N863AS

Part: HEAT SHIELD — CRACKED (APU) · airframe 44,045 hrs · 39,389 cycles

APU HEAT SHIELD HAS A CRACK AT THE 6 O' POSITION. FILED CLOSED (9/23/2020). REMOVED AND REPLACED APU EXHAUST HEAT SHIELD, IN REF TO CRJ200 AMM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 43,839 hrs · 39,165 cycles

CABIN FLOOR SEAT TRACK AT RBL9 FROM FS559.00+3-FS559.00+85 IS CORRODED. (C-CHECK) RO 7/10/2020 REMOVED CORROSION ON CABIN FLOOR SEAT TRACK AT RBL9 FROM FS559.00+3-FS559.00+85. FOUND TO BE OUT OF LIMITS. FABRICATED A NEW SEAT TRACK P/N 601R31032-9. SEAT TRACK INSTALLED ON JOB 2748791. COMPLIED WITH ALL STEPS OF REPAIR B, REF REO.

Part: STRAP — CORRODED (FUSELAGE) · airframe 43,839 hrs · 39,165 cycles

EVIDENCE OF CORROSION FOUND ON STRAP AT FS 333, BETWEEN STR 25L AND 26L. (C-CHECK) RO 7/10/2020 REPAIRED DAMAGED AREA PER REO. LEAK CHECK GOOD. COMPLIED WITH TASK CARD.

Part: SKIN — DENTED (FUSELAGE) · airframe 43,839 hrs · 39,165 cycles

FUSELAGE SKIN BETWEEN FS589-FS605, STR 24R-26R IS DENTED. (C-CHECK) RO 7/10/2020 HAND DRESSED DENTS (3EA) LOCATED AT FUSELAGE SKIN BETWEEN FS589-FS605, STR 24R-26R REO. ALL THREE DENTS FOUND TO BE OUT OF LIMITS DUE TO DENTS IN ADJACENT PANELS IN THE CIRCUMFERENTIAL DIRECTION. REF SRM. SUMITTED TO ENGINEERING AND RECEIVED REO (ALL STEPS COMPLIED WITH). WITHIN LIMITS. RESTORED FINISH.

Part: SKIN — DENTED (FUSELAGE) · airframe 43,839 hrs · 39,165 cycles

FUSELAGE SKIN BETWEEN FS700-FS718, STR 14L-15L IS DENTED. (C-CHECK) RO 7/10/2020 HAND DRESSED DENTS (2EA) ON THE FUSELAGE SKIN BETWEEN FS700-FS718, STR 14L-15L REF REO. AFT DENT FOUND TO BE WITHIN LIMITS. FWD DENT FOUND TO BE OUT OF LIMITS REF SRM. SUBMITTED TO ENGINEERING AND RECIEVED MHI RJ REO (ALL STEPS COMPLIED WITH). RESTORED FINISH.

Part: SKIN — DENTED (FUSELAGE) · airframe 43,839 hrs · 39,165 cycles

FUSELAGE SKIN BETWEEN FS589-FS605, STR 21L-22L IS DENTED. (C-CHECK) RO 7/10/2020 DRESSED OUT DENT ON FUSELAGE SKIN BETWEEN FS589-FS605, STR 21L-22L REF REO. EVALUATED AND FOUND TO BE OUT OF LIMITS DUE TO FASTENER PROXIMITY REF SRM. SUBMITTED TO ENGINEERING AND RECIEVED REO. (ALL STEPS COMPLIED WITH). WITHIN LIMITS. RESTORED FINISH.

Part: FRAME — CHAFED (FUSELAGE) · airframe 43,839 hrs · 39,165 cycles

FRAME AT FS654.5 IS CHAFED THROUGH JUST FORWARD OF THE APU EXHAUST PORT. (C-CHECK) RO 7/10/2020 REPAIRED FRAME AT FS654.5 JUST FORWARD OF THE APU EXHAUST PORT REF REO. SEE CONTINUATION CARD FOR DETAILS

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 43,839 hrs · 39,165 cycles

SEAT TRACK SUPPORT CAP RBL 9 JUST FWD OF FS 574.0 TO FS 621.0 HAS CORROSION. (C-CHECK) RO 7/10/2020 REMOVE CORROSION FROM SEAT TRACK SUPPORT CAP ON RBL 9 FWD OF FS 574 - FS 621.0 REF SRM. BLENDED AREA FOUND TO BE OUT OF LIMITS REO. INSTALLED NEW REPLACEMENT FLOORBEAM CAP P/N 601R35031-3 AT RBL9 BETWEEN FS 574 AND FS 621 REF DWG AND REO. SEE CONTINUATION CARD FOR DETAILS.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 43,839 hrs · 39,165 cycles

SEAT TRACK SUPPORT CAP FROM FS 559.0 TO FS 574.0 RBL 9 HAS CORROSION. (C-CHECK) RO 7/10/2020. REMOVED AND REPLACED SEAT TRACK SUPPORT CAP FROM FS559.00 TO FS574.00 RBL 9. COMPLIED WITH ALL STEPS OF THE REPAIR. REF REO AND DRAWING. COMPLIED WITH TASK CARD.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 43,839 hrs · 39,165 cycles

SEAT TRACK AT FS 559+80 - FS 574.0 RBL 9 HAS CORROSION. (C-CHECK) RO 7/10/2020 REMOVED AND REPLACED CARGO TIE DOWN TRACKS AT FS559.00+80 - FS574.00 RBL 9 DUE TO CORROSION FOUND TO BE OUT OF LIMITS REF AMM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 43,839 hrs · 39,165 cycles

SMALL PIECE OF SEAT TRACK AT FS 559+112-FS 574.0 LBL 27 HAS CORROSION. (C-CHECK) RO 7/10/2020 FABRICATED NEW SEAT TRACK USING N126-2075, PO TX3728 PER REO.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 43,839 hrs · 39,165 cycles

SEAT TRACK CAP RBL 27 AT FS 559+112 TO JUST AFT OF FS 559.0 HAS CORROSION. (C-CHECK) RO 7/10/2020 REMOVED AND REPLACED SEAT TRACK CAP AT RBL27 FROM FS559.00-FS559.00+112. COMPLIED WITH ALL STEPS OF THE REPAIR. REF REO AND DRAWING. COMPLIED WITH CARD.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 43,839 hrs · 39,165 cycles

CORROSION ON LEFT HAND FLOOR SILL AT FS 349. (C-CHECK) RO 7/10/2020 REPAIRED LT FLOOR SILL AT FS 349 REF REO. SEE CONTINUATION CARD FOR DETAILS.

Part: PANEL — CORRODED (FUSELAGE) · airframe 43,839 hrs · 39,165 cycles

RT PRESSURE FLOOR SILL PANEL HAS SEVERAL AREA OF CORROSION BETWEEN FS 499 AND FS 559. (C-CHECK) RO 7/10/2020 REPAIRED THE RT PRESSURE FLOOR SILL PANEL BETWEEN FS 499 AND FS 559 REF REO. REFERENCE THE CONTINUE CARD FOR DETAILS.

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 43,839 hrs · 39,165 cycles

THE PAX DOOR INTERCOSTAL DD5 AFT HAS CORROSION. (C-CHECK) RO 7/10/2020 REMOVED THE CORROSION FROM THE PAX DOOR INTERCOSTAL AFT DD5 REF SRM. BLENDED AREA FOUND TO BE OUT OF LIMITS REF SRM. WET INSTALLED AND FILLET SEALED THE PAX DOOR INTERCOSTAL DD5 AFT REF SRM AND DRAWING. SEE CONTINUATION CARD FOR DETAILS. PRESSURE CHECKS GOOD.

