| 01-19-2 |
General Electric Engine |
Superseded by 03-5-10 |
| 01-19-3 |
Rolls-Royce Engine |
Replace HPT spacer as sepcified; revise Instruction for Continued Airworthiness | Citation X |
| 01-19-51 |
Eurocopter |
Superseded by 02-8-16 |
| 01-19-52 |
Bell |
Remove and replace main rotor pendulum weight support as specified | 222 |
| 01-19-6 |
Rolls-Royce Engine |
Replace HPT disc as specified | Gulfstream G-I |
| 01-2-10 |
Raytheon |
Inspect lower forward wing bolts for trademark; replace as specified | Duke |
| 01-2-11 |
Bell |
Remove specified main rotor mast assembly and replace | 204B |
| 01-2-13 |
Cessna |
Inspect DC power battery switch; replace as specified | CitationJet 1 |
| 01-2-3 |
Bell |
Inspect each collective lever assembly for raised forging boss; modify as specified | 206A,B,L,L1,L3 |
| 01-2-5 |
Bombardier |
Modify wiring of fuel port flood light housing of fuel service panel | CL-600-2B16 |
| 01-20-1 |
Pratt & Whitney Engine |
Repetitively perform visual inspection of compressor bleed valve assembly components as specified | PT6A-114A |
| 01-20-14 |
Fairchild |
Superseded by 02-8-2 |
| 01-20-18 |
Robinson |
Remove vertical stabilizer and inspect nutplate on channels | R44 |
| 01-20-3 |
Bell |
Install high altitude tail rotor static stop yield indicator as specified if equipped w/high altitude tail rotor kit | 206L-4 |
| 01-20-4 |
Agusta |
Modify each passenger sliding door as specified | A109E |
| 01-20-51 |
Rolls-Royce Engine |
Replace helical torquemeter gearshaft assemblies as specified | various models |
| 01-20-7 |
Raytheon |
Replace bus bars as specified | 400A |
| 01-21-2 |
Honeywell Int. Engine |
Revise AFM as specified, replace electronic engine controls | Cessna 441 |
| 01-21-6 |
Gulfstream |
Visually inspect engine electrical connections of fire extinguisher bottles as specified | G-V |
| 01-22-1 |
Enstrom |
Superseded by 02-8-3 |
