N951SW
Registered owner: SKYWEST AIRLINES INC, UT (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
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.
184 reports on file, 2003-12-30 – 2026-07-07.
Part: WINDSHIELD — CRACKED (ZONE 200) · airframe 43,288 hrs · 37,550 cycles
RIGHT WINDSHIELD CRACK AND R WSHLD HEAT CAUTION MESSAGE CLIMBING THROUGH 18,000 FEET. (FLIGHT 6097) OPEN
Part: FRAME — CHAFED (ZONE 100) · airframe 43,287 hrs · 37,548 cycles
DURING AUDIT OF TASK CARD 53-350-500 IT WAS FOUND THAT THERE IS A CHAFED FRAME AREA AFT OF APU EXHAUST BS 654.50. REPAIRED FRAME AFT OF APU EXHAUST BS 654.5 IAW SRM 51-42-06, 51-42-21, DWG 601R35004, REV BJ, AND REO 601R-53-61-8529, REV.--. COMPLIED WITH TASK CARD 51-900-1003-SKY.
Part: SEAT TRACK — OUT OF LIMITS (ZONE 200) · airframe 43,287 hrs · 37,548 cycles
REMOVE AND REPLACE DAMAGED OUT OF LIMITS SEAT RAIL BEAM P/N 601R35031-263. SEE JOB HN00303609, CAMP# 31969028. (32083421). (C-CHECK RO 06/25/2026)REMOVED AND REPLACED SEAT RAIL BEAM AT LBL27 BETWEEN APPROX. FS574 AND FS621. IAW SRM 51-42-06, SRM 51-42-21, REO 601R-53-61-3778, REV.-B AND DWG 601R35031, SHEET 7, REV AG. COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY. MAJOR REPAIR.
Part: ANGLE — CRACKED (ZONE 200) · airframe 43,287 hrs · 37,548 cycles
CO-PILOT SIDE POST OTBD LWR ANGLE CRACKED. REPLACED CO-PILOT SIDE POST OTBD LOWER ANGLE IAW DWG 601R33007, REV -U, SRM 51-42-21, AND COMPLIED WITH TASK CARD 51-900-1003-SKY.
Part: FLOORBEAM — DAMAGED (ZONE 200) · airframe 43,287 hrs · 37,548 cycles
AT BS 574, RBL 36 FLOOR SUPPORT HAS A SCRIBE LINE ACROSS THE TOP. INSTALLED NEW TOP CAP STRIP AT BS 574 AT APPOX RBL36 IAW SRM 51-42-06, SRM 51-42-15, AND DWG 601R35031, REV AG. FOR FASTENER CALL OUTCOMPLIED WITH TASK CARD 51-900-1003-SKY.
Part: HINGE FITTING — CORRODED (ZONE 300 ELEV) · airframe 43,287 hrs · 37,548 cycles
UPON REMOVAL ON JOB HN00303104 CAMP 31954799, FOUND LT ELEVATOR L/E HINGE FITTING ASSY, ES 16.52 TO HAVE PITTING CORROSION IN BEARING BORES ON BOTH HINGE HALVES. REPLACE HINGE FITTING ASSY. INSTALLED 1 EA NEW L/E HINGE FITTING ASSY ON L/H ELEVATOR AT ES16.52 REF DWG 601R24025 REV -G, SRM 51-42-06, AND SRM 51-42-21. COMPLIED WITH SKY CARD 51-900-1003-SKY.
Part: BULKHEAD WEB — CRACKED (ZONE 200) · airframe 43,287 hrs · 37,548 cycles
UPON REMOVAL FWD FLOORBEAM ANGLE AT BS 280 BETWEEN RBL 9 AND LBL 9, FOUND CRACKED. REPAIRED BULKHEAD WEB IAW REO 601R-53-11-926, REV -B, & REO 601R-53-21-3811, REV -, COMPLIED WITH TASK CARD 51-900-1003-SKY.
Part: HINGE ARM — GOUGED (ZONE 500 FLAP) · airframe 43,287 hrs · 37,548 cycles
LEFT INBOARD FLAP HINGE ARM WS 80.50 ATTACH LUG GOUGED. REPAIRED GOUGED DAMAGE ON LT INBD FLAP HINGE ARM WS 80.50 ATTACH LUG IAW REO 601R-57-54-392 REV -. COMPLIED WITH SKYCARD 51-900-1003-SKY. MAJOR REPAIR.
Part: FLOORBEAM — CRACKED (ZONE 200) · airframe 43,287 hrs · 37,548 cycles
CRACKED ON ANGLE AT FLOORBEAM ON BS 621 BETWEEN LBL 27 & LBL 35. COMPLIED WITH GREO 601R-53-61-117, REV -E. FABRICATED AND INSTALLED NEW ANGLE IAW REO 601R-53-61-8533, REV. --, AND RESTORED FINISH AND APPLIED CIC, PRESSURE LEAK CHECK GOOD AT THIS TIME. COMPLIED WITH 51-900-1003-SKY.
Part: WINDSHIELD — CRACKED (ZONE 200) · airframe 43,287 hrs · 37,548 cycles
PILOT SIDE WINDOW CRACKED ALL AROUND THE EDGES OF THE WINDOW. INSTALLED NEW/SERVICEABLE PILOT SIDE WINDOW IAW AMM 56-12-01-400-801. COMPLIED WITH 56-220-1000-SKY.
Part: INTERCOSTAL — CORRODED (ZONE 200) · airframe 43,287 hrs · 37,548 cycles
PASSENGER DOOR SURROUND STRUCTURE STR 21L INTERCOSTAL (BACKUP SILL) BS 310 - 319.70 IS CORRODED THROUGH AND CRACKED. REMOVED AND REPLACED INTERCOSTAL AT STR 21L BETWEEN BS 310 & 333. IAW SRM 51-42-06, SRM 51-42-21, AND DRAWING 601R31527, REV AM, SHEET 2. COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY. MAJOR REPAIR.
Part: SKIN — SCRATCHED (ZONE 100) · airframe 43,287 hrs · 37,548 cycles
CIRCUMFERENTIAL FUSELAGE SPLICE AT BS 280, BETWEEN STR 23-22 LT, HAS SCRATCHES, COMPLIED WITH REO 601R-53-00-936 REV-, ALL STEPS, STEP 1 ENSURED BLEND-OUTS WERE PERFORMED TO A SMOOTH CONTOUR, STEP 2 PERFORMED NDT (SEE STEP 2A OF THIS CONTINUE CARD), STEP 3 REPLACED AFFECTED FASTENERS AND STEP 4 RESTORED FINISH TO AREA.COMPLIED WITH 51-900-1003-SKY, LEAK CHECK GOOD.
Part: RIB — CRACKED (ZONE 600) · airframe 43,287 hrs · 37,548 cycles
CRACK NOTED ON RT WING BATT RIB AT WS48.3. REMOVED AND REPLACED RT WING BATT RIB AT WS48.3 REF. SRM 51-42-21 REV. AND DWG 600-10204, REV-M. COMPLIED WITH TASK CARD 51-900-1003-SKY.
Part: DOUBLER — CORRODED (ZONE 100) · airframe 43,287 hrs · 37,548 cycles
CORROSION NOTED ON DOUBLER COMMON TO ELECTRICAL CONNECTORS J410 AND J412 AT RT RIB REAR SPAR ASSY. AT WS53.60. REMOVED AND INSTALLED NEW DOUBLER ANGLE ON BATT RIB, WS53.6 PER CRJ200 SRM 51-42-06 AND DWG NO. 601R10203 REV -G. OPS CHECK GOOD. COMPLIED TASK CARD 51-900-1003-SKY. SEE CONTINUATION FOR DETAILS.
Part: RETAINER — CORRODED (ZONE 800) · airframe 43,287 hrs · 37,548 cycles
AVIONICS BAY DOOR FORWARD LEFT SEAL RETAINER CORRODED. REMOVED AND INSTALLED NEW AVIONICS BAY DOOR FORWARD LEFT SEAL RETAINER IAW SRM 51-42-06 AND DWG CC670-38651 REV -E. COMPLIED WITH TASK CARD 51-900-1003-SKY.
