N953SW
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 | 2010-04-29 – 2010-04-29 | Operator named in NTSB report |
| SKYWEST AIRLINES INC | Operator | 2010-04-29 – 2010-04-29 | Operator named in NTSB report |
Accident & incident history
Maintenance disclosures
TAKING OFF WELL ABOVE MINTO. AFTER REACHING TOC A 200LB LESS, GOT TO SECOND FIX AT PLANNED FUEL WEIGHT. DURING CRUISE AND ARRIVAL LANDING FUEL WEIGHT CONTINUED DEACREASING IN A RAPID TREND AND AFTER GETTING TO MINIMUM FUEL, HAD TO DIVERT TO ALTERNATE. FUEL BURN AND THRUST SETTINGS SEEMS NORMAL AT 1200 LB/HR PER ENGINE. (FLIGHT 5912 - FILED CLOSED) OCM PERFORMED A VISUAL CHECK OF THE FUEL TANK EXTERIOR IAW AMM 29-11-00-210-801, AMM 28-11-00-210-803 AND FOUND NO FUEL LEAKS IAW AMM 28-11-00-790-802. ALSO COMPLETED A FUEL MLI CHECK OF BOTH WINGS IAW AMM 12-11-28-750-804 AND FOUND TO BE WITHIN 2% OF EICAS READINGS NO DISCREPANCIES NOTED ON MLI CHECK. OK FOR RETURN TO SERVICE.
PROX SYS CHAN CAUTION. RAN QRH. LANDING GEAR CAME DOWN. (FLIGHT 5335 - FILED CLOSED) AFTER MAINTENANCE (REF: AML 1549668), MESSAGE CLEARED. PERFORMED AN OPS CHECK OF THE PSEU IN REF TO AMM 32-61-00. OPS CHECK GOOD. PERFORMED MLG EXTENSION AND RETRACTION IN REF TO AMM 32-30-00. OPS CHECK GOOD. NO FURTHER DEFECTS NOTED AT THIS TIME.
PROX SYS CHAN CAUTION. RAN QRH. LANDING GEAR CAME DOWN. (FLIGHT 5335 - FILED OPEN) THIS IS CURRENTLY A WORK IN PROGRESS
L SIDE WINDOW BORKEN DURING CLIMB AT FL240. DIVERTED TO KLAS. (FLIGHT 5117 - FILED CLOSED) THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 29276079 WITH THE FOLLOWING CORRECTIVE ACTION: "COMPLIED WITH TASK CARD 56-220-1000-SKY REMOVED AND REPLACED LH WINDOW. LEAK CHECK AND OPS CHECK GOOD AT THIS TIME. TORQUE WRENCH INFO:SN 0224112161EXP: 02/28/2025SN: 0914804475EXP: 12/31/2024"
GEAR DISAGREE WARNING AFTER SELECTING LANDING GEAR LEVER DOWN IN FLIGHT. RAN QRH TO PULL LANDING GEAR MANUAL RELEASE HANDLE. AFTER PULLING THE GEAR MANUAL RELEASE HANDLE GOT ALL 3 GEAR DN WITH NO MESSAGE. (FLIGHT 5624 FILED CLOSED)THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 27928709 WITH THE FOLLOWING CORRECTIVE ACTION: "REFERENCE CP 27928800, CP 27932259, CP 27932518 AND CP 27932521 FOR CORRECTIVE ACTIONS."
GEAR DISAGREE WARNING AFTER SELECTING LANDING GEAR LEVER DOWN IN FLIGHT. RAN QRH TO PULL LANDING GEAR MANUAL RELEASE HANDLE. AFTER PULLING THE GEAR MANUAL RELEASE HANDLE GOT ALL 3 GEAR DN WITH NO MESSAGE. (FLIGHT 5624 FILED OPEN)THIS IS CURRENTLY A WORK IN PROGRESS.
ANTI-ICE DUCT WARNING MESSAGE APPEARED WHILE IN CRUISE. QRH RESOLVED THE ISSUE. (FLIGHT 4797 FILED OPEN)PERFORMED OPERATIONAL TEST OF THE ENGINE-COWL ANTI-ICE SYSTEM PER CRJ-200 AMM TASK 30-22-00-710-802, OPS CHECK GOOD.
ANTI-ICE DUCT WARNING MESSAGE APPEARED WHILE IN CRUISE. QRH RESOLVED THE ISSUE. (FLIGHT 4797 FILED CLOSED)PERFORMED OPERATIONAL TEST OF THE ENGINE-COWL ANTI-ICE SYSTEM PER CRJ-200 AMM TASK 30-22-00-710-802, OPS CHECK GOOD.
LH LWR WING PLANK FWD OF THE MLG CUTOUT, W.S. 45.0 TO W.S. 47.61, HAS CHAFFING. (C-CHECK RO 10/29/2023) BLENDED OUT CHAFE ON LH LOWER WING PLANK FWD OF THE MLG CUTOUT, W.S 45.0 T0 47.61. REF CRJ 200 SRM 51-12-00RECEIVED ENGINEERING SUPPORT , FOR CHAFFING BETWEEN WING LOWER SKIN PLANK & MLG FAIRING LBL45 - RBL45. MEASUREMENTS ARE NOMINAL SKIN THICKNESS= 0.300" REF CRJ-200 SRM 57-21-31 MINIMUM READING PER NDT=0.277" MAX BLEND DEPTH WITHIN ZONE A IN BE 2.LEND AREA IS 0.040" . WITHIN LIMITS REF REO 601R-57-21-880 REV-D DATED 2017/03/06, NOTE 2. COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY
POSSIBLE CRACK AT F.S. 319 FRAME, FWD SIDE AT STGR 2R. (C-CHECK RO 10/29/2023) COMPLIED WITH PERMANENT REPAIR ON FRAME SECTOR FS319. BETWEEN STRG-1R -STGR -2R, ENSURED ALL REQUIREMENTS ARE MET IN REF REO 601R-53-21-3650 REV-- DATED 2023-09-06. COMPLIED WITH TASK CARD 51-900-1003-SKY REMOVE AND REPLACE FS605 FRAME SECTOR AT STGE 17L-19L. (C-CHECK RO 10/29/2023) REMOVED AND INSTALLED NEW FRAME SECTOR AT FS605 BETWEEN STRG17L AND 19L REF CRJ 200 SRM 51-42-06 AND DWG 601R36026 REV AE. COMPLIED WITH 51-900-1003-SKY AND PRESSURE CHECKS GOOD . SEE CONTINUATION CARD FOR DETAILS
LBL 27 - APROX FS 621 - FLOOR BEAM ATTACHMENT TO REAR PRESSURE BULKHEAD HAS ERRANT HOLE ON INBD SIDE (27069818) (C-CHECK RO 10/29/2023) PLUGGED REDUNDANT HOLE PER REO 601R-53-61-8066 REV--, DATED 2023-08-17. COMPLIED WITH SKYCARD 51-900-1003-SKY. NO WEIGHT CHANGE
