N928EV

Part: WARNING MESSAGE — ACTIVATED (WING OVERHEAT) · airframe 37,124 hrs · 34,911 cycles

WE RECEIVED A WING OVERHEAT WARNING MSG AND THEN ANTI ICE DUCT WARNING MSG ON CLIMB OUT FROM DEN, RAN QRH AND IT CLEARED BOTH MSGS. TURNED IT BACK ON AND GOT BOTH MSG AGAIN. DID NOT LAND OVERWEIGHT AND DID NOT DECLARE EMERGENCY. (FLIGHT 4663 FILED OPEN)THIS IS CURRENTLY A WORK IN PROGRESS.

Part: CONNECTOR — NOT SEATED (WING OVERHEAT) · airframe 37,124 hrs · 34,911 cycles

RECEIVED A WING OVERHEAT WARNING MSG AND THEN ANTI ICE DUCT WARNING MSG ON CLIMB OUT FROM DEN, RAN QRH AND IT CLEARED BOTH MSGS. TURNED IT BACK ON AND GOT BOTH MSG AGAIN. DID NOT LAND OVERWEIGHT AND DID NOT DECLARE EMERGENCY. (FLIGHT 4663 FILED CLOSED)THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 27776012 WITH THE FOLLOWING CORRECTIVE ACTION: "TROUBLESHOT THE WING OVERHEAT AND ANTI-ICE DUCT WARNING MESSAGE REFERENCING THE APPLICABLE STEPS IN FIM 36-20-00 AND 30-10-00. REMOVED THE RH WING LEADING EDGE ASSY AND INSPECTED THE WIRING, LOOKING FOR DESCREPACIES WITH WIRING AND FOUND THAT THE PIN IN SP2WK WAS NOT PROPERLY SEATED IN THE SPLICE AND THAT IT HAD THE INSULATION EXPOSED ABOVE THE SPLICE. REMOVED AND REPLACED THE PIN AT SPLICE SP2WK REFERENCING THE APPLICABLE STEPS IN ESPM 20-16-00. FOUND THERMAL SWITCH S24WK HAD THE GROUNDING WIRE COMING OFF THE SWITCH. REMOVED AND REPLACED THE WING OVERHEAT THERMAL SWITCH S24WK REFERENCING THE APPLICABLE STEPS IN AMM 36-21-07. WHEN REMOVING THE RH WING LEADING EDGE, WHILE REMOVING THE CLAMP FOR THE PICCOLO TUBE AT W.S. 139.54 FOUND CLAMP LOOSE. REMOVED AND REPLACED THE ANTI-ICE DUCT CLAMP AT W.S. 139.54 REFERENCING THE APPLICABLE STEPS IN AMM 30-11-41. WITH THE LEADING EDGE REMOVED, ALSO INSPECTED THE ALL THE PICCOLO

Part: TRACK — CRACKED (CARGO DOOR) · airframe 35,494 hrs · 33,359 cycles

CARGO DOOR FORWARD TRACK LOWER BRACKET HAS A CRACK (FILED CLOSED) REPLACED CARGO DOOR FORWARD TRACK LOWER BRACKET IN REFERENCE TO CRJ 200 SRM 51-42-06

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 32,995 hrs · 31,055 cycles

CABIN FLOOR BEAM BETWEEN FS 473-FS 484, RBL 9 INBOARD FLANGE HAS CORROSION ON UPPER SURFACE. C-CHECK RO 11/24/2020. REPAIRED CABIN FLOOR BEAM BETWEEN FS 473-FS 484 RBL 9 INBOARD FLANGE CORROSION, IAW MHIRJ REO SKY CARD. W&B PROVIDED, FORM 337 IS ATTACHED. REF ATTACHED CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.

Part: RETAINER — CORRODED (RT AILERON) · airframe 32,995 hrs · 31,055 cycles

RT AILERON OUTBOARD HINGE BOLT RETAINER AND HARDWARE CORRODED. C-CHECK RO 11/24/2020. REMOVED AND REPLACED CORRODED RETAINER AND HARDWARE AT RT AILERON OUTBOARD HINGE (NR 4), IAW CRJ-200-AMM.

Part: BONDING WIRE — CORRODED (RT ELEVATOR) · airframe 32,995 hrs · 31,055 cycles

RT ELEVATOR INBOARD HINGE BONDING WIRE HARDWARE IS CORRODED AND OUTBOARD HINGE BOLT AND ANTI ROTATION HARDWARE ARE CORRODED. C-CHECK RO 11/24/2020. REMOVE AND REPLACED CORRODED HARDWARE AT INBOARD HINGE BONDING WIRE AND OUTBOARD HINGE BOLT AND ANTI ROTATION BUSHING, IAW CRJ-200-AMM. BOND CHECK GOOD AT THIS TIME.

Part: BONDING WIRE — CORRODED (LT ELEVATOR) · airframe 32,995 hrs · 31,055 cycles

LT ELEVATOR INBOARD HINGE BONDING WIRE HARDWARE IS CORRODED AND OUTBOARD HINGE BOLT AND ANTI ROTATION HARDWARE ARE CORRODED. C-CHECK RO 11/24/2020. REPLACED LT ELEVATOR INBOARD HINGE BONDING WIRE HARDWARE, OUTBOARD HINGE BOLT AND NUT AND ANTI ROTATION HARDWARE, IAW CRJ200 AMM REF CONTINUATION CARD.

Part: ANGLE — DAMAGED (FUSELAGE) · airframe 32,995 hrs · 31,055 cycles

CLIP P/N: 601R38891-1 AT FS 310 STGR 20L REQUIRES FABRICATION. C-CHECK RO 11/24/2020. FABRICATED NEW CLIP OUT OF MATERIAL S9144-4, IAW CRJ200 SRM AND DWG.

Part: STOP FITTING — CHAFED (PAX DOOR) · airframe 32,995 hrs · 31,055 cycles

PAX DOOR FUSELAGE FWD UPPER PIN STOP FITTING IS CHAFED. C-CHECK RO 11/24/2020. REMOVED AND INSTALLED SERVICEABLE PAX DOOR FUSEALAGE UPPER FWD STOP FITTING, IAW CRJ 200 AMM.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 32,995 hrs · 31,055 cycles

CORROSION ON SEAT TRACKS AT FS 559+4-FS 559+86 WAS FOUND TO BE OUT LIMITS. REQUIRES FABRICATION. C-CHECK RO 11/24/2020. FABRICATED SEAT TRACK FOR LBL AND RBL 9 AT FS 559+4-559+86. REFERENCE CONTINUATION CARD FOR THE WORK PERFORMED.

