N699BR

Part: TRUNNION — DAMAGED (ZONE 500) · airframe 46,708 hrs · 40,409 cycles

WHILE REMOVING LH MLG ASSY DAMAGED OCCURRED ON THE LH MLG MOUNTING TRUNNION. (FILED CLOSED)COMPLIED WITH REO 601R-57-21-3971 DATED: 2025-09-11 PERMANENT DISPOSITION FOR BLENDED GOUGE DAMAGE TO MLG TRUNNION FITTING FWD AND AFT LUG FACES, LHS ALL NDT'S COMPLIED WITH AND NO DEFECTS NOTED AT THIS TIME. COMPLIED WITH TASK CARD 51-900-1003-SKY. COMPLETED M-337.

Part: BUSHING — DAMAGED (ZONE 500) · airframe 46,708 hrs · 40,409 cycles

WHILE REMOVING LH MLG ASSY DAMAGED OCCURRED ON THE LH AFT MLG PIVOT BUSHING. (FILED CLOSED)COMPLIED WITH REO 601R-57-21-3972 DATED: 2025-09-11 TEMPORARY DISPOSITION FOR BLENDING GOUGE DAMAGE ON FACE OF FWD AND AFT MLG TRUNNION BUSHINGS, LHS. ALL NDT'S COMPLIED WITH AND NO DEFECTS NOTED AT THIS TIME. COMPLIED WITH TASK CARD 51-900-1003-SKY. COMPLETED M-337. REF CHILD CAMP FOR MCO FOR PERMANENT REPAIR.

Part: SKIN — DENTED (ZONE 100) · airframe 46,708 hrs · 40,409 cycles

FOUND DENT LOCATED AT APROXIMATELY FS187.5 AND BELOW PANEL 121AL (FILED CLOSED) COMPLIED WITH REO 601R-53-11-4017 DATED: 2025-09-08 REV: -- TEMPORARY DISPOSITION FOR DENTS ON FUSELAGE SKINS BTW FS185.00 - FS193.00 AND STR 23L - STR24L & FS177.00 - FS185.00 AND STR 23R - STR24R. ALL NDT'S COMPLIED WITH AND NO DEFECTS NOTED AT THIS TIME. COMPLIED WITH TASK CARD 51-900-1003-SKY. COMPLETED FORM M-337. REF CHILD FOR MCO FOR PERMANENT REPAIR AND RE-INSPECTS. COMPLETED FORM M-257 AND ENTERED IN THE ADM SYSTEM (#N699BR-9827)

Part: SKIN — DENTED (ZONE 100) · airframe 46,708 hrs · 40,409 cycles

FOUND DENT LOCATED AT APROXIMATELY FS181 AND JUST BELOW PANEL 122AR. (FILED CLOSED) COMPLIED WITH REO 601R-53-11-4017 DATED: 2025-09-08 REV: -- TEMPORARY DISPOSITION FOR DENTS ON FUSELAGE SKINS BTW FS185.00 - FS193.00 AND STR 23L - STR24L & FS177.00 - FS185.00 AND STR 23R - STR24R. ALL NDT'S COMPLIED WITH AND NO DEFECTS NOTED AT THIS TIME. COMPLIED WITH TASK CARD 51-900-1003-SKY. COMPLETED FORM M-337. REF CP 30824628 FOR MCO FOR PERMANENT REPAIR AND RE-INSPECTS. COMPLETED FORM M-257 AND ENTERED IN THE ADM SYSTEM (#N699BR-9828)

Part: ACTUATOR — FAILED (LT MLG) · airframe 44,647 hrs · 38,213 cycles

GEAR DISAGREE WARNING MESSAGE ON APPROACH QUICK CYCLE TO UP POSITION THEN DOWN RESOLVED IT NEXT STEP QRH (FLIGHT 5434 - FILED CLOSED) ON TASK CARD 32-730-764, THE FOLLOWING TOOL WAS ENTERED: TORQUE WRENCH SN- 0606507170 EXPIRATION- 10/12/24.REMOVED AND REPLACED LH MLG SIDE STAY ACTUATOR PER THE AMM 32-32-01 AND TASK CARD 32-730-764. FUNCTIONAL TEST GOOD AT THIS TIME. INSPECTED LH MLG UPLOCK ASSEMBLY AND UPLOCK PIN FOR FREEDOM OF MOVEMENT AND CONDITION. REF. AML 1370671 FOR TROUBLESHOOTING. NO GEAR DISAGREE WARNING MESSAGE APPEARING AT THIS TIME.

Part: LANDING GEAR — WARNING MESSAGE (LEFT) · airframe 44,447 hrs · 37,990 cycles

*CAT II DOWNGRADED*D:LEFT MAIN GEAR DISAGREE ON FINAL AFTER SELECTING GEAR DOWN.C:MEL 32-30-1CAT "A" DUE 1 FLT DAY 04/27/2024MX ACTION COMPLIED WITH. GEAR PINS INSTALLED.LEFT MAIN GEAR DISAGREE ON FINAL AFTER SELECTING GEAR DOWN. (FLIGHT 5535 FILED CLOSED)APR 27, 2024 STATION: IND--REFER TO EAML 1338307 FOR MX ACTIONS AND WORK PERFORMED. PERFORMED MULTIPLE OPERATIONAL CHECKS OF THE EXTENSION AND RETRACTION SYSTEM IAW AMM 32-30-00. OPERATIONAL CHECK GOOD. NO DEFECTS NOTED. COMPLIED WITH CAT II RETURN TO SERVICE TASK CARD 34-220-1021-SKY. AIRCRAFT IS NOW CAT II AUTHORIZED. DMI CLEARED. PLACARDS REMOVED. WAITING FOR SMOD APPROVAL.

Part: WIRE HARNESS — FAULTED (NLG WOW) · airframe 44,120 hrs · 37,620 cycles

ON DESCENT RECEIVED STEERING INOP CAUTION MESSAGE. AFTER APPROXIMATELY 1 MINUTE RECEIVED WOW INPUT CAUTION FOLLOWED BY WOW OUTPUT FAIL STATUS MESSAGE. PERFORMED QRH AND MESSAGES REMAINED. ON GEAR EXTENSION MESSAGES EXTINGUISHED. NORMAL STEERING RESTORED AFTER LANDING. PERFORMED BITE CHECK ON PROXIMITY SENSOR ELECTRONIC UNIT, NO FAULTS FOUND REFERENCE CRJ200 AMM 32-61-01. REMOVED AND REPLACED NOSE LANDING GEAR WOFFW SENSOR HARNESS IN REFERENCE WITH CRJ200 AMM 32-61-05. PERFORMED OPERATIONAL TEST OF PROXIMITY SENSOR SYSTEM IN REFERENCE WITH CRJ200 AMM 32-61-00. PERFORMED NOSE LANDING GEAR EXTENSION/RETRACTION OPERATIONAL TEST IN REFERENCE WITH CRJ200 AMM 32-33-00. PERFORMED NOSE LANDING GEAR STEERING OPERATIONAL CHECK IN REFERENCE WITH CRJ200 AMM 32-51-00. ALL SYSTEMS AND OPS CHECK IS GOOD AT THIS TIME. A/C OK FOR SERVICE.

