JET AVIATION AG / BASEL, SWITZERLAND

JET AVIATION AG / BASEL, SWITZERLAND CERTIFICATION COMPLIANCE No.: 98XN9-102 NC: B737-700IM REG.: VP-BBJ S/N: 29273 AMDT. 25-77 REV.: IR ISSUED DATE: 7/6/99 WORDING OF REGULATION MOC DOCUMENT DESCRIPTION CERTIFICATION COMPLIANCE A/C: B737-700IGW REG.: VP-BBJ S/N: 29273 DOCUMEN 98XN9-102 DATE: 7/6/99 SCOPE: All modification carried out within the project 98XN9 is subject to approval under FAR 25, Arndt. 77. The basic aircraft is certified under FAR 25. DEPT:i:%inir nt AG DATE: 7/6/99 PREPARED: a g -----V;:t 2 DEPT.: ' -airi-)N DATE: 7/6/99 -mayO t CHECKED: de/W DEPT.: DATE: APPROVED: ye.c,c,,M,tr-c? e.,:\ V Seite 1 1 PROT0 A/C: 8737-7001G REG.: VP-BW SIN: 29273 AMDT. 25-77 REV.: ISSUED DATE: IR 7/6/99 MOC DOCUMENT DESCRIPTION MOC CODES USED IN CCS 1. SYSTEM DESCRIPTION 1 2. STRESS REPORT 2 3. GROUND CHECK 3 4. FLIGHT CHECK 4 5. DRAWING 5 6. STC 6 7. ANALYSIS 7 8. AA INSPECTION 8 9. ENGINEERING ORDER 9 10. LISTS 10 11. AFM SUPPLEMENTS 11 DEPT.: rer. AL, DATE: 7/6/99 , . /c..ini, c.....ewnt 9 DEPTJET Np<1.,O.2ON "'acneeporai A 7/6/99 DEPT.: " DATE: PREPARED: 77 _./ Ate; CHECKED: Zia e a 4 APPROVED: L. / 4.- CJ Sae 2 PROT1 JET AVIATION AG I BASEL, SWITZERLAND NC: B737-700IG1A REG.: VP-BBJ S/N: 29273 AMDT. 25-77 REV.: IR ISSUED DATE: 7/6/99 MOC DOCUMENT DESCRIPTION REV. NO REVISION PAGES STATUS DESCRIPTION REMARKS DATE IR ALL Initial Release 7/6/99 DEPT.:JET *fling AG DATE: 7/6/99 Froi;:errIng . •opartrnan• DEPT.: JET an91O14 -P, ATE: 7/6/99 EngiritCfrit De CHECKED: zieleag DEPT.: DATE: APPROVED: PREPARED: rVe.-- Seite 3 PROT2 NC: B737-700IGV1 REG.: VP-BBJ S/N: 29273 AMDT. 25-77 REV.: IR ISSUED DATE: 3/10/99 MOC DOCUMENT DESCRIPTION FAR 25.29 Empty weight and corresponding center of gravity 7 Weight and Balance Report MK-14M (a,b) A new weighing will be done after modification. A new Weight and Balance Report reflects the new center of Gravity. DEPT.tFT 4Clin I DATE: 7/6/99 DEPT.3 ET 4-n Elva CHECKED: ATE: 7/6/99 -t-e- DEPT.: DATE: APPROVED: - .,/ >114.22.0.-_\ PREPARED: __/;,a(ie.- tee Serve 4 PROT3 A/C: B737-700IGIA REG.: VP-BBJ S/N: 29273 AMDT. 25-77 REV.: IR ISSUED DATE: 7/6/99 MOC DOCUMENT DESCRIPTION FAR 25.301 Loads 2 3 4 7 10 Stress Report 98XN9-104 Groundcheck: 98XN9-105-01 98XN9-105-02 98XN9-105-03 98XN9-105-04 98XN9-105-05 98XN9-105-06 98XN9-105-07 98XN9-105-08 98XN9-105-09 98XN9-105-10 98XN9-105-11 98XN9-105-12 Flightcheck: 98XN9-109-01 98XN9-109-02 98XN9-109-03 98XN9-109-04 98XN9-109-05 98XN9-109-06 98XN9-109-07 98XN9-109-08 98XN9-109-09 98XN9-109-10 98XN9-109-11 98XN9-109-12 Weight and Balance Report MK-14 M Supp. Equi. List MK-10M (a-c) The following load conditions are taken into account: Upward 3.0g, Foreward 9.0g, Sideward 3.0g and 4.0g on seats, Downward 6.0g and Rearward 1.5g. Gust Load Conditions and Decompression Loads. The whole installation is calculated and tested on ground and in flight. DEPT.* - DATE: 7/6/99 .1E.T AVIATION A Engineering Dk r PREPARED: //~• "ie.' DEPTJET WION Do Do nt ATE: 7/6/99 CHECKED: laitt4 DEPT.: ' DATE: APPROVED: A4-1 .5z,,,,ctz.. - \ Seite 5 PROT4 NC: B737-700IGNA REG.: VP-BE3J S/N: 29273 AMDT. 25-77 REV.: IR ISSUED DATE: 7/6/99 MOC DOCUMENT DESCRIPTION FAR 25.303 Factor of safety 2 The Stress Report considers the factor of safety. The factor 1.5 is included in the ultimate loads. They are multiplied by the following fitting factor. Furniture: fs=1.15 DEPT.:JET AVIATION AGDATE: 7/6/99 Engineering Departme PREPARED: / de. DEPT.: JE TI ATE: 7/6/99 Er. rt CHECKED: 7 ,i-d-ceei DEPT.: DATE: APPROVEDV. i.;\ (4..6.64.-\ Seite 6 PROT5 NC: B737-700IGW REG.: VP-BBJ SIN: 29273 AMDT. 25-77 REV.: IR ISSUED DATE: 7/6/99 MOC DOCUMENT DESCRIPTION FAR 25.305 Strength and deformation 2 (a) No interference with safe operation. 