# N826AS: 1997 Canadair CL-600-2B19, registration cancelled 2015-02-27

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: February 27, 2015
- Status when cancelled: Valid registration
- Airframe: [Canadair CL-600-2B19](https://openairdocs.org/model/canadair-cl-600-2b19) (registry code 1900309)
- 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: 7210
- Year built: 1997
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: January 21, 1998
- Certificate issued: December 18, 2014
- Last registry action: December 18, 2014
- Mode S code: AB4736
- Owner when cancelled: [Strong Tower Properties X LLC](https://openairdocs.org/faa-owner/STRONG%20TOWER%20PROPERTIES%20X%20LLC)
- Location: [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington)
- Owner type: Corporation
- Owner's area on the map: 39.7965° N, 75.6128° W: Placed by OpenAirDocs at the center of ZIP code 19807, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N826AS
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=826AS
- Page: https://openairdocs.org/deregistered/N826AS-2015-02-27

From the FAA registry file of October 29, 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 Canadair CL-600-2B19: https://openairdocs.org/model/canadair-cl-600-2b19.md

## Service difficulty reports (127, newest 50)

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

- [SDR ASOA2014062710762](https://openairdocs.org/sdr/ASOA2014062710762), Jun 25, 2014: PROXIMITY SENSOR. OUT OF ADJUST. MAIN GEAR WAS CYCLING UP AND DOWN AFTER TAKEOFF, NOSE GEAR WAS UNKNOWN, RAN THE GEAR DISAGREE CHECKLIST THE QRH AND LANDED WITH THREE GREEN AFTER EMERGENCY GEAR
- [SDR ASOA2014050710468](https://openairdocs.org/sdr/ASOA2014050710468), May 3, 2014: WIRE. DAMAGED. EMERGENCY FLOODLIGHT INOPERATIVE AT BULKHEAD. REPAIRED WIRE SPLICE CONNECTOR IAW ESPM 20-17-31. SYSTEM OPS CHECKED GOOD. NO FURTHER ACTION.
- [SDR ASOA2013032503250](https://openairdocs.org/sdr/ASOA2013032503250), Mar 19, 2013: BLADES. DAMAGED. RT ENGINE FLAMED OUT ON DESCENT AT 4000 & 250 KIAS. ATTEMPTED RELIGHT UNSUCCESSFUL. COMPLIED WITH WITH AREA C BOROSCOPE INSPECTION IAW MANUAL 72-00-00. FOUND DA
- [SDR ASOA2012092602304](https://openairdocs.org/sdr/ASOA2012092602304), Sep 23, 2012: WIRE. SHORTED. EMERGENCY LIGHTS COME ON IN ARM POSTION. FOUND WIRE LQ1AZZ SHORTED IAW ESPM 20-12-01. INSTALLED SPLICE ON WIRE LQ1AZZ IAW ESPM 20-16-00. PERFORMED OPS TEST OF S
- [SDR ASOA2012092602303](https://openairdocs.org/sdr/ASOA2012092602303), Sep 23, 2012: CONNECTOR. DAMAGED. EMERGENCY LIGHTS AT PAX DOOR INOPERATIVE. EMERGENCY LIGHT HAS A CONNECTOR DAMAGED. INSTALLED NEW PIN AND CONNECTOR ONTO WIRE OF EMERGENCY LIGHT IAW ESPM 20-11-0
- [SDR ASOA2012092602301](https://openairdocs.org/sdr/ASOA2012092602301), Sep 11, 2012: STRUCTURE. CORRODED. PAX DOOR AFT BOTTOM CORNER CORRODED. REMOVED PAX DOOR AFT BOTTOM CORNER (2 PART) IAW SRM 51-42-06. INSTALLED NEW ASD AFT BOTTOM CORNER (2 PART) IAW SRM 51-42-06
