N930EV

Part: A/C PACK — FAULTED (ZONE 100) · airframe 38,790 hrs · 36,999 cycles

DURING CLIMB IN DEN LEFT PACK DID NOT COME ON AND WE GOT CABIN ALT CAUTION AND FOLLOWED WITH CBAIN ALT WARNING. (FLIGHT 5024 - FILED OPEN) REF AML 1502615 FOR LH PACK DEFERRAL AND AML 1502517 FOR PASSENGER O2 MASKS DEPLOYED CORRECTIVE ACTION.

Part: A/C PACK — WARNING MESSAGE (ZONE 100) · airframe 38,790 hrs · 36,999 cycles

DURING CLIMB IN DEN LEFT PACK DID NOT COME ON AND WE GOT CABIN ALT CAUTION AND FOLLOWED WITH CBAIN ALT WARNING. (FLIGHT 5024 - FILED CLOSED) REF AML 1502615 FOR LH PACK DEFERRAL AND AML 1502517 FOR PASSENGER O2 MASKS DEPLOYED CORRECTIVE ACTION.

Part: FLOOR SUPPORT — CORRODED · airframe 37,722 hrs · 35,890 cycles

RH PRESS FLOOR ANGLE FROM FS 501-FS 509 HAS SIGNS OF CORROSION (C-CHECK RO 5/13/2024) REPAIRED CORROSION DAMAGE AT FS 501-509 RH FLOOR SILL ANGLE IAW REO 601R-53-41-666 REV-C DATE 2012-11-06, CRJ200 SRM 51-12-00, SRM 51-25-06, AND SRM 51-25-16. NDT PERFORMED BY BARON NDT LLC, FAA CRS# 5NDR545D, REPORT# S032124-1, P.O.# 171407, DATE OF INSPECTION 21 MAR 2024, SEE REPORT FOR DETAILS.

Part: RIVET — WORN · airframe 37,722 hrs · 35,890 cycles

LH MLG DOOR FWD SIDE HAS EXCESSIVE WEAR, EVALUATE (C-CHECK RO 5/13/2024) REPAIRED L/H MLG DOOR FWD SIDE IAW REO 601R-52-82-102 AND CRJ200 SRM 51-42-06 AND CRJ200 SRM 52-82-00 CRJ200 SRM, 51-25-06 AND CRJ200 SRM 51-40-11 AND CRJ200 SRM 51-24-36 AND CRJ200 SRM 51-25-16 CRJ200 SRM 51-21-11. ET WORK COMPLETED BY BARON NDT, LLC, FAA CRS# 5NDR545D, REPORT # S032824-5, PO NUMBER 171407, DATE OF INSPECTION 28 MAR 2024.CALIBRATED TOOLS USED: DIGITAL CALIPERS: AV-7805 . CAL DUE DATE:JAN25 SCALE AV4800 DUE DEC 2024

Part: RIVET — DAMAGED · airframe 37,722 hrs · 35,890 cycles

NUTPLATE FASTENER HOLE ON STRAP AND UNDERLYING MATING SUB STRUCTURE AT FS 559.00 STR 17L FOUND TO HAVE OBLONG CONDITION (C-CHECK RO 5/13/2024) REPAIRED AND FABRICATED CONICAL WASHER P/N: 601R-53-41-3232 ON SUB STRUCTURE AT F.S 559.00 STR 17 LH IAW MHIRJ REO 601R-53-41-3232 REV-A ;DATE: 2024-04-10 AND IAW CRJ 200 SRM 53-00-00, SRM 53-41-45 AND CRJ 200 AMM 21-32-00. NDT PERFORMED BY BARON NDT LLC CRS# 5NDR545D REPORT: S040824-1. SEE REPORT FOR DETAILS.CAL TOOLS DIGITAL CALIPER ID: AV7803 CAL DUE: JAN-2025

Part: UNKNOWN — CORRODED · airframe 37,722 hrs · 35,890 cycles

SIGNS OF CORROSION AT RH PRESS SILL FS515 (C-CHECK RO 5/13/2024) REMOVED CORROSION ON RH PRESS SILL FS515 IAW REO 601R-53-41-666. REV. -C. DATE: 2012-11-06. NDT PERFORMED BY BARON NDT, LLC, FAA CRS# 5NDR545D. REPORT # S031324-13. AND CRJ-200 SRM 51-21-06, SRM 51-21-11, SRM 51-25-06, SRM 51-25-16. CAL TOOL CALIPER CAL DUE JAN 2025

Part: SUPPORT — CORRODED · airframe 37,722 hrs · 35,890 cycles

SIGNS OF CORROSION AT RH PRESS SILL FS501 (C-CHECK RO 5/13/2024) REPAIRED CORROSION DAMAGE AT FS 501 RH FLOOR SILL PANEL IAW REO 601R-53-41-666 REV-C DATE 2012-11-06 CRJ200 SRM 51-25-06, AND SRM 51-25-16, SRM 51-21-11, SRM 51-21-06. NDT PERFORMED BY BARON NDT LLC, FAA CRS# 5NDR545D, REPORT# S031424-2, P.O.#171407, DATE OF INSPECTION 14 MAR 2024 SEE REPORT FOR DETAILS.

Part: LOCK FASTENER — CORRODED · airframe 37,722 hrs · 35,890 cycles

SIGNS OF CORROSION ADN MISSING PAINT UNDER PRESSURE FLOOR PANEL LH SIDE IN AND/OR AROUND FASTENERS FS451BLENDED OUT CORROSION UNDER PRESSURE FLOOR PANEL AT FS451. BLENDS PERFORMED ARE WITHIN LIMITS. TREAETED, PRIMED, AND APPLIED TOPCOAT TO REPAIR AREA IAW BOMBARDIER REO 601R-53-41-666 REV-C 2012-11-06, CRJ200 SRM 51-45-00, 51-42-21, 51-21-11,51-25-06, 51-25-16. NDT PERFORMED BY BARON NDT, LLC FAA CRS# 5NDR545D REPORT# S022624-3 P.O# 171069 DATE OF INSPECTION: 26FEB2024 OK JC910589

Part: UNKNOWN — CORRODED · airframe 37,722 hrs · 35,890 cycles

SIGNS OF CORROSION ON MULTIPLE FASTENERS UNDER FLOOR PANEL RH SIDE IN AND/OR AROUND FASTENERS AT FS428 (C-CHECK RO 5/13/2024) REPAIRED CORROSION DAMAGE @ FS 428.00 R/H FLOOR SILL PANEL NUT PLATE IAW REO 601R53-41-666 REV-C DATE: 2012-11-06. NDT PERFORMED BY BARON NDT, LLC, FAA. CRS# 5NDR545D REPORT # S030124-12 P.O. # 171069 DATED: 01 MAR 2024. SEE REPORT FOR DETAILS. CRJ 200 SRM 51-21-11, 51-25-06, 51-25-16 ALSO UTILIZED FOR REPAIR.

Part: NUT — CORRODED · airframe 37,722 hrs · 35,890 cycles

SIGNS OF CORROSION AND MISSING PAINTUNDER PRESSURE FLOOR PANEL SH SIDE IN AND/OR AROUND FASTENERS FS457 (C-CHECK RO 5/13/2024) REMOVED CORROSION UNDER PRESSURE FLOOR PANEL, LEFT SIDE F.S. 457. FOUND TO BE WITHIN LIMITS IAW BOMBARIDIER REO 601R-53-41-666 REV.C DATED 2012-11-06. CRJ200 SRM 51-21-11, SRM 51-25-16. SRM 51-25-06, SRM 51-42-06, SRM 51-45-00, AMM 51-23-00, NDT PERFORMED BY BARON NDT, LLC, FAA CRS #5NDR545D REPORT #S030124-17, P.O. #171069 DATED: 01-MAR-2024 AND IAW CRJ 200 AMM 21-31-00

Part: UNKNOWN — CORRODED · airframe 37,722 hrs · 35,890 cycles

SIGNS OF CORROSION ON MULTIPLE FASTENERS UNDER FLOOR PANEL RH SIDE IN AND/OR AROUND FASTENERS FS457 (C-CHECK RO 5/13/2024) REPAIRED CORROSION DAMAGE AT FS 457 RH FLOOR SILL PANEL AROUND. NDT PERFORMED BY BARON NDT LLC, FAA CRS# 5NDR545D REPORT # S030124-11, P.O. # 171069 DATED 01 MAR 2024 SEE REPORT FOR DETAIL. ALL IAW REO 601R-53-41-666 REC-C DATE 2012-11-06, SRM 51-12-00, SRM 51-25-06, SRM 51-25-16CAL TOOL - DEPTH GAUGE- AV7277, CAL DUE-07 AUG 24

Part: UNKNOWN — DAMAGED · airframe 37,722 hrs · 35,890 cycles

DAMAGED FASTENER HOLE AT FS559.00+5 LBL27 (C-CHECK RO 5/13/2024) PERFORMED REPAIR ON FS 559.00+5 LBL27 PER REO 60IR-53-41-3228. REV. -- DATE: 2024-04-08, REO 60IR-53-41-3228. REV--(P1) DATE: 2024-04-01 AND CRJ-200 SRM 53-00-00. CRJ-200 SRM 51-45-00. CRJ-200 SRM 51-40-11. CRJ-200 AMM 20-10-00. NDT PERFORMED BY BARON NDT, LLC, FAA CRS# 5NDR545D. REPORT # S040824-2. CALIBRATED TOOL USED: SCALE AV-4800 CAL DUE DEC 2024

Part: UNKNOWN — CHAFED · airframe 37,722 hrs · 35,890 cycles

DURING THE AUDIT OF 1C TASK CARD 53-280-300, INTERNAL ZONAL INSPECTION OF THE CARGO COMPARTMENT, IT WAS NOTED THAT THERE IS EVIDENCE OF MULTIPLE FASTENER CHAFES/CONTACT ON THE FWD SIDE OF THE FS 621 BULKHEAD. PLEASE INVESTIGATE AND REPAIR AS REQUIRED. (C-CHECK RO 5/13/2024) PERFORMED REPAIR ON FS 621 FWD SIDE BULKHEAD PER REO 601R-53-61-8181. REV. --. DATE: 2024-04-01. NDT PERFORMED BY BARON NDT, LLC, FAA CRS# 5NDR545D. REPORT # S040124-2. CRJ-200 SRM 57-71-19 AND CRJ-200 SRM 51-42-06. CALL TOOLS AV-7277 CAL AUG 2024, AV-7806 CAL AUG 2024

