**FEDERAL AVIATION ADMINISTRATION**

**AIRWORTHINESS DIRECTIVES**

**SMALL AIRCRAFT, ROTORCRAFT, GLIDERS,**

**BALLOONS, & AIRSHIPS**

**BIWEEKLY 2002-17**

This electronic copy may be printed and used in lieu of the FAA biweekly
paper copy.

U.S. Department of Transportation

Federal Aviation Administration

Regulatory Support Division

Delegation and Airworthiness Programs Branch, AIR-140

P. O. Box 26460

Oklahoma City, OK 73125-0460

FAX 405-954-4104

Biweekly 2002-01

  ------------ ---------- ----------------- ----------------------------------
  2001-26-13              Pilatus Aircraft  PC-7

  2001-26-25              Grob-Werke        Sailplane: G102 Club Astir III,
                                            G102 Club Astir IIIb, and G102
                                            Standard Astir III

  2002-01-02              Turbomeca S.A.    Engine: Arrius 1A
  ------------ ---------- ----------------- ----------------------------------

Biweekly 2002-02

+--------+---------+----------------+---------------------------------+
| 2000   | C, S    | Eurocopter     | Rotorcraft: AS-350B, BA, B1,    |
| -20-19 | 86-     | France         | B2, B3, C, D, and D1, and       |
|        | 15-10R2 |                |                                 |
|        |         |                | AS-355E, F, F1, F2 and N        |
+--------+---------+----------------+---------------------------------+
| 2001   | FR      | MD Helicopters | Rotorcraft: MD900               |
| -25-51 |         |                |                                 |
+--------+---------+----------------+---------------------------------+
| 2001   | FR      | Eurocopter     | Rotorcraft: EC135               |
| -26-52 |         | Deutschland    |                                 |
+--------+---------+----------------+---------------------------------+
| 2001   | FR      | Eurocopter     | Rotorcraft: AS350B, B1, B2, B3, |
| -26-53 |         | France         | BA, D, and AS355E               |
+--------+---------+----------------+---------------------------------+
| 2002   |         | British        | HP.137 Jetstream Mk.1,          |
| -01-05 |         | Aerospace      | Jetstream Series 200, Jetstream |
|        |         |                | Series 3101, and Jetstream      |
|        |         |                | Model 3201                      |
+--------+---------+----------------+---------------------------------+
| 2002   |         | Eurocopter     | Rotorcraft: AS332L2             |
| -01-06 |         | France         |                                 |
+--------+---------+----------------+---------------------------------+
| 2002   |         | Bell           | Rotorcraft: 430                 |
| -01-07 |         | Helicopter     |                                 |
|        |         | Textron Canada |                                 |
+--------+---------+----------------+---------------------------------+
| 2002   |         | Pilatus        | PC-7, PC-12, and PC-12/45       |
| -01-09 |         | Aircraft       |                                 |
+--------+---------+----------------+---------------------------------+
| 2002   |         | Raytheon       | 65-90, 65-A90, B90, C90, C90A,  |
| -01-10 |         | Aircraft       | 65-A90-1, 65-A90-4, E90, and    |
|        |         |                | H-90                            |
+--------+---------+----------------+---------------------------------+
| 2002   |         | Pilatus        | BN-2, BN-2A, BN-2A-2, BN-2A-3,  |
| -01-11 |         | Britten-Norman | BN-2A-6, BN-2A-8,               |
|        |         |                |                                 |
|        |         |                | BN-2A-9, BN-2A-20, BN-2A-21,    |
|        |         |                | BN-2A-26, BN-2A-27,             |
|        |         |                |                                 |
|        |         |                | BN-2B-20, BN-2B-21, BN-2B-26,   |
|        |         |                | BN-2B-27, BN-2T, BN-2T-4R,      |
|        |         |                |                                 |
|        |         |                | BN2A MK. III, BN2A MK. III-2,   |
|        |         |                | and BN2A MK. III-3              |
+--------+---------+----------------+---------------------------------+

**Biweekly 2002-03**

+--------+---------+----------------+---------------------------------+
| 2001   |         | Honeywell      | Engine: LTS101-600A-2,          |
| -25-04 |         | International  | LTS101-600A-3, LTP101-600A-1A,  |
|        |         |                | LTP101-700A-1A Turboprop        |
+--------+---------+----------------+---------------------------------+
| 2001   | FR      | Eurocopter     | Rotorcraft: EC 155B             |
| -26-54 |         | France         |                                 |
+--------+---------+----------------+---------------------------------+
| 2002   | S       | Fairchild      | SA26-AT, SA226-AT, SA226-T,     |
| -01-16 | 8       | Aircraft       | SA226-T(B), SA226-TC, SA227-AC, |
|        | 6-24-11 |                | SA227-AT, SA227-TT              |
|        | &       |                |                                 |
|        |         |                |                                 |
|        | 8       |                |                                 |
|        | 6-25-04 |                |                                 |
+--------+---------+----------------+---------------------------------+
| 2002   |         | Eurocopter     | Rotorcraft: SE 3130, SE 313B,   |
| -01-30 |         | France         | SA 315B, SE 3160, SA 316B,      |
|        |         |                | SA 316C, SA 3180, SA 318B, SA   |
|        |         |                | 318C, and SA 319B               |
+--------+---------+----------------+---------------------------------+
| 2002   | S       | Bell           | Rotorcraft: HH-1K, TH-1F,       |
| -01-31 | 200     | Helicopter     | TH-1L, UH-1A, UH-1B, UH-1E,     |
|        | 0-22-51 |                | UH‑1F, UH-1H, UH-1L, and UH-1P, |
|        |         |                | SW204, SW204HP, SW205, and      |
|        |         |                | SW205A-1                        |
+--------+---------+----------------+---------------------------------+
| 2002   |         | Eagle Aircraft | 150B                            |
| -02-01 |         | PTY            |                                 |
+--------+---------+----------------+---------------------------------+
| 2002   | E       | Eurocopter     | Rotorcraft: AS350B, AS350BA,    |
| -02-51 |         | France         | AS350B1, AS350B2, AS350B3,      |
|        |         |                | AS350C, AS350D, AS350D1,        |
|        |         |                | AS355E, AS355F, AS355F1,        |
|        |         |                | AS355F2, AS355N, and EC130 B4   |
+--------+---------+----------------+---------------------------------+
| 2002   | E, S    | Eurocopter     | Rotorcraft: AS350B, AS350BA,    |
| -03-52 | 200     | France         | AS350B1, AS350B2, AS350B3,      |
|        | 2-02-51 |                | AS350C, AS350D, AS350D1,        |
|        |         |                | AS355E, AS355F, AS355F1,        |
|        |         |                | AS355F2, AS335N, and EC130 B4   |
+--------+---------+----------------+---------------------------------+

**Biweekly 2002-04**

  ------------ ---------- ----------------- ----------------------------------
  2001-26-55   FR         Eurocopter France Rotorcraft: AS350B, AS350B1,
                                            AS350B2, AS350BA, AS350B3, AS350C,
                                            AS350D, AS350D1, AS355E, AS355F,
                                            AS355F1, AS355F2, and AS355N

  2002-02-10              Pilatus Britten   BN-2, BN-2A, BN-2A-2, BN-2A-3,
                          Norman            BN-2A-6, BN-2A-8, BN-2A-9,
                                            BN-2A-20, BN-2A-21, BN-2A-26,
                                            BN-2A-27, BN-2B-20, BN-2B-21,
                                            BN-2B-26, BN-2B-27, BN-2T, and
                                            BN-2T-4R

  2002-02-11              Pilatus Britten   BN-2, BN-2A, BN-2A-2, BN-2A-3,
                          Norman            BN-2A-6, BN-2A-8, BN-2A-9,
                                            BN-2A-20, BN-2A-21, BN-2A-26,
                                            BN-2A-27, BN-2B-20, BN-2B-21,
                                            BN-2B-26, BN-2B-27, BN-2T,
                                            BN-2T-4R, BN2A MK.III, BN2A
                                            MK.III-2, and BN2A MK.III-3

  2002-03-01              Honeywell         Engine: T5311A, T5311B, T5313B,
                          International     T5317A, T5317B, and former
                                            military T53-L-11, T53-L-11A,
                                            T53-L-11B, T53-L-11C, T53-L-11D,
                                            T53-L-11A S/SA, T53-L-13B,
                                            T53-L-13B S/SA, T53-L-13B S/SB,
                                            and T53-L-703 Turboshaft

  2002-03-02   S 98-13-03 British Aerospace HP.137 Jetstream Mk.1, Jetstream
                                            Series 200, Jetstream Series 3101
  ------------ ---------- ----------------- ----------------------------------

Biweekly 2002-04 continued

  ------------ ------------ ----------------- ----------------------------------
  2002-03-03                Socata-Groupe     TBM 700
                            Aerospatiale      

  2002-03-04                Pilatus Britten   BN-2, BN-2A, BN-2A-2, BN-2A-3,
                            Norman            BN-2A-6, BN-2A-8, BN-2A-9,
                                              BN-2A-20, BN-2A-21, BN-2A-26,
                                              BN-2A-27, BN-2B-20, BN-2B-21,
                                              BN-2B-26, BN-2B-27, BN-2T,
                                              BN-2T-4R, BN2A MK.III, BN2A
                                              MK.III-2, and BN2A MK.III-3

  2002-03-09                Honeywell         Engine: LTS101 Series Turboshaft
                            International     and LTP101 Series Turboprop

  2002-03-16   S 2000-18-52 Bell Helicopters  OH-13E, OH-13H, and OH-13S
                            (See AD)          

  2002-04-51   E            Textron Lycoming  Engine: LTIO-540 and TIO-540 (See
                                              AD)
  ------------ ------------ ----------------- ----------------------------------

Biweekly 2002-05

  ------------ ---------- ----------------- ----------------------------------
  2002-04-07              Eurocopter France Rotorcraft: AS350BA and B2

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

Biweekly 2002-06

+--------+---------+----------------+---------------------------------+
| 2002   | R1      | Honeywell      | Engine: LTS101 Series           |
| -03-09 |         | International  | Turboshaft and LTP101 Series    |
|        |         |                | Turboprop                       |
+--------+---------+----------------+---------------------------------+
| 2002   | FR, S   | Eurocopter     | Rotorcraft: AS350B, AS350BA,    |
| -03-52 | 200     | France         | AS350B1, AS350B2, AS350B3,      |
|        | 2-02-51 |                | AS350C, AS350D, AS350D1,        |
|        |         |                | AS355E, AS355F, AS355F1,        |
|        |         |                | AS355F2, AS355N, and EC130 B4   |
+--------+---------+----------------+---------------------------------+
| 2002   | S       | Socata-Groupe  | MS 892A-150, MS 892E-150, MS    |
| -05-04 | 7       | Aerospatiale   | 893A, MS 893E, MS 894A, MS      |
|        | 7-15-06 |                | 894E, Rallye 150T, and Rallye   |
|        |         |                | 150ST                           |
+--------+---------+----------------+---------------------------------+
| 2002   |         | Cirrus Design  | SR20 and SR22                   |
| -05-05 |         | Corporation    |                                 |
+--------+---------+----------------+---------------------------------+
| 2002   | COR, S  | Sikorsky       | Rotorcraft: S-76A               |
| -05-06 | 8       | Aircraft       |                                 |
|        | 6-09-11 | Corporation    |                                 |
+--------+---------+----------------+---------------------------------+
| 2002   |         | Eurocopter     | Rotorcraft: AS350B, AS350B1,    |
| -06-04 |         | France         | AS350B2, AS350B3, AS350BA,      |
|        |         |                | AS350C, AS350D, AS350D1,        |
|        |         |                | AS355E, AS355F, AS355F1,        |
|        |         |                | AS355F2, and AS355N             |
+--------+---------+----------------+---------------------------------+
| 2002   |         | Transport      | Appliance: Mode C 621A-3 Air    |
| -06-05 |         | Category       | Traffic Control (ATC)           |
|        |         | Airplanes      | Transponder(s)                  |
|        |         |                |                                 |
|        |         | Rockwell       |                                 |
|        |         | Collins        |                                 |
+--------+---------+----------------+---------------------------------+
| 2002   |         | Rolls-Royce    | Engine: 250-C28, -C28B, and     |
| -06-08 |         | Corp.          | -C28C                           |
+--------+---------+----------------+---------------------------------+
| 2002   | E, S    | Bell           | Rotorcraft: 407                 |
| -06-52 | 200     | Helicopter     |                                 |
|        | 0-02-12 | Textron Canada |                                 |
+--------+---------+----------------+---------------------------------+

Biweekly 2002-07

  ------------ ---------- ----------------- ----------------------------------
  2002-06-06              Rockwell Collins, Appliance: TDR-94 and TDR-94D Mode
                          Inc.              S Transponders

  2002-06-10              Pilatus Aircraft  PC-12 and PC-12/45

  2002-07-01              Cessna            P206C, TP206C, P206D, TP206D,
                                            P206E, TP206E, U206C, TU206C,
                                            U206D, TU206D, U206E, TU206E,
                                            U206F, TU206F, U206G, TU206G, 207,
                                            T207, 207A, T207A, 210G, 210H,
                                            210J, 210K, T210K, 210L, T210L,
                                            210M, T210M, 210N, T210N, P210N,
                                            T210G, T210H, T210J
  ------------ ---------- ----------------- ----------------------------------

Biweekly 2002-08

  ------------ ------------ ----------------- ----------------------------------
  2001-24-51   FR           MD Helicopters,   Rotorcraft: 600N
                            Inc.              

  2002-06-52   FR, S        Bell Helicopter   Rotorcraft: 407
               2000-02-12   Textron Canada    

  2002-08-01                Fairchild         SA226-AT, SA226-T, SA226-T(B),
                            Aircraft, Inc.    SA226-TC, SA227-AC, SA227-AT, and
                                              SA227-TT

  2002-08-02   S 2001-20-14 Fairchild         SA226-AT, SA226-T, SA226-T(B),
                            Aircraft, Inc.    SA226-TC, SA227-AC, SA227-AT,
                                              SA227-TT, and SA227-TT(300)

  2002-08-03   S 2001-22-01 Enstrom           Rotorcraft: F-28, F-28A, F-28C,
                            Helicopter Corp.  F-28F, 280, 280C, 280F and 280FX
  ------------ ------------ ----------------- ----------------------------------

Biweekly 2002-09

+--------+---------+----------------+---------------------------------+
| 2001   | FR, S   | Schweizer      | Rotorcraft: 269A, 269A-1, 269B, |
| -25-52 | 7       | Aircraft Corp. | 269C, and TH-55A                |
|        | 6-18-01 |                |                                 |
+--------+---------+----------------+---------------------------------+
| 2002   | FR,     | Eurocopter     | Rotorcraft: AS350B, AS350BA,    |
| -03-52 | COR, S  | France         | AS350B1, AS350B2, AS350B3,      |
|        | 200     |                | AS350C, AS350D, AS350D1,        |
|        | 2-02-51 |                | AS355E, AS355F, AS355F1,        |
|        |         |                | AS355F2, AS355N, and EC130 B4   |
+--------+---------+----------------+---------------------------------+
| 2002   | COR,    | Fairchild      | SA226-AT, SA226-T, SA226-T(B),  |
| -08-02 |         | Aircraft, Inc. | SA226-TC, SA227-AC, SA227-AT,   |
|        | S       |                | SA227-TT, and SA227-TT(300)     |
|        | 200     |                |                                 |
|        | 1-20-14 |                |                                 |
+--------+---------+----------------+---------------------------------+
| 2002   |         | Piaggio Aero   | P-180                           |
| -08-04 |         | Industries     |                                 |
|        |         | S.p.A.         |                                 |
+--------+---------+----------------+---------------------------------+
| 2002   | S       | Eurocopter     | Rotorcraft: SA341G, SA342J, and |
| -08-16 | 200     | France         | SA-360C                         |
|        | 1-19-51 |                |                                 |
+--------+---------+----------------+---------------------------------+
| 2002   | E       | Bell           | Rotorcraft: 205A, A-1 and B     |
| -08-53 |         | Helicopter     |                                 |
|        |         | Textron, Inc.  |                                 |
+--------+---------+----------------+---------------------------------+
| 2002   | E       | Bell           | Rotorcraft: 222, 222B, 222U,    |
| -08-54 |         | Helicopter     | and 230                         |
|        |         | Textron Canada |                                 |
+--------+---------+----------------+---------------------------------+
| 2002   |         | Eurocopter     | Rotorcraft: AS332L2             |
| -09-03 |         | France         |                                 |
+--------+---------+----------------+---------------------------------+
| 2002   |         | Bell           | 205A, 205A-1, 205B, 212, 412,   |
| -09-04 |         | Helicopter     | 412EP, and 412CF                |
|        |         | Textron, Inc.  |                                 |
+--------+---------+----------------+---------------------------------+
|        |         |                |                                 |
+--------+---------+----------------+---------------------------------+
| **Bi   |         |                |                                 |
| weekly |         |                |                                 |
| 200    |         |                |                                 |
| 2-10** |         |                |                                 |
+--------+---------+----------------+---------------------------------+
| 2002   | S       | Hartzell       | Propellers: ( )HC-( )( )Y( )-(  |
| -09-08 | 7       | Propellers     | )( )( ) Compact Series          |
|        | 7-12-06 |                |                                 |
|        | R2      |                |                                 |
+--------+---------+----------------+---------------------------------+
| 2002   |         | Honeywell      | Engine: T53 Series              |
| -09-09 |         | International  |                                 |
+--------+---------+----------------+---------------------------------+
| 2002   | COR,    | SOCATA         | TBM 700                         |
| -09-11 |         |                |                                 |
|        | S       |                |                                 |
|        | 200     |                |                                 |
|        | 1-05-03 |                |                                 |
+--------+---------+----------------+---------------------------------+
| 2002   | COR     | Raytheon       | C90A                            |
| -09-12 |         |                |                                 |
+--------+---------+----------------+---------------------------------+
| 2002   |         | Cessna         | 441                             |
| -09-13 |         |                |                                 |
+--------+---------+----------------+---------------------------------+
| 2002   | E, S    | Bell           | Rotorcraft: 204B, 205A, A-1,    |
| -09-51 | 200     | Helicopters    | and B                           |
|        | 2-08-53 |                |                                 |
+--------+---------+----------------+---------------------------------+
| 2002   | S       | MD Helicopters | Rotorcraft: MD-900              |
| -10-05 | 200     |                |                                 |
|        | 1-07-09 |                |                                 |
+--------+---------+----------------+---------------------------------+

