N881AS

Part: BLADES — DAMAGED (NR 2 ENGINE) · airframe 40,710 hrs · 37,881 cycles

NR 2 ENGINE SEIZED ON CLIMB OUT. LOUD AGGRESSIVE BANG FROM ENGINE. ITT IN THE RED. N1 ROLLED BACK. RAN QRC QRH FOR SEVERE ENGINE FAILURE IN FLIGHT. SHUT DOWN ENGINE. NO OVERWEIGHT LANDING. NORMAL LANDING. (FLIGHT 5405) DUE TO RT ENGINE EXPERIENCING AN UNRECOVERABLE COMPRESSOR STALL, PERFORMED BORESCOPE INSPECTION OF RT ENGINE COMPRESSOR SECTION REF EM 72-00-00. FOUND EXTENSIVE DAMAGE TO VARIOUS STAGES OF COMPRESSOR BLADES. ORIG SUBMISSION DATE: 11/28/2022

Part: NONE — FAILED · airframe 40,338 hrs · 37,523 cycles

L 14TH DUCT WARNING MESSAGE. QRH PROCEDURE DID NOT CLEAR MESSAGE. RETURNED TO KPSC AS DIRECTED BY QRH (FLIGHT #5788 FILED CLOSED) INSPECTED L/H 14TH STAGE DUCTS IN AFT EQUIPMENT BAY REFERENCING CRJ 200 AMM TASK 36-12-04, FOUND CONNECTION BETWEEN DUCT AND SUPPORT TO BE LOOSE. SECURED DUCT AS REQUIRED, PERFORMED LEAK CHECK, NOTED NO LEAKS.

Part: NONE — FAILED · airframe 39,932 hrs · 37,134 cycles

NOSE GEAR DISAGREE AND NOSE DOOR OPEN WARNING MESSAGE ON APPROACH. RAN QRH. REQUIRED MANUAL GEAR EXTENSION. WARNING MESSAGES EXTINGUISHED FOLLOWED BY A PRECAUTIONARY LANDING (FLIGHT 5247 - FILED CLOSED) REMOVED AND REPLACED NLG SELECTOR VOVLE PER CRJ200 AMM 32-33-10, PERFORMED FUNCTIONAL TEST OF THE EXTENSION AND RETRACTION SYSTEM (REF.TASK 32-30-00-720-801), FUNCTION CHECK GOOD, NO LEAK NOTED, NO MESSAGES NOTED

Part: SPOILER SYS — FAULTED · airframe 38,563 hrs · 35,916 cycles

D:GND SPLR DEPLOY SHORT FINAL. QRH COMPLIED WITH. / C: MEL 27-65-1B / CAT C DUE ON 08/07/2021 / GND SPLR DEPLOY SHORT FINAL. QRH COMPLIED WITH. (FLIGHT 5856 - FILED CLOSED) JUL 28, 2021 STATION: SFO--CREW REPORTED NO OVERWEIGHT LANDING, DID NOT DEPLOY MASK. CREW REPORTED GND SPLR OTBD PAIR NOT GREEN ON SYNOPTIC PAGE. DEFERRED OTBD GND SPLR SYS PER MEL 27-65-1B. MX ACTION C/W.

Part: INTERCOSTAL — CRACKED (BS 460) · airframe 38,563 hrs · 35,916 cycles

PRESSURE FLOOR INTERCOSTAL K601R38908-2001 AT FS460 HAS CRACK AT LBL9 ATTACH FASTENER HOLE. (C-CHECK RO 7/27/2021) REPAIRED PRESSURE FLOOR INTERCOSTAL K601R38908-2001 AT FS460.00 BETWEEN LBL9 & LBL18. REF REO 601R-53-41-2940 REV -- DATED 2021-06-29, CRJ200 SRM 51-42-06, & DWG 601R31172. COMPLIED WITH TASK CARD 51-900-1003-SKY.

Part: DRAG ANGLE — ELONGATED (AFT PAX DOOR) · airframe 38,563 hrs · 35,916 cycles

MULTIPLE ELONGATED HOLES ON AFT PAX DOOR DRAG ANGLE. (C-CHECK RO 7/27/2021) REMOVED, REPLACED, AND INSTALLED PAX DOOR AFT, DRAG ANGLE REF. CRJ200 SRM 51-42-06, CRJ200 SRM 51-42-13, AND DWG 601R31707 REV -E. COMPLIED WITH 51-900-1003-SKY

Part: WEB — CRACKED (PAX DOOR) · airframe 38,563 hrs · 35,916 cycles

CRACK ON AFT PAX DOOR WEB WHERE STEP PANEL 832DT AND TOP PANEL MEET. (C-CHECK RO 7/27/2021) REMOVED AND REPLACED NEW AFT PAX DOOR WEB P/N 601R31707-11S INSTALLED REF BOMBARDIER REO 601R-52-11-702 REV -E DATED 2016-08-14 AND BOMBARDIER DWG 601R31707 REV E AND CRJ 200 SRM 51-42-06. COMPLIED WITH 51-900-1003-SKY

Part: LANDING — DAMAGED (LT WING) · airframe 38,563 hrs · 35,916 cycles

THE CUT-OUT/LAND FOR PANEL 572AL HAS 2EA. ELONGATED HOLES. (C-CHECK RO 7/27/2021) REPAIRED THE CUT OUT LAND FOR PANEL 572AL REF REO 601R-57-31-1368 REV -- 2021-07-12, SKYCARD 51-900-1003 STRUCTURAL MAJOR REPAIR COMPLIED WITH.

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 38,563 hrs · 35,916 cycles

CORROSION ON PAX DOOR, DD7 AFT INTERCOSTAL (C-CHECK RO 7/27/2021) REMOVED AND INSTALLED NEW DD7 AFT INTERCOSTAL. REF DWG# 601R31702 REV -N & CRJ200 SRM 51-42-06. COMPLIED WITH TASK CARD 51-900-1003-SKY. PRESSURE LEAK CHECK WAS SATISFACTORY. SEE CONTINUATION CARD FOR FULL DETAILS.

Part: BRACKET — CORRODED (PAX DOOR) · airframe 38,563 hrs · 35,916 cycles

CORROSION ON PAX DOOR BRACKET, COMMON TO DD4 AFT INTERCOSTAL (C-CHECK RO 7/27/2021) REMOVED AND INSTALLED NEW PAX DOOR BRACKET COMMON TO DD4 AFT INTERCOSTAL. REF DWG# 601R31702 REV -N & CRJ200 SRM 51-42-06. COMPLIED WITH TASK CARD 51-900-1003-SKY. PRESSURE LEAK CHECK WAS SATISFACTORY. SEE CONTINUATION CARD FOR FULL DETAILS.

Part: BRACKET — CORRODED (PAX DOOR) · airframe 38,563 hrs · 35,916 cycles

CORROSION ON PAX DOOR BRACKET, COMMON TO DD6 AFT INTERCOSTAL (C-CHECK RO 7/27/2021) REMOVED AND INSTALLED NEW PAX DOOR BRACKET COMMON TO DD6 AFT INTERCOSTAL. REF DWG# 601R31702 REV -N & CRJ200 SRM 51-42-06. COMPLIED WITH TASK CARD 51-900-1003-SKY. PRESSURE LEAK CHECK WAS SATISFACTORY.

Part: FORMER — CORRODED (PAX DOOR) · airframe 38,563 hrs · 35,916 cycles

PAX DOOR CORROSION ON EXSISTING FORMER REPAIR FS347.27 UNDER AFT GUIDE PULLEY MOUNT BETWEEN INTERCOSTALS DD4 AND DD5 (C-CHECK RO 7/27/2021) REMOVED AND REPLACED PAX DOOR FORMER AT FS 347.37 REF CRJ200 SRM 51-42-06, CRJ200 SRM 51-42-21, AND DWG 601R31702 REV N. COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY. ALL CHECKS GOOD. SEE CONTINUATION CARD FOR FULL DETAILS.

Part: INTERCOSTAL — DAMAGED (PAX DOOR) · airframe 38,563 hrs · 35,916 cycles

PAX DOOR INTERCOSTAL FWD DD4 HAS A DRILL START LOCATED ON UPPERFLANGE (C-CHECK RO 7/27/2021) REMOVED AND REPLACED FWD DD4 INTERCOSTAL REF CRJ200 SRM 51-42-06 AND DWG 601R31702 REV -N. ALL CHECKS GOOD. SEE CONTINUATION CARD FOR FULL DTAILS. COMPLIED WITH TASK CARD 51-900-1003-SKY

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 38,563 hrs · 35,916 cycles

CORROSION ON PAX DOOR CENTER INTERCOSTAL DD6, FS327.763 (C-CHECK RO 7/27/2021) REMOVED AND REPLACED PAX DOOR CENTER INTERCOSTAL DD6 REF CRJ200 SRM 51-42-06, 51-42-21 AND DWG 601R31702 REV N. ALL CHECKS GOOD. SEE CONTINUAION CARD FOR FULL DETAILS. COMPLIED WITH TASK CARD 51-900-1003-SKY

Part: GUSSET — CORRODED (BS 310) · airframe 38,563 hrs · 35,916 cycles

PASSENGER DOOR SURROUND STRUCTURE GUSSET CORRODED FS310.00 APPROX. WL135.681. (MARKED) (C-CHECK RO 7/27/2021) CORROSION ON GUSSET PASSENGER DOOR SURROUND STRUCTURE GUSSET FS310.00 APPROX. WL135.681 IS AROUND FASTENER HOLES AND IS OUT OF LIMITS REF CRJ200 SRM 53-00-00. REMOVED BAD GUSSET REF CRJ200 SRM 51-42-06. FABRICATED REPLACEMENT PASSENGER DOOR SURROUND STRUCTURE GUSSET FS310.00 APPROX. WL135.681 (PART# 601R31096-51) ON JOB 2749675 OP 148 CAMP 22931958. ORDERED AND RECEIVED REPLACEMENT FASTENERS AND INSTALLED REPLACEMENT GUSSET WITH REPLACEMENT FASTENERS REF DRW. 601R31096 REV D. AND REF CRJ200 SRM 51-42-06. COMPLIED WITH TASK CARD 51-900-1003-SKY.

Part: GUSSET — CORRODED (BS 310) · airframe 38,563 hrs · 35,916 cycles

PASSENGER DOOR SURROUND STRUCTURE GUSSET CORRODED FS310.00 APPROX. STRG. 9. (MARKED) (C-CHECK RO 7/27/2021) CORROSION ON GUSSET PASSENGER DOOR SURROUND STRUCTURE GUSSET FS310.00 APPROX. STRG. 9 IS AROUND FASTENER HOLES AND IS OUT OF LIMITS REF CRJ200 SRM 53-00-00. REMOVED BAD GUSSET REF CRJ200 SRM 51-42-06. ORDERED AND RECEIVED REPLACEMENT GUSSET PART# 600-31109-45. ORDERED AND RECEIVED REPLACEMENT FASTENERS AND INSTALLED REPLACEMENT GUSSET WITH REPLACEMENT FASTENERS REF DRW. 601R31109 REV F. AND REF CRJ200 SRM 51-42-06. COMPLIED WITH TASK CARD 51-900-1003-SKY.

Part: GUSSET — CORRODED (BS 310) · airframe 38,563 hrs · 35,916 cycles

PASSENGER DOOR SURROUND STRUCTURE GUSSET CORRODED FS310.00 APPROX. WL115.07. (MARKED) (C-CHECK RO 7/27/2021) CORROSION ON GUSSET PASSENGER DOOR SURROUND STRUCTURE GUSSET FS310.00 APPROX. WL115.07 IS AROUND FASTENER HOLES AND IS OUT OF LIMITS REF CRJ200 SRM 53-00-00. REMOVED BAD GUSSET REF CRJ200 SRM 51-42-06. ORDERED AND RECEIVED REPLACEMENT GUSSET PART# 601R31098-15. LOCATED FASTENER HOLES IN REPLACEMENT GUSSET REF CRJ200 SRM 51-42-06. ORDERED AND RECEIVED REPLACEMENT FASTENERS AND INSTALLED REPLACEMENT GUSSET WITH REPLACEMENT FASTENERS REF DRW. 601R31109 REV F. AND REF CRJ200 SRM 51-42-06. COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY.

Part: GUSSET — CORRODED (BS 310) · airframe 38,563 hrs · 35,916 cycles

PASSENGER DOOR SURROUND STRUCTURE GUSSET CORRODED FS310.00 APPROX. WL144.18. (MARKED) (C-CHECK RO 7/27/2021) REMOVED AND INSTALLED REPLACEMENT GUSSET WITH REPLACEMENT FASTENERS REF DRW. 601R31096 REV D. AND REF CRJ200 SRM 51-42-06. FOUND TO OUT OF LIMITS REF CRJ 200 SRM 53-00-00. COMPLIED WITH 51-900-1003-SKY

Part: GUSSET — CORRODED (BS 310) · airframe 38,563 hrs · 35,916 cycles

*PASSENGER DOOR SURROUND STRUCTURE GUSSET CORRODED FS310.00 BETWEEN STGR14L & STGR15L. (MARKED) (C-CHECK RO 7/27/2021) CORROSION ON GUSSET PASSENGER DOOR SURROUND STRUCTURE GUSSET FS310.00 STGR14L & STGR15L IS AROUND FASTENER HOLES AND IS OUT OF LIMITS REF CRJ200 SRM 53-00-00. REMOVED BAD GUSSET REF CRJ200 SRM 51-42-06. ORDERED AND RECEIVED REPLACEMENT GUSSET PART# 601R31109-97. LOCATED FASTENER HOLES IN REPLACEMENT GUSSET REF CRJ200 SRM 51-42-06. ORDERED AND RECEIVED REPLACEMENT FASTENERS AND INSTALLED REPLACEMENT GUSSET WITH REPLACEMENT FASTENERS REF DRW. 601R31109 REV F. AND REF CRJ200 SRM 51-42-06. COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY.

