N925EV

Part: LANDING GEAR — WARNING MESSAGE (ZONE 700) · airframe 40,457 hrs · 39,348 cycles

GEAR DISAGREE WARNING ALONG WITH ASSOCIATED NOSE DOOR WARNING ON TAKEOFF. BOTH MAINS RETRACTED AND SHOWED UP BUT NOSE GEAR INDICATION SHOWED LINES. QRH RESOLVED ISSUE. RECEIVED 3 GREEN DN INDICATIONS. RTF (FLIGHT 5807 - FILED CLOSED)TROUBLESHOT GEAR DISAGREE WITH NLG DASHED OUT ON RETRACTION IN REFERENCE TO CRJ 200 FIM 32-60-09. PERFORMED VISUAL INSPECTION OF THE NLG. NO DEFECTS NOTED. INSURED ALL CANNON PLUGS TO BE TIGHT AND SECURED. FOUND ALL CANNON PLUGS TO BE SECURE. READ FAULT LOG FROM PSEU IN REFERENCE TO CRJ 200 FIM 32-60-05. FOUND CODES S23 FAR, S34 NEAR, S21 NEAR, S22 FAR, S31 FAR, S32 FAR, S30 FAR DI15 ON, DI14 ON. SUSPECT ISSUE TO BE WITH S23 FAR, NOSE GEAR OLEO EXTENDED. JACKED NLG IN REFERENCE TO CRJ 200 AMM 07-12-03. FOUND NLG TO NOT CENTER AND NOT EXTEND THE FULL 14.5 INCHES LIKE IT SHOULD. REVIEWED AIRCRAFT HISTORY, FOUND STRUT TO BE RECENTLY REPACKED. REF CP 30154369. SUSPECT AIR WAS STUCK IN STRUT. PERFORMED FULL NLG SHOCK STRUT SERVICE IN REFERENCE TO TASK CARD 12-710-003. DURING STRUT SERVICE, THE PUCK WAS HEARD MOVING UP AND DOWN LIKE IT SHOULD. RE-JACKED NLG, STRUT NOW EXTENDS TO THE FULL 14.5 INCHES AND FULLY CENTERS AS IT SHOULD. PERFORMED MULTIPLE NLG SWINGS IN REFERENCE TO CRJ 200 AMM 32-30-00. ALSO JACKED TH

Part: HEATER — SMOKE (COCKPIT WINDOW) · airframe 40,234 hrs · 39,102 cycles

SMOKE IN COCKPIT FROM CP SIDE WINDSHIELD HEAT. QRH RESOLVED ISSUE. (FLIGHT 5025 - FILED OPEN)THIS IS CURRENTLY A WORK IN PROGRESS

Part: TERMINAL BLOCK — SMOKE (ZONE 200) · airframe 40,246 hrs · 39,117 cycles

SMOKE IN COCKPIT FROM CP SIDE WINDSHIELD HEAT. QRH RESOLVED ISSUE. (FLIGHT 5025 - FILED CLOSED)TROUBLESHOT COCKPIT SMOKE EVENT PER FIM 21-21-00 AND FOUND WHILE INSPECTING L/H WINDSHIELD WITH HEAT ON, FOUND LIGHT SMOKE COMING OUT BETWEEN L/H WINDSHIELD HEAT POWER BLOCK AND PANE ATTACH POINT. SHUTTING WINDSHIELD HEAT OFF THE SMOKE STOPS. REMOVED AND REPLACED L/H WINDSHIELD ASSY. REF. CRJ M/M 56-11-01. C/W TASK CARD 56-220-1000-SKY FOR WINDSHIELD REPLACEMENT. PERFORMED OPS CHECK OF WINDSHIELD/WINDOW HEAT AND OPS CHECK GOOD REF. CRJ M/M 30-41-01. PERFORMED OPS CHECK OF WINDSHIELD WIPERS REF. M/M 30-42-00 AND OPS CHECK GOOD. PRESSURIZED AIRCRAFT AND NO LEAKS NOTED FROM L/H WINDSHIELD REPLACEMENT.

