# N398UA: 2023 Costruzioni Aeronautiche Tecna P2006T

- Status: Valid registration
- Airframe: [Costruzioni Aeronautiche Tecna P2006T](https://openairdocs.org/model/costruzioni-aeronautiche-tecna-p2006t) (registry code 0330001, 4 seats)
- Engine: [Rotax 912S3](https://openairdocs.org/engine/rotax-912s3) (registry code 55594)
- Data sheets: [TCDS A62CE](https://openairdocs.org/tcds/A62CE) (Costruzioni Aeronautiche Tecnam S.P.A.), [TCDS E00051EN](https://openairdocs.org/tcds/E00051EN) (BRP-Rotax GmbH & Co KG) (OpenAirDocs)
- Serial number: 398/US
- Year built: 2023
- Type: Fixed wing multi engine
- Engine type: 4 cycle
- Airworthiness: Standard, normal
- Airworthiness date: April 16, 2024
- Certificate issued: March 24, 2025
- Expires: March 31, 2032
- Mode S code: A4A244
- Registered owner: [Ab Prop Plane I LLC](https://openairdocs.org/faa-owner/AB%20PROP%20PLANE%20I%20LLC)
- Location: [Metairie, LA](https://openairdocs.org/faa-place/LA/Metairie)
- Owner type: LLC
- Owner's area on the map: 30.0102° N, 90.1626° W: Placed by OpenAirDocs at the center of ZIP code 70002, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=398UA
- Page: https://openairdocs.org/aircraft/N398UA

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): 24 in force

### Matched by airframe (Costruzioni Aeronautiche Tecna P2006T)

- [AD 2026-19-06](https://openairdocs.org/ad/2026-19-06): Aileron Control System · Costruzioni Aeronautiche Tecnam P2006T. Effective Oct 13, 2026
- [AD 2021-22-22](https://openairdocs.org/ad/2021-22-22): Nose/Tail Landing Gear · Costruzioni Aeronautiche Tecnam P2006T. Effective Dec 3, 2021
- [AD 2018-15-07](https://openairdocs.org/ad/2018-15-07): Flight Controls · Costruzioni Aeronautiche Tecnam P2006T. Effective Sep 4, 2018
- [AD 2015-02-09](https://openairdocs.org/ad/2015-02-09): Engine Exhaust · Costruzioni Aeronautiche Tecnam P2006T. Effective Mar 5, 2015
- [AD 2014-11-09](https://openairdocs.org/ad/2014-11-09): Power Plant · Costruzioni Aeronautiche Tecnam P2006T. Effective Jul 15, 2014
- [AD 2014-02-07](https://openairdocs.org/ad/2014-02-07): Landing Gear · Costruzioni Aeronautiche Tecnam P2006T. Effective Mar 14, 2014
- [AD 2013-04-09](https://openairdocs.org/ad/2013-04-09): Wings · Costruzioni Aeronautiche Tecnam P2006T. Effective Apr 9, 2013
- [AD 2012-18-04](https://openairdocs.org/ad/2012-18-04): Landing Gear · Costruzioni Aeronautiche Tecnam P2006T. Effective Oct 22, 2012
- [AD 2011-13-02](https://openairdocs.org/ad/2011-13-02): Landing Gear · Costruzioni Aeronautiche Tecnam P2006T. Effective Jul 22, 2011