Part: TRUNNION — DAMAGED (RT MLG) · airframe 32,995 hrs · 31,055 cycles

WHILE WORKING SB601R-57-046 FOUND ONE HOLE TO BE OVERSIZED ON RT TRUNNION. C-CHECK RO 11/24/2020. REPAIRED OVERSIZED FASTENER HOLE ON RT MLG TUNNION, IAW MHIRJ REO. TASK CARD AND FORM M-337 COMPLETED, NO WEIGHT CHANGE.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 32,995 hrs · 31,055 cycles

CLIP ANGLE BETWEEN FS 621 AND FS 625 AT RBL 45 WL 93 IS CRACKED. C-CHECK RO 11/24/2020. REMOVED CRACKED CLIP ANGLE AND REPLACED WITH A SERVICEABLE BETWEEN FS 621 AND FS 625 AT RBL 45 WL 93, IAW CRJ200 SRM. APPLIED PROTECTIVE FINISH, IAW CRJ200 SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 32,995 hrs · 31,055 cycles

CLIP ANGLE BETWEEN FS 621 AND FS 625 AT LBL 45 WL 93 IS CRACKED. C-CHECK RO 11/24/2020. REMOVED CRACKED CLIP ANGLE AND REPLACED WITH A SERVICEABLE BETWEEN FS 621 AND FS 625 AT LBL 45 WL 93, IAW CRJ200 SRM. APPLIED PROTECTIVE FINISH, IAW CRJ200 SRM.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 32,995 hrs · 31,055 cycles

STGR 20L INTERCOSTAL IS CORRODED BETWEEN FS 310 AND FS 319. C-CHECK RO 11/24/2020. REMOVED AND REPLACED STGR 20L INTERCOSTAL BETWEEN FS 310 AND FS 319, IAW CRJ 200 SRM. CW SKY CARD NO WEIGHT CHANGES M-337 IS ATTACHED. REF ATTACHED CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 32,995 hrs · 31,055 cycles

FLOOR SUPPORT BOLT HOLE DOUBLER AT FS 288 LBL 37 IS CORRODED. C-CHECK RO 11/24/2020. REPLACED FLOOR SUPPORT BOLT HOLE DOUBLER AT FS 288 LBL 37. REFERENCE CONTINUATION CARD FOR THE WORK PERFORMED.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 32,995 hrs · 31,055 cycles

LBL 9 FLOOR SEAT TRACK FS 399-FS 409+128 SEGMENT IS CORRODED. C-CHECK RO 11/24/2020. REMOVED AND REPLACED LBL 9 FLOOR SEAT TRACK AT FS 339 TO FS 409+128, IAW CRJ200 AMM. SEE SONTINUATION CARD FOR DETAILS.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 32,995 hrs · 31,055 cycles

RBL 9 FLOOR SEAT TRACK FS 364-FS 399 SEGMENT IS CORRODED. C-CHECK RO 11/24/2020. REMOVED AND REPLACED SEAT TRACK AT RBL 9 FS 364-399. REFERENCE CONTINUATION CARD FOR THE WORK PERFORMED.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 32,995 hrs · 31,055 cycles

FLOOR SUPPORT BOLT DOUBLER AT FS 308 LBL 20 IS CORRODED. C-CHECK RO 11/24/2020. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS, IAW CRJ 200 SRM. REMOVED AND REPLACED FLOOR SUPPORT BOLT DOUBLER AT FS 308, IAW CRJ 200 SRM. REFERENCE CONTINUATION CARD FOR WORK PERFORMED.

Part: FLOORBEAM — CORRODED (CABIN) · airframe 32,995 hrs · 31,055 cycles

FS 349 FLOOR CROSSBEAM IS CORRODED AT RBL 41. C-CHECK RO 11/24/2020. REPAIRED FLOOR SUPPORT CROSSBEAM AT FS 349 RBL 41, IAW BOMBARDIER REO. COMPLETED TASK CARD AND FORM 337, NO WEIGHT CHANGE.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 32,995 hrs · 31,055 cycles

LBL 9 FLOOR SEAT TRACK FS 364-FS 399 SEGMENT IS CORRODED. C-CHECK RO 11/24/2020. REMOVED AND REPLACED SEAT TRACK AT LBL 9 BETWEEN FS 364-FS 399, IAW CRJ-200 AMM.

Part: STRAP — CORRODED (CABIN FLOORBEAM) · airframe 32,995 hrs · 31,055 cycles

FS 559 RBL 27-36 FLOOR BEAM STRAP IS CORRODED. C-CHECK RO 11/24/2020. REMOVED AND REPLACED FLOOR BEAM STRAP AT FS 559 RBL 27 TO 36, IAW CRJ-200 SRM.

Part: STRAP — CORRODED (CABIN FLOORBEAM) · airframe 32,995 hrs · 31,055 cycles

FS 559 LBL 27 TO 36 FLOOR BEAM STRAP IS CORRODED. C-CHECK RO 11/24/2020. REMOVED AND REPLACED LT FLOOR BEAM STRAP AT FS 559 LBL 27 TO 36, IAW CRJ-200 SRM.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 32,995 hrs · 31,055 cycles

FS 559+4-559+86 LBL 9 AND RBL 9 FLOOR SEAT TRACKS HAVE MULTIPLE AREAS OF CORROSION AROUND SCREW HOLES. C-CHECK RO 11/24/2020. REMOVED AND REPLACED SEAT TRACK AT FS 559+4-559+86 LBL 9 AND RBL 9. REFERENCE CONTINUATION CARD FOR WORK PERFORMED.

Part: DOOR SILL — CORRODED (CARGO BAY) · airframe 32,995 hrs · 31,055 cycles

CARGO DOOR SILL HAS SEVERAL AREAS OF CORROSION AROUND SCREW HOLES. C-CHECK RO 11/24/2020. REPAIRED CARGO DOOR SILL, IAW BOMBARDIER REO AND SKY CARD NO WEIGHT CHANGE WAS REQUIRED, M337 FORM HAS BEEN SUBMITTED. REF ATTACHED CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.

Part: BOLT — CORRODED (LT SPOILERON) · airframe 32,995 hrs · 31,055 cycles

LT SPOILERON HINGE BOLT RETENSION ANGLE ATTACH HARDWARE CORRODED AND REQUIRES REPLACEMENT. C-CHECK RO 11/24/2020. REMOVED AND REPLACED LT SPOILERON HINGE BOLT RETENTION ANGLE ATTACHMENT HARDWARE WITH SERVICEABLE HARDWARE, IAW CRJ 200 AMM, SRM.

Part: SCREW — CORRODED (RT SPOILER) · airframe 32,995 hrs · 31,055 cycles

RT FLIGHT SPOILER HINGE BOLT NUT RETENTION ANGLE HARDWARE CORRODED AND REQUIRES REPLACEMENT. C-CHECK RO 11/24/2020. REMOVED AND REPLACED RT FLIGHT SPOILER HINGE BOLT RETENTION ANGLE HARDWARE WITH SERVICEABLE HARDWARE, IAW CRJ 200 AMM AND SRM.

Part: TEE FITTING — CRACKED (FUSELAGE) · airframe 32,995 hrs · 31,055 cycles

RBL 9.00 HAS A CRACKED "T" FITTING ON THE INBOARD SIDE OF BEAM AT FS 461.00. C-CHECK RO 11/24/2020. REMOVED AND REPLACED "T" FITTING AT FS 461.00, IAW CRJ 200 SRM.

Part: ANGLE — CRACKED (INTERCOSTAL) · airframe 32,995 hrs · 31,055 cycles

FS 484.00 INTERCOSTAL CLIPS ARE CRACKED AT LBL 27.00 AND LBL 36.00. C-CHECK RO 11/24/2020. REMOVED, FABRICATED, AND INSTALLED CLIPS AT FS 484 INTERCOSTAL AT LBL 27 AND LBL 36, IAW CRJ 200 SRM AND REO. REFERENCE CONTINUATION CARD FOR WORK PERFORMED.

