PENN,rAN AENOS~RVICE1INC.
Transcription
PENN,rAN AENOS~RVICE1INC.
I ':-'/ ... -:' " j / . :... PENN,rAN AENOS~RVICE1 INC. ;>,IQC) nA 111 n("'J\[') 1\1r !f'()n" PENN 'fJ\N, I,J y, I.-I!);:! qSO~) - .... 180 H.P. SUPERHAWK (315) 536-2333 ...--------. u_.. FAA APPROVED SUPPLEMENTAL AIRPLANE FLIGHT MANUAL FOR CESSNA REG. NO. SER. NO. 172N ~ ~ ~ This Supplement must be carried in the aircraft when it is modified by the installation of a 180 HP engine and the gross weight is increased in accordance with STCSA703GL. The information contained herein supplements or supersedes the basic placards and markings only in tho~e areas lis~ed. ~ ?' FAA APPROVED:' 1 , .c..6x.',t) {{I~ W. F Horn, Manager Chic go Aircraft Certification Office FAA Central Region DATE: June 11, 1985 PaQe 1 of 4 PENN YAN AERO SERVICE INC. FAA APPROVED SUPPLEMENTALAIRPLANE FLIGHT MANUAL FOR CESSNA 172SERIESAIRCRAFT . .. LOG OF REVISIONS ~ Rev. NQ. A NQ. 4 Description FAA Approved Added performance information to section 5 for clarification Renumbered pages Irwin N Brumer Manager, NYACO APR ,1 3 1994 - Page 2 of 4 \ Penn Yan Aero Service, Inc. Supplemental Airplane Flight Manual for Cessna 172N 2499 Bath Road, Airport Penn Yan, NY 14527-9599 SECTIONI - Limitations A. The following placard must be displayed in full view of the pilot: THIS AIRCRAFT HAS BEEN MODIFIED BY THE INSTALLATION OF A 180 HP ENGINE PER STC SA703GL. IT MUST BE OPERATED AS A NORHALCATEGORY AIRPLANE IN COMPLIANCE WITH THE OPERATING LIMITATIONS AS STATED IN THE FORM OF PLACARDS, MARKINGS AND MANUALS. B. For the N model a"ircraft the following adjacent to the flap position selector placard switch: must be displayed . MAXIMUMFLAP TRAVEL IS 30° C. The following limits apply to the normal category only. - MaximumGross Weight 2550 lbs. C.G. Range 41.0" to 47.3" at 2550 lbs. 35.0" to 47.3" at 1950 lbs. or less Straight line variation between points given. - " FAA APPROVED JUN 111!85 DATED: Pag e.3 of 4- .. Section 3 Emerqency Procedures NO CHANGE Section 4 Normal Procedures NO CHANGE Section 5 Performance Performance of the Cessna 172 series aircraft, when it is modified by the installation of a 180 HP engine and the gross weight is increased, in accordance with STC SA703GL, will be equal to or better than the basic airplane CAUTION:- .. The fuel consumption and range/endurance information originally presented for this model do not apply to this STC modification: increased fuel consumption and reduced range/ endurance can be expected with the 180 hp engine installed. FAA APPROVED DATE: Revised: APR.13 1994 . Page 4 Of 4 [ CURVE NO. 133S1 Furl F-LO\Jvs.PERCENT, RAT[O POJE(\ Ii I/CO LYCOM1 NG 0-360) {BGHP5£R IE5 COMPRE5510N RATIO SPfJRk /1DVllNce - 8, s-o; 1 ' 25° (3Tc. , ,A ., , \) , I A" . 'T 7 1/ :r: / . -.... -I 0 . «\,.( ,vY " .I? .'\j /' - V'J ;; :S .....t, I () -J -. II .. (" 11'\ i}Y "'V I'" -J ,\ L.J .:::> lL. ..... u ./ / / / / I " , . 1/ S-O '0 , 70 80 PER CEN T RFltE D POW'tR .. 10 IDO .Power Chart ....... 111I.AIL TIIIIp. 108.. 10"..... . 111.. . II"..... 1. .. 121.. 70"...... 7'" ..... ... ....... All. ... If ... 1,000 2,000 3,000 59 55 52 48 2290 2310 2330 2350 2370 2390 2410 2430 2440 2460 2480 2500 2500 2520 2540 2560 SL 1,000 2,000 3,000 4,000 5,000 6,000 7,000 45 41 38 34 2370 2390 2410 2430 2460 2470 2520 2540 2560 2580 2580 2600 2620 2640 4,000 5,000 6,000 7,000 8,000 AIL SL IU!II . 2490 2510 31 2450 2530 2600 9,000 10,000 11,000 27 23 19 2470 2490 2510 2550 .. 2570 2590 2620 12,000 16 2530 - - -- 8,000 9,000 10,000 11,000 12,000 .A