+--------------------------------+-------------------------------------+
|                                | ### TCDS NUMBER E00063EN            |
+--------------------------------+-------------------------------------+
|                                | REVISION: 3                         |
+--------------------------------+-------------------------------------+
|                                |                                     |
+--------------------------------+-------------------------------------+
| U.S. DEPARTMENT OF             | DATE: [July 2, 2002]{.underline}    |
| TRANSPORTATION                 |                                     |
+--------------------------------+-------------------------------------+
|                                | GENERAL ELECTRIC COMPANY            |
+--------------------------------+-------------------------------------+
|                                |                                     |
+--------------------------------+-------------------------------------+
| FEDERAL AVIATION               | MODELS:                             |
| ADMINISTRATION                 |                                     |
+--------------------------------+-------------------------------------+
|                                | CF34-8C1; CF34-8C5; CF34-8C5A1;     |
|                                | CF34-8C5B1;                         |
|                                |                                     |
|                                | CF34-8C5A2; CF34-8C5A3;             |
+--------------------------------+-------------------------------------+
| TYPE CERTIFICATE DATA SHEET    | CF34-8D1; CF34-8D3; CF34-8D5;       |
|                                | CF34-8D6                            |
+--------------------------------+-------------------------------------+
|                                | CF34-8E2; CF34-8E2A1; CF34-8E5;     |
|                                | CF34-8E5A1;                         |
|                                |                                     |
|                                | CF34-8E5A2; CF34-8E6; CF34-8E6A1    |
+--------------------------------+-------------------------------------+

Engines of models described herein conforming with this data sheet and
other approved data on file with the Federal Aviation Administration,
meet the minimum standards for use in certificated aircraft in
accordance with pertinent aircraft data sheets and applicable portions
of the Federal Aviation Regulations, provided they are installed,
operated, and maintained as prescribed by the approved manufacturers
manuals and other approved instructions.

TYPE CERTIFICATE (TC) HOLDER: General Electric Aircraft Engines (GE)

1000 Western Avenue

Lynn, Massachusetts 01910

+--------------+--------+--------+--------+--------+--------+--------+
| **I.         | **CF34 | **CF34 | **     | **     | **     | **     |
| MODELS**     | -8C1** | -8C5** | CF34-8 | CF34-8 | CF34-8 | CF34-8 |
|              |        |        | C5A1** | C5B1** | C5A2** | C5A3** |
+--------------+--------+--------+--------+--------+--------+--------+
| TYPE         | Dual   |        |        |        |        |        |
|              | rotor, |        |        |        |        |        |
|              | axial  |        |        |        |        |        |
|              | flow,  |        |        |        |        |        |
|              | high   |        |        |        |        |        |
|              | bypass |        |        |        |        |        |
|              | ratio  |        |        |        |        |        |
|              | tur    |        |        |        |        |        |
|              | bofan; |        |        |        |        |        |
|              | single |        |        |        |        |        |
|              | stage  |        |        |        |        |        |
|              | fan,   |        |        |        |        |        |
|              | ten    |        |        |        |        |        |
|              | stage  |        |        |        |        |        |
|              | axial  |        |        |        |        |        |
|              | compr  |        |        |        |        |        |
|              | essor, |        |        |        |        |        |
|              | a      |        |        |        |        |        |
|              | nnular |        |        |        |        |        |
|              | comb   |        |        |        |        |        |
|              | ustion |        |        |        |        |        |
|              | ch     |        |        |        |        |        |
|              | amber, |        |        |        |        |        |
|              | two    |        |        |        |        |        |
|              | stage  |        |        |        |        |        |
|              | high   |        |        |        |        |        |
|              | pr     |        |        |        |        |        |
|              | essure |        |        |        |        |        |
|              | tu     |        |        |        |        |        |
|              | rbine, |        |        |        |        |        |
|              | four   |        |        |        |        |        |
|              | stage  |        |        |        |        |        |
|              | low    |        |        |        |        |        |
|              | pr     |        |        |        |        |        |
|              | essure |        |        |        |        |        |
|              | tu     |        |        |        |        |        |
|              | rbine, |        |        |        |        |        |
|              | a      |        |        |        |        |        |
|              | thrust |        |        |        |        |        |
|              | re     |        |        |        |        |        |
|              | verser |        |        |        |        |        |
|              | (C     |        |        |        |        |        |
|              | F34-8D |        |        |        |        |        |
|              | and    |        |        |        |        |        |
|              | --8E   |        |        |        |        |        |
|              | models |        |        |        |        |        |
|              | only), |        |        |        |        |        |
|              | aft    |        |        |        |        |        |
|              | core   |        |        |        |        |        |
|              | cowl   |        |        |        |        |        |
|              | (C     |        |        |        |        |        |
|              | F34-8D |        |        |        |        |        |
|              | and    |        |        |        |        |        |
|              | --8E   |        |        |        |        |        |
|              | models |        |        |        |        |        |
|              | only), |        |        |        |        |        |
|              | e      |        |        |        |        |        |
|              | xhaust |        |        |        |        |        |
|              | n      |        |        |        |        |        |
|              | ozzle, |        |        |        |        |        |
|              | st     |        |        |        |        |        |
|              | arter, |        |        |        |        |        |
|              | and a  |        |        |        |        |        |
|              | Full   |        |        |        |        |        |
|              | Aut    |        |        |        |        |        |
|              | hority |        |        |        |        |        |
|              | D      |        |        |        |        |        |
|              | igital |        |        |        |        |        |
|              | Engine |        |        |        |        |        |
|              | C      |        |        |        |        |        |
|              | ontrol |        |        |        |        |        |
|              | (F     |        |        |        |        |        |
|              | ADEC). |        |        |        |        |        |
+--------------+--------+--------+--------+--------+--------+--------+
| RATINGS (See |        |        |        |        |        |        |
| NOTE 5)      |        |        |        |        |        |        |
|              |        |        |        |        |        |        |
| Sea level    |        |        |        |        |        |        |
| static       |        |        |        |        |        |        |
| thrust, lb   |        |        |        |        |        |        |
+--------------+--------+--------+--------+--------+--------+--------+
| Maximum      | 13790  | 14510  | \- -   | 13790  | 14510  | \- -   |
| takeoff (5   |        |        |        |        |        |        |
| min.)        |        |        |        |        |        |        |
|              |        |        |        |        |        |        |
| (See NOTES   |        |        |        |        |        |        |
| 13,15 and    |        |        |        |        |        |        |
| 18)          |        |        |        |        |        |        |
+--------------+--------+--------+--------+--------+--------+--------+
| Normal       | 12670  | 13360  | 13630  | 12670  | 14050  | 14510  |
| takeoff (5   |        |        |        |        |        |        |
| min.)        |        |        |        |        |        |        |
|              |        |        |        |        |        |        |
| (See NOTES   |        |        |        |        |        |        |
| 13 and 15)   |        |        |        |        |        |        |
+--------------+--------+--------+--------+--------+--------+--------+
| Maximum      | 13277  | 13680  | \- -   | 13280  | 13680  | \- -   |
| continuous   |        |        |        |        |        |        |
|              |        |        |        |        |        |        |
| (See NOTE    |        |        |        |        |        |        |
| 13)          |        |        |        |        |        |        |
+--------------+--------+--------+--------+--------+--------+--------+

+--------------+--------+--------+--------+--------+--------+--------+
| CONTROL      |        |        |        |        |        |        |
| STSYEM       |        |        |        |        |        |        |
|              |        |        |        |        |        |        |
| COMPONENT    |        |        |        |        |        |        |
+--------------+--------+--------+--------+--------+--------+--------+
| Fuel         | 4      | \- -   | \- -   | \- -   | \- -   | \- -   |
| Control,     | 120T01 |        |        |        |        |        |
| Woodward     |        |        |        |        |        |        |
|              |        |        |        |        |        |        |
| Governor     |        |        |        |        |        |        |
+--------------+--------+--------+--------+--------+--------+--------+
| Full         | 4      | \- -   | \- -   | \- -   | \- -   | \- -   |
| Authority    | 120T00 |        |        |        |        |        |
| Digital      |        | \- -   | \- -   | \- -   | \- -   | \- -   |
| Engine       | 9      |        |        |        |        |        |
|              | 238M66 | \- -   | \- -   | \- -   | \- -   | \- -   |
| Control      |        |        |        |        |        |        |
| (FADEC),     | 4      | \- -   | \- -   | \- -   | \- -   | \- -   |
|              | 096T33 |        |        |        |        |        |
| Loc          |        |        |        |        |        |        |
| kheed/Martin | 4      |        |        |        |        |        |
|              | 120T04 |        |        |        |        |        |
| Ignition     |        |        |        |        |        |        |
| System       |        |        |        |        |        |        |
|              |        |        |        |        |        |        |
| 2 Ignition   |        |        |        |        |        |        |
| Exciters,    |        |        |        |        |        |        |
|              |        |        |        |        |        |        |
| Unison       |        |        |        |        |        |        |
|              |        |        |        |        |        |        |
| 2 Ignition   |        |        |        |        |        |        |
| Plugs,       |        |        |        |        |        |        |
| Federal      |        |        |        |        |        |        |
|              |        |        |        |        |        |        |
| Mogul        |        |        |        |        |        |        |
|              |        |        |        |        |        |        |
| / Champion   |        |        |        |        |        |        |
|              |        |        |        |        |        |        |
| Fuel Pump,   |        |        |        |        |        |        |
| Argotech     |        |        |        |        |        |        |
+--------------+--------+--------+--------+--------+--------+--------+

