# N832AS: 1998 Canadair CL-600-2B19, registration cancelled 2016-01-07

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: January 7, 2016
- 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: 7243
- Year built: 1998
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: June 16, 1998
- Certificate issued: May 12, 2004
- Last registry action: January 10, 2014
- Mode S code: AB5FD9
- Owner when cancelled: [U S Bank Na Trustee](https://openairdocs.org/faa-owner/U%20S%20BANK%20NA%20TRUSTEE)
- Location: [Boston, MA](https://openairdocs.org/faa-place/MA/Boston)
- Owner type: Corporation
- Owner's area on the map: 42.3582° N, 71.0519° W: Placed by OpenAirDocs at the center of ZIP code 02110, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N832AS
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=832AS
- Page: https://openairdocs.org/deregistered/N832AS-2016-01-07

From the FAA registry file of October 27, 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 (143, newest 50)

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

- [SDR ASOA2014051410492](https://openairdocs.org/sdr/ASOA2014051410492), May 10, 2014: SIGN. BROKEN. EXIT SIGN IN GALLEY AREA FELL OFF AND IS BROKEN, LIGHT LENS COVERS, INCLUDING EMERGENCY LIGHT. REPLACED THE GALLEY EXIT SIGN IAW AMM 33-51-13, OPS CHECKED GOOD.
- [SDR ASOA2013122709698](https://openairdocs.org/sdr/ASOA2013122709698), Dec 24, 2013: SENSOR. FAILED. GEAR DISAGREE MESSAGE DURING SELECTION OF GEAR UP. COMPLETED WITH QRH, MANUALLY EXTENDED GEAR. NOSE GEAR DID NOT SHOW UP AND LOCKED DURING THE GEAR DISAGREE. AL
- [SDR ASOA2013102309245](https://openairdocs.org/sdr/ASOA2013102309245), Oct 20, 2013: BULKHEAD. CRACKED. BS 202 BULKHEAD IS CRACKED. CUT OUT AND REMOVED ALL CRACKS FROM 202 BULKHEAD AND REMOVED ALL BURRS IAW STEP 1 AND STEP 2 OF REO 601R-53-11-563, REV C. FABRICATE
- [SDR ASOA2013082808913](https://openairdocs.org/sdr/ASOA2013082808913), Aug 26, 2013: HEAT EXCHANGER. DENTED. CLIMBING THROUGHT FL210, ALL AIRFLOW FROM GASPERS STOPPED CABIN STARTED TO SLOWLY CLIMB. WE STARTED A EMERGENCY DESCENT AND RETURN TO DEPARTURE. REPEAT WRITE UP
- [SDR ASOA2013080808850](https://openairdocs.org/sdr/ASOA2013080808850), Aug 5, 2013: LIGHT. INOPERATIVE. RT LOWER EMERGENCY EXIT LIGHT AT EMERGENCY EXIT IS INOPERATIVE. R & R RT LOWER EMERGENCY EXIT LIGHT AT OVERWING EMERGENCY EXIT IAW AMM 33-51-10-400-801. OPS CHE
- [SDR ASOA2013080608836](https://openairdocs.org/sdr/ASOA2013080608836), Jul 19, 2013: ACCESS PANEL. CRACKED. CRACK INDICATION NOTED POSSIBLY CORROSION ON THE LT WING LOWER PLANK ACCESS HOLE LANDING FOR PANEL 550FB, 65 PERCENT FULL SCREEN HEIGHT FAILING NDT. COMPLIED WI
- [SDR ASOA2013080508827](https://openairdocs.org/sdr/ASOA2013080508827), Jul 17, 2013: SKIN. CORRODED. UPPER FUSELAGE ADF ANTENNA CUTOUT HAS FRETTING DAMAGE AROUND CIRCUMFERENCE AND SCREW HOLES APPROX 6" L X .125 W X .005 AT WORST LOCATION. REPAIRED IAW BSC EO CL
