/CHECKp. 565
05-51-28-200-002-A – Procedure after Fluid Spillagep. 565
+05-51-29 – INSPECTION AFTER ABNORMAL PAX/CREW DOOR MOVEMENTp. 566
+05-51-29 PB 601 CONF 00 – INSPECTION AFTER ABNORMAL PAX/CREW DOOR MOVEMENT – INSPECTION/CHECKp. 566
+05-51-29-200-001-A – Inspection after Abnormal Movement of the Pax/Crew Doorp. 566
Figure 05-51-29-991-00100-A – Passenger/Crew Doorsp. 572
+05-51-31 – INSPECTION AFTER SIGNIFICANT MLG VIBRATION AT TOUCH-DOWNp. 573
+05-51-31 PB 601 CONF 00 – INSPECTION AFTER SIGNIFICANT MLG VIBRATION AT TOUCH-DOWN – INSPECTION/CHECKp. 573
+05-51-31-200-001-A – Inspection after Significant MLG Vibration at Touch-Downp. 573
Figure 05-51-31-991-00100-A – Bottom Cardan Joint – Clearancesp. 579
Figure 05-51-31-991-00200-A – Botton Cardan Joint- Clearencesp. 580
+05-51-34 – INSPECTION AFTER ENGINE WINDMILLING (AFTER ENGINE IN-FLIGHT SHUT-DOWN)p. 581
+05-51-34 PB 601 CONF 00 – INSPECTION AFTER ENGINE WINDMILLING (AFTER ENGINE IN-FLIGHT SHUT-DOWN) – INSPECTION/CHECKp. 581
05-51-34-200-001-A – Inspection after Engine Windmilling (After Engine In-Flight Shut-Down)p. 581
+05-51-35 – INSPECTION AFTER IMPACT ON WING TIP /FENCEp. 582
+05-51-35 PB 601 CONF 00 – INSPECTION AFTER IMPACT ON WING TIP /FENCE – INSPECTION/CHECKp. 582
+05-51-35-200-001-A – Inspection after Impact on Wing Tip/Fencep. 582
Figure 05-51-35-991-00100-A – Wing Tip and Wing Tip Fencep. 586
+05-51-41 – INSPECTION AFTER OVERWEIGHT TAXIINGp. 587
+05-51-41 PB 601 CONF 00 – INSPECTION AFTER OVERWEIGHT TAXIING – INSPECTION/CHECKp. 587
05-51-41-200-001-A – Inspection after Overweight Taxiingp. 587
+05-51-42 – INSPECTION AFTER VERY HIGH WINDS ON GROUNDp. 594
+05-51-42 PB 601 CONF 00 – INSPECTION AFTER VERY HIGH WINDS ON GROUND – INSPECTION/CHECKp. 594
05-51-42-200-001-A – Inspection after Very High Winds on Groundp. 594
+05-51-43 – INSPECTIONS AFTER WORK ON SYSTEM ELECTRICAL INSTALLATIONp. 599
+05-51-43 PB 501 CONF 00 – INSPECTIONS AFTER WORK ON SYSTEM ELECTRICAL INSTALLATION – ADJUSTMENT/TESTp. 599
05-51-43-700-001-A – Inspection after Work on System Electrical Installationp. 599
+05-51-44 – INSPECTION AFTER FLIGHT WITH HIGH LATERAL LOADSp. 603
+05-51-44 PB 601 CONF 00 – INSPECTION AFTER FLIGHT WITH HIGH LATERAL LOADS – INSPECTION/CHECKp. 603
+05-51-44-200-001-A – Inspection after Aircraft Operation with High Lateral Accelerationp. 603
Figure 05-51-44-991-00100-A – Inlet Cowl: Engine Interface and Rear Bulkheadp. 612
Figure 05-51-44-991-00200-A – Fan Cowl Doors: Hinge and Latch Fittingsp. 613
Figure 05-51-44-991-00300-A – Thrust Reverser: Hinge Fittingsp. 614
Figure 05-51-44-991-00400-A – Thrust Reverser: Latch Fittingsp. 615
Figure 05-51-44-991-00500-A – Exhaust Nozzle: Engine Interfacep. 618
+05-51-45 – INSPECTION AFTER FLIGHT IN SEVERE ICING CONDITIONSp. 619
+05-51-45 PB 601 CONF 00 – INSPECTION AFTER FLIGHT IN SEVERE ICING CONDITIONS – INSPECTION/CHECKp. 619
05-51-45-200-001-A – Inspection after Flight in Severe Icing Conditionsp. 619
+05-53 – PRESSURIZATION TEST OF FUSELAGE (LEAKAGE CHECKS) AFTER A/C ABNORMAL OPERATION OR REPAIRp. 620
+05-53-00 – PRESSURIZATION TEST OF FUSELAGE (LEAKAGE CHECKS) AFTER A/C ABNORMAL OPERATION OR REPAIRp. 620
+05-53-00 PB 501 CONF 00 – PRESSURIZATION TEST OF FUSELAGE (LEAKAGE CHECKS) AFTER A/C ABNORMAL OPERATION OR REPAIR – ADJUSTMENT/TESTp. 620
05-53-00-780-001-A – Test for Leakage in the Repair Area at a Differential Pressure of 280 mbar (4.06 psi)p. 620
