EFTA01123795.pdf

JET AVIATION AG / BASEL, SWITZERLAND NC: B737-700IM S/N: 29273 REV.: IR CERTIFICATION COMPLIANCE No.: 98XN9-102 REG.: VP-BBJ AMDT. 25-77 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 AG DATE: 7/6/99 DEPT.: ' -airi-)N DATE: 7/6/99 DEPT.: DATE: nt -mayO t PREPARED: a g ----- V;:t2 CHECKED: de/W APPROVED: ye.c,c,,M,tr-c? e.,:\ V 1 Seite 1 EFTA01123795 JET AVIATION AG / BASEL, SWITZERLAND A/C: 8737-7001G SIN: 29273 REV.: IR CERTIFICATION COMPLIANCE No.: 98XN9-102 REG.: VP-BW AMDT. 25-77 ISSUED DATE: 7/6/99 WORDING OF REGULATION 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 DEPTJET Np< 1.,O .2ON A : 7/6/99 DEPT.: „ DATE: , . /c.. ini, c.... .ewnt 9 "'acneeporai • PREPARED: 77 _./ Ate; CHECKED: / Zia ea 4 APPROVED:L. , / 4.- CJ Sae 2 EFTA01123796 JET AVIATION AG I BASEL, SWITZERLAND NC: B737-700IG1A S/N: 29273 REV.: IR CERTIFICATION COMPLIANCE No.: 98XN9-102 REG.: VP-BBJ AMDT. 25-77 ISSUED DATE: 7/6/99 WORDING OF REGULATION MOC DOCUMENT DESCRIPTION REVISION STATUS REV. NO PAGES DESCRIPTION REMARKS DATE IR ALL Initial Release 7/6/99 DEPT.:JET *fling AG DATE: 7/6/99 DEPT.: JET an91O14 -P, ATE: 7/6/99 DEPT.: DATE: Froi;:errIng . •opartrnan• EngiritCfrit De PREPARED: rVe.-- CHECKED: . zieleag APPROVED: Seite 3 EFTA01123797 JET AVIATION AG / BASEL, SWITZERLAND NC: B737-700IGV1 S/N: 29273 REV.: IR CERTIFICATION COMPLIANCE No.: 98XN9-102 REG.: VP-BBJ AMDT. 25-77 ISSUED DATE: 3/10/99 WORDING OF REGULATION 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 n -4 ATE: 7/6/99 DEPT.: . DATE: Elva PREPARED: __/;,a(ie.- CHECKED: tee-t-e- APPROVED: - . >114.22.0.-_\ ,/ Serve 4 EFTA01123798 JET AVIATION AG / BASEL, SWITZERLAND A/C: B737-700IGIA S/N: 29273 REV.: IR CERTIFICATION COMPLIANCE No.: 98XN9-102 REG.: VP-BBJ AMDT. 25-77 ISSUED DATE: 7/6/99 WORDING OF REGULATION MOC DOCUMENT DESCRIPTION FAR 25.301 Loads 2 Stress Report 98XN9-104 (a-c) The following load conditions are 3 Groundcheck: 98XN9-105-01 taken into account: 98XN9-105-02 Upward 3.0g, Foreward 9.0g, 98XN9-105-03 Sideward 3.0g and 4.0g on seats, 98XN9-105-04 Downward 6.0g and Rearward 1.5g. 98XN9-105-05 Gust Load Conditions and Decompression 98XN9-105-06 Loads. 98XN9-105-07 The whole installation is calculated and 98XN9-105-08 tested on ground and in flight. 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 7 Weight and Balance Report MK-14 M 10 Supp. Equi. List MK-10M DEPT.*.1E.T - DATE: 7/6/99 DEPTJET WION ATE: 7/6/99 DEPT.: ‘ DATE: AVIATION A Do nt Engineering D kr PREPARED: //~• "ie.' CHECKED: laitt4 APPROVED: A4-1 .5z,,,,ctz..—\ Seite 5 EFTA01123799 JET AVIATION AG / BASEL, SWITZERLAND NC: B737-700IGNA S/N: 29273 REV.: IR CERTIFICATION COMPLIANCE No.: 98XN9-102 REG.: VP-BE3J AMDT. 25-77 ISSUED DATE: 7/6/99 WORDING OF REGULATION MOC DOCUMENT DESCRIPTION FAR 25.303 Factor of safety 2 Stress Report 98XN9-104 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 DEPT.: JE TI ATE: 7/6/99 DEPT.: Engineering Departme ____--- DATE: Er. rt de. PREPARED: / CHECKED: 7 ,i-d-ceei APPROVEDV.. .-i.;\ (4..6.64.