### Matched by engine (Rotax 912S3)

- [AD 2026-16-11](https://openairdocs.org/ad/2026-16-11): Reciprocating Engine Front Section · BRP-Rotax 912 F2, 912 F3, 912 F4 and 16 more. Effective Aug 28, 2026
- [AD 2023-17-13](https://openairdocs.org/ad/2023-17-13): Reciprocating Engine Front Section · BRP-Rotax 912 F2, 912 F3, 912 F4 and 16 more. Effective Sep 20, 2023
- [AD 2019-10-04](https://openairdocs.org/ad/2019-10-04): Reciprocating Engine Cylinder Section · BRP-Rotax 912 F2, 912 F3, 912 F4 and 6 more. Effective Jul 10, 2019
- [AD 2016-23-04](https://openairdocs.org/ad/2016-23-04): Carburetor floats · BRP-Rotax 912 F2, 912 F3, 912 F4 and 6 more. Effective Dec 7, 2016
- [AD 2016-13-04](https://openairdocs.org/ad/2016-13-04): Engine coolant temperature limit · BRP--POWERTRAIN 912 F2, 912 F3, 912 F4 and 6 more. Effective Jul 27, 2016
- [AD 2013-15-19](https://openairdocs.org/ad/2013-15-19): Excessive oil consumption · BRP--POWERTRAIN 912 F2, 912 F3, 912 F4 and 6 more. Effective Aug 27, 2013
- [AD 2012-16-13](https://openairdocs.org/ad/2012-16-13): Pressure side fuel hose · BRP--POWERTRAIN 912 F2, 912 F3, 912 F4 and 3 more. Effective Sep 10, 2012
- [AD 2012-04-03](https://openairdocs.org/ad/2012-04-03): Oil pump attachment bolts · BRP--POWERTRAIN 912 S2, 912 S3 and 914 F2. Effective Mar 16, 2012
- [AD 2011-25-02](https://openairdocs.org/ad/2011-25-02): Crankshaft · BRP--POWERTRAIN 912 F2, 912 F3, 912 F4 and 6 more. Effective Dec 22, 2011
- [AD 2011-12-04](https://openairdocs.org/ad/2011-12-04): Washers · Bombardier-Rotax 912 F3, 912 S2, 912 S3 and 4 more. Effective Jun 27, 2011
- [AD 2010-20-23](https://openairdocs.org/ad/2010-20-23): Engine crankcase · Bombardier-Rotax 912 F2, 912 F3, 912 F4 and 6 more. Effective Nov 8, 2010
- [AD 2010-18-14](https://openairdocs.org/ad/2010-18-14): Fuel pressure · Bombardier-Rotax 912 F2, 912 F3, 912 F4 and 3 more. Effective Oct 13, 2010
- [AD 2005-01-14](https://openairdocs.org/ad/2005-01-14): Valve train on all engines · BRP--POWERTRAIN 912 F2, 912 F3, 912 F4 and 6 more. Effective Feb 15, 2005
- [AD 2002-19-09](https://openairdocs.org/ad/2002-19-09): Fuel pump assembly · BRP--POWERTRAIN 912 F2, 912 F3, 912 F4 and 3 more. Effective Oct 10, 2002
- [AD 2002-16-07](https://openairdocs.org/ad/2002-16-07): Valve Spring Retainers · BRP--POWERTRAIN 912 F2, 912 F3, 912 F4 and 6 more. Effective Sep 3, 2002

### Historical (superseded or no longer in force)

- [AD 2013-07-12](https://openairdocs.org/ad/2013-07-12) (historical): Cylinder heads · BRP--POWERTRAIN 912 F2, 912 F3, 912 F4 and 6 more. Effective Apr 30, 2013
- [AD 2002-21-16](https://openairdocs.org/ad/2002-21-16) (historical): Valve train · Bombardier-Rotax 912 F2, 912 F3, 912 F4 and 6 more. Effective Oct 28, 2002

## Information bulletins (advisory) (3 in force)

- [SAIB CE-18-03](https://openairdocs.org/saib/CE-18-03): TIME LIMITS/MAINTENANCE CHECKS - Costruzioni Aeronautiche Tecnam P2006T Wrong Rudder Trim Actuator Part Number. Issued Nov 15, 2017
- [SAIB NE-05-84R1](https://openairdocs.org/saib/NE-05-84R1): Reciprocating Engine Liquid Cooling: Bombardier-Rotax 912 & 914 Series Engines. Issued Sep 10, 2009
- [SAIB NE-08-36](https://openairdocs.org/saib/NE-08-36): BRP-Rotax 912 A, 912 F, 912 S, & 914 F Series Reciprocating Engines. Issued Jul 16, 2008

## NTSB investigations

None matched to N398UA.

## FAA accident and incident reports

None matched to N398UA.

