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 | on 2016-12-14 | Operator named in NTSB report |
Accident & incident history
Operated by SKYWEST AIRLINES INC (per NTSB report)
Maintenance disclosures
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
138 reports on file, 2004-09-29 – 2024-09-15.
Part: PLATE — DAMAGED (ZONE 800) · airframe 44,709 hrs · 38,111 cycles
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.
Part: INTERCOSTAL — CRACKED (ZONE 100) · airframe 44,709 hrs · 38,111 cycles
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.
Part: HINGE ARM — CRACKED (ZONE 600) · airframe 44,709 hrs · 38,111 cycles
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.
Part: LUG — GOUGED (ZONE 300) · airframe 44,709 hrs · 38,111 cycles
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
Part: HINGE BRACKET — GOUGED (ZONE 300) · airframe 44,709 hrs · 38,111 cycles
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.
Part: SKIN — DAMAGED (RT ELEVATOR) · airframe 44,709 hrs · 38,111 cycles
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
Part: HINGE — DAMAGED (ZONE 600) · airframe 44,709 hrs · 38,111 cycles
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.
Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 44,709 hrs · 38,111 cycles
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
Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 44,709 hrs · 38,111 cycles
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.
Part: SKIN — DAMAGED (ZONE 600) · airframe 44,709 hrs · 38,111 cycles
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
Part: SKIN — WORN (ZONE 100) · airframe 44,709 hrs · 38,111 cycles
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.
Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 44,709 hrs · 38,111 cycles
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.
Part: SEAT TRACK — NICKED (ZONE 200) · airframe 44,709 hrs · 38,111 cycles
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.
Part: SKIN — DAMAGED (ZONE 500) · airframe 44,709 hrs · 38,111 cycles
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.
Part: SEAT TRACK — NICKED (ZONE 200) · airframe 44,709 hrs · 38,111 cycles
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
Part: SEAT TRACK — NICKED (ZONE 200) · airframe 44,709 hrs · 38,111 cycles
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.
Part: SEAT TRACK — NICKED (ZONE 200) · airframe 44,709 hrs · 38,111 cycles
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
Part: PRESSURE DECK — CORRODED (ZONE 200) · airframe 44,709 hrs · 38,111 cycles
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.
Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 44,709 hrs · 38,111 cycles
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.
Part: FITTING — DAMAGED (ZONE 300) · airframe 44,709 hrs · 38,111 cycles
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.
Part: ANGLE — CRACKED (ZONE 200) · airframe 44,709 hrs · 38,111 cycles
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
Part: LANDING — BENT (A/C DOOR) · airframe 44,709 hrs · 38,111 cycles
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
Part: PRESSURE BLKHD — CRACKED (ZONE 200) · airframe 44,709 hrs · 38,111 cycles
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.
Part: SKIN — MECHANIC ERROR (ZONE 200) · airframe 44,709 hrs · 38,111 cycles
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.
Earlier reports · 2004–2022 · 114 reports
2022
Part: NONE — FAILED · airframe 43,777 hrs · 37,247 cycles
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)."
2021
Part: SPOILER — OUT OF LIMITS (RIGHT) · airframe 41,287 hrs · 35,007 cycles
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).
2020
Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 40,186 hrs · 33,964 cycles
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
Part: FITTING — CORRODED (FUSELAGE) · airframe 40,186 hrs · 33,964 cycles
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
Part: PAINT — DAMAGED (DOOR SILL) · airframe 40,186 hrs · 33,964 cycles
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.
Part: ANGLE — CRACKED (FUSELAGE) · airframe 40,186 hrs · 33,964 cycles
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.
Part: FLOORBEAM — BROKEN (FUSELAGE) · airframe 40,186 hrs · 33,964 cycles
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
Part: ATTACH FITTING — CORRODED (FUSELAGE) · airframe 40,186 hrs · 33,964 cycles
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.
Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 40,186 hrs · 33,964 cycles
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.
Part: FLOOR SUPPORT — BROKEN (FUSELAGE) · airframe 40,186 hrs · 33,964 cycles
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
Part: FRAME — CORRODED (FUSELAGE) · airframe 40,186 hrs · 33,964 cycles
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
Part: DOUBLER — CRACKED (FUSELAGE) · airframe 40,186 hrs · 33,964 cycles
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.
Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 40,186 hrs · 33,964 cycles
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.
Part: ANGLE — CRACKED (FUSELAGE) · airframe 40,186 hrs · 33,964 cycles
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.
Part: ANGLE — CRACKED (FUSELAGE) · airframe 40,186 hrs · 33,964 cycles
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.