- [SDR ASOA2013080908851](https://openairdocs.org/sdr/ASOA2013080908851), Jul 16, 2013: BULKHEAD. CRACKED. FS 621 BULKHEAD, LBL 27.50 FAILS NDT WITH INDICATION 50 PERCENT SCREEN HEIGHT BETWEEN WL 104 AND 110. REPAIRED IAW REO 601R-53-61-1285, REV D DATED 10/31/2011.
- [SDR ASOA2013080808849](https://openairdocs.org/sdr/ASOA2013080808849), Jul 16, 2013: BULKHEAD. CHAFED. FS 621 BULKHEAD HAS SIX CHAFED AREAS AT WL 102: LBL 27.5-RBL 36.20. REPAIRED IAW REO 601R-53-61-2155.
- [SDR ASOA2013080808848](https://openairdocs.org/sdr/ASOA2013080808848), Jul 16, 2013: FLOOR SUPPORT. CORRODED. CARGO COMPARTMENT RT FLOOR SUPPORT HAS MINOR CORROSION AROUND FASTENER HOLES FROM FS 559+80 TO 559+112. COMPLIED WITH REO 601R-53-00-526. REMOVED FLOOR SUPPORT 
- [SDR ASOA2013072508776](https://openairdocs.org/sdr/ASOA2013072508776), Jul 16, 2013: BULKHEAD. CRACKED. FS 621, BULKHEAD RBL 27.50 FAILS NDT WITH INDICATION 50 PERCENT SCREEN HEIGHT AT WL 109 AND 110. REPAIRED IAW REO 601R-53-61-1285, REV D, DATED 10/31/2011.
- [SDR ASOA2013072508775](https://openairdocs.org/sdr/ASOA2013072508775), Jul 16, 2013: BULKHEAD. CRACKED. FS 621 BULKHEAD FAILS NDT RBL 18 WITH INDICATION 50 PERCENT SCREEN HEIGHT WL 123 AND 124. REPAIRED IAW REO 601R-53-61-1285, REV D, DATED 10/31/2011.
- [SDR ASOA2013072508774](https://openairdocs.org/sdr/ASOA2013072508774), Jul 16, 2013: BULKHEAD. CRACKED. FS 621 BULKHEAD FAILS NDT WITH INDICATION 50 PERCENT SCREEN HEIGHT BL 0 BETWEEN WL 109 AND 111. REPAIRED IAW SRM 51-41-04 AND REO 601R-53-61-1285, REV D, DATED 
- [SDR ASOA2013072508773](https://openairdocs.org/sdr/ASOA2013072508773), Jul 16, 2013: BULKHEAD. CRACKED. FS 621 BULKHEAD, LBL 18 FAILS NDT WITH INDICATION 50 PERCENT SCREEN HEIGHT BETWEEN WL 117.5 AND 118.5. REPAIRED IAW SRM 51-42-06, 51-41-04 AND REO 601R-53-61-12
- [SDR ASOA2013072508772](https://openairdocs.org/sdr/ASOA2013072508772), Jul 16, 2013: BULKHEAD. CRACKED. FS 621 BULKHEAD LBL 27.50 FAILS NDT WITH INDICATION FULL SCREEN HEIGHT AT UPPER CARGO TRACK WL 131. REPAIRED IAW SRM 51-42-06 AND REO 601R-53-61-1541, REV D DAT
- [SDR ASOA2013072308750](https://openairdocs.org/sdr/ASOA2013072308750), Jul 16, 2013: ANGLE. CRACKED. FS 280, LBL 9.0 INBD SUPPORT ANGLE CRACKED. REPAIRED IAW SRM 51-42-21, 51-20-06, REO 601R-53-11-726 AND REO 601R-53-11-926.
- [SDR ASOA2013072308749](https://openairdocs.org/sdr/ASOA2013072308749), Jul 16, 2013: SUPPORT ANGLE. CRACKED. FS 621 CARGO DOOR BEAM BOTTOM SUPPORT ANGLE IS CRACKED. REMOVED CRACKED SUPPORT ANGLE IAW SRM 51-42-21. INSTALLED NEW SERVICEABLE BRACKET ANGLE IAW SRM 51-42-21
- [SDR ASOA2013071808724](https://openairdocs.org/sdr/ASOA2013071808724), Jul 16, 2013: LENS. CRACKED. EMERGENCY LIGHT COVER CRACKED. REMOVED AND INSTALLED NEW EMERGENCY LIGHT COVER IAW MM 41-10, 33-60-13.
- [SDR ASOA2013020702970](https://openairdocs.org/sdr/ASOA2013020702970), Feb 4, 2013: LAMP. BURNED OUT. RT EXTERIOR AFT EMERGENCY LIGHT INOP. REPLACED LAMP IAW AMM 33-51-21, OPS CHECK GOOD.