## 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 N398UA not matched to an aircraft (83, newest 50)

They name N398UA, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR 2008UALA06222](https://openairdocs.org/sdr/2008UALA06222), Sep 8, 2008: FAN. FAULTY. CREW REPORT: ALT EQUIP COOLING FAN INTERMITTENT AT FL250 SAMC TEXT: PACKS AND CABIN PRESSURIZATION NORMAL, ALT EQUIP COOLING EXHAUST FAN 'OFF' LIGHT FLICKERING 
- [SDR 2008UALA04173](https://openairdocs.org/sdr/2008UALA04173), Aug 8, 2008: UNKNOWN. UNKNOWN. EQUIPMENT COOLING EXHAUST OFF LIGHT ILLUM. REPLACE MULTIPLE PARTS (ALT EXHAUST BLOWER, EXHAUST AIRFLOW DETECTOR, TURBOFAN VALVE)
- [SDR 2008UALA03160](https://openairdocs.org/sdr/2008UALA03160), Jun 2, 2008: LIGHT. UNSECURE. FLOOR EMERGENCY LIGHTING STRIP PULLED UP AT 1B. FOUND LIGHT ASSEMBLY LOOSE. SECURED LIGHT ASSEMBLY. AC OK FOR SERVICE.
- [SDR 2008UALA02601](https://openairdocs.org/sdr/2008UALA02601), May 4, 2008: SKIN. CORRODED. AFT CARGO PIT AREA AROUND NR 3 VHF ANTENNA CUT-OUT AT BS 727D +10" IS CORRODED BETWEEN STRINGERS S-27L AND S- 27R AT BL0 AND WL148. MAJOR REPAIR ACCOMPLISHED, R
- [SDR 2008UALA02582](https://openairdocs.org/sdr/2008UALA02582), May 4, 2008: RIB. CRACKED. RT WING WBL 135.5 LOWER RIB LOWER CHORD BETWEEN WING STRINGERS S2 AND S3. MAJOR REPAIR ACCOMPLISHED, REMOVED DAMAGE AND VERIFIED DAMAGE REMOVAL WITH HFEC. INSTA
- [SDR 2008UALA02600](https://openairdocs.org/sdr/2008UALA02600), May 3, 2008: OXYGEN MASK. FAULTY. FIRST OFFICER'S MASK LINES ARE FRAYED. REPLACED FIRST OFFICERS O2 MASK REF MM 25-11-11 PG 201 OP CHECKED GOOD. AC OK FOR SERVICE.
- [SDR 2008UALA02599](https://openairdocs.org/sdr/2008UALA02599), May 3, 2008: OXYGEN MASK. FAULTY. CAPTAIN O2 MASK LINES ARE FRAYED. REPLACED CAPTAINS O2 MASK REF MM 25-11-11 PG 201 OP CHECKED GOOD. AC OK FOR SERVICE.
- [SDR 2008UALA02581](https://openairdocs.org/sdr/2008UALA02581), May 3, 2008: STRUCTURE. CRACKED. FWD GALLEY DOOR, LOWER HINGE CUTOUT CRACKED IN TWO PLACES. MAJOR REPAIR ACCOMPLISHED, CRACK DAMAGES WERE CONTAINED AND REPAIR DOUBLER WITH FILLERS WAS INSTALLED
- [SDR 2008UALA02580](https://openairdocs.org/sdr/2008UALA02580), May 3, 2008: STRINGER. CRACKED. STRINGER 15L END FITTING IS CRACKED BETWEEN BS 348.2 AND 380. MAJOR REPAIR ACCOMPLISHED, REPLACED SPLICE CHANNEL.
- [SDR 2008UALA02579](https://openairdocs.org/sdr/2008UALA02579), May 2, 2008: SKIN. DENTED. RT HORIZONTAL STABILIZER LOWER EXTERNAL SKIN HAS 3 DENTS GROUPED TOGETHER 109 TO 124 INCHES FROM INBOARD EDGE AND 11 INCHES FROM LEADING EDGE. MAJOR REPAIR ACCO