DURING AUDIT OF 40K TASK CARD 55-340-602(DETAILED INSPECTION OF THE RIGHT ELEVATOR FRONT SPAR ASSEMBLY) FOUND THAT THE RH ELEVATOR HAS DAMAGE ON INBOARD SIDE OF FRONT SPAR. (C-CHECK RO 10/29/2023) REPAIRED ELEVATOR IB LE DAMAGE TO THE FRONT SPAR PER MHIRJ BLEND REPAIR REO 601R-55-21-584 REV -- DATED 2023-09-04, SEE CONTINUE CARD FOR DETAILS.COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY (CL600-2B19) STRUCTURAL MAJOR REPAIRCOMPLIED WITH SKYWEST FORM M-337
DURING AUDIT OF 1C TASK CARD 53-310-301(EXTERNAL ZONAL INSPECTION OF THE AFT FUSELAGE, FS621.00 TOFS755.00) FOUND AFT EQ BAY DOOR HAS DENTED CENTER INTERCOSTAL. (C-CHECK RO 10/29/2023) REMOVED DAMAGED INTERCOSTAL FROM AFT EQUIPMENT COMPARTMENT DOOR PER REF CRJ 200 SRM 51-42-06. INSTALLED THE NEW INTERCOSTAL ON AFT EQUIPMENT BAY DOOR PER MHI DWG# 600-35128, REV -H AND REF CRJ 200 SRM 51-42-06
ANGLE ON FRAME AT FS589 BETWEEN STR 23R - 23L IS CORRODED. (C-CHECK RO 10/29/2023) REPLACED ANGLE AT FRAME FS589 REF CRJ200 SRM 51-42-06 AND DWG#601R36025 REV-P. COMPLIED WITH SKY CARD 51-900-1003-SKY
RIVET COUNTER SINKS ARE DAMAGED AT LWR NUTPLATE HOLE UNDER 141AL (MARKED). (C-CHECK RO 10/29/2023) REPAIRED RIVET COUNTER SINKS UNDER ACCESS PANELS 141AL REF REO 601R-53-21-3648 REV-- DATED 2023-09-12 . COMPLIED WITH 51-900-1003-SKY AND PRESSURE CHECKS GOOD .SEE CONTINUATION CARD FOR DETAILS
L/H ON WING PLANK FUEL ASSESS PANEL LOCATION 540BB HAS EVIDENCE OF FRETTING. (C-CHECK RO 10/29/2023) PERFORMED REPAIR ON LH WING PLANK ON FUEL PANEL 540BB. PER ALL STEPS OF REO 601R-57-21-030 REV -L DATED 2014-02-05. NO LEAKS NOTED. COMPLIED WITH ALL STEPS OF REO 601R-57-21-3787 REV -- DATED: 2023-08-30. SEE CONTINUATION FOR DETAILS. COMPLIED WITH TASK CARD 51-900-1003-SKY
COCKPIT FLOOR SUPPORT ANGLE IS CRACKED (C-CHECK RO 10/29/2023) REMOVED AND INSTALLED NEW COCKPIT FLOOR SUPPORT ANGLE. REF: REO 601R-53-11-926 REV -B DATE 2006/5/10.COMPLIED WITH 51-900-1003-SKY
PASSENGER DOOR PIANO HINGE HALF ON FUSELAGE SIDE FAILED THE GO NO-GO CHECK OF THE DIAMETER OF THE HOLES. (C-CHECK RO 10/29/2023) REMOVED AND INSTALLED NEW PAX DOOR PIANO HINGE FUSELAGE SIDE IAW CRJ 200 SRM 53-21-23 AND DWG 601R31527 REV. AM, REO 601R-53-21-656 REV -A DATED 2017-03-06 AND REO 601R-53-21-814 REV. B DATED 2017-06-05. COMPLIED WITH 51-900-1003-SKY AND PRESSURE CHECK GOOD . SEE CONTINUATION CARD FOR DETAILS.
RBL9 FLOORBEAM STRUCTURE AT FS280 OUTBOARD ANGLE CLIP CRACKED (C-CHECK RO 10/29/2023) REMOVED AND REPLACED FS280 FLOOR SUPPORT CLIP AT RBL9 OUTBOARD.. REF: REO 601R-53-11-926 REV -B DATE 2006/5/10COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY (CL600-2B19) STRUCTURAL MAJOR REPAIRCOMPLIED WITH SKYWEST FORM M-337
RBL9 FLOORBEAM STRUCTURE AT FS280 INBOARD ANGLE CLIP CRACKED (C-CHECK RO 10/29/2023) INSTALLED NEW FS280 FLOOR SUPPORT CLIP AT RBL9 INBOARD.. REF: PREVIOUSLY INCORPERATED REO 601R-53-11-926 REV -B DATE 2006/5/10.COMPLIED WITH 51-900-1003-SKY
BRACKET CRACKED BELOW LH WINDSHIELD SIDE POST (BELOW THE SILL MARKED) (C-CHECK RO 10/29/2023) REMOVED AND INSTALLED NEW BRACKET AT BELOW LH WINDSHIELD SIDE POST (BELOW THE SILL MARKED) REF CRJ200 SRM 51-42-06, CRJ200 SRM 51-42-21 AND DWG #601R34032 REV (V). COMPLIED WITH 51-900-1003-SKY AND PRESSURE CHECK GOOD . SEE CONTINUATION CARD FOR DETAILS
PAX DOOR HINGE, DOOR SIDE, ROLL PIN HOLE IS ELONGATED (C-CHECK RO 10/29/2023) REMOVED AND INSTALLED NEW PAX DOOR HINGE REF CRJ 200 SRM 52-10-31,DWG 601R31702 REV. N AND REO 601R-52-11-2987 REV. -- DATED 2023-08-21 . COMPLIED WITH 51-900-1003-SKY AND PRESSURE CHECK GOOD. SEE CONTINUATION CARD FOR DETAILS
DURING REMOVAL OF FLOOR SUPPORT CLIP, DISCOVERED CRACK IN FS280 BULKHEAD LOWER WEB AT RBL9. (C-CHECK RO 10/29/2023) REMOVED AND REPLACED EXISTING REPAIR PARTS @ FS280.00 BULKHEAD LOWER WEB. REF: REO 601R-53-11-926 REV -B DATE 2006/05/10COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY (CL600-2B19) STRUCTURAL MAJOR REPAIRCOMPLIED WITH SKYWEST FORM M-337
FRAME AT FS574 STGR25R- STRG26L HAS CORROSION (C-CHECK RO 10/29/2023) REMOVED CORROSION FROM FS574 TGR25R- STRG26L FRAME OUTER FLANGE AND REPAIRED REF. REO 601R-53-61-8078 REV. -- DATED 2023-09-06 STEPS 1-5. ALL STEPS COMPLIED WITH. COMPLIED WITH TASK CARD 51-900-1003-SKY. NO LEAKS NOTED.
