Common use of General Appearance Clause in Contracts

General Appearance. The Aircraft shall be clean by commercial passenger airline standards, cosmetically acceptable, interior complete, and prepared to be placed into scheduled revenue airline operations. Interior items which may be broken shall be repaired or replaced. All decals, signs and placards shall be clean, secure and legible in the English language. The Aircraft shall meet the following minimum requirements: (i) Fuselage, Wings and Empennage - The fuselage shall be within Maintenance Program approved limits regarding dents and abrasions and loose or pulled rivets; all leading edges shall be within Maintenance Program approved limits regarding damage occurring since delivery; the airframe, Engines and wings shall be free of fuel, oil and hydraulic leaks so as to allow unrestricted operation; all leading edges and fuselage areas which are aerodynamically critical shall be free of any scab patches other than those required by the Manufacturer and shall be repaired with repairs which are permanent in nature in accordance with the SRM, or are made in accordance with the Manufacturer's approval. (ii) Interior - Ceilings, sidewalls, bulkhead panels shall be clean, free of cracks and within Maintenance Program approved limits regarding dents; all carpets and seat covers shall be in good condition and clean and meet FAR fire resistance regulations; all seats shall be serviceable and in good condition. All safety equipment shall be installed at the correct stations, a loose equipment check list and location drawings shall accompany the Aircraft and a loose equipment inventory shall be drawn up on the Delivery Date and checked on the day of return of the Aircraft. (iii) Cockpit - All fairing panels shall be free of cracks and shall be clean; all floor coverings shall be clean and effectively sealed and secured, all seat covers and cushions shall be in good condition and clean and shall, as applicable, conform to FAA fire resistance regulations. All seats shall be fully serviceable and in good condition. All instruments and light panels shall be clean, secure and legible, function in accordance with their intended purpose and have all lighting operating properly. (iv) Landing, Gear and Wheel Xxxxx - The landing gear and all wheel xxxxx shall be clean, free of leaks, and repaired as necessary. The main and nose landing gear components and their associated actuators and parts shall be in a good operating condition. (v) Cargo Compartment, Galleys and Toilets - All cargo compartment panels shall be installed and be in good condition so as to comply with extended range operations requirements. The cargo compartments, galleys and toilet of the Aircraft shall be in a clean and presentable condition and all cargo securing system components shall be serviceable; all galley inserts (to the extent delivered with the Aircraft) shall be redelivered with the Aircraft. (vi) Windows - Any delamination, and crazing of the windshields and cabin windows of the Aircraft shall be within approved limits of the Maintenance Program and shall be properly sealed. (vii) Doors - All the doors of the Aircraft shall be free moving, correctly rigged and properly sealed and all door assist mechanisms shall be charged in accordance with the AMM.

General Appearance. The Aircraft shall be clean by commercial passenger airline standards, cosmetically acceptable, interior complete, and prepared to be placed into scheduled revenue airline operations. Interior items which may be broken shall be repaired or replaced. All decals, signs and placards shall be clean, secure and legible in the English language. The Aircraft shall meet the following minimum requirements: (i) Fuselage, Wings and Empennage - The fuselage shall be within Maintenance Program approved limits regarding dents and abrasions and loose or pulled rivets; all leading edges shall be within Maintenance Program approved limits regarding damage occurring since delivery; the airframe, Engines and wings shall be free of fuel, oil and hydraulic leaks so as to allow unrestricted operation; all leading edges and fuselage areas which are aerodynamically critical shall be free of any scab patches other than those required by the Manufacturer and shall be repaired with repairs which are permanent in nature in accordance with the SRM, or are made in accordance with the Manufacturer's approval. (ii) Interior - Ceilings, sidewalls, bulkhead panels shall be clean, free of cracks and within Maintenance Program approved limits regarding dents; all carpets and seat covers shall be in good condition and clean and meet FAR fire resistance regulations; all seats shall be serviceable and in good condition. All safety equipment shall be installed at the correct stations, a loose equipment check list and location drawings shall accompany the Aircraft and a loose equipment inventory shall be drawn up on the Delivery Date and checked on the day of return of the Aircraft. (iii) Cockpit - All fairing panels shall be free of cracks and shall be clean; all floor coverings shall be clean and effectively sealed and secured, all seat covers and cushions shall be in good condition and clean and shall, as applicable, conform to FAA fire resistance regulations. All seats shall be fully serviceable and in good condition. All instruments and light panels shall be clean, secure and legible, function in accordance with their intended purpose and have all lighting operating properly. (iv) Landing, Gear and Wheel Xxxxx Wells - The landing gear and all wheel xxxxx shall wexxx xhall be clean, free of leaks, and repaired xxxxxred as necessary. The main and nose landing gear components and their associated actuators and parts shall be in a good operating condition. (v) Cargo Compartment, Galleys and Toilets - All cargo compartment panels shall be installed and be in good condition so as to comply with extended range operations requirements. The cargo compartments, galleys and toilet of the Aircraft shall be in a clean and presentable condition and all cargo securing system components shall be serviceable; all galley inserts (to the extent delivered with the Aircraft) shall be redelivered with the Aircraft. (vi) Windows - Any delamination, and crazing of the windshields and cabin windows of the Aircraft shall be within approved limits of the Maintenance Program and shall be properly sealed. (vii) Doors - All the doors of the Aircraft shall be free moving, correctly rigged and properly sealed and all door assist mechanisms shall be charged in accordance with the AMM.

