# N842AS: 1999 Bombardier CL-600-2B19, registration cancelled 2019-02-25 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: February 25, 2019 - Exported to: Mexico - 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: 7304 - Year built: 1999 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: April 15, 1999 - Certificate issued: June 12, 2018 - Last registry action: June 12, 2018 - Mode S code: AB8758 - Owner when cancelled: [Frontera Flight Holdings Inc](https://openairdocs.org/faa-owner/FRONTERA%20FLIGHT%20HOLDINGS%20INC) - Location: [Dover, DE](https://openairdocs.org/faa-place/DE/Dover) - Owner type: Corporation - Owner's area on the map: 39.1815° N, 75.4736° W: Placed by OpenAirDocs at the center of ZIP code 19901, within about 5 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N842AS - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=842AS - Page: https://openairdocs.org/deregistered/N842AS-2019-02-25 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 Bombardier CL-600-2B19: https://openairdocs.org/model/bombardier-cl-600-2b19.md ## Service difficulty reports (201, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR ASOA2015060112960](https://openairdocs.org/sdr/ASOA2015060112960), May 28, 2015: HANDLE. LACK OF LUBE. "PAX DOOR STOW", CAUTION MESSAGE AND DOOR WILL NOT OPEN FROM INSIDE OR OUTSIDE AT GATE. TESTED MAIN PAX DOOR. LUBRICATED OUTER HANDLE, DOOR OPS CHECKS OK IAW AM - [SDR ASOA2015022712312](https://openairdocs.org/sdr/ASOA2015022712312), Feb 26, 2015: DOOR. NONE. MAIN AIRSTAIR DOOR WAS HARD TO OPEN ON. PERFORMED OPS CHECK OF MAIN PAX DOOR IAW AMM 52-10-00. NO DEFECTS FOUND. OUTER HANDLES FLUSH. INNER MARKINGS LINE UP. - [SDR ASOA2015022512271](https://openairdocs.org/sdr/ASOA2015022512271), Feb 21, 2015: DOOR. NONE. PAX DOOR WILL NOT OPEN, OPENED PAX DOOR ALL CHECKS GOOD IAW AMM 52-11-00. - [SDR ASOA2014112611791](https://openairdocs.org/sdr/ASOA2014112611791), Nov 21, 2014: SKIN. DAMAGED. AFT SKIN AT BS 640 - 755 STR 20L-20R, FOUND CRACKED, BUCKLED, DENTED AND DEFORMED. - [SDR ASOA2014061810678](https://openairdocs.org/sdr/ASOA2014061810678), Jun 14, 2014: LIGHT. DAMAGED. FLOOR LEVEL EMERGENCY FLOODLIGHT AT GALLEY DAMAGED. R & R FLOODLIGHT IAW AMM 33-51-19. SYSTEM OPS CHECKED GOOD. - [SDR ASOA2014042910417](https://openairdocs.org/sdr/ASOA2014042910417), Apr 18, 2014: ISOLATOR. CRACKED. LT LOWER SIDE OF AFT PRESSURE BULKHEAD HAS TWO BAD ISOLATORS CRACKED. INSTALLED NEW ISOLATORS IAW SRM 51-42-13. - [SDR ASOA2014042910416](https://openairdocs.org/sdr/ASOA2014042910416), Apr 18, 2014: WIRE. BROKEN. EMERGENCY LIGHT IS INOPERATIVE, AFT INBD. FOUND TWO WIRES ON