# N833AS: 1998 Bombardier CL-600-2B19, registration cancelled 2017-04-25

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: April 25, 2017
- Status when cancelled: Valid registration
- Airframe: [Bombardier CL-600-2B19](https://openairdocs.org/model/bombardier-cl-600-2b19) (registry code 1390008)
- Engine: [GE CF34 series](https://openairdocs.org/engine/ge-cf34-series) (registry code 30015)
- Data sheets: [TCDS A21EA-1](https://openairdocs.org/tcds/A21EA-1) (OpenAirDocs)
- Serial number: 7246
- Year built: 1998
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: July 2, 1998
- Certificate issued: April 25, 2017
- Last registry action: April 25, 2017
- Mode S code: AB6390
- Owner when cancelled: [Airwheel Crj200 Fund II LLC](https://openairdocs.org/faa-owner/AIRWHEEL%20CRJ200%20FUND%20II%20LLC)
- Location: [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington)
- Owner type: Corporation
- Owner's area on the map: 39.7376° N, 75.6671° W: Placed by OpenAirDocs at the center of ZIP code 19808, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N833AS
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=833AS
- Page: https://openairdocs.org/deregistered/N833AS-2017-04-25

From the FAA registry file of October 28, 2026, cancelled registrations. Owners' street addresses are left out. The Mode S code belongs to the N-number, not the airframe.

ADs and bulletins for the Bombardier CL-600-2B19: https://openairdocs.org/model/bombardier-cl-600-2b19.md

## Service difficulty reports (169, newest 50)

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR ASOA2015072813396](https://openairdocs.org/sdr/ASOA2015072813396), Jul 28, 2015: BATTERY PACK. INOPERATIVE. OVERWING EMERGENCY LIGHTS ON LT AND RT SIDES INOPERATIVE. R & R THE NR 3 BATTERY PACK IAW AMM 33-51-04. REF IPC 33-51-04, ITEM 137. OPS CHECKED GOOD.
- [SDR ASOA2013121109609](https://openairdocs.org/sdr/ASOA2013121109609), Dec 7, 2013: LAMP. BURNED OUT. RT SIDE FWD EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP IAW AMM 33-51-21. OPS CHECKED GOOD.
- [SDR ASOA2013103009315](https://openairdocs.org/sdr/ASOA2013103009315), Oct 29, 2013: SMOKE WARNING. ILLUMINATED. SMOKE INDICATION , CARGO SMOKE WARNING, BLEW CARGO BOTTLE, AND DIVERTED.
- [SDR ASOA2013091209000](https://openairdocs.org/sdr/ASOA2013091209000), Sep 8, 2013: LIGHT. INOPERATIVE. THE EXTERIOR EMERGENCY FLOODLIGHT AFT OF THE RT WING EMERGENCY EXIT IS INOPERATIVE. R & R THE FLOODLIGHT IAW AMM 33-51-21-400-801. OPS CHECKED GOOD IAW AMM 33-5
- [SDR ASOA2013091208999](https://openairdocs.org/sdr/ASOA2013091208999), Aug 27, 2013: SKIN. CRACKED. SKIN FAILS NDT INBD SIDE APPROX 8" LT 60 PERCENT SCREEN HEIGHT (X .250). REPAIRED IAW EC/TC EO 600-57-81 AND REO 601R-57-71-030, REV K.
- [SDR ASOA2013091208998](https://openairdocs.org/sdr/ASOA2013091208998), Aug 27, 2013: SKIN. CRACKED. SKIN FAILS NDT AROUND ENTIRE HOLE. REPAIRED IAW REO 601R-57-21-1992, ECTC EO 600-57-81 AND REO 601R-57-21-030, REV K.
- [SDR ASOA2013091208997](https://openairdocs.org/sdr/ASOA2013091208997), Aug 27, 2013: SKIN. CRACKED. SKIN FAILS NDT MULTIPLE INDICATIONS INBD SIDE OF HOLE 50 PERCENT SCREEN HEIGHT. 1" L X .250. REPAIRED IAW EC/TC EO 600-57-81 AND REO 601R-57-71-030, REV K.
- [SDR ASOA2013091208996](https://openairdocs.org/sdr/ASOA2013091208996), Aug 27, 2013: SKIN. CRACKED. SKIN FAILS NDT INBD SIDE 50 PERCENT SCREEN HEIGHT .200 X .200. REPAIRED IAW EC/TC EO 600-57-81 AND REO 601R-57-71-030, REV K.
- [SDR ASOA2013091208995](https://openairdocs.org/sdr/ASOA2013091208995), Aug 27, 2013: SKIN. CRACKED. SKIN FAILS NDT WITH INDICATION ON INBD SIDE OF HOLE 2" L X .200 50 PERCENT SCREEN HEIGHT. REPAIRED IAW EC/TC EO 600-57-81 AND IAW REO 601R-57-71-030, REV K.
- [SDR ASOA2013091208994](https://openairdocs.org/sdr/ASOA2013091208994), Aug 26, 2013: SKIN. CRACKED. SKIN FAILS NDT AFT SIDE OF HOLE .200 X .200, 60 PERCENT SCREEN HEIGHT. REPAIRED IAW EC/TC EO 600-57-81 AND IAW REO 601R-57-71-030, REV K.
- [SDR ASOA2013091208993](https://openairdocs.org/sdr/ASOA2013091208993), Aug 26, 2013: SKIN. CRACKED. SKIN FAILS NDT INDICATIONS INBD & OTBD SIDE OF HOLE .500 X .250 70 PERCENT SCREEN HEIGHT. REPAIRED IAW EC/TC EO 600-57-81 AND IAW REO 601R-57-71-030, REV K.
- [SDR ASOA2013091208992](https://openairdocs.org/sdr/ASOA2013091208992), Aug 26, 2013: ANGLE. CRACKED. LT WING HAS A CRACKED ANGLE JUST FWD & INBD OF MLG. REMOVED 601R10213-11, ANGLE TO REPLACE WITH NEW ANGLE IAW SRM . INSTALLED ANGLE, PN 601R10213-11 IAW SRM 51-
- [SDR ASOA2013091208991](https://openairdocs.org/sdr/ASOA2013091208991), Aug 21, 2013: STRUCTURE. CRACKED. RIGHT BOOST PUMP CUTOUT HOLE FAILS NDT WITH INDICATIONS ON AFT SIDE OF HOLE ON LANDING, GREATER THAN 50 PERCENT SCREEN HEIGHT, APROX 1. ALSO, HAS SMALLER INDICA
- [SDR ASOA2013091208990](https://openairdocs.org/sdr/ASOA2013091208990), Aug 21, 2013: SKIN. CRACKED. FOUND CARGO DOOR LOWER AFT CORNER FUSELAGE SKIN HAS INDICATION NOTED APRPOX .1" IN LENGTH 90 PERCENT FSH AT THIS LOCATION. IT ALSO, HAS PROTRUDING DENT .2" L X 
- [SDR ASOA2013083008937](https://openairdocs.org/sdr/ASOA2013083008937), Aug 19, 2013: TRUNNION. CRACKED. INDICATION NOTED IN RT SIDE TURNNION FITTING FASTENER HOLE, 6TH HOLE AFT 9 INDICATION NOTED IN TRUNNION FITTING. 60 PERCENT FULL SCREEN HEIGHT AT OTBD SIDE OF H
- [SDR ASOA2013082808923](https://openairdocs.org/sdr/ASOA2013082808923), Aug 19, 2013: POST. CRACKED. FS 409.128, RBL 18 VERTICAL POST HAD INDICATIONS NOTED IN THE AFT FLANGE RADIUS AT WL 69, REPAIRED IAW REO 601R-53-41-889.
- [SDR ASOA2013091208989](https://openairdocs.org/sdr/ASOA2013091208989), Aug 16, 2013: SKIN. CRACKED. SUSPECT CRACK AT RT WING WS 148.019, EXTENDING OUT FROM A FASTENER. SUSPECTED CRACK IS LOCATED AFT OF THE AFT WING SPAR BESIDE THE PIE PANEL AND DIRECTLY BELOW 
- [SDR ASOA2013082808922](https://openairdocs.org/sdr/ASOA2013082808922), Aug 15, 2013: POST. CRACKED. FS 409+128, RBL 18 VERTICAL POST HAD INDICATIONS NOTED IN THE AFT FLANGE RADIUS AT WL 69. REMOVED VERTICAL POST IAW SRM 51-42-06. INSTALLED POST IAW SRM 51-42-0
- [SDR ASOA2013082208898](https://openairdocs.org/sdr/ASOA2013082208898), Aug 15, 2013: POST. CRACKED. LBL 18 FS 409+128 OTBD VERT POST HAS AN INDICATION NOTED IN THE AFT FLANGE RADIUS AT WL 69 APPROX .250" LONG X 50 PERCENT FSH. FAILED NDT INSPECTION. REMOVED OT
- [SDR ASOA2013091208988](https://openairdocs.org/sdr/ASOA2013091208988), Aug 14, 2013: HINGE. GOUGED. PAX DOOR HINGE HALF ON FUSELAGE HAS ONE GOUGED LUG. LUG IS NEXT TO LAST LUG ON AFT END APPROX .025" L X .004" DEEP. REPAIRED IAW REO 601R-53-21-814, TYPE 1. MAJ
- [SDR ASOA2013091208987](https://openairdocs.org/sdr/ASOA2013091208987), Aug 14, 2013: SKIN. DENTED. LT WING INBD GROUND SPOILER LOWER INBD SKIN HAS 2 EA DENTS APPROX .100 L X.100 W X .030 D. REPAIRED IAW REO 601R-57-71-382, REV "A".
- [SDR ASOA2013083008936](https://openairdocs.org/sdr/ASOA2013083008936), Aug 14, 2013: SKIN. CHAFED. LEFT AILERON UPPER FIXED L/E IS CHAFED AT THREE LOCATIONS APPROX 6.0 INCHES LONG, .400 INCHES WIDE AND .012 INCHES DEEP. REPAIRED IAW REO 601R-57-60-013.
- [SDR ASOA2013082208897](https://openairdocs.org/sdr/ASOA2013082208897), Aug 14, 2013: SEAT TRACK. CORRODED. SEAT TRACK FS 409 AND 409+128 CORRODED IN SEVERAL AREAS. REMOVED CABIN SEAT TRACK IAW AMM 53-01-11-00-802. LOCATED & INSTALLED SEAT TRACK IAW AMM 53-01-11-400-8
- [SDR ASOA2013082208896](https://openairdocs.org/sdr/ASOA2013082208896), Aug 14, 2013: SEAT TRACK. CORRODED. SEAT TRACK FS 349 AND FS 409 CORRODED IN SEVERAL AREAS. REMOVED SEAT TRACK IAW 53-01-11-000-802. DRILLED DEBURRED IAW AMM 53-01-11-400-802. INSTALLED NEW SEAT T
- [SDR ASOA2013082208895](https://openairdocs.org/sdr/ASOA2013082208895), Aug 14, 2013: ANGLE. CORRODED. FS 280.00 FWD J ANGLE IS CORRODED. REMOVED CORRODED ANGLE IAW SRM 51-42-06 AND 51-42-21. LOCATED, DRILLED AND INSTALLED NEW ANGLE IAW SRM 51-40-11, 51-42-06 AND
- [SDR ASOA2013082208894](https://openairdocs.org/sdr/ASOA2013082208894), Aug 14, 2013: ANGLE. CRACKED. BS 484 ANGLE AT RBL 27 IS CRACKED. R & R CRACKED CLIP WITH NEW IAW SRM 51-42-21 AND 51-40-11.
- [SDR ASOA2013082208893](https://openairdocs.org/sdr/ASOA2013082208893), Aug 14, 2013: ANGLE. CRACKED. LT BS 484 ANGLE AT LBL 27 IS CRACKED. R & R CRACKED ANGLE WITH NEW IAW SRM 51-42-21 AND 51-40-11.
- [SDR ASOA2013062103863](https://openairdocs.org/sdr/ASOA2013062103863), Jun 17, 2013: FLASHLIGHT. INTERMITTENT. PILOT FLASHLIGHT WORKS INTERMITTENTLY. R & R CAPTAIN'S FLASHLIGHT IAW AMM 25-61-04, OPS CHECKED GOOD.
- [SDR ASOA2012091202190](https://openairdocs.org/sdr/ASOA2012091202190), Sep 8, 2012: INVERTER. UNSERVICEABLE. EMERGENCY EXIT DOOR LIGHTED SIGN AT ROW 8A HALF LIGHT. R & R NR 2 INVERTER IAW AMM 33-51-07. OPS CHECKED GOOD.
- [SDR ASOA2012091202189](https://openairdocs.org/sdr/ASOA2012091202189), Sep 8, 2012: LAMP. BURNED OUT. EMERGENCY EXIT DOOR LIGHTED SIGN AT ROW 8D INOPERATIVE. R & R LAMP IAW AMM 33-51-13. OPS CHECKED GOOD.
- [SDR ASOA2011121702377](https://openairdocs.org/sdr/ASOA2011121702377), Dec 17, 2011: RELAY. FAILED. EMERGENCY LIGHTS FLICKERING. R & R ACCESS BUSS UNDER VOLTAGE RELAY (K1XD) IAW AMM 24-51-27. OPS CHECKED GOOD. OPS CHECK OF EMERGENCY LIGHT SYS IAW AMM 33-51-01.
- [SDR ASOA201101517](https://openairdocs.org/sdr/ASOA201101517), Aug 8, 2011: WIRE. MISINSTALLED. LOWER EMERGENCY LIGHT AT LT OVERWING EXIT IS INOPERATIVE. TROUBLESHOOT AND FOUND SPLICES ON WIRES MISSING. INSTALLED 2 NEW QUICK DISCONNECT SPLICES ON THE EMERG
- [SDR ASOA201101486](https://openairdocs.org/sdr/ASOA201101486), Aug 8, 2011: CROSSBEAM. CORRODED. CORROSION FOUND ON FS 349 CROSSBEAM AT SERVICE DOOR. REPAIRED IAW REO 601R-53-61-1541.
- [SDR ASOA201101480](https://openairdocs.org/sdr/ASOA201101480), Aug 5, 2011: SIGN. INOPERATIVE. RT SERVICE DOOR EXIT SIGN BETA LIGHTS HAS AN LIGHT INTENSITY LESS THAN 100. REMOVED AND REPLACED IAW AMM 33-51-09-400-802. FUNCTIONAL TESTED GOOD IAW AMM TASK 3
- [SDR ASOA201101460](https://openairdocs.org/sdr/ASOA201101460), Aug 5, 2011: PRESSURE BLKHD. CRACKED. REAR PRESSURE BULKHEAD IS CRACKED ABOVE CARGO DOOR, OVER AFT TRACK. PRESSURE BULKHEAD REPAIRED IAW ARM 51-52-06.
- [SDR ASOA201101459](https://openairdocs.org/sdr/ASOA201101459), Aug 5, 2011: PRESSURE PANEL. MISREPAIRED. PRESSURE FLOOR DOUBLER CORRODED AFT OF FS 439.00 RBL43. APPEARS TO BE 10F6 UNDOCUMENTED DOUBLERS INSTALLED ON PRESSURE FLOOR. REMOVED CORROSION IAW SRM 51-21-06
- [SDR ASOA201101467](https://openairdocs.org/sdr/ASOA201101467), Aug 4, 2011: SEAT TRACK. CORRODED. 3 INCH SEAT RAIL FWD OF FS 621.00 AT LBL 9.00 HAS CORROSION ON SURFACE IN CARGO COMPARTMENT. REMOVED SEAT TRACK AND TRANSFERRED HOLES TO NEW SEAT TRACK IAW SRM 
- [SDR ASOA201101466](https://openairdocs.org/sdr/ASOA201101466), Aug 4, 2011: SEAT TRACK. CORRODED. SHORT SEAT RAIL BETWEEN FS 559.00+80-FS559.00+96 AT RBL 27.00 HAS SURFACE CORROSION IN CARGO COMPARTMENT. REMOVED SEAT TRACK AND TRANSFERRED HOLES TO NEW SEAT T
- [SDR ASOA201101465](https://openairdocs.org/sdr/ASOA201101465), Aug 4, 2011: SEAT TRACK. CORRODED. SHORT SEAT RAIL BETWEEN FS 559.00+80-FS559.00+96 AT RBL 9.00 HAS SURFACE CORROSION IN CARGO COMPARTMENT. REMOVED SEAT TRACK AND TRANSFERRED HOLES TO NEW SEAT TR
- [SDR ASOA201101464](https://openairdocs.org/sdr/ASOA201101464), Aug 4, 2011: SEAT TRACK. CORRODED. SHORT SEAT RAIL BETWEEN FS 559.00+80-FS559.00+96 AT LBL 9.00 HAS SURFACE CORROSION IN CARGO COMPARTMENT. REMOVED SEAT TRACK AND TRANSFERRED HOLES TO NEW SEAT TR
- [SDR ASOA201101463](https://openairdocs.org/sdr/ASOA201101463), Aug 4, 2011: SEAT TRACK. CORRODED. SHORT SEAT RAIL BETWEEN FS 559.00+80-FS559.00+96 AT LBL 27.00 HAS SURFACE CORROSION IN CARGO COMPARTMENT. REMOVED SEAT TRACK AND TRANSFERRED HOLES TO NEW SEAT T
- [SDR ASOA201101462](https://openairdocs.org/sdr/ASOA201101462), Aug 4, 2011: SEAT TRACK. CORRODED. SHORT SEAT RAIL BETWEEN FS 559.00+112-572.00 AT RBL 9.00 HAS SURFACE CORROSION IN CARGO COMPARTMENT. REMOVED SEAT TRACK AND TRANSFERRED HOLES TO NEW SEAT TRACK 
- [SDR ASOA201101457](https://openairdocs.org/sdr/ASOA201101457), Aug 4, 2011: SEAT TRACK. CORRODED. SHORT SEAT RAIL BETWEEN FS 559.00+112-FS572.00 AT LBL 9.00 HAS SURFACE CORROSION IN CARGO COMPARTMENT. REMOVED SEAT TRACK AND TRANSFERRED HOLES TO NEW SEAT TRAC
- [SDR ASOA201101451](https://openairdocs.org/sdr/ASOA201101451), Aug 4, 2011: ANGLE. CORRODED. CORROSION FOUND ANGLE AT FS 349 AT SERVICE DOOR UNDER TEFLON CAP. REMOVED ANGLE & FOUND CORROSION TO BE OUT OF LIMITS IAW SRM 51-21-06. INSTALLED SERVICABLE ANG
- [SDR ASOA201101450](https://openairdocs.org/sdr/ASOA201101450), Aug 4, 2011: STRUCTURE. CORRODED. CORROSION FOUND AT FS 349 AT PAX DOOR UNDER TEFLON CAP. BLENDED CORROSION & FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00.
- [SDR ASOA201101449](https://openairdocs.org/sdr/ASOA201101449), Aug 4, 2011: NUT PLATE. CORRODED. PASSENGER DOOR SILL PLATE ANGLE CORRODED. UPON FURTHER INSPECTION FOUND 5 NUT CLIPS ONLY TO BE CORRODED. R & R IAW MINOR REPAIR.
- [SDR ASOA201101448](https://openairdocs.org/sdr/ASOA201101448), Aug 4, 2011: FLOORBEAM. CRACKED. INBD AND OTBD CLIPS CRACKED AT FS280 LBL9. REMOVED CRACKED CLIPS INBD AND OTBD AT FS 280, LBL9 IAW SRM 51-42-00. INSTALLED NEW CLIPS AT FS 280, LBL9, INBD AND O
- [SDR ASOA201101447](https://openairdocs.org/sdr/ASOA201101447), Aug 4, 2011: FLOORBEAM. CRACKED. INBD AND OTBD CLIPS CRACKED AT FS 280 RBL 9. REMOVED AND INSTALLED IAW SRM 51-42-00.
- [SDR ASOA201101446](https://openairdocs.org/sdr/ASOA201101446), Aug 4, 2011: FRAME. CORRODED. FRAME CORRODED AT FS319.70, STR 26R. REMOVED FRAME LOWER SECTION IAW SRM 51-42-06 & 51-42-21. DRILLED NEW SECTION OF FRAME & INSTALLED IAW SRM 51-42-06.
- [SDR ASOA201101445](https://openairdocs.org/sdr/ASOA201101445), Aug 4, 2011: FRAME. CORRODED. CORROSION AT FRAME FS 333 STR 26 & 27R. REMOVED CORROSION, FRAME FOUND TO BE WITHIN ALLOWABLE DAMAGE LIMITS SRM 53-00-00.

All 169: https://openairdocs.org/deregistered/N833AS-2017-04-25/reports.md

## FAA accident and incident reports (1)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Incident 20020108001379I](https://openairdocs.org/incident/20020108001379I), Jan 8, 2002: Cndair CL6002B19 (N833AS), Pittsburgh, PA. (-23) An atlantic southeast airlines flight #4595 suffered a hydraulic failure and diverted to pit on January 8, 2002, at 1132 local time. The CL-600 landed on…

## Other aircraft with N833AS

- [Registered now](https://openairdocs.org/aircraft/N833AS): Ea Vision EA J100, S/N EAVUAV502585851

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