N903EV

Part: NONE — FAILED · airframe 41,737 hrs · 38,473 cycles

L PACK HI PRESS CAUTION MESSAGE AFTER TAKE OFF. RAN THE QRH, DID NOT RESOLVE ISSUE. RETURNED TO FIELD. (FLIGHT 4762 - FILED CLOSED)REMOVED AND REPLACED LH A/C PRESSURE SWITCH PER CRJ 200 AMM 21-51-22. OPS CHECK GOOD DEFECTS NOTED.

Part: NONE — DENTED · airframe 41,438 hrs · 38,186 cycles

TRANSFER FROM EAML 896303 : CREATED FROM FORWARD DISCREPANCY. PLEASE REFERENCE AML 896216 DURING BURST TIRE INSPECTION FOUND MULTIPLE LARGE DENTS ON FUSELAGE AFT OF NOSE LANDING GEAR. THIS HAS BEEN DETERMINED TO BE A MAJOR REPAIR PER GMM 3-26 (FILED - CLOSED) COMPLIED WITH TRIPLER AND DOUBLER REPAIRS TO FUSELAGE SKIN PANEL BETWEEN FS 235.00 - FS 280.00 & STR25L - STR25R AT DAMAGE LOCATIONS #1 AND #4 IN REFERENCE TO REO 601R-53-11-3767 REV-- DATE 2022-05-07, AND REO 601R-51-00-309 REV A. COMPLIED WITHSTRUCTURAL MAJOR REPAIR RII CARD 51-900-1003-SKY. / *MAJOR REPAIR / REFER TO CP 24753180 FOR DRESS-BACK OF DENT #2, #3, #5,#6, #7, #8, AND #9 / REFER TO CP 24765434 FOR NDT OF DRESS-BACK/REWORK LOCATIONS / REFER TO CP 24758980 FOR NDT OF CUTOUT OF DENT #4 / REFER TO CP 24764343 FOR NDT OF CUTOUT OF DENT #1 / REFER TO CP 24772274 FOR PRESSURIZATION CHECK OF REPAIRS

Part: NONE — FAILED · airframe 40,630 hrs · 37,470 cycles

GEAR DISAGREE WARNING MESSAGE ON THE CLIMB OUT OF FAT. NOSE GEAR REMAINED DOWN WHILE MAIN GEAR RETRACTED NORMALLY. WHEN PULLING THE MANUAL GEAR RELEASE HANDLE AS PER THE QRH ALL GEAR EXTENDED INDICATING GREEN AND LOCKED. ASSOCIATED NW STEERING CAUTION MESSAGE DURING THE DISAGREE WARNING BUT CLEARED WITH COMPLETION OF THE QRH PROCEDURE. (FLIGHT 5516 - FILED CLOSED) THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 23719032 WITH THE FOLLOWING CORRECTIVE ACTION: "REFER TO CP 23719895 - T/S GEAR DISAGREE, REFER TO CP 23719931 - REPACKED NLG SHOCK STRUT. REFER TO CP 23719797 - PERFORMED FULL NLG STRUT SERVICE, REFER TO CP 23719808 - LANDING GEAR MECHANICAL AND HYDRAULIC HEALTH CHECK, NO DEFECTS WERE NOTED DURING NUMEROUS GEAR SWINGS."

Part: NONE — MALFUNCTIONED · airframe 40,629 hrs · 37,469 cycles

ON DEPARTURE OUT OF FAT GEAR DISAGREE WARNING. NOSE GEAR REMAINED DOWN, MAIN GEAR RETRACTED NORMALLY. AFTER FOLLOWING QRH ALL GEAR EXTENDED AND LOCKED DOWN. ASSOCIATED NW STEERING CAUTION MESSAGE WITH DISAGREE. MESSAGED CLEARED AFTER QRH. (FL# 6971 - FILED CLOSED) THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 23681470 WITH THE FOLLOWING CORRECTIVE ACTION: "INSPECTED NLG AND FOUND WOW NO.2 AND CENTERED HARNESS ASSEMBLY DAMAGED, CENTERED HARNESS BRACKET BENT. REMOVED AND REPLACED THE WOW NO.2 AND CENTERED HARNESS ASSEMBLY WITH A SERVICEABLE HARNESS. REMOVED AND REPLACED BRACKET WITH A NEW BRACKET. PERFORMED NUMEROUS GEAR SWINGS WITH NO FAULTS NOTED, EVERYTHING SATISFACTORY. CLEARED PSEU STORED CODES AND PERFORMED OPERATIONAL TEST OF PSS SYSTEM. ALL FOUND SATISFACTORY."

Part: WINDSHIELD — ARCED (COCKPIT) · airframe 39,443 hrs · 36,411 cycles

CLIMBING THROUGH 22,000FT FO NOTICED SOME ARCING GOING VERTICALLY FROM THE LEFT LOWER THIRD OF CAPT WINDSHIELD, ARCING PROGRESSED HALFWAY UP THE WINDSHIELD, AND THEN A POP WAS HEARD AND WINDSHIELD SHATERRED TO THE OUTER EDGES, NO PRESSURIZATION LOSS, NO EMERGENCY DECLARED, NO OVERWEIGHT LANDING FLIGHT 4704 - FILED CLOSED REMOVED DAMAGED LH WINDSHIELD REFERENCING APPLICABLE STEPS OF CRJ200 AMM 56-11-01. INSTALLED SERVICEABLE LH WINDSHIELD PER TASK CARD 56-220-1000-SKY AND AMM 56-11-01, LEAK CHECKS AND OPS CHECK GOOD AT THIS TIME. AIRCRAFT OK FOR SERVICE. / TORQUE WRENCH: / S/N- 0819102467 / CAL DUE- 06/30/2021

Part: WARNING MESSAGE — FALSE ACTIVATION (TE FLAP SYS)

FLAPS FAIL CAUTION MESSAGE ON APPROACH TO SGF WHEN SELECTING FLAPS 8 AND 20. FLAPS EICAS INDICATION REMAINED AT 0. RAN QRH. FILED CLOSED RO 10/4/2020. RESET AND OPERATED FLAPS 5 FULL CYCLES AND COMPLETED AD COMPLIANCE FORM. OK TO CONTINUE IN SERVICE FOR 10 FLIGHT CYCLES. COMPLIED WITH IN ACCORDANCE WITH FIM FMRP CHAPTER 27 RESET PROCEDURES AND AD. MCI CREATED FOR FULL AD COMPLIANCE BY MCC.

Part: STIFFENER — CORRODED (PAX DOOR) · airframe 38,551 hrs · 35,576 cycles

CORROSION FOUND UPPON REMOVAL OF PAX DOOR AFT WEB STIFFENER PN 601R317722-1 (C-CHECK) RO 4/4/2020 REMOVED AND REPLACED PAX DOOR AFT WEB STIFFENER. REF CRJ 200 SRM. SEE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.

Part: STIFFENER — CRACKED (PAX DOOR) · airframe 38,551 hrs · 35,576 cycles

CRACK FOUND AT PAX DOOR AFT WEB STIFFENER PN 601R317721-1 (C-CHECK) RO 4/4/2020 REMOVED AND REPLACED PAX DOOR AFT WEB STIFFENER. REF CRJ 200 SRM. SEE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.

Part: FRAME — CRACKED (FUSELAGE) · airframe 38,551 hrs · 35,576 cycles

JUST ABOVE AFT CARGO ENTRY AT FS 605.0 STR 9L THERE IS A SUSPECT CRACK AT RIVET LOCATION. ABOVE AND BELOW THE STRINGER. (C-CHECK) RO 4/4/2020 REPAIRED FS605 STR9L FRAME REF BOMBARDIER REO. NO LEAKS NOTED. SEE CONTINUE CARD FOR DETAILS.

Part: STOP FITTING — CHAFED (FUSELAGE) · airframe 38,551 hrs · 35,576 cycles

* AVIONICS BAY DOOR CUTOUT, R/H AFT STOP FITTING ON FUSELAGE IS CHAFED, MARKED. (C-CHECK) RO 4/4/2020 INSTALLED NEW AFT R/H STOP FITTING IN AVIONICS BAY DOOR CUTOUT PER DRAWING COMPLETED SKYWEST TASKCARD.

Part: STOP FITTING — CHAFED (FUSELAGE) · airframe 38,551 hrs · 35,576 cycles

* AVIONICS BAY DOOR CUTOUT, L/H FORWARD STOP FITTING ON FUSELAGE IS CHAFED, MARKED. (C-CHECK) RO 4/4/2020 INSTALLED NEW FORWARD L/H STOP FITTING IN AVIONICS BAY DOOR CUTOUT PER DRAWING COMPLETED SKYWEST TASKCARD.

Part: ATTACH ANGLE — CORRODED (NLG WW) · airframe 38,551 hrs · 35,576 cycles

* INSIDE NOSE WHEEL WELL FWD WALL AT FS 169.0 HAS CORROSION ON ATTACH ANGLE (C-CHECK) RO 4/4/2020 REMOVED AND REPLACED NLG WHEEL WELL FWD WALL BOTTOM ATTACH ANGLE AT FS169 REF CRJ200 SRM AND BOMBARDIER DWG. SEE CONTINUE CARD FOR DETAILS.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 38,551 hrs · 35,576 cycles

LBL 9 FLOOR SEAT TRACK AT APROX, FS. 349-409+128 HAS MULTI AREAS OF CORROSION (MARKED IN RED) (C-CHECK) RO 4/4/2020 REPLACED THE PASSENGER SEAT RAILS (LBL9 BTWN FS394.00 - FS409+128). REF CRJ200 AMM TASK. REPLACED HARDWARE AS NEEDED

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 38,551 hrs · 35,576 cycles

*CORROSION FOUND ON R/H FLOOR SILL FROM FS 559 TO APPROX FS 559+86. AT MULTIPLE LOCATIONS. (MARKED WITH RED GREASE PENCIL) (C-CHECK) RO 4/4/2020 INSTALLED NEW R/H FLOOR SILL FROM FS559.00+48 TO FS559.00+112. REF BOMBARDIER DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 38,551 hrs · 35,576 cycles

FS.333 FRAME FROM STRG. 26L TO 26R CORRODED (MARKED) (C-CHECK) RO 4/4/2020 REPLACED FS333 LOWER FRAME SECTOR PER DRAWING AND CRJ200SRM. COMPLETED SKYWEST TASK CARD.

Part: POST — DEFECTIVE (FUSELAGE) · airframe 38,551 hrs · 35,576 cycles

F.S 409+128 BL 0.0 LH AFT VERTICAL POST RADIUS DEFECT NOTED. (C-CHECK) RO 4/4/2020 REMOVED AND REPLACED FS409+128 RH AND LH POST AT BL0 AND LH ATTACHING CLIP REF BOMBARDIER DWG AND REO. NO LEAKS NOTED. SEE CONTINUE CARD FOR DETAILS. CCOMPLIED WITH ATTACHED TASK.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 38,551 hrs · 35,576 cycles

RBL 9 FLOOR SEAT TRACK AT APROX. FS . 349-409+128 HAS MULTI. AREAS OF CORROSION (MARKED IN RED) (C-CHECK) RO 4/4/2020 REPLACED THE PASSENGER SEAT RAILS (RBL9 BTWN FS394.00 - FS409+128). REF CRJ200 AMM TASK. REPLACED HARDWARE AS NEEDED.

Part: MOUNT BRACKET — CRACKED (PAX DOOR) · airframe 38,551 hrs · 35,576 cycles

*PAX DOOR ASSIST MOTOR, MOUNT BRACKET IS CRACKED. (LOWER BRACKET WHEN DOOR IN OPEN POSITION) (C-CHECK) RO 4/4/2020 REMOVED AND REPLACED PAX DOOR MOTOR ASSIST MOUNT BRACKET. REF CRJ 200 SRM. SEE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.

Part: WEB — CORRODED (PAX DOOR) · airframe 38,551 hrs · 35,576 cycles

*PAX DOOR AFT WEB HAS CORROSION ON THE STEP MOUNT FACES. (TRED AND RISER) (AREAS MARKED WITH RED GREASE PENCIL) (C-CHECK) RO 4/4/2020 REPLACED AFT PAX DOOR WEB REF CRJ200 SRM AND BOMBARDIER REO. SEE CONTINUE CARD FOR DETAILS OF WORK PERFORMED.

Part: FLAP — CHAFED (PAX DOOR) · airframe 38,551 hrs · 35,576 cycles

*PAX DOOR PRESSURE VENT FLAP IS CHAFED ON THE INNER SURFACE IN 3EA LOCATIONS. (AREAS MARKED WITH RED GREASE PENCIL) (C-CHECK) RO 4/4/2020 REMOVED AND REPLACED THE PAX DOOR PRESSURE VENT FLAP REF. CRJ200 AMM. OPS TEST GOOD

Part: PLATE — CORRODED (FUSELAGE) · airframe 38,551 hrs · 35,576 cycles

* PAX DOOR CUTOUT INSIDE FWD LOWER CORNER HAS CORROSION ON SEAL RETAINER BACKING PLATE (C-CHECK) RO 4/4/2020 REMOVED CORROSION FROM PAX DOOR CUTOUT INSIDE FWD LOWER CORNER ON SEAL RETAINER BACKING PLATE REF CRJ200 SRM, BLENDED AREA IS 100% MATERIAL LOSS, REMOVED AND INSTALLED 1EA NEW PASSENGER DOOR SEAL SURROUND ON PAX DOOR CUTOUT INSIDE FWD LOWER CORNER REF CRJ200 SRM AND BOMBARDIER DWG, AND BOMABRDIER REO, RESTORED FINISH REF CRJ200 SRM, SEE CONTINUATION CARD FOR DETAILS. SEE ATTACHED TASK

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 38,551 hrs · 35,576 cycles

*CORROSION FOUND ON L/H FLOOR BEAM CAP LBL 9 FROM FS 559 TO APPROX FS 559+80 AT MULTIPLE AREAS. (MARKED WITH RED GREASE PENCIL) (C-CHECK) RO 4/4/2020 REPAIRED LBL9 FLOOR BEAM FLANGE BETWEEN FS559 AND FS559+16 PER REO AND COMPLETED THE TASK CARD. BLENDED CORROSION ON LBL9 FLOOR BEAM CAP FROM FS559+16 TO FS559+80 IS WITHIN LIMITS PER REO.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 38,551 hrs · 35,576 cycles

L/H MOST AFT SIDE SEAT RAIL @ APPROX.. FS.544 HAS 8 EA. MARKED IN RED LOCATIONS OF DAMAGE/CORROSION (C-CHECK) RO 4/4/2020 REPLACED SIDE SEAT TRACK L/H FS544 WITH A SERVICEABLE UNIT REF CRJ-200 AMM AND REO, SEE CONTINUATION CARD FOR DETAILS.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 38,551 hrs · 35,576 cycles

R/H MOST AFT SIDE SEAT RAIL DAMAGED AT 4EA. MARKED RED LOCATIONS( CORRODED, GOUGED ,SCRATCHED) (C-CHECK) RO 4/4/2020 REPLACED RH SEAT TRACK (FS559.00+16 - FS559.00+112) WITH A SERVICEABLE UNIT REF CRJ-200 AMM, SEE CONTINUATION CARD FOR DETAILS.

