# N825AS: 1997 Canadair CL-600-2B19, registration cancelled 2016-03-29 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: March 29, 2016 - Exported to: Canada - 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: 7207 - Year built: 1997 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: December 5, 1997 - Certificate issued: October 9, 2015 - Last registry action: October 9, 2015 - Mode S code: AB437F - Owner when cancelled: [Wells Fargo Bank Northwest Na Trustee](https://openairdocs.org/faa-owner/WELLS%20FARGO%20BANK%20NORTHWEST%20NA%20TRUSTEE) - Location: [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City) - Owner type: Corporation - Owner's area on the map: 40.7558° N, 111.8843° W: Placed by OpenAirDocs at the center of ZIP code 84111, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N825AS - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=825AS - Page: https://openairdocs.org/deregistered/N825AS-2016-03-29 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 Canadair CL-600-2B19: https://openairdocs.org/model/canadair-cl-600-2b19.md ## Service difficulty reports (154, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR ASOA2014090211175](https://openairdocs.org/sdr/ASOA2014090211175), Aug 29, 2014: DOOR. LACK OF LUBE. PASSENGER DOOR WOULD NOT OPEN. LUBED PASSENGER DOOR AND OPS CHECK IAW AMM 52-11-00. - [SDR ASOA2014030610089](https://openairdocs.org/sdr/ASOA2014030610089), Feb 20, 2014: SKIN. CRACKED. RT FUEL ACCESS PANEL HOLE 640EB HAS MULITPLE INDICATIONS ON THE AFT, INBD & OTBD SIDES 50 PERCENT FCH. FAILED NDT. REMOVED PANEL 640EB FOR INSPECTION IAW AMM 28 - [SDR ASOA2014030610088](https://openairdocs.org/sdr/ASOA2014030610088), Feb 20, 2014: SKIN. CRACKED. LEFT FUEL ACCESS PANEL HOLE 540EB HAS MULTIPLE INDICATIONS ON INBD, OTBD, FWD & AFT SIDES 60 PERCENT FCH. FAILED NDT. COMPLIED WITH EC/TC EO 600-57-81. C/W IAW - [SDR ASOA2014030610087](https://openairdocs.org/sdr/ASOA2014030610087), Feb 20, 2014: SKIN. CRACKED. RIGHT FUEL ACCESS PANEL HOLE 650AB HAS MULTIPLE INDICATIONS ON THE FWD, INBD & OTBD SIDES 50 PERCENT FCH. FAILED NDT. COMPLIED WITH EC/TC EO 600-57-81. C/W IAW - [SDR ASOA2014030610086](https://openairdocs.org/sdr/ASOA2014030610086), Feb 20, 2014: ACCESS PANEL. CRACKED. RIGHT FUEL ACCESS PANEL 640AB HAS MULTIPLE INDICATIONS ON THE AFT SIDE 80 PERCENT FCH. FAILED NDT. REMOVED PANEL 640AB FOR INSPECTION IAW AMM 25-11-01-000-802. - [SDR ASOA2014030610085](https://openairdocs.org/sdr/ASOA2014030610085), Feb 20, 2014: SKIN. CORRODED. RIGHT FUEL ACCESS PANEL HOLE 610AB HAS MULTIPLE INDICATIONS ON INBD 7 FWD SIDE 50 PERCENT FCH. FAILED NDT. COMPLIED WITH EC/TC EO 600-57-81. C/W IAW REO 601R-57 - [SDR ASOA2014030610084](https://openairdocs.org/sdr/ASOA2014030610084), Feb 20, 2014: SKIN. CRACKED. RIGHT