Rich:
You have all of the stigmata of a chronic seat remover-installer. Reading your instructions had me breaking out in a cold sweat, since I suffer from the same condition (slightly worse, since I've done mine 1.12 billion times). I think that I suffer from PTSD (Post-Traumatic Seat Disorder).
Steve
KAP140 Autopilot Pitch Fault
Moderators: Rick, Lance Murray
- Rich
- 5 Diamonds Member
- Posts: 4608
- Joined: Mon Aug 30, 2010 12:40 pm
- First Name: Rich
- Aircraft Type: DA40
- Aircraft Registration: N40XE
- Airports: S39 Prineville OR
- Has thanked: 145 times
- Been thanked: 1187 times
Re: KAP140 Autopilot Pitch Fault
Try one other thing, Jehan. With the trim wheel in its stuck state, try pushing the stick all the way forward when trying to move the trim wheel. I've noted that the trim starts to get somewhat sticky with the stick vertical or fully back, particularly if the trim friction block is a bit contaminated.
2002 DA40-180: MT, PowerFlow, 530W/430W, KAP140, ext. baggage, 1090 ES out, 2646 MTOW, 40gal., Surefly, Flightstream 210, Orion 600 LED, XeVision, Aspen E5
- jehan
- 2 Diamonds Member
- Posts: 13
- Joined: Sun Mar 14, 2021 3:52 am
- First Name: Jehan
- Aircraft Type: DA40
- Aircraft Registration: N647DS
- Airports: KGEU
- Has thanked: 5 times
Re: KAP140 Autopilot Pitch Fault
Thanks Rich,
I will test the "trim wheel in stuck state, try pushing the stick all the way forward when trying to move the trim wheel."
Here is the image of the mechanism from IPC. Just wanted to confirm if the "gear segment" is referring to the chain-sprocket piece of hardware. thanks,
Jehan
I will test the "trim wheel in stuck state, try pushing the stick all the way forward when trying to move the trim wheel."
Here is the image of the mechanism from IPC. Just wanted to confirm if the "gear segment" is referring to the chain-sprocket piece of hardware. thanks,
Jehan
- jehan
- 2 Diamonds Member
- Posts: 13
- Joined: Sun Mar 14, 2021 3:52 am
- First Name: Jehan
- Aircraft Type: DA40
- Aircraft Registration: N647DS
- Airports: KGEU
- Has thanked: 5 times
Re: KAP140 Autopilot Pitch Fault
One question with regards to the functioning of KAP140. As I understand there are all together 3 servos i.e. Roll servo, Pitch servo and Pitch Trim servo. When we are doing autopilot test on the ground, for Roll servo (since it is only one) it is clear that the heading bug will help move this one and as a result the stick will appear to move laterally. When it comes to pitch test... we have two servos. If memory serves, before this problem that I reported the whole stick was moving i.e. the pitch servo was in motion. However, on this particular day, I noticed instead of the stick, the pitch trim servo was in motion, i.e. the trim wheel started moving. So the question is: have I done something that demanded the pitch trim servo to move instead of the pitch servo to act? I understand pitch servo is coarse control as compared to pitch trim servo. I will appreciate if you can shed some light on this topic. Thanks
- Rich
- 5 Diamonds Member
- Posts: 4608
- Joined: Mon Aug 30, 2010 12:40 pm
- First Name: Rich
- Aircraft Type: DA40
- Aircraft Registration: N40XE
- Airports: S39 Prineville OR
- Has thanked: 145 times
- Been thanked: 1187 times
Re: KAP140 Autopilot Pitch Fault
No, it's the part on the opposite side. Get rev 8 (current) of the AMM and check out section 27-38-00, especially page 7, paragraph 3, where there is a really excellent description of this operation.jehan wrote: ↑Tue Dec 28, 2021 10:24 pm Thanks Rich,
I will test the "trim wheel in stuck state, try pushing the stick all the way forward when trying to move the trim wheel."