3 Groundcheck: 98XN9-105-01 (b) The proof of strengh is shown in the 98XN9-105-02 stress report. 98XN9-105-03 (c-f) N/A for this modification 98XN9-105-04 98XN9-105-05 98XN9-105-06 98XN9-105-07 98XN9-105-08 98XN9-105-09 98XN9-105-10 98XN9-105-11 98XN9-105-12 4 Flightcheck: 98XN9-109-01 98XN9-109-02 98XN9-109-03 98XN9-109-04 98XN9-109-05 98XN9-109-06 98XN9-109-07 98XN9-109-08 98XN9-109-09 98XN9-109-10 98XN9-109-11 98XN9-109-12 5 J.A. DWG: MK-01M DEPT:JET AVIATION AG DATE: 7/8/99 DEPT • -.J ET ION 7/6/99 DEPT.: DATE: Engineering Depart PREPARED: Deportment 3.1, 9- En De CHECKED: aiaae-t APPROVED: 4->Z Cbdee Selte 7 PROT6 NC: B737-700IGA REG.: VP-BBJ S/N: 29273 AMDT. 25-77 REV.: IR ISSUED DATE: 7/6/99 MOC DOCUMENT DESCRIPTION FAR 25.307 Proof of structure Refer to FAR 25.305 (a-c) The strength of the main structure is not influenced by this modification. All structural installations are performed in accordance with standard practice set forth in FAA AC43.13-1A&2A. (d) Refer to FAR 25.305 FAR 25.321 General - Flight loads Refer to FAR 25.301 and 25.305 FAR 25.331 General - Flight Maneuver and gust conditions DEPMJET AVIATION AGDATE: 7/6/99 Enp;neerIng Department n - DEPT.:JET TeroN AGDATE: 7/6/99 EngirW DEPT.: DATE: PREPARED: L/7 /54.et---- CHECKED: 'Zig e e4n APPROVED:p i",7>V4A4C\ Seite 8 PROT7 NC: B737-7001GVN REG.: VP-BBJ S/N: 29273 AMDT. 25-77 REV.: IR ISSUED DATE: 7/6/99 MOC DOCUMENT DESCRIPTION FAR 25.341 Gust and turbulence loads FAR 25.365 Pressurized compartment loads Amdt 25-0 FAR 25.471 General - Ground loads DEPT :JET AVIATION AG DATE: 7/6/99 Engin wring Department DEPTJEr AO DATE: 7/6/99 En ' DEPT.: DATE: PREPARED: d age-- CHECKED: z ,./ _Sabi APPROVED: 47 P4\ Seite 9 PROT8 NC: B737-700IGIA REG.: VP-BBJ S/N: 29273 AMDT. 25-77 REV.: IR ISSUED DATE: 06.07.99 MOC DOCUMENT DESCRIPTION FAR 25.561 General-Emergency landing conditions Amdt 25-59 FAR 25.562 Emergency Landing Dynamic Conditions 9 2 10 10 2 Eng. Order: 98XN9-250000 Supp. Equip. List MK-10M (a-c) Refer to 25.301 for load factor. (d) Seats are existing or TSO C127 approved by AMP. All items of mass are attached to structure taking the focres mentioned in b (3) into accoun or are stowed in an adequate manner. (a),(b),(c),(1),(2),(3),(4),(7),(8) All seats and divans occupied for take-off and landing are TSO C127 approved. Flight Attendant Seats are TSO C127 approved. DEPT.:JET AVIATION AG DATE: 06.07.99 Engineering D rtme - PREPARED: dee--- DEPT.:JET m. w -i 06.07.99 Enginatt . CHECKED: asp, DEPT.: DATE: APPROVED' / cy/..4-----\,_ • 4 ' 4 / 1. Seite 10 PROT9 NC: B737-700IGV% REG.: VP-BBJ S/N: 29273 AMDT. 25-77 REV.: IR ISSUED DATE: 716/99 MOC DOCUMENT DESCRIPTION FAR 25.571 Damage Tolerance and Fatigue Evaluation Arndt. 25-0 of Structure to 25-77 FAR 25.581 Lightning protection 2 10 Mech. Master Dwg. List MK1-01M (a-e) A Damage Tolerance Report is provided for all antenna installations. (a-b) All installed metallic components are bonded to the airframe as noted on dwg. DEPL;ET AVIATION AG DATE: 7/6199 angineoring DepattAent ,.2 PREPARED: 44 A DEPT 4E r gyfGttiION DATE: 7/6/99 Engi CHECKED: ,. el(ZieZe ail , DEPT.: DATE: APPROVED:d ,k (sci'L__\: z Seite 11 PROT10 A/C: B737-700IG REG.: VP-BBJ I S/N: 29273 AMDT. 25-77 REV.: IR ISSUED DATE: 7/6/99 MOC DOCUMENT DESCRIPTION FAR 25.601 General Design and construction 10 All items are NAS/AN/MS-Standard or 3 Groundcheck: 98XN9-105-01 TSO approved and installed in accordance 98XN9-105-02 with practices set forth in FAA AC43.13-1A 98XN9-105-03 &2A. 98XN9-105-04 98XN9-105-05 The whole installation is tested on ground 98XN9-105-06 and in flight. 