R/H FLOOR SILL BETWEEN FS310.00 TO FS319.70 HAS CORROSION (MARKED) (C-CHECK RO 10/29/2023) REMOVED CORROSION ON RH FLOOR SILL BETWEEN FS310.00 TO FS319.70. REF CRJ-200 SRM 51-21-06. ORIGINAL THICKNESS OF 0.063". REMAINING THICKNESS OF 0.028" MATERIAL LOSS OF 0.035". FOUND TO BE OUT OF LIMITS. REF REO 601R-53-00-530 REV -A DATED 2014-10-07 WHICH ALLOWS 0.015" MATERIAL LOSS. REMOVED DAMAGED RH FLOOR SILL AND INSTALLED NEW RH FLOOR SILL BETWEEN FS310.00 TO FS319.70. REF CRJ-200 SRM 51-42-06, CRJ-200 SRM 51-42-20 AND DWG 601R31148 REV AC. COMPLIED WITH 51-900-1003-SKY
L/H FLOOR BEAM AT FS559.00 BETWEEN LBL27 AND L/H FLOOR SILL HAS CORROSION (MARKED) (C-CHECK RO 10/29/2023) REMOVED AND REPLACED LH FLOOR STRAP/BEAM AT F.S. 559.00 BETWEEN LBL27 AND LH FLOOR SILL, REF CRJ 200 SRM 51-42-06, CRJ 200 SRM 51-45-00 AND DWG 601R31025 REV N. NO LEAKS NOTED. COMPLIED WITH 51-900-1003-SKY
FS280.00 SEAT RAIL STRUCTURE AT LBL9 OUTBOARD ANGLE CLIP CRACKED (MARKED) (C-CHECK RO 10/29/2023) FABRICATED, LOCATED, DRILLED AND INSTALLED THE FS280 FLOOR SUPPORT CLIP AT LBL9 OUTBOARD WITH 2024 T-42 .050" P.O. # T70541. REF: PREVIOUSLY INCORPERATED REO 601R-53-11-926 REV -B DATE 2006/5/10 NOTE 20. COMPLIED WITH 51-900-1003-SKY
FS280.00 SEAT RAIL STRUCTURE AT LBL9 INBOARD ANGLE CLIP CRACKED (MARKED) (C-CHECK RO 10/29/2023) REMOVED AND REPLACED FS280 FLOOR SUPPORT CLIP AT LBL9 INBOARD.. REF: REO 601R-53-11-926 REV -B DATE 2006/5/10COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY STUCTURAL MAJOR REPAIR COMPLIED WITH SKYWEST FORM M-337
R/H FLOOR BEAM AT FS559.00 BETWEEN RBL27 AND R/H FLOOR SILL HAS CORROSION (MARKED) (C-CHECK RO 10/29/2023) REMOVED AND INSTALLED NEW REPLACEMENT STRAP P/N 601R31025-29 AT FS.559.00 R/H PRESSURE FLOOR SUPPORT STRUCTURE BETWEEN RBL 27 & RBL 36 PER CRJ200 SRM 51-42-06 & SRM 51-45-00 REF. BOMBARDIER DWG. 601R31025 REV. N . NO LEAKS NOTED. COMPLIED WITH 51-900-1003-SKY
FRAME @ FS 589.00 STR 25L- 25R HAS CORROSION AROUND LWR EDGE OF FRAME (C-CHECK RO 10/29/2023) REMOVED AND INSTALLED NEW LOWER SECTION FRAME AT FS 589.00 BETWEEN STRG 20L-20R CRJ200 SRM 51-42-06 , CRJ200 SRM 51-42-21 , AND DWG#601R36025 REV-P. NO LEAKS NOTED. COMPLED WITH 51-900-1003-SKY
L/H SEAT RAIL BEAM AT LBL27 BETWEEN FS605.00 TO FS621.00 HAS CORROSION (MARKED) (C-CHECK RO 10/29/2023) PERFORMED REPAIR TO LH SEAT RAIL FLOOR BEAM LOCATED AT LBL27 FS605 - FS621. PER ALL STEPS OF REO 601R-53-61-8066 REV -- DATED 2023-08-17. BLEND REPAIR ONLY NO WEIGHT CHANGE.
