| 92-16-7 |
Cessna |
Repetitively inspect horiz stab forward attach bulkhead; modify if cracked | 441 |
| 92-16-18 |
Cessna |
Supersedes 78-6-3 & 88-19-2 | modify & reinstall Enviroform-type commuter seats; modify seat tracks if indicated | 402,404,421,441 |
| 92-16-14 |
Beech |
Replace flame arrestor filter if phenolic honeycomb material | 400A |
| 92-16-12 |
BAe |
Revised 11/93 | install fluid vent masts on undercarriage fairings & plug specific existing vents per SB | DH/BH/HS/BAe 125 series |
| 92-16-11 |
Fairchild |
Modify horiz. stabilizer aft spar attachment fittings & stabilizer skin; repetitively inspect radius of rib splice straps; if cracked, modify | SA226, -227 |
| 92-15-7 |
Text-Lyc |
Supersedes 87-11-9 | inspect eng PT rotors & blades ev 50 hrs TIS or 300 CIS; replace if cracked; observe PT operating speed limits | LTS101, LTP101 series |
| 92-15-6 |
Beech |
Supersedes 91-23-7 | superseded by 93-24-3 |
| 92-15-4 |
BAe |
Install steel torque links on right & left main gear & reduce torque link & knuckle axial clearances per SB.32-226-3257A | 125-800A |
| 92-15-2 |
Beech |
Replace eng mount nut & bolt w/ones inspected by magnetic particle technique | 400 (SN -1 thru -65), MU-300 (SN -3 thru -91) |
| 92-15-16 |
Precis. Airmo. |
Superseded by 93-19-4 |
| 92-15-15 |
Piper |
Install gusset attachments to cracked eng mount structure | PA-36-300,-375 |
| 92-15-14 |
Piper |
Install vacuum gauge markings; enter limits in AFM | PA-46-310P,-350P |
| 92-15-13 |
Beech |
Supersedes 90-4-4 | recurringly inspect wing front spar lower cap for corrosion/ cracks; when specified, replace structural components; if reinforcing strap installed, inspect, adjust and/or replace per SIRM | specific 99s without wing mod kit |
| 92-15-11 |
P&W Eng |
Remove compressor delivery air line (P3) filter assembly | PT6A turbo |
| 92-15-1 |
Beech |
Replace improperly heat-treated bolts in eng truss-to-firewall | 90,99,100,200,300 |
| 92-13-9 |
Canadair |
Supersedes 92-3-6 | correct/replace crossed wires, unlocked pins in fire exting. sys &, if applicable, eng fire detect & warning sys | CL-600-1A11, -2A12, -2B16 |
| 92-13-7 |
Piper |
Replace empennage countersunk rivets w/universal head rivets | PA-46-310P,-350P |
| 92-13-6 |
Piper |
Install elevator trim cable guide sleeve | PA-46-310P, -350P |
| 92-13-5 |
Piper |
Install/reinstall clevis-head bolt in nose gear centering spring asmbly | PA-34-200,-T |
| 92-13-4 |
Piper |
Supersedes 90-23-18 | until dual fuel drain kit installed, use drain procedure stated in SB827A; revise POH & flight manual | PA-23-150,-160 |
