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TECHLOG TRAINING MANUAL MANUAL
TECHLOG TRAINING MANUAL SKIN

The maximum value of acceptable differences of the two primary altimeters systems exceeds 75 ft.

A defect or system defect cannot be rectified and must be operative for RVSM operations in accordance with the MEL.

Damage exists around the pitot-static probes and Angle Of Attack Vane areas that is outside of SRM limits for RVSM operation.

RELEASE OF AIRCRAFT FOR NON-RVSM OPERATIONĪn aircraft must not be released for RVSM operation in the event of any of the following,:

That meets the tolerance stated in the AMM can be used. In the event that a system test of the pitot and/or static air system is required to be carried out in accordance with the AMM, only the test equipment.Paint conformance: chapter 11 of the AMM provides guidelines for marking (painting) conformance in the immediate area around the flush static ports.Functional and operational tests of all systems and equipment applicable to RVSM must be carried out in accordance with the applicable AMM reference.If the damage is outside of the limits for RVSM operation, the aircraft must be released for non-RVSM operation

TECHLOG TRAINING MANUAL SKIN

Any damage observed in the areas of the static ports, pitot probes and angle of attack vanes must be assessed and inspected for skin waviness, surface roughness and fastener flushness in accordance with the SRM chapter 51-10-03 and AMM 51-10-00.

During the external inspection of the aircraft, particular attention must be paid to the condition of the static ports, pitot probes and angle of attack vanes, and the condition of the fuselage skin near each of these ports and probes.

Following any repairs, either covered or not covered by the SRM in the areas of the static ports, pitot probes and angle of attack vanes, the applicable skin surface in this area must be inspected for skin waviness, surface roughness and fastener flushness in accordance with the AMM 51-10-00.

SRM 51-10-01), must be referred to Boeing for a repair design review

Any repairs, not covered by the SRM that may affect the integrity of continuing RVSM approval, such as those affecting alignment of pitot probes or repairs to dents or deformations in the areas of the static ports and angle of attack vanes, (ref.

Strict adherence to the SRM chapter 51-10-03 must be exercised concerning aerodynamic requirements applicable to any structural repairs in the areas of the static ports, pitot probes and angle of attack vanes.

TECHLOG TRAINING MANUAL MANUAL

Therefore, the Operating manual (OM), Airplane Flight Manual (AFM) and Minimum Equipment List (MEL) are amended with respect to procedures and limitations for dispatch of aircraft for RVSM operations.

Since RVSM operation requires these systems to be installed and serviceable, failures of these systems will result in non-compliance with RVSM. RVSM compliance also places requirements on other systems such as auto-pilot, altitude alerter and ATC transponder systems. Failure to so rectify or repair the airframe or equipment required for RVSM operation must result in the aircraft being removed, temporarily or permanently, from RVSM operations.

Also, any defects affecting equipment required for RVSM operation must be rectified in accordance with the relevant Maintenance Manual (AMM) as appropriate. It must be ensured that any apparent minor damage to the airframe in the areas of ports and probes affecting the height keeping performance of the aircraft will be repaired in accordance with an approved Structural Repair Manual (SRM). Special requirements have been established for operation of aircraft in airspace designated as Reduced Vertical Separation Minimum (RVSM) airspace. that can be applied to approved operators of approved aircraft operating in upper airspace between flight level (FL) 290 and FL 410 inclusive in designated regions. RVSM is the generic term applied to a reduction in vertical separation from 2000 ft. The procedure is concerned with maintenance practices, which must be used to ensure continued airworthiness in respect of RVSM operation. It is necessary to employ continuous airworthiness maintenance procedures to ensure that the aircraft’s static pressure sensing, altimetry and associated peripheral systems provide an acceptable standard of height keeping performance.