Part: PANEL — CORRODED (FUSELAGE) · airframe 43,839 hrs · 39,165 cycles

LT PRESSURE FLOOR SILL PANEL HAS SEVERAL AREA OF CORROSION BETWEEN FS 409+112 AND FS 559. (C-CHECK) RO 7/10/2020 REPAIRED THE LT PRESSURE FLOOR SILL PANEL BETWEEN FS 409.00+112 AND FS 559.00. REF REO REFERENCE THE CONTINUE CARD FOR DETAILS.

Part: STRAP — CORRODED (FUSELAGE) · airframe 43,839 hrs · 39,165 cycles

STRAP AT FS 559 HAS CORROSION BETWEEN APPROXIMATE LBL33 AND LBL44. (C-CHECK) RO 7/10/2020 BLENDED CORROSION, REF SRM. NDT MEASURED THICKNESS AND FOUND PART TO BE OUT OF LIMITS, SEE CONTINUATION FOR DETAILS. REMOVED AND REPLACED FLOOR STRAP, 601R3125, AND HARDWARE WITH LIKE HARDWARE, REF SRM AND DWG. COMPLIED WITH TASK CARD. LEAK CHECK GOOD.

Part: HINGE BRACKET — CHAFED (RUDDER) · airframe 43,839 hrs · 39,165 cycles

RUDDER UPPER CENTER HINGE BRACKET ON VERTICAL STABILIZER IS CHAFED ON TOP SURFACE JUST FORWARD OF THE SPHERICAL BEARING. (C-CHECK) RO 7/10/2020 BLENDED CHAFE ON UPPER HINGE BRACKET TOP SURFACE TO A SMOOTH CONTOUR (20:1 TRANSITION). REF SRM. BLEND MEASURES .020" DEEP X .900" LONG X .600" WIDE. THERE ARE NO ALLOWABLE DAMAGE LIMITS GIVEN FOR FITTINGS, FOUND TO BE OUT OF LIMITS. REPAIRED RUDDER UPPER CENTER HINGE REF REO. SEE CONTINUATION CARD FOR DETAILS.

Part: HINGE BRACKET — CHAFED (RUDDER) · airframe 43,839 hrs · 39,165 cycles

RUDDER LOWER CENTER HINGE BRACKET ON VERTICAL STABILIZER IS CHAFED ON TOP SURFACE JUST FORWARD OF THE SPHERICAL BEARING. (C-CHECK) RO 7/10/2020 BLENDED CHAFE ON RUDDER LOWER CENTER HINGE BRACKET TOP SURFACE TO A SMOOTH CONTOUR (20:1 TRANSITION). REF SRM. BLEND MEASURES .009" DEEP X .700" LONG X .240" WIDE. THERE ARE NO ALLOWABLE DAMAGE LIMITS GIVEN FOR FITTINGS, FOUND TO BE OUT OF LIMITS. REPAIRED RUDDER LOWER CENTER HINGE REF REO.

Part: FITTING — CRACKED (FUSELAGE) · airframe 43,839 hrs · 39,165 cycles

CLIP AT STR14R, FS621-FS625, IS CRACKED. (C-CHECK) RO 7/10/2020 REMOVED AND INSTALLED NEW CLIP AT STGR 14R BETWEEN FS621 AND FS625 REF SRM AND REO. SEE CONTINUATION CARD FOR DETAILS.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 43,839 hrs · 39,165 cycles

INTERCOSTAL / CLIP COMMON TO THE SKIN AT STR14L, FS621-FS625, IS CRACKED. (C-CHECK) RO 7/10/2020 REMOVED AND INSTALLED CLIP/INTERCOSTAL COMMON TO THE OUTER SKIN AT STR 14L BETWEEN FS 621 AND 625 REF SRM AND DRAWING. SEE CONTINUATION CARD FOR DETAILS.

Part: FITTING — CRACKED (FUSELAGE) · airframe 43,839 hrs · 39,165 cycles

CLIP AT STR14L, FS621-FS625, IS CRACKED. (C-CHECK) RO 7/10/2020 REMOVED AND INSTALLED NEW CLIP AT STGR 14L BETWEEN FS621 AND FS625 REF CSRM AND REO. SEE CONTINUATION CARD FOR DETAILS.

Part: RETAINER — CORRODED (SERVICE DOOR) · airframe 43,839 hrs · 39,165 cycles

UPON PROVIDED ACCES TO TREATMANT OF CORROSION DAMAGE ON SERVICE DOOR SEAL LWR AFT CORNER RETAINER FOUND CORROSION DAMAGE AT DOOR FRAME LWR AFT PAN SECTION. (C-CHECK) RO 7/10/2020 REMOVED CORROSION DAMAGE FROM SERVICE DOOR LWR AFT FRAME PAN SECTION REF SRM. ORIGINAL MATERIAL THICKNESS IS .063", LOWEST REMAINING THICKNESS IS .057", MATERIAL REMOVED IS .006", MAX ALLOWABLE IS .006" OR 10%. FOUND TO BE OUT OF LIMITS DUE TO DAMAGE ON MULTIPLE ELEMENTS. REF SRM. COMPLIED WITH MHI REO. SUBJECT CONDITION IS STRUCTURALLY ACCEPTABLE PER MHI REO.

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 43,839 hrs · 39,165 cycles

PASSENGER DOOR MIDDLE INTERCOSTAL AT DD3 CORRODED. (C-CHECK) RO 7/10/2020 REMOVED THE CORROSION FROM THE PAX DOOR INTERCOSTAL MID DD3 REF SRM. BLENDED AREA FOUND TO BE OUT OF LIMTS REF SRM. WET INSTALLED AND FILLET SEALED THE PAX DOOR MID INTERCOSTAL DD3 REF SRM AND DRAWING. SEE CONTINUATION CARD FOR DETALS.

Part: BRACKET — CRACKED (PAX DOOR) · airframe 43,839 hrs · 39,165 cycles

PASSENGER DOOR SUPPORT WHEEL SYSTEM CABLE BRACKET AT BOTTOM OF STAIRS APPEARS CRACKED. (C-CHECK) RO 7/10/2020 REMOVED CRACKED SUPPORT WHEEL CABLE BRACKET ASSY ON AFT SIDE OF BOTTOM STEP AND INSTALLED NEW BRACKET ASSY P/N 601R317186-1 REF SRM.

Part: STOP FITTING — CRACKED (PAX DOOR) · airframe 43,839 hrs · 39,165 cycles

PASSENGER DOOR PULL-IN LEVER TORQUE TUBE STOP FITTING CORRODED AND APPEARS CRACKED. (C-CHECK) RO 7/10/2020 REPLACED PASSENGER DOOR LOWER TORQUE TUBE STOP FITTING P/N 601R38923-3 AND RELATED HARDWARE, REF AMM, PERFORMED OPERATIONAL TEST OF THE PASSENGER DOOR, TESTS GOOD? FOR COMPLETE DETAILS OF WORK PERFORMED SEE ATTACHED CONTINUATION CARD.

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 43,839 hrs · 39,165 cycles

PASSENGER DOOR MIDDLE INTERCOSTAL AT DD2 CORRODED. (C-CHECK) RO 7/10/2020 REMOVED THE CORROSION FROM THE PAX DOOR INTERCOSTAL MID DD2 REF SRM. BLENDED AREA FOUND TO BE OUT OF LIMITS SRM. WET INSTALLED AND FILLET SEALED THE PAX DOOR MID INTERCOSTAL DD2 REF SRM AND DRAWING. SEE CONTINUATION CARD FOR DETAILS. PRESSURE CHECK GOOD.

Part: FORMER — CORRODED (PAX DOOR) · airframe 43,839 hrs · 39,165 cycles

PASSENGER DOOR FORMER AT FS329.50 BETWEEN DD5 AND DD4 CORRODED. (C-CHECK) RO 7/10/2020 REMOVED THE CORROSION FROM THE PAX DOOR FORMER AT FS329.50 BETWEEN INTERCOSTAL DD5 AND DD6 REF SRM. BLENDED AREA FOUND TO BE OUT OF LIMITS REF SRM. WET INSTALLED AND FILLET SEALED THE PAX DOOR FORMER AT FS329.50 BETWEEN DD5 AND DD4 REF SRM AND DRAWING. SEE CONTINUATION CARD FOR DETAILS. PRESSURE CHECK GOOD.