L/H PRESSURE FLOOR SILL FROM FS 409+128 TO FS 559 HAS MULTIPLE SPOT OF CORROSION (C-CHECK RO 10/29/2023) REMOVED CORROSION ON LH PRESSURE FLOOR BETWEEN FS409+128 TO FS559 REF CRJ200 SRM 51-21-06. EVALUATED 23EA BLENDS ON LH PRESSURE FLOOR BETWEEN FS409+112 TO FS559 BLEND 1 0.8L X 1.1W X 0.005D BLEND 2 1.2L X 1.7D X 0.000D BLEND 3 1.4L X 0.8W X 0.000D BLEND 4 1.5L X 2.4W X 0.000D BLEND 5 2.1L X 1.6W X 0.003D BLEND 6 1.1L X 1.8W X 0.006D BLEND 7 1.7L X 2.2W X 0.002D BLEND 8 2.4L X 0.8W X 0.003D BLEND 9 1.0L X 1.6W X 0.006D BLEND 10 1.2L X 2.0W X 0.001D BLEND 11 1.6L X 2.1W X 0.003D BLEND 12 1.7L X 1.3W X 0.001D BLEND 13 1.5L X 1.0W X 0.006D BLEND 14 1.4L X 0.9W X 0.002D BLEND 15 2.3L X 1.8W X 0.001D BLEND 16 2.3L X 1.8W X 0.000D BLEND 17 0.8L X 1.3W X 0.004D BLEND 18 1.6L X 0.8W X 0.004D BLEND 19 1.2L X 1.9W X 0.002D BLEND 20 1.4L X 1.1W X 0.004D BLEND 21 1.6L X 1.4W X 0.003D BLEND 22 1.3L X 1.4W X 0.007D BLEND 23 1.6L X 1.6W X 0.008D MAXIMUM ALLOWABLE DEPTH 0.015 IN CM AND 0.025 IN NCM. LARGEST DEPTH IS 0.008. ALL BLENDS WITHIN LIMITS REF REO 601R-53-41-666 REV-C DATED 2012-11-06 TUC9234 CAL DUE 31OCT23 MACT3497
NLG - AFT DOOR CUTOUT - AFT L/H NLG DOOR CUTOUT RADIUS HAS SUSPECTED CRACK - APROX FS 235 (C-CHECK RO 10/29/2023) CUT AWAY DAMAGED / CRACKED AREA AND PERFORMED DOUBLER REPAIR AS PER REO 601R-53-11-048 REV. -D, DATED 06/10/15, SEE CONTINUE CARD FOR DETAILS. OPS AND LEAK CHECKS GOOD. COMPLIED WITH 51-900-1003-SKY & M-337
NLG - AFT DOOR CUTOUT - AFT R/H NLG DOOR CUTOUT RADIUS HAS SUSPECTED CRACK - APROX FS 235 (C-CHECK RO 10/29/2023) PERFORMED REO 601R-53-11-048 REV. -D ISSUED 06/10/15 REPAIR TO AFT RH NLG CUTOUT RADIUS. COMPLIED WITH 51-900-1003-SKY
R/H PRESSURE FLOOR SILL FROM FS 409+128 TO FS 559 HAS MULTIPLE SPOT OF CORROSION (C-CHECK RO 10/29/2023) REPAIRED CORROSION AT 16EA LOCATIONS ALONG RH PRESSURE FLOOR SILL FROM F.S. 409+128 TO 559.0 PER MHIRJ REO 601R-53-41-3185REV -- DATED 2023-08-28 AND BOMBARDIER REO 601R-53-41-666 REV -C DATED 2012-11-06 COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY (CL600-2B19) STRUCTURAL MAJOR REPAIR COMPLIED WITH SKYWEST FORM M-337
MULTIPLE AREAS OF CORROSION ON THE EXTERNAL LOWER SKIN WHERE FORWARD WING FAIRINGS ( 191BB AND 192BB ) ATTACH AT FASTENER HOLES. (C-CHECK RO 10/29/2023) REMOVED MULTIPLES AREAS OF CORROSION ON THE EXTERNAL LOWER SKIN WHERE FORWARD WING FAIRINGS ( 191BB AND 192BB ) ATTACH AT FASTENER HOLES. REF CRJ200 SRM 51-21-06. COMPLIED WITH REO 601R-53-31-1289 REV. -- DATED 2023-09-09. NO LEAKS NOTED. COMPLIED WITH 51-900-1003-SKY
LEFT WING BATT RIB WS48.30 ANGLE ON THE FORWARD END OF THE CAP IS CRACKED. (C-CHECK RO 10/29/2023) REMOVED AND REPLACED LH WING BATT RIB ANGLE AT W.S. 48.30 WITH NEW, REF CRJ 200 SRM 51-42-06, CRJ 200 SRM 51-42-21 AND DWG 600-10204 REV -L. COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY (CL600-2B19) STRUCTURAL MAJOR REPAIR COMPLIED WITH SKYWEST FOMR M-337
FWD RH BATT RIB WS53 IS CRACKED (MARKED) (C-CHECK RO 10/29/2023) INSTALLED NEW BAT RIB, FWD RH SIDE AT WS53.00. PER DWG 601R10203 REV-G AND CRJ 200 SRM 51-42-21. COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY
STGR3L CRACKED AT FS379.00. (C-CHECK RO 10/29/2023) REMOVED AND INSTALLED NEW ANGLE AT STGR3L AT FS 379.00 REF CRJ-200-SRM 53-00-03 AND CRJ-200-SRM 51-42-06. COMPLIED WITH 51-900-1003-SKY AND PRESSURE CHECKS GOOD . SEE CONTINUATION CARD FOR DETAILS
STGR3L ATTACHING STRUCTURE TO FS280.00 BULKHEAD IS CRACKED. (C-CHECK RO 10/29/2023) REMOVED AND INSTALLED NEW REPLACEMENT END ANGLE P/N 600-31057-19 ON STGR 3L AT FS.280 PER CRJ200 SRM 51-42-06 & SRM 51-42-21 REF. BOMBARDIER DWG. 600-31057 REV. P, NO LEAKS NOTED. COMPLIED WITH 51-900-1003-SKY
LEFT WING BATT RIB WS53.60 ANGLE ON THE FORWARD END INBOARD SIDE IS CORRODED. (C-CHECK RO 10/29/2023) WET INSTALLED NEW LH BATT RIB ASSY AT WS53.60 REF CRJ-200 SRM 51-42-21, CRJ-200 SRM 51-42-06 AND DRAWING NO: 601R10203 REV-G. COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY
CLUSTER OF CHAFES BETWEEN FS589-FS605 STGR22R-STGR25R (MARKED) (C-CHECK RO 10/29/2023) REPAIRED CLUSTER OF CHAFES BETWEEN FS589-FS605 STGR22R-STGR25R REF CRJ200 SRM 51-42-06 , REO 601R-53-61-8077 REV -- DATE 2023-09-06 AND REO 601R-51-00-309 REV -A DATE 2017-08-23. COMPLIED WITH 51-900-1003-SKY AND PRESSURE CHECKS GOOD. SEE CONTINUATION CARD FOR DETAILS
SERVICE DOOR FORWARD FORMER IS CORRODED EXTERNALY ALONG THE BOTTOM OF THE FORMER, (MARKED) (C-CHECK RO 10/29/2023) REPLACED FWD FORMER (LOWER FWD PAN) P/N 601R38437-2 ON SERVICE DOOR, REF. CRJ200 SRM 51-42-06 & STRUCTURE ASSEMBLY, SERVICE DOOR DWG. 601R38304, REV. BN. COMPLIED WITHTASK CARD 51-900-1003-SKY.
RH WING TRAILING EDGE RIB AT WS130.0 HAS A CRACK (C-CHECK RO 10/29/2023) REPAIRED CRACKED RH TRAILING EDGE RIB AT W.S. 130.0 PER MHIRJ REO 601R-57-51-1022 REV -- DATED 2023-08-07COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY (CL600-2B19) STRUCTURAL MAJOR REPAIRCOMPLIED WITH SKYWEST FORM M-337
LEFT INBOARD FLAP VANE LEADING EDGE IS CHAFED AT WS97. S/N 111 (C-CHECK RO 10/29/2023) REMOVED AND INSTALLED NEW L/H INBOARD FLAP VANE LEADING EDGE CRJ 200 SRM 51-42-13 AND DRAWING 601R14302 REV E. COMPLIED WITH 51-900-1003-SKY AND SEE CONTINUATION CARD FOR DETAILS
WHILE IN CRUISE GEAR DISAGREE WARNING MESSAGE CAME ON, THE GEAR FUNCTIONED NORMALLY ON LANDING. R&R DOWNLOCK PROXIMITY SENSOR HARNESS IAW AMM. SWUNG ALL 3 GEAR MULTIPLE TIMES WITHOUT ANY DEFECTS IAW AMM. OPS CHECKS GOOD.