Part: UNKNOWN — CHAFED (UNKNOWN) · airframe 43,123 hrs · 36,610 cycles

R/WING AILERON UPPER FIXED LEADING EDGE NEEDS TO REPLACE DURING CHAFFED DAMAGE OUT OF LIMIT. (C-CHECK RO 6/25/2023) REPLACED R/WING AILERON UPPER FIXED LEADING EDGE SKIN WITH NEW PN PN CC670-13052-4 PO# T- 7801-00009 REF CRJ 200 SRM 51-42-21 AND BOMBARDIER DWG CC670-13000 REV D, COMPLIED WITH SKY CARD 51-900-1003-SKY STRUCTURAL MAJOR REPAIR.

Part: UNKNOWN — CORRODED (UNKNOWN) · airframe 43,123 hrs · 36,610 cycles

UPON REMOVAL ON JOB 2780195 OP 89 CAMP# 26584720, FOUND L/H ELEVATOR L/E HINGE FITTING ASSY. P/N 600-24043-1 @ ES16.52 TO BE CORRODED IN BEARING BORE. REPLACE HINGE FITTING ASSY. (C-CHECK RO 6/25/2023) REMOVED AND REPLACED L/H ELEVATOR HINGE FITTING ASSY. P/N 600-24043-1 LOCATED ON L/E @ ES16.52 , REF. CRJ200 SRM 51-42-06 , CRJ200 SRM 51-42-21. BOMBARDIER DWG #601R24025, REV. G. AND COMPLIED WITH SKYCARD 51-900-1003-SKY.

Part: UNKNOWN — CORRODED (UNKNOWN) · airframe 43,123 hrs · 36,610 cycles

LEFT HAND FLOOR SEAT RAIL BETWEEN FS399.0 TO FS409.00+4 CORRODED (C-CHECK RO 6/25/2023) REMOVED AND INSTALLED NEW L/H CABIN FLOOR SEAT TRACK RAIL BETWEEN FS 399 TO FS 409.00+4 REF CRJ-200-AMM 53-01-11-000-802 AND CRJ-200-AMM 53-01-11-400-802. SEE CONTINUATION CARD FOR DETAILS

Part: UNKNOWN — CORRODED (UNKNOWN) · airframe 43,123 hrs · 36,610 cycles

LEFT HAND FLOOR SEAT RAIL BETWEEN FS364 TO FS399.0 CORRODED (C-CHECK RO 6/25/2023) REMOVED AND INSTALLED NEW L/H CABIN FLOOR SEAT TRACK RAIL BETWEEN FS 364 TO FS 399.0 REF CRJ-200-AMM 53-01-11-000-802 AND CRJ-200-AMM 53-01-11-400-802. SEE CONTINUATION CARD FOR DETAILS

Part: UNKNOWN — CORRODED (UNKNOWN) · airframe 43,123 hrs · 36,610 cycles

RIGHT HAND FLOOR SEAT RAIL BETWEEN FS399.0 TO FS409.00+4 CORRODED (C-CHECK RO 6/25/2023) REMOVED AND INSTALLED NEW RH CABIN FLOOR SEAT TRACK RAIL BETWEEN FS 399.0 TO FS 409.00+4 REF CRJ-200-AMM 53-01-11-000-802 AND CRJ-200-AMM 53-01-11-400-802. SEE CONTINUATION CARD FOR DETAILS

Part: UNKNOWN — CORRODED (UNKNOWN) · airframe 43,123 hrs · 36,610 cycles

SERVICE DOOR LOWER SILL. TOP SIDE OF THE LOWER SILL , UNDER THE FORWARD LOCK FITTING CORRODED. (C-CHECK RO 6/25/2023) REPLACED SERVICE DOOR LOWER SILL ANGLE PN 601R38303-253 PO# T000068450 REF. CRJ200 SRM 51-42-36 REV 39, DATED MARCH 10, 2021, CRJ200 SRM 51-42-06 REV 39, DATED MARCH 10, 2021, CRJ200 SRM 51-42-21 REV 39, DATED MARCH 10, 2021, AND DRAWING 601R38303 REV AR. COMPLIED WITH 51-900-1003-SKY AND PRESSURE CHECKS GOOD. SEE CONTINUATION CARD FOR DETAILS.

Part: UNKNOWN — CORRODED (UNKNOWN) · airframe 43,123 hrs · 36,610 cycles

RH WING TO FUSE/MLG SIDE BRACKET FWD, SEALANT COVERING NUT WAS NOT COMPLETLY SEALED AND APPEARS TO HAVE RUST BLEEDING FROM IT. SEALANT NEEDS TO BE REMOVED FOR INSPECTION. FLAGGED (C-CHECK RO 6/25/2023) REMOVED RH MLG SIDE-BRACE SHAFT FITTING CAP SEAL AND SEALANT AROUND NUT, FOUND INTERGRANULAR CORROSION. BLENDED CORROSION DAMAGE TO THE MLG SIDE BRACE FITTING CENTER SECTION BORE REF CRJ 200 SRM 51-21-06 , AND CRJ 200 AMM 57-21-28-400-801. RECEIVED AND COMPLIED WITH ALL STEPS OF REO 601R-57-21-3762 REV -- DATED 2023-06-09. COMPLIED WITH TASK CARD 51-900-1003-SKY. SEE CONTINUATION FOR FURTHER DETAILS.

Part: UNKNOWN — CORRODED (UNKNOWN) · airframe 43,123 hrs · 36,610 cycles

SEAT TRACK IS CORRODED FS559+112 - 574.00 LBL9 (C-CHECK RO 6/25/2023) REMOVED SEAT TRACK AT FS559+112 - 574.00 LBL9 REF CRJ 200 AMM 53-00-49-000-801. INSTALLED NEW SEAT TRACK.. REF CRJ 200 AMM 53-00-49-400-801. SEE CONTINUATION CARD FOR DETAILS

Part: UNKNOWN — CHAFED (UNKNOWN) · airframe 43,123 hrs · 36,610 cycles

CHAFFING IN SEVERAL AREAS ON LH LOWER WING PLANK AT APPROX WS45 FS513.0 (MARKED) (C-CHECK RO 6/25/2023) REPAIRED LH LOWER WING PLANK AT APPROX WS45 FS513.0 REF REO 601R-57-21-3758 REV -- DATED 2023-05-31 AND REO 601R-57-21-880 REV D DATED 2017-03-06. COMPLIED WITH 51-900-1003-SKY AND LEAK CHECKS GOOD .BLEND ONLY NO WEIGHT CHANGE. SEE CONTINUATION CARD FOR DETAILS