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 43,839 hrs · 39,165 cycles

PASSENGER DOOR MIDDLE INTERCOSTAL AT DD4 CORRODED. (C-CHECK) RO 7/10/2020 REMOVED THE CORROSION FROM THE PAX DOOR INTERCOSTAL MID DD4 REF SRM. BLENDED AREA FOUND TO BE OUT OF LIMITS REF SRM. WET INSTALLED AND FILLET SEALED THE PAX DOOR MID INTERCOSTAL DD4 REF SRM AND DRAWING. PRESSURE CHECK GOOD. SEE CONTINUATION CARD FOR DETAILS.

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 43,839 hrs · 39,165 cycles

PASSENGER DOOR AFT INTERCOSTAL AT DD4 CORRODED. (C-CHECK) RO 7/10/2020 REMOVED THE CORROSION FROM THE PAX DOOR INTERCOSTAL AFT DD4 REF SRM. BLENDED AREA FOUND TO BE OUT OF LIMITS REF SRM. WET INSTALLED AND FILLET SEALED THE PAX DOOR AFT INTERCOSTAL DD4 REF SRM AND DRAWING. SEE CONTINUATION CARD FOR DETAILS. PRESSURE CHECK GOOD.

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 43,839 hrs · 39,165 cycles

PASSENGER DOOR CLIP FOR FWD INTERCOSTAL AT DD6, AND AT APPROX FS320 CORRODED. (C-CHECK) RO 7/10/2020 REMOVED AND INSTALLED NEW PAX DOOR CLIP / CLEAT COMMON TO INTERCOSTAL FWD DD6 AT APPROX FS320 REF SRM AND DRAWING. SEE CONTINUATION CARD FOR DETAILS.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 43,839 hrs · 39,165 cycles

CLIP COMMON TO THE SKIN AT STR13L, FS621-FS625, IS CRACKED. (C-CHECK) RO 7/10/2020 REMOVED AND INSTALLED CLIP/INTERCOSTAL COMMON TO THE OUTER SKIN AT STR13L BETWEEN FS621 AND 625 REF SRM AND DRAWING. SEE CONTINUATION CARD FOR DETAILS.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 43,839 hrs · 39,165 cycles

PASSENGER DOOR SUSPECT CRACK AT THE AFT STAIR DRAG ANGLE. (C-CHECK) RO 7/10/2020 REPLACED THE CRACKED AFT STAIR DRAG ANGLE REF SRM.

Part: FASTENER — CORRODED (RT SPOILER) · airframe 43,839 hrs · 39,165 cycles

RT OUTBOARD GROUND SPOILER ACTUATOR LINK HAS CORRODED HARDWARE. (C-CHECK) RO 7/10/2020 REMOVED AND REPLACED RT OTBD GROUND SPOILER LINK HARDWARE REF AMM. ALL CHECKS GOOD.

Part: FASTENER — CORRODED (RT SPOILER) · airframe 43,839 hrs · 39,165 cycles

RT INBOARD GROUND SPOILER ACTUATOR LINK HAS CORRODED HARDWARE. (C-CHECK) RO 7/10/2020 REMOVED AND REPLACED THE RT INBD GROUND SPOILER ACTUATOR LINK HARDWARE REF AMM. ALL CHECKS GOOD.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 43,839 hrs · 39,165 cycles

PASSENGER DOOR SURROUND STRUCTURE: LOWER FLOOR SUPPORT ANGLE HAS CORROSION AROUND FASTENERS. (C-CHECK) RO 7/10/2020 REMOVED CORROSION FROM PAX DOOR FLOOR SUPPORT LWR ANGLE FLANGE (NEXT TO DOOR AFT HAND RAIL LINK MOUNTING BRACKET) PER SRM. ORIGINAL THICKNESS=.063" REMAINING THICKNESS=.052" MATERIAL LOSS=.011" ALLOWABLE LOSS=.006" FOUND TO BE OUT OF LIMITS DUE TO THICKNESS AND PROXIMITY TO FASTENERS. REF SRM. ENGINEERING PROVIDED. THE SUBJECT REWORKED CONDITION IS STRUCTURALLY ACCEPTABLE PROVIDED ALL 6 STEPS ARE MET IN REO.

Part: ANGLE — CORRODED (SERVICE DOOR) · airframe 43,839 hrs · 39,165 cycles

SERVICE DOOR INTERNAL STRUCTURE: CLIP INSIDE LIGHTENING CUT-OUT JUST AFT OF THE INNER HANDLE ACCESS AREA HAS CORROSION. (C-CHECK) RO 7/10/2020 BLENDED CORROSION, REF SRM. FOUND TO BE OUT OF LIMITS. FABRICATED AND REPLACED ANGLE CLIP, P/N: 601R38304-49 REF DRAWING, SRM. RECIEVED APPROVAL FROM ENGINEERING TO USE ALTERNATE FASTENERS AS PER REO. SEE CONTINUATION CARD FOR DETAILS.

Part: SKIN — CORRODED (FUSELAGE) · airframe 43,839 hrs · 39,165 cycles

EXTERNAL SKIN IS CORRODED AT APPROX FS559+96-559+112, STR26L-26R. (C-CHECK) RO 7/10/2020 BLENDED CORROSION, REF SRM 51-21-06. FOUND TO BE OUT OF LIMITS. NO ALLOWABLE DAMAGE IN DISCREPANT AREA. SUBMITTED TO ENGINEERING AND RECIEVED DISPOSITION OF REO. COMPLIED WITH REO.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 43,839 hrs · 39,165 cycles

SERVICE DOOR SURROUND STRUCTURE: UPPER FLOOR SUPPORT ANGLE HAS CORROSION. (C-CHECK) RO 7/10/2020 REMOVED 2 EACH SOLID FASTENERS WITH CORROSION AT THE SERVICE DOOR SURROUND STRUCTURE UPPER FLOOR SUPPORT ANGLE REFERENCE SRM, INSTALLED NEW SOLID FASTENERS AND APPLIED FINISH TO SUPPORT ANGLE.

Part: RETAINER — CORRODED (SERVICE DOOR) · airframe 43,839 hrs · 39,165 cycles

SERVICE DOOR: LOWER SEAL RETAINER IS CORRODED. (C-CHECK) RO 7/10/2020 REMOVED CORROSION DAMAGE FROM SERVICE DOOR SILL LWR AFT CORNER RETAINER REF SRM. BLENDED AREA FOUND TO BE OUT OF LIMTS REF SRM. INSTALLED NEW SVC DOOR SILL LWR AFT RETAINER ANGLE P/N 6041R38304-267 REF SRM AND DWG. SSE CONTINUATION CARD FOR DETAILS.

Part: SKIN — CORRODED (FUSELAGE) · airframe 43,839 hrs · 39,165 cycles

EXTERNAL SKIN IS CORRODED AT APPROX FS559+44, STR25L-25R. (C-CHECK) RO 7/10/2020 BLENDED CORROSION ON EXTERNAL SKIN AT FS 559+44 BETWEEN STR 25L-25R REF SRM. BLENDED AREA FOUND TO BE OUT OF LIMITS REF SRM. REPAIRED EXTERNAL SKIN AT FS 559+44 BETWEEN STR 25L-25R REF REO.

