N986SW
Registered owner: SKYWEST AIRLINES INC, UT (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| SKYWEST AIRLINES, INC. (SWIA) | Operator | 2016-12-14 – 2016-12-14 | Operator named in NTSB report |
| SKYWEST AIRLINES INC | Operator | 2016-12-14 – 2016-12-14 | Operator named in NTSB report |
Accident & incident history
Maintenance disclosures
CARGO DOOR FUSELAGE KICK PLATE HAS DAMAGED DOME NUTS (C-CHECK RO 9/24/2024) REPAIRED FUSELAGE SKIN COMMON TO KICKPLATE BELOW CARGO DOOR OPENING LOCATED BETWEEN FS589.00 AND FS621.00, STGR. 17L TO 19L AND REMOVED AND REPLACED DAMAGE DOME NUTS AND DAMAGED KICKPLATE PANEL WITH NEW KICKPLATE PANEL REF REO 601R-53-61-8229 REV --, DATED 2024-09-20. COMPLIED WITH ALL STEPS. COMPLIED WITH 51-900-1003-SKY. SEE CONTINUATION FOR DETAILS.
INTERCOSTAL LOCATED BETWEEN FS 654.50 AND FS 672.00 AT STGR. 4L, COMMON TO APU INTAKE DOOR ACTUATOR IS CRACKED ON FWD END. (MARKED) CAMP# 28777931 (C-CHECK RO 9/24/2024) REMOVED AND INSTALLED NEW INTERCOSTAL BETWEEN F/S 654.5 AND F/S 672 AT STRG 4L COMMON TO APU INTAKE DOOR IAW CRJ 200 SRM 51-42-06 AND DWG 601R35210 REV M. COMPLETED SKYWEST TASK CARD 51-900-1003-SKY.
R/H OUTBOARD FLAP HINGE ARM AT WS 220 CRACKED AFT END. (C-CHECK RO 9/24/2024) REPAIRED R/H OUTBOARD FLAP HINGE ARM AT WS 220 CRACKED AFT END REF. DWG 601R14699 REV. B, CRJ 200 SRM 51-42-06-00, AND DWG NO. 601R14629 REV. M. COMPLETED SKYWEST TASK CARD 51-900-1003-SKY.
L/H ELEVATOR HINGE BRACKET GOUGED (BL55.8896) H STAB SIDE (C-CHECK RO 9/24/2024) REPAIRED GOUGE ON THE L/H ELEVATOR HINGE BRACKET LOCATED AT BL55.8896 ON THE HORIZONTAL STAB SIDE REF CRJ-200 SRM 51-12-00 AND REO 601R-55-11-766, REV --, DATED 2024-08-16. COMPLIED WITH ALL STEPS. COMPLIED WITH 51-900-1003-SKY. SEE CONTINUATION FOR DETAILS.
L/H OTBD LUG OF H. STAB PIVOT FITTING ASSY HAS SEVERAL LIGHT GOUGES (C-CHECK RO 9/24/2024) REPAIRED GOUGE DAMAGES ON L/H OTBD LUG OF H. STAB PIVOT FITTING ASSY REF REO 601R-55-11-765 REV-- DATED 2024-08-17, COMPLIED WITH TASK CARD 51-900-1003-SKY
R/H ELEVATOR INBD EDGE FWD AREA HAS DAMAGE (DENT & GOUGE) (C-CHECK RO 9/24/2024) REPAIRED DAMAGE ON R/H ELEVATOR INBD LEADING EDGE REF REO 601R-55-21-601 REV-- DATED 2024-08-16, COMPLIED WITH TASK CARD 51-900-1003-SKY
RIGHT WING INBOARD AILERON HINGE INBOARD LUG HAS PITTING. (C-CHECK RO 9/24/2024) REMOVED PITTING BY REAMING RH WING INBOARD TRAILING EDGE, INBOARD LUG TO 3RD OVERSIZE, FABRICATED AND INSTALLED 3RD OVERSIZE BUSHING. REF - REO 601R-57-51-015 REV NC DATED AUG 09 1995.COMPLIED WITH TASK CARD 51-900-1003-SKY.
SEAT TRACK AT APPROXIMATELY FS364.0 TO FS394.0 RBL9 CORRODED AS MARKED (C-CHECK RO 9/24/2024) REMOVED AND REPLACED SEAT RAIL AT FS364.0 -FS396.0 RBL 9.0 REF CRJ200 AMM 53-01-11-04, SEAT RAIL FABRICATED REF REO 601R-53-00-485 REV-D DATED 2018-01-29
SEAT TRACK AT APPROXIMATELY FS364.0 TO FS394.0 LBL9 CORRODED AS MARKED (C-CHECK RO 9/24/2024) REMOVED AND REPLACED LH SIDE SEAT RAIL AT FS364.0 TO FS394.0, LBL 9 REF CRJ200 AMM 53-01-11-000-802 AND CRJ200 SRM 53-01-11-400-802.
RH WING OTBD FLAP HAS SMOKING RIVETS ON TOP EXTERNAL SKIN (C-CHECK RO 9/24/2024) REPAIRED RH WING OTBD FLAP HAS SMOKING RIVETS ON TOP EXTERNAL SKIN REF RE0 601R-57-53-1298 REV- DATED 2024-08-18. COMPLIED WITH TASK CARD 51-900-1003-SKY
LEFT SIDE SEAT RAIL, FS364.0-FS379.0 HAS NICKS, HN00174898 (C-CHECK RO 9/24/2024) REPLACED LH SIDE SEAT RAIL FROM FS364-379 USING NEW HARDWARE REF CRJ 200 AMM 53-01-11-400-802.