LAMP ASSY BROKEN. REPAIRED WIRES IAW 0ESPM 20-16-00. PERFORMED OPS TEST OF EMERGENCY LIGHTING IAW 0 - [SDR ASOA2014042910412](https://openairdocs.org/sdr/ASOA2014042910412), Apr 12, 2014: ACCESS PANEL. CRACKED. CRACK DISCOVERED ON ON RT WING LOWER PLANK, T/E AT WS 119.58 REMOVED UPPER & LOWER SKIN AND LOWER ACCESS PANELS IAW SRM 57-42-06 & 51-42-10. MAJOR REPAIR. - [SDR ASOA2014042910411](https://openairdocs.org/sdr/ASOA2014042910411), Apr 9, 2014: ANGLE. CRACKED. RT ANGLE BRACKET AT AFT FUSELAGE S13AR, FS 261 HAS CRACK AT LOWER AFT RIVET HOLE, MARKED W/TAPE. R & R RT ANGLE BRACKET AT AFT FUSELAGE STR 15A, FS 261 IAW SRM - [SDR ASOA2014042910410](https://openairdocs.org/sdr/ASOA2014042910410), Apr 9, 2014: ANGLE. CRACKED. LT ANGLE BRACKET AT AFT FUSELAGE S15L, FS 261 HAS CRACK AT LOWER AFT RIVET HOLE. REMOVED ANGLE BRACKET IAW SRM 51-42-06. INSTALLED ANGLE BRACKET IAW SRM 51-42-0 - [SDR ASOA2014042910409](https://openairdocs.org/sdr/ASOA2014042910409), Apr 7, 2014: SEAT TRACK. CORRODED. CORROSION ON LBL 9 SEAT TRACK BS 559 - 559+80. FOUND TO BE OUT OF LIMIT IAW SRM 51-21-00. REMOVED SEAT TRACK IAW SRM 51-41-02. INSTALLED SEAT TRACK IAW AMM 53-0 - [SDR ASOA2014042910408](https://openairdocs.org/sdr/ASOA2014042910408), Apr 7, 2014: SEAT TRACK. CORRODED. CORROSION ON LBL 9, SEAT TRACK BS 394 - 409+128. FOUND TO BE OUT OF LIMITS IAW SRM 53-21-49. R & R SEAT TRACK IAW AMM 53-01-1-000-802 AND 53-01-11-400-802. - [SDR ASOA2014042910407](https://openairdocs.org/sdr/ASOA2014042910407), Apr 7, 2014: SEAT TRACK. CORRODED. CORROSION ON RBL 9, SEAT TRACK BS 394 - 409+128. FOUND TO BE OUT OF LIMITS IAW SRM 53-21-49. REMOVED CORRODED SEAT TRACK IAW AMM 53-01-11-000-802. INSTALLED NEW - [SDR ASOA2014042910406](https://openairdocs.org/sdr/ASOA2014042910406), Apr 7, 2014: SEAT TRACK. CORRODED. CORROSION ON LBL 9, SEAT TRACK BS 364-409. FOUND TO BE OUT OF LIMITS IAW SRM 53-21-49. REMOVED CORRODED SEAT TRACK IAW SRM 53-01-11-000-802. INSTALLED NEW SEAT - [SDR ASOA2014042910405](https://openairdocs.org/sdr/ASOA2014042910405), Apr 7, 2014: FLOOR SUPPORT. CORRODED. CORROSION ON RT FLOOR SUPPORT BETWEEN BS 295 - 310. REPAIRED FLOOR SUPPORT BETWEEN BS 280 & 409+128 IAW REO 601R-53-00-530. - [SDR ASOA2014042910404](https://openairdocs.org/sdr/ASOA2014042910404), Apr 7, 2014: SEAT TRACK. CORRODED. CORROSION ON RBL 9 SEAT TRACK BS 364 - 394, R & R SEAT TRACK IAW AMM 53-01-11-000-802 AND 53-01-11-400-802. - [SDR ASOA2014042910403](https://openairdocs.org/sdr/ASOA2014042910403), Apr 7, 2014: STRUCTURE. CRACKED. PAX DOOR EDGE MEMBER CRACKED AT FWD LOCATION. COMPLIED WITH EC/TC REO 601R-52-11-279 IAW REO 601R-52-11-279. - [SDR