Part: GUSSET — CORRODED (BS 310) · airframe 38,563 hrs · 35,916 cycles

*PASSENGER DOOR SURROUND STRUCTURE GUSSET CORRODED FS310.00 BETWEEN STGR11L & STGR12L. (MARKED) (C-CHECK RO 7/27/2021) REMOVED AND INSTALLED NEW PAX DR SURROUND GUSSET AT FS310 BETWEEN STGR 11L-12L REF CRJ 200 SRM 51-42-06 SEE CONTINUATION CARD FOR DETAILS. COMPLIED WITH 51-900-1003-SKY. COMPLETED FORM M-337.

Part: GUSSET — CORRODED (BS 310) · airframe 38,563 hrs · 35,916 cycles

*PASSENGER DOOR SURROUND STRUCTURE GUSSET CORRODED FS310.00 BETWEEN STGR12L & STGR13L. (MARKED) (C-CHECK RO 7/27/2021) REMOVED AND INSTALLED NEW PASSENGER DOOR SURROUND STRUCTURE GUSSET. FS310.00 BETWEEN STGR12L & STGR13L RESTORED FINISH AND APPLIED CIC REF:CRJ200 SRM 51-42-21, CRJ200 SRM 51-21-11, CRJ200 SRM 51-21-16 AND DWG 601R31109 REV-F. COMPLIED WITH 51-900-1003-SKY.

Part: SKIN — DENTED (BS 625-640) · airframe 38,563 hrs · 35,916 cycles

* DENTS IN FUSELAGE SKIN FS625.30-FS640.00 BETWEEN STGR22L & STGR21L (C-CHECK RO 7/27/2021) REPAIRED DENTED FUSELAGE SKIN FROM FS621.00 TO FS640.00 BETWEEN STGR21L & STGR22L. REF REO 601R-53-61-7677 REV -- DATED 2021-07-05, CRJ200 SRM 51-42-21, & CRJ200 SRM 51-42-22. COMPLIED WITH TASK CARD 51-900-1003-SKY

Part: HINGE — CORRODED (LT ELEVATOR) · airframe 38,563 hrs · 35,916 cycles

* L/H ELEVATOR #3 HINGE ON H STAB HAS CORRODED HARDWARE (C-CHECK RO 7/27/2021) INSTALLED NEW BONDING JUMPER AND HARDWARE. BONDING TEST GOOD REF CRJ 200 AMM 51-80-00-400-802

Part: HINGE — CORRODED (LT ELEVATOR) · airframe 38,563 hrs · 35,916 cycles

* L/H ELEVATOR #1 HINGE ON H STAB HAS CORRODED HARDWARE (C-CHECK RO 7/27/2021) REMOVED AND REPLACED HARDWARE ON L/H ELEVATOR #1 HINGE ON H STAB REF CRJ 200 SRM 51-41-02

Part: ACCESS PANEL — CORRODED (LT WING) · airframe 38,563 hrs · 35,916 cycles

*LH LOWER WING PLANK ACCESS HOLE 510AB FLANGE HAS CORROSION LOWER SIDE. (C-CHECK RO 7/27/2021) BLENDED CORROSION FROM LWR SIDE OF LH LOWER WING PLANK ACCESS HOLE 510AB FLANGE TO A SMOOTH CONTOUR AND RESTORED FINISH. REMAINING MATERIAL IN REWORKED AREAS IS WITHIN LIMITS. REF REO 601R-57-21-030 REV -L DATED 2014-02-05, DWG# 601R10045 REV AE. COMPLIED WITH 51-900-1003-SKY NO DEFECTS NOTED

Part: HINGE — CORRODED (LT ELEVATOR) · airframe 38,563 hrs · 35,916 cycles

* L/H ELEVATOR #2 HINGE ON H STAB HAS CORRODED HARDWARE (C-CHECK RO 7/27/2021) REMOVED AND REPLACED HARDWARE ON L/H ELEVATOR #2 HINGE ON H STAB REF CRJ 200 SRM 51-41-02

Part: HINGE — CORRODED (RT ELEVATOR) · airframe 38,563 hrs · 35,916 cycles

* R/H ELEVATOR #2 HINGE ON H STAB HAS CORRODED HARDWARE (C-CHECK RO 7/27/2021) REMOVED AND REPLACED HARDWARE ON R/H ELEVATOR #2 HINGE ON H STAB REF CRJ 200 SRM 51-41-02

Part: HINGE — CORRODED (LT ELEVATOR) · airframe 38,563 hrs · 35,916 cycles

* L/H ELEVATOR #4 HINGE ON H STAB HAS CORRODED HARDWARE (C-CHECK RO 7/27/2021) REMOVED AND REPLACED HARDWARE ON L/H ELEVATOR #4 HINGE ON H STAB REF CRJ 200 SRM 51-41-02

Part: HINGE — CORRODED (RT ELEVATOR) · airframe 38,563 hrs · 35,916 cycles

* R/H ELEVATOR #3 HINGE ON H STAB HAS CORRODED HARDWARE (C-CHECK RO 7/27/2021) INSTALLED NEW BONDING JUMPER AND HARDWARE ON RH ELEVATOR #3 HINGE BONDING TEST GOOD REF CRJ 200 AMM 51-80-00-400-802, SEE CONTINUATION CARD FOR DETAILS.

Part: ACCESS PANEL — CORRODED (LT WING) · airframe 38,563 hrs · 35,916 cycles

*LH LOWER WING PLANK ACCESS HOLE 540BB FLANGE HAS CORROSION LOWER SIDE. (C-CHECK RO 7/27/2021) BLENDED CORROSION FROM LWR SIDE OF LH LOWER WING PLANK ACCESS HOLE 540BB FLANGE TO A SMOOTH CONTOUR AND RESTORED FINISH. REMAINING MATERIAL IN REWORKED AREAS IS WITHIN LIMITS. REF GENERIC REO 601R-57-21-030 REV -L DATED 2014-02-05 AND DWG# 601R10044 REV AF. SEE CONTINUATION CARD FOR DETAILS. COMPLIED WITH 51-900-1003-SKY

Part: FLOORBEAM — CRACKED (BS 280) · airframe 38,563 hrs · 35,916 cycles

UPON REMOVAL STEP FOR FS 280.0 FLOOR BEAM REPAIR , FOUND CRACK ON COCKPIT FLOOR SUPPORT ANGLE . (C-CHECK RO 7/27/2021) REPLACED COCKPIT FLOOR SUPPORT ANGLE WITH NEW 600-34017-351 PO T-59936 REF BOMBARDIER DWG 600-34017 REV AD AND CRJ 200 SRM 51-42-06. COMPLIED WITH SKY CARD 51-900-1003-SKY STRUCTURAL MAJOR REPAIR.

Part: HINGE — CORRODED (RT ELEVATOR) · airframe 38,563 hrs · 35,916 cycles

* R/H ELEVATOR #4 HINGE ON H STAB HAS CORRODED HARDWARE (C-CHECK RO 7/27/2021) REMOVED AND REPLACED HARDWARE ON R/H ELEVATOR #4 HINGE ON H STAB REF CRJ 200 SRM 51-41-02

Part: DOOR SILL — CRACKED (BS 364) · airframe 38,563 hrs · 35,916 cycles

*AFT SIDE LOWER SILL PAX DOOR FS 364.00 BETWEEN STRG 17L AND 18L UNDER SIDE HAS A POSSIBLE CRACK AT INBOARD FASTENER FOR AFT CLEAT AS MARKED. (C-CHECK RO 7/27/2021) REPAIRED PAX DOOR LWR LONGERON BETWEEN FS349.00 AND FS364.00. REF REO 601R-53-21-3461 REV -- DATED 2021-07-01. COMPLIED WITH 51-900-1003-SKY

Part: HINGE ARM — DAMAGED (LT WING TE FLAP) · airframe 38,563 hrs · 35,916 cycles

*L/H INBD FLAP, INBD HINGE ARM, HAS FOD DAMAGE AT HINGE LOCATION ON ARM. (AREA MARKED) (C-CHECK RO 7/27/2021) REPAIRED AREA L/H INBD FLAP, INBD HINGE ARM, FOD DAMAGE AT HINGE LOCATION ON ARM BY COMPLYING WITH REO 601R-57-54-330 REV-- DATED 2021-06-16 (SEE CONTINUATION FOR DETAILS) COMPLIED WITH 51-900-1003-SKY, COMPLETED FORM M-337 SEE CONTINUATION CARD FOR DETAILS.

Part: SKIN — CHAFED (LT WING) · airframe 38,563 hrs · 35,916 cycles

LH LOWER WING SKIN HAS CHAFING DAMAGE BY FLAP ACTUATOR FARING 583AB AND 586AB AS MARKED. (C-CHECK RO 7/27/2021) BLENDED AND REMOVED CHAFING DAMAGE ON LOWER WING SKIN COMMON TO FAIRINGS 583AB AND 586AB. REF. CRJ200 SRM 51-12-00 / NO DAMAGE ALLOWED IAW CRJ 200 SRM 57-21-00 / COMPLIED WITH REO 601R-57-21-3490 REV-A DATED 2021-07-22 TO REPAIR LH LOWER WING SKIN CHAFING DAMAGE BY FLAP ACTUATOR FARING 583AB AND 586AB. SEE CONTINUATION CARD FOR MAINTANANCE DETAILS. COMPLIED WITH TASK CARD 51-900-1003-SKY

Part: ACCESS PANEL — ELONGATED (ZONE 100) · airframe 38,563 hrs · 35,916 cycles

FASTENER HOLES AROUND LH FWD ACCESS PANEL 131AL ARE ELONGATED AS MARKED (C-CHECK RO 7/27/2021) REPAIRED FASTENER HOLES AROUND LH FWD ACCESS PANEL 131AL REF REO 601R-53-11-3703 REV €“ DATED 2021-06-18 STEPS 1-11. ALL STEPS COMPLIED WITH. COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY. PRESSURE CHECK GOOD. SEE CONTINUATION CARD FOR FULL DETAILS.

Part: BULKHEAD WEB — CRACKED (BS 280) · airframe 38,563 hrs · 35,916 cycles

PERFORM A FULL REPAIR TO BULKHEAD WEB FS 280.0 LBL 20.75 TO RBL 20.75 PER REO 601R-53-11-926 REV B DATED 2006/05/10 ,DUE TO CRACK TO LONG OUT OF LIMIT FOR LOCAL REPAIR. (C-CHECK RO 7/27/2021) PERFORMED A FULL REPAIR TO BULKHEAD WEB FS 280.0 LBL 20.75 TO RBL 20.75 AT LOWER FLOOR LEVEL PER REO 601R-53-11-926 REV B DATED 2006/05/10 . COMPLIED WITH SKY CARD 51-900-1003-SKY

Part: FLOORBEAM — CORRODED (BS 349 RBL27) · airframe 38,563 hrs · 35,916 cycles

*FS 349 FLOOR CROSSBEAM CAP BETWEEN RBL 27 AND RH FLOOR SILL HAS EXFOLIATION CORROSION. (C-CHECK RO 7/27/2021) REMOVED AND REPLACED ANGLE P/N 601R38783-13. FS 349 FLOOR CROSSBEAM CAP BETWEEN RBL 27 AND RH FLOOR SILL. REF DWG# 601R386651, REV --, CRJ-200 SRM 51-42-06. COMPLIED WITH TASK CARD 51-900-1003-SKY, SEE CONTINUATION CARD FOR FURTHER DETAILS.

Part: MOUNT — CORRODED (BS 308 LBL20) · airframe 38,563 hrs · 35,916 cycles

*FLOOR STRUCTURE: ENTRANCE CABINET MOUNT TOP PLATE AT APPROX FS 308 / LBL 20 HAS EVIDENCE OF CORROSION. (C-CHECK RO 7/27/2021) REPLACED ENTRANCE CABINET MOUNT TOP PLATE AT FS308.00 & LBL 20. REF CRJ200 DWG# 601R38670 REV -T & CRJ200 SRM 51-42-13. COMPLIED WITH TASK CARD 51-900-1003.