Part: UNKNOWN — DENTED (UNKNOWN) · airframe 43,123 hrs · 36,610 cycles

CARGO DOOR LOWER AFT DR SEAL SUPPORT IS DENTED (C-CHECK RO 6/25/2023) REMOVED AND INSTALLED NEW CARGO DOOR LOWER AFT SEAL DOOR SUPPORT REF CRJ-200 SRM 51-42-06 AND DWG CC670-38702 REV C. COMPLIED WITH 51-900-1003-SKY AND PRESSURE CHECKS GOOD . SEE CONTINUATION CARD FOR DETAILS

Part: UNKNOWN — CHAFED (UNKNOWN) · airframe 43,123 hrs · 36,610 cycles

CHAFFING IN SEVERAL AREAS ON RH LOWER WING PLANK AT APPROX WS45 FS513.0 (MARKED) (C-CHECK RO 6/25/2023) REPAIRED RH LOWER WING PLANK AT APPROX WS45 FS513.0 REF REO 601R-57-21-3758 REV -- DATED 2023-05-31 AND REO 601R-57-21-880 REV D DATED 2017-03-06. COMPLIED WITH 51-900-1003-SKY AND LEAK CHECKS GOOD . BLEND OUT ONLY NO WEIGHT CHANGE SEE CONTINUATION CARD FOR DETAILS

Part: UNKNOWN — CRACKED (UNKNOWN) · airframe 43,123 hrs · 36,610 cycles

CLIP ATTACHED TO FS202 BULKHEAD IN HYD COMPARTMENT AREA IS APPEARS CRACKED (MARKED) (C-CHECK RO 6/25/2023) REMOVED AND INSTALLED NEW REPLACEMENT BRACKET ATTACHED TO FS202 BULKHEAD IN HYD COMPARTMENT.REF CRJ200 SRM 51-42-21,DWG NO:600-33042 REV AB. COMPLIED WITH 51-900-1003-SKY AND PRESSURE CHECK GOOD . SEE CONTINUATION CARD FOR DETAILS

Part: UNKNOWN — CRACKED (UNKNOWN) · airframe 43,123 hrs · 36,610 cycles

RIGHT WHEEL WELL WS48.30 - BATT RIB IS CRACKED AT THE FORWARD AND AFT END. (MARKED) (C-CHECK RO 6/25/2023) REMOVED AND REPLACED RIGHT WHEEL WELL WS48.30 - BATT RIB. REF DRAWING NUMBER 600-10389 REV NC AND CRJ200 SRM 51-42-21 RRESTORED FINISH. REF: CRJ-200 SRM 51-21-16. COMPLIED WITH 51-900-1003-SKY AND M-337. SEE CONTINUE CARD FOR DETAILS

Part: UNKNOWN — CORRODED (UNKNOWN) · airframe 43,123 hrs · 36,610 cycles

LEFT WHEEL WELL WS53.60 - FORWARD END OF THE BATT RIB CHANNEL IS CORRODED. (MARKED) (C-CHECK RO 6/25/2023) REMOVED AND INSTALLED NEW CHANNEL P/N 601R10203-27 ON LH WHEEL WELL WS53.60 PER CRJ 200 SRM 51-42-21 AND DWG # 601R10203 REV -G. COMPLIED WITH 51-900-1003-SKY AND M-337. SEE CONTINUE CARD FOR DETAILS

Part: UNKNOWN — CORRODED (UNKNOWN) · airframe 43,123 hrs · 36,610 cycles

LEFT WHEEL WELL WS53.60 - FORWARD END OF THE BATT RIB DOUBLER IS CORRODED. (MARKED) (C-CHECK RO 6/25/2023) REMOVED AND INSTALLED NEW DOUBLER PN 601R13203-33 PER CRJ 200 SRM 51-42-06 AND DWG # 601R10203 REV -G. COMPLIED WITH 51-900-1003-SKY AND M-337. SEE CONTINUE CARD FOR DETAILS

Part: UNKNOWN — CRACKED (UNKNOWN) · airframe 43,123 hrs · 36,610 cycles

LEFT WING WS48.30 - BATT RIB IS CRACKED. (MARKED) (C-CHECK RO 6/25/2023) REMOVED AND INSTALLED NEW BATT RIB AT WS 48.30 PER CRJ 200 SRM 51-42-21 AND DWG # 601R10203 REV -GCOMPLIED WITH TASK CARD 51-900-1003-SKY

Part: UNKNOWN — CRACKED (UNKNOWN) · airframe 43,123 hrs · 36,610 cycles

LEFT WING WS48.30 - BATT RIB ANGLE IS CRACKED. (MARKED) (C-CHECK RO 6/25/2023) REMOVED AND INSTALLED NEW LH WING AT WS48.30 - BATT RIB ANGLE PER CRJ 200 SRM 51-42-21 AND DWG # 600-10204 REV-K COMPLIED WITH 51-900-1003-SKY AND M-337. SEE CONTINUE CARD FOR DETAILS

Part: UNKNOWN — CRACKED (UNKNOWN) · airframe 43,123 hrs · 36,610 cycles

CRACKED CLEAT AT FS193 STRG16L (C-CHECK RO 6/25/2023) FABRICATED REPAIR CLEAT AT FS 193.00 STR 16 LH 2024 T3 .032 PO#T66202 REF CRJ 200 SRM 51-24-21 AND DRAWING GC215-0094 REV NCREMOVED AND REPLACED CLEAT WITH NEW PART AT FS 193.00 STRG 16 LH REF CRJ 200 SRM 51-42-06 AND DRAWING GC219-1200 REV PCOMPLIED WITH TASK CARD 51-900-1003-SKY

Part: UNKNOWN — CORRODED (UNKNOWN) · airframe 43,123 hrs · 36,610 cycles

PAX DOOR INTERCOSTAL DD4 IS CORRODED MULTIPLE SURFACES (C-CHECK RO 6/25/2023) REMOVED AND INSTALLED NEW PAX DOOR AFT DD4 INTERCOSTAL REF CRJ-200 SRM 51-42-06 AND DWG 601R31702 REV N. PRESSURE CHECK GOOD . COMPLIED WITH 51-900-1003-SKY AND SEE CONTINUATION CARD FOR DETAILS

Part: UNKNOWN — BENT (UNKNOWN) · airframe 43,123 hrs · 36,610 cycles

GROUND AIR CONDITIONING DOOR SILL LANDING FWD AND AFT ARE BENT INWARD (MARKED) (C-CHECK RO 6/25/2023) INSTALLED NEW REPLACEMENT 601R35226-31 FWD LANDING ANGLE FS576.83 STRINGER 22R TO STRINGER 24R REF CRJ200 SRM 51-42-06. DWG 601R35226 REV-N SEE CONTINUATION FOR DETAILS,LEAK CHECK GOOD COMPLIED WITH SKY CARD 51-900-1003-SKY