- [SDR 2008UALA02557](https://openairdocs.org/sdr/2008UALA02557), May 1, 2008: DOOR FRAME. CRACKED. FWD CARGO DOOR FWD FRAME IS CRACKED AT LWR STOP FITTING. MAJOR REPAIR ACCOMPLISHED, INSTALLED NESTED ANGLE REPAIR.
- [SDR 2008UALA02556](https://openairdocs.org/sdr/2008UALA02556), May 1, 2008: DOOR FRAME. CRACKED. FWD CARGO DOOR FRAME CRACKED AT LOWER AFT STOP FITTING. MAJOR REPAIR ACCOMPLISHED: REPLACED LOWER AFT FRAME.
- [SDR 2008UALA02555](https://openairdocs.org/sdr/2008UALA02555), May 1, 2008: FRAME. DAMAGED. AFT CARGO DOOR, UPPER FWD CORNER INTERIOR FRAME HAS SEVERAL PREVIOUS TOOLING MARKS. MAJOR REPAIR ACCOMPLISHED, REPLACED FWD UPPER FRAME.
- [SDR 2008UALA02554](https://openairdocs.org/sdr/2008UALA02554), May 1, 2008: DOOR FRAME. DAMAGED. AFT CARGO DOOR, AFT SIDE INTERIOR FRAME HAS PREVIOUS TOOLING DAMAGE APPROX 8 INCH ABOVE LATCH TORQUE TUBE. MAJOR REPAIR ACCOMPLISHED, REPLACED AFT LOWER FRAME.
- [SDR 2008UALA02553](https://openairdocs.org/sdr/2008UALA02553), May 1, 2008: DOOR FRAME. CRACKED. FWD GALLEY DOOR AFT FRAME CRACKED AT INBOARD SIDE OF 3RD STOP FITTING FROM THE TOP. MAJOR REPAIR ACCOMPLISHED, INSTALLED REPAIR DOUBLER.
- [SDR 2008UALA02552](https://openairdocs.org/sdr/2008UALA02552), May 1, 2008: DOOR FRAME. CRACKED. FWD GALLEY DOOR FWD LOWER FRAME IS CRACKED AT THREE FASTENER HOLES UNDER STOP FITTING. MAJOR REPAIR ACCOMPLISHED, REMOVED DAMAGED SECTION. INSTALLED FRAME REPAI
- [SDR 2008UALA02551](https://openairdocs.org/sdr/2008UALA02551), May 1, 2008: WEB. GOUGED. FWD GALLEY DOOR INTERIOR SIDE OF UPPER HINGE SUPPORT WEB GOUGED AT GUIDE ARM BOLT COVER PLATE. MAJOR REPAIR ACCOMPLISHED, REPLACED SUPPORT WEB.
- [SDR 2008UALA02550](https://openairdocs.org/sdr/2008UALA02550), May 1, 2008: ANGLE. CRACKED. FWD GALLEY DOOR INTERIOR WINDOW BAY SUPPORT ANGLE FOR MECHANISM BOX IS CRACKED. MAJOR REPAIR ACCOMPLISHED, REPLACED SUPPORT ANGLE.
- [SDR 2008UALA02549](https://openairdocs.org/sdr/2008UALA02549), May 1, 2008: DOOR FRAME. CRACKED. FWD GALLEY DOOR LOWER AFT FRAME CRACKED UNDER STOP FITTING. MAJOR REPAIR ACCOMPLISHED, REPLACED AFT LWR FRAME.
- [SDR 2008UALA02493](https://openairdocs.org/sdr/2008UALA02493), Apr 28, 2008: SPLICE PLATE. DAMAGED. FWD CARGO DOOR CUTOUT, FWD UPPER INNER CORNER, TOMAHAWK SPLICE SUPPORT PLATE HAS 20 ELONGATED HOLES, THIS PLATE TIES STR 18R INNER CHORD WITH THE BS 440 FRAME I