LH WING OTBD FLAP HAS SMOKING RIVETS ON UPPER EXTERNAL SKIN (C-CHECK RO 9/24/2024) REMOVED AND REPLACED 7EA RIVETS ON LH WING OTBD FLAP AND COMPLIED WITH ALL STEPS (1-5) OF REO 601R-57-53-1297, REV --, 2024-08-17. COMPLIED WITH 51-900-1003-SKY. SEE CONTINUATION FOR DETAILS.
LH SIDE APRON HAS WEAR ON EXTERNAL SKIN BETWEEN FS 513.00 - 559.00 FROM CONTACT WITH TRAILING EDGE UPPER AND LOWER SHROUDS (C-CHECK RO 9/24/2024) REPAIRED LH APRON SKIN PER REO 601R-53-41-115 (REV A) DATED 2005-07-20. AND REO 601R-57-51-1051 REV -- DATED 2024-08-17COMPLETED SKYWEST TASK CARD 51-900-1003-SKY.
RIGHT SIDE SEAT RAIL, FS409.0-FS409.0+16 HAS NICKS, HN00174897 (C-CHECK RO 9/24/2024) REMOVED AND REPLACED RH SIDE SEAT RAIL AT FS409.00 TO FS409.0+16 REF CRJ200 AMM 53-01-11-000-802 AND CRJ200 SRM 53-01-11-400-802.
SEAT TRACK LBL9, FS409.0-FS409.0+12 HAS NICKS AND SCRATCHES, HN00174890 (C-CHECK RO 9/24/2024) REMOVED AND REPLACED SEAT TRACK FROM FS396.0 -FS 409.0+128 LBL 9.0 REF CRJ200 AMM 53-01-11-000-802 & CRJ200 AMM 53-01-11-400-802, SEAT TRACK FABRICATED IAW REO 601R-53-00-485 REV-D DATED 2018-01-29
LEFT HAND SIDE SEAT RAIL SECTION FS546.00 TO FS559.0+80, HAS AND INDENTATION AT APPROXIMATELY FS559.0+56. (C-CHECK RO 9/24/2024) REMOVED AND REPLACED LH SIDE SEAT RAIL AT FS546.00 TO FS559.0+80 REF CRJ200 AMM 53-01-11-000-802 AND CRJ200 SRM 53-01-11-400-802. SEE CONTINUATION FOR DETAILS.
SEAT TRACK RBL9, FS409.0-FS409.0+12 HAS NICKS AND SCRATCHES CORROSION AND MISSING PROTECTIVE FINISH, HN00174891 (C-CHECK RO 9/24/2024) REMOVED AND REPLACED SEAT RAIL FROM FS396.0 - FS409.0+128 RBL 9.0 REF CRJ200 AMM 53-01-11-04, SEAT RAIL FABRICATED IAW REO 601R-53-00-485 REV-D DATED 2018-01-29
LEFT HAND PRESSURE FLOOR SILL HAS MULTIPLE AREAS OF CORROSION BETWEEN FS409.00+128 AND FS559.0 AS MARKED (C-CHECK RO 9/24/2024) REPAIRED 3EA SILL PANEL BLENDS AND 2EA SILL ANGLE BLENDS BETWEEN FS409.00+128 AND FS559.0 IN LIMITS REF REO 601R-53-41-666 REV. -C DATED 2012-11-06. PRESSURE CHECK GOOD. COMPLIED WITH 51-900-1003-SKY.
LEFT HORIZONTAL PIVOT FITTING, OUTER AND INNER FITTING HAS IMPACT DAMAGE. (C-CHECK RO 9/24/2024) REMOVED CHAFE DAMAGE FROM LH HORIZONTAL PIVOT FITTING , (OUTER OTBD), (INNER INBD) AND (INNER OTBD), NDT INSPECTED NO DEFECT NOTED, RESTORED FINISH, REF MHIRJ REO 601R-55-31-463 REV - - DATED 2024-08-16 STEPS 1-3 FOR COMPLETE DETAILS OF WORK PERFORMED SEE ATTACHED COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY.
AFT EQUIPMENT BAY, SUSPECT ANGLE CRACKED AT FS625.30, STRINGER 14L. (C-CHECK RO 9/24/2024) REMOVED AND REPLACED INTERCOSTAL ANGLE AT STR 14L FS625.3 (P/N 601-35012-51) REF CRJ200 SRM 51-42-21-00, DWG 601-35012 REV-D, REO 601R-53-61-422 REV NCDATED 2001-08-23, COMPLIED WITH TASK CARD 51-900-1003-SKY
RIGHT PRESSURE FLOOR SILL MEMBER FS409.0+128 - 559.0 HAS MULTIPLE AREAS OF CORROSION. (MARKED) (C-CHECK RO 9/24/2024) BLENDED 9 EA AREAS ON R/H PRESSURE FLOOR SILL MEMBER FROM FS409+128-559 REF CRJ 200 SRM 51-21-06. FOUND TO BE WITHIN LIMITS. COMPLIED WITH ALL STEPS OF REO 601R-53-41-666 REV-C, DATED 2012-11-06 DISPOSITION 2.1. COMPLIED WITH TASK CARD 51-900-1003-SKY.