+------------------+-------+---+------+---+-------+-------+-------+-------+
| **I. MODELS**    | **    | * |      | * |       | **CF  | **CF  | **CF  |
| **(continued)**  | CF34- | * |      | * |       | 34-8C | 34-8C | 34-8C |
|                  | 8C1** | C |      | C |       | 5B1** | 5A2** | 5A3** |
|                  |       | F |      | F |       |       |       |       |
|                  |       | 3 |      | 3 |       |       |       |       |
|                  |       | 4 |      | 4 |       |       |       |       |
|                  |       | - |      | - |       |       |       |       |
|                  |       | 8 |      | 8 |       |       |       |       |
|                  |       | C |      | C |       |       |       |       |
|                  |       | 5 |      | 5 |       |       |       |       |
|                  |       | * |      | A |       |       |       |       |
|                  |       | * |      | 1 |       |       |       |       |
|                  |       |   |      | * |       |       |       |       |
|                  |       |   |      | * |       |       |       |       |
+------------------+-------+---+------+---+-------+-------+-------+-------+
| FUEL             | Fuel  |   |      |   |       |       |       |       |
|                  | confo |   |      |   |       |       |       |       |
|                  | rming |   |      |   |       |       |       |       |
|                  | to GE |   |      |   |       |       |       |       |
|                  | Jet   |   |      |   |       |       |       |       |
|                  | Fuel  |   |      |   |       |       |       |       |
|                  | Spe   |   |      |   |       |       |       |       |
|                  | cific |   |      |   |       |       |       |       |
|                  | ation |   |      |   |       |       |       |       |
|                  | No.   |   |      |   |       |       |       |       |
|                  | D5    |   |      |   |       |       |       |       |
|                  | 0TF2, |   |      |   |       |       |       |       |
|                  | cu    |   |      |   |       |       |       |       |
|                  | rrent |   |      |   |       |       |       |       |
|                  | revi  |   |      |   |       |       |       |       |
|                  | sion, |   |      |   |       |       |       |       |
|                  | is    |   |      |   |       |       |       |       |
|                  | appli |   |      |   |       |       |       |       |
|                  | cable |   |      |   |       |       |       |       |
|                  | for   |   |      |   |       |       |       |       |
|                  | all   |   |      |   |       |       |       |       |
|                  | mo    |   |      |   |       |       |       |       |
|                  | dels. |   |      |   |       |       |       |       |
|                  | See   |   |      |   |       |       |       |       |
|                  | GEK   |   |      |   |       |       |       |       |
|                  | 1     |   |      |   |       |       |       |       |
|                  | 05094 |   |      |   |       |       |       |       |
|                  | (CF   |   |      |   |       |       |       |       |
|                  | 34-8C |   |      |   |       |       |       |       |
|                  | 1/8C5 |   |      |   |       |       |       |       |
|                  | mod   |   |      |   |       |       |       |       |
|                  | els), |   |      |   |       |       |       |       |
|                  | GEK   |   |      |   |       |       |       |       |
|                  | 1     |   |      |   |       |       |       |       |
|                  | 12044 |   |      |   |       |       |       |       |
|                  | (CF   |   |      |   |       |       |       |       |
|                  | 34-8D |   |      |   |       |       |       |       |
|                  | mod   |   |      |   |       |       |       |       |
|                  | els), |   |      |   |       |       |       |       |
|                  | GEK   |   |      |   |       |       |       |       |
|                  | 1     |   |      |   |       |       |       |       |
|                  | 12034 |   |      |   |       |       |       |       |
|                  | (CF   |   |      |   |       |       |       |       |
|                  | 34-8E |   |      |   |       |       |       |       |
|                  | mod   |   |      |   |       |       |       |       |
|                  | els), |   |      |   |       |       |       |       |
|                  | Oper  |   |      |   |       |       |       |       |
|                  | ating |   |      |   |       |       |       |       |
|                  | Ins   |   |      |   |       |       |       |       |
|                  | truct |   |      |   |       |       |       |       |
|                  | ions, |   |      |   |       |       |       |       |
|                  | for   |   |      |   |       |       |       |       |
|                  | spe   |   |      |   |       |       |       |       |
|                  | cific |   |      |   |       |       |       |       |
|                  | fuels |   |      |   |       |       |       |       |
|                  | app   |   |      |   |       |       |       |       |
|                  | roved |   |      |   |       |       |       |       |
|                  | per   |   |      |   |       |       |       |       |
|                  | the   |   |      |   |       |       |       |       |
|                  | su    |   |      |   |       |       |       |       |
|                  | bject |   |      |   |       |       |       |       |
|                  | speci |   |      |   |       |       |       |       |
|                  | ficat |   |      |   |       |       |       |       |
|                  | ions. |   |      |   |       |       |       |       |
+------------------+-------+---+------+---+-------+-------+-------+-------+
| OIL              | Oil   |   |      |   |       |       |       |       |
|                  | confo |   |      |   |       |       |       |       |
|                  | rming |   |      |   |       |       |       |       |
|                  | to GE |   |      |   |       |       |       |       |
|                  | Spe   |   |      |   |       |       |       |       |
|                  | cific |   |      |   |       |       |       |       |
|                  | ation |   |      |   |       |       |       |       |
|                  | No.   |   |      |   |       |       |       |       |
|                  | D5    |   |      |   |       |       |       |       |
|                  | 0TF1, |   |      |   |       |       |       |       |
|                  | cu    |   |      |   |       |       |       |       |
|                  | rrent |   |      |   |       |       |       |       |
|                  | revi  |   |      |   |       |       |       |       |
|                  | sion, |   |      |   |       |       |       |       |
|                  | is    |   |      |   |       |       |       |       |
|                  | appli |   |      |   |       |       |       |       |
|                  | cable |   |      |   |       |       |       |       |
|                  | for   |   |      |   |       |       |       |       |
|                  | all   |   |      |   |       |       |       |       |
|                  | mo    |   |      |   |       |       |       |       |
|                  | dels. |   |      |   |       |       |       |       |
|                  | See   |   |      |   |       |       |       |       |
|                  | GEK   |   |      |   |       |       |       |       |
|                  | 1     |   |      |   |       |       |       |       |
|                  | 05094 |   |      |   |       |       |       |       |
|                  | (CF   |   |      |   |       |       |       |       |
|                  | 34-8C |   |      |   |       |       |       |       |
|                  | 1/8C5 |   |      |   |       |       |       |       |
|                  | mod   |   |      |   |       |       |       |       |
|                  | els), |   |      |   |       |       |       |       |
|                  | GEK   |   |      |   |       |       |       |       |
|                  | 1     |   |      |   |       |       |       |       |
|                  | 12044 |   |      |   |       |       |       |       |
|                  | (CF   |   |      |   |       |       |       |       |
|                  | 34-8D |   |      |   |       |       |       |       |
|                  | mod   |   |      |   |       |       |       |       |
|                  | els), |   |      |   |       |       |       |       |
|                  | GEK   |   |      |   |       |       |       |       |
|                  | 1     |   |      |   |       |       |       |       |
|                  | 12034 |   |      |   |       |       |       |       |
|                  | (CF   |   |      |   |       |       |       |       |
|                  | 34-8E |   |      |   |       |       |       |       |
|                  | mod   |   |      |   |       |       |       |       |
|                  | els), |   |      |   |       |       |       |       |
|                  | Oper  |   |      |   |       |       |       |       |
|                  | ating |   |      |   |       |       |       |       |
|                  | Ins   |   |      |   |       |       |       |       |
|                  | truct |   |      |   |       |       |       |       |
|                  | ions, |   |      |   |       |       |       |       |
|                  | for   |   |      |   |       |       |       |       |
|                  | spe   |   |      |   |       |       |       |       |
|                  | cific |   |      |   |       |       |       |       |
|                  | oils  |   |      |   |       |       |       |       |
|                  | app   |   |      |   |       |       |       |       |
|                  | roved |   |      |   |       |       |       |       |
|                  | per   |   |      |   |       |       |       |       |
|                  | the   |   |      |   |       |       |       |       |
|                  | su    |   |      |   |       |       |       |       |
|                  | bject |   |      |   |       |       |       |       |
|                  | speci |   |      |   |       |       |       |       |
|                  | ficat |   |      |   |       |       |       |       |
|                  | ions. |   |      |   |       |       |       |       |
+------------------+-------+---+------+---+-------+-------+-------+-------+
| PRINCIPAL        | (D    |   | \- - |   | \- -  | \- -  | **-   | **-   |
| DIMENSIONS AND   | emoun |   |      |   |       |       | -**   | -**   |
| MEASUREMENTS     | table |   | 15   |   | \- -  | (De   |       |       |
|                  | Ass   |   | 1.57 |   |       | mount | \- -  | \- -  |
| Length, inches   | embly |   |      |   | \- -  | ablee |       |       |
|                  | less  |   | 6    |   |       |       | \- -  | \- -  |
| Maximum          | f     |   | 0.66 |   | \- -  | \- -  |       |       |
| diameter, inches | luids |   |      |   |       |       | \- -  | \- -  |
|                  | to    |   | 2780 |   | \- -  | \- -  |       |       |
| Weight, pounds   | fill; |   |      |   |       |       | \- -  | \- -  |
|                  | see   |   | 1    |   | \- -  | \- -  |       |       |
| (includes        | In    |   | 73.9 |   |       |       | \- -  | \- -  |
| residual fuel    | stall |   |      |   | \- -  | \- -  |       |       |
| and oil)         | ation |   | 9    |   |       |       | \- -  | \- -  |
|                  | M     |   | 9.78 |   |       | \- -  |       |       |
| Center of        | anual |   |      |   |       |       | \- -  | \- -  |
| Gravity          | GEK   |   | 9    |   |       | \- -  |       |       |