98XN9-105-07 98XN9-105-08 98XN9-105-09 98XN9-105-10 98XN9-105-11 98XN9-105.12 4 Flightcheck: 98XN9-109-01 98XN9-109-02 98XN9-109-03 98XN9-109-04 98XN9-109-05 98XN9-109-06 98XN9-109-07 98XN9-109-08 98XN9-109-09 98XN9-109-10 98XN9-109-11 98XN9-109-12 DEPT.:JET AVIATION AGATE: 7/6/99 DEPT.: JETW 7/6/99 DEPT.: DATE: Engineering Department stoto_ PREPARED: Engi 0 CHECKED: APPROVED: j.. : 1), :Z,:ez c ,-eat),Cat Seite 12 PROT11 NC: B737-700IGV1 REG.: VP-BBJ S/N: 29273 AMDT. 25-77 REV.: IR ISSUED DATE: 7/6/99 MOC DOCUMENT DESCRIPTION FAR 25.603 Materials FAR 25.605 Fabrication methods FAR 25.607 Fasteners 10 [repeated 3 times] 2 Mech. Master Dwg. List MK1-01M J.A. Process Specifications Supp. Equi. List MK-10M Mech. Master Dwg List MK1-01M (a-c)AII Hardware is NAS/AN/MS-Standard approved and installed in accordance with practices set forth in FAA AC43.13-1A &2A. Major componants are or approved by evaluation and/or testing. (a-b) Only approved fabrication methods are used. Specified in the J.A. Process Spec. and in accordance with practices set forth in FAA AC43.13-1A & 2A. (a-c) All Hardware is NAS/ AN/ MS-Standard approved. Locking devices are used in accordance with practices set forth in FAA AC43.13-1A &2A. Major componants are or approved by evaluation and/or testing. DEPT.: DATE: 7/6/99 PREPARED: 'git. - DEPT.: 7/6/99 CHECKED: //iea DEPT.: DATE: APPROVED: ,,, ,,1 - >ith,,-;42N Seite 13 PROT12 NC: B737.700IGW REG.: VP-BBJ S/N: 29273 AMDT. 25-77 REV.: IR ISSUED DATE: 7/6/99 MOC DOCUMENT DESCRIPTION FAR 25.609 Protection of structure 10 Mech. Master Dwg List MK1-01M (a) The whole installation is protected in accordance to the standards of SRM or as noted on the dwg. (b) Ventilation and drainage is installed where necessary. FAR 25.611 Accessibility provisions 10 Mech. Master Dwg List MK-01M The accessability is applied for the whole modification. FAR 25.613 Material strength properties and design values 2 (a-e) All Hardware is NAS/ AN/ MS-Standard 10 Mech. Master Dwg List MK-01M approved. All values and strength properties are based on experience, tests and the Stress Report. Major componants are or approved by evaluation and/or testing. FAR 25.619 Special factors 2 (a-c) All special factors are applied in the Stress Report. DEPT.: DATE: 7/6/99 DEPT.: TE: 7/6/99 DEPT.: DATE: PREPARED: 6,Z 7 a- - CHECKED: V 1,e(de-eft APPROVED: A, .4. - liq.6 C.J Seite 14 PROT13 NC: B737-700IMM1 REG.: VP-BBJ S/N: 29273 AMDT. 25-77 REV.: IR ISSUED DATE: 7/6/99 MOC DOCUMENT DESCRIPTION FAR 25.623 Bearing factor 2 (a-b) All bearing factors are applied in the FAR 25.625 Fitting factors Amdt 25-59 2 Stress Report. (a-c) The whole installation is based on experienced designs and approved data. FAR 25.771 Pilot Compartment 4 Flightcheck: 98XN9-109-01 All factors are applied in the Stress Report. (d) Each seat and berth is TSO C127 approved by AMP. (a-d) No Change to basic aircraft FAR 25.772 Pilot Comprtment Doors 5 Floorplan 250010-01/98XN9 (e )Vibritions and noise characteristics are taken into account for all cockpit installation and tested during flight. (a-b) No change to basic aircraft DEPTI€T AVIATION AG DATE: 7/6/99 Engineering De;,:zIrit DEPT.:. ETIrtlION G DATE: 7/6/99 0* t DEPT.: DATE: PREPARED: eAle: CHECKED: - ettaiett APPROVED: 'tf -'\1t.a.e.(.\ Selte 15 PROT14 NC: B737-700IGV% REG.: VP-BBJ S/N: 29273 AMDT. 25-77 REV.: IR ISSUED DATE: 06.07.99 MOC DOCUMENT DESCRIPTION FAR 25.777 Cockpit Controls Project Description 98XN9-500 (a-h) The cockpit controls are not affected by the cockpit modification. FAR 25.783 Doors 9 Eng. Order 98XN9-250000 (a-) No change to basic aircraft 2 Stress Report 98XN9-04 0) All lavatory doors are designed frangible FAR 25.785 Seats, berths, safety belts, and harnesses Amdt 25-59 7 Burn Test Report 98XN9-107-01 (a-b) For each occupant a seat will be pro- 9 Eng. Order: 98XN9-250000 vided with operating placards and descrip- 10 Supp. Equip. List. MK-10M tion in the Outfitting Manual. (c) All Seats and Divans are TSO C127 approved by AMP,if intended