Part: VANE — CHAFED (TE FLAP) · airframe 37,722 hrs · 35,890 cycles

R/H I/B FLAP VANE EXISTING REPAIR IN MIDDLE CHAFFED (C-CHECK RO 5/13/2024) REPAIRED R/H I/B FLAP VANE SKIN IAW CRJ200 SRM 57-52-00,57-52-00 REPAIR #1,51-21-11,51-25-06 AND 51-25-16 AMM 27-54-10.CALIBRATED TOOLS USED: DEPTH GUAGE AV-7277 CAL DUE: AUG 2024, SCALE AV8473 CAL DUE: AUG 2024

Part: UNKNOWN — WARNING MESSAGE (UNKNOWN) · airframe 37,198 hrs · 35,325 cycles

ON DEPARTURE WHILE SELECTING THE GEAR UP WE RECEIVED STEERING INOP (C) MSG. FOLLOWING THAT MSG WE GOT A GEAR DISAGREE (W) MSG AND A NOSE DOOR (W) MSG. NOSE DOOR (W) MSG WENT AWAY ON ITS OWN. NOSE GEAR WAS SHOWING DOWN ON EICAS WHEN THE HANDLE WAS IN THE UP POSITION. COMPLIED WITH QRH AND IT CLEARED THE MSG AND THE GEAR WENT UP. AFTER COMPLETING QRH, PERFORMED THE QRH FOR STEERING INOP AND IT CLEARED THE STEERING MSG. NO FURTHER ISSUES AFTER BOTH QRH WAS C/W. DID NOT LAND OVERWEIGHTDID NOT DECLARE EMERGENCY (FLIGHT 5375 FILED OPEN)

Part: UNKNOWN — WARNING MESSAGE (UNKNOWN) · airframe 37,198 hrs · 35,325 cycles

ON DEPARTURE WHILE SELECTING THE GEAR UP WE RECEIVED STEERING INOP (C) MSG. FOLLOWING THAT MSG WE GOT A GEAR DISAGREE (W) MSG AND A NOSE DOOR (W) MSG. NOSE DOOR (W) MSG WENT AWAY ON ITS OWN. NOSE GEAR WAS SHOWING DOWN ON EICAS WHEN THE HANDLE WAS IN THE UP POSITION. COMPLIED WITH QRH AND IT CLEARED THE MSG AND THE GEAR WENT UP. AFTER COMPLETING QRH, PERFORMED THE QRH FOR STEERING INOP AND IT CLEARED THE STEERING MSG. NO FURTHER ISSUES AFTER BOTH QRH WAS C/W. DID NOT LAND OVERWEIGHTDID NOT DECLARE EMERGENCY (FLIGHT 5375 FILED CLOSED)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 36,583 hrs · 34,737 cycles

OVERSPED LANDING GEAR DURING RETRACTION ON GO-AROUND AT APPROX 220 KIAS. NOSE GEAR DID NOT INDICATE UP. ONCE BELOW 200 THE NOSE GEAR RETRACTED AND ALL GEAR INDICATED UP. TURNED HYD PUMPS 3B AND 2 ON PER QRH. GEAR LOWERED NORMALLY, INDICATED DN, AND NORMAL LANDING MADE. (FLT 5603 FILED CLOSED) PLEASE REFERENCE AML 1141900 PERFORMED AN OVERSPEED CONDITION INSPECTION BY COMPLYING WITH APPLICABLE STEPS OF THE AMM 05-51-04. NO DISCREPANCIES WERE FOUND AT THIS TIME.

Part: NONE — FAULTY · airframe 35,494 hrs · 33,740 cycles

L EMER DOOR CAUTION MESSAGE CONTINUOUSLY CAME ON, NO PRESSURIZATION ISSUE AND HAD GREEN DOOR INDICATOR (FLIGHT #6971 FILED CLOSED) THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 25375145 WITH THE FOLLOWING CORRECTIVE ACTION: "LEFT OVERWING EMERGENCY EXIT DOOR AND INDIACTION OPS CHECK GOOD AT THIS TIME REFERENCING AMM 52-21-00 AND AMM 52-70-10. OK FOR SERVICE."

Part: STIFFENER — CRACKED (ZONE 100) · airframe 33,184 hrs · 31,672 cycles

UPON ACCESS FOR BELL CRANK REPAIR FOUND UPPER STIFFENER AT WS 00 IN MLG WHEEL WELL TO BE CRACKED (C-CHECK RO 4/1/2021) UPPER STIFFENER LISTED IN DISCREPANCY IS LOCATED AT W.S. 48.30. REMOVED AND REPLACED UPPER STIFFENER IN R/H MLG WHEEL WELL, W.S. 48.30 I.A.W. BOMBARDIER CRJ200 SRM 51-42-21 REV.38B, DATED 11/25/2020. REFERENCE CONTINUATION CARD FOR WORK PERFORMED. COMPLETED SKYWEST FORM M-337 AND M131. SKYWEST TASK CARD 51-900-1003-SKY COMPLIED WITH. WEIGHT AND BALANCE NOT AFFECTED.

Part: BELLCRANK — ABNORMAL (LT MLG) · airframe 33,184 hrs · 31,672 cycles

UPON INITIAL GEAR SWING LH BELLCRANK WAS CLOCKED INCORRECTLY CAUSING DAMAGE TO BELLCRANK AND SURROUNDING STRUCTURE (C-CHECK RO 4/1/2021) REPAIRED BELLCRANK AND SURROUNDING STRUCTURE IAW MHIRJ REO 601R-53-41-2887 REV -- DATED 2021-03-29. REFERENCE CONTINUATION CARD FOR WORK PERFORMED. ATTACHED TASK CARD 51-900-1003-SKY AND M-337 WITH NEGLIGABLE WEIGHT CHANGE AT 0.25 POUNDS ADDED.

Part: BELLCRANK — ABNORMAL (MLG) · airframe 33,184 hrs · 31,672 cycles

UPON INITIAL GEAR SWING LH AND RH BELLCRANKS WERE CLOCKED INCORRECTLY CAUSING THE BELLCRANKS TO BREAK AND SURROUNDING STRUCTURAL DAMAGE (C-CHECK RO 4/1/2021) REPAIRED LH & RH BELLCRANK AND SURROUNDING STRUCTURE IAW MHIRJ REO 601R-53-41-2888 REV -- DATED 2021-03-29. REFERENCE CONTINUATION CARD FOR WORK PERFORMED TASK CARD 51-900-1003-SKY AND M-337 ATTACH WEIGHT CHANGE IS NEGLIGABLE AT 0.75 POUNDS

Part: FAIRING — CHAFED (LEFT) · airframe 33,184 hrs · 31,672 cycles

L/H STUB FAIRING HAS CHAFING DAMAMGE AND INTERNAL BRACKET IS ALLOWING MOVEMENT. (C-CHECK RO 4/1/2021) INSTALLED NEW HARDWARE ON L/H STUB FAIRING TO CORRECT THE INTERNAL BRACKET AND LET THE STUB FAIRING FUNCTION CORRECTLY IAW CRJ 200 AMM 53-82-01-400-808. REF CONTINUATION CARD FOR DETAILS AND WORK PERFORMED.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 33,184 hrs · 31,672 cycles

LBL 9 FLOOR BEAM CAP HAS SEVERAL AREAS OF CORROSION BETWEEN F.S. 409.00 AND 409.00+128. (C-CHECK RO 4/1/2021) REPAIRED LBL 9 FLOOR BEAM CAP CORROSION BETWEEN F.S. 409.00 AND 409.00+128 IAW CRJ 200 SRM 53-00-43 AND REO 601R-53-31-1184 REV.-- DATED 2021-03-10. FORM 337 AND MAJOR REPAIR TASK CARD 51-900-1003-SKY COMPLETED AND ATTACHED. NO WEIGHT CHANGE, SEE ATTACHED CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.

Part: NUT — CORRODED (RT WING) · airframe 33,184 hrs · 31,672 cycles

RH WING HINGE BOX ATTACHING HARDWARE NUTS FWD AND AFT AT WS 178, WS 220, AND WS 264 ARE CORRODED/ RUSTED AND REQUIRE REPLACEMENT. (C-CHECK RO 4/1/2021) REMOVED AND INSTALLED SERVICEABLE HARDWARE ON R/H FLAP HINGE BOX WS 178.00,WS 220.00AND WS 264.00 IAW CRJ 200 AMM 57-21-35-000-801/802/AND 803.INSTALL 57-21-35-400-801,802 AND 803.

Part: NUT — CORRODED (LT WING HINGE) · airframe 33,184 hrs · 31,672 cycles

LH AFT HINGE BOX NUTS AT WS 264, FWD HINGE BOX NUT AT WS 220, AND FWD AND AFT HINGE BOX NUTS AT WS 178 ARE CORRODED/RUSTED AND REQUIRE REPLACMENT. (C-CHECK RO 4/1/2021) REMOVED AND REPLACED LH AFT HINGE BOX NUTS AT WS 264, FWD HINGE BOX NUT AT WS 220, AND FWD AND AFT HINGE BOX NUTS AT WS 178 IAW CRJ 200 AMM'S 57-21-35-000/400-801,802,803 REFERENCE CONTINUATION CARD FOR WORK PERFORMED

Part: TRUNNION — DAMAGED (RT MLG) · airframe 33,184 hrs · 31,672 cycles

R/H TRUNNION AFT HOLE IN STRAP IS OVERSIZED. (C-CHECK RO 4/1/2021) REPAIRED RIGHT HAND MLG TRUNNION AFT HOLE LOCATION (#16) IAW MHIRJ REO 601R-57-21-3428, REV -- DATED 2021-02-26. SEE CONTINUE CARD FOR DETAILS OF WORK PERFORMED. FORM 337 AND MAJOR REPAIR TASK CARD 51-900-1003-SKY COMPLETED AND ATTACHED. REFERENCE CONTINUE CARD FOR WORK PERFORMED. NO WEIGHT CHANGE NOTED.