Part: WIRE HARNESS — DAMAGED (INDICATION SYS) · airframe 40,058 hrs · 38,914 cycles

ON DEPARTURE FROM DENVER RECEIVED A NOSE DOOR OPEN AND GEAR DISAGREE WARNING MESSAGES. MESSAGES CLEARED WITH QRH (FLIGHT 5083 - FILED CLOSED) ARRIVED AT A/C INTERROGATED PSEU AND BASED ON THE INPUT REASONABLENESS TABLE TABLE 103 IN FIM 32-60-05 IT APPEARS THAT THE S23 NOSE GEAR OLEO EXTENDED SHOULD BE NEAR AND NOT FAR. PERFORMED A GVI OF THE NLG AND FOUND NLG OLEO EXTENDED AND CENTERED SENSOR HARNESS ASSY TO HAVE BEEN DEFORMED/CRUSHED. FOUND NLG OLEO BRACKET SUB ASSEMBLY TO HAVE MINOR BEND, PLEASE REFERENCE AML 1536168 FOR R&R. REMOVED AND REPLACED NLG OLEO EXTENDED AND CENTERED SENSOR HARNESS ASSY IN REF WITH CRJ 200 AMM 31-61-25. OPS CHECK GOOD AT THIS TIME, CYCLED NLG MULTIPLE TIMES WITHOUT ANY DISCREPANCIES IN REF WITH CRJ 200 AMM 32-30-00.

Part: SELECTOR VALVE — FAULTED (ZONE 700) · airframe 39,231 hrs · 38,043 cycles

GEAR DISAGREE ON GEAR EXTENSION ON FINAL. RAN QRH AND CYCLED THE GEAR TWICE NORMALLY WITH 30 SECOND DELAY. MESSAGE PERSISTED. QUICK CYCLED GEAR UNDER DIRECTION OF QRH AND THEN GOT THREE GEAR DOWN AND LOCKED. (FLIGHT 5391 - FILED CLOSED) THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 28703800 WITH THE FOLLOWING CORRECTIVE ACTION: "SEE CP # 28704915 FOR TROUBLESHOOTING AND REMOVAL AND REPLACEMENT OF THYE SELECTOR VALVE. SEE CP # 28703878 FOR FDR DOWNLOAD. "

Part: WARNING MESSAGE — FALSE ACTIVATION (TE FLAPS) · airframe 38,921 hrs · 37,711 cycles

D:DUE TO FLAPS FAIL CAUTION. FLAPS 0 LANDING, COMPLY WITH FULL FLAP EVAULATION PER AD 2009-06-12/09.C: FLAP FAILCAT A DUE WITHIN 10 CYCLES BY TAC 37720. SMOD APPROVAL REQIRED FOR RTS. FLAPS FAIL CAUTION. FLAPS 0 LANDING. (FLIGHT 4663) RESET AND OPERATED FLAPS 5 FULL CYCLES AND COMPLETED AD 2009-06-12/10 COMPLIANCE FORM. OK TO CONTINUE IN SERVICE FOR 10 FLIGHT CYCLES. COMPLIED WITH IN ACCORDANCE WITH FIM FMRP CHAPTER 27 RESET PROCEDURES AND AD 2009-06-12 TRACKING CREATED FOR FULL AD COMPLIANCE BYMCC.

Part: VANE — CHAFED (RT WING TE FLAP) · airframe 38,826 hrs · 37,607 cycles

RH INBD FLAP VANE CHAFED AT WS104.099 (C-CHECK RO 5/9/2024) REPAIRED R/H I/B FLAP VANE L/E SKIN AT W.S. 104.099 IAW CRJ200 SRM 57-52-00 AND 57-52-00 REPAIR #1. NDT PERFORMED BY BARON NDT LLC CRS#: 5NDR545D REPORT#: S032524-1 DATED 25MAR2024. SEE REPORT FOR DETAILS.