- [SDR 2008UALA02453](https://openairdocs.org/sdr/2008UALA02453), Apr 27, 2008: DOOR FRAME. CRACKED. FWD GALLEY DOOR AFT FRAME CRACKED AT INBD SIDE OF OPENING FOR STOP FITTING, 3RD FROM BOTTOM. BLENDED DAMAGE FROM FRAME AND ACCMP'D NDT. FABRICATED AND INSTALLED
- [SDR 2008UALA02441](https://openairdocs.org/sdr/2008UALA02441), Apr 25, 2008: SKIN. DENTED. UPPER LT FUSELAGE SKIN HAS SHARP DENT BS 386 STR 16L. REMOVED AND REPLACED DAMAGE. VERIFIED DAMAGE REMOVAL WITH HFEC. INSTALLED REPAIR DOUBLER, TRIPLER AND FILL
- [SDR 2008UALA02440](https://openairdocs.org/sdr/2008UALA02440), Apr 25, 2008: INTERCOSTAL. DAMAGED. AFT CARGO BAY BETWEEN BS 847 AND 867 AN INTERCOSTAL WAS BLENDED BEYOND LIMITS AT S26R. MAJOR REPAIR ACCOMPLISHED, REPLACED THE INTERCOSTAL.
- [SDR 2008UALA02421](https://openairdocs.org/sdr/2008UALA02421), Apr 24, 2008: CREASE BEAM. CORRODED. AFT GALLEY DOOR INNER CREASE BEAM UPPER SURFACE CORRODED AT STA 947-986. MAJOR REPAIR ACCOMPLISHED: INSTALLED NEW CREASE BEAM.
- [SDR 2008UALA02420](https://openairdocs.org/sdr/2008UALA02420), Apr 24, 2008: FLOORBEAM. CORRODED. AFT FLOORBEAM CORRODED AT FLOOR BOARD HOLES STA 986.5 RBL 20-32 UPPER AND LOWER SURFACE. MAJOR REPAIR ACCOMPLISHED: FABRICATED & INSTALLED FLOORBEAM UPPER TEE C
- [SDR 2008UALA02346](https://openairdocs.org/sdr/2008UALA02346), Apr 21, 2008: SKIN. DAMAGED. AFT GALLEY DOOR, LOWER INNER SKIN HAS EVIDENCE OF DAMAGE CUTOUT AND NO REINFORCEMENT REPAIR. MAJOR REPAIR ACCOMPLISHED, FABRICATED AND INSTALLED INNER SKIN EXTE
- [SDR 2008UALA02289](https://openairdocs.org/sdr/2008UALA02289), Apr 18, 2008: SKIN. DAMAGED. UPPER RT FUSELAGE SKIN BS 420 STR 6R, EXISTING REPAIR DOUBLER HAS DEGRADED SEALANT CAUSING PRESS LEAK. MAJOR REPAIR ACCOMPLISHED, REPLACED THE REPAIR WITH A DOU
- [SDR 2008UALA02288](https://openairdocs.org/sdr/2008UALA02288), Apr 18, 2008: SKIN. DENTED. UPPER LT FUSELAGE SKIN HAS DENT BS 384 1 INCH ABOVE STR 15L. MAJOR REPAIR ACCOMPLISHED, REMOVED THE DAMAGE. VERIFIED DAMAGE REMOVAL WITH HFEC. INSTALLED REPAIR 
- [SDR 2008UALA02287](https://openairdocs.org/sdr/2008UALA02287), Apr 18, 2008: WEB. CRACKED. FUSELAGE HORIZ WEB HAS CRACK, BS 188-196.5 AT FLOOR LEVEL LT SIDE EMANATING FROM AFT INBD CUTOUT AND PROMINATING FROM AFT INBD CUTOUT. MAJOR REPAIR ACCOMPLISHED
- [SDR 2008UALA02115](https://openairdocs.org/sdr/2008UALA02115), Apr 10, 2008: FRAME. DAMAGED. RT FUSELAGE FRAME BS 440 HAS MISDRILLED HOLES AT STR'S 14-15-16. MAJOR REPAIR ACCOMPLISHED: REPLACED FWD FRAME.
