License Holder Ultimately responsible for monitoring his own personal applicable license, license attachment, rating, authorization and/or certificates Control of Flight Documents, additional Information and Data The flight crew and ultimately the PIC shall ensure that administrative duties are accurately and fully completed after each flight or series of flights and that the following documents are returned to the NP Flight Operations or delegated person: Phase From Records, Flight Documents, additional Information and Data Via To Post Flight PIC Operational Flight Plan ATS Flight Plan Mass and Balance AIS information Other Report Forms […] […] Control of Flight Documents Task Document / Form Responsibility Sort Check form for completeness form for accuracy legibility If there are any mistakes, if the form is illegible, or if more information is required return form to author Check if any further action must be taken or further reports need to be made and carry out if required Store in applicable file […] […] Daily Journey Log Technical Flight Log Deferred / Defect List Control of Report Forms Task Form / Report Responsibility Sort Check form for completeness Check form for accuracy Check legibility If there are any mistakes, if the form is illegible, or more information is required return form to author Check form for any violations or infractions Check severity of report Define further action / initiate corrective actions Make copies if required If needed distribute to further parties Perform notifying and reporting Monitor corrective action Establish feedback to author Proximity and Air Traffic Incident Report Form“. (Attachment 3) AIP Germany Chapter 1.14 […] BFU/LBA Accident, Incident and Occurrence Report Form […] Flight Duty, Duty and Rest Period Record […] Duty Time violation Captain´s Decision Report […]
CIRCUMSTANCES DATE: Place: Remarks: SELECT THE CATEGORIES CONCERNED Flight phase: □ Towing □ Maneuver □ Pre-flight inspection □ Refueling □ Start-up □ Descent □ Translation/Taxiing □ Final Approach □ Take-off □ Landing □ Climb < 500ft □ Engine shutdown □ Climb > 500ft □ Post-flight insp. □ Cruise Flight Conditions: □ VFR □ IFR □ VMC □ IMC □ Mountain □ Over water □ Day □ Night □ cond. □ Missions: □ Training □ Ferrying □ Transport of passengers or □ Night flight □ Emergency proc. training □ Auto-rotation training DOCUMENTS USED Reference flight manual: Revision: Language: FLIGHT CONDITIONS Meteorological Conditions: DESCRIPTION OF THE OCCURRENCE
Appendix 2 – Maintenance Occurrence Report MAINTENANCE OCCURRENCE REPORT No. IDENTIFICATION OF THE AIRCRAFT Type of Aircraft Version S/N Flight hours Customer Country CIRCUMSTANCES DATE: Place: Maintenance Phases: SELECT THE CATEGORIES CONCERNED Maintenance □ Scheduled maintenance □ Towing □ Unscheduled maintenance □ Refuelling □ Repair □ Pre-flight inspection □ Training/maintenance □ Post-flight inspection MAINTENANCE CONDITIONS Select the relevant area (ATA Chapter 53) Check your a/c □ 21 Air-conditioning system □ 22 Automatic pilot □ 23 Communication systems □ 24 Electrical system □ 25 Equipment, furnishings □ 26 Fire protection system □ 28 Fuel system □ 29 Hydraulic system □ 30 Protection against rain and ice □ 31 Recording/information system □ 32 Landing gear □ 33 Lights/lamps □ 34 Navigation system/flight data □ 36 Pneumatic system □ 39 Electrical/electronic equip. and panel □ 45 Maintenance centralization system □ 46 Display integration system □ 49 External power generation system □ 52 Doors and protection covers □ 53 Fuselage □ 55 Stabiliser □ 56 Windshield □ 67 Flight controls □ 71/72 Electrical installation □ 73 power supply system □ 74 Lighting system □ 76 Engine control □ 77 Engine indicators □ 79 Oil cooling system □ 80 Engine start-up system □ 85 Optional equipment