for TOL. The cover material and foam is tested and listed in the Bum Test Report. (d-) Each safety belt and harness is existing BOEING, TSO C39 or C127approved by AMP or manufactured in accordance with TSO approved production method. FAR 25.787 Stowage compartments 2 (a-b) The stowage comply with this paragraph, based on experienced designs and 10 Supp. Equi. List MK-10M the Stress Report. Mech. Dwg List MK-01M (c) All used compartment lamps are TSO approved. DEPT.: JET AVIATION MI:PATE: 06.07.99 DEPT.:JE1 06.07.99 DEPT.: DATE: Engineering Dey,rt t 54"wtincrDATE: Engi , zer PREPARED: CHECKED: 4.7/WeVC."6.4 APPROVED: ci Q2.e;(7-\ Seite 16 PROT15 NC: B737-700IG REG.: VP-BBJ S/N: 29273 I AMDT. 25-77 REV.: IR ISSUED DATE: 7/6/99 MOC DOCUMENT DESCRIPTION FAR 25.789 Retention of items of mass in passenger and 10 Mech. Master Dwg List MK-01M (a) The installation is based on experienced Crew compartment and galleys 9 Eng. Order 98XN9-250000 designs and all items of mass are attached 2 and secured and tested on Bound and in flight. All galley storage compartments are secured with double latching system. (b) Each interphone is designed to remain in the existing position. FAR 25.791 Passenger information sings and placards 5 J.A. DWG.: 110010-01/98XN9 (a-e) All required Signs and Placards are 332550-01/98XN9 installed and shown on these Dwg's and /or 332550-02/98XN9 mentioned in the Eng. Order. 332550-01/98XN9 9 Eng. Order 98XN9-250000 FAR 25.793 Floor surfaces 7 Burn Test Report 98XN9-107-01 For all areas slip resistant carpets are used. In the galley area, a non-slip non-conductive wet carpet is installed for hygenic purpose. All installed floor cover materials are tested and listed in the Bum Test Report. No change to NC FAR 25.801 Ditching 10 Supp. Equip. List. MK-10M (a-e) No change to the ditching characteristic of the NC. Ditching equipment is provided as required. DEPT.: DATE: 7/6/99 DEPT.: A 7/6/99 DEPT.: DATE: PREPARED: d r _i_-?fire---- CHECKED: (7 (4161:6661 APPROVED: 4, r>g, f, k ,!.•_ \ Seite 17 PROT16 NC: B737-700IGVi REG.: VP-BBJ S/N: 29273 AMDT. 25-77 REV.: IR ISSUED DATE: 7/6/99 MOC DOCUMENT DESCRIPTION FAR 25.803 Emergency evacuation 5 J.A. Dwg: 250010-01/98XN9 (a-c) This modification reduces the number of occupants compared B737-700. (d-e) Access to the emergency exit is provided with respect to FAA Exemption No. 6820A. FAR 25.807 Passenger emergency exits 5 J.A. Dwg: (a) No change in the dimensions of the basic emergency exits. (b) No change in the step down distance. (c) N/A (d) The remaining number of emergency exits are sufficient to apply to this paragraph. FAR 25.809 Emergency exit arrangements 5 J.A. Dwg: (a-h) No change to basic NC. DEPT.SET AVIATION AG DATE: 7/6/99 Engineering Doparef, DEPT - ;JET N, ATE: 7/6/99 /Join e Ment . DEPT.: DATE: PREPARED: "7- 0,e-- --. CHECKED: We je W, APPROVED: it, 624 Seite 18 PROT17 JET AVIATION AG BASEL, SWITZERLAND 1 NC: B737-700IG S/N: 29273 REG.: VP-BBJ AMDT. 25-77 MOC DOCUMENT REV.: IR ISSUED DATE: 7/6/99 DESCRIPTION FAR 25.811 Emergency exit marking FAR 25.812 Emergency lighting DEPT.: DATE: 7/6/99 DEPT.: PREPARED: ,27Ze_./ CHECKED: 9 9 3 5 Eng. Order: 98XN9-250000 Engineering Order 98XN9-250000 Groundcheck: 98XN9-105-01 98XN9-105-05 J.A. Dwg.: 335050-01/98XN9 335050.02/98XN9 335050-03/98XN9 335051-01/98XN9 335051-02/98XN9 335051-03/98XN9 Lighting Level Analysis 98XN9-103-L Transverse Seperation Analysis 98XN9-103 (a) Each Emergency Exit is marked. (b) The identity and location of each passenger emergency exit is recognisable from a distance equal to the width of the cabin. (c) Means is provided. (d) The location of each passenger emergency exit is indicated by a sign visible to occupants approaching along the main passenger aisle. (e-f) No change to basic T/C. (g) The wording