- [SDR ASOA2012092602300](https://openairdocs.org/sdr/ASOA2012092602300), Sep 11, 2012: STRUCTURE. CORRODED. PAX DOOR FWD BOTTOM CORNER CORRODED. REMOVED FWD BOTTOM CORNER (2 PART) IAW SRM 51-42-06. INSTALLED NEW ASD FWD BOTTOM CORNER IAW SRM 51-42-06, 51-42-21. REPAIR
- [SDR ASOA2012092602299](https://openairdocs.org/sdr/ASOA2012092602299), Sep 6, 2012: FLOOR SUPPORT. CORRODED. DURING REINSPECTION IAW EO 600-53-216/01 ADDITIONAL CORROSION ON LT FLOOR SUPPORT FROM FS 409 + 128 - FS 559.00 WAS FOUND. REMOVED CORROSION IAW SRM 51-21-06 35
- [SDR ASOA2012092602298](https://openairdocs.org/sdr/ASOA2012092602298), Sep 6, 2012: FLOOR SUPPORT. CORRODED. DURING REINSPECTION IAW EO 600-53-216/01 FOUND ADDITIONAL CORROSION ON FLOOR SUPPORT FROM FS 409 + 128 TO FS 559.0 ON RT SIDE. REMOVED CORROSION IAW SRM 51-21-0
- [SDR ASOA2012092602297](https://openairdocs.org/sdr/ASOA2012092602297), Sep 5, 2012: ISOLATOR. BROKEN. TWO ISOLATORS BROKEN ON AFT BULKHEAD. REMOVED AND REPLACED ISOLATORS IAW SRM 51-42-13.
- [SDR ASOA2012092602296](https://openairdocs.org/sdr/ASOA2012092602296), Sep 5, 2012: DRAG ANGLE. CRACKED. PAX DOOR AFT DRAG ANGLE CRACKED AT RIVET. REPAIRED IAW GREO 601R-52-11-513. COMPLIED WITH EC/TC REO 601R-52-11-513.
- [SDR ASOA201200946](https://openairdocs.org/sdr/ASOA201200946), Mar 18, 2012: FLAP SYSTEM. UNKNOWN. FLAPS FAIL AT ZERO WHEN SELECTING FLAPS AT EIGHT. EMERGENCY DECLARED . COMPLIED WITH AD 2009-06-12. PERFORMED TROUBLESHOOTING IAW FIM 27-50-00. FOUND NO FAULTS 
- [SDR ASOA201200366](https://openairdocs.org/sdr/ASOA201200366), Feb 1, 2012: WARNING MESSAGE. FALSE ACTIVATION. AT FL 290, RECEIVED A HYD NR 2 HIGH TEMP CAUTION MESSAGE. COMPLIED WITH QRH AN LANDED AT NEAREST SUITABLE AIRPORT. EMERGENCY DECLARED. COULD NOT DUPLICATE COMPL
- [SDR ASOA201200347](https://openairdocs.org/sdr/ASOA201200347), Jan 29, 2012: BPSU. OUT OF ADJUST. FLAP FAIL AT ZERO DEGREES. EMERGENCY DECLARED. RIGGED LT AND RT BPSU, IAW AMM 27-51-01, PERFORMED ADJUSTMENT TEST OF FECU IAW AMM 27-51-05-05. OPS CHECKED GOOD,
- [SDR ASOA201200049](https://openairdocs.org/sdr/ASOA201200049), Jan 4, 2012: DETECTOR. FAILED. FLAPS FAILED AT 0 DEGREES DURING CRUISE ALT NORMAL LANDING. EMERGENCY DECLARED. R & R SKEW DETECTION UNIT IAW AMM 27-51-15.
- [SDR ASOA201102431](https://openairdocs.org/sdr/ASOA201102431), Dec 21, 2011: PUMP. FAILED. CLIMBING OUT OF SAV RECEIVED HYD 2 HI TEMP. FOLLOWED QRH TEMP CONTINUED TO CLIMB ABOVE 135 DEGREES C. DIVERTED, IAW QRH. EMERGENCY DECLARED. R & R NR 2 ENGINE D
- [SDR ASOA201102258](https://openairdocs.org/sdr/ASOA201102258), Nov 27, 2011: BATTERY PACK. DISCHARGED. EMERGENCY LIGHTS LEFT IN ON POSTION OVERNIGHT AND DISCHARGED THE BATTERIES, EMERGENCY LIGHTS NOW INOP. OPS CHECKED GOOD IAW AMM 33-51-00.
