# N762BC: 2021 Raymond M Steele RAINBOW SKYREACH PTY

- Status: Valid registration
- Airframe: [Raymond M Steele RAINBOW SKYREACH PTY](https://openairdocs.org/model/raymond-m-steele-rainbow-skyreach-pty) (registry code 05640AE, 2 seats)
- Engine: [Rotax 912ULS series](https://openairdocs.org/engine/rotax-912uls-series) (registry code 55572)
- Serial number: CH247C
- Year built: 2021
- Type: Fixed wing single engine
- Engine type: Reciprocating
- Kit: Aerosport LLC SKYREACH BUSHCAT
- Airworthiness: Experimental, amateur built
- Airworthiness date: October 7, 2021
- Certificate issued: May 17, 2021
- Expires: May 31, 2028
- Mode S code: AA4912
- Registered owner: [Steele Raymond M](https://openairdocs.org/faa-owner/STEELE%20RAYMOND%20M)
- Location: [Allison Park, PA](https://openairdocs.org/faa-place/PA/Allison%20Park)
- Owner type: Individual
- Owner's area on the map: 40.5752° N, 79.9563° W: Placed by OpenAirDocs at the center of ZIP code 15101, 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=762BC
- Page: https://openairdocs.org/aircraft/N762BC

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. The registry lists only the engine series, so ADs for every Rotax 912ULS model are included.

## ADs that may apply (OpenAirDocs): 0 in force

### Matched by airframe (Raymond M Steele RAINBOW SKYREACH PTY)

None in force.

### Matched by engine (Rotax 912ULS series)

None in force.

## Information bulletins (advisory)

None matched.

## NTSB investigations

None matched to N762BC.

## FAA accident and incident reports

None matched to N762BC.