Part: BRACKET — CHAFED (PAX DOOR) · airframe 38,551 hrs · 35,576 cycles

*PAX DOOR MOTOR ASSIST CABLE PULLEY, SWIVEL BRACKET IS CHAFED. (C-CHECK) RO 4/4/2020 REMOVED PAX DOOR MOTOR ASSIST SWIVEL PULLEY BRACKET ASSY REF CRJ200 AMM AND INSTALLED NEW PAX DOOR MOTOR ASSIST SWIVEL PULLEY BRACKET ASSY REF CRJ200 AMM. (PARTS REPLACED = 1 YOKE ASSY, 1 PULLEY, 2 CLEVIS PINS, 3 COTTER PINS, 1 SPECIAL WASHER, 4 FLAT WASHERS)

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 38,551 hrs · 35,576 cycles

EVIDENCE OF CORROSION FOUND ON AFT CARGO DOOR SILL (C-CHECK) RO 4/4/2020 REPLACED CARGO DOOR SILL PER DRAWING 601R35011 (REV N) AND REO AND CRJ200SRM. COMPLETED SKYWEST TASK CARD.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 38,551 hrs · 35,576 cycles

L/H APROX. F.S 513- TO 544 SIDE SEAT TRACK HAS MULTIPLE AREAS OF DAMAGE/CORROSION (AS MARKED IN RED) (C-CHECK) RO 4/4/2020 REPLACED SIDE SEAT TRACK L/H APPROX. FS513 TO 544 WITH A SERVICEABLE UNIT REF CRJ-200 AMM, SEE CONTINUATION CARD FOR DETAILS.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 38,551 hrs · 35,576 cycles

SIDE SEAT TRACK JUST FWD OF L/H EMER. EXIT HAS AREAS OF MARKED (IN RED) CORROSION (C-CHECK) RO 4/4/2020 REPLACED PASSENGER SIDE SEAT RAIL (LH FS409.00 + 112 - FS439.00). REF CRJ200 AMM TASK. REPLACED HARDWARE AS NEEDED TORQUE WRENCH TUC4980 CAL DUE 31 JAN 21 SEE CONTINUATION CARD FOR ADDITIONAL DETAILS

Part: FLOORBEAM — BUCKLED (FUSELAGE) · airframe 38,551 hrs · 35,576 cycles

LBL 9 FROM FS409+16-409+64 FLOORBEAM LOWER OUTBOARD FLANGE BUCKLED IN MULTIPLE SPOTS (AS MARKED IN RED AND TAPE (C-CHECK) RO 4/4/2020 REMOVED AND REPLACED WITH NEW FS409+16 0 FS409+64, LBL9 FLOOR BEAM WEB REF CRJ200 SRM AND BOMBARDIER DWG. COMPLIED WITH TASK CARD

Part: FRAME — CORRODED (FUSELAGE) · airframe 38,551 hrs · 35,576 cycles

FS.319.70 FRAME FROM STRG. 26L TO 26R CORRODED (MARKED) (C-CHECK) RO 4/4/2020 REMOVED AND REPLACED FS319.70 LOWER FRAME SECTOR REF SRM AND BOMBARDIER DWG. COMPLIED WITH TASK CARD. SEE CONTINUE CARD FOR DETAILS. NO LEAKS.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 38,551 hrs · 35,576 cycles

SIDE SEAT TRACK JUST BELOW L/H EMER. EXIT HAS AREAS OF MARKED (IN RED) CORROSION (C-CHECK) RO 4/4/2020 REPLACED SIDE SEAT TRACK JUST BELOW L/H EMER. EXIT WITH A SERVICEABLE UNIT REF CRJ-200 AMM, SEE CONTINUATION CARD FOR DETAILS.

Part: FRAME — CORRODED (FUSELAGE) · airframe 38,551 hrs · 35,576 cycles

FS.310 FRAME FROM STRG. 26L TO 26R CORRODED (MARKED) (C-CHECK) RO 4/4/2020 REMOVED AND REPLACED FS310 BELLY FRAME SECTOR REF BOMBARDIER DWG, NO LEAKS NOTED. SEE CONTINUE CARD FOR DETAILS.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 38,551 hrs · 35,576 cycles

L/H SIDE SEAT RAIL FROM APROX. FS 409+16 TO 409+112 HAS MULTI. AREAS OF CORROSION (MARKED IN RED) (C-CHECK) RO 4/4/2020 REPLACED PASSENGER SIDE SEAT RAIL (LH FS409.00 + 16 - FS409.00 + 112). REF CRJ200 AMM TASK. REPLACED HARDWARE AS NEEDED. ALSO REF REO. TORQUE WRENCH TUC4980 CAL DUE 31 JAN 21 SEE CONTINUATION CARD FOR ADDITIONAL DETAILS

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 38,551 hrs · 35,576 cycles

R/H SIDE SEAT RAIL FROM APROX. FS 409+16 TO 409+112 HAS MULTI. AREAS OF CORROSION (MARKED IN RED) (C-CHECK) RO 4/4/2020 REPLACED R/H SIDE SEAT TRACK FROM APPROX. FS409+16 TO FS409+112 WITH A SERVICEABLE UNIT REF CRJ-200 AMM, SEE CONTINUATION CARD FOR DETAILS.

Part: FITTING — CRACKED (FUSELAGE) · airframe 38,551 hrs · 35,576 cycles

* FS 625 CLIP IS CRACKED AT STR 14L L/H SIDE (C-CHECK) RO 4/4/2020 REMOVED AND REPLACED CLIP P/N 601R-35012-52 AT AFT FS 625 STR 14L LH REF BOMBARDIER DWG AND CRJ200 SRM. SEE ATTACHED SKY CARD.

Part: FITTING — CRACKED (FUSELAGE) · airframe 38,551 hrs · 35,576 cycles

* AFT EQUIPTMENT FS 625 CLIP IS CRACKED AT STR 14R R/H SIDE. (C-CHECK) RO 4/4/2020 REMOVED AND REPLACED CLIP AT AFT FS 625 STR 14R RH REF BOMBARDIER DWG AND CRJ200 SRM. SEE ATTACHED SKY CARD

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 38,551 hrs · 35,576 cycles

* THE FLOOR BEAM AT LBL27.00 FROM FS424.00 TO FS559.00 HAS MULTIPLE LOCATIONS OF CORROSION. (MARKED) (C-CHECK) RO 4/4/2020 REPAIRED THE FLOOR BEAM CORROSION AT LBL27.00 FROM FS424.00 TO FS559.00 REF REO. COMPLETED M-337

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 38,551 hrs · 35,576 cycles

* THE SEAT TRACK AT RBL9.00 HAS MULTIPLE LOCATIONS OF CORROSION FROM FS409.00+128 TO FS559.00. (MARKED (C-CHECK) RO 4/4/2020 REMOVED SEAT TRACK FOUND TO BE OUT OF LIMITS OF CORROSION. WET INSTALLED FABRICATED REPLACEMENT SEAT TRACK FROM FS409.00+128 TO FS559.00 RBL9.00. REF. REO.

Part: SUPPORT STRAP — CORRODED (FUSELAGE) · airframe 38,551 hrs · 35,576 cycles

* THE FLOOR SUPPORT STRAP BETWEEN THE CENTER FLOOR SUPPORT BEAM AND RBL9.00 AT FS559.00 HAS CORROSION. (MARKED) (C-CHECK) RO 4/4/2020 FLOOR SUPPORT STRAP AT FS 559.00 RBL 9 ORIGINAL THICKNESS IS 0.050 REF CRJ 200 SRM. REMAINING THICKNESS IS 0.045. MATERIAL LOST IS 0.005. FOUND OUT OF LIMIT REF CRJ 200 SRM

Part: STOP FITTING — CHAFED (FUSELAGE) · airframe 38,551 hrs · 35,576 cycles

* AVIONICS BAY DOOR RH STOP FITTING ON FUSELAGE HAS A CHAFED STOP PAD. (C-CHECK) RO 4/4/2020 REMOVED AND REPLACED CHAFED STOP PAD WITH 1 EA NEW STOP PAD IN THE R/H STOP FITTING PER CRJ-200 SRM

Part: ANGLE — CORRODED (FUSELAGE) · airframe 38,551 hrs · 35,576 cycles

* SERVICE DOOR SURROUND €“ LOWER SILL AREA €“ KICK ANGLE HAS CORROSION. (C-CHECK) RO 4/4/2020 REMOVED AND REPLACED BAD SERVICE DOOR SURROUND KICK ANGLE WITH NEW ANGLE. REF BOMBARDIER DWG, CRJ200 SRM OPS CHECK GOOD

Part: STOP FITTING — GOUGED (FUSELAGE) · airframe 38,551 hrs · 35,576 cycles

* AVIONICS BAY DOOR FORWARD RH STOP FITTING ON FUSELAGE GOUGED. (C-CHECK) RO 4/4/2020 INSTALLED NEW FORWARD R/H STOP FITTING IN AVIONICS BAY DOOR CUTOUT PER DRAWING COMPLETED SKYWEST TASKCARD

Part: ANGLE — CORRODED (FUSELAGE) · airframe 38,551 hrs · 35,576 cycles

* THE RH FLOOR SILL ANGLE HAS MULTIPLE LOCATIONS OF CORROSION FROM FS409.00+128 TO FS559.00. (MARKED) (C-CHECK) RO 4/4/2020 REPAIRED DAMAGED AREAS AND COMPLIED WITH ALL STEPS BOMBARDIER REO ENSURED ALL OTHER REQUIREMENT OF GENERIC REO ARE MET.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 38,551 hrs · 35,576 cycles

* THE FLOOR BEAM AT RBL9.00 FROM FS409.00+128 TO FS559.00 HAS MULTIPLE LOCATIONS OF CORROSION. (MARKED) (C-CHECK) RO 4/4/2020 REPAIRED FLOOR BEAM AT RBL9 FROM FS409+128 TO FS559 PER REO. COMPLETED SKYWEST TASK CARD.

Part: SUPPORT STRAP — CORRODED (FUSELAGE) · airframe 38,551 hrs · 35,576 cycles

* THE FLOOR SUPPORT STRAP FROM RH FLOOR SILL TO RBL27.00 HAS CORROSION AT FS559.00. (MARKED) (C-CHECK) RO 4/4/2020 REPLACED FLOOR SUPPORT STRAP AT RH FLOOR SILL TO RBL27.00 AT FS559 REF CRJ200 SRM AND DWG. NO LEAKS. SEE ATTACHED TASK. SEE CONTINUE CARD FOR DETAILS.

Part: PANEL — CORRODED (FUSELAGE) · airframe 38,551 hrs · 35,576 cycles

* THE LH FLOOR SILL PANEL HAS MULTIPLE LOCATIONS OF CORROSION FROM FS409.00+128 TO FS559.00. (MARKED) (C-CHECK) RO 4/4/2020 REMOVED CORROSION FROM LH FLOOR SILL PANEL FROM FS409+128 TO FS559 COMPLIED WITH ALL STEPS OF BOMBARDIER REO AND BOMBARDIER REO. COMPLETED SKYWEST TASK CARD.

Part: PANEL — CORRODED (FUSELAGE) · airframe 38,551 hrs · 35,576 cycles

* THE RH FLOOR SILL PANEL HAS MULTIPLE LOCATIONS OF CORROSION FROM FS409.00+128 TOFS559.00. (MARKED) (C-CHECK) RO 4/4/2020 REPAIRED RH FLOOR SILL PANEL CORROSION FROM FS409.00+128 TOFS559.00 PER REO. COMPLETED SKYWEST TASK CARD.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 38,551 hrs · 35,576 cycles

* THE SEAT TRACK AT LBL9.00 HAS MULTIPLE LOCATIONS OF CORROSION FROM FS409.00+128 TO FS559.00. (MARKED) (C-CHECK) RO 4/4/2020 REMOVED SEAT TRACK FOUND TO BE OUT OF LIMITS OF CORROSION. WET INSTALLED FABRICATED REPLACEMENT SEAT TRACK FROM FS409.00+128 TO FS559.00 LBL9.00. REF. REO

Part: STRIKER — CORRODED (FUSELAGE) · airframe 38,551 hrs · 35,576 cycles

* SERVICE DOOR SURROUND €“ LOWER SILL AREA €“ SEAL STRIKER HAS CORROSION. (C-CHECK) RO 4/4/2020 REPLACED SERVICE DOOR LWR SEAL STRIKER REF. CRJ200 SRM AND BOMBARDIER DRAWING. LEAK PRESURE LEAK CHECK GOOD. COMPLIED WITH SKYWEST TASK CARD

Part: SUPPORT STRAP — CORRODED (FUSELAGE) · airframe 38,551 hrs · 35,576 cycles

* THE FLOOR SUPPORT STRAP FROM LH FLOOR SILL TO LBL27.00 HAS CORROSION AT FS559.00. (MARKED) (C-CHECK) RO 4/4/2020 REPLACED FLOOR SUPPORT STRAP AT LH FLOOR SILL TO LBL27.00 AT FS559 REF CRJ200 SRM. AND DWG. NO LEAKS. SEE ATTACHED TASK. SEE CONTINUE CARD FOR DETAILS.

Part: SUPPORT STRAP — CORRODED (FUSELAGE) · airframe 38,551 hrs · 35,576 cycles

* THE FLOOR SUPPORT STRAP BETWEEN THE CENTER FLOOR SUPPORT BEAM AND LBL9.00 AT FS559.00 HAS CORROSION. (MARKED) (C-CHECK) RO 4/4/2020 BLEND OUT CORROSION. FLOOR SUPPORT FLANGE STRAP AT FS 559.00 LBL 9 ORIGINAL THICKNESS IS 0.063 REF CRJ 200 SRM. REMAINING THICKNESS IS 0.062. MATERIAL LOST IS 0.001. FOUND OUT OF LIMIT REF CRJ 200 SRM.