Part: ANGLE — CORRODED (RT SPOILERON) · airframe 32,995 hrs · 31,055 cycles

RT SPOILERON BOLT RETENTION ANGLES ATTACH HARDWARE CORRODED/RUSTED. C-CHECK RO 11/24/2020. REMOVED AND REPLACED THE ATTACHMENT HARDWARE ON THE RT SPOILERON RETENTION ANGLE WITH SERVICEABLE ATTACHMENT HARDWARE, IAW CRJ 200 AMM, SRM.

Part: ANGLE — CRACKED (INTERCOSTAL) · airframe 32,995 hrs · 31,055 cycles

FS 484.00 INTERCOSTAL CLIP IS CRACKED AT RBL 36.00. C-CHECK RO 11/24/2020. REMOVED CRACKED CLIP AT FS 484 RBL 36, FABRICATED, LOCATED, DRILLED AND INSTALLED REPLACEMENT CLIP IAW REO.

Part: PRESSURE BLKHD — DAMAGED (AFT) · airframe 32,995 hrs · 31,055 cycles

FS 621 BULKHEAD HAS CHAFED RIVET HEAD AT RBL 18 AT APPROXIMATELY WL 82. C-CHECK RO 11/24/2020. REMOVED AND REPLACED FS 621 BULKHEAD RIVET AT RBL 18 AT APPROXIMATELY WL 82, IAW CRJ 200 SRM. REF ATTACHED CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 32,995 hrs · 31,055 cycles

LT SIDE SEAT TRACK FS 364-409+16 SEGMENT IS CORRODED. C-CHECK RO 11/24/2020. LT SIDE SEAT TRACK FS 364-409+16 SEGMENT IS CORRODED. REMOVED SEAT TRACK, LOCATED DRILLED COUNTERSUNKED AND INSTALLED NEW SIDE SEAT RAIL REFERENCE CONTINUATION CARD FOR THE WORK PERFORMED.

Part: FRAME — CORRODED (ZONE 100) · airframe 32,995 hrs · 31,055 cycles

FS 605 FRAME IS CORRODED BETWEEN STGR 20L AND STGR 18R. C-CHECK RO 11/24/2020. REMOVED AND REPLACED FS 605 FRAME BETWEEN STGR 20L AND 20R, IAW CRJ 200 SRM AND SKY CARD. NO WEIGHT CHANGE AND M377 FORM HAS BEEN COMPLETED. REF ATTACHED CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.

Part: FRAME — CORRODED (FUSELAGE) · airframe 32,995 hrs · 31,055 cycles

FS 589 FRAME IS CORRODED BETWEEN STGR 20L AND STRG 18R. C-CHECK RO 11/24/2020. REMOVED AND REPLACED FS 589 FRAME BETWEEN STGR 20L AND STGR 20R, IAW CRJ 200 SRM AND ATTACHED SKY CARD NO WEIGHT CHANGE FORM 337 IS ATTACHED. REF ATTACHED CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.

Part: FLOORBEAM — CRACKED (CABIN) · airframe 32,995 hrs · 31,055 cycles

FS 280 FLOOR CROSSBEAM IS CRACKED AT LBL 12 AND RBL 12. C-CHECK RO 11/24/2020. REPAIRED IAW GREO. COMPLETED TASK CARD AND ATTACHED 337. WEIGHT CHANGE OF 1.25 LBS AT FS 280.

Part: FRAME — CORRODED (FUSELAGE) · airframe 32,995 hrs · 31,055 cycles

FS 333 FRAME IS CORRODED BETWEEN STGR 26L AND STGR 25R. C-CHECK RO 11/24/2020. INSTALLED SERVICEABLE 333 LOWER FRAME BETWEEN STR 26L AND 25R, IAW CRJ 200 SRM. COMPLETED TASK CARD AND ATTACHED COMPLETED FORM 337, NO WEIGHT CHANGE. REFERENCE CONTINUATION CARD FOR WORK PERFORMED.

Part: BOLT — CORRODED (RT AILERON) · airframe 32,995 hrs · 31,055 cycles

RT AILERON INBOARD PCU HARDWARE IS CORRODED INBOARD. C-CHECK RO 11/24/2020. REMOVED AND REPLACED RT INBOARD AILERON PCU MOUNTING BOLTS, IAW CRJ 200 AMM AND REMOVED THE UNSERVICEABLE HARDWARE FOR THE RT INBOARD AILERON PUC OUTPUT LINK AND PLACED SERVICEABLE HARDWARE WITH RT AILERON TO BE INSTALLED WITH IT ON CAMP NR 21230370 JOB: 9800675 OP: 5175.

Part: SKIN — CORRODED (FUSELAGE) · airframe 32,995 hrs · 31,055 cycles

FUSELAGE SKIN FOR WING TO FUSELAGE FAIRINGS 191BB AND 192BB ATTACHMENT AREA IS CORRODED. C-CHECK RO 11/24/2020. REPAIRED FUSELAGE SKIN AT THE WING TO FUSELAGE FAIRINGS 191BB AND 192BB, IAW MHIRJ REO. COMPLETED TASK CARD AND ATTACHED FORM 337, DTA IS DUE WITHIN 12 MONTHS FROM ISSUE OF REO. NO WEIGHT CHANGE.

Part: INTERCOSTAL — CORRODED (BS 333-349)

DURING PAX DOOR HINGE REPLACEMENT FOUND CORROSION ON INTERCOSTAL AT STGR 21 BETWEEN STA 333.00 & STA 349.00. FILED CLOSED RO 9/4/2020. REMOVED AND REPLACED WITH SERVICEABLE INTERCOSTAL P/N 601R31527-19 AT STGR 21 LT BETWEEN STA 333.00 & STA 349.00, REF DWG, SRM.

Part: HINGE — WORN (PAX DOOR) · airframe 32,894 hrs · 30,934 cycles

PAX DOOR FUSELAGE SIDE HINGE WORN TO LIMITS. CAUSING ALIGNMENT PROBLEM FOR PAX DOOR, FILED CLOSED. REMOVED AND REPLACED PAX DOOR HINGE (AIRFRAME SIDE), REFERENCE APPLICABLE STEPS IN SRM. SEE CP 21388140 & CP 21384976 FOR FURTHER MAINTENANCE.

Part: BOLT — CORRODED (RT AILERON) · airframe 32,995 hrs · 31,055 cycles

REMOVE & REINSTALL RT AILERON TO PERFORM REPLACMENT OF AILERON BEARINGS, BUSHINGS, AND HARDWARE PER AMM. USE NEW BOLTS WHEN REINSTALLING AILERON, IAW AMM. COMPLY WITH TASK CARD. C-CHECK RO 11/24/2020. REMOVED & REINSTALLED RT AILERON TO PERFORM REPLACMENT OF AILERON BEARINGS, BUSHINGS, AND HARDWARE PER AMM. USED NEW BOLTS WHEN REINSTALLING AILERON, IAW AMM. COMPLIED WITH TASK CARD.

