- Registered owner
- Redlands Flying Club
- Location
- Redlands, CA
- Owner type
- Corporation
- Serial number
- 2843127
- Year built
- 1998
- Type
- Fixed wing single engine
- Engine
- Reciprocating
- Airworthiness
- Standard, normal, utility
- Airworthiness date
- March 17, 1998
- Certificate issued
- May 31, 2005
- Expires
- July 31, 2027
- Mode S code
- A4ED40
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 30
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1977 | 2 |
|---|---|
| 1979 | 3 |
| 1980 | 3 |
| 1986 | 2 |
| 1989 | 1 |
| 1996 | 2 |
| 1999 | 1 |
| 2000 | 1 |
| 2001 | 1 |
| 2004 | 1 |
| 2005 | 2 |
| 2006 | 2 |
| 2008 | 2 |
| 2009 | 1 |
| 2010 | 1 |
| 2013 | 1 |
| 2015 | 1 |
| 2016 | 1 |
| 2017 | 1 |
| 2018 | 2 |
| 2021 | 1 |
| 2022 | 1 |
| 2024 | 2 |
Airframe · Piper PA-28-181
AD 2024-14-03Autopilot SystemAD 2024-10-04Wing, Attach FittingsAD 2022-03-15Fuel Quantity IndicatorInformation bulletins that may apply · 17
Advisory, not mandatory.
See all 18 bulletins
NTSB investigations
No NTSB investigations matched to N4163WMatched by N-number and event date, checked against the reported serial number, make and model. Investigations from before this aircraft carried the mark are under Earlier aircraft. Investigations on Piper PA-28-181 aircraft
FAA incident reports
No FAA accident or incident reports matched to N4163WMatched by N-number and event date, checked against the reported make and model. Reports from before this aircraft carried the mark are under Earlier aircraft. Reports on Piper PA-28-181 aircraft
Service difficulty reports · 5
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR 2003FA0001244Gear · failedPILOT REPORTED AIRCRAFT WOULD NOT START, UPON INSPECTION FOUND BENDIX ON STARTER SHATTERED AND THE TEETH ON STARTER RING GALLED. RECOMMEND RE-EVALUATE STRENGTH OF MATERIAL USED TO MANUFACTURE BENDIX.SDR 2003FA0000821Connector · burnedDURING MAINTENANCE ON AIRCRAFT TECHNICIAN FOUND CONNECTOR P5 PINS 5 AND 6 SHOWS SIGNS OF OVERHEATING AND DISCOLORING OF CONNECTOR AND PINS. THESE PINS GO TO THE NAVIGATION LIGHTS. PROBABLE CAUSE OF OVERHEATING IS CURRENT DRAW EXCEEDING DESIGN OF CONNECTORS ASDR 2003FA0000797Screw · looseDURING FLEET-WIDE INSPECTION, FOUND SCREW THAT ATTACHES CONTROL WHEEL TO CONTROL SHAFT LOOSE. RECOMMEND DIFFERENT METHOD OF ATTACHMENT OR THE USE OF A LOCKING/SAFETY DEVICE.SDR VJ32001F00015Distributor Blk · wornMAGNETO REMOVED FROM ENGINE FOR 500 HOUR INSPECTION IAW THE MM. REMOVED THE REAR COVER AND THE DISTRIBUTOR BLOCK FROM MAGNETO AND FOUND THE CARBON BRUSH WORN. CARBON DUST WAS FOUND ON THE FLAT PART OF THE CAP. THE WEARER ON THIS BRUSH IS ABOVE NORMAL FOR 50SDR 20000809SH018Control Cable · frayedLEFT AILERON BALANCE CABLE FRAYED, LOCATED UNDER THE REAR SEATS. (X)
STCs that may be installed · 333
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Piper PA-28-181
STC SA02571SEInstallation of Garmin G500/G600 TXi Integrated Avionics System (Primary Flight Display, Multi-Function Display, and Engine Indicating System Display).STC SA01800SEFabrication and installation of new or replacement of existing instrument panel lights dimmer control.STC SA01861SEFabrication and installation of Landing Light Controller