Part: BRACKET — CORRODED (FUSELAGE) · airframe 38,551 hrs · 35,576 cycles

* SERVICE DOOR SURROUND €“ LOWER SILL AREA €“ BRACKET COMMON TO FS 319 AND LOWER SILL HAS CORROSION. (C-CHECK) RO 4/4/2020 REPLACED SERVICE DOOR SURROUND FWD LWR CLEAT. REF CRJ200 SRM AND DWG. COMPLIED WITH TASK CARD STRUCTURAL MAJOR REPAIR (**RII**) SEE CONTINUATION CARD FOR ADDITIONAL DETAILS COMPLIED WITH TASK CARD STRUCTURAL MAJOR REPAIR (**RII**)

Part: RIB — CRACKED (RT WING) · airframe 38,551 hrs · 35,576 cycles

* R/H BATT RIB CAP AT WS 48.30 IS CRACKED (C-CHECK) RO 4/4/2020 INSTALLED NEW R/H BATT RIB CAP AT WS 48.30 REF CRJ200 SRM, BOMBARDIER DWG AND BOMBARDIER DWG. COMPLETED SKYWEST TASK CARD.

Part: RIB — CRACKED (LT WING) · airframe 38,551 hrs · 35,576 cycles

* L/H BATT RIB ANGLE AT WS 48.30 IS CRACKED (C-CHECK) RO 4/4/2020 REPLACED LH BATT RIB ANGLE AT WS 48.30. REF CRJ200SRM AND BOMBARDIER REO .BOMBARDIER DWG. COMPLETED SKYWEST TASK CARD.

Part: RIB — CRACKED (RT WING) · airframe 38,551 hrs · 35,576 cycles

* R/H BATT RIB WEB AT WS 53.60 IS CRACKED (C-CHECK) RO 4/4/2020 REPLACED R/H BATT RIB WEB AT WS 53.60 REF CRJ200 SRM AND BOMBARDIER DWG. SEE ATTACHED TASK. NO LEAKS NOTED. SEE CONTINUE CARD FOR DETAILS.

Part: FITTING — CRACKED (COCKPIT) · airframe 38,551 hrs · 35,576 cycles

LEFT WINDSHIELD SIDE POST BOTTOM OUTBD CLIP CRACKED (C-CHECK) RO 4/4/2020 INSTALLED NEW LEFT WINDSHIELD SIDE POST BOTTOM OUTBOARD CLIP REF BOMBARDIER DWG AND CRJ-200 SRM, COMPLIED WITH SKYWEST TASK CARD, SEE CONTINUATION CARD FOR DETAILS,

Part: SKIN — DENTED (FUSELAGE) · airframe 38,551 hrs · 35,576 cycles

DENT FOUND BELOW CARGO DOOR 6.8" AFT OF F.S. 605.0 AND BETWEEN STGR 18L AND 19L. PLOT, MAP, AND EVALUATE DAMAGE IF WITHIN ACCEPTABLE LIMITS OR REWORKED, ELIMINATE EVIDENCE USING STANDARD ACFT PRACTICES. (C-CHECK) RO 4/4/2020 REPAIRED DENT PER REO. COMPLETED SKYWEST TASK CARD.

Part: SKIN — DENTED (LT SPOILER) · airframe 38,551 hrs · 35,576 cycles

DENT DAMAGE WAS FOUND TO L/H FLIGHT SPOILER TOP SKIN SURFACE. PLOT, MAP, AND EVALUATE DAMAGE IF WITHIN ACCEPTABLE LIMITS OR REWORKED, ELIMINATE EVIDENCE USING STANDARD ACFT PRACTICES. (C-CHECK) RO 4/4/2020 L/H FLIGHT SPOILER DENTS OUT OF LIMITS REPLACED WITH SERVIEABLE SPOILER REF CRJ-200 AMM, OPS CHECK GOOD.

Part: FASTENER — CORRODED (RT SPOILER) · airframe 38,551 hrs · 35,576 cycles

R/H FLIGHT SPOILER BONDING WIRE ATTACH HARDWARE HAS CORROSION (C-CHECK) RO 4/4/2020 REMOVED AND INSTALED NEW HARDWARE FOR R/H WING FLIGHT SPOILER INBOARD AND OUTBOARD BONDING WIRES REF CRJ200 SRM. PERFORMED ELECTRICAL BONDING TEST FOR R/H WING FLIGHT SPOILER REF CRJ200 AMM. BONDING TEST GOOD. CALIBRATED TOOL USED P/N TUC4608 CAAL DUE DATE 29-FEB-20

Part: FASTENER — CORRODED (LT SPOILER) · airframe 38,551 hrs · 35,576 cycles

* L/H OUTBD GROUND SPOILER HAS CORROSION ON PCU LINK HARDWARE (C-CHECK) RO 4/4/2020 REMOVED AND REPLACED HARDWARE AT L/H OTBD GRND SPOILER PCU LINK REF CRJ-200 AMM ,OPS CHECK GOOD

Part: FASTENER — CORRODED (RT SPOILER) · airframe 38,551 hrs · 35,576 cycles

R/H OUTBD GROUND SPOILER PCU ATTACH LINK HARDWARE HAS CORROSION (C-CHECK) RO 4/4/2020 REPLACED HARDWARE FOR RH OTBD GRND SPOILER PCU ATTACMENT LINK REF CRJ-200 AMM, OPS CHECK GOOD.

Part: FASTENER — CORRODED (RT SPOILER) · airframe 38,551 hrs · 35,576 cycles

R/H INBD GROUND SPOILER PCU ATTACH LINK HARDWARE HAS CORROSION (C-CHECK) RO 4/4/2020 REMOVED AND REPLACED HARDWARE FOR R/H INBD GRND SPOLIER ATTACHING LINK WITH NEW HARDWARE P/N: NAS6205-12D, MS17826-5 (2EA), NAS6305419D REF CRJ-200 AMM

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 38,551 hrs · 35,576 cycles

COMPLY WITH SCHEDULED MAINTENANCE CODE: AD - COMPLY WITH PARAGRAPH (J) OF AD BY: (J)(1) DOING A NONDESTRUCTIVE INSPECTION FOR CRACKING OF THE FORWARD FACE OF THE FUSELAGE STATION (FS) 621 PRESSURE BULKHEAD, IN ACCORDANCE WITH AWLOF BOMBARDIER. (J)(2) MODIFYING THE RPB AND DOING A NONDESTRUCTIVE INSPECTION FOR CRACKING OF THE FS 621 PRESSURE BULKHEAD WEB, IN ACCORDANCE WITH BOMBARDIER REPAIR ENGINEERING ORDER (REO). AND MARKING THIS CAMP AS "STRUCTURAL REPAIR," WHICH WILL GENERATE AN RA FOR TRACKING THE SDIR FOR THIS REO ON THIS AIRPLANE, PART NUMBER: - , SERIAL NUMBER: 7621, POSITION: (C-CHECK) RO 4/4/2020 COMPLIED WITH PARAGRAPH (J) OF AD BY: (J)(1) DOING A NONDESTRUCTIVE INSPECTION FOR CRACKING OF THE FORWARD FACE OF THE FUSELAGE STATION (FS) 621 PRESSURE BULKHEAD, IN ACCORDANCE WITH AWL OF BOMBARDIER. (J)(2) MODIFYING THE RPB AND DOING A NONDESTRUCTIVE INSPECTION FOR CRACKING OF THE FS 621 PRESSURE BULKHEAD WEB, IN ACCORDANCE WITH BOMBARDIER REPAIR ENGINEERING ORDER (REO). AND; MARKING THIS CAMP AS "STRUCTURAL REPAIR," WHICH WILL GENERATE AN RA FOR TRACKING THE SDIR FOR THIS REO ON THIS AIRPLANE. COMPLIED WITH REO COMPLETED SKYWEST TASK CARD.

Part: ANGLE — WEAK (FUSELAGE) · airframe 38,551 hrs · 35,576 cycles

COMPLY WITH REO 601R-53-41-1116 REPAIR & REINFORCEMENT FOR FS 559.00 LWR CAP ANGLES BL 9.00 & 18.00 LHS & RHS (C-CHECK) RO 4/4/2020 COMPLIED WITH REO REPAIR & REINFORCEMENT FOR FS 559.00 LWR CAP ANGLES BL 9.00 & 18.00 LHS & RHS COMPLETED SKYWEST TASK CARD.

Part: BEARING — CORRODED (LT AILERON) · airframe 38,551 hrs · 35,576 cycles

REMOVE & REINSTALL LH 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 4/4/2020 REMOVED AND INSTALLED LH AILERON REF AMM. OPS TEST GOOD, RIG CHECK GOOD. COMPLIED WITH SKYWEST TASK CARD

Part: BEARING — CORRODED (RT AILERON) · airframe 38,551 hrs · 35,576 cycles

REMOVE & REINSTALL RH 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 4/4/2020 REMOVED AND INSTALLED RH AILERON REF AMM. OPS TEST GOOD, RIG CHECK GOOD. COMPLIED WITH SKYWEST TASK CARD

Part: STRINGER — CRACKED (FUSELAGE) · airframe 35,907 hrs · 33,296 cycles

STRINGER 3L IS CRACKED AROSS FASTENERS AT FS 379. REPAIRED IAW SRM 53-00-03 AND SRM SUPPLEMENT 53-00-03.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 35,907 hrs · 33,296 cycles

AFT CARGO BAY SEAT RAIL BEAM AT LBL9 HAS CORROSION BETWEEN FS589.0 AND 605.0. REMOVED AND REPLACED BEAM IAW SRM 51-42-21, 51-42-22, AND EC/TC REO 601R-53-61-3780 REV A DATED 2011-07-15.

Part: BULKHEAD — CHAFED (FUSELAGE) · airframe 35,907 hrs · 33,296 cycles

EVALUATE OR REPAIR RT 9G LAVATORY BULKHEAD AFT SIDE DAMAGE AT INSERT/RIVNUT LOCATIONS. COMPLIED WITH EC/TC EO CL-600-2B19-53-L05832 REV 0 DATED 2018-09-13.

Part: BULKHEAD — CHAFED (FUSELAGE) · airframe 35,907 hrs · 33,296 cycles

EVALUATE OR REPAIR CENTER 9G BULKHEAD AFT SIDE DAMAGE AT INSERT/RIVNUT LOCATIONS. COMPLIED WITH EC/TC EO CL-600-2B19-53-L05831 REV 0 DATED 2018-09-13.

Part: BULKHEAD — CHAFED (FUSELAGE) · airframe 35,907 hrs · 33,296 cycles

, EVALUATE OR REPAIR LT 9G BULKHEAD AFT SIDE DAMAGE AT INSERT/RIVNUT LOCATIONS. COMPLIED WITH EC/TC EO CL-600-2B19-53-L05830 REV 0 DATED 2018-09-13.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 35,907 hrs · 33,296 cycles

TRACK SEGMENT BETWEEN FS 612 AND FS 617 CORRODED. REMOVED AND REPLACED SEGMENT IAW AMM 53-00-49-400-801.

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 35,907 hrs · 33,296 cycles

PAX DOOR INTERCOSTAL LOCATED 18" FROM HINGE BETWEEN FS 320 AND FS 338 (ABOVE OUTER HANDLE) IS CORRODED. REMOVED AND REPLACED INTERCOSTAL IAW SRM 51-42-06 AND 51-42-21.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 35,907 hrs · 33,296 cycles

LT PRESSURE FLOOR SILL ANGLES ARE CORRODED BETWEEN FS 513.00 TO FS 559.00. COMPLIED WITH EC/TC REO 601R-53-41-666 01 AND REO 601R-53-41-666 REV C DATED 11/06/2012 AS WRITTEN.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 35,907 hrs · 33,296 cycles

RT PRESSURE FLOOR SILL ANGLE CORRODED BETWEEN AT FS 513.00. REO 601R-53-41-2366 HAS BEEN ACCOMPLISHED AND ALL STEPS HAVE BEEN DOCUMENTED AND SIGNED FOR ON A NON-ROUTINE WORK CARD. COMPLIED WITH EC/TC REO 601R-53-41-666 01 AND REO 601R-53-41-666 REV C DATED 11/06/2012 AS WRITTEN.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 35,907 hrs · 33,296 cycles

LT PRESSURE FLOOR SILL ANGLES ARE CORRODED BETWEEN FS 473.15 TO FS 484.00. REO 601R-53-41-2367 HAS BEEN ACCOMPLISHED AND ALL STEPS HAVE BEEN DOCUMENTED AND SIGNED FOR ON A NON-ROUTINE WORK CARD. COMPLIED WITH EC/TC REO 601R-53-41-666 01 AND REO 601R-53-41-666 REV C DATED 11/06/2012 AS WRITTEN.

Part: STIFFENER — CHAFED (PAX DOOR) · airframe 35,907 hrs · 33,296 cycles

PASSENGER DOOR PRESSURE VENT FLAP HAS TWO CHAFED STIFFENERS. REPAIR TO THE NICK/GOUGE ON THE VENT FLAP ON THE PAX DOOR IS COMPLETED IAW REO 601R-52-11-1040. THE REPAIR MEETS ALL REQUIREMENTS FOR REO 601R-52-11-1040.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 35,907 hrs · 33,296 cycles

RT PRESSURE FLOOR SILL IS CORRODED AROUND NUTPLATE HOLES FS 529.00 TO FS 544.00. COMPLIED WITH EC/TC REO 601R-53-41-666 01 AND REO 601R-53-41-666 REV C DATED 11/06/2012 AS WRITTEN.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 35,907 hrs · 33,296 cycles

LT PRESSURE FLOOR SILL IS CORRODED AROUND NUTPLATE HOLES BETWEEN FS 424.00 AND FS 461.00. COMPLIED WITH EC/TC REO 601R-53-41-666 01 AND REO 601R-53-41-666 REV C DATED 11/06/2012 AS WRITTEN.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 35,907 hrs · 33,296 cycles

RT PRESSURE FLOOR SILL ANGLES ARE CORRODED BETWEEN FS 529.00 TO FS 544.00. COMPLIED WITH EC/TC REO 601R-53-41-666 01 AND REO 601R-53-41-666 REV C DATED 11/06/2012 AS WRITTEN.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 35,907 hrs · 33,296 cycles

LT PRESSURE FLOOR SILL ANGLES BETWEEN FS 424.00 AND FS 461.00 ARE CORRODED. COMPLIED WITH EC/TC REO 601R-53-41-666 01 AND REO 601R-53-41-666 REV C DATED 11/06/2012 AS WRITTEN.