Part: ANCHOR FITTING — CORRODED (PAX DOOR) · airframe 38,563 hrs · 35,916 cycles

* PAX DOOR AFT ANCHOR FITTING HAS CORRODED HARDWARE. FLAGGED (C-CHECK RO 7/27/2021) REMOVED AND INSTALLED NEW HARDWARE TO PAX DOOR AFT ANCHOR TORQUE LEVEL 35LB TUC4978 CAL DUE 30-JUN-21 REF CRJ 200 AMM 52-11-17-000-802 AND 52-11-17-400-802

Part: FLOOR SUPPORT — CORRODED (BS 409) · airframe 38,563 hrs · 35,916 cycles

* MULTIPLE CORROSION SPOTS FOUND AT FLOOR BEAM APPROX F.S409.00+32-409.00+128 AT STGR25R (AREA MARKED) (C-CHECK RO 7/27/2021) REMOVED AND REPLACED RBL9 (STGR25R) FLOOR BEAM CAP BETWEEN FS409.00+32 AND FS409.00+128. REF REO 601R-53-31-1198 REV--, DATED 2021-06-15, DWG 601R31117 REV E, DWG 601R31024 REV D, DWG 601R31005 REV B, DWG 601R31030 REV -P, CRJ 200SRM 53-00-43, CRJ200 SRM 51-42-21, AND CRJ200 SRM 51-42-22. COMPLIED WITH TASK CARD 51-900-1003-SKY

Part: ANCHOR FITTING — CORRODED (PAX DOOR) · airframe 38,563 hrs · 35,916 cycles

* PAX DOOR FWD ANCHOR FITTING HAS CORRODED HARDWARE. FLAGGED (C-CHECK RO 7/27/2021) REMOVED AND REPLACED PAX DOOR FWD ANCHOR FITTING AND CORRODED HARDWARE WITH A SERVICEABLE FWD ANCHOR FITTING AND NEW ATTACHMENT HARDWARE IAW CRJ-200 AMM 52-11-17-000-804 AND 52-11-17-400-804, ADJUSTED PAX DOOR COUNTERBALANCE SYSTEM REF CRJ-200 AMM 52-11-17-820-802, CHECKED GOOD, SEE CONTINUATION CARD FOR DETAILS.

Part: FLOOR SUPPORT — CORRODED (BS 409) · airframe 38,563 hrs · 35,916 cycles

* MULTIPLE SURFACE CORROSION FOUND ON FLOOR BEAM APPROX F.S409.00+32--409.00+128 AT STGR25L (AREA MARKED) (C-CHECK RO 7/27/2021) REMOVED AND INSTALLED NEW FLOOR BEAM CAP AT LBL 9.0 BETWEEN F/S 409+32 AND F/S 409-128 IAW REO 601R-53-31-1198 REV. -- DATED 2021-06-15. COMPLIED WITH TASK CARD 51-900-1003-SKY

Part: FLOOR SUPPORT — CORRODED (BS 559) · airframe 38,563 hrs · 35,916 cycles

* MULTIPLE CORROSION SPOTS FOUND ON FLOOR BEAM APPROX F.S559.80 AT STGR25R (AREA MARKED). (C-CHECK RO 7/27/2021) REMOVED AND REPLACED RBL9 (STGR 25R) FLOORBEAM CAP BETWEEN FS559.00+5 AND FS570.00. REF REO 601R-53-51-593 REV -- DATED 2021-06-16, DWG 601R31119 REV H, CRJ200 SRM 51-42-34, AND CRJ200 SRM 51-42-21. COMPLIED WITH TASK CARD 51-900-1003-SKY

Part: MOUNT — CORRODED (BS 286 RBL38) · airframe 38,563 hrs · 35,916 cycles

*FLOOR STRUCTURE: G1 GALLEY MOUNT TOP PLATE AT APPROX FS 286 / RBL 38 HAS EVIDENCE OF CORROSION. (C-CHECK RO 7/27/2021) REMOVED AND REPLACED GALLEY PLATE P/N: 601R38669-65. FLOOR STRUCTURE G1 GALLEY AT APPROX FS 286 / RBL 38. REF: DWG# 601R38669, REV -N, CRJ 200, SRM 51-42-10.COMPLIED WITH 51-900-1003-SKY

Part: MOUNT — CORRODED (BS 317 RBL5) · airframe 38,563 hrs · 35,916 cycles

*FLOOR STRUCTURE: G1 GALLEY MOUNT TOP PLATE AT APPROX FS 317 / RBL 5 HAS EVIDENCE OF CORROSION. (C-CHECK RO 7/27/2021) REPLACED GALLEY 1 MOUNT TOP PLATE AT APPROX FS 317 / RBL 5. REF CRJ200 SRM 51-42-13 AND DWG# 601R38669 REV -N. COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY.

Part: RIB — CRACKED (LT WING) · airframe 38,563 hrs · 35,916 cycles

* L/H BATT RIB WEB CRACKED AT UPPER FASTENERS WS 53.60 (C-CHECK RO 7/27/2021) REPAIRED CRACKED LH BATT RIB AT WS5.6 REF BOMBARDIER REO 601R-57-51-046 REV B DATED 2002-02-28 SEE CONTINUATION CARD FOR DETAILS. COMPLIED WITH 51-900-1003-SKY, COMPLETED FORM M-337.

Part: SEAT TRACK — CORRODED (BS 409) · airframe 38,563 hrs · 35,916 cycles

* LH SIDE SEAT RAIL IS CORRODED IN AREA OF FS409+128 AND FWD. MARKED WITH GREASE PENCIL (C-CHECK RO 7/27/2021) REMOVED AND INSTALLED TWO NEW L/H SIDE SEAT TRACKS FWD OF FS409.00+128. REF CRJ200 AMM 53-01-11-000-802 & CRJ200 AMM 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (BS 409) · airframe 38,563 hrs · 35,916 cycles

* LEFT SIDE SEAT RAIL STRUCTURE AFT OF FS409.0+128 IS CORRODED. MARKED WITH GREASE PENCIL (C-CHECK RO 7/27/2021) REMOVED AND INSTALLED TWO NEW SIDE SEAT TRACKS WITH NEW HARDWARE AFT OF FS409.00+128. REF CRJ200 AMM 53-01-11-000-802 & CRJ200 AMM 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (BS 409) · airframe 38,563 hrs · 35,916 cycles

* RH SIDE SEAT RAIL U CHANNEL IS CORRODED. SIDE SEAT RAIL STRUCTURE FORWARD OF FS409.0 +128 IN AREA'S. CIRCLED WITH GREASE PENCIL. (C-CHECK RO 7/27/2021) REMOVED AND REPLACEDRH SIDE SEAT RAIL U CHANNEL (P/N 601R38312-89) FWD AT FS364.00 TO FS409.00+16. REF: CRJ 200, AMM 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (BS 409) · airframe 38,563 hrs · 35,916 cycles

* RIGHT SIDE SEAT RAIL STRUCTURE AFT OF FS409.0+128 HAS MULTABLE AREA'S OF CORROSION. (C-CHECK RO 7/27/2021) REMOVED AND INSTALLED NEW R/H SIDE SEAT RAIL FS409.00+112 TO FS449.00 WITH NEW HARDWARE. REF CRJ200 AMM 53-01-11-000-802 & CRJ200 AMM 53-01-11-400-802. NO OTHER CORROSION PRESENT ON RIGHT SIDE SEAT RAIL STRUCTURE AFT OF FS409.0+128

Part: SEAT TRACK — CORRODED (BS 409) · airframe 38,563 hrs · 35,916 cycles

* RIGHT SIDE SEAT RAIL STRUCTURE IS CORRODED FORWARDOF FS409.0 +128 MARKED WITH GREASE PENCIL (C-CHECK RO 7/27/2021) REMOVED AND REPLACED RIGHT SIDE SEAT RAIL TRACK (P/N 601R38312-31) OF FS364.00 TO FS409.00+16, AND SEAT RAIL TRACK(P/N601R38312-29) OF FS409.00+16 TO FS409.00+128. REF: CRJ 200, AMM 53-01-11-400-802.

Part: HINGE — GOUGED (RT WING TE FLAP) · airframe 38,563 hrs · 35,916 cycles

* RH OTBD FLAP HINGE BOX AFT ATTACH FITTING AT WS220.00 GOUGED (C-CHECK RO 7/27/2021) BLENDED DAMAGE ON R/H OTBD FLAP HINGE BOX AFT ATTACH FITTING AT WS220.00 TO A SMOOTH CONTOUR AND RESTORED FINISH. REMAINING MATERIAL IN REWORKED AREA IS WITHIN LIMITS. REF REO 601R-57-21-3485 REV -- DATED 2021-06-11. / COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY.

Part: RIB — CRACKED (RT WING) · airframe 38,563 hrs · 35,916 cycles

R/H BATT RIB ANGLE P/N 601R10203-25 CRACKED (C-CHECK RO 7/27/2021) REMOVED AND REPLACED R/H BATT RIB ANGLE P/N 601R10203-25. REF DWG 601R10203 REV -G AND CRJ200 SRM 51-42-21. COMPLIED WITH TASK CARD 51-900-1003-SKY.

Part: INTERCOSTAL — CRACKED (PAX DOOR) · airframe 38,563 hrs · 35,916 cycles

POTENTIAL CRACK ON PAX DOOR INTERCOSTAL AT DD1 AFT SIDE OF DOOR. (MARKED) (C-CHECK RO 7/27/2021) REMOVED DAMAGED INTERCOSTAL. REPLACED AND INSTALLED NEW DD1 INTERCOSTAL P/N 601R31902-318 REF. CRJ200 SRM 51-42-06, AND DWG# 601R31702 REV -N. COMPLIED WITH 51-900-1003-SKY

Part: PCU — CORRODED (RT SPOILER) · airframe 38,563 hrs · 35,916 cycles

* RH OTBD GROUND SPOILER TO PCU HARDWARE CORRODED (C-CHECK RO 7/27/2021) REMOVED CORRODED HARDWARE RIGHT OUTBOARD GROUND SPOILER TO PCU REF CRJ 200 AMM 27-65-01-000-801 AND INSTALLED NEW HARDWARE REF CRJ 200 AMM 27-65-01-400-801. OPERATIONAL TEST GOOD REF CRJ 200 AMM 27-65-00-710-801.

Part: HINGE — CORRODED (LT WING SPOILER) · airframe 38,563 hrs · 35,916 cycles

* LH FLIGHT SPOILER HINGE HARDWARE CORRODED (C-CHECK RO 7/27/2021) REMOVED AND REPLACED 4 BOLTS, 4 NUTS, 12 WASHERS AND 4 COTTER PINS. REF. CRJ200 AMM 27-64-05-000-801 AND CRJ200 AMM 27-64-05-400-801 CALIBRATED TOOL USED TUC 5659 CAL DUE DATE 28 FEB 22

Part: HINGE — CORRODED (RT SPOILER) · airframe 38,563 hrs · 35,916 cycles

* RH OTBD GROUND SPOILER HINGE HARDWARE CORRODED (C-CHECK RO 7/27/2021) REMOVED CORRODED HINGE HARDWARE RIGHT OUTBOARD GROUND SPOILER REF CRJ 200 AMM 27-65-01-000-801 AND INSTALLED NEW HARDWARE REF CRJ 200 AMM 27-65-01-400-801. OPERATIONAL TEST GOOD REF CRJ 200 AMM 27-65-00-710-801.

Part: PCU — CORRODED (RT SPOILER) · airframe 38,563 hrs · 35,916 cycles

* RH FLIGHT SPOILER INBD AND OTBD PCU€™S HARDWARE IS CORRODED (C-CHECK RO 7/27/2021) REMOVED CORRODED HARDWARE RIGHT FLIGHT SPOILER INBOARD AND OUTBOARD PCUS REF CRJ 200 AMM 27-62-01-000-801 AND INSTALLED NEW HARDWARE REF CRJ 200 AMM 27-62-01-400-801. OPERATIONAL TEST GOOD REF CRJ 200 AMM 27-64-00-710-801.

Part: HINGE — CORRODED (RT SPOILER) · airframe 38,563 hrs · 35,916 cycles

* RH FLIGHT SPOILER HINGE HARDWARE IS CORRODED (C-CHECK RO 7/27/2021) REMOVED CORRODED HINGE HARDWARE RIGHT FLIGHT SPOILER HINGE REF CRJ 200 AMM 27-64-05-000-801 AND INSTALLED NEW HARDWARE REF CRJ 200 AMM 27-64-05-400-801. OPERATIONAL TEST GOOD REF CRJ 200 AMM 27-64-00-710-801.

Part: HINGE — CORRODED (LT SPOILER) · airframe 38,563 hrs · 35,916 cycles

* LH OTBD GROUND SPOILER HINGE HARDWARE CORRODED (C-CHECK RO 7/27/2021) REMOVED AND REPLACED LH OTBD GROUND SPOILER HINGE IAW CRJ-200 AMM 27-65-01-000-801 AND 27-65-01-400-801, OPERATIONAL TEST CHECKED GOOD, SEE CONTINUATION CARD FOR DETAILS.

Part: HINGE — CORRODED (RT SPOILER) · airframe 38,563 hrs · 35,916 cycles

* RH INBD GROUND SPOILER HINGE HARDWARE CORRODED (C-CHECK RO 7/27/2021) REMOVED AND REPLACED R/H I/B GROUND SPOILER HINGE HARDWARE IAW CRJ-200 AMM 27-65-01-000-801 AND 27-65-01-400-801, OPERATIONAL TEST CHECKED GOOD, SEE CONTINUATION CARD FOR DETAILS.

Part: FASTENER — DAMAGED (RT WING TE FLAP) · airframe 38,563 hrs · 35,916 cycles

RH OUTBOARD FLAP HAS 9EA SMOKING RIVETS AT APPROX WS226.51. (C-CHECK RO 7/27/2021) REPAIRED RH OUTBOARD FLAP 9EA SMOKING RIVETS AT APPROX WS226.51 BY COMPLYING WITH REO 601R-57-53-1220 REV-- DATED 2021-06-21, COMPLIED WITH TASK CARD 51-900-1003-SKY, SEE CONTINUATION CARD FOR DETAILS.