| Location, inches | 10    |   | 9.35 |   |       |       |       |       |
|                  | 5093) |   |      |   |       |       |       |       |
| Engine Station   |       |   |      |   |       |       |       |       |
|                  | 1     |   |      |   |       |       |       |       |
| Butt Line        | 52.28 |   |      |   |       |       |       |       |
|                  |       |   |      |   |       |       |       |       |
| Water Line       | 60.66 |   |      |   |       |       |       |       |
|                  |       |   |      |   |       |       |       |       |
|                  | 2704  |   |      |   |       |       |       |       |
|                  |       |   |      |   |       |       |       |       |
|                  | 173.2 |   |      |   |       |       |       |       |
|                  |       |   |      |   |       |       |       |       |
|                  | 99.6  |   |      |   |       |       |       |       |
|                  |       |   |      |   |       |       |       |       |
|                  | 99.1  |   |      |   |       |       |       |       |
+------------------+-------+---+------+---+-------+-------+-------+-------+
| **II. MODELS**   | **    |   | **CF |   | **    | **    | **    |       |
|                  | CF34- |   | 34-8 |   | CF34- | CF34- | CF34- |       |
|                  | 8D1** |   | D3** |   | 8D5** | 8D6** | 8E2** |       |
+------------------+-------+---+------+---+-------+-------+-------+-------+
| TYPE             | Dual  |   |      |   |       |       |       |       |
|                  | r     |   |      |   |       |       |       |       |
|                  | otor, |   |      |   |       |       |       |       |
|                  | axial |   |      |   |       |       |       |       |
|                  | flow, |   |      |   |       |       |       |       |
|                  | high  |   |      |   |       |       |       |       |
|                  | b     |   |      |   |       |       |       |       |
|                  | ypass |   |      |   |       |       |       |       |
|                  | ratio |   |      |   |       |       |       |       |
|                  | turb  |   |      |   |       |       |       |       |
|                  | ofan; |   |      |   |       |       |       |       |
|                  | s     |   |      |   |       |       |       |       |
|                  | ingle |   |      |   |       |       |       |       |
|                  | stage |   |      |   |       |       |       |       |
|                  | fan,  |   |      |   |       |       |       |       |
|                  | ten   |   |      |   |       |       |       |       |
|                  | stage |   |      |   |       |       |       |       |
|                  | axial |   |      |   |       |       |       |       |
|                  | c     |   |      |   |       |       |       |       |
|                  | ompre |   |      |   |       |       |       |       |
|                  | ssor, |   |      |   |       |       |       |       |
|                  | an    |   |      |   |       |       |       |       |
|                  | nular |   |      |   |       |       |       |       |
|                  | combu |   |      |   |       |       |       |       |
|                  | stion |   |      |   |       |       |       |       |
|                  | cha   |   |      |   |       |       |       |       |
|                  | mber, |   |      |   |       |       |       |       |
|                  | two   |   |      |   |       |       |       |       |
|                  | stage |   |      |   |       |       |       |       |
|                  | high  |   |      |   |       |       |       |       |
|                  | pre   |   |      |   |       |       |       |       |
|                  | ssure |   |      |   |       |       |       |       |
|                  | tur   |   |      |   |       |       |       |       |
|                  | bine, |   |      |   |       |       |       |       |
|                  | four  |   |      |   |       |       |       |       |
|                  | stage |   |      |   |       |       |       |       |
|                  | low   |   |      |   |       |       |       |       |
|                  | pre   |   |      |   |       |       |       |       |
|                  | ssure |   |      |   |       |       |       |       |
|                  | tur   |   |      |   |       |       |       |       |
|                  | bine, |   |      |   |       |       |       |       |
|                  | a     |   |      |   |       |       |       |       |
|                  | t     |   |      |   |       |       |       |       |
|                  | hrust |   |      |   |       |       |       |       |
|                  | rev   |   |      |   |       |       |       |       |
|                  | erser |   |      |   |       |       |       |       |
|                  | (CF   |   |      |   |       |       |       |       |
|                  | 34-8D |   |      |   |       |       |       |       |
|                  | and   |   |      |   |       |       |       |       |
|                  | --8E  |   |      |   |       |       |       |       |
|                  | m     |   |      |   |       |       |       |       |
|                  | odels |   |      |   |       |       |       |       |
|                  | o     |   |      |   |       |       |       |       |
|                  | nly), |   |      |   |       |       |       |       |
|                  | aft   |   |      |   |       |       |       |       |
|                  | core  |   |      |   |       |       |       |       |
|                  | cowl  |   |      |   |       |       |       |       |
|                  | (CF   |   |      |   |       |       |       |       |
|                  | 34-8D |   |      |   |       |       |       |       |
|                  | and   |   |      |   |       |       |       |       |
|                  | --8E  |   |      |   |       |       |       |       |
|                  | m     |   |      |   |       |       |       |       |
|                  | odels |   |      |   |       |       |       |       |
|                  | o     |   |      |   |       |       |       |       |
|                  | nly), |   |      |   |       |       |       |       |
|                  | ex    |   |      |   |       |       |       |       |
|                  | haust |   |      |   |       |       |       |       |
|                  | no    |   |      |   |       |       |       |       |
|                  | zzle, |   |      |   |       |       |       |       |
|                  | sta   |   |      |   |       |       |       |       |
|                  | rter, |   |      |   |       |       |       |       |
|                  | and a |   |      |   |       |       |       |       |
|                  | Full  |   |      |   |       |       |       |       |
|                  | Auth  |   |      |   |       |       |       |       |
|                  | ority |   |      |   |       |       |       |       |
|                  | Di    |   |      |   |       |       |       |       |
|                  | gital |   |      |   |       |       |       |       |
|                  | E     |   |      |   |       |       |       |       |
|                  | ngine |   |      |   |       |       |       |       |
|                  | Co    |   |      |   |       |       |       |       |
|                  | ntrol |   |      |   |       |       |       |       |
|                  | (FA   |   |      |   |       |       |       |       |
|                  | DEC). |   |      |   |       |       |       |       |
+------------------+-------+---+------+---+-------+-------+-------+-------+
| RATINGS          |       |   |      |   |       |       |       |       |
|                  |       |   |      |   |       |       |       |       |
| (See NOTE 5)     |       |   |      |   |       |       |       |       |
|                  |       |   |      |   |       |       |       |       |
| Sea level static |       |   |      |   |       |       |       |       |
| thrust, lb       |       |   |      |   |       |       |       |       |
+------------------+-------+---+------+---+-------+-------+-------+-------+
| Maximum takeoff  | 13830 |   | 1    |   | 14470 | \- -  | 13300 |       |
| (5 min.)         |       |   | 4240 |   |       |       |       |       |
|                  |       |   |      |   |       |       |       |       |
| (See NOTES 13,15 |       |   |      |   |       |       |       |       |
| and 18)          |       |   |      |   |       |       |       |       |
+------------------+-------+---+------+---+-------+-------+-------+-------+
| Normal takeoff   | 12730 |   | 1    |   | 13280 | \- -  | 12410 |       |
| (5 min.)         |       |   | 3140 |   |       |       |       |       |
|                  |       |   |      |   |       |       |       |       |
| (See NOTES 13    |       |   |      |   |       |       |       |       |
| and 15)          |       |   |      |   |       |       |       |       |
+------------------+-------+---+------+---+-------+-------+-------+-------+
| Maximum          | 13420 |   | 1    |   | 13940 | \- -  | 12540 |       |
| continuous       |       |   | 3870 |   |       |       |       |       |
|                  |       |   |      |   |       |       |       |       |
| (See NOTE 13)    |       |   |      |   |       |       |       |       |
+------------------+-------+---+------+---+-------+-------+-------+-------+
| CONTROL STSYEM   |       |   |      |   |       |       |       |       |
|                  |       |   |      |   |       |       |       |       |
| COMPONENT        |       |   |      |   |       |       |       |       |
+------------------+-------+---+------+---+-------+-------+-------+-------+
| Fuel Control,    | 41    |   | \- - |   | \- -  | \- -  | \- -  |       |
| Woodward         | 20T01 |   |      |   |       |       |       |       |
|                  |       |   | \- - |   | \- -  | \- -  | \- -  |       |
| Governor         | 41    |   |      |   |       |       |       |       |
|                  | 20T00 |   | \- - |   | \- -  | \- -  | \- -  |       |
| Full Authority   |       |   |      |   |       |       |       |       |
| Digital Engine   | 92    |   | \- - |   | \- -  | \- -  | \- -  |       |
|                  | 38M66 |   |      |   |       |       |       |       |
| Control (FADEC), |       |   | \- - |   | \- -  | \- -  | \- -  |       |
|                  | 40    |   |      |   |       |       |       |       |
| Lockheed/Martin  | 96T33 |   |      |   |       |       |       |       |
|                  |       |   |      |   |       |       |       |       |
| Ignition System  | 41    |   |      |   |       |       |       |       |
|                  | 20T04 |   |      |   |       |       |       |       |
| 2 Ignition       |       |   |      |   |       |       |       |       |
| Exciters,        |       |   |      |   |       |       |       |       |
|                  |       |   |      |   |       |       |       |       |
| Unison           |       |   |      |   |       |       |       |       |
|                  |       |   |      |   |       |       |       |       |
| 2 Ignition       |       |   |      |   |       |       |       |       |
| Plugs, Federal   |       |   |      |   |       |       |       |       |
|                  |       |   |      |   |       |       |       |       |
| Mogul            |       |   |      |   |       |       |       |       |
|                  |       |   |      |   |       |       |       |       |
| / Champion       |       |   |      |   |       |       |       |       |
|                  |       |   |      |   |       |       |       |       |
| Fuel Pump,       |       |   |      |   |       |       |       |       |
| Argotech         |       |   |      |   |       |       |       |       |
+------------------+-------+---+------+---+-------+-------+-------+-------+