- [SDR ASOA201101631](https://openairdocs.org/sdr/ASOA201101631), Sep 1, 2011: COOLING DUCT. DISCONNECTED. COOL CAUTION MESSAGE DISPLAYED SHORTLY AFTER T/O, RAN QRH PRECEDURE, MESSAGE PERSISTED, ED T-4 EACH DISLAYED OVERHEAT AND ALL MESSAGE EXTINGUISHED. ( ACFT DIVER
- [SDR ASOA201101120](https://openairdocs.org/sdr/ASOA201101120), Jun 4, 2011: DOOR. BINDING. PAX DOOR WILL NOT OPEN FROM OUTSIDE. OPS CHECK PAX DOOR SEVERAL TIMES IAW AMM 52-11-00. OPS CHECK GOOD NO FURTHER DEFECTS FOUND.
- [SDR ASOA201100527](https://openairdocs.org/sdr/ASOA201100527), Mar 19, 2011: LATCH. BINDING. F/A STATES THAT MAIN CABIN DOOR LATCH WOULD NOT ACTUATE THE FIRST FEW TIMES TRIED TO OPEN THE DOOR UPON ARRIVAL. OPERATED PAX DOOR SEVERAL TIMES NO DEFECTS NOTE
- [SDR ASOA201100433](https://openairdocs.org/sdr/ASOA201100433), Mar 6, 2011: DOOR. LACK OF LUBE. MAIN DOOR CATCHES WHEN TRYING TO OPEN FROM OUTSIDE. PERFORMED LUBRICATION OF PAX DOOR IAW AMM 12-20-52. OPS CHECK GOOD AT THIS TIME. (CLOSED)
- [SDR ASOA201100432](https://openairdocs.org/sdr/ASOA201100432), Mar 6, 2011: HANDLE. DAMAGED. MAIN DOOR WILL NOT OPEN. RESECURED PAX DOOR INSIDE HANDLE STRAP IAW AMM 52-11-02. OPS CHECK GOOD AT THIS TIME. (CLOSED)
- [SDR ASOA201100176](https://openairdocs.org/sdr/ASOA201100176), Jan 28, 2011: HANDLE. OUT OF RIG. PAX DOOR HANDLE IS VERY HARD TO OPEN AND STOW. APPEARS TO BE IMPROPERLY RIGGED. REMOVED PAX DOOR ACCESS PANELS. REMOVED CLOSING PLATE UNDER BOTTOM FOLDING STOP 
- [SDR ASOA201100159](https://openairdocs.org/sdr/ASOA201100159), Jan 24, 2011: LIGHT. BROKEN. FLOOR EMERGENCY FLOOD LIGHT ON WARDROBE IS BROKEN. REPLACED EMERGENCY FLOOR LIGHT ON LOWER WARDROBE ASSY IAW AMM 33-51-19-400-801. OPS CHECKED GOOD IAW AMM 35-5
- [SDR ASOA201100158](https://openairdocs.org/sdr/ASOA201100158), Jan 24, 2011: SKIN. CORRODED. CORROSION ON BELLY SKIN AROUND FASTENERS STA 559+112 TO FS 574 BETWEEN STR 23R-24L.
- [SDR ASOA201100127](https://openairdocs.org/sdr/ASOA201100127), Jan 19, 2011: FRAME. CORRODED. FS 333, FRAME IN BELLY IS CORRODED. PRIMED AND PAINTED REPAIR AREA IAW SRM 51-25-01. THIS REPAIR REQUIRES MAJOR/MINOR CLASSIFICATION IAW ASA SOP 5702. THIS REPA
- [SDR ASOA201100141](https://openairdocs.org/sdr/ASOA201100141), Jan 14, 2011: SKIN. CORRODED. CORROSION ON BELLY SKIN AROUND FASTENERS STA 559+112 TO 574 BETWEEN STR 23R-24L. DOUBLER INSTALLED IAW REO 601R-53-61-3943
- [SDR ASOA201100077](https://openairdocs.org/sdr/ASOA201100077), Jan 10, 2011: BEAM. CRACKED. ON THE ECU SUPPORT FRAME THE OTBD FWD BEAM ASSY IS CRACKED, PN 601R95156-66, AND THE INBD BEAM ASSY IS GOUGED. REMOVED INBD BEAM ASSY, PN 601R95155-76, IAW SRM 
- [SDR ASOA201100051](https://openairdocs.org/sdr/ASOA201100051), Jan 10, 2011: INTERCOSTAL. CORRODED. INTERCOSTAL CAP AT FS 559.00+80 BETWEEN RBL 9, 27 & FLOOR SUPPORT IS CORRODED. R & R INTERCOSTAL CAP AT FS 559.00+80 BETWEEN RBL 27 & RBL 9 FLOOR SUPPORT IAW SR