Part: SKIN — CORRODED (FUSELAGE) · airframe 43,839 hrs · 39,165 cycles

EXTERNAL SKIN IS CORRODED AT APPROX FS559+34, STR26L. (C-CHECK) RO 7/10/2020 BLENDED CORROSION, REF SRM 51-21-06. FOUND REMAINING MATERIAL TO BE OUT OF LIMITS, REF SRM. SUBMITTED TO ENGINEERING, WHO APPROVED A DISPOSTION FOR BLENDED CORROSION DAMAGE TO FUSELAGE SKIN. COMPLETED ALL STEPS OF REO. LEAK CHECK GOOD.

Part: FASTENER — CORRODED (LT SPOILER) · airframe 43,839 hrs · 39,165 cycles

LT INBOARD GROUND SPOILER ACTUATOR LINK HAS CORRODED HARDWARE. (C-CHECK) RO 7/10/2020 REMOVED AND REPLACED LT I/B GROUND SPOILER ACTUATOR LINK HARDWARE IAW AMM. OPS CHECK GOOD.

Part: PLATE — CORRODED (PAX DOOR) · airframe 43,839 hrs · 39,165 cycles

PASSENGER DOOR SURROUND STRUCTURE: AFT ANCHOR, SERRATED MOUNTING PLATE HAS CORROSION ON ITS OUTBOARD SIDE. (C-CHECK) RO 7/10/2020 REMOVED DAMAGED SERRATED MOUNTING PLATE FROM PASSENGER DOOR AFT ANCHOR FITTING AND INSTALLED NEW P/N 600-3801-6 REF AMM, PERFORMED OPERATIONAL TEST OF THE PASSENGER DOOR COUNTERBALANCE TEST GOOD? FOR COMPLETE DETAILS OF WORK PERFORMED SEE ATTACHED CONTINUATION CARD.

Part: SKIN — GOUGED (CARGO DOOR) · airframe 43,839 hrs · 39,165 cycles

CARGO DOOR INTERNAL STRUCTURE: HAS LIGHT GOUGING, AND SOME CORROSION, ON THE RIVET TAILS AND STRUCTURE BELOW THE HANDLE MECHANISM. (C-CHECK) RO 7/10/2020 ORDER AND RECEIVED NEW CARGO DOOR DUE TO INNER SKIN BEING OUT OF LIMITS SEE 21093161 JOB 2748791 OP 184 FOR INSTALL. SEE CONTINUATION CARD FOR DETAILS.

Part: SKIN — DENTED (LT WING) · airframe 43,839 hrs · 39,165 cycles

LEFT WING, LOWER WING PLANK, INBD OF WS50 AND FORWARD OF THE WING TANK ACCESS HOLES, APPEARS TO BE DENTED. (C-CHECK) RO 7/10/2020 REPAIRED LT LOWER WING PLANK INBOARD OF WS50 AND FORWARD OF THE WING TANK ACCESS HOLE REF MHIRJ REO. SEE CONTINUATION CARD FOR DETAILS.

Part: UPLOCK ROLLER — FAILED (NLG) · airframe 41,670 hrs · 37,325 cycles

GEAR DISAGREE NOSE GEAR DID NOT GO DOWN. CYCLED GEAR HANDLE PER QRH AND ALL GEAR DOWN AND LOCKED. (FLT#5529) FO: 05/01/2019 CLOSED REMOVED AND REPLACED NLG UPLOCK ROLLER AND BRACKET WITH SERVICEABLE UNITS IAW AMM. OPS CHECK GOOD AT THIS TIME. PERFORMED FULL STRUCT SERVICE OF NLG STRUCT IAW AMM. OPS CHECK GOOD AT THIS TIME.

Part: UPLOCK ROLLER — SLOW (NLG) · airframe 41,670 hrs · 37,325 cycles

EXTENDED GEAR AT 180 KTS, RECEIVED GEAR DISAGREE WARNING MESSAGE. AFTER ABOUT 20 SECONDS, THE GEAR INDICATED DOWN BEFORE WE COULD EVEN START THE QRH PROCEDURE. (FLT#5574) CLOSED REMOVED AND REPLACED NLG UPLOCK ROLLER AND BRACKET WITH SERVICEABLE UNITS. OPS CHECK GOOD AT THIS TIME. PERFORMED FULL STRUT SERVICE OF NLG STRUT IAW AMM.

Part: LINE — LEAKING (NR 2 ENGINE) · airframe 41,524 hrs · 37,161 cycles

ENGINE TWO LOW OIL PRESSURE IN FLIGHT. ENGINE SHUT DOWN IN FLIGHT ACCOMPLISHED. (FLT#5223) REMOVED AND REPLACED OIL SUPPLY LINE IAW AMM. NO LEAKS NOTED AFTER ENGINE RUNS.

Part: GEARBOX — FAILED (THROTTLE SYS) · airframe 41,364 hrs · 37,017 cycles

RIGHT ENGINE THRUST LEVER JAMMED ON APPROACH. DECLARED AN EMERGENCY. LANDED WITHOUT INCIDENT. (FLT#3111) FO: 03/04/2019 CLOSED REMOVED AND REPLACED RT ENGINE THROTTLE GEARBOX IAW AMM. OPS CHECK GOOD AT THIS TIME. THROTTLE MOVEMENT SMOOTH AT THIS TIME.

Part: PUMP — FAILED (HYD SYSTEM) · airframe 41,044 hrs · 36,755 cycles

RIGHT ENGINE OIL PRESS ABNORMAL FLUCTUATIONS IN FLIGHT. FLUCTUATIONS WENT RED. COMPLIED WITH QRH PROCEDURE AND PERFORMED IN FLIGHT ENGINE SHUTDOWN. REPO FLT - NO PAX. (FLT#4980) CLOSED REMOVED AND REPLACED RT ENGINE EDP HYD PUMP IAW AMM. OPS CHECK GOOD. NO LEAKS FOUND. RT ENGINE OIL PRESSURE WITHIN LIMITS IAW AMM.

Part: BUSHING — FAILED (LT ELEVATOR) · airframe 40,296 hrs · 36,021 cycles

LEFT ELEVATOR HINGE BUSHINGS FAILED. REPLACED THE HINGE BUSHINGS AND BEARINGS IAW SRM.

Part: RIB — CRACKED (RWS 53) · airframe 40,296 hrs · 36,021 cycles

RIGHT MLG WHEEL WELL ABOVE HARNESS CONNECTORS, STRUCTURE WAS CRACKED. REPAIRED THE RT MLG WHEEL WELL BATT RIB AT WS 53.60 IAW SRM.

Part: FLOOR SUPPORT — CORRODED (BS 428-542) · airframe 40,296 hrs · 36,021 cycles

LEFT PRESSURE FLOOR SUPPORT HAD CORROSION, FROM BS 428 TO 542. REMOVED THE CORROSION ON THE FLOOR SUPPORT IAW REO.

Part: FLOOR SUPPORT — CORRODED (BS 428-557) · airframe 40,296 hrs · 36,021 cycles

RIGHT FLOOR SUPPORT HAD CORROSION, FROM BS 428 TO 557. REMOVED THE CORROSION IAW REO.

Part: WEB — DAMAGED (PAX DOOR) · airframe 40,296 hrs · 36,021 cycles

FWD PAX DOOR WEB DAMAGED. INSTALLED A NEW PAX DOOR FWD SIDE WEB IAW SRM.

Part: WEB — DAMAGED (PAX DOOR) · airframe 40,296 hrs · 36,021 cycles

AFT PAX DOOR WEB WAS DAMAGED. REMOVED AND REPLACED THE PAX DOOR AFT WEB IAW SRM.

Part: FRAME — CORRODED (BS 605) · airframe 40,296 hrs · 36,021 cycles

BS 605 FRAME HAD CORROSION. REPAIRED THE FRAME IAW REO.

Part: FLOORBEAM — CORRODED (BS 559) · airframe 40,296 hrs · 36,021 cycles

BS 559 RBL 27 - 43, FLOORBEAM HAD CORROSION. REMOVED AND REPLACED THE FLOORBEAM ANGLE IAW SRM.