De-icing/Anti-icing First step: De-icing Second step: (1) 0 °C (32 °F) and above Heated fluid/water mixture with a freezing point of at least 10 °C (18 °F) below OAT Heated or a heated fluid/water mixture Heated fluid/water mixture with a freezing point of at least 10 °C (18 °F) below OAT below 0 °C (32 °F) down to LOUT Heated fluid/water mixture with a freezing point at OAT or below (1) To be applied before step fluid freezes. NOTE 1: Temperature of water or fluid/water mixtures shall be at least 60 °C (140 °F) at the nozzle. Upper temperature limit shall not exceed fluid and aircraft manufacturer's recommendations. NOTE 2: This table is applicable for the use of Type I Holdover Time Guidelines. If holdover times are not required, a temperature of 60 °C (140 °F) at the nozzle is desirable. NOTE 3: To use Type I Holdover Time Guidelines, at least 1 litre/m2 (~2 Gals/100ft2) must be applied to the de-iced surfaces. CAUTION: Wing skin temperatures may be lower than OAT. If this condition is identified, a stronger mixture (more glycol) may need to be used to ensure a sufficient freezing point buffer. Table 2 - Guidelines for the application of Type II and Type IV fluid/water mixtures (minimum concentrations) as a function of OAT OAT One-Step Procedure Two-Step Procedure De-icing/Anti-icing First step: De-icing Second step: (1) 0 °C (32 °F) and above Heated water or a heated Type I, II or IV fluid/water mixture 50/50 Heated/unheated Type II or IV fluid/water mixture below 0 °C (32 °F) down to LOUT 50/50 Heated (3) Type II or IV fluid/water mixture 50/50 Heated/unheated Type II or IV fluid/water mixture below -3 °C (27 °F) to °C (7 °F) 75/25 Heated/unheated Type II or IV fluid/water mixture
proximity to the ground, and the maintenance of a safe flight path in these phases can be very difficult. Do not take-off if a thunderstorm is overhead or approaching. At destination, hold clear if a thunderstorm is overhead or approaching. Divert if necessary. Avoid severe thunderstorms even at the cost of diversion or an intermediate landing. If avoidance is impossible, the procedures recommended in these paragraphs should be followed. Ensure that our aeroplanes are adequately secured on the ground when severe thunderstorm activity is forecast or present. Use of weather radar - guidance to pilots FLIGHT LEVEL ECHO CHARACTERISTICS Shape Intensity Gradient of intensity * Rate of change Up to 200 Avoid by 10 echoes with hooks, fingers and scalloped Avoid by 5 miles: echoes with sharp edges or strong intensities Avoid by 5 miles: echoes with strong gradients of intensity Avoid by 10 miles: echoes showing rapid change of shape, height or intensity 200 – 250 Avoid all echoes by 10 miles. 250 – 300 Avoid all echoes by 15 miles. 300 Avoid all echoes by 20 miles. *: Applicable to sets with Iso-Echo or a colour display. Iso-Echo produces a hole in a strong echo when the returned signal is above a pre-set value. Where the return around a hole is narrow, there is a strong gradient of intensity. NOTE 1: If storm clouds have to be overflown, always maintain at least 5,000 ft vertical separation from cloud tops. It is difficult to estimate this separation but ATC or Met information on the altitude of the tops may be available for guidance. NOTE 2: If the aeroplane is not equipped with radar or it is inoperative, avoid by 10 miles any storm that by visual inspection is tall, growing rapidly or has an anvil top. NOTE 3: Intermittently monitor long ranges on radar to avoid getting into situations where no alternative remains but the penetration of hazardous areas NOTE 4: Avoid flying under a cumulonimbus overhang. If such flight cannot be avoided, tilt antenna full up occasionally to determine, if possible, whether precipitation (which may be hail) exists in or is falling from the overhang. Icing conditions Frost, ice, snow or slush contamination can seriously affect flight characteristics Contamination increases weight and disturbs airflow. Critical surfaces, which include upper wing surfaces, control surfaces and engine cowlings, must be free of contamination unless otherwise permitted by the aircraft manufacturer
Signed statement of PIC to airport authority Speyer AIP Germany Part III X United t.b.d Approval by airport authority X B Web familiarisation required B Mountainous environment B Web based qualification required B Glide angle > 3° B Mountainous environment M O T W