General Appearance. The Aircraft shall be clean by commercial passenger airline standards, cosmetically acceptable, interior complete, and prepared to be placed into scheduled revenue airline operations. Interior items which may be broken shall be repaired or replaced. All decals, signs and placards shall be clean, secure and legible in the English language. The Aircraft shall meet the following minimum requirements: (i) Fuselage, Wings and Empennage - The fuselage shall be within Maintenance Program approved limits regarding dents and abrasions and loose or pulled rivets; all leading edges shall be within Maintenance Program approved limits regarding damage occurring since delivery; the airframe, Engines and wings shall be free of fuel, oil and hydraulic leaks so as to allow unrestricted operation; all leading edges and fuselage areas which are aerodynamically critical shall be free of any scab patches other than those required by the Manufacturer and shall be repaired with repairs which are permanent in nature in accordance with the SRM, or are made in accordance with the Manufacturer's approvalapproval or FAA approved data. (ii) Interior - Ceilings, sidewalls, bulkhead panels shall be clean, free of cracks and within Maintenance Program approved limits regarding dents; all carpets and seat covers shall be in good condition and clean and meet FAR fire resistance regulations; all seats shall be serviceable and in good condition. All safety equipment shall be installed at the correct stations, a loose equipment check list and location drawings shall accompany the Aircraft and a loose equipment inventory shall be drawn up on the Delivery Date and checked on the day of return of the Aircraft. (iii) Cockpit - All fairing panels shall be free of cracks and shall be clean; all floor coverings shall be clean and effectively sealed and secured, all seat covers and cushions shall be in good condition and clean and shall, as applicable, conform to FAA fire resistance regulations. All seats shall be fully serviceable and in good condition. All instruments and light panels shall be clean, secure and legible, function in accordance with their intended purpose and have all lighting operating properly. (iv) Landing, Gear and Wheel Xxxxx - The landing gear and all wheel xxxxx shall be clean, free of leaks, and repaired as necessary. The main and nose landing gear components and their associated actuators and parts shall be in a good operating condition. (v) Cargo Compartment, Galleys and Toilets - All cargo compartment panels shall be installed and be in good condition so as to comply with extended range operations requirements. The cargo compartments, galleys and toilet of the Aircraft shall be in a clean and presentable condition and all cargo securing system components shall be serviceable; all galley inserts (to the extent delivered with the Aircraft) shall be redelivered with the Aircraft. (vi) Windows - Any delamination, and crazing of the windshields and cabin windows of the Aircraft shall be within approved limits of the Maintenance Program and shall be properly sealed. (vii) Doors - All the doors of the Aircraft shall be free moving, correctly rigged and properly sealed and all door assist mechanisms shall be charged in accordance with the AMM.