GOUND AIR CONDITIONING DOOR LAND BENT FORWARD AND AFT EDGES. (C-CHECK RO 9/24/2024) REMOVED AND REPLACED FORWARD AND AFT LANDINGS FOR GROUND AIR-CONDITIONING DOOR REF CRJ200 SRM 51-42-06-00 AND DWG 601R35226 REV-P, COMPLIED WITH TASK CARD 51-900-1003-SKY
COMPLY WITH SCHEDULED MAINTENANCE CODE: AD 2019-08-04/02 40000 FC - COMPLY WITH PARAGRAPH (J) OF AD 2019-08-04 BY: (J)(1) DOING A NONDESTRUCTIVE INSPECTION FOR CRACKING OF THE FORWARD FACE OF THE FUSELAGE STATION (FS) 621 PRESSURE BULKHEAD, IN ACCORDANCE WITH AWL 53-61-153 OF BOMBARDIER TR 2B-2187, DATED JUNE 22, 2011, TO APPENDIX B̉‰AIRWORTHINESS LIMITATIONS, OF PART 2 OF THE BOMBARDIER CL-600-2B19 MRM. (J)(2) MODIFYING THE RPB AND DOING A NONDESTRUCTIVE INSPECTION FOR CRACKING OF THE FS 621 PRESSURE BULKHEAD WEB, IN ACCORDANCE WITH BOMBARDIER REPAIR ENGINEERING ORDER (REO) 601R-53-61-1240, REVISION D, DATED OCTOBER 31, 2016. AND MARKING THIS CAMP AS "STRUCTURAL REPAIR," WHICH WILL GENERATE AN RA FOR TRACKING THE SDIR FOR THIS REO ON THIS AIRPLANE, PART NUMBER: - , SERIAL NUMBER: 7967, POSITION: (C-CHECK RO 9/24/2024) COMPLIED WITH PARAGRAPH (J) OF AD 2019-08-04 BY:(J)(1) DOING A NONDESTRUCTIVE INSPECTION FOR CRACKING OF THE FORWARD FACE OF THE FUSELAGE STATION (FS) 621 PRESSURE BULKHEAD, IN ACCORDANCE WITH AWL 53-61-153 OF BOMBARDIER TR 2B-2187, DATED JUNE 22, 2011, TO APPENDIX B̉‰AIRWORTHINESS LIMITATIONS, OF PART 2 OF THE BOMBARDIER CL-600-2B19 MRM.(J)(2) MODIFYING THE RPB AND DOING A NONDESTRUCTIVE INSPECTION FOR CRACKING OF THE FS 621 PRESSURE BULKHEAD WEB, IN ACCORDANCE WITH BOMBARDIER REPAIR ENGINEERING ORDER (REO) 601R-53-61-1240, REVISION D, DATED OCTOBER 31, 2016.AND;MARKING THIS CAMP AS "STRUCTURAL REPAIR," WHICH WILL GENERATE AN RA FOR TRACKING THE SDIR FOR THIS REO ON THIS AIRPLANE.COMPLIED WITH SERIAL NUMBER 7967.COMPLETED SKYWEST TASK CARD 51-900-1003-SKY.
COMPLY WITH SCHEDULED MAINTENANCE CODE: RA58215-601R-53-21-3299 N986SW MXCODEID51600-PR - FUSELAGE BELOW THE SERVICE DOOR CUTOUT HAS 1EA MIS DRILLED HOLE REQUIRES EVAL CORRECTIVELY REPAIRED MISSED DRILLED HOLE WITH PLATE SUPPORT IAW BOMBARDIER REO 601R-53-21-3299-REV B , 3/31/2020. TEMPORARY REPAIR VALID FOR 6000 FLIGHT HOURS., PART NUMBER: - , SERIAL NUMBER: 7967, POSITION: (C-CHECK RO 9/24/2024) COMPLIED WITH PERMANENT REPAIR OF 1 EA. MIS-DRILLED HOLE ON FUSELAGE BELOW SERVICE DOOR CUT-OUT REF REO 601R-53-21-3699 REV --, DATED 2024-09-07. COMPLIED WITH ALL STEPS. COMPLIED WITH TASK CARD 51-900-1003-SKY. SEE CONTINUATION FOR DETAILS. LEAK CHECK GOOD.
GEAR DISAGREE AFTER TAKE OFF WHEN BRINGING GEAR UP. RAN QRH AND BROUGHT GEAR BACK DOWN. GEAR DISAGREE CLEARED. DECLARED EMERGENCY AND LANDED IN ORD. (FLIGHT #5416 FILED CLOSED) THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 25487820 WITH THE FOLLOWING CORRECTIVE ACTION: "PERFORMED SERVICING OF THE NLG SHOCK STRUT WITH OIL AND NITROGEN WITH AIRCRAFT ON JACKS. PERFORMED EXTENSION/RETRACTION CHECK OF THE NLG AND BOTH MLG'S AND ON GEAR RETRACTION NLG FAILED TO GO FULLY UP AN LOCKED. UPON FURTHER INSPECTION FOUND THE NLG SHOCK STRUT COULD BE COMPRESSED BY HAND EVEN AFTER BEING FULLY SERVICED INDICATING THE INTERNAL FLOATING PISTION DID NOT PROPERLY SEAT. PERFORMED SERVICING OF THE NLG SHOCK STRUT WITH OIL AND NITROGEN WITH THE AIRCRAFT ON GROUND AND VERIFIED THE FLOATING PISTON SEATED. PERFORMED EXTENSION/RETRACTION CHECK OF THE NLG AND LH AND RH MLG. OPS CHECK GOOD AT THIS TIME. (REF. CP 25487827 AND CP 25488136 FOR WORK PERFORMED). (REF. CP 25489858 FOR FUNCTIONAL TEST OF THE EXTENSION/RETRACTION SYSTEM)."