FUSELAGE SKIN DAMAGE AT FS 640-654 AND STR'S 23L-24L. (C-CHECK) RO: 05/02/2019 REPAIRED FUSELAGE SKIN DAMAGE AT FS 640-654 AND STR'S 23L-24L. BY EXTERNAL DOUBLER IAW REO.
RT WING PLANK MOST AFT FASTENER HOLE ON END OF STRAP OVERSIZED. (C-CHECK) RO: 05/02/2019 COMPLIED WITH REPAIR OF RT WING PLANK MOST AFT FASTENER HOLE ON END OF STRAP OVERSIZED IAW REO.
LT ELEVATOR TRAILING EDGE HAS DAMAGE NOTED APPROXIAMTELY 3 INCHES AND 6 INCHES FROM IB EDGE. (C-CHECK) RO: 05/02/2019 REPAIRED LT ELEVATOR IAW SRM AND REO.
PAX DOOR FWD AND AFT CLEATS CORRODED AROUND NUTPLATES. (C-CHECK) RO: 05/02/2019 REMOVED AND INSTALLED NEW CLEATS P/N 601R31527-137 AND 601R31527-217, IAW SRM.
LT ND RT FS621 TO FS625 OBILQUE ANGLES ARE CRACKED. (C-CHECK) RO: 05/02/2019 REMOVED & REPLACED LT & RT 621 OBLIQUE ANGLES P/N 60135012-51 & 60135012-52 IAW SRM.
NOTICED PAINT-LIKE SMELL UPON STARTING APU AND SWITCHING BLEEDS ON FINAL APPROACH. IMMEDIATELY SWITCHED BACK TO ENGINE BLEEDS. THIS REDUCED THE SMELL IN THE COCKPIT. FA REPORTED THAT THE SMELL HAD ACTUALLY BEGUN CLOSER TO TOP OF DESCENT. (FLT#3742) DEFERRED PACK IAW MEL.
GEAR DISAGREE AND NOSE DOOR OPEN WARNING MESSAGE AFTER TAKEOFF WHEN SELECTING THE LANDING GEAR UP. THE NOSE GEAR STAYED IN THE DOWN POSITION. WE LEVELED OFF AND MAINTAINED 200KT. JUST BEFORE RUNNING THE QRH THE NOSE GEAR RETRACTED AND THE NOSE DOOR CLOSED ON ITS OWN. PERFORMED BOTH QRH PROCEDURES AND RETURNED TO GNV FOR A NORMAL LANDING AND NO FURTHER INCIDENT. (FLT#3830) CLOSED ADJUSTED PS4GA TO CORRECT RANGE IAW AMM. PERFORMED GEAR EXTENSION AND RETRACTION TEST FOR SEVERAL CYCLES IAW AMM. GEAR SWING SUCCESSFUL. OPS CHECK GOOD. NO DEFECTS OR MESSAGES SHOWING AT THIS TIME.
GEAR DISAGREE MASTER WARNING ON TAKE OFF. NOSE WHEEL CAME UP AFTER A DELAY AND MESSAGE CLEARED. (FLT 4857) CLOSED REMOVED AND REPLACED NLG UP LOCK PIN ASSY. PERFORMED NLG RETRACTION/EXTENSION CHECK. OPS. CK, A/C GOOD FOR SERVICE
NOSE DOOR OPEN WARNING MESSAGE ON GEAR RETRACTION ON DEPARTURE. RETURNED TO FIELD. (FLT#2626) FO: 09/28/2018 CLOSED REMOVED AND REPLACED THE NLG DOOR SELECTOR VALVE IAW AMM. OPS AND LEAK CHECK GOOD.
GEAR DISAGREE AFTER TAKEOFF, NOSE GEAR DID NOT GO INTO TRANSITION. REMOVED AND REPLACED THE NOSE LANDING GEAR PRIORITY VALVE. OPS AND LEAK CHECKS GOOD. CYCLED NOSE LANDING GEAR MULTIPLE TIMES, OPS CHECK GOOD IAW AMM.
GEAR DISAGREE WARNING MESSAGE WHEN BRINGING GEAR UP AFTER TAKE OFF. NOSE GEAR DID NOT COME UP. RAN QRH PROCEDURES FOR GEAR DISAGREE WARNING. QRH PROCEDURES RESULTED IN GEAR DOWN AND LOCKED. IAW QRH LANDING GEAR MANUAL RELEASE HANDLE WAS PULLED. REMOVED AND REPLACED NLG PRIORITY VALVE, AND NLG WOW HARNESS IAW AMM. OPS CHECKED GOOD.
NOSE GEAR DISAGREE AFTER TAKE-OFF. REPLACED THE NLG PROXIMITY SENSOR BRACKET.
CABIN FLOOR SUPPORT, BS 559+80 TO 559+86 BLEND FOUND OUT OF LIMITS. REPAIRED IAW REO.
FRAME AT BS 333, STRINGER 27 CORRODED OUT OF LIMITS. REPLACED THE FRAME IAW DWG.
LBL 27, BS 585 TO 609 FLOOR SUPPORT HAS CORROSION AROUND SCREW HOLES. INSTALLED A NEW SERVICEABLE FLOOR SUPPORT IAW DWG AND REO.
BS 605, STRINGER 26R TO 25L FRAME HAS CORROSION. REPAIRED IAW REO.
FRAME AT BS 589, STRINGER 22L HAS CORROSION. REPAIR THE FRAME IAW REO.
FLOORBEAM AT BS 349, RBL 41 TO 43 HAS CORROSION ON THE END. REPAIRED IAW REO.
SERVICE DOOR LOWER SILL CORRODED AT FWD LATCH. REPLACED SERVICE DOOR SILL ANGLE IAW SRM. OPS CHECKED GOOD.
LEFT MLG DRY BAY, BAT PANEL STIFFENER CRACKED. REPLACED THE STIFFENER IAW SRM AND DWG.
RIGHT MLG DRY BAY, BAT PANEL STIFFENER CRACKED. REPLACED THE STIFFENER IAW SRM AND DWG.
