# Airworthiness directives, 2002

FAA airworthiness directives effective in 2002: 448 ADs with their full text, status and the aircraft they apply to.

Page 1 of 9 · 448 ADs

- [AD 2002-23-18](https://openairdocs.org/ad/2002-23-18.md): Rockwell Collins LRA-900 radio altimeters · Boeing MD-11 and MD-11F · Effective Dec 31, 2002 · Supersedes AD 98-24-51
- [AD 2002-23-17](https://openairdocs.org/ad/2002-23-17.md): Electrical Wiring Installations · Boeing MD-90-30 · Effective Dec 31, 2002
- [AD 2002-23-14](https://openairdocs.org/ad/2002-23-14.md): High Pressure Compressor (HPC) Front Hubs · Pratt & Whitney Division JT8D-209, JT8D-217, JT8D-217A and 2 more · Historical · Effective Dec 31, 2002 · Replaced by AD 2006-17-07
- [AD 2002-23-13](https://openairdocs.org/ad/2002-23-13.md): Turbine Exhaust Ducts · Pratt & Whitney Canada PT6A-11, PT6A-110, PT6A-112 and 20 more · Effective Dec 31, 2002
- [AD 2002-22-17](https://openairdocs.org/ad/2002-22-17.md): Inboard forward flap bellcranks · Cessna 208 and 208B · Historical · Effective Dec 31, 2002 · Replaced by AD 2004-17-01
- [AD 2002-23-09](https://openairdocs.org/ad/2002-23-09.md): Torx Head Blade Root Lag Screws · MT-Propeller Entwicklung MTV-3 and MTV-9-B · Effective Dec 30, 2002 · Supersedes AD 99-14-06
- [AD 2002-23-08](https://openairdocs.org/ad/2002-23-08.md): Low Pressure (LP) Turbine Stage 2 Discs · Rolls-Royce RB211-535E4-37, RB211-535E4-B-37 and RB211-535E4-B-75 · Historical · Effective Dec 30, 2002 · Replaced by AD 2003-17-15
- [AD 2002-13-09](https://openairdocs.org/ad/2002-13-09.md): Rotating engine parts · Pratt & Whitney Division JT8D-209, JT8D-217, JT8D-217A and 2 more · Historical · Effective Dec 30, 2002 · Replaced by AD 2005-18-02
- [AD 2002-23-05](https://openairdocs.org/ad/2002-23-05.md): Circuit Breakers for the Auxiliary Hydraulic Pump System and the King KHF 950 High Frequency Communication System(s) · Cessna 750 · Effective Dec 26, 2002
- [AD 2002-23-03](https://openairdocs.org/ad/2002-23-03.md): Longitudinal Drive Link and Nonrotating Swashplate Assemblies · MD Helicopters MD900 · Effective Dec 26, 2002
- [AD 2002-23-02](https://openairdocs.org/ad/2002-23-02.md): Airworthiness Limitations Section (ALS) - Critical Life-Limited Parts · General Electric CF34-8C1 · Effective Dec 26, 2002
- [AD 2002-22-51](https://openairdocs.org/ad/2002-22-51.md): Main rotor support static mast (mast) · MD Helicopters MD900 · Emergency AD · Effective Dec 26, 2002
- [AD 2002-22-13](https://openairdocs.org/ad/2002-22-13.md): Flight management computers (FMC) · Bombardier CL-600-2B16 (CL-604), CL-600-2B19 (Regional Jet Series 100), 400A and 2 more · Effective Dec 20, 2002
- [AD 2002-22-04](https://openairdocs.org/ad/2002-22-04.md): Engine compartment fuel · Stemme Stemme S10-VT · Effective Dec 20, 2002
- [AD 2002-22-03](https://openairdocs.org/ad/2002-22-03.md): Main Landing Gear Front Attachment Brackets · Pilatus PC-7 · Effective Dec 20, 2002
- [AD 2002-22-02](https://openairdocs.org/ad/2002-22-02.md): Engine Mount Bracket · B-N Group BN-2, BN-2A, BN-2A-2 and 17 more · Effective Dec 20, 2002