- [SDR 2008UALA02114](https://openairdocs.org/sdr/2008UALA02114), Apr 10, 2008: INTERCOSTAL. CRACKED. FWD ENTRY DOOR FUSELAGE CUTOUT, S7L INTERCOSTAL CRACKED IN RADIUS FWD END ON THE AFT SIDE OF FRAME AT BS 294.5. MAJOR REPAIR ACCOMPLISHED: REPLACED INTERCOSTAL 
- [SDR 2008UALA02113](https://openairdocs.org/sdr/2008UALA02113), Apr 10, 2008: INTERCOSTAL. CRACKED. FWD ENTRY DOOR FUSELAGE CUTOUT, STRINGER 9L INTERCOSTAL CRACKED IN UPPER RADIUS FWD END ON THE AFT SIDE OF FRAME BS 294.5. MAJOR REPAIR ACCOMPLISHED: REPLACED I
- [SDR 2008UALA02112](https://openairdocs.org/sdr/2008UALA02112), Apr 10, 2008: CREASE BEAM. CORRODED. AFT GALLEY DOOR INNER CREASE BEAM UPPER SURFACE CORRODED AT STA 947-986. MAJOR REPAIR ACCOMPLISHED: INSTALLED NEW CREASE BEAM.
- [SDR 2008UALA02111](https://openairdocs.org/sdr/2008UALA02111), Apr 10, 2008: ATTACH FITTING. CRACKED. FWD ENTRY DOOR FUSELAGE CUTOUT AT BS 294.5 UPPER INTERCOSTAL CLIP CRACKED IN RADIUS STRINGER 11L. MAJOR REPAIR ACCOMPLISHED: REPLACED THE CLIP.
- [SDR 2008UALA02110](https://openairdocs.org/sdr/2008UALA02110), Apr 10, 2008: ANGLE. CRACKED. FWD ENTRY DOOR FUSELAGE CUTOUT BS 294.5 L-ANGLE CRACKED AT AFT END BELOW THE RADIUS AT S10L. MAJOR REPAIR ACCOMPLISHED: REPLACED I-B 'H' STRAP, AUX INTERCOSTAL 
- [SDR 2008UALA02109](https://openairdocs.org/sdr/2008UALA02109), Apr 10, 2008: FLOORBEAM. CORRODED. AFT FLOORBEAM CORRODED AT FLOOR BOARD HOLES STA 986.5 RBL 20-32 UPPER AND LOWER SURFACE. MAJOR REPAIR ACCOMPLISHED: FABRICATED & INSTALLED FLOORBEAM UPPER "T" C
- [SDR 2008UALA02108](https://openairdocs.org/sdr/2008UALA02108), Apr 10, 2008: CREASE BEAM. CORRODED. AFT ENTRY DOOR INNER CREASE BEAM UPPER SURFACE CORRODED AT STA 952-986. MAJOR REPAIR ACCOMPLISHED: INSTALLED NEW CREASE BEAM.
- [SDR 2008UALA02107](https://openairdocs.org/sdr/2008UALA02107), Apr 10, 2008: SKIN. DAMAGED. UPPER RT FUSELAGE SKIN BS 420 STR 6R, EXISTING REPAIR DOUBLER HAS DEGRADED SEALANT CAUSING PRESSURE LEAK. MAJOR REPAIR ACCOMPLISHED: REPLACED THE REPAIR WITH DO
- [SDR 2008UALA02106](https://openairdocs.org/sdr/2008UALA02106), Apr 10, 2008: SKIN. GOUGED. UPPER FUSELAGE CROWN SKIN HAS DEEP GOUGE BS 288 STR 2L. MAJOR REPAIR ACCOMPLISHED: FABRICATED AND INSTALLED EXTERNAL FUSELAGE SKIN DOUBLER-TRIPLER REPAIR.
- [SDR 2008UALA02105](https://openairdocs.org/sdr/2008UALA02105), Apr 10, 2008: SKIN. DENTED. UPPER LT FUSELAGE SKIN HAS SHARP DENT BS 386 STR 16L. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGE AND VERIFIED DAMAGE REMOVAL WITH HFEC. INSTALLED REPAIR DOUBLER,
