# N927HA: 2021 Balony Kubicek Spol Sro BB26XR - Status: Valid registration - Airframe: [Balony Kubicek Spol Sro BB26XR](https://openairdocs.org/model/balony-kubicek-spol-sro-bb26xr) (registry code 1370521, 1 seats) - Engine: [NONE](https://openairdocs.org/engine/none) (registry code 00000) - Data sheets: [TCDS B04CE](https://openairdocs.org/tcds/B04CE) (Kubíček Factory s.r.o) (OpenAirDocs) - Serial number: 1903 - Year built: 2021 - Type: Balloon - Engine type: None - Airworthiness: Standard, balloon - Airworthiness date: February 3, 2022 - Certificate issued: January 5, 2022 - Expires: January 31, 2029 - Mode S code: ACD8DB - Registered owner: [Indy Hot Air LLC](https://openairdocs.org/faa-owner/INDY%20HOT%20AIR%20LLC) - Location: [Westfield, IN](https://openairdocs.org/faa-place/IN/Westfield) - Owner type: LLC - Owner's area on the map: 40.0628° N, 86.0578° W: Placed by OpenAirDocs at the center of ZIP code 46062, within about 3 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=927HA - Page: https://openairdocs.org/aircraft/N927HA From the FAA registry file of October 24, 2026. ADs below are matched by the registry's airframe and engine model codes. They may apply; each AD's applicability can narrow it by serial number, part number or installed equipment. This is not a compliance determination. ## ADs that may apply (OpenAirDocs): 0 in force ### Matched by airframe (Balony Kubicek Spol Sro BB26XR) None in force. ### Matched by engine (NONE) None in force. ## Information bulletins (advisory) None matched. ## NTSB investigations None matched to N927HA. ## FAA accident and incident reports None matched to N927HA. ## Reports on N927HA not matched to an aircraft (1) They name N927HA, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. - [Incident 19970807028559I](https://openairdocs.org/incident/19970807028559I), Aug 7, 1997: Dhav DHC8102 (N927HA), Philadelphia, PA, Minor damage. Narrative: the outer cylinder (p/n 8814-9) of the nosegear assembly cracked during taxi at phl. This is the third crack on this part since 1995. Investigation… ## Service difficulty reports None filed for this aircraft. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. ## Service difficulty reports on N927HA not matched to an aircraft (18) They name N927HA, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. - [SDR HNAA0200083](https://openairdocs.org/sdr/HNAA0200083), Nov 21, 2002: WINDSHIELD. CRACKED. L/H Forward Sindshield shattered in flight at 16,000 FT. A/C diverted to GSP the windshield fram was inspected and the windscreen replaced. - [SDR HNAA0200081](https://openairdocs.org/sdr/HNAA0200081), Nov 19, 2002: WINDSHIELD. CRACKED. After Take-off F/O's windshield cracked. A/C returned to DCA where windshield was replaced. - [SDR HNAA0200024](https://openairdocs.org/sdr/HNAA0200024), Mar 2, 2002: CABLE. BROKEN. During aircraft taxi from terminal to hanger by maintenance, there was a loss of right brake control. Subsequent inspection found broken cable at #1 brake valve - [SDR HNAA0200014](https://openairdocs.org/sdr/HNAA0200014), Feb 2, 2002: FRAME. CORRODED. AT LEFT HAND EMERGENCY EXIT CORROSION FOUND ON FRAME AT STATION X366 AFT SIDE BELOW EMERGENCY EXIT. FRAME THICKNESS IS .040. DEPTH OF CORROSION AT EDGE OF FRAME - [SDR HNAA0200013](https://openairdocs.org/sdr/HNAA0200013), Jan 19, 2002: SKIN PANEL. CORRODED. Skin corroded and cracked at station x182 and stringer 33. Replaced skin panel. - [SDR HNAA0200016](https://openairdocs.org/sdr/HNAA0200016), Jan 18, 2002: SEAT TRACK. CORRODED. RT INBOARD SEAT RAIL CORRODED BETWEEN