- Registered owner
- Apex Tower Group LLC
- Location
- Spring, TX
- Owner type
- LLC
- Serial number
- 501-0128
- Year built
- 1979
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, normal
- Airworthiness date
- November 30, 1979
- Certificate issued
- January 24, 2025
- Expires
- January 31, 2032
- Mode S code
- A63DDF
From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every Pratt & Whitney Canada JT15D-1 model are included below.
On this page
Airworthiness directives that may apply · 19
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1975 | 1 |
|---|---|
| 1980 | 2 |
| 1988 | 1 |
| 1993 | 2 |
| 1998 | 2 |
| 2001 | 1 |
| 2004 | 3 |
| 2006 | 1 |
| 2007 | 1 |
| 2008 | 1 |
| 2013 | 1 |
| 2015 | 1 |
| 2023 | 2 |
| 2025 | 1 |
See all 20 ADs
Information bulletins that may apply · 4
Advisory, not mandatory.
Historical bulletins · 1
NTSB investigations
No NTSB investigations matched to N501CFMatched 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 Cessna 501 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 · 4
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR 2006FA0000721Seat · crackedUPPER CHAIR BASE ASSEMBLY CRACKED AT CHAIR BACK ATTACH POINTS. ALSO, PREVIOUS INAPPROPRIATE REPAIR. CHAIR WAS REPAIRED IAW STC, STRUCTURAL SEAT REPAIR. (K)SDR R2J2004F00001Control Cable · misinstalledDURING PHASE 5 INSPECTION, UPON REINSTALLING LT WING FLAP CABLES, NOTICED AIRCRAFT WAS DIFFERENT THAN MM DATA AS TO ROUTING OF FLAP CABLES ON LT OB BELLCRANK. EXPERIMENTED AND CONTACTED MFG TECH SUPPORT. FOUND DATA ON PG 27-50-01 PG 203 FIG 201 (SHEET 2) SHOSDR R2J2004F00000Brace · mismanufacturedWHILE REINSTALLING LT WING FLAP CABLES DURING PHASE 5 INSPECTION, NOTICED CABLE RUN TOO CLOSE TO STRUCTURE. INVESTIGATION AND NOTIFIED MFG TECH SUPPORT. IT WAS DETERMINED LT BRACE 5511037-3 AND RIB 5525130, CABLE PASS THRU WERE INCORRECTLY LOCATED DURING MANSDR 97ZZZX2028Hose · failedDURING CRUISE AT FL 370, PRESSURIZATION SET FOR FL 380 WITH CABIN AT APPROX 7,000 FEET. CREW HEARD A DULL NOISE, CABIN OXY MASK DEPLOYED, MASTER WARN RED LIGHTS AND CABIN ALTITUDE INCREASING. ACFT DIVERTED FOR REPAIR. FOUND FAILED BLEED SYS HOSE AND A NON-
STCs that may be installed · 170
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Cessna 501
STC SA04837NYInstallation of AeroLED's Holdings, LLC., position lights, navigation lights, strobe lights and beacon lightsSTC SA12345IBReplacement of the Halon Type 1211 portable fire extinguisher with the Halotron BrX portable fire extinguisherSTC SA2622NMInstallation of Precise Flight Pulselite Control Unit in landing/taxi system. (767-200 B17) (DHC-8 101)