FUEL ACCESS PANEL HOLE 650CB HAS MULTIPLE INDICATIONS, GROUND THE ENTIRE CIRCUMFERENCE 70 PERCENT FCH. FAILED NDT. COMPLIED WITH EC/TC EO 600-57-81. - [SDR ASOA2014030610083](https://openairdocs.org/sdr/ASOA2014030610083), Feb 20, 2014: SKIN. CRACKED. LT FUEL ACCESS PANEL HOLE 550CB HAS MULTIPLE INDICATIONS ON INBD 78 FWD SIDE 5 PERCENT FCH. FAILED NDT. COMPLIED WITH EC/TC EO 600-57-81. - [SDR ASOA2014030610082](https://openairdocs.org/sdr/ASOA2014030610082), Feb 20, 2014: SKIN. CRACKED. RT FUEL ACCESS PANEL HOLE 650DB HAS MULTIPLE INDICATIONS ON THE OTBD SIDE 70 PERCENT FCH. FAILED NDT. COMPLIED WITH EC/TC EO 600-57-81. C/W IAW REO 601R-57-21-0 - [SDR ASOA2014030610081](https://openairdocs.org/sdr/ASOA2014030610081), Feb 19, 2014: STRAP. CORRODED. PASSENGER DOOR CUTOUT AT FS 349 BETWEEN STRINGERS 3-4L, THE UPPER INNER FRAME STRAP IS CORRODED. FABBED FRAME STRAP IAW EO DWG SNIEO 600-31153 FROM 7075-T6 PO 7 - [SDR ASOA2014030610080](https://openairdocs.org/sdr/ASOA2014030610080), Feb 19, 2014: SKIN. CRACKED. RT WING ACCESS PANEL HOLE 640CB HAS MULTIPLE INDICATIONS ON THE RT SIDE 50 PERCENT FSH FAILED NDT. COMPLIED WITH EC/TC EO 600-57-81. C/W IAW REO 601R-57-21-030 - [SDR ASOA2014030610079](https://openairdocs.org/sdr/ASOA2014030610079), Feb 19, 2014: SKIN. CRACKED. RIGHT WING ACCESS PANEL HOLE 640FB HAS MULTIPLE INDICATIONS ON THE INBD SIDE 60 PERCENT FSH FAILED NDT. COMPLIED WITH EC/TC EO600-57-81. C/W IAW REO:601R-57-21- - [SDR ASOA2014030610078](https://openairdocs.org/sdr/ASOA2014030610078), Feb 19, 2014: SKIN. CRACKED. LT WING ACCESS PANEL HOLE 540FB HAS MULTIPLE INDICATIONS ON THE OTBD SIDE 50 PERCENT FSH FAILED NDT. COMPLIED WITH EC/TC EO 600-57-81. C/W IAW REO 601R-57-21-03 - [SDR ASOA2014030610077](https://openairdocs.org/sdr/ASOA2014030610077), Feb 14, 2014: ANGLE. CRACKED. LBL 27, BS 484 INBD ANGLE IS CRACKED. R & R IAW SRM 51-42-21 AND SRM 51-42-06. - [SDR ASOA2014030610076](https://openairdocs.org/sdr/ASOA2014030610076), Feb 14, 2014: ANGLE. CRACKED. RBL 27, BS 484 ANGLE IS CRACKED. R & R ANGLE IAW SRM 51-42-06 AND SRM 51-42-21. - [SDR ASOA2014030510071](https://openairdocs.org/sdr/ASOA2014030510071), Feb 14, 2014: ANGLE. CRACKED. RBL 36, BS 484.00, ANGLE CRACKED. R & R ANGLE IAW REO 601R-53-41-059 AND REO 601R-53-41-059, REV B. - [SDR ASOA2014030510070](https://openairdocs.org/sdr/ASOA2014030510070), Feb 14, 2014: SKIN. CRACKED. RIGHT BOOST PUMP CUTOUT HAS MULTIPLE INDICATIONS ALL AROUND THE VERTICAL & HORIZ LANDING, 50 PERCENT FSH FAILED NDT. COMPLIED WITH REO: 601R-57-21-2124. - [SDR ASOA2014030510069](https://openairdocs.org/sdr/ASOA2014030510069), Feb 12, 2014: FLOOR PANEL. CORRODED. TWO AREAS ON LT FLOOR PANEL ARE BEYOND MAXIMUM BLEND DEPTH LIMITS OF REO 601R-53-41-666, SUBSECTION 1.1 AND TABLE 1, REV.C 