ASOA2014042910402](https://openairdocs.org/sdr/ASOA2014042910402), Apr 6, 2014: FRAME. CORRODED. FRAME CRACKED AT BS 338 TOP OF DOOR. COMPLIED WITH REO 601R-52-11-402 FOR REPAIR. MAJOR REPAIR. - [SDR ASOA2014042910401](https://openairdocs.org/sdr/ASOA2014042910401), Apr 6, 2014: FRAME. CRACKED. FRAME CRACKED AT BS 320.10, TOP OF DOOR. COMPLIED WITH REO 601R-52-11-402 FOR REPAIR. MAJOR REPAIR. - [SDR ASOA2014042910400](https://openairdocs.org/sdr/ASOA2014042910400), Apr 6, 2014: ISOLATOR. BROKEN. BROKEN ISOLATER ON REAR PRESSURE BULKHEAD. R & R BROKEN ISOLATOR ON REAR PRESSURE BULKHEAD IAW SRM 51-42-13. - [SDR ASOA2014042910399](https://openairdocs.org/sdr/ASOA2014042910399), Apr 5, 2014: SEAT TRACK. CORRODED. LEFT SEAT TRACK SEGMENT CORRODED IN TWO SPOTS, BS 552 -559+24. FOUND OUT OF LIMITS IAW SRM 53-41-49. R & R SIDE SEAT TRACK IAW AMM 53-01-011-000/400-802 AND EC/ - [SDR ASOA2014042910398](https://openairdocs.org/sdr/ASOA2014042910398), Apr 5, 2014: SEAT TRACK. CORRODED. LT SIDE SEAT TRACK SEGMENT AT FS 409.20. SEAT TRACK FOUND OUT OF LIMITS IAW SRM 53-31-49, PAGE 101. COMPLETED FABRICATION OF REPAIR SECTION INSTALLED REPAIR IAW - [SDR ASOA2014042910397](https://openairdocs.org/sdr/ASOA2014042910397), Apr 5, 2014: SEAT TRACK. CORRODED. LEFT SEAT TRACK SEGMENT IS CORRODED AT BS 400. REMOVED DAMAGED SEAT TRACK IAW AMM 53-01-11-0000-802 FROM BS 364 - 409+16. INSTALLED NEW SEAT TRACK IAW AMM 53-01 - [SDR ASOA2014042910396](https://openairdocs.org/sdr/ASOA2014042910396), Apr 4, 2014: LIGHT. INOPERATIVE. EMERGENCY LIGHT ON RT SIDE FROM 1-6 SEATS IS INOPERATIVE. REPLACED EMERGENCY LIGHT IAW CMM 33-60-13. - [SDR ASOA2014042910395](https://openairdocs.org/sdr/ASOA2014042910395), Apr 4, 2014: WIRE. BROKEN. EMERGENCY LIGHT ON FWD WARDROBE HAS A BROKEN WIRE. REPAIRED BROKEN WIRE IAW ESPM 20-17-10. PERFORMED OPS TEST OF THE EMERGENCY LIGHTING IAW AMM 33-1-00-710-801, - [SDR ASOA2014022810042](https://openairdocs.org/sdr/ASOA2014022810042), Feb 27, 2014: LAMP. BURNED OUT. CABIN CEILING NR 3 EMERGENCY LIGHT INOPERATIVE. REPLACED LAMPS IAW AMM 33-51-16. OPS CHECKED GOOD. - [SDR ASOA2013042603450](https://openairdocs.org/sdr/ASOA2013042603450), Apr 22, 2013: BATTERY PACK. DISCHARGED. EMERGENCY LIGHTS INOPERATIVE. CHARGED BATTERY PACKS. OPS CHECKED OK IAW AMM 33-51-00. - [SDR ASOA201201275](https://openairdocs.org/sdr/ASOA201201275), Apr 6, 2012: RIB. CRACKED. LEFT HORIZONTAL STAB ANGLE AND STRAP UNDER UPPER SURFACE OF STAB TIP FAIRING HAS LIGHTNING STRIKE DAMAGE. ON INSTALLATION OF UPPER ANGLE, FOUND A CRACKED NR 9 R - [SDR ASOA201201261](https://openairdocs.org/sdr/ASOA201201261), Apr 3, 2012: FLOOR