Part: ROLL PIN — MIGRATED (HINGE) · airframe 35,907 hrs · 33,296 cycles

PAX DOOR HINGE IS GOUGED ON FUSELAGE SIDE OF HINGE AFT LANDING FROM MIGRATED ROLL PIN. COMPLIED WITH EC/TC REO 601R-53-21-814 AS WRITTEN.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 35,907 hrs · 33,296 cycles

LT PRESSURE FLOOR SILL ANGLES ARE CORRODED BETWEEN FS 513.00 TO FS 559.00. REO 601R-53-41-2367 HAS BEEN ACCOMPLISHED AND ALL STEPS HAVE BEEN DOCUMENTED AND SIGNED FOR ON A NON-ROUTINE WORK CARD. COMPLIED WITH EC/TC REO 601R-53-41-666 01 AND REO 601R-53-41-666 REV C DATED 11/06/2012 AS WRITTEN.

Part: SKIN — DENTED (FUSELAGE) · airframe 35,907 hrs · 33,296 cycles

DENT FUSELAGE LOWER SKIN BETWEEN FS409+16 AND FS409-32 AND STRINGER 21 LEFT TO STRINGER 22 LEFT. COMPLIED WITH TEMPORARY REPAIR PER REO 601R-53-31-906. REPAIRED DAMAGE IAW SRM 53-00-31 REPAIR 1.

Part: DOOR SILL — CRACKED (FUSELAGE) · airframe 35,907 hrs · 33,296 cycles

CRACK ON DOOR SILL OF PAX DOOR. (100 FH INSPECTION 200) FO: 7/12/2018 CLOSED REPAIR COMPLETED IAW REO.

Part: DOOR SILL — CRACKED (FUSELAGE) · airframe 35,865 hrs · 33,253 cycles

CRACK ON DOOR SILL OF PAX DOOR. FO: 7/12/2018. WORK IN PROGRESS.

Part: UNKNOWN — FAILED (NLG) · airframe 34,778 hrs · 32,315 cycles

GEAR DISAGREE IN FLIGHT. RETURN TO FIELD. FLT (5016). FO: 1/15/2018. CLOSED. REPLACED NLG.

Part: PROXIMITY SENSOR — FAILED (NLG) · airframe 33,933 hrs · 31,481 cycles

GEAR DISAGREE EICAS MESSAGE WITH A RED NOSE GEAR INDICATION. REMOVED AND REPLACED THE NLG DOWNLOCK PROXIMITY SENSOR PS2GA IAW AMM. OPS CHECKED GOOD. PERFORMED TESTS OF MLG EXTENSION & RETRACTION SYSTEM IAW AMM. OPS CHECKED GOOD.

Part: WIRE HARNESS — FAILED (NR 2 DOWNLOCK) · airframe 33,413 hrs · 30,880 cycles

GEAR DISAGREE FOR NOSE GEAR. DIVERTED. REMOVED AND REPLACED THE DOWNLOCK NR 2 SENSOR HARNESS IAW AMM. OPS CHECKED GOOD.

Part: FRAME — CORRODED (BS 364) · corrosion level 2 · airframe 32,758 hrs · 30,199 cycles

FRAME CORRODED AT BS 364 BETWEEN STRINGERS 26L AND 26R. REPAIRED THE FRAME IAW EC/TC EA 20-2016-324. AIRCRAFT APPROVED FOR RETURN TO SERVICE.

Part: FLOORBEAM — CORRODED (BS 559) · corrosion level 2 · airframe 32,758 hrs · 30,199 cycles

FLOORBEAM CORRODED AT BS 559+112, LBL 27. REPAIRED THE FLOORBEAM IAW EC/TC EO 600-53-0780. AIRCRAFT APPROVED FOR RETURN TO SERVICE.

Part: INTERCOSTAL — CORRODED (BS 349-364) · corrosion level 2 · airframe 32,758 hrs · 30,199 cycles

INTERCOSTAL CORRODED FORWARD OF AVIONICS DOOR BETWEEN BS 349 AND 364, STRINGERS 27L AND 27R. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM 51-42-06. AIRCRAFT APPROVED FOR RETURN TO SERVICE.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 32,758 hrs · 30,199 cycles

PAX DOOR AFT DRAG ANGLE CRACKED. REPAIRED THE DRAG ANGLE IAW EC/TC REO 601R-52-11-513. AIRCRAFT APPROVED FOR RETURN TO SERVICE.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 32,708 hrs · 30,149 cycles

DURING C CHECK FOUND PAX DOOR AFT DRAG ANGLE CRACKED AT MOTOR ASSIST CABLE SUPPORT BRACKET. MTC REPAIRED CRACK IAW EC/TC REO 601R-52-11-513 AND REO 601R-52-11-513 REV B.

Part: FRAME — CORRODED (BS 364) · airframe 32,708 hrs · 30,149 cycles

DISCOVERED FRAME BS 364 CORRODED BETWEEN STRINGERS 26L AND 26R. REPAIRED IAW EA 20-2016-324 AND ECTC EA 20-2016-324. THIS IS CLASSIFIED AS A MAJOR REPAIR.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 32,708 hrs · 30,149 cycles

DURING C CHECK FOUND SEAT TRACK CORRODED AT RBL9 FS364-394. MTC R & R SET TRACK IAW AMM 53-01-11-000-802 & 53-01-11-400-802. C/W EC/TC REO 601R-53-00-485 AND RIL 4354.

Part: SEAT TRACK — CORRODED (BS 364-394) · airframe 32,708 hrs · 30,149 cycles

SEAT TRACK HAS CORRODED. REMOVED AND REPLACED THE SEAT TRACK RBL 9, BS 364-394 IAW AMM 53-01-11-000-802 & 53-01-11-400-802.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 32,708 hrs · 30,149 cycles

DURING C CHECK FOUND LT FLOOR SILL CORRODED AT FS559-559+32. MTC C/W EC/TC REO 601R-53-00-526 & GREO 601R-53-00-526.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 32,708 hrs · 30,149 cycles

PAX DOOR DRAG AFT ANGLE CRACKED AT MOTOR ASSIST CABLE SUPPORT BRACKET. REPAIRED CRACKED PAX DOOR AFT DRAG ANGLE IAW ECTC REO 601R-52-11-513 AND REO 601R-52-11-513 REV B, TYPE II REPAIR. ALL DEFECTS CORRECTED

Part: SEAT TRACK — CORRODED (BS 364-394) · airframe 32,708 hrs · 30,149 cycles

DURING C CHECK FOUND SEAT TRACK CORRODED AT LBL 9 BS 364-394. R & R SEAT TRACK IAW AMM 53-01-11-000-802 & 53-01-11-400-802.

Part: INTERCOSTAL — CORRODED (BS 349-364) · airframe 32,708 hrs · 30,149 cycles

INTERCOSTAL 27L CORRODED FWD OF AVIONICS DOOR BETWEEN BS 349 & 364. R & R THE INTERCOSTAL IAW SRM 51-42-06, PG 23. B

Part: FLOORBEAM — CORRODED (BS 559) · airframe 32,708 hrs · 30,149 cycles

FLOORBEAM HAS CORROSION AT BS 559+112 AT LBL 27. REPAIRED THE AREA IAW REO 601R-53-00-027 AND EC/TC EO 600-53-0780. THIS IS CLASSIFIED AS A MAJOR REPAIR.

Part: SIGN — BROKEN (CABIN) · airframe 32,051 hrs · 29,564 cycles

EMERGENCY EXIT SIGN OVER GALLEY DOOR IS BROKEN. R & R SERVICE DOOR EMERGENCY SIGN, TOP IAW AMM 33-51-13. NO FURTHER DEFECT NOTED AT THIS TIME.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 31,479 hrs · 29,035 cycles

PAX DOOR OUTSIDE EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED THE EMERGENCY LIGHT LENS, TWISTED BULB OUT OF SOCKET, INSTALLED NEW BULB BY TWISTING IT BACK IN THE SOCKET REINSTALLED CORNER OF THE LIGHT ASSY IAW AMM 33-51-21-000-801 & 33-51-21-400-801. EMERGENCY LIGHTS OPS TEST GOOD IAW SRM 33-51-00-710-801.

Part: LIGHT — DAMAGED (CABIN) · airframe 30,941 hrs · 28,555 cycles

FLOOR-LEVEL EMERGENCY FLOODLIGHT AT SERVICE DOOR DAMAGED. R & R FLOODLIGHT IAW AMM 33-51-19. SYSTEM OPS CHECKED GOOD. NO FURTHER ACTION.

Part: LANDING GEAR — MALFUNCTIONED (LEFT) · airframe 30,592 hrs · 28,235 cycles

GEAR UP DISAGREE INDICATION AFTER TAKEOFF. LEFT MAIN GEAR INDICATED UNSAFE. ACFT RETURNED TO DEPARTURE AFTER T/O, EMERGENCY ACTIONS: LANDING GEAR RETRACTION SYSTEM. COMPLIED WITH VISUAL INSPECTION OF LT MLG AND UPLOCK ASSY IAW AMM 32-32-05. COMPLIED WITH FUNCTIONAL CHECK OF THE LANDING GEAR EXT/RET/ SYSTEM IAW AMM 32-32-00. OPS CHECK GOOD.

Part: MECHANISM — DIRTY (PAX DOOR) · airframe 30,274 hrs · 27,949 cycles

F/A REPORTS THAT MAIN PAX DOOR LEVER IS STICKING WHEN TRYING TO OPEN DOOR. REMOVED DEBRIS & TRASH FROM DOOR OPERATING MECHANISM. MAIN DOOR OPERATES OPENS AND CLOSES NORMALLY NOW IAW AMM 52-11-03.

Part: DOOR — LACK OF LUBE (MAIN PAX) · airframe 29,873 hrs · 27,589 cycles

MAIN CABIN DOOR WOULD NOT OPEN AT GATE. CLEANED AND LUBRICATED PAX DOOR INNER HANDLE IAW AMM 12-2-52. OPS CHECK GOOD.

Part: SKIN — CRACKED (LT WING) · airframe 28,426 hrs · 26,188 cycles

CRACK INDICATIONS NOTED AT LT LOWER WING PLANK ACCESS PANEL LANDING. REPAIRED IAW REO 601R-57-21-030, REV. L .

Part: SKIN — CRACKED (LT WING) · airframe 28,426 hrs · 26,188 cycles

INDICATIONS NOTED AT LT LOWER WING SKIN ACCESS PANEL LANDING. REPAIRED IAW 601R-57-21-030, REV L.

Part: SKIN — CRACKED (LT WING) · airframe 28,426 hrs · 26,188 cycles

INDICATIONS NOTED AT LT LOWER WING SKIN ACCESS PANEL LANDING. REPAIRED IAW REO 601R-57-21-030, REV L 2014-02-05.

Part: SKIN — CRACKED (RT WING) · airframe 28,426 hrs · 26,188 cycles

INDICATIONS NOTED AT RT LOWER WING SKIN ACCESS PANEL LANDING. REPAIRED IAW REO 601R-57-21-030, REV L.

Part: SKIN — CRACKED (RT WING) · airframe 28,426 hrs · 26,188 cycles

INDICATIONS NOTED AT RT WING ACCESS PANEL LANDING. REPAIRED IAW REO 601R-57-21-030 REV.L 2014-02-05.

Part: ACCESS PANEL — CRACKED (RT WING) · airframe 28,426 hrs · 26,188 cycles

INDICATIONS NOTED AT RT WING ACCESS PANEL. REPAIRED IAW REO 601R-57-21-030, REV L 2014-02-05.

Part: SKIN — CRACKED (LT WING) · airframe 28,426 hrs · 26,188 cycles

INDICATIONS NOTED AT LT LOWER WING SKIN ACCESS PANEL LANDING. REPAIRED IAW REO 601R-57-21-030, REV L 2014-02-05.

Part: SKIN — CRACKED (RT WING) · airframe 28,426 hrs · 26,188 cycles

LOWER RT WING ACCESS PANEL LANDING HAS MULTIPLE INDICATIONS OF CORROSION NOTED. REMOVED CORROSION IAW EA 15-2014-197, SECTION 1 1A.

Part: ISOLATOR — CRACKED (BS 621) · airframe 28,394 hrs · 26,154 cycles

FS 621 BULKHEAD HAS SEVEN ISOLATORS FOUND CRACKED AND/OR BROKEN. R & R THE BROKEN ISOLATORS IAW SRM 51-42-06, PT SL2337.3.

Part: ATTACH ANGLE — DAMAGED (BS 280) · airframe 28,414 hrs · 26,171 cycles

ON REMOVAL OF THE ATTACHMENT ANGLE AT LBL 9.0 WHERE FLOOR SUPPORT ATTACHES TO BS 280 CROSSBEAM, UNDER OTBD ANGLE FOUND TOP HOLE IN FLOORBEAM WEB TO BE ELONGATED. REPAIRED IAW REO 24-2014-559.

Part: ANGLE — CORRODED (BS 280 FLOORBEAM) · airframe 28,394 hrs · 26,154 cycles

FOUND FWD J-ANGLE, BS 280 BETWEEN LBL 12 AND RBL 12 TO HAVE CORROSION. LOCATED, DRILLED & INSTALLED FWD J CHANNEL IAW SRM 51-40-11, 51-42-06.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 28,412 hrs · 26,170 cycles

FS 280, FLOORBEAM INBD AND OTBD CLIPS AT RBL 9 ARE CRACKED. REMOVED INBD AND OTBD FLOORBEAM CLIPS AT FS 280 IAW SRM 51-42-21. INSTALLED SERVICEABLE OTBD & INBD FLOORBEAM CLIPS AT RBL 9, FS 280 IAW SRM 51-42-21. COMPLIED WITH REO 601R-53-11-2706, REV ISSUE.

Part: SKIN — CORRODED (BS 559) · airframe 28,394 hrs · 26,154 cycles

FUSELAGE EXTERIOR SKIN HAS MINOR CORROSION AROUND FASTENERS FROM BS 559+32 - 559+54 STRINGERS 25L-25R. COMPLIED WITH CORROSION REPAIR IAW EA 25-2014-290 PART 1.