2012-11-06. C/W REO 601R-53-41-1777 F - [SDR ASOA2014030510068](https://openairdocs.org/sdr/ASOA2014030510068), Feb 11, 2014: POST. CRACKED. FOUND FS 409.00+128 VERTICAL POST RBL 18.0 INBD SIDE HAS INDICATION NOTED AT AFT FLANGE RADIUS APPROX .300" LONG 60 PERCENT FSH. FAILED NDT INSPECTION. REMOVED, - [SDR ASOA2014030510067](https://openairdocs.org/sdr/ASOA2014030510067), Feb 11, 2014: ISOLATOR. CRACKED. FOUND REAR PRESSURE BULKHEAD ISOLATORS CRACKED AT LBL 27.50 AND LBL 9.50, WL 98. REMOVED UNSERVICEABLE ISOLATOR MOUNTS IAW SRM 51-42-13. INSTALLED 2 EA NEW ISOL - [SDR ASOA2014030510066](https://openairdocs.org/sdr/ASOA2014030510066), Feb 11, 2014: ANGLE. CRACKED. CARGO DOOR SUPPORT BEAM LOWER AFT ANGLE CRACKED APPROX 0.3" WIDE. R & R ANGLE ON CARGO DOOR SUPPORT BEAM IAW SRM 51-42-21. - [SDR ASOA2014030510065](https://openairdocs.org/sdr/ASOA2014030510065), Feb 11, 2014: BULKHEAD. CRACKED. FOUND REAR PRESSURE BULKHEAD WEB HAS MULTIPLE CRACK INDICATIONS NOTED AT LBL 0, WL 91-48 APPROX 7 INCHES, AREA 50 PERCENT FSH, FAILED NDT INSPECTION. REPAIRED I - [SDR ASOA2014030510064](https://openairdocs.org/sdr/ASOA2014030510064), Feb 11, 2014: BULKHEAD. CRACKED. FOUND REAR PRESSURE BULKHEAD WEB HAS A CRACK INDICATION NOTED AT LBL 36.20, WL 79.0 APPROX .6 INCHES IN LENGTH 100 PERCENT FSH FAILED NDT INSPECTION. COMPLIED W - [SDR ASOA2014030510063](https://openairdocs.org/sdr/ASOA2014030510063), Feb 10, 2014: STRINGER. CRACKED. STRINGER 3L CRACKED APPROX 0.70" LONG AT BS 280.8. REPAIRED IAW SRM 51-42-06. REPAIRED IAW SNIEO 601R-31522. - [SDR ASOA2014030510062](https://openairdocs.org/sdr/ASOA2014030510062), Feb 8, 2014: FINGER DOUBLER. CORRODED. FINGER DOUBLERS CORRODED IN MULTIPLE AREAS FS 409+128 - 559. COMPLIED WITH EC/TC REO 601R-53-41-666-01 AND REO 601R-53-41-666, REV C. REPAIRED IAW REO 601R-53-5 - [SDR ASOA2014030510061](https://openairdocs.org/sdr/ASOA2014030510061), Feb 8, 2014: SKIN. CORRODED. SKIN & FINGER DOUBLERS HAVE CORROSION IN MULTIPLE AREAS BS 409+128-559. COMPLIED WITH EC/TC REO 601R-53-41-66601 AND REO 601R-53-41-666, REV C. - [SDR ASOA2014030510060](https://openairdocs.org/sdr/ASOA2014030510060), Feb 8, 2014: CARGO TRACK. CORRODED. CARGO TRACK RBL 9 BS 559+80-574 CORRODED. R & R CARGO TRACK IAW AMM 53-01-11-000-802, AMM 53-01-11-400-802, AMM 53-01-11-400-802 AND REO 601R-53-00-485, REV. - [SDR ASOA2014030510059](https://openairdocs.org/sdr/ASOA2014030510059), Feb 8, 2014: CARGO TRACK. CORRODED. CARGO TRACK LBL 9, BS 559+80-621 CORRODED. R & R CARGO TRACK IAW AMM 53-01-11-000-802, AMM 53-01-11-400-802 AND REO NR 601R-53-00-485, REV. - [SDR ASOA2014030510058](https://openairdocs.org/sdr/ASOA2014030510058), Feb 8, 2014: FLOOR SUPPORT. CORRODED. FLOOR SUPPORT AT LBL 27, BS 574-621 CORRODED. REMOVED FLOOR SUPPORT IAW SRM 51-42-21, 