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. 625
05-53-00-780-002-A – Test for Leakage in the Repair Area at a Differential Pressure of 550 mbar (7.97 psi)p. 630
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. 635
05-53-00-780-003-A – Test to Measure the Structural Leakagep. 640
05-53-00-780-003-A-01 – Test to Measure the Structural Leakage (with AIDS)p. 646
+05-54 – DEMAGNETIZATIONp. 652
+05-54-00 – DEMAGNETIZATIONp. 652
+05-54-00 PB 201 CONF 00 – DEMAGNETIZATION – MAINTENANCE PRACTICESp. 652
05-54-00-860-001-A – Demagnetization of the External Parts of the Frames of the Windshield and Sliding Windowsp. 652
+05-56 – LEVELING AND MEASUREMENT AFTER A/C ABNORMAL OPERATIONp. 654
+05-56-00 – LEVELING AND MEASUREMENT AFTER A/C ABNORMAL OPERATIONp. 654
+05-56-00 PB 601 CONF 00 – LEVELING AND MEASUREMENT AFTER A/C ABNORMAL OPERATION – INSPECTION/CHECKp. 654
+05-56-00-200-001-A – Inspection/Check of the Leveling and Measurement after Abnormal Operation of the Aircraftp. 654
Figure 05-56-00-991-00100-A – Datump. 662
Figure 05-56-00-991-00200-A – Position of the Datum Points on the Fuselagep. 663
Figure 05-56-00-991-00300-A – Table 1 (Dimensions in Millimeters / Inches)p. 664
Figure 05-56-00-991-00500-A – Table 2 (Dimensions in Millimeters / Inches)p. 665
Figure 05-56-00-991-00700-A – Check of the Z Variations of the Bottom Wing Points and the Bottom Fuselage Pointsp. 666
Figure 05-56-00-991-00800-A – Measurement of the X, Y and Z Position of the Bottom Fuselage Pointsp. 667
Figure 05-56-00-991-00900-A – Z Values of the Horizontal Datum Points of the Fuselagep. 668
Figure 05-56-00-991-01000-A – Measurement of the Wing Points and the Horizontal Stabilizer Pointsp. 669
Figure 05-56-00-991-01100-A – Angular Values of the Wing Points and the Horizontal Stabilizer Pointsp. 670
Figure 05-56-00-991-01200-B – Verticality Check of the Vertical Stabilizerp. 671
Figure 05-56-00-991-01300-A – X Position of the Point 32Lp. 672
Figure 05-56-00-991-01400-A – XY Values of the Engine Pylonsp. 673
Figure 05-56-00-991-01500-D – X and Y Positions of the Landing Gearsp. 674
Figure 05-56-00-991-01600-A – Symmetry of the Main Landing Gearsp. 675
+05-56-00-200-002-A – Preparation for Measurement of the Aircraftp. 676
Figure 05-56-00-991-02000-A – Location of the Measurement Points on the Wingsp. 679
Figure 05-56-00-991-01700-A – Location of the Measurement Points on the Fuselagep. 680
Figure 05-56-00-991-01800-A – Location of the Measurement Points on the Vertical Stabilizer and THSp. 681
Figure 05-56-00-991-01900-A – Location of the Measurement Points on the Engine Pylonsp. 682
Figure 05-56-00-991-02100-A – Location of the Measurement Points on the Landing Gearsp. 683
+05-57 – AIRCRAFT STABILITYp. 684
+05-57-00 – AIRCRAFT STABILITYp. 684
+05-57-00 PB 201 CONF 00 – AIRCRAFT STABILITY – MAINTENANCE PRACTICESp. 684
+05-57-00-200-001-A – Aircraft Stabilityp. 684
Figure 05-57-00-991-02500-A – Aircraft on its Wheels (on Dry Ground) (Applicable to a parked or towed aircraft).p. 687
Figure 05-57-00-991-02600-A – Aircraft on its Wheels (on Wet Ground) (applicable to a parked or towed aircraft)p. 688
Figure 05-57-00-991-02700-A – Aircraft on Jacksp. 689
Figure 05-57-00-991-02800-A – Aircraft on Forward Jack or on Nose Wheel Jackp. 690
Figure 05-57-00-991-02900-A – Aircraft on one Main Gear Wheel Jackp. 691