  ------------ ---------- ------------------ ----------------------------------
  **Biweekly                                 
  2002-11**                                  

  2002-10-13              Raytheon Aircraft  58P, 60, A60, B60, and 65-88
                          Company            

  2002-10-14              Bombardier-Rotax   Engine: 914 F Series
                          GmbH               

  2002-11-01              Eurocopter         Rotorcraft: EC135
                          Deutschland        

  2002-11-02              Raytheon Aircraft  390
                          Company            

  2002-11-05              Air Tractor, Inc.  AT-400, AT-401, AT-401B, AT-402,
                                             AT-402A, AT-402B, AT-501, AT-802,
                                             and AT-802A
  ------------ ---------- ------------------ ----------------------------------

**Biweekly 2002-12**

  ------------ ------------ ----------------- ----------------------------------
  2002-11-03                Air Tractor, Inc. AT-502, AT-502A, AT-502B, AT-503A

  2002-11-07                Raytheon Aircraft E55, E55A, A56TC, 58, 58A, 58P,
                                              58PA, 58TC, and 58TCA

  2002-11-09                Bell Helicopter   Rotorcraft: 407

  2002-11-10   S 2001-25-08 Sikorsky          Rotorcraft: S-70A, S-70C

  2002-12-02                Eurocopter France Rotorcraft: AS332L2

  2002-12-03                Eurocopter France Rotorcraft: AS332L2
  ------------ ------------ ----------------- ----------------------------------

**Biweekly 2002-13**

  ------------ ------------ ----------------- ----------------------------------
  2002-11-03   COR          Air Tractor, Inc. AT-502, AT-502A, AT-502B, AT-503A

  2002-12-07   S 2000-18-53 Textron Lycoming  Engine: O--320--H1AD, --H1BD,
                                              --H2AD, --H2BD, --H3AD, ‑H3BD,
                                              (L)O--360,--A1AD, --A1F6D,
                                              --A1G6D, --A1LD, --A3AD, --A4AD,
                                              --A5AD, --E1A6D, IO--360--A1B6D,
                                              --A1D6D, --A3B6D, --A3D6D,
                                              --C1E6D, --J1AD, --J1A6D,
                                              (L)TO--360,--A1A6D, ‑C1A6D,
                                              --E1A6D, --F1A6D, TIO--360--C1A6D,
                                              (L)HIO‑360‑E1AD, --E1BD, --F1AD,
                                              O--540--H1A5D, --H1B5D, ‑H2A5D,
                                              --H2B5D, --J1A5D, --J1B5D,
                                              --J1C5D, --J1D5D, ‑J2A5D, --J2B5D,
                                              --J2C5D, --J2D5D, --J3A5D,
                                              --J3C5D, --L3C5D, IO‑540‑C4D5D,
                                              --K1A5D, --K1B5D, --K1E5D,
                                              --K1F5D, ‑K1G5D, --K1J5D, --L1A5D,
                                              ‑L1B5D, --M1A5D, --M1B5D, --M2A5D,
                                              ‑T4A5D, --T4B5D, --T4C5D, --U1A5D,
                                              ‑U1B5D, --V4A5D, ‑W1A5D, --W3A5D,
                                              (L)TIO--540--K1AD, --S1AD,
                                              --AA1AD, ‑AB1AD, --AB1BD, --F2BD,
                                              --J2BD, --N2BD, ‑R2AD, --T2AD,
                                              ‑V2AD, AEIO--540--L1B5D,
                                              TIO--541--E Series,
                                              TIGO--541--D1A, --D1B, --E1A,
                                              IO--720--A1BD, --B1BD, --C1BD,
                                              --D1BD, --D1CD

  2002-12-09                Honeywell         Engine: TPE331-11U, -12B, -12JR,
                            International     -12UA, -12UAR, and ‑12UHR Series
                                              Turboprop

  2002-12-14   S 99-23-07   Eurocopter France Rotorcraft: SA330F, G, SA330J,
                                              AS332C, L, and L1

  2002-13-04   S 2000-11-51 Teledyne          Engine: C-125, C145, O-300,
                            Continental       IO-360, TSIO-360, and LTSIO-520-AE
                                              Series Reciprocating

  2002-13-05                MD Helicopters    Rotorcraft: 369D, 369E, 369F, and
                                              369FF

  2002-13-06                Eurocopter        Rotorcraft: BO-105A, BO-105C,
                            Deutschland       BO-105 C-2, BO-105 CB-2, BO-105
                                              CB-4, BO-105S, BO-105 CS-2, BO-105
                                              CBS-2, BO-105 CBS-4, and BO-105LS
                                              A-1

  2002-13-51   E            Bell Helicopters  Rotorcraft: HH‑1K, TH‑1F, TH‑1L,
                                              UH‑1A, UH‑1B, UH‑1E, UH‑1F, UH‑1H,
                                              UH‑1L, UH‑1P; SW204, SW204HP,
                                              SW205, and SW205A‑1
  ------------ ------------ ----------------- ----------------------------------

**Biweekly 2002-14**

  ------------ ---------- ----------------- ----------------------------------
  2002-13-02              Air Tractor       AT-300, AT-301, AT-302, and
                                            AT-400A

  2002-13-07              Honeywell, Inc.   Appliance: Inertial Reference Unit

  2002-13-08              de Havilland      DHC-2 Mk.I, DHC-2 Mk. II, and
                                            DHC-2 Mk. III

  2002-13-11              Eurocopter France Rotorcraft: EC120B

  2002-14-01              Eurocopter France Rotorcraft: AS332L and AS332L1

  2002-14-17   S 99-12-01 Eurocopter        Rotorcraft: EC135
                          Deutschland       

  2002-14-18              Glaser-Dirks      Sailplane: DG-400 and DG-800A
                          Flugzeugbau       

  2002-14-51   E          Agusta S.p.A      Rotorcraft: A109E and A119
  ------------ ---------- ----------------- ----------------------------------

**Biweekly 2002-15**

+--------+---------+----------------+---------------------------------+
| 2002   | COR     | Teledyne       | Engine: C-125, C145, O-300,     |
| -13-04 |         | Continental    | IO-360, TSIO-360, and           |
|        | S       |                | LTSIO-520-AE Series             |
|        | 200     |                | Reciprocating                   |
|        | 0-11-51 |                |                                 |
+--------+---------+----------------+---------------------------------+
| 2002   |         | Rockwell       | Appliance: Air Data Computers   |
| -14-19 |         | Collins        | (ADC)                           |
+--------+---------+----------------+---------------------------------+
| 2002   | COR     | Pilatus        | PC-12 and PC-12/45              |
| -14-22 |         | Aircraft       |                                 |
+--------+---------+----------------+---------------------------------+
| 2002   |         | Turbomeca S.A. | Engine: Arriel Models 1A, 1A1,  |
| -14-26 |         |                | 1B, 1D, and 1D1 Turboshaft      |
+--------+---------+----------------+---------------------------------+
| 2002   |         | de Havilland   | DHC-2, Mk. I, DHC-2 Mk. II, and |
| -14-28 |         |                | DHC-2 Mk. III                   |
+--------+---------+----------------+---------------------------------+
| 2002   |         | Diamond        | Sailplane: H-36 \'\'Dimona\'\', |
| -15-01 |         | Aircraft       | HK 36 R \'\'Super Dimona\'\',   |
|        |         |                | HK 36 TC, HK 36 TS, HK 36 TTC,  |
|        |         |                | HK 36 TTC-ECO, HK 36 TTC-ECO    |
|        |         |                | (Restricted Category), and HK   |
|        |         |                | 36 TTS                          |
+--------+---------+----------------+---------------------------------+
| 2002   |         | Hamilton       | Appliance: Auxiliary Power      |
| -15-02 |         | Sundstrand     | Units (APU\'s)                  |
|        |         | Power Sys.     |                                 |
+--------+---------+----------------+---------------------------------+
| 2002   | E       | Sikorsky       | Rotorcraft: S76A, B, and C      |
| -15-51 |         |                |                                 |
+--------+---------+----------------+---------------------------------+

**Biweekly 2002-16**

  ------------ ------------ ----------------- ----------------------------------
  2002-08-54   FR           Bell Helicopter   Rotorcraft: 222, 222B, 222U, 230

  2002-09-51   FR, S        Bell Helicopter   Rotorcraft: 204B, 205A, A-1, and B
               2002-08-53                     

  2002-13-51   FR           Bell Helicopter,  Rotorcraft: HH-1K, TH-1F, TH-1L,
                            (See AD)          UH-1A, UH-1B, UH-1E, UH-1F, UH-1H,
                                              UH-1L, and UH-1P; SW204, SW204HP,
                                              SW205, and SW205A-1

  2002-15-04                Honeywell         Engine: T5313B, T5317 Series, and
                            International     former military T53 Series
                                              Turboshaft

  2002-15-05                Turbomeca         Engine: Makila 1 A, 1 A1, and 1 A2
                                              Turboshaft

  2002-15-06                Air Tractor       AT-802 and AT-802A

  2002-15-07                MD Helicopters    Rotorcraft: MD900

  2002-15-08                Eurocopter France Rotorcraft: EC120B, EC155B,
                                              SA330F, SA330G, SA330J, AS332C,
                                              AS332L, AS332L1, AS332L2, AS350B,
                                              AS350BA, AS350B1, AS350B2,
                                              AS350B3, AS350D, AS355E, AS355F,
                                              AS355F1, AS355F2, AS355N,
                                              AS-365N2, AS 365 N3, SA-365N, and
                                              SA-365N1
  ------------ ------------ ----------------- ----------------------------------

**Biweekly 2002-17**

+--------+---------+----------------+---------------------------------+
| 2002   | COR     | Bell           | Rotorcraft: 222, 222B, 222U,    |
| -08-54 |         | Helicopter     | 230                             |
+--------+---------+----------------+---------------------------------+
| 2002   | S       | Univair        | (ERCO) 415-C, 415-CD, 415-D,    |
| -16-04 | 46      | Aircraft       | 415-E, 415-G, (Forney) F-1, and |
|        | -38-03, |                | F-1A                            |
|        |         |                |                                 |
|        | 8       |                |                                 |
|        | 6-22-09 |                |                                 |
+--------+---------+----------------+---------------------------------+
| 2002   |         | Bo             | Engine: 912 F, 912 S, and 914 F |
| -16-07 |         | mbardier-Rotax | Series Reciprocating            |
|        |         | GmbH           |                                 |
+--------+---------+----------------+---------------------------------+
| 2002   |         | Barry Aviation | Sailplane: Model PZL-Krosno     |
| -16-17 |         |                | KR-03A \'\'Peregrine\'\'        |
|        |         |                | (Puchatek)                      |
+--------+---------+----------------+---------------------------------+
| 2002   |         | Turbomeca S.A. | Engine: Arriel 2S1, 2B and 2 C  |
| -16-25 |         |                | Turboshaft                      |
+--------+---------+----------------+---------------------------------+
| 2002   | COR     | Bo             | Engine: 912 F series and 914 F  |
| -16-26 |         | mbardier-Rotax | series reciprocating            |
|        |         | GmbH           |                                 |
+--------+---------+----------------+---------------------------------+
| 2002   | E, S    | Agusta S.p.A.  | Rotorcraft: A109E               |
| -17-51 | 0       |                |                                 |
|        | 2-14-51 |                |                                 |
+--------+---------+----------------+---------------------------------+
| 2002   | E, S    | Agusta S.p.A.  | Rotorcraft: A119                |
| -17-52 | 0       |                |                                 |
|        | 2-14-51 |                |                                 |
+--------+---------+----------------+---------------------------------+
| 2002   | E       | Textron        | Engine: LTIO-540 and TIO-540    |
| -17-53 |         | Lycoming       |                                 |
+--------+---------+----------------+---------------------------------+

**BW 2002-17**

**BELL HELICOPTER TEXTRON CANADA**

**AIRWORTHINESS DIRECTIVE**

**SMALL AIRCRAFT, ROTORCRAFT, GLIDERS, BALLOONS, & AIRSHIPS**

**EDITORIAL CORRECTION** *\[Federal Register: August 21, 2002 (Volume
67, Number 162); Page 54259;
www.access.gpo.gov/su_docs/aces/aces140.html\]*

**2002-08-54 Bell Helicopter Textron Canada:** Amendment 39-12835,
Docket No. 2002-SW-22-AD.

**Applicability:** The following model helicopters with the listed part
number (P/N) installed, certificated in any category:

  ------------ ---------------------------- -------------------- --------------------
  **Model**    **With hub assembly P/N**    **With grip assembly **With pitch horn
                                            P/N**                assembly P/N**

  \(1\) 222 or 222--011--101--103, -105,    222--010--104--105   222--011--104--101
  222B         -107, or -109                                     

               222--012--101--103, or -107  222--012--104--101   222--012--102--101

  \(2\) 222U   222--011--101--105, -107, or 222--010--104--105   222--011--104--101
               -109                                              

               222--012--101--103, OR -107  222--012--104--101   222--012--102--101

  \(3\) 230    222--012--101--105, or -109  222--012--104--101   222--012--102--101
  ------------ ---------------------------- -------------------- --------------------

**Note 1:** This AD applies to each helicopter identified in the
preceding applicability provision, regardless of whether it has been
otherwise modified, altered, or repaired in the area subject to the
requirements of this AD. For helicopters that have been modified,
altered, or repaired so that the performance of the requirements of this
AD is affected, the owner/operator must request approval for an
alternative method of compliance in accordance with paragraph (d) of
this AD. The request should include an assessment of the effect of the
modification, alteration, or repair on the unsafe condition addressed by
this AD; and if the unsafe condition has not been eliminated, the
request should include specific proposed actions to address it.

**Compliance:** Required as indicated, unless accomplished previously.

To prevent failure of the grip or pitch horn and subsequent loss of
control of the helicopter, if either the grip or pitch horn has
accumulated 1250 or more hours time-in-service (TIS) since initial
installation on any helicopter, accomplish the following:

\(a\) Before further flight and thereafter at intervals not to exceed 8
hours TIS:

\(1\) Wipe clean the main rotor grip and pitch horn surfaces to remove
grease and dirt in the check area as shown in Figure 1 of this AD:

![](media/image2.png){width="6.797916666666667in"
height="8.275694444444444in"}

\(2\) Visually check both main rotor grips for a crack, paying
particular attention to the inboard and outboard tangs/portions of the
grip, which are in direct contact with the pitch horns and the main
rotor blades. Check the area to at least 3 inches beyond the grip/pitch
and grip/blade contact areas as shown in Figure 2 of this AD:

![](media/image3.png){width="4.395138888888889in" height="5.9in"}

\(3\) Visually check all visible portions of each pitch horn for a
crack. Pay particular attention to the attachment lugs of the pitch
horns, which are in direct contact with the inboard tangs of the main
rotor grips, as shown in Figure 3 of this AD, and the four large bolt
cutouts, as shown in Figure 4 of this AD:

![](media/image4.png){width="5.704861111111111in"
height="5.335416666666666in"}

![](media/image5.png){width="4.876388888888889in"
height="6.519444444444445in"}

\(4\) An owner/operator (pilot) may perform the visual check required by
this AD. The pilot must enter compliance with paragraph (a) of this AD
into the helicopter maintenance records in accordance with 14 CFR 43.11
and 91.417(a)(2)(v)). A pilot may perform this check because it involves
only a visual check for a crack in the grip or pitch horn and can be
performed equally well by a pilot or a mechanic.

\(b\) Within 7 days or 10 hours TIS, whichever occurs first, and
thereafter at intervals not to exceed 25 hours TIS, using a 10-power or
higher magnifying glass, visually inspect each grip and pitch horn for a
crack in accordance with the Accomplishment Instructions, Part II,
paragraphs 1 and 2, of Bell Helicopter Textron Alert Service Bulletin
Nos. 222U-02-64, 222-02-93, and 230-02-26, all dated April 1, 2002, as
applicable.

\(c\) If a crack is found, replace the unairworthy grip or pitch horn
with an airworthy part before further flight.

\(d\) An alternative method of compliance or adjustment of the
compliance time that provides an acceptable level of safety may be used
if approved by the Manager, Regulations Group, FAA. Operators shall
submit their requests through an FAA Principal Maintenance Inspector,
who may concur or comment and then send it to the Manager, Regulations
Group.

**Note 2:** Information concerning the existence of approved alternative
methods of compliance with this AD, if any, may be obtained from the
Regulations Group.

\(e\) Special flight permits may be issued in accordance with 14 CFR
21.197 and 21.199 to operate the helicopter to a location where the
inspection requirements of paragraph (b) of this AD can be accomplished.

\(f\) The inspection shall be done in accordance with the Accomplishment
Instructions, Part II, paragraphs 1 and 2, of Bell Helicopter Textron
Alert Service Bulletin Nos. 222U-02-64, 222-02-93, and 230-02-26, all
dated April 1, 2002, as applicable. This incorporation by reference was
approved by the Director of the Federal Register in accordance with 5
U.S.C. 552(a) and 1 CFR part 51. Copies may be obtained from Bell
Helicopter Textron Canada, 12,800 Rue de l\'Avenir, Mirabel, Quebec
J7J1R4, telephone (450) 437-2862 or (800) 363-8023, fax (450) 433-0272.
Copies may be inspected at the FAA, Office of the Regional Counsel,
Southwest Region, 2601 Meacham Blvd., Room 663, Fort Worth, Texas; or at
the Office of the Federal Register, 800 North Capitol Street, NE., suite
700, Washington, DC.