<table>
<colgroup>
<col style="width: 27%" />
<col style="width: 12%" />
<col style="width: 0%" />
<col style="width: 2%" />
<col style="width: 9%" />
<col style="width: 0%" />
<col style="width: 4%" />
<col style="width: 6%" />
<col style="width: 0%" />
<col style="width: 7%" />
<col style="width: 4%" />
<col style="width: 0%" />
<col style="width: 9%" />
<col style="width: 2%" />
<col style="width: 0%" />
<col style="width: 12%" />
</colgroup>
<tbody>
<tr class="odd">
<td><strong>II. MODELS</strong> <strong>(continued)</strong></td>
<td colspan="3"><strong>CF34-8D1</strong></td>
<td colspan="3"><strong>CF34-8D3</strong></td>
<td colspan="3"><strong>CF34-8D5</strong></td>
<td colspan="3"><strong>CF34-8D6</strong></td>
<td colspan="3"><strong>CF34-8E2</strong></td>
</tr>
<tr class="even">
<td>FUEL</td>
<td colspan="15">Fuel conforming to GE Jet Fuel Specification No.
D50TF2, current revision, is applicable for all models. See GEK 105094
(CF34-8C1/8C5 models), GEK 112044 (CF34-8D models), GEK 112034 (CF34-8E
models), Operating Instructions, for specific fuels approved per the
subject specifications.</td>
</tr>
<tr class="odd">
<td>OIL</td>
<td colspan="15">Oil conforming to GE Specification No. D50TF1, current
revision, is applicable for all models. See GEK 105094 (CF34-8C1/8C5
models), GEK 112044 (CF34-8D models), GEK 112034 (CF34-8E models),
Operating Instructions, for specific oils approved per the subject
specifications.</td>
</tr>
<tr class="even">
<td><p>PRINCIPAL DIMENSIONS AND MEASUREMENTS</p>
<p>Length, inches</p></td>
<td colspan="3" rowspan="7"><p>(FAR 33 Propulsion System; see
Installation Manual GEK 112043)</p>
<p>121.18</p>
<p>62.65</p>
<p>3147.6</p>
<p>174.97</p>
<p>99.28</p>
<p>100.17</p></td>
<td colspan="3" rowspan="7"><p>- -</p>
<p>- -</p>
<p>- -</p>
<p>- -</p>
<p>- -</p>
<p>- -</p>
<p>- -</p></td>
<td colspan="3" rowspan="7"><p>- -</p>
<p>- -</p>
<p>- -</p>
<p>- -</p>
<p>- -</p>
<p>- -</p>
<p>- -</p></td>
<td colspan="3" rowspan="7"><p>- -</p>
<p>- -</p>
<p>- -</p>
<p>- -</p>
<p>- -</p>
<p>- -</p>
<p>- -</p></td>
<td colspan="3" rowspan="7"><p>(FAR 33 Propulsion System; see
Installation Manual GEK 112033)</p>
<p>- -</p>
<p>- -</p>
<p>- -</p>
<p>175.01</p>
<p>99.43</p>
<p>100.07 </p></td>
</tr>
<tr class="odd">
<td>Maximum diameter, inches</td>
</tr>
<tr class="even">
<td><p>Weight, pounds</p>
<p>(includes residual fuel and oil)</p></td>
</tr>
<tr class="odd">
<td>Center of Gravity Location, inches</td>
</tr>
<tr class="even">
<td><blockquote>
<p>Engine Station</p>
</blockquote></td>
</tr>
<tr class="odd">
<td><blockquote>
<p>Butt Line</p>
</blockquote></td>
</tr>
<tr class="even">
<td>Water Line</td>
</tr>
<tr class="odd">
<td><strong>III. MODELS</strong></td>
<td><strong>CF34-8E2A1</strong></td>
<td colspan="3"><strong>CF34-8E5</strong></td>
<td colspan="4"><strong>CF34-8E5A1</strong></td>
<td colspan="3"><strong>CF34-8E5A2</strong></td>
<td colspan="3"><strong>CF34-8E6</strong></td>
<td><strong>CF34-8E6A1</strong></td>
</tr>
<tr class="even">
<td>TYPE</td>
<td colspan="15">Dual rotor, axial flow, high bypass ratio turbofan
single stage fan, ten stage axial compressor, annular combustion
chamber, two stage high pressure turbine, four stage low pressure
turbine, a thrust reverser (CF34-8D and –8E models only), aft core cowl
(CF34-8D and –8E models only), exhaust nozzle, starter, and a Full
Authority Digital Engine Control (FADEC).</td>
</tr>
<tr class="odd">
<td><p>RATINGS (See NOTE 5)</p>
<p>Sea level static thrust, lb</p></td>
<td colspan="2"></td>
<td colspan="3"></td>
<td colspan="2"></td>
<td colspan="3"></td>
<td colspan="3"></td>
<td colspan="2"></td>
</tr>
<tr class="even">
<td><p>Maximum takeoff (5 min.)</p>
<p>(See NOTES 13,15 and 18)</p></td>
<td colspan="2">13300</td>
<td colspan="3">14510</td>
<td colspan="2">- -</td>
<td colspan="3">- -</td>
<td colspan="3">14050</td>
<td colspan="2">- -</td>
</tr>
</tbody>
</table>