Part: ATTACH FITTING — CORRODED (LT SPOILER PCU) · airframe 38,563 hrs · 35,916 cycles

* LH FLIGHT SPOILER OTBD PCU ATTACH HARDWARE CORRODED (C-CHECK RO 7/27/2021) REMOVED AND REPLACED LH FLIGHT SPOILER OTBD PCU ATTACH HARDWARE IAW CRJ-200 AMM 27-62-01-000-801 AND 27-62-01-400-801, OPERATIONAL TEST CHECKED GOOD, SEE CONTINUATION CARD FOR DETAILS.

Part: HINGE — CORRODED (LT SPOILER) · airframe 38,563 hrs · 35,916 cycles

* LH INBD GROUND SPOILER HINGE HARDWARE CORRODED (C-CHECK RO 7/27/2021) REMOVED AND REPLACED LH INBD GROUND SPOILER HINGE HARDWARE IAW CRJ-200 AMM 27-65-01-000-801 AND 27-65-01-400-801, OPERATIONAL TEST CHECKED GOOD, SEE CONTINUATION CARD FOR DETAILS.

Part: PCU — CORRODED (LT SPOILER) · airframe 38,563 hrs · 35,916 cycles

* LH OTBD GROUND SPOILER PCU HARDWARE CORRODED (C-CHECK RO 7/27/2021) REMOVED AND REPLACED LH OTBD GROUND SPOILER PCU HARDWARE IAW CRJ-200 AMM 27-65-01-000-801 AND 27-65-01-400-801, OPERATIONAL TEST CHECKED GOOD, SEE CONTINUATION CARD FOR DETAILS.

Part: HINGE — CORRODED (RT SPOILER) · airframe 38,563 hrs · 35,916 cycles

* RH SPOILERON HINGE HARDWARE IS CORRODED (C-CHECK RO 7/27/2021) REMOVED AND REPLACED RH SPOILERON IB AND OB HINGE ATTACHING HARDWARE IAW CRJ-200 AMM 27-64-01-000-801 AND 27-64-01-400-801, OPERATIONAL TEST CHECKED GOOD, SEE CONTINUATION CARD FOR DETAILS.

Part: PCU — CORRODED (LT SPOILER) · airframe 38,563 hrs · 35,916 cycles

* LH INBD GROUND SPOILER PCU HARDWARE CORRODED (C-CHECK RO 7/27/2021) REMOVED AND REPLACED LH INB GROUND SPOILER PCU HARDWARE REF CRJ-200 AMM 27-63-01-000-801, AND 27-63-01-400-801

Part: PCU — CORRODED (RT SPOILERON) · airframe 38,563 hrs · 35,916 cycles

* RH SPOILERON INBD AND OTBD PCU€™S LOWER ATTACH HARDWARE CORRODED (C-CHECK RO 7/27/2021) REMOVED CORRODED LOWER ATTACH HARDWARE RIGHT SPOILERON INBOARD AND OUTBOARD PCUS REF CRJ 200 AMM 27-62-01-000-801 AND INSTALLED NEW HARDWARE REF CRJ 200 AMM 27-62-01-400-801. OPERATIONAL TEST GOOD REF CRJ 200 AMM 27-64-00-710-801.

Part: HINGE — CORRODED (LT SPOILERON) · airframe 38,563 hrs · 35,916 cycles

* LH SPOILERON HINGE HARDWARE IS CORRODED (C-CHECK RO 7/27/2021) REMOVED AND REPLACED 4 BOLTS, 4 NUTS, 12 WASHERS AND 4 COTTER PINS ON LH SPOILERON HINGE. REF. CRJ200 AMM 26-64-01-000-801 AND CRJ200 AMM 27-64-01-400-801 CALIBRATED TOOL USED TUC5659 CAL DUE 28 FEB 22

Part: RIB — CRACKED (RT WING) · airframe 38,563 hrs · 35,916 cycles

*R/H BATT RIB WEB CRACKED AT UPPER FASTENERS WS53.60 (C-CHECK RO 7/27/2021) REMOVED DAMAGED R/H BATT RIB. REPLACED AND INSTALLED NEW BATT RIB P/N 601R10203-28 AT WS53.60 REF. CRJ200 SRM 51-42-21, AND DWG 601R10203 REV -G. COMPLIED WITH TASK CARD 51-900-1003-SKY

Part: FRAME — BENT (BS 700 S1L-R) · airframe 38,563 hrs · 35,916 cycles

* AFT EQUIPMENT BAY FS700.00 FRAME BENT BETWEEN STGR 1L & STGR 1R (MARKED) (C-CHECK RO 7/27/2021) HAND DRESSED FS700.00 FRAME LWR LIP TO ORIGINAL CONTOUR AND INSTALLED REINFORCEMENT REPAIR ANGLE. REO 601R-53-61-7661 REV -- DATED 2021-06-21. COMPLIED WITH TASK CARD 51-900-1003-SKY.

Part: ANGLE — CRACKED (LT WING) · airframe 38,563 hrs · 35,916 cycles

* L/H WING CAP ATTACHED TO LOWER SIDE OF UPPER WING SKIN AT WS 48.30 CRACKED (C-CHECK RO 7/27/2021) REMOVED AND INSTALLED NEW LH WING CAP ATTACHED AT LOWER SIDE OF UPPER WING SKIN AT WS4.830 REF CRJ 200 SRM 51-42-21 AND BOMBARDIER DWG 601R10204 REV J COMPLIED WITH 51-900-1003-SKY, COMPLETED FORM M-337. SEE CONTINUATION CARD FOR DETAILS.

Part: ATTACH ANGLE — CRACKED (RT WING) · airframe 38,563 hrs · 35,916 cycles

* R/H WING ANGLE ATTACHED TO LOWER SIDE OF UPPER WING SKIN AT WS48.30 CRACKED. (C-CHECK RO 7/27/2021) REMOVED DAMAGED ANGLE, REPLACED AND INSTALLED NEW ANGLE P/N 600-10204-28 REF. CRJ200 SRM 51-42-21, CRJ200 SRM 51-42-06, AND DWG 600-10204 REV -M. COMPLIED WITH TASK CARD 51-900-1003-SKY

Part: BRACKET — CRACKED (LT MLG WW) · airframe 38,563 hrs · 35,916 cycles

* LH MLG WHEEL WELL BRACKET P/N 601R75262-159 IS CRACKED (MARKED) (C-CHECK RO 7/27/2021) REMOVED AND INSTALLED NEW BRACKET IN THE LH MLG WHEEL WELL. REF CRJ200 SRM 51-42-06 SEE CONTINUATION CARD FOR FURTHER DETAILS

Part: ATTACH ANGLE — CRACKED (LT WING) · airframe 38,563 hrs · 35,916 cycles

* L/H WING ANGLE ATTACHED TO LOWER SIDE OF UPPER WING SKIN AT WS48.30 CRACKED. (C-CHECK RO 7/27/2021) REMOVED AND INSTALLED NEW LH WING ANGLE ATTACHED TO UPPER SIDE OF WING SKIN AT WS48.3 REF CRJ 200 SRM 51-42-06 AND DWG 600-10204 REV M. COMPLIED WITH 51-900-1003-SKY, COMPLETED FORM M-337. SEE CONTINUATION CARD FOR DETAILS.

Part: ATTACH ANGLE — CRACKED (RT WING) · airframe 38,563 hrs · 35,916 cycles

* R/H WING CAP ANGLE ATTACHED TO LOWER SIDE OF UPPER WING SKIN AT WS48.30 CRACKED. (C-CHECK RO 7/27/2021) REMOVED DAMAGED CAP ANGLE, REPLACED AND INSTALLED NEW R/H WING CAP ANGLE P/N 600-10389-2 ATTACHED TO LOWER SIDE OF UPPER WING SKIN PANEL AT WS48.30 REF. CRJ200 SRM 51-42-06, CRJ200 SRM 51-42-21, AND DWG 601R10204 REV -J. COMPLIED WITH TASK CARD 51-900-1003-SKY.

Part: VANE — CHAFED (LT WING TE FLAP) · airframe 38,563 hrs · 35,916 cycles

LH INBOARD FLAP VANE REPAIR STRIP INBOARD SIDE IS CHAFED THROUGH (C-CHECK RO 7/27/2021) CHAFE DAMAGE IS 100% THROUGH REPAIR STRIP AND NO ALLOWABLE LIMITS PROVIDED FOR STRIP IN CRJ200 SRM CHAPTER 57. PER SKYWEST REQUEST REPLACE L/H FLAP VANE L/E SKIN INBD SIDE. / INSTALLED NEW L/H FLAP VANE L/E SKIN INBD SIDE PER CRJ200 SRM 51-42-13 AND DWG NO 601R14302 REV E / COMPLIED WITH TASK CARD 51-900-1003-SKY

Part: SKIN — CHAFED (LT AILERON) · airframe 38,563 hrs · 35,916 cycles

* LEFT SIDE AILERON UPPER LEADING EDGE SKIN IS CHAFFED ALONG ITS ENTIRE LENGTH. (C-CHECK RO 7/27/2021) REPLACED LEFT SIDE AILERON UPPER LEADING EDGE SKIN P/N 601R13031-165 REF CRJ 200 SRM 51-42-06 AND DWG 601R13031 REV K. REO 670-57-61-194 REV -C DATED 2019-01-07. COMPLIED WITH 51-900-1003-SKY

Part: HOUSING — CHAFED (DOOR HANDLE) · airframe 38,563 hrs · 35,916 cycles

* GALLEY SERVICE DOOR EXTERIOR HANDLE HOUSING HAS CHAFFES. (C-CHECK RO 7/27/2021) REPAIRED GALLEY SERVICE DOOR EXTERIOR HANDLE HOUSING PER BOMBARDIER REO 601R-52-41-235 REV -A 2017-06-07 AND MHIRJ REO 601R-52-41-468 REV -- 2021-06-11 / BLEND OUT OF DAMAGE ONLY, WEIGHT CHANGE NEGLIGIBLE. COMPLIED WITH TASK CARD 51-900-1003-SKY

Part: WEB — CRACKED (TRU BAY) · airframe 38,563 hrs · 35,916 cycles

* LEFT SIDE TRU BAY FLOOR WEB HAS SUSPECTED CRACK NEAR ACCUMULATOR PRESSURE GAUGES. (C-CHECK RO 7/27/2021) REPAIRED LEFT SIDE TRU BAY FLOOR WEB REF REO 601R-53-11-081 REV NC DATED 97-07-02. SEE CONTINUATION CARD FOR DETAILS. COMPLIED WITH 51-900-1003-SKY

Part: SKIN — DENTED (BS 265-295 S24R) · airframe 38,563 hrs · 35,916 cycles

ADM#N881AS-6539. 26 BLENDS FOUND ON LOWER FUSELAGE, FS265.00- FS295.00 STGR24R FOR REPAIR REFERENCE REO 601R-53-00-733 FOR MEASUREMENTS OF BLENDS. PERMANENT REPAIR REQUIRED AT C CHECK. (C-CHECK RO 7/27/2021) EVALUATED, HAND DRESSED 26 IDENTIFIED DENTS, RESTORED FINISH. REF REO 601R-51-00-309 REV -A DATED 2017-08-23. THE REWORKED CONDITION OF THE REMAINING DENT€™S DIMENSIONS IS STRUCTURALLY ACCEPTABLE FOR €Œ6000 FLIGHT HOURS€? FROM TIME OF INCORPORATION OF REO 601R-53-00-849 AT €ŒREV --€Œ PROVIDED IT IS VISUALLY INSPECTED FOR DAMAGE PROPAGATION AT INTERVALS THAT DO NOT EXCEED €Œ600 FLIGHT HOURS€?. REF REO 601R-53-00-849 REV -- DATED 2021-07-20 & REO 601R-53-00-733 REV -- DATED 2019-06-24. COMPLIED WITH TASK CARD 51-900-1003-SKY

Part: ACM — WEAK (LEFT) · airframe 36,145 hrs · 33,840 cycles

THE CREW REPORTED STRONG ODOR OF FUEL FROM LEFT PACK WITH BLEEDS ON ENGINE OR APU. APPEARS TO BE STRONGER WITH LEFT PACK OUTPUT SET TO ABOVE 40 DEGRESS C. MAINTENANCE PLACED LEFT PACK ON MEL. SUPPLEMENT TO FOLLOW.

Part: FLOORBEAM — DAMAGED (BS 574) · airframe 36,104 hrs · 33,809 cycles

REF: CO# 7496618 JOB# 7749668 OP# 4: FOUND TWO ELONGATED HOLES NEAR F.S. 574.00 L/H SIDE. (1EA) HOLE ON INBD ANGLE OF FWD TIE DOWN AND ANOTHER ON THE FLOOR SUPPORT BEAM AT ANGLE ATTACHING POINT. HOLE ON ANGLE MEASURES .223" AND HOLE ON FLOOR SUPPORT BEAM MEASURES .273" BOTH HOLES SHOULD MEASURE .162" DIAMETER. C/A: REPAIRED DAMAGE I.A.W. STS ENGINEERING SOLUTIONS EA# 30-2018-313 REV.--, DATED 11/26/2018 AND EXPRESSJET EC/TC EA 30-2018-313 REV0, DATED 2018/11/27.