Part: ANGLE — WEAK (FUSELAGE) · airframe 32,995 hrs · 31,055 cycles

COMPLY WITH REO 601R-53-41-1116 REPAIR & REINFORCEMENT FOR FS 559.00 LOWER CAP ANGLES BL 9.00 & 18.00 LT & RT. C-CHECK RO 11/24/2020. COMPLIED WITH REO REPAIR & REINFORCEMENT FOR FS 559.00 LOWER CAP ANGLES BL 9.00 & 18.00 LT & RT, REF ATTACHED CARD. W&B PROVIDED FORM M337 IS ATTACHED SPECIAL DETAILED INSPECTION, PER NDTM IS DUE AT 40000 FLIGHT CYCLES WITH A REPEAT EVERY 22852 FLIGHT CYCLES CURRENT CYCLES 31055.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 29,629 hrs · 28,106 cycles

CORROSION ON SERVICE DOOR SILL FLOOR PROTECTOR PLATE AROUND UPPER FASTENER HOLES. (C-CHECK) RO: 11/29/2018. REPLACED SERVICE DOOR FLOOR PROTECTOR PLATE REF SRM 51-40-11.

Part: PANEL — CHAFED (RT AILERON) · airframe 29,629 hrs · 28,106 cycles

RT AILERON PANEL 699AB IS CHAFED. (C-CHECK) RO: 11/29/2018. BLENDED CHAFED TO A SMOOTH CONTOUR REF SRM 51-12-00.

Part: PANEL — CHAFED (RT AILERON) · airframe 29,629 hrs · 28,106 cycles

RT AILERON PANEL 699BB IS CHAFED (C-CHECK) RO: 11/29/2018. BLENDED CHAFED TO A SMOOTH CONTOUR REF REO 601R-57-61-661.

Part: HINGE — GOUGED (FUSELAGE) · airframe 29,629 hrs · 28,106 cycles

PAX DOOR HINGE FUSELAGE SIDE AFT LANDING GOUGED. (C-CHECK) RO: 11/29/2018. REPAIRED PAX DOOR FUSELAGE SIDE HINGE REF REO 601R-53-21-3036.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 29,629 hrs · 28,106 cycles

CARGO DOOR SILL JUST INSIDE DOOR CUTOUT HAS CORROSION . (C-CHECK) RO: 11/29/2018. REMOVED AND INSTALLED NEW CARGO DOOR SILL REF REO 601R-53-61-1574.

Part: STOP FITTING — CORRODED (FUSELAGE) · airframe 29,629 hrs · 28,106 cycles

CARGO DOOR STOP FITTINGS (2 EA) HAVE CORROSION. (C-CHECK) RO: 11/29/2018. REMOVED AND INSTALLED NEW CARGO DOOR STOP FITTINGS WITH NEW HARDWARE REF SRM 51-41-02.

Part: DOOR SILL — CRACKED (FUSELAGE) · airframe 29,629 hrs · 28,106 cycles

PASSENGER DOOR UPPER LT SILL IS CRACKED. (C-CHECK) RO: 11/29/2018. REPAIRED PASSENGER DOOR UPPER LT SILL REF SRM 53-00-03 AND REO 601R-53-21-3033.

Part: SHROUD — CHAFED (LT AILERON) · airframe 29,629 hrs · 28,106 cycles

LT AILERON UPPER L/E CHAFED. (C-CHECK) RO: 11/29/2018. BLENDED & REMOVED CHAFE MARKS ON LT AILERON UPPER LEADING EDGE SHROUD AS REQUIRED PER REO 670-57-61-194.

Part: CUP — CORRODED (PAX DOOR) · airframe 29,629 hrs · 28,106 cycles

PASSENGER DOOR LOWER SILL, FWD HAND RAIL ARM CUP HAS CORROSION. (C-CHECK) RO: 11/29/2018. REMOVED AND REPLACED PAX DOOR, FWD HANDRAIL ARM CUP AND CLEAT REF SRM 51-42-06.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 29,629 hrs · 28,106 cycles

PASSENGER DOOR LOWER SILL ANGLE HAS CORROSION. (C-CHECK) RO: 11/29/2018. REMOVED AND INSTALLED NEW PASSENGER DOOR LOWER SILL ANGLE REF SRM 51-42-06.

Part: PANEL — CHAFED (RT WING) · airframe 29,629 hrs · 28,106 cycles

ZONE 600 PANEL 699CB IS CHAFED. (C-CHECK) RO: 11/29/2018. R&R PANEL 699CB REF 51-40-11 AND 51-21-16.

Part: PANEL — CHAFED (LT AILERON) · airframe 29,629 hrs · 28,106 cycles

LT AILERON LOWER FIXED CENTER AND O/B L/E CHAFED. (C-CHECK) RO: 11/29/2018. REMOVED AND REPLACED DAMAGED LT AILERON LOWER FIXED PANEL REF SRM 51-42-06,

Part: PANEL — CHAFED (LT AILERON) · airframe 29,629 hrs · 28,106 cycles

LT AILERON PANEL 599CB IS CHAFED. (C-CHECK) RO: 11/29/2018. REMOVED AND REPLACED LT AILERON PANEL 599CB REF SRM 51-40-11.

Part: SHROUD — CHAFED (RT AILERON) · airframe 29,629 hrs · 28,106 cycles

RT AILERON UPPER L/E CHAFED. (C-CHECK) RO: 11/29/2018. BLENDED & REMOVED CHAFE MARKS ON RT AILERON UPPER LEADING EDGE SHROUD AS REQUIRED PER REO 670-57-61-194.

Part: AILERON — CHAFED (RT WING) · airframe 29,629 hrs · 28,106 cycles

RT AILERON LOWER CENTER FIXED L/E CHAFED. (C-CHECK) RO: 11/29/2018. BLENDED OUT CHAFFING DAMAGE ON RT AILERON LOWER CENTER FIXED L/E REF SRM 51-12-00.

Part: PAN — GOUGED (CARGO DOOR) · airframe 29,629 hrs · 28,106 cycles

CARGO DOOR HANDLE PAN GOUGED. (C-CHECK) RO: 11/29/2018. REMOVED AND REPLACED CARGO DOOR HANDLE HOUSING REF SRM 51-42-21.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 29,629 hrs · 28,106 cycles

SERVICE DOOR CUTOUT FLOOR SUPPORT ANGLE AT FS 319.7 HAS CORROSION. (C-CHECK) RO: 11/29/2018. REMOVED & REPLACED CORRODED FLOOR SUPPORT ANGLE.

Part: PANEL — CHAFED (LT WING) · airframe 29,629 hrs · 28,106 cycles

LT WING PANEL IS CHAFED. (C-CHECK) RO: 11/29/2018. REPAIRED LT WING PANEL REF SRM 51-40-11.

Part: PANEL — CHAFED (LT WING) · airframe 29,629 hrs · 28,106 cycles

LT WING PANEL 599AB IS CHAFED. (C-CHECK) RO: 11/29/2018. REPAIRED LT WING PANEL 599AB REF SRM 51-40-11.

Part: CAP — DENTED (PAX DOOR) · airframe 29,629 hrs · 28,106 cycles

PAX DOOR FWD AND AFT UPPER CORNER CAPS DENTED. (C-CHECK) RO: 11/29/2018. REPAIRED PAX DOOR AFT UPPER CORNER CAP REF REO 670-52-11-159. REPLACED PAX DOOR FWD UPPER CORNER CAP REF SRM 51-42-06.

Part: DOOR — DENTED (CABIN) · airframe 29,629 hrs · 28,106 cycles

FORWARD EDGE OF MAIN CABIN DOOR DENTED. (C-CHECK) RO: 11/29/2018. REPAIRED UPPER FORWARD EDGE OF MAIN CABIN DOOR REF REO 601R-52-11-2637.

Part: FLAP SYSTEM — FAILED (TE FLAPS) · airframe 28,481 hrs · 26,915 cycles

FLAP FAIL CAUTION MESSAGE EN-ROUTE, WITH FLAPS IN THE ZERO. DECLARED AN EMERGENCY. RESET AND OPERATED FLAPS AND COMPLETED AN AD. OK TO CONTINUE IN SERVICE..

Part: RETAINER — CHAFED (PAX DOOR SEAL) · airframe 25,664 hrs · 23,967 cycles

PAX DOOR SEAL RETAINER CHAFED IN MULTIPLE PLACES AT THE HALF HINGE AREA. REPLACED THE PAX DOOR SEAL RETAINER IAW REO. OPS CHECKED GOOD.

Part: TRANSMITTER — UNKNOWN (RADIO SYS) · airframe 23,639 hrs · 22,049 cycles

INFLIGHT LOST COMM 1 & 2 UNABLE TO TRANSMIT OR RECEIVE. RTU'S REMAINED ON. COULD NOT DUPLICATE.

Part: BULKHEAD — SCRATCHED (BS 621) · airframe 22,173 hrs · 20,708 cycles

THERE HAVE BEEN PREVIOUS REPAIRS TO THE AFT BAGGAGE BAY BULKHEAD, BS 621, RBL 18.00. IT HAS BEEN SCRATCHED IN THE CENTER BY A SCREW. C-CHECK, RO 2/10/15, REMOVED DAMAGED DOUBLER AND INSTALL FABRICATED DOUBLER TO THE AFT BAGGAGE BAY BULKHEAD, FSD 621, RBL18.00, REF REO PRESSURE CHECK GOOD REF AMM. COMPLIED WITH ST 51-900-1003.

Part: BULKHEAD — SCRATCHED (BS 621) · airframe 22,173 hrs · 20,708 cycles

THERE HAVE BEEN PREVIOUS REPAIRS TO THE AFT CARGO BAY BULKHEAD, BS 621, RBL 27.50. IT HAS BEEN SCRATCHED IN THE CENTER BY A SCREW. C-CHECK, RO 2/10/15, REMOVED DAMAGED DOUBLER AND INSTALLED NEW FABRICATED DOUBLER TO THE AFT BAGGAGE BAY BULKHEAD FS621, RBL27.50 REF REO PRESSURE CK, GOOD REF AMM. COMPLIED WITH ST 51-900-1003.

Part: BULKHEAD — SCRATCHED (BS 621) · airframe 22,173 hrs · 20,708 cycles

THERE HAVE BEEN PREVIOUS REPAIRS TO THE AFT BAGGAGE BAY BULKHEAD, BS 621, LBL 27.50. IT HAS BEEN SCRATCHED IN THE CENTER BY A SCREW. C-CHECK, RO 2/10/15, REMOVED DAMAGE AND INSTALLED A NEW FABRICATED DOUBLER TO THE AFT BAGGAGE BAY BULKHEAD, FS621, LBL 27.50 REF REO PRESSURE CHECK GOOD REF AMM. COMPLIED WITH ST 51-900-1003.

Part: BULKHEAD — SCRATCHED (BS 621) · airframe 22,173 hrs · 20,708 cycles

THERE HAVE BEEN PREVIOUS REPAIRS TO THE AFT BAGGAGE BAY BULKHEAD, BS 621, LBL 18.00. IT HAS BEEN SCRATCHED IN THE CENTER BY A SCREW. C-CHECK, RO 2/10/15, REMOVED DAMAGED DOUBLER AND INSTALLED FABRICATED DOUBLER TO THE AFT BAGGAGE BAY BULKHEAD, FS621, LBL18.00, REF REO PRESSURE CHECK GOOD REF AMM. COMPLIED WITH ST 51-900-1003.

Part: DOOR SILL — CORRODED (CARGO BAY) · airframe 22,173 hrs · 20,708 cycles

CARGO DOOR SILL HAS CORROSION AROUND THE SCREW HOLES. FLAGGED. R & R BAGGAGE BAY DOOR SILL IAW REO. FOUND SILL TO BE OUT LIMITS OF REO AFTER BLENDING, WEIGHT OF PARTS, OFF 0.5 LBS AND THE WEIGHT OF PARTS, ON 0.52LBS, WEIGHT ADDED .02LBS. COMPLIED WITH ST 51-900-1003.

Part: BULKHEAD — SCRATCHED (BS 621) · airframe 22,173 hrs · 20,708 cycles

THERE HAVE BEEN PREVIOUS REPAIRS TO THE AFT BAGGAGE BAY BULKHEAD, BS 621, RBL 36.20. IT HAS BEEN SCRATCHED IN THE CENTER BY A SCREW. C-CHECK, RO 2/10/15, REMOVED DAMAGED DOUBLER AND INSTALLED FABRICATED DOUBLER TO THE AFT BAGGAGE BAY BULKHEAD, FS621, RBL36.20, REF REO. PRESSURE CHECK GOOD REF AMM. COMPLIED WITH ST 51-900-1003.

Part: BULKHEAD — CRACKED (BS 621) · airframe 22,173 hrs · 20,708 cycles

CRACK NOTED ON AFT PRESSURE BULKHEAD, FWD FACE, BENEATH LINER SUPPORT ASSY LOCATED ON RBL 9 APPROXIMATELY WL80 NEAR FLOOR LEVEL. C-CHECK, RO 2/10/15, REMOVED DAMAGED PORTION AND INSTALLED FABRICATED REPAIR PARTS ON AFT PRESSURE BULKHEAD, FWD FACE, BENEATH LINER SUPPORT ASSY LOCATED ON RBL9 APPROXIMATELY WL80 NEAR FLOOR LEVEL IAW REO PRESSURE CHECK GOOD REF AMM. COMPLIED WITH ST 51-900-1003.

Part: ACTUATOR — MALFUNCTIONED (THRUST REVERSER) · airframe 21,423 hrs · 20,111 cycles

DURING FLIGHT, RECEIVED RT THRUST REVERSER UNLOCKED CAUTION MESSAGE. CLEANED STOW AND DEPLOY SWITCH, LUBED THRUST REVERSER BALL SCREW ACTUATORS AS REQUIRED. OPS CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (FLASHLIGHT) · airframe 20,909 hrs · 19,738 cycles

F/A FLASHLIGHT BATTERY INDICATOR LIGHT NOT FLASHING. R & R F/A'S FLASHLIGHT BATTERY. OPS CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 20,872 hrs · 19,710 cycles

EMERGENCY LIGHT PODS 2 AND 4 ARE INOPERATIVE. R & R NR 4 BATTERY PACK IAW AMM.

Part: BULKHEAD — CRACKED (BS 202) · airframe 20,806 hrs · 19,662 cycles

CRACK NOTED BY NDT ON BS 202 BULKHEAD AT PARK BRAKE CABLE INTERFACE. C-CHECK, BULKHEAD REPAIRED IAW REO AND AMM.

Part: PANEL — CHAFED (LT AILERON) · airframe 20,806 hrs · 19,662 cycles

LEFT WING AILERON LOWER OTBD PANEL CHAFED. C-CHECK, R & R THE LT WING AILERON PANEL IAW SRM.

Part: LENS — CRACKED (EMERGENCY LIGHT) · airframe 20,806 hrs · 19,662 cycles

EMERGENCY EXIT SIGN LENS ON CEILING PANEL 263ALC IS CRACKED. C-CHECK, R & R THE LENS IAW AMM.

Part: SEAT TRACK — CORRODED (BS 394-409) · airframe 20,806 hrs · 19,662 cycles

SEAT TRACK RBL 9 BS 394-409 CORRODED BEYOND LIMITS. C-CHECK, REMOVED SEAT TRACK IAW AMM AND SRM.

Part: SEAT TRACK — CORRODED (BS 364-390) · airframe 20,806 hrs · 19,662 cycles

SEAT TRACK RBL 9 BS 364-390 CORRODED. C-CHECK, R & R SEAT TRACK IAW AMM.

Part: LIGHT — CRACKED (CABIN) · airframe 20,806 hrs · 19,662 cycles

EMERGENCY LIGHT CRACKED. C-CHECK, REPLACED EMERGENCY LIGHT IAW AMM.

Part: SEAT TRACK — CORRODED (BS 364-409) · airframe 20,806 hrs · 19,662 cycles

SEAT TRACK HAS CORROSION AT BS 364 - 409 + 16. C-CHECK, REPLACED IAW SRM.

Part: FLOOR SUPPORT — CRACKED (BS 409-559) · airframe 20,806 hrs · 19,662 cycles

FLOOR SUPPORT BS 409+128 - 559 CRACKED. C-CHECK, R & R IAW SRM.

Part: FLOOR SUPPORT — CRACKED (BS 409-559) · airframe 20,806 hrs · 19,662 cycles

FLOOR SUPPORT BS 409+128 - 559 CRACKED. C-CHECK, R & R IAW SRM.

Part: FLOOR PANEL — DETERIORATED (COCKPIT) · airframe 19,561 hrs · 18,371 cycles

FLOOR PANEL SPONGY AFT OF CENTER CONSOLE IN FLIGHT COMPARTMENT. REPAIRED IAW REO 601R-53-00-170, REV "A". MAJOR REPAIR IAW GMM 3-3.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 17,991 hrs · 16,772 cycles

LEFT NR 3 EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP IAW AMM 33-51-21, OPS CHECKED GOOD.

Part: LAMP — BURNED OUT (EMERGENCY LIGHTS) · airframe 17,861 hrs · 16,640 cycles

RT EXTERIOR NR 8 EMERGENCY LIGHT INOPERATIVE. LAMPED EMERGENCY LIGHT IAW AMM 33-51-21, OP'S CHECKED GOOD.

Part: FLOOR SUPPORT — CORRODED (BS 499) · airframe 17,814 hrs · 16,593 cycles

RIGHT UPPER SURFACE OF RT PRESSURE FLOOR SUPPORT IS CORRODED AROUND ONE FASTENER LOCATION AT APPROX FS 499.00. C/W OF REO 601R-53-41-666.

Part: BULKHEAD — CRACKED · airframe 17,774 hrs · 16,554 cycles

FOUND REAR PRESSURE BULKHEAD WEB HAS INDICATION NOTED AT LBL 27.50, WL 130, APPROX .4" IN LENGTH 100 PERCENT FSH FAILED NDT INSPECTON. C/W ECTC REO 601R-53-61-1541, AND MET ALL THE REQUIREMENTS OF REO 601R-53-61-1541 REV D, DATED 10/31/11.

Part: POST — CRACKED · airframe 17,774 hrs · 16,554 cycles

FOUND FS 409+128 VERTICAL POST BL 0.0 RT SIDE HAS INDICATION NOTED APPROX .2 INCHES IN LENGTH 70 PERCENT FSH AT AFT FLANGE RADIUS WL 69.0. FAILED NDT INSPECTION. REMOVED VERTICAL POST IAW SRM 51-42-06 AT BL 0. LOCATED AND DRILLED NEW SERVICEABLE VERTICAL POST IAW SRM 51-40-11. INSTALLED NEW SERVICEABLE VERTICAL POST IAW REO 601R-53-41-889. COMPLIED WITH EC/TC REO 601R-523-41-889.

Part: BULKHEAD — CRACKED · airframe 17,774 hrs · 16,554 cycles

FOUND REAR PRESSURE BULKHEAD WEB THAT SURROUNDS THE LINTEL ATTACHMENT FITTING HAS INDICATION NOTED APPROX .2" IN LENGTH 90 PERCENT FSH FAILED NDT INSPECTION. REPAIRED IAW EC/TC REO 601R-53-61-1230 AND REO 601R-53-61-1230, REV F DATED 10/31/2011 AS WRITTEN. SDR CLOSED.

Part: POST — CRACKED (BS 409) · airframe 17,774 hrs · 16,554 cycles

FOUND FS 409+128 VERTICAL POST RBL 18.0 OTBD SIDE HAS INDICATION NOTED APPROX .2" IN LENGTH 50 PERCENT FSH AT AFT FLANGE RADIUS WL 69.0. FAILED NDT INSPECTION. REMOVED VERTICAL POSTS IAW SRM 51-42-06. LOCATED AND DRILLED NEW SERVICEABLE OTBD VERTICAL POST IAW SRM 51-40-11. COMPLIED WITH EC/TC REO 601R-53-41-889 AND MET ALL THE REQUIREMENTS OF REO 601R-523-41-889 REV A. FOUND TO BE SATISFACTORY.

Part: ANGLE — CRACKED (BS 559) · airframe 17,814 hrs · 16,593 cycles

FOUND FS 559 BULKHEAD RT SIDE CAP ANGLE HAS INDICATION NOTED AT RBL 18.0 APPROX .2" IN LENGTH 50 PERCENT FSH. FAILED NDT INSPECTION. C/W ECTC REO 601R-53-41-609 02 AND MET ALL THE REQUIREMENTS OF REO 601R-53-41-609 REV B, SHEET 3 TO 11 ARE AT REV A OF REO, DEVIATION E.

Part: ANGLE — CRACKED (BS 484) · airframe 17,814 hrs · 16,593 cycles

LEFT FS 484 ANGLES ARE CRACKED INBD OF LBL 36 & OTBD OF LBL 27. COMPLIED WITH REO 601R-53-41-059.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 17,774 hrs · 16,554 cycles

FS 280 ANGLES ARE CRACKED AT RBL 9 AND LBL 9 INBD AND OTBD SIDES. REMOVED CRACKED ANGLES . REPLACED WITH NEW ANGLES IAW SRM 51-42-21. SDR CLOSED.

Part: ANGLE — CORRODED (BS 484) · airframe 17,814 hrs · 16,593 cycles

RIGHT FS 484 ANGLE IS CRACKED INBD OF RBL 36. COMPLIED WITH REO 601R-53-41-059.

Part: ANGLE — CRACKED (BS 625) · airframe 17,814 hrs · 16,593 cycles

LT AND RT UPPER FS 625 OBLIQUE ANGLES ARE CRACKED. R & R LT AND RT FS 625 OBLIQUE ANGLES IAW SRM 51-42-21.

Part: SUPPORT FITTING — CRACKED (WINDSHIELD) · airframe 17,814 hrs · 16,593 cycles

LEFT WINDSHIELD SIDE POST SUPPORT FITTING IS CRACKED. R & R SIDE POST SUPPORT FITTING IAW SRM 51-42-21.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 16,831 hrs · 15,512 cycles

CAPTAIN'S FLASHLIGHT INOPERATIVE. INSTALLED NEW FLASHLIGHT. OPS CHECKED GOOD IAW AMM 25-61-04.

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 16,466 hrs · 15,096 cycles

EMERGENCY EXIT SIGN ON FWD SIDE OF THE SERVICE DOOR MOUNTED TO GALLEY IS MISSING THE COVER THAT INDICATES "EXIT". INSTALLED A NEW EXIT LIGHT COVER IAW AMM 33-51-10. (SDR CLOSED)

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 16,165 hrs · 14,769 cycles

CEILING EMERGENCY LIGHTS INOPERATIVE AT THE MID (NR2) POSITION AND AFT (NR 4) POSITION IN CABIN. RELAMPED IAW AMM 33-51-16. OPS CHECKED GOOD.

Part: ANGLE — CRACKED (PAX DOOR) · airframe 15,788 hrs · 14,337 cycles

CRACK UNDER ASD DOOR SKIN AT THE AFT RADIUS REF WO 203521, N/R 7. COMPLIED WITH REINSPECTION OF CRACK UNDER ASD DOOR SKIN AT THE AFT RADIUS IAW REO 601R-52-11-1360. CRACK WITHIN LIMITS OK FOR SERVICE.

Part: BATTERY PACK — UNSERVICEABLE (EMERGENCY LIGHT) · airframe 15,534 hrs · 14,058 cycles

CABIN CEILING EMERGENCY LIGHT 2ND FROM FRONT INOPERATIVE. R & R NR 4 EMERGENCY BATTERY PACK IAW AMM 33-51-04. R & R NR 4 EMERGENCY BATTERY PACK IAW AMM 33-51-04.

Part: BATTERY PACK — UNSERVICEABLE (EMERGENCY LIGHT) · airframe 15,534 hrs · 14,058 cycles

FUSELAGE RT AFT MOST EXTERNAL EMERGENCY LIGHT INOPERATIVE. R & R NR 4 EMERGENCY BATTERY PACK IAW AMM 33-51-04.

Part: SIGN — BROKEN (EMERGENCY LIGHT) · airframe 15,242 hrs · 13,746 cycles

WARDROBE VERTICAL EMERGENCY EXIT SIGN HAS BROKEN FRAME. R & R WARDROBE VERTICAL EMERGENCY EXIT SIGN IAW AMM 33-51-10. OPS CK GOOD.

Part: SKIN — CRACKED (FUSELAGE) · airframe 15,044 hrs · 13,518 cycles

CRACKED UNDER ASD DOOR SKIN AT THE AFT RADIOUS REF. NO FUTHER DEFECTS NOTED IAW REO601R-52-11-1360.

Part: SKIN — CRACKED (DOOR) · airframe 15,044 hrs · 13,518 cycles

CRACK UNDER ASD ON DOOR SKIN AT THE AFT RADIUS. (OPEN) WORK COMPLETED IAW COMPLIED WITH TEMP DISPOSITION REO 601R-52-11-1360, REV A, ZONE 5, CRACK IS AT .775".

Part: A/C PACK — ODOR · airframe 13,725 hrs · 12,012 cycles

ON CLIMB OUT,THRU 10,000, EXPIRIENCE AN ACRID ODOR LIKE BURNING PLASTIC. NEVER SAW ANY SMOKE AND THE F/A COULD SMELL IT ALSO AT STATION, NO ODOR IN THE PAX COMPARTMENT. (AIR CONDITIONING PACKS (LT PACK)( AIR CONDITIONING PACKS (LT PACK) (ITEM RESOLVE UNDER MDDR: 568045-1) R & R LT PACK ACM IAW AMM 21-51-10. OPS AND LEAK CHECK OK. DEFER CLEARED. PLACARD REMOVED.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 13,361 hrs · 11,590 cycles

RT OVERWING FWD EMERGENCY LIGHT INOP. R & R BULB IAW AMM 33-51-21, OPS CK GOOD. R & R BULB IAW AMM 33-51-21. OPS CK GOOD.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 13,361 hrs · 11,590 cycles

CABIN NR 3 CEILING EMERG LIGHT INOP AND MISSING LENS. R & R EMERGENCY LIGHT BULB AND LENS IAW AMM 32-51-16. OPS CK GOOD. R & R EMERGENCY LIGHT BULB AND LENS IAW AMM 32-51-16. OPS CK GOOD. (CLOSED)

Part: SUPPORT ANGLE — CRACKED (NR 2 NACELLE) · airframe 12,945 hrs · 11,106 cycles

NR 2 ENG FAIRING SUPPORT ANGLE CRACKED AFT OF FWD YOKE AT 2 O'CLOCK POSITION. REMOVED AND REINSTALLED NR 2 ENG FAIRING SUPPORT ANGLE IAW CRJ 200 SRM 51-42-20. (SDR CLOSED)

Part: ANGLE — CRACKED (PAX DOOR) · airframe 12,945 hrs · 11,106 cycles

PAX DOOR AFT SIDE " L " ANGLE CRACKED IN MIDDLE OF DOOR. REPAIRED PAX DOOR AFT SIDE "L" ANGLE IAW REO 601R-52-11-513.

Part: INTERCOSTAL — CRACKED (PAX DOOR) · airframe 12,945 hrs · 11,106 cycles

PAX DOOR LWR AFT CORNER UNDER CORNER CAP A ' L ' ANGLE IS CRACKED. REMOVED INTERCOSTAL IAW SRM 51-42-11. LOCATED / DRILLED NEW INTERCOSTAL IAW SRM 51-42-06 AND INSTALLED NEW INTERCOSTAL IAW SRM 51-42-06.

Part: PLACARD — PEELING (PAX DOOR) · airframe 12,945 hrs · 11,106 cycles

PAX DOOR EXIT SIGN CORNER PEELING. R & R PLACARD REF MM 11-30-00 PG'S 401, 402.

Part: PLACARD — DAMAGED (ESCAPE HATCH) · airframe 12,945 hrs · 11,106 cycles

CREW ESCAPE HATCH EXIT PLACARD FADED. R & R CREW ESCAPE HATCH PLACARD IAW MM 11-20-00 PG 401 THRU 404.

Part: FAIRING — BROKEN (NR 1 ENG STANG) · airframe 12,945 hrs · 11,106 cycles

NR 1 ENGINE TOP STANG FAIRING BROKEN. RECEIVED NEW NR1 ENGINE TOP STANG FAIRING PN 228-50253-805, TAG AB0166 TO BE INSTALLED ON W/O 1005869 CN 9000-0001.

Part: PLACARD — MISSING (AIRSTAIR DOOR) · airframe 12,657 hrs · 10,789 cycles

EXIT DECAL MISSING AIRSTAIR DOOR. INSTALLED NEW PLACARD PER AMM 11-20-00.