+------------------+-------+-------+-------+-------+-------+-------+
| Normal takeoff   | 13300 | 13420 | 14050 | 14510 | 13420 | 14050 |
| (5 min.)         |       |       |       |       |       |       |
|                  |       |       |       |       |       |       |
| (See NOTES 13    |       |       |       |       |       |       |
| and 15)          |       |       |       |       |       |       |
+------------------+-------+-------+-------+-------+-------+-------+

+------------------+-------+-------+-------+-------+-------+-------+
| Maximum          | 12540 | 13520 | \- -  | \- -  | \- -  | \- -  |
| continuous       |       |       |       |       |       |       |
|                  |       |       |       |       |       |       |
| (See NOTE 13)    |       |       |       |       |       |       |
+------------------+-------+-------+-------+-------+-------+-------+

<table style="width:100%;">
<colgroup>
<col style="width: 25%" />
<col style="width: 12%" />
<col style="width: 0%" />
<col style="width: 12%" />
<col style="width: 0%" />
<col style="width: 12%" />
<col style="width: 12%" />
<col style="width: 0%" />
<col style="width: 11%" />
<col style="width: 0%" />
<col style="width: 12%" />
</colgroup>
<tbody>
<tr class="odd">
<td><strong>III. MODELS (cont)</strong></td>
<td colspan="2"><strong>CF34-8E2A1</strong></td>
<td colspan="2"><strong>CF34-8E5</strong></td>
<td><strong>CF34-8E5A1</strong></td>
<td><strong>CF34-8E5A2</strong></td>
<td colspan="2"><strong>CF34-8E6</strong></td>
<td colspan="2"><strong>CF34-8E6A1</strong></td>
</tr>
<tr class="even">
<td>CONTROL SYSTEM COMPONENTS</td>
<td rowspan="3"><p>4120T01</p>
<p>4120T00</p>
<p>9238M66</p>
<p>4096T33</p>
<p>4120T04</p></td>
<td colspan="2" rowspan="3"><p>- -</p>
<p>-</p>
<p>- -</p>
<p>- -</p>
<p>- -</p>
<p>- -</p></td>
<td colspan="2" rowspan="3"><p>- -</p>
<p>- -</p>
<p>- -</p>
<p>- -</p>
<p>- -</p></td>
<td rowspan="3"><p>- -</p>
<p>- -</p>
<p>- -</p>
<p>- -</p>
<p>- -</p></td>
<td colspan="2" rowspan="3"><p>- -</p>
<p>- -</p>
<p>- -</p>
<p>- -</p>
<p>- -</p></td>
<td colspan="2" rowspan="3"><p>- -</p>
<p>- -</p>
<p>- -</p>
<p>- -</p>
<p>- -</p></td>
</tr>
<tr class="odd">
<td><p>Fuel Control,</p>
<p>Woodward Governor</p></td>
</tr>
<tr class="even">
<td><p>Full Authority Digital Engine</p>
<p>Control (FADEC),</p>
<p>Lockheed/Martin</p>
<p>Ignition System</p>
<p>2 Ignition Exciters,</p>
<p>Unison</p>
<p>2 Ignition Plugs,</p>
<p>Federal Mogul / Champion</p>
<p>Fuel Pump,</p>
<p>Argotech</p></td>
</tr>
<tr class="odd">
<td>FUEL</td>
<td colspan="10">Fuel conforming to GE Jet Fuel Specification No.
D50TF2, current revision, is applicable for all models. See GEK 112034
(CF34-8E models), Operating Instructions, for specific fuels approved
per the subject specifications</td>
</tr>
<tr class="even">
<td>OIL</td>
<td colspan="10">Oil conforming to GE Specification No. D50TF1, current
revision, is applicable for all models. See GEK 112034 (CF34-8E models),
Operating Instructions, for specific oils approved per the subject
specifications.</td>
</tr>
<tr class="odd">
<td><p>PRINCIPAL DIMENSIONS AND MEASUREMENTS</p>
<p>Length, inches</p></td>
<td colspan="2" rowspan="7"><p>(FAR 33 Propulsion System; see
Installation Manual GEK 112033)</p>
<p>121.18</p>
<p>62.65</p>
<p>3147.6</p>
<p>175.01</p>
<p>99.43</p>
<p>100.07 </p></td>
<td colspan="2" rowspan="7"><p>- -</p>
<p>- -</p>
<p>- -</p>
<p>- -</p>
<p>- -</p>
<p>- -</p>
<p>- -</p></td>
<td rowspan="7"><p>- -</p>
<p>- -</p>
<p>- -</p>
<p>- -</p>
<p>- -</p>
<p>- -</p>
<p>- -</p></td>
<td colspan="2" rowspan="7"><p>- -</p>
<p>- -</p>
<p>- -</p>
<p>- -</p>
<p>- -</p>
<p>- -</p>
<p>- -</p></td>
<td colspan="2" rowspan="7"><p>- -</p>
<p>- -</p>
<p>- -</p>
<p>- -</p>
<p>- -</p>
<p>- -</p>
<p>- -</p></td>
<td rowspan="7"><p>- -</p>
<p>- -</p>
<p>- -</p>
<p>- -</p>
<p>- -</p>
<p>- -</p>
<p>- -</p></td>
</tr>
<tr class="even">
<td>Maximum diameter, inches</td>
</tr>
<tr class="odd">
<td><p>Weight, pounds</p>
<p>(includes residual fuel and oil)</p></td>
</tr>
<tr class="even">
<td><p>Center of Gravity Location,</p>
<p>inches</p></td>
</tr>
<tr class="odd">
<td><blockquote>
<p>Engine Station</p>
</blockquote></td>
</tr>
<tr class="even">
<td><blockquote>
<p>Butt Line</p>
<p>Water Line</p>
</blockquote></td>
</tr>
<tr class="odd">
<td></td>
</tr>
</tbody>
</table>

+------------------------+---------------------------------------------+
| CERTIFICATION BASIS:   | 1\) CF34-8C1-Federal Aviation Regulation    |
|                        | Part 33, effective February 1, 1965, as     |
|                        |                                             |
|                        | amended by amendments 33-1 through 33-19,   |
|                        | and Equivalent Safety Finding               |
|                        |                                             |
|                        | with respect to the following regulations:  |
|                        | 33.77(a) and 33.77(b) Foreign               |
|                        |                                             |
|                        | Object Ingestion -- Birds                   |
|                        |                                             |
|                        | 2\) CF34-8C5 (All Models), CF34-8D (All     |
|                        | Models) and CF34-8E (All Models) -          |
|                        |                                             |
|                        | Federal Aviation Regulations (FAR) Part 33, |
|                        | effective March 26, 1998, including         |
|                        |                                             |
|                        | Amendments 33-1 through 33-20               |
|                        |                                             |
|                        | 3\) All Engine models- Federal Aviation     |
|                        | Regulations (FAR) Part 34,                  |
|                        |                                             |
|                        | Amendment 3 effective February 3, 1999.     |
|                        | ICAO Emissions Standards,                   |
|                        |                                             |
|                        | Annex 16, Volume 2, Second Edition 1993,    |
|                        | Part 3, Chapter 2 is also part              |
|                        |                                             |
|                        | of this basis.                              |
|                        |                                             |
|                        | > Type Certificate                          |
|                        |                                             |
|                        | [Model]{.underline} [Date of                |
|                        | Application]{.underline} [No. E00063EN      |
|                        | Issued/Amended]{.underline}                 |
|                        |                                             |
|                        | CF34-8C1 May 1, 1997 November 30, 1999      |
|                        |                                             |
|                        | CF34-8C5 May 31, 2000 April 12, 2002        |
|                        |                                             |
|                        | CF34-8C5A1 May 31, 2000 April 12, 2002      |
|                        |                                             |
|                        | CF34-8C5B1 May 31, 2000 April 12, 2002      |
|                        |                                             |
|                        | CF34-8C5A2 May 31, 2000 April 12, 2002      |
|                        |                                             |
|                        | CF34-8C5A3 May 31, 2000 April 12, 2002      |
|                        |                                             |
|                        | CF34-8D1 May 31, 2000 April 12, 2002        |
|                        |                                             |
|                        | CF34-8D3 May 31, 2000 April 12, 2002        |
|                        |                                             |
|                        | CF34-8D5 May 31, 2000 April 12, 2002        |
|                        |                                             |
|                        | CF34-8D6 May 31, 2000 April 12, 2002        |
|                        |                                             |
|                        | CF34-8E2 May 31, 2000 April 12, 2002        |
|                        |                                             |
|                        | CF34-8E2A1 May 31, 2000 April 12, 2002      |
|                        |                                             |
|                        | CF34-8E5 May 31, 2000 April 12, 2002        |
|                        |                                             |
|                        | CF34-8E5A1 May 31, 2000 April 12, 2002      |
|                        |                                             |
|                        | CF34-8E5A2 May 31, 2000 April 12, 2002      |
|                        |                                             |
|                        | CF34-8E6 May 31, 2000 April 12, 2002        |
|                        |                                             |
|                        | CF34-8E6A1 May 31, 2000 April 12, 2002      |
+------------------------+---------------------------------------------+
| PRODUCTION CERTIFICATE | CF34-8C1 Production Certificate No. 108     |
+------------------------+---------------------------------------------+

  -----------------------------------------------------------------------
  **NOTES**

  -----------------------------------------------------------------------

Notes 1 through 22 applicable to models as specified

**NOTE** **1.** Maximum permissible engine operating speeds for the
engine rotors are as follows:

+--------------------------+-------+-------+-------+-------+-------+
|                          | *     | *     | **[CF | **[CF |       |
|                          | *[CF3 | *[CF3 | 34-8D | 34-8E |       |
|                          | 4-8C1 | 4-8C5 | ]{.un | ]{.un |       |
|                          | ]{.un | (all  | derli | derli |       |
|                          | derli | mo    | ne}** | ne}** |       |
|                          | ne}** | dels) |       |       |       |
|                          |       | ]{.un | **    | **    |       |
|                          |       | derli | [(all | [(all |       |
|                          |       | ne}** | mo    | mo    |       |
|                          |       |       | dels) | dels) |       |
|                          |       |       | ]{.un | ]{.un |       |
|                          |       |       | derli | derli |       |
|                          |       |       | ne}** | ne}** |       |
+--------------------------+-------+-------+-------+-------+-------+
| Low pressure rotor (N1), |       |       |       |       |       |
| rpm                      |       |       |       |       |       |
+--------------------------+-------+-------+-------+-------+-------+
| Maximum takeoff          | 7360  | 7360  | 7360  | 7360  |       |
+--------------------------+-------+-------+-------+-------+-------+
| > Normal takeoff         | 7247  | 7360  | 7360  | 7360  |       |
+--------------------------+-------+-------+-------+-------+-------+
| Maximum continuous       | 7360  | 7360  | 7360  | 7360  |       |
+--------------------------+-------+-------+-------+-------+-------+
|                          |       |       |       |       |       |
+--------------------------+-------+-------+-------+-------+-------+
| High pressure rotor      |       |       |       |       |       |
| (N2), rpm                |       |       |       |       |       |
+--------------------------+-------+-------+-------+-------+-------+
| > Maximum takeoff        | 17710 | 17710 | 17710 | 17710 |       |
+--------------------------+-------+-------+-------+-------+-------+
| > Normal takeoff         | 17515 | 17710 | 17710 | 17710 |       |
+--------------------------+-------+-------+-------+-------+-------+
|                          |       |       |       |       |       |
+--------------------------+-------+-------+-------+-------+-------+
| Maximum continuous       | 17437 | 17470 | 17470 | 17470 |       |
+--------------------------+-------+-------+-------+-------+-------+

Refer to GE Engine Manual GEK 105091 (CF34-8C1/8C5 models), GEK 112041
(CF34-8D models), GEK 112031 (CF34-8E models) and other manual or
inspection requirements when limits are exceeded.