STATION X182 TO X222. REMOVED AND REPLACED SEAT RAIL IN ACCORDANCE WITH RD8-53-3074. - [SDR HNAA0200015](https://openairdocs.org/sdr/HNAA0200015), Jan 18, 2002: GUSSET. CORRODED. FOUND CORROSION ON GUSSET AT STATION X354 STRINGER 21 RT. MFG NEW GUSSET AND INSTALLED. - [SDR HNAA0100025](https://openairdocs.org/sdr/HNAA0100025), Apr 13, 2001: ENGINE. DEFECTIVE. SMOKE IN CABIN AND FLIGHT COMPARTMENT, SMELLED LIKE HOT DUCT. DECLARED EMERGENCY AND DIVERTED TO BUFFALO. AIRCRAFT FERRIED TO SBY. FOUND OIL IN HEAT EXCHANGER A - [SDR HNAA0100024](https://openairdocs.org/sdr/HNAA0100024), Apr 11, 2001: BALLAST. OVERHEATED. F/A NOTICED SMOKE AND ELECTRICAL SMELL IN CABIN. FOUND CENTER OVERHEAD LIGHT AT ROW 8 DIM AND BALLAST EXTREMELY HOT TO THE TOUCH. REPLACED THE LUMINAIRE/BALLAST - [SDR HNAA9900140](https://openairdocs.org/sdr/HNAA9900140), Oct 29, 1999: SMOKE DETECTOR. MALFUNCTIONED. BAGGAGE SMOKE WARNING LIGHT ILLUMINATED INFLIGHT AND EXTINGISHED ON LANDING. COULD NOT DUPLICATE PROBLEM ON GROUND. REMOVED AND REPLACED NUMBER 1 SMOKE DETECTOR - [SDR HNAA9900019](https://openairdocs.org/sdr/HNAA9900019), Jan 27, 1999: RETRACT MECH. MALFUNCTIONED. LANDING GEAR DOORS WOULD NOT CLOSE UNTIL NOSE GEAR TOUCHED DOWN ON LANDING. REPLACED 3261-K9 (P/N DSC182-2) RELAY. - [SDR HNAA9892794](https://openairdocs.org/sdr/HNAA9892794), Dec 21, 1998: SKIN. CORRODED. UNDER COCKPIT FLOOR MINOR SURFACE CORROSION TO THE SKIN ADJACENT TO STRINGER 31 RT, .020 DEPTH CORROSION TO THE SKIN APPROXIMATELY 3 INCHES LONG AT STRINGER 32 - [SDR HNAA9892793](https://openairdocs.org/sdr/HNAA9892793), Nov 28, 1998: STRINGER. CORRODED. JAX - FOUND CORROSION ON STRINGER 31 RT BETWEEN STATION 167 AND 182 WITH A LOSS OF 50 PERCENT OF MATERIAL. REPAIRED IAW RD8-53-1243. (M) - [SDR HNAA9892792](https://openairdocs.org/sdr/HNAA9892792), Nov 28, 1998: STRINGER. CORRODED. JAX - CORROSION WAS REPAIRED ON STRINGER 32 RT IAW EO8-53-98-385. (M) - [SDR 95ZZZX4242](https://openairdocs.org/sdr/95ZZZX4242), Jul 29, 1995: EEL BATT PACKS. FAILED. PHN/BWI - FLT 3260 - DURING PRE-FLIGHT WALK-AROUND, FOUND NUMEROUS INTERIOR AND EXTERIOR EMERGENCY LIGHTS INOP. REMOVED AND REPLACED THE EMERGENCY BATTERY PACKS - [SDR 95ZZZM130](https://openairdocs.org/sdr/95ZZZM130), May 12, 1995: AUTO FEATHER LTS. MALFUNCTIONED. FLT 3068 - PHL-LYH - AIRCRAFT RETURNED TO THE GATE WHEN THE AUTO FEATHER LIGHTS WOULD NOT ILLUMINATE DURING STATIC TEST WHILE ENGINES WERE RUNNING, BUT THE PROP - [SDR 95ZZZZ94](https://openairdocs.org/sdr/95ZZZZ94), Jan 22, 1995: PROP. OUT OF BALANCE. FLT 72 - ORF-PHF - AIRCRAFT HAS VIBRATION ABOVE 180 KNOTS. AIRCRAFT TURNED BACK TO ORF AND LANDED WITHOUT INCIDENT. PERFORMED PROP BALANCE AND ADJUSTED PROP BAL - [SDR 95ZZZZ93](https://openairdocs.org/sdr/95ZZZZ93), Jan 20, 1995: OIL. REQ'D SERVICE. FLT 3264 - EWN-CLT - NR 2 ENGINE OIL PRESSURE CAUTION LIGHT AND ENGINE OIL PRESSURE GAUGE ILLUMINATED AFTER TAKEOFF. AIRCRAFT TURNED BACK AND LANDED IN EWN WITH ## STCs that may be installed (OpenAirDocs) (1) Approved for this aircraft's airframe or engine model, in force first, then newest. The registry doesn't record which STCs an aircraft has; its records do. ### Approved for the airframe (Balony Kubicek Spol Sro BB26XR) - [STC SB04407AT](https://openairdocs.org/stc/SB04407AT): Installation of the DBI-III Omega. Balloonacy, Ltd. LLC ## Related - Other Balony Kubicek Spol Sro BB26XR aircraft: https://openairdocs.org/model/balony-kubicek-spol-sro-bb26xr/aircraft.md - The NONE engine: https://openairdocs.org/engine/none.md --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.