- [SDR ASOA2012082402095](https://openairdocs.org/sdr/ASOA2012082402095), Aug 20, 2012: FAN. FAILED. DISPLAY COOL CAUTION MESSAGE IN FLIGHT. FOLLOWED QRH. WHEN SWITCHING FROM NORMAL TO FLIGHT ALTERNATE SMELLED ELECTRICAL BURNING ODOR FOR 10 SECONDS. RECEIVED OD
- [SDR ASOA2012072001948](https://openairdocs.org/sdr/ASOA2012072001948), Jul 17, 2012: DOOR. BINDING. AIRSTAIR DOOR REQUIRES EXCESSIVE FORCE TO OPEN, DOOR STICKS IN CLOSED POSITION. PERFORMED OPS CHECK ON AIRSTAIR DOOR IAW AMM 52-11-00. OPS CHECKED GOOD. SDR CLO
- [SDR ASOA2012071101885](https://openairdocs.org/sdr/ASOA2012071101885), Jul 5, 2012: BRACKET. UNSERVICEABLE. GEAR DISAGREE WARNING MESSAGE CLIMBING THROUGH 14,000 FT. COMPLETED QRH PROCEDURE. EMERGENCY DECLARED, ACFT RETURNED TO DEPARTURE, LANDED NORMALLY. R & R NLG WO
- [SDR ASOA201201633](https://openairdocs.org/sdr/ASOA201201633), May 10, 2012: HYDRAULIC LINE. DISCONNECTED. ON LANDING, LOST BRAKING, ALL TIRES BLOWN EXCEPT LEFT OTBD. R & R ALL MLG TIRES IAW AMM 32-41-01. FOUND HYD QUICK DISCONETION LINE LOOSE. RESECURED LINE IAW AMM
- [SDR ASOA201200803](https://openairdocs.org/sdr/ASOA201200803), Mar 7, 2012: UNKNOWN. MULTIPLE FAIL. STARTED APU AT 10K AFTER A COUPLE OF MINUTES, TRANSFERED THE BLEEDS TO APU. RECEIVED AN APU OVERTEMP FOLLOWED BY APU FIRE, FOLLOWED BY APU FIRE FAIL, RAN 1A1 CO
- [SDR ASOA201101954](https://openairdocs.org/sdr/ASOA201101954), Oct 12, 2011: STEP. CRACKED. PAX DOOR LOWER STEP IS CRACKED. R & R LOWER PAX DOOR STEP IAW AMM 52-11-04. OP'S CHECKED GOOD.
- [SDR ASOA201101549](https://openairdocs.org/sdr/ASOA201101549), Aug 21, 2011: HANDLE. BINDING. F/A REPORTS PAX DOOR IS HARD TO OPEN DUE TO LATCH STICKING. CYCLED PAX DOOR SEVERAL TIMES NO DEFECTS NOTED AT THIS TIME OPS CHECKED GOOD IAW AMM 52-11-01. OK FO
- [SDR ASOA201101537](https://openairdocs.org/sdr/ASOA201101537), Aug 19, 2011: SIGN. BROKEN. EMERGENCY EXIT SIGN ON MAIN CABIN DOOR BULKHEAD IS BROKEN. R & R EXIT SIGN IAW AMM 33-51-01. OPS CHECKED GOOD.
- [SDR ASOA201101470](https://openairdocs.org/sdr/ASOA201101470), Aug 6, 2011: DOOR. BINDING. MAIN PAX WOULD NOT UNLATCH/OPEN. PERFORMED OPS TEST OF PASSENGER DOOR. DOOR OPS CHECKED GOOD IAW AMM 52-11-05. NO DISCREPANCIES NOTED. ACFT OK FOR SERVICE.
- [SDR ASOA201101407](https://openairdocs.org/sdr/ASOA201101407), Jul 29, 2011: FLOORBEAM. CORRODED. FS 349, SERVICE DOOR FLOOR SUPPORT CORRODED. COMPLY WITH STEPS 3 AND 4 OF REO 601R-53-21-1321. COMPLIED WITH STEP 3 OF REO 601R-53-21-1321. COMPLY WITH STEP 4 O
- [SDR ASOA201101393](https://openairdocs.org/sdr/ASOA201101393), Jul 28, 2011: FLOOR SUPPORT. CORRODED. PAX DOOR FLOOR SUPPORT ANGLE JUST ABOVE SILL CORRODED. FORMED AND BENT PAX DOOR FLOOR SUPPORT ANGLE IAW SRM 51-24-21 AND DWG 601R31527. HEAT TREATED FORMED REPA