## 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 N762BC not matched to an aircraft (58, newest 50)

They name N762BC, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR DALA2016050103624](https://openairdocs.org/sdr/DALA2016050103624), Apr 29, 2016: INTERCOSTAL. CORRODED. CORROSION ON AFT CARGO, RT INTERCOSTAL UPPER ANGLE BETWEEN BS 1280-1300 BELOW OTBD SIDE OF TRANSITION PANEL. R & R 1 EA INTERCOSTAL WEB AND 1EA UPPER ANGLE IAW 
- [SDR DALA2016050103623](https://openairdocs.org/sdr/DALA2016050103623), Apr 29, 2016: INTERCOSTAL. CORRODED. LEFT BS 820-840 UPON REMOVEL OF TRANSITION PANEL. INTERCOSTAL HAS CORROSION ON LOWER FLANGE THAT ATTACHES TO SKIN. LOCATED BETWEEN LT STR 27 AND LT STR 28. FOUN
- [SDR DALA2016050203602](https://openairdocs.org/sdr/DALA2016050203602), Apr 29, 2016: SUPPORT. CORRODED. LOWER WTB FAIRING SUPPORT FS 900/LBL 14-RBL 24; T EXTRUSION AND SPLICE ANGLES ON FWD AND AFT SIDES CORRODED. BLENDED AND FOUND TO BE OUT OF LIMITS. ACCOMPLISHED
- [SDR DALA2016042903598](https://openairdocs.org/sdr/DALA2016042903598), Apr 28, 2016: SLIDE. DAMAGED. L1 DOOR SLIDE PACKBOARD FWD BLADE SLOT TORN AT INBD SIDE. ESCAPE SLIDE L-1 DOOR TO BE INSTALLED ON TASK-CARD.
- [SDR DALA2016042703537](https://openairdocs.org/sdr/DALA2016042703537), Apr 26, 2016: SLIDE. DAMAGED. R2 DOOR ESCAPE SLIDE DAMAGED AT UPPER RT CORNER. PROCURED FROM STOCK R-2 DOOR ESCAPE SLIDE O/H TO BE INSTALLED ON TASK CARD.
- [SDR DALA2016042703536](https://openairdocs.org/sdr/DALA2016042703536), Apr 26, 2016: TORQUE SHAFT. CORRODED. VERTICAL STABILIZER, LT SYS RUDDER PCU BELLCRANK TORQUE SHAFT HAS SURFACE CORROSION. ASSY LT SYS RUDDER PCU AREA IAW AMM 20-11, SRM AND AMM 27-21 OPS CHECK GOOD
- [SDR DALA2016042703531](https://openairdocs.org/sdr/DALA2016042703531), Apr 26, 2016: FLOORBEAM. DAMAGED. TOILET FLUSH LINE BRACKET RIVET HAS ELONGATED HOLE AND TOOLING DAMAGE ON MAIN CABIN FLOORBEAM WEB AT BS 310.5, LBL 53. ACCOMPLISHED PERMANENT REPAIR FOR TOOLING
- [SDR DALA2016042703527](https://openairdocs.org/sdr/DALA2016042703527), Apr 26, 2016: FLOOR SUPPORT. CORRODED. CORROSION UNDER 1 EA NUTPLATE IN AFT CARGO UPPER FLOOR SUPPORT AT BS 1450 RBL-13. ACCOMPLISHED AFT CARGO UPPER FLOOR SUPPORT AT BS 1450, RBL 13 BY REPLACEMENT I
- [SDR DALA2016042703526](https://openairdocs.org/sdr/DALA2016042703526), Apr 26, 2016: FRAME. DENTED. DENT ON AFT CARGO LT FRAME UPPER FLANGE AT BS 1360 ABOVE STR 26L. EVALUATED DENT AND FOUND OUT OF LIMITS IAW SRM. FABRICATED AND INSTALLED REPAIR IAW SRM.
- [SDR DALA2016042703528](https://openairdocs.org/sdr/DALA2016042703528), Apr 25, 2016: FLOOR SUPPORT. CORRODED. CORROSION ON AFT CARGO BILGE FLOOR SUPPORT LOWER FLANGE BETWEEN BS 1460-1480, RBL-13. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. REPLACEMENT IAW SRM.