Part: ANGLE — CORRODED (BS 280) · airframe 28,394 hrs · 26,154 cycles

CORROSION ON BS 280 J-ANGLE BETWEEN LBL 9 AND RBL 9. FOUND CORROSION TO BE ON AFT J-ANGLE PREVIOUS REPAIR FILTER ANGLE, PN 601R-53-11-136-1 FROM REO:601R-53-11-136, REV A CORROSION IS OM TOPSIDE AND BOTTOMSIDE AT NUTPLATE LOCATIONS AND CORROSION RUNS DOWN AND AROUND TOPSIDE FWD RADIUS BETWEEN AFT J-ANGLE AND BULKHEAD WEB. CORROSION IS OUT OF LIMITS WITH OVERLAPPING ELEMENTS IAW SRM 53-00-00 T/R 53-27, FIG 101(SHEET 3). PREVIOUS REPAIR ANGLE FILLER, PN 601R-53-11-136-1 ON FS 280.00 AFT J-ANGLE BETWEEN LBL 14 AND RBL 13 REQUIRES REMOVAL, EVALUATED AND SUBMITTED TO ENGINEERING FOR BLEND REPAIR OR REPLACEMENT. COMPLIED WITH THE FABRICATION OF ATTACHMENT PARTS EO 600-53-91. C/W 01 IAW EO 600-53-91. C/W AND MEETS ALL ITS REQUIREMENTS.

Part: FLOOR SUPPORT — CORRODED (BS 364-409) · airframe 28,412 hrs · 26,170 cycles

CORROSION ON LT AND RT FLOOR SUPPORT CAPS FROM FS 364 TO FS 409.00+128 AT VARIOUS LOCATIONS LBL 9 AND RBL 9. FOUND CORROSION TO BE FROM FS 409.00+5 TO FS 409.00+128. REMOVED FASTENERS AND DISPLACED LT FLOOR SUPPORT CAP FROM FS 409+5 TO FS 409+128 IAW SRM 51-42-06, 51-42-21 AND 57-42-21 SRM. FABRICATED AND INSTALLED NEW FLOOR SUPPORT CAP AT LBL 9 BETWEEN FS 409+5 AND 409+128 IAW REO:601R-53-31-829 P1. REMOVED RT FLOOR SUPPORT, CAP FROM FS 409.00+5 TO FS 409.00+128 IAW SRM 51-42-06 AND 51-42-21. FABRICATED AND INSTALLED NEW FLOOR SUPPORT CAP AT RBL 9.0 BETWEEN FS 409+5 AND 409+28 IAW REO:601R-53-31-829 P1.

Part: SKIN — CORRODED (BS 559) · airframe 28,412 hrs · 26,170 cycles

FUSELAGE SKIN EXTERIOR SURFACE HAS MINOR CORROSION AROUND FASTENERS FROM FS 559 TO FS 559+10 BETWEEN STRS 25L AND 25R. REMOVED FASTENERS FROM FS 559 TO FS 559+10 BETWEEN STR 25L TO 25R IAW SRM 51-42-21. BLENDED AREA AROUND FASTENER HOLES REMOVING CORROSION IAW SRM 51-21-06. MATERIAL .004 WITHIN LIMITS IAW SRM 51-00-31 AND T/R 53-33. DAMAGE WAS FOUND TO BE IN A NO DAMAGE ZONE FROM FS 559 TO FS 559+10, ENGINEERING REQUIRED. COMPLIED WITH REPAIR OF CORROSION REMOVAL BETWEEN FS 559 TO FS 559+10 BETWEEN STR 25L TO 25R IAW STS EA 25-2014-293, SECTION 1, PERMANENT REPAIR 1.

Part: STRUCTURE — CHAFED (LT MLG DOOR) · airframe 28,414 hrs · 26,171 cycles

REPAIRED LT MLG DOOR L/E CHAFED 2.1" LONG, .025" DEEP, .200 WIDE NEXT TO BRUSH ASSEMBLY. REPAIRED LT MLG DOOR L/E IAW STS EA 32-2014-115, REV P2. RECEIVED FINAL EA STS EA 32-2014-115. COMPLIED WITH EC/TC REO 601R-52-82-034 01, REACCOMPLISHMENT, REPAIR TO MLG DOOR INNER SKIN CHAFING AND REO 601R-52-82-034, REV NC AS WRITTEN.

Part: SEAT TRACK — CORRODED (BS 364-409) · airframe 28,414 hrs · 26,171 cycles

CORROSION ON SEAT TRACK AT RBL 9 FS 364 TO 409.00+128 AT VARIOUS LOCATIONS. R & R SEAT TRACK IAW SRM 51-41-02.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 28,412 hrs · 26,170 cycles

FS 280, FLOORBEAM INBD AND OTBD CLIPS AT LBL 9 ARE CRACKED. REMOVED INBD & OTBD CLIPS ON FLOORBEAM, LBL 9 AT FS 280 IAW SRM 51-42-21. INSTALLED SERVICEABLE INBD & OTBD CLIPS ON FLOORBEAM LBL 9 AT FS 280 IAW SRM 51-42-21. COMPLIED WITH REO 601R-53-11-2706, REV ISSUE.

Part: FLOOR SUPPORT — CORRODED (BS 409) · airframe 28,394 hrs · 26,154 cycles

CORROSION ON RT FLOOR SUPPORT AT BS 409. REPAIRED THE FLOOR SUPPORT BETWEEN BS 280 - 409+128 IAW REO:601R-53-00-530.

Part: FLOOR SUPPORT — CORRODED (BS 409) · airframe 28,394 hrs · 26,154 cycles

CORROSION ON LT FLOOR SUPPORT AT BS 409+32. REPAIRED THE FLOOR SUPPORT BETWEEN BS 280 - 409+128 IAW REO:601R-53-00-530.

Part: ANGLE — CORRODED (PAX DOOR SILL) · airframe 28,412 hrs · 26,170 cycles

PASSENGER DOOR LOWER SILL ANGLE REPLACEMENT. R & R PASSENGER DOOR CAP ANGLE FOR LOWER SILL ANGLE REPLACEMENT BY REMOVING STRUCTURAL FASTENERS COMMON TO THE STRUCTURE. LOWER SILL ANGLE, ITEM 28, REQUIRES REPLACEMENT. REF SRM 53-21-23, FIG 2, FOR LOCATION.

Part: FLOOR SUPPORT — CORRODED (BS 559-574) · airframe 28,394 hrs · 26,154 cycles

LEFT FLOOR SUPPORT CORRODED AROUND FASTENER HOLES FROM BS 559+80 - 574. REPAIRED IAW REO 601R-53-00-526 AND GREO 601R-53-00-526, REV.

Part: BUSHING — DETERIORATED (RT AILERON) · airframe 28,412 hrs · 26,170 cycles

RIGHT AILERON INBD LUG AT INBD PCU ATTACHMENT POINT HAS MIGRATED BUSHING. REMOVED MIGRATED BUSHING, INSTALLED OVER SIZE BUSHING USING AMS5569 15-5PH H1000, PO 30012 MATERIAL IAW REO 601R-57-61-004, REV C AND DEVIATION, REO 601R-57-61-505, REV B. C/W ECTC REO 601R-57-61-004. REO 601R-57-61-505, REV B HAS BEEN ACCOMPLISHED.

Part: FLOOR SUPPORT — CORRODED (BS 559-589) · airframe 28,394 hrs · 26,154 cycles

RT FLOOR SUPPORT CORRODED AROUND FASTENER HOLES BS 559+80 - 589. REPAIRED IAW REO 601R-53-00-526 01 AND GREO 601R-53-00-526, REV.

Part: FLOOR SUPPORT — CORRODED (BS 409-559) · airframe 28,411 hrs · 26,169 cycles

LEFT FLOOR SUPPORT FROM BS 409+128 - 559 HAS SEVERAL AREAS OF CORROSION. REPAIRED IAW REO 601R-53-41-666, REV C.

Part: FLOOR SUPPORT — CORRODED (BS 409-559) · airframe 28,411 hrs · 26,169 cycles

RIGHT FLOOR SUPPPORT FROM BS 409+128 - 559 HAS SEVERAL AREAS OF CORROSION. REPAIRED IAW REO 601R-53-41-666 01 & REO 601R-53-41-666, REV C.

Part: ANGLE — CRACKED (BS 484) · airframe 28,394 hrs · 26,154 cycles

LT ANGLE AT BS 484, LBL 27 IS CRACKED AT UPPER CORNER. REPAIRED IAW REO 601R-53-41-059.

Part: FLOOR SUPPORT — CORRODED (BS 409-424) · airframe 28,412 hrs · 26,170 cycles

CORROSION ON FLOOR SUPPORT BS 409+128 - 424 RBL 9. CORROSION EXCEEDS LIMITS IAW SRM 53-27. REPAIRED IAW REO 601R-55-41-1841.

Part: SKIN — CHAFED (RT AILERON) · airframe 28,407 hrs · 26,165 cycles

RT AILERON UPPER SKIN SHROUD IS CHAFED FROM CENTER FITTINGS OF AILERON TO INBD EDGE OF AILERON. DEEPEST DAMAGE MEASURING APPROX. .015". MAX DAMAGE ALLOWED .005". BLENDED TO A SMOOTH CONTOUR RT AILERON UPPER SKIN SHROUD FROM CENTER FITTINGS OF AILERON TO INBD EDGE OF AILERON. .001" MATERIAL REMOVED IAW REO 601R-57-60-013. COMPLIED WITH REO 601R-57-60-013, REV A. COMPLIED WITH EC/TC REO 601R-57-60-013 IAW REO 601R-57-60-013 REV A.

Part: ISOLATOR — CRACKED (BS 621 BULKHEAD) · airframe 28,394 hrs · 26,154 cycles

FWD SIDE OF BS 621, BULKHEAD HAS ONE CRACKED ISOLATOR ON LT SIDE THIRD ROW FROM THE BOTTOM. R & R THE ISOLATOR IAW SRM 51-42-13.

Part: BEARING — FAILED (RUDDER) · airframe 28,407 hrs · 26,165 cycles

THE RUDDER MIDDLE HINGE POINT FITTINGS ON THE VERTICAL STABILIZER HAVE WORN BEARINGS. R & R RUDDER MIDDLE HINGE POINT FITTINGS BEARINGS IAW RIL 0602, REV F, TYPE 2. PERFORMED BEARING BACKLASH OF THE RUDDER SYS 1, 2, AND 3 IAW AMM 27-21-00-220-810. SYS 1 WAS AT .024, 2 WS AT .044 AND 3 WS AT .024 BACKLASH. COMPLIED WITH EC/TC RIL 0602, REPAIR TYPE II REPLACEMENT OF THE SWAGED BEARING IAW RIL 0602, REV F DATED 07/09/14 AS WRITTEN.

Part: ISOLATOR — CRACKED (BS 621 BULKHEAD) · airframe 28,394 hrs · 26,154 cycles

FWD SIDE OF BS 621 BULKHEAD HAS THREE CRACKED ISOLATORS ON RT SIDE MOST OTBD. R & R THE ISOLATORS IAW SRM 51-42-13.

Part: BEARING — FAILED (ELEVATOR) · airframe 28,407 hrs · 26,165 cycles

LEFT ELEVATOR SYS NR 3 FAILED BEARING BACKLASH. BACKLASH IS .240, MAX ALLOWED .210, .030 OUT OF LIMITS. REMOVED THE LT ELEVATOR SYS NR 1, 2 AND 3 BEARINGS, PN MS14103-6, MS14103-5 AND MS14103-4 IAW AMM 20-26-00-910-807. INSTALLED LT ELEVATOR SYSTEM NR 1, NR 2 AND NR 3 BEARING USING PN MS14103-6, MS14103-5 AND MS14103-4, PO W21655, W29835, W29974 IAW AMM 20-26-00-910-808, REV 49, DATED MAY 10/2014. REMOVED LT ELEVATOR PCU BUSHINGS PN 600-10300-59 3 EA AND PN NAS538B7P013 3, EA IAW AMM 20-26-00-910-802. INSTALLED LT ELEVATOR PSU BUSHINGS, PN 600-10300-59, 3 EA AND PN NAS538B7P013, 3 EA IAW AMM 20-26-00-910-804, REV 49. C/W ECTC RIL 0183 AND RIL 0183, REV B, DATED 1/24/14 AS WRITTEN. PERFORMED BACKLASH TEST OF LT ELEV, BEARING BACKLASH IAW AMM 27-31-00-220-84. BEARING BACKLASH MEASURED AT .140. BACKLASH GOOD.

Part: SKIN — CORRODED (BS 559) · airframe 28,407 hrs · 26,165 cycles

SKIN HAS LIGHT CORROSION BS 559+84 - 559+96, STRINGER 22R. FOUND CORROSION TO BE OUT OF LIMITS IAW SRM 53-00-31-01, TR 53-33. BLENDED CORRODED AREAS IAW SRM 51-12-00.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 28,407 hrs · 26,165 cycles

PASSENGER DOOR AFT DRAG ANGLE IS CRACKED. COMPLIED WITH REPAIR TO PAX DOOR STAIR AFT DRAG ANGLE IAW REO 601R-52-11-513.

Part: CIRCUIT BREAKER — TRIPPED (EMERGENCY LIGHTS) · airframe 27,970 hrs · 25,767 cycles

EMERGENCY LIGHTS DO NOT ILLUMINATE. SYSTEM SELF RESET IAW MCC NO FURTHER ACTION REQUIRED.

Part: DOOR — UNKNOWN · airframe 27,812 hrs · 25,614 cycles

MAIN PASSANGER DOOR DOES NOT OPEN NORMALLY, DIFFICULT TO OPEN, HANGS UP PART WAY THROUGH THE TRAVEL OF THE DOOR OPEN LEVER. PERFORMED VISUAL INSPECTION AND OPS CHECK OF PAX DOOR IAW AMM 52-11-00. OPS CHECKED GOOD. NO DEFECTS FOUND AT THIS TIME.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 27,240 hrs · 25,012 cycles

EMERGENCY LIGHT ABOVE ROW 3 INOPERATIVE. R & R EMERGENCY LIGHT NR 1 BATTERY PACK IAW AMM 33-51-04. OPS CHECKED GOOD.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 25,576 hrs · 23,396 cycles

FOD DAMAGE TO ACFT BELLY. OPEN.

Part: SEAT TRACK — CORRODED (BS 409-559) · airframe 24,333 hrs · 22,117 cycles

SEAT TRACK FROM FS 409.128 TO 559.16 CORRODED. REMOVED CORROSION IAW SRM 51-21-06, MAX MATERIAL REMOVED AT LOCATION R3, FIG 101, .012 DEEP. MATERIAL REMOVED WITHIN LIMITS OF SRM 53-21-49. REMOVED AND REPLACED SEAT TRACK IAW AMM 53-01-11-000-802.

Part: BEAM — CORRODED (BS 349) · airframe 24,331 hrs · 22,116 cycles

FS 349.00 TRANSVERSE BEAM HAS CORROSION AT RBL 40. FROM AFDL 400640: FS 349.00 TRANSVERSE BEAM IS CORRODED BEYOND 10 PERCENT LIMITS AT RBL 40 IAW SRM 53-00-00-01, T/R 53-27, FIG 102, SHEET 2. REPAIRED FS 349.00 TRANSVERSE BEAM AT RBL 49 IAW REO 601R-53-21-2340.