RIGHT FLAP VANE SKIN LEADING EDGE WORN AT THREE SPOTS. BLENDED WITHIN LIMITS. REPLACED THE FLAP VANE SKIN LEADING CAPS .
LEFT AILERON LOWER INBOARD AND OUTBOARD FIXED LEADING EDGES ARE CHAFED. REPLACED FIXED LEADING EDGES IAW SRM.
LEFT INBOARD FLAP VANE LEADING EDGE SKIN IS CHAFED IN 3 PLACES. REMOVED AND REPLACED FLAP VANE LEADING EDGE SKIN IAW SRM
FUSELAGE SKIN DENTED, STRINGER 21 AND 22R, BS 718. INSTALLED A REPAIR DOUBLER IAW SRM.
CREW RECEIVED A GEAR DISAGREE THE NOSE STAY DOWN AND MAINS CAME UP, WOW INPUT MESSAGE AND A STEER INOPERATIVE. AIRCRAFT RETURNED TO THE FIELD . SERVICED NLG AND EXTENSION RETRACTION CHECK AS REQUIRED IAW AMM. NO OTHER DEFECTS NOTED.
AFTER TAKING OFF AND CLIMBING THRU FL 600 THE CREW HEARD A THUMP AND THE NR 1 ITT STARTED FLASHING RED FOLLOWED BY AN ENGINE VIBRATION. CREW SHUT THE ENGINE DOWN AND RETURNED TO DEPARTURE. CREW DECLARED AN EMERGENCY. THE EXCEEDANCE PAGE OF THE MDC SHOWED THE NR 1 ENGINE GOING TO 1233 DEG C FOR 5.1 SECONDS FOLLOWED BY A SECOND EVENT OF 1219 DEG C FOR 14 SECONDS. R & R LT ENGINE IAW AMM. OPS CHECKS AND LEAK CHECKS GOOD.
BS 202 BULKHEAD AT PARKING BRAKE CABLE PASS THRU CRACKED. REPAIRED FWD PRESSURE BULKHEAD IAW REO.
SERVICE DOOR HINGE ARM IS CHAFED AT UPPER AFT EDGE. C-CHECK, RO 4/9/15, REPAIRED CHAFE TO SERVICE DOOR HINGE ARM AT UPPER AFT EDGE, COMPLIED WITH ALL STEPS OF PERMANENT REPAIR. REF STS EA.
PAX DOOR LOWER LT END CAP DENTED. REPAIRED DENT ON PAX DOOR LOWER LT END CAP REF REO.
PAX DOOR UPPER RT FITTING CAM GOUGED. REPAIRED PAX DOOR UPPER RT FITTING CAM REF STS EA.
LT INBD FLAP, AT INBD FLAP VANE ACTUATOR, UPPER SKIN INTERNAL SURFACE IS CHAFED. C-CHECK, RO 4/9/15, REPAIRED LT INBD FLAP AT INBD FLAP VANE ACTUATOR UPPER SKIN INTERNAL REF REO.
FA EMERGENCY FLASHLIGHT IS INOPERATIVE. REMOVED AND REPLACED FORWARD FA FLASHLIGHT BATTERY IAW AMM.
MID CABIN EXIT ROW SIGN FOUR FACING ANNUNCIATOR LIGHTS MISSING COLORED COVERS. REPLACED MID CABIN EXIT ROW REAR FACING ANNUNCIATOR LIGHT IAW AMM.
NR 4 OVERHEAD EMERGENCY IS BURNED OUT. REPLACED LAMP.
LOSS OF ALL FLUID IN HYD SYSTEM NR 3. COMPLIED WITH QRH, & PERFORMED MANUAL GEAR EXTENSION. FLT 5650 REPLACED O-RING FOR BLANKING CAP ON NR 3 HYD MANIFOLD IAW AMM.
MID CABIN CURVED EMERGENCY EXIT SIGN WILL NOT ILLUMINATE ON FWD FACING SIDE. ALSO NOTED LT & RT MID CABIN EMERGENCY EXIT SIGNS WILL NOT ILLUMINATE AS WELL AS EXTERIOR RT FWD MOST EXIT LAMP. FLT#5658 REPLACED TB 105-1, 105-2, 105-3, 105-4, & REPLACED NR 2 ELBP & CHARGER. PN AD-2013-1A, SN ON 57132, SN OFF 69299.
LT WING FWD EMERGENCY EXIT LIGHT IS BURNED OUT. FLT#6494 RELAMPED.
PAX DOOR FWD PULL IN LEVER IS CHAFED. C-CHECK REMOVED CHAFE FROM PAX DOOR FWD PULL IN LEVER IAW REO.
RT WING LIGHT CORROSION ON BOTTOM LIP OF FUEL PANEL 640BB. C-CHECK REMOVED CORROSION FROM RT WING PLANK AT ACCESS HOLE 640BB IAW REO.
RT WING, RT FLAP VANE SKIN, INBD FOREFLAP HAS A CHAFE MARK AT CENTER. C-CHECK BLENDED CHAFE ON RT INBD FLAP VANE FOREFLAP CENTER SECTION IAW REO.
RT WING, RIGHT FLAP VANE SKIN, INBD FOREFLAP HAS A CHAFE MARK OTBD. C-CHECK REMOVED CHAFED OUT OF LIMITS VANE CAP & INSTALLED NEW LE SKIN VANE CAP, PN 601R14303-44S ON RT INBD FLAP VANE OTBD SECTION IAW REO.
LT INBD FLAP VANE LE CHAFED AT OTBD EDGE NEXT TO ACTUATOR ROD END. C-CHECK BLENDED CHAFE ON LT INBD FLAP VANE LE AT OTBD EDGE NEXT TO ACTUATOR ROD END IAW REO.
LT INBD FLAP VANE LE CHAFED ON INBD ACTUATOR ROD END. C-CHECK BLENDED CHAFED AREA ON LT INBD FLAP VANE LE INBD SECTION IAW REO.
LT INBD FLAP VANE LE CHAFED AT CENTER ACTUATOR ROD END. C-CHECK BLENDED OUT CHAFED AREA ON LT INBD FLAP VANE LE CENTER SECTION IAW REO.
AFT CEILING EMERGENCY EXIT SIGN ABOVE ROW 8 IS BURNED OUT. (FLT 6340) REPLACED AFT CEILING EMERGENCY EXIT SIGN ABOVE ROW 8.
MAIN CABIN DOOR OPERATES ON ITS OWN. (FLT 5597) REPLACED PASSENGER DOOR ACTUATOR CONTROL RELAY AND PASSENGER DOOR POWER ASSIST SYSTEM.
