# Service difficulty reports: N862AS, cancelled Mar 8, 2023 A list on [N862AS, cancelled Mar 8, 2023](https://openairdocs.org/deregistered/N862AS-2023-03-08.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. Page 1 of 3 · 112 reports - [SDR SWIA2019090446259](https://openairdocs.org/sdr/SWIA2019090446259.md): Transmitter · failed · Sep 4, 2019 · N862AS · Cndair CL6002B19 · Trailing Flap Position Indicating System > ENROUTE HYD CAUTION 1B AND 2B DISPLAYED. EMERGENCY DECLARED. QRH FOLLOWED. MSGS CLEARED. (FLT#5675) CLOSED REMOVED AND REPLACED RT FLAP POSITION TRANSMITTER IAW AMM. RAN OPERATIONAL TEST OF ACMP IAW AMM TO VERIFY THE CORRECT ACTION WITH HYDRAULICS AND FLAP POS - [SDR ASOA2018121465343](https://openairdocs.org/sdr/ASOA2018121465343.md): Skin · dented · Dec 6, 2018 · N862AS · Cndair CL6002B19 · Fuselage Main, Plate/Skin > REF: CO# 7476718 JOB# 7747675 OP# 62: FUSELAGE SKIN REPAIR REQUIRED BELOW CARGO DOOR BETWEEN FS 605.0 TO FS 625.0 AND STR 18L TO 22L. C/A: PERFORMED PERMANENT REPAIR I.A.W. EXPRESSSJET ECTC REO 601R-53-61-6789. - [SDR ASOA2018121435341](https://openairdocs.org/sdr/ASOA2018121435341.md): Skin · corroded · Nov 30, 2018 · N862AS · Cndair CL6002B19 · Wing, Plate/Skin > REF: CO# 7476718 JOB# 7747675 OP# 57 LOWER WING PLANK CUTOUT FOR RH BOOST PUMP HAS MULTIPLE INDICATIONS NOTED AROUND ENTIRE CIRCUMFERENCE ON HORZ AND VERTICAL SURFACE 50% FSH. FAILED NDT INSP. C/A: PERFORMED MAJOR REPAIR CARD NO: REO 601R-57-21-2908 BLENDED TO - [SDR ASOA2018121495342](https://openairdocs.org/sdr/ASOA2018121495342.md): Floor Support · corroded · Nov 29, 2018 · N862AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure > REF: CO# 7476718 JOB# 7747671 OP# 105: CORROSION FOUND ON PRESSURE FLOOR SILLS F.S. 409.00+128 TO F.S. 559.00 BETWEEN LBL 36-45 AND RBL 36-45. C/A: PERFORMED A MAJOR REPAIR ON FLOOR SILLS FS 409-128 TO 559 BETWEEN LBL 36-45 AND RBL 36-45 I.A.W. EXPRESSJET WO 5 - [SDR ASOA2018121475340](https://openairdocs.org/sdr/ASOA2018121475340.md): Skin · dented · Nov 27, 2018 · N862AS · Cndair CL6002B19 · Fuselage Main, Plate/Skin > REF: CO# 7476718 OP# 62 FUSELAGE SKIN HAS 1 EA DENT BETWEEN FS605 AND FS589 FROM STR 24L TO 25L. C/A PERFORMED PERMANENT REPAIR IAW EXPRESSJET ECTC EA 32-2018-239 - [SDR ASOA2018121475339](https://openairdocs.org/sdr/ASOA2018121475339.md): Skin · cracked · Nov 27, 2018 · N862AS · Cndair CL6002B19 · Wing, Plate/Skin > REF: CO#7476718 JOB# 7747675 OP#43 R/H LOWER WING PLANK AND STRAP JOINT CRACKED AT RWS 148.00. C/A REPAIRED DAMAGE IAW EXPRESSJET ECTC REO 601R-57-21-130 01. - [SDR ASOA2018121475338](https://openairdocs.org/sdr/ASOA2018121475338.md): Angle · cracked · Nov 27, 2018 · N862AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure > REF: CO# 7476718 JOB# 7747671 OP# 83: F.S.484, RBL 36.00 INBD AND OUTBD CLIPS ARE CRACKED. C/A: REPAIRED DAMAGE I.A.W. BOMBARDIER REO 601R-53-41-2393 REV.A, DATED 2018-11-18, EXPRESSJET EC/TC REO 601R-53-41-2393 REV.0, DATED 2018-11-19, BOMBARDIER REO 601R-53- - [SDR SWIA2018042444597](https://openairdocs.org/sdr/SWIA2018042444597.md): Oil System · low pressure · Apr 22, 2018 · N862AS · Cndair CL6002B19 · Engine Oil Pressure > RIGHT ENGINE FAILED IN FLIGHT, THE RIGHT ENG OIL PRESSURE MASTER WARNING, PRESSURE SHOWED ZERO. REMOVED AND REPLACED THE RT ENGINE ASSY IAW AMM. OPS AND LEAK CHECKED GOOD. - [SDR SWIA201844188](https://openairdocs.org/sdr/SWIA201844188.md): Bracket · damaged · Jan 23, 2018 · N862AS · Cndair CL6002B19 · Landing Gear Position and Warning > AFTER TAKE OFF, AND DURING RETRACTION OF THE GEAR, A DISAGREE NLG DOOR OPEN CAUTION MESSAGE. REMOVED AND REPLACED THE NLG NR 2 WOW SENSOR BRACKET IAW AMM. OPS CHECKED GOOD. - [SDR SWIA2018012544188](https://openairdocs.org/sdr/SWIA2018012544188.md): Warning System · activated · Jan 23, 2018 · N862AS · Cndair CL6002B19 · Landing Gear Position and Warning > AFTER TAKE OFF ON RETRACTION GEAR DISAGREE NLG DOOR OPEN CAUTION. (FLT 3198) 01/24/2018 WORK IN PROGRESS. - [SDR SWIA201642605](https://openairdocs.org/sdr/SWIA201642605.md): Door Sill · corroded · Aug 30, 2016 · N862AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure > EVIDENCE OF CORROSION ON THE CARGO BAY FLOOR SILL AT APPROXIMATELY FS 574.00 AND FS 621.00 AROUND NUT PLATES. CARGO DOOR FLOOR SILL REPLACED IAW REO. - [SDR SWIA201642609](https://openairdocs.org/sdr/SWIA201642609.md): Vane · chafed · Aug 28, 2016 · N862AS · Cndair CL6002B19 · Trailing Edge Flaps > LEFT INBD FLAP HAS CHAFE ON OTBD VANE L/E. REPLACED LT INBD FLAP VANE OTBD WEAR CAP WITH NEW PN K601R14302-7 IAW SRM. - [SDR SWIA201642608](https://openairdocs.org/sdr/SWIA201642608.md): Vane · chafed · Aug 28, 2016 · N862AS · Cndair CL6002B19 · Trailing Edge Flaps > LEFT INBD FLAP HAS CHAFE ON INBD VANE L/E. REPLACED LT INBD FLAP VANE, INBD WEAR CAP WITH NEW PN K601R14302-15 IAW SRM. - [SDR SWIA201642607](https://openairdocs.org/sdr/SWIA201642607.md): Vane · chafed · Aug 28, 2016 · N862AS · Cndair CL6002B19 · Trailing Edge Flaps > LEFT INBD FLAP HAS CHAFE AT CENTER VANE L/E. REPLACED LT INBD FLAP VANE, CENTER WEAR CAP WITH NEW PN K601R14302-7 IAW SRM. - [SDR SWIA201642606](https://openairdocs.org/sdr/SWIA201642606.md): Frame · corroded · Aug 27, 2016 · N862AS · Cndair CL6002B19 · Fuselage Main, Frame > AT FS 349.0 FRAME IS CORRODED FROM STR 25 LT TO STR 25 RT. REMOVED AND INSTALLED NEW LOWER FRAME SECTOR AT FS 349.00 IAW REO AND SRM. - [SDR SWIA201642604](https://openairdocs.org/sdr/SWIA201642604.md): Skin · dented · Aug 25, 2016 · N862AS · Cndair CL6002B19 · Trailing Edge Flaps > DENT ON LT SIDE INBD FLAP BOTTOM SKIN LOCATED WS 67.00. REPAIRED DENT IAW SRM. - [SDR SWIA201641884](https://openairdocs.org/sdr/SWIA201641884.md): Bracket · bent · Feb 16, 2016 · N862AS · Cndair CL6002B19 · Landing Gear Retraction/Extension System > NOSE GEAR WOULD NOT RETRACT. RETURNED TO FIELD. FOUND THE NOSE GEAR PROXIMITY SWITCH BRACKET WAS BENT FROM IMPROPER TOW STRAP PLACEMENT. R & R PROXIMITY SWITCH AND BRACKET. OPS CK GOOD. - [SDR SWIA201439902](https://openairdocs.org/sdr/SWIA201439902.md): Bypass Valve · failed · Nov 10, 2014 · N862AS · Cndair CL6002B19 · Cabin Cooling System > RT PACK HIGH TEMP CAUTION. NO CONTROL