Part: TRUNNION — DAMAGED (LT MLG) · airframe 33,184 hrs · 31,672 cycles

L/H TRUNNION AFT HOLE IN STRAP IS OVERSIZED (C-CHECK RO 4/1/2021) REPAIRED LEFT HAND TRUNNION AFT HOLE IN STRAP (#14) IAW MHIRJ REO 601R-57-21-3427, REV -- DATED 2021-02-26. REFERENCE CONTINUE CARD FOR WORK PERFORMED. FORM 337 AND MAJOR REPAIR TASK CARD 51-900-1003-SKY COMPLETED AND ATTCHED. NO WEIGHT CHANGE NOTED.

Part: TRUNNION — FAILED (RT MLG) · airframe 33,184 hrs · 31,672 cycles

RH MLG TRUNNION FASTENER HOLE #7 HAS AN INDICATION .1" LONG BY 40% FSH. FAILED NDT INSPECTION(REFERENCE NDT REPORT & ATTACHMENTS FOR LOCATION). (C-CHECK RO 4/1/2021) REPAIRED RIGHT HAND MLG TRUNNION FASTENER HOLE #14 IAW MHIRJ REO 601R-57-21-3428, REV -- DATED 2021-02-26. FORM 337 AND MAJOR REPAIR TASKCARD 51-900-1003-SKY COMPLETED AND ATTACHED. NO WEIGHT CHANGE, SEE CONTINUE CARD FOR WORK PERFORMED.

Part: TRUNNION — CRACKED (LT MLG) · airframe 33,184 hrs · 31,672 cycles

LH MLG TRUNNION FASTENER HOLES AS FOLLOWS EACH HAS INDICATIONS ,1" LONG AND 45% FSH IN LOCATION #4, AND 65% FSH IN LOCATIONS #8, & #13. FAILED NDT INSPECTION. (REFERENCE NDT REPORT & ATTACHMENTS FOR LOCATION). (C-CHECK RO 4/1/2021) REPAIRED LEFT HAND TRUNNION FASTENER HOLE LOCATIONS #8,#15 AND #19 IAW MHIRJ REO 601R-57-21-3427. FORM 337 AND MAJOR REPAIR TASKCARD 51-900-1003-SKY COMPLETED AND ATTACHED. NO WEIGHT CHANGE. REFERENCE CONTINUE CARD FOR DETAILS OF WORK PERFORMED.

Part: NUT — CORRODED (RT AILERON) · airframe 33,184 hrs · 31,672 cycles

RH AILERON HINGE #4 ANIT ROTATION PLATE NUT AND WASHER CORRODED. (C-CHECK RO 4/1/2021) REMOVED AND INSTALLED NEW SERVICEABLE NUT AND WASHER ON R/H AILERON HINGE #4 ANTI ROTATION PLATE IAW CRJ 200 AMM 20-21-00-910-801.

Part: ANCHOR FITTING — CORRODED (PAX DOOR) · airframe 33,184 hrs · 31,672 cycles

PAX DOOR AFT ANCHOR FITTING IS CORRODED IN (2) LOCATIONS AND IS CRACKED ON THE AFT SIDE. (C-CHECK RO 4/1/2021) INSTALLED SERICABLE PAX DOOR ANCHR FITTING AND STOP PLATE COVER I.A.W. CRJ-200 AMM TASK 52-11-17-400-804

Part: PLATE — CORRODED (PAX DOOR) · airframe 33,184 hrs · 31,672 cycles

PAX DOOR FORWARD ANCHOR FITTING SERATED PLATE IS CORRODED. (C-CHECK RO 4/1/2021) INSTALLED SERICABLE PAX DOOR ANCHOR FITTING I.A.W. CRJ-200 AMM TASK 52-11-17-400-804

Part: SPLICE ANGLE — CRACKED (FUSELAGE) · airframe 33,184 hrs · 31,672 cycles

STRINGER 3L IS CRACKED AT F.S. 280.00. (C-CHECK RO 4/1/2021) ON INVESTIGATION FOUND NO DAMAGE TO THE STRINGER 3L. FOUND SPLICE ANGLES INBOARD AND OUTBOARD TO BE CRACKED. REMOVED AND REPLACED SPLICE ANGLES IAW CRJ 200 SRM 51-42-21 AND 51-42-06. NO CHANGE TO WEIGHT, SKYCARD 51-900-1003-SKY AND M-337 ATTACHED.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 33,184 hrs · 31,672 cycles

L/H PRESSURE FLOOR SILL IS CORRODED AROUND (1) FASTENER, LOCATED (2) FASTENERS OUTBOARD OF BLEND #18 AS CALLED OUT IN REO 601R-53-41-2442 REV.--, DATED 2019-02-18. (C-CHECK RO 4/1/2021) BLENDED OUT CORROSION ON L/H PRESSURE SILL AROUND 1 FASTNER LOCATED 2 FASTENERS OUTBOARD OF BLEND #18 APPROX. F.S. 409+128.00, LBL 42 IAW BOMBARDIER REO 601R-53-41-666 REV-C DATED 2012-11-06. FORM 337 AND MAJOR REPAIR TASKCARD 51-900-1003-SKY COMPLETED AND ATTACHED. NO WEIGHT CHANGE, SEE CONTINUATION FOR WORK PERFORMED

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 33,184 hrs · 31,672 cycles

L/H PRESSURE FLOOR SILL IS CORRODED AROUND (1) FASTENER LOCATED FORWARD OF THE FASTENER CALLED OUT AT LOCATION #12 OF REO 601R-53-41-2442 REV.--, DATED 2019-02-18. (C-CHECK RO 4/1/2021) REPAIRED IAW REO 601R-53-41-666 REV C DATED 11/6/2012 DISPOSITION 1.2 AND REO 601R-53-41-2442 REV-- DATED 2019-02-18. REFERENCE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED. FORM 337 AND MAJOR REPAIR TASK CARD 51-900-1003-SKY COMPLETED AND ATTACHED. NO WEIGHT CHANGE NOTED

Part: PLATE — CORRODED (PAX DOOR) · airframe 33,184 hrs · 31,672 cycles

PAX DOOR AFT ANCHOR FITTING SERATED PLATE IS CORRODED. (C-CHECK RO 4/1/2021) REMOVED AND REPLACED PAX DOOR AFT ANCHOR FITTING SERATED PLATE WITH SERVICABLE P/N: 600-38061-6 I.A.W CRJ-200 AMM TASK 52-11-17-400-804.

Part: SEAT TRACK — DAMAGED (CABIN) · airframe 33,184 hrs · 31,672 cycles

LH CABIN FLOOR SEAT RAIL AT LBL9 BETWEEN F.S. 409.00+64 AND F.S. 409.00+128 REQUIRES FABRICATION. (C-CHECK RO 4/1/2021) FABRICATED, LOCATED AND DRILLED SEAT TRACK ON LH CABIN FLOOR AT LBL9 BETWEEN FS 409+64 AND FS 409+128 IAW: CRJ200-SRM-51-40-11

Part: ATTACH BOLT — CORRODED (RT WING TE FLAP) · airframe 33,184 hrs · 31,672 cycles

RH WING VANE PANEL 695BB BOLT KEEPER ATTACH BOLTS ARE CORRODED (C-CHECK RO 4/1/2021) REMOVED AND REPLACED RH WING VANE PANEL 695BB BOLT KEEPER ATTACH BOLTS (4 BOLTS) IAW CRJ 200 AMM 27-54-05-000/400-801.

Part: NUT — CORRODED (LT WING TE FLAP) · airframe 33,184 hrs · 31,672 cycles

LH WING VANE PANEL 595BB LH OUTBOARD ATTACH NUT IS CORRODED (C-CHECK RO 4/1/2021) REMOVED AND REPLACED LH WING VANE PANEL 595BB LH OUTBOARD ATTACH NUT FROM HINGE BOX ASSEMBLY AT W.S220.00 IAW CRJ200 AMM REF: 57-21-35-000-802 AND 57-21-35-400-802. TORQUE WRENCH P/N: WVACT374, S/N: 4030657807, CALIBRATION DATE: 07/15/2020, DUE DATE: 07/30/2021.

Part: ATTACH BOLT — CORRODED (INDICATOR) · airframe 33,184 hrs · 31,672 cycles

LH WING AILERON POSITION INDICATOR UNDER PANEL 598BB HAS ATTACH HARDWARE IS CORRODED (C-CHECK RO 4/1/2021) REMOVED AND REPLACED HARDWARE ON LH WING AILERON POSITION INDICATOR UNDER PANEL 598BB AS REQUIRED IAW CRJ 200 AMM 27-15-15-000/400-801. REFFERENCE ATTACHED CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.

Part: ATTACH BOLT — CORRODED (RT WING SPOILER) · airframe 33,184 hrs · 31,672 cycles

RH WING MULTI-FUNCTIONAL SPOILER INBOARD / OUTBOARD ACTUATORS LOWER ATTACH HARDWARE IS CORRODED (C-CHECK RO 4/1/2021) REMOVED AND REPLACED RH WING MULTI-FUNCTIONAL SPOILER INBOARD/ OUTBOARD ACTUATOR'S LOWER ATTACH HARDWARE IAW CRJ 200 AMM 27-62-01-000/400-801.OPS CHECK THE RH MULTI-FUNCTION SPOILER IB/OB ACTUATOR IAW CRJ 200 AMM 27-64-00-710-801. SEE CONTINUATION CARD FOR WORK COMPLETED.