NR 1 EMERGENCY OVERHEAD LIGHTS ROW 2 BURNED OUT. (FLT 4728) RELAMPED EMERGENCY LIGHTS.
OVERHEAD LIGHT NR 2 IS BURNED OUT. (FLT 7807) RELAMPED OVERHEAD LIGHT.
NR 1 EMERGENCY OVERHEAD LIGHT BURNED OUT. (FLT 5373) RELAMPED EMERGENCY LIGHT.
MAIN CABIN DOOR WILL NOT OPEN. (FLT 7757) FOUND MAIN CABIN DOOR ASSIST MOTOR BUTTON STUCK IN THE DOOR. CLEANED DOOR ASSIST BUTTON.
NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6275) RELAMPED EMERGENCY LIGHT.
GALLEY EMERGENCY ENTRANCE LIGHTS OFF. (FLT 5319) REPLACED NR 1 INVERTER IAW CRJ AMM.
NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5332) RELAMPED EMERGENCY LIGHT.
FLT 6377, LEFT REAR OVERWING EMERGENCY EXIT LIGHT IS OUT. RELAMPED EMERGENCY LIGHT.
FLT 6377, RIGHT FORWARD OVERWING EMERGENCY EXIT LIGHT IS OUT. RELAMPED EMERGENCY LIGHT.
NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6259) RELAMPED EMERGENCY LIGHT.
ALL 3 OVERWING EMERGENCY EXIT LIGHTS ON RIGHT SIDE AND THE FORWARD LEFT OVERWING EMERGENCY LIGHT ARE OUT. (FLT 4595) RELAMPED EMERGENCY LIGHT.
NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4496) RELAMPED EMERGENCY LIGHT.
PASSENGER DOOR WARNING MESSAGE WILL NOT EXTINGUISH. (FLT 4589) INSPECTED AND FOUND PASSENGER DOOR CONNECTOR P7MB AND J7MB CORRODED AND BURNT. REPLACED PASSENGER DOOR HARNESS ASSEMBLY AND PASSENGER DOOR CONNECTOR.
NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4674) RELAMPED EMERGENCY LIGHT.
NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5414) RELAMPED EMERGENCY LIGHT.
NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4542) RELAMPED EMERGENCY LIGHT.
NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5494) RELAMPED EMERGENCY LIGHT.
NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6532) RELAMPED EMERGENCY LIGHT.
FS 559.0 BULKHEAD CRACKED AT RIGHT SIDE. (C-CHECK) REPAIR PER REO.
FS 621 BULKHEAD IS CRACKED AT LINTEL FITTING. (C-CHECK) REPAIR PER REO.
LEFT WINDSHIELD POST SUPPORT LOWER FITTING CRACKED. (C-CHECK) REPAIR PER SRM.
FS 280 BEAM CRACK AT LBL 1. (C-CHECK) REPAIRED PER REO.
NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5355) RELAMPED EMERGENCY LIGHT.
NR 3 OVERHEAD EMERGENCY LIGHT IS BURNED OUT. (FLT 2845) RELAMPED EMERGENCY LIGHT.
RIGHT FORWARD OVERWING EMERGENCY LIGHT IS OUT. (FLT 3045) RELAMPED EMERGENCY LIGHT.
NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6663) RELAMPED EMERGENCY LIGHT.
THE 2ND TO LAST OVERHEAD EMERGENCY EXIT LIGHT IS OUT. (FLT 6719) RELAMPED EMERGENCY LIGHT.
NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4579) RELAMPED EMERGENCY LIGHT.
OVERHEAD NR 3 EMERGENCY LIGHT IS OUT. (FLT 5821)RELAMPED.
LEFT WING CENTER EXTERIOR EMERGENCY EXIT LIGHT IS OUT. (FLT 4769) RELAMPED EMERGENCY LIGHT.
RIGHT FORWARD EXTERIOR EMERGENCY EXIT LIGHT IS OUT. (FLT 4769) RELAMPED EMERGENCY LIGHT.
EMERGENCY LIGHT INOPERATIVE ABOVE ROW 10. (FLT 6639) RELAMPED EMERGENCY LIGHT.
PAX DOOR HARD TO OPEN. (MX) FOUND PAX DOOR ASSIST STUCK. POWERED DOWN AIRCRAFT - DOOR ASSIST RESET.
LEFT ENGINE FORWARD MOUNT SHOW SIGNS OF PITTING. (ENGINE CHANGE) INSTALLED SERVICEABLE MOUNT.
NR 3 CEILING E-LIGHT INOP. (FLT 6520) RELAMPED EMERGENCY LIGHT.
THE 3RD OVERHEAD EMERGENCY LIGHT INOP. (FLT 6180) RELAMPED EMERGENCY LIGHT.
NR 3 EMERGENCY OVERHEAD FLOOD LIGHT INOP. (FLT 5986)RELAMPED.
NR 2 OVERHEAD EMERGENCY CEILING FLOOD LIGHT INOP. (FLT 6369) RELAMPED EMERGENCY LIGHT.
NR 1 EMERGENCY CEILING LIGHT INOP. (FLT 6359) RELAMPED EMERGENCY LIGHT.
NR 2 CEILING EMERGENCY LIGHT INOP. (FLT 6734) RELAMPED EMERGENCY LIGHT.
EMERGENCY CEILING LIGHT IN AFT OF AIRCRAFT INOP. (FLT 5987) RELAMPED EMERGENCY LIGHT .
NR 3 EMERGENCY CEILING LIGHT INOP. (FLT 6015) RELAMPED.
NR 2 OVERHEAD EMERGENCY LIGHT INOP. (FLT 6039) RELAMPED EMERGENCY LIGHT.
FS 559 PRESSURE BULKHEAD CRACKED AT LBL 18. (C CHECK) REPAIRED PER REO.
C-CHECK, FS 559 PRESSURE BULKHEAD FRAME CAP ANGLE RADIUS CRACKED. REPAIRED PER REO.
C-CHECK, FS 280 RIGHT AFT BULKHEAD GOUGED. REPAIRED PER REO.
OVERHEAD EMERGENCY FLOODLIGHT INOP. (FLT 5815) RELAMPED EMERGENCY LIGHT.
AFT EMERGENCY CEILING FLOODLIGHT INOP. (FLT 6141) RELAMPED EMERGENCY LIGHT.
VARIOUS EMERGENCY LIGHTING INOP. (FLT 6420)REPLACED INVERTER.
NR 2 EMERGENCY EXIT LIGHT INOP. (FLT 6337) RELAMPED EMERGENCY LIGHT.