SUPPORT. CORRODED. PAX DOOR THRESHOLD FLOOR SUPPORT HAS MINOR CORROSION. REMOVED AND REPLACED IAW SRM 51-42-06, 51-42-13 AND 51-42-21. - [SDR ASOA201201141](https://openairdocs.org/sdr/ASOA201201141), Apr 3, 2012: FLOORBEAM. CORRODED. CORROSION ON FLOORBEAM AT LBL 35 ON FS 349. TREATED AND REFINISHED BLEND AREAS IAW SRM 51-21-06, STEP 3D. - [SDR ASOA201201139](https://openairdocs.org/sdr/ASOA201201139), Apr 3, 2012: WEB. CORRODED. RIGHT PRESSURE FLOOR SILL PANEL AND SILL ANGLES HAVE NUMEROUS AREAS OF CORROSION BETWEEN FS 409+128 AND 559. BLENDED CORROSION IAW REO 601R-53-41-666. FOUND OUT - [SDR ASOA201201137](https://openairdocs.org/sdr/ASOA201201137), Apr 3, 2012: WEB. CORRODED. LEFT PRESSURE FLOOR SILL PANEL AND SILL ANGLES HAVE NUMEROUS AREAS OF CORROSION BETWEEN FS 409+128 AND 559. BLENDED OUT AREAS OF CORROSION IAW REO 601R-53-41-66 - [SDR ASOA201201135](https://openairdocs.org/sdr/ASOA201201135), Apr 3, 2012: FLOOR SUPPORT. CORRODED. AFT LOWER FLOOR SUPPORT ANGLE IS CORRODED. R & R AFT LOWER FLOOR SUPPORT ANGLE IAW SRM 51-42-21. REPAIR CLASSIFIED AS MINOR. - [SDR ASOA201201133](https://openairdocs.org/sdr/ASOA201201133), Apr 3, 2012: FLOORBEAM. CORRODED. CORROSION ON FLOORBEAM AT LBL 35 ON FS 349. REMOVED CORROSION IAW SRM 51-21-06, STEP 3D. FOUND OUT OF LIMITS IAW SRM 53-00-00, FIG 102. REPLACED IAW SRM 51-40-1 - [SDR ASOA201201115](https://openairdocs.org/sdr/ASOA201201115), Apr 2, 2012: FLOOR SUPPORT. CRACKED. LEFT AND RIGHT FWD EQUIPMENT BAY FLOOR SUPPORT AT FS 193.00 IS CRACKED APPROX .5L. REPAIRED IAW REO 601R-53-11-245, REV B. - [SDR ASOA201201097](https://openairdocs.org/sdr/ASOA201201097), Mar 29, 2012: GLOWSTRIP. MISSING. 232EZ AFT PHOTOLUMINESCENT STRIP MISSING. INSTALLED NEW PHOTOLUMINESCENT STRIP IAW AMM 11-30-00-400-801. - [SDR ASOA201201088](https://openairdocs.org/sdr/ASOA201201088), Mar 29, 2012: ISOLATOR. CRACKED. THREE ISOLATORS ON BS 621 BULKHEAD ARE CRACKED. R & R ISOLATORS IAW SRM 51-42-13. - [SDR ASOA201201086](https://openairdocs.org/sdr/ASOA201201086), Mar 29, 2012: SUPPORT. CRACKED. FS 484.00, LBL 27.00 VERTICAL SUPPORT CRACKED. R & R VERTICAL SUPPORT CLIP IAW SRM 51-42-21. - [SDR ASOA201201084](https://openairdocs.org/sdr/ASOA201201084), Mar 29, 2012: FLOORBEAM. CRACKED. FS 484.00, RBL 27 AND RBL 36 FLOORBEAM CRACKED. R & R IAW SRM 51-42-21. - [SDR ASOA201201082](https://openairdocs.org/sdr/ASOA201201082), Mar 29, 2012: SUPPORT BRACKET. CRACKED. PILOT WINDSHIELD SIDE POST AFT LOWER SUPPORT BRACKET CRACKED. REMOVED CRACKED PILOT WINDSHIELD AFT LOWER POST BRACKET. FIT, DRILLED AND INSTALLED NEW BRACKET IA - [SDR ASOA201201080](https://openairdocs.org/sdr/ASOA201201080), Mar 