- [SDR 2008UALA02104](https://openairdocs.org/sdr/2008UALA02104), Apr 10, 2008: SKIN. DENTED. UPPER LT FUSELAGE SKIN HAS DENT BS 384 1" ABOVE STR 15L. MAJOR REPAIR ACCOMPLISHED: RMV'D THE DAMAGE. VERIFIED DAMAGE RMVL WITH HFEC. INSTALLED REPAIR DOUBLER, 
- [SDR 2008UALA02103](https://openairdocs.org/sdr/2008UALA02103), Apr 10, 2008: STRAP. CRACKED. 'H' STRAP AT STR 13L HINGE LOCATION BTWN BS 294-303, STRINGER SPLICE CHANNEL CRACKED AT AFT EDGE. MAJOR REPAIR ACCOMPLISHED: REPLACED THE INBD 'H' STRAP, INTERC
- [SDR 2008UALA02102](https://openairdocs.org/sdr/2008UALA02102), Apr 10, 2008: FLOORBEAM. CRACKED. CABIN LONGITUDINAL FLOORBEAM HAS A CRACK AT LIGHTENING HOLE JUST BELOW SEAT TRACK, RBL 25" BS 669. MAJOR REPAIR ACCOMPLISHED: STOP DRILLED CRACK & VERIFIED CRAC
- [SDR 2008UALA02101](https://openairdocs.org/sdr/2008UALA02101), Apr 10, 2008: FLOORBEAM. CRACKED. CABIN LONGITUDINAL FLOORBEAM HAS A CRACK AT LIGHTENING HOLE JUST BELOW SEAT TRACK, LBL 25" BS 665. MAJOR REPAIR ACCOMPLISHED: STOP DRILLED THE CRACKS AND VERIFI
- [SDR 2008UALA02099](https://openairdocs.org/sdr/2008UALA02099), Apr 10, 2008: PRESSURE PANEL. CRACKED. CABIN WING BOX UPPER PRESS DECK IS CRACKED BS 664 LBL 31". FABRICATED & INSTALLED REPAIR DOUBLER ON UPPER SURFACE OF PRESSURE DECK REF MM53-21-98 PG 801 & SRM51
- [SDR 2008UALA02098](https://openairdocs.org/sdr/2008UALA02098), Apr 10, 2008: SKIN. GOUGED. UPPER FUSELAGE CROWN SKIN GOUGED AT BS 284 STR 4L. MAJOR REPAIR ACCOMPLISHED: INSTALLED REPAIR DOUBLER/TRIPLER REPAIR.
- [SDR 2008UALA02097](https://openairdocs.org/sdr/2008UALA02097), Apr 10, 2008: SKIN. CRACKED. FWD ENTRY DOOR, INNER SKIN AND FRAME CRACKED AT AFT SIDE STOP PIN JUST BELOW CENTERING FITTING. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGE & INSTALLED REPAIR DOU
- [SDR 2008UALA02096](https://openairdocs.org/sdr/2008UALA02096), Apr 10, 2008: DOOR FRAME. CRACKED. FWD ENTRY DOOR, LOWER FWD FRAME CRACKED NEAR INNER RADIUS. MAJOR REPAIR ACCOMPLISHED: CUTOUT DAMAGE & INSTALLED EXTERNAL FRAME DOUBLER REPAIR. 
- [SDR 2008UALA02095](https://openairdocs.org/sdr/2008UALA02095), Apr 10, 2008: FRAME. CRACKED. BS 616 LT OVERWING FRAME IS CRACKED AT INNER CHORD. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGE AND VERIFIED REMOVAL WITH HFEC. INSTALLED REPAIR ANGLE AND FILLER.
- [SDR 2008UALA02094](https://openairdocs.org/sdr/2008UALA02094), Apr 10, 2008: SKIN. CRACKED. FWD ENTRY DOOR LOWER HINGE CUTOUT HAS 2 CRACK INDICATIONS AT FASTENER HOLES AT FWD END OF CUTOUT. MAJOR REPAIR ACCOMPLISHED, CUTOUT THE DAMAGES COMMON THE THE B

