PA-42-720(AdvancedTrainer)
MAINTENANCEMANUAL
B. Fuselage Repairs -Pressurized Section (continued)
"J" Stringer Splice (Typical) R-1 and R-2
View A -A
12 ( Per Side) Rivets, MS20470-AD4 Equally Spaced with .375 Edge Margin.
EFFECTIVITY:
040-999
Jan 10/9051-70-00
PIPER AIRCRAFT
PA-42-720(Advanced Trainer)
MAINTENANCE MANUAL
B. FuselageRepairs-Pressurized Section (continued)
Bulkhead Repair (continued) R-3
9 Each MS20470AD4
EvenlySpaced
9 Each MS20470AD4
Evenly Spaced
17 Each MS20470AD4
EvenlySpaced
17 Each MS20470AD4
to Match Bulkhead
A
Repair for Left and Right Sides Similar Repair may be made using P/N 56287-18 bulkhead.
StructuralRepairs
Figure 801 (Sheet 2 of 17)
EFFECTIVITY:
040-999 51-70-00Jan10/90
PIPERAIRCRAFT
PA-42-720(AdvancedTrainer)
MAINTENANCEMANUAL
B. FuselageRepairs-PressurizedSection(continued)
BulkheadRepairR-4
On
PickupExistingPattern
View A-A TrimBackToClearCups
Repairfor Left and RightSidesSimilar Material:.0402024-T3Aluminum
StructuralRepairs
Figure801 (Sheet3 of 17)
EFFECTIVITY: 040-999
Jan
109051-70-0010/90
PIPERAIRCRAFT
PA-42-720(Advanced Trainer)
MAINTENANCEMANUAL
B. FuselageRepairs-Pressurized Section (continued)
Repairof Inner Skin (Typical) R-5
F.S.113.0
I Viewof Inner Skin Installation withRepairAccomplished 24 Each MS20470-AD4Rivets Pickup Existing Pattern
0
8 Each MS20470-AD4 RivetsEquallySpaced 4.25"
Material:.040 2024-T3 Aluminum
StructuralRepairs Figure801 (Sheet 4 of 17)
EFFECTIVITY: 040-999
51-70-00
PIPERAIRCRAFT
PA-42-720(AdvancedTrainer)
MAINTENANCEMANUAL
B. FuselageRepairs-Pressurized Section(continued)
BulkheadRepair(continued)
R-6
A
F.S.25.6
9 Each MS20470-AD4
Rivets 10Each MS20470-AD4
Rivets(Existing)
ExistingHole
View A-A
Repairfor Left and Right SidesSimilar Repairmay be made fromP/N 56286-2 bulkhead withflangesremoved.
StructuralRepairs
Figure801 (Sheet 5 of 17)
EFFECTIVITY:
040-999
PAGE6 51-70-00
Jan 10/90
PIPERAIRCRAFT PA-42-720(Advanced Trainer) MAINTENANCEMANUAL B. FuselageRepairs-PressurizedSection(continued) BulkheadRepair(continued) R-7
TypicalBulkheadLocation
PickupExistingPattern( 4 Each) -26 EachMS20470-AD4Rivets Bulkhead F.S.297.38 Bulkhead F.S. 280.0
A
View A A
RepairmaybemadefromP/N56261-4bulkhead withflangesremoved.
StructuralRepairs
Figure801 (Sheet6of17)
EFFECTIVITY:
040-999
PAGE
51-70-00
Jan 10/907
PIPER AIRCRAFT PA-42-720 (Advanced Trainer)
MAINTENANCEMANUAL
B. FuselageRepairs-Pressurized Section (continued)
Typical Fuselage Center Bulkhead Repair
R-8
-Angle
Center Bulkhead
LongitudinalBeam Assembly Repair for Left and Right Sides Similar Material:.050 2024-T3 Aluminum StructuralRepairs Figure801 (Sheet 7 of 17) EFFECTIVITY: 040-999
PAGRE8
Jan 10/90 51-70-00
PIPER AIRCRAFT
PA-42-720 (Advanced Trainer)
MAINTENANCE MANUAL
B. Fuselage Repairs -Pressurized Section (continued)
Fuselage Skin Repair (Typical) R-9 and R-10
Note:
Stop Drill Cracks Before Adding Doubler
6 Each MS20470-AD5 Rivets 7 Each MS20470 -AD5 Rivets
6 Each MS20470-AD5 Rivets 7 Each MS20470 -AD5 Rivets
Material: .080 2024-T3 Clad Aluminum Bevel Sides 45 ° X .070
Structural Repairs Figure 801 (Sheet 8 of 17)
EFFECTIVITY: 040-999 51-70-00 PAGE9
PIPERAIRCRAFT
PA-42-720(Advanced Trainer)
MAINTENANCEMANUAL
B. Fuselage Repairs -Pressurized Section (continued)
BulkheadShelfRepair R-11
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