- Registered owner
- Schreiber Jeffrey H
- Location
- Mundelein, IL
- Owner type
- Individual
- Serial number
- 28R-35170
- Year built
- 1969
- Type
- Fixed wing single engine
- Engine
- Reciprocating
- Airworthiness
- Standard, normal
- Airworthiness date
- April 3, 1969
- Certificate issued
- March 14, 2019
- Expires
- March 31, 2029
- Mode S code
- AD22CF
From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every Lycoming I0360 model are included below.
On this page
Airworthiness directives that may apply · 76
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1964 | 1 |
|---|---|
| 1966 | 1 |
| 1967 | 2 |
| 1969 | 3 |
| 1971 | 2 |
| 1972 | 4 |
| 1973 | 2 |
| 1974 | 1 |
| 1975 | 3 |
| 1976 | 1 |
| 1977 | 4 |
| 1978 | 1 |
| 1979 | 2 |
| 1980 | 2 |
| 1981 | 1 |
| 1982 | 2 |
| 1986 | 1 |
| 1989 | 2 |
| 1991 | 1 |
| 1992 | 1 |
| 1993 | 1 |
| 1994 | 1 |
| 1995 | 1 |
| 1996 | 5 |
| 1997 | 1 |
| 1998 | 4 |
| 2000 | 1 |
| 2001 | 1 |
| 2002 | 1 |
| 2003 | 2 |
| 2004 | 1 |
| 2005 | 2 |
| 2006 | 6 |
| 2007 | 1 |
| 2008 | 3 |
| 2009 | 1 |
| 2010 | 3 |
| 2011 | 1 |
| 2012 | 3 |
| 2013 | 1 |
| 2015 | 1 |
| 2017 | 2 |
| 2018 | 2 |
| 2021 | 2 |
| 2022 | 2 |
| 2024 | 2 |
| 2026 | 1 |
Airframe · Piper PA-28R-200
AD 2024-14-03Autopilot SystemAD 2022-03-15Fuel Quantity IndicatorAD 2020-26-16Wing SparInformation bulletins that may apply · 28
Advisory, not mandatory.
See all 32 bulletins
NTSB investigations
No NTSB investigations matched to N9455NMatched 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-28R-200 aircraft
FAA incident reports · 1
FAA accident and incident reports matched to this aircraft by N-number and event date, checked against the reported make and model.
Service difficulty reports · 2
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR 99ZZZX4059Stud · brokenROUGH ENGINE IN-FLIGHT. FOUND BROKEN CYLINDER HOLD DOWN STUDS NR 3 CYLINDER TOP RIGHT, BOTTOM RIGHT AND INSIDE, .3750 INCH STUDS ADJACENT ALSO BROKEN. OVERHAULED 8-18-93. PULLED AILERON AND CYLINDERS AND FOUND CYLINDER HOLD-DOWN BOLTS NOT PROPERLY TORQUED.SDR 99ZZZX3162Stud · failedPEN YAN O.H. 8-93 WO NR 11057 TOTAL TIME 1,671 HRS. PILOT EXPERIENCED ROUGH RUNNING ENGINE. NR 3 CYLINDER HOLD-DOWN STUDS TOP AND BOTTOM RIGHT SNAPPED OFF A CYLINDER FLANGE. TOP 2 CENTER STUDS SNAPPED AT FLANGE. BOTTOM RIGHT CENTER STUD SNAPPED AT CASE. SM
STCs that may be installed · 398
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-28R-200
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