Here is the image of the mechanism from IPC. Just wanted to confirm if the "gear segment" is referring to the chain-sprocket piece of hardware.
pitch trim assembly.png
thanks,
Jehan
2002 DA40-180: MT, PowerFlow, 530W/430W, KAP140, ext. baggage, 1090 ES out, 2646 MTOW, 40gal., Surefly, Flightstream 210, Orion 600 LED, XeVision, Aspen E5
- Rich
- 5 Diamonds Member
- Posts: 4608
- Joined: Mon Aug 30, 2010 12:40 pm
- First Name: Rich
- Aircraft Type: DA40
- Aircraft Registration: N40XE
- Airports: S39 Prineville OR
- Has thanked: 145 times
- Been thanked: 1187 times
Re: KAP140 Autopilot Pitch Fault
Hard to say. Basically the pitch and pitch-trim servos work together with the FC and try to maintain VS or ALT. When on the ground and the plane really can not react to the desired commands it's anybody's guess what the the AP decides what is necessary. I have observed this myself when checking the AP on the ground.jehan wrote: ↑Tue Dec 28, 2021 10:51 pm One question with regards to the functioning of KAP140. As I understand there are all together 3 servos i.e. Roll servo, Pitch servo and Pitch Trim servo. When we are doing autopilot test on the ground, for Roll servo (since it is only one) it is clear that the heading bug will help move this one and as a result the stick will appear to move laterally. When it comes to pitch test... we have two servos. If memory serves, before this problem that I reported the whole stick was moving i.e. the pitch servo was in motion. However, on this particular day, I noticed instead of the stick, the pitch trim servo was in motion, i.e. the trim wheel started moving. So the question is: have I done something that demanded the pitch trim servo to move instead of the pitch servo to act? I understand pitch servo is coarse control as compared to pitch trim servo. I will appreciate if you can shed some light on this topic. Thanks
2002 DA40-180: MT, PowerFlow, 530W/430W, KAP140, ext. baggage, 1090 ES out, 2646 MTOW, 40gal., Surefly, Flightstream 210, Orion 600 LED, XeVision, Aspen E5
- jehan
- 2 Diamonds Member
- Posts: 13
- Joined: Sun Mar 14, 2021 3:52 am
- First Name: Jehan
- Aircraft Type: DA40
- Aircraft Registration: N647DS
- Airports: KGEU
- Has thanked: 5 times
Re: KAP140 Autopilot Pitch Fault
Thanks,Rich wrote: ↑Tue Dec 28, 2021 11:07 pmNo, it's the part on the opposite side. Get rev 8 (current) of the AMM and check out section 27-38-00, especially page 7, paragraph 3, where there is a really excellent description of this operation.jehan wrote: ↑Tue Dec 28, 2021 10:24 pm Thanks Rich,
I will test the "trim wheel in stuck state, try pushing the stick all the way forward when trying to move the trim wheel."
Here is the image of the mechanism from IPC. Just wanted to confirm if the "gear segment" is referring to the chain-sprocket piece of hardware.
pitch trim assembly.png
thanks,
Jehan
Please see if this drawing makes sense in light of page 7 paragraph 3.
Thanks,
Jehan
- Rich
- 5 Diamonds Member
- Posts: 4608
- Joined: Mon Aug 30, 2010 12:40 pm
- First Name: Rich
- Aircraft Type: DA40
- Aircraft Registration: N40XE
- Airports: S39 Prineville OR
- Has thanked: 145 times
- Been thanked: 1187 times
Re: KAP140 Autopilot Pitch Fault
It's correct for nose-down trim. Remember, trim-tab movement is opposite to what it causes in the elevator.jehan wrote: ↑Wed Dec 29, 2021 1:34 amThanks,Rich wrote: ↑Tue Dec 28, 2021 11:07 pmNo, it's the part on the opposite side. Get rev 8 (current) of the AMM and check out section 27-38-00, especially page 7, paragraph 3, where there is a really excellent description of this operation.jehan wrote: ↑Tue Dec 28, 2021 10:24 pm Thanks Rich,
I will test the "trim wheel in stuck state, try pushing the stick all the way forward when trying to move the trim wheel."
Here is the image of the mechanism from IPC. Just wanted to confirm if the "gear segment" is referring to the chain-sprocket piece of hardware.
pitch trim assembly.png
thanks,
Jehan
Please see if this drawing makes sense in light of page 7 paragraph 3.
pitch trim assembly v2.png
Thanks,
Jehan
2002 DA40-180: MT, PowerFlow, 530W/430W, KAP140, ext. baggage, 1090 ES out, 2646 MTOW, 40gal., Surefly, Flightstream 210, Orion 600 LED, XeVision, Aspen E5