- Registered owner
- Ponderosa Aviation LLC
- Location
- Safford, AZ
- Owner type
- LLC
- Serial number
- 11383
- Year built
- 1977
- Type
- Fixed wing multi engine
- Engine
- Turbo-prop
- Airworthiness
- Standard, normal
- Airworthiness date
- October 14, 1983
- Certificate issued
- April 3, 2026
- Expires
- April 30, 2033
- Mode S code
- A56FDB
Rockwell International 690BTCDS 2A4Airframe · Rockwell International 690BEngine modelAiResearch TPE331-5&6SER
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 21
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1977 | 1 |
|---|---|
| 1978 | 1 |
| 1979 | 1 |
| 1984 | 1 |
| 1988 | 1 |
| 1994 | 4 |
| 1995 | 2 |
| 1996 | 1 |
| 1998 | 5 |
| 1999 | 1 |
| 2000 | 1 |
| 2005 | 2 |
| 2006 | 1 |
| 2010 | 1 |
| 2013 | 1 |
Airframe · Rockwell International 690B
AD 2013-09-05FuselageAD 2009-25-02Upper wing skinsAD 2006-15-01Inboard and center aileron hinge fittingsInformation bulletins that may apply · 1
Advisory, not mandatory.
Airframe · Rockwell International 690B
SAIB 2023-14Landing Gear Retract/Extend SystemNTSB investigations
No NTSB investigations matched to N45AZMatched 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 Rockwell International 690B 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 95ZZZX6317Control Cable · frayedDURING C/W TWIN COMMANDER SB NR 195B, FOUND BOTH AFT RUDDER CABLES TO HAVE NUMEROUS CABLE STRANDS BROKEN. THE INSTRUCTIONS IN THE SB DO NOT ADDRESS THE REMOVAL OR INSPECTION AS OUTLINED IN AC 43.13-1A, CHAPTER 4, PARAGRAPH 198, FIGURE 4.14. THE SB PROCEDURE SDR 95ZZZX6316Control Cable · frayedDURING C/W TWIN COMMANDER SB NR 195B, FOUND BOTH AFT RUDDER CABLES TO HAVE NUMEROUS CABLE STRANDS BROKEN. THE INSTRUCTIONS IN THE SB DO NOT ADDRESS THE REMOVAL OR INSPECTION AS OUTLINED IN AC 43.13-1A, CHAPTER 4, PARAGRAPH 198, FIGURE 4.14. THE SB PROCEDURE
STCs that may be installed · 155
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Rockwell International 690B
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