Part: FRAME — CORRODED (BS 319) · airframe 40,296 hrs · 36,021 cycles

FRAME, BS 319.7 HAD CORROSION ON BOTH THE FORWARD & AFT FACES AND ON THE FLANGE, STRINGERS 24L TO 27L. REMOVED AND REPLACED THE FRAME SECTION IAW SRM. ALL CHECKED GOOD.

Part: THROTTLE CABLE — BINDING (RIGHT) · airframe 38,714 hrs · 34,315 cycles

DURING APPROACH, RT THROTTLE BINDING IN FLIGHT. CREW DECLARED AN EMERGENCY, LANDED WITHOUT INCIDENT. REPLACED THE THROTTLE CABLE IAW AMM.

Part: WIRE HARNESS — FAILED (MLG SWITCH) · airframe 38,634 hrs · 34,216 cycles

GEAR DISAGREE. REMOVED AND REPLACED SWITCH HARNESS. FUNCTIONAL TEST OF LANDING GEAR EXTENSION AND RETRACTION SATISFACTORY IAW AMM.

Part: SKIN — CRACKED (LT WING) · airframe 36,510 hrs · 31,964 cycles

CRACK ON LT WING PLANK AT REAR SPAR AT WS 148. REPAIRED WING PLANK IAW REO. NO LEAKS NOTED.

Part: STIFFENER — CHAFED (FUSELAGE) · airframe 36,510 hrs · 31,964 cycles

AFT SIDE FS 621.00 BULKHEAD VERTICAL STIFFENER AT BL 0.0 CHAFED. BLENDED AFT SIDE FS 621.00, BULKHEAD VERTICAL STIFFENER AT BL 0.0 IAW STS EA PERFORMED NDT WITH NO DEFECTS NOTED, RESTORED FINISH.

Part: RECEPTACLE — GOUGED (SERVICE DOOR) · airframe 36,510 hrs · 31,964 cycles

SERVICE DOOR OUTER HANDLE RECEPTACLE GOUGED. REPAIRED IAW STS EA.

Part: HINGE — GOUGED (FUSELAGE) · airframe 36,510 hrs · 31,964 cycles

PASSENGER DOOR PIANO HINGE, FUSELAGE SIDE AFT LANDING, NR 27 IS GOUGED. PASSENGER DOOR HINGE R & R WITH NEW HINGE IAW SRM. NO LEAKS NOTED, PN 600-31529-15.

Part: PANEL — DEFECTIVE (STABILIZER) · airframe 36,510 hrs · 31,964 cycles

LEFT LOWER STABILIZER VISOR PANEL FAILED GAP CHECK. LT LOWER VISOR PANEL REPLACED. GAP CHECK GOOD IAW AMM.

Part: PANEL — DEFECTIVE (STABILIZER) · airframe 36,510 hrs · 31,964 cycles

RIGHT UPPER STABILIZER VISOR PANEL FAILED GAP CHECK. RT UPPER VISOR PANEL REPLACED. GAP CHECK GOOD.

Part: PANEL — DEFECTIVE (STABILIZER) · airframe 36,510 hrs · 31,964 cycles

RIGHT LOWER STABILIZER VISOR PANEL FAILED GAP CHECK. RIGHT LOWER VISOR PANEL REPLACED.

Part: RELAY — FAILED (EMERGENCY LIGHTS) · airframe 32,736 hrs · 28,064 cycles

EMERGENCY LIGHTS TURN ON WHEN THE F/A SWITCH IS OFF AND PILOTS IS IN ARM. REPLACED THE RELAY. OP CHECKED GOOD.

Part: STRINGER — CORRODED (BS 333) · airframe 32,053 hrs · 27,401 cycles

CORROSION UNDER FRAME BS 333 ON STRINGER 26L. C-CHECK, PERFORMED STRINGER SPLICE REPAIR IAW SRM.

Part: SKIN — CORRODED (BS 333) · airframe 32,053 hrs · 27,401 cycles

CORROSION UNDER FRAME BS 333 AT STR 26 AND 27L. C-CHECK, PERFORMED REPAIR ON SKIN IAW EA.

Part: SPAR — GOUGED (HORIZONTAL STAB) · airframe 32,053 hrs · 27,401 cycles

RT HORIZONTAL STABILIZER AFT SPAR, OTBD ELEVATOR HINGE HAS A GOUGE. C-CHECK, REPAIRED GOUGE IAW EA.

Part: SPAR — CHAFED (HORIZONTAL STAB) · airframe 32,053 hrs · 27,401 cycles

RT HORIZONTAL STABILIZER AFT SPAR, CENTER ELEVATOR HINGE HAS CHAFE DAMAGE. C-CHECK, REPAIRED CHAFE DAMAGE IAW EA.

Part: FLOORBEAM — CRACKED (BS 484) · airframe 32,053 hrs · 27,401 cycles

FLOORBEAM ANGLE AT BS 484, LBL 36 IS CRACKED. C-CHECK, INSTALLED NEW FLOORBEAM ANGLE IAW REO 601R-53-41-059, REV B.

Part: FRAME — CORRODED (BS 333) · airframe 32,053 hrs · 27,401 cycles

BS 333 FRAME HAS CORROSION ALONG BOTTOM AFT SIDE FROM S25R - 25L. C-CHECK, R & R FRAME IAW SRM.

Part: FLOORBEAM — CRACKED (BS 484) · airframe 32,053 hrs · 27,401 cycles

FLOORBEAM ANGLE AT BS 484, RBL 27 IS CRACKED. C-CHECK, R & R FLOORBEAM ANGLE IAW REO.

Part: RIB — CRACKED (RT AILERON) · airframe 32,053 hrs · 27,401 cycles

RIGHT AILERON RIB HAS A CRACK AT UPPER FLANGE ATTACH FASTENER, AFT OF INTERCOSTAL. C-CHECK, REMOVED AND INSTALLED NEW AILERON IAW AMM.

Part: FLOORBEAM — CRACKED (BS 484) · airframe 32,053 hrs · 27,401 cycles

CABIN LEFT INBD BS 484, FLOORBEAM ANGLE CRACKED. C-CHECK, R & R FLOORBEAM ANGLE IAW REO.

Part: STIFFENER — CRACKED (BS 409) · airframe 32,053 hrs · 27,401 cycles

BS 409+128, VERTICAL POST AT LBL 18 CRACKED ON INBD AND OTBD SIDES. C-CHECK, R & R VERTICAL POST IAW SRM AND REO.

Part: FRAME — CORRODED (BS 349) · airframe 32,053 hrs · 27,401 cycles

BS 349 FRAME HAS CORROSION ALONG BOTTOM AFT SIDE S25 - 27L. C-CHECK, INSTALLED NEW FRAME IAW REO.

Part: RIB — CHAFED (PAX DOOR VENT) · airframe 32,053 hrs · 27,401 cycles

PASSENGER DOOR VENT FLAP RIB CHAFED FROM ICE BREAK CABLE. C-CHECK, BLENDED CHAFE WITHIN LIMITS OF AND RESTORED FINISH IAW REO.

Part: SKIN — CHAFED (LT WING TE FLAP) · airframe 32,053 hrs · 27,401 cycles

LEFT WING INBD FLAP VANE LOWER L/E CAP SKIN IS CHAFE APPROXIMATELY 28 INCHES FROM OTBD EDGE. C-CHECK, BLENDED OUT DAMAGE RESTORED FINISH IAW REO.

Part: SKIN — CHAFED (LT AILERON) · airframe 32,053 hrs · 27,401 cycles

LEFT WING AILERON UPPER L/E CHAFED. C-CHECK, REPAIRED LT AILERON IAW REO.