IN EITHER AUTO OR MANUAL. PACK TEMP INDICATED 110 DEGREES C. R & R RT PACK DUAL BYPASS VALVE IAW AMM. ALL OPS GOOD. NO LEAKS NOTED. PN: 808440-2, SN ON: 9611055, SN OFF: 2000425. - [SDR SWIA2014061638178](https://openairdocs.org/sdr/SWIA2014061638178.md): Bulkhead · cracked · Jun 9, 2014 · N862AS · Cndair CL6002B19 · Fuselage Main, Bulkhead > CRACK IN BS 202 BULKHEAD WHERE PARKING BRAKE ROD PASSES THROUGH. REPAIRED IAW REO. - [SDR SWIA2014061638179](https://openairdocs.org/sdr/SWIA2014061638179.md): Skin · damaged · May 31, 2014 · N862AS · Cndair CL6002B19 · Trailing Edge Flaps > DENT AND GOUGE IN TOP SKIN ON RT INBD FLAP 10 INCHES FROM AFT EDGE. REPAIRED FLAP IAW EA. - [SDR SWIA2014061638187](https://openairdocs.org/sdr/SWIA2014061638187.md): Panel · cracked · May 30, 2014 · N862AS · Cndair CL6002B19 · Standard Practices/Structures > PANEL 221BLC IS CRACKED. C-CHECK, REPAIRED CRACKED PANEL 221BLC IAW EA. - [SDR SWIA2014061638186](https://openairdocs.org/sdr/SWIA2014061638186.md): Bulkhead Web · damaged · May 30, 2014 · N862AS · Cndair CL6002B19 · Fuselage Main, Bulkhead > DEFECTS NOTED ON AFT PRESSURE BULKHEAD WEB FWD FACE C-CHECK, REPAIRED DEFECTS IAW REO. - [SDR SWIA2014061638185](https://openairdocs.org/sdr/SWIA2014061638185.md): Skin · corroded · May 30, 2014 · N862AS · Cndair CL6002B19 · Fuselage Main, Plate/Skin > FRETTING ALL THE WAY AROUND AVIONICS BAY DOOR CUTOUT ON INNER SURFACE OF SKIN. C-CHECK, REMOVED FRETTING ALL THE WAY AROUND AVIONICS BAY DOOR INNER SURFACE, IAW REO. - [SDR SWIA2014061638184](https://openairdocs.org/sdr/SWIA2014061638184.md): Vane · chafed · May 30, 2014 · N862AS · Cndair CL6002B19 · Trailing Edge Flaps > RT INBD FLAP VANE IS CHAFED NEAR INBD SIDE. C-CHECK, REMOVE CHAFE ON THE RT INBD FLAP VANE NEAR THE INBD SIDE IAW REO. - [SDR SWIA2014061638183](https://openairdocs.org/sdr/SWIA2014061638183.md): Vane · chafed · May 30, 2014 · N862AS · Cndair CL6002B19 · Trailing Edge Flaps > RIGHT INBD FLAP VANE IS CHAFED NEAR CENTER. C-CHECK, REMOVED CHAFE ON RT INBD FLAP VANE NEAR THE CENTER IAW REO. - [SDR SWIA2014061638182](https://openairdocs.org/sdr/SWIA2014061638182.md): Vane · chafed · May 30, 2014 · N862AS · Cndair CL6002B19 · Trailing Edge Flaps > RT INBD FLAP VANE IS CHAFED NEAR OTBD SIDE. C-CHECK, REMOVED CHAFE ON RT INBD FLAP VANE NEAR OTBD SIDE IAW REO. - [SDR SWIA2014061638181](https://openairdocs.org/sdr/SWIA2014061638181.md): Skin · chafed · May 30, 2014 · N862AS · Cndair CL6002B19 · Ailerons > RT AILERON TOP L/E IS CHAFED IN TWO AREAS NEAR CENTER. C-CHECK, REPAIRED RT AILERON UPPER SKIN IAW REO. - [SDR SWIA2014061638180](https://openairdocs.org/sdr/SWIA2014061638180.md): Skin · chafed · May 30, 2014 · N862AS · Cndair CL6002B19 · Ailerons > LT AILERON TOP L/E IS CHAFED IN TWI AREAS NEAR OTBD SIDE. C-CHECK, REPAIRED LT AILERON UPPER SKIN IAW REO. - [SDR SWIA201436228](https://openairdocs.org/sdr/SWIA201436228.md): Battery Pack · discharged · Feb 1, 2014 · N862AS · Cndair CL6002B19 · Emergency Lighting > AFT FLOOR LEVEL LIGHTS & OVERHEAD EMERGENCY LIGHTS DO NOT ILLUMINATE. FLT 2601 REPLACED NR 