- [AD 2002-24-06](https://openairdocs.org/ad/2002-24-06.md): Low pressure (LP) fuel tubes · Rolls-Royce Deutschland TAY 620-15 and TAY 650-15 · Historical · Effective Dec 18, 2002 · Replaced by AD 2003-05-04
- [AD 2002-24-05](https://openairdocs.org/ad/2002-24-05.md): Upper chord · Boeing 727 Series (all) · Historical · Effective Dec 18, 2002 · Replaced by AD 2005-05-19
- [AD 2002-20-08](https://openairdocs.org/ad/2002-20-08.md): Fuel quantity indication system · British Aerospace Regional Jetstream 3201 · Effective Dec 18, 2002 · Supersedes AD 2000-09-13
- [AD 2002-23-10](https://openairdocs.org/ad/2002-23-10.md): First Outboard Flap Control Rod and the Bleed Air Duct · Piaggio Aero Industries P-180 · Effective Dec 17, 2002
- [AD 2002-22-16](https://openairdocs.org/ad/2002-22-16.md): Exhaust pip ejector · Airbus Helicopters AS355N · Effective Dec 17, 2002 · Supersedes AD 2000-05-15
- [AD 2002-22-15](https://openairdocs.org/ad/2002-22-15.md): Locking pins · Airbus Helicopters EC 155B · Effective Dec 17, 2002
- [AD 2002-21-11](https://openairdocs.org/ad/2002-21-11.md): Horizontal stabilizer · Extra Flugzeugproduktions- und Vertriebs- EA-300S · Historical · Effective Dec 17, 2002 · Replaced by AD 2007-02-11
- [AD 2002-22-14](https://openairdocs.org/ad/2002-22-14.md): Main rotor tension-torsion (TT) straps · Bell Helicopter Textron 204B, 205A, 205A-1 and 4 more · Effective Dec 13, 2002 · Supersedes AD 80-17-09
- [AD 2002-22-12](https://openairdocs.org/ad/2002-22-12.md): Titeflex hoses · BAE Systems ATP, Avro 146-RJ100A, Avro 146-RJ70A and 122 more · Effective Dec 13, 2002
- [AD 2002-22-11](https://openairdocs.org/ad/2002-22-11.md): Injection wheel · Turbomeca Artouste IIIB, Artouste IIIB1 and Artouste IIID · Historical · Effective Dec 13, 2002 · Replaced by AD 2005-26-13
- [AD 2002-22-01](https://openairdocs.org/ad/2002-22-01.md): Engine secondary vent line · Zlin Aircraft a.s. Z-143L and Z-242L · Effective Dec 13, 2002
- [AD 2002-23-16](https://openairdocs.org/ad/2002-23-16.md): Chart holder assembly · Boeing MD-90-30 · Effective Dec 11, 2002
- [AD 2002-23-15](https://openairdocs.org/ad/2002-23-15.md): Lower lobe panel · Boeing 747-100 Series, 747-200B Series, 747-200C Series and 5 more · Effective Dec 11, 2002
- [AD 94-20-04 R1](https://openairdocs.org/ad/94-20-04-R1.md): V-tail · Remove V tail and install a Beech Model F33A straight tail (D'Shannon Products STC SA2149CE) · Historical · Effective Dec 10, 2002 · Replaced by AD 94-20-04 R2
- [AD 2002-21-13](https://openairdocs.org/ad/2002-21-13.md): V-tail · Textron 35, 35R, A35 and 1 more · Effective Dec 10, 2002 · Supersedes AD 98-13-02
- [AD 2002-21-08](https://openairdocs.org/ad/2002-21-08.md): Aileron assembly · Pilatus PC-6 · Historical · Effective Dec 6, 2002 · Replaced by AD 2006-13-11
- [AD 2002-23-01](https://openairdocs.org/ad/2002-23-01.md): Forward engine cross spar assembly · Gulfstream Aerospace LP Galaxy and Gulfstream 200 · Effective Nov 29, 2002
- [AD 2002-21-17](https://openairdocs.org/ad/2002-21-17.md): Fan duct and fan exit guide vane · Pratt & Whitney Division JT8D-209, JT8D-217, JT8D-217A and 2 more · Effective Nov 29, 2002
- [AD 2002-21-14](https://openairdocs.org/ad/2002-21-14.md): Escape slide · Boeing 757-200 Series, 757-200CB Series and 757-300 Series · Effective Nov 29, 2002