Part: BULKHEAD — DAMAGED (NOT REPORTED) · airframe 36,104 hrs · 33,809 cycles

REF: CO# 7496618 JOB# 7749663 OP# 1: REPAIR DAMAGE TO L/H SIDE 9G BULKHEAD AFT SIDE AT INSERT/RIVNUT LOCATIONS.C/A: REPAIRED DAMAGE I.A.W. BOMBARDIER EO# CL-600-2B19-53-L05913 DATED 11/21/2018 AND EXPRESSJET EC/TC EO# CL-600-2B19-53-L05913 REV.0, DATED 2018-11-26.

Part: BULKHEAD — DAMAGED (FUSELAGE) · airframe 36,104 hrs · 33,809 cycles

REPAIR DAMAGE TO CENTER 9G BULKHEAD AFT SIDE AT INSERT/RIVNUT LOCATIONS. REPAIRED DAMAGE IAW EO CL-600-2B19-53-L05914 DATED 11/21/2018 AND EC/TC EO CL-600-2B19-53-L05914 REV 0, DATED 2018-11-26.

Part: SKIN — CRACKED (RT WING) · airframe 36,104 hrs · 33,809 cycles

REF: CO# 7496618 JOB# 7749665 OP# 35: LOWER WING PLANK CUTOUT FOR R/H BOOST PUMP HAS AN INDICATION NOTED ON THE LOWER SURFACE OF THE WNG PLANK ON THE AFT SIDE OF CUT OUT. INDICATION IS .150" LONG BY 100% FSH. FAILED NDT INSPECTION.C/A: REPAIRED DAMAGE I.A.W. BOMBARDIER REO 601R-57-21-2581 REV.A, DATED 2018/11/29 AND EXPRESSJET EC/TC REO 601R-57-21-2581 REV.0, DATED 2018/11/30.

Part: SKIN — DENTED (BS 235-250) · airframe 36,103 hrs · 33,809 cycles

REF: CO# 7496618 JOB# 7749665 OP# 30: 2EA DENTS ON FUSELAGE SKIN BETWEEN F.S.235.00 AND F.S.250.00, STRINGER 24L AND STRINGER 25L.C/A: REPAIRED DAMAGE I.A.W. BOMBARDIER REO 601R-53-11-3352 REV.A, DATED 2018/11/29 AND EXPRESSJET EC/TC REO 601R-53-11-3352 REV.A, DATED 2018/11/30.

Part: BULKHEAD — DAMAGED (FUSELAGE) · airframe 36,104 hrs · 33,809 cycles

REPAIR DAMAGE TO RT 9G BULKHEAD AFT SIDE INSERT/RIVNUT LOCATIONS. REPAIRED DAMAGE IAW EO CL-600-2B19-53-L05915 DATED 11/21/2018 AND EC/TC EO CL-600-2B19-53-L05915.

Part: SKIN — DENTED (LT WING TE FLAP) · airframe 36,104 hrs · 33,809 cycles

REF: CO# 7496618 JOB# 7749661 OP# 28: DENT ON L/H INBOARD FLAP, LOWER SURFACE APPROX. 3.50" FROM INBOARD EDGE AND 1.00" FROM TRAILING EDGE. .500" IN DIAMETER, .020" DEEP. C/A: REPAIRED DAMAGE I.A.W. BOMBARDIER CRJ200 SRM 57-20-00, REPAIR #3 - INBOARD FLAP AND VANE- REPAIR NO.3- NON-FLUSH REPAIR TO INBOARD FLAP SKIN- , REV. 36, DATED MAY 10/2017.

Part: WIRE HARNESS — DEFECTIVE (NLG) · airframe 35,362 hrs · 32,977 cycles

GEAR DISAGREE ON CLIMB OUT JUST PRIOR TO FL180. NOSE GEAR POSITION INDICATION MISSING (HASHED OUT). BTMS CAME UP ALSO. LASTED FOR 10 SECONDS AND WARNING AND GEAR INDICATIONS WENT AWAY. SHORTLY AFTER, THE GEAR INDICATION CAME UP AGAIN WITH A MISSING NOSE GEAR INDICATION BUT NO GEAR DISAGREE. DID NOT HEAR OR FEEL ANY WIND RESISTANCE INDICATING THE NOSE DOOR/GEAR WAS OPEN OR DOWN. (FLT 3569) CLOSED REMOVED AND REPLACED NLG DOWN LOCK HARNESS NR 2 IAW AMM. PERFORMED GEAR SWING WING NO FAULTS NOTED.

Part: BULKHEAD WEB — NO TEST (BS 621) · 31,182 cycles

FOUND REAR PRESSURE BULKHEAD WEB HAS 9 AREAS THAT FAILED NDT INSPECTION. REPAIRED THE PRESSURE BULKHEAD WEB.

Part: FLOOR SUPPORT — CORRODED (BS 570-621) · 31,182 cycles

CARGO BAY FLOOR SUPPORT AT BS 570 - 621, LBL 27 CORRODED. REMOVED AND REPLACED THE FLOOR SUPPORT IAW REO.

Part: CARGO TRACK — CORRODED (BS 559-570) · 31,182 cycles

CARGO TRACK AT RBL 9 BETWEEN BS 559+80 AND 570 CORRODED. REMOVED AND REPLACED IAW AMM.

Part: FLOOR SUPPORT — CORRODED (NOT REPORTED) · 31,182 cycles

CARGO BAY FLOOR SUPPORT AT LBL 9 CORRODED. REMOVED AND REPLACED THE FLOOR SUPPORT IAW REO.

Part: SKIN — DENTED (RT WING TE FLAP) · 31,182 cycles

RIGHT INBD FLAP UPPER SKIN DENTED. REPAIRED THE FLAP SKIN IAW SRM.

Part: LIGHT — BROKEN (CABIN) · airframe 32,372 hrs · 29,647 cycles

ON ENTERING ACFT, FOUND WHITE EMERGENCY EXIT LIGHT, DETACHED FROM BULKHEAD. REMOVED AND REPLACED THE LIGHT IAW AMM 33-51-19. OPS CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (FLASHLIGHT) · airframe 29,855 hrs · 26,954 cycles

F/A FLASHLIGHT INOPERATIVE. REPLACED BATTERIES IN FLASHLIGHT IAW 25-60-00.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHTS) · airframe 29,824 hrs · 26,919 cycles

EMERGENCY LIGHT AT THE RT EXIT, LEFT OF SERVICE DOOR, IS INOPERATIVE. FOUND THE CONNECTORS IMPROPERLY SEATED. RESEATED THE CONNECTORS & THE EMERGENCY LIGHT OPS TESTED GOOD IAW AMM 33-51-13-400-801 & AMM 33-51-00-710-801.

Part: ANGLE — CRACKED (BS 621) · airframe 29,824 hrs · 26,918 cycles

FS 621 LT OBLIQUE ANGLE IS CRACKED. R & R FS 621 LT OBLIQUE ANGLE, PN:601-35012-51 IAW SRM 51-40-11 AND 51-42-21.

Part: FLOOR SUPPORT — CORRODED (BS 442) · airframe 29,824 hrs · 26,918 cycles

LEFT CABIN PRESSURE FLOOR SILL IS CORRODED AROUND A NUTPLATE AT FS 442.00. BLENDED AREA ON LT SIDE CABIN FLOOR SILL AT FS 424 IAW SRM 51-21-06. REMOVED .007 OF MATERIAL. FOUND TO BE OUT OF LIMITS IAW SRM 53-41-45. C/W EC/TC REO:601R-53-41-666 AND REO:601R-53-41-666, REV C, DATED 11/06-2012 AS WRITTEN.

Part: ISOLATOR — BROKEN (BS 621 BULKHEAD) · airframe 29,824 hrs · 26,918 cycles

MULTIPLE BROKEN ISOLATORS ON FS 621.00 BULKHEAD. R & R 7 EA ISOLATORS ON FS 621.00 BULKHEAD IAW SRM 51-42-06.

Part: FRAME — CORRODED (BS 349) · airframe 29,824 hrs · 26,918 cycles

FS 349, FRAME, LOWER FLANGES CORRODED 26L-26R. FOUND FS 349 TO BE OUT OF LIMITS IAW SRM 53-00-00, TR 53-27. REMOVED FS 349 LOWER FRAME SEGMENT IAW SRM 51-42-06 AND 51-42-21. INSTALLED NEW SERVICEABLE FS 349 LOWER FRAME SECTOR IAW SRM 51-42-06, 51-42-21 AND SRM TR 51-32.

Part: FRAME — CORRODED (BS 333) · airframe 29,824 hrs · 26,918 cycles

FS 333 FRAME IS CORRODED BETWEEN STR 26L AND 26R. REMOVED FS 333 FLOORBOARD SUPPORT ASSY TO FOM IAW SRM 51-42-06. INSTALLED SERVICEABLE FS 333 FLOOR SUPPORT ASSY IAW SRM 51-42-06. REMOVED CORRODED FRAME SEGMENT AT FS 333 IAW SRM 51-42-06 AND 51-42-21. INSTALLED NEW FS 333 FRAME SEGMENT IAW SRM 51-42-06, 51-42-21 AND 51-77-00. PAINTED REPAIR IAW SRM 51-25-01 AND APPLIED CORROSION INHIBITING COMPOUND IAW MM 51-25-56-390-802.

Part: SEAT TRACK — CORRODED (BS 409-559) · airframe 29,824 hrs · 26,918 cycles

SEAT TRACK CORRODED LBL BS 409+122 TO 559+80. REMOVED SEAT TRACK IAW SRM 51-41-02. LOCATED AND DRILLED NEW SERVICEABLE FLOOR SEAT TRACK IAW REO 601R-53-00-485, STEPS 1-4. AND REPLACED WITH NEW FABRICATED SEAT TRACK IAW REO 601R-53-00-485.

Part: INTERCOSTAL — CORRODED (BS 364-656) · airframe 29,824 hrs · 26,918 cycles

LATCH PIN INTERCOSTAL BETWEEN STR 27 AND STR 26L IS CORRODED ON LOWER FLANGE JUST FWD OF FS 364 AND AT ABOUT FS 356. REMOVED INTERCOSTAL BETWEEN STR 27 AND STR 26L IAW SRM 51-42-06 AND 51-42-21. LOCATED AND DRILLED NEW SERVICEABLE INTERCOSTAL BETWEEN STR 27 AND STR 26L IAW SRM 51-40-11 AND INSTALLED INTERCOSTAL IAW SRM 51-42-06 AND 51-42-21 AND TR 51-32. FOUND INTERCOSTAL BETWEEN STR 27 AND STR 26L TO BE OUT OF LIMITS IAW SRM 53-00-00, TR 53-27.

Part: INTERCOSTAL — CORRODED (BS 364) · airframe 29,824 hrs · 26,918 cycles

INTERCOSTAL FWD OF FS 364 AND RT OF STR 27 IS CORRODED ON LOWER FLANGE LATCH PIN. FOUND ITERCOSTAL FORWARD OF FS 364, RT OF STR 27 TO BE OUT OF LIMITS IAW SRM 53-00-00, TR 53-27. REMOVED INTERCOSTAL FORWARD OF FS 364 RT OF STR 27 IAW SRM 51-42-06 AND 51-42-21. LOCATED, DRILLED NEW SERVICEABLE INTERCOSTAL AT STR 27 AND STR 26R IAW SRM 51-40-11 AND INSTALLED INTERCOSTAL IAW SRM 51-42-06 AND 51-42-21 AND TR 51-32.

Part: BULKHEAD WEB — CRACKED (BS 621) · airframe 29,824 hrs · 26,919 cycles

FOUND REAR PRESSURE BULKHEAD WEB HAS INDICATIONS NOTED AT BL 0.0 BETWEEN WL 128 TO WL 134 APPROX 5" IN LENGTH 50 PERCENT FSH. FAILED NDT INSPECTION. COMPLIED WITH REO 601R-53-61-5456, REV, DATED 2015/03/17 IN IT'S ENTIRETY. COMPLIED WITH EC/TC REO 601R-53-61-1285 AND GREO 601R-53-61-1285, REV D DATED 10/31/2011 AS WRITTEN. REO 601R-53-61-5456, REV HAS BEEN ACCOMPLISHED AND ALL STEPS HAVE BEEN DOCUMENTED AND SIGNED FOR ON A NON-ROUTINE WORK CARD.

Part: BRACKET — CORRODED (BS 319-349) · airframe 29,824 hrs · 26,918 cycles

SERVICE DOOR LOWER SILL JOINT BRACKETS AT FS 319.70 AND FS 349 ARE CORRODED. REMOVED SERVICE DOOR T-FITTING JOINT BRACKET AT FS 319.70 FOR REPLACEMENT IAW SRM 51-42-21. INSTALLED SERVICE DOOR T-FITTING JOINT BRACKET AT FS 349.00 IAW SRM 51-42-21. REMOVED SERVICE DOOR T-FITTING JOINT BRACKET AT S 349.00 FOR REPLACEMENT IAW SRM 51-42-21. INSTALLED SERVICE DOOR T-FITTING JOINT BRACKET AT FS 349.00 IAW SRM 51-42-21. REMOVED MID SERVICE DOOR THRESHOLD BRACKET FOR ACCESS IAW SRM 51-42-06. INSTALLED MID SERVICE DOOR THRESHOLD BRACKET IAW SRM 51-42-21.

