N929EV

Part: OUTFLOW VALVE — OBSTRUCTED (ZONE 100) · airframe 40,209 hrs · 37,452 cycles

EMERGENCY DESCENT DUE TO RAPID DEPRESSURIZATION AT 33K FT. CALL FROM FA ABOUT A LOUD BANG FOLLOWED BY LOSS OF PRESSURIZATION. RAN QRC & QRH, LANDED WITHOUT ANY ISSUES. (FLIGHT 5053) DURING PRESSURIZATION OPS CHECKS FOUND ONCE 6.0 DELTA P IS REACHED RATE INDICATION DROPPED TO 0 FOLLOWED BY DASHED OUT CABIN ALT, RATE & DELTA P INDICATIONS. ALSO LOST CONTROL OF CABIN PRESSURE CONTROL PANEL. REFERENCE AML 1779091 FOR REPLACEMENT OF CABIN PRESSURE CONTROL PANEL. REFERENCE AML 1779093 FOR REPLACEMENT OF CABIN PRESSURE ACQUISITION MODULE (CPAM). DURING GVI OF OUTFLOW VALVES FOUND PLASTIC BAG STUCK IN RT OUTFLOW VALVE. REFERENCE AML 1779158 FOR REMOVAL AND INSPECTION OF OUTFLOW VALVES. PERFORMED GVI & LEAK CHECK OF ALL DOOR SEALS & MATING SURFACES, NO DISCREPANCIES NOTED. PERFORMED GVI OF ECS DUCTING IN AFT E/E BAY FOR DAMAGE & PROPER CONNECTION. NO DISCREPANCIES WITH DUCTING. PERFORMED PRESSURIZATION CHECK, ACFT HOLDS AT DELTA P 4.0 WITH NO FLUCTUATIONS IAW AMM 21-31-00. DURING PRESSURIZATION INSPECTED FOR ANY LOUD BANGING SOUNDS SPECIFICALLY AROUND THE PAX & SERVICE DOORS. NO SOUND EXISTS.

Part: CABIN PRESSURE — PRESSURE LOSS (ZON E200) · airframe 40,209 hrs · 37,452 cycles

EMERGENCY DESCENT DUE TO RAPID DEPRESSURIZATION AT 33K FEET. GOT A CALL FROM FA ABOUT A LOUD BANG FOLLOWED BY LOSS OF PRESSURIZATION. RAN QRC AND QRH AND LANDED WITHOUT ANY ISSUES. (FLIGHT 5053 - FILED OPEN)

Part: SKIN — GROUND DAMAGE (ZONE 100) · airframe 39,895 hrs · 37,131 cycles

EXTERIOR DAMAGE FROM LAV SERVICING TRUCK NEAR AFT POTABLE WATER PANEL: UPON INSPECTION, FOUND DAMAGE TO FUSELAGE STRUCTURE BETWEEN FS574 €“ FS589.00 AND BTW STR 17R-18R. IMPACT (LAVATORY CART) CAUSED DAMAGE TO MULTIPLE PARTS. REFER TO REO 601R-53-61-8383 TABLE 1 FOR REPORTED DAMAGE LOCATIONS & DETAILS. (FLIGHT 5092 - FILED CLOSED) REMOVED TEMPORARY REPAIR WHERE DAMAGE IS LOCATED BETWEEN FS574 - FS589.00 AND BETWEEN STR 17R-18R. ACCOMPLISHED REO 601R-53-61-8386 REV -- DATED 10-01-2025.  RESTORED FINISH TO OUTER SURFACE OF REPAIRED AREA. PERFORMED LEAK CHECK OF REPAIR AREA. LEAK CHECK GOOD REF: REO 601R-53-61-8386 REV-- DATED 10-01-2025.

Part: RETAINER — BENT (ZONE 800) · airframe 39,489 hrs · 36,777 cycles

MCD LOWER SEAL RETAINER BENT NEAR AFT RADIUS. (FILED CLOSED)REMOVED AND REPLACED MCD LOWER CENTER AND LOWER AFT SEAL RETAINERS WITH REFERENCE TO REO 601R-51-11-915, REV. -- DATED 1/04/2006 AND SRM 51-42-06. COMPLETED 51-900-1003-SKY AND M-337. REFERENCE CP 30392947 FOR LEAK CHECK.

Part: STEERING SYS — INOPERATIVE (ZONE 700) · airframe 39,098 hrs · 36,360 cycles

STEERING INOP CAUTION MESSAGE AFTER TAKEOFF. RAN QRH MESSAGE PERSISTED. (FLIGHT 5452 - FILED CLOSED) T/S "STEERING INOP" CAUTION MESSAGE PER CRJ200 FIM 32-50-01, INSPECTED NOSE LANDING GEAR HYDRAULIC COMPARTMENT AND FOUND CONNECTOR PS1 FOR STEERING PRESSURE SWITCH LOOSE AND DIRTY. CLEANED AND RECONNECTED CANNON PLUG PS1 PER CRJ200 ESPM 20-17-10 AND CRJ200 AMM 32-51-35. PERFORMED SEVERAL OPS CHECK OF NOSE WHEEL STEERING PER CRJ200 AMM 32-51-00, OPS CHECK GOOD, NO DEFECTS NOTED.

Part: INTERCOSTAL — DAMAGED (ZONE 200) · airframe 38,762 hrs · 36,015 cycles

TRANSFERRED FROM CAMP 29417867. REF AML# 1498041: DUE TO BIRDSTRIKE DAMAGE, RH INTERCOSTAL AT BL6.10 IS DAMAGED. THIS HAS BEEN DEEMED A MAJOR REPAIR AND REQUIRES AN M-337 (FILED CLOSED) DUPLICATE WRITE UP. SEE ML 29460469 FOR MAJOR REPAIR - DUE TO BIRD STRIKE DAMAGE REMOVED AND REPLACED INTERCOSTAL BETWEEN FS202.75 - FS193.00 AND BETWEEN RBL 10.0 - BL 0.00. REMOVED AND REPLACED RIGHT SEALING STRIP AT RBL 10.0 AND BETWEEN FS 169.00 - FS 193.00. REMOVED SEVERAL BLIND CHERRY RIVETS AND INSTALLED PERMANENT SOLID RIVETS BETWEEN FS 169.00 - FS 202.75 ALL IN REF TO MHIRJ 200 SRM 51-42-06 SOLID RIVETS INSTALLATION SRM 51-22-00 FAYING SEALANT APPLICATION AND SRM 51-77-00 REPLACEMENT OF STRUCTUAL COMPONENTS

Part: INTERCOSTAL — DAMAGED (ZONE 100) · airframe 38,757 hrs · 36,011 cycles

TRANSFERRED FROM CAMP 29417867. REF AML# 1498041: DUE TO BIRDSTRIKE DAMAGE, RH INTERCOSTAL AT BL6.10 IS DAMAGED. THIS HAS BEEN DEEMED A MAJOR REPAIR AND REQUIRES AN M-337 (FILED OPEN) THIS IS CURRENTLY A WORK IN PROGRESS