REMOVED UPPER BOLT AND ASSOCIATED HARDWARE ON INBD RH FLIGHT SPOILER PCU (NAS6306U21D) FILED CLOSED REPLACED UPPER BOLT, ANTI-ROTATION DEVICE, BUSINGS AND CSTL NUT ON INBD RH FLIGHT SPOILER PCU (NAS6306U21D) IN ATTEMPT TO FIX OUT OF LIMITS FLIGHT SPOILER BACKLASH. FAILED FLIGHT SPOILER BACKLASH AFTER NEW HARDWARE, SEE ORIGINAL BACKASH TASK CARD FOR CONTINUATION (CP 22402440-1).
FLT COMP CTR FLOOR PANEL SUPPORT ANGLE AT FWD SIDE OF FS 280.00 FLOOR SUPPORT SPANWISE BEAM IS CRACKED AT LBL 8.0 (C-CHECK) RO 4/2/2020 REMOVED AND REPLACED CRACKED ANGLE IAW CRJ-200 SRM
PASSENGER DOOR CUTOUT FWD FRAME HAS CORRODED SERRATED FITTING (C-CHECK) RO 4/2/2020 REMOVED AND REPLACED FITTING IAW CRJ200 AMM. OPS TEST C/W ON CP 20671670 W/O 1018284 8000 0084 SN 7664823 PN 600-38061-11 TAG BB5670 NAS1303-9 A74427
FLOOR SUPPORT STRUCTURE HAS A CRACK ON FS 280.00 AFT FACE BY FLOOR POST AT LBL9 (C-CHECK) RO 4/2/2020 REPAIRED FS 280 FLOOR SUPPORT STRUCTURE AT LBL 9 IAW REO.
FLOOR SUPPORT STRUCTURE HAS DOUBLER CRACKED AT FS 280.00 RBL 13 (C-CHECK) RO 4/2/2020 REPAIRED FLOOR SUPPORT STRUCTURE AT FS 280 RBL 13 IAW BOMBA REO.
FLOOR SUPPORT STRUCTURE HAS CRACKED O/B ANGLE AT RBL 9 ON FS 280.00 (C-CHECK) RO 4/2/2020 REPAIRED O/B ANGLE OF FLOOR SUPPORT STRUCTURE AT RBL 9 ON FS 280 IAW BOMBA REO.
FLOOR SUPPORT STRUCTURE HAS A BROKEN TAB AT FS 295.00 BETWEEN LBL 27 AND LBL 34 (C-CHECK) RO 4/2/2020 REMOVED AND REPLACED TAB AT STATION 295 BETWEEN LBL 27 AND LBL 34 IAW CRJ200 SRM
FLOOR SUPPORT STRUCTURE HAS CRACKED I/B ANGLE AT RBL 9 ON FS 280.00 (C-CHECK) RO 4/2/2020 REPAIRED I/B ANGLE AT RBL 9 ON FS 280 IAW CRJ 200 SRM.
FLOOR SUPPORT STURCTURE HAS CRACKED UPPER ANGLE AT RBL 9 ON FS 280.00 (C-CHECK) RO 4/2/2020 REPAIRED FLOOR SUPPORT STRUCTURE UPPER ANGLE AT RBL 9 AT FS 280 IAW BOMBA REO.
FLOOR SUPPORT STRUCTURE HAS FS 280.00 WITH MULTIPLE CRACKS BETWEEN RBL 15 AND LBL 15 (C-CHECK) RO 4/2/2020 REPAIRED FLOOR STRUCTURE SUPPORT AT FS 280 BETWEEN RBL 15 AND LBL 15 IAW BOMBA REO.
PAX DOOR LOWER SILL CHAFED UNDER POWER CABLE (C-CHECK) RO 4/2/2020 REMOVED SURFACE FINISH IAW CRJ 200 SRM, DAMAGE FOUND TO BE IN PAINT ONLY; RESTORED SURFACE FINISH.
FLOOR BEAM ATTACHMENT FITTING TO RPB AT RBL27 HAS MINOR CORROSION AT FLOOR BOARD ATTACHMENT HDWR (OTBD FLANGE) (C-CHECK) RO 4/2/2020 REPAIRED FLOOR BEAM IAW BOMBARDIER REO.