General Appearance. The Aircraft shall be clean by commercial passenger airline standards, cosmetically acceptable, interior complete, and prepared to be placed into scheduled revenue airline operations. Interior items which may be broken shall be repaired or replaced. All decals, signs and placards shall be clean, secure and legible in the English language. The Aircraft shall meet the following minimum requirements: (i) Fuselage, Wings and Empennage - The fuselage shall be within Maintenance Program approved limits regarding dents and abrasions and loose or pulled rivets; all leading edges shall be within Maintenance Program approved limits regarding damage occurring since delivery; the airframe, Engines and wings shall be free of fuel, oil and hydraulic leaks so as to allow unrestricted operation; all leading edges and fuselage areas which are aerodynamically critical shall be free of any scab patches other than those required by the Manufacturer and Lessor (or its designee) and shall be repaired with repairs which are permanent in nature in accordance with the Structural Repair Manual ("SRM"), or are made in accordance with the Manufacturer's and Lessor's (or its designee's) approval. (ii) Interior - Ceilings, sidewalls, bulkhead panels shall be clean, free of cracks and within Maintenance Program approved limits regarding dents; all carpets and seat covers shall be in good condition and clean and meet FAR fire resistance regulations; all seats shall be serviceable and in good condition. All safety equipment shall be installed at the correct stations, a loose equipment check list and location drawings shall accompany the Aircraft and a loose equipment inventory shall be drawn up on the Embraer Delivery Date and checked on the day of return of the AircraftTermination Date. (iii) Cockpit - All fairing panels shall be free of cracks and shall be clean; all floor coverings shall be clean and effectively sealed and secured, all seat covers and cushions shall be in good condition and clean and shall, as applicable, conform to FAA fire resistance regulations. All seats shall be fully serviceable and in good condition. All instruments and light panels shall be clean, secure and legible, function in accordance with their intended purpose and have all lighting operating properly. (iv) Landing, Gear and Wheel Xxxxx - The landing gear and all wheel xxxxx shall be clean, free of leaks, and repaired as necessary. The main and nose landing gear components and their associated actuators and parts shall be in a good operating condition. (v) Cargo Compartment, Galleys and Toilets - All cargo compartment panels shall be installed and be in good condition so as to comply with extended range operations requirements. The cargo compartments, galleys and toilet of the Aircraft shall be in a clean and presentable condition and all cargo securing system components shall be serviceable; all galley inserts (to the extent delivered with the Aircraft) shall be redelivered with the Aircraft. (vi) Windows - Any delamination, and crazing of the windshields and cabin windows of the Aircraft shall be within approved limits of the Maintenance Program and shall be properly sealed. (vii) Doors - All the doors of the Aircraft shall be free moving, correctly rigged and properly sealed and all door assist mechanisms and shall be charged in accordance with the AMM.

General Appearance. The Aircraft shall be clean by commercial passenger airline standards, cosmetically acceptable, interior complete, and prepared to be placed into scheduled revenue airline operations. Interior items which may be broken shall be repaired or replaced. All decals, signs and placards shall be clean, secure and legible in the English language. The Aircraft shall meet the following minimum requirements: (i) Fuselage, Wings and Empennage - The fuselage shall be within Maintenance Program approved limits regarding dents and abrasions and loose or pulled rivets; all leading edges shall be within Maintenance Program approved limits regarding damage occurring since delivery; the airframe, Engines and wings shall be free of fuel, oil and hydraulic leaks so as to allow unrestricted operation; all leading edges and fuselage areas which are aerodynamically critical shall be free of any scab patches other than those required by the Manufacturer and shall be repaired with repairs which are permanent in nature in accordance with the SRM, or are made in accordance with the Manufacturer's approval. (ii) Interior - Ceilings, sidewalls, bulkhead panels shall be clean, free of cracks and within Maintenance Program approved limits regarding dents; all carpets and seat covers shall be in good condition and clean and meet FAR fire resistance regulations; all seats shall be serviceable and in good condition. All safety equipment shall be installed at the correct stations, a loose equipment check list and location drawings shall accompany the Aircraft and a loose equipment inventory shall be drawn up on the Delivery Date and checked on the day of return of the Aircraft. (iii) Cockpit - All fairing panels shall be free of cracks and shall be clean; all floor coverings shall be clean and effectively sealed and secured, all seat covers and cushions shall be in good condition and clean and shall, as applicable, conform to FAA fire resistance regulations. All seats shall be fully serviceable and in good condition. All instruments and light panels shall be clean, secure and legible, function in accordance with their intended purpose and have all lighting operating properly. (iv) Landing, Gear and Wheel Xxxxx Wells - The landing gear and all wheel xxxxx xxxxl wells shall be clean, free of leakslexxx, and repaired as necessary. The main and nose landing gear components and their associated actuators and parts shall be in a good operating condition. (v) Cargo Compartment, Galleys and Toilets - All cargo compartment panels shall be installed and be in good condition so as to comply with extended range operations requirements. The cargo compartments, galleys and toilet of the Aircraft shall be in a clean and presentable condition and all cargo securing system components shall be serviceable; all galley inserts (to the extent delivered with the Aircraft) shall be redelivered with the Aircraft. (vi) Windows - Any delamination, and crazing of the windshields and cabin windows of the Aircraft shall be within approved limits of the Maintenance Program and shall be properly sealed. (vii) Doors - All the doors of the Aircraft shall be free moving, correctly rigged and properly sealed and all door assist mechanisms shall be charged in accordance with the AMM.