Part: SEAT TRACK — CORRODED (RT CABIN) · airframe 33,184 hrs · 31,672 cycles

RH CABIN SIDE SEAT RAILS ARE CORRODED BETWEEN F.S. 424.00 AND F.S. 559.00+32. (C-CHECK RO 4/1/2021) REMOVED AND REPLACED WITH NEW R/H CABIN SIDE SEAT RAILS BETWEEN FS 424 AND FS 559.00+32 IAW CRJ 200 AMM 53-01-11-400-802

Part: POST — CRACKED (FUSELAGE) · airframe 33,184 hrs · 31,672 cycles

FUSELAGE FS409+128 VERTICAL POST AT BL0 HAS AN INDICATION .2" LONG BY 80% FSH IN THE AFT RADIUS OF BOTH THE RH & LH SIDES @WL69. FAILED NDT INSPECTION. (C-CHECK RO 4/1/2021) FUSELAGE FS409+128 VERTICAL POST AT BL0 WAS REMOVED AND A NEW POST INSTALLED IAW REO 601R-53-41-889 REV D. WITH NO WEIGHT CHANGE. TASK CARD 51-900-1003-SKY AND M-337 ATTATCHED

Part: SEAT TRACK — CORRODED (RT CABIN) · airframe 33,184 hrs · 31,672 cycles

RH CABIN FLOOR SEAT RAIL AT RBL9 IS CORRODED BETWEEN F.S. 409.00+96 AND F.S. 409.00+112. (C-CHECK RO 4/1/2021) REMOVED AND REPLACED R/H CABIN FLOOR SEAT RAIL AT RBL 9 BETWEEN F.S. 399 AND 409+126 IAW CRJ200 AMM 53-01-11-000-802 AND 53-01-11-400-802. REFER TO CAMP 22328672 FOR PART FABRICATION

Part: POST — CRACKED (FUSELAGE) · airframe 33,184 hrs · 31,672 cycles

FUSELAGE FS409+128 VERTICAL POST AT RBL18 HAS AN INDICATION .2" LONG BY 60% FSH IN THE AFT RADIUS OF THE INBD SIDE @ WL69. FAILED NDT INSPECTION. (C-CHECK RO 4/1/2021) REMOVED AND INSTALLED NEW SERVICEABLE VERTICAL POST AT RBL 18 IAW REO 601R-53-41-889 REV D DATED 2018-10-04. FORM 337 AND MAJOR REPAIR TASK CARD COMPLETED AND ATTACHED. WEIGHT CHANGE NEGLIGIBLE . REFERENCE CONTINUE CARD FOR DETAILS.

Part: SEAT TRACK — CORRODED (LT CABIN) · airframe 33,184 hrs · 31,672 cycles

LH CABIN FLOOR SEAT RAIL AT LBL9 IS CORRODED BETWEEN F.S. 409.00+64 AND F.S. 409.00+128. (C-CHECK RO 4/1/2021) INSTALLED SERVICEABLE LH CABIN FLOOR SEAT RAIL AT LBL 9 BETWEEN FS409.00+64 AND FS409.00+128 IAW CRJ 200 AMM 53-01-11-400-802

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 33,184 hrs · 31,672 cycles

APU INLET DOOR ACTUATOR INTERCOSTAL AT F.S. 654.50 STGR 4L IS CRACKED AT BOTTOM FWD CORNER. (C-CHECK RO 4/1/2021) REPAIRED DAMAGE ON THE APU INLET DOOR ACTUATOR INTERCOSTAL AT F.S. 654.50 STGR 4L IAW MHIRJ REO 601R-53-62-300 REV -- DATED 2021-02-23. REFERENCE CONTINUATION FOR WORK PERFORMED.

Part: RETAINER — CORRODED (ESCAPE HATCH) · airframe 33,184 hrs · 31,672 cycles

CREW ESCAPE HATCH SEAL RETAINER ATTACHING HARDWARE IS CORRODED AT 10EA. LOCATIONS. (MARKED WITH RED GREASE PENCIL) (C-CHECK RO 4/1/2021) REMOVED AND REPLACED CREW ESCAPE HATCH RETAINER HARDWARE IAW CRJ 200 AMM 52-22-07-000/400-802

Part: HANDLE — GOUGED (AFT CARGO DOOR) · airframe 33,184 hrs · 31,672 cycles

AFT CARGO DOOR OUTER HANDLE IS GOUGED AT (4EA) LOCATIONS. (C-CHECK RO 4/1/2021) REMOVED DAMAGED DOOR HANDLE ASSEMBLY AND INSTALLED A NEW ASSEMBLY IAW CRJ 200 SRM 51-42-21. OPERATIONAL CHECKS AND PRESSURE CHECKS ARE GOOD. TASK CARD 51-900-1003-SKY AND M-337 ATTACHED WITH NO CHANGE TO WEIGHT

Part: RETAINER — CORRODED (E/E BAY DOOR) · airframe 33,184 hrs · 31,672 cycles

MAIN AVIONICS DOOR SEAL RETAINER IS CORRODED AROUND ENTIRE DOOR. (C-CHECK RO 4/1/2021) REMOVED AND REPLACED MAIN AVIONICS SEAL RETAINER IAW CRJ 200 SRM 51-42-06 REFERENCE CONTINUATION CARD FOR WORK PERFORMED

Part: RETAINER — DAMAGED (AFT CARGO DOOR) · airframe 33,184 hrs · 31,672 cycles

AFT CARGO DOOR SEAL RETAINER IS DAMAGED AT THE LOWER AFT CORNER. (C-CHECK RO 4/1/2021) REMOVED DAMAGED SEAL RETAINER AND INSTALLED ANEW SERVICABLE SEAL RETAINER IAW CRJ 200 SRM 51-42-06. NO CHANGE TO WEIGHT. PRESSURE CHECK AND OPERATIONAL CHECKS GOOD. TASK CARD 51-900-1003-SKY AND M-337 ARE ATTACHED

Part: BEAM — CORRODED (SERVICE DOOR) · airframe 33,184 hrs · 31,672 cycles

COMPLY WITH SCHEDULED MAINTENANCE CODE: RA47138-601R-52-41-244 N930EV -PR - BLENDED CORROSION ON LWR AFT PAN OF SERVICE DOOR REF REO 601R-52-41-244 REV -- DATED 2016-12-27. PERFORM PERM REPAIR WITHIN 14000 FH FROM TIME OF INCORPORATION OF REV --, PART NUMBER: 601R38302-91 - DOOR ASSY, SRVC/EMER EXIT, SERIAL NUMBER: 8014, POSITION: ONLY (C-CHECK RO 4/1/2021) PERMANENT REPAIR WAS ACCOMPLISHED BY REMOVING DAMAGED LOWER AFT CORNER PAN AND INSTALLING A NEW LOWER AFT CORNER IAW CRJ 200 SRM 51-42-06, 51-42-13, AND 51-41-02. NO CHANGE TO WEIGHT, TASK CARD 51-900-1003-SKY AND M-337 ATTACHED

Part: BUSHING — NOT REPORTED (LT AILERON) · airframe 33,184 hrs · 31,672 cycles

REMOVE AND REPLACE BUSHINGS AND HARDWARE ON LH AILERON WING AFT SPAR REF CRJ 200 AMM 20-26-00-910-804 (C-CHECK RO 4/1/2021) REMOVED AND REPLACED BUSHINGS AND HARDWARE ON LH AILERON WING AFT SPAR REF CRJ 200 AMM 20-26-00-910-804 & REO_601R-57-51-941 REV.-- DATED 2021-03-12. SEE ATTACHED CONTINUATION CARD FOR WORK PERFORMED.

Part: BRACKET — DAMAGED (CENTERING SENSOR) · airframe 31,312 hrs · 29,961 cycles

GEAR DISAGREE. NOSE WHEEL DID NOT RETRACT AFTER TAKEOFF. RAN QRH AND RETURNED TO ORD. NOSE WHEEL STEERING DID DISENGAGE MOMENTARILY DURING TAXI IN TO THE GATE. (FLT#5071) CLOSED REPLACED OLEO/CENTERING SENSOR BRACKET.

Part: SEAL — FAILED (NLG) · airframe 31,064 hrs · 29,733 cycles

ON CLIMBOUT, RECEIVED GEAR DISAGREE AND NOSE DOOR OPEN WARNING MESSAGES. RAN QRH PROCEDURES AND RETURNED TO ORD. REMOVED AND REPLACED NLG SLIDING MEMBER ASSY AND NLG FLOATING PISTON SEALS IAW AMM.

Part: PROXIMITY SWITCH — FAULTY (NLG) · airframe 30,856 hrs · 29,559 cycles

NOSE GEAR DID NOT COME UP AFTER TAKEOFF. FL 5270 CLOSED. REMOVED AND REPLACED NOSE LANDING GEAR WOW NR 2 AND CENTERED HARNESS ASSEMBLY AND CENTERED BRACKET.

Part: SKIN — DENTED (RT WING) · airframe 29,652 hrs · 28,495 cycles

DENT ON RT WING LEADING EDGE. FLIGHT 3110. FO: 11/30/2018. CARRIED FORWARD FOR RESCHEDULING, TIME REMAINING UNTIL NEXT RE-INSPECTION IS DUE OR UNTIL PERMANENT REPAIR IS REQUIRED.

Part: SKIN — DENTED (RT WING LE) · airframe 29,723 hrs · 28,559 cycles

DENT ON RH WING LEADING EDGE. (FLT#3110) FO: 11/30/2018. CLOSED C/W REO.

Part: SKIN — CRACKED (RT AILERON) · airframe 28,553 hrs · 27,499 cycles

CRACK IN RIGHT AILERON. CRACK IS LOCATED ABOUT 1/4" IN FROM THE OUTBOARD END OF THE AILERON AND EXTENDS FROM THE TRAILING EDGE FORWARD ABOUT 2" ON THE UPPER SURFACE AND ABOUT 1 1/2" ON THE LOWER SURFACE. (FLT 3130) CLOSED COMPLIED WITH TEMP REPAIR IAW REO. AIRCRAFT OK FOR SERVICE AT THIS TIME.

Part: PROXIMITY SENSOR — BENT (MLG) · airframe 27,377 hrs · 26,201 cycles

GEAR DISAGREE NOSE GEAR WOULD NOT COME UP. ADJUSTED THE PROXIMITY SENSORS.

Part: SIGNAL COND UNIT — FAILED (RT ENGINE OIL) · airframe 27,056 hrs · 25,770 cycles

RT ENGINE OIL PRESSURE FLUCTUATED DURING CRUISE, FLAGGING LOWER RED LIMIT. RT OIL PRESSURE WARNING ACTIVATED ONCE MOMENTARILY AT CRUISE. OIL TEMP LOWER THAN OTHER SIDE, DIVERTED. REMOVED AND REPLACED THE SIGNAL CONDITIONING UNIT & ENGINE OIL TEST PANEL IAW AMM. OPS CHECKED GOOD.