Part: INTERCOSTAL — DENTED (ZONE 100) · airframe 38,757 hrs · 36,011 cycles

TRANSFER FROM EAML 1506706 : TRANSFERRED FROM CAMP 29417867. REF AML# 1498041: DUE TO BIRDSTRIKE DAMAGE, RH INTERCOSTAL AT BL6.10 P/N: 600-33011-68, REF , AL ALY ALCD 2024-T42, 0.032€? NOM. THK., REF IS DAMAGED. DAMAGE IS A DENT: 1.00€? L X 0.250€? W X 0.375€? D. NO CRACKS OBSERVED. THIS HAS BEEN DETERMINED TO BE A MAJOR REPAIR, FORM M337 WIL BE REQUIRED. (FILED OPEN) THIS IS CURRENTLY A WORK IN PROGRESS

Part: SEAL — DAMAGED (ZONE 100) · airframe 38,762 hrs · 36,015 cycles

TRANSFER FROM EAML 1506706 : TRANSFERRED FROM CAMP 29417867. REF AML# 1498041: DUE TO BIRDSTRIKE DAMAGE, RH INTERCOSTAL AT BL6.10 P/N: 600-33011-68, REF , AL ALY ALCD 2024-T42, 0.032€? NOM. THK., REF IS DAMAGED. DAMAGE IS A DENT: 1.00€? L X 0.250€? W X 0.375€? D. NO CRACKS OBSERVED. THIS HAS BEEN DETERMINED TO BE A MAJOR REPAIR, FORM M337 WIL BE REQUIRED. (FILED CLOSED) DUE TO BIRD STRIKE DAMAGE REMOVED AND REPLACED INTERCOSTAL BETWEEN FS202.75 - FS193.00 AND BETWEEN RBL 10.0 - BL 0.00. REMOVED AND REPLACED RIGHT SEALING STRIP AT RBL 10.0 AND BETWEEN FS 169.00 - FS 193.00. REMOVED SEVERAL BLIND CHERRY RIVETS AND INSTALLED PERMANENT SOLID RIVETS BETWEEN FS 169.00 - FS 202.75 ALL IN REF TO MHIRJ 200 SRM 51-42-06 SOLID RIVETS INSTALLATION SRM 51-22-00 FAYING SEALANT APPLICATION AND SRM 51-77-00 REPLACEMENT OF STRUCTUAL COMPONENTS

Part: SKIN — CRACKED (ZONE 100) · airframe 38,753 hrs · 36,010 cycles

NOSE SKIN BETWEEN FS169.00-193.00 IS CRACKED (FILED CLOSED) REPLACED NOSE SKIN BETWEEN FS169.00-193.00 IN REFERENCE TO CRJ 200 SRM 51-42-06

Part: PROXIMITY SENSOR — FAULTED (NLG) · airframe 37,961 hrs · 35,121 cycles

GEAR DISAGREE WARNING MESSAGE AFTER TAKEOFF. NOSE WHEEL DID NOT COME UP. (FLIGHT 5378 - FILED CLOSED) PLEASE REFERENCE AML 1384104 PLEASE REFERENCE AML 1384105 PLEASE REFERENCE AML 1384107 PLEASE REFERENCE AML 1384108UPON COMPLETION OF REMOVAL AND REPLACEMENT OF DAMAGED PROX SENSORS, PERFORMED GEAR SWINGS OF NLG REF CRJ 200 AMM 32-33-00, OPS CHECK GOOD AT THIS TIME. PERFORMED OPS CHECK OP NLG PROXIMITY SENSORS REF CRJ 200 AMM 32-61-00-710-801, OPS CHECK GOOD AT THIS TIME NO FURTHER FAULTS FOUND. NO MORE MESSAGE PRESENT AT THIS TIME. AIRCRAFT OKAY FOR CONTINUED SERVICE.

Part: UNKNOWN — DAMAGED (UNKNOWN) · airframe 37,511 hrs · 34,628 cycles

CLASSIFICATION OF MAJOR/MINOR DAMAGE REQUIRED PER GMM 3.25 AND 3.26MCI TYPE: SERVICEABLE / NEEDS ATTENTION (FILED OPEN)APR 04, 2024 STATION: ATW--DAMAGE REQUIRES MAJOR REPAIR IAW 3.26

Part: NONE — NONE (NONE) · airframe 37,528 hrs · 34,652 cycles

CLASSIFICATION OF MAJOR/MINOR DAMAGE REQUIRED PER GMM 3.25 AND 3.26MCI TYPE: SERVICEABLE / NEEDS ATTENTION (FILED CLOSED)APR 04, 2024 STATION: ATW--DAMAGE REQUIRES MAJOR REPAIR IAW 3.26 APR 10, 2024 STATION: MKE -- REFERENCE AML 1324409. DAMAGE WAS PREVIOUSLY CLASSIFIED. ALSO REFERENCE CP# 28039060 DAMAGE WAS ISOLATED TO SERVICE DOOR ONLY AND SERVICE DOOR WAS REMOVED AND REPLACED ON 4/4/24. THIS CAMP IS NO LONGER REQUIRED.

Part: UNKNOWN — DENTED (UNKNOWN) · airframe 36,981 hrs · 34,074 cycles

DENT DAMAGE FOUND TO RH SIDE OF THE FUSELAGE, BELOW THE FORWARD EDGE OF THE RH ENGINE, AND IN THE PRESSURE VESSEL. THE DENT IS LOCATED ON THE FUSELAGE BETWEEN FS574.00 AND FS589.00 AND BETWEEN WL 97.50 AND WL 79.50. DENT MEASURES 15€? IN WIDTH BY 12 13/16€? IN HEIGHT AND IS 0.423€? DEEP. THE DENT IS CENTERED ON A DOUBLE ROW OF RIVETS. REF. AML 1229759 FOR ORIGINAL DISCREPANCY. (FLIGHT 4744 FILED CLOSED)THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 27322221 WITH THE FOLLOWING CORRECTIVE ACTION: "REPAIRED DENT DAMAGE TO FUSELAGE SKIN BETWEEN FS574.00 - FS589.00 AND STR14R - STR16R IN REF TO REO 601R-53-61-8102, REV--, DATED 2023-11-24. COMPLIED WITH TASK CARD 51-900-1003-SKY."

Part: UNKNOWN — DENTED · airframe 36,228 hrs · 33,323 cycles

MULTIPLE DENTS NOTED ON EXTERIOR SKIN BELOW CARGO DOOR CUTOUT (MARKED) (C-CHECK RO 4/30/2023) COMPLIED WITH DISPOSITION FOR DENTS AND BLEND TO FUSELAGE SKIN BETWEEN FS605 - FS621 AND STR 18L - STR 19L REF REO 601R-53-61-8000 REV -- 2023-04-12. COMPLIED WITH TASK CARD 51-900-1003-SKY. LEAK CHECK GOOD

Part: UNKNOWN — CRACKED · airframe 36,228 hrs · 33,323 cycles

FS.280 HAS A CRACKED CLIP ON THE INBD SIDE OF LBL 9 (MARKED) (C-CHECK RO 4/30/2023) REMOVED CRACKED CLIP, FS 280 LBL9 INBD SIDE AND INSTALLED NEW CLIP PER DWG#601R31113 REV AD AND CRJ 200 SRM 51-42-21. SEE CONTINUATION CARD FOR DETAILS. M-337 AND SKYWEST TASK CARD 51-900-1003-SKY COMPLIED WITH.