Part: ANGLE — CORRODED (ZONE 100) · airframe 43,287 hrs · 37,548 cycles
UNDERFLOOR BS 605, ANGLE BETWEEN STR 20 - 21 LT, WAS CORRODED, REMOVED AND INSTALLED NEW ANGLE AT BS 605 BETWEEN STR 20L- STR 21L IAW SRM 51-42-06, SRM 51-42-21, & DWG 601R36026, REV AF, RESTORED FINISH TO OUTER SKIN RIVETS AND INSIDE ANGLE AREA IAW SRM 51-21-16, COMPLIED WITH 51-900-1003-SKY
Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 43,287 hrs · 37,548 cycles
UNDERFLOOR BS 559+48, RBL 9-27, FLOORBEAM HAS CORROSION, REMOVED AND REPLACED THE PLATE AT FS 559+48 BETWEEN LBL9 AND LBL27. IAW SRM 51-42-06, SRM 51-42-15, AND DWG 601R32215, REV. M, SHEET 8. COMPLIED WITH TASK CARD 51-900-1003-SKY. MAJOR REPAIR.
Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 43,287 hrs · 37,548 cycles
UNDERFLOOR BS 589, LBL 9 - 27, FLOORBEAM WAS CORRODED, INSTALLED A NEW TOP CAP STRIP IAW SRM 51-42-21, REV 39, 51-42-06, REV 39, SRM 51-42-15, REV 39, AND DWG. 601R35031 REV. AG COMPLIED WITH TASK CARD 51-900-1003-SKY.
Part: SKIN — DENTED (ZONE 800) · airframe 43,287 hrs · 37,548 cycles
PASSENGER DOOR INNER SKIN UNDERNEATH FWD STAIR WEB DRAG ANGLE DENTED NEXT TO A HOLE. COMPLIED REPAIR STEPS 1 TO 15 ON PASSENGER DOOR INNER SKIN BETWEEN DOOR DATUM 6 AND DOOR DATUM 7 OF REO 601R-52-11-3096, REV. --. COMPLIED TASK CARD 51-900-1003-SKY.
Part: WINDSHIELD — CRACKED (ZONE 200) · airframe 43,287 hrs · 37,548 cycles
PILOT WINDSHIELD HAS POSSIBLE CRACK LT LOWER SIDE. INSTALLED NEW SERVICEABLE PILOT WINDSHIELD IAW AMM 56-11-01-400-801.
Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 43,287 hrs · 37,548 cycles
FLOOR SUPPORT HAD MULTIPLE SPOTS OF CORROSION AT LBL 27 BETWEEN BS 574 - 621. REPLACEMENT OF FLOOR SUPPORT AT LBL 27 BETWEEN BS 574 AND BS 606.5 PERFORMED ON JOB HN00307254, CAMP 32083421. REPAIRED END FITTING AT LBL 27 BETWEEN BS 606.5 AND BS 621 IAW REO 601R-53-61-8509, REV--. COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY. MAJOR REPAIR.
Part: LUG — DAMAGED (ZONE 800) · airframe 43,287 hrs · 37,548 cycles
PASSENGER DOOR HINGE LUGS ELONGATED ON FUSELGE SIDE. INSTALLED NEW PASSENGER DOOR HINGE ON FUSELAGE SIDE. IAW SRM 53-21-23 REPAIR NR -01 AND REO 601R-53-21-656, REV. B. COMPLIED WITH 51-900-1003-SKY. LEAK CHECKED GOOD.
Part: SKIN — GOUGED (ZONE 500 AILERON) · airframe 43,287 hrs · 37,548 cycles
LEFT AILERON LEADING EDGE GOUGED AND CHAFED IN MULTIPLE LOCATIONS. REPLACED THE LH AILERON LEADING EDGE SKIN IAW DWG CC670-13000, REV-D, SRM 51-42-06, SRM 51-42-21, AND SRM 51-42-22. COMPLIED WITH TASK CARD 51-900-1003-SKY.
Part: SKIN — GOUGED (ZONE 600 AILERON) · airframe 43,287 hrs · 37,548 cycles
RIGHT AILERON LEADING EDGE GOUGED AND CHAFED IN MULTIPLE LOCATIONS. REPLACED RT AILERON LEADING EDGE SKIN IAW DWG 601R13031, REV-K , SRM 51-42-06 AND SRM 51-42-13. COMPLIED WITH TASK CARD 51-900-1003-SKY.
Part: HOUSING — GOUGED (ZONE 800) · airframe 43,287 hrs · 37,548 cycles
CARGO DOOR EXTERIOR HANDLE HOUSING GOUGED. FOUND DAMAGE TO BE OUT OF LIMITS IAW REO 601R-52-31-086, REV -. REMOVED AND REPLACED CARGO DOOR EXTERIOR HANDLE HOUSING ASSY. IAW SRM 51-40-11, SRM 51-42-21, SRM 51-23-00 AND DWG CC670-38702, REV -F. RESTORED FINISH TO REWORK AREA IAW SRM 51-25-01. COMPLIED WITH TASK CARD 51-900-1003-SKY.
Part: RIB — CORRODED (ZONE 500) · airframe 43,287 hrs · 37,548 cycles
LEFT WING BATT RIB WS53.60 FORWARD END, ANGLE IS CORRODED ON THE FLANGE AND WEB. REMOVED AND INSTALLED NEW ANGLE ON LEFT WING BATT RIB WS53.60 FWD. IAW DWG 601R10203, REV G. AND SRM 51-42-21, SRM 51-42-06 AND SRM 51-42-15. OPS TESTED GOOD. COMPLIED WITH TASK CARD 51-900-1003-SKY.
Part: RETAINER — CORRODED (ZONE 800) · airframe 43,287 hrs · 37,548 cycles
AVIONIC BAY DOOR FORWARD RIGHT ANGLE UNDER SEAL RETAINER HAS CORROSION AROUND FASTENER HOLES. REMOVED AND INSTALLED NEW FORWARD RIGHT ANGLE ON AVIONICS BAY DOOR IAW SRM 51-42-06, SRM 51-42-21, SRM 51-41-02, AND DWG CC670-38651 REV -E. OPS & LEAK CHKD GOOD. COMPLIED WITH TASK CARD 51-900-1003-SKY.
Part: RETAINER — CORRODED (ZONE 800) · airframe 43,287 hrs · 37,548 cycles
AVIONIC BAY DOOR AFT RIGHT ANGLE UNDER SEAL RETAINER HAS CORROSION AROUND FASTENER HOLES. REMOVED AND REPLACED AFT RIGHT ANGLE ON AVIONICS BAY DOOR IAW SRM 51-42-06, SRM 51-42-21, SRM 51-41-02, AND DWG CC670-38651 REV -E SHEET 1. COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY STRUCTURAL MAJOR REPAIR (**RII**)
Part: VANE — DENTED (ZONE 600 FLAP) · airframe 43,287 hrs · 37,548 cycles
RIGHT OTBD FLAP VANE LEADING EDGE DENTED ON INBD END. REPAIRED DENTED AREA ON THE RH OTBD FLAP VANE LEADING EDGE AT INBD END IAW SRM 51-42-13, REV 39, AND DWG 601R14502, REV D. COMPLIED WITH TASK CARD 51-900-1003-SKY.
Part: FLOORBEAM — DAMAGED (ZONE 200) · airframe 43,287 hrs · 37,548 cycles
AT BS 574, RBL 36 FLOORBEAM HAS A SCRIBE LINE ACROSS THE TOP. REMOVED AND REPLACED FLOORBEAM CAP STRIP AT BS 574 BETWEEN RBL 9 AND RBL 27 IAW SRM 51-42-06, REV-. COMPLIED WITH TASK CARD 51-900-1003-SKY AND DWG. 601R35031 REV. AG.
Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 43,287 hrs · 37,548 cycles
FLOOR SUPPORT LBL 9 JUST FORWARD OF BS 621 CORRODED AROUND NUTPLATES. REMOVED CORROSION FROM FLOOR SUPPORT LBL 9 JUST FORWARD OF BS 621 IAW REO 601R-53-61-8497. REV. -, ALL STEPS COMPLIED WITH. COMPLIED WITH TASK CARD 51-900-1003-SKY.
Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 43,287 hrs · 37,548 cycles
RIGHT PRESSURE FLOOR SUPPPORT HAS MULTIPLE AREAS OF CORROSION. REPAIRED MULTIPLE AREAS OF CORROSION IAW SRM 51-26-00, GREO 601R-53-41-666, REV-C, & REO 601R-53-41-3421 REV-. COMPLIED WITH TASK CARD 51-900-1003-SKY. PRESSURE LEAK CHECK GOOD AT THIS TIME.
Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 43,287 hrs · 37,548 cycles
LEFT PRESSURE FLOOR SILL HAS MULTIPLE AREAS OF CORROSION BETWEEN APPROX. BS 409+128 - BS 559. REMOVED MULTIPLE AREAS OF CORROSION ON LT PRESSURE FLOOR SILL BETWEEN APPROX. BS 409+128 - 559 IAW SRM 51-21-06. REV. 39. COMPLIED W/ ALL STEPS OF REO 601R-53-41-3420, REV--. COMPLIED W/ SKYWEST TASK CARD 51-900-1003-SKY.
Part: SKIN — CORRODED (ZONE 600) · airframe 43,287 hrs · 37,548 cycles
RBL45 RT WING LOWER PLANK TRAILING EDGE AREA, CORRODED & CHAFFED FROM THE WING TO BODY FAIRING. REPAIRED RBL45 RT WING LOWER PLANK TRAILING EDGE IAW REO 601R-57-21-4071 REV -. COMPLIED WITH TASK CARD 51-900-1003-SKY.
Part: SKIN — CORRODED (ZONE 500) · airframe 43,287 hrs · 37,548 cycles
LBL 45 LT WING LOWER PLANK TRAILING EDGE AREA, CORRODED & CHAFED FROM THE WING TO BODY FAIRING. REPAIRED LBL 45 LT WING LOWER PLANK TRAILING EDGE AREA IAW GREO 601R-57-21-880, REV-D. NOTES/STEPS 1, 2, 3,5,6,7,9 AND10.,COMPLIED WITH 51-900-1003-SKY, FUEL LEAK CHECK GOOD.
Part: SKIN — DAMAGED (ZONE 100) · airframe 43,287 hrs · 37,548 cycles
TWO SCREW HOLES ELONGATED ON LT SIDE EXTERNAL SKIN BETWEEN BS 409+80 - 409+96, STR 18L- STR 20L. RECEIVED AND COMPLIED WITH REO 601R-53-31-1369 REV.--, COMPLIED WITH 51-900-1003-SKY, LEAK CHECK GOOD.
Part: SKIN — CORRODED · airframe 43,287 hrs · 37,548 cycles
EXTERNAL SKIN IS CORRODED AT SEVERAL LOCATIONS SURROUND SCREW HOLES COMMON TO PANEL 195BB. REPAIRED EXTERNAL SKIN COMMON TO PANEL 195BB IAW REO 601R-53-00-937 REV --. COMPLIED WITH TASK CARD 51-900-1003-SKY.
Part: SKIN — GOUGED (ZONE 100) · airframe 43,287 hrs · 37,548 cycles
LEFT EXTERNAL SKIN IS GOUGED BETWEEN BS 559+96 - 574, STR 19L - 21L. REPAIRED LT EXTERNAL SKIN IAW REO 601R-53-00-937, REV--. COMPLIED WITH TASK CARD 51-900-1003-SKY.
Earlier reports · 2003–2020 · 146 reports
2020
Part: LINK — OUT OF LIMITS (ENGINE MOUNT)
OUT OF LIMIT INDICATION WAS DISCOVERED DURING ULTRASONIC TEST NDT 71-23-103 PART 4. TSN & CSN UNKNOWN PER OPERATOR.
Part: SKIN — CHAFED (RT FLAP VANE) · airframe 41,770 hrs · 36,207 cycles
RIGHT INBOARD FLAP VANE LEADING EDGE CHAFED AT OUTBOARD STOP .010" DEEP REQUIRES REPLACEMENT. C-CHECK RO 12/04/2020. REMOVED DAMAGED LEADING EDGE CAP AND INSTALLED A NEW PART, IAW CRJ 200 SRM.
Part: SKIN — CHAFED (RT FLAP VANE) · airframe 41,770 hrs · 36,207 cycles
RIGHT INBOARD FLAP VANE LEADING EDGE CHAFED AT MIDDLE-OUTBOARD STOP .010" DEEP REQUIRES REPLACEMENT. C-CHECK RO 12/04/2020. REMOVED AND INSTALLED NEW RT INBOARD FLAP VANE LEADING EDGE, IAW CRJ 200 SRM. SEE CONTINUATION CARD FOR DETAILS OF WORK PREFORMED.
Part: ANGLE — CRACKED (CABIN) · airframe 41,770 hrs · 36,207 cycles
RT UPPER OBLIQUE ANGLE BETWEEN FS 621.00 AND FS 625.00 IS CRACKED. C-CHECK RO 12/04/2020. REPLACED RT UPPER OBLIQUE ANGLE BETWEEN FS 621.00 AND FS 625.00, IAW CRJ-200 SRM. SEE CONTINUE CARD FOR DETAILS OF WORK PERFORMED.
Part: SKIN — CHAFED (RT FLAP VANE) · airframe 41,770 hrs · 36,207 cycles
RIGHT INBOARD FLAP VANE LEADING EDGE CHAFED AT INBOARD STOP .020" DEEP REQUIRES REPLACEMENT. C-CHECK RO 12/04/2020. REMOVED DAMAGED RT INBOARD FLAP VANE LEADING EDGE INBOARD CAP AND INSTALLED A NEW INBOARD CAP, IAW CRJ 200 SRM.
Part: FLOORBEAM — CRACKED (CABIN) · airframe 41,770 hrs · 36,207 cycles
RBL 9 FLOORBEAM INBOARD CLIP AT FS 280 IS CRACKED. C-CHECK RO 12/04/2020. REMOVED DAMAGED INBOARD CLIP ON RBL 9 ATTACHED AT FS 280 AND INSTALLED NEW SERVICEABLE CLIP, IAW CRJ200-SRM AND RE0.
Part: SEAT TRACK — CORRODED (CABIN) · airframe 41,770 hrs · 36,207 cycles
LBL 9 SEAT TRACK FROM FS 409 TO 409+126 HAS SEVERAL AREAS OF CORROSION. C-CHECK RO 12/04/2020. REMOVED AND REPLACED SEAT TRACK, IAW CRJ 200 AMM.
Part: SKIN — CHAFED (LT FLAP VANE) · airframe 41,770 hrs · 36,207 cycles
LEFT INBOARD FLAP VANE LEADING EDGE CHAFED AT INBOARD .018" OUT OF LIMIT REQUIRES REPLACEMENT. C-CHECK RO 12/04/2020. REMOVED LT INBOARD FLAP LEADING EDGE INBOARD PANEL AND INSTALLED A NEW PANEL, IAW CRJ 200 SRM.
Part: FLOOR SUPPORT — CORRODED · airframe 41,770 hrs · 36,207 cycles
PAX DOOR FLOOR SUPPORT ANGLE IS CORRODED. C-CHECK RO 12/04/2020. REPLACED PAX DOOR FLOOR SUPPORT ANGLES. REFERENCE CONTINUATION CARD FOR WORK PREFORMED.
Part: STRAP — CORRODED (FUSELAGE) · airframe 41,770 hrs · 36,207 cycles
RT OUTBOARD STRAP AT FS 559.00 CORRODED IN SEVERAL AREAS 601 R31025-29. C-CHECK RO 12/04/2020. REMOVED DAMAGED RT OUTBOARD STRAP AT FS 559 AND INSTALLED NEW SERVICEABLE STRAP, IAW CRJ200-SRM.
Part: FLOORBEAM — CRACKED (ZONE 200) · airframe 41,770 hrs · 36,207 cycles
LBL 9 FLOORBEAM INBOARD CLIP AT FS 280 IS CRACKED. C-CHECK RO 12/04/2020. REMOVED DAMAGED INBOARD CLIP AT LBL 9 ATTACHED TO FS 280 AND INSTALLED NEW SERVICEABLE CLIP, IAW REO, AND CRJ200-SRM.