Part: SKIN — CORRODED (LT WING) · airframe 32,053 hrs · 27,401 cycles

CORROSION ON LT WINGLET UPPER RADIUS SKIN. C-CHECK, REMOVED CORRODED STRAP ON LT WING TIP AFT UPPER FAIRING AND INSTALLED NEW STRAP IAW EDRN.

Part: BULKHEAD — CRACKED (BS 621) · airframe 32,044 hrs · 27,390 cycles

DURING EDDY CURRENT INSPECTION ON THE AFT PRESSURE BULKHEAD FWD FACE BS 621 AT BL 0. FOUND A CRACK EXTENDING VERTICALY 7 INCHES LONG FROM WL 113 TO WL 106. REPAIRED IAW REO.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 32,044 hrs · 27,390 cycles

EMERGENCY LIGHTS WILL NOT STAY ON WHEN ATTEMPTING TO RUN TEST. CHARGED BATTERIES WITH APU. OPS CHECKED GOOD IAW AMM.

Part: INVERTER — FAILED (EMERGENCY LIGHTS) · airframe 31,773 hrs · 27,113 cycles

FLOOR EMERGENCY LIGHT NEXT TO SEAT 1CD DOES NOT ILLUMINATE. REPLACED FWD EMERGENCY LIGHT INVERTER NR 1 IAW AMM.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 31,781 hrs · 27,123 cycles

MAIN CABIN DOOR AND GALLEY SERVICE DOOR EXIT LIGHTS DO NOT ILLUMINATE. REPLACED NR 1 BATTERY, CHARGER AND TB110 NR 1 TERMINAL BLOCK, AND REPLACED MAIN CABIN DOOR, GALLEY SERVICE DOOR EXIT LIGHT BULBS IAW AMM.

Part: LIGHT — FAILED (CABIN) · airframe 31,658 hrs · 27,000 cycles

FLOOR LEVEL EMERGENCY LIGHTS BEHIND ROW 9 DO NOT ILLUMINATE. R & R EMERGENCY LIGHT IAW AMM.

Part: APU — CONTAMINATED (APU BAY) · airframe 31,566 hrs · 26,905 cycles

STRONG FUEL ODOR THROUGHOUT CABIN WHEN PITCHING DOWN FOR LANDING. CLEANED RESIDUAL FUEL IN APU CONTAINMENT COMPARTMENT.

Part: BRACKET — BENT (NLG) · airframe 30,794 hrs · 26,120 cycles

GEAR DISAGREE & A GEAR DOOR OPEN WARNING. FLT 2637 REPLACED NLG WOW SENSOR BRACKET. ADJUSTED PROX SENSOR & PERFORMED NLG SWING. OPERATIONS CHECKED GOOD. PN ON OFF 16215-105 SN ON OFF N/A.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 30,718 hrs · 26,043 cycles

CORNER LIGHT BULB BURNED OUT ON OVERWING EXIT SIGN. FLT 2646 RELAMPED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,083 hrs · 25,406 cycles

EMERGENCY OVERHEAD POD LIGHT BURNED OUT. FLT#2605 RELAMPED.

Part: SKIN — DENTED (FUSELAGE) · airframe 29,704 hrs · 25,011 cycles

LT AFT FS SKIN BETWEEN FS736.00 & FS755.00. & STRINGERS 18L - 20L, IS DENTED & DAMAGED. SERVICE REPAIRED FS SKIN IAW REO.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,686 hrs · 23,880 cycles

NR 2 EMERGENCY OVERHEAD LIGHT BURNED OUT. (FLT 2627) RELAMPED EMERGENCY LIGHT.

Part: BRACKET — BENT (NLG) · airframe 28,222 hrs · 23,334 cycles

NOSE GEAR DISAGREE INDICATION WARNING. (FLT 2608) REPOSITIONED NOSE GEAR SENSOR BRACKET SO THAT TARGET WOULD NOT HIT THE SENSOR.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,965 hrs · 23,058 cycles

RIGHT FUSELAGE NR 2 AND NR 4 EMERGENCY LIGHTS ARE OUT. (SERVICE) RELAMPED EMERGENCY LIGHTS.

Part: TRUNNION — CRACKED (RT WING) · airframe 27,965 hrs · 23,058 cycles

FOUR CRACKS ON RIGHT WING TRUNNION. (C-CHECK) REPAIR OF THE RIGHT WING TRUNNION PER REO.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 27,965 hrs · 23,058 cycles

ANGLE CRACKED AFT OF FS 621 BULKHEAD AT STRINGER 14L AND 14R. (C-CHECK) REPLACED ANGLE AFT OF FS 621 BULKHEAD AT STRINGER 14L AND 14R IN REFERENCE TO CRJ 200 SRM.

Part: POST — CRACKED (FUSELAGE) · airframe 27,965 hrs · 23,058 cycles

CRACK ON RIGHT FS 409+128 VERTICAL POST RBL 18 IN OUTBOARD C-CHANNEL, AFT RADIUS. (C-CHECK) REPAIRED PER REO.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 27,965 hrs · 23,058 cycles

CRACK ON FS 621 AFT PRESSURE BULKHEAD FORWARD FACE AT WL 131.0 LBL 27.5 ABOVE AFT CARGO DOOR TRACK. (C-CHECK) REPAIRED PER REO.

Part: POST — CRACKED (FUSELAGE) · airframe 27,965 hrs · 23,058 cycles

CRACK ON FS 409+128 CENTER VERTICAL POST BL 0.0 IN LEFT C-CHANNEL, AFT RADIUS. (C-CHECK) REPLACED POST ON FS 409+128 BL 0.0 IN REFERENCE TO CRJ-200 SRM.

Part: CABLE — FAILED (CABIN) · airframe 27,838 hrs · 22,937 cycles

AFT FLOOR LEVEL EMERGENCY ILLUMINATION SYSTEM IS OUT. (FLT 4642) REPLACED FLOOR TRACK CABLE.

Part: CONNECTOR — DIRTY (CABIN) · airframe 27,838 hrs · 22,937 cycles

RIGHT SIDE FLOOR LEVEL EMERGENCY LIGHT IS OUT. (FLT 4642) CLEANED CONNECTIONS ON RIGHT SIDE FLOOR LEVEL EMERGENCY LIGHT.

Part: LIGHT — DISCONNECTED (CABIN) · airframe 27,724 hrs · 22,826 cycles

AFT EMERGENCY FLOOR LEVEL LIGHTING STRIP IS OUT. (FLT 4740) FOUND AFT EMERGENCY LIGHT STRIP WAS NOT CONNECTED. RECONNECTED EMERGENCY LIGHTING.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,162 hrs · 22,265 cycles

AFT 3 FEET OF FLOOR LEVEL EMERGENCY LIGHTS ARE OUT. (SERVICE) REPLACED AFT SEGMENT OF FLOOR EMERGENCY LIGHTS.

Part: CHARGER — FAILED (CABIN) · airframe 26,968 hrs · 22,084 cycles

NR 1 AND NR 2 OVERHEAD EMERGENCY LIGHTS ARE OUT. (FLT 4468) REPLACED LAST ELBP CHARGER.

Part: CHARGER — FAILED (CABIN) · airframe 26,757 hrs · 21,890 cycles

FLOOR EMERGENCY LIGHTING FROM 9 ROW AFT IS OUT. (FLT 4736) REPLACED NR 4 EMERGENCY BATTERY CHARGER.