\(g\) This amendment becomes effective on August 21, 2002, to all
persons except those persons to whom it was made immediately effective
by Emergency AD 2002-08-54, issued May 2, 2002, which contained the
requirements of this amendment.

**Note 3:** The subject of this AD is addressed in Transport Canada
(Canada) AD CF-2002-23, dated April 2, 2002.

Issued in Fort Worth, Texas, on July 25, 2002.

Eric Bries,

Acting Manager, Rotorcraft Directorate, Aircraft Certification Service.

\[FR Doc. 02-19486 Filed 8-5-02; 8:45 am\]

BILLING CODE 4910-13-P

**BW 2002-17**

**UNIVAIR AIRCRAFT CORPORATION**

**AIRWORTHINESS DIRECTIVE**

**SMALL AIRCRAFT, ROTORCRAFT, GLIDERS, BALLOONS, & AIRSHIPS**

**2002-16-04 Univair Aircraft Corporation:** Amendment 39-12843; Docket
No. 2000-CE-79-AD; Supersedes AD 46-38-03 and AD 86-22-09, Amendment
39-5457.

\(a\) *What airplanes are affected by this AD?* This AD affects all
serial numbers of Models (ERCO) 415-C, (ERCO) 415-CD, (ERCO) 415-D,
(ERCO) 415-E, (ERCO) 415-G, (Forney) F-1, and (Forney) F-1A airplanes
that:

\(1\) are certificated in any category; and

\(2\) have the gascolator connected to the side of the carburetor. This
AD does not affect those airplanes with the gascolator mounted on the
firewall.

\(b\) *Who must comply with this AD?* Anyone who wishes to operate any
of the airplanes identified in paragraph (a) of this AD must comply with
this AD.

\(c\) *What problem does this AD address?* The actions specified by this
AD are intended to prevent failure of the fuel line fittings or the
gascolator because of the current airplane design configuration
(aluminum fuel line nipples, aluminum fuel line elbows, and/or no double
support tubes on the gascolator). Such failure could result in a lack of
fuel to the engine with consequent loss of control of the airplane.

\(d\) *What actions must I accomplish to address this problem?* To
address this problem, you must accomplish the following:

  -------------------------- --------------------------- ----------------
  **Actions**                **Compliance**              **Procedures**

  \(1\) Visually inspect the Inspect within the next 25  In accordance
  fuel line nipple and elbow ours time-in-service (TIS)  with Univair
  located between the        after September 13, 2002    Service Bulletin
  carburetor and gascolator  (the effective date of this No. 24B, dated
  for cracks or              AD) and replace prior to    January 29,
  misalignment, and replace  further flight after the    2002.
  as necessary.              inspection. You must        
                             inspect even if you have    
                             inspected previously.       

  \(2\) Replace any aluminum Within the next 25 TIS      In accordance
  fuel line nipple with one  after September 13, 2002    with Univair
  made of brass or steel.    (the effective date of this Service Bulletin
                             AD), unless already         No. 24B, dated
                             accomplished (compliance    January 29,
                             with AD 86--22--09 and/or   2002.
                             Univair Service Bulletin    
                             No. 24A, dated August 22,   
                             1986).                      

  \(3\) Replace any aluminum Within the next 25 hours    In accordance
  fuel elbow fitting with    TIS after September 13,     with Univair
  one made of brass or       2002 (the effective date of Service Bulletin
  steel. Manufacturer        this AD), unless already    No. 24B, dated
  replacement parts numbers  accomplished (compliance    January 29,
  are referenced in the      with AD 46--38--03).        2002.
  service information.                                   
  -------------------------- --------------------------- ----------------

+-------------------------+---------------------------+----------------+
| \(4\) Inspect for the   | Inspect within the next   | In accordance  |
| existence of double     | 25 hours TIS after        | with Univair   |
| support tubes on the    | September 13, 2002 (the   | Service        |
| gascolator and install  | effective date of this    | Bulletin No.   |
| these tubes if they do  | AD) and install the       | 24B, dated     |
| not exist, as follows:  | double support tubes      | January 29,    |
|                         | prior to further flight   | 2002.          |
| \(i\) For all affected  | after the inspection,     |                |
| airplanes except for    | unless already            |                |
| (Forney) F--1 and       | accomplished (compliance  |                |
| (Forney) F--1A          | with Univair Service      |                |
| airplanes, install part | Bulletin No. 24A, dated   |                |
| numbers 48076 and 48096 | August 22, 1986).         |                |
| (or FAA-approved        |                           |                |
| equivalent part         |                           |                |
| numbers) double support |                           |                |
| tubes; and              |                           |                |
|                         |                           |                |
| \(ii\) For all affected |                           |                |
| (Forney) F--1 and       |                           |                |
| (Forney) F1--A          |                           |                |
| airplanes, install part |                           |                |
| numbers 48098 and 48099 |                           |                |
| (or FAA-approved        |                           |                |
| equivalent part         |                           |                |
| numbers) double support |                           |                |
| tubes.                  |                           |                |
+-------------------------+---------------------------+----------------+
| \(5\) Do not install,   | As of September 13, 2002  | Not            |
| on any affected         | (the effective date of    | Applicable.    |
| airplane, an aluminum   | this AD).                 |                |
| fuel line nipple or     |                           |                |
| aluminum elbow.         |                           |                |
+-------------------------+---------------------------+----------------+
| \(6\) Do not install a  | As of September 13, 2002  | Not            |
| gascolator on the side  | (the effective date of    | Applicable.    |
| of the carburetor on    | this AD).                 |                |
| any affected airplane,  |                           |                |
| unless the double       |                           |                |
| support tubes specified |                           |                |
| in paragraph (d)(4)(i)  |                           |                |
| or (d)(4)(ii) of this   |                           |                |
| AD are installed.       |                           |                |
+-------------------------+---------------------------+----------------+

\(e\) *Can I comply with this AD in any other way?*

\(1\) You may use an alternative method of compliance or adjust the
compliance time if:

\(i\) Your alternative method of compliance provides an equivalent level
of safety; and

\(ii\) The Manager, Denver Aircraft Certification Office (ACO), approves
your alternative. Submit your request through an FAA Principal
Maintenance Inspector, who may add comments and then send it to the
Manager, Denver ACO.

\(2\) Alternative methods of compliance approved in accordance with AD
46-38-03 and/or AD 86-22-09, which are superseded by this AD, are not
approved as alternative methods of compliance with this AD.

**Note:** This AD applies to each airplane identified in paragraph (a)
of this AD, regardless of whether it has been modified, altered, or
repaired in the area subject to the requirements of this AD. For
airplanes that have been modified, altered, or repaired so that the
performance of the requirements of this AD is affected, the
owner/operator must request approval for an alternative method of
compliance in accordance with paragraph (e) of this AD. The request
should include an assessment of the effect of the modification,
alteration, or repair on the unsafe condition addressed by this AD; and,
if you have not eliminated the unsafe condition, specific actions you
propose to address it.

\(f\) *Where can I get information about any already-approved
alternative methods of compliance?* Contact Elizabeth Bumann, Aerospace
Engineer, FAA, Denver Aircraft Certification Office, 26805 East 68th
Avenue, Room 214, Denver, Colorado 80249; telephone: (303) 342-1083;
facsimile: (303) 342-1088.

\(g\) *What if I need to fly the airplane to another location to comply
with this AD?* The FAA can issue a special flight permit under Secs.
21.197 and 21.199 of the Federal Aviation Regulations (14 CFR 21.197 and
21.199) to operate your airplane to a location where you can accomplish
the requirements of this AD.

\(h\) *Are any service bulletins incorporated into this AD by
reference?* Actions required by this AD must be done in accordance with
Univair Service Bulletin No. 24B, dated January 29, 2002. The Director
of the Federal Register approved this incorporation by reference under 5
U.S.C. 552(a) and 1 CFR part 51. You can get copies from Univair
Aircraft Corporation, 2500 Himalaya Road, Aurora, Colorado 80011. You
can look at copies at the FAA, Central Region, Office of the Regional
Counsel, 901 Locust, Room 506, Kansas City, Missouri, or at the Office
of the Federal Register, 800 North Capitol Street, NW., Suite 700,
Washington, DC.

\(i\) *Does this AD action affect any existing AD actions?* This
amendment supersedes AD 46-38-03 and AD 86-22-09, Amendment 39-5457.

\(j\) *When does this amendment become effective?* This amendment
becomes effective on September 13, 2002.

Issued in Kansas City, Missouri, on July 30, 2002.

Michael Gallagher,

Manager, Small Airplane Directorate, Aircraft Certification Service.

\[FR Doc. 02-19874 Filed 8-9-02; 8:45 am\]

BILLING CODE 4910-13-P

**BW 2002-17**

**BOMBARDIER-ROTAX GMBH**

**AIRWORTHINESS DIRECTIVE**

**ENGINE**

**SMALL AIRCRAFT, ROTORCRAFT, GLIDERS, BALLOONS, & AIRSHIPS**

**2002-16-07 Bombardier-Rotax GmbH:** Amendment 39-12846. Docket No.
2002-NE-17-AD.

**Applicability**

This airworthiness directive (AD) is applicable to Bombardier-Rotax GmbH
type 912 F, 912 S, and 914 F series reciprocating engines with the
serial numbers (SN\'s) in Table 1 of this AD, and all engines that have
been converted to a single valve spring arrangement at engine repair or
general overhaul. Table 1 follows:

  ------------------------- ---------------------------------------------
  **TABLE 1.---ENGINE       
  SERIES BY SN**            

  **Engine model**          **Engine SN**

  912 F                     4,412.757 to 4,412.794

                            4,412.796 to 4,412.807

  912 S                     4,922.501 to 4,922.534

                            4,922.536 to 4,922.552

                            4,922.554 to 4,922.577

                            4,922.579 to 4,922.636

  914 F                     4,420.039 to 4,420.048

                            4,420.050 to 4,420.067

                            4,420.069 to 4,420.082

                            4,420.084 to 4,420.097

                            4,420.099 to 4,420.114

                            4,420.116 to 4,420.155

                            4,420.157 to 4,420.253
  ------------------------- ---------------------------------------------

These engines are installed on, but not limited to, Diamond Aircraft
Industries, DA20-A1, Diamond Aircraft Industries GmbH Model HK 36 TTS,
Model HK 36TTC, and Model HK 36 TTC-ECO, Iniziative Industriali Italiane
S.p.A. Sky Arrow 650 TC and Sky Arrow 650 TCN, Aeromot-Industria
Mecanico Metalurgica ltda., Models AMT-300 and AMT-200S, and Stemme
S10-VT aircraft.

**Note 1:** This AD applies to each engine identified in the preceding
applicability provision, regardless of whether it has been modified,
altered, or repaired in the area subject to the requirements of this AD.
For engines that have been modified, altered, or repaired so that the
performance of the requirements of this AD is affected, the
owner/operator must request approval for an alternative method of
compliance in accordance with paragraph (c) of this AD. The request
should include an

assessment of the effect of the modification, alteration, or repair on
the unsafe condition addressed by this AD; and, if the unsafe condition
has not been eliminated, the request should include specific proposed
actions to address it.

**Compliance**

Compliance with this AD is required as indicated, unless already done.

To prevent cracking of the valve spring retainers resulting in possible
engine failure while in-flight, do the following:

**Replacement Procedure**

\(a\) Replace valve spring retainers part number (P/N) 854.182, of
single valve spring configuration, with valve spring retainers P/N
854.184, in accordance with 3.1.1 of the Accomplishment Instructions of
Mandatory Service Bulletin (MSB) SB-912-022/SB-914-011, dated March,
2001, using the compliance times in the following Table 2:

  ----------------------------------- -----------------------------------
  **TABLE 2.---COMPLIANCE SCHEDULE**  

  **Engine flight hours (FH) on the   **Replace**
  effective date of this AD**         

  \(1\) 0 FH (new engine)             Before installing on aircraft.

  \(2\) 10 hours or less ..           Within 10 FH after the effective
                                      date of this AD.

  \(3\) More than 10 but less than or Within 25 FH after the effective
  equal to 25 FH.                     date of this AD.

  \(4\) More than 25 FH               Before exceeding 100 FH.
  ----------------------------------- -----------------------------------

\(b\) For engines that have had the oil system accessed during repair or
maintenance, replace the valve spring retainers in accordance with 3.1.1
of the Accomplishment Instructions of Mandatory Service Bulletin (MSB)
SB-912-022/SB-914-011, dated March, 2001, within 10 FH after the
effective date of this AD.

**Alternative Methods of Compliance**

\(c\) An alternative method of compliance or adjustment of the
compliance time that provides an acceptable level of safety may be used
if approved by the Manager, Engine Certification Office (ECO). Operators
must submit their requests through an appropriate FAA Principal
Maintenance Inspector, who may add comments and then send it to the
Manager, ECO.

**Note 2:** Information concerning the existence of approved alternative
methods of compliance with this airworthiness directive, if any, may be
obtained from the ECO.

**Special Flight Permits**

\(d\) Special flight permits may be issued in accordance with Secs.
21.197 and 21.199 of the Federal Aviation Regulations (14 CFR 21.197 and
21.199) to operate the aircraft to a location where the requirements of
this AD can be done.

**Documents That Have Been Incorporated by Reference**

\(e\) The replacements must be done in accordance with Bombardier-Rotax
GmbH Mandatory Service Bulletin (MSB) SB-912-022/SB-914-011, dated
March, 2001. This incorporation by reference was approved by the
Director of the Federal Register in accordance with 5 U.S.C. 552(a) and
1 CFR part 51. Copies may be obtained from Bombardier-Rotax GmbH, Welser
Strasse 32, A-4623 Gunskirchen, Austria; telephone 7246-601-232; fax
7246-601-370. Copies may be inspected at the FAA, New England Region,
Office of the Regional Counsel, 12 New England Executive Park,
Burlington, MA; or at the Office of the Federal Register, 800 North
Capitol Street, NW, suite 700, Washington, DC.

**Note 3:** The subject of this AD is addressed in Austro Control
airworthiness directive No. 108.

**Effective Date**

\(f\) This amendment becomes effective on September 3, 2002.

Issued in Burlington, Massachusetts, on August 2, 2002.

Jay J. Pardee,

Manager, Engine and Propeller Directorate, Aircraft Certification
Service.

\[FR Doc. 02-20266 Filed 8-15-02; 8:45 am\]

BILLING CODE 4910-13-P

**BW 2002-17**

**BARRY AVIATION, LLC**

**AIRWORTHINESS DIRECTIVE**

**SMALL AIRCRAFT, ROTORCRAFT, GLIDERS, BALLOONS, & AIRSHIPS**

**2002-16-17 Barry Aviation, LLC:** Amendment 39-12856; Docket No.
2002-CE-30-AD.

\(a\) *What sailplanes are affected by this AD?* This AD applies to
Model PZL-Krosno KR-03A \'\'Peregrine\'\' (Puchatek) sailplanes, serial
numbers 03-01 through 03-24 and 04-01 through 04-20, that are
certificated in any category.

**Note 1:** PZL-Krosno previously held the type certificate for these
sailplanes.

\(b\) *Who must comply with this AD?* Anyone who wishes to operate any
of the sailplanes identified in paragraph (a) of this AD must comply
with this AD.

\(c\) *What problem does this AD address?* The actions specified by this
AD are intended to prevent cracking in the horizontal stabilizer
attachment fittings, which could result in the horizontal stabilizer
separating from the sailplane with consequent loss of control of the
sailplane.

\(d\) *What must I do to address this problem?* To address this problem,
you must accomplish the following actions:

  --------------------------- ----------------- -------------------------------
  **Actions**                 **Compliance**    **Procedures**

  \(1\) Inspect the           Inspect within 10 Inspect in accordance with
  horizontal stabilizer       hours             Barry Aviation ''KROSNO KR--03A
  attachment fittings to      time-in-service   Glider'' Service Bulletin No.
  ensure that the correct     (TIS) after       1--02, dated June 10, 2002.
  fittings are installed:.    August 30, 2002   Replace in accordance with WSK
  (i) If part number (P/N)    (the effective    ''PZL--KROSNO'' Service
  NS--03/08/93--01L/P         date of this AD). Bulletin No. BE--29/KR--03A/93,
  attachment fittings (or     Replace prior to  dated November 16, 1993.
  FAA-approved equivalent     further flight    
  part numbers) are           after the         
  installed, no further       inspection.       
  action is required by this                    
  paragraph. (ii) If the                        
  attachment fittings are                       
  P/Ns other than                               
  NS--03/08/93--01L/P (or                       
  FAA-approved equivalent                       
  part numbers), replace the                    
  fittings with the P/N                         
  NS--03/08/93--01L/P                           
  attachment fittings (or                       
  FAA-approved equivalent                       
  part numbers).                                

  \(2\) Incorporate a ''NO    Within 10 hours   Use paint or a permanent
  LIFT'' placard to the       TIS after August  placard and add the words ''NO
  vertical stabilizer.        30, 2002 (the     LIFT'' to both sides of the
                              effective date of vertical stabilizer near the
                              this AD).         top and leading edge. Use
                                                letters that are at least .5
                                                inch and a color that contrasts
                                                with the color of the airplane,
                                                e.g., use red on a blue
                                                airplane.
  --------------------------- ----------------- -------------------------------

\(e\) *Can I comply with this AD in any other way?* You may use an
alternative method of compliance or adjust the compliance time if:

\(1\) Your alternative method of compliance provides an equivalent level
of safety; and

\(2\) The Manager, Atlanta Aircraft Certification Office (ACO), approves
your alternative. Submit your request through an FAA Principal
Maintenance Inspector, who may add comments and then send it to the
Manager, Atlanta ACO.

**Note 2:** This AD applies to each sailplane identified in paragraph
(a) of this AD, regardless of whether it has been modified, altered, or
repaired in the area subject to the requirements of this AD. For
sailplanes that have been modified, altered, or repaired so that the
performance of the requirements of this AD is affected, the
owner/operator must request approval for an alternative method of
compliance in accordance with paragraph (e) of this AD. The request
should include an assessment of the effect of the modification,
alteration, or repair on the unsafe condition addressed by this AD; and,
if you have not eliminated the unsafe condition, specific actions you
propose to address it.