Part: STRINGER — CRACKED (BS 379) · airframe 29,824 hrs · 26,919 cycles

FS 379, STRINGER 3L IS CRACKED AT ATTACHMENT TO PAX DOOR LINTEL. REMOVED FASTENERS IN REPAIR AREA OF STRINGER 3L IAW SRM 53-00-03. REINSTALLED REMOVED FASTENERS AT STR REPAIR AREA IAW SRM 53-00-03. CUT AND REMOVED STRINGER IN REPAIR AREA IAW SRM 53-00-03. SPLICED IN NEW STRINGER SECTION TO REPAIR DAMAGED STRIKER IAW SRM 53-00-03. COMPLIED WITH STR SPLICE REPAIR IN ITS ENTIRETY IAW SRM 53-00-03. COMPLIED WITH EC/TC EO 600-53-0755 AND SRM 53-00-03, FIG 202, SHEET 1, STRINGER SPLICE AS WRITTEN. C/W AMM 25-28-01-400-804.

Part: SKIN — CORRODED (BS 319-349) · airframe 29,824 hrs · 26,919 cycles

EXTERNAL FUSELAGE SKIN HAS SURFACE FILIFORM CORROSION UNDER SERVICE DOOR SCUFF PLATE FS 319.70 TO FS 349. REMOVED CORROSION FROM FUSELAGE SKIN UNDER SERVICE DOOR SCUFF PLATE BETWEEN FS 319.70 TO FS 349 MAX MATERIAL REMOVED .005 DAMAGE WAS WITHIN DEPTH LIMITS IAW SRM TR 53-33 BUT EXCEEDED THE 1.00 IN FROM FASTENER. C/W EA 12-2015-088 SECTION 1. STS ENGINEERING SOLUTIONS EA 12-2015-088, REV 1R HAS BEEN ACCOMPLISHED.

Part: BRACKET — CRACKED (BS 281) · airframe 29,824 hrs · 26,919 cycles

FS 281 ATTACHMENT BRACKET FROM PAX DOOR LINTEL TO FS 280 BULKHEAD IS CRACKED. REMOVED CRACKED BKT AT FS 280 AND STR 3L. AFTER FURTHER INVESTIGATION FOUND MATING BRACKET TO BE CRACKED IAW SRM 51-42-06. LOCATED, DRILLED AND INSTALLED, 2EA, BRACKET PN 600-31057-19 & -20 IAW SRM 51-42-06, 51-40-06 & 51-40-11.

Part: FLOOR SUPPORT — CORRODED (BS 349-364) · airframe 29,824 hrs · 26,919 cycles

SERVICE DOOR AFT FLOOR SILL IS CORRODED FROM FS 349 TO FS 364. COMPLIED WITH REO 601R-53-21-2064.

Part: SKIN — CRACKED (RT WING) · airframe 29,824 hrs · 26,919 cycles

LOWER WING RT BOOST PUMP CUTOUT FOR PANEL 610CB HAS MULTIPLE INDICATIONS NOTED ON VERTICAL SURFACE GREATER THAN 50 PERCENT FSH AROUND ENTIRE CIRCUMFERENCE. FAILED NDT INSP. NOTED PITTING AT RT LOWER WING BOOST PUMP CUTOUT. BLENDED PITT CORROSION AT RT LOWER WING BOOST PUMP CUTOUT FOR PANEL 610CB IAW SRM 51-21-16. REMOVED APPROX .007 TO .009 MATERIAL. PERFORMED VISUAL AND BLENDED RT BOOST PUMP LANDING SMOOTH IAW STS EA 32-2015-092. TRIMMED RT BOOST PUMP COVER, PN 601R62182-13 IAW STS EA 32-2015-092. COMPLIED WITH STS EA 32-2015-092. EA 32-2015-092 REV A HAS BEEN ACCOMPLISHED.

Part: SEAT TRACK — CORRODED (BS 349-364) · airframe 29,824 hrs · 26,919 cycles

LT SIDE SEAT RAIL RETAINER BETWEEN FS 349 AND FS 364 IS CORRODED. REMOVED CORROSION AT FS 349 LT SIDE SEAT RAIL RETAINER IAW SRM 51-21-06, MATERIAL REMOVED .008, ORIGINAL THICKNESS .040 2024-T42 CLAD. DAMAGE ALLOWANCE IAW TEMPORARY REVISION 53-27, PG 106 OF SRM. FOUND OUT OF LIMITS. C/W STS EA 12-2015-093. REPAIRED IAW STS ENGINEERING SOLUTIONS EA 12-2015-093 REV 1R.

Part: SKIN — CRACKED (RT WING) · airframe 29,824 hrs · 26,919 cycles

RT WING LOWER WING PLANK IS CRACKED AT WS 148.019 RHS. REO 601R-58-21-2311, REV HAS BEEN ACCOMPLISHED AND ALL STEPS HAVE BEEN DOCUMENTED AND SIGNED FOR ON A NON-ROUTINE WORK CARD.

Part: WIRE — OUT OF POSITION (EMERGENCY LIGHTS) · airframe 28,775 hrs · 25,898 cycles

BETA LIGHT AT ASD, BETA LIGHT AT SERVICE DOOR AND EXIT LIGHT AT SERVICE DOOR INOPERATIVE. FOUND POWER SUPPLY WIRES SWAPPED, INSTALLED POWER SUPPLY WIRES CORRECTLY IAW AMM-33-51-09, OPS CHECKS GOOD, NO DEFECTS NOTED.

Part: SIGN — INOPERATIVE (EMERGENCY LIGHTS) · airframe 28,659 hrs · 25,773 cycles

FWD BULKHEAD NEAR PASSENGER DOOR EXIT SIGN INOPERATIVE. R & R FWD BULKHEAD NEAR PASSENGER DOOR EXIT SIGN ASSY IAW AMM 33-51-10. COMPLIED WITH EMERGENCY LIGHT, OPS TEST IAW AMM 33-51-00. OPS CK GOOD.

Part: BRACKET — CRACKED (PAX DOOR) · airframe 27,417 hrs · 24,481 cycles

PAX DOOR CRACKED AT ASSIST PULLEY BRACKET ON AFT FRAME UNDER INNER SKIN. REPAIRED IAW REO IAW 601R-52-11-2194.

Part: ANCHOR FITTING — CRACKED · airframe 27,417 hrs · 24,481 cycles

AFT ANCHOR FITTING CRACKED IN TWO PLACES. REPAIRED IAW 601R-52-116 01.

Part: STRUCTURE — CRACKED (PAX DOOR) · airframe 27,417 hrs · 24,481 cycles

ASD HAS CRACK NEAR POWER ASSIST PULLEY BRACKET. CUT OUT DAMAGE & REPAIRED IAW 601R-52-11-2194.

Part: SKIN — DAMAGED (RT WING) · airframe 26,067 hrs · 23,075 cycles

FOUND AN OVERSIZED HOLE ON LOWER WING PANEL AT WS 65.75 RT SIDE. REPAIRED IAW REO 601R-57-21-1884 & NDTM PT 6 53-00-097. MAJOR REPAIR.

Part: BULKHEAD — CRACKED (BS 621) · airframe 26,067 hrs · 23,075 cycles

FS 621 BULKHEAD FWD FACE FAILS NDT. REPAIRED IAW REO 601R-53-61-1541 REV D.

Part: BRACKET — CRACKED (WINDSHIELD) · airframe 26,067 hrs · 23,075 cycles

WINDSHIELD POST AT BL 0.0 RT SIDE BRACKET IS CRACKED IN RADIUS APPROX .250L. REMOVED CRACKED WINDSHIELD POST BRACKET RT SIDE IAW SRM 51-42-21. LOCATED & DRILLED NEW SERVICEABLE WINDSHIELD POST RT BRACKET IAW SRM 51-40-11. INSTALLED NEW SERVICEABLE WINDSHIELD POST LOWER RT BRACKET IAW SRM 51-42-21.

Part: POST — CRACKED (BS 409) · airframe 26,067 hrs · 23,075 cycles

RBL 18.0 FS 409.0+128 VERTICAL POST OTBD SIDE HAS A CRACK INDICATION NOTED AT WL 69.0 IN THE AFT FLANGE RADIUS, APPROX .4" X 50 PERCENT FSH FAILED NDT. REMOVED VERTICAL POST AND LOCATED AND DRILLED NEW VERTICAL POST IAW SRM 51-40-11. INSTALLED POST IAW REO 601R-53-41-889 STEPS 1 THRU 4.

Part: ISOLATOR — BROKEN (BULKHEAD) · airframe 26,067 hrs · 23,075 cycles

REAR PRESSURE BULKHEAD FWD FACE HAS BROKEN ISOLATOR. R & R BROKEN ISOLATOR AT REAR PRESSURE BULKHEAD IAW SRM 51-42-13.

Part: ANGLE — CRACKED (BS 621-625) · airframe 26,067 hrs · 23,075 cycles

FS 621-625 OBLIQUE ANGLE CRACKED. REMOVED OBLIQUE ANGLE. FIT, DRILLED & INSTALLED NEW ANGLE IAW SRM 51-42-21.

Part: FITTING — CRACKED (COCKPIT WIDOW) · airframe 26,067 hrs · 23,075 cycles

CO-PILOT'S WINDSHIELD SIDE POST LOWER AFT FITTING IS CRACKED. R & R FITTING IAW SRM 51-42-21.

Part: FITTING — CRACKED (COCKPIT WINDOW) · airframe 26,067 hrs · 23,075 cycles

PILOT'S WINDSHIELD SIDE POST LOWER AFT FITTING CRACKED. R & R FITTING IAW SRM 51-42-21.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 26,067 hrs · 23,075 cycles

FS 280.00 ANGLE INBD OF LBL 9.0 IS CRACKED. REMOVED INBD LBL 9 FS 280 ANGLE IAW SRM 51-42-21. REPLACED WITH NEW SERVICEABLE ANGLE AT FS 280 LBL 9.0 IAW SRM 51-42-21 INBD SIDE OF FLOORBEAM AT LBL 9.0.

Part: ANGLE — CRACKED (BS 280) · airframe 26,067 hrs · 23,075 cycles

FS 280.00 TWO ANGLES INBD AND OTBD OF RBL 9.0 CRACKED. REMOVED INBD AND OTBD RBL 9, FS 280 ANGLES IAW SRM 51-42-21. INSTALLED NEW SERVICEABLE OTBD RBL 9, FS 280 ANGLES IAW SRM 51-42-21.

Part: SEAT TRACK — CORRODED (BS 399.5-409) · airframe 26,067 hrs · 23,075 cycles

SEAT TRACK FROM FS 399.5 TO FS 409+128 CORRODED. REMOVED SEAT TRACK IAW SRM 51-41-02. FABRICATED SEAT TRACK IAW GREO 601R-53-00-485. INSTALLED SEAT TRACK IAW SRM 51-41-02.

Part: LAMP — BURNED OUT (CABIN) · airframe 25,508 hrs · 22,466 cycles

AFT MOST CEILING EMERGENCY LIGHT INOPERATIVE. LAMPED EMERGENCY FLOOD LIGHT. OPS CHECKED GOOD.

Part: PLACARD — DETERIORATED (CABIN) · airframe 23,694 hrs · 20,537 cycles

PAX DOOR OPEN AND EXIT PLACARD DETERIORATED. R & R PAX DOOR OPEN AND EXIT PLACARDS IAW AMM 11-30-00. R & R PAX DOOR OPEN AND EXIT PLACARDS IAW AMM 11-30-00.

Part: INVERTER — FAILED (EMERGENCY LIGHTS) · airframe 23,458 hrs · 20,270 cycles

RT OVERWING EXIT HAS AN EXIT SIGN INOPERATIVE. REMOVED THE EMERGENCY LIGHT INVERTER AND INSTALLED A NEW INVERTER IAW AMM 33-51-07.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 23,061 hrs · 19,829 cycles

RT EXTERIOR EMERGENCY LIGHT NR2 POSITION IS OUT. RELAMPED RT EXTERIOR EMERGENCY LIGHT NR 2 POSITION IAW AMM 33-51-21, OPS CHECK GOOD.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 22,208 hrs · 18,884 cycles

EXTERNAL EMERGENCY LIGHT NOT WORKING ON FWD OF THE RIGH OVERWING EXIT. REPLACED BULB WITH SERVICEABLE BULB PN 1317 AND REINSTALLED SAME SERVICEABLE LENS ON EXTERNAL EMER LIGHT FWD OF RT OVERWING EXIT IAW AMM 33-51-21-400-801. PERFORMED THE OPERATION TEST OF THE EMER LIGHTS IAW AMM 33-51-00-710-801. OPS TEST GOOD AT THIS TIME.

Part: FLOORBEAM — CORRODED (BS 621-574) · airframe 22,183 hrs · 18,858 cycles

FLOORBEAM AT LBL 27, FS 621 TO FS 574 HAS CORROSION AROUND FASTENER HOLES. WHILE COMPLYING WITH LT ELEV CONTROL CABLE RIG FOUND RT ELEV FUSE CABLE TENSIONS LOW. RETENSIONED RT ELEV CONTROL CABLES IN FUSE IAW AMM 27-31-00-830-808.

Part: SILL — CRACKED (BS 589) · airframe 22,183 hrs · 18,858 cycles

ANGLE UNDER CARGO FLOOR DOOR SILL AT FS 589 IS CRACKED. REPLACED & INSTALLED A NEW ANGLE IAW SRM 51-42-21. THIS REPAIR REQUIRES MINOR/MAJOR CLASSIFICATION. THIS REPAIR IS CLASSIFIED AS A MINOR REPAIR.