of the emergency exit sign is in english. (a) Emergency lighting is installed. (b) Emergency Exit signs are manufactured to meet the requirements of this subchapter. (c) The general illumination in the passenger cabin along the centerline of main passen- ger aisle is at seat armrest height and at 40 inch intervals not less than 0.05 fticd. (d) The illumination of not less than 0.02 ft/cd at the floor level leading to each emergency exit is given. a ATE: 7/6/99 aae Sede 19 DEPT.: APPROVED: At/ '(,6,C DATE: PROT18 A/C: B737-700IGN REG.: VP-BBJ SIN: 29273 AMDT. 25-77 REV.: IR ISSUED DATE: 7/6/99 MOC DOCUMENT DESCRIPTION FAR 25.812 Emergency lighting (M) 5 J.A. Dwg.: 335052-01/98XN9 (e) Floor proximity emergency escape 335052-02/98XN9 path marking is installed. 335052-03/98XN9 (f-k) No change to basic T/C. 335052-04/98XN9 (0 The emergency lighting system is 335053-01/98XN9 installed in accordance with the FAR 335053-02/98XN9 requirements. 335052-03/98XN9 335053-04/98XN9 335054-01/98XN9 335054.02/98XN9 335054-03/98XN9 335054-04/98XN9 335054-05/98XN9 FAR 25.813 Emergency exit access 5 J.A. Dwg.: (a-f) Access to each Emergency Exit is provided.The RHS Emergency Exit Hatch is slightly obstructred, but this exit is not required as per FAA Exemption No. 6820A. FAR 25.815 Width of aisle 5 J.A. Dwg.: The width of aisle is applied in the arrangement of this modification. FAR 25.817 Maximum number of seats abreast 5 J.A. Dwg.: The number of seats abreast (max.2) are considered in the arrangement of this modification. DEPT.: DATE: 7/6/99 DEPT.: STE: 7/6/99 DEPT.: DATE: 4 . Al. - CHECKED: /7 e / /&2O APPROVED:, i-46(44---\ PREPARED: Seite 20 PROT19 JET AVIATION AG I BASEL SWITZERLAND NC: B737-700IG REG.: VP-BBJ 111 SIN: 29273 AMDT. 25-77 REV.: IR ISSUED DATE: 7/6/99 MOC DOCUMENT DESCRIPTION FAR 25.831 Ventilation 10 J.A. Dwg.list: MK-01M (a) Is complied by the modification. (b-c) No change to the basic system. 9 Eng. Order: 96XN9-250000 (e-f) System is described in the Eng. Order. FAR 25.841 Pressurized cabins 4 Flight Check: 98XN9-109-01 (a) Due to the antenna installation a pressurization test in the cabin is performed. (b) No change to valves, controles, and 10 Mech. Master Dwg List MK-01M indicator for controlling cabin pressure. A cabin leak check is performed. FAR 25.851 Fire extinguishers except (b) 5 J.A. Dwg: 256010-01/98XN9 New fire extinguishers are installed as shown 9 Eng. Order: 98XN9-250000 in the drawing mentioned beside. DEPT.: DATE: 7/6/99 DEPT.: DATE: 7/6/99 DEPT.: DATE: PREPARED: /?Ai CHECKED: id eate APPROVED: ,;,/ L i3 Seite 21 PROT20 NC: 6737-7001MA REG.: VP-BBJ S/N: 29273 AMDT. 25-77 REV.: IR ISSUED DATE: 06.07.99 MOC DOCUMENT DESCRIPTION FAR 25.853 Compartment interiors Amdt 25-32 5 7 J.A. Dwg: 250012-01/98XN9 Bum Test Report 98XN9-107-01 (a) All materials are TSO approved or/ and tested and listed in the Bum Test Report. (b) Seatcushions are burn tested as per the the specification of this paragraph. 9 Eng. Order: 98XN9-250000 (d-g) Ashtrays are provided as required. FAR 25.854 Lavatory fire protection except (b) 9 Eng. Order 98XN9-250000 (h) Waste containers are fully closed and tested. Each lavatory is equipped with a smoke FAR 25.855 Cargo or baggage compartment Amdt 25-59 5 J.A. Dwg.: 261650-01/98XN9 detector system, which provides an audible warning in the passenger cabin. In addition, in the VIP bathroom a warning light and an audible warning is installed which will be readily detected by a flight attendant. Fuel Tanks installed in accordance with Pats STC. No other change to basic T/C. DEPMJE1 AV!ATI ATEt 06.07.99 DEPT.: JET AV O Ad/ATE: 06.07.99 DEPT.: ' DATE: A Engineering ar - PREPARED: - Engin e A- CHECKED: APPROVED: iS/,i 1601\ J Seite 22 PROT21 NC: B737-700IG% REG.: VP-BBJ S/N: 29273 AMDT. 25-77 REV.: IR ISSUED DATE: 06.07.99 MOC DOCUMENT DESCRIPTION FAR 25.858 Cargo compartment fire detection FAR 25.869 Fire protection: Systems Cargo Fire Protection System Retrofit Kit installed as per STC ST00405LA-D. (a) All electrical items are TSO approved or standard materials. (b) No change to basic T/C. (c) Refer to FAR 25.1453 DEPT.:JET AVIATION AGDATE: 06.07.99 Engineering DeparaTS #.