Part: UNKNOWN — CRACKED · airframe 36,228 hrs · 33,323 cycles

L/ WING WS 48.3 UPPER FWD BATT ANGLE CRACKED . (C-CHECK RO 4/30/2023) REPLACED L/ WING WS 48.3 UPPER FWD BATT ANGLE WITH NEW PN 600-10204-27 PO# T60652 REF CRJ 200 SRM 51-42-06 AND BOMBARDIER DWG 600-10204 REV M .COMPLIED WITH SKY CARD 51-900-1003 SKY STRUCTURAL MAJOR REPAIR.

Part: UNKNOWN — CHAFED · airframe 36,228 hrs · 33,323 cycles

LH APRON SKIN CHAFED BY WING P SEAL. (C-CHECK RO 4/30/2023) COMPLIED WITH REPAIR TO LH APRON SKIN AS PER REO 601R-53-41-115 REV -A DATE 2005-07-20. M337 AND SKYWEST TASK CARD 51-900-1003-SKY COMPLIED WITH.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 36,228 hrs · 33,323 cycles

LH REPLACEMENT TRUNNION REQUIRES SERVICE BULLETIN 601R-57-048 REV C DATED 06/06/2013 RE-INCORPORATION. (C-CHECK RO 4/30/2023) COMPLIED WITH ALL STEPS OF FINAL REO 601R-57-21-3728 REV -- DATED 2023-04-05 ON LH REPLACEMENT TRUNNION. M-337 AND SKYWEST TASK CARD 51-900-1003-SKY COMPLIED WITH.

Part: UNKNOWN — CRACKED · airframe 36,228 hrs · 33,323 cycles

LH MLG TRUNNION REQUIRES REPLACEMENT DUE TO FINDING CRACKED HOLES (C-CHECK RO 4/30/2023) REMOVED OLD LH TRUNNION AND STEEL STRAP AND INSTALLED NEW LH TRUNNION AND STEEL STRAP REF REO 601R-57-21-3714 REV -- DATED 2023-04-05 AND BOMBARDIER RIL #3690 REV B DATED 15 MAR 2023. COMPLIED WITH MAJOR REPAIR FORM M-337 AND SKYWEST TASKCARD 51-911-1003-SKY. SEE ATTACHED CONTINUE CARD FOR WORK ACCOMPLISHED.

Part: UNKNOWN — CORRODED · airframe 36,228 hrs · 33,323 cycles

RH WING LOWER WING PLANK ACCESS HOLE 610AB HAS CORROSION.FLAGGED (C-CHECK RO 4/30/2023) REPAIRED RH WING LOWER WING PLANK ACCESS HOLE 610AB REF REO 601R-57-21-3717 REV-- DATED: 2023-03-23 AND SRM 51-21-06. SEE CONTINUE CARD FOR DETAILS. M-337 AND SKYWEST TASK CARD 51-900-1003-SKY COMPLIED WITH.

Part: UNKNOWN — CRACKED · airframe 36,228 hrs · 33,323 cycles

L/H MLG WHEEL WELL - TRUNION RIB BRACKET (BAT) HAS SUSPECTED CRACK - WS 48 (C-CHECK RO 4/30/2023) REPLACED L/H MLG WHEEL WELL - TRUNION RIB BRACKET (BAT) WITH NEW PN 600-10389-1 REF CRJ 200 SRM 51-42-21 AND BOMBARDIER DWG 600-10204 REV M . COMPLIED WITH SKY CARD 51-900-1003-SKY STRUCTURAL MAJOR REPAIR.

Part: UNKNOWN — CORRODED · airframe 36,228 hrs · 33,323 cycles

R/H FLOOR SEAT RAIL FROM FS409.0+128 TO FS559.0 HAS SEVERAL SPOTS OF CORROSION (MARKED WITH RED GREASE PENCIL.) (C-CHECK RO 4/30/2023) REMOVED AND INSTALLED NEW RH FLOOR SEAT RAIL PN 20276-288-0-0A BETWEEN FS 409.00 +128 AND FS 559.00 PER CRJ 200 AMM 53-01-11-400-802 TOOL USED C-ID : TUC6039 CAL 30-AUG-22 DUE : 31-AUG-23. COMPLIED WITH ALL STEPS OF REO 601R-53-00-485 REV D DATED 01/29/18

Part: UNKNOWN — DENTED · airframe 36,228 hrs · 33,323 cycles

PAX DOOR INTERCOSTAL AFT DD1 UPPER FLANGE HAS DENT. (C-CHECK RO 4/30/2023) EVALUATED REPAIR AND FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED WITH NEW PAX DOOR INTERCOSTAL AT DD1 REF BOMBARDIER DWG 601R31702 REV-N, CRJ 200 AND SRM 51-42-06. PRESSURE CHECK GOOD. SKYWEST TASK CARD 51-900-1003-SKY COMPLIED WITH. SEE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.

Part: UNKNOWN — CORRODED · airframe 36,228 hrs · 33,323 cycles

PAX DOOR INTERCOSTAL MID DD3 HAS CORROSION BETWEEN FRAMES FS320-FS338 (C-CHECK RO 4/30/2023) EVALUATED REPAIR AND FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED WITH NEW PAX DOOR INTERCOSTAL AT DD3 REF BOMBARDIER DWG 601R31702 REV-N, AND CRJ 200 SRM 51-42-06. PRESSURE CHECK GOOD. SKYWEST TASK CARD 51-900-1003-SKY COMPLIED WITH. SEE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.

Part: UNKNOWN — CORRODED · airframe 36,228 hrs · 33,323 cycles

INTERCOSTAL MID DD4 HAS CORROSION BETWEEN FRAMES FS320-FS338 (C-CHECK RO 4/30/2023) EVALUATED REPAIR AND FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED WITH NEW PAX DOOR INTERCOSTAL AT DD4 REF BOMBARDIER DWG 601R31702 REV-N, CRJ 200 SRM 51-42-06 AND CRJ 200 SRM 51-42-21. PRESSURE CHECK GOODSKYWEST TASK CARD 51-900-1003-SKY COMPLIED WITH. SEE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.

Part: UNKNOWN — CRACKED · airframe 36,228 hrs · 33,323 cycles

DURING WORKING ON SB 601R-57-046 REV C DATED 12/20/012 , FOUND 4 CRACKED HOLES AT .3310" AND ONE NO CRACKED OVERSIZED HOLE (.3410") ON RIGHT WING (AS MARKED) (C-CHECK RO 4/30/2023) COMPLIED WITH REO 601R-57-21-3715 REV -- DATED 2023-03-18 FOR REPAIR 4 CRACKED HOLES AND ONE OVERSIZED HOLE (.3410") ON RIGHT WING . COMPLIED WITH SKY CARD 51-900-1003-SKY STRUCTURAL MAJOR REPAIR.

Part: UNKNOWN — CORRODED · airframe 36,228 hrs · 33,323 cycles

PAX DOOR INTERCOSTAL MID DD6 HAS CORROSION BETWEEN FRAMES FS320-FS338 (C-CHECK RO 4/30/2023) EVALUATED REPAIR AND FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED WITH NEW PAX DOOR INTERCOSTAL AT DD6 REF BOMBARDIER DWG 601R31702 REV-N, CRJ 200 SRM 51-42-06 AND CRJ 200 SRM 51-42-21. PRESSURE CHECK GOOD. SKYWEST TASK CARD 51-900-1003-SKY COMPLIED WITH. SEE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.