Part: SKIN — DAMAGED (LT ELEVATOR) · airframe 38,826 hrs · 37,607 cycles

LH ELEVATOR SKIN ABOVE HINGE #2 DAMAGED, EVAL (C-CHECK RO 5/9/2024) PERFORMED REPAIR AT L/H ELEVATOR SKIN ABOVE HINGE #2 IAW CRJ 200 REO 601R-55-21-591 REV -- DATE: 2024-03-15,SRM 55-20-00,SRM 51-24-36,SRM 51-12-00,SRM 51-25-06,SRM 51-25-16, PERFORMED NDT ET.

Part: SHROUD — DAMAGED (HORIZONTAL STAB) · airframe 38,826 hrs · 37,607 cycles

LE SHROUD RH SIDE H STAB DAMAGED (C-CHECK RO 5/9/2024) REPAIRED RH SIDE HORIZONTAL STABILIZER OF THE LEADING EDGE SHROUD BETWEEN FSS 31.999 TO FSS 67.790 IAW MHIRJ REO 601R-55-11-757 REV -- DATE: 2024-04-25 AND IAW CRJ 200 AMM 20-22-01, AMM 55-10-00 AND CRJ 200 SRM 51-26-01, SRM 55-11-07, SRM 51-42-21,SEE REPORT FOR DETAILSUSED TOOLS DEPTH GAUGE ID: AV-7277 CAL DUE: 07-AUG-24

Part: SHROUD — DAMAGED (HORIZONTAL STAB) · airframe 38,826 hrs · 37,607 cycles

LE SHROUD LH SIDE H STAB DAMAGED (C-CHECK RO 5/9/2024) REPAIRED LH SIDE HORIZONTAL STABILIZER LEADING EDGE SHROUD BETWEEN FSS31.999 TO FSS67.790 IAW REO 601R-55-11-757 REV -- DATE: 2024-04-25, CRJ 200 AMM 20-22-01, AMM 55-10-00, CRJ 200 SRM 51-42-06, SRM 51-42-13, SRM 51-42-21, SRM 55-00-31 AND SRM 55-11-07 AND NDTM PART 1 51-20-09. NDT PERFORMED BY BARON NDT, LLC CRS# 5NDR545D REPORT # S031324-1. SEE REPORT FOR DETAILS. ADDITIONAL REO'S: REO 601R-55-11-757 REV --(P1) DATE: 2024-03-05, REO 601R-55-11-757 REV --(P2) DATE: 2024-03-13, REO 601R-55-11-757 REV --(P3) DATE: 2024-03-22,CAL TOOL: DEPTH GAUGE ID: AV-7277 CAL DUE: 07-AUG-24

Part: SKIN — DENTED (CARGO DOOR) · airframe 38,826 hrs · 37,607 cycles

ADM N925EV-8460THERE IS A SCRATCH AND TWO DENTS ON THE UPPER FWD OF DOOR WHEN CLOSED, SCRATCH IS JUST THOUGH PAINT, MEASURING 26.75 IN FROM TOP OF DOOR, AND 4.75 IN FROM FWD EDGE. PLEASE PLOT, MAP, AND EVALUATE DAMAGE. IF FOUND WITHIN LIMITS, ELIMINATE ALL EVIDENCE OF DAMAGE USING AIRCRAFT STANDARD PRACTICES/PROCEDURES. (C-CHECK RO 5/9/2024) REPAIRED 2 DENTS AND 26,75" SCRATCH ON PAX DOOR IAW MHIRJ REO 601R-52-11-3009 REV P1 DATE 2024-02-23,REO 601R-52-11-3009 REV P2 DATE 2024-02-28, MHIRJ REO 601R-52-11-3009 REV -- DATE 2024-03-14 ,CRJ 200 SRM 51-26-01, 52-00-31, 51-12-00, 51-42-06, 51-21-11, 51-25-06, 51-25-01 AND AMM 52-11-10CAL TOOLS:DIGITAL CALIPER ID: AV-.7803 CAL DUE: JAN-2025, DEPTH GAUGE ID: AV-7277 CAL DUE: 07-AUG-2024. SCALE ID:AV-3788 CAL DUE: 7-AUG-2024NDT PERFORMED BY BARON NDT,LLC FAA CRS# 4NDR454D REPORT# S022624-1 P.O# 171116 DATED 28-FEB-2024,SEE REPORT FOR DETAILS