100 percent N1 rotor speed is 7,400 rpm, 100 percent N2 rotor speed is
17,820 rpm.

**NOTE** **2.** Maximum permissible temperatures are as follows:

Interturbine temperature (T45)\*, °F(°C)

+-----------------------+--------+--------+--------+--------+--------+
|                       | [CF3   | [CF3   | [CF34- | [CF34- | [CF34- |
|                       | 4-8C1] | 4-8C5] | 8C5A1] | 8C5B1] | 8C5A2] |
|                       | {.unde | {.unde | {.unde | {.unde | {.unde |
|                       | rline} | rline} | rline} | rline} | rline} |
+-----------------------+--------+--------+--------+--------+--------+
| Maximum takeoff (5    | 1760   | 1814   | \- -   | \- -   | \- -   |
| min) See Note 18      | (96    | (990)  |        |        |        |
|                       | 0)\*\* |        |        |        |        |
+-----------------------+--------+--------+--------+--------+--------+
| > Maximum takeoff (2  | 1794   | 1843   | \- -   | \- -   | \- -   |
| > min. out of a total | (97    | (1006) |        |        |        |
| > of 5 minutes)       | 9)\*\* |        |        |        |        |
| > \*\*\*              |        |        |        |        |        |
+-----------------------+--------+--------+--------+--------+--------+
| > Normal takeoff (5   | 1689   | 1736   | 1754   | 1738   | 1783   |
| > min)                | (92    | (947)  | (957)  | (948)  | (973)  |
|                       | 0)\*\* |        |        |        |        |
+-----------------------+--------+--------+--------+--------+--------+
| > Normal takeoff (2   | 1723   | 1765   | 1783   | 1767   | 1812   |
| > min. out of a total | (93    | (963)  | (973)  | (964)  | (989)  |
| > of 5 minutes)\*\*\* | 9)\*\* |        |        |        |        |
+-----------------------+--------+--------+--------+--------+--------+
| Maximum continuous    | 1701   | 1760   | \- -   | \- -   | \- -   |
|                       | (92    | (960)  |        |        |        |
|                       | 7)\*\* |        |        |        |        |
+-----------------------+--------+--------+--------+--------+--------+
|                       |        |        |        |        |        |
+-----------------------+--------+--------+--------+--------+--------+
|                       |        |        |        |        |        |
+-----------------------+--------+--------+--------+--------+--------+
|                       |        |        |        |        |        |
+-----------------------+--------+--------+--------+--------+--------+
|                       | [CF34- | [CF3   | [CF3   | [CF3   | [CF3   |
|                       | 8C5A3] | 4-8D1] | 4-8D3] | 4-8D5] | 4-8D6] |
|                       | {.unde | {.unde | {.unde | {.unde | {.unde |
|                       | rline} | rline} | rline} | rline} | rline} |
+-----------------------+--------+--------+--------+--------+--------+
| Maximum takeoff (5    | 1814   | \- -   | \- -   | \- -   | \- -   |
| min) See Note 18      | (990)  |        |        |        |        |
+-----------------------+--------+--------+--------+--------+--------+
| > Maximum takeoff (2  | 1843   | \- -   | \- -   | \- -   | \- -   |
| > min. .out of a      | (1006) |        |        |        |        |
| > total of 5          |        |        |        |        |        |
| > minutes)\*\*\*      |        |        |        |        |        |
+-----------------------+--------+--------+--------+--------+--------+
| > Normal takeoff (5   | 1814   | 1739   | \- -   | 1733   | \- -   |
| > min)                | (990)  | (948)  |        | (945)  |        |
+-----------------------+--------+--------+--------+--------+--------+
| > Normal takeoff (2   | 1843   | 1768   | \- -   | 1762   | \- -   |
| > min. . out of a     | (1006) | (964)  |        | (961)  |        |
| > total of 5          |        |        |        |        |        |
| > minutes)\*\*\*      |        |        |        |        |        |
+-----------------------+--------+--------+--------+--------+--------+
| Maximum continuous    | 1760   | \- -   | \- -   | \- -   | \- -   |
|                       | (960)  |        |        |        |        |
+-----------------------+--------+--------+--------+--------+--------+

**NOTE 2. (continued)** Maximum permissible temperatures are as follows:

Interturbine temperature (T45)\*, °F(°C)

+-----------------------+--------+--------+--------+--------+--------+
|                       | [CF3   | [CF34- | [CF3   | [CF34- | [CF34- |
|                       | 4-8E2] | 8E2A1] | 4-8E5] | 8E5A1] | 8E5A2] |
|                       | {.unde | {.unde | {.unde | {.unde | {.unde |
|                       | rline} | rline} | rline} | rline} | rline} |
+-----------------------+--------+--------+--------+--------+--------+
| Maximum takeoff (5    | 1814   | \- -   | \- -   | \- -   | \- -   |
| min) See Note 18      | (990)  |        |        |        |        |
+-----------------------+--------+--------+--------+--------+--------+
| > Maximum takeoff (2  | 1843   | \- -   | \- -   | \- -   | \- -   |
| > min. out of a total | (1006) |        |        |        |        |
| > of 5 minutes)\*\*\* |        |        |        |        |        |
+-----------------------+--------+--------+--------+--------+--------+
| > Normal takeoff (5   | 1755   | 1814   | 1740(  | 1783   | 1814   |
| > min)                | (957)  | (990)  | 949)   | (973)  | (990)  |
+-----------------------+--------+--------+--------+--------+--------+
| > Normal takeoff (2   | 1784   | 1843   | 1769   | 1812   | 1843   |
| > min. out of a total | (973)  | (1006) | (965)  | (989)  | (1006) |
| > of 5 minutes)\*\*\* |        |        |        |        |        |
+-----------------------+--------+--------+--------+--------+--------+
| Maximum continuous    | 1760   | \- -   | \- -   | \- -   | \- -   |
|                       | (960)  |        |        |        |        |
+-----------------------+--------+--------+--------+--------+--------+
|                       |        |        |        |        |        |
+-----------------------+--------+--------+--------+--------+--------+
|                       |        |        |        |        |        |
+-----------------------+--------+--------+--------+--------+--------+
|                       | [CF3   | [CF34- |        |        |        |
|                       | 4-8E6] | 8E6A1] |        |        |        |
|                       | {.unde | {.unde |        |        |        |
|                       | rline} | rline} |        |        |        |
+-----------------------+--------+--------+--------+--------+--------+
| Maximum takeoff (5    | 1814   | \- -   | ##     | ##     | ##     |
| min) See Note 18      | (990)  |        |        |        |        |
+-----------------------+--------+--------+--------+--------+--------+
| > Maximum takeoff (2  | 1843   | \- -   |        |        |        |
| > min. out of a total | (1006) |        |        |        |        |
| > of 5 minutes)\*\*\* |        |        |        |        |        |
+-----------------------+--------+--------+--------+--------+--------+
| > Normal takeoff (5   | 1771   | 1814   |        |        |        |
| > min)                | (966)  | (990)  |        |        |        |
+-----------------------+--------+--------+--------+--------+--------+
| > Normal takeoff (2   | 1800   | 1843   |        |        |        |
| > min. out of a total | (982)  | (1006) |        |        |        |
| > of 5 minutes)\*\*\* |        |        |        |        |        |
+-----------------------+--------+--------+--------+--------+--------+
| Maximum continuous    | 1760   | \- -   |        |        |        |
|                       | (960)  |        |        |        |        |
+-----------------------+--------+--------+--------+--------+--------+

\*The interturbine temperature is measured by 5 probes (10
thermocouples) mounted in the low pressure turbine casing.

\*\* For the CF34-8C1 engine model, maximum takeoff, normal takeoff and
maximum continuous T45 limits may be exceeded transiently as a result of
OBV activation provided T45 does not exceed 1869°F (1021°C) for 30
seconds, and does not exceed a temperature limit that ramps from 1869°F
(1021°C) to 1794°F (979°C) over the next 30 seconds, as defined in GE
Operating Instructions GEK 105094. The total number of transient
occurrences as a result of OBV activation above a T45 of 1794°F (979°C)
is limited to a maximum of 10 occurrences as defined in GE Engine Manual
GEK 105091.

\*\*\* The 2-minute interturbine temperature (T4.5) limits (2 minutes
out of 5 minutes takeoff time) are intended to cover engine T4.5
overshoot characteristics which occur during engine stabilization at
constant Takeoff thrust.

For the CF34-8C1 engine model, additional transient temperature and time
limits for starting are defined in GE Operating Instructions GEK 105094.

Refer to GE Engine Manual GEK 105091 (CF34-8C1/8C5 models), GEK 112041
(CF34-8D models), GEK 112031 (CF34-8E models) for inspection
requirements when limits are exceeded.

Oil tank temperatures\*\*\*\*, °F (°C)

  --------------------------- -------- -------- -------- -------- --------
  **ALL MODELS**                                                  

  Continuous operation        311                                 
                              (155)                               

  Transient operation         325                                 
                              (163)                               

  \*\*\*\*Transient operation                                     
  above 311° F (155º C) is                                        
  limited to 15 minutes.                                          
  --------------------------- -------- -------- -------- -------- --------

Fuel inlet temperature (at engine fuel filter inlet), °F (°C)

+---+------------------------+--------+--------+------+-------+----------+
| * |                        | #      | #      |      |       |          |
| * |                        |        |        |      |       |          |
| A |                        |        |        |      |       |          |
| L |                        |        |        |      |       |          |
| L |                        |        |        |      |       |          |
| M |                        |        |        |      |       |          |
| O |                        |        |        |      |       |          |
| D |                        |        |        |      |       |          |
| E |                        |        |        |      |       |          |
| L |                        |        |        |      |       |          |
| S |                        |        |        |      |       |          |
| * |                        |        |        |      |       |          |
| * |                        |        |        |      |       |          |
+---+------------------------+--------+--------+------+-------+----------+
| C |                        |        |        |      |       |          |
| o |                        |        |        |      |       |          |
| n |                        |        |        |      |       |          |
| t |                        |        |        |      |       |          |
| i |                        |        |        |      |       |          |
| n |                        |        |        |      |       |          |
| u |                        |        |        |      |       |          |
| o |                        |        |        |      |       |          |
| u |                        |        |        |      |       |          |
| s |                        |        |        |      |       |          |
| o |                        |        |        |      |       |          |
| p |                        |        |        |      |       |          |
| e |                        |        |        |      |       |          |
| r |                        |        |        |      |       |          |
| a |                        |        |        |      |       |          |
| t |                        |        |        |      |       |          |
| i |                        |        |        |      |       |          |
| o |                        |        |        |      |       |          |
| n |                        |        |        |      |       |          |
+---+------------------------+--------+--------+------+-------+----------+
|   | > Jet A, Jet A1, Jet B | 250    |        |      |       |          |
|   |                        | (121)  |        |      |       |          |
+---+------------------------+--------+--------+------+-------+----------+
|   | > JP8                  | 250    |        |      |       |          |
|   |                        | (121)  |        |      |       |          |
+---+------------------------+--------+--------+------+-------+----------+
|   | > JP5                  | 250    |        |      |       |          |
|   |                        | (121)  |        |      |       |          |
+---+------------------------+--------+--------+------+-------+----------+
|   | > JP4, JP4/JP5 mixture | 250    |        |      |       |          |
|   |                        | (121)  |        |      |       |          |
+---+------------------------+--------+--------+------+-------+----------+
|   | > Ground Operation     | 250    |        |      |       |          |
|   |                        | (121)  |        |      |       |          |
+---+------------------------+--------+--------+------+-------+----------+

**NOTE** **3.** FUEL AND OIL PRESSURE LIMITS

Fuel: At engine pump inlet: minimum pressure of 5 PSID above the true
vapor pressure of the fuel with a vapor/liquid ratio of zero with
aircraft boost operative. Operating range 5 PSIG to 50 PSIG. At engine
motive flow discharge: minimum pressure of 150 PSIG at idle or above.
Operating range is 150 PSIG to 800 PSIG. See GE Installation Manual GEK
105093 (CF34-8C1/8C5 models), GEK 112043 (CF34-8D models), GEK 112033
(CF34-8E models) for additional limits.

Oil: At idle on the ground, 25 PSID minimum to 60 PSID maximum. At
takeoff, 45 PSID minimum to 95 PSID maximum. Operating range, 25 PSID to
95 PSID. See GE Installation Manual GEK 105093 (CF34-8C1/8C5 models),
GEK 112043 (CF34-8D models), GEK 112033 (CF34-8E models) for additional
limits.

**NOTE** **4.** ACCESSORY DRIVE PROVISIONS (ALL MODELS)

+--------+---------+------+-----+-------+---------+---+------+-----+
| Acc    | L       | S    | HP  | Dire  | Torque  | M | Over | Sh  |
| essory | ocation | peed | (   | ction | (lb-in) | a | hung | ear |
|        | on AGB  |      | Rat | Of    |         | x |      | Tor |
|        | Axis    | (    | ed) | Rot   | Static  | . | Mo   | que |
|        |         | rpm) |     | ation | / Cont  | A | ment |     |
|        |         |      |     |       | /       | c |      | (   |
|        |         |      |     | f     | O       | c | (lb  | lb- |
|        |         |      |     | acing | verload | . | -in) | in) |
|        |         |      |     | AGB   |         | W |      |     |
|        |         |      |     |       |         | t |      |     |
|        |         |      |     |       |         | . |      |     |
|        |         |      |     |       |         | ( |      |     |
|        |         |      |     |       |         | l |      |     |
|        |         |      |     |       |         | b |      |     |
|        |         |      |     |       |         | ) |      |     |
+--------+---------+------+-----+-------+---------+---+------+-----+
| Lub    | Axis-C  | 7898 | 6   | CCW   | 300     | 1 | 33   | 7   |
| e/Scav | Fwd     |      |     |       | /48/ NA | 0 |      | 50- |
| O      |         |      |     |       | (1)     | . |      | 850 |
| ilPump |         |      |     |       |         | 3 |      |     |
+--------+---------+------+-----+-------+---------+---+------+-----+
| IDG    | Axis-C  | 7898 | 7   | CW    | 675 (1) | 8 | 720  | 314 |
|        | Aft     |      | 4.8 |       | /597/   | 1 | Max  | 4-3 |
|        |         |      | (2) |       | 1129 (5 | . | imum | 648 |
|        |         |      |     |       | min)(4) | 2 |      |     |
|        |         |      |     |       |         | ( |      |     |
|        |         |      |     |       | 1605 (5 | 6 |      |     |
|        |         |      |     |       | sec)(4) | ) |      |     |
+--------+---------+------+-----+-------+---------+---+------+-----+
| Air    | Axis-D  | 1    | N/A | CW    | 2112,   | 2 | 113  | 630 |
| T      | Aft     | 2234 |     |       | 4200    | 7 |      | 0-7 |
| urbine |         |      |     |       | (3) /   | . |      | 500 |
| S      |         |      |     |       | NA / NA | 7 |      |     |
| tarter |         |      |     |       |         |   |      |     |
+--------+---------+------+-----+-------+---------+---+------+-----+
| Hyd    | Axis-G  | 4825 | 30  | CW    | 573 (1) | 1 | 38.4 | 2   |
| raulic | Fwd     |      |     |       | (5) /   | 3 |      | 004 |
| Pump   |         |      |     |       | 392 /   | . |      | ma  |
|        |         |      |     |       | 670     | 9 |      | xi- |
|        |         |      |     |       |         | D |      | mum |
|        |         |      |     |       |         | r |      |     |
|        |         |      |     |       |         | y |      |     |
+--------+---------+------+-----+-------+---------+---+------+-----+
| Alte   | Axis-E  | 8103 | 4   | CCW   | NA / NA | 3 | 2.6  | N/A |
| rnator | Aft     |      |     |       | / NA    | . |      |     |
|        |         |      |     |       |         | 0 |      |     |
+--------+---------+------+-----+-------+---------+---+------+-----+
| Fuel   | Axis-F  | 8319 | 40  | CW    | 180 (1) | 2 | 113  | 12  |
| Pump   | Aft     |      |     |       | /303/NA | 3 |      | 55- |
|        |         |      |     |       |         |   |      |     |
|        |         |      |     |       |         |   |      | 1   |
|        |         |      |     |       |         |   |      | 380 |
+--------+---------+------+-----+-------+---------+---+------+-----+

CW - Clockwise CCW - Counter Clockwise

Accessory Speeds are based on Core Speed: 17000 rpm

> \(1\) -40° F SLS
>
> \(2\) HP is constant over the operating range with slight variations
> due to changes in efficiency. HP extraction is 74.8 HP at 7898 rpm
> (pad speed) and 73.5 HP at 4618 rpm (pad speed). The 5 minute overload
> rating is 82.7 HP and the 5 second overload rating is 117.6 HP.
>
> \(3\) 2112 in-lbs at 59° F SLS, 4200 in-lbs at --40° F SLS
>
> \(4\) Overload at 4618 rpm (pad speed)

(5) 573 in-lbs at 626 rpm (pad speed)

(6) Includes oil and V band coupling

**NOTE** **5.** Engine ratings are based on calibrated test stand
performance under the following conditions:

1.  Static sea level standard conditions of 59° F and 29.92 inches Hg.

2.  No aircraft accessory loads or air extraction.

3.  No anti-icing; no inlet distortion; no inlet screen losses; and 100%
    ram recovery.

4.  Inlet bellmouth and cowl system as described in GE Installation
    Manual GEK 105093 (CF34-8C1/8C5 models), GEK 112043 (CF34-8D
    models), GEK 112033 (CF34-8E models).

5.  Specified fuel having an average lower heating value of 18,500
    BTU/lb (CF34-8C1/-8C5 models); 18,550 BTU/lb (CF34-8D and --8E
    models); specified lube oil.

**NOTE** **6.** Air Bleed Extraction - maximum customer air bleed
extraction is as follows: Customer bleed air is available from either
stages 6 or 10 (compressor discharge) of the compressor at all operating
conditions at or above idle. (No compressor bleed is permitted below
idle.). Customer bleed is scheduled to switch from stage 10 bleed at low
power operation to stage 6 bleed at high power operation as described in
GE Installation Manual GEK 105093 (CF34-8C1/8C5 models), GEK 112043
(CF34-8D models), GEK 112033 (CF34-8E models).