FLOOR SUPPORT STRUCTURE HAS A BROKEN TAB AFT OF FS 295.00 AT LBL 27 (C-CHECK) RO 4/2/2020 REMOVED AND REPLACED WITH 2 EA NEW FLOOR SUPPORT STRUCTURE TABS AFT OF FS 295.00 AT LBL 27 IAW CRJ200 SRM
FRAME 333 FROM 26L TO 26R CORRODED (C-CHECK) RO 4/2/2020 REMOVED AND REPLACED DAMAGED FRAME SECTION AT FS333 FROM 23L TO 23R IAW CRJ 200 SRM
L/H WING LOWER PLANK ACCESS HOLE 540EB HAS NICK (C-CHECK) RO 4/2/2020 REMOVED DAMAGE, RESTORED FINISH IAW BOMB CRJ-200 REO LEAK CHECK ACCOMPLISHED ON AAR W.O 1018283 ZONE 5000 ITEM 0002 S/N 7665261
FLOOR SUPPORT BEAM "BATHTUB" FITTING CRACKED AT FS461.00 RBL9 OTBD SIDE (C-CHECK) RO 4/2/2020 INSTALLED NEW FITTING IAW CRJ 200 SRMS
RH SIDE SEAT TRACK STICK RETAINER #5 IS GOUGED AND CORRODED ON NUTPLATE ATTACH OPENINGS (C-CHECK) RO 4/2/2020 REMOVED AND REPLACED WITH NEW SEAT TRACK STICK RETAINER AND STANDOFFS IAW CRJ-200 SRM
LH SIDE SEAT TRACK STICK #6 HAS CORROSION IN SEVERAL AREAS NOT JUST AT DOT (C-CHECK) RO 4/2/2020 REMOVED CORRODED SEAT TRACK AND REPLACED WITH NEW SEAT TRACK IAW CRJ-200 AMM AND REO
LH SIDE SEAT TRACK STICK RETAINER #5 GOUGED AND CORRODED ON NUTPLATE ATTACH OPENINGS (C-CHECK) RO 4/2/2020 REMOVED AND REPLACED LH SIDE SEAT TRACK STICK RETAINER IAW CRJ-200 SRM
LH SIDE SEAT TRACK STICK #5 HAS CORROSION IN SEVERAL AREAS NOT JUST AT DOT (C-CHECK) RO 4/2/2020 REMOVED CORRODED SEAT TRACK AND REPLACED WITH NEW SEAT TRACK IAW CRJ 200 AMM
LH SIDE SEAT TRACK STICK #4 HAS CORROSION IN SEVERAL AREAS NOT JUST AT DOT (C-CHECK) RO 4/2/2020 REMOVED AND REPLACED LH SIDE SEAT TRACK STICK #4 IAW CRJ-200 AMM AND BOMBARDIER REO
LH SIDE SEAT TRACK STICK RETAINER #3 GOUGED AND CORRODED ON NUTPLATE ATTACH OPENINGS (C-CHECK) RO 4/2/2020 REMOVED AND REPLACED WITH NEW SEAT TRACK RETAINER IAW CRJ-200
LH SIDE SEAT TRACK STICK #3 HAS CORROSION IN SEVERAL AREAS NOT JUST AT DOT (C-CHECK) RO 4/2/2020 REMOVED ORIGINAL SIDE SEAT TRACK DUE TO CORROSION BEING OUT OF LIMITS, REPLACED WITH NEW FINISHED SIDE SEAT TRACK IAW CRJ 200 AMM
LH SIDE SEAT TRACK STICK #2 HAS CORROSION IN SEVERAL AREAS NOT JUST AT DOT (C-CHECK) RO 4/2/2020 REMOVED CORRODED SEAT TRACK AND REPLACED WITH NEW SEAT TRACK IAW CRJ-200 AMM AND REO
RH SIDE SEAT TRACK STICK #3 HAS CORROSION IN SEVERAL AREAS NOT JUST AT DOT (C-CHECK) RO 4/2/2020 REMOVED AND REPLACED RH SIDE SEAT TRACK IAW CRJ 200 AMM
RH SIDE SEAT TRACK STICK #4 HAS CORROSION IN SEVERAL AREAS NOT JUST AT DOT (C-CHECK) RO 4/2/2020 REMOVED CORRODED SEAT TRACK AND INSTALLED NEW SEAT TRACK IAW CRJ-200 AMM AND REO
RH SIDE SEAT TRACK STICK #5 HAS CORROSION IN SEVERAL AREAS NOT JUST AT DOT (C-CHECK) RO 4/2/2020 REMOVED AND REPLACED RH SIDE SEAT TRACK STICK #5 IAW CRJ-200 AMM AND BOMBARDIER REO
RH SIDE SEAT TRACK STICK #6 HAS CORROSION IN SEVERAL AREAS NOT JUST AT DOT (C-CHECK) RO 4/2/2020 REMOVED CORRODED SEAT TRACK AND INSTALLED NEW SEAT TRACK IAW CRJ-200 AMM AND REO
RH PRESSURE FLOOR WEB CORRODED AT FLOOR BOARK ATTACHMENT HDWR LOCATIONS FS504.00+128 TO FS559.0 (C-CHECK) RO 4/2/2020 REPAIRED RH FLOOR "L" ANGLE FROM 473-FS513 IAW:CRJ200-BOMBA-REO.
RH SIDE SEAT TRACK STICK #2 HAS CORROSION IN SEVERAL AREAS NOT JUST AT DOT (C-CHECK) RO 4/2/2020 REMOVED RH SIDE SEAT TRACK DUE TO CORROSION BEING OUT OF LIMITS, REPLACED WITH NEW SIDE SEAT TRACK
STRINGER ATTACH CLIP CRACKED @ FS 280.0 STGR 3L. (C-CHECK) RO 4/2/2020 REMOVED CRACKED ATTACH CLIP AT STGR L3 AND FS. 280 REPLACED WITH NEW ATTACH CLIP IAW CRJ 200 SRM AND SRM
AFT PRESS BULKHEAD 621 HAS MULTIPLE RIVET HEADS THAT ARE CHAFED CIRCLED IN RED GREASE PENCILE (C-CHECK) RO 4/2/2020 REMOVED AND REPLACED 7EA DAMAGED RIVETS IAW CRJ 200 SRM
SERVICE DOOR THRESHOLD PLATE IS CORRODED (C-CHECK) RO 4/2/2020 LOCATED AND DRILLED NEW SERVICE DOOR THRESHOLD PLATE IAW CRJ-200 SRM.