------ PREPARED: DEPT4IET AVIAT Engineerin CHECKED: Ac DATE: 06.07.99 DEPT.: DATE: APPROVED: - 2171/acja._ Selte 23 PROT22 NC: 8737-7001MA REG.: VP-BBJ S/N: 29273 AMDT. 25-77 REV.: IR ISSUED DATE: 06.07.99 FAR 25.1301 General - Function and installation MOC DOCUMENT Eng. Orders: 98XN9-250000 DESCRIPTION (a-c) Refer to E.O., equipment description and installation details. Refer to AFM Supplement for operating limitations. Requirements are met by the installation of approved systems and materials as per TSO, MIL-STD, etc... (d) The whole equipment is installed/modified in accordance with the Eng. Orders and tested on ground and in flight. FAR 25.1307 Miscellaneous equipment FAR 25.1309 Equipment, systems and installation 9 10 11 3 4 3 Conformity list 98XN9-101-E AFM Supplement 98XN9-201-01 Groundcheck 98XN9-105-01/105-02/ 105-03/-04/-05/-06/-07/-08/-09/-10/-11/-12 Flightchecks: 98XN9-109-01/-02/-03/ 04/05/06/07/08/09/10111/12 Groundcheck 98XN9-105-01/105-02/ 105-03/105-04/105-05/06/07/08/09/10/ 11/12/ Transverse Separation Analysis 98XN9-103 Lighting Level Analysis 98XN9-103-L EMI Test Plan (a-e) No change to basic T/C. (a-b) Compliance is shown by analysis, design and technical dwg's and testing on ground and in flight. The installation and cable routing is made in accordance with FAA AC 43.13-2A. All Hardware is MS-Standard approved. Major Components are or approved by evaluation and/or testing.The basic T/C has not been degraded. This compliance is met. c) Additional waming indicators are installed to alert the crew to Cabin Systems malfunction and to enable them to take appropriate correc- tive action. DEPT.:JET AVIATION AWATE: 06.07.99 1/4 Engineering De tette 3 r - ''V a PREPARED: DEPT.: JE1 AVIAI Engineering D CHECKED: Seite 24 06.07.99 DEPT.: APPROVED: PROT23 JET AVIATION AG I BASEL, SWITZERLAND NC: B737-700IG9 REG.: VP-BBJ 111 SIN: 29273 AMDT. 25-77 REV.: IR ISSUED DATE: 7/6/99 MOC DOCUMENT DESCRIPTION FAR 25.1309 Equipment, systems and installation (=) 7 Electrical Load Analysis MK-11E (e-f) None of the new systems is to be essen- tial. Load shedding complies with philosophy set forth in general design practices. (g) N/A FAR 25.1316 System lightning protection (a-c) No change to basic T/C. FAR 25.1321 Arrangement and visibility (a-e) No additional flight navigation and power- plant instruments installed. No change to basic T/C. FAR 25.1322 Waming, caution and advisory lights 5 J.A. Dwg.: 3910-500-01/BBJ (a) N/A 391051-01/98XN9 (b) Amber caution lights are installed for 391056-01/98XN9 indicating situations which possibly need 391058-01/98XN9 corrective action. (c-d) Green lights show safe operation. DEPT •r 7/6/99 - Lnr_jinge D ION epa DEPT.: DATE: 7/6/99 DEPT.: DATE: - PREPARED: /atiel CHECKED: Z, VV----- APPROVED: Seite 25 PROT24 JET AVIATION AG I BASEL, SWITZERLAND A/C: B737-7001G REG.: VP-BBJ I Stfil: 29273 AMDT. 25-77 REV.: IR ISSUED DATE: 7/6/99 MOC DOCUMENT DESCRIPTION FAR 25.1351 General - Electrical system FAR 25.1353 Electrical equipment and installations FAR 25.1355 Distribution system 7 9 5 Electrical Load Analysis MK-11E Eng. Order 98XN9-250000 J.A. Electrical Dwg. List MK-01E (a-1) New el loads are installed in comp- liance with drawings based on Electrical Load Analysis. System capacity is not exceeded. (a-2) The requirements of FAR 25.1309 are met. (b-c) N/A (d) No change to basic T/C. (a) Electrical equipment controls and wiring are installed so that operation of any unit or system of units will not adversely affect the simultaneous operation of any other electri- cal unit or system essential to the safe operation. (b) Cables are grouped, routed and spaced so that damage to essential circuits will be minimized if there are faults in heavy current carrying cables. c) No storage batteries installed. (a) AC and DC bus distribution covering the required modification.