FLOOR ILLUMINATION EMERGENCY LIGHTING INOP. (FLT 6497) CLEANED CONNECTIONS.
EXIT ROW EMERGENCY LIGHT INOP. (FLT 5946) RELAMPED EMERGENCY LIGHT.
FLT 6595 - AFT FLOOR EMERGENCY LIGHTS INOP. REPLACED INVERTER.
FLT 6595 - RIGHT EXTERIOR EMERGENCY LIGHT INOP. RELAMPED.
EMERGENCY CEILING FLOOD LIGHT INOP. (FLT 6403) RELAMPED EMERGENCY FLOOD LIGHT.
FLT 6024 - MAIN DOOR FLOOR LEVEL EMERGENCY LIGHT INOP. REPLACED NR 2 ELBP.
FLT 6687 - EMERGENCY EXIT CEILING CENTER LIGHT BULB INOP. RELAMPED.
FLT 6589 - NR 3 EMERGENCY LIGHT INOP. RELAMPED.
FLT 6752 - BURNED OUT BULB IN ENTRY WAY FLOOR LEVEL CABIN EMERGENCY LIGHT. REPLACED FLOOD LIGHT ASSEMBLY.
FLT 5866 - CEILING EMERGENCY LIGHT INOP. RELAMPED.
FLT 6719 - RIGHT WING FORWARD EMERGENCY EXIT LIGHT INOP. RELAMPED.
AFT EMERGENCY CEILING FLOODLIGHT INOP. (FLT 6050)RELAMPED.
EMERGENCY EXIT SIGN BY MAIN CABIN DOOR BURNED OUT (FLT 6589). RELAMPED EMERGENCY LIGHT.
FIRST CEILING EMERGENCY LIGHT IS INOP (FLT 6450). RELAMPED EMERGENCY LIGHT.
ADG DEPLOYED AFTER TAKE OFF. (FLT 6769) RESTOWED ADG IAW MM 24-23-01 AND REPLACED ADG AUTO DEPLOYMENT CONTROL UNIT IAW MM 24-23-15. OPS CHECK GOOD.
LEFT WINDSHIELD CRACKED. DIVERTED TO DLH, FLIGHT NR 5951. REPLACED LEFT WINDSHIELD IAW AMM 56-11-01, LEAK AND OPS CHECK GOOD, PN: NP-139321-13, SN OFF: 03076H8781.
AFT PRESS BULKHEAD FS 625 STRINGER CLIPS STR14L CLIPS CRACKED, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED NEW CLIP P/N 601-35012-51 PO NR 62509 IAW CRJ200 SRM 51-42-06 AND 51-42-21.
FORWARD EMERGENCY FLOOD LIGHT INOP. RELAMPED FORWARD EMERGENCY FLOOD LIGHT. OPERATIONAL CHECKS GOOD.
FLAPS FAIL CAUTION MSG. INSTALLED SERVICEABLE BPSU IAW 27-56-00. ALSO ADJUSTED FECU POTS, OPERATIONAL CHECK GOOD.
FLAP FAIL CAUTION MSG. REPLACED FECU IAW CRJ MM 27-51-05. OPERATIONAL CHECK GOOD.
CENTER STRIP OF EMERGENCY PATHWAY LIGHTING INOP. CLEANED CONNECTOR AS REQUIRED. OPERATIONAL CHECK GOOD.
RUDDER TRIM SWITCH INTERMITTENT. REPLACED TRIM CONTROL PANEL FOR AILERON AND RUDDER . OPERATIONAL CHECK GOOD.
RT WING DOWN AILERON TRIM INTERMITTENT. REPLACED AILERON TRIM SWITCH AS REQUIRED, OPERATIONAL CHECK GOOD.
PASSENGER DOOR AFT DRAG ANGLE CRACKED. ITEM FOUND AT C-CHECK INSPECTION. DRAG ANGLE REPAIRED IAW CRJ REO 601R-52-11-513.
FLOORBEAM RBL 9.0 ATTACH ANGLE IS CRACKED AT FS 280.0. ITEM FOUND AT C-CHECK INSPECTION. REPLACED ANGLE IAW CRJ SRM 51-40-11, 51-42-06, 51-42-21, 51-25-16, AND 51-23-00.
LEFT FLOORBEAM ANGLE AT FS 621.00 IS CRACKED. ITEM FOUND AT C-CHECK INSPECTION. CRACKED FLOOR SUPPORT REPAIRED IAW CRJ REO 601R-53-61-117 REV B.
CARGO DOOR SILL BETWEEN FS 574 - 621 HAS AREAS OF CORROSION AROUND ANCHOR NUTS. ITEM FOUND AT C-CHECK INSPECTION. BLENDED AND ASSESSED CORROSION IAW CRJ SRM 53-0-00 101, FOUND TO BE WITHIN LIMITS. MATERIAL REMOVED .001. AREA REPROTECTED IAW SRM 51-21-11, 51-25-16.
SPOILERONS FAULT STATUS MESSAGE IN FLIGHT. REMOVED AND REPLACED RIGHT INBOARD SPOILERON PCU IAW CRJ MM 27-62-01. OPERATIONAL CHECK GOOD.
RUDDER TRIM SWITCH INOPERATIVE. REMOVED AND REPLACED RUDDER TRIM PANEL IAW AMM 27-41-25, OPERATIONAL CHECKED GOOD.
FIRST OFFICER'S SIDE WINDOW CRACKED ON DESCENT TO LAX. REMOVED AND REPLACED RIGHT SIDE WINDOW IAW 56-12-01. P/N OFF NP139322-001, S/N OFF 03080H9346.
ON DESCENT INTO SBA, CAPTAINS SIDE WINDOW CRACKED FROM LOWER FRONT TO UPPER REAR. REMOVED AND REPLACED CAPTAINS SIDE WINDOW IAW CRJ MM 56-12-01. P/N 601R-33033-11, S/N OFF 03013H4162.
STAB TRIM CHANNEL 2 WILL NOT ENGAGE. REMOVED AND REPLACED MCU AND HSTA. OPERATIONAL CHECK GOOD IAW CRJ MM CH 27-41-01. HSTA P/N: 9386-3, S/N OFF: 1080.
STAB TRIM CH NR 2 WILL NOT ENGAGE. REPLACED STAB/MACH TRIM CONTROL PANEL. OPS CHECK GOOD IAW MM 27-00-00. P/N 601R51706-3.
CREW REPORTS LEFT FLAP INDICATES 15 DEGREES INTERMITTENTLY IN FLIGHT. REMOVED AND REPLACED LEFT FLAP POSITION TRANSMITTER ASSEMBLY IAW CRJ MM 27-55-00. OPS CHECK GOOD.