-\ Seite 6 EFTA01123800 JET AVIATION AG / BASEL, SWITZERLAND NC: B737-700IGW SIN: 29273 REV.: IR CERTIFICATION COMPLIANCE No.: 98XN9-102 REG.: VP-BBJ AMDT. 25-77 ISSUED DATE: 7/6/99 WORDING OF REGULATION MOC DOCUMENT DESCRIPTION FAR 25.305 Strength and deformation 2 Stress Report 98XN9-104 (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 • ION • 7/6/99 DEPT.: DATE: -.JET Deportment Engineering Depart En De Cbdee PREPARED: 3.1, 9- CHECKED: aiaae-t APPROVED: 4->Z Selte 7 EFTA01123801 JET AVIATION AG / BASEL, SWITZERLAND NC: B737-700IGA S/N: 29273 REV.: IR CERTIFICATION COMPLIANCE No.: 98XN9-102 REG.: VP-BBJ AMDT. 25-77 ISSUED DATE: 7/6/99 WORDING OF REGULATION 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 Refer to FAR 25.301 and 25.305 DEPMJET AVIATION AGDATE: 7/6/99 DEPT.:JET TeroN AGDATE: 7/6/99 DEPT.: DATE: EngirW Enp;neerIng Department n ___ - PREPARED: L/7 /54.et---- CHECKED: 'Zig ee4n APPROVED:p i",7>V4A4C\ Seite 8 EFTA01123802 JET AVIATION AG / BASEL, SWITZERLAND NC: B737-7001GVN S/N: 29273 REV.: IR CERTIFICATION COMPLIANCE No.: 98XN9-102 REG.: VP-BBJ AMDT. 25-77 ISSUED DATE: 7/6/99 WORDING OF REGULATION MOC DOCUMENT DESCRIPTION FAR 25.341 Gust and turbulence loads Refer to FAR 25.301 and 25.305 FAR 25.365 Pressurized compartment loads Amdt 25-0 Refer to FAR 25.301 and 25.305 FAR 25.471 General - Ground loads Refer to FAR 25.301 and 25.305 DEPT:JET AVIATION AG DATE: 7/6/99 DEPTJEr AO DATE: 7/6/99 DEPT.: DATE: Engin wring Department En ' PREPARED: d age-- CHECKED: z ,./ _Sabi APPROVED: 47 P4\ Seite 9 EFTA01123803 JET AVIATION AG / BASEL, SWITZERLAND NC: B737-700IGIA S/N: 29273 REV.: IR CERTIFICATION COMPLIANCE No.: 98XN9-102 REG.: VP-BBJ AMDT. 25-77 ISSUED DATE: 06.07.99 WORDING OF REGULATION MOC DOCUMENT DESCRIPTION FAR 25.561 General-Emergency landing conditions Amdt 25-59 9 Eng. Order: 98XN9-250000 (a-c) Refer to 25.301 for load factor. 2 Stress Report 98XN9-104 (d) Seats are existing or TSO C127 approved 10 Supp. Equip. List MK-10M 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. FAR 25.562 Emergency Landing Dynamic Conditions 10 Supp. Equip. List MK-10M (a),(b),(c),(1),(2),(3),(4),(7),(8) 2 Stress Report 98XN9-104 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 DEPT.:JET m. w -i : 06.07.99 DEPT.: DATE: Engineering D rtme — Enginatt . PREPARED: dee--- CHECKED: asp, APPROVED'• 4/ ' 4 cy/..4-----\,_ / 1. Seite 10 EFTA01123804 JET AVIATION AG / BASEL, SWITZERLAND NC: B737-700IGV% S/N: 29273 REV.: IR CERTIFICATION COMPLIANCE No.: 98XN9-102 REG.: VP-BBJ AMDT. 25-77 ISSUED DATE: 716/99 WORDING OF REGULATION MOC DOCUMENT DESCRIPTION FAR 25.571 Damage Tolerance and Fatigue Evaluation Arndt. 25-0 2 Stress Report 98XN9-104 (a-e) A Damage Tolerance Report is provided of Structure to 25-77 for all antenna installations. FAR 25.581 Lightning protection 10 Mech. Master Dwg. List MK1-01M (a-b) All installed metallic components are bonded to the airframe as noted on dwg. DEPL;ET AVIATION AG DATE: 7/6199 DEPT4E r gyfttiION DATE: 7/6/99 DEPT.: DATE: G / angineoring DepattAent ,.2 Engi PREPARED: 44 A e./..-- CHECKED: -; ,. el(ZieZe ail , z APPROVED:d ,k (sci‘L__\: Seite 11 EFTA01123805 JET AVIATION AG / BASEL, SWITZERLAND A/C: B737-700IG S/N: 29273 REV.: IR CERTIFICATION COMPLIANCE No.: 98XN9-102 REG.: VP-BBJ I AMDT. 25-77 ISSUED DATE: 7/6/99 WORDING OF REGULATION MOC DOCUMENT DESCRIPTION FAR 25.601 General Design and construction 10 Supp. Equip. List MK-10M 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: stoto_ Engineering Department Engi . 0 PREPARED: CHECKED: -- ,, ,-eat),Cat APPROVED: j.. : 1), :Z,:ez c Seite 12 EFTA01123806 JET AVIATION AG / BASEL, SWITZERLAND NC: B737-700IGV1 S/N: 29273 REV.: IR CERTIFICATION COMPLIANCE No.: 98XN9-102 REG.: VP-BBJ AMDT. 25-77 ISSUED DATE: 7/6/99 WORDING OF REGULATION MOC DOCUMENT DESCRIPTION FAR 25.603 Materials 10 Supp. Equip. List MK-10M (a-c)AII Hardware is NAS/AN/MS-Standard 10 Mech. Master Dwg. List MK1-01M 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. FAR 25.605 Fabrication methods J.A. Process Specifications (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. FAR 25.607 Fasteners 10 Supp. Equi. List MK-10M (a-c) All Hardware is NAS/ AN/ MS-Standard Mech. Master Dwg List MK1-01M approved. Locking devices are used in accordance 2 Stress Report 98XN9-104 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 DEPT.: : 7/6/99 DEPT.: DATE: PREPARED: ‘git.