4 ELBP IAW AMM, PN ON AD-2013-1A, SN ON 126606, PN OFF 2013-1A & SN OFF 101363. - [SDR SWIA201335663](https://openairdocs.org/sdr/SWIA201335663.md): Battery Pack · discharged · Dec 16, 2013 · N862AS · Cndair CL6002B19 · Emergency Lighting > EMERGENCY LIGHTS DO NOT ILLUMINATE. FLT 2627 CHARGED UP ELBP'S. OPERATIONS CHECKED GOOD ON EMERGENCY LIGHTS - [SDR SWIA201232288](https://openairdocs.org/sdr/SWIA201232288.md): Charger · failed · Nov 30, 2012 · N862AS · Cndair CL6002B19 · Emergency Lighting > EMERGENCY FLOOR LIGHT 2ND 3RD 4TH STRIP IS NOT LIT. (FLT 2660) REPLACED NR 1 EMERGENCY LIGHT BATTERY CHARGER. - [SDR SWIA201231659](https://openairdocs.org/sdr/SWIA201231659.md): Trunnion · cracked · Aug 13, 2012 · N862AS · Cndair CL6002B19 · Wing, Landing Gear Attach Fittings > CRACK INDICATIONS ON 4 HOLES EACH IN LEFT AND RIGHT MLG TRUNNION LOWER PLANK. (C-CHECK) REPAIRED PER REO. - [SDR SWIA201231661](https://openairdocs.org/sdr/SWIA201231661.md): Floor Support · damaged · Aug 12, 2012 · N862AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure > FLOOR SUPPORT BEAM LBL 9 IN BETWEEN FS 589 AND FS 605 BLEND OUT IS OUT OF LIMIT. (C-CHECK) REPLACED FLOOR SUPPORT BEAM LBL 9 IN BETWEEN FS 569 AND FS 621 PER CRJ-200 SRM. - [SDR SWIA201231660](https://openairdocs.org/sdr/SWIA201231660.md): Floor Support · damaged · Aug 12, 2012 · N862AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure > FLOOR SUPPORT BEAM LBL 27 IN BETWEEN FS 589 AND FS 605 BLEND OUT IS OUT OF LIMIT. (C-CHECK) REPLACED FLOOR SUPPORT BEAM LBL 27 IN BETWEEN FS 569 AND FS 621 PER CRJ200 SRM. - [SDR SWIA201231662](https://openairdocs.org/sdr/SWIA201231662.md): Sill · cracked · Aug 11, 2012 · N862AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure > CRACK ON AFT CARGO DOOR SILL AT FS 605. (C-CHECK) REPAIRED DAMAGED AREA OF AFT CARGO DOOR SILL AT FS 605. - [SDR SWIA201231667](https://openairdocs.org/sdr/SWIA201231667.md): Panel · chafed · Aug 9, 2012 · N862AS · Cndair CL6002B19 · Aircraft Structures > PANEL 326CL HAS CHAFING. (C-CHECK) REPAIRED PANEL 326CL AS PER CRJ 200 SRM. - [SDR SWIA201231666](https://openairdocs.org/sdr/SWIA201231666.md): Post · cracked · Aug 9, 2012 · N862AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure > CRACK ON LEFT FS 409+128 VERTICLE POST AT LBL 18, OUTBOARD C-CHANNEL IN AFT RADIUS. (C-CHECK) REPLACED LEFT FS 409+128 VERTICLE OUTBOARD POST AT LBL 18 PER REO. - [SDR SWIA201231665](https://openairdocs.org/sdr/SWIA201231665.md): Post · cracked · Aug 9, 2012 · N862AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure > CRACK ON RIGHT FS 409+128 VERTICLE POST AT RBL 18, INBOARD C-CHANNEL IN AFT RADIUS. (C-CHECK) REPLACED VERTICLE POST AT RBL 18 IN REFERENCE TO REO. - [SDR SWIA201231664](https://openairdocs.org/sdr/SWIA201231664.md): Post · cracked · Aug 9, 2012 · N862AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure > CRACK ON RIGHT FS 409+128 VERTICLE POST AT RBL 18, OUTBOARD C-CHANNEL IN AFT RADIUS. (C-CHECK) REPLACED VERTICLE POST AT RBL 18 IN REFERENCE TO REO. - [SDR SWIA201231663](https://openairdocs.org/sdr/SWIA201231663.md): Floor