Part: TARGET — OUT OF RIG (RT MLG) · airframe 25,887 hrs · 24,431 cycles

GEAR DISAGREE ON RT MLG. GEAR WAS RETRACTED THEN MANUALLY EXTENDED. DECLARED AN EMERGENCY. ACFT LANDED SAFELY. FOUND THE RT UPLOCK MLG TARGET OUT OF RIG, RERIGGED AND OPS CHECKED GOOD.

Part: WARNING MESSAGE — FALSE ACTIVATION (DUCT OVERHEAT) · airframe 24,135 hrs · 22,574 cycles

LEFT 14TH DUCT MESSAGE OVERTEMP ON CLIMBOUT. CREW FOLLOWED QRH AND TOOK ENGINE TO IDLE. CREW DECLARED EMERGENCY. R & R BLEED DUCT INSIDE PYLON, OPS CHECKED GOOD. R & R LT PYLON SENSING ELEMENT IAW AMM. OPS CHECK GOOD.

Part: MOUNT — CHAFED (THRUST REVERSER) · airframe 21,876 hrs · 20,589 cycles

LEFT THRUST REVERSER MAIN TRACK AFT MOUNT LUG AT 5 O'CLOCK IS CHAFED,C-CHECK RO 2/19/15. MEASURED DEPTH OF CHAFE DAMAGE. DAMAGE IS .046" AND FOUND TO BE BEYOND ALLOWABLE LIMITS, REF REO. R & R LT THRUST REVERSER MAIN TRACK AT 5 O`CLOCK POSITION REF AMM. WORK DONE IN REFERENCE TO REO. LT THRUST REVERSER REPLACED ON JOB 2801431, OP 124.

Part: LUG — CHAFED (THRUST REVERSER) · airframe 21,876 hrs · 20,589 cycles

RIGHT THRUST REVERSER MAIN TRACK SUPPORT LUGS AT 7 O'CLOCK ARE CHAFED. C-CHECK, RO 2/19/15, EVALUATED RT T/R MAIN TRACK SUPPORT LUGS AT 7 O`CLOCK. CHAFE DAMAGE MEASURES .051. DAMAGE EXCEEDS LIMITS. REF REO. NEW THRUST REVERSER INSTALLED ON JOB 2801435, OP 102, MX TRANS NR 11846523, REF JOB 2801435, OP110, CAMP 11850132 FOR PARTS TRACKING PURPOSES ONLY.

Part: BULKHEAD WEB — CRACKED (BS 621) · airframe 21,876 hrs · 20,589 cycles

FS 621, BULKHEAD WEB AT LBL 27.50 HAS CRACK AT TOP OF CARGO DOOR TRACK. C-CHECK, RO 2/19/15. REPAIRED CRACK AT FS 621, BULKHEAD WEB AT LBL 27.50, AT TOP OF CARGO DOOR TRACK REF REO.

Part: TRACK — CHAFED (THRUST REVERSER) · airframe 21,876 hrs · 20,589 cycles

LEFT THRUST REVERSER HAS BOTTOM OTBD MAIN TRACK AFT END CHAFING MARK AGAINST BLOCKER DOOR. C-CHECK RO 2/19/15, REPAIRED LT THRUST REVERSER REF REO & SB CF-34-NEEDS PERFORMED, SB ACCOMPLISHED ON JOB 2801435, OP 101, CAMP11845915. DUE TO REO BEING TEMPORARY LT THRUST REVERSER IS REPLACED ON JOB 2801431 OP 124, CAMP 1183197, REO.

Part: STRUCTURE — FAILED (DOOR CUTOUT) · airframe 21,876 hrs · 20,589 cycles

PAX DOOR CUTOUT HAS A BENT EXTRUSION NEAR THE FWD UPPER LOCKPIN HOLE, ON AIRCRAFT SIDE. C-CHECK, RO 2/19/15, COMPLIED WITH REO. TYPE I PERMANENT REPAIR.

Part: STRUCTURE — CORRODED (BS 574-621) · airframe 21,876 hrs · 20,589 cycles

AFT CARGO HAS CORROSION AROUND NUT-PLATE HOLES AT FLOOR EDGE MEMBER LT SIDE AT FS 574.00 TO FS 621.0, C-CHECK, RO 2/19/15. BLENDED CORROSION ON AFT CARGO SILL AROUND NUT-PLATES HOLES AT FS574.00 TO FS621.0 REF AMM. ORIGINAL MATERIAL THICKNESS ON CARGO FLOOR SILL WAS .050" REF AMM. REMAINING MATERIAL THICKNESS WAS .023 AND .027" WAS REMOVED. BLENDED AREA IS OUT OF LIMITS REF SRM 53-61-23. CAMP 11855100, JOB 2801431, OP121 FOR REPLACEMENT CARGO SILL. WORK DONE IN REF TO SRM.

Part: SKIN — DENTED (BS 605) · airframe 21,876 hrs · 20,589 cycles

LOWER FUSELAGE SKIN HAS DENT AT FS 605.00 BETWEEN STR 25L AND 26L. PERFORMED PERMANENT REPAIR ON LOWER SKIN AT FS 605.00 IAW STS EA WORK DONE IN REF TO STS EA.

Part: BULKHEAD — CRACKED (BS 621) · airframe 21,876 hrs · 20,589 cycles

FS 621, BULKHEAD HAS 2 CRACKS AT LINTEL FITTING. C-CHECK, RO 2/19/15, REPAIRED FS 621 BULKHEAD LINTEL FITTING REF REO. NO LEAKS NOTED, COMPLIED WITH ST.

Part: SKIN — DENTED (RT WING) · airframe 21,876 hrs · 20,589 cycles

RIGHT WING UPPER SURFACE HAS SMALL DENT IN BETWEEN THE SPOILERON AND FLIGHT SPOILER. C-CHECK, REPAIRED RT WING UPPER SURFACE SMALL DENT BETWEEN THE SPOILERON AND FLIGHT SPOILER, REF STS, EA STS EA. WORK DONE IN REFERENCE TO STS EA.

Part: SKIN — DENTED (BS 606) · airframe 21,876 hrs · 20,589 cycles

DENT AT FUSELAGE STA 606.0 BETWEEN STRINGERS L18 AND L19. FOUND DENT TO WITHIN LIMITS IAW REO. PERMANENT REPAIR DUE AT NEXT C-CHECK, COMPLETED PERMANENT REPAIR FOR DENT AT FUSELAGE STA 606.0 BETWEEN STRINGER L18 AND L19 IAW STS EA.

Part: CONTROL PANEL — FAILED (PAX OXYGEN) · airframe 20,847 hrs · 19,750 cycles

AIRCRAFT THOUGHT IT WAS ABOUT 15,000 FT AT THE GATE AND DROPPED THE PAX OXYGEN MASKS. REMOVED AND REPLACED CPAM IAW AMM.

Part: FLAP SYSTEM — FAILED · airframe 20,994 hrs · 19,879 cycles

FLAPS FAILED AT 20, RETURN TO FIELD. RAN QRH. RESET FLAPS IAW FIM. RAN FLAPS FIVE FULL CYCLES. OK TO CONTINUE IN SERVICE FOR 10 FLIGHT CYCLES IAW AD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 20,390 hrs · 19,405 cycles

AFT EMERGENCY CEILING EXIT LIGHT INOPERATIVE. R & R NR 2 BATTERY PACK IAW AMM.

Part: BATTERY PACK — INOPERATIVE (FLASHLIGHT) · airframe 20,295 hrs · 19,329 cycles

F/A FLASHLIGHT INOPERATIVE. R & R FLASHLIGHT BATTERIES IAW AMM 25-60-00, NO FURTHER DEFECT NOTED.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 20,125 hrs · 19,158 cycles

F/A FLASHLIGHT INTERMITTENTLY WORKING. REPLACED BATTERY IAW AMM 25-60-00. OK FOR SERVICE.

Part: SELECTOR VALVE — FAILED (MLG) · airframe 19,028 hrs · 18,043 cycles

LOWERED GEAR HANDLE FOR LANDING, RECEIVED GEAR DISAGREE WARNING. BOTH MAIN GEAR FAILED TO EXTEND. RAN QRH. MANUAL EXTENSION SUCCESSFUL, EMERGENCY ACTIONS, R & R MLG EXTENTION AND RETRACTION SELECTOR VLAVE IAW AMM 32-32-10 AND IPC 32-32-10, FIG 1 ITEM 30. OPS CHECKS AND FUNCTIONAL CHECK GOOD ACFT OK FOR SVC, ALL RII COMPLIED IAW GMM 3-3.

Part: SKIN — BURNED (FUSELAGE) · airframe 18,505 hrs · 17,504 cycles

TWO BURN MARKS BETWEEN FS 280 AND 295, BETWEEN STRINGERS 26 AND 27L. DRILLED OUT DAMAGE, 1 DAMAGE TO A NR 30 AND 1 TO NR 40 IAW REO 601R-53-00-115, REV C. INSTALLED FASTENERS IAW REO 601R-53-00-115, REV C. MAJOR REPAIR.

Part: SKIN — BURNED (BS 461 S26L) · airframe 18,506 hrs · 17,505 cycles

BURN ON FUEL ACCESS PANEL AT FS 461 AT STRINGER 26L. BLENDED TWO BURNS IAW SRM 51-12-00. FOUND TO BE OUT OF LIMITS. ROTO-PEENED, RE-WORKED AREA IAW SRM 51-24-11. RESTORED SURFACE FINISH TO RE-WORKED AREA SRM 51-25-01. MAJOR REPAIR IAW GMM 5-3.

Part: SKIN — BURNED (BS 473.15) · airframe 18,506 hrs · 17,505 cycles

BURN MARK AT BS 473.15 AT STRINGER 26L. BLENDED BURN IN SKIN REF SRM 51-12-00. DETERMINED TO BE OUT OF LIMITS (NO LIGHTNING BURNS ALLOWED TO WING SKINS). ROTO-PEENED, RE-WORKED AREA IAW SRM 51-24-11. RESTORED SURFACE FINISH TO RE-WORKED AREA SRM 51-25-01. MAJOR REPAIR IAW GMM 5-3.