Part: UNKNOWN — DENTED (UNKNOWN) · airframe 38,731 hrs · 37,492 cycles

FOUND DENT ON THE LEADING EDGE OF THE FLAP-VANE ON THE LEFT OB FLAP AT APPROX. F/STA 210.50 (FILED CLSOED) FOUND DENT AT LEFT WING O/B FLAP VANE F.S. 210.50 TO BE OUT OF LIMITS PER SRM 57-53-00 FIG 102 SHEET 3. NO DENTS PERMITTED. REF CP 27621022 FOR FURTHER ACTION.

Part: SKIN — ERODED (RT WING) · airframe 38,826 hrs · 37,607 cycles

COMPLY WITH SCHEDULED MAINTENANCE CODE: RA69059-601R-57-41-1120 N925EV MXCODEID56580-PR - RH WING CENTER LEADING EDGE PANEL (630JL) HAS EROSION. COMPLIED WITH REO 601R-57-41-1120, REV. --, 2021-04-26 IN ITS ENTIRETY (STEPS 1-5). THIS REPAIR IS VALID FOR 6000 FLIGHT HOURS. , PART NUMBER: - , SERIAL NUMBER: 7831, POSITION: (C-CHECK RO 5/9/2024) REMOVED AND REPLACED RH WING CENTER LEADING EDGE PANEL 630JL PERMANENT REPAIR COMPLIED IAW MHIRJ REO 601R-57-41-1120 REV-- 2021-04-26 AND IAW CRJ 200 SRM 51-42-10, SRM 51-42-06, SRM 51-40-11, SRM 51-21-11, SRM 51-25-06 AND IAW CRJ 200 AMM 30-11-41

Part: SKIN — DAMAGED (LT WING) · airframe 38,826 hrs · 37,607 cycles

COMPLY WITH SCHEDULED MAINTENANCE CODE: RA69006-601R-57-41-1119 N925EV MXCODEID56249-PR - LH WING CENTER LEADING EDGE PANEL (530JL) HAS EROSION. REMOVED EROSION DAMAGE ON L/H WING CENTER LEADING EDGE PANEL 530JL REF CRJ 200 SRM 51-12-00. COMPLIED WITH REO 601R-57-41-1119 REV (--) 2021-04-26 STEPS 1-5 DUE TO EROSION DAMAGE REMOVAL BEING OUT OF LIMITS REF CRJ 200 SRM 57-41-31. THIS REPAIR IS VALID FOR 6000 FLIGHT HOURS. , PART NUMBER: - , SERIAL NUMBER: 7831, POSITION: (C-CHECK RO 5/9/2024) REMOVED AND REPLACED LH WING CENTER LEADING EDGE PANEL 530 JL IAW REO 601R-57-41-1119 REV (--) 2021-04-26 AND CRJ 200 SRM 51-42-06, SRM 51-42-10, AMM 30-11-41, SRM, 51-40-11, SRM 51-21-11, AMM 57-41-01

Part: GUIDE — ERODED (RT WING) · airframe 38,826 hrs · 37,607 cycles

COMPLY WITH SCHEDULED MAINTENANCE CODE: RA69883-601R-57-41-1124 925EV MXCODEID56613-PR - RH WING OUTBOARD LEADING EDGE (630KL) HAS EROSION. COMPLIED WITH TEMPORARY REPAIR PER REO601R-57-41-1124, REV--, DATED 2021-05-04. PERMANENT REPAIR DUE WITHIN 6000 FLT HRS BY 40757.6 TAT, PART NUMBER: - , SERIAL NUMBER: 7831, POSITION: (C-CHECK RO 5/9/2024) REMOVED AND REPLACED R/H OUTBOARD L/E SKIN PANEL# 630KL IAW CRJ 200 AMM 57-41-01,SRM 51-42-06,SRM 51-42-10,AMM 30-11-41, SRM