Part: UNKNOWN — CRACKED · airframe 36,228 hrs · 33,323 cycles

CRACK NOTED AT L/H SIDE OF TRU BAY FLOOR BETWEEN FRAME 193 AND THE BRAKE ACCUMULATOR GAUGES (MARKED) (C-CHECK RO 4/30/2023) REPAIRED LH TRU BAY FLOOR BETWEEN FRAME 193 AND THE BRAKE ACCUMULATOR GAUGES PER REO 601R-53-11-111 REV NC DATE 98-MAR-18, SRM 51-42-06 REV 39 DATED MARCH 10/2021 AND 51-21-16 REV 39 DATED MARCH 10/2021. COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY AND M-337 FORM

Part: UNKNOWN — CORRODED · airframe 36,228 hrs · 33,323 cycles

R/H PRESSURE FLOOR SILL PANEL FS 409+128 - FS559.00 HAS MULTIPLE AREA'S OF CORROSION AROUND SCREW HOLES. CIRCLED WITH A GREASE PENCIL. (C-CHECK RO 4/30/2023) REPAIRED MULITPLE AREAS OF CORROSION AROUND THE SCREW HOLES ON THE RH PRESSURE FLOOR SILL PANEL @ FS.409+128 - FS.559 AND FOUND TO BE WITHIN LIMITS REF REO 601R-53-41-666 REV -C DATED 2012-11-06 AND CRJ200 SRM 51-21-06 REV 39, DATED MARCH 10/2021. COMPLIED WITH TASK CARD 51-900-1003-SKY. SEE CONTINUATION FOR FURTHER DETAILS.

Part: UNKNOWN — DAMAGED · airframe 36,228 hrs · 33,323 cycles

FLOOR BEAM ATTACHMENT TO THE REAR PRESSURE BULKHEAD LBL9 HAS AN ERRANT HOLE THRU THE INBOARD FLANGE FS617.25. (MARKED IN RED) (C-CHECK RO 4/30/2023) COMPLIED WITH ALL STEPS OF REO 601R-53-61-7989 REV-- DATE:2023-04-03. COMPLIED WITH TASK CARD 51-900-1003-SKY. SEE CONTINUATION FOR FURTHER DETAILS.

Part: UNKNOWN — CRACKED · airframe 36,228 hrs · 33,323 cycles

*SUSPECTED CRACK AT PAX DOOR AFT FORMER BETWEEN DD6-DD5 (MARKED) (C-CHECK RO 4/30/2023) SUSPECTED CRACK CONFIRMED. REMOVED AND REPLACED WITH NEW PAX DOOR AFT FORMER REF BOMBARDIER DWG 601R31702 REV-N, CRJ 200 SRM 51-42-06 AND CRJ 200 SRM 51-42-21. PRESSURE CHECK GOOD. SKYWEST TASK CARD 51-900-1003-SKY COMPLIED WITH. SEE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.

Part: UNKNOWN — CRACKED · airframe 36,228 hrs · 33,323 cycles

CLIP ON INTERCOSTAL IS CRACKED, FS621.00 - FS625 STGR14L. (MARKED) (C-CHECK RO 4/30/2023) REMOVED DAMAGED AND INSTALLED NEWLY DRILLED ANGLE ATTACHING TO INTERCOSTAL ATFS621.00 - FS625 STGR14L REF CRJ200 SRM 51-42-21 AND DWG 601-35012 REV-D. M337 AND SKYWEST TASK CARD 51-900-1003-SKY COMPLIED WITH.

Part: UNKNOWN — CRACKED · airframe 36,228 hrs · 33,323 cycles

L/H SIDE LEFT WINDSHIELD SIDE SIDEPOST SUPPORT STRUCTURE HAS SUSPECT CRACK AT RADIUS. (C-CHECK RO 4/30/2023) REMOVED AND INSTALLED NEW REPLACEMENT L/H SIDE LEFT WINDSHIELD SIDEPOST SUPPORT ANGLE.REF CRJ200 SRM 51-42-06,SRM 51-42-13 DWG:601R34032 REV-V. LEAK CHECK GOOD. SEE CONTINUE CARD FOR DETAILS. COMPLIED WITH TASK CARD 51-900-1003-SKY AMD M- 337

Part: UNKNOWN — CRACKED · airframe 36,228 hrs · 33,323 cycles

EVALUATE POSSIBLE CRACK ON LEFT ENG. PYLON CANTED RIB. (MARKED) (C-CHECK RO 4/30/2023) REMOVED AND INSTALLED 1 EA NEW LOWER DRAG BRACE ON LH ENGINE PYLON PN 601-37030-1 PER CRJ 200 SRM 51-42-21 AND DWG # 601-37003 REV T. SEE CONTINUATION FOR FURTHER DETAILS.

Part: UNKNOWN — CRACKED · airframe 36,228 hrs · 33,323 cycles

R/H SIDE WINDSHIELD SIDE POST AFT LOWER CLIP IS CRACKED AT RADIUS. (C-CHECK RO 4/30/2023) REMOVED AND INSTALLED NEW AFT LOWER CLIP PART NUMBER 601R33235-4 AT RH SIDE WINDSHIELD REF. CRJ200 SRM 51-42-21. DRW NO.601R33007 REV-U. COMPLIED WITH TASK CARD 51-900-1003-SKY

Part: UNKNOWN — CRACKED · airframe 36,228 hrs · 33,323 cycles

COMPLY WITH SCHEDULED MAINTENANCE CODE: RA74501-601R-53-11-2381 929EV-PR1 - LEFT NOSE ELECTRONIC BAY ACCESS DOOR AFT LATCH CUT-OUT HAS A CRACK. COMPLIED WITH TEMP REPAIR ON LEFT NOSE ELECTRONIC BAY ACCESS DOOR AFT LATCH CUT-OUT IN REFERENCE TO REO 601R-53-11-2381 REV A DATED 2019-07-15. PERMANENT REPAIR DUE AT NEXT 'C' CHECK, PART NUMBER: - , SERIAL NUMBER: 8007, POSITION: (C-CHECK RO 4/30/2023) COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY. REMOVED AND REPLACED LEFT NOSE ELECTRONIC BAY ACCESS DOOR SKIN(P/N:600-33052-145). REF CRJ200 SRM 51-42-06, 51-42-13, & 51-42-22. DWG# 600-33052 REV-Y. REO 601R-53-11-3844 REV-- DATED 2023-03-2017. COMPLIED WITH REO 601R-53-11-3851 REV-- DATED 2023-03-28 (CURRENT CERTIFIED RVSM MAPPING IS STILL VALID) NO FURTHER ACTIONS REQUIRED. SEE CONTINUATION CARD FOR FURTHER DETAILS.