(Compliance is satis- fied) (c) None of the installed systems requires two independent power sources, therefore N/A. DEPT.: DATE: 7/6/99 PREPARED: cg at ae DEPT.: ; DATE: 7/6/99 CHECKED: ei DEPT.: DATE: APPROVED: (-)1Att 4c...\ Selte 26 PROT25 NC: B737-700IGIA REG.: VP-BBJ S/N: 29273 AMDT. 25-77 REV.: IR ISSUED DATE: 7/6/99 MOC DOCUMENT DESCRIPTION FAR 25.1357 Circuit protective devices 5 J.A. Electrical Dwg. List MK-01E (a) All systems connected via appropriate circuit breakers to minimize distress to the electrical system in the event of wiring faults or serious malfunction of the system or con- nected equipment. (b) No change to basic TIC. (c) All circuit breakers installed will open when a fault exists regardless of the position of operating control. (d) All cabin system circuit breakers are installed in the cabin CB-Panel , cockpit or power distribution CB -Panels and labelled in the cockpit. (e) No new essential system installed. (f) The required number (in this case 2) is as spare parts on board. (g) N/A FAR 25.1381 Instrument lights 5 J.A. Dwg.: 3910-500-01/BBJ (a) Sufficient illumination for the Satcom 391051-01/98XN9 System Controls, Door Waming Panel, Smoke 391056-01/98XN9 Panel and Master Control Panel is provided. 391058-01/98XN9 (b) New devices are dimmable. DEPT.: DATE: ...... - 7/6/99 DATE: 7/6/99 DEPT.: DEPT.: DATE: PREPARED: CHECKED: 7,777 APPROVED: /.., ,/rNiCt/Leilta___\ ) Sok, 27 PROT26 NC: B737-700IG REG.: VP-BBJ SIN: 29273 I AMDT. 25-77 REV.: IR ISSUED DATE: 7/6/99 MOC DOCUMENT DESCRIPTION FAR 25.1411 General 10 Supp. Equip. List. MK-10M (a-g) Emergency equipment is provided. 5 256010-01/98XN9 Emergency equip. layout FAR 25.1415 Ditching equipment 10 Supp. Equip. List. MK-10M (a-e)Ditching equipment is installed as per the requirements of this paragraph. FAR 25.1421 Megaphones 10 Supp. Equip. List. MK-10M Megaphone installed FAR 25.1423 Public address system 5 J.A. Ding.: 233150-01/98XN9 (a-b) Speakers rearranged due to new. 233150-02/98XN9 configuratiuon 233151-01/98XN9 FAR 25.1431 Electronic equipment 9 Eng. Orders: 98XN9-250000 (a) Critical environmental conditions are considered. 3 Ground Check/EMI Summary (b) No radio or electronic equipment installed which must be supplied under the requirements 4 Flight Check/EMI Summary of § 25.1355 (c) (c) Equipment and wiring installed and kept separate so that simultaneous operating of any other radio or electronic unit is not affected. FAR 25.1439 Protective breathing equipment No modifications have been performed in the class A, B, or E cargo compartments. DEPTJET AVIOWN A TE: 7/6/99 ATE: DEPT.:J:7 AVIATION A 7/6/99 DEPT.: DATE: Engineeriaity Mart t Erigineerin a nt PREPARED: I 2.-&...e(0 CHECKED: - AS APPROVED: ye ,,i7"i/vav ,i_f .. Seite 28 PROT27 NC: B737-7001G1 REG.: VP-BBJ S/N: 29273 AMDT. 25-77 REV.: IR ISSUED DATE: 06.07.99 MOC DOCUMENT DESCRIPTION FAR 25.1441 Oxygen equipment and supply 3 Groundcheck 98XN9-105-03 (a) A new passenger oxygen system is 4 Flightcheck 98XN9-109-03 installed during this modification. 