Part: DOUBLER — CORRODED (DOOR FRAME) · airframe 22,183 hrs · 18,858 cycles

LOWER DOOR FRAME DOUBLER AT FS 319.70 AND FS 349.00, RBL 42 SHOWS EVIDENCE OF CORROSION. REO 601R-53-21-1261 HAS BEEN ACCOMPLISHED AND ALL STEPS HAVE BEEN DOCUMENTED AND SIGNED FOR ON A NON-ROUTINE WORKCARD. ALL RII'S HAVE BEEN ACCOMPLISHED BY A TRAINED, QUALIFIED, AND AUTHORIZED RII INSPECTOR IAW GMM 3-3 PROCEDURES PRIOR TO THE ACFT BEING RETURNED TO SERVICE. RII FOUND TO BE SATISFACTORY: 5300083 3/27/11". (CLOSED)

Part: FLOORBEAM — CORRODED (BS 349) · airframe 22,183 hrs · 18,858 cycles

FLOORBEAM & CAP ARE CORRODED AT FS 349 BETWEEN RBL 27 & 45. REPAIRED IAW REO 601R-53-21-1262.

Part: ANGLE — CORRODED · airframe 22,183 hrs · 18,858 cycles

PASSENGER DOOR SILL AND SILL ANGLE ARE CORRODED BETWEEN FS 319.0 AND 349.0, SAFETIED AND OPS TEST OF THE PAX DOOR WARNING SYS IS GOOD IAW AMM 52-70-04-710-803. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW SOP.

Part: POST — CRACKED (BS 409) · airframe 22,183 hrs · 18,858 cycles

FOUND FS 409.0+128 VERT POST BL 0.0 HAS INDICATIONS NOTED AT WL 69.0 AFT FLANGE RADIUS LT SIDE INDICATION NOTED APPROX .2" IN LENGTH 50 PERCENT FSH AND RT SIDE INDICATION NOTED APPROX .2" IN LENGTH 50 PERCENT FSH. BOTH POST FAILED NDT INSP. REMOVED VERT POST (2 EA) AT FS 409+128, BL 0.0 IAW SRM 51-42-06 & 51-42-21. LOCATED, DRILLED & DEBURRED NEW POST (2 EA) AT FS 409+128 BL 0.0 IAW SRM 51-40-11. POST AT FS 409+128 BL 0.0 REQUIRES INSTALLATION. INSTALLED NEW SERVICEABLE 409+128 BL 0.0 POST IAW SRM 51-42-06 AND STEPS 1 THRU 5 OF EC/TC REO 601R-53-41-889. C/W EC/TC REO 601R-53-41-889 AND MET ALL THE REQUIREMENTS OF REO 601R-53-41-889, REV A RII FOUND TO BE SATISFACTORY C/W 5300044. (CLOSED)

Part: SILL — CORRODED (FUSELAGE) · airframe 22,183 hrs · 18,858 cycles

PAX DOOR SILL AND SILL ANGLE ARE CORRODED BETWEEN FS 319.0 & FS 349.0. REMOVED LIGHT SURFACE CORROSION FROM SILL IAW SRM 51-21-06. ORIGINAL MAT'L 0.100"", MAT'L REMOVED 0.005"", MAT'L REMAINING 0.095"", MAT'L REMOVED WITHIN LIMITS SRM 51-00-00.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 22,183 hrs · 18,858 cycles

CARGO SEAT TRACK CORRODED LBL 9 . R & R CARGO SEAT TRACK IAW AMM 20-21-00-910-801.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 22,183 hrs · 18,858 cycles

FLOOR SUPPORT CLIP AT FS 280 LBL 9 OTBD SIDE IS CRACKED APPROX .500". REMOVED AND INSTALLED FLOOR SUPPORT CLIP AT FS 280 LBL 9 OTBD SIDE IAW SRM 51-42-21. REPAIR CLASSIFIED AS MINOR.

Part: FLOOR SUPPORT — CORRODED (BS 574-621) · airframe 22,183 hrs · 18,858 cycles

FLOOR SUPPORT AT LBL 27, FS 621 TO FS 574, HAS CORROSION AROUND FASTENER HOLES. COMPLIED WITH EC/TC REO 601R-53-61-3778 AND REO 601R-53-61-3778.

Part: UNKNOWN — CORRODED (BS 559) · airframe 22,183 hrs · 18,858 cycles

CORROSION ON RBL 9 AT FS 559+96 FLOORBEAM. TRIMMED OUT FLOORBEAM IAW SRM 53-00-43, PG 201. PERFORMED EDDY CURRENT INSPECTION, NO INDICATIONS FOUND. FABRICATED AND INSTALLED FLOORBEAM REPAIR IAW SRM 53-00-43.

Part: FLOORBEAM — CORRODED (BS 349) · airframe 22,183 hrs · 18,858 cycles

FLOORBEAM & CAP ARE CORRODED FS 349 BETWEEN LBL 27 AND LBL 45. REMOVED CORROSION IAW SRM 51-21-06. MATERIAL REMOVED WAS .003" TO .004", NOT EXCEEDING 10 PERCENT IAW SRM 53-00-00, FIG 102. TREATED, PRIMED & PAINTED AERA IAW SRM 51-21-11. CLASSIFIED AS A MINOR REPAIR.

Part: BRACKET — CORRODED (BS 349) · airframe 22,183 hrs · 18,858 cycles

LOWER FRAME BRACKET AT STA 349.00 RBL 42 SHOWS EVIDENCE OF CORROSION. REPAIRED IAW SRM 51-42-21. REPAIR CLASSIFIED AS MINOR.

Part: FLOORBEAM — CORRODED (BS 349) · airframe 22,183 hrs · 18,858 cycles

FLOORBEAM & CAP ARE CORRODED AT FS 349 BETWEEN RBL 27 & RBL 45. FOUND OUT OF LIMITS IAW SRM 53-00-00, FIG 101, SHT 3. REPAIRED IAW REO 601R-53-21-1262.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 22,183 hrs · 18,858 cycles

FLOOR SUPPORT CLIP AT FS 280 RBL 9 OTBD SIDE IS CRACKED. R & R NEW FLOOR SUPPORT CLIP AT FS 280 RBL 9 OTBD SIDE IAW SRM 51-42-21. THIS REPAIR REQUIRES MAJOR/MINOR CLASSIFICATION IAW ASA SOP 5702. THIS REPAIR IS CLASSIFIED AS A MINOR REPAIR IAW ASA SOP 5702. (CLOSED)

Part: DOUBLER — CORRODED (BS 319-349) · airframe 22,183 hrs · 18,858 cycles

LOWER DOOR FRAME DOUBLER AT FS 319.70 AND FS 349.00 RBL 42 SHOWS EVIDENCE OF CORROSION. INSPECTED LOWER DOOR FRAME DOUBLER FORWARD AND AFT UPPER TABS AND FOUND CORROSION TO BE APPROX .003 DEEP. BLENDED UNIFORMALLY ACROSS ENTIRE FACE OF UPPER TABS NOT MORE THAN .004 DEEP MAX. COMPLIED WITH STEPS 1, 2 & 3 OF REO 601R-53-21-1261. PERFORMED EDDY CURRENT IAW NDTM 51-20-06. NO INDICATIONS NOTED.

Part: SILL — CORRODED (BS 409-559) · airframe 22,183 hrs · 18,858 cycles

RT PRESSURE FLOOR SILL AND SILL ANGLES HAVE CORROSION BETWEEN FS 409+128 AND FS 559.0. ACCOMPLISHED STEP 1 OF REO 601R-53-41-1391 IAW REO 601R-53-41-1391 DID NOT EXCEED MAX REPORTED DEPTH IAW REO 601R-53-41-1391. COMPLIED WITH STEP 2 OF REO. PERFORMED NDT. NO INDICATONS NOTED.

Part: SILL — CORRODED (BS 409) · airframe 22,183 hrs · 18,858 cycles

LEFT PRESSURE FLOOR SILL AND ALL ANGLES HAVE CORROSION BETWEEN FS 409+128 AND FS 559.0. ACCOMPLISHED STEP 1 OF REO 601R-53-41-1391 IAW REO 601R-53-41-1391. DID NOT EXCEED MAX. REPORTED DEPTHS IAW REO 601R-53-41-1391. COMPLIED WITH STEP 2 OF REO NDT REPAIRED AREAS. NO INDICATIONS NOTICED.

Part: FLOOR SUPPORT — CRACKED (BS 484) · airframe 22,183 hrs · 18,858 cycles

FS 484, FLOORBEAM ANGLE ON THE OTBD SIDE OF PRESSURE FLOORBEAM LBL 27 IS CRACKED. REMOVED ANGLE IAW SRM 51-42-21. INSTALLED NEW ANGLE IAW SRM 51-42-21. REPAIR CLASSIFIED AS MINOR.

Part: ISOLATOR — BROKEN (BS 621 BULKHEAD) · airframe 22,183 hrs · 18,858 cycles

ISOLATOR BROKEN ON FWD FACE OF 621 BULKHEAD APPROX 20" ABOVE FLOOR AT LBL 9 AND RBL 9. R & R ISOLATOR FWD FACE 621 BULKHEAD LBL 9 AND RBL 9 IAW SRM 51-42-06. THIS REPAIR IS CLASSIFIED AS A MINOR REPAIR IAW SOP 5702.

Part: FLOOR SUPPORT — CORRODED (BS 310-319) · airframe 22,183 hrs · 18,858 cycles

RT FLOOR SILL STRUCTURE IS CORRODED FS 310-319 AND FLOOR SUPPORT TIE FITTING AT FS 319. REMOVED RT FLOOR SILL STRUCTURE FS 310.0-319.0 IAW SRM 51-42-06. INSTALLED NEW RT FLOOR SILL STRUCTURE PN 601R38303-225 IAW SRM 51-42-06.

Part: FLOOR SUPPORT — CRACKED (BS 484) · airframe 22,183 hrs · 18,858 cycles

FS 484 FLOORBEAM ANGLE ON THE OTBD SIDE OF PRESSURE FLOORBEAM RBL 27 IS CRACKED. INSTALLED NEW ANGLE AT FS 484, RBL 27 IAW SRM 51-42-21. REPAIR CLASSIFIED AS MINOR.

Part: SEAT TRACK — CORRODED (BS 364) · airframe 22,183 hrs · 18,858 cycles

SEAT TRACK AT LBL 9 BETWEEN FS 364.00 CORRODED ON FWD END. FOUND OUT OF LIMITS IAW SRM 53-21-49. SEAT TRACKS AT LBL 9 AND RBL BETWEEN FS 364 AND FS 399.55 ARE AND REQUIRE REPLACEMENT. REPLACE SEAT TRACKS AT LBL 9 AND RBL 9 BETWEEN FS 364 AND FS 399.5. REPLACED SEAT TRACK IAW SRM 51-41-04. REPAIR CLASSIFIED AS A MINOR REPAIR.

Part: BRACKET — CORRODED (BS 319) · airframe 22,183 hrs · 18,858 cycles

LOWER FRAME BRACKET AT FS 319.70 RBL 42, SHOWS HEAVY CORROSION. LOCATED NEW BRACKET IAW SRM 51-42-06, 51-42-21. INSTALLED IAW SRM 51-42-21. REPAIR CLASSIFIED AS MINOR.

Part: ANGLE — CRACKED (BS 621-625) · airframe 22,183 hrs · 18,858 cycles

RT 621-625 OBLIQUE ANGLE IS CRACKED. INSTALLED NEW SERVICEABLE 621-625 OBLIQUE ANGLE PN 601-35012-52 IAW SRM 51-42-21. THIS REPAIR REQUIRES MAJOR/MINOR CLASSIFICATION IAW SOP 5702. THIS REPAIR IS CLASSIFIED AS A MINOR REPAIR IAW SOP 5702.

Part: ANGLE — CRACKED (BS 621-625) · airframe 22,183 hrs · 18,858 cycles

LT 621-625 OBLIQUE ANGLE IS CRACKED. INSTALLED NEW SERVICEABLE 621-625 LT SIDE PN 601-35012-51 OBLIQUE ANGLE IAW SRM 51-42-21. THIS REPAIR IS CLASSIFIED AS A MINOR REPAIR IAW SOP 5702.

Part: FRAME — CRACKED (BS 700 S9R) · airframe 22,183 hrs · 18,858 cycles

FRAME IN AFT EQUIPMENT BAY AT FS 700 S9R IS CRACKED AT BOTTOM RIVET APPROX 1"L. REPAIRED FRAME IAW SRM 53-00-15, REPAIR NR 2 AND REO 601R-53-61-4017.