All 83: https://openairdocs.org/aircraft/N398UA/unmatched-reports.md

## STCs that may be installed (OpenAirDocs) (17)

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 (Costruzioni Aeronautiche Tecna P2006T)

- [STC SA02571SE](https://openairdocs.org/stc/SA02571SE): Installation of Garmin G500/G600 TXi Integrated Avionics System (Primary Flight Display, Multi-Function Display, and Engine Indicating System Display). Garmin International Inc
- [STC SA02636SE](https://openairdocs.org/stc/SA02636SE): Installation of Garmin GPS 175 Navigation System and GNX 375 Navigation System with ADS-B In/Out Transponder. Garmin International Inc
- [STC SA02019SE-D](https://openairdocs.org/stc/SA02019SE-D): Installation of Garmin Model GTN 625/635/650; 725/750 Navigation System. Garmin International Inc
- [STC SA02511SE](https://openairdocs.org/stc/SA02511SE): Installation of replacement fuel quantity indicator sending unit(s). CiES Inc
- [STC SA04046CH PAGE 1](https://openairdocs.org/stc/SA04046CH%20PAGE%201): Installation of L-3 GENESIS (TM) Electronic Standby Instrument System (ESI-500/MAG-500). Acron Aviation Inc
- [STC SA02658SE](https://openairdocs.org/stc/SA02658SE): Installation of Garmin GI 275 Multi-Function Display System. Garmin International Inc
- [STC SA02444AK](https://openairdocs.org/stc/SA02444AK): Approval of the L-3 Communications NGT 9000/9000R ADS-B system installed. ADS-B Technologies LLC
- [STC SA00198MC](https://openairdocs.org/stc/SA00198MC): Installation of mission equipment, to include operator console, RADAR, radome, equipment rack and various antenna. Spec Ops Technology LLC
- [STC SA01714WI](https://openairdocs.org/stc/SA01714WI): Installation of a Garmin transponders: (a) GTX 330/330D/33/33D with ADS-B Out functionality; (b) GTX 335/335R/345/345R with ADS-B Out and In functionality; or (c) GTX 335R/345R with ADS-B Out functionality in select airplanes installed with G950/G1000 systems. Garmin International Inc
- [STC SA02153LA-D PAGE 1](https://openairdocs.org/stc/SA02153LA-D%20PAGE%201): Installation of Garmin G600 Primary Flight Display (PFD) and Multifunction Display (MFD) System. Garmin International Inc
- [STC SA02493AK](https://openairdocs.org/stc/SA02493AK): Installation of airborne surveillance Multi Mission Platform (MMP). Borsight, Inc
- [STC SA04063NY](https://openairdocs.org/stc/SA04063NY): Installation of the mission system Leica City Mapper (Sensor Unit and its respective server, cockpit display and operator stand and display). S4A Solutions For Aviation, S.L
- [STC SA02119SE PAGE 1](https://openairdocs.org/stc/SA02119SE%20PAGE%201): Installation of Garmin GDL 88 ADS-B UAT Transceiver System. Garmin International Inc
- [STC SA02442AK PAGE 1](https://openairdocs.org/stc/SA02442AK%20PAGE%201): Approval of the L-3 Communications NGT 2000/2500 ADS-B system. ADS-B Technologies, LLC
- [STC SA02121SE](https://openairdocs.org/stc/SA02121SE): Installation of Garmin GTS 825 (TAS) or GTS 855 (TCAS I) Traffic System. Garmin International Inc
- [STC SA02153LA-D](https://openairdocs.org/stc/SA02153LA-D) (historical): Installation of Garmin G600 Primary Flight Display (PFD) and Multifunction Display (MFD) System. Garmin International Inc

### Approved for the engine (Rotax 912S3)

- [STC SE01966WI](https://openairdocs.org/stc/SE01966WI): Use of GAMI G100UL High Octane Unleaded Avgas in spark ignition piston aircraft engines. General Aviation Modifications Inc

## Related

- Other Costruzioni Aeronautiche Tecna P2006T aircraft: https://openairdocs.org/model/costruzioni-aeronautiche-tecna-p2006t/aircraft.md
- The Rotax 912S3 engine: https://openairdocs.org/engine/rotax-912s3.md

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