Support · corroded · Aug 9, 2012 · N862AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure > CORROSION ON FLOOR SUPPORT BEAMS BETWEEN FS 589.00 AND FS 605.00. (C-CHECK) REPAIRED FLOOR SUPPORT BEAMS BETWEEN FS 589.00 AND FS 605.00 IN REFERENCE TO CRJ200 SRM. - [SDR SWIA201231397](https://openairdocs.org/sdr/SWIA201231397.md): Light · damaged · Jul 27, 2012 · N862AS · Cndair CL6002B19 · Emergency Lighting > SERVICE DOOR CABIN EMERGENCY LIGHT FIXTURE IS DAMAGED. (SERVICE) REPLACED SERVICE DOOR EMERGENCY LIGHT FIXTURE IN REFERENCE TO MM. - [SDR SWIA201231217](https://openairdocs.org/sdr/SWIA201231217.md): Light · inoperative · Jul 11, 2012 · N862AS · Cndair CL6002B19 · Emergency Lighting > LAST OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 8436055) RELAMPED EMERGENCY LIGHT. - [SDR SWIA201231047](https://openairdocs.org/sdr/SWIA201231047.md): Light · inoperative · Jun 16, 2012 · N862AS · Cndair CL6002B19 · Emergency Lighting > NR 1 OVERHEAD EMERGENCY LIGHTS ARE OUT. (FLT 4483) RELAMPED EMERGENCY LIGHTS. - [SDR SWIA201230690](https://openairdocs.org/sdr/SWIA201230690.md): Light · inoperative · May 10, 2012 · N862AS · Cndair CL6002B19 · Emergency Lighting > NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4837) RELAMPED EMERGENCY LIGHT. - [SDR SWIA201230360](https://openairdocs.org/sdr/SWIA201230360.md): Light · inoperative · Apr 10, 2012 · N862AS · Cndair CL6002B19 · Emergency Lighting > NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4502) RELAMPED EMERGENCY LIGHT. - [SDR SWIA201229593](https://openairdocs.org/sdr/SWIA201229593.md): Light · inoperative · Feb 13, 2012 · N862AS · Cndair CL6002B19 · Emergency Lighting > AFT OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4496) RELAMPED EMERGENCY LIGHT. - [SDR SWIA201229481](https://openairdocs.org/sdr/SWIA201229481.md): Light · inoperative · Feb 3, 2012 · N862AS · Cndair CL6002B19 · Emergency Lighting > NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4799) RELAMPED EMERGENCY LIGHT. - [SDR SWIA201229417](https://openairdocs.org/sdr/SWIA201229417.md): Actuator · out of rig · Jan 29, 2012 · N862AS · Cndair CL6002B19 · Trailing Edge Flap Actuator > RIGHT ROLLING FORCE UPON EXTENSION OF FLAPS. (FLT 4658) RE-RIGGED FLAP ACTUATOR R-4. - [SDR SWIA201128954](https://openairdocs.org/sdr/SWIA201128954.md): Light · inoperative · Dec 17, 2011 · N862AS · Cndair CL6002B19 · Emergency Lighting > NR 1 OVERHEAD EMERGENCY LIGHT INOPERATIVE. (SERVICE) RELAMPED EMERGENCY LIGHT. - [SDR SWIA201128950](https://openairdocs.org/sdr/SWIA201128950.md): Light · inoperative · Dec 15, 2011 · N862AS · Cndair CL6002B19 · Emergency Lighting > LAST ROW EMERGENCY CEILING OVERHEAD LIGHT IS INOPERATIVE. (FLT 4517) RELAMPED EMERGENCY LIGHT. Next page: https://openairdocs.org/deregistered/N862AS-2023-03-08/reports.md?page=2 ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE n_number = 'N862AS' AND deregistration_id = 'N862AS-2023-03-08' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N862AS-2023-03-08/reports --- 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.