- [AD 2002-21-09](https://openairdocs.org/ad/2002-21-09.md): Cockpit enclosure window sill · Boeing DC-9-11, DC-9-12, DC-9-13 and 15 more · Effective Nov 29, 2002
- [AD 2002-21-01](https://openairdocs.org/ad/2002-21-01.md): Electrical terminal contact pins · Airbus A319-111, A319-112, A319-113 and 66 more · Effective Nov 27, 2002 · Supersedes AD 2001-10-13
- [AD 2002-21-15](https://openairdocs.org/ad/2002-21-15.md): Second stage turbine stator inner seal support · Honeywell International TPE331-1, TPE331-2, TPE331-2UA and 9 more · Effective Nov 26, 2002
- [AD 2002-21-12](https://openairdocs.org/ad/2002-21-12.md): Main transmission assembly · Agusta A109E · Effective Nov 26, 2002
- [AD 2002-21-07](https://openairdocs.org/ad/2002-21-07.md): Main rotor spindle attachment bolt · Sikorsky S-76A, S-76B and S-76C · Effective Nov 25, 2002
- [AD 2002-22-10](https://openairdocs.org/ad/2002-22-10.md): Horizontal stabilizer slat (slat) · Bell Helicopter Textron Canada 407 · Effective Nov 21, 2002 · Supersedes AD 2000-20-18
- [AD 2002-22-09](https://openairdocs.org/ad/2002-22-09.md): Multi-purpose air intake · Airbus Helicopters AS332C, AS332L and AS332L1 · Effective Nov 21, 2002
- [AD 2002-17-51](https://openairdocs.org/ad/2002-17-51.md): Tail rotor blades · Agusta A109E · Historical · Effective Nov 21, 2002 · Replaced by AD 2002-25-51
- [AD 2002-23-06](https://openairdocs.org/ad/2002-23-06.md): Crankshaft gear retaining bolts · Textron Lycoming, AVCO AEIO-540, AEIO-540-D4A5, AEIO-540-D4B5 and 46 more · Historical · Effective Nov 19, 2002 · Replaced by AD 2004-05-24
- [AD 2002-22-08](https://openairdocs.org/ad/2002-22-08.md): Propeller hubs · Hartzell Propeller HD-E6C-3 · Effective Nov 19, 2002
- [AD 2002-22-06](https://openairdocs.org/ad/2002-22-06.md): Combustion chamber liner assembly · Honeywell International ALF502R-3, ALF502R-3A, ALF502R-4 and 4 more · Effective Nov 18, 2002
- [AD 2002-20-04](https://openairdocs.org/ad/2002-20-04.md): Exhaust system · SOCATA TB 21 · Effective Nov 18, 2002
- [AD 2002-22-05](https://openairdocs.org/ad/2002-22-05.md): Outboard mid-flap · Boeing 737-100 Series, 737-200 Series, 737-200C Series and 3 more · Historical · Effective Nov 15, 2002 · Replaced by AD 2003-24-08
- [AD 2002-19-10](https://openairdocs.org/ad/2002-19-10.md): Upper longeron and upper diagonal tube · Air Tractor AT-402, AT-402A, AT-402B and 3 more · Historical · Effective Nov 15, 2002 · Replaced by AD 2004-15-15
- [AD 2002-22-07](https://openairdocs.org/ad/2002-22-07.md): Inboard main flap · Boeing 767 Series (all) · Historical · Effective Nov 14, 2002 · Replaced by AD 2003-11-16

Next page: https://openairdocs.org/ad.md?year=2002&page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
SELECT d.ad_number, d.status, d.subject, d.makes, d.models, d.effective_date
FROM 'https://openairdocs.org/data/latest/faa_directive.parquet' d
WHERE year(coalesce(d.effective_date, d.publication_date, d.issue_date)) = 2002
ORDER BY coalesce(d.effective_date, d.publication_date, d.issue_date) DESC, d.ad_number DESC
```

This list as a web page: https://openairdocs.org/ad?year=2002

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.