- [SDR ASOA201100050](https://openairdocs.org/sdr/ASOA201100050), Jan 10, 2011: SKIN. CRACKED. FUSELAGE SKIN IS CRACKED AT FS 235, LT SIDE BL 6.0, RT SIDE HAS BEEN PREVIOUSLY REPAIRED USING REO 601R-53-11-048. REPAIRED IAW REO 601R-53-11-2038.
- [SDR ASOA201100076](https://openairdocs.org/sdr/ASOA201100076), Jan 7, 2011: INTERCOSTAL. CRACKED. CARGO TIE DOWN PAN AFT LOCATION HAS OTBD, AFT END CRACKED AT FASTENER HOLE ON INTERCOSTAL. R & R INTERCOSTAL, 601R35031-205, IAW SRM 51-42-06. (CLOSED)
- [SDR ASOA201100075](https://openairdocs.org/sdr/ASOA201100075), Jan 6, 2011: STRINGER. CORRODED. STRINGER 26 RT HEAVILY CORRODED/PITTED AROUND RIVETS APPROX 1/2" 0 0.035" DEEP A FS 336 & 338. INSTALLED NEW STRINGER SEGMENT IAW SRM 53-00-03.
- [SDR ASOA201100042](https://openairdocs.org/sdr/ASOA201100042), Jan 6, 2011: ANGLE. CRACKED. ANGLE UNDER CARGO SUPPORT SILL CRACKED. R & R ANGLE WITH SERVICEABLE ANGLE IAW SRM 51-42-21. THIS REPAIR IS CLASSIFIED AS A MINOR REPAIR IAW ASA SOP 5702.
- [SDR ASOA201100036](https://openairdocs.org/sdr/ASOA201100036), Jan 5, 2011: POST. CRACKED. FOUND FS 409+128 VERTICAL POST RBL 18.0 INBD SIDE HAS INDICATION NOTED APPROX .2" IN LENGTH 55 PERCENT FSH AT WL 69.0 AFT FLANGE RADIUS. FAILED NDT INSP. REMOVE
- [SDR ASOA201100035](https://openairdocs.org/sdr/ASOA201100035), Jan 5, 2011: SKIN. CORRODED. CORROSION ON BELLY SKIN AROUND FASTENERS STA 559+112 TO 574, BETWEEN STR 23R-24L. REMOVED CORROSION FROM BELLY SKIN IAW SRM 51-21-06. FOUND TO BE WITHIN LIMITS 
- [SDR ASOA201100034](https://openairdocs.org/sdr/ASOA201100034), Jan 5, 2011: FRAME. CORRODED. FS 333, FRAME IN BELLY IS CORRODED. REMOVED CORRODED FRAME FROM FS 333 IAW SRM 51-42-06 AND 51-742-21. LOCATED AND DRILLED NEW FS 333 FRAME PIN 601R32004-55 AND
- [SDR ASOA201100030](https://openairdocs.org/sdr/ASOA201100030), Jan 4, 2011: SEAT TRACK. CORRODED. LT AND RT FWD SEAT TRACK SEGMENTS ARE CORRODED. REMOVED 1 EA LT & RT FWD FLOOR SEAT TRACK SEGMENTS DUE TO CORROSION IAW AMM 53-01-11-000-802, STEPS 3B1-3B3. INS
- [SDR ASOA201100029](https://openairdocs.org/sdr/ASOA201100029), Jan 4, 2011: ISOLATOR. CRACKED. FS 621, PRESS BULKHEAD HAS CRACKED ISOLATORS AT RBL 27 (1), LBL 18 (2), LBL 27. REMOVED ISOLATOR MOUNTS. R & R ISOLATOR BRACKETS PN SL2337-3. REINSTALLED ISOLAT
- [SDR ASOA201100028](https://openairdocs.org/sdr/ASOA201100028), Jan 4, 2011: SILL. CORRODED. INTERCOSTAL CAP AT FS 589 BETWEEN RBL 27 AND FLOOR SUPPORT SILL IS CORRODED. REMOVED MINOR CORROSION ON INTERCOSTAL CAP, MAT LOSS .006 IAW SRM 51-21-06, 51-21-1
- [SDR ASOA201100027](https://openairdocs.org/sdr/ASOA201100027), Jan 4, 2011: FLOOR SUPPORT. CORRODED. RT CARGO FLOOR SUPPORT FROM FS 621 TO 559+112 IS CORRODED. REMOVED MINOR CORROSION FROM RT FLOOR SUPPORT IAW SRM 51-21-06 APPROX .001 - .002. MATERIAL REMOVED W
- [SDR ASOA201100026](https://openairdocs.org/sdr/ASOA201100026), Jan 4, 2011: SEAT TRACK. CORRODED. CARGO SEAT TRACK AT LBL 9 FS 621, FS 574 AND FS 559+80 IS CORRODED. REMOVED MINOR CORROSION ON INTERCOSTAL CAP, MAT LOSS .006 IAW SRM 51-21-06, 51-21-11 & 51-25