Part: BULKHEAD — CRACKED (BS 409) · airframe 21,632 hrs · 18,233 cycles

WHILE PERFORMING AWL2 53-41-124, FOUND A SUSPECT CRACK LOCATED AT FS 409+128 PRESSURE BULKHEAD FWD FACE COMING FROM LOWER EDGE OF THE INBD U CHANNEL AT LBL 27.00. CRACK GOES UP AND PAST FIRST LOWEST FASTENER HOLE (BUT NOT PAST THE NEXT FASTENER HOLE UP) THAT ATTACHES THE CHANNEL TO BULKHEAD WEB. WORK COMPLETED/ PERFORMED ET INSP OF SUSPECT CRACK AT FS 409+128 PRESSURE BULKHEAD FWD FACE COMING FROM LOWER EDGE OF THE INBD U CHANNEL AT LT BL 36.00 IAW NDTM PART 1, 51-20-06. REPAIRED CRACKED BULKHEAD POST AT FS 409+128 AT LBL 27 IAW EC/TC REO 601R-53-41-056 WO 176783.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 21,315 hrs · 17,866 cycles

BOTH CAPT & F/O FLASHLIGHTS INOP. REPLACED CAPT & F/O BATTERIES IN FLASHLIGHT AND OPS CHECK GOOD AS REQUIRED IAW AMM 25-60-01. ACFT OK FOR SERVICE. (CLOSED)

Part: COVER — MISSING (EMERGENCY LIGHTS) · airframe 21,289 hrs · 17,839 cycles

EMERGENCY EXIT AISLE ILLUMINATION LIGHT COVER, FELL OFF, RED BULB COVER MISSING. RE-LAMPED EXIT LIGHT IAW AMM 33-51-14 AND RE-SECURED CKS GOOD.

Part: WARNING LIGHT — ILLUMINATED · airframe 19,641 hrs · 15,976 cycles

L 14TH DUCT WARNING IN FLIGHT. RAN QRH. MESSAGE REMAINED THROUGH REMAINDER OF FLIGHT. [EMERGENCY DECLARED]

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 18,552 hrs · 14,906 cycles

GEAR DISAGREE UPON SELECTION OF GEAR UP. RAN QRH, LANDED UNEVENTFULLY. EMERGENCY DECLARED. A/C RETURNED TO ATL AFTER T/O.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 18,415 hrs · 14,787 cycles

JOB 8749615 OPERATION 96 / LT FS 718 CRACKED ABOVE AND BELOW STG 11.

Part: ANGLE — DAMAGED (FUSELAGE) · airframe 18,415 hrs · 14,787 cycles

JOB 8749615 OPERATION 133 / LT FS 559.0 CAP ANGLE HAS AN INDICATION NOTED AT LBL 18.0 APPROX .2 INCHES IN LENGTH 80 PERCENT FSH AND RT FS 559.0 WEB HAS AN INDICATION NOTED AT WL 58.70 APPROX .1 INCH IN LENGTH 25 PERCENT FSH FS 559.0. FAILED NDT INSPECTION. COMPLIED WITH REPAIR OF FS 559 PRESSURE BULKHEAD BETWEEN LBL 27 AND RBL 27 IAW REO 601R-53-41-260 AND DEVIATION PER REO 601R-53-41-875. COMPLIED WITH EC/TC REO 601R-53-41-260 REV.C.

Part: POST — DAMAGED (FUSELAGE) · airframe 18,415 hrs · 14,787 cycles

JOB 8749615 OPERATION 160 / RT FS 409.0+128 RBL 18 I/B VERTICAL POST AT WL 69.0 HAS A INDICATION NOTED APPROX .2 INCHES IN LENGTH 50 PERCENT FULL SCREEN HEIGHT FAILED NDT INSPECTION. REMOVED POST IAW SRM 51-42-06. FABRICATE NEW POST AND INSTALLED IAW SRM 51-24-21.

Part: POST — DAMAGED (FUSELAGE) · airframe 18,415 hrs · 14,787 cycles

JOB 8749615 OPERATION 162 / LT FS 409.0+128 LBL18 I/B VERTICAL POST AT WL 69.0 HAS AN INDICATION NOTED APPROX .2 INCHES IN LENGTH 60 PERCENT FULL SCREEN HEIGHT FAILED NDT INSPECTION. FABRICATED AND INSTALLED VERTICAL POST AS PER SAMPLE IAW SRM 51-24-16 AND DWG 601R32208.

Part: REPAIR — CRACKED (FUSELAGE) · airframe 18,415 hrs · 14,787 cycles

RIGHT FS 484 INTERCOSTAL CRACKED 1 INCH LONG UNDER CABIN FLOOR PANEL 262DRF. FABRICATED AND INSTALLED REPAIR ANGLE IAW REO 601R-53-41-059.

Part: REPAIR — CRACKED (FUSELAGE) · airframe 18,415 hrs · 14,787 cycles

JOB 8749611 OPERATION 245 / LEFT FS 484 FLOOR SUPPORT CRACKED 1 INCH LONG UNDER CABIN FLOOR PANEL 261DLF. FABRICATED AND INSTALLED REPAIR ANGLE IAW REO 601R-53-41-059.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 16,921 hrs · 13,427 cycles

EMERGENCY FLOOR TRACK LIGHTING AT 5CD INOP. REMOVED AND REPLACED EMERGENCY FLOOR TRACK LIGHTING AT 5CD IAW AMM 33-51-01. OPS CHECK GOOD. (B)

Part: HANDLE — CRACKED (PAX DOOR) · airframe 15,238 hrs · 12,014 cycles

MAIN PAX DOOR OUTER HANDLE CRACKED.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 15,142 hrs · 11,904 cycles

FS 621 PRESSURE WEB IS CRACKED AROUND LINTEL FITTING. REPAIRED FS 621 PRESSURE WEB AT LINTEL FITTING IAW REO 601R-53-61-1230; REO 601R-53-61-2312; AND ASA EC/TC REO 601R-53-61-2312; EC/TC REO 601R-53-61-1230.

Part: FITTING — CRACKED (FUSELAGE) · airframe 15,142 hrs · 11,904 cycles

FS 280 AT LBL 9 I/B & O/B CLIPS CRACKED. ALL WORK ACCOMPLISHED USING CRJ 200 SERIES SRM 51-21-11, 51-23-00, 51-24-16, 51-25-06, 51-25-16, 51-42-06, 51-42-13, 51-42-21, & 51-42-02.

Part: FITTING — CRACKED (FUSELAGE) · airframe 15,142 hrs · 11,904 cycles

FS 280 AT RBL 9 O/B CLIP CRACKED. REWORK ACCOMPLISHED USING CRJ 200 SERIES SRM 51-21-11, 51-23-00, 51-24-16, 51-25-16, 51-25-16, 51-42-21, & REO PL601R-53-11-926.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 15,142 hrs · 11,904 cycles

LEFT FS 621 TO FS 625 OBLIQUE ANGLE CRACKED. LOCATED AND DRILLED SERVICEABLE OBLIQUE ANGLE IAW CRJ 200 SRM 51-40-11.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 15,142 hrs · 11,904 cycles

RIGHT FS 621 TO FS 625 OBLIQUE ANGLE CRACKED. LOCATED AND DRILLED NEW OBLIQUE ANGLE PER CRJ 200 SRM 51-42-20, AND REO 601R-53-61-422.

Part: PLACARD — UNKNOWN (ESCAPE HATCH) · airframe 15,142 hrs · 11,904 cycles

EMERGENCY ESCAPE HATCH NEEDS THE FOLLOWING EXTERIOR PLACARDS EMERGENCY EXIT (INSTRUCTION PLACARD), OPEN PLACARD, ARROW INDICATION PLACARD AND CLOSED PLACARD.

Part: SUPPORT ANGLE — CRACKED (PAX DOOR) · airframe 15,142 hrs · 11,904 cycles

PAX DOOR IS CRACKED ON THE INNER AFT SUPPORT ANGLE 35.3 INCHES FROM LWR EDGE OF DOOR. CRACK IS APPROX 1.5 INCH LONG. REWORK DONE AS REFERENCED IN CRJ 200 SERIES SRM 51-21-11, 51-23-00, 51-42-13, & 51-42-22.

Part: SWITCH — UNKNOWN (NLG STEERING) · airframe 14,020 hrs · 10,790 cycles

A -STEERING INOP- CAUTION MESSAGE AFTER T/O. FOLLOWED QRH, MESSAGE WENT OUT WITH NWS SWITCH OFF. STEERING RE-SET WITH SWITCH AFTER LANDING. EMERGENCY DECLARED.

Part: WEB — CRACKED (FUSELAGE) · airframe 13,655 hrs · 10,483 cycles

LEFT BOX BEAM LOWER WEB CRACKED IN RADIUS.

Part: BEAM — CRACKED (FUSELAGE) · airframe 13,655 hrs · 10,483 cycles

RIGHT BOX BEAM CRACKED AT FWD INBOARD SIDE. WORK COMPLETED IN ACCORDANCE WITH CRJ 200 NDTM 51-20-06, REO 601R-53-61-366, REO 601R-53-61-366 PER CRJ 200 NDTM 51-20-06, REO 601R-53-61-366 REV. F CM20420, REO 601R-53-61-366 CM20420, AND REO 601R-53-61-366.

Part: FRAME — CRACKED (BS 640) · airframe 13,655 hrs · 10,483 cycles

LEFT FS 640 CRACKED. FLT 4454 CX. REPAIRED IAW CRJ 200 NDTM 51-20-06, REO 601R-53-061, SB 601R-53-061 PER CRJ 200 NDTM 51-20-06, REO601R-53-061, REO 601R-53-061, REO601R-53-061, REO601R-54-005, AND REO601R-53-061.

Part: STEP — CRACKED (AFT AIRSTAIR) · airframe 12,816 hrs · 9,809 cycles

A/S/D BOTTOM STEP CRACKED AT ATTACHMENT BRACKET

Part: ODOR — DETECTED (COCKPIT) · airframe 12,396 hrs · 9,486 cycles

SMELL OF SMOKE IN COCKPIT NOTICED ON DESCENT. A/C SWAP TO 884, FLT 4608 DEL 180 MINS.

Part: BRACKET — CRACKED (AIR STAIR DOOR) · airframe 12,280 hrs · 9,392 cycles

A/S/D AFT. CABLE COUNTER BALANCE ANCHOR BRACKET CRACKED

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 12,156 hrs · 9,303 cycles

FOUND PAX DOOR EMERG EXIT LIGHT HAS BULBS INOP.

Part: SEAL — OUT OF POSITION (FUSELAGE)

DURING A GROUND INSPECTION, THE PASSENGER DOOR WAS DIFFICULT TO CLOSE. MAINTENANCE FOUND THE PASSENGER DOOR SEAL OUT OF THE CHANNEL AND REINSTALLED IT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)

Part: ANGLE — CRACKED (FUSELAGE)

DURING A HANGAR INSPECTION, THE RT SIDE FS 640 REINFORCING ANGLE WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE DOUBLER ON THE RT SIDE FS 640 REINFORCING ANGLE IAW SRM. (K)

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING A HANGAR CHECK IN MCN, THE EMERGENCY LIGHTS AT THE PASSENGER DOOR AND OVERHEAD IN THE CABIN WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 1 BATTERY PACK. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: STEP — BROKEN (PAX DOOR)

DURING A GROUND INSPECTION, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND BROKEN. MAINT REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. OPS CHECK GOOD. AC OK FOR SERVICE. (K)

Part: STEP — CRACKED (PAX DOOR)

DURING AN A CHECK IN MCN, THE PASSENGER DOOR BOTTOM STEP WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR BOTTOM STEP. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: CLIP — CRACKED (FUSELAGE)

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

Part: FLOOR SUPPORT — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE LEFT AND RIGHT FLOOR SUPPORT ANGLES AT FS 621 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE LEFT AND RIGHT FLOOR SUPPORT ANGLES AT FS 621 IAW ASA EO 600-53-0105. (M)

Part: APU — FAILED (APU BAY)

DURING APPROACH INTO ATL FROM MYR, THE CREW RECEIVED AND AUXILIARY POWER UNIT FAULT, SHUTDOWN, MESSAGE WITH THE NR 1 GENERATOR DEFERRED. AN EMEGENCY WAS DECLARED AND THE AIRCRAFT LANDED SAFELY IN ATL. MAINTENANCE REMOVED AND REPLACED THE AUXILIARY POWER UNIT. OPS AND LEAK CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: STRIKER — DAMAGED (PAX DOOR SEAL)

FLT 4499 - DURING A GROUND INSPECTION IN ATL, THE PASSENGER DOOR WAS HARD TO LATCH. UPON INSPECTION, MAINTENANCE FOUND THE PASSENGER DOOR SEAL STRIKER DAMAGED AND REPAIRED IT IAW REO 601R-52-11-008. MAINTENANCE ALSO LUBRICATED THE DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: DOOR — MALFUNCTIONED (MAIN PAX)

FLT 4719 - DURING A GROUND INSPECTION IN ATL, THE PASSENGER DOOR WAS HARD TO CLOSE ACCOMPANIED BY A PRESSURE SQUEAL AT ALTITUDE. MAINTENANCE REPLACED THE EPOXY AT THE CENTER SPADE FITTINGS ON THE PASSENGER DOOR AND PRESSURIZED THE AIRCRAFT WITH NO SQUEAL NOTED. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: STEP — BROKEN (FUSELAGE)

FLT 4721 - DURING A GROUND INSPECTION IN ATL, THE PASSENGER DOOR BOTTOM STEP BRACKET WAS FOUND BROKEN OFF. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR BOTTOM STEP ASSEMBLY. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: HANDLE — BINDING (PAX DOOR)

FLT 4853 - DURING A GROUND INSPECTION IN DFW, THE PASSENGER DOR WAS HARD TO OPEN. MAINTENANCE LUBRICATED THE PASSENGER DOOR OTUER HANDLE. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)