- [SDR DALA2016042603368](https://openairdocs.org/sdr/DALA2016042603368), Apr 25, 2016: BEARING. CORRODED. RT WING OTBD, MAIN FLAP OTBD BALL SCREW GIMBAL UPPER PIVOT BEARING AND IMMEDIATE AREA SHOWING RUST. PROCURED PART. INSTALLATION AND OP'S CHECK ACCOMPLISHED ON T
- [SDR DALA2016042503364](https://openairdocs.org/sdr/DALA2016042503364), Apr 22, 2016: INTERCOSTAL. CORRODED. CORROSION ON AFT CARGO INTERCOSTAL ON OTBD SIDE OF WEB, LOWER FLANGE AND UPPER ANGLE BETWEEN BS 1360-1380 BELOW OTBD SIDE OFTRANSITION PANEL ACP 0600-156-01Z. R
- [SDR DALA2016042303362](https://openairdocs.org/sdr/DALA2016042303362), Apr 22, 2016: FRAME. DENTED. THREE DENTS ON AFT CARGO LT FRAME AT BS 1320 BETWEEN STR 25-26L. TRIMMED-OUT DENTS IAW SRM 53-00-07, FIG 201 REPAIR 5. ACCOMPLISHED PERMANENT REPAIR IAW SRM 53-
- [SDR DALA2016042203258](https://openairdocs.org/sdr/DALA2016042203258), Apr 21, 2016: FRAME. GOUGED. MAIN CABIN RT SIDE BS 1280 FRAME HAS 2 EA GOUGE MARKS. ACCOMPLISHED PERMANENT REPAIR ON MAIN CABIN RT SIDE BS 1280 FRAME STR 9R TO STR 14R IAW ER/A 544719-14AD 
- [SDR DALA2016042203257](https://openairdocs.org/sdr/DALA2016042203257), Apr 20, 2016: HINGE. CORRODED. CASTING FOR MLG DOOR AFT HINGE HAS SEVERAL CORROSION PITS. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. R & R KEELBEAM SUPPORT CASTING REF DWG & SRM.
- [SDR DALA2016042103254](https://openairdocs.org/sdr/DALA2016042103254), Apr 20, 2016: FRAME. DENTED. FWD CARGO COMPARTMENT LT SIDE FRAME BS 680 HAS 2 EA DENTS BETWEEN STR 23L AND 25L. TRIMMED OUT AND ACCOMPLISHED PERMANENT REPAIR REF SRM.
- [SDR DALA2016042203319](https://openairdocs.org/sdr/DALA2016042203319), Apr 19, 2016: FRAME. DENTED. FWD CARGO COMPARTMENT LT SIDE FRAME BS 580 HAS TWO DENTS BETWEEN STR 23L AND 25L. EVALUATED DAMAGE, FABRICATED AND INSTALLED. REPAIR IAW SRM.
- [SDR DALA2016042003152](https://openairdocs.org/sdr/DALA2016042003152), Apr 19, 2016: GIRT BAR. WORN. R-4 DOOR GIRT BAR ACTUATION SYS HAS GIRT BAR LIFTER BUSHINGS WORN FWD AND AFT CAM LIFTER BUSHINGS WORN. FWD AND AFT REMOVED AND INSTALLED R4 DOOR GIRT BAR ACTUA
- [SDR DALA2016042203259](https://openairdocs.org/sdr/DALA2016042203259), Apr 18, 2016: FLOOR SUPPORT. CORRODED. CORROSION ON AFT CARGO BILGE INTERCOSTAL OTBD LOWER FLANGE BETWEEN BS 1320-1340, RBL-10.5. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. R & R INTERCOSTAL AN
- [SDR DALA2016042003151](https://openairdocs.org/sdr/DALA2016042003151), Apr 17, 2016: INTERCOSTAL. CORRODED. CORROSION ON AFT CARGO BILGE INTERCOSTAL ON BOTH SIDES OF WEBAND ON LOWER FLANGE BETWEEN BS 1520-1540, RBL-3. REMOVED AFT CARGO BILGE INTERCOSTAL ON BS 1520-154
- [SDR DALA2016042003173](https://openairdocs.org/sdr/DALA2016042003173), Apr 16, 2016: INTERCOSTAL. CORRODED. CORROSION ON AFT CARGO BILGE INTERCOSTAL LOWER FLANGE BETWEEN STR 1300-1320, RBL-17. REMOVED CORROSION BLEND OUT FOUND TO BE OUT OF LIMITS IAW SRM 53-00-04 ALLO