Part: ANGLE — CORRODED (BS 605) · airframe 24,329 hrs · 22,115 cycles

FS 605 LOWER FRAME REINFORCING ANGLE IS CORRODED. REMOVED AND INSTALLED REINFORCING ANGLE IAW SRM 51-42-06.

Part: SKIN — CORRODED (RT WING) · airframe 24,329 hrs · 22,115 cycles

RT LOWER WING PLANK ACCESS HOLE NR 10 AT WS 188.040, 650BB HAS CORROSION AT INBD END MEASURING APPROX 1.4" LONG X .10" WIDE X .003" DEEP. COMPLIED WITH ECTC EO 600-57-81 C/W IAW REO 601R-57-21-030 REV H.

Part: FLOORBEAM — CORRODED (BS 589) · airframe 24,329 hrs · 22,115 cycles

FLOORBEAM TEE AT FS 589.00 BETWEEN LBL 9 AND LBL 27 IS CORRODED. BLENDED CORROSION, MATERIAL REMOVED .005 TO .007 MAX. COMPLIED WITH SRM 53-61-43, SRM 53-00-00, SRM 51-12-00, NDTM 51-20-08.

Part: FRAME — CORRODED (BS 605) · airframe 24,329 hrs · 22,115 cycles

FS 605.00 FRAME IS CORRODED BETWEEN STR 26 AND 27L. REMOVED LOWER SECTOR OF FRAME IAW SRM 51-42-06. LOCATED ALL FASTENER HOLES IN SERVICEABLE FRAME IAW SRM 51-40-11. INSTALLED SERVICEABLE FRAME IAW SRM 51-42-06 & SRM 51-42-21.

Part: SKIN — CORRODED (LT WING) · airframe 24,329 hrs · 22,115 cycles

LEFT LOWER WING PLANK ACCESS HOLE 8 AT WS 136.676, 540FB HAS CORROSION AT INBD, OTBD ENDS AND 2 PLACES ON AFT EDGE. INBD CORROSION MEASURES APPROX 2" LONG X .12" WIDE X .002" DEEP. OTBD CORROSION MEASURES APPROX 4.7" LONG X .11" WIDE X .002" DEEP. CORROSION ON AFT EDGE MEASURES APPROX 1.4" LONG X .10" WIDE X .002" DEEP AND 1" LONG X .10" WIDE X .002" DEEP. COMPLIED WITH ECTC EO 600-57-81, & REO 601R-57-21-030, REV H.

Part: SKIN — CORRODED (LT WING) · airframe 24,329 hrs · 22,115 cycles

LEFT LOWER WING PLANK ACCESS HOLE NR 10 AT WS 188.040, 550BB HAS CORROSION AT INBD AND OTBD ENDS. INBD CORROSION MEASURES APPROX 1.3" LONG X .10" WIDE X .002" DEEP. OTBD CORROSION MEASURES APPROX 1.5" LONG X .11" WIDE X .002" DEEP. COMPLIED WITH ECTC EO 600-57-81, & REO 601R-57-21-030, REV H.

Part: SKIN — CORRODED (LT WING) · airframe 24,329 hrs · 22,115 cycles

LEFT LOWER WING PLANK ACESS HOLE NR 5 AT WS 76.161, 540CB HAS CORROSION AT OTBD END MEASURING APPROX 1.3" LONG X .10" WIDE X .002" DEEP. COMPLIED WITH ECTC EO 600-57-81 & REO 601R-57-21-030, REV H.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 24,329 hrs · 22,114 cycles

SEAT TRACK AT RBL 9, FS 559+48 HAS AREAS OF CORROSION. REMOVED CORRODED SEAT TRACK IAW AMM 53-01-11-000-802. INSTALLED NEW SEAT TRACK IAW AMM 53-01-11-400-802.

Part: ACCESS PANEL — CORRODED (RT WING) · airframe 24,329 hrs · 22,115 cycles

RT LOWER WING PLANK ACCESS HOLE AT WS 54.897, PNL 640BB HAS CORROSION AT INBD AND OTBD ENDS. INBD CORROSION MEASURES APPROX 9" LONG X .13" WIDE X .002" DEEP. OTBD CORROSION MEASURES APPROX 9" LONG X .16" WIDE X .002" DEEP (HOLE NR1). C/W ECTC EO 600-57-81 C/W IAW REO 601R-57-21-030, REV H AND FWD ALL REQUIRED FORMS TO STRUCTURES ENGINEERING.

Part: SKIN — CORRODED (LT WING) · airframe 24,329 hrs · 22,115 cycles

LEFT LOWER WING PLANK ACCESS HOLE NR 15 AT WS 294.048, 550GB HAS CORROSION MEASURING APPROX 1.3" LONG X 1.0" WIDE X .002" DEEP. COMPLIED WITH ECTC EO 600-57-81 & REO 601R-57-21-030, REV H.

Part: FLOORBEAM — CORRODED (BS 559) · airframe 24,329 hrs · 22,114 cycles

LEFT FLOORBEAM AT FS 559 LBL 27-36 IS CORRODED. R & R DAMAGED FLOORBEAM AT FS 559 LBL 27-36 WITH NEW IAW SRM 51-42-06.

Part: FLOOR SUPPORT — CORRODED (BS 449-513) · airframe 24,329 hrs · 22,114 cycles

LT PRESSURE FLOOR SUPPORT HAS CORROSION BS 499 TO 513. REPAIRED IAW EC/TC REO 601R-53-41-666 AND REO 601R-53-41-666, REV B.

Part: SEAT TRACK — CORRODED (BS 364-394) · airframe 24,329 hrs · 22,114 cycles

RT FWD SEAT TRACK IS CORRODED AT RBL 9 BS 364 - 394. REMOVED DAMAGED FLOOR SEAT TRACK AND INSTALLED A NEW SEAT TRACK IAW AMM 53-01-11-400-802.

Part: SKIN — CORRODED (LT WING) · airframe 24,329 hrs · 22,115 cycles

LT LOWER WING PLANK ACCESS HOLE NR 1 AT WS 54.897, 540BB HAS CORROSION AT BOTH ENDS. INBD CORROSION MEASURES APPROX 6" LONG X .18" WIDE X .003" DEEP. OTBD CORROSION MEASURES APPROX 7.5" LONG X .16" WIDE X .002" DEEP. COMPLIED WITH ECTC EO 600-57-81 & REO 601R-57-21-030, REV H.

Part: FLOOR SUPPORT — CORRODED (BS 574-621) · airframe 24,329 hrs · 22,115 cycles

FLOOR SUPPORT CORRODED AT LBL 27, FS 574 TO FS 621. REMOVED DAMAGED FLOOR SUPPORT IAW SRM 51-42-06, 51-42-01 AND 51-42-22. FOUND FLOOR SUPPORT TO BE CORRODED BEYOND LIMITS IAW SRM 53-00-00. COMPLIED WITH ECTC REO 601R-53-61-3778 AND GREO 601R-53-61-3778 REV A. LOCATED AND DRILLED NEW SERVICEABLE FLOOR SUPPORT IAW SRM 51-40-11.

Part: FLOOR SUPPORT — CORRODED (BS 484-513) · airframe 24,329 hrs · 22,114 cycles

RT PRESSURE FLOOR SUPPORT DOUBLER HAS CORROSION AT FS 484 TO 513. REPAIRED IAW EC/TC REO 601R-53-41-666 AND REO 601R-53-41-666, REV B.

Part: SKIN — CORRODED (LT WING) · airframe 24,329 hrs · 22,115 cycles

LEFT LOWER WING PLANK ACCESS HOLE NR 12 AT WS 230.415, 550DB HAS CORROSION AT INBD AND OTBD ENDS. INBD CORROSION MEASURES APPROX 1" LONG X .07" WIDE X .001" DEEP. OTBD CORROSION MEASURES APPROX 1.1" LONG X .08" WIDE X .001" DEEP. COMPLIED WITH ECTC EO 600-57-81 & REO 601R-57-21-030, REV H.

Part: FLOOR SUPPORT — CRACKED (BS 484) · airframe 24,331 hrs · 22,116 cycles

RT FLOOR SUPPORT ANGLE CRACKED AT FS 484 RBL 27. R & R RT FLOOR SUPPORT ANGLE AT FS 484, RBL 27 IAW SRM 51-42-21.

Part: POST — CRACKED (BS 409) · airframe 24,331 hrs · 22,116 cycles

FS 409+128 VERTICAL POST AT RBL 18 FAILS NDT WITH AN INDICATION ON INBD AFT RADIUS ON UPPER POST GREATER THAN 50 PERCENT SCREEN HEIGHT. REMOVED POST IAW SRM 51-42-06 7 51-42-22. INSTALLED NEW POST ASSY IAW SRM 51-42-06, 51-42-22 & REO 601R-53-41-889.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 24,329 hrs · 22,114 cycles

PASSENGER DOOR AFT DRAG ANGLE IS CRACKED. R & R THE PAX DOOR AFT WEB DRAG ANGLE SRM 51-42-06.

Part: LIGHT — BROKEN (CABIN) · airframe 24,331 hrs · 22,116 cycles

THE RT SIDE AISLE EMERGENCY LIGHT BROKEN AND PIECED TOGETHER. ON REPAIR OF RT EMERGENCY LIGHT, FOUND LT SIDE TO ALSO BE DAMAGED. REPAIRED LT AND RT EMERGENCY LIGHTS IAW AMM SUPPLEMENT AND AMM 33-51-01-400-805.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 24,299 hrs · 22,080 cycles

NR 1 CABIN CEILING EMERGENCY FLOOD LIGHT INOPERATIVE. RELAMPED NR 1 CABIN CEILING EMERGENCY FLOOD LIGHT. OPS CHECKED GOOD IAW AMM 33-51-00.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 24,111 hrs · 21,882 cycles

CABIN SECOND FROM FRONT CEILING EMERGENCY LIGHT INOPERATIVE. RELAMPED EMERGENCY FLOOD LIGHT IAW AMM 33-51-16, OP'S CHECKED GOOD.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 23,766 hrs · 21,502 cycles

NR 7 EXTERIOR EMERGENCY LIGHT IS INOPERATIVE. RELAMPED EMERGENCY LIGHT IAW AMM 33-51-21. OPS CHECKED GOOD.

Part: SEAT TRACK — CORRODED (BS 409-424) · airframe 23,437 hrs · 21,136 cycles

RT SEAT TRACK BETWEEN FS 409.00 AND 424.00 IS CORRODED. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01, FOUND OUT OF LIMITS IAW SRM 53-21-49-101-001-A01. REMOVED RT SEAT TRACK BETWEEN FS 409.00 AND FS 424.00 IAW AMM 53-01-11. INSTALLED SEAT TRACK IAW AMM 53-01-11.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 23,437 hrs · 21,136 cycles

LEFT FUSELAGE 3RD FROM FRONT EMERGENCY LIGHT IS INOPERATIVE. R & R EMERGENCY LIGHT LAMP LOCATED ON LT SIDE FUSELAGE 3RD FROM FRONT, OPS CK GOOD, IAW AMM 33-51-21.

Part: BRACKET — DAMAGED (MLG PROX SENSOR) · airframe 23,303 hrs · 20,976 cycles

AFTER TAKEOFF SELECTED GEAR LEVER UP AND RECEIVED WOW OUTPUT FAIL STATUS MESSAGE. ACFT RETURNED TO DEPARTURE AND AN EMERGENCY WAS DECLARED. FOUND NLG OLEO CENTERED/EXTENDED PROXIMITY SENSOR AND PROXIMITY SENSOR BRACKET DAMAGED. R & R SUPPORT BRACKET IAW CMM 32-20-04. R & R NLG OLEO CENTERED/EXTENDED PROXIMITY SENSOR PS14GA IAW AMM 32-61-05. ADJUSTED PROXIMITY SENSORS IAW AMM 32-61-05. OPS TEST OF PSS GOOD IAW AMM 32-61-00. NO DEFECTS NOTED AT THIS TIME. ACFT OK FOR SERVICE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 22,940 hrs · 20,565 cycles

NR 3 EXTERIOR EMERGENCY LIGHTS INOPERATIVE. RELAMPED NR 3 EXTERIOR EMERGENCY LIGHTS. OPS CHECKED GOOD IAW AMM 33-51-00.

Part: SMOKE DETECTOR — FALSE INDICATION (CARGO BAY) · airframe 22,902 hrs · 20,519 cycles

RECEIVED SMOKE CARGO WARNING. COMPLIED WITH QRH. DISCHARGED BOTTLE 1 & 2. R & R CARGO SMOKE DETECTOR IAW AMM 26-15-01. SMOKE DETECTORS, OPS TESTED GOOD.

Part: BATTERY — WEAK (FLASHLIGHT) · airframe 20,993 hrs · 18,377 cycles

COCKPIT LEFT AND FLIGHT ATTENDANT FLASHLIGHTS DIM. REPLACED CAPT AND F/A'S FLASHLIGHT BATTERIES OPS CK GOOD IAW CRJ 200 AMM 25-61-00.

Part: PRIORITY VALVE — MALFUNCTIONED (NLG DOOR) · airframe 20,574 hrs · 17,872 cycles

ON TAKEOFF-GEAR DISAGREE AND NOSE DOOR OPEN WARNING MESSAGES AND WOW INPUT CAUTION AND STEERING INOP CAUTION MESSAGE. ADDITIONALLY WOW OUTPUT FAIL STATUS MSG. NOSE GEAR INDICATED DOWN AND LOCKED. COMPLIED WITH QRH WOW INPUT CAUTION WAS THE ONLY MEESAGE WE COULD NOT EXTINGUISH (TOWER PUT EMERGENCY EQUIPMENT ON STANDBY) R & R NLG PRIORITY VALVE IAW AMM 32-33-15. FUNCTIONAL CHECK GOOD IAW AMM 32-30-00. R & R PSEU IAW AMM 32-61-01. FUNCTIONAL TEST GOOD IAW AMM 32-61-00. ALL LANDING PROXIMITY SENSOR GAPS GOOD IAW AMM 32-61-05. (CLOSED)

Part: WARNING SYSTEM — FALSE INDICATION (MLG) · airframe 20,566 hrs · 17,865 cycles

GEAR DISSAGREE AFTER TAKEOFF (WARNING) WOW IMPUT (CAUTION) NWS INOP (CAUTION). (A/C RETURNED TO MEM AFTER T/O -- EMERGENCY DECLARED) PERFORMED FUNCTIONAL TEST OF LANDING GEAR EXTENSION AND RETRACTION SYS IAW AMM 32-30-00 NO DEFECTS NOTED AT THIS TIME PERFORMED OPS TEST OF THE NOSE WHEEL STEERING SYS IAW AMM 32-51-00. ALL OPS CKS GOOD, NO DEFECTS NOTED AT THIS TIME. (CLOSED)

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 19,673 hrs · 16,830 cycles

EMERGENCY EXIT LIGHT AT WARDROBE (LOWER) GALLEY & SERVICE DOOR LOWER TRIM PANEL INOPERATIVE. R & R NR 1 BATTERY PACK IAW EMERGENCY LIGHTS IAW AMM TASK 33-51-04-000-801 AND 33-51-04-400-801. OPS CHECK GOOD.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 19,672 hrs · 16,830 cycles

FOUND REAR PRESSURE BULKHEAD WEB THAT SURROUNDS THE LINTEL ATTACHMENT FITTING HAS INDICATION NOTED APPROX .2" IN LENGTH 70 PERCENT FSH. FAILED NDT INSPECTION. REPAIR PER EC/TC REO 601R-53-61-1230 HAS BEEN COMPLETE AND THE REPAIR C/W THE REQUIREMENTS OF ECTC AND REO 601R-53-61-1230 REV D.

