- Registered owner
- Cowlishaw Brenda L
- Location
- Bulverde, TX
- Owner type
- Individual
- Serial number
- H003
- Year built
- 2012
- Type
- Balloon
- Engine
- None
- Airworthiness
- Experimental, amateur built
- Airworthiness date
- June 9, 2012
- Certificate issued
- February 14, 2018
- Expires
- February 29, 2028
- Mode S code
- A6A108
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 0
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
No ADs matched this aircraft’s modelsADs on appliances, propellers and installed equipment aren’t matched by model; check those separately.
Information bulletins that may apply
Advisory, not mandatory.
No bulletins matched this aircraft’s models
NTSB investigations
No NTSB investigations matched to N526UPMatched 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 Albert F Padelt PHY-37 aircraft
FAA incident reports
No FAA accident or incident reports matched to N526UPMatched 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 Albert F Padelt PHY-37 aircraft
Service difficulty reports
No reports matched to N526UPGeneral aviation reporting is voluntary. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Reports on Albert F Padelt PHY-37 aircraft
Reports on N526UP not matched to an aircraft · 132
They name N526UP, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.
SDR WRNA200800002Frame · crackedDURING B-CHECK INSPECTION, RIGHT FRAME AT STATION 2674.85 WAS FOUND CRACKED AT WL 325. REMOVED DAMAGE SECTION OF FRAME, FABRICATED AND INSTALLED REPAIR DOUBLERS IAW 747 SRM 51-40-03 FIG 2.SDR WRNA200800001Bulkhead · chafedDURING B-CHECK WHILE ACCOMPLISHING AD 2007-19-19, NR 1 PYLON STRUT FORWARD ENGINE MOUNT BULKHEAD CORD WAS FOUND WITH CHAFED RADIUS AT LOWER INBOARD END. FABRICATED AND INSTALLED REPAIR ANGLE IAW BOEING SKETCH SR1-733824930-1. THIS REPAIR IS TEMPORARY AND REQSDR WRNA200700063Sensor · no testDURING TAKEOFF, AT 80 KNOTS, CREW RECEIVED A STALL WARNING, TAKEOFF WAS ABORTED. AOA FAILED TEST IAW B747 MM 27-32-00 PG 507. REPLACED AOA SENSOR
IAW 747 MM 27-32-01 PG 102. SYSTEM TEST GOOD IAW 747 MM 27-32-00 PG 507. AIRCRAFT RELEASED FOR SERVICE.
See all 132 unmatched reportsSTCs that may be installed
No STCs matched this aircraft’s modelsSTCs change type-certificated designs, and this aircraft isn’t type certificated.