AFT PRESS BULKHEAD 621 HAS MULTIPLE BROKEN / CRACKED ISOLATORS MARKED WITH RED GREASE PENCILE RED X (C-CHECK) RO 4/2/2020 REMOVED AND REPLACED 7EA ISOLATORS IAW CRJ200 SRM
LH WING TO BODY SIDE FAIRING INTERCOSTAL IS CRACKED IN 2 SPOTS JUST FWD OF FS 475.15. (C-CHECK) RO 4/2/2020 REMOVED AND REPLACED LH WING TO BODY FAIRING ATTACH ANGLE (IMPROPERLY IDENTIFIED AS INTERCOSTAL IN DISCREPANCY), IAW CRJ 200 SRM
LH WING TO BODY SIDE FAIRING INTERCOSTAL IS CRACKED AT FS 461 (C-CHECK) RO 4/2/2020 REMOVED AND REPLACED LH WING TO BODY SIDE FAIRING ATTACH BRACKET (IMPROPERLY IDENTIFIED AS INTERCOSTAL IN DISCREPANCY) IAW CRJ 200 SRM
RH WING TO BODY SIDE FAIRING INTERCOSTAL IS CRACKED AT FS 449.85 (C-CHECK) RO 4/2/2020 REMOVED/REPLACED BODY SIDE FAIRING ATTACH ANGLE (IMPROPERLY IDENTIFIED AS INTERCOSTAL IN DISCREPANCY) IAW CRJ 200 SRM
AFT PRESS BULKHEAD 621 HAS MULTIPLE CHAFES CIRCLED IN RED GREASE PENCILE (C-CHECK) RO 4/2/2020 REPAIRED ALL CHAFED AREAS IAW BOMBA REO.
LH WING TO BODY SIDE FAIRING INTERCOSTAL IS CRACKED AT ABOUT FS 449.85 (C-CHECK) RO 4/2/2020 REMOVED AND REPLACED LH WING TO BODY SIDE FAIRING ATTACH BRACKET (IMPROPERLY IDENTIFIED AS INTERCOSTAL IN DISCREPANCY), IAW CRJ 200 SRM
RH WING TO BODY SIDE FAIRING INTERCOSTAL IS CRACKED JUST AFT OF FS 473.15 (C-CHECK) RO 4/2/2020 REMOVED/REPLACED BRACKET IAW CRJ 200 SRM
RIGHT ELEVATOR CENTER HINGE ON STAB SIDE HAS TOOLING DAMAGE (C-CHECK) RO 4/2/2020 REPAIRED DAMAGED HINGE IAW REO
LH WING AFT SPAR TO AUX SPAR DRAG ANGLE SUPPORT STRUCTURE AT WS 48.0 CRACKED (C-CHECK) RO 4/2/2020 REMOVED CRACKED ANGLE AND INSTALLED NEW ANGLE IAW CRJ 200 SRM
RT WING I/B FLAP LOWER SURFACE HAS DENT (C-CHECK) RO 4/2/2020 REPAIRED DAMAGE IAW BOMBA REO REV:-- DATE:2010/01/07
PAX DOOR AFT PULLEY BRACKET CHAFED FROM CONTACT WITH PULLEY. (C-CHECK) RO 4/2/2020 REMOVED AND REPLACED PULLEY BRACKET IAW CRJ200 AMM
SERVICE DOOR THRESHOLD HARDWARE CORRODED (C-CHECK) RO 4/2/2020 RECEIVED NEW PARTS, INSTALLATION ACCOMPLISHED ON WO# 1018283/2000/0001 SN# 7665203 CP# 20428312 / PN NAS1152-3 TN B23600 / PN NAS1581K3T12 TN A85737 / PN AN525-10R9 TN A83762, A86634
LEFT ENGINE FAILURE IN FLIGHT. LOUD NOISE FROM LEFT ENGINE. LEFT ENGINE OIL PRESS WARNING MESSAGE. COMPLIED WITH QRH. RTF. (FLT#5108) FO: 07/23/2019 CLOSED REMOVED AND REPLACED LT ENGINE ASSY IAW AMM. OPS AND LEAK CHECKS GOOD.
BS 621 BULKHEAD IS CHAFED BEYOND LIMITS AT RBL18, LBL 18 AND LBL 27. REPAIRED THE BULKHEAD IAW REO.
CORRODED FLOOR SUPPORT, BS 616 TO 621, LBL 27. BLENDED THE CORROSION IAW SRM. REPLACED THE NUTPLATE IAW SRM.
EXTERNAL SKIN HAS CHAFE DAMAGE FWD OF BS 559+96 BELOW AFT LAV FILLER, STRINGER 22R. REPAIRED THE SKIN IAW REO.
RIGHT SIDE OF STRINGER 27 BETWEEN BS 394 AND 409, A SHIM HAS CORROSION. INSTALLED A NEW STRINGER AND SHIM IAW REO.
CORROSION ON CARGO DOOR SILL BS 581 TO 616. INSTALLED A NEW CARGO DOOR SILL IAW REO.
AVONICS DOOR FWD FITTING ON BS 364, RT AND LT SIDE ARE GOUGED AND SCRATCHED. REPAIRED THE AVIONICS DOOR FWD FITTING IAW SRM.
CORROSION ON THE FLOOR SUPPORT, BS 589 TO 616, LBL 27 INBD. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM.
CARGO COMPARTMENT, BS 621 BULKHEAD, RBL 9 AT 13 INCHES, RBL 18,27 AND 36 AT 30 INCHES CHAFED. REMOVED THE CHAFES ON THE REAR PRESSURE BULKHEAD IAW SRM.
AFT EQUIPMENT BAY, OTBD OF LBL 36, AT BS 621, BELOW STRINGER 16L, STIFFENER IS CRACKED. REMOVED AND REPLACED THE STIFFENER IAW SRM.
EVIDENCE OF POSSIBLE CORROSION ON PAX DOOR SILL. REMOVED AND REPLACED THE DOOR SILL ANGLE IAW SRM.
EVIDENCE OF CORROSION ON SERVICE DOOR SILL ANGLE AT APPROX BS 295, STRINGER 17R. REMOVED CORROSION IAW REO.
LEFT LOWER SURFACE OF AILERON HAS A DENT. REPAIRED THE AILERON LOWER SURFACE IAW REO.
LEFT INBD FLAP VANE CAP AT THE CENTER LOCATION CHAFED. R & R LT INBD FLAP VANE CAP IAW SRM.
LT INBD FLAP VANE L/E CHAFED AT INBD POSITION. INSTALLED PN: 601R14303-53 IAW REO.
LEFT INBD FLAP VANE L/E CHAFED AT OTBD POSITION. REMOVED AND INSTALLED LT INBD FLAP OTBD VANE CAP IAW SRM.
SERVICE DOOR EMERGENCY EXIT LIGHT BROKEN. SERVICE, R & R SERVICE DOOR EMERGENCY EXIT LIGHT ASSY IAW AMM.
RT OVERWING EXIT SIGN BULBS ARE BURNED OUT. REPLACED THE BULBS.
RIGHT ENGINE FOUND GALLING ON OTBD BUSHING OF AFT ENGINE MOUNT. INSTALLED A SERVICEABLE RT ENGINE AFT SPHERICAL BUSHING IAW AMM.
RIGHT ENGINE FOUND GALLING ON OTBD HOUSING OF AFT ENGINE PYLON MOUNT. R & R OTBD HOUSING OF AFT ENGINE PYLON MOUNT IAW AMM.
RIGHT ENGINE FWD MOUNT LINK ASSY AND CLAMP UP BUSHING HAVE GALLING. INSTALLED SERVICABLE MOUNT LINK ASSY AND CLAMP UP BUSHING ONTO MOUNT YOKE IAW AMM.
FLOOR LEVEL EMERGENCY EXIT SIGN BULB IS BURNED OUT. FLT6485 RELAMPED.
EMERGENCY LIGHT POD IS INOPERATIVE. FLT#6356 RELAMPED.
NR 3 EMERGENCY OVERHEAD LIGHT IS BURNED OUT. (FLT 5519) REPLACED NR 2 EMERGENCY OVERHEAD LIGHT.
MOST OUTBOARD FLEX SHAFT RUSTED INTO THE OUTBOARD FLAP OUTBOARD ACTUATOR. (C-CHECK) REPLACED LEFT OUTBOARD FLAP OUTBOARD ACTUATOR AND NR 5 FLEX DRIVE IN REFERENCE TO CRJ200 AMM.
NR 4 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6410) RELAMPED EMERGENCY LIGHT.
TWO FORWARD EXTERIOR EMERGENCY LIGHTS ON RIGHT SIDE ARE OUT. (FLT 5652) RELAMPED EMERGENCY LIGHTS.
AFT OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5410) RELAMPED EMERGENCY LIGHT.
NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5362) RELAMPED EMERGENCY LIGHT.
AFT 2 EXTERIOR EMERGENCY LIGHTS ON THE RIGHT SIDE ARE OUT. (FLT 6324) RELAMPED EMERGENCY LIGHTS.
NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6315) RELAMPED EMERGENCY LIGHT.
RIGHT OVERWING AFT EMERGENCY EXIT LIGHT IS OUT. (FLT 5650) RELAMPED EMERGENCY LIGHT.
NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6369) RELAMPED EMERGENCY LIGHT.
BOTH OVERWING EMERGENCY LIGHTS AFT OF OVERWING EMERGENCY EXIT DOOR ARE OUT. (SERVICE) RELAMPED EMERGENCY LIGHTS.
NR 4 CEILING EMERGENCY LIGHT IS OUT. (FLT 5381) RELAMPED EMERGENCY LIGHT.
NR 4 CEILING EMERGENCY LIGHT IS BURNED OUT. (FLT 6428) RELAMPED EMERGENCY LIGHT.
FS 621 AFT PRESSURE BULKHEAD CRACKED FORWARD SIDE WEB AT AFT CARGO TRACK. (C-CHECK) REPAIR PER REO.
FS 559.0 PRESSURE BULKHEAD CRACKED AT LEFT SIDE. (C-CHECK) REPAIRED PER REO.
FLOOR SUPPORT ANGLE FORWARD SIDE OF FS 280 BEAM IS CRACKED. (C-CHECK) REPLACED FLOOR SUPPORT ANGLE PER SRM.
NR 4 CEILING EMERGENCY LIGHT IS OUT. (FLT 6978) RELAMPED EMERGENCY LIGHT.
EMERGENCY LIGHT ABOVE ROW 10 OUT. (FLT 6370) RELAMPED EMERGENCY LIGHT.
THE 3RD OVERHEAD EMERGENCY LIGHT FROM BACK INOPERATIVE. (FLT 7017) RELAMPED EMERGENCY LIGHT.
AFT CEILING EMERGENCY LIGHT INOPERATIVE. (FLT 6533) RELAMPED EMERGENCY LIGHT.
MAIN CABIN DOOR CABLE BINDING UP, CANNOT OPEN THE MCD MORE THAN HALF WAY. (FLT 6898) REPLACED MAIN CABIN DOOR ASSIST MOTOR ASSEMBLY.
NR 3 OVERHEAD EMERGENCY LIGHT INOP. (FLT 6811) RELAMPED EMERGENCY LIGHT.
UNABLE TO CONTROL CABIN ALTITUDE. (FLT 6551) REPLACED LEFT PACK PRSOV AND RIGHT PACK DUAL BYPASS VALVE.
RIGHT SIDE EXTERNAL EMERGENCY LIGHT INOP. (FLT 6517) RELAMPED EMERGENCY LIGHT.
FS 280 BULKHEAD WEB DAMAGED. (C CHECK) REPAIRED PER REO.
FS 280 CLIPS CRACKED. (C CHECK) REPLACED PER SRM.
FLT 6303 - ALTIMETER FLUCTUATION. REPLACED NR 2 ADC.
FLT 6543 - THIRD EMERGENCY LAMP OUT IN CEILING. RELAMPED.
FLT 1010 - FOUND PLUG AND JACK 167 CORRODED. REPLACED PLUG, CONNECTOR, AND PINS.
CEILING EMERGENCY EXIT LIGHT IS BURNED OUT. FLIGHT 6274. RELAMPED EMERGENCY LIGHT IAW AMM 33-51-16. OPS CHECK GOOD.
F/O`S CHART HOLDER SHORTED OUT. (FLIGHT NR 6438) SECURED HARDWARE ON CHART HOLDER. OPS CHECK GOOD.
AFT FLOOR SUPPORT CRACKED AT FS 621 AND LBL 41, FOUND AT C-CHECK. INSTALLED REPAIR PARTS PER REO 601R-53-61-117 REV A.
CRACK FOUND ON SUPPORT ANGLE AT FS625 LBL40 AND WL 98, FOUND AT C-CHECK. REPLACED ANGLE AT FS 625 LBL 40 AND WL 98 PER REO 601R-53-61-422.
FLT 5925 - RIGHT THRUST REVERSER UNLOCKED MESSAGE APPEARED. RETURNED TO FIELD. REPLACED RIGHT ENGINE THRUST REVERSER PDU WITH SERVICEABLE UNIT IAW CRJ 200 AMM 78-32-03. OPS CHECK GOOD.
FLIGHT ATTENDANT REPORTS BURNING ODOR FROM GALLEY, FLIGHT NR 6205. REPLACED LEFT HOT JUG PER CRJ MM 25-32-02. OPS CHECKED GOOD.
WHILE CRUISING AT 32,000 FEET WITH AUTOPILOT ENGAGED, STAB TRIM AND MACH TRIM MESSAGES APPEARED. NEITHER STAB OR MACH TRIM WOULD RE-ENGAGE. AUTOPILOT WORKED NORMALLY. REPLACED THE NR 2 FCC CARD PER MM 22-12-14. P/N: 622-9815-904, S/N ON: 10JXC, S/N OFF: 1L3NM.
STAB CH 1 WILL NOT ENGAGE. REPLACED HORIZONTAL STAB MOTOR CONTROL UNIT REF AMM 27-42-05. OPERATIONAL CHECK GOOD.
STAB TRIM CH 1 PUSH BUTTON STICKY. REPLACED STAB TRIM 1 MACH TRIM CONTROL PANEL REF CRJ MM 27-41-25. OPERATIONAL CHECK GOOD.
FOUND FLAP SKEW SYSTEM INOP. INSTALLED NEW SKEW UNIT IAW 27-51-15. OPERATIONAL CHECK GOOD.
STAB TRIM CH1 INOP STATUS MSG ILLUMINATES IN FLIGHT. REPLACED CA'S STAB TRIM SWITCH ON YOKE. OPERATIONAL CHECK GOOD IAW MM 27-41-00.
FLAPS FAIL CAUTION MESSAGE AFTER TAKEOFF. INTEROGATED FECU MOST PROBABLE CAUSE WAS FLAP CONTROL LEVER. PERFORMED OPERATIONAL CHECKS OF FLAP CONTROL LEVER, NO DEFECTS NOTED. ALSO PERFORMED RIG CHECK, BPSU AND MOTOR/BRAKE TORQUE CHECK. NO DEFECTS NOTED AT THIS TIME IAW 27-50-00. OPERATIONAL CHECK GOOD.
DURING TAXI OUT MOVED FLAP LEVER OUT OF 0 DEGREES TO 8 DEGREES. RECEIVED FLAPS FAIL MESSAGE. REPLACED FLAP CONTROL LEVER IAW MM 27-51-01. OPERATIONAL CHECK GOOD.
(STALL FAIL) CAUTION MESSAGE APPEARED AT FL290, 285KIAS. REPLACED STALL WARNING ACTUATOR PUSHER, OPERATIONAL CHECK GOOD.
FLT SPLRS FAULT, I/B AND O/B GND SPLR FAULT MESSAGES. REPLACED NR 1 SECU. OPERATIONAL CHECK GOOD IAW MM 27-61-00.
DURING FLAP RETRACTION AFTER LANDING, FLAPS FAIL MESSAGE ON ED-1 APPEARED. RE-RIGGED FLAP SYS BPSU IAW AMM 27-52-10. OPERATIONAL CHECK GOOD.