Figure 05-57-00-991-03000-A – Aircraft Jacked at Main and Nose Gears for Wheel Changep. 692
Figure 05-57-00-991-03100-A – Aircraft on its Wheels (on Ice Ground)p. 693
+05-59 – NON-REVENUE FLIGHT – REQUIREMENTS FOLLOWING MAINTENANCE ACTIONSp. 694
+05-59-00 – NON-REVENUE FLIGHT – REQUIREMENTS FOLLOWING MAINTENANCE ACTIONSp. 694
+05-59-00 PB 001 CONF 00 – NON-REVENUE FLIGHT – REQUIREMENTS FOLLOWING MAINTENANCE ACTIONS – DESCRIPTION AND OPERATIONp. 694
Generalp. 694
Engine Replacementp. 695
+05-59-32 – FERRY FLIGHT WITH GEAR DOWNp. 696
+05-59-32 PB 201 CONF 00 – FERRY FLIGHT WITH GEAR DOWN – MAINTENANCE PRACTICESp. 696
05-59-32-869-001-A – Preparation for Flight with Gear Downp. 696
05-59-32-869-002-A – Return to Normal Operation after a Flight with Gear Downp. 698
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 44 – CABIN SYSTEM
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 – (CFMB) – STANDARD PRACTICES – ENGINE
Chapter 71 – (CFMB) – POWER PLANT
Chapter 72 – (CFMB) – ENGINE
Chapter 73 – (CFMB) – ENGINE FUEL AND CONTROL
Chapter 74 – (CFMB) – IGNITION
Chapter 75 – (CFMB) – AIR
Chapter 76 – (CFMB) – ENGINE CONTROLS
Chapter 77 – (CFMB) – ENGINE INDICATING
Chapter 78 – (CFMB) – EXHAUST
Chapter 79 – (CFMB) – OIL
Chapter 80 – (CFMB) – STARTING
Taken together, this document gives a line or base maintenance technician the complete task-card content behind Chapter 05: the AMTOSS-numbered zonal inspection tasks that make up the aircraft’s scheduled walkaround and detailed visual inspection program, plus the full set of unscheduled/event-driven checks a crew must run after things like a hard landing, lightning strike, bird strike, tire burst, brake overheat, turbulence encounter, dust storm or volcanic ash exposure, and other abnormal operating events. Each task follows the standard AMM task-card format – reason for the job, work zones and access panels, referenced tasks, job set-up, procedure steps, and close-up – so it reads exactly like the source manual used on the ramp and in the hangar.
What This Airbus A318 A319 A320 A321 Chapter 05 Manual Enables
With this Airbus A318/A319/A320/A321 Time Limits and Maintenance Checks manual, a technician can carry out the full program of zonal general visual inspections across the fuselage, wings, empennage, engines/nacelles/pylons, landing gear, and doors, following the same AMTOSS task numbering and access-panel references used in operational maintenance planning. It also provides the complete set of unscheduled inspection procedures required after abnormal events – hard landings, overweight landings, lightning strikes, bird or hail strikes, tire failures, brake overheats, severe turbulence, and more – along with aircraft leveling, jacking, weighing, and stability procedures. Having the correct chapter and revision on hand matters because these procedures set the pass/fail criteria and access requirements that keep an inspection compliant with the approved maintenance program – working from an outdated or wrong-revision task can mean missing damage or repeating work unnecessarily. This Airbus A318 A319 A320 A321 Chapter 05 Time Limits Maintenance Checks Manual downloads instantly as a PDF after purchase, with no shipping or waiting – open it on a laptop, tablet, or phone in the hangar, or print out only the pages you need for the job at hand.
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