[Location]{.underline} [Maximum Demonstrated Bleed Air (% of Total
Compressor Airflow)]{.underline}

CF34-8C1 CF34-8C5 CF34-8D CF34-8E

(all models) (all models) (all models)

Compressor Stage 6 8 8 8 8

Compressor Stage 10 (Compressor Discharge) 12.75 12.75 12.75 12.0

Maximum Allowable Bleed \-\-- 12.75 12.75 12.0

**NOTE** **7.** A minimum core speed (N2) must be maintained to ensure
engine operation in icing conditions. The FADEC Power Management
controls ground and flight idle core speeds above the minimum speed
demonstrated for FAR 33.68, Induction System Icing. At low ambient
temperatures, the minimum permissible ground and flight idle speeds
correspond to N2=58.47% (9,940 rpm) which is a non-adjustable limit,
preset in the FADEC Power Management schedules. As ambient temperatures
increase, the minimum permissible core speed increases as scheduled by
the FADEC Power Management based upon N2 or PS3 control schedules.

**NOTE** **8.** The maximum permissible inlet distortion for these
engines is specified in GE Installation Manual GEK 105093 (CF34-8C1/8C5
models), GEK 112043 (CF34-8D models), GEK 112033 (CF34-8E models).

**NOTE** **9.** For the CF34-8C1 and the CF34-8C5 model series, the FAR
33 engine type design definition is provided by:

Model List CF34**-**8C1G01 (Left Hand Demountable Engine)

Model List CF34-8C1G02 (Right Hand Demountable Engine)

Model List CF34**-**8C5G01 (Left Hand Demountable Engine)

Model List CF34-8C5G02 (Right Hand Demountable Engine)

Model List CF34**-**8C5A1G01 (Left Hand Demountable Engine)

Model List CF34-8C5A1G02 (Right Hand Demountable Engine)

Model List CF34**-**8C5B1G01 (Left Hand Demountable Engine)

Model List CF34-8C5B1G02 (Right Hand Demountable Engine)

Model List CF34**-**8C5A2G01 (Left Hand Demountable Engine)

Model List CF34-8C5A2G02 (Right Hand Demountable Engine)

Model List CF34**-**8C5A3G01 (Left Hand Demountable Engine)

Model List CF34-8C5A3G02 (Right Hand Demountable Engine)

For the CF34-8D and CF34-8E model series, the engine manufacturer
supplies the Nacelle System. The following Aft Core Cowl and Thrust
Reverser systems, which are a part of this Nacelle system, have been
certified for the listed engine models under this type certificate in
accordance with Federal Aviation Regulation (FAR), Part 33. The FAR 33
engine type design definition is provided by:

  ----------------- ----------------- ----------------- -----------------
                    **ENGINE MODEL    **AFT CORE COWL   **THRUST REVERSER
                    LIST**            PARTS LIST**      PARTS LIST**

                    CF34-8D1          14F0001           14G0001

                    CF34-8D3          14F0001           14G0001

                    CF34-8D5          14F0001           14G0001

                    CF34-8D6          14F0001           14G0001

                    CF34-8E2          15F0001           15G0001

                    CF34-8E2A1        15F0001           15G0001

                    CF34-8E5          15F0001           15G0001

                    CF34-8E5A1        15F0001           15G0001

                    CF34-8E5A2        15F0001           15G0001

                    CF34-8E6          15F0001           15G0001

                    CF34-8E6A1        15F0001           15G0001
  ----------------- ----------------- ----------------- -----------------

**NOTE** **10.** Life limits, established for critical components, are
published in FAA approved GE Engine Manual GEK 105091 (CF34-8C1/8C5
models), GEK 112041 (CF34-8D models), GEK 112031 (CF34-8E models).

**NOTE** **11.** Recommended maintenance inspection intervals are
published in GE Engine Manual GEK 105091 (CF34-8C1/8C5 models), GEK
112041 (CF34-8D models), GEK 112031 (CF34-8E models).

**NOTE** **12.** The operating temperature limit for specific components
and accessories specified in GE Installation Manual GEK 105093
(CF34-8C1/8C5 models), GEK 112043 (CF34-8D models), GEK 112033 (CF34-8E
models) must be observed when installing the engine.

**NOTE** **13.** For CF34-8C1, CF34-8C5 (all models), CF34-8D (all
models) and CF34-8E (all models), static thrusts at sea level are rated
at 86ºF ambient temperature and below for normal takeoff and maximum
takeoff. Maximum Continuous thrust is rated at 77ºF and below at cruise
altitudes. The computer performance decks for calculating engine
performance are as follows:

[Engine Model]{.underline} [Computer Deck No.]{.underline}

CF34-8C1 L0073A

CF34-8C5 G0175C

CF34-8C5A1 G0175C

CF34-8C5B1 L0073A

CF34-8C5A2 G0175C

CF34-8C5A3 G0175C

CF34-8D1 G0175E

CF34-8D3 G0175E

CF34-8D5 G0175E

CF34-8D6 G0175E

CF34-8E2 G0175D

CF34-8E2A1 G0175D

CF34-8E5 G0175D

CF34-8E5A1 G0175D

CF34-8E5A2 G0175D

CF34-8E6 G0175D

CF34-8E6A1 G0175D

**NOTE** **14.** CF34-8C1, CF34-8C5 (all models), CF34-8D (all models)
and CF34-8E (all models), engines comply with the applicable fuel
venting and exhaust emission requirements of Part 34, Amendment 3,
effective February 3, 1999.

**NOTE** **15.** The time limit at the normal takeoff rating is five
minutes and shall include any time accumulated above the normal takeoff
rating.

**NOTE** **16.** TIME LIMITED DISPATCH CRITERIA

> Criteria pertaining to the dispatch and maintenance requirements for
> the engine control systems are specified in the airworthiness section
> of the Engine Manuals, GEK 105091 (CF34-8C1/8C5 models), GEK 112041
> (CF34-8D models), GEK 112031 (CF34-8E models), which define the
> various configurations and maximum operating intervals.

**NOTE** **17.** Overhaul of the CF34-8C1, CF34-8C5 (all models),
CF34-8D (all models) and CF34-8E (all models),

components is only authorized via approved component manuals.

**NOTE** **18.** The 5 minute maximum takeoff time limit may be extended
to 10 minutes for one engine

inoperative operation in multi-engine aircraft.

**NOTE** **19.** Refer to Operating Instructions GEK 105094
(CF34-8C1/8C5 models), GEK 112044 (CF34-8D models), GEK 112034

(CF34-8E models) for engine warm-up procedure.

**NOTE** **20.** Refer to Operating Instructions GEK 105094
(CF34-8C1/8C5 models), GEK 112044 (CF34-8D models), GEK 112034

(CF34-8E models) for thrust reverser operation.

**NOTE** **21.** The CF34-8C1, CF34-8C5 (all models), CF34-8D (all
models) and CF34-8E (all models), engine normal

takeoff interturbine temperature (T45) limit has been established to
assure that a fully degraded engine at the

normal takeoff rating will achieve the maximum takeoff rated thrust
without exceeding the maximum

takeoff T45 limit.

**NOTE** **22.** The above models incorporate the following
characteristics:

[Model]{.underline} [Characteristics]{.underline}

CF34-8C1 Basic Model

CF34-8C5 Derivative of CF34-8C1; side mounted; increased T45 and thrust
rating

CF34-8C5A1 Derivative of CF34-8C1; side mounted; increased T45 and
thrust rating

CF34-8C5B1 Derivative of CF34-8C1; side mounted; increased T45

CF34-8C5A2 Derivative of CF34-8C1; side mounted; increased T45 and
thrust rating

CF34-8C5A3 Derivative of CF34-8C1; side mounted; increased T45 and
thrust rating

CF34-8D1 Derivative of CF34-8C1; top mounted; increased T45 and thrust
rating; includes thrust

> reverser and aft core cowl

CF34-8D3 Derivative of CF34-8C1; top mounted; increased T45 and thrust
rating; includes thrust

> reverser and aft core cowl

CF34-8D5 Derivative of CF34-8C1; top mounted; increased T45 and thrust
rating; includes thrust

> reverser and aft core cowl

CF34-8D6 Derivative of CF34-8C1; top mounted; increased T45 and thrust
rating; includes thrust

> reverser and aft core cowl

CF34-8E2 Derivative of CF34-8C1; top mounted; increased T45; includes
thrust reverser and aft core

> cowl

CF34-8E2A1 Derivative of CF34-8C1; top mounted; increased T45; includes
thrust reverser and aft core

> cowl

CF34-8E5 Derivative of CF34-8C1; top mounted; increased T45 and thrust
rating; includes thrust

> reverser and aft core cowl

CF34-8E5A1 Derivative of CF34-8C1; top mounted; increased T45 and thrust
rating; includes thrust

> reverser and aft core cowl

CF34-8E5A2 Derivative of CF34-8C1; top mounted; increased T45 and thrust
rating ; includes thrust

> reverser and aft core cowl

CF34-8E6 Derivative of CF34-8C1; top mounted; increased T45 and thrust
rating; includes thrust

reverser and aft core cowl

CF34-8E6A1 Derivative of CF34-8C1; top mounted; increased T45 and thrust
rating; includes thrust

> reverser and aft core cowl

**\-- END\--**