Part: SEAT TRACK — CORRODED (CABIN) · airframe 41,770 hrs · 36,207 cycles
RBL 9 SEAT TRACK BETWEEN FS 409.0 AND 409+126 HAS SEVERAL AREAS OF CORROSION. C-CHECK RO 12/04/2020. REMOVED DAMAGED SEAT TRACK, LOCATED AND DRILLED NEW SEAT TRACK AND INSTALLED, IAW CRJ 200 SRM AND AMM.
Part: SKIN — CHAFED (LT FLAP VANE) · airframe 41,770 hrs · 36,207 cycles
LEFT INBOARD FLAP VANE LEADING EDGE CHAFED AT OUTBOARD .010" OUT OF LIMIT REQUIRES REPLACEMENT. C-CHECK RO 12/04/2020. LT INBOARD FLAP LEADING EDGE OUTBOARD PANEL WAS REMOVED AND NEW PART INSTALLED, IAW CRJ 200 SRM.
Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 41,770 hrs · 36,207 cycles
FLOOR SUPPORT EXTRUSION HAS TWO AREAS OF CORROSION AT RBL 9 BETWEEN FS 409+5 AND FS 409+8. C-CHECK RO 12/04/2020. PERFORMED REPAIR AT FLOOR SUPPORT EXTRUSION AT RBL 9 BETWEEN FS 409+5 AND 409+8, IAW CRJ 200 SRM. COMPLIED WITH TASK CARD AND ATTACHED COMPLETED FORM 337. NO WEIGHT CHANGES NOTED.
Part: ISOLATOR — BROKEN (PRESSURE BLKHD) · airframe 41,770 hrs · 36,207 cycles
FORWARD SIDE OF FS 621 PRESSURE BULKHEAD HAS TWO BROKEN ISOLATORS. 1 RBL 27 BOTTOM, 1 RBL 45 BOTTOM. C-CHECK RO 12/04/2020. REMOVED TWO EACH DAMAGED ISOLATOR MOUNTS INSTALL NEW, IAW CRJ200 SRM.
Part: PLATE — CRACKED (CARGO BAY) · airframe 41,770 hrs · 36,207 cycles
CARGO DOOR FLOOR SILL CORRODED IN NUMEROUS AREAS AND ALSO IS CRACKED. C-CHECK RO 12/04/2020. REMOVED AND REPLACED CARGO DOOR FLOOR SILL, IAW REO CRJ-200 SRM. MAJOR REPAIR TASK & FORM M-337 COMPLETED AND ATTACHED. NO WEIGHT CHANGE REQUIRED. REFERENCE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.
Part: ISOLATOR — GOUGED (PRESSURE BLKHD) · airframe 41,770 hrs · 36,207 cycles
FS 621 PRESSURE BULKHEAD FORWARD SIDE HAS THE TOP ISOLATOR BRACKET AT RBL 18 WITH 2 GOUGES IN RADIUS. C-CHECK RO 12/04/2020. REMOVED DAMAGED ISOLATOR BRACKET, FABRICATED A NEW BRACKET AND INSTALLED, IAW BOMBARDIER REO.
Part: PRESSURE BLKHD — CHAFED (AFT CABIN) · airframe 41,770 hrs · 36,207 cycles
FORWARD SIDE OF FS 621 PRESSURE BULKHEAD HAS A CHAFED RIVET AT WL 86.5, RBL 18. C-CHECK RO 12/04/2020. REPLACED CHAFE RIVETS AT FS 621 BULKHEAD AT WL 86.5 RBL 18 UPON FURTHER INVESTIGATION FOUND AND REPLACED 5 EA CHAFE RIVETS ON 621 BULKHEAD, IAW CRJ200 SRM.
Part: FLOORBEAM — CRACKED (ZONE 200) · airframe 41,770 hrs · 36,207 cycles
LBL 9 FLOOR BEAM OB CLIP AT FS 280 IS CRACKED. C-CHECK RO 12/04/2020. REMOVED DAMAGED CLIP ON LBL 9 FLOOR BEAM ATTACHED TO FS 280 AND INSTALLED NEW SERVICEABLE CLIP, IAW REO, AND CRJ200-SRM.
Part: FLOORBEAM — CRACKED (ZONE 200) · airframe 41,770 hrs · 36,207 cycles
RBL 9 FLOOR BEAM OUTBOARD CLIP AT FS 280 IS CRACKED. C-CHECK RO 12/04/2020. REMOVED DAMAGED CLIP ON RBL 9 FLOOR BEAM ATTACHED TO FS 280 AND INSTALLED NEW SERVICEABLE CLIP, IAW CRJ200-SRM AND REO.
2019
Part: STRINGER — CORRODED (FUSELAGE) · airframe 69,684 hrs · 41,054 cycles
STRINGER 28L CORRODED BETWEEN STA 360+12' TO 360+15' / CUT CORRORED STR 28L BAT STA. 388 FABRICATED NEW STRINGER 28L AND STRINGER SPLICE FOR STA 388 STR 28L MATERIAL USED STRINGER BAC 1498-138 P.O 1593006 AND SPLICE MATERIAL 7530449 P.O 1617089.PICK UP HOLES AND TRIMED AS PER BOEING 737 SRM 53-00-03-2R-1 REPAIR 1 FIG 205 TREATED AND PROMED AND INSTALLED STRINGER REPAIR AS PER REF BOEING 737 SRM 51-20-01-0G-0 & 737 SRM 53-00-03-2R-1 REPAIR
2018
Part: FRAME — BENT (VERTICAL STAB) · airframe 37,879 hrs · 32,692 cycles
VERTICAL STABILIZER HAS A WARPED/BENT WEB AROUND THE STINGER LIGHT CONDUIT. (C-CHECK) REMOVED AND INSTALLED NEW FRAME ON VERTICAL STABILIZER REF SRM 51-42-06.
Part: SKIN — CHAFED (RT WING) · airframe 37,879 hrs · 32,692 cycles
RT LOWER WING SKIN CHAFED.(C-CHECK) REPAIRED RT LOWER WING SKIN, COMPLIED WITH REO 601R-57-21-880.
Part: SKIN — CHAFED (LT WING) · airframe 37,879 hrs · 32,692 cycles
LT LOWER WING SKIN CHAFFED. (C-CHECK) REPAIRED LT LOWER WING SKIN REF REO 601R-57-21-2881.
Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 37,879 hrs · 32,692 cycles
FLOORBOARD SUPPORT ANGLE IS CORRODED. (C-CHECK) R&R DAMAGED FLOOR SUPPORT ANGLE REF SRM 51-42-06.
Part: CAP — DENTED (PAX DOOR) · airframe 37,879 hrs · 32,692 cycles
PAX DOOR AFT LOWER CORNER IS DENTED. (C-CHECK) REMOVED AND REPLACED PAX DOOR AFT LOWER CAP REF SRM 51-42-13.
Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 37,879 hrs · 32,692 cycles
SERVICE DOOR THRESHOLD HAS CORROSION. (C-CHECK) R&R SERVICE DOOR THRESHOLD PLATE AND DOME NUT PLATES. REF SRM 51-21-06, SRM 51-40-11.
Part: GUIDE PLATE — CHAFED (TE FLAP) · airframe 37,879 hrs · 32,692 cycles
LT FLAP PANEL IS CHAFED & GOUGED ON GUIDE PLATE. (C-CHECK) REMOVED AND REPLACED GUIDE PLATE. REF SRM 57-55-00, 57-00-00 AND 51-42-06, CLEARANCE CHECKED GOOD.
Part: CAP — DENTED (PAX DOOR) · airframe 37,879 hrs · 32,692 cycles
PAX DOOR FWD LOWER CORNER IS DENTED. (C-CHECK) REMOVED AND REPLACED PAX DOOR FWD LOWER CAP REF SRM 51-42-13.
Part: SKIN — DENTED (FUSELAGE) · airframe 37,879 hrs · 32,692 cycles
FUSELAGE SKIN DENT AFT ACCESSORY DOOR. (C-CHECK) REWORKED DENT IAW REO 601R-51-00-309.
Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 37,879 hrs · 32,692 cycles
PAX DOOR INTERCOSTAL CORRODED. (C-CHECK) REMOVED AND INSTALLED NEW PAX DOOR INTERCOSTAL REF SRM 51-42-06.