- [SDR ASOA201101389](https://openairdocs.org/sdr/ASOA201101389), Jul 27, 2011: FLOOR SUPPORT. CORRODED. SERVICE DOOR ENTRANCE FLOOR SUPPORT ANGLE ABOVE SILL AT FS 349 CORRODED. REPAIRED IAW SRM 51-41-02.
- [SDR ASOA201101332](https://openairdocs.org/sdr/ASOA201101332), Jul 14, 2011: FRAME. CORRODED. CORROSION FOUND AT FS 349 FRAME ON FRONT AND AFT FACE AT S27L. REMOVED CORROSION AND FOUND TO BE WITHIN LIMITS IAW SRM 51-21-06.
- [SDR ASOA201101376](https://openairdocs.org/sdr/ASOA201101376), Jul 11, 2011: DOOR. OUT OF ADJUST. EMERGENCY EXIT DOOR, LT, IS BINDING WHEN OPENING. CHECK DOOR FOR PROPER OPERATION, ADJUST AS REQ. CHECK DOOR FOR PROPER OPERATION, ADJUST AS REQ. FOUND RESISTAN
- [SDR ASOA201101288](https://openairdocs.org/sdr/ASOA201101288), Jul 6, 2011: FLOOR SUPPORT. CORRODED. CORROSION FOUND ON LBL 27 FS 568-621 FLOOR SUPPORT. REMOVED DAMAGED FLOOR SUPPORT IAW SRM 51-42-06, 51-42-20. ITEM 2. FOUND OUT OF LIMITS. INSTALLED FLOOR SUPPO
- [SDR ASOA201101286](https://openairdocs.org/sdr/ASOA201101286), Jul 5, 2011: FLOORBEAM. CRACKED. FS 484 OTBD, RBL27 FLOOR SUPPORT ANGLE CRACKED PREVIOUS REPAIRED ANGLE MK7236. R & R FLOOR SUPPORT ANGLE IAW SRM 51-40-11, 51-42-21. THIS IS A MINOR REPAIR.
- [SDR ASOA201101285](https://openairdocs.org/sdr/ASOA201101285), Jul 5, 2011: FLOORBEAM. CORRODED. FLOOR SUPPORT AT FS 349.00 LT SIDE UNDER PANEL 231CLF CORRODED. CLEAN CORROSION IAW 51-21-06 AND VERIFY LIMITS. REMOVED CORROSION FROM FS 349 CROSSBEAM AT LBL 4
- [SDR ASOA201101284](https://openairdocs.org/sdr/ASOA201101284), Jul 5, 2011: FLOOR SUPPORT. CORRODED. FS 295 OTBD OF LBL 27 FLOOR SUPPORT BOX CORRODED. REMOVED CORROSION IAW SRM 51-21-06. REMOVED DAMAGE EXCEEDS ALLOWABLE LIMITS IAW SRM 53-00-00, FIG 102.
- [SDR ASOA201101283](https://openairdocs.org/sdr/ASOA201101283), Jul 5, 2011: WEB. CRACKED. FS 280 WEB CRACKED AT ALTERNATE EXTENSION PULLY BRACKET. PERFORMED ET INSPECTION IAW NDT INSPECTION PROCEDURES ET-2. ANGLE VERIFIED AS CRACKED. CUT OUT DAMAGED 
- [SDR ASOA201101282](https://openairdocs.org/sdr/ASOA201101282), Jul 5, 2011: WEB. CRACKED. FS 280 WEB CRACKED AT ALTERNATE EXTENSION PULLY BRACKET. PERFORMED ET INSPECTION OF WEB IAW NDT INSPECTION PROCEDURE ET-2. WEB IS VERIFIED AS CRACKED. WEB REPAI
- [SDR ASOA201101281](https://openairdocs.org/sdr/ASOA201101281), Jul 5, 2011: STRUCTURE. CRACKED. FS 280, LBL 9 INBD CLIP CRACKED. REMOVED DAMAGED CLIP, LOCATED AND DRILLED NEW CLIP IAW SRM 51-40-11, 51-42-20. PERFORMED NDI IAW REO 601R-53-11-926, NO INDICAT
- [SDR ASOA201101280](https://openairdocs.org/sdr/ASOA201101280), Jul 5, 2011: STRUCTURE. CRACKED. FS 280, RBL 9 INBD CLIP CRACKED. REMOVED CRACKED CLIP IAW SRM 51-42-20. FABRICATED NEW CLIP IAW REO 601R-53-11-926 NOTE 20. INSTALLED NEW CLIP IAW REO 601R-53-1
- [SDR ASOA201101279](https://openairdocs.org/sdr/ASOA201101279), Jul 5, 2011: STRUCTURE. CRACKED. FS 280, RBL 9 OTBD CLIP CRACKED. REMOVED DAMAGED CLIP IAW SRM 51-42-20. FABRICATED NEW CLIP IAW REO 601R-53-11-926 NOTE 20 IAW EC/TC 601R-53-11-926. PERFORMED N