9 Eng. Order 98XN9-250000 (b-d) No change to basic crew system. FAR 25.1443 Minimum mass flow of supplemental oxygen FAR 25.1445 Equipment standards for the oxygen distributing system FAR 25.1447 Equipment standarts for oxygen dispensing units FAR 25.1449 Means for determining use of oxygen FAR 25.1450 Chemical oxygen generators 3 Refer to §25.1450 Refer to FAR 25.1441 Groundcheck 98XN9-105-03 All additional Oxygen generators are approved equipment. (a-e) All additional oxygen equipment is approved aircraft equipment. (a)No change to basic crew oxygen system. Passenger system seperated from crew system (b) Portable oxygen bottles are provided. No change to basic T/C. No change to basic T/C. (a-c) New Oxygen Generators are installed 4 5 9 Flightcheck 98XN9-109-03 J.A. Dwg.: 350010-01/98XN9 Eng. Order 98XN9-250000 The oxygen generators are manufactured and certified under TSO Approval. The operation of the containers is tested on ground and in flight. DEPT.: JET AVIATION MDATE: 06.07.99 DEPT.:JET ION TE: 06.07.99 DEPT.: DATE: Engineering art77 i Prig' De mei.: PREPARED: 5. Arr.---- CHECKED: zieKe_Ket. APPROVED: 71a52 ,C"---\ \ Serve 29 PROT28 NC: B737-700IGIA REG.: VP-BBJ S/N: 29273 AMDT. 25-77 REV.: IR ISSUED DATE: 06.07.99 MOC DOCUMENT DESCRIPTION FAR 25.1450 Chemical oxygen generators 3 Groundcheck 98XN9-105-03 (a-c) New Oxygen Generators are installed 4 9 Flightcheck 98XN9-109-03 Eng. Order: 98XN9-250000 The oxygen generators are 5 J.A. Dwg.: 352150-01/98XN9 352151-01/98XN9 352151-02/98XN9 352152-01/98XN9 352152-02/98XN9 352153-01/98X N9 manufactured and certified under ISO Approval. FAR 25.1453 Protection of oxygen equipment from rupture FAR 25.1455 Draining of fluids subject to freezing 3 352154-01/98XN9 352155-01/98XN9 Groundcheck 98XN9-105-11 N/A All drains are designed and located so that 4 9 Flightcheck 98XN9-109-11 Engineering Order 98XN9-250000 no ice can occur on the airplane surface. DEPT.. DATE: 06.07.99 DEPT.: JETAttAT ATE: 08.07.99 DEPT.: DATE: JET AVIATI Engj3/4 rtm n CHECKED: .&aae'r APPROVED: till L,I2.6\ Ennineerin PREPARED: W11-"---- Seite 30 PROT29 A/C: B737-700IGV% REG.: VP-BBJ SIN: 29273 AMDT. 25-77 REV.: IR ISSUED DATE: 06.07.99 MOC DOCUMENT DESCRIPTION FAR 25.1459 Flight data recorder FAR 25.1519 Weight, center of gravity and weight distribution FAR 25.1529 Instructions for continued Airwothiness 7 9 Weight and Balance Report MK-14M Maintenance Manual MK-06 Eng. Order: 98XN9-250000 No change to basic T/C. A new Weight and Balance Report will be performed. All necessary description, operation and maintenance of the system are contained in the E.O. and/or part of the Maintenance Manual MK-06. DEPT.: DATE: 06.07.99 J0f14 1/44042FT-- E in en .n, ment DATE: 06.07.99 DEPT-*JET d' Eng y CHECKED: 4, _zat ie2ear DEPT.: DATE: APPROVED: i ---\ PREPARED: Seite 31 PROT30 NC: B737-700IG REG.: VP-BBJ S/N: 29273 I AMDT. 25-77 REV.: IR ISSUED DATE: 7/6/99 MOC DOCUMENT DESCRIPTION FAR 25.1541 Markings and placards - General FAR 25.1557 Miscellaneous marking and placards 9 Eng. Order: 98XN9-250000 (a) All new systems are marked and labelled as required for safe operation. (b) No change to basic T/C (c) Refer to 25.811 (d) No change to basic T/C. DEPT,:ut: i AviA I JUN HG pATE: 7/6/99 t.nwneering Dep PREPARED: r DEPT.: - , DATE: 7/6/99 CHECKED: eja DEPT.: 7E: 1 APPROVED: too Seite 32 PROT31 NC: B737-700IGIA REG.: VP-BBJ S/N: 29273 AMDT. 26-77 REV.: IR ISSUED DATE: 7/6/99 MOC DOCUMENT DESCRIPTION FAR 25.1561 Safety equipment 5 J.A. Dwg: 256010-01/98XN9 (a-e)Emergency equipment is provided and 9 Eng. Order 98XN9-250000 marked. For locations refer to J.A. DWG. FAR 25.1581 General - Airplane flight manuals 11 AFMS 98XN9-201-01 (a-b) Changes to operation limitations are shown in the AFM Supplement. (d) Table of contents is included. FAR 25.1583 Operating limitations 7 Weight and Balance Report MK-14M (a-b) No change to basic T/C. (c) Refer to new Weight and Balance (d-) No change to basic T/C. DEPT.' DATE: 7/6/99 JET AVIATION AG DEPT.: . DATE: 7/6/99 DEPT.: k- DATE: engineering Depart PREPARED: a.--- - CHECKED: af APPROVED: , /tha Seite 33 PROT32