51-42-20 & 51-42-06. INSTALLED NEW FLOOR SUPPORT IAW REO 601R-53-61-3778, - [SDR ASOA2014030510057](https://openairdocs.org/sdr/ASOA2014030510057), Feb 8, 2014: FLOOR SUPPORT. CORRODED. FLOOR SUPPORT AT RBL 45 IS CORRODED FROM BS 559+80 - 574. REPAIRED IAW SRM 51-42-06 & 51-42-21 AND IAW REO 601R-53-00-526. - [SDR ASOA2013121309645](https://openairdocs.org/sdr/ASOA2013121309645), Dec 10, 2013: LIGHT. MISSING. SHORT PORTION OF EMERGENCY LIGHT AT 18B MISSING. SECURED EMERGENCY LIGHT IAW AMM 33-51-01. NO FURTHER DEFECTS NOTED. - [SDR ASOA201201095](https://openairdocs.org/sdr/ASOA201201095), Mar 29, 2012: CONNECTOR. LOOSE. CLIMBING THROUGH FL 220, RECEIVED RT ENGINE OIL PRESSURE WARNING WITH OIL PRESSURE AT 15 PSI. OIL TEMPERATURE WAS NORMAL OIL PRESS READ NORMAL AFTER DESCENT. (A - [SDR ASOA201201078](https://openairdocs.org/sdr/ASOA201201078), Mar 29, 2012: SCAVENGE PUMP. FAILED. RIGHT ENGINE OIL PRESSURE MASTER CAUTION AT 18000 FT. EMERGENCY DECLARED. R & R RT LUBE AND SCAVENGE PUMP IAW AMM 79-21-01. LEAK AND OPS CHECKED GOOD. - [SDR ASOA201200502](https://openairdocs.org/sdr/ASOA201200502), Feb 15, 2012: FLOOR SUPPORT. CORRODED. SERVICE DOOR SILL FLOOR SUPPORT ANGLE CORRODED. REPAIRED IAW AMM 20-21-00-910-001 AND 20-24-00-910-802. - [SDR ASOA201200436](https://openairdocs.org/sdr/ASOA201200436), Feb 8, 2012: ANGLE. CRACKED. NLG CUTOUT CORNERS CRACKED AFT OF FOLLOW -UP DOOR HINGES (RADIUS). REPAIRED IAW REO 601R-53-11-0048 IAW 601R-53-11-0048, REV C. - [SDR ASOA201200546](https://openairdocs.org/sdr/ASOA201200546), Feb 6, 2012: ANGLE. CORRODED. SERVICE DOOR SILL FWD UPPER ANGLE CORRODED. R & R CORRODED ANGLE IAW DWG NR 601R38303. - [SDR ASOA201200412](https://openairdocs.org/sdr/ASOA201200412), Feb 6, 2012: SEAT TRACK. CORRODED. SEAT TRACK FS 394 TO 409+128 AT RBL 9.0 HAS CORROSION DAMAGE. SEAT TRACK IS OUT OF LIMITS IAW SRM 53-21-49, FIG 101. R & R SEAT TRACK IAW AMM 53-01-11-000-802 A - [SDR ASOA201200410](https://openairdocs.org/sdr/ASOA201200410), Feb 6, 2012: SEAT TRACK. CORRODED. SEAT TRACK FS 409+128 TO 559.0 AT RBL 9.0 HAS CORROSION DAMAGE. SEAT TRACK IS OUT OF LIMITS IAW SRM 51-21-49, FIG 101. R & R SEAT TRACK IAW AMM 53-01-11-000-807 - [SDR ASOA201200408](https://openairdocs.org/sdr/ASOA201200408), Feb 6, 2012: ATTACH ANGLE. CRACKED. ATTACH ANGLE CRACKED AFT EQUIPMENT BAY RT SIDE AT PRESSURE BULKHEAD ABOUT 12 INCHES BELOW ENGINE SUPPORT BEAM. REMOVED CRACKED ATTACH ANGLE IAW SRM 51-42-06. IN - [SDR ASOA201200406](https://openairdocs.org/sdr/ASOA201200406), Feb 6, 2012: ATTACH ANGLE. CRACKED. ATTACH FITTING CRACKED AFT EQUIPMENT BAY LT SIDE AT PRESSURE BULKHEAD ABOVE ENGINE SUPPORT BEAM. REMOVED CRACKED ATTACH ANGLE IAW SRM 51-42-06. LOCATED SERVICEA - [SDR ASOA201200398](https://openairdocs.org/sdr/ASOA201200398), Feb 3, 