Part: SKIN — BURNED (BS 295-310) · airframe 18,505 hrs · 17,504 cycles

ONE BURN MARK BETWEEN FS 295 AND 310, BETWEEN STRINGERS 27 AND 26L. DRILLED OUT DAMAGE TO A NR 30 IAW REO 601R-53-00-115, REV C. INSTALLED 1 FASTENER BETWEEN FS 295 AND FS 310, BETWEEN STGR 27 AND STGR 26L IAW REO 601R-53-00-115, REV C. CLASSIFIED AS A MAJOR REPAIR.

Part: SKIN — BURNED (BS 310-319) · airframe 18,505 hrs · 17,504 cycles

ONE BURN MARK BETWEEN FS 310.00 AND 319.70, BETWEEN STRINGERS 27 AND 26L. DRILLED OUT DAMAGE TO A NR 30 IAW REO 601R-53-00-115, REV C. INSTALLED ONE FASTENER BETWEEN FS 310 AND FS 319, BETWEEN STGR 27 AND STGR 26L IAW REO 601R-53-00-115, REV C. CLASSIFIED AS A MAJOR REPAIR.

Part: SKIN — BURNED (LT WING) · airframe 18,506 hrs · 17,505 cycles

LEFT WING LOWER WING PLANK HAS LIGHTNING BURN AT OTBD AFT SKIN EDGE OF FUEL TANK ACCESS PANEL 610AB CUTOUT. BLENDED BURN ON LT WING LOWER WING PLANK REF SRM 51-12-00. DETERMINED TO BE OUT OF LIMITS (LIGHTNING STRIKE NOT ALLOWED TO WING PLANK). ROTO-PEENED RE-WORKED AREA IAW SRM 51-24-11. RESTORED SURFACE FINISH TO RE-WORKED AREA SRM 51-25-01. MAJOR REPAIR IAW GMM 5-3.

Part: SKIN — BURNED (BS 424-439) · airframe 18,506 hrs · 17,505 cycles

BURN MARK BETWEEN FS 424 AND 439, BETWEEN STRINGER 27 AND 26L. BLENDED BURN IN SKIN SRM 51-12-00. BLEND MEASURES .013" D, .450"L, .500"W. DETERMINED TO BE OUT OF LIMITS (NO LIGHTNING DAMAGE ALLOWED TO WING SKINS). ROTO-PEENED, RE-WORKED AREA IAW SRM 51-24-11. RESTORED SURFACE FINISH TO RE-WORKED AREA SRM 51-25-01. THIS IS CONSIDERED A MAJOR REPAIR IAW GMM 5-3.

Part: SKIN — BURNED (BS 409) · airframe 18,505 hrs · 17,504 cycles

ONE BURN MARK BETWEEN FS 409.00 AND 409+16, AT STRINGER 26L. REMOVED BURNED FASTENER FOUND COUNTERSINK DAMAGED STEPPED UP HOLE TO A NR 6 FASTENER HOLE AND ALL DAMAGE IS GONE AFTER CONTER SINK IAW REO 601R-53-00-115, REV C. INSTALLED NEW FASTENER BETWEEN FS 409 AND FS 409+16, AT STGR 26L IAW REO 601R-53-00-115, REV C. CLASSIFIED AS A MAJOR REPAIR.

Part: SKIN — BURNED (BS 449) · airframe 18,506 hrs · 17,505 cycles

2 BURN MARKS AT FS 449.85 AT STRINGER 26L. BLENDED 2 BURNS IN SKIN REF SRM 51-12-00. DETERMINED TO BE OUT OF LIMITS (NO LIGHTNING BURNS ALLOWED TO WING SKINS). ROTO-PEENED, RE-WORKED AREA IAW SRM 51-24-11. RESTORED SURFACE FINISH TO RE-WORKED AREA SRM 51-25-01. THIS IS CONSIDERED A MAJOR REPAIR IAW GMM 5-3.

Part: SKIN — BURNED (FUSELAGE) · airframe 18,505 hrs · 17,504 cycles

TWO BURN MARKS AT FS 169.00 ON BOTTOM, 1 IS 3" TO THE LEFT OF CENTERLINE AND 1 IS 4" TO THE RT OF CENTERLINE. REPAIRED IAW REO 601R-53-00-115, REV C, STS EA 12-2013-293, SRM 51-25-01. MAJOR REPAIR.

Part: SKIN — BURNED (BS 280-295) · airframe 18,506 hrs · 17,505 cycles

FOUND ONE BURN BETWEEN FS 295 AND 280 BETWEEN STRG 26L AND 27L. DRILLED OUT DAMAGE TO A NR 40 IAW REO 601R-53-115. INSTALLED 1 EA FASTENER BETWEEN FS 295 AND FS 280, BETWEEN STGR 26L AND STGR 27 IAW REO 601R-53-00-115, REV C. MAJOR REPAIR,

Part: SKIN — BURNED (BS 409-424) · airframe 18,506 hrs · 17,505 cycles

TWO BURN MARKS BETWEEN FS 409+128 AND FS 424, BETWEEN STRINGER 27L AND 26L. BLENDED BURNS, REF SRM 51-12-00. BLEND A MEASURES .021" D, .450"L, .600"W. BLEND B MEASURES .015" D, .500"L, .500"W. DAMAGE FOUND TO BE OUT OF LIMITS (NO LIGHTNING STRIKE ALLOWED TO WING SKINS). ROTO-PEENED, RE-WORKED AREA IAW SRM 51-24-11. RESTORED SURFACE FINISH TO RE-WORKED AREA SRM 51-25-01. THIS IS CONSIDERED A MAJOR REPAIR IAW GMM 5-3.

Part: LOCK — LACK OF LUBE (PAX DOOR) · airframe 18,354 hrs · 17,337 cycles

PAX DOOR HARD TO OPEN FROM INSIDE CABIN. INSPECTED AND LUBED LOCK MECHANISM IAW AMM 52-11-00, OPS CHECKS NORMAL, ACFT OK FOR SVC.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,854 hrs · 16,800 cycles

EMERGENCY LIGHT, INOPERATIVE. R & R EMERGENCY LIGHT IAW AMM 33-51-19. OPS CHECKED GOOD.

Part: BULKHEAD — CRACKED (AFT) · airframe 17,691 hrs · 16,638 cycles

REAR PRESSURE BULKHEAD WEB AFT SIDE AT ABOUT 8:45 O`CLOCK POSITION HAS A CRACKED CLIP. R & R REAR PRESSURE BULKHEAD WEB AFT SIDE AT ABOUT 8:45 0'CLOCK POSITION CLIP IAW SRM 51-42-20.

Part: ANGLE — CRACKED (BS 559 BULKHEAD) · airframe 17,691 hrs · 16,638 cycles

PRESSURE BULKHEAD WEB CAP ANGLE CRACKED AT FS 559 LBL 18.00. RECEIVED AND COMPLIED WITH REO 601R-53-41-1650.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 17,683 hrs · 16,631 cycles

PAX DOOR LOWER SILL ANGLE CORRODED AT FWD SECTION. REMOVED CORROSION IAW 51-21-06. COMPLIED WITH REO 601R-53-21-2390.

Part: SEAT TRACK — CORRODED (BS 473-477) · airframe 17,683 hrs · 16,631 cycles

SEAT TRACK CORRODED FS 473-477 RBL 9. R & R CORRODED SEAT TRACK WITH NEW IAW AMM 53-01-11-000-802 AND 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (BS 484-487) · airframe 17,683 hrs · 16,631 cycles

SEAT TRACK CORRODED FS 484 - 487 RBL 9. R & R CORRODED SEAT TRACK WITH NEW IAW AMM 53-01-11-000-802 AND 53-01-11-400-802.

Part: SILL — CORRODED (FUSELAGE) · airframe 17,683 hrs · 16,631 cycles

CARGO DOOR SILL PLATE HAS MINOR CORROSION. REMOVED CORROSION IAW SRM 51-21-06.

Part: FLOOR SUPPORT — CORRODED · airframe 17,691 hrs · 16,638 cycles

MINOR CORROSION AROUND SCREW HOLES ON LBL 27, JUST INBD OF CARGO DOOR. REMOVED CORROISON MATERIAL LOSS MORE THAN 50 PERCENT FOUND TO BE OUT OF LIMITS IAW SRM 53-61-43+ 53-00-00. REMOVED AFT LT FUSELAGE FLOOR CAP. LOCATED AND DRILLED NEW TRACK IAW SRM 51-40-11. INSTALLED FLOOR CAP IAW SRM 51-42-22, 51-42-34, 51-42-20 AND REP 601R-53-61-3778. RECEIVED & COMPLIED WITH REO 601R-53-61-3778 & GREO 601R-53-61-3778 REV A DATED 7/15/2011. COMPLETED AND ATTACHED FORM M335. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW ASA SOP 5702.

Part: SEAT TRACK — CORRODED (BS 473-477) · airframe 17,683 hrs · 16,631 cycles

SEAT TRACK CORRODED FS 473- 477 LBL 9. R & R CORRODED SEAT TRACK WITH NEW SEAT TRACK IAW AMM 53-01-11-000-802 AND 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (BS 409) · airframe 17,683 hrs · 16,631 cycles

SEAT TRACK CORRODED FS 409+100-409+105 RBL 9. R & R SEAT TRACK WITH NEW SERVICEABLE SEAT TRACK IAW TASKS 53-01-11-000-802 AND 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (BS 364-369) · airframe 17,683 hrs · 16,631 cycles

SEAT TRACK CORRODED AT FS 364-369 LBL 9. REMOVED CORRODED SEAT TRACK IAW AMM 53-01-11-000-802. INSTALLED NEW SEAT TRACK IAW AMM 53-01-11-420-001.

Part: SEAT TRACK — CORRODED (BS 409) · airframe 17,683 hrs · 16,631 cycles

SEAT TRACK CORRODED, FS 409+80-FS 409+84 RBL 9. REMOVED UNSERVICABLE SEAT TRACK IAW AMM TASK 53-01-11-000-802. INSTALLED NEW SERVICABLE SEAT TRACK IAW AMM TASK 53-01-44-400-802.

Part: ANGLE — CORRODED (DOOR HINGE) · airframe 17,683 hrs · 16,631 cycles

REMOVE FOUR ANGLES ON HINGE SIDE OF PAX DOOR, FOUND TO BE CORRODED. REMOVED FOUR ASD HINGE SIDE LT, ANGLES IAW SRM 51-42-06. INSTALLED FOUR PAX DOOR HINGE SIDE L ANGLES IAW SRM 51-42-06 WITH SERVICABLE PART.

Part: CHANNEL — CORRODED (DOOR HINGE) · airframe 17,683 hrs · 16,631 cycles

PAX DOOR HINGE SIDE CENTER CHANNEL FOUND TO BE CORRODED. REMOVED CHANNEL IAW SRM 51-42-06 51-42-21. INSTALLED PAX DOOR HINGE CHANNEL IAW SRM 51-42-06 51-42-21 WITH SERVICABLE PART.

Part: SEAT TRACK — CORRODED (BS 364-394) · airframe 17,683 hrs · 16,631 cycles

SEAT TRACK CORRODED AT FS 364-394 RBL 9. REMOVED CORRODED SEAT TRACK AT FS 364-394 IAW AMM 53-01-11-000-802. INSTALLED NEW SEAT TRACK IAW AMM 53-01-11-420-001.

Part: FLOOR PANEL — CRACKED (BS 193) · airframe 17,683 hrs · 16,631 cycles

LT TRU FLOOR PANEL CRACKED ON LT SIDE. REPAIRED ELECTRICAL BAY FLOOR PANEL AT FS 193 IAW GREO 601R-53-11-000 AND COMPLIED WITH GREO 601R-53-11-111.

Part: DOOR — NO TEST (RT OVERWING) · airframe 17,691 hrs · 16,638 cycles

RT OVER WING EXIT FAILED FUNCTIONAL CHECK AT 60 POUNDS OF PULL. RT OVERWING EXIT FUNCTIONAL TEST GOOD IAW CH 52-21-00-720-801. COMPLIED WITH POWER ON FUNCTION CHECK OF RT OVERWING EXIT OPS CHECKED OK, PULL FORCE AT 38 NR , (LIMIT 30 +- 10) SPB 88079 12/26/12 IAW TASK 52-21-00-720-801.

Part: ADG — MALFUNCTIONED · airframe 17,244 hrs · 16,166 cycles

ADG CAME OUT WITH BOTH GENERATOR WORKING. ACFT RETURNED TO DEPARTURE. EMERGENCY DECLARED. PERFORMED OPS CHECKED OF ADG IAW AMM 24-23-01.

Part: LIGHT — CRACKED (CABIN) · airframe 17,244 hrs · 16,166 cycles

VERTICAL EMERGENCY EXIT FLOOR LIGHT HOUSING CRACKED ON FORWARD WARDROBE. R & R VERTICAL EMERGENCY EXIT FLOOR LIGHT ASSY ON WARDROBE IAW AMM 33-51-09. OPS CHECKED GOOD.

Part: CHANNEL — CRACKED (PAX DOOR) · airframe 16,557 hrs · 15,417 cycles

PAX DOOR BETWEEN FS 329.5 AND FS 338 AFT CHANNEL, POSSIBLY CRACKED. COMPLIED WITH NDT EDDY CURRENT INSPECTION IAW NDTM 51-20-06 PART 1. CONFIRMED CRACK. REPAIRED IAW REO 601R-52-11-279.

Part: PUSH-PULL CABLE — BINDING (RT THROTTLE) · airframe 16,534 hrs · 15,388 cycles

RIGHT THRUST LEVER CAUSED NO CHANGE IN ENGINE POWER SETTING (94 PERCENT). ALL OTHER ENGINE PARAMETERS REMAINED NORMAL. FOLLOWED QRH FOR JAMMED THROTTLE. SHUTDOWN ENGINE IN FLT. DIVERTED, EMERGENCY DECLARED. R & R RT PYLON PUSH-PULL THROTTLE CABLE IAW IAW AMM 76-11-09. NEW CALBE OPS CHECKED CORRECTLY.

Part: TARGET — OUT OF POSITION (PROXIMITY SENSOR) · airframe 16,536 hrs · 15,390 cycles

ON GEAR RETRACTION, NOSE GEAR INDICATED DOWN ALONG WITH NLG DOOR OPEN. DIVERTED. INSPECTED NLG. FOUND NLG OLEO CENTERED/EXTENDED PROXIMITY SENSOR (PS14GA) SENSOR-TO-TARGET OFFSET OUT OF CLEARANCE. REPOSITIONED TARGET IAW AMM 32-61-05. GAP AND SENSOR-TO-TARGET OFFSET IN DIMENSIONS. PERFORMED RETRACTION AND EXTENSION OF GEAR IAW AMM 32-30-00. OPS CHECKED NORMAL.

Part: LINE — LEAKING (APU FUEL) · airframe 15,080 hrs · 13,787 cycles

SMELL OF JET FUEL FROM BOTH PACKS ON TAXI WITH APU RUNING AND WHILE CLIMBING WITH ENGINES RUNING. FOUND APU SUPPLY LEAKING REALLY BAD. R & R APU FUEL SUPPLY (PN AE7010201G0240), PERFORMED LEAK CHECK IAW AMM 49-31-01. NEW LINE DOES NOT LEAK. (CLOSED)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 14,902 hrs · 13,594 cycles

SEVERAL EMERGENCY LIGHTS INOP. R & R NR 2 ELT BATTERY PACK IAW AMM 33-51-04. OPS CHECK GOOD. NO FURTHER DEFECTS NOTED AT THIS TIME.

Part: FLASHLIGHT — BROKEN (CABIN) · airframe 13,409 hrs · 11,888 cycles

F/O'S FLASHLIGHT BROKEN. R & R FLASHLIGHT IAW AMM 25-60-01. (CLOSED)

Part: ISOLATOR — CRACKED (BULKHEAD) · airframe 12,863 hrs · 11,239 cycles

CARGO BAY AFT BULKHEAD MOUNT ISOLATOR IS CRACKED AT LBL 27, 2ND UP FROM FLOOR. (RESOLVED ON W/O: 164029 TASKCARD: N/R-00472 ) R & R CARGO BAY AFT BULKHEAD MOUNT ISOLATOR AT LBL 27 2ND UP FROM FLOOR IAW SRM 51-42-06. (CLOSED)

Part: BULKHEAD — CRACKED (BS 202) · airframe 12,863 hrs · 11,239 cycles

BS 202 BULKHEAD IS CRACKED ON THE UPPER LOCATION FOR THE BRAKE CABLE HOLE. CRACK IS APPROX .4 LONG. C/W EC/TC REO 601R-53-11-563 AND REO 601R-53-11-563.

Part: FLOORBEAM — CORRODED (CARGO BAY) · airframe 12,863 hrs · 11,239 cycles

CARGO ENTRY FLOOR EDGE MEMBER HAS CORROSION AROUND NUTPLATE HOLES. REMOVED CARGO DOOR SILL PLATE IAW SRM 51-42-06, 51-42-21 AND 51-42-13, FOUND DOOR SILL TO BE OUT OF LIMITS IAW SRM 53-61-23. FABRICATED CARGO BAY FLOOR SILL USING 2024-T3 .050 PO NR W3776 IAW PART REMOVED IAW REO 601R-53-61-1574 REV A, ASA EC/TC REO 6014R-53-61-1574, STEP 2. COMPLIED WITH STEP 6 OF ASA EC/TC REO 601R-53-61-1574. PERFORMED EDDY CURRENT OF CARGO FLOOR SILL PLATE CUTLINE IAW NDTM 51-20-06. NO INDICATIONS NOTED. INSTALLED SILL PLATE AND DOUBER. C/W ALL STEPS OF EC/TC REO 601R-53-61-1574.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 12,863 hrs · 11,239 cycles

FS 280 FLOOR SUPPORT ANGLE CRACKED APPROX 1" LONG AT UPPER FLANGE OUTBD OF GEAR MANUAL RELEASE PULLEY BRACKET LBL 9.0. C/W STEP 1 AND 2 OF ASA ECTC, REO 601R-53-11-138. C/W SEP 3 OF ASA ECTC REO 601R-53-11-138. C/W STEP 4 OF ASA ECTC REO 601R-53-11-138. C/W STEP 5 OF ASA ECTC REO 601R-53-11-138. C/W STEP 6 OF ASA ECTC REO 601R-53-11-138. C/W STEP 7 AND8 OF ASA ECTC REO 601R-53-11-138. C/W SEP 9 OF ASA ECTC REO 601R-53-11-138. C/W STEPS 10,11 AND 12 OF AS ECTC REO601R-53-11-138. C/W STEPS 13 AND 14 OF ASA EC/TC REO 601R-53-11-138.

Part: LIGHT — BROKEN (CABIN) · airframe 12,863 hrs · 11,239 cycles

WARDROBE EXIT LIGHT ASSY IS BROKEN. R & R THE BOTTOM VERTICAL WARDROBE EXIT LIGHT ASSY IAW AMM 33-51-10-000-801 AND 33-51-10-400-801. AN OPS TEST OF THE EMERGENCY LIGHTS IS DUE. PERFORMED OPS TEST OF EMERGENCY LIGHTS IAW AMM 33-51-00-710-801. OPS TEST GOOD.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 12,863 hrs · 11,239 cycles

PAX DOOR AFT DRAG ANGLE CRACKED APPROX 1" LONG. REPAIRED PAX DOOR AFT DRAG ANGLE IAW ASA EC/TC REO 601R-52-11-513.

Part: INTERCOSTAL — CRACKED (BS 484) · airframe 12,863 hrs · 11,239 cycles

RT FS 484.00 INTERCOSTAL IS CRACKED AT RBL 36 AND ANGLE IS CRACKED AT RBL 27. REMOVED CABLE GUIDE TO ACCESS INTERCOSTAL MOD IAW SRM 51-41-04. NO TENSION LOSS. REMOVED ANGLE IAW SRM 51-42-06. INSTALLED NEW ANGLE. REPAIRED FS 484 INTERCOSTAL AT RBL 27 AND RBL 36 IAW REO 601R-53-41-059. INSTALLED CABLE GUIDE IAW SRM 51-41-04 AND AMM 20-24-00-910-801. REPAIR TO THE INTERCOSTALS AT FS 484 BETWEEN BL 27 AND 36.00 IS COMPLETED IAW REO 601R-53-41-059 AND MEETS WITH ALL THEIR REQUIREMENTS, ALL STEPS C/W.

Part: INTERCOSTAL — CRACKED (BS 484) · airframe 12,863 hrs · 11,239 cycles

LEFT FS 484.00 INTERCOSTAL IS CRACKED AT LBL 36. REMOVED CABLE GUIDE AT FS 484.00, LBL 36 TO ACCESS INTERCOSTAL MOD IAW SRM 51-41-04. NO TENSION LOSS. REINSTALL CABLE GUIDE. REPAIRED FS 484 INTERCOSTAL AT LBL 36 IAW REO 601R-53-41-059 AND INSTALLED CABLE GUIDE IAW SRM 51-41-04 AND AMM 20-24-00-910-801. REPAIR TO THE INTERCOSTALS AT FS 484 BETWEEN BL 27.00 AND BL 36.0 IS COMPLETED IAW REO 601R-53-41-059 AND MEETS WITH ALL THEIR REQUIREMENTS, ALL STEPS C/W.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 12,838 hrs · 11,210 cycles

NR1 AND NR2 CABIN CEILING EMERGENCY LIGHTS INOP. R & R NR 1 AND NR 2 EMERGENCY CEILING FLOODLIGHTS IAW AMM 33-51-16. OPS CHECK GOOD. R & R NR1 AND NR2 EMERGENCY CEILING FLOODLIGHTS IAW AMM 33-51-16. OPS CHECK GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 12,838 hrs · 11,210 cycles

CABIN CEILING CURVED EMERGENCY EXIT SIGN FWD LAMP INOP. (RESOLVED ON W/O: 162971, TASKCARD: N/R-00007 ) R & R CABIN CEILING CURVED EMERGENCY EXIT SWD LAMP IAW AMM 33-51-14. OPS CHECK GOOD. R & R CABIN CEILING CURVED EMERGENCY EXIT SWD LAMP IAW AMM 33-51-14. OPS CHECK GOOD. (CLOSED)

Part: VALVE — FAILED (MLG) · airframe 11,890 hrs · 10,129 cycles

RECEIVED "GEAR DISAGREE" DURING GEAR EXTENSION, MAIN WERE GREEN, NOSE WAS WHITE RAN CHECK LIST AND PULLED EXT HANDLE. THAT GAVE US 3 GREEN. NOSE DOOR OPEN MSG WAS SHOWING WITH GEAR DISAGREE MSG (EMERGENCY DECLARED).

Part: LANDING GEAR — MALFUNCTIONED (MAINS) · airframe 11,710 hrs · 9,936 cycles

INBOUND AFTER SELECTING LDG GEAR LEVER TO DOWN POSITION AT 3000' AND 180 KTS RECIEVED GEAR DISAGREE WARNING. NOSE GEAR INDICATED DOWN, 2 MAINS INDICATED UP. FOLLOWED QRH, RECYCLED 6 TIMES WITH NO HELP. PULLED LANDING GEAR MANUAL RELEASE, MAINS EXTENDED AND SHOWED DOWN ON EICAS. NORMAL LANDING, HYD PRESS NORMAL THROUGHOUT. MAIN GEAR ICON ON EICAS NEVER CHANGED FROM "UP" UNTIL MANUAL RELEASE. EMERGENCY DECLARED BY ATC AND TRUCKS ON STAND BY AS A PRECAUTION.

Part: LANDING GEAR — MALFUNCTIONED · airframe 11,710 hrs · 9,936 cycles

RECEIVED MLG DISAGREE ON APPROACH. FOLLOWED QRH, MANUAL RELEASE HANDLE WOULD NOT STOW. EMERGENCY DECLARED. LANDING GEAR RETRACTION SYSTEM.

Part: LANDING GEAR — MALFUNCTIONED · airframe 11,709 hrs · 9,935 cycles

RECEIVED GEAR DISSAGREE ON APPROACH. MAIN GEAR WOULD NOT COME DOWN. [EMERGENCY DECLARED] ( LANDING GEAR RETRACTION SYS )

Part: OIL SYSTEM — OVERTEMP (NR 1 ENGINE) · airframe 11,542 hrs · 9,751 cycles

DURING CLIMB OUT OF ATL NR 1 ENG OIL TEMP INCREASED AMBER AT 150+ F/O PULLED OUT QRH & IT ALREADY WAS RED 163 & RAN QRH. AFTER IDLING FOR ALMOST 2 MIN FINALLY STARTED DECREASING. LOWERED TO IDLE & STILL SHOWING 131' (RT SHOWING 99) ALSO NR 1 OIL PRESS WAS 5 TO 10 PSI LESS [EMERGENCY DECLARED -- AIRCRAFT RETURNED TO ATL AFTER T/O]

Part: ENGINE — OVERTEMP (LEFT) · airframe 11,511 hrs · 9,710 cycles

LT ENGINE OIL TEMP ROSE TO 169 DEGREES C CLIMBING OUT OF FL180, COMPLIED WITH QRH PULLED POWER TO IDLE, TEMP RETURNED TO GREEN RANGE. KEPT ENG AT IDLE UNTIL LANDING. SHUTDOWN AFTER LANDING [EMERGENCY DECLARED -- ACFT RETURNED TO DEPARTURE AFTER T/O].

Part: FLAP — FAILED (WING) · airframe 9,832 hrs · 8,085 cycles

FLAP FAIL AT 20 DEGREES ON APPROACH. EMERGENCY DECLARED. FLT 5589X2,5528X2

Part: ATTACH FITTING — CRACKED (BS 625) · airframe 8,728 hrs · 7,113 cycles

IN AFT EQUIP BAY, FS 625, LT CLIP CRACKED AT APPROX 8 O`CLOCK POSITION. REMOVED AND REPLACED FS 625, LT CLIP AT APPROX 8 O`CLOCK POSITION. ALL WORK DONE IAW CRJ200 SRM 51-42-06 M. (S)

Part: ATTACH FITTING — CRACKED (BS 625) · airframe 8,728 hrs · 7,113 cycles

IN AFT EQUIP BAY, FS 625, RT CLIP CRACKED AT APPROX 4 O`CLOCK POSITION. REMOVED AND REPLACED FS 625, RT CLIP AT APPROX 4 O`CLOCK POSITION. ALL WORK DONE IAW CRJ 200 SRM 51-42-06. (S)

Part: FLOORBEAM — CRACKED (BS 280) · airframe 8,728 hrs · 7,113 cycles

FS 280.00 FLOORBEAM OUTBOARD CLIP AT RBL 9 IS CRACKED. REMOVED AND REPLACED BROKEN CLIP WITH NEW AT RBL 9 FS 280 FLOORBEAM OUTBOARD, ALSO FOUND INBOARD CLIP NEEDED REPLACING AND REPLACED SAME. WORK DONE IAW CRJ200 SRM 51-42-20. (S)

Part: FLOORBEAM — CRACKED (BS 280) · airframe 8,728 hrs · 7,113 cycles

FL280.00 FLOORBEAM INBOARD AND OUTBOARD CLIP AT LBL 9 ARE CRACKED. REMOVED AND REPLACED BROKEN CLIPS WITH NEW CLIPS AT LBL 9 FS 280 FLOORBEAM, INBOARD AND OUTBOARD. WORK DONE IAW CRJ200 SRM 51-42-20. (S)

Part: CHANNEL — CRACKED (CARGO DOOR TRACK) · airframe 8,728 hrs · 7,113 cycles

CARGO DOOR FWD TRACK SUPPORT LOWER U CHANNEL IS CRACKED REMOVED AND REPLACED CARGO DOOR FWD TRACK SUPPORT LOWER U CHANNEL PER SRM 51-42-06. (B)

Part: SUPPORT ANGLE — CRACKED (BS 621)

LT FS 621 SUPPORT ANGLE CRACKED. REPAIRED ITEM BY ACCOMPLISHMENT OF REO 601R-53-61-117. RII REQUIREMENTS MET PER SP 607.

Part: ANGLE — CRACKED (BS 621)

RIGHT FS 621 ANGLE CRACKED. JOB COMPLETED REPAIRED ITEM BY ACCOMPLISHMENT OF REO 601R-53-61-117. RII REQUIREMENTS MET PER SP 607. JOB COMPLETE [SUPPLEMENTAL SDR CLOSED 6/25/08] (B)

Part: STEP — CRACKED (PAX DOOR) · airframe 8,728 hrs · 7,113 cycles

BOTTOM STEP CRACKED AT SIDE ARM ATTACH POINT. (B) REMOVED AND REPLACED ASD BOTTOM STEP IAW AMM 52-11-00. (S)

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 6,675 hrs · 5,368 cycles

F/A'S FLASHLIGHT INOP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 6,459 hrs · 5,205 cycles

EMERGENCY LIGHTS WN COME ON. FLT 4914 DEL 16 MINS.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 5,913 hrs · 4,783 cycles

CAPTAIN'S FLASHLIGHT BULB INOP.

Part: UNKNOWN — UNKNOWN (PITCH TRIM) · airframe 5,299 hrs · 4,335 cycles

PITCH TRIM RAN AWAY WHILE HAND FLYING AFTER T/O. DISCONNECTED TRIM, TRIM RAN NOSE DOWN 2.6 DEGREES. AIRCRAFT RETURNED TO ABE AFTER T/O. EMERGENCY EQUIPMENT ON STANDBY.

Part: WARNING MESSAGE — FALSE ACTIVATION (NLG STEERING) · airframe 4,228 hrs · 3,539 cycles

STEERING INOP MESSAGE RIGHT AFTER TAKEOFF. FOLLOWED QRH, MESSAGE WENT OUT WITH NWS OFF AFTER LANDING. CREW WAS ABLE TO RESET WITH SWITCH. EMERGENCY DECLARED.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 3,944 hrs · 3,290 cycles

EMERGENCY LIGHT OFF INDICATION LIGHT HAS A LIGHT BULB INOP.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 3,831 hrs · 3,195 cycles

RANRC 155. CORROSION AROUND FLOORBOARD SCREW HOLES IN FLOOR BEAM ADJACENT TO CARGO DOOR SILL.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT)

DURING A GROUND INSPECTION IN CAE, THE LOWER EMERGENCY EXIT SIGNS AT ROW 8 ON BOTH SIDES WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMPS IN THE LOWER EMERGENCY EXIT SIGNS AT ROW 8 ON BOTH SIDES. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)