\(f\) Where can I get information about any already-approved alternative
methods of compliance? Contact William O. Herderich, Aerospace Engineer,
FAA, Atlanta Aircraft Certification Office, 1895 Phoenix Boulevard,
suite 450, Atlanta, Georgia 30349; telephone: (770) 703-6082; facsimile:
(770) 703-6097; e-mail: <william.o.herderich@faa.gov>.

\(g\) Are any service bulletins incorporated into this AD by reference?
Actions required by this AD must be done in accordance with WSK
\'\'PZL-KROSNO\'\' Service Bulletin No. BE-29/KR-03A/93, dated November
16, 1993; and Barry Aviation \'\'KROSNO KR-03A Glider\'\' Service
Bulletin No. 1-02, dated June 10, 2002. The Director of the Federal
Register approved this incorporation by reference under 5 U.S.C. 552(a)
and 1 CFR part 51. You may get copies from Barry Aviation, LLC, 11600
Aviation Boulevard, suite 16, West Palm Beach, Florida 33412. You may
view this information at FAA, Central Region, Office of the Regional
Counsel, 901 Locust, Room 506, Kansas City, Missouri, or at the Office
of the Federal Register, 800 North Capitol Street, NW., suite 700,
Washington, DC.

\(h\) When does this amendment become effective? This amendment becomes
effective on August 30, 2002.

Issued in Kansas City, Missouri, on August 6, 2002.

Michael Gallagher,

Manager, Small Airplane Directorate, Aircraft Certification Service.

\[FR Doc. 02-20400 Filed 8-15-02; 8:45 am\]

BILLING CODE 4910-13-P

**BW 2002-17**

**TURBOMECA S.A.**

**AIRWORTHINESS DIRECTIVE**

**ENGINE**

**SMALL AIRCRAFT, ROTORCRAFT, GLIDERS, BALLOONS, & AIRSHIPS**

**2002-16-25 Turbomeca S.A.:** Amendment 39-12864. Docket No.
2001-NE-10-AD.

**Applicability**

This airworthiness directive (AD) is applicable to Turbomeca S.A. Arriel
models 2 S1, 2 B, and 2 C turboshaft engines. These engines are
installed on, but not limited to Sikorsky S76, Eurocopter France
\'\'Ecureuil\'\' AS 350 B3, and Eurocopter France \'\'Dauphin\'\' AS 365
N3 helicopters.

**Note 1:** This AD applies to each engine identified in the preceding
applicability provision, regardless of whether it has been modified,
altered, or repaired in the area subject to the requirements of this AD.
For engines that have been modified, altered, or repaired so that the
performance of the requirements of this AD is affected, the
owner/operator must request approval for an alternative method of
compliance in accordance with paragraph (e) of this AD. The request
should include an assessment of the effect of the modification,
alteration, or repair on the unsafe condition addressed by this AD; and,
if the unsafe condition has not been eliminated, the request should
include specific proposed actions to address it.

**Compliance**

Compliance with this AD is required as indicated, unless already done.

To prevent fuel leakage, which may cause engine fires that could lead to
an in-flight engine shutdown, damage to the helicopter, and forced
landing, do the following:

**Inspections and Actions**

\(a\) For the fuel metering high pressure/low pressure (HP/LP) pump
assemblies listed by serial number (SN) in Appendix 1 of Turbomeca
Service Bulletin (SB) No. 292 73 2803, dated July 2, 1999, do the
following:

\(1\) After the last flight of each day, within five minutes of engine
shutdown, perform a visual inspection of the floor of the helicopter
engine bay for fuel leaks.

\(2\) If evidence of a fuel leak is observed, inspect the fuel metering
HP/LP pump assembly for leakage and if leakage is observed, replace with
a serviceable pump assembly before further flight.

\(3\) If visual inspection of the floor of the helicopter engine bay for
fuel leaks reveals no leaks, do either of the following:

\(i\) Continue repetitive visual inspections of the floor of the
helicopter engine bay for fuel leaks in accordance with paragraph (a)(1)
of this AD, and perform repetitive visual inspections of the fuel
metering HP/LP pump assembly for fuel leaks at intervals not to exceed
50 hours of operation. If evidence of fuel leaking is observed, replace
the pump assembly with a serviceable pump assembly before further
flight, in accordance with Turbomeca SB No. 292 73 2803, dated July 2,
1999; or

\(ii\) Remove the pump assembly and inspect to determine if pump body
material wall thickness is below the minimum material thickness, in
accordance with Section 2 of Turbomeca SB No. 292 73 2803, dated July 2,
1999. If pump body material wall thickness is at or above the minimum
material thickness, mark the pump assembly by adding a letter \'\'x\'\'
to the end of the SN.

\(b\) Replace the fuel metering HP/LP pump assembly if listed by SN in
Appendix 1 of Turbomeca Service Bulletin (SB) No. 292 73 2803, dated
July 2, 1999, with a serviceable pump assembly by December 31, 2006.

**Definition**

\(c\) For the purposes of this AD, a serviceable pump assembly is a fuel
metering HP/LP pump assembly not listed by SN in Appendix 1 of Turbomeca
SB No. 292 73 2803, dated July 2, 1999, or a fuel metering HP/LP pump
assembly listed by SN in Appendix 1 whose pump body material wall
thickness has been determined by inspection to be at or above the
minimum material thickness, and marked in accordance with paragraph
(a)(3)(ii) of this AD.

**Terminating Action**

\(d\) Replacement, or verification of correct wall thickness of a fuel
metering HP/LP pump assembly that is listed in Appendix 1 of Turbomeca
SB No. 292 73 2803, dated July 2, 1999, with a serviceable pump assembly
as defined in paragraph (c) of this AD, is considered terminating action
for the inspection requirements specified in paragraph (a) of this AD.

**Alternative Methods of Compliance**

\(e\) An alternative method of compliance or adjustment of the
compliance time that provides an acceptable level of safety may be used
if approved by the Manager, Engine Certification Office (ECO). Operators
must submit their request through an appropriate FAA Principal
Maintenance Inspector, who may add comments and then send it to the
Manager, ECO.

**Note 2:** Information concerning the existence of approved alternative
methods of compliance with this airworthiness directive, if any, may be
obtained from the ECO.

**Special Flight Permits**

\(f\) Special flight permits may be issued in accordance with Secs.
21.197 and 21.199 of the Federal Aviation Regulations (14 CFR 21.197 and
21.199) to operate the aircraft to a location where the requirements of
this AD can be done.

**Documents That Have Been Incorporated by Reference**

\(g\) The inspections and removals must be done in accordance with
Turbomeca SB No. 292 73 2803, dated July 2, 1999. This incorporation by
reference was approved by the Director of the Federal Register in
accordance with 5 U.S.C. 552(a) and 1 CFR part 51. Copies may be
obtained from Turbomeca, 40220 Tarnos, France; telephone (33) 05 59 64
40 00; fax (33) 05 59 64 60 80. Copies may be inspected at the FAA, New
England Region, Office of the Regional Counsel, 12 New England Executive
Park, Burlington, MA; or at the Office of the Federal Register, 800
North Capitol Street, NW., Suite 700, Washington, DC.

**Note 3:** The subject of this AD is addressed in Direction Generale de
L\'Aviation Civile (DGAC) Airworthiness Directive AD 99-285(A), dated
July 13, 1999.

**Effective Date**

\(h\) This amendment becomes effective on September 26, 2002.

Issued in Burlington, Massachusetts, on August 14, 2002.

Mark C. Fulmer,

Acting Manager, Engine and Propeller Directorate, Aircraft Certification
Service.

\[FR Doc. 02-21355 Filed 8-21-02; 8:45 am\]

BILLING CODE 4910-13-P

**BW 2002-17**

**BOMBARDIER-ROTAX GMBH**

**AIRWORTHINESS DIRECTIVE**

**ENGINE**

**SMALL AIRCRAFT, ROTORCRAFT, GLIDERS, BALLOONS, & AIRSHIPS**

**EDITORIAL CORRECTION:** *The effective date of the preamble in this AD
which published in the Federal Register today is incorrect. The correct
effective date should be August 30, 2002. The FAA will issue a
correction. We have corrected this copy.*

**2002-16-26 Bombardier-Rotax GmbH:** Amendment 39-12865. Docket No.
2002-NE-08-AD.

**Applicability**

This airworthiness directive (AD) is applicable to Bombardier-Rotax GmbH
type 912 F series reciprocating engines serial number (SN) 4,412.796, or
lower, and 914 F series reciprocating engines SN 4,420.313, or lower.
These engines are installed on, but not limited to, Aeromot-Industria
Mecanico Metalurgica Itda. model AMT-300, Diamond Aircraft Industries
DA20-A1, Diamond Aircraft Industries GmbH Model HK 36 TTS, Iniziative
Industriali Italiane S.p.A. Sky Arrow 650 series, and Stemme S10-VT
aircraft.

**Note 1:** Examples of lower SN\'s are 4,412.795, 4,412.794, and
4,412.793, and 4,420.312, 4,420.311, and 4,420.310.

**Note 2:** This AD applies to each engine identified in the preceding
applicability provision, regardless of whether it has been modified,
altered, or repaired in the area subject to the requirements of this AD.
For engines that have been modified, altered, or repaired so that the
performance of the requirements of this AD is affected, the
owner/operator must request approval for an alternative method of
compliance in accordance with paragraph (c) of this AD. The request
should include an assessment of the effect of the modification,
alteration, or repair on the unsafe condition addressed by this AD; and,
if the unsafe condition has not been eliminated, the request should
include specific proposed actions to address it.

**Compliance**

Compliance with this AD is required as indicated, unless already done.

To prevent oil loss caused by cracks in the engine crankcase, which
could lead to in-flight failure of the engine and forced landing, do the
following:

**Initial Inspection**

\(a\) Within 50 hours time-in-service (TIS) from the effective date of
this AD, perform a visual inspection as follows:

\(1\) Inspect the engine crankcase (item 1, Figure 1 of this AD) for
cracks especially in the area of cylinder 1 upper side (item 2), between
cylinder 1 and 3 upper side (item 3), and cylinder 4 lower side (item
4).

![](media/image6.png){width="6.79375in" height="9.043055555555556in"}
(2) Cracks in crankcases of engines with a ROTAX cooling air baffle may
not be easily visible, and oil leaks may be an indication of cracks.
Visually inspect for oil leaks in areas of (item 2) and (item 3).

\(3\) If oil leaks are found, determine the source by either using a
borescope or removing the object blocking the view such as the air
baffle or accessory, and perform the inspection.

\(4\) If the engine crankcase is cracked, replace engine before further
flight. Repair oil leaks from any other cause.

**Note 3:** Information concerning this inspection can be found in
Bombardier-Rotax mandatory service bulletins No\'s. SB-912-029, dated
May 2001/SB-914-018, Revision 1, dated December 2001.

**Repetitive Inspections**

\(b\) Visually inspect the engine crankcase (item 1, Figure 1 of this
AD) for cracks at each 100-hour, annual, or progressive inspection, or
within 110 hours TIS since last inspection, whichever occurs first, in
accordance with paragraph (a) of this AD.

**Alternative Methods of Compliance**

\(c\) An alternative method of compliance or adjustment of the
compliance time that provides an acceptable level of safety may be used
if approved by the Manager, Engine Certification Office (ECO). Operators
must submit their requests through an appropriate FAA Principal
Maintenance Inspector, who may add comments and then send it to the
Manager, ECO.

**Note 4:** Information concerning the existence of approved alternative
methods of compliance with this airworthiness directive, if any, may be
obtained from the ECO.

**Special Flight Permits**

\(d\) Special flight permits may be issued in accordance with Secs.
21.197 and 21.199 of the Federal Aviation Regulations (14 CFR 21.197 and
21.199) to operate the aircraft to a location where the requirements of
this AD can be done.

**Note 5:** The subject of this AD is addressed in Austro Control
airworthiness directive No. 107 R1, dated December 1, 2001.

**Effective Date**

\(e\) This amendment becomes effective on August 30, 2002.

Issued in Burlington, Massachusetts, on August 7, 2002.

Jay J. Pardee,

Manager, Engine and Propeller Directorate, Aircraft Certification
Service.

\[FR Doc. 02-20679 Filed 8-14-02; 8:45 am\]

BILLING CODE 4910-13-P

**BW 2002-17**

**AGUSTA S.p.A.**

**AIRWORTHINESS DIRECTIVE**

**EMERGENCY**

**SMALL AIRCRAFT, ROTORCRAFT, GLIDERS, BALLOONS, & AIRSHIPS**

**2002-17-51 AGUSTA S.p.A.: Docket No. 2002-SW-42-AD. Supersedes
Emergency AD 2002-14-51, Docket No. 2002-SW-35-AD.**

Applicability: Model A109E helicopters, with tail rotor blade, part
number 109-8132-01-111, installed, certificated in any category.

Note 1: This AD applies to each helicopter identified in the preceding
applicability provision, regardless of whether it has been otherwise
modified, altered, or repaired in the area subject to the requirements
of this AD. For helicopters that have been modified, altered, or
repaired so that the performance of the requirements of this AD is
affected, the owner/operator must request approval for an alternative
method of compliance in accordance with paragraph (e) of this AD. The
request should include an assessment of the effect of the modification,
alteration, or repair on the unsafe condition addressed by this AD; and
if the unsafe condition has not been eliminated, the request should
include specific proposed actions to address it.

Compliance: Required as indicated, unless accomplished previously.

To prevent failure of the tail rotor blade and subsequent loss of
control of the helicopter, accomplish the following:

\(a\) Before further flight, install a placard in the helicopter and
mark the airspeed indicator at 140 knots indicated airspeed (KIAS) to
indicate a reduction in the helicopter never exceed speed (Vne) of 28
KIAS in accordance with the Compliance Instructions, Part I, of Agusta
Alert Bollettino Tecnico No. 109EP-30, Revision A, dated July 25, 2002
(BT).

\(b\) Before each start of the helicopter engines, visually check both
sides of each tail rotor blade for a crack in the area depicted in
Figure 1 of this AD. An owner/operator (pilot) holding at least a
private pilot certificate may perform this visual check and must enter
compliance with this paragraph into the aircraft maintenance records in
accordance with 14 CFR 43.11 and 91.417(a)(2)(v). See Figure 1:

![](media/image7.png){width="7.15in" height="5.471527777777778in"}

Note 2: Paint irregularities on the tail rotor blade may be due to a
crack.

\(c\) Within 25 hours time-in-service (TIS), and thereafter at intervals
not to exceed 25 hours TIS, and anytime there is an increase in
vibration levels, using a 5x or higher magnifying glass, visually
inspect each tail rotor blade for a crack before further flight in
accordance with the Compliance Instructions, Part III, paragraphs 1.
through 5., of the BT. Reporting to Agusta Service Engineering is not
required. If you are unable to determine by the visual inspection
whether there is a crack, dye penetrant inspect the tail rotor blade for
a crack in accordance with the Compliance Instructions, Part III,
paragraph 6., of the BT.

\(d\) Replace any cracked tail rotor blade with an airworthy blade
before further flight.

\(e\) An alternative method of compliance or adjustment of the
compliance time that provides an acceptable level of safety may be used
if approved by the Manager, Regulations Group, Rotorcraft Directorate,
FAA. Operators shall submit their requests through an FAA Principal
Maintenance Inspector, who may concur or comment and then send it to the
Manager, Regulations Group.

Note 3: Information concerning the existence of approved alternative
methods of compliance with this AD, if any, may be obtained from the
Regulations Group.

\(f\) Special flight permits will not be issued.

\(g\) Copies of the applicable service information may be obtained from
Agusta, 21017 Cascina Costa di Samarate (VA) Italy, Via Giovanni Agusta
520, telephone 39 (0331) 229111, fax 39 (0331) 229605-222595.

\(h\) **Emergency AD 2002-17-51, issued August 19, 2002, becomes
effective upon receipt.**

Note 4: The subject of this AD is addressed in Ente Nazionale per
l'Aviazione Civile (Italy) AD No. 2002-384, dated July 29, 2002.

FOR FURTHER INFORMATION CONTACT: Jim Grigg, Aviation Safety Engineer,
FAA, Rotorcraft Directorate, Rotorcraft Standards Staff, Fort Worth,
Texas 76193-0110, telephone (817) 222-5490, fax (817) 222-5961.

Issued in Fort Worth, Texas, on August 19, 2002.

David A. Downey,

Manager, Rotorcraft Directorate,

Aircraft Certification Service.

**BW 2002-17**

**AGUSTA S.p.A.**

**AIRWORTHINESS DIRECTIVE**

**EMERGENCY**

**SMALL AIRCRAFT, ROTORCRAFT, GLIDERS, BALLOONS, & AIRSHIPS**

**2002-17-52 AGUSTA S.p.A.: Docket No. 2002-SW-43-AD. Supersedes
Emergency AD 2002-14-51, Docket No. 2002-SW-35-AD.**

Applicability: Model A119 helicopters, with hub and tail rotor blades
assembly, part number (P/N) 109-8131-02-149, or tail rotor blades, P/N
109-8132-01-111, installed, certificated in any category.

Note 1: This AD applies to each helicopter identified in the preceding
applicability provision, regardless of whether it has been otherwise
modified, altered, or repaired in the area subject to the requirements
of this AD. For helicopters that have been modified, altered, or
repaired so that the performance of the requirements of this AD is
affected, the owner/operator must request approval for an alternative
method of compliance in accordance with paragraph (i) of this AD. The
request should include an assessment of the effect of the modification,
alteration, or repair on the unsafe condition addressed by this AD; and
if the unsafe condition has not been eliminated, the request should
include specific proposed actions to address it.

Compliance: Required as indicated, unless accomplished previously.