Part: FORMER — CORRODED (PAX DOOR) · airframe 37,879 hrs · 32,692 cycles
PAX DOOR AFT FORMER CORRODED. (C-CHECK) REMOVED AND INSTALLED PAX DOOR AFT FORMER REF SRM 51-42-06.
Part: SKIN — CHAFED (COWLING) · airframe 37,879 hrs · 32,692 cycles
CORE COWL CHAFED ON OUTER SKIN. (C-CHECK) REPAIRED CORE COWL CHAFES PER CMM 71-12-01-300-822-A01. OPS CHECKS GOOD.
Part: SKIN — DENTED (LT WING) · airframe 37,879 hrs · 32,692 cycles
DENT ON LEFT WING LEADING EDGE. (C-CHECK) REMOVED AND REPLACED NEW LE SKIN REF SRM 51-42-06. ALL CHECKS GOOD.
2017
Part: SKIN — DENTED (BS 605-621) · airframe 35,977 hrs · 30,709 cycles
FUSELAGE SKIN DENTED AT THE AFT OF CARGO DOOR OPENING, BETWEEN BS 605 - 621, STRINGERS 15L - 16L. REPAIRED THE SKIN IAW SRM AND REO.
Part: WIRE HARNESS — DAMAGED (NLG) · airframe 35,949 hrs · 30,671 cycles
GEAR DISAGREE. RETURNED TO FIELD. REPLACED THE DAMAGED NOSE GEAR WIRE HARNESS.
2016
Part: FLOOR SUPPORT — CORRODED (BS 574-621) · airframe 34,051 hrs · 28,706 cycles
AFT CARGO FLOOR SUPPORT BS 621 TO 574 RBL 41.75 HAS CORROSION AT VARIOUS NUT PLATE LOCATIONS. REPAIRED IAW REO.
Part: PANEL — CHAFED (RIGHT WING) · airframe 34,051 hrs · 28,706 cycles
RIGHT WING PANEL 699AB IS CHAFED. INSTALLED A NEW PANEL IAW SRM.
Part: PLATE — CORRODED (SERVICE DOOR) · airframe 34,051 hrs · 28,706 cycles
SERVICE DOOR PROTECTOR PLATE HAS CORROSION ON UNDER SIDE OF TOP EDGE AROUND SCREW HOLES. REMOVED AND REPLACED SERVICE DOOR PROTECTOR PLATE IAW SRM.
Part: STRUCTURE — CORRODED (PAX DOOR) · airframe 34,051 hrs · 28,706 cycles
CORROSION AROUND SCREW HOLES UNDER PANEL 832GL OF PAX DOOR. REPAIRED IAW EA.
Part: STRUCTURE — CORRODED (PAX DOOR) · airframe 34,051 hrs · 28,706 cycles
CORROSION AROUND SCREW HOLES UNDER PANEL 832BL OF PAX DOOR. REPAIRED IAW EA.
Part: STRUCTURE — CORRODED (PAX DOOR) · airframe 34,051 hrs · 28,706 cycles
CORROSION AROUND SCREW HOLES UNDER PANEL 832ER OF PAX DOOR. REPAIRED IAW EA.
Part: REINFORCEMENT — DAMAGED (BS 559) · airframe 34,051 hrs · 28,706 cycles
REPAIR & REINFORCEMENT FOR BS 559 LWR CAP ANGLES LBL 9 & RBL 18 DUE TO DAMAGE. REPAIRED & REINFORCED IAW REO. PRESSURE LEAK CHECKED GOOD..
2014
Part: TRUNNION — CRACKED (RT MLG) · airframe 29,464 hrs · 24,538 cycles
RIGHT MLG TRUNION HAS FOUR CRACK INDICATIONS AND ONE EXISTING OVERSIZE HOLE. REPAIRED RT MLG TRUNNION IAW REO.
Part: TRUNNION — CRACKED (LT MLG) · airframe 29,464 hrs · 24,538 cycles
FOUND A CRACK INDICATION ON THE LT MLG TRUNNION, HOLE IS REAMED TO 0.330. REPAIRED IAW REO.
Part: VANE — CHAFED (LT WING TE FLAP) · airframe 29,464 hrs · 24,538 cycles
LEFT INBD FLAP, CENTER VANE CAP CHAFED BEYOND LIMITS. REMOVED AND REPLACED WITH NEW FABRICATED VANE CAP IAW SRM.
Part: FLOORBEAM — CRACKED (BS 280) · airframe 29,464 hrs · 24,538 cycles
BS 280 FLOORBEAM OTBD ANGLE RBL 9 IS CRACKED, R & R THE ANGLE IAW REO.
Part: SKIN — CHAFED (RT WING TE FLAP) · airframe 29,464 hrs · 24,538 cycles
RIGHT INBD FLAP INNER SKIN CHAFED FROM GOUND WIRE CONTACT . REMOVED DAMAGE IAW SRM AND FOUND WITHIN LIMITS IAW REO.
Part: VANE — CHAFED (RT WING TE FLAP) · airframe 29,464 hrs · 24,538 cycles
RIGHT INBD FLAP, INBD VANE CAP IS CHAFED. BLENDED INBD FLAP, INBD VANE CAP, IAW REO.
Part: VANE — CHAFED (LT WING TE FLAP) · airframe 29,464 hrs · 24,538 cycles
LEFT INBD FLAP, CENTER VANE CAP IS CHAFED. BLENDED IAW REO AND FOUNDOUT OF LIMITS, REPLACED.
Part: SKIN — CHAFED (LT WING TE FLAP) · airframe 29,464 hrs · 24,538 cycles
LEFT INBD FLAP INNER SKIN CHAFED FROM GOUND WIRE CONTACT. REMOVED DAMAGE IAW SRM AND FOUND TO BE WITHIN LIMITS IAW REO.
Part: HINGE — GOUGED (PAX DOOR) · airframe 29,464 hrs · 24,538 cycles
PASSENGER DOOR HINGE HALF, DOOR SIDE, THIRD LUG FROM AFT END GOUGED, C-CHECK, RO 10/3/14. BLENDED GOUGE ON PAX DOOR HINGE HALF, DOOR SIDE, THIRD LUG FROM AFT END. ORIGINAL MATERIAL THICKNESS 0.120". MATERIAL REMAINING 0.121". WITHIN LIMITS IAW REO. TYPE I, ITEMS 1, 2, 3. REMAINING WALL THICKNESS MUST BE GREATER THAN 0.100". REO COMPLIED WITH.
Part: VANE — CHAFED (LT WING TE FLAP) · airframe 29,464 hrs · 24,538 cycles
LEFT INBD FLAP, INBD VANE CAP IS CHAFED. BLENDED IAW REO AND FOUND OUT OF LIMITS,
Part: VANE — CHAFED (LT WING TE FLAP) · airframe 29,464 hrs · 24,538 cycles
LEFT INBD FLAP, OTBD VANE CAP IS CHAFED. BLENDED LEFT INBD FLAP, OTBD VANE CAP IAW REO. REPLACED VANE CAP.
Part: VANE — CHAFED (RT WING TE FLAP) · airframe 29,464 hrs · 24,538 cycles
RIGHT INBD FLAP, OTBD VANE CAP IS CHAFED. BLENDED RT INBD FLAP, OTBD VANE CAP IAW REO. BLEND OUT OF LIMITS, REPLACED THE VANE CAP.
Part: SKIN — DENTED (PAX DOOR) · airframe 29,464 hrs · 24,538 cycles
PAX DOOR LOWER FWD END CAP DENTED WHERE HANDRAIL IMPACTS FROM CLOSED POSITION, C-CHECK, DENT IN PAX DOOR FWD. DENT IS SMOOTH WITH NO NICK, CREASE OR GOUGE, NO OTHER DAMAGE NOTED. DENT IS ALLOWABLE IAW REO.
Part: TRUNNION — GOUGED (LT MLG) · airframe 29,464 hrs · 24,538 cycles
LEFT FWD MLG TRUNNION BUSHING AFT EXTERNAL SURFACE HAS A SMALL GOUGE AT THE 0600 POSITION. COMPLIED WITH IAW REO. COMPLIED WITH PERMANENT REPAIR OF THE LT FWD. MLG TRUNNION BUSHING AFT EXTERNAL SURFACE IAW REO.