- [SDR DALA2016042003172](https://openairdocs.org/sdr/DALA2016042003172), Apr 16, 2016: INTERCOSTAL. CORRODED. CORROSION ON AFT CARGO BILGE INTERCOSTAL LOWER FLANGE BETWEEN BS 1300-1320 LBL-17. REMOVED CORROSION IAW SRM 53-00-04, FIG 101 AD 1, PG 103. FOUND TO BE OUT OF 
- [SDR DALA2016041703006](https://openairdocs.org/sdr/DALA2016041703006), Apr 16, 2016: HINGE. CORRODED. SUPPORT CASTING FOR MLG DOOR CENTER HINGE HAS CORROSION ON FWD SIDE LOWER FLANGE, AND AFT SIDE TOP OF MID FLANGE. REMOVED CORROSION AND FOUND TO BE OUT OF LIMIT
- [SDR DALA2016041703005](https://openairdocs.org/sdr/DALA2016041703005), Apr 16, 2016: FRAME. DENTED. FWD CARGO COMPARTMENT L/T SIDE FRAME BD 620 HAS ONE DENT, STR 23L. TRIMMED OUT DAMAGE, ACCOMPLISHED PERMANENT REPAIR IAW SRM.
- [SDR DALA2016041603001](https://openairdocs.org/sdr/DALA2016041603001), Apr 14, 2016: HINGE. CORRODED. CASTING CORRODED TOP AND BOTTOM OF FLANGE. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. R & R MLG DOOR FWD HINGE AT KEEL BS 1072 LBL6-RBL6 IAW SRM.
- [SDR DALA2016041502947](https://openairdocs.org/sdr/DALA2016041502947), Apr 14, 2016: STIFFENER. CORRODED. CORROSION ON BULKHEAD STIFFENER LOWER SIDE BS 900 LBL 8. REMOVED CORROSION ON STIFFENER AT LOWER SIDE STA 900, LBL 7.5. ORIGINAL THICKNESS IS .180", MATERIAL LO
- [SDR DALA2016041502946](https://openairdocs.org/sdr/DALA2016041502946), Apr 14, 2016: STIFFENER. CORRODED. CORROSION ON BULKHEAD STIFFENER LOWER SIDE BS 900, RBL 10. REMOVED CORROSION ON STIFFENER AT LOWER SIDE BS 900, RBL 7.5 ORIGINAL THICKNESS IS .180", MATERIAL LO
- [SDR DALA2016042703379](https://openairdocs.org/sdr/DALA2016042703379), Apr 13, 2016: CASE. CORRODED. RUDDER TRIM ACTUATOR CASE HARDWARE BADLY RUSTED. R & R VERTICAL STABILIZER RUDDER TRIM ACTUATOR IAW AMM 27-21. OPS CK GOOD.
- [SDR DALA2016041402944](https://openairdocs.org/sdr/DALA2016041402944), Apr 13, 2016: FRAME. DENTED. DENT ON AFT CARGO, LT FRAME UPPER FLANGE AT BS 1340 ABOVE STR 26L. TRIMMED-OUT 1 EA DENT ON FRAME UPPER FLANGE AT BS 1340, ABOVE STR 26L REF SRM 53-00-07, REPAI
- [SDR DALA2016041402942](https://openairdocs.org/sdr/DALA2016041402942), Apr 13, 2016: FRAME. DENTED. FWD CARGO COMPARTMENT RT SIDE FRAME BS 700 HAS 2 EA DENTS STR 23R TO STR 24R. TRIMMED-OUT 2 EA DENTS ON FRAME AT BS 700, STR 23R-STR 24R REF SRM 53-00-07, REPAI
- [SDR DALA2016041502945](https://openairdocs.org/sdr/DALA2016041502945), Apr 12, 2016: KEELBEAM. CORRODED. KEELBEAM BS 1060-1072 LBL5 AND FASTENERS CORRODED AT SEVERAL SPOTS. R & R NEW FASTENERS AND STIFFENERS, PN 70016533830001, BS 1060-1072, LBL5-RBL5 IAW DWG 149N8
- [SDR DALA2016043003600](https://openairdocs.org/sdr/DALA2016043003600), Apr 11, 2016: INTERCOSTAL. CORRODED. CORROSION ON AFT CARGO BILGE INTERCOSTAL ON INBD LOWER FLANGE AND OTBD FWD CHANNEL BETWEEN BS 1500-1520, LBL-2.9. REMOVED CORROSION AND FOUND TO BE OUT OF LIMIT
- [SDR DALA2016041302917](https://openairdocs.org/sdr/DALA2016041302917), Apr 11, 2016: SKIN. CORRODED. AFT FUSELAGE TAIL COMPARTMENT, BS 1883-1885, LBL10-RBL10, SKIN AND FASTENERS CORRODED. REMOVED SKIN STRAP AFT LOWER BS 1885, STR 25L TO 25R. ORIG MATERIAL THICK
- [SDR DALA2016041002778](https://openairdocs.org/sdr/DALA2016041002778), Apr 9, 2016: ANGLE. CORRODED. CORROSION ON AFT CARGO LT INTERCOSTAL UPPER ANGLE BETWEEN BS 1480-1500, LBL 24.5 UNDER OTBD SIDE OF TRANSITION PANEL. REMOVED CORROSION ON AFT CARGO LT INTERCOS
- [SDR DALA2016042003150](https://openairdocs.org/sdr/DALA2016042003150), Apr 8, 2016: INTERCOSTAL. CORRODED. CORROSION ON AFT CARGO BILGE INTERCOSTAL LOWER FLANGE BETWEEN BS 1300-1320, LBL-3. REMOVED CORROSION AT INTERCOSTAL LOWER FLANGE BETWEEN BS 1300-1320, LBL3. ORI
- [SDR DALA2016040802776](https://openairdocs.org/sdr/DALA2016040802776), Apr 7, 2016: CREASE BEAM. CORRODED. UPON REMOVAL OF FLOORBOARD 230-41 IAW JIC 2020-2376 MAIN CABIN LT CREASE BEAM INBD CHORD CORRODED IN MULTIPLE SPOTS BETWEEN BS 800 AND BS 880. COMPLIED WITH ERA
- [SDR DALA2016040802773](https://openairdocs.org/sdr/DALA2016040802773), Apr 7, 2016: FLOORBEAM. CORRODED. CORROSION ON FLOORBEAM LOWER CHORD BS 310, LBL 51 TO LBL 60. COMPLIED WITH ERA 544723-14, REV ORIGINAL.
- [SDR DALA2016040802728](https://openairdocs.org/sdr/DALA2016040802728), Apr 7, 2016: FLOORBEAM. CORRODED. CORROSION ON FLOORBEAM UPPER TEE BS 310, LBL 17 TO LBL 21. COMPLIED WITH ERA 544722-14, REV ORIGINAL ON FUSELAGE FLOOR BEAM UPPER TEE AT BS 310.5, LBL 17-LBL 21
- [SDR DALA2016040502666](https://openairdocs.org/sdr/DALA2016040502666), Apr 4, 2016: SEAT TRACK. CORRODED. CORROSION ON MAIN CABIN SEAT TRACK BS 1320-1350, RBL 24. BLENDED AND FOUND TO BE OUT OF LIMITS. ACCOMPLISHED PERMANENT REPAIR IAW SRM.
- [SDR DALA2016040802774](https://openairdocs.org/sdr/DALA2016040802774), Apr 2, 2016: INTERCOSTAL. CORRODED. CORROSION ON AFT CARGO LT INTERCOSTAL UPPER ANGLE BETWEEN BS 1200 - 1220, LBL 24.5 JUST BELOW OTBD SIDE OF LT TRANSITION PANEL. REMOVED UPPER ANGLE IAW SRM 51-4
- [SDR DALA2016040402561](https://openairdocs.org/sdr/DALA2016040402561), Apr 1, 2016: SKIN. DENTED. LEFT INBD MAIN FLAP UPPER OTBD PANEL HAS CHAFE DAMAGE 0-36" FROM THE OTBD END. ACCOMPLISHED REPAIR, DAMAGE DIMENSION IS APPROXIMATELY 1" X 11" OF THE DISCREPANT
- [SDR DALA2016040402560](https://openairdocs.org/sdr/DALA2016040402560), Apr 1, 2016: SKIN. DENTED. LT WING INBD MAIN FLAP UPPER SURFACE HAS 2 GOUGED DENTS 53" FROM INBD END/ 19"-22" FROM T/E. ACCOMPLISHED PERMANENT REPAIR ON LT WING INBD MAIN FLAP UPPER SURFA
- [SDR DALA2016040102550](https://openairdocs.org/sdr/DALA2016040102550), Mar 31, 2016: SKIN. DAMAGED. RT WING INBD MAIN FLAP UPPER SKIN HAS 2 EA CREASES 47"-49" FROM INBD END/ 18.5"-22.5" FROM T/E. ON RT WING INBD MAIN FLAP UPPER SKIN REPAIRED 2 EA CREASES 47"-4
- [SDR DALA2016040102549](https://openairdocs.org/sdr/DALA2016040102549), Mar 31, 2016: SKIN. DENTED. LEFT WING INBD MAIN FLAP T/E WEDGE LOWER SKIN DENTED 63.5"-77" FROM OTBD END. ACCOMPLISHED REPAIR OT THE DISCREPANT AREA ON THE UPPER SURFACE, APPROX 1" X 10" A
- [SDR DALA2016033102548](https://openairdocs.org/sdr/DALA2016033102548), Mar 28, 2016: SEAT TRACK. CORRODED. CORROSION ON MAIN CABIN SEAT TRACK SUPPORT BS 1640, RBL 45. R & R NEW SEAT TRACK SUPPORT BETWEEN BS 1600-BS 1640, RBL 45 IAW DWG 146N5120.
- [SDR DALA2016032802349](https://openairdocs.org/sdr/DALA2016032802349), Mar 24, 2016: SKIN. DENTED. RIGHT WING INBD MAIN FLAP T/E WEDGE LOWER SKIN DENTED 63.5 - 77" FROM OTBD END. ACCOMPLISHED REPAIR OF THE DISCREPANT AREA ON RT WING INBD MAINFLAP T/E WEDGE LO
- [SDR DALA2016042903596](https://openairdocs.org/sdr/DALA2016042903596), Mar 23, 2016: STRAP. CORRODED. CORROSION MAIN CABIN FLOOR STABILIZER STRAP, BS 740, LBL 26. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. FABRICATED REPAIR AND INSTALLED IAW SRM.
- [SDR DALA2016032502343](https://openairdocs.org/sdr/DALA2016032502343), Mar 23, 2016: SEAT TRACK. GOUGED. MAIN CABIN SEAT TRACK CROWN LBL 45 AT BS 1545 HAS A DEEP GOUGED. BLENDED GOUGED ON MAIN CABIN SEAT TRACK CROWN AT BS 1545, LBL 45. MATERIAL LOSS OF 0.033", FOUN
- [SDR DALA2016040502668](https://openairdocs.org/sdr/DALA2016040502668), Mar 22, 2016: STRAP. CRACKED. MAIN CABIN FLOOR STRUCTURE STABILIZER STRAP LBL 45, BS 365 CRACKED. REMOVED AND INSTALLED NEW SECCION OF STABILIZER STRAP AT MAIN CABIN FLOOR STRUCTURE STABILIZ
- [SDR DALA2016040502667](https://openairdocs.org/sdr/DALA2016040502667), Mar 22, 2016: STRAP. CRACKED. MAIN CABIN FLOOR STRUCTURE STABILIZER STRAP BS LBL 26, BS 365 TO BS 377 CRACKED MIDSPAN. REMOVED AND INSTALLED NEW SECTION OF STABILIZER STRAP AT MAIN CABIN FLO

All 58: https://openairdocs.org/aircraft/N762BC/unmatched-reports.md

## STCs that may be installed (OpenAirDocs)

None matched to this aircraft's models.

## Earlier aircraft with N762BC

The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N762BC before.

- [Cancelled 2004-04-12](https://openairdocs.org/deregistered/N762BC-2004-04-12): Embraer EMB-120ER, S/N 120.119. Exported to Nigeria. Owner: [Jp Morgan Trust Co Na Trustee](https://openairdocs.org/faa-owner/JP%20MORGAN%20TRUST%20CO%20NA%20TRUSTEE), [San Francisco, CA](https://openairdocs.org/faa-place/CA/San%20Francisco)

## Related

- Other Raymond M Steele RAINBOW SKYREACH PTY aircraft: https://openairdocs.org/model/raymond-m-steele-rainbow-skyreach-pty/aircraft.md
- The Rotax 912ULS series engine: https://openairdocs.org/engine/rotax-912uls-series.md

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