Part: POST — CRACKED (BS 409) · airframe 19,673 hrs · 16,830 cycles

FOUND FS 409.0 + 128 VERTICAL POST RBL 18 OTBD SIDE HAS INDICATION NOTED AT WL 69 AFT FLANGE RADIUS APPROX .2" IN LENGTH 60 PERCENT FSH FAILED NDT INSP. REMOVED VERTICAL POST COMMON TO FS 409+128 AT RBL 18 IAW SRM 51-42-06. VERTICAL POST FS 409+128.0 RBL 18 REQUIRES INSTALL. LOCATED & DRILLED SERVICEABLE VERTICAL POST 409+128 RBL 18 OTBD SIDE IAW SRM 51-40-11. OK TO INSTALL POST. VERTICAL POST FS 409+128 RBL 18 REQUIRES INSTALL. INSTALLED 409+128 RBL 18 POST IAW SRM 51-42-06 & REO 601R-53-41-889. FS 409+128 RBL 18 POST REQUIRES SEAM SEAL & PAINT. SEAM SEALED FS 409+128 RBL 18 POST IAW AMM 51-23-00-390-804. PAINTED SAID AREA IAW SRM 51-25-26.

Part: POST — CRACKED (BS 409) · airframe 19,672 hrs · 16,830 cycles

FOUND FS 409.0+128 VERTICAL POST LBL 18 AFT FLANGE RADIUS APPROX .2" IN LENGTH 60 PERCENT FSH FAILED NDT INSP. REMOVED FS 409+128 LBL 18 INBD AND OTBD POSTS IAW SRM 51-42-06 SECTION 11(A-B) LOCATED SERVICEABLE OTBD POST IAW SRM 51-42-06 SECTION 7(A-B). ASSEMBLED INBD AND OTBD POSTS IAW SRM 51-42-06 SECTION 9(A) AND FIG 8. REINSTALLED FS 409+128 LBL 18 INBD POST AND NEW SERVICEABLE OTBD POST IAW REO 601R-53-41-889 & SRM 51-42-06. PAINTED REPAIRED AREA IAW SRM 51-25-16. C/W EC/TC REO 601R-53-41-889 AND MET ALL THE REQUIREMENTS OF REO 601R-53-41-889.

Part: BULKHEAD — CRACKED (BS 559) · airframe 19,673 hrs · 16,830 cycles

FS 559.0 BULKHEAD WEB & CAP ANGLE HAS (5) HFEL INDICATIONS NOTED AS LISTED: (1) IN WEB 70 PERCENT FSH 0.5" LONG AT RBL 18.0 WL 59.10 (2) IN WEB 60% FSH0.5" LONG AT RBL 9.0 WL 54.10 (3) IN CAP ANGLE 60 PERCENT FSH 0.2" LONG BELOW RBL 18.0 POST (4) IN CAP ANGLE 50 PERCENT FSH 0.2" LONG BELOW LBL 18.0 POST (5) IN CAP ANGLE 50 PERCENT FSH 0.2" LONG BELOW LBL 9.0 POST. FAILS NDT INSPECTION. COMPLIED WITH EC/TC REO 601R-53-41-260 IAW REO 601R-53-41-260.

Part: FRAME — CRACKED (BS 714 S11R) · airframe 19,673 hrs · 16,830 cycles

RT FS 714 AT STRINGER 11 IS CRACKED IN RADIUS. THIS DISCREPANCY WILL BE REPAIRED WITH THE INCORPORATION OF S/B 601R-53-055 STRUCTURAL REPAIR AT FS 718. REF CO 762110 JOB 8762115 OP 5238 FOR DETAILS.

Part: ANCHOR FITTING — CRACKED (PAX DOOR) · airframe 19,673 hrs · 16,830 cycles

PAX DOOR FWD ANCHOR FITTING IS CRACKED AND HAS CORRODED HARDWARE. REMOVED AND REPLACED FWD PASSENGER DOOR COUNTERBALANCE ANCHOR FITTING IAW AMM 52-11-17-000-804 AND 52-11-17-400-804. ADJUSTED PASSENGER DOOR COUNTERBALANCE IAW AMM TASK 52-11-17-820-802. OPS CHECK GOOD.

Part: SEAT TRACK — CORRODED (BS 621) · airframe 19,673 hrs · 16,830 cycles

CARGO COMPARTMENT SEAT RAIL BETWEEN FS 621.00, LBL 9 IS CORRODED. REMOVED CORRODED SEAT RAIL & INSTALLED NEW SERVICEABLE SEAT RAIL IAW SRM 51-41-02.

Part: SEAT TRACK — CORRODED (BS 583) · airframe 19,673 hrs · 16,830 cycles

CARGO COMPARTMENT SEAT RAIL AT FS 583.00 LBL 9 IS CORRODED. REMOVED AND REPLACED CARGO COMPARTMENT SEAT RAIL IAW SRM 51-41-02.

Part: SIGN — BROKEN (EMERGENCY LIGHT) · airframe 19,673 hrs · 16,830 cycles

GALLEY EXIT LIGHT TRIM PANEL LIGHT BASE BROKEN. REMOVED UNSERVICEABLE EMG EXIT SIGN ASSY FROM GALLEY TRIM PANEL IAW AMM TASK 33-51-10-000-801 AND INSTALLED NEW SERVICEABLE EMG EXIT SIGN ASSY ON THE GALLEY TRIM PANEL IAW AMM TASK 33-51-10-400-801. OPS CHECK OF EXIT LIGHT DUE. GALLEY TRIM PNL EMERGENCY EXIT SIGN OPS CHECK OK, IAW MM 33-51-00-710-801.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 19,673 hrs · 16,830 cycles

PAX DOOR AFT DRAG ANGLE CRACKED IN PREVIOUSLY REPAIRED AREA. REPAIRED THE PAX DOOR AFT DRAG ANGLE IAW ASA EC/TC REO 601R-52-11-513 AND REO 601R-52-11-513 REV A.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 19,673 hrs · 16,830 cycles

EXIT SIGN LENS ABOVE SERVICE DOOR, BROKEN. REMOVED & REPLACED LIGHTED EXIT SIGN ABOVE SERVICE DOOR WITH SERVICEABLE LIGHT ASSY IAW MM 33-51-13-000-801 & 33-51-13-400-801. OPS CHECKS OK, IAW MM 33-51-00-710-801.

Part: SEAT TRACK — CORRODED (BS 574-559) · airframe 19,673 hrs · 16,830 cycles

CARGO COMPARTMENT FLOOR SEAT RAIL BETWEEN FS 574.00 AND FS 559.00+112 RBL 9 IS CORRODED. SEAT TRACK REMOVED IAW AMM 53-01-00-802. INSTALLED SEAT TRACK IAW SRM 51-41-02.

Part: SEAT TRACK — CORRODED (BS 574) · airframe 19,673 hrs · 16,830 cycles

CARGO COMPARTMENT FLOOR SEAT RAIL BETWEEN FS 574.00 AND FS 559.00+112 LBL 9 IS CORRODED. SEAT TRACK REMOVED IAW AMM 53-01-000-802. INSTALLED SEAT TRACK IAW SRM 51-41-02.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 19,673 hrs · 16,830 cycles

CARGO COMPARTMENT FLOOR SEAT RAIL BETWEEN FS 559.00+80 AND 559+96 RBL 27 IS CORRODED. REMOVED & REPLACED SEAT TRACK IAW SRM 51-41-02.

Part: PLACARD — DAMAGED (ESCAPE HATCH) · airframe 19,673 hrs · 16,830 cycles

JOB 8762111 OPERATION 46/ CREW ESCAPE HATCH REQUIRES PAINT & SILKSCREENS. PAINTED CREW ESCAPE HATCH IAW SRM 51-25-01. APPLIED NEW SILKSCREENS ON HATCH IAW MM 11-10-03-400-801.

Part: GLOWSTRIP — CRACKED (CABIN) · airframe 19,673 hrs · 16,830 cycles

FWD LT & RT, AFT LT & RT PHOTOLUMINESCENT FLOOR LIGHT STRIPS ARE CRACKED. RECEIVED SERVICEABLE FLOOR TRACK (PHOTOLUMINESCENT STYLE). REF 8762111, OP 34 FOR REMOVAL AND INSTALLATION.

Part: LIGHT — INOPERATIVE (NR 2 EXTERIOR) · airframe 19,199 hrs · 16,299 cycles

NR 2 EXTERIOR EMERGENCY LIGHT OUT.

Part: STEP — BROKEN (PAX DOOR) · airframe 18,951 hrs · 16,032 cycles

PAX DOOR BOTTOM STEP BROKEN.

Part: LIGHT — MISSING (CABIN) · airframe 18,486 hrs · 15,582 cycles

DURING LC2 FOUND EMERGENCY TRACK LIGHTING SPARE SEGMENTS MISSING. REPLACED SPARE TRACKS SEGMENTS IAW EO600-33-0015LC MCO CLEARED.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 18,430 hrs · 15,531 cycles

ON LC2 INSP, FOUND CRACK AT FS202.00 PRESSURE BLKHD NEAR PARKING BRAKE CABLE.

Part: STEP — CRACKED (PAX DOOR) · airframe 18,188 hrs · 15,301 cycles

PAX DOOR BOTTOM STEP CRACKED.

Part: FLAP — FAILED (WING) · airframe 17,488 hrs · 14,653 cycles

FLAP FAIL MSG WHEN SELECTING 0-8 ON APPROACH, SPEED 200 KNOTS, EMERGENCY DECLARED.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT)

LEFT EXTERIOR EMERGENCY LIGHT NR 5 OUT. REMOVED AND REPLACED LAMP AT NR 5 LIGHT ASSY OPS CK GOOD IAW AMM 33-51-21 (SDR CLOSED). (A)

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 16,339 hrs · 13,604 cycles

RT WING FWD EMERGENCY LIGHT INOP. REMOVED AND REPLACED RT WING FWD EMERGENCY LIGHT BULB IAW CRJ 200 AMM 33-43-01, OPS CK GOOD.

Part: BULKHEAD — CRACKED (BS 280) · airframe 15,220 hrs · 12,666 cycles

PILOT'S BULKHEAD AT FS 280 AND RBL 9.0 IS CRACKED.

Part: ANGLE — CORRODED (BS 280) · airframe 15,220 hrs · 12,666 cycles

FS 280 FWD UPPER ANGLE HAS CORROSION.

Part: ANGLE — CRACKED (BS 484) · airframe 15,220 hrs · 12,666 cycles

CLIP CRACKED O/B OF RBL 27, RESOLVED ON W/O: 77977 TASKCARD: N/R-00281. REMOVED CRACKED FS 484 RBL 27O/B CLIP. FABRICATED SERVICEABLE CLIP FROM S6144-3 ANGLE IAW CRJ SRM 53-41-43. OK TO ALODINE, PRIME, AND TOPCOAT. INSTALLED SERVICEABLE CLIP IAW CRJ SRM 51-42-21 JM 14031. OK TO TOPCOAT FASTENERS. APPLIED TOPCOAT TO FASTENERS IAW CRJ 200 SRM 51-21-16.

Part: ANGLE — CORRODED (EMERGENCY EXIT) · airframe 15,220 hrs · 12,666 cycles

CORROSION ON 2 ANGLES ON BOTTOM OF LT EMERGENCY EXIT (FLAGGED).

Part: STRUCTURE — CORRODED (RT OVERWING) · airframe 15,220 hrs · 12,666 cycles

AAR-8020 - RT OVERWING EMERGENCY EXIT HAS CORROSION INSIDE LOWER ACCESS HOLE ON AFT SIDE.

Part: SKIN — CRACKED (PAX DOOR) · airframe 15,220 hrs · 12,666 cycles

PASSENGER DOOR HAS A CRACK IN AFT SKIN OF DOOR STEP SUPPORT, UNDER RAIL STOP BRACKET IN STEP RADIUS. REPAIRED DAMAGE TO PAX DOOR STEP SUPPORT AFT SIDE IAW ASA EC/TC REO 601R-52-11-702.

Part: SKIN — CRACKED (PAX DOOR) · airframe 15,220 hrs · 12,666 cycles

PASSENGER DOOR HAS A CRACK IN FWD SKIN OF DOOR STEP SUPPORT, UNDER RAIL STOP BRACKET IN STEP RADIUS. REPAIRED DAMAGE TO PAX DOOR STEP SUPPORT FWD SIDE IAW ASA EC/T/C REO 601R-52-11-702.

Part: WEB — CRACKED (FUSELAGE) · airframe 15,220 hrs · 12,666 cycles

WEB CRACKED OB OF LBL 9 UNDER PARKING BRAKE PULLEY HOUSING.

Part: PLACARD — UNKNOWN (ESCAPE HATCH) · airframe 15,220 hrs · 12,666 cycles

EXTERNAL DECALS ON CREW ESCAPE HATCH REQUIRE REPLACEMENT.

Part: FITTING — CRACKED (FUSELAGE) · airframe 15,220 hrs · 12,666 cycles

CLIP CRACKED INBOARD OF LBL 36, RESOLVED ON W/O: 77977 TASKCARD: N/R-00248. REMOVED CRACKED FS 484 CLIP INBOARD OF LBL 36. FABRICATED SERVICEABLE CLIP FROM 2024T-3 .063 IAW CRJ SRM 51-24-16. OK TO ALODINE, PRIME, ABD TOPCOAT. APPLIED FINISH TO CLIP IAW CRJ 200 SRM 51-16-21. INSTALLED SERVICEABLE CLIP IAW CRJ SRM 51-42-21. OK TO TOPCOAT FASTENERS. APPLIED TOPCOAT TO FASTENERS IAW CRJ 200 SRM 51-16-21 JM 14031 12/15/07.

Part: FITTING — CRACKED (BS 472) · airframe 15,220 hrs · 12,666 cycles

BATHTUB FITTING CRACKED AT FS 472 O/B OF RBL 9.00. REMOVED CRACKED BATHTUB FITTING, LOCATED NEW SERVICEABLE FITTING P/N 600-31068-19 AND INSTALLED IAW CRJ 200 SRM 51-42-21. OK TO TOPCOAT FASTENERS. APPLIED TOPCOAT TO FASTENERS IAE CRJ SRM 51-21-16.

Part: FITTING — CRACKED (FUSELAGE) · airframe 15,220 hrs · 12,666 cycles

CLIP CRACKED O/B OF LBL 27, RESOLVED ON W/O: 77977 TASKCARD: N/R-00247. REMOVED CRACKED FS 487 LBL 27 O/B CLIP. FABRICATED SERVICEABLE CLIP FROM S6144-3 ANGLE IAW CRJ 200 SRM 53-41-43. OK TO ALODINE, PRIME, AND TOPCOAT. INSTALLED SERVICEABLE CLIP IAW CRJ SRM 51-42-21 JM 14031. OK TO TOPCOAT FASTENERS. APPLIED TOPCOAT TO FASTENERS IAW CRJ 200 SRM 51-21-16 JM 14031 12/15/07.

Part: PIVOT ASSY — GOUGED (HORIZONTAL STAB) · airframe 15,220 hrs · 12,666 cycles

HORIZONTAL STABILIZER RT OUTER PIVOT PIN HAS GOUGE, POSSIBLE CRACK ON I/B END NEXT TO ANTI-ROTATION TAB.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 15,220 hrs · 12,666 cycles

AAR-2011 - LT WINDSCREEN EMERGENCY EXIT SIGN HAS 3 INOP LAMPS.

Part: BRACKET — BROKEN (TE FLAP) · airframe 15,220 hrs · 12,666 cycles

RT O/B FLAP, O/B HINGE ARM CENTER BRACKET FOR ATTACHING FLAP FAIRING 697BB, I/B END IS BROKEN OFF. REMOVED CRACKED BRACKET FOR FLAP FAIRING DUPILCATED PART & TOPCOATED. INSTALLED PART IAW CRJ SRM 51-42-13.

Part: LATCH — BROKEN (SERVICE DOOR) · airframe 15,105 hrs · 12,573 cycles

EXTERNAL SERVICES DOOR HAS (1) BROKEN LATCH.

Part: STEP — SEPARATED (PAX DOOR) · airframe 15,105 hrs · 12,573 cycles

PAX DOOR BOTTOM STEP SEPARATING AT ATTACH POINT.

Part: UNKNOWN — ODOR (CABIN) · airframe 14,540 hrs · 12,100 cycles

PASSENGER IN SEAT 8A REPORTED AN ELECTRICAL SMOKE SMELL ON APPROACH. FLT 4914 DEL 26 MINS.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 14,279 hrs · 11,893 cycles

CREW REPORTS CAPTAIN`S FLASHLIGHT INOP.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 13,657 hrs · 11,421 cycles

LEFT WINDSHIELD SHATTERED. EMERGENCY DECLARED. FLTS 4213, 4214 CX.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 13,594 hrs · 11,364 cycles

FOUND EMERGENCY LIGHT ON CEILING AT ROW 5 IS INOP.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 13,161 hrs · 11,042 cycles

FIRST OFFICER`S FLASHLIGHT INOP.

Part: WARNING SYSTEM — MALFUNCTIONED (NLG STEERING) · airframe 12,652 hrs · 10,676 cycles

ON T/O RECEIVED A -STEERING INOP- MESSAGE. COMPLIED WITH QRN 13-5. NO FURTHER ACTION. RE-ENGAGED ON THE GROUND. EMERGENCY VEHICLES ON STANDBY AS A PRECAUTION.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 12,148 hrs · 10,279 cycles

EMERGENCY FLOOR STRIP LIGHTING BETWEEN ROW 3CD AND 6CD INOP.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 11,517 hrs · 9,784 cycles

RANRC 338 FWD RT OF RT BRAKE FUSE BRACKET OS ANOTHER CRACKED BRACKET AS MARKED.

Part: CONTROL CABLE — DAMAGED (LT AILERON) · airframe 11,517 hrs · 9,784 cycles

RANRC 328 LT AILERON CONTROL SYSTEM CABLE CONNECTED TO I/B SIDE OF TENSION REGULATOR TO TBI IN LT MLG WHEEL WELL HAS SEVERAL BROKEN STRANDS.

Part: CONTROL CABLE — DAMAGED (LT AILERON) · airframe 11,517 hrs · 9,784 cycles

RANRC 329 LT AILERON CONTROL SYSTEM CABLE CONNECTED TO I/B SIDE OF TENSION REGULATOR TO TBI IN LT MLG WHEEL WELL HAS SEVERAL BROKEN STRANDS.

Part: FRAME — CRACKED (FUSELAGE) · airframe 11,517 hrs · 9,784 cycles

RANRC 299 FS 574 FRAME LOWER U CHANNEL IS CRACKED AT LBL42. MARKED

Part: HINGE — BROKEN (ESCAPE HATCH) · airframe 11,517 hrs · 9,784 cycles

RANRC 291 CREW ESCAPE HATCH HAS 2 BROKEN HINGES.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 11,517 hrs · 9,784 cycles

RANRC 241. FLOORBEAM HAS MINOR CORROSION ON UPPER SURFACE AT RBL 42 FROM FS 559 & 80 TO FS 621.

Part: SUPPORT — CRACKED (PAX DOOR) · airframe 11,517 hrs · 9,784 cycles

CRACK ON PAX DOOR SUPPORT DOUBLER AT FS 338.9 UNDER PANEL. REMOVED PAX DOOR STEPS 832AT AND 832FT, FOR ACCESS TO DOUBLER AND AFT PULL IN LEVER, IAW CRJ AMM 52-11-04 AND 52-11-23. REMOVED DOUBLER AND FABRICATED WITH S1710-4 EXTRUSION IAW CRJ SRM 52-10-14, FIG 1. OK TO INSTALL. INSTALLED DOUBLER IAW CRJ SRM 51-42-13 AND 51-42-21. REINSTALLED PAX DOOR AFT PULL IN LEVER ASSY. IAW CRJ AMM 52-11-23. OPS CHECK GOOD. REINSTALLED STEP 832AT AND 832FT, IAW CRJ AMM 52-11-04. (SDR CLOSED)

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 11,517 hrs · 9,784 cycles

RANRC 243. FLOORBEAM HAS MINOR CORROSION ON UPPER SURFACE AT RBL 42 FROM FS 559 & 80 TO FS 621.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 11,517 hrs · 9,784 cycles

RANRC 241 FLOORBEAM HAS MINOR CORROSION ON UPPER SURFACE AT RBL 42 FROM FS 559 & 80 TO FS 621.

Part: DOUBLER — CRACKED (PAX DOOR) · airframe 11,517 hrs · 9,784 cycles

RANRC 245 CRACK ON PAX DOOR SUPPORT DOUBLER AT FS 338.9 UNDER PANEL.

Part: ANGLE — CRACKED (PAX DOOR) · airframe 11,517 hrs · 9,784 cycles

RANRC 225. PAX DOOR AFT DRAG ANGLE CRACKED.

Part: STEP — CORRODED (PAX DOOR) · airframe 11,517 hrs · 9,784 cycles

RANRC 226. SURFACE CORROSION UNDER PAX DOOR STEP 832 ET.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 11,499 hrs · 9,768 cycles

EMER EXIT LIGHT AT SERVICE DOOR HAS BULBS INOP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 11,479 hrs · 9,750 cycles

LEFT EXTERNAL OVER/WING AFT EMERGENCY LIGHT IS INOP.

Part: ANCHOR FITTING — CRACKED (AIR STAIR DOOR) · airframe 11,466 hrs · 9,739 cycles

ASD FWD COUNTERBALANCE ANCHOR MOUNT CRACKED.

Part: CABLE — FAULTY (CABIN)

DURING A GROUND INSPECTION, THE FRONT HALF EMERGENCY FLOOR LIGHTS WERE FOUND TO BE DIM. MAINTENANCE REMOVED AND REPLACED THE ELECTRICAL CABLE ASSEMBLY FOR THE FRONT HALF EMERGENCY FLOOR LIGHTS. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)

Part: FLASHLIGHT — DISCHARGED (COCKPIT)

FLT 4500 - DURING A GROUND INSPECTION IN SHV, THE CAPTAINS AND FIRST OFFICERS FLASHLIGHTS WERE FOUND TO BE VERY DIM. MAINTENANCE REMOVED AND REPLACED THE CAPTAINS AND FIRST OFFICERS FLASHLIGHTS. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: LAMP — BURNED OUT (EMERGENCY LIGHT)

FLT 4260 - DURING A GROUND INSPECTION IN VPS, THE EMERGENCY CEILING LIGHT, AT ROW 4, WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE EMERGENCY CEILING LIGHT AT ROW 4. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: DOUBLER — CRACKED (BS 640)

DURING AN A C-CHECK IN BTR, THE LEFT FS 640 DOUBLER, AT STRINGER 9L, WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE LEFT FS 640 DOUBLER, AT STRINGER 9L. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: WINDSHIELD — FAILED (COCKPIT)

FLT 4463 - DURING CRUISE FROM ATL-MDT, AT APPROXIMATELY 27,000 FEET THE FIRST OFFICERS WINDSHIELD SHATTERED FOLLOWED BY A SMALL GLOW AT THE BASE OF THE RIGHT WINDSHIELD. THE CREW THEN RECEIVED A R WSHLD HEAT CAUTION MESSAGE. THE QRH WAS COMPLIED WITH AND AN EMERGENCY WAS DECLARED. THE AIRCRAFT LANDED SAFELY IN MDT. MAINTENANCE REMOVED AND REPLACED THE NR 3 WINDSHIELD. OPERATIONAL AND LEAK CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: PLATE — CRACKED (FUSELAGE)

DURING A C-CHECK, THE CARGO COMPARTMENT FLOOR LANDING SILL PLATE AT FS605 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE CARGO COMPARTMENT FLOOR LANDING SILL PLATE AT FS 605 IAW EO. (K)

Part: CLIP — CRACKED (FUSELAGE)

DURING A C-CHECK, THE LT AND RT FS484 INTERCOSTAL AFT CLIPS OB WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE LT AND RT FS 484 INTERCOSTAL AFT CLIPS OB IAW EO. (K)

Part: CLIP — CRACKED (FUSELAGE) · airframe 7,664 hrs

DURING A C-CHECK, THE LT FS 484 INTERCOSTAL AFT CLIP IB WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE FS 484 INTERCOSTAL AFT CLIP IB IAW EO. (K)

Part: SUPPORT BEAM — CRACKED (FUSELAGE)

DURING A C-CHECK, THE RT LOWER OB ENGINE SUPPORT BEAM AT BL 36.20 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE RT LOWER OB ENGINE SUPPORT BEAM AT BL 36.20 IAW EO. (K)

Part: SUPPORT BEAM — CRACKED (FUSELAGE)

DURING A C-CHECK, THE AFT EQUIPMENT BAY CENTER ENGINE SUPPORT BEAM UPPER AND LOWER WEB AT BL0 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE AFT EQUIPMENT BAY CENTER ENGINE SUPPORT BEAM UPPER AND LOWER WEB AT BL0 IAW EO. (K)

Part: CLIP — CRACKED (FUSELAGE)

DURING A C-CHECK, THE LT AND RT CLIPS AT FS 625 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE LT AND RT CLIPS AT FS 625. (K)

Part: FLOOR SUPPORT — CRACKED (FUSELAGE)

DURING A C-CHECK, THE LT AND RT FLOOR SUPPORT ANGLES AT FS 621 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE LT AND RT FLOOR SUPPORT ANGLES AT FS 621 IAW EO. (K)

Part: CLIP — CRACKED (FUSELAGE)

DURING A C-CHECK, THE RT IB CLIP AT FS 280 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE RT IB CLIP AT FS 280. (K)

Part: TRANSFORMER — BURNED OUT (COCKPIT CONSOLE)

FLT 4742 - DURING APPROACH INTO DFW FROM MLU, ALL THREE CREW MEMBERS REPORTED SMELLING A STRONG ELECTRICAL SMOKE ODOR, BUT COULD NOT LOCALIZE THE SOURCE. THE AIRCRAFT LANDED SAFELY IN DFW. MAINTENANCE RAN THE ENGINES BUT COULD NOT DUPLICATE THE ODOR. MAINTENANCE THEN TURNED ON ALL THE LIGHTS AND FOUND THE LEFT NOSE LANDING LIGHT INOPERATIVE. THE LIGHT WAS REPLACED BUT WAS NO HELP. AFTER FOLLOWING THE SCHEMATICS IT WAS DETERMINED THAT TRANSFORMER T3LE WAS THE CAUSE OF THE ODOR. MAINTENANCE REMOVED AND REPLACED THE BURNED OUT TRANSFORMER. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT)

DURING AN OVERNIGHT INSPECTION IN VPS, THE EMERGENCY EXIT LIGHT BY THE SERVICE DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT LAMP BY THE SERVICE DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: CONTROL UNIT — INTERMITTENT (BLEED SYSTEM)

DURING DESCENT, THE CREW RECEIVED A 14 TH STAGE DUCT MESSAGE. THE QRH WAS COMPLIED WITH AND THE THRUST LEVER WAS REDUCED TO IDLE AT WHICH TIME THE MESSAGE EXTINGUISHED. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED THE LT BLEED LEAK CONTROL UNIT. ENGINE RUNS AND OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE.

Part: BULB — BURNED OUT (EMERGENCY LIGHT)

DURING GROUND INSPECTION IN DFW, THE LT EXTERIOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BURNED OUT EXTERIOR LIGHT BULB. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DURING GROUND INSPECTION IN ATL, THE LEFT OVERWING EMERGENCY LIGHT BULB WAS FOUND TO BE BURNED OUT. MAINTENANCE REMOVED AND REPLACED THE BURNED OUT EMERGENCY LIGHT BULB. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)