Part: CHARGER — FAILED (CABIN) · airframe 26,734 hrs · 21,864 cycles

NR 2 & 4 OVERHEAD EMERGENCY LIGHTS ARE OUT. (SERVICE) REPLACED ALL 4 EMERGENCY LIGHT CHARGER ASSEMBLIES.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,734 hrs · 21,864 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4718) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,680 hrs · 21,810 cycles

AFT OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4458) RELAMPED EMERGENCY LIGHT.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 26,564 hrs · 21,692 cycles

ALL EMERGENCY LIGHTS THAT RUN OFF OF NR 4 BATTERY PACK ARE OUT. (SERVICE) INSTALLED NEW BATTERY CHARGER ASSEMBLY.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 26,498 hrs · 21,622 cycles

FLOOR LEVEL EMERGENCY LIGHTING STRIP DOES NOT ILLUMINATE AFT OF OVERWING EXITS. (FLT 4562) REPLACED NR 4 EMERGENCY LIGHT BATTERY PACK AND CHARGER. P/N: AD-2013-1A S/N OFF: 82524

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 26,213 hrs · 21,372 cycles

RIGHT OVERWING EXTERIOR EMERGENCY EXIT LIGHT IS OUT. (FLT 4458) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,082 hrs · 21,236 cycles

LEFT OVERWING FORWARD EMERGENCY LIGHT IS OUT. (FLT 4458) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 26,067 hrs · 21,222 cycles

OVERHEAD EMERGENCY EXIT SIGN AT ROW 8 IS OUT. (SERVICE) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,052 hrs · 21,210 cycles

NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4686) RELAMPED EMERGENCY LIGHT.

Part: CONNECTOR — BROKEN (NLG) · airframe 26,023 hrs · 21,184 cycles

NOSE GEAR UP DISAGREE. (FLT 4584) REPLACED PSEU AND PSEU CONNECTOR.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,868 hrs · 21,037 cycles

RIGHT AFT OVERWING EMERGENCY LIGHT IS OUT. (FLT 4587) RELAMPED EMERGENCY LIGHT.

Part: WIRE HARNESS — FAULTY (NLG) · airframe 25,810 hrs · 20,987 cycles

NOSE WHEEL GEAR DISAGREE. (FLT 4788) REPLACED THE NLG ELECTRICAL HARNESS ASSEMBLY S21.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,194 hrs · 20,462 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4582) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,603 hrs · 19,924 cycles

EMERGENCY LIGHT ABOVE ROW 10 IS INOPERATIVE. (FLT 4594) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,800 hrs · 19,235 cycles

NR 2 EMERGENCY CEILING LIGHT INOP. (FLT 4747) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,732 hrs · 19,176 cycles

NR 3 EMERGENCY FLOODLIGHT INOP. (FLT 4812) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 22,889 hrs · 18,432 cycles

EMERGENCY LIGHT INOP IN REAR OF AIRCRAFT. (FLT 4503) OPERATIONAL CHECK OF LIGHT NORMAL.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 22,762 hrs · 18,322 cycles

FORWARD BULKHEAD PARKING BRAKE CABLE ACCESS PORT CRACKED. (SVC CHECK)

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,802 hrs · 17,563 cycles

NR 4 CEILING EMERGENCY LIGHT INOP. (FLT 4608) RELAMPED EMERGENCY LIGHT.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 20,860 hrs · 16,848 cycles

FLT 4680 - CEILING LEVEL EMERGENCY FLOODLIGHT ABOVE ROW 10 INOP. RELAMPED.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 20,392 hrs · 16,504 cycles

DURING C-CHECK, FS 280 FLOORBEAM LBL9 UPPER FLANGE CRACKED. REPAIRED PER SRM.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 20,392 hrs · 16,504 cycles

C-CHECK, 2 CLIPS AT FS 280 BELOW FLOOR LINE RBL9 CRACKED. REPAIRED PER SRM.

Part: ANGLE — CRACKED (BS 625 S14R) · airframe 20,392 hrs · 16,504 cycles

DURING C-CHECK, FS 625 RIGHT SIDE ANGLE AT STR14 CRACKED. REPLACED PER REO.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 19,519 hrs · 15,834 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS BURNED OUT. FLIGHT 3888. INSTALLED A SERVICEABLE BULB. OPS CHECKS GOOD.

Part: WEB — CRACKED (PAX DOOR) · airframe 15,671 hrs · 12,912 cycles

PAX DOOR - THE FWD WEB IS CRACKED UNDER THE HANDRAIL STOW BRACKET AND IN THE RADIUS BETWEEN THE 3RD & 4TH FIXED STEPS. (DISCOVERED DURING C-CHECK INSPECTION) INSTALLED EXTERNAL DOUBLER, REPAIR ANGLES & HANDRAIL STOW BRACKET ON THE FWD PAX DOOR SIDE PNL IAW CRJ200 REO 601R-52-11-702, REV A REPAIR ZONE 2.

Part: ATTACH BRACKET — CRACKED (BS 484) · airframe 15,671 hrs · 12,912 cycles

FOUND LT STA484 BL27 AND BL36 CLIPS CRACKED UPPER RADIUS, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED ANGLE, CLIP AND PULLEY GUIDE PER REO 601R 53-41-059.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 15,671 hrs · 12,912 cycles

LT MLG WHEEL WELL HAS BRAKE TRANSDUCER BRACKET CRACKED BROKEN ON TOP MID AREA OF WHEEL WELL, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED NEW PART PER CRJ200 SRM 51-40-06 PG 1-3; 15-17.

Part: WEB — CRACKED (PAX DOOR) · airframe 15,671 hrs · 12,912 cycles

PAX DOOR - THE AFT WEB IS CRACKED UNDER THE HANDRAIL STOW BRACKET AND IN THE RADIUS BETWEEN THE 3RD & 4TH FIXED STEPS. (DISCOVERED DURING C-CHECK INSPECTION) INSTALLED REPAIRS TO PAX DOOR STEP 2 & 3 AFT SIDE WALL IAW CRJ200 REO 601R-52-11-702 REV A "REPAIR FOR MULTI-SITE DAMAGES: ZONE 2,3,4" (SHEET 8).

Part: HANDLE — CRACKED (PAX DOOR) · airframe 15,671 hrs · 12,912 cycles

PAX DOOR - THE OUTER HANDLE IS CRACKED. (DISCOVERED DURING C-CHECK INSPECTION) REPLACED PAX DOOR OUTER HANDLE AS PER CRJ200 AMM 52-11-03-000-802 7 52-11-03-400-802.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 15,671 hrs · 12,912 cycles

CRACK AT LOWER FLOORBEAM ST280 LT BL10. (DISCOVERED DURING C-CHECK INSPECTION) INSTALLED REPAIR ANGLE, CLIPS AND FILLERS AT STA 280, LBL10.0 IAW CRJ200 REO 601R-53-11-171, REV C, REPAIR SCHEME A.

Part: BRACKET — CRACKED (RT WING) · airframe 15,671 hrs · 12,912 cycles

RT MLG WHEEL WELL BRAKE TRANSDUCER BRACKET CRACKED BROKEN ON TOP MID AREA OF WHEEL WELL, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED NEW PART PER CRJ200 SRM 51-42-06 PG 1-3, 15-17.

Part: MOUNT BRACKET — CRACKED (PAX DOOR) · airframe 15,671 hrs · 12,912 cycles

PAX DOOR - THE DOOR ASSIST MOTOR MOUNTING BRACKET IS CRACKED. (DISCOVERED DURING C-CHECK INSPECTION)INSTALLED NEW STIFFENER IAW CRJ200 SRM 51-40-11 & SRM 51-42-06.

Part: STRINGER CLIP — CRACKED (BS 625) · airframe 15,671 hrs · 12,912 cycles

625 14L AND 14R CLIPS CRACKED, DISCOVERED DURING C-CHECK INSPECTION. REPLACED CRACKED CLIPS AT 14L & 14R ZONE 625 AS PER CRJ200 SRM 51-42-21.