Part: CABLE — BINDING (PAX DOOR) · airframe 11,278 hrs · 9,362 cycles

PAX DR WILL NOT OPEN. CABLES ON DOOR APPEAR TO BE BINDING ON SOMETHING. IT TOOK SEVERAL ATTEMPTS OF CLOSING AND OPENING THE DOOR BEFORE IT FINALLY OPENED. ( PASSENGER DOOR POWER ASSIST SYS )

Part: FLOOR SUPPORT — CRACKED (FUSELAGE)

RT FS 621.00 FLOOR SUPPORT ANGLE IS CRACKED IN OUTBOARD RADIUS. RESOLVED ON W/O 90038 TASKCARD N/R 00181. REPAIRED RT FS 621.00 FLOOR SUPPORT ANGLE IAW REO 601R-53-61-117 REV C STEPS 1-7. REQUIRES TOP COAT. APPLIED TOP COAT AS NEEDED IAW CRJ 200 SRM 51-25-01. PRESSURE CHECK DUE. PERFORMED LEAK CHECK OF RT 621.00 FLOOR SUPPORT ANGLE IAW CRJ AMM TASK 21-32-00-863-801. NO LEAKS NOTED AT THIS TIME. C/W ASA REO 601R-53-61-117. [SUPPLEMENTAL SDR CLOSED 6/24/08] (A)

Part: FLOOR SUPPORT — CRACKED (FUSELAGE)

LT FS 621.00 FLOOR SUPPORT ANGLE IS CRACKED IN OUTBOARD RADIUS. RESOLVED ON W/O 90038 TASKCARD N/R 00182. REPAIRED LT FS 621.00 FLOOR SUPPORT ANGLE IAW REO 610R-53-61-117 REV C STEPS 1-7. REQUIRES TOP COAT. APPLIED TOPCOAT AS NEEDED IAW CRJ 200 SRM 51-25-01. LEAK CHECK DUE. PERFORMED LEAK CHECK OF LT 621.00 FLOOR SUPPORT ANGLE IAW CRJ AMM TASK 21-32-00-863-801. NO LEAKS NOTED AT THIS TIME. C/W ASA REO 610R-53-61-117. [SUPPLEMENTAL SDR CLOSED 6/24/08] (A)

Part: ANCHOR FITTING — CRACKED (PAX DOOR)

THE AFT PAX DOOR ANCHOR FITTING IS CRACKED AND SWIVEL FITTING HOLE ELONGATED. REMOVED AND REPLACED PAX DOOR AFT ANCHOR FITTING ASSY WITH A NEW SERVICEABLE ANCHOR FITTING ASSY IAW CRJ 200 MM 52-11-17-400-804 STEP 2A-2B (3) CRJ 200 MM 52-11-17-400-804 CLOSEOUT DUE. COMPLIED WITH CLOSEOUT (STEP 3) IAW CRJ 200 AMM 52-11-17-400-804. [SUPPLEMENTAL SDR CLOSED 6/24/08] (A)

Part: PLACARD — WORN (PAX DOOR) · airframe 8,838 hrs · 7,079 cycles

THE PAX DOOR EXIT PLACARD IS WORN. REMOVED AND REPLACED WORN PAX DOOR EXIT PLACARD WITH A NEW EXIT PLACARD IAW CRJ AMM TASK 11-20-00-400-801. SUPPLEMENTAL SDR CLOSED 6/19/08.

Part: HANDLE — BENT (PAX DOOR) · airframe 8,838 hrs · 7,079 cycles

THE PAX DOOR EXTERIOR HANDLE IS CRACKED AND THE FLAP HANDLE IS BENT. REMOVED AND REPLACED CRACKED PAX DOOR OUTER HANDLE WITH A NEW SERVICEABLE OUTER HANDLE IAW BOMBARDIER SB 601R-52-119 REV. A. REMOVED AND REPLACED BENT/CRACKED PAX DOOR OUTER HANDLE FLAP WITH A NEW SERVICEABLE FLAP IAW SRM 51-42-06. . OPS TEST DUE AND PAIN REQUIRED. PAINTED HANDLE ON PAX DOOR TO MATCH COLOR SCHEME IAW SRM 51-25-01. OPS TEST DUE. PERFORMED OPS TEST OF THE PAX DOOR OUTER HANDLE IAW AMM 52-11-03-710-802. OPS CHECK IS GOOD AT THIS TIME. (A)

Part: INTERCOSTAL — CRACKED (BS 621-755 S14L) · airframe 8,838 hrs · 7,079 cycles

LT INTERCOSTAL ANGLE BETWEEN FS 621.00 AND FS 755.00 AT STRINGER 14 IS CRACKED APPROX 1 INCH LONG. REMOVED AND REPLACED LT INTERCOSTAL BETWEEN FS 621 AT STRINGER 14 WITH NEW SERVICEABLE INTERCOSTAL IAW BOMBARDIER REO 601R-53-61-422 AND CRJ 200 SRM 51-42-21. SUPPLEMENTAL SDR CLOSED 6/24/08. (A)

Part: INTERCOSTAL — CRACKED (FUSELAGE)

RT INTERCOSTAL ANGLE BETWEEN FA 625.00 AT STR 14 HAS A 1" CRACK. REMOVED AND REPLACED RT INTERCOSTAL WITH NEW SERVICEABLE INTERCOSTAL IAW REO 601R-53-61-422 AND SRM 51-42-21. (A)

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 6,911 hrs · 5,473 cycles

F/A'S FLASHLIGHT INOP.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 6,161 hrs · 4,899 cycles

F/O FLASHLIGHT BATTERIES INOP.

Part: PLACARD — WORN (EMERGENCY EXIT) · airframe 5,980 hrs · 4,765 cycles

RIGHT EMERGENCY EXIT PLACARD WORN.

Part: PLACARD — DAMAGED (OVERWING EXIT) · airframe 5,980 hrs · 4,765 cycles

RIGHT SIDE OVERWING EXIT NIGHT GLOW PLACARD UNREADABLE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 5,952 hrs · 4,743 cycles

CABIN AFT MOST CEILING EMERGENCY LIGHT INOP.

Part: UNKNOWN — LEAKING (HYD SYSTEM) · airframe 5,506 hrs · 4,429 cycles

CLIMBING OUT OF BTR RECEIVED HYD 2 LOW PRESS MSG WITH ZERO QTY AND ZERO PSI. EN ROUTE TO ATL A/C DIVERTED TO GPT. EMERGENCY DECLARED.

Part: WARNING LIGHT — ILLUMINATED (NLG STEERING) · airframe 4,360 hrs · 3,566 cycles

"STEERING INOP" CAUTION MSG APPEARED WHILE CLIMBING THROUGH 6000 FT. (AN EMERGENCY WAS DECLARED)

Part: CLIP — CRACKED (FUSELAGE) · airframe 3,966 hrs · 3,251 cycles

LEFT OUTBOARD 280 CLIP IS CRACKED.

Part: ANCHOR FITTING — CRACKED (FUSELAGE)

DURING A HANGAR INSPECTION, THE PASSENGER DOOR FORWARD ANCHOR FITTING WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR FORWARD ANCHOR FITTING. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)

Part: STEP — CRACKED (PAX DOOR)

DURING A HANGAR INSPECTION IN MCN, THE PASSENGER DOOR BOTTOM STEP, AT THE STAY ROD ATTACH BRACKET, WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE PASSENGER DOOR BOTTOM STEP, AT THE STAY ROD ATTACH BRACKET, IAW CRJ SRM 51-73-00. OPS CHEKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: LAMP — BURNED OUT (EMERGENCY LIGHT)

DURING A GROUND INSPECTION IN VPS, THE CEILING EMERGENCY LIGHT, AT ROW 10, WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN CEILING EMERGENCY LIGHT, AT ROW 10. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT)

DURING A GROUND INSPECTION IN CAE, THE LEFT FORWARD EMERGENCY FLOODLIGHT WAS FOUND TO INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE LEFT FORWARD EMERGENCY FLOODLIGHT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)