Part: UNKNOWN — DAMAGED · airframe 36,228 hrs · 33,323 cycles

COMPLY WITH REO 601R-53-41-1116 REPAIR & REINFORCEMENT FOR FS 559.00 LWR CAP ANGLES BL 9.00 & 18.00 LHS & RHS (C-CHECK RO 4/30/2023) COMPLIED WITH REO 601R-53-41-1116 REV-C, 2017-03-09, REPAIR & REINFORCEMENT FOR FS 559.00 LWR CAP ANGLES BL 9.00 & 18.00 LHS & RHS, REF CRJ200 SRM51-42-06 AND CRJ200SRM51-42-21. LEAK TEST GOOD. COMPLIED WITH TASK CARD 51-900-1003-SKY.

Part: PCU — OUT OF TOLERANCE (LT SPOILER) · airframe 33,766 hrs · 31,116 cycles

LT INBOARD FLIGHT SPLR PCU RESISTANCE VALUE MEASURED AT SECU PLUG: 2P1CN-A PINS: 11A/12A WAS FOUND TO BE OUT OF RANGE (1.007 K OHMS). REMOVED AND REPLACED LT INBOARD FLIGHT SPOILER PCU, IAW CRJ 200 AMM 27-62-01 REF CP 22194277-1 FOR LEAK CHECK. REF CP 22194288-1 FOR OPERATIONAL CHECK.

Part: PCU — OUT OF TOLERANCE (LT SPOILERON) · airframe 33,766 hrs · 31,116 cycles

LT INBOARD SPOILERON PCU RESISTANCE VALUE MEASURED AT SECU PLUG: 2P1CN-B PINS: 1A/2A WAS FOUND TO BE OUT OF RANGE (1.015 K OHMS). REMOVED AND REPLACED LT INBOARD SPOILERON PCU, PER AMM 27-62-01 REF CP 22193782 FOR LEAK CHECK REF CP 22193864 FOR OPERATIONS CHECK.

Part: SKIN — DAMAGED (RT ELEVATOR) · airframe 30,980 hrs · 28,570 cycles

RH ELEVATOR SKIN UPPER I/B THERE ARE TOOLING MARKS AROUND FASTENERS. (C-CHECK) RO: 06/09/2019 REPAIRED RH ELEVATOR UPPER INBD SKIN IAW REO.

Part: POST — CRACKED (BS 409) · airframe 30,980 hrs · 28,570 cycles

6EA FS409+128 VERT POSTS HAVE CRACK INDICATIONS NOTED IN THE AFT RADIUS AT WL69,. ALL 6 INDICATION FAILED NDT. (C-CHECK) REMOVED AND REPLACED 6EA FS409+128 VERT POSTS IAW REO.

Part: STRAP — CORRODED (BS 559) · airframe 26,086 hrs · 24,144 cycles

CORROSION ON FLOOR SUPPORT STRAP AT BS 559, LBL 40. REMOVED AND REPLACED THE STRAP IAW SRM.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 26,086 hrs · 24,144 cycles

COCKPIT FLOORBEAM AT BS 280, BTW LBL 11 - RBL 11 HAS CORROSION. REMOVED AND REPLACED THE FLOORBEAM ANGLE IAW SRM.

Part: VANE — CHAFED (LT WING TE FLAP) · airframe 21,692 hrs · 20,187 cycles

LEFT INBD FLAP VANE, CENTER L/E CHAFED BEYOND LIMTS. R & R LT INBD FLAP VANE CENTER L/E REF SRM.

Part: VANE — CHAFED (RT WING TE FLAP) · airframe 21,692 hrs · 20,187 cycles

RIGHT INBD FLAP VANE, CENTER L/E CHAFED BEYOND LIMITS. R & R RT INBD FLAP VANE CENTER L/E REF SRM. COMPLETED M337.

Part: BULKHEAD — UNKNOWN (BS 559) · airframe 21,692 hrs · 20,187 cycles

ACCOMPLISH REO TO LT SIDE FS 559 PRESSURE BULKHEAD, ACCOMPLISHED REO TO LT SIDE BS 559, PRESSURE BULKHEAD. COMPLIED WITH ST 51-900-1003, ATTACHED BTAC M-210B FOR WORK PERFORMED.

Part: SKIN — GOUGED (LT MLG DOOR) · airframe 21,692 hrs · 20,187 cycles

LEFT MLG DOOR GOUGE ON INNER SKIN INBD FWD, MARKED. REPAIRED LT MLG DOOR GOUGE ON INNER SKIN INBD FWD REF STS EA.

Part: BULKHEAD — UNKNOWN (BS 559) · airframe 21,692 hrs · 20,187 cycles

ACCOMPLISHED REO TO RT SIDE BS 559, PRESSURE BULKHEAD, ACCOMPLISHED REO TO THE RT SIDE BS 559, PRESSURE BULKHEAD. COMPLIED WITH ST 51-900-1003, ATTACHED BTAC FROM M-210B FOR WORK PERFORMED.

Part: PROXIMITY SENSOR — OUT OF ADJUST (MLG) · airframe 20,859 hrs · 19,496 cycles

NLG DISAGREE. GEAR WOULD NOT COME UP. RETURNED TO DEPARTURE. ADJUSTED PS14GA PROXIMITY SENSOR IAW AMM. OPS CHECK GOOD. PERFORMED MULTIPLE GEAR SWINGS IAW AMM. OPS CHECKED GOOD.

Part: STRUCTURE — DENTED (RT ENGINE) · airframe 20,497 hrs · 19,192 cycles

RIGHT ENGINE NOSE COWL HAS A DENT AT 6 O'CLOCK POSITION. REPAIRED IAW EA. NO DEFECTS NOTED.

Part: LAMP — FAILED (EMERGENCY LIGHT) · airframe 20,345 hrs · 19,057 cycles

RIGHT FWD MOST EXTERNAL EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMPS RT FWD MOST EXTERNAL EMERGENCY LIGHT IAW AMM.

Part: TRIM SYSTEM — MALFUNCTIONED (RUDDER) · airframe 19,497 hrs · 18,405 cycles

RECEIVED RUDDER TRIM RUNAWAY. OPEN.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 19,455 hrs · 18,375 cycles

MULTIPLE EMERGENCY LIGHTS DO NOT ILLUMINATE. CHARGED ELBP SWITCH IN ARM POSITION FOR 15 MIN. OPS CHECK GOOD IAW AMM.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 18,490 hrs · 17,383 cycles

NR 5 EXTERNAL EMERGENCY LIGHT INOPERATIVE. REPLACED LAMPS IAW AMM 33-51-21. OPS CHECKED GOOD.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 18,206 hrs · 17,077 cycles

FWD WARDROBE EMERGENCY FLOOR FLOODLIGHT LENS IS MISSING. R & RLIGHT ASSY IAW AMM 33-51-19. OPS CHECKED GOOD.

Part: LENS — DAMAGED (EMERGENCY LIGHT) · airframe 17,738 hrs · 16,604 cycles

INTERIOR EMERGENCY CEILING LIGHT LENS COVER AT ROW 12 DAMAGED. R & R INTERIOR EMERGENCY CEILING LIGHT LENS COVER AT ROW 12 IAW AMM 33-51-16.

Part: BPSU — FAILED (TE FLAPS) · airframe 17,735 hrs · 16,601 cycles

RECEIVED FLAPS FAIL CAUTION MESSAGE DURING CRUISE AT FL270, RAN QRH, EMERGENCY DECLARED. PERFORMED A 0 DEG FLAP LANDING. R & R RT BPSU IAW AMM 27-51-10, IPC 27-51-00 ITEM 10H. OPS CHECKED GOOD.

Part: FLASHLIGHT — CRACKED (CABIN) · airframe 17,696 hrs · 16,558 cycles

WARDROBE FLASHLIGHT HAS A CRACKED HEAD. INSTALLED SERVICEABLE FLASHLIGHT IN WARDROBE IAW AMM 25-24-01-400-801.

Part: ATTACH ANGLE — CORRODED (BS 574-621) · airframe 17,696 hrs · 16,558 cycles

LOWER CARGO DOOR SEAL PLATE FROM FS 574 TO 621 HAS CORROSION AROUND NUTPLATE HOLES. R & R CARGO DOOR SEAL PLATE ATTACH ANGLE AT FS 589 IAW SRM 51-42-21.

Part: FLOOR SUPPORT — CORRODED (BS 574-621) · airframe 17,696 hrs · 16,558 cycles

CARGO FLOOR SUPPORT IS CORRODED AROUND NUTPLATE HOLES ON OTBD SIDE FROM FS 574 TO 621 ON LBL 27. REMOVED FLOOR SUPPORT IAW SRM 51-42-06, 51-42-21, 51-42-36. INSTALLED FLOOR SUPPORT IAW REO 601R-53-61-3778, REV A & 601R-53-61-4722.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 17,696 hrs · 16,558 cycles

FOUND REAR PRESSURE BULKHEAD WEB HAS INDICATION NOTED AT LBL 27.50, WL 130 APPROX .3" IN LENGTH 100 PERCENT FSH FAILED NDT INSPECTION. COMPLIED WITH EC/TC REO 601R-53-61-1541 AND MET ALL THE REQUIREMENTS OF REO 601R-53-61-1541, REV D.

Part: ATTACH ANGLE — CRACKED (W-B FAIRING) · airframe 17,696 hrs · 16,558 cycles

LT UPPER WING UNDER WING TO FUSELAGE FAIRING 161DL FAIRING ATTACHMENT ANGLE AT FS 449.85 IS CRACKED. R & R LT UPPER WING UNDER WING TO FUSELAGE FAIRING 161DL FAIRING ATTACHMENT ANGLE AT FS 449.85 IAW SRM 51-42-06.

Part: ATTACH ANGLE — CRACKED (W-B FAIRING) · airframe 17,696 hrs · 16,558 cycles

RT UPPER WING UNDER WING TO FUSELAGE FAIRING 162DL FAIRING ATTACHMENT ANGLE AT FS 449.85 IS CRACKED. R & R RT UPPER WING UNDER WING TO FUSELAGE FAIRING 162DL FAIRING ATTACHMENT ANGLE AT FS 449.85 IAW SRM 51-42-06.

Part: BULKHEAD — CRACKED (BS 202) · airframe 17,696 hrs · 16,558 cycles

FORWARD FUSELAGE UNDER HYD ACCESS PANEL 121AL AT FS 202.00 BULKHEAD PARKING BRAKE CABLE PASS THROUGH HOLE IS CRACKED. REPAIRED IAW REO 601R-53-11-563, REV B AND REO 601R-53-11-2417, REV B. SDR CLOSED.

Part: INTERCOSTAL — CRACKED (BS 484) · airframe 17,696 hrs · 16,558 cycles

INTERCOSTAL ATTACHED TO PRESSURE FLOOR AT FS 484 BETWEEN LBL 27 AND LBL 36 IS CRACKED AT INBD END. REMOVED CRACKED ANGLE AT FS 484 LBL 27 IAW SRM 51-42-21 AND SRM 51-42-06. INSTALLED SERVICEABLE FS 484 LBL 27 ANGLE IAW SRM 51-42-06 AND SRM 51-42-21. SDR CLOSED.

Part: INTERCOSTAL — CRACKED (BS 484) · airframe 17,696 hrs · 16,558 cycles

INTERCOSTAL ATTACHED TO FUSELAGE PRESSURE FLOOR AT FS 484 BETWEEN RBL 27 AND RBL 36 IS CRACKED AT BOTH ENDS AT RADIUS OF ANGLES. REPAIR TO THE INTERCOSTALS AT FS 484 BETWEEN BL 27.00 AND BL 36.00 IS COMPLETED IAW REO 601R-53-41-059 AND MEETS WITH ALL THEIR REQUIREMENTS. SDR CLOSED.

Part: ANGLE — CRACKED (BS 625) · airframe 17,675 hrs · 16,538 cycles

LEFT OBLIQUE ANGLE AT FS 625 IN MX BAY IS CRACKED. REMOVED DAMAGED LT OBLIQUE ANGLE. LOCATED, DRILLED AND INSTALLED NEW LT OBLIQUE ANGLE AND PRIMED AND PAINTED IAW SRM 51-40-11, 51-42-06 AND 51-25-01.

Part: FLOORBEAM — CRACKED (BS 484) · airframe 17,675 hrs · 16,538 cycles

FLOORBEAM AT FS 484 BETWEEN LBL 27 AND LBL 36 IS CRACKED AT INBD END. REMOVED CRACKED ANGLE AT FS 484 LBL 27 IAW SRM 51-42-21 AND SRM 51-42-06. INSTALLED SERVICEABLE FS 484, LBL 27 ANGLE IAW SRM 51-42-06 AND SRM 51-42-21.

Part: FLOORBEAM — CRACKED (BS 484) · airframe 17,675 hrs · 16,538 cycles

FLOORBEAM AT FS 484 BETWEEN RBL 27 AND RBL 36 IS CRACKED AT BOTH ENDS AT RADIUS OF ANGLES. INSTALLED SERVICEABLE FS 484 ANGLE AT RBL 36.00 IAW REO 601R-53-41-059, REV B. REMOVED FS 484 ANGLE AT RBL 27 IAW SRM 51J-42-21 AND SRM 51-42-06.

Part: ANGLE — CRACKED (BS 625) · airframe 17,696 hrs · 16,558 cycles

LEFT OBLIQUE AT FS 625 IN MX BAY IS CRACKED. REMOVED DAMAGED LT OBLIQUE CLIPS AT FS 625. LOCATED, DRILLED AND INSTALLED NEW LT OBLIQUE CLIP AT FS 625 AND PRIMED AND PAINTED IAW SRM 51-40-11, 51-42-06 AND 51-25-01. SDR CLOSED.

Part: UPLOCK — UNSERVICEABLE (NLG) · airframe 16,975 hrs · 15,770 cycles

COMPLETED LANDING CHECKLIST, NOTICED THE NOSE GEAR INDICATOR SHOWED YELLOW DASHED BOX FOLLOWED BY RED DASHED BOX FOLLOWED BY ASSOCITATED MESSAGES. FOLLOWED QRH PROCEDURES. AFTER THIRD ATTEMPT TO LOWER GEAR, HAD 3 GREEN INDICATIONS. LANDED WITHOUT INCIDENT. EMERGENCY DECLARED. R & R NLG UPLOCK IAW AMM 32-32-05. OPS CHECKED GOOD,

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 15,606 hrs · 14,261 cycles

CABIN CEILING EMERGENCY LIGHT 2ND FROM FRONT INOPERATIVE. RELAMPED CABIN CEILING EMERGENCY LIGHT 2ND FROM FRONT AS REQUIRED. OPS CK GOOD IAW AMM 33-51-00.

Part: LIGHT — BROKEN (EMERGENCY EXIT) · airframe 13,941 hrs · 12,405 cycles

EXIT SIGN AT PAX DOOR HAS BROKEN OUT FROM WALL. R & R FLOOR LEVEL EMERGENCY EXIT LIGHT AT PAX DOOR, IAW AMM 33-51-01, OPS CHECK GOOD. (CLOSED)

Part: LIGHT — INOPERATIVE (CABIN) · airframe 13,935 hrs · 12,397 cycles

EXTERIOR RT AFT FUSELAGE EMERGENCY (OVER WING) LIGHT IN-OP. R & R RT AFT FUSELAGE EXTERIOR LIGHT IAW AMM 33-51-21. OP CKS GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 13,761 hrs · 12,194 cycles

RT MOST AFT EMERGENCY LIGHT INOP. R & R NR 4 EMERGENCY LIGHT BATTERY PACK IAW AMM 33-51-04. OPS CHECK GOOD. R & R NR 4 EMERGENCY LIGHT BATTERY PACK IAW AMM 33-51-04. OPS CHECK GOOD. (CLOSED)

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 13,761 hrs · 12,194 cycles

LT MOST AFT EMERGENCY LIGHT INOP. RELAMPED LT AFT EXTERIOR EMERGENCY LIGHT IAW AMM 33-51-21. OPS CHECK GOOD. RELAMPED LT AFT EXTERIOR EMERGENCY LIGHT IAW AMM 33-51-21. OPS CHECK GOOD.

Part: ENGINE — FAILED (NR 2) · airframe 13,321 hrs · 11,665 cycles

ON FINAL APPROACH INTO NR 2 ENGINE HAD EXCESS VIBRATION AND THEN FAILED. HAD DETAILS OF OTHER SYMPTOMS. EMERGENCY DECLARED. (N2 WENT TO 0) (N2 TO 0) RT ENG WAS CHANGED REF WO 170440 FOR ALL WORK PERFORMED.

Part: WIRE — DISCONNECTED (EMERGENCY LIGHTS) · airframe 12,882 hrs · 11,156 cycles

NUMBER 4 EMERGENCY LIGHT BATTERY PACK & CHARGER - DOES NOT ILLUMINATE LIGHTS. T/S AND FOUND WIRE PULLED OUT OF TB 107. RESET POWER WIRE INTO TB 107 IAW WDM 33-51-00 AND OP CHECK GOOD IAW AMM 33-51-00-710-801.

Part: FLOOR SUPPORT — CRACKED (BS 280) · airframe 12,875 hrs · 11,147 cycles

CABIN FLOOR SUPPORT STRUCTURE FS 280 & RBL 9.0 HAS A CRACKED CLIP. REMOVED DAMAGED FLOOR SUPPORT STRUCTURE CLIP AT F.S. 280 RBL 9 O/B CLIP IAW SRM 51-42-06 AND 51-42-21. INSTALLED SERVICEABLE CLIP IAW SRM 51-42-21 AND 51-42-06.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 12,875 hrs · 11,147 cycles

CARGO COMPARTMENT SEAT TRACKS CORRODED AT LBL 9 AND RBL 9 AND RBL 27. REMOVED CORROSION ON CARGO COMP SEAT TRACKS LBL 9, RBL 9 AND RBL 27 IAW SRM 51-21-06 STEP 3D 1, 2 & 3. COMPLIED WITH SRM 51-12-00. PERFORMED LPI ON BLENDED AREAS ON CARGO BAY SEAT TRACKS LBL 9, RBL 9 AND RBL 27 IAW NDTM 51-20-08. NO INDICATIONS NOTED AT THIS TIME. INSTALLED NEW SCREWS IN CARGO BAY SEAT RAILS IAW AMM 53-01-11-400-802 PROCEDURE 2 PARA, B STEPS 6 AND 7. APPLIED CORROSION PREVENTION TREATMENT IAW SRM 51-21-11 PARA.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 12,875 hrs · 11,147 cycles

FOUND REAR PRESSURE BULKHEAD WEB THAT SURROUND THE LINTEL ATTACHMENT FITTING HAS INDICATION NOTED APPROX .1" IN LENGTH 50 PERCENT FSH. FAILED NDT INSP. (RESOLVED ON W/O: 157513 TASKCARD: N/R-00305 ) REPAIR IAW EC/TC REO 601R-53-61-1230 HAS BEE COMPLETE & THE REPAIR C/W THE REQUIREMENTS OF EC/TC & REO 601R-53-61-1230, REV D.

Part: SUPPORT BEAM — CRACKED (FUSELAGE) · airframe 12,875 hrs · 11,147 cycles

FOUND CARGO DOOR SUPPORT BEAM AFT LOWER ANGLE IS CRACKED APPROX .3" IN LENGTH. R & R CARGO DOOR SUPPORT BEAM AFT LOWER ANGLE IAW SRM 51-42-21.

Part: FLOOR SUPPORT — CRACKED (BS 280) · airframe 12,875 hrs · 11,147 cycles

CLIP AT RBL 9 FS 280 INBD LOCATION IS CRACKED. REMOVED DAMAGED CLIP AT FS 280 RBL 9 INBD SIDE IAW SRM 51-42-06 AND 51-42-21. SERVICEABLE CLIP REQUIRES INSTALLATION. INSTALLED SERVICEABLE CLIP IAW SRM 51-42-21 AND 51-42-06.

Part: LIGHT — CRACKED (CABIN) · airframe 12,875 hrs · 11,147 cycles

WARDROBE FLOOR LEVEL EMERGENCY LIGHT BASE IS CRACKED. R & R WARDROBE FLOOR LEVEL EMERGENCY LIGHT BASE IAW MM 33-51-13-000-801 AND 33-51-13-400-801. OPS CHECK GOOD IAW MM 33-51-00-710-801.

Part: FLOOR SUPPORT — CRACKED (BS 280) · airframe 12,875 hrs · 11,147 cycles

CABIN FLOOR SUPPORT CLIPS AND STRUCTURE IS CRACKED AT FS 280.0 LBL 9.0. REPARIED CABIN FLOOR SUPPORT CLIPS AND STRUCTURE IAW REO 601R-53-11-138. APPLIED CORROSION PREVENTATIVE ON AREA IAW AMM 51-25-56-390-802.

Part: FLOOR SUPPORT — CORRODED (BS 319-330) · airframe 12,875 hrs · 11,147 cycles

RT FLOOR EDGE MEMBER FWD OF SERVICE DOOR FS 319 TO 330 HAS CORROSION. CORROSION MEASURES .004 AT DEEPEST POINT. THIS IS WITHIN REPAIRABLE LIMITS IAW SRM 53-21-43 AND 53-00-00. REMOVED CORROSION IAW SRM 51-21-06 LIGHT AND MODERATE CORROSION REMOVAL. REMOVED FLOOR EDGE MEMBER TO ACCESS CORROSION. REINSTALLED SAME SERVICEABLE FLOOR EDGE MEMBER IAW SRM 51-42-06.

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 12,069 hrs · 10,228 cycles

FLAPS FAIL MESSAGE WHEN SELECTING FLAP 8 DEGREES. EMERGENCY DECLARED. RESET FLAP SYSTEM IAW AS 2009-06-12 MOVED TO MCO EXP 10 FLT CYCLES.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 8,954 hrs · 7,283 cycles

AFT EMER CEILING LIGHT INOP RELAMPED AFT EMER CEILING LIGHT IAW AMM 33-51-16. OPS CK GOOD. (B)

Part: SUPPORT BRACKET — CRACKED (BS 529-531) · airframe 8,839 hrs · 7,174 cycles

LT MLG WHEEL WELL HYD SUPPORT BRACKET AT FS 529.35 TO FS 531.75 BETWEEN LBL 18 AND LBL 27 IS CRACKED .750 INCH LONG. REMOVED CRACKED BRACKET, INSTALLED NEW BRACKET P/N 601R75262-159 IAW CRJ 200 SRM 51-42-06. (S)

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 8,839 hrs · 7,174 cycles

PAX DOOR AFT DRAG ANGLE IS CRACKED JUST ABOVE ASSIST MOTOR PULLEY. CUT AWAY DAMAGED PROTION OF DRAG ANGLE IAW REO 601R5211513 REV.A, STEP 1-2. COMPLIED WITH HFEC IAW REO 601R-52-11-513, STEP 3 AND NDTM PT 1 51-20-06. NO INDICATIONS NOTED AT THIS TIME. INSTALLED REPAIR PARTS FOR AFT DRAG ANGLE IAW REO 601R-52-11-513 REV A, STEPS 4-12. (B)

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 8,839 hrs · 7,174 cycles

BRACKET AND ATTACHING ANGLE ONN RT ACM SUPPORT STRUCTURE ARE CRACKED, MARKED. REMOVED CRACKED BRACKET AND ANGLE AND INSTALLED NEW SERVICEABLE PARTS IAW SRM 51-42-06. (B)

Part: INTERCOSTAL — CRACKED (BS 621-625) · airframe 8,839 hrs · 7,174 cycles

INTERCOSTAL CRACKED RT FS 621.0-625.0 IN RADIUS APPROX 1 INCH IN LENGTH. REMOVED CRACKED ANGLE AND INSTALLED NEW SERVICEABLE PART IAW SRM 51-42-06. (B)

Part: PLACARD — WORN (CABIN) · airframe 8,839 hrs · 7,174 cycles

CREW ESCAPE HATCH EXTERIOR "EMERGENCY EXIT" PLACARD IS WORN. APPLIED NEW SILKSCREEN EXIT PLACARD IAW MM 11-10-03-400-801. (B)

Part: HANDLE — CRACKED (PAX DOOR) · airframe 8,839 hrs · 7,174 cycles

PAX DOOR OUTER HANDLE IS CRACKED. REMOVED CRACKED HANDLE INSTALLED NEW HANDLE KIT 601R52-119K1 IAW AMM 52-11-03-400-802. PAX DOOR HANDLE REQUIRES FUNCTIONAL TEST. PERFORMED FUNCTIONAL TEST OF THE PAX DOOR OUTER HANDLE IAW AMM -52-11-03-720-802. FUNCTIONAL TEST GOOD. REMOVED STEP 832DT TO ACCESS REPAIR AND REINSTALLED SAME SERVICEABLE STEP IAW CRJ 200 AMM 52-11-04-400-805. OK TO INSTALL. ASA RII COMPLIED WITH.

Part: FLOORBEAM — CRACKED (BS 621) · airframe 8,839 hrs · 7,174 cycles

FS 484 RIGHT INTERCOSTAL CLIP IS CRACKED 1/4" BL27.00 O/B. REPAIRED INTERCOSTAL CLIP AT FS 484 AT RBL 36.00 IAW REO 601R-53-41-059 AND REO 601R-53-41-059.

Part: FLOORBEAM — CRACKED (BS 621) · airframe 8,839 hrs · 7,174 cycles

FS 621 ANGLE IS CRACKED .5 INCH LEFT SIDE FLOOR SUPPORT. C/W REPAIR TO FLOOR SUPPORT ANGLE AT FS 621 IAW REO 601R-53-61-117. ALL WORK C/W IAW REO 601R-53-61-117. (B)

Part: FLOORBEAM — CRACKED (BS 621) · airframe 8,839 hrs · 7,174 cycles

FS 621 ANGLE IS CRACKED .5 INCH RIGHT SIDE FLOOR SUPPORT. REPAIR TO FLOOR SUPPORT ANGLE FS 621 IAW REO 601R-53-61-117. WORK C/W IAW REO 601R-53-61-117. (B)

Part: INTERCOSTAL — CRACKED (BS 621-625) · airframe 8,839 hrs · 7,174 cycles

LT INTERCOSTAL CRACKED, FS 621.0-625.0 IN RADIUS APPROX 1 INCH IN LENGTH. REMOVED CRACKED ANGLE AND INSTALLED NEW SERVICEABLE PART IAW SRM 31-42-08. (B)

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 8,450 hrs · 6,821 cycles

FLAPS FAIL MSG WHEN RETRACTING FROM 8 TO 0 AFTER TAKEOFF. F/CTL PAGE SHOWED ZERO DEGREES ON BOTH SIDES BUT RECEIVED FLAP OVERSPEED AURAL WARNING ABOVE 230 KTS ZERO FLAP LANDING IN ATL, VERTICAL SPEED AT TOUCHDOWN 100 FPM. EMERGENCY DECLARED.

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 6,723 hrs · 5,410 cycles

EMERGENCY LIGHTS -OFF- LIGHT HAS A LIGHT BULB INOP INSIDE COCKPIT.

Part: STEP — CRACKED (ASD) · airframe 5,905 hrs · 4,789 cycles

ASD BOTTOM STEP CRACKED.

Part: WARNING MESSAGE — ILLUMINATED (ANTI SKID SYS) · airframe 4,803 hrs · 3,965 cycles

AT GEAR RETRACTION GOT I/B ANTI SKID MSG, MLG DISAGREE MSG STAB/MACH TRIM DISCONNECT AND PROX SYSTEM STATUS MSG. ALL MESSAGES CLEARED AFTER RUNNING QRH FOR GEAR DISAGREE. A/C RETURNED TO DAB AFTER T/O, EMERGENCY DECLARED.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 4,021 hrs · 3,370 cycles

ANTI ICE DUCT MSG. FOLLOWED QRH MSG CLEARED, MSG REAPPEARED WITH WING ANTI-ICE SELECTED OFF AND 14TH STAGE VLV CLOSED. ENROUTE TO ATL A/C DIVERTED TO TRI DUE TO MTC. AN EMERGENCY WAS DECLARED.

Part: FRAME — CRACKED (BS 718) · airframe 4,001 hrs · 3,353 cycles

FOUND LEFT SIDE FS 718 FRAME CRACKED (MARKED).

Part: PLACARD — DAMAGED (CABIN) · airframe 4,001 hrs · 3,353 cycles

FOUND EXIT PLACARDS DAMAGED BY LT OVERWING EXIT.