29, 2012: SUPPORT BRACKET. CRACKED. CO-PILOT WINDSHIELD SIDE POST AFT LOWER SUPPORT BRACKET CRACKED. R & R LOWER AFT WINDSHIELD POST BRACKET IAW SRM 51-42-20. - [SDR ASOA201201074](https://openairdocs.org/sdr/ASOA201201074), Mar 28, 2012: SKIN. CORRODED. FUSELAGE SKIN CORRODED BETWEEN FS 559+80 TO FS 559+112 AT STR 23R. REMOVED LIGHT CORROSION IAW SRM 51-21-06. - [SDR ASOA201201072](https://openairdocs.org/sdr/ASOA201201072), Mar 28, 2012: SKIN. CORRODED. FUSELAGE SKIN HAS AREA OF CORROSION AT FS 559 +112 AT STR 24R. REMOVED LIGHT CORROSION IAW SRM 51-21-06. - [SDR ASOA201201070](https://openairdocs.org/sdr/ASOA201201070), Mar 28, 2012: SKIN. CORRODED. FUSELAGE EXTERNAL SKIN HAS AREA OF CORROSION AT STR 24R AT BS 559.00 +112. REMOVED LIGHT CORROSION IAW SRM 51-21-06. - [SDR ASOA201201068](https://openairdocs.org/sdr/ASOA201201068), Mar 28, 2012: POST. CRACKED. FS 409+128 VERTICAL POST BL 0 FAILS NDT WITH A CRACK INDICATION IN LT AFT RADIUS OF POST WITH AN INDICATION GREATER THAN 50 PERCENT SCREEN HEIGHT APPROX .2 LONG - [SDR ASOA201201259](https://openairdocs.org/sdr/ASOA201201259), Mar 27, 2012: FLOOR SUPPORT. CORRODED. PAX DOOR THRESHOLD VERTICAL FLOOR SUPPORT HAS MINOR CORROSION. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00. REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 51-42-06 A - [SDR ASOA201201093](https://openairdocs.org/sdr/ASOA201201093), Mar 27, 2012: FLOOR SUPPORT. CORRODED. LOWER FLOOR SUPPORT ANGLE CORRODED. REMOVED LWR FLOOR SUPPORT ANGLE IAW SRM 51-42-21, 51-42-10, 51-42-06 AND 51-42-34. LOCATED & DRILLED NEW FLOOR SUPPORT & INS - [SDR ASOA201201058](https://openairdocs.org/sdr/ASOA201201058), Mar 27, 2012: FLOOR PANEL. CRACKED. LEFT & RIGHT FWD EQUIPMENT COMPARTMENT FLOOR STRUCTURE AT FS 193.00 IS CRACKED APPROX .5L. TRIMMED CRACKED SECTION OF FLOOR WEB IAW REO 601R-53-11-245. PERFORME - [SDR ASOA201201056](https://openairdocs.org/sdr/ASOA201201056), Mar 27, 2012: SEAT TRACK. CORRODED. SEAT TRACK CORRODED AT LBL 9.0 FROM 409+128 TO 559. REMOVED SEAT TRACK IAW AMM 53-01-11-000-802. INSTALLED NEW SERVICEABLE SEAT TRACK IAW SRM 51-41-02 AND AMM 5 - [SDR ASOA201201054](https://openairdocs.org/sdr/ASOA201201054), Mar 27, 2012: SEAT TRACK. CORRODED. SEAT TRACK CORRODED AT RBL 9.0 FROM FS 409+128 TO 559.00. REMOVED SEAT TRACK IAW AMM 53-01-11-000-802. INSTALLED NEW SEAT TRACK IAW MM TASK 53-01-11-400-802. All 201: https://openairdocs.org/deregistered/N842AS-2019-02-25/reports.md ## Other aircraft with N842AS - [Registered now](https://openairdocs.org/aircraft/N842AS): Ea Vision EA J100, S/N EAVUAV502585856 --- 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.