To prevent failure of the tail rotor blade and subsequent loss of
control of the helicopter, accomplish the following:

\(a\) Before further flight, install a placard in the helicopter and
mark the airspeed indicator at 132 knots indicated airspeed (KIAS) to
indicate a reduction in the helicopter never exceed speed (Vne) by 30
KIAS. Make and install the placard in accordance with the Compliance
Instructions, Part I, of Agusta Alert Bollettino Tecnico No. 119-6,
Revision A, dated July 12, 2002 (BT). On the glass of the airspeed
indicator, apply a red mark over the value of 132 KIAS.

\(b\) Before each start of the helicopter engine, visually check both
sides of each tail rotor blade for a crack in the area depicted in
Figure 1 of this AD. An owner/operator (pilot) holding at least a
private pilot certificate may perform this visual check and must enter
compliance with this paragraph into the aircraft maintenance records in
accordance with 14 CFR 43.11 and 91.417(a)(2)(v). See Figure 1:

![](media/image8.png){width="5.927083333333333in" height="4.5625in"}

Note 2: Paint irregularities on the tail rotor blade may be due to a
crack.

\(c\) Within 25 hours time-in-service (TIS), and thereafter at intervals
not to exceed 25 hours TIS, and any time an increase in vibration levels
occur, using a 5x or higher magnifying glass, visually inspect each tail
rotor blade for a crack in accordance with the Compliance Instructions,
Part III, paragraphs 1. through 5., of the BT. Reporting to Agusta
Service Engineering is not required. If you are unable to determine by
the visual inspection whether there is a crack, dye penetrant inspect
the tail rotor blade for a crack in accordance with the Compliance
Instructions, Part III, paragraph 6., of the BT.

\(d\) Replace any cracked tail rotor blade with an airworthy blade
before further flight.

\(e\) Not later than October 30, 2002, in accordance with the Compliance
Instructions, Part IV, and Figure 2 of the BT:

\(1\) Install a new grip and bushing assembly, P/N 109-8131-02-147, into
tail rotor hub and blade assembly, P/N 109-8131-02-149;

\(2\) Reidentify the modified tail rotor hub and grips assembly, P/N
109-8131-02-141, as P/N 109-8132-01-153; and

\(3\) Reidentify the modified tail rotor hub and blade assembly, P/N
109-8131-02-149, as P/N 109-8131-02-155.

Returning the grips to the manufacturer is not required by this AD.

\(f\) After completing the actions required by paragraph (e) of this AD,
remove the Vne placard and the airspeed indicator marking at 132 KIAS
that were installed in accordance with paragraph (a) of this AD.
Modifying and reidentifying the parts as required by paragraph (e) of
this AD is terminating actions for the requirements of paragraph (a) of
this AD and restores the original Vne.

\(g\) After completing the actions required by paragraph (e) of this AD,
establish a retirement life of 1,000 hours TIS for tail rotor control
rod, P/N 109-0135-02-101.

\(h\) After completing the actions required by paragraph (e) of this AD,
revise the helicopter Airworthiness Limitations Section of the Agusta
Model A119 helicopter maintenance manual by inserting a 1,000 hour TIS
retirement life for each tail rotor control rod, P/N 109-0135-02-101.

\(i\) An alternative method of compliance or adjustment of the
compliance time that provides an acceptable level of safety may be used
if approved by the Manager, Regulations Group, Rotorcraft Directorate,
FAA. Operators shall submit their requests through an FAA Principal
Maintenance Inspector, who may concur or comment and then send it to the
Manager, Regulations Group.

Note 3: Information concerning the existence of approved alternative
methods of compliance with this AD, if any, may be obtained from the
Regulations Group.

\(j\) Special flight permits will not be issued.

\(k\) Copies of the applicable service information may be obtained from
Agusta, 21017 Cascina Costa di Samarate (VA) Italy, Via Giovanni Agusta
520, telephone 39 (0331) 229111, fax 39 (0331) 229605-222595.

\(l\) **Emergency AD 2002-17-52, issued August 21, 2002, becomes
effective upon receipt.**

Note 4: The subject of this AD is addressed in Ente Nazionale per
l'Aviazione Civile (Italy) AD No. 2002-367, dated July 16, 2002.

FOR FURTHER INFORMATION CONTACT: Richard Monschke, Aviation Safety
Engineer, FAA, Rotorcraft Directorate, Rotorcraft Standards Staff, Fort
Worth, Texas 76193-0110, telephone (817) 222-5116, fax (817) 222-5961.

Issued in Fort Worth, Texas, on August 21, 2002.

David A. Downey,

Manager, Rotorcraft Directorate,

Aircraft Certification Service.

**BW 2002-17**

**TEXTRON LYCOMING**

**AIRWORTHINESS DIRECTIVE**

**ENGINE**

**EMERGENCY**

**SMALL AIRCRAFT, ROTORCRAFT, GLIDERS, BALLOONS, & AIRSHIPS**

**2002‑17‑53** **Textron Lycoming**: Docket No. 20002‑NE‑03‑AD.
Supersedes Emergency AD 2002‑04‑51.

## Applicability

This AD is applicable to all Textron Lycoming LTIO-540 and TIO-540
engines, rated at 300 HP or greater.

**Note 1**:  This AD applies to each engine identified in the preceding
applicability provision, regardless of whether it has been modified,
altered, or repaired in the area subject to the requirements of this AD.
For engines that have been modified, altered, or repaired so that the
performance of the requirements of this AD is affected, the
owner/operator must request approval for an alternative method of
compliance in accordance with paragraph (e) of this AD. The request
should include an assessment of the effect of the modification,
alteration, or repair on the unsafe condition addressed by this AD; and,
if the unsafe condition has not been eliminated, the request should
include specific proposed actions to address it.

## Compliance

Compliance with this AD is required before further flight.

To prevent crankshaft failure, which could result in total engine power
loss, in-flight engine failure and possible forced landing, do the
following:

\(a\) For any engine listed in Table 1 of this AD, replace the
crankshaft before further flight with a crankshaft that is not listed by
SN in Table 2 of this AD. Tables 1 and 2 follow:

Table 1 List of Engine SN's

  --------------- ---------- --------------- ----------- --------------- -----------
  MODEL           ENGINE S/N MODEL           ENGINE S/N  MODEL           ENGINE S/N

  LTIO-540-F2BD   1144-68A   LTIO-540-J2B    2641-68A    LTIO-540-J2BD   1885-68A

  LTIO-540-F2BD   1272-68A   LTIO-540-J2B    2650-68A    LTIO-540-J2BD   1908-68A

  LTIO-540-F2BD   1465-68A   LTIO-540-J2B    2694-68A    LTIO-540-J2BD   1940-68A

  LTIO-540-F2BD   1871-68A   LTIO-540-J2B    2807-68A    LTIO-540-J2BD   1941-68A

  LTIO-540-F2BD   1874-68A   LTIO-540-J2B    2865-68A    LTIO-540-J2BD   1994-68A

  LTIO-540-F2BD   2103-68A   LTIO-540-J2B    2888-68A    LTIO-540-J2BD   2111-68A

  LTIO-540-F2BD   2645-68A   LTIO-540-J2B    2968-68A    LTIO-540-J2BD   2286-68A

  LTIO-540-F2BD   2988-68A   LTIO-540-J2B    2991-68A    LTIO-540-J2BD   2330-68A

  LTIO-540-J2B    345-68A    LTIO-540-J2B    2994-68A    LTIO-540-J2BD   2419-68A

  LTIO-540-J2B    376-68A    LTIO-540-J2BD   149-68A     LTIO-540-J2BD   2450-68A

  LTIO-540-J2B    701-68A    LTIO-540-J2BD   172-68A     LTIO-540-J2BD   2485-68A

  LTIO-540-J2B    703-68A    LTIO-540-J2BD   186-68A     LTIO-540-J2BD   2500-68A
  --------------- ---------- --------------- ----------- --------------- -----------

  -------------- ----------- --------------- ----------- --------------- -----------
  LTIO-540-J2B   788-68A     LTIO-540-J2BD   217-68A     LTIO-540-J2BD   2667-68A

  LTIO-540-J2B   877-68A     LTIO-540-J2BD   297-68A     LTIO-540-J2BD   2813-68A

  LTIO-540-J2B   1017-68A    LTIO-540-J2BD   355-68A     LTIO-540-J2BD   2823-68A

  LTIO-540-J2B   1127-68A    LTIO-540-J2BD   530-68A     LTIO-540-J2BD   2844-68A

  LTIO-540-J2B   1159-68A    LTIO-540-J2BD   648-68A     LTIO-540-J2BD   2846-68A

  LTIO-540-J2B   1206-68A    LTIO-540-J2BD   732-68A     LTIO-540-J2BD   2856-68A

  LTIO-540-J2B   1252-68A    LTIO-540-J2BD   741-68A     LTIO-540-J2BD   2900-68A

  LTIO-540-J2B   1282-68A    LTIO-540-J2BD   752-68A     LTIO-540-J2BD   2912-68A

  LTIO-540-J2B   1333-68A    LTIO-540-J2BD   839-68A     LTIO-540-J2BD   2932-68A

  LTIO-540-J2B   1401-68A    LTIO-540-J2BD   979-68A     LTIO-540-J2BD   2942-68A

  LTIO-540-J2B   1426-68A    LTIO-540-J2BD   980-68A     LTIO-540-J2BD   2986-68A

  LTIO-540-J2B   1488-68A    LTIO-540-J2BD   999-68A     LTIO-540-J2BD   2990-68A

  LTIO-540-J2B   1566-68A    LTIO-540-J2BD   1027-68A    LTIO-540-J2BD   2992-68A

  LTIO-540-J2B   1928-68A    LTIO-540-J2BD   1048-68A    LTIO-540-J2BD   2993-68A

  LTIO-540-J2B   1984-68A    LTIO-540-J2BD   1058-68A    LTIO-540-J2BD   3001-68A

  LTIO-540-J2B   2018-68A    LTIO-540-J2BD   1186-68A    TIO-540-A2B     2169-61A

  LTIO-540-J2B   2079-68A    LTIO-540-J2BD   1249-68A    TIO-540-A2B     4732-61A

  LTIO-540-J2B   2094-68A    LTIO-540-J2BD   1271-68A    TIO-540-A2B     5911-61A

  LTIO-540-J2B   2108-68A    LTIO-540-J2BD   1331-68A    TIO-540-A2B     6274-61A

  LTIO-540-J2B   2164-68A    LTIO-540-J2BD   1344-68A    TIO-540-A2B     6468-61A

  LTIO-540-J2B   2168-68A    LTIO-540-J2BD   1395-68A    TIO-540-A2B     6629-61A

  LTIO-540-J2B   2317-68A    LTIO-540-J2BD   1517-68A    TIO-540-A2B     7277-61A

  LTIO-540-J2B   2331-68A    LTIO-540-J2BD   1563-68A    TIO-540-A2B     7931-61A

  LTIO-540-J2B   2455-68A    LTIO-540-J2BD   1598-68A    TIO-540-A2B     10119-61A

  LTIO-540-J2B   2572-68A    LTIO-540-J2BD   1716-68A    TIO-540-A2B     10292-61A

  LTIO-540-J2B   2622-68A    LTIO-540-J2BD   1775-68A    TIO-540-A2B     10453-61A

  LTIO-540-J2B   2636-68A    LTIO-540-J2BD   1868-68A    TIO-540-A2B     10742-61A

  TIO-540-A2B    11111-61A   TIO-540-AE2A    6955-61A    TIO-540-AE2A    10537-61A

  TIO-540-A2C    1678-61A    TIO-540-AE2A    6959-61A    TIO-540-AE2A    10540-61A

  TIO-540-A2C    3038-61A    TIO-540-AE2A    7738-61A    TIO-540-AE2A    10545-61A

  TIO-540-A2C    3280-61A    TIO-540-AE2A    7825-61A    TIO-540-AE2A    10547-61A

  TIO-540-A2C    3558-61A    TIO-540-AE2A    8254-61A    TIO-540-AE2A    10552-61A

  TIO-540-A2C    3654-61A    TIO-540-AE2A    9647-61A    TIO-540-AE2A    10559-61A

  TIO-540-A2C    4067-61A    TIO-540-AE2A    9761-61A    TIO-540-AE2A    10560-61A

  TIO-540-A2C    4141-61A    TIO-540-AE2A    9777-61A    TIO-540-AE2A    10569-61A

  TIO-540-A2C    4281-61A    TIO-540-AE2A    9804-61A    TIO-540-AE2A    10572-61A

  TIO-540-A2C    4611-61A    TIO-540-AE2A    9822-61A    TIO-540-AE2A    10578-61A

  TIO-540-A2C    4824-61A    TIO-540-AE2A    9838-61A    TIO-540-AE2A    10591-61A
  -------------- ----------- --------------- ----------- --------------- -----------

  -------------- ----------- -------------- ----------- -------------- -----------
  TIO-540-A2C    5324-61A    TIO-540-AE2A   9849-61A    TIO-540-AE2A   10593-61A

  TIO-540-A2C    5937-61A    TIO-540-AE2A   9853-61A    TIO-540-AE2A   10594-61A

  TIO-540-A2C    6618-61A    TIO-540-AE2A   9952-61A    TIO-540-AE2A   10595-61A

  TIO-540-A2C    7264-61A    TIO-540-AE2A   10027-61A   TIO-540-AE2A   10603-61A

  TIO-540-A2C    7401-61A    TIO-540-AE2A   10072-61A   TIO-540-AE2A   10608-61A

  TIO-540-A2C    7516-61A    TIO-540-AE2A   10168-61A   TIO-540-AE2A   10620-61A

  TIO-540-A2C    7763-61A    TIO-540-AE2A   10173-61A   TIO-540-AE2A   10622-61A

  TIO-540-A2C    7961-61A    TIO-540-AE2A   10338-61A   TIO-540-AE2A   10645-61A

  TIO-540-A2C    7965-61A    TIO-540-AE2A   10382-61A   TIO-540-AE2A   10646-61A

  TIO-540-A2C    8309-61A    TIO-540-AE2A   10387-61A   TIO-540-AE2A   10647-61A

  TIO-540-A2C    8810-61A    TIO-540-AE2A   10393-61A   TIO-540-AE2A   10648-61A

  TIO-540-A2C    8855-61A    TIO-540-AE2A   10405-61A   TIO-540-AE2A   10650-61A

  TIO-540-A2C    8965-61A    TIO-540-AE2A   10408-61A   TIO-540-AE2A   10756-61A

  TIO-540-A2C    9134-61A    TIO-540-AE2A   10427-61A   TIO-540-AE2A   10758-61A

  TIO-540-A2C    9410-61A    TIO-540-AE2A   10436-61A   TIO-540-AE2A   10759-61A

  TIO-540-A2C    9440-61A    TIO-540-AE2A   10448-61A   TIO-540-AE2A   10760-61A

  TIO-540-A2C    9833-61A    TIO-540-AE2A   10449-61A   TIO-540-AE2A   10762-61A

  TIO-540-A2C    9863-61A    TIO-540-AE2A   10451-61A   TIO-540-AE2A   10766-61A

  TIO-540-A2C    9895-61A    TIO-540-AE2A   10455-61A   TIO-540-AE2A   10781-61A

  TIO-540-A2C    9988-61A    TIO-540-AE2A   10459-61A   TIO-540-AE2A   10785-61A

  TIO-540-A2C    10401-61A   TIO-540-AE2A   10462-61A   TIO-540-AE2A   10793-61A

  TIO-540-A2C    11147-61A   TIO-540-AE2A   10463-61A   TIO-540-AE2A   10979-61A

  TIO-540-AE2A   2543-61A    TIO-540-AE2A   10466-61A   TIO-540-AE2A   10989-61A

  TIO-540-AE2A   2650-61A    TIO-540-AE2A   10471-61A   TIO-540-AE2A   11001-61A

  TIO-540-AE2A   4777-61A    TIO-540-AE2A   10479-61A   TIO-540-AE2A   11012-61A

  TIO-540-AE2A   5068-61A    TIO-540-AE2A   10489-61A   TIO-540-AE2A   11013-61A

  TIO-540-AE2A   5110-61A    TIO-540-AE2A   10495-61A   TIO-540-AE2A   11015-61A

  TIO-540-AE2A   5468-61A    TIO-540-AE2A   10499-61A   TIO-540-AE2A   11016-61A

  TIO-540-AE2A   6038-61A    TIO-540-AE2A   10510-61A   TIO-540-AE2A   11017-61A

  TIO-540-AE2A   6575-61A    TIO-540-AE2A   10535-61A   TIO-540-AE2A   11035-61A

  TIO-540-AE2A   11053-61A   TIO-540-AH1A   10458-61A   TIO-540-AH1A   10702-61A

  TIO-540-AE2A   11057-61A   TIO-540-AH1A   10472-61A   TIO-540-AH1A   10703-61A

  TIO-540-AE2A   11058-61A   TIO-540-AH1A   10481-61A   TIO-540-AH1A   10707-61A

  TIO-540-AE2A   11065-61A   TIO-540-AH1A   10486-61A   TIO-540-AH1A   10714-61A

  TIO-540-AE2A   11066-61A   TIO-540-AH1A   10492-61A   TIO-540-AH1A   10719-61A

  TIO-540-AE2A   11087-61A   TIO-540-AH1A   10500-61A   TIO-540-AH1A   10722-61A

  TIO-540-AE2A   11093-61A   TIO-540-AH1A   10501-61A   TIO-540-AH1A   10723-61A

  TIO-540-AE2A   11108-61A   TIO-540-AH1A   10508-61A   TIO-540-AH1A   10725-61A
  -------------- ----------- -------------- ----------- -------------- -----------

  -------------- ----------- -------------- ----------- -------------- -----------
  TIO-540-AE2A   11112-61A   TIO-540-AH1A   10519-61A   TIO-540-AH1A   10734-61A

  TIO-540-AE2A   11119-61A   TIO-540-AH1A   10524-61A   TIO-540-AH1A   10748-61A

  TIO-540-AE2A   11133-61A   TIO-540-AH1A   10530-61A   TIO-540-AH1A   10749-61A

  TIO-540-AE2A   11137-61A   TIO-540-AH1A   10533-61A   TIO-540-AH1A   10750-61A

  TIO-540-AE2A   11142-61A   TIO-540-AH1A   10567-61A   TIO-540-AH1A   10755-61A

  TIO-540-AE2A   11159-61A   TIO-540-AH1A   10570-61A   TIO-540-AH1A   10773-61A

  TIO-540-AE2A   11167-61A   TIO-540-AH1A   10573-61A   TIO-540-AH1A   10776-61A

  TIO-540-AE2A   11184-61A   TIO-540-AH1A   10583-61A   TIO-540-AH1A   10778-61A

  TIO-540-AE2A   11188-61A   TIO-540-AH1A   10587-61A   TIO-540-AH1A   10790-61A

  TIO-540-AE2A   11190-61A   TIO-540-AH1A   10588-61A   TIO-540-AH1A   10797-61A

  TIO-540-AE2A   11191-61A   TIO-540-AH1A   10600-61A   TIO-540-AH1A   10798-61A

  TIO-540-AE2A   11194-61A   TIO-540-AH1A   10607-61A   TIO-540-AH1A   10799-61A

  TIO-540-AE2A   11195-61A   TIO-540-AH1A   10619-61A   TIO-540-AH1A   10800-61A

  TIO-540-AE2A   11196-61A   TIO-540-AH1A   10629-61A   TIO-540-AH1A   10801-61A

  TIO-540-AE2A   11197-61A   TIO-540-AH1A   10632-61A   TIO-540-AH1A   10802-61A

  TIO-540-AE2A   11231-61A   TIO-540-AH1A   10633-61A   TIO-540-AH1A   10814-61A

  TIO-540-AE2A   11259-61A   TIO-540-AH1A   10634-61A   TIO-540-AH1A   10818-61A

  TIO-540-AH1A   671-61A     TIO-540-AH1A   10635-61A   TIO-540-AH1A   10822-61A

  TIO-540-AH1A   2346-61A    TIO-540-AH1A   10640-61A   TIO-540-AH1A   10833-61A

  TIO-540-AH1A   3545-61A    TIO-540-AH1A   10652-61A   TIO-540-AH1A   10836-61A

  TIO-540-AH1A   3948-61A    TIO-540-AH1A   10653-61A   TIO-540-AH1A   10840-61A

  TIO-540-AH1A   8268-61A    TIO-540-AH1A   10657-61A   TIO-540-AH1A   10843-61A

  TIO-540-AH1A   10138-61A   TIO-540-AH1A   10658-61A   TIO-540-AH1A   10849-61A

  TIO-540-AH1A   10343-61A   TIO-540-AH1A   10659-61A   TIO-540-AH1A   10852-61A

  TIO-540-AH1A   10352-61A   TIO-540-AH1A   10664-61A   TIO-540-AH1A   10853-61A

  TIO-540-AH1A   10378-61A   TIO-540-AH1A   10666-61A   TIO-540-AH1A   10854-61A

  TIO-540-AH1A   10382-61A   TIO-540-AH1A   10672-61A   TIO-540-AH1A   10861-61A

  TIO-540-AH1A   10398-61A   TIO-540-AH1A   10678-61A   TIO-540-AH1A   10867-61A

  TIO-540-AH1A   10406-61A   TIO-540-AH1A   10679-61A   TIO-540-AH1A   10872-61A

  TIO-540-AH1A   10434-61A   TIO-540-AH1A   10680-61A   TIO-540-AH1A   10873-61A

  TIO-540-AH1A   10450-61A   TIO-540-AH1A   10688-61A   TIO-540-AH1A   10878-61A

  TIO-540-AH1A   10456-61A   TIO-540-AH1A   10700-61A   TIO-540-AH1A   10879-61A

  TIO-540-AH1A   10457-61A   TIO-540-AH1A   10701-61A   TIO-540-AH1A   10881-61A

  TIO-540-AH1A   10897-61A   TIO-540-AH1A   11122-61A   TIO-540-AJ1A   10114-61A

  TIO-540-AH1A   10952-61A   TIO-540-AH1A   11124-61A   TIO-540-AJ1A   10243-61A

  TIO-540-AH1A   10953-61A   TIO-540-AH1A   11129-61A   TIO-540-AJ1A   10341-61A

  TIO-540-AH1A   10954-61A   TIO-540-AH1A   11134-61A   TIO-540-AJ1A   10354-61A

  TIO-540-AH1A   10955-61A   TIO-540-AH1A   11138-61A   TIO-540-AJ1A   10355-61A
  -------------- ----------- -------------- ----------- -------------- -----------

  -------------- ----------- -------------- ----------- -------------- -----------
  TIO-540-AH1A   10957-61A   TIO-540-AH1A   11139-61A   TIO-540-AJ1A   10356-61A

  TIO-540-AH1A   10958-61A   TIO-540-AH1A   11140-61A   TIO-540-AJ1A   10357-61A

  TIO-540-AH1A   10965-61A   TIO-540-AH1A   11141-61A   TIO-540-AJ1A   10362-61A

  TIO-540-AH1A   10966-61A   TIO-540-AH1A   11157-61A   TIO-540-AJ1A   10367-61A

  TIO-540-AH1A   10968-61A   TIO-540-AH1A   11158-61A   TIO-540-AJ1A   10369-61A

  TIO-540-AH1A   10973-61A   TIO-540-AH1A   11165-61A   TIO-540-AJ1A   10371-61A

  TIO-540-AH1A   10984-61A   TIO-540-AH1A   11183-61A   TIO-540-AJ1A   10372-61A

  TIO-540-AH1A   10985-61A   TIO-540-AH1A   11238-61A   TIO-540-AJ1A   10373-61A

  TIO-540-AH1A   10986-61A   TIO-540-AH1A   11243-61A   TIO-540-AJ1A   10377-61A

  TIO-540-AH1A   10987-61A   TIO-540-AH1A   11246-61A   TIO-540-AJ1A   10384-61A

  TIO-540-AH1A   10988-61A   TIO-540-AH1A   11247-61A   TIO-540-AJ1A   10385-61A

  TIO-540-AH1A   10997-61A   TIO-540-AH1A   11250-61A   TIO-540-AJ1A   10388-61A

  TIO-540-AH1A   10998-61A   TIO-540-AH1A   11251-61A   TIO-540-AJ1A   10389-61A

  TIO-540-AH1A   10999-61A   TIO-540-AH1A   11258-61A   TIO-540-AJ1A   10390-61A

  TIO-540-AH1A   11019-61A   TIO-540-AH1A   11260-61A   TIO-540-AJ1A   10391-61A

  TIO-540-AH1A   11020-61A   TIO-540-AH1A   11261-61A   TIO-540-AJ1A   10400-61A

  TIO-540-AH1A   11022-61A   TIO-540-AH1A   11263-61A   TIO-540-AJ1A   10404-61A

  TIO-540-AH1A   11026-61A   TIO-540-AH1A   11270-61A   TIO-540-AJ1A   10416-61A

  TIO-540-AH1A   11038-61A   TIO-540-AH1A   11271-61A   TIO-540-AJ1A   10428-61A

  TIO-540-AH1A   11042-61A   TIO-540-AH1A   11272-61A   TIO-540-AJ1A   10437-61A

  TIO-540-AH1A   11047-61A   TIO-540-AH1A   11273-61A   TIO-540-AJ1A   10440-61A

  TIO-540-AH1A   11059-61A   TIO-540-AH1A   11274-61A   TIO-540-AJ1A   10444-61A

  TIO-540-AH1A   11060-61A   TIO-540-AH1A   11275-61A   TIO-540-AJ1A   10445-61A

  TIO-540-AH1A   11079-61A   TIO-540-AH1A   11277-61A   TIO-540-AJ1A   10446-61A

  TIO-540-AH1A   11080-61A   TIO-540-AH1A   11278-61A   TIO-540-AJ1A   10454-61A

  TIO-540-AH1A   11081-61A   TIO-540-AH1A   11282-61A   TIO-540-AJ1A   10469-61A

  TIO-540-AH1A   11082-61A   TIO-540-AH1A   11293-61A   TIO-540-AJ1A   10470-61A

  TIO-540-AH1A   11083-61A   TIO-540-AH1A   11299-61A   TIO-540-AJ1A   10477-61A

  TIO-540-AH1A   11097-61A   TIO-540-AH1A   11300-61A   TIO-540-AJ1A   10478-61A

  TIO-540-AH1A   11098-61A   TIO-540-AH1A   11309-61A   TIO-540-AJ1A   10483-61A

  TIO-540-AH1A   11099-61A   TIO-540-AJ1A   4377-61A    TIO-540-AJ1A   10484-61A

  TIO-540-AH1A   11104-61A   TIO-540-AJ1A   8171-61A    TIO-540-AJ1A   10490-61A

  TIO-540-AH1A   11109-61A   TIO-540-AJ1A   8627-61A    TIO-540-AJ1A   10491-61A

  TIO-540-AH1A   11118-61A   TIO-540-AJ1A   9442-61A    TIO-540-AJ1A   10497-61A

  TIO-540-AH1A   11120-61A   TIO-540-AJ1A   9634-61A    TIO-540-AJ1A   10503-61A

  TIO-540-AH1A   11121-61A   TIO-540-AJ1A   10059-61A   TIO-540-AJ1A   10504-61A

  TIO-540-AJ1A   10506-61A   TIO-540-AJ1A   10674-61A   TIO-540-AJ1A   10807-61A

  TIO-540-AJ1A   10512-61A   TIO-540-AJ1A   10675-61A   TIO-540-AJ1A   10809-61A
  -------------- ----------- -------------- ----------- -------------- -----------

  -------------- ----------- -------------- ----------- -------------- -----------
  TIO-540-AJ1A   10518-61A   TIO-540-AJ1A   10676-61A   TIO-540-AJ1A   10812-61A

  TIO-540-AJ1A   10520-61A   TIO-540-AJ1A   10686-61A   TIO-540-AJ1A   10815-61A

  TIO-540-AJ1A   10521-61A   TIO-540-AJ1A   10689-61A   TIO-540-AJ1A   10816-61A

  TIO-540-AJ1A   10525-61A   TIO-540-AJ1A   10690-61A   TIO-540-AJ1A   10820-61A

  TIO-540-AJ1A   10526-61A   TIO-540-AJ1A   10691-61A   TIO-540-AJ1A   10821-61A

  TIO-540-AJ1A   10527-61A   TIO-540-AJ1A   10693-61A   TIO-540-AJ1A   10824-61A

  TIO-540-AJ1A   10542-61A   TIO-540-AJ1A   10696-61A   TIO-540-AJ1A   10827-61A

  TIO-540-AJ1A   10543-61A   TIO-540-AJ1A   10697-61A   TIO-540-AJ1A   10831-61A

  TIO-540-AJ1A   10544-61A   TIO-540-AJ1A   10698-61A   TIO-540-AJ1A   10832-61A

  TIO-540-AJ1A   10551-61A   TIO-540-AJ1A   10699-61A   TIO-540-AJ1A   10834-61A

  TIO-540-AJ1A   10555-61A   TIO-540-AJ1A   10704-61A   TIO-540-AJ1A   10835-61A

  TIO-540-AJ1A   10561-61A   TIO-540-AJ1A   10705-61A   TIO-540-AJ1A   10841-61A

  TIO-540-AJ1A   10562-61A   TIO-540-AJ1A   10713-61A   TIO-540-AJ1A   10842-61A

  TIO-540-AJ1A   10563-61A   TIO-540-AJ1A   10717-61A   TIO-540-AJ1A   10844-61A

  TIO-540-AJ1A   10564-61A   TIO-540-AJ1A   10721-61A   TIO-540-AJ1A   10845-61A

  TIO-540-AJ1A   10565-61A   TIO-540-AJ1A   10727-61A   TIO-540-AJ1A   10846-61A

  TIO-540-AJ1A   10574-61A   TIO-540-AJ1A   10728-61A   TIO-540-AJ1A   10848-61A

  TIO-540-AJ1A   10580-61A   TIO-540-AJ1A   10729-61A   TIO-540-AJ1A   10856-61A

  TIO-540-AJ1A   10582-61A   TIO-540-AJ1A   10730-61A   TIO-540-AJ1A   10857-61A

  TIO-540-AJ1A   10586-61A   TIO-540-AJ1A   10731-61A   TIO-540-AJ1A   10858-61A

  TIO-540-AJ1A   10589-61A   TIO-540-AJ1A   10736-61A   TIO-540-AJ1A   10860-61A

  TIO-540-AJ1A   10596-61A   TIO-540-AJ1A   10737-61A   TIO-540-AJ1A   10864-61A

  TIO-540-AJ1A   10601-61A   TIO-540-AJ1A   10738-61A   TIO-540-AJ1A   10865-61A

  TIO-540-AJ1A   10604-61A   TIO-540-AJ1A   10746-61A   TIO-540-AJ1A   10868-61A

  TIO-540-AJ1A   10605-61A   TIO-540-AJ1A   10747-61A   TIO-540-AJ1A   10874-61A

  TIO-540-AJ1A   10615-61A   TIO-540-AJ1A   10752-61A   TIO-540-AJ1A   10875-61A

  TIO-540-AJ1A   10617-61A   TIO-540-AJ1A   10753-61A   TIO-540-AJ1A   10876-61A

  TIO-540-AJ1A   10624-61A   TIO-540-AJ1A   10769-61A   TIO-540-AJ1A   10877-61A

  TIO-540-AJ1A   10627-61A   TIO-540-AJ1A   10770-61A   TIO-540-AJ1A   10895-61A

  TIO-540-AJ1A   10628-61A   TIO-540-AJ1A   10771-61A   TIO-540-AJ1A   10896-61A

  TIO-540-AJ1A   10631-61A   TIO-540-AJ1A   10774-61A   TIO-540-AJ1A   10960-61A

  TIO-540-AJ1A   10641-61A   TIO-540-AJ1A   10779-61A   TIO-540-AJ1A   10961-61A

  TIO-540-AJ1A   10654-61A   TIO-540-AJ1A   10783-61A   TIO-540-AJ1A   10962-61A

  TIO-540-AJ1A   10661-61A   TIO-540-AJ1A   10784-61A   TIO-540-AJ1A   10972-61A

  TIO-540-AJ1A   10662-61A   TIO-540-AJ1A   10786-61A   TIO-540-AJ1A   10976-61A

  TIO-540-AJ1A   10667-61A   TIO-540-AJ1A   10787-61A   TIO-540-AJ1A   10977-61A

  TIO-540-AJ1A   10668-61A   TIO-540-AJ1A   10803-61A   TIO-540-AJ1A   10980-61A

  TIO-540-AJ1A   10669-61A   TIO-540-AJ1A   10804-61A   TIO-540-AJ1A   10981-61A
  -------------- ----------- -------------- ----------- -------------- -----------

  -------------- ----------- -------------- ----------- -------------- -----------
  TIO-540-AJ1A   10673-61A   TIO-540-AJ1A   10805-61A   TIO-540-AJ1A   10982-61A

  TIO-540-AJ1A   10983-61A   TIO-540-AJ1A   11185-61A   TIO-540-J2B    1234-61A

  TIO-540-AJ1A   10991-61A   TIO-540-AJ1A   11189-61A   TIO-540-J2B    2315-61A

  TIO-540-AJ1A   10992-61A   TIO-540-AJ1A   11193-61A   TIO-540-J2B    2453-61A

  TIO-540-AJ1A   10993-61A   TIO-540-AJ1A   11198-61A   TIO-540-J2B    3167-61A

  TIO-540-AJ1A   10994-61A   TIO-540-AJ1A   11199-61A   TIO-540-J2B    3218-61A

  TIO-540-AJ1A   10995-61A   TIO-540-AJ1A   11203-61A   TIO-540-J2B    3590-61A

  TIO-540-AJ1A   10996-61A   TIO-540-AJ1A   11205-61A   TIO-540-J2B    3692-61A

  TIO-540-AJ1A   11003-61A   TIO-540-AJ1A   11210-61A   TIO-540-J2B    4412-61A

  TIO-540-AJ1A   11005-61A   TIO-540-AJ1A   11215-61A   TIO-540-J2B    4421-61A

  TIO-540-AJ1A   11009-61A   TIO-540-AJ1A   11219-61A   TIO-540-J2B    4457-61A

  TIO-540-AJ1A   11010-61A   TIO-540-AJ1A   11221-61A   TIO-540-J2B    4612-61A

  TIO-540-AJ1A   11011-61A   TIO-540-AJ1A   11223-61A   TIO-540-J2B    4861-61A

  TIO-540-AJ1A   11014-61A   TIO-540-AJ1A   11224-61A   TIO-540-J2B    4907-61A

  TIO-540-AJ1A   11030-61A   TIO-540-AJ1A   11232-61A   TIO-540-J2B    5402-61A

  TIO-540-AJ1A   11034-61A   TIO-540-AJ1A   11233-61A   TIO-540-J2B    5544-61A

  TIO-540-AJ1A   11043-61A   TIO-540-AJ1A   11234-61A   TIO-540-J2B    5757-61A

  TIO-540-AJ1A   11044-61A   TIO-540-AJ1A   11235-61A   TIO-540-J2B    5842-61A

  TIO-540-AJ1A   11045-61A   TIO-540-AJ1A   11236-61A   TIO-540-J2B    5955-61A

  TIO-540-AJ1A   11046-61A   TIO-540-AJ1A   11237-61A   TIO-540-J2B    5976-61A

  TIO-540-AJ1A   11061-61A   TIO-540-AJ1A   11239-61A   TIO-540-J2B    5991-61A

  TIO-540-AJ1A   11069-61A   TIO-540-AJ1A   11248-61A   TIO-540-J2B    6088-61A

  TIO-540-AJ1A   11089-61A   TIO-540-AJ1A   11249-61A   TIO-540-J2B    6256-61A

  TIO-540-AJ1A   11092-61A   TIO-540-AJ1A   11252-61A   TIO-540-J2B    6743-61A

  TIO-540-AJ1A   11096-61A   TIO-540-AJ1A   11253-61A   TIO-540-J2B    6751-61A

  TIO-540-AJ1A   11113-61A   TIO-540-AJ1A   11256-61A   TIO-540-J2B    6837-61A

  TIO-540-AJ1A   11123-61A   TIO-540-AJ1A   11266-61A   TIO-540-J2B    7639-61A

  TIO-540-AJ1A   11127-61A   TIO-540-AJ1A   11267-61A   TIO-540-J2B    7948-61A

  TIO-540-AJ1A   11128-61A   TIO-540-AJ1A   11268-61A   TIO-540-J2B    8092-61A

  TIO-540-AJ1A   11150-61A   TIO-540-AJ1A   11279-61A   TIO-540-J2B    8192-61A

  TIO-540-AJ1A   11151-61A   TIO-540-AJ1A   11280-61A   TIO-540-J2B    8246-61A

  TIO-540-AJ1A   11153-61A   TIO-540-AJ1A   11285-61A   TIO-540-J2B    8353-61A

  TIO-540-AJ1A   11164-61A   TIO-540-AJ1A   11286-61A   TIO-540-J2B    8852-61A

  TIO-540-AJ1A   11166-61A   TIO-540-AJ1A   11290-61A   TIO-540-J2B    8883-61A

  TIO-540-AJ1A   11168-61A   TIO-540-AJ1A   11292-61A   TIO-540-J2B    9071-61A

  TIO-540-AJ1A   11169-61A   TIO-540-AJ1A   11296-61A   TIO-540-J2B    9300-61A

  TIO-540-AJ1A   11172-61A   TIO-540-AJ1A   11308-61A   TIO-540-J2B    9307-61A

  TIO-540-AJ1A   11175-61A   TIO-540-F2BD   7357-61A    TIO-540-J2B    9687-61A
  -------------- ----------- -------------- ----------- -------------- -----------

  -------------- ----------- -------------- ----------- -------------- -----------
  TIO-540-AJ1A   11176-61A   TIO-540-F2BD   7596-61A    TIO-540-J2B    9847-61A

  TIO-540-AJ1A   11177-61A   TIO-540-F2BD   8368-61A    TIO-540-J2B    9851-61A

  TIO-540-AJ1A   11178-61A   TIO-540-F2BD   9810-61A    TIO-540-J2B    9941-61A

  TIO-540-AJ1A   11181-61A   TIO-540-F2BD   9839-61A    TIO-540-J2B    10100-61A

  TIO-540-J2B    10214-61A   TIO-540-J2BD   4455-61A    TIO-540-J2BD   9993-61A

  TIO-540-J2B    10301-61A   TIO-540-J2BD   4710-61A    TIO-540-J2BD   10175-61A

  TIO-540-J2B    10366-61A   TIO-540-J2BD   4863-61A    TIO-540-J2BD   10219-61A

  TIO-540-J2B    10431-61A   TIO-540-J2BD   4945-61A    TIO-540-J2BD   10695-61A

  TIO-540-J2B    10443-61A   TIO-540-J2BD   5391-61A    TIO-540-J2BD   10741-61A

  TIO-540-J2B    10515-61A   TIO-540-J2BD   5405-61A    TIO-540-J2BD   10828-61A

  TIO-540-J2B    10528-61A   TIO-540-J2BD   5720-61A    TIO-540-J2BD   10830-61A

  TIO-540-J2B    10571-61A   TIO-540-J2BD   5750-61A    TIO-540-J2BD   11077-61A

  TIO-540-J2B    10576-61A   TIO-540-J2BD   6020-61A    TIO-540-J2BD   11146-61A

  TIO-540-J2B    10577-61A   TIO-540-J2BD   6045-61A    TIO-540-J2BD   11148-61A

  TIO-540-J2B    10637-61A   TIO-540-J2BD   6089-61A    TIO-540-J2BD   11149-61A

  TIO-540-J2B    10638-61A   TIO-540-J2BD   6422-61A    TIO-540-J2BD   11192-61A

  TIO-540-J2B    10655-61A   TIO-540-J2BD   6441-61A    TIO-540-J2BD   11227-61A

  TIO-540-J2B    10743-61A   TIO-540-J2BD   6561-61A    TIO-540-J2BD   11255-61A

  TIO-540-J2B    10810-61A   TIO-540-J2BD   6582-61A    TIO-540-S1AD   2574-61A

  TIO-540-J2B    10811-61A   TIO-540-J2BD   6646-61A    TIO-540-S1AD   3744-61A

  TIO-540-J2B    10862-61A   TIO-540-J2BD   7085-61A    TIO-540-S1AD   7554-61A

  TIO-540-J2B    10863-61A   TIO-540-J2BD   7108-61A    TIO-540-S1AD   8149-61A

  TIO-540-J2B    11032-61A   TIO-540-J2BD   7501-61A    TIO-540-S1AD   8331-61A

  TIO-540-J2B    11033-61A   TIO-540-J2BD   7502-61A    TIO-540-S1AD   8781-61A

  TIO-540-J2B    11037-61A   TIO-540-J2BD   7562-61A    TIO-540-S1AD   9815-61A

  TIO-540-J2B    11070-61A   TIO-540-J2BD   7678-61A    TIO-540-S1AD   9982-61A

  TIO-540-J2B    11101-61A   TIO-540-J2BD   7790-61A    TIO-540-S1AD   10078-61A

  TIO-540-J2B    11135-61A   TIO-540-J2BD   7892-61A    TIO-540-S1AD   10089-61A

  TIO-540-J2B    11136-61A   TIO-540-J2BD   7975-61A    TIO-540-S1AD   10969-61A

  TIO-540-J2B    11187-61A   TIO-540-J2BD   8239-61A    TIO-540-S1AD   11055-61A

  TIO-540-J2B    11289-61A   TIO-540-J2BD   8405-61A    TIO-540-U2A    1103-61A

  TIO-540-J2BD   842-61A     TIO-540-J2BD   8409-61A    TIO-540-U2A    2505-61A

  TIO-540-J2BD   1679-61A    TIO-540-J2BD   8439-61A    TIO-540-U2A    3184-61A

  TIO-540-J2BD   2171-61A    TIO-540-J2BD   8615-61A    TIO-540-U2A    4641-61A

  TIO-540-J2BD   2340-61A    TIO-540-J2BD   8617-61A    TIO-540-U2A    4658-61A

  TIO-540-J2BD   2372-61A    TIO-540-J2BD   8780-61A    TIO-540-U2A    7269-61A

  TIO-540-J2BD   2543-61A    TIO-540-J2BD   8871-61A    TIO-540-U2A    8530-61A

  TIO-540-J2BD   3176-61A    TIO-540-J2BD   8963-61A    TIO-540-U2A    8566-61A
  -------------- ----------- -------------- ----------- -------------- -----------

  -------------- ---------- -------------- ----------- -------------- -----------
  TIO-540-J2BD   3193-61A   TIO-540-J2BD   9025-61A    TIO-540-U2A    9064-61A

  TIO-540-J2BD   3259-61A   TIO-540-J2BD   9026-61A    TIO-540-U2A    9517-61A

  TIO-540-J2BD   3370-61A   TIO-540-J2BD   9137-61A    TIO-540-U2A    9794-61A

  TIO-540-J2BD   3532-61A   TIO-540-J2BD   9164-61A    TIO-540-U2A    10136-61A

  TIO-540-J2BD   3818-61A   TIO-540-J2BD   9343-61A    TIO-540-U2A    10241-61A

  TIO-540-J2BD   3918-61A   TIO-540-J2BD   9355-61A    TIO-540-U2A    10553-61A

  TIO-540-J2BD   4138-61A   TIO-540-J2BD   9463-61A    TIO-540-U2A    10585-61A

  TIO-540-J2BD   4213-61A   TIO-540-J2BD   9573-61A    TIO-540-U2A    11073-61A

  TIO-540-J2BD   4217-61A   TIO-540-J2BD   9662-61A    TIO-540-U2A    11074-61A

  TIO-540-J2BD   4240-61A   TIO-540-J2BD   9793-61A    TIO-540-V2AD   8560-61A

  TIO-540-J2BD   4241-61A   TIO-540-J2BD   9846-61A                   

  TIO-540-J2BD   4248-61A   TIO-540-J2BD   9965-61A                   

  TIO-540-J2BD   4371-61A   TIO-540-J2BD   9980-61A                   
  -------------- ---------- -------------- ----------- -------------- -----------

**Table 2 List of Crankshaft SN's**

  -------------- ------------ ------------ ------------ ------------ ------------ --
  **CRANKSHAFT                                                                    
  SN's**                                                                          

  V537912175     V537912648   V537912901   V537912959   V537913227   V537913281   

  V537912176     V537912649   V537912902   V537912961   V537913228   V537913282   

  V537912185     V537912650   V537912903   V537912962   V537913229   V537913284   

  V537912190     V537912657   V537912904   V537912965   V537913230   V537913285   

  V537912195     V537912663   V537912906   V537912966   V537913231   V537913286   

  V537912199     V537912859   V537912907   V537912967   V537913232   V537913288   

  V537912201     V537912861   V537912908   V537912968   V537913233   V537913289   

  V537912202     V537912862   V537912909   V537912971   V537913234   V537913292   

  V537912203     V537912863   V537912910   V537912973   V537913235   V537913293   

  V537912204     V537912865   V537912911   V537912974   V537913236   V537913294   

  V537912207     V537912866   V537912912   V537912975   V537913237   V537913295   

  V537912209     V537912867   V537912914   V537912976   V537913238   V537913297   

  V537912210     V537912868   V537912915   V537912977   V537913239   V537913502   

  V537912212     V537912869   V537912916   V537912978   V537913240   V537913503   

  V537912213     V537912870   V537912917   V537912979   V537913241   V537913504   

  V537912225     V537912871   V537912918   V537912980   V537913242   V537913506   

  V537912226     V537912872   V537912919   V537912981   V537913243   V537913507   

  V537912607     V537912873   V537912920   V537913197   V537913244   V537913508   

  V537912608     V537912875   V537912921   V537913198   V537913245   V537913509   

  V537912610     V537912876   V537912924   V537913199   V537913246   V537913512   

  V537912611     V537912877   V537912925   V537913201   V537913249   V537913514   

  V537912612     V537912878   V537912928   V537913202   V537913251   V537913516   

  V537912613     V537912879   V537912930   V537913203   V537913252   V537913517   
  -------------- ------------ ------------ ------------ ------------ ------------ --

  ------------ ------------ ------------ ------------ ------------ ------------
  V537912615   V537912880   V537912932   V537913204   V537913253   V537913520

  V537912616   V537912882   V537912938   V537913205   V537913255   V537913521

  V537912617   V537912883   V537912944   V537913208   V537913256   V537913523

  V537912619   V537912884   V537912945   V537913209   V537913257   V537913525

  V537912622   V537912885   V537912946   V537913210   V537913258   V537913526

  V537912623   V537912886   V537912947   V537913212   V537913259   V537913527

  V537912624   V537912887   V537912948   V537913213   V537913260   V537913528

  V537912625   V537912889   V537912949   V537913214   V537913262   V537913529

  V537912626   V537912890   V537912950   V537913215   V537913265   V537913530

  V537912627   V537912892   V537912951   V537913218   V537913267   V537913532

  V537912628   V537912893   V537912952   V537913219   V537913268   V537913533

  V537912635   V537912894   V537912953   V537913220   V537913271   V537913534

  V537912642   V537912896   V537912954   V537913221   V537913273   V537913535

  V537912643   V537912897   V537912955   V537913222   V537913274   V537913536

  V537912644   V537912898   V537912956   V537913223   V537913275   V537913537

  V537912645   V537912899   V537912957   V537913224   V537913276   V537913538

  V537912647   V537912900   V537912958   V537913226   V537913279   V537913541

  V537913542   V537914183   V537914312   V537915046   V537915480   V537916019

  V537913543   V537914214   V537914313   V537915049   V537915481   V537916112

  V537913544   V537914257   V537914314   V537915050   V537915485   V537916114

  V537913546   V537914258   V537914317   V537915051   V537915486   V537916115

  V537913548   V537914259   V537914318   V537915052   V537915487   V537916116

  V537913549   V537914260   V537914319   V537915053   V537915488   V537916117

  V537913550   V537914261   V537914322   V537915055   V537915490   V537916119

  V537913551   V537914262   V537914324   V537915056   V537915491   V537916120

  V537913552   V537914265   V537914326   V537915298   V537915492   V537916122

  V537913555   V537914266   V537914329   V537915299   V537915493   V537916123

  V537913556   V537914268   V537914330   V537915300   V537915495   V537916124

  V537913557   V537914271   V537914500   V537915301   V537915497   V537916126

  V537913559   V537914272   V537915012   V537915302   V537915498   V537916127

  V537913560   V537914273   V537915013   V537915304   V537915499   V537916128

  V537913561   V537914274   V537915014   V537915305   V537915500   V537916129

  V537913578   V537914275   V537915015   V537915306   V537915501   V537916130

  V537913676   V537914276   V537915016   V537915307   V537915699   V537916132

  V537913680   V537914277   V537915017   V537915308   V537915991   V537916134

  V537913683   V537914278   V537915018   V537915309   V537915992   V537916135

  V537913684   V537914282   V537915019   V537915311   V537915994   V537916137

  V537913687   V537914283   V537915020   V537915313   V537915995   V537916138

  V537913688   V537914286   V537915022   V537915314   V537915996   V537916139
  ------------ ------------ ------------ ------------ ------------ ------------

  ------------ ------------ ------------ ------------ ------------ ------------
  V537913691   V537914287   V537915023   V537915315   V537915997   V537916141

  V537913694   V537914288   V537915024   V537915316   V537915998   V537916142

  V537913697   V537914289   V537915026   V537915317   V537915999   V537916143

  V537913699   V537914290   V537915027   V537915318   V537916000   V537916144

  V537913700   V537914291   V537915028   V537915319   V537916001   V537916145

  V537913701   V537914292   V537915029   V537915320   V537916003   V537916146

  V537913702   V537914293   V537915030   V537915321   V537916004   V537916147

  V537913703   V537914294   V537915032   V537915322   V537916005   V537916148

  V537913704   V537914296   V537915033   V537915323   V537916006   V537916149

  V537913707   V537914297   V537915034   V537915324   V537916007   V537916151

  V537913709   V537914299   V537915035   V537915325   V537916008   V537916408

  V537913710   V537914300   V537915036   V537915326   V537916009   V537916409

  V537913711   V537914301   V537915038   V537915327   V537916010   V537916410

  V537913712   V537914304   V537915039   V537915473   V537916011   V537916411

  V537913714   V537914305   V537915040   V537915474   V537916012   V537916412

  V537913866   V537914306   V537915041   V537915475   V537916013   V537916413

  V537913995   V537914307   V537915042   V537915476   V537916015   V537916414

  V537913998   V537914308   V537915043   V537915477   V537916016   V537916415

  V537913999   V537914310   V537915044   V537915478   V537916017   V537916416

  V537914141   V537914311   V537915045   V537915479   V537916018   V537916417

  V537916418   V537916715   V537916974   V537917208   V537917258   V537917571

  V537916419   V537916717   V537916975   V537917209   V537917259   V537917698

  V537916420   V537916718   V537916976   V537917212   V537917260   V537917699

  V537916421   V537916719   V537916977   V537917214   V537917527   V537917745

  V537916422   V537916720   V537916978   V537917215   V537917528   V537917926

  V537916423   V537916721   V537916979   V537917217   V537917529   V537917927

  V537916424   V537916724   V537916980   V537917218   V537917530   V537917928

  V537916425   V537916725   V537916981   V537917219   V537917532   V537917929

  V537916426   V537916726   V537916982   V537917221   V537917533   V537917930

  V537916427   V537916727   V537916983   V537917222   V537917534   V537917931

  V537916428   V537916728   V537916985   V537917223   V537917535   V537917932

  V537916430   V537916729   V537916986   V537917224   V537917536   V537917933

  V537916431   V537916730   V537917029   V537917225   V537917537   V537917934

  V537916432   V537916732   V537917031   V537917226   V537917538   V537917935

  V537916433   V537916734   V537917032   V537917227   V537917539   V537917936

  V537916434   V537916735   V537917033   V537917228   V537917541   V537917937

  V537916435   V537916736   V537917034   V537917229   V537917542   V537917938

  V537916436   V537916737   V537917037   V537917230   V537917543   V537917939

  V537916437   V537916739   V537917039   V537917231   V537917545   V537917940
  ------------ ------------ ------------ ------------ ------------ ------------

  ------------ ------------ ------------ ------------ ------------ ------------
  V537916439   V537916740   V537917042   V537917232   V537917546   V537917941

  V537916531   V537916741   V537917043   V537917233   V537917547   V537917942

  V537916532   V537916742   V537917044   V537917234   V537917548   V537917944

  V537916533   V537916743   V537917045   V537917235   V537917550   V537917946

  V537916534   V537916745   V537917047   V537917236   V537917551   V537917947

  V537916535   V537916746   V537917049   V537917238   V537917552   V537917948

  V537916536   V537916747   V537917050   V537917239   V537917554   V537917949

  V537916537   V537916748   V537917051   V537917240   V537917555   V537917950

  V537916538   V537916749   V537917052   V537917241   V537917556   V537917952

  V537916539   V537916750   V537917123   V537917242   V537917557   V537917953

  V537916541   V537916957   V537917195   V537917243   V537917558   V537917954

  V537916543   V537916959   V537917196   V537917244   V537917559   V537917955

  V537916544   V537916960   V537917197   V537917245   V537917560   V537917956

  V537916614   V537916961   V537917198   V537917246   V537917561   V537917957

  V537916706   V537916962   V537917199   V537917247   V537917562   V537917958

  V537916707   V537916963   V537917200   V537917248   V537917563   V537917959

  V537916708   V537916967   V537917201   V537917251   V537917564   V537917960

  V537916709   V537916968   V537917202   V537917252   V537917565   V537917966

  V537916710   V537916969   V537917203   V537917253   V537917566   V537917967

  V537916711   V537916970   V537917204   V537917254   V537917567   V537917968

  V537916712   V537916971   V537917205   V537917255   V537917568   V537917969

  V537916713   V537916972   V537917206   V537917256   V537917569   V537917972

  V537916714   V537916973   V537917207   V537917257   V537917570   V537917973

  V537917974   V537918289   V537918495   V537918969   V537919297   V537919508

  V537917975   V537918290   V537918496   V537918970   V537919298   V537919509

  V537917976   V537918292   V537918497   V537919026   V537919299   V537919510

  V537917977   V537918293   V537918498   V537919027   V537919300   V537919511

  V537917978   V537918294   V537918499   V537919028   V537919301   V537919512

  V537917979   V537918295   V537918920   V537919029   V537919302   V537919513

  V537917980   V537918296   V537918922   V537919030   V537919303   V537919514

  V537917981   V537918297   V537918923   V537919031   V537919450   V537919515

  V537917982   V537918298   V537918925   V537919032   V537919460   V537919516

  V537917983   V537918299   V537918926   V537919033   V537919471   V537919518

  V537917984   V537918300   V537918927   V537919034   V537919472   V537919519

  V537918257   V537918301   V537918928   V537919035   V537919473   V537919520

  V537918258   V537918393   V537918929   V537919036   V537919474   V537919521

  V537918259   V537918461   V537918930   V537919037   V537919475   V537919522

  V537918260   V537918462   V537918931   V537919038   V537919476   V537919523

  V537918261   V537918463   V537918933   V537919039   V537919477   V537919524
  ------------ ------------ ------------ ------------ ------------ ------------

  ------------ ------------ ------------ ------------ ------------ ------------
  V537918262   V537918464   V537918934   V537919040   V537919478   V537919525

  V537918263   V537918465   V537918935   V537919042   V537919480   V537919526

  V537918264   V537918467   V537918936   V537919043   V537919482   V537919527

  V537918265   V537918468   V537918937   V537919044   V537919483   V537919528

  V537918266   V537918469   V537918938   V537919045   V537919484   V537919529

  V537918267   V537918470   V537918940   V537919091   V537919485   V537919803

  V537918268   V537918471   V537918941   V537919096   V537919486   V537919804

  V537918269   V537918472   V537918942   V537919147   V537919487   V537919805

  V537918270   V537918473   V537918946   V537919277   V537919488   V537919806

  V537918272   V537918474   V537918948   V537919278   V537919489   V537919807

  V537918273   V537918475   V537918950   V537919279   V537919490   V537919808

  V537918274   V537918476   V537918951   V537919281   V537919491   V537919809

  V537918275   V537918477   V537918952   V537919282   V537919492   V537919810

  V537918276   V537918478   V537918953   V537919283   V537919493   V537919811

  V537918277   V537918479   V537918954   V537919284   V537919494   V537919813

  V537918278   V537918480   V537918956   V537919285   V537919495   V537919818

  V537918279   V537918481   V537918958   V537919286   V537919496   V537919819

  V537918280   V537918482   V537918959   V537919287   V537919497   V537919820

  V537918281   V537918483   V537918960   V537919288   V537919498   V537919821

  V537918282   V537918486   V537918961   V537919289   V537919499   V537919822

  V537918283   V537918487   V537918962   V537919290   V537919500   V537919823

  V537918284   V537918488   V537918963   V537919291   V537919501   V537919824

  V537918285   V537918489   V537918964   V537919293   V537919503   V537919825

  V537918286   V537918491   V537918966   V537919294   V537919505   V537919826

  V537918287   V537918492   V537918967   V537919295   V537919506   V537919828

  V537918288   V537918493   V537918968   V537919296   V537919507   V537919830

  V537919831   V537920371   V537920937   V537920983   V537921420   V537921586

  V537919832   V537920372   V537920938   V537920984   V537921421   V537921587

  V537919833   V537920373   V537920939   V537920986   V537921422   V537921588

  V537919834   V537920374   V537920940   V537920987   V537921423   V537921589

  V537919835   V537920375   V537920941   V537920988   V537921424   V537921590

  V537919836   V537920376   V537920942   V537920989   V537921425   V537921591

  V537919837   V537920377   V537920943   V537921296   V537921426   V537921592

  V537919838   V537920378   V537920944   V537921297   V537921427   V537921593

  V537919839   V537920379   V537920945   V537921299   V537921428   V537921594

  V537919840   V537920382   V537920946   V537921300   V537921429   V537921595

  V537919841   V537920383   V537920947   V537921302   V537921430   V537921596

  V537919843   V537920384   V537920948   V537921303   V537921431   V537921597

  V537919850   V537920385   V537920949   V537921304   V537921432   V537921598
  ------------ ------------ ------------ ------------ ------------ ------------

  ------------ ------------ ------------ ------------ ------------ ------------
  V537919853   V537920387   V537920950   V537921306   V537921433   V537921599

  V537919855   V537920388   V537920951   V537921308   V537921434   V537921600

  V537919856   V537920390   V537920952   V537921309   V537921435   V537921601

  V537919858   V537920392   V537920953   V537921310   V537921437   V537921764

  V537920345   V537920393   V537920954   V537921311   V537921438   V537921765

  V537920346   V537920394   V537920956   V537921312   V537921439   V537921766

  V537920347   V537920909   V537920957   V537921313   V537921561   V537921767

  V537920348   V537920910   V537920958   V537921314   V537921562   V537921768

  V537920349   V537920911   V537920959   V537921315   V537921563   V537921769

  V537920350   V537920913   V537920960   V537921316   V537921565   V537921770

  V537920351   V537920915   V537920962   V537921317   V537921566   V537921771

  V537920352   V537920916   V537920963   V537921398   V537921567   V537921773

  V537920353   V537920918   V537920964   V537921399   V537921568   V537921775

  V537920354   V537920919   V537920966   V537921400   V537921569   V537921776

  V537920355   V537920920   V537920967   V537921401   V537921570   V537921777

  V537920356   V537920921   V537920968   V537921402   V537921571   V537921778

  V537920357   V537920922   V537920969   V537921403   V537921572   V537921779

  V537920358   V537920923   V537920970   V537921404   V537921573   V537921780

  V537920359   V537920925   V537920971   V537921406   V537921574   V537921781

  V537920360   V537920926   V537920973   V537921407   V537921575   V537921782

  V537920361   V537920927   V537920974   V537921408   V537921576   V537921783

  V537920362   V537920928   V537920975   V537921409   V537921577   V537921784

  V537920363   V537920929   V537920976   V537921410   V537921578   V537921786

  V537920364   V537920930   V537920977   V537921412   V537921579   V537921787

  V537920365   V537920931   V537920978   V537921413   V537921580   V537921789

  V537920367   V537920932   V537920979   V537921414   V537921582   V537921790

  V537920368   V537920933   V537920980   V537921417   V537921583   V537921791

  V537920369   V537920934   V537920981   V537921418   V537921584   V537921792

  V537920370   V537920935   V537920982   V537921419   V537921585   V537921793

  V537921794   V537922089   V537922576   V537922621   V537923013   V537924078

  V537921795   V537922090   V537922577   V537922622   V537923014   V537924079

  V537921796   V537922092   V537922578   V537922623   V537923015   V537924080

  V537921797   V537922093   V537922579   V537922624   V537923016   V537924081

  V537921798   V537922094   V537922580   V537922625   V537923017   V537924082

  V537921799   V537922095   V537922581   V537922626   V537923018   V537924083

  V537921800   V537922096   V537922582   V537922627   V537923019   V537924084

  V537921801   V537922097   V537922583   V537922628   V537923020   V537924086

  V537921802   V537922098   V537922584   V537922629   V537923021   V537924089

  V537922053   V537922099   V537922585   V537922630   V537923022   V537924090
  ------------ ------------ ------------ ------------ ------------ ------------

  ------------ ------------ ------------ ------------ ------------ ------------
  V537922054   V537922100   V537922587   V537922631   V537923023   V537924091

  V537922055   V537922101   V537922588   V537922632   V537923025   V537924092

  V537922056   V537922102   V537922589   V537922979   V537923026   V537924093

  V537922057   V537922103   V537922590   V537922980   V537923027   V537924094

  V537922058   V537922104   V537922591   V537922983   V537923028   V537924095

  V537922060   V537922105   V537922592   V537922984   V537923029   V537924096

  V537922061   V537922548   V537922593   V537922985   V537923859   V537924098

  V537922062   V537922549   V537922594   V537922986   V537923861   V537924099

  V537922064   V537922550   V537922595   V537922987   V537923862   V537924100

  V537922065   V537922551   V537922596   V537922988   V537923863   V537924101

  V537922066   V537922552   V537922597   V537922989   V537923864   V537924102

  V537922067   V537922554   V537922598   V537922990   V537923865   V537924103

  V537922068   V537922555   V537922599   V537922991   V537923866   V537924387

  V537922069   V537922556   V537922600   V537922992   V537923867   V537924388

  V537922070   V537922557   V537922601   V537922993   V537923868   V537924389

  V537922071   V537922558   V537922602   V537922994   V537923869   V537924390

  V537922072   V537922559   V537922603   V537922995   V537923870   V537924391

  V537922074   V537922560   V537922604   V537922996   V537923871   V537924392

  V537922075   V537922561   V537922605   V537922997   V537923872   V537924393

  V537922076   V537922563   V537922606   V537922998   V537923873   V537924394

  V537922077   V537922564   V537922607   V537922999   V537923874   V537924395

  V537922078   V537922565   V537922609   V537923000   V537923875   V537924396

  V537922079   V537922566   V537922610   V537923002   V537923876   V537924397

  V537922080   V537922567   V537922611   V537923003   V537923878   V537924398

  V537922081   V537922568   V537922612   V537923004   V537923880   V537924400

  V537922082   V537922569   V537922613   V537923005   V537923882   V537924401

  V537922083   V537922570   V537922614   V537923006   V537923883   V537924402

  V537922084   V537922571   V537922615   V537923007   V537923885   V537924403

  V537922085   V537922572   V537922616   V537923008   V537923887   V537924406

  V537922086   V537922573   V537922618   V537923009   V537923888   V537924407

  V537922087   V537922574   V537922619   V537923010   V537924075   V537924408

  V537922088   V537922575   V537922620   V537923012   V537924076   V537924409

  V537924410   V537924585   V537924736   V537924872   V537924917   V537925015

  V537924411   V537924586   V537924738   V537924873   V537924918   V537925016

  V537924412   V537924693   V537924739   V537924874   V537924919   V537925017

  V537924413   V537924694   V537924740   V537924875   V537924920   V537925018

  V537924414   V537924695   V537924742   V537924876   V537924921   V537925020

  V537924415   V537924696   V537924833   V537924877   V537924922   V537925021

  V537924417   V537924697   V537924834   V537924878   V537924923   V537925023
  ------------ ------------ ------------ ------------ ------------ ------------

  ------------ ------------ ------------ ------------ ------------ ------------
  V537924418   V537924698   V537924835   V537924879   V537924924   V537925024

  V537924419   V537924699   V537924836   V537924880   V537924925   V537925025

  V537924420   V537924700   V537924837   V537924881   V537924926   V537925026

  V537924421   V537924701   V537924838   V537924882   V537924927   V537925027

  V537924422   V537924702   V537924839   V537924884   V537924928   V537925028

  V537924423   V537924703   V537924840   V537924885   V537924930   V537925029

  V537924424   V537924704   V537924841   V537924886   V537924931   V537925030

  V537924425   V537924705   V537924842   V537924887   V537924932   V537925031

  V537924426   V537924706   V537924843   V537924888   V537924933   V537925032

  V537924427   V537924707   V537924844   V537924889   V537924934   V537925033

  V537924428   V537924708   V537924845   V537924890   V537924935   V537925034

  V537924429   V537924709   V537924846   V537924891   V537924937   V537925035

  V537924430   V537924710   V537924847   V537924892   V537924938   V537925036

  V537924431   V537924711   V537924848   V537924893   V537924939   V537925037

  V537924432   V537924712   V537924849   V537924894   V537924941   V537925038

  V537924433   V537924713   V537924850   V537924895   V537924942   V537925039

  V537924434   V537924714   V537924851   V537924896   V537924943   V537925040

  V537924435   V537924715   V537924852   V537924897   V537924944   V537925041

  V537924436   V537924716   V537924853   V537924899   V537924945   V537925042

  V537924567   V537924717   V537924854   V537924900   V537924947   V537925044

  V537924568   V537924718   V537924855   V537924901   V537924948   V537925045

  V537924569   V537924719   V537924856   V537924902   V537925001   V537925047

  V537924570   V537924720   V537924857   V537924903   V537925002   V537925048

  V537924571   V537924721   V537924859   V537924904   V537925003   V537925049

  V537924572   V537924722   V537924860   V537924905   V537925004   V537925050

  V537924573   V537924723   V537924861   V537924906   V537925005   V537925051

  V537924574   V537924724   V537924862   V537924908   V537925006   V537925052

  V537924576   V537924725   V537924863   V537924909   V537925007   V537925054

  V537924577   V537924726   V537924864   V537924910   V537925008   V537925055

  V537924578   V537924727   V537924865   V537924911   V537925009   V537925056

  V537924580   V537924729   V537924866   V537924912   V537925010   V537925057

  V537924581   V537924731   V537924868   V537924913   V537925011   V537925058

  V537924582   V537924732   V537924869   V537924914   V537925012   V537925059

  V537924583   V537924733   V537924870   V537924915   V537925013   V537925060

  V537924584   V537924734   V537924871   V537924916   V537925014   V537925061

  V537925062   V537925096   V537925129   V537925164   V537925272   V537925305

  V537925063   V537925097   V537925130   V537925165   V537925273   V537925306

  V537925064   V537925098   V537925131   V537925166   V537925274   V537925307

  V537925065   V537925099   V537925132   V537925167   V537925275   V537925308
  ------------ ------------ ------------ ------------ ------------ ------------

  ------------ ------------ ------------ ------------ ------------ ------------
  V537925066   V537925100   V537925133   V537925168   V537925276   V537925309

  V537925067   V537925101   V537925134   V537925169   V537925277   V537925310

  V537925068   V537925102   V537925135   V537925170   V537925278   V537925311

  V537925069   V537925103   V537925138   V537925244   V537925279   V537925312

  V537925070   V537925104   V537925139   V537925245   V537925280   V537925313

  V537925071   V537925105   V537925140   V537925246   V537925281   V537925314

  V537925072   V537925106   V537925141   V537925247   V537925282   V537925315

  V537925073   V537925107   V537925142   V537925248   V537925283   V537925316

  V537925074   V537925108   V537925143   V537925249   V537925284   V537925317

  V537925076   V537925109   V537925144   V537925250   V537925285   V537925318

  V537925078   V537925110   V537925145   V537925251   V537925286   V537925319

  V537925079   V537925111   V537925146   V537925252   V537925287   V537925320

  V537925080   V537925112   V537925147   V537925253   V537925288   V537925321

  V537925081   V537925113   V537925148   V537925254   V537925289   V537925322

  V537925082   V537925114   V537925149   V537925255   V537925290   V537925576

  V537925083   V537925115   V537925150   V537925256   V537925291   V537925578

  V537925084   V537925116   V537925151   V537925257   V537925293   V537925579

  V537925085   V537925117   V537925152   V537925258   V537925294   V537925580

  V537925086   V537925118   V537925153   V537925259   V537925295   V537925582

  V537925087   V537925119   V537925155   V537925260   V537925296   V537925583

  V537925088   V537925120   V537925156   V537925262   V537925297   V537925584

  V537925089   V537925121   V537925157   V537925264   V537925298   V537925585

  V537925090   V537925122   V537925158   V537925265   V537925299   V537925586

  V537925091   V537925123   V537925159   V537925267   V537925300   V537925587

  V537925092   V537925125   V537925160   V537925268   V537925301   V537925722

  V537925093   V537925126   V537925161   V537925269   V537925302   

  V537925094   V537925127   V537925162   V537925270   V537925303   

  V537925095   V537925128   V537925163   V537925271   V537925304   
  ------------ ------------ ------------ ------------ ------------ ------------

\(b\) For engines that have had a crankshaft replaced after September
30, 1999, replace any crankshaft that has a SN listed in Table 2 of this
AD.

\(c\) After receipt of this AD, do not install any crankshaft removed in
accordance with paragraph (a) or (b) of this AD into any engine.

\(d\) After receipt of this AD, do not install any crankshaft that has a
SN listed in Table 2 of this AD on an LTIO-540 or TIO-540 model engine.

\(e\) An alternative method of compliance or adjustment of the
compliance time that provides an acceptable level of safety may be used
if approved by the Manager, New York Aircraft Certification Office
(NYACO). Operators must submit their requests through an appropriate FAA
Principal Maintenance Inspector, who may add comments and then send it
to the Manager, NYACO.

**Note 2**: Information concerning the existence of approved alternative
methods of compliance with this airworthiness directive, if any, may be
obtained from the NYACO.

\(f\) Special flight permits may be issued in accordance with sections
21.197 and 21.199 of the Federal Aviation Regulations (14 CFR 21.197 and
21.199) to operate the airplane to a location where the requirements of
this AD can be done.

\(g\) **Emergency AD 2002-17-53, issued August 16, 2002, supersedes
Emergency AD 2002-04-51 and becomes effective upon receipt.**

**FOR FURTHER INFORMATION CONTACT:** Norman Perenson, Aerospace
Engineer, New York Aircraft Certification Office, FAA, Engine and
Propeller Directorate, 10 Fifth Street, 3^rd^ floor, Valley Stream, NY
11581-1200; telephone (516) 256‑7537; fax (516) 568‑2716.

Issued in Burlington, Massachusetts on August 16, 2002.

Jay J. Pardee,

Manager, Engine and Propeller Directorate,

Aircraft Certification Service.