Part: UNKNOWN — ELONGATED (UNKNOWN) · airframe 43,123 hrs · 36,610 cycles

PAX DOOR HINGE (ACFT. SIDE) HAS MULTIPLE LUG HOLES ELONGATED. (C-CHECK RO 6/25/2023) REMOVED AND INSTALLED NEW HINGE (FUSELAGE SIDE) PN 601R31671-15 REF CRJ 200 SRM 53-21-23 STEP 4.R-U, BOMBARDIER DWG 601R31527 REV AM AND REO 601R-53-21-656 REV A DATED 2017/03/06. COMPLIED WITH 51-900-1003-SKY AND PRESSURE CHECK GOOD. SEE CONTINUATION CARD FOR DETAILS

Part: UNKNOWN — DENTED (UNKNOWN) · airframe 43,123 hrs · 36,610 cycles

DENT ON EXTERIOR SKIN AT FS265 BETWEEN STGR26L-STGR25L (C-CHECK RO 6/25/2023) REPAIRED EXTERIOR SKIN AT FS265 BETWEEN STGR26L-STGR25L REF REO 601R-53-11-3867 REV -- DATED 2023-06-06. COMPLIED WITH 51-900-1003-SKY AND PRESSURE CHECKS GOOD . SEE CONTINUATION CARD FOR DETAILS

Part: UNKNOWN — CORRODED (UNKNOWN) · airframe 43,123 hrs · 36,610 cycles

PAX DOOR FORMER SECTION @ FS 313.56 CORRODED. (C-CHECK RO 6/25/2023) REMOVED AND INSTALLED NEW FORMER P/N 601R318086-1 AT FS313.56 REF CRJ200 SRM 51-42-06, SRM 51-42-13 AND DWG # 601R31702 REV -N.. COMPLIED WITH 51-900-1003-SKY AND PRESSURE CHECKS GOOD. SEE CONTINUATION CARDS FOR DETAILS

Part: UNKNOWN — CORRODED (UNKNOWN) · airframe 43,123 hrs · 36,610 cycles

PAX DOOR FWD. FORMER @ FS 311.75 CORRODED. (C-CHECK RO 6/25/2023) REMOVED AND INSTALLED NEW PAX DOOR FWD FORMER ASSEMBLY FS311.75 REF CRJ200 SRM 51-42-06, SRM 51-42-21, SRM 51-42-13 AND DWG 601R31702 REV -N. COMPLIED WITH 51-900-1003-SKY AND PRESSURE CHECKS GOOD . SEE CONTINUATION CARD FOR DETAILS

Part: UNKNOWN — CORRODED (UNKNOWN) · airframe 43,123 hrs · 36,610 cycles

PAX DOOR INTERCOSTAL DD6 (MID) CORRODED. (C-CHECK RO 6/25/2023) REMOVED AND INSTALLED NEW DD6 MID INTERCOSTAL REF CRJ200 SRM 51-42-06, SRM 51-42-21 AND DWG 601R31702 REV -N. COMPLIED WITH 51-900-1003-SKY AND PRESSURE CHECKS GOOD . SEE CONTINUATION CARD FOR DETAILS

Part: NONE — FAILED · airframe 42,699 hrs · 36,214 cycles

AFTER TAKEOFF WE GOT A GEAR DISAGREE AND NOSE DOOR OPEN MASTER WARNING. RAN QRC FOR NOSE DOOR OPEN FIRST AND THAT FIXED BOTH MESSAGES. (FLIGHT 3570 - FILED CLOSED) THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 25062266 WITH THE FOLLOWING CORRECTIVE ACTION: "FOUND PS14GA - NLG OLEO CENTERED/EXTENDED BRACKET TO BE BENT AND PS14GA - NLG OLEO CENTERED/EXTENDED OUT OF RIG. REMOVED AND REPLACED PS14GA - NLG OLEO CENTERED/EXTENDED BRACKET IAW CMM 32-20-04. RERIGGED PS14GA - NLG OLEO CENTERED/EXTENDED IAW CRJ 200 AMM 32-61-05. OPS CHECK. "

Part: STRAP — CORRODED (FUSELAGE) · airframe 38,384 hrs · 32,349 cycles

LEFT HAND FLOOR SUPPORT STRAP CORRODDED AT FS 559.0 FROM LBL 43 TO LBL 27 MARKED. (C-CHECK) 09/14/19 BLENDED OUT CORROSION ON LEFT HAND FLOOR SUPPORT STRAP. REMOVED AND INSTALLED NEW STRAP IAW SRM. LEAK CHECK GOOD.

Part: FRAME — CORRODED (FUSELAGE) · airframe 38,384 hrs · 32,349 cycles

FRAME 605.0 CORRODDED ON FORWARD SIDE FROM APROX LEFT STR 18 TO RIGHT STR 25 MARKED. (C-CHECK) RO: 09/14/19 REMOVED AND INSTALLED NEW FRAME SECTOR IAW SRM. LEAK CHECK GOOD.

Part: STRAP — CORRODED (FUSELAGE) · airframe 38,384 hrs · 32,349 cycles

EXTERNAL FUSELAGE FS559 ATTACHMENT FLANGE FOR FAIRING 163AB FUSELAGE SIDE HAS DETERIORATED SEALANT PAD AND CORROSION ALL THE WAY ACROSS. (C-CHECK) RO: 09/14/19 REMOVED CORROSION ON EXTERNAL FUSELAGE ATTACHMENT FLANGE FOR FAIRING. REMOVED AND REPLACED 2 EA STRAPS AND 1 EA STIFFENER. APPLIED NEW SEALANT PAD FOR ACCESS PANEL IAW SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 38,384 hrs · 32,349 cycles

FLOORBEAM LIP CORRODDED FROM FS621 TO 574 LBL 9 MARKED. (C-CHECK) RO: 09/14/19 BLENDED OUT CORROSION ON FLOORBEAM LIP IAW SRM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 38,384 hrs · 32,349 cycles

FLOOR SUPPORT ANGLE CRACKED AT LBL 32 FS 484.0 MARKED. (C-CHECK) RO: 09/14/19 REMOVED AND REPLACED CRACKED ANGLE WITH FABRICATED NEW ONE IAW REO. LEAK CHECK GOOD.

Part: STRAP — CORRODED (FUSELAGE) · airframe 38,384 hrs · 32,349 cycles

RIGHT HAND FLOOR SUPPORT STRAP CORRODDED AT FS 559.0 FROM RBL 43 TO RBL 27 MARKED. (C-CHECK) RO: 09/14/19 BLENDED OUT CORROSION ON RIGHT HAND FLOOR SUPPORT STRAP AT FS 559.0 FROM LBL 43 TO LBL 27, FOUND STRAP TO BE OUT OF LIMITS, REMOVED AND INSTALLED NEW STRAP IAW SRM. LEAK CHECK GOOD.

Part: HINGE ARM — CHAFED (SERVICE DOOR) · airframe 38,384 hrs · 32,349 cycles

SERVICE DOOR HINGE ARM CHAFED. (C-CHECK) RO: 09/14/19 REMOVED CHAFE ON SERVICE DOOOR HINGE ARM IAW REO. ALL CHECKS GOOD.