- [SDR ASOA201100025](https://openairdocs.org/sdr/ASOA201100025), Jan 4, 2011: SEAT TRACK. CORRODED. CARGO SEAT TRACK AT RBL 27, FS 559+80 IS CORRODED. INSTALLED NEW CARGO TRACK IAW AMM 53-01-11-400-802.
- [SDR ASOA201100024](https://openairdocs.org/sdr/ASOA201100024), Jan 4, 2011: SEAT TRACK. CORRODED. CARGO SEAT TRACK AT RBL 9 FS 559+112 AND 559+80 IS CORRODED. R & R SEAT TRACK SEGMENT IAW AMM 20-21-00-910-801.
- [SDR ASOA201100023](https://openairdocs.org/sdr/ASOA201100023), Jan 4, 2011: FLOOR SUPPORT. CORRODED. FLOORBEAM CAP AT RBL 9 FS 621 TO FS 574 IS CORRODED. BLENDED CORROSION OF FLOORBEAM CAP IAW REO 601R-53-00-005. FOUND TO BE OUT OF LIMITS. REMOVED FLOORBEAM CAP
- [SDR ASOA201100022](https://openairdocs.org/sdr/ASOA201100022), Jan 4, 2011: INTERCOSTAL. CORRODED. INTERCOSTAL CAP AT FS 589 BETWEEN RBL 9 AND 27 IS CORRODED. REMOVED MINOR CORROSION ON INTERCOSTAL CAP, MAT LOSS .006 IAW SRM 51-21-06, 51-21-11 & 51-25-16. REP
- [SDR ASOA201100021](https://openairdocs.org/sdr/ASOA201100021), Jan 4, 2011: INTERCOSTAL. CORRODED. INTERCOSTAL CAP AT FS 589 BETWEEN LBL 9 AND 27 IS CORRODED. REMOVED MINOR CORROSION ON INTERCOSTAL CAP AT FS 589 BETWEEN RBL & LBL 9 MAT LOSS .006 IAW SRM 51-21
- [SDR ASOA201100020](https://openairdocs.org/sdr/ASOA201100020), Jan 4, 2011: INTERCOSTAL. CORRODED. INTERCOSTAL CAP AT FS 589 BETWEEN RBL AND LBL 9 IS CORRODED. BLENDED CORROSION ON FLOORBEAM IAW REO 601R-53-60-005, REV A AND FOUND TO BE OUT OF LIMITS REO 601R
- [SDR ASOA201100019](https://openairdocs.org/sdr/ASOA201100019), Jan 4, 2011: FLOOR SUPPORT. CORRODED. FLOORBEAM CAP AT RBL 27, FS 621 TO 574 IS CORRODED. BLENDED CORROSION ON FLOORBEAM CAP LBL 27 IAW REO 601R-53-60-005, REV A AND FOUND TO BE OUT OF LIMITS IAW RE
- [SDR ASOA201100018](https://openairdocs.org/sdr/ASOA201100018), Jan 4, 2011: SILL. CORRODED. CARGO DOOR CUTOUT FLOOR SUPPORT SILL IS CORRODED. REPLACED CARGO DOOR SILL PLATE IAW REO 601R-53-61-1574 & REO 601R-53-61-1574.
- [SDR ASOA201100013](https://openairdocs.org/sdr/ASOA201100013), Jan 3, 2011: FRAME. CRACKED. LT AND RT 718 FRAMES ARE CRACKED BEHIND THE ACM'S. REF MWC CO 7210411, JOB 8721046, OPS 17 AND 18.

All 127: https://openairdocs.org/deregistered/N826AS-2015-02-27/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 20110515018749I](https://openairdocs.org/incident/20110515018749I), May 15, 2011: Canadair CL-600-2B19 (N826AS), Chicago, IL, No damage. A flight attendant suffered a laceration to her forehead when she struck it on a drawer of the beverage cart. She had a headache and was bleeding. The captain…

## Other aircraft with N826AS

- [Registered now](https://openairdocs.org/aircraft/N826AS): Ea Vision EA J100, S/N EAVUAV502585847

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