- [SDR ASOA201101278](https://openairdocs.org/sdr/ASOA201101278), Jul 5, 2011: ANGLE. CORRODED. FS 280 FWD J-ANGLE CORRODED IN FLIGHT DECK DOORWAY. REMOVED J-ANGLE IAW SRM 51-42-06 AND SRM 51-42-21. LOCATED AND DRILLED FASTENER HOLES IN NEW J-ANGLE IAW SRM
- [SDR ASOA201101277](https://openairdocs.org/sdr/ASOA201101277), Jul 5, 2011: ANGLE. CRACKED. FS 280 LT ANGLE CRACKED OTBD OF RBL 27. VERIFY POSSIBLE CRACK (NDT) AND LENGTH. PERFORMED RT INSP IAW MAC NDT INSPECTED PROCEDURE ET-2 NO INDICATIONS NOTED AT T
- [SDR ASOA201101276](https://openairdocs.org/sdr/ASOA201101276), Jul 5, 2011: FLOOR SUPPORT. CORRODED. FLOOR SUPPORT FITTING AT FS 310 BY SERVICE DOOR CORRODED. REMOVED FLOOR SUPPORT IAW SRM 51-42-20. DRILLED & REAMED NEW FLOOR SUPPORT IAW REO 601R-53-21-1332 & A
- [SDR ASOA201101275](https://openairdocs.org/sdr/ASOA201101275), Jul 5, 2011: FLOOR SUPPORT. CORRODED. FS 349 AT SERVICE DOOR FLOOR SUPPORT CORRODED. REMOVED CORROSION IAW SRM 51-21-06. FOUND TO BE OUT OF LIMITS. REPAIRED IAW REO 601R-53-21-1321.
- [SDR ASOA201101274](https://openairdocs.org/sdr/ASOA201101274), Jul 5, 2011: FLOOR SUPPORT. CORRODED. SERVICE DOOR ENTRANCE FLOOR SUPPORT ANGLE ABOVE SILL AT FS 349, CORRODED. REMOVED ANGLE IAW SRM 51-42-06, 51-42-13, 51-42-21. INSTALLED ANGLE IAW SRM 51-42-06 A
- [SDR ASOA201101265](https://openairdocs.org/sdr/ASOA201101265), Jun 30, 2011: CARGO TRACK. CORRODED. 5 CARGO BAY TIE DOWN POINTS ARE CORRODED, 3 AT LBL 27.00 2 AT LBL 9.0. REMOVED CORRODED FTGS (5 PLACES ) AND REPLACED WITH NEW FTGS IAW SRM 51-41-02.
- [SDR ASOA201101259](https://openairdocs.org/sdr/ASOA201101259), Jun 30, 2011: CARGO TRACK. CORRODED. CARGO TRACK AT APPROX FS 574 CORRODED. R & R CARGO TRACK IAW AMM 20-21-00-02 AND 53-01-11-04.
- [SDR ASOA201101248](https://openairdocs.org/sdr/ASOA201101248), Jun 30, 2011: FRAME. CORRODED. FS 319.70 FRAME CORRODED FROM STR 25-27L. R & R FRAME IAW SRM 51-42-06. MAJOR REPAIR.

All 143: https://openairdocs.org/deregistered/N832AS-2016-01-07/reports.md

## FAA accident and incident reports (2)

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 20100402031339I](https://openairdocs.org/incident/20100402031339I), Apr 2, 2010: Canadair CL-600-2B19 (N832AS), Savannah, GA, No damage. Nose door open, and gear disagree warning after gear retraction on takeoff [a/c returned to sav after t/o](landing gear retraction system )
- [Incident 20001212036569I](https://openairdocs.org/incident/20001212036569I), Dec 12, 2000: Cndair CL6002B19 (N832AS), Omaha, NE. (-23) Atlantic southeast airlines flight 4424 returned after departure from Omaha, NE. Due to a cargo door light illumination. The aircraft landed without…

## Other aircraft with N832AS

- [Registered now](https://openairdocs.org/aircraft/N832AS): Ea Vision EA J100, S/N EAVUAV502585850

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