2012: SEAT TRACK. CORRODED. SEAT TRACK FS 364 TO 396 AT RBL 9.0 HAS CORROSION DAMAGE. SEAT TRACK OUT OF LIMITS IAW SRM 53-21-49, FIG 101. REMOVED SEAT TRACK IAW AMM 53-01-11-000-802. INSTA - [SDR ASOA201200396](https://openairdocs.org/sdr/ASOA201200396), Feb 3, 2012: SEAT TRACK. CORRODED. SEAT TRACK FS 364-396 AT LBL 9.0 HAS CORROSION DAMAGE. SEAT TRACK FOUND OUT OF LIMITS IAW SRM 53-21-49, FIG 101. R & R SEAT TRACK IAW AMM 53-01-11-000-802 & AMM - [SDR ASOA201200394](https://openairdocs.org/sdr/ASOA201200394), Feb 3, 2012: SUPPORT ANGLE. CORRODED. SERVICE DOOR SILL FLOOR SUPPORT ANGLE CORRODED. REMOVED CORROSION IAW SRM 51-26-00. .031" OF MATERIAL REMOVED- .026" MATERIAL REMAINING. REMOVED SILL SUPPORT AN - [SDR ASOA201200392](https://openairdocs.org/sdr/ASOA201200392), Feb 3, 2012: FLOORBEAM. CORRODED. FLOORBEAM FS 280 HAS CORROSION DAMAGE. REMOVED CORROSION IAW SRM 51-21-06. REMOVED FLOORBEAM ANGLE IAW SRM 51-42-06. DRILLED NEW ANGLE IAW SRM 51-40-11. - [SDR ASOA201200390](https://openairdocs.org/sdr/ASOA201200390), Feb 3, 2012: FLOORBEAM. CORRODED. CORROSION AROUND NUTPLATE ON FS 280.00 FLOORBEAM. REMOVED CORROSION IAW SRM 51-21-06. PERFORMED UT THICKNESS INSPECTION IAW MAC NDT PRODCEDURES UT-3. MIN MATERI - [SDR ASOA201200388](https://openairdocs.org/sdr/ASOA201200388), Feb 3, 2012: SEAT TRACK. CORRODED. SHORT SEAT TRACK BETWEEN FLOOR PANELS 281BLF AND 281FRF HAS CORROSION. SEAT TRACK FOUND OUT OF LIMITS IAW SRM 53-61-49. REMOVED AND REPLACED SEAT TRACK IAW AMM - [SDR ASOA201200386](https://openairdocs.org/sdr/ASOA201200386), Feb 3, 2012: SEAT TRACK. CORRODED. SHORT SEAT TRACK HAS CORROSION AT LBL9 BETWEEN FLOOR PANEL 281HLF AND 281BLF. SEAT TRACK FOUND OUT OF LIMITS IAW SRM 53-61-49, FIG 101. R & R SEAT TRACK IAW AMM - [SDR ASOA201200384](https://openairdocs.org/sdr/ASOA201200384), Feb 3, 2012: SEAT TRACK. CORRODED. SEAT TRACK HAS CORROSION AT RBL 9 AT 9G BULKHEAD. SEAT TRACK FOUND OUT OF LIMITS IAW SRM 53-21-49, FIG 101. R & R SEAT TRACK IAW AMM 53-01-11-000-802 AND AMM 53 - [SDR ASOA201200382](https://openairdocs.org/sdr/ASOA201200382), Feb 3, 2012: ATTACH FITTING. CRACKED. RIGHT FS 484 PRESSURE FLOOR INTERCOSTAL HAS CRACKED ATTACH FITTING AT RBL 27.0. REMOVED DAMAGED ANGLE IAW SRM 51-42-06. INSTALLED NEW ANGLE IAW SRM AND DWG NR 6 - [SDR ASOA201200380](https://openairdocs.org/sdr/ASOA201200380), Feb 3, 2012: ATTACH FITTING. CRACKED. LEFT FS 484 PRESSURE FLOOR INTERCOSTAL HAS CRACKED ATTACH FITTING AT LBL 27.0. REMOVED AND INSTALLED NEW ATTACH FITTING IAW SRM 51-42-21. All 154: https://openairdocs.org/deregistered/N825AS-2016-03-29/reports.md ## Other aircraft with N825AS - [Registered now](https://openairdocs.org/aircraft/N825AS): Ea Vision EA J100, S/N EAVUAV502585846 --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.