— CHECKED: APPROVED: ,,, ,,1—>ith,,-;42N //iea Seite 13 EFTA01123807 JET AVIATION AG / BASEL, SWITZERLAND NC: B737.700IGW S/N: 29273 REV.: IR CERTIFICATION COMPLIANCE No.: 98XN9-102 REG.: VP-BBJ AMDT. 25-77 ISSUED DATE: 7/6/99 WORDING OF REGULATION 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 Stress Report 98XN9-104 (a-e) All Hardware is NAS/ AN/ MS-Standard 10 Mech. Master Dwg List MK-01M approved. Supp. Equip. List MK-10M 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 Stress Report 98XN9-104 (a-c) All special factors are applied in the Stress Report. DEPT.: DATE: 7/6/99 DEPT.: / TE: 7/6/99 DEPT.: DATE: V 1 PREPARED: 6,Z 7 a- - CHECKED: ,e(de-eft APPROVED: ./A, .4./ - liq.6 C.J \ • Seite 14 EFTA01123808 JET AVIATION AG / BASEL, SWITZERLAND NC: B737-700IMM1 S/N: 29273 REV.: IR CERTIFICATION COMPLIANCE No.: 98XN9-102 REG.: VP-BBJ AMDT. 25-77 ISSUED DATE: 7/6/99 WORDING OF REGULATION MOC DOCUMENT DESCRIPTION FAR 25.623 Bearing factor 2 Stress Report 98XN9-104 (a-b) All bearing factors are applied in the Stress Report. FAR 25.625 Fitting factors Amdt 25-59 2 Stress Report 98XN9-104 (a-c) The whole installation is based on experienced designs and approved data. All factors are applied in the Stress Report. (d) Each seat and berth is TSO C127 approved by AMP. FAR 25.771 Pilot Compartment 4 Flightcheck: 98XN9-109-01 (a-d) No Change to basic aircraft (e )Vibritions and noise characteristics are taken into account for all cockpit installation and tested during flight. FAR 25.772 Pilot Comprtment Doors 5 Floorplan 250010-01/98XN9 (a-b) No change to basic aircraft DEPTI€T AVIATION AG DATE: 7/6/99 DEPT.:. ETIrtlION GDATE: 7/6/99 DEPT.: DATE: Engineering De;,:zIrit • 0* t PREPARED: eAle: CHECKED: - ettaiett APPROVED: 'tf -‘\1t.a.e.(.\ Selte 15 EFTA01123809 JET AVIATION AG / BASEL, SWITZERLAND NC: B737-700IGV% S/N: 29273 REV.: IR CERTIFICATION COMPLIANCE No.: 98XN9-102 REG.: VP-BBJ AMDT. 25-77 ISSUED DATE: 06.07.99 WORDING OF REGULATION 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 exis- ting BOEING, TSO C39 or C127approved by AMP or manufactured in accordance with TSO approved production method. FAR 25.787 Stowage compartments 2 Stress Report 98XN9-104 (a-b) The stowage comply with this para- graph, 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 54„wtincrDATE: 06.07.99 DEPT.: , DATE: Engineering Dey,rt t Engi , zer -- ')_. PREPARED: -- CHECKED: /WeVC."6.4 4.7 APPROVED: ci Q2.e;(7-\ Seite 16 EFTA01123810 JET AVIATION AG / BASEL, SWITZERLAND NC: B737-700IG S/N: 29273 REV.: IR CERTIFICATION COMPLIANCE No.: 98XN9-102 REG.: VP-BBJ I AMDT. 25-77 ISSUED DATE: 7/6/99 WORDING OF REGULATION 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 Stress Report 98XN9-104 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 EFTA01123811 JET AVIATION AG / BASEL, SWITZERLAND NC: B737-700IGVi S/N: 29273 REV.: IR CERTIFICATION COMPLIANCE No.: 98XN9-102 REG.: VP-BBJ AMDT. 25-77 ISSUED DATE: 7/6/99 WORDING OF REGULATION 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: 250010-01/98XN9 (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: 250010-01/98XN9 (a-h) No change to basic NC. DEPT.SET AVIATION AG 7/6/99 DEPT;JET - N, ATE: 7/6/99 DEPT.: DATE: DATE: Engineering Doparef, ---