Part: ATTACH BRACKET — CRACKED (BS 484) · airframe 15,671 hrs · 12,912 cycles

FOUND RT STA484 BL27 CLIP CRACKED UPPER RADIUS, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED CLIPS AT BL27 AND BL36 PER REO 601R 53-41-059 NOTES 1-4.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 15,671 hrs · 12,912 cycles

CRACK AT LOWER FLOORBEAM ST280 RBL10. (DISCOVERED DURING C-CHECK INSPECTION) INSTALLED REPAIR ANGLE, FILLER & NEW CLIP AT STA 280, RBL10.0 IAW CRJ200 REO 601R-53-11-171 REV C REPAIR SCHEME A.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 13,914 hrs · 11,588 cycles

FIRST CABIN CEILING LEVEL EMERGENCY FLOODLIGHT INOP. REPLACED FIRST CEILING LIGHT FOR INTERIOR EMERGENCY LIGHTING SYSTEM. OPERATIONAL CHECKS GOOD, PN 1317.

Part: TRIM SYSTEM — INOPERATIVE (STAB) · airframe 13,338 hrs · 11,172 cycles

PILOT SIDE STAB TRIM INOPERATIVE. REPLACED CAPTAIN'S STAB TRIM SWITCH ASSEMBLY IAW MM 27-41-05.

Part: COMPUTER — MALFUNCTIONED (STALL PROTECTION) · airframe 13,073 hrs · 10,974 cycles

CONTINUOUS CYCLE, ON/OFF OF STALL FAIL CAUTION MSG. REPLACED STALL PROTECTION COMPUTER IAW MM 27-35-01. OPERATIONAL CHECK GOOD, PN ON 3995100208 SN OFF 681.

Part: DOOR — OPEN (O2 SERVICE) · airframe 1,225 hrs · 10,339 cycles

FLIGHT 5487 - STALL FAIL MESSAGE AFTER TAKEOFF. FOUND O2 SERVICE DOOR AND GALLEY WATER SERVICE DOOR OPEN. INSPECTED AND FOUND LATCHES WORK PROPERLY. CLOSED DOORS.

Part: LIGHT — INOPERATIVE (CABIN)

DURING HANGAR MAINTENANCE IN BTR, THE AFT EMERGENCY CEILING LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE AFT EMERGENCY CEILING LIGHT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: CONNECTOR — DISCONNECTED (CABIN)

DURING A GROUND INSPECTION, THE EMERGENCY FLOOR TRACK LIGHT BETWEEN ROWS 6 AND 7 OPERATIED INTERMITTENTLY. MAINTENANCE RESECURED THE CONNECTION TO THE EMERGENCY FLOOR TRACK LIGHT BETWEEN ROWS 6 AND 7 AND ALSO REMOVED AND REPLACED A SECTION OF THE FLOOR TRACK COVER. OPERATIONAL CHECKS GOOD. AIRCRAFT OF FOR SERVICE.

Part: STEP — BROKEN (PAX DOOR) · airframe 9,484 hrs

DURING A ROUTINE SERVICE CHECK, THE LOWER STEP ON THE PASSENGER DOOR WAS FOUND BROKEN AND THE STEP ACTUATING ROD WAS FOUND BENT. MAINTENANCE REMOVED AND REPLACED THE LOWER STEP ASSEMBLY AND REPAIRED THE STEP ACTUATING ROD ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE.

Part: ACM — ODOR (LEFT & RIGHT)

DURING DESCENT, AN OILY ODOR FILLED THE CABIN AND COCKPIT. THE AIRCRAFT LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED THE LT AND RT AIR CYCLE MACHINES. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE.

Part: HANDLE — BROKEN (E/E BAY DOOR)

DUIRNG AN OVERNIGHT CHECK IN DFW, THE AVIONICS BAY DOOR HANDLE WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE AVIONICS BAY DOOR HANDLE ASSEMBLY. DURING INSTALLATION THE DOOR HANDLE CRACKED AROUND THE FLANGE. MAINTENANCE REMOVED AND REPLACED THE DOOR HANDLE DOOR ASSEMBLY AGAIN. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: LIGHT — MISSING (CABIN)

DURING A GROUND INSPECTION, THE EMERGENCY FLOOR LIGHT NEAR ROW 8 WAS FOUND MISSING. MAINTENANCE REPLACED THE EMERGENCY FLOOR LIGHT NEAR ROW 8. OPERATION CHECKS GOOD. AIRCRAFT OK FOR SERVICE.

Part: CLIP — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE CLIPS AT FS 484, LBL 36 AND RBL 36 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE CLIPS AT FS 484, LBL 36 AND RBL 36 IAW ASA EO 600-53-0098. (M)

Part: CLIP — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE CLIP AT FS 484, RBL 27 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE CLIP AT FS 484, RBL 27 IAW ASA EO 600-53-0098. (M)

Part: CLIP — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE CLIPS AT FS 280, LBL 9 INBOARD AND OUTBOARD WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE CLIPS AT FS 280, LBL 9 INBOARD AND OUTBOARD IAW SRM 51-42-21. (M)

Part: SILL — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE CARGO DOOR SILL PLATE AT FS 562.72-589 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE CARGO DOOR SILL PLATE AT FS 562.72-589 IAW ASA EO 600-53-0095. (M)

Part: SUPPORT BEAM — CRACKED (CENTER ENGINE)

DURING A C-CHECK IN MCN, THE CENTER ENGINE SUPPORT BEAM UPPER AND LOWER WEB AT BL 0 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE CENTER ENGINE SUPPORT BEAM UPPER AND LOWER WEB AT BL 0 IAW ASA EO 600-53-0072. (M)

Part: STEP — CRACKED (PAX DOOR)

DURING A C-CHECK IN MCN, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE IS REMOVING AND REPLACING THE BOTTOM STEP ON THE PASSENGER DOOR. (M)

Part: INTERCOSTAL — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE INTERCOSTALS AT FS 621-625.30 NEAR STRINGERS 14L AND 14R WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE INTERCOSTALS AT FS 621-625.30 NEAR STRINGERS 14L AND 14R. (M)

Part: FLOOR SUPPORT — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE FLOOR SUPPORT ANGLES AT FS 621, AFT PRESSURE BULKHEAD IN THE CARGO AREA ON THE LEFT AND RIGHT SIDES WERE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE FLOOR SUPPORT ANGLES AT FS 621, AFT PRESSURE BULKHEAD IN THE CARGO AREA ON THE LEFT AND RIGHT SIDES IAW ASA EO 600-53-0105. (M)

Part: CLIP — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE CLIP AT FS 280, RBL 9 INBOARD WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE CLIP AT FS 280, RBL 9 INBOARD IAW SRM 51-42-21. (M)

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT)

DURING A GROUND INSPECTION, THE EMERGENCY EXIT LIGHT AT THE PASSENGER DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE EMERGENCY EXIT LIGHT AT THE PASSENGER DOOR. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: LAMP — BURNED OUT (CABIN)

DURING SCHEDULED INSPECTION, THE AFT CEILING EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BURNED OUT EMERGENCY LIGHT BULB. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE.

Part: BULB — BURNED OUT (CABIN)

FLT 4787 - DURING A SCHEDULED INSPECTION IN XNA, THE LEFT EXTERNAL EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BURNED OUT EXTERIOR EMERGENCY LIGHT BULB. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: HYDRAULIC LINE — RUPTURED (RT ENGINE)

FLT 4696 - DURING FLIGHT FROM ATL TO SWF, PILOT SAW RIGHT SIDE HYDRAULIC QUANTITY AND PRESSURE INDICATIONS AT ZERO. AN EMERGENCY WAS DECLARED. AIRCRAFT RETURNED TO ATL WITH NO FURTHER INCIDENTS. MAINTENANCE FOUND PRESSURE LINE ON THE RIGHT ENGINE TO BE RUPTURED. MAINTENANCE REMOVED AND REPLACED HYDRAULIC PRESSURE LINE ON RIGHT ENGINE. THE ENGINE DRIVEN PUMP WAS ALSO REPLACED DUE TO IT OPERATING WITHOUT FLUID FOR 46 MINUTES. OPERATIONAL AND LEAK CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. (M)