Part: INTERCOSTAL — CORRODED (SERVICE DOOR) · airframe 38,384 hrs · 32,349 cycles

SERVICE DOOR INTERCOSTAL AT HINGE ARM MECHANISM HAS CORROSION. (C-CHECK) RO: 09/14/19 BLENDED OUT CORRISION ON THE SERVICE DOOR INTERCOSTAL IAW SRM. ALL CHECKS GOOD AND THE CORROSION DAMAGE FOUND IS ACCEPTABLE IAW REO.

Part: FRAME — CORRODED (FUSELAGE) · airframe 38,384 hrs · 32,349 cycles

CORROSION FOUND ON LOWER FRAME SECTOR AT FS349.00 BETWEEN STR 26L- STR 26R. (C-CHECK) RO: 09/14/19 FOUND LOWER FRAME SECTOR AT FS349.00 BETWEEN STGR 26L- STGR 26R TO BE OUT OF LIMITS, REMOVED AND INSTALLED NEW FRAME SECTOR IAW SRM. LEAK CHECK GOOD.

Part: FRAME — CORRODED (FUSELAGE) · airframe 38,384 hrs · 32,349 cycles

CORROSION FOUND ON LOWER FRAME SECTOR FS409.0 AFT LOWER ANGLE BETWEEN STR 26L- STR 26R. (C-CHECK) RO: 09/14/19 FOUND LOWER FRAME SECTOR FS409.0 AFT LOWER ANGLE BETWEEN STR 26L- STR 26R. TO BE OUT OF LIMITS, REPLACED WITH NEW LOWER ANGLE IAW SRM. LEAK CHECK GOOD.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 38,384 hrs · 32,349 cycles

PASSENGER CABIN STR 3L AFT OF FS379.0 IS CRACKED. (C-CHECK) RO: 09/14/19 COMPLETED STRINGER REPAIR IAW SRM. INSTALLED NEW STRINGER SECTION WITH 2 EA SPLICES. LEAK CHECK GOOD.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 38,384 hrs · 32,349 cycles

PASSENGER CABIN STR 3L AFT OF FS280 CLIPS ARE CRACKED. (C-CHECK) RO: 09/12/19 REMOVED AND INSTALLED NEW CLIPS IN THE PAX CABIN IAW SRM. LEAK CHECK GOOD.

Part: ACCESS PANEL — CORRODED (PAX DOOR) · airframe 38,384 hrs · 32,349 cycles

CORROSION AROUND SCREW HOLES OF PAX DOOR ACCESS PANELS 832AL, 832GL, 832BR, 832ER, 832HL, AND 832EL. (C-CHECK) RO: 09/14/19 BLENDED CORROSIONS AROUND SCREW HOLES OF PAX DOOR ACCESS PANELS IAW SRM. REPLACED PAX DOOR PANELS IAW SRM.

Part: HOUSING — CHAFED (CARGO DOOR) · airframe 38,384 hrs · 32,349 cycles

CARGO DOOR EXTERNAL HANDLE HOUSING HAS CHAFING DAMAGE. (C-CHECK) RO: 09/14/2019 BLENDED OUT DAMAGE ON CARGO DOOR EXTERNAL HANDLE HOUSING. REMOVED AND INSTALLED NEW CARGO DOOR EXTERNAL HANDLE HOUSING IAW SRM.

Part: OIL SYSTEM — FLUCTUATES (LT ENGINE) · airframe 35,352 hrs · 29,760 cycles

LEFT ENGINE OIL PRESSURE FLUCTUATED INFLIGHT BETWEEN 25-45 PSI. OIL PRESSURE WARNING. ENGINE SHUTDOWN ON APPROACH. OPEN

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 34,129 hrs · 28,555 cycles

PAX DOOR CENTER INTERCOSTAL HAS CORROSION AROUND WIRE HARNESS HOLE CUTOUT AT BS 315 - 335. REMOVED AND REPLACED THE PAX DOOR CENTER INTERCOSTAL IAW SRM. PRESSURIZATION LEAK CHECKS GOOD.

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 34,129 hrs · 28,555 cycles

PAX DOOR INTERCOSTAL HAS CORROSION ON UPPER FLANGE TOP SIDE AND UNDERNEATH AT NUTPLATE LOCATIONS. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM. PRESSURIZATION LEAK CHECK GOOD.

Part: WEB — CORRODED (PAX DOOR) · airframe 34,129 hrs · 28,555 cycles

PAX DOOR AFT WEB HAS CORROSION. INSTALLED A NEW WEB. INSTALLED ALL STIFFENERS, ANGLES AND COUNTERBALANCE HOSING IAW SRM.

Part: SENSOR — OUT OF ADJUST (NLG) · airframe 33,373 hrs · 27,650 cycles

GEAR DISAGREE ON NLG. NLG SLOW TO RETRACT. ADJUSTED TORQUE LINK PROXIMITY BRACKET SENSOR AND TARGET. OPS CHECKED GOOD.

Part: PROXIMITY SENSOR — CRUSHED (MLG) · airframe 32,838 hrs · 27,100 cycles

AIRCRAFT RETURNED TO THE FIELD WITH A GEAR DISAGREE. REPLACED THE CRUSHED PROXIMITY SENSOR BRACKET, ADJUSTED THE SENSOR AND SWUNG GEAR, OPS GOOD.

Part: BULKHEAD — CRACKED (BS 202) · airframe 29,323 hrs · 23,727 cycles

FWD PRESSURE BULKHEAD CRACKED WHERE PARKING BRAKE CABLE PASSES THROUGH. THIS HAS BEEN DETERMINED TO BE A MAJOR REPAIR. A5 INSP, INSTALLED DOUBLER ON FWD PRESSURE BULKHEAD WHERE PARKING BRAKE CABLE PASSES THROUGH FS 202.75, BL 23.71 IAW REO.

Part: DETECTOR — FAILED (TE FLAPS) · airframe 28,311 hrs · 22,977 cycles

FLAPS FAILED AT 18A ON APPROACH. RAN QRH AND THEN LANDED. R & R THE FLAP SKEW DETECTION UNIT IAW AMM. OPS CHECKED GOOD AT THIS TIME.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 27,523 hrs · 22,343 cycles

RIGHT EXTERIOR EMERGENCY LIGHT JUST FORWARD OF THE EMERGENCY EXIT DOOR IS INOPERATIVE. REPLACED THE LAMPS IAW AMM.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 27,085 hrs · 22,003 cycles

NR 4 RT WING EMERGENCY LIGHT IS BURNED OUT. REPLACED THE LAMP IAW AMM.

Part: SKIN — DENTED (TE FLAP) · airframe 25,667 hrs · 20,934 cycles

LT WING INBD FLAP HAS A DENT ON LOWER SKIN APPROXIMATELY .032 INCHES DEEP X .700 INCHES LONG X .700 INCHES WIDE. DENT IS 4 INCHES FROM TE & 7 INCHES FROM INBD SIDE. C-CHECK REPAIRED LT WING INBD FLAP IAW SRM & STS EA.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 25,207 hrs · 20,570 cycles

FLT 6228, AFT EMERGENCY OVERHEAD LIGHT BURNED OUT. REPLACED LAMPS.