Part: ACCESS PANEL — NICKED (LT WING) · airframe 40,186 hrs · 33,964 cycles
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
Part: FITTING — CRACKED (FUSELAGE) · airframe 40,186 hrs · 33,964 cycles
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
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 40,186 hrs · 33,964 cycles
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
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 40,186 hrs · 33,964 cycles
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
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 40,186 hrs · 33,964 cycles
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
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 40,186 hrs · 33,964 cycles
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
Part: ANGLE — CORRODED (FUSELAGE) · airframe 40,186 hrs · 33,964 cycles
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.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 40,186 hrs · 33,964 cycles
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
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 40,186 hrs · 33,964 cycles
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
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 40,186 hrs · 33,964 cycles
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
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 40,186 hrs · 33,964 cycles
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
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 40,186 hrs · 33,964 cycles
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
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 40,186 hrs · 33,964 cycles
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
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 40,186 hrs · 33,964 cycles
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
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 40,186 hrs · 33,964 cycles
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
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 40,186 hrs · 33,964 cycles
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
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 40,186 hrs · 33,964 cycles
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
Part: ATTACH BRACKET — CRACKED (FAIRING) · airframe 40,186 hrs · 33,964 cycles
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
Part: ATTACH ANGLE — CRACKED (FAIRING) · airframe 40,186 hrs · 33,964 cycles
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
Part: RIVET — CHAFED (FUSELAGE) · airframe 40,186 hrs · 33,964 cycles
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
Part: ISOLATOR — CRACKED (FUSELAGE) · airframe 40,186 hrs · 33,964 cycles
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
Part: BULKHEAD — CHAFED (FUSELAGE) · airframe 40,186 hrs · 33,964 cycles
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.
Part: INTERCOSTAL — CRACKED (FAIRING) · airframe 40,186 hrs · 33,964 cycles
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
Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 40,186 hrs · 33,964 cycles
SERVICE DOOR THRESHOLD PLATE IS CORRODED (C-CHECK) RO 4/2/2020 LOCATED AND DRILLED NEW SERVICE DOOR THRESHOLD PLATE IAW CRJ-200 SRM.
Part: ATTACH BRACKET — CRACKED (FAIRING) · airframe 40,186 hrs · 33,964 cycles
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
Part: INTERCOSTAL — CRACKED (FAIRING) · airframe 40,186 hrs · 33,964 cycles
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
Part: ANGLE — CRACKED (LT WING) · airframe 40,186 hrs · 33,964 cycles
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
Part: HINGE — DAMAGED (RT ELEVATOR) · airframe 40,186 hrs · 33,964 cycles
RIGHT ELEVATOR CENTER HINGE ON STAB SIDE HAS TOOLING DAMAGE (C-CHECK) RO 4/2/2020 REPAIRED DAMAGED HINGE IAW REO
Part: SKIN — DENTED (TE FLAP) · airframe 40,186 hrs · 33,964 cycles
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
Part: PULLEY BRACKET — CHAFED (PAX DOOR) · airframe 40,186 hrs · 33,964 cycles
PAX DOOR AFT PULLEY BRACKET CHAFED FROM CONTACT WITH PULLEY. (C-CHECK) RO 4/2/2020 REMOVED AND REPLACED PULLEY BRACKET IAW CRJ200 AMM
Part: FASTENER — CORRODED (FUSELAGE) · airframe 40,186 hrs · 33,964 cycles
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
2019
Part: ENGINE — FAILED (LEFT) · airframe 38,963 hrs · 32,889 cycles
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.
2018
Part: BULKHEAD WEB — CHAFED (BS 621) · airframe 35,772 hrs · 30,060 cycles
BS 621 BULKHEAD IS CHAFED BEYOND LIMITS AT RBL18, LBL 18 AND LBL 27. REPAIRED THE BULKHEAD IAW REO.
Part: FLOOR SUPPORT — CORRODED (BS 616-621) · airframe 35,772 hrs · 30,060 cycles
CORRODED FLOOR SUPPORT, BS 616 TO 621, LBL 27. BLENDED THE CORROSION IAW SRM. REPLACED THE NUTPLATE IAW SRM.
Part: SKIN — CHAFED (BS 559) · airframe 35,772 hrs · 30,060 cycles
EXTERNAL SKIN HAS CHAFE DAMAGE FWD OF BS 559+96 BELOW AFT LAV FILLER, STRINGER 22R. REPAIRED THE SKIN IAW REO.
Part: FITTING — GOUGED (BS 364) · airframe 35,772 hrs · 30,060 cycles
AVONICS DOOR FWD FITTING ON BS 364, RT AND LT SIDE ARE GOUGED AND SCRATCHED. REPAIRED THE AVIONICS DOOR FWD FITTING IAW SRM.
Part: DOOR SILL — CORRODED (BS 581-616) · airframe 35,772 hrs · 30,060 cycles
CORROSION ON CARGO DOOR SILL BS 581 TO 616. INSTALLED A NEW CARGO DOOR SILL IAW REO.
Part: FLOOR SUPPORT — CORRODED (BS 589-616) · airframe 35,772 hrs · 30,060 cycles
CORROSION ON THE FLOOR SUPPORT, BS 589 TO 616, LBL 27 INBD. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM.
Part: SHIM — CORRODED (BS 394-409) · airframe 35,772 hrs · 30,060 cycles
RIGHT SIDE OF STRINGER 27 BETWEEN BS 394 AND 409, A SHIM HAS CORROSION. INSTALLED A NEW STRINGER AND SHIM IAW REO.
Part: STIFFENER — CRACKED (BS 621) · airframe 35,772 hrs · 30,060 cycles
AFT EQUIPMENT BAY, OTBD OF LBL 36, AT BS 621, BELOW STRINGER 16L, STIFFENER IS CRACKED. REMOVED AND REPLACED THE STIFFENER IAW SRM.
Part: BULKHEAD WEB — CHAFED (BS 621) · airframe 35,772 hrs · 30,060 cycles
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.
Part: DOOR SILL — CORRODED (PAX DOORWAY) · airframe 35,772 hrs · 30,060 cycles
EVIDENCE OF POSSIBLE CORROSION ON PAX DOOR SILL. REMOVED AND REPLACED THE DOOR SILL ANGLE IAW SRM.
Part: DOOR SILL — CORRODED (BS 295) · airframe 35,772 hrs · 30,060 cycles
EVIDENCE OF CORROSION ON SERVICE DOOR SILL ANGLE AT APPROX BS 295, STRINGER 17R. REMOVED CORROSION IAW REO.
Part: SKIN — DENTED (LT AILERON) · airframe 35,772 hrs · 30,060 cycles
LEFT LOWER SURFACE OF AILERON HAS A DENT. REPAIRED THE AILERON LOWER SURFACE IAW REO.
2016
Part: VANE — CHAFED (LT WING TE FLAP) · airframe 31,109 hrs · 25,752 cycles
LEFT INBD FLAP VANE CAP AT THE CENTER LOCATION CHAFED. R & R LT INBD FLAP VANE CAP IAW SRM.
Part: VANE — CHAFED (LT WING TE FLAP) · airframe 31,109 hrs · 25,752 cycles
LEFT INBD FLAP VANE L/E CHAFED AT OTBD POSITION. REMOVED AND INSTALLED LT INBD FLAP OTBD VANE CAP IAW SRM.
Part: VANE — CHAFED (LT WING TE FLAP) · airframe 31,109 hrs · 25,752 cycles
LT INBD FLAP VANE L/E CHAFED AT INBD POSITION. INSTALLED PN: 601R14303-53 IAW REO.
2014
Part: LIGHT — BROKEN (CABIN) · airframe 26,942 hrs · 22,140 cycles
SERVICE DOOR EMERGENCY EXIT LIGHT BROKEN. SERVICE, R & R SERVICE DOOR EMERGENCY EXIT LIGHT ASSY IAW AMM.
Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 26,932 hrs · 22,134 cycles
RT OVERWING EXIT SIGN BULBS ARE BURNED OUT. REPLACED THE BULBS.
Part: BUSHING — GALLED (RT ENGINE MOUNT) · airframe 26,819 hrs · 22,055 cycles
RIGHT ENGINE FOUND GALLING ON OTBD BUSHING OF AFT ENGINE MOUNT. INSTALLED A SERVICEABLE RT ENGINE AFT SPHERICAL BUSHING IAW AMM.
Part: MOUNT — GALLED (RT ENGINE) · airframe 26,819 hrs · 22,055 cycles
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.
Part: MOUNT — GALLED (RT ENGINE) · airframe 26,819 hrs · 22,055 cycles
RIGHT ENGINE FOUND GALLING ON OTBD HOUSING OF AFT ENGINE PYLON MOUNT. R & R OTBD HOUSING OF AFT ENGINE PYLON MOUNT IAW AMM.
2013
Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 25,528 hrs · 21,059 cycles
FLOOR LEVEL EMERGENCY EXIT SIGN BULB IS BURNED OUT. FLT6485 RELAMPED.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,026 hrs · 20,691 cycles
EMERGENCY LIGHT POD IS INOPERATIVE. FLT#6356 RELAMPED.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,852 hrs · 19,791 cycles
NR 3 EMERGENCY OVERHEAD LIGHT IS BURNED OUT. (FLT 5519) REPLACED NR 2 EMERGENCY OVERHEAD LIGHT.
2012
Part: FLEX DRIVE — CORRODED (TE FLAP) · airframe 22,344 hrs · 18,664 cycles
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.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,853 hrs · 17,479 cycles
NR 4 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6410) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 20,557 hrs · 17,241 cycles
TWO FORWARD EXTERIOR EMERGENCY LIGHTS ON RIGHT SIDE ARE OUT. (FLT 5652) RELAMPED EMERGENCY LIGHTS.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,384 hrs · 17,100 cycles
AFT OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5410) RELAMPED EMERGENCY LIGHT.
2011
Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,975 hrs · 16,738 cycles
NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5362) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,749 hrs · 16,554 cycles
AFT 2 EXTERIOR EMERGENCY LIGHTS ON THE RIGHT SIDE ARE OUT. (FLT 6324) RELAMPED EMERGENCY LIGHTS.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,687 hrs · 16,494 cycles
NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6315) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,687 hrs · 16,494 cycles
RIGHT OVERWING AFT EMERGENCY EXIT LIGHT IS OUT. (FLT 5650) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,643 hrs · 16,466 cycles
NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6369) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,175 hrs · 16,088 cycles
BOTH OVERWING EMERGENCY LIGHTS AFT OF OVERWING EMERGENCY EXIT DOOR ARE OUT. (SERVICE) RELAMPED EMERGENCY LIGHTS.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,122 hrs · 16,048 cycles
NR 4 CEILING EMERGENCY LIGHT IS OUT. (FLT 5381) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,997 hrs · 15,947 cycles
NR 4 CEILING EMERGENCY LIGHT IS BURNED OUT. (FLT 6428) RELAMPED EMERGENCY LIGHT.
Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 18,429 hrs · 15,505 cycles
FS 621 AFT PRESSURE BULKHEAD CRACKED FORWARD SIDE WEB AT AFT CARGO TRACK. (C-CHECK) REPAIR PER REO.
Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 18,611 hrs · 15,647 cycles
FLOOR SUPPORT ANGLE FORWARD SIDE OF FS 280 BEAM IS CRACKED. (C-CHECK) REPLACED FLOOR SUPPORT ANGLE PER SRM.
Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 18,611 hrs · 15,647 cycles
FS 559.0 PRESSURE BULKHEAD CRACKED AT LEFT SIDE. (C-CHECK) REPAIRED PER REO.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,828 hrs · 15,021 cycles
NR 4 CEILING EMERGENCY LIGHT IS OUT. (FLT 6978) RELAMPED EMERGENCY LIGHT.
2010
Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,607 hrs · 14,824 cycles
EMERGENCY LIGHT ABOVE ROW 10 OUT. (FLT 6370) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,386 hrs · 14,647 cycles
THE 3RD OVERHEAD EMERGENCY LIGHT FROM BACK INOPERATIVE. (FLT 7017) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,122 hrs · 14,432 cycles
AFT CEILING EMERGENCY LIGHT INOPERATIVE. (FLT 6533) RELAMPED EMERGENCY LIGHT.
Part: CABLE — BINDING (CABIN DOOR) · airframe 17,083 hrs · 14,398 cycles
MAIN CABIN DOOR CABLE BINDING UP, CANNOT OPEN THE MCD MORE THAN HALF WAY. (FLT 6898) REPLACED MAIN CABIN DOOR ASSIST MOTOR ASSEMBLY.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 16,529 hrs · 13,911 cycles
NR 3 OVERHEAD EMERGENCY LIGHT INOP. (FLT 6811) RELAMPED EMERGENCY LIGHT.
Part: SHUTOFF VALVE — FAILED (AC BAY) · airframe 14,825 hrs · 12,518 cycles
UNABLE TO CONTROL CABIN ALTITUDE. (FLT 6551) REPLACED LEFT PACK PRSOV AND RIGHT PACK DUAL BYPASS VALVE.
2009
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 13,966 hrs · 11,809 cycles
RIGHT SIDE EXTERNAL EMERGENCY LIGHT INOP. (FLT 6517) RELAMPED EMERGENCY LIGHT.
Part: FITTING — CRACKED (FUSELAGE) · airframe 13,613 hrs · 11,516 cycles
FS 280 CLIPS CRACKED. (C CHECK) REPLACED PER SRM.
Part: BULKHEAD — DAMAGED (FUSELAGE) · airframe 13,613 hrs · 11,516 cycles
FS 280 BULKHEAD WEB DAMAGED. (C CHECK) REPAIRED PER REO.
Part: ADC — FAULTY (NR 2) · airframe 13,047 hrs · 11,072 cycles
FLT 6303 - ALTIMETER FLUCTUATION. REPLACED NR 2 ADC.
Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 12,246 hrs · 10,456 cycles
FLT 6543 - THIRD EMERGENCY LAMP OUT IN CEILING. RELAMPED.
Part: CONNECTOR — CORRODED · airframe 12,190 hrs · 10,412 cycles
FLT 1010 - FOUND PLUG AND JACK 167 CORRODED. REPLACED PLUG, CONNECTOR, AND PINS.
2008
Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 11,053 hrs · 9,510 cycles
CEILING EMERGENCY EXIT LIGHT IS BURNED OUT. FLIGHT 6274. RELAMPED EMERGENCY LIGHT IAW AMM 33-51-16. OPS CHECK GOOD.
Part: HOLDER — SHORTED (COCKPIT) · airframe 10,830 hrs · 9,307 cycles
F/O`S CHART HOLDER SHORTED OUT. (FLIGHT NR 6438) SECURED HARDWARE ON CHART HOLDER. OPS CHECK GOOD.
2007
Part: SUPPORT ANGLE — CRACKED (BS 625) · airframe 9,422 hrs · 8,101 cycles
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.
Part: FLOORBEAM — CRACKED (BS 621) · airframe 9,422 hrs · 8,101 cycles
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.
Part: DRIVE UNIT — MALFUNCTIONED (THRUST REVERSER) · airframe 8,505 hrs · 7,331 cycles
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.
Part: COFFEEMAKER — ODOR (GALLEY) · airframe 8,161 hrs · 7,027 cycles
FLIGHT ATTENDANT REPORTS BURNING ODOR FROM GALLEY, FLIGHT NR 6205. REPLACED LEFT HOT JUG PER CRJ MM 25-32-02. OPS CHECKED GOOD.
Part: COMPUTER — MALFUNCTIONED (AUTOPILOT SYS) · airframe 7,270 hrs · 6,276 cycles
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.
2006
Part: CONTROL UNIT — MALFUNCTIONED (MOTOR) · airframe 4,229 hrs · 3,643 cycles
STAB CH 1 WILL NOT ENGAGE. REPLACED HORIZONTAL STAB MOTOR CONTROL UNIT REF AMM 27-42-05. OPERATIONAL CHECK GOOD.
Part: BUTTON — STUCK (STAB TRIM) · airframe 4,174 hrs · 3,597 cycles
STAB TRIM CH 1 PUSH BUTTON STICKY. REPLACED STAB TRIM 1 MACH TRIM CONTROL PANEL REF CRJ MM 27-41-25. OPERATIONAL CHECK GOOD.
Part: DETECTOR — MALFUNCTIONED (TE FLAPS) · airframe 4,122 hrs · 3,553 cycles
FOUND FLAP SKEW SYSTEM INOP. INSTALLED NEW SKEW UNIT IAW 27-51-15. OPERATIONAL CHECK GOOD.
Part: TRIM SWITCH — MALFUNCTIONED (YOKE) · airframe 4,029 hrs · 3,479 cycles
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.
Part: WARNING LIGHT — FALSE ACTIVATION (TE FLAPS) · airframe 3,930 hrs · 3,387 cycles
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.
Part: CONTROL LEVER — MALFUNCTIONED (TE FLAPS) · airframe 3,770 hrs · 3,232 cycles
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.
Part: ACTUATOR — MALFUNCTIONED (STICK-PUSHER) · airframe 3,674 hrs · 3,146 cycles
(STALL FAIL) CAUTION MESSAGE APPEARED AT FL290, 285KIAS. REPLACED STALL WARNING ACTUATOR PUSHER, OPERATIONAL CHECK GOOD.
2005
Part: CONTROL UNIT — MALFUNCTIONED (SPOILER) · airframe 1,835 hrs · 1,599 cycles
FLT SPLRS FAULT, I/B AND O/B GND SPLR FAULT MESSAGES. REPLACED NR 1 SECU. OPERATIONAL CHECK GOOD IAW MM 27-61-00.
2004
Part: BPSU — OUT OF RIG (TE FLAPS) · airframe 206 hrs · 207 cycles
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.