Part: HANDLE — GOUGED (CARGO DOOR) · airframe 29,464 hrs · 24,538 cycles
CARGO DOOR HANDLE HAS CHAFE AND GOUGES, REPAIRED CARGO DOOR HANDLE BY BLENDING CHAFE/GOUGE DAMAGE. IAW SRM AND REO HANDLE WAS ORIGINALLY OUT OF LIMITS.
Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 28,817 hrs · 24,022 cycles
CEILING EMERGENCY FLOODLIGHT NR 3 IS INOPERATIVE. REPLACED THE LAMP IAW AMM.
Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 28,777 hrs · 23,984 cycles
RT NR 3 EXTERIOR EMERGENCY LIGHT INOPERATIVE. R & R LAMP IAW AMM.
Part: ACM — FAILED (LEFT) · airframe 28,762 hrs · 23,970 cycles
DURING TAXI IN, LOUD WHINING NOISE FROM UNDERNEATH FLIGHT DECK. NOISE WENT AWAY AND SHORTLY AFTER SMOKE STARTED COMING OUT FROM FO'S SIDE VENT. F/A REPORTED SMOKE MID CABIN. TURNED BOTH PACKS OFF. SMOKE DISSIPATED. R & R LT ACM IAW AMM.
Part: LAMP — BURNED OUT (EMERGENCY LIGHTS) · airframe 28,280 hrs · 23,510 cycles
NR 2 AISLE CEILING EMERGENCY LIGHT BURNED OUT, REPLACED LAMP.
2013
Part: STRUT — MALFUNCTIONED (NLG) · airframe 26,959 hrs · 22,459 cycles
RECEIVED NOSE DOOR OPEN WARNING MESSAGE & GEAR DISAGREE WARNING MESSAGE. RETURNED TO MKE. FLT#7333 FOUND NLG STRUT NOT FULLY EXTENDED CAUSING WOW & CENTERED PROXY SENSORS TO NOT READ. LOWERED NLG & PERFORMED FULL STRUT SERVICE. PERFORMED SEVERAL RETRACTION EXTENSIONS OF LANDING GEAR INCLUDING AN EMERGENCY EXTENSION IAW AMM.
Part: LIGHT — BROKEN (CABIN) · airframe 26,603 hrs · 22,181 cycles
EMERGENCY LIGHT AT FLOOR LEVEL NEAR MAIN CABIN DOOR BROKEN. FLT#5328 RELAMPED.
Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 26,416 hrs · 22,033 cycles
FLT 5228, NR 3 EMERGENCY OVERHEAD LIGHT IS BURNED OUT. REPLACED LAMP.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,881 hrs · 21,624 cycles
NR 2 EMERGENCY OVERHEAD LIGHT IS BURNED OUT. (FLT 5596) RELAMPED EMERGENCY LIGHT.
Part: SKIN PANEL — CORRODED (LT WING) · airframe 25,238 hrs · 21,057 cycles
LEFT WING FUEL ACCESS 540BB WING PLANK ACCESS HOLE HAS FRETTING CORROSION. (C-CHECK) REPAIRED FUEL ACCESS HOLE 540BB IAW REO.
Part: SKIN PANEL — CORRODED (RT WING) · airframe 25,238 hrs · 21,057 cycles
RIGHT WING FUEL ACCESS 650 DB WING PLANK ACCESS HOLE HAS FRETTING CORROSION. (C-CHECK) REPAIRED FUEL ACCESS HOLE 650DB IAW REO.
Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 25,238 hrs · 21,057 cycles
TRU BAY FLOOR HAS CRACK AT LEFT AFT AREA. (C-CHECK) REPAIRED CRACK IN TRU BAY FLOOR AT LEFT AFT AREA IAW REO.
Part: BEAM — CRACKED (FUSELAGE) · airframe 25,238 hrs · 21,057 cycles
FS 280 BEAM IS CRACKED AT RBL 11. (C-CHECK) REPAIRED FS 280 BEAM AT RBL 11 IAW REO.
Part: BEAM — CRACKED (FUSELAGE) · airframe 25,238 hrs · 21,057 cycles
FS 280 BEAM IS CRACKED AT LBL 8. (C-CHECK) REPAIRED CRACKED FS 280 BEAM IAW REO.
2012
Part: CONNECTOR — LOOSE (CABIN) · airframe 24,149 hrs · 20,115 cycles
FORWARD SECTION OF GREEN EMERGENCY FLOOR LIGHTING IS OUT. (FLT 7795) SECURED A LOOSE CONNECTION ON THE FLOOR LIGHT.
Part: ATTACH FITTING — FAILED (CABIN) · airframe 24,149 hrs · 20,115 cycles
EMERGENCY FLOOR LIGHTING AT ROWS 2-5 ARE OUT. (FLT 7335) REPLACED CABLE ATTACHMENT AT ROW 5. P/N: 5946-5, S/N OFF: NSN
Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,668 hrs · 19,675 cycles
NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5427) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,571 hrs · 19,602 cycles
NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5519) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — ODOR (LAVATORY) · airframe 23,445 hrs · 19,497 cycles
FLT 5320, HOT PLASTIC ODOR IN LAVATORY. FOUND LAVATORY LIGHT ASSEMBLY TO HAVE BURNING ODOR. REPLACED LAVATORY LIGHT ASSEMBLY IAW AMM.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,407 hrs · 19,469 cycles
NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6259) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,227 hrs · 19,325 cycles
LAST OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6374) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,971 hrs · 19,123 cycles
NR 1 AND 4 EMERGENCY EXIT LIGHTS IN THE CENTER AISLE CEILING ARE INOPERATIVE. (FLT 6205) RELAMPED EMERGENCY LIGHTS.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,844 hrs · 19,017 cycles
NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6231) RELAMPED EMERGENCY LIGHT.
2011
Part: SOCKET — UNSECURE (CABIN) · airframe 22,532 hrs · 18,730 cycles
NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4574) RE-SECURED SOCKET AND BULB IN THIRD OVERHEAD EMERGENCY FLOOD LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,532 hrs · 18,730 cycles
NR 3 OVERHEAD EMERGENCY LIGHTS ARE OUT. (SERVICE) RELAMPED EMERGENCY LIGHTS.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,312 hrs · 18,545 cycles
NR 1 AND NR 4 OVERHEAD EMERGENCY LIGHTS ARE OUT. (FLT 6436) RELAMPED EMERGENCY LIGHTS.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,249 hrs · 18,499 cycles
RIGHT WING FORWARD AND AFT EXTERIOR EMERGENCY EXIT LIGHTS INOPERATIVE. (FLT 4749) RELAMPED EMERGENCY LIGHTS.
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 22,249 hrs · 18,499 cycles
LEFT WING EXTERIOR CENTER EMERGENCY EXIT LIGHT INOPERATIVE. (FLT 4749) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,249 hrs · 18,499 cycles
1ST AND LAST OVERHEAD EMERGENCY LIGHTS INOPERATIVE. (FLT 4782) RELAMPED EMERGENCY LIGHTS.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,952 hrs · 18,232 cycles
NR 4 CEILING EMERGENCY LIGHT IS OUT. (FLT 6230) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,439 hrs · 17,819 cycles
FIRST OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6851) RELAMPED EMERGENCY LIGHT.
Part: YOKE — CORRODED (ENGINE MOUNT) · airframe 21,361 hrs · 17,758 cycles
RIGHT ENGINE YOKE MOUNT LINK ASSEMBLY IS CORRODED. (ENGINE CHANGE) REPLACED THE RIGHT ENGINE UPPER YOKE LINK ASSEMBLY.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,342 hrs · 17,743 cycles
NR 1 CEILING EMERGENCY LIGHT IS OUT. (SERVICE) RELAMPED EMERGENCY LIGHT.
Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 21,318 hrs · 17,725 cycles
FS 621 PRESSURE BULKHEAD WEB CRACKED AT CARGO DOOR TRACK. (C-CHECK) REPAIRED PER REO.
Part: BEAM — CRACKED (FUSELAGE) · airframe 21,546 hrs · 17,914 cycles
LEFT SIDE FS 280 BEAM CRACKED. (C-CHECK) REPAIRED PER REO.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,116 hrs · 17,565 cycles
CEILING EMERGENCY LIGHT AT LAST ROW BURNED OUT. (FLT 6292) RELAMPED EMERGENCY LIGHT.
2010
Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 20,279 hrs · 16,866 cycles
AFT CENTER CABIN CEILING EMERGENCY EXIT SIGN INOPERATIVE. (SERVICE) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,537 hrs · 15,433 cycles
NR 3 EMERGENCY FLOOD LIGHT INOP. (FLT 4711) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,976 hrs · 14,974 cycles
MOST AFT OVERHEAD EMERGENCY LIGHT INOP. (FLT 5989) RELAMPED EMERGENCY LIGHT.
2009
Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,590 hrs · 14,658 cycles
FORWARD OVERHEAD EMERGENCY LIGHT INOP. (FLT 6064)RELAMPED.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,258 hrs · 14,372 cycles
NR 2 CEILING EMERGENCY LIGHT INOP. (FLT 6509) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,117 hrs · 14,261 cycles
FIRST CEILING LEVEL EMERGENCY FLOOD LIGHT INOP. (FLT 6840) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 16,856 hrs · 14,058 cycles
RIGHT WING CENTER EMERGENCY EXIT LIGHT INOP. (FLT 6497) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 16,856 hrs · 14,058 cycles
NR 3 OVERHEAD EMERGENCY LIGHT INOP. (FLT 5842) RELAMPED EMERGENCY LIGHT.
Part: SUPPORT BEAM — CRACKED (FUSELAGE) · airframe 16,772 hrs · 13,995 cycles
ENGINE SUPPORT BEAM UPPER STIFFENER CRACKED. (C CHECK) REPLACED PER SRM.
Part: ANGLE — CRACKED (FUSELAGE) · airframe 17,129 hrs · 14,269 cycles
FS 484 ANGLES AND CLIPS CRACKED. (C CHECK) REPAIRED PER REO.
Part: FITTING — CRACKED (FUSELAGE) · airframe 17,129 hrs · 14,269 cycles
FS 625 CLIPS CRACKED. (C CHECK) REPLACED PER SRM.
Part: ANGLE — CRACKED (CARGO DOOR) · airframe 17,129 hrs · 14,269 cycles
CARGO DOOR SUPPORT BEAM ANGLE CRACKED. (C CHECK) REPLACED PER SRM.
Part: ISOLATOR — CRACKED (FUSELAGE) · airframe 17,129 hrs · 14,269 cycles
FS 621 ISOLATORS CRACKED. (C CHECK) REPLACED PER SRM.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 16,682 hrs · 13,929 cycles
EMERGENCY LIGHT BURNED OUT. (FLT 6683) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 16,645 hrs · 13,899 cycles
OVERHEAD EMERGENCY LIGHT NR 3 INOP. (FLT 5951) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 16,481 hrs · 13,769 cycles
MOST AFT OVERHEAD EMERGENCY LIGHT INOP. (FLT 6504) RELAMPED EMERGENCY LIGHT.
Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 16,247 hrs · 13,581 cycles
FLT 4559 - ONE CEILING LEVEL EMERGENCY FLOODLIGHT INOP. RELAMPED.
Part: LAMP — BURNED OUT (EMERGENCY LIGHTS) · airframe 16,000 hrs · 13,378 cycles
FLT 6682 - CABIN OVERHEAD EMERGENCY LIGHT INOP. RELAMPED.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 15,814 hrs · 13,243 cycles
FLT 6221 - OVERHEAD EMERGENCY LIGHTS WILL NOT STAY ON. CHARGED SYSTEM FOR 20 MINUTES.
Part: LAMP — BURNED OUT (EMERGENCY LIGHTS) · airframe 15,501 hrs · 12,990 cycles
FLT 5859 - LEFT WING MIDDLE EMERGENCY EXIT LIGHT INOP. RELAMPED.
Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 15,501 hrs · 12,990 cycles
FLT 5859 - RIGHT WING FORWARD EMERGENCY EXIT LIGHT INOP. RELAMPED.
2008
Part: WINDOW — CRACKED (COCKPIT) · airframe 15,198 hrs · 12,758 cycles
FLT 6617 - CAPTIAN SIDE WINDOW CRACKED.
Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 15,037 hrs · 12,626 cycles
FLT 6474 - NR 3 EMERGENCY CEILING FLOODLIGHT INOP. RELAMPED.
Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 14,258 hrs · 11,965 cycles
AFT STRIP OF FLOOR EMERGENCY LIGHTS ARE INOP. FLIGHT 5846. REPLACED NR 4 EMERGENCY LIGHT POWER INVERTER AS REQUIRED. OPS CHECKS GOOD.
Part: LIGHT — BROKEN (CABIN) · airframe 12,876 hrs · 10,783 cycles
PAX DOOR FLOOR EMERGENCY FLOOD LIGHT ASSEMBLY IS BROKEN. REPLACED PAX DOOR FLOOR EMERGENCY LIGHT ASSEMBLY IAW AMM 33-51-00.
2007
Part: STRUCTURE — CRACKED (CARGO BAY) · airframe 13,111 hrs · 10,973 cycles
FOUND AT C-CHECK, CARGO BAY FLOOR IS CRACKED AT STA 574 AND LBL42. COMPLIED WITH REPAIRS IAW PER CRJ200 REO601R-53-61-1741.
Part: ACTUATOR — CRACKED (HORIZ STAB) · airframe 13,111 hrs · 10,973 cycles
FOUND AT C-CHECK, HORIZONTAL STABILIZER ACTUATOR CHASSIS IS CRACKED ON RIGHT SIDE. REPLACED HORIZONTAL STABILIZER TRIM ACTUATOR IAW CRJ200 AMM TASK 27-42-01-400-801 AND 27-42-01-000-801.
Part: BUSHING — CORRODED (ENGINE MOUNT) · airframe 13,111 hrs · 10,973 cycles
FOUND AT C-CHECK, LEFT ENGINE MOUNT HAT BUSHINGS AND FLOATING BUSHINGS SHOW SIGNS OF CORROSION. REPLACED ENGINE MOUNT HAT BUSHINGS AND FLOATING BUSHINGS PER CRJ200 AMM 71-21-01-400-801.
Part: LINK — CORRODED (ENGINE MOUNT) · airframe 13,111 hrs · 10,973 cycles
FOUND AT C-CHECK, LEFT ENGINE MOUNT FORWARD LINK IS CORRODED. REPLACED LEFT ENGINE FORWARD MOUNT LINK AND BUSHING PER CRJ200 AMM 71-21-01-400-801, P/N 601-37016-5, S/N RJ/SWA/0064.
Part: BEAM — CRACKED (FUSELAGE) · airframe 13,111 hrs · 10,973 cycles
STA 280 BEAM IS CRACKED JUST OUTBOARD OF COCKPIT DOOR OPENING ON RIGHT SIDE, FOUND AT C-CHECK. INSTALLED REPAIR PARTS AT STN 280 AND RBL9.0 PER RJ200 REO 601R-53-11-171 REV D REPAIR SCHEME B.
Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 11,349 hrs · 9,495 cycles
FLT 6688 - LEFT SIDE EXTERIOR EMERGENCY EXIT LIGHT IS INOP. RELAMPED LEFT AFT EMERGENCY LIGHT BULB IAW MM 33-51-00. OP CHECK GOOD.
2006
Part: HANDLE — CRACKED (PAX DOOR) · airframe 8,689 hrs · 7,355 cycles
PASSENGER DOOR OUTER HANDLE CRACKED, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED NEW PASSENGER DOOR OUTER HANDLE PN 601R 31763-1 PER CRJ200 AMM 52-11-03-400-802. OPERATIONAL CHECKS GOOD.
Part: FITTING — CRACKED (FUSELAGE) · airframe 8,689 hrs · 7,355 cycles
FS 280 CLIPS AT RBL 9 INBOARD AND OUTBOARD ARE CRACKED, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED 2 NEW CLIPS P/N 601R31113-58 ON THE RBL 9 AT FS 280 AS PER CRJ200 SRM REF 51-42-06 PG 11; 51-42-21 PG 17.
Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 8,689 hrs · 7,355 cycles
FS 621 FLOOR SUPPORT FRAME ON LEFT SIDE CRACKED, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED REPAIR PARTS TO FS 321 ON LEFT SIDE PER REO 601R 53-61-117.
Part: FITTING — CRACKED (FUSELAGE) · airframe 8,689 hrs · 7,355 cycles
FS 625 CLIP CRACKED ON RIGHT SIDE OUTBOARD NEAR STRINGER 15, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED NEW CLIP -52 AT RT FS 625 PER CRJ200 SRM 51-42-21.
Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 8,689 hrs · 7,355 cycles
PASSENGER DOOR DRAG ANGLE CRACKED, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED ANGLE SECTION PER REO 601R-52-11-513 REV 'A'.
Part: FITTING — CRACKED (FUSELAGE) · airframe 8,689 hrs · 7,355 cycles
FS 484 CLIP AT RBL 27 CRACKED, DISCOVERED DURING C-CHECK INSPECTION. REPLACED CRACKED CLIP AT FS 484 AND RBL 27.00 WITH NEW CLIP P/N 601R31171-9 PO 60148 IAW REO 601R-53-41-059 REV 'A'.
Part: FITTING — CRACKED (FUSELAGE) · airframe 8,689 hrs · 7,355 cycles
FS 280 CLIPS AT LBL9 INBOARD AND OUTBOARD ARE CRACKED, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED 2 NEW ANGLE BRACKETS AT FS 280 LBL9 AT FLOOR LEVEL AS PER CRJ200 SRM 51-42-21 PG 1-21 AND 51-42-06 PG 1-20.
Part: TRIM SWITCH — INOPERATIVE (COCKPIT) · airframe 7,354 hrs · 6,192 cycles
DURING FLIGHT, CAPT SIDE STAB TRIM SWITCH STOPPED WORKING IN NOSE DOWN DIRECTION. REPLACED CAPT SIDE STAB TRIM SWITCH IAW 27-41-05.
Part: CONTROL UNIT — MALFUNCTIONED (SPOILER) · airframe 7,033 hrs · 5,919 cycles
SPOILERON FAULT MSG INFLIGHT. REPLACED NR 1 SECU IAW CRJ 200 MM 27-61-05 AND REPLACED RT OB FLIGHT SPOILER IAW CRJ 200 MM 27-62-00. OPERATIONAL CHECK GOOD, PN 49-164-06 OFF 01840, PN 27000-7 SN MAL 6742.
2005
Part: DAMPER — MALFUNCTIONED (ELEVATOR) · airframe 6,454 hrs · 5,426 cycles
RECEIVED A -FLUTTER DAMPER STATUS MSG- INFLIGHT. REPLACED RT ELEVATOR INBOARD FLUTTER DAMPER IAW CRJ MM 27-34-05. OPERATIONAL CHECK GOOD.
Part: PCU — MALFUNCTIONED (SPOILERS) · airframe 5,827 hrs · 4,888 cycles
ON TAXI OUT, SPOILERON FAULT STATUS MSG. REPLACED RT INBOARD SPOILERON PCU IAW CRJ MM 27-61-01. OPERATIONAL CHECK GOOD.
Part: ACTUATOR — MALFUNCTIONED (HORIZONTAL STAB) · airframe 5,531 hrs · 4,644 cycles
ON START AT THE GATE,STAB CH 1 INOP STATUS MSG ILLUMINATED. REPLACED HORIZONTAL STAB TRIM ACTUATOR IAW CRJ 200 M/M 27-42-01 AND REPLACED MOTOR CONTROL UNIT IAW CRJ 200 M/M 27-42-05. OPERATIONAL CHECK GOOD, PN 7062-3; SN OFF 2001.
Part: CONTROL UNIT — INOPERATIVE (HORIZ STAB TRIM) · airframe 5,454 hrs · 4,589 cycles
STAB CH1 INOP STATUS MESSAGE INFLIGHT. REPLACED HSTCU WITH A SERVICEABLE UNIT. OPERATIONAL CHECK GOOD.
Part: CONTROL UNIT — MALFUNCTIONED (SPOILER) · airframe 5,197 hrs · 4,386 cycles
ON TAXI OUT RECEIVED INBOARD GROUND SPOILER, FLIGHT SPOILER, AND SPOILERON CAUTION MESSAGES. REPLACED NR 2 SECU IAW MM 27-61-05.
Part: CONTROL UNIT — MALFUNCTIONED (STALL PROTECTION) · airframe 5,016 hrs · 4,256 cycles
STALL FAIL CAUTION MESSAGE ILLUMINATED OUT OF 1000 FT ON DEPARTURE AND REMAINED ON UNTIL LANDING. REMOVED AND REPLACED SPS CONTROL UNIT PER CRJ MM 27-35-01, OPERATIONAL CHECK GOOD. P/N 3995100208, S/N OFF 1047.
Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 4,905 hrs · 4,170 cycles
FIVE MINUTES AFTER TAKEOFF, EMERGENCY LIGHTS TURNED ON AND REMAINED ON FOR ABOUT 35 MINUTES. RESET CB4-C2 BREAKER. CHECKED CHARGER OUTPUT AT ALL FOUR PACKS AND FOUND OK. ALL ELBP'S DEAD. REMOVED AND REPLACED ALL ELBP'S. OPERATIONAL CHECKED GOOD IAW CRJ MM 33-51-04.
Part: ACTUATOR — MALFUNCTIONED (HORIZONTAL STAB) · airframe 4,744 hrs · 4,024 cycles
STAB TRIM CH 2 WILL NOT ENGAGE. REMOVED HSTA AND MCU IAW MM 27-40-00, 27-42-01, 27-42-05. OPERATIONAL CHECK GOOD. P/N 7062-3, S/N OFF 1092.
Part: CONTROL PANEL — MALFUNCTIONED (HORIZ STAB TRIM) · airframe 4,659 hrs · 3,944 cycles
STAB TRIM CHANNEL 2 INOPERATIVE. INSTALLED SERVICEABLE HSTCU IAW CRJ 200 MM 27-41-01, OPERATIONAL CHECK GOOD.
2004
Part: TRIM SWITCH — INOPERATIVE (FO'S YOKE) · airframe 3,692 hrs · 3,132 cycles
FO STAB TRIM INOPERATIVE IN NOSE UP DIRECTION. REPLACED FO'S YOKE TRIM SWITCH WITH SERVICEABLE UNIT IAW CRJ MM 27-41-01, OPERATIONAL CHECK GOOD.
Part: RUDDER PEDAL — OUT OF ADJUST (COCKPIT) · airframe 2,802 hrs · 2,341 cycles
WHEN MOVING RUDDER PEDALS FOR TAXI CHECK, CLICKING NOISE HEARD AND FELT ON CAPTAIN'S SIDE ONLY. REMOVED AND REPLACED RUDDER PEDAL ADJUSTMENT ROD AND SCREW ACTUATOR IAW MM 27-21-01. OPS CHECKS GOOD.
2003
Part: SPOILER — MALFUNCTIONED · airframe 1,732 hrs · 1,477 cycles
WHEN DEPLOYING FLIGHT SPOILERS SHARP LT ROLLING MOMENT AND THEN LEVELED OUT. WHEN RETRACTING SPOILERS, ALSO A MOMENTARY SHARP ROLLING MOMENT. NO FAULTS FOUND. CYCLED SPOILERS MANY TIMES IAW MM 27-61-00. COULD NOT DUPLICATE DISCREPANCY.
Part: COMPUTER — MALFUNCTIONED (FLT CONTROL) · airframe 1,732 hrs · 1,477 cycles
A/P DISCONNECTED IN FLIGHT WHEN FLIGHT DIRECTOR FAILED ON F/O'S SIDE. A/P WOULD NOT RE-ENGAGE ON CAPTAIN'S SIDE. AFTER 15 MINUTES F/O'S FLIGHT DIRECTOR CAME BACK AND RE-ENGAGED A/P. REMOVED AND REPLACED FCC NR 2. OPS CHECKS GOOD IAW CRJ MM 22-12-14.