Part: RETAINER — DAMAGED (CABIN DOOR) · airframe 24,526 hrs · 20,050 cycles

LOUD SOUND COMING FROM MAIN CABIN DOOR. PRESSURIZATION IS STABLE. (FLT 6365) FOUND DAMAGE TO THE MAIN CABIN DOOR SEAL RETAINER AT DOOR FS 320.10, DAMAGE IS OUT OF LIMITS. REPLACED MAIN CABIN DOOR LOWER FWD AND LOWER CENTER SEAL RETAINERS, AND REPLACED PAX DOOR SEAL, IAW REO, SRM AND AMM.

Part: INVERTER — FAILED (CABIN) · airframe 24,374 hrs · 19,934 cycles

EMERGENCY LIGHT OUT AT SEAT 8 A&B. (FLT 6505) REPLACED NR 2 EMERGENCY LIGHT INVERTER.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,374 hrs · 19,934 cycles

EMERGENCY EXIT LIGHT LOWER OVERWING EXIT ROW 8 C/D DOES NOT ILLUMINATE. (SERVICE) REPLACED EMERGENCY EXIT LIGHT AT LOWER OVERWING EXIT AT 8 C/D.

Part: LIGHT — DISCONNECTED (CABIN) · airframe 24,374 hrs · 19,934 cycles

EMERGENCY STRIP AT ROW 8 A/B DOES NOT ILLUMINATE. (FLT 6467) RECONNECTED EMERGENCY EXIT LOWER LIGHT STRIP AT ROW 8 A/B.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 24,276 hrs · 19,847 cycles

EMERGENCY EXIT SIGN BY LEFT OVERWING FAILS TO ILLUMINATE. (FLT 5652) RELAMPED EMERGENCY EXIT SIGN.

Part: CONNECTOR — DIRTY (CABIN) · airframe 24,239 hrs · 19,820 cycles

EMERGENCY LIGHT 8A/B DOES NOT ILLUMINATE. (FLT 5245) CLEANED CONNECTIONS ON ROW 8AB FLOOR LEVEL EMERGENCY LIGHT.

Part: PANEL — DEFECTIVE (COCKPIT) · airframe 23,534 hrs · 19,279 cycles

CAPTAIN'S RTU SCREEN IS COMING LOOSE FROM IT'S HOUSING. (FLT 6324) REPLACED CAPT'S RTU DISPLAY PANEL. P/N 622-9852-106 S/N ON 1778 S/N OFF 13G7P

Part: WINDOW — CRACKED (COCKPIT) · airframe 23,163 hrs · 18,974 cycles

F/O'S SIDE WINDOW IS CRACKED. (FLT 6197) REPLACED FIRST OFFICER'S SIDE WINDOW IAW AMM. P/N OFF: NP13922-001 S/N OFF: A01337209.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,030 hrs · 18,863 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5239) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,030 hrs · 18,863 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6415) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,838 hrs · 18,709 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5630) RELAMPED EMERGENCY LIGHT.

Part: UPLOCK HOOK — FAILED (LT MLG) · airframe 22,582 hrs · 18,497 cycles

LEFT MAIN LANDING GEAR DISAGREE ON RETRACTION. (FLT 4728) REPLACED LEFT MAIN LANDING GEAR UPLOCK HOOK ASSEMBLY. P/N: 17051-101, S/N OFF: CWDD2412-03

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,554 hrs · 18,468 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4673) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,481 hrs · 18,400 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5387) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,057 hrs · 18,038 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4552) RELAMPED EMERGENCY LIGHT.

Part: SENSOR — MALFUNCTIONED (AC BAY) · airframe 21,860 hrs · 17,858 cycles

LEFT PACK OVERTEMP SMOKE FROM GASPER FANS. (FLT 5670) REPLACED LEFT PACK TEMPERATURE SENSOR, THE LEFT PACK, AND THE LEFT DUAL BYPASS VALVE. PN: 782790-15 SN: OFF 200010194, PN: 808440-2 SN: 200303025

Part: COALESCER BAG — DIRTY (AC BAY) · airframe 21,860 hrs · 17,858 cycles

SMOKE TOILET AT 1000 ABL. (FLT 6281) REPLACED WATER SEPARATOR COALESCERS IN REF TO AMM.

Part: GENERATOR — FAILED (APU) · airframe 21,860 hrs · 17,858 cycles

RECEIVED AN APU GENERATOR OFF CAUTION. CABIN AND COCKPIT FILLED WITH SMOKE. (FLT 6326) REPLACED APU GENERATOR IAW CRJ 200 AMM. PN: 720845E SN: OFF 4764

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHT) · airframe 21,633 hrs · 17,670 cycles

EXIT SIGN EMERGENCY LIGHT IS OUT. (FLT 6428) FOUND CONNECTOR ON NR 1 BATTERY CHARGER INVERTER NOT SECURED. RESECURED CONNECTOR.

Part: CHARGER — FAILED (CABIN) · airframe 21,527 hrs · 17,602 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT AND AFT SIDE OF CURVED OVERWING OVERHEAD EXIT SIGN IS OUT. (FLT 5356) REPLACED NR 3 BATTERY CHARGER.

Part: COALESCER BAG — DIRTY (AC BAY) · airframe 21,170 hrs · 17,312 cycles

SMELLED SMOKE IN COCKPIT. (FLT 6458) REPLACED BOTH RIGHT AND LEFT ACM COALESCER SOCKS.

Part: POST — CRACKED (FUSELAGE) · airframe 21,090 hrs · 17,235 cycles

RIGHT VERTICAL POST AT FS 409+128 CRACKED AT RBL 18 INBOARD C-CHANNEL IN AFT RADIUS. (C-CHECK) REPAIR PER SRM.

Part: DOOR FRAME — GOUGED (FUSELAGE) · airframe 22,481 hrs · 18,400 cycles

PASSENGER DOOR FRAME 310.00 STR 5 AREA IS GOUGED. (C-CHECK) REPAIRED PER REO.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 22,481 hrs · 18,400 cycles

CRACK ON THE RIGHT SIDE OF FS 559.0 PRESSURE BULKHEAD. (C-CHECK) REPAIRED PER REO.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 22,481 hrs · 18,400 cycles

PASSENGER DOOR STAIR STRUCTURE AFT DRAG ANGLE HAS CRACK. (C-CHECK) REPAIRED PER REO.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 22,481 hrs · 18,400 cycles

FLOOR SUPPORT ANGLE CRACKED AT FS 621 LEFT SIDE. (C-CHECK) REPAIRED PER REO.

Part: TRACK — DIRTY (SERVICE DOOR) · airframe 20,984 hrs · 17,147 cycles

SERVICE DOOR IS DIFFICULT TO OPEN FROM THE OUTSIDE. (FLT 5403) CLEANED SERVICE DOOR TRACKS AND ROLLERS.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 20,791 hrs · 17,002 cycles

RIGHT SIDE EXTERIOR AFT OVERWING EMERGENCY LIGHT IS OUT. (FLT 5332) RELAMPED EMERGENCY LIGHT.

Part: SENSOR — OUT OF ADJUST (NLG) · airframe 20,806 hrs · 17,017 cycles

NOSE LANDING GEAR DISAGREE ON TAKEOFF. (FLT 6453) ADJUSTED NLG P4 14GA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,765 hrs · 16,983 cycles

NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6268) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,631 hrs · 16,858 cycles

NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4502) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,586 hrs · 16,814 cycles

NR 1 CEILING EMERGENCY LIGHT IS OUT. (FLT 6331) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,492 hrs · 16,737 cycles

FIRST OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6241) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 20,388 hrs · 16,663 cycles

RIGHT EXTERIOR MIDDLE FUSELAGE EMERGENCY LIGHT IS OUT. (FLT 4749) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,325 hrs · 16,616 cycles

AFT CEILING EMERGENCY LIGHT IS OUT. (FLT 4645) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,226 hrs · 16,533 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5336) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,196 hrs · 16,510 cycles

OVERHEAD EMERGENCY LIGHT AT ROW 2 IS OUT. (FLT 5628) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,678 hrs · 16,166 cycles

AFT OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6304) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,550 hrs · 16,060 cycles

NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6961) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,430 hrs · 15,969 cycles

NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6852) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,001 hrs · 15,619 cycles

NR 2 EMERGENCY LIGHT IN CEILING IS OUT. (FLT 3099) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,798 hrs · 15,421 cycles

OVERHEAD NR 3 EMERGENCY LIGHT OUT. (FLT 6541) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,723 hrs · 15,361 cycles

LAST OVERHEAD EMERGENCY LIGHT INOPERATIVE. (FLT 6900) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,472 hrs · 15,166 cycles

AFT EMERGENCY CEILING LIGHT INOPERATIVE. (FLT 6262) RELAMPED EMERGENCY LIGHT.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 16,508 hrs · 13,545 cycles

INTERCOSTAL AT FS 484 CRACKED. (C CHECK) REPAIRED PER REO.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 16,508 hrs · 13,545 cycles

FS 559 BULKHEAD CAP ANGLE RADIUS CRACKED. (C CHECK) REPAIRED PER REO.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 16,924 hrs · 13,903 cycles

INTERCOSTAL AT FS 484 CRACKED. (C CHECK) REPAIRED PER REO.

Part: FITTING — CRACKED (FUSELAGE) · airframe 16,924 hrs · 13,903 cycles

LBL 9 AT FS 280 CLIPS CRACKED. (C CHECK) REPAIRED PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 16,425 hrs · 13,485 cycles

NR 1 CABIN OVERHEAD EMERGENCY LIGHT INOP. (FLT 6590) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 15,746 hrs · 12,894 cycles

CEILING LEVEL EMERGENCY FLOODLIGHT INOP. (FLT 2555) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 15,631 hrs · 12,791 cycles

OVERHEAD EMERGENCY LIGHT INOP. (FLT 2582) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 15,455 hrs · 12,631 cycles

NR 3 EMERGENCY CEILING LIGHT INOP. (FLT 5821) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 15,292 hrs · 12,500 cycles

REAR MOST EMERGENCY LIGHT INOP. (FLT 6387) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 15,292 hrs · 12,500 cycles

RIGHT CENTER EMERGENCY LIGHT INOP. (FLT 6658) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 15,110 hrs · 12,357 cycles

NR 4 CEILING EMERGENCY FLOOD LIGHT INOP. (FLT 6020) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 15,068 hrs · 12,324 cycles

CEILING LEVEL EMERGENCY LIGHT INOP. (FLT 5998) RELAMPED EMERGENCY LIGHT.

Part: SIGN — INOPERATIVE (EMERGENCY LIGHTS) · airframe 14,196 hrs · 11,652 cycles

FLT 6668 - EMERGENCY EXIT LIGHTS INOP. REPLACED SIGN.

Part: LAMP — BURNED OUT (EMERGENCY LIGHTS) · airframe 14,018 hrs · 11,515 cycles

FLT 4420 - NR 1CEILING EMERGENCY FLOOD LIGHT INOP. RELAMPED.

Part: GLOWSTRIP — MISSING (CABIN) · airframe 13,739 hrs · 11,294 cycles

FLT 6019 - PHOTO LUMINESCENCT STRIP MISSING, 3 FEET AT ROW 4. RESECURED PHOTO LUMINESCENT FLOOR STRIP.

Part: WIRE — DAMAGED (CABIN) · airframe 13,375 hrs · 11,000 cycles

FLT 5917 - OVERHEAD EMERGENCY EXIT LIGHT INOP AT ROW 8. REPAIRED WIRING.

Part: O-RING — LEAKING (HYD SYSTEM) · airframe 13,242 hrs · 10,895 cycles

FLT 6562 - GEAR DISAGREE WARNING ON GEAR EXTENSION WITH HYDRAULIC SYSTEM 3 SHOWING ZERO. REPLACED DAMAGED O-RING AND SWUNG GEAR.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 13,135 hrs · 10,810 cycles

C-CHECK, FLOOR SUPPORT ATTACH CLIPS AT FS 280 RBL 9 CRACKED. REPLACED PER SRM.

Part: FITTING — CORRODED (RT ENGINE) · airframe 13,135 hrs · 10,810 cycles

C-CHECK, RIGHT ENGINE THRUST FITTING CORRODED. REPLACED PER AMM.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 13,135 hrs · 10,810 cycles

C-CHECK, FLOOR SUPPORT ATTACH CLIP AT FS 280 LBL 9 CRACKED. REPLACED PER SRM.

Part: FITTING — CORRODED (LT ENGINE) · airframe 13,135 hrs · 10,810 cycles

C-CHECK, LEFT ENGINE THRUST FITTING CORRODED. REPLACED PER AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 8,954 hrs · 7,449 cycles

RIGHT FORWARD EMERGENCY LIGHT OUT BY GALLEY DOOR INOP. FLT 4690 DEL 44 MINS.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 8,856 hrs · 7,372 cycles

F/O FLASHLIGHT INOP.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 8,140 hrs · 6,815 cycles

AFT DRAG ANGLE ON PAX DOOR CRACKED (MARKED). REMOVED REQUIRED FASTNERS AND CUT AWAY SECTION OF DRAG ANGLE AS SHOWN IN ASA REO 601R-52-11-513 PERFORMED STEPS 2 -7 OF ASA REO 601R-52-16-513 BEGAN INSTALLATION OF REPAIR PARTS. GOT ALL FASTENERS SHOT THOUGH THE ANGLE FWD TO AFT PART OF ANGLES AND 5 SOILDS SHOT I/B TO O/B THOUGH ANGLE. ALL WORK PERFORMED IAW ASA REO 601R-52-11-513 COMPLETED INSTALLATION OF REPAIR . ALL WORK PER ASA REO 601R-52-16-513 (CLOSED 11/03/06)

Part: STRINGER CLIP — CRACKED (BS 280) · airframe 8,140 hrs · 6,815 cycles

LEFT AND RIGHT 280 CLIPS CRACKED I/B SIDE.

Part: ANGLE — CRACKED (BS 621) · airframe 8,140 hrs · 6,815 cycles

LEFT 621 ANGLE CRACKED AS MARKED. REMOVED DAMAGED SECTION OF FLOOR ANGLE. FABRICATED ALL REPAIR PARTS FROM SERVICEABLE ANGLE P/N 601R35031-241. OK TO INSTALL. BEGAN INSTALLATION OF REPAIR PARTS. INSTALLED 2EA NUTPLATES AND ALL LOCK FASTENERS SAVE 4 ON THE O/B MOST END OF ANGLE. ALL WORK DONE IAW REO 601R-53-61-117. COMPLETED INSTALLATION OF ALL REMAINING FASTENERS AND TOPCOATED IAW ASA REO 601R-53-61-117, REV "C". (CLOSED 11/01/06)

Part: INTERCOSTAL — CRACKED (BS 484) · airframe 8,140 hrs · 6,815 cycles

LEFT FS 484 INTERCOSTAL CRACKED, O/B OF LBL 27.

Part: INTERCOSTAL — CRACKED (BS 484) · airframe 8,140 hrs · 6,815 cycles

RIGHT FS 484 INTERCOSTAL CLIP CRACKED, O/B OF RBL 27.

Part: RIB — CRACKED (LT WING) · airframe 8,140 hrs · 6,815 cycles

LEFT BATTERY RIB CRACKED AS MARKED. REMOVED ACCESS PANEL AND 2EA CONNECTORS TO FOM. REPAIR OF LT BATT RIB. REMOVED DOUBLERS AND CUT OUT DAMAGE ON LT BATTERY RIB. FABRICATED -5 ANGLE, SALVAGE REWORK ANGLE PER REPAIR 2, SHEET 5, IAW REO 601R-57-51-046 AND APPLIED FINISH A023 IAW CRJ SRM 51-25-16. OK TO INSTALL REPAIR PART. FABRICATED -7 FILLER . WET INSTALLED DETAILS USING MS20470AD5 RIVETS AND HST10AG5 LOCK FASTENERS IAW REO 601R-57-51-046. AWAITING 2EA RIVETS AND CONNECTORS. INSTALLED LAST 2EA RIVETS MS20470AD5 AND REINSTALLED CONNECTORS IAW REO 601R-57-51-046. OPS CHECK REQUIRED. PERFORMED OPS CHECK, FOUND TO BE GOOD. (CLOSED 11/01/06)

Part: ANGLE — CRACKED (BS 621) · airframe 8,140 hrs · 6,815 cycles

RIGHT 621 ANGLE CRACKED AS MARKED. CUT AWAY DAMAGED PORTION OF P/N 601R35031-239 ANGLE AT FS 621 BETWEEN RBL 36 AND RBL 27 PER REO 601R-53-61-117. TOUCHED UP FINISH AT CUT LINE A032 PER SRM 51-21-16. FABRICATED -2 ANGLE, -4 REPAIR ANGLE, AND -6 STRAP ITEMS FROM P/N 601R35031-241 PER NOTE "7" OF REO 601R-53-61-117 AND TOUCHED UP FINISH A023 ON REWORKED AREAS PER CRJ SRM 51-25-16. OK TO INSTALL REPAIR PARTS. BEGAN INSTALLATION OF REPAIR PARTS. INSTALLED 2EA NUTPLATES AND ALL LOCK FASTENERS. ALL WORK DONE IAW REO 601R-53-61-117. COMPLETED INSTALLATION OF ALL REMAINING FASTENERS AND TOPCOATED IAW ASA REO 601R-53-61-117. REV C. (CLOSED 11/01/06)

Part: LIGHT — INOPERATIVE (CABIN) · airframe 7,967 hrs · 6,670 cycles

A QUARTER OF THE EMERGENCY FLOOR LIGHTING IS OUT.

Part: HANDLE — CRACKED (FUSELAGE)

DURING A HANGAR INSPECTION, THE PASSENGER DOOR EXTERNAL HANDLE WAS FOUND TO BE CRACKED IN THE LOCK HOLE. MAINTENANCE WILL REMOVE AND REPLACE THE PASSENGER DOOR EXTERNAL HANDLE. (K)

Part: ANCHOR FITTING — CRACKED (DOOR)

DURING A HANGAR INSPECTION, THE PASSENGER DOOR FORWARD ANCHOR FITTING WAS FOUND TO BE CRACKED. MAINTENANCE WILL REMOVE AND REPLACE THE PASSENGER DOOR FORWARD ANCHOR FITTING. (K)

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 5,937 hrs · 5,037 cycles

CAPTAIN`S WINDOW IS CRACKED (SIDE WINDOW). REPLACED CAPTAIN`S SIDE VIEW WINDOW IAW AMM 56-00-00, 56-11-01, 56-12-01. OPERATIONAL CHECK GOOD. PN/OFF 601R33033-11, SN/OFF 03119H3055.

Part: SMOKE DETECTOR — MALFUNCTIONED (CARGO BAY) · airframe 4,315 hrs · 3,705 cycles

CARGO SMOKE WARNING MSG FOR 5 SECS THEN EXTINGUISHED. REPLACED AFT CARGO SMOKE DETECTOR. OPERATIONAL CHECK GOOD.

Part: CLIP — CRACKED (FLOORBEAM) · airframe 3,848 hrs · 3,304 cycles

CLIP AT STA 625 RIGHT SIDE APPROX STR 15 IS CRACKED. ITEM FOUND AT C-CHECK INSPECTION.

Part: CONTROL UNIT — DEFECTIVE (HORIZONTAL STAB)

STAB TRIM FAILURE. DECLARED EMERGENCY AND DIVERTED TO HSV. LANDED UNEVENTFULLY. RESET HSTCU IAW CRJ FIM.

Part: PDU — INOPERATIVE (THRUST REVERSER)

DURING AIRCRAFT OPERATION THE CREW REPORTED THE RIGHT HAND THRUST REVERSER WOULD NOT DEPLOY. THE POWER DRIVE UNIT WAS FOUND INOPERATIVE AND REPLACED. A SATISFACTORY FUNTIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RETURNED TO SERVICE.

Part: SMOKE DETECTOR — FAULTY (CARGO BAY)

DURING CLIMB, THE CREW REPORTED AN INDICATION OF SMOKE IN THE CARGO COMPARTMENT THE CARGO FIRE BOTTLES WERE BLOWN. THE AIRCRAFT RETURNED TO ORD AND LANDED WITHOUT INCIDENT. MAINTENANCE PERSONNEL REPLACED CARGO SMOKE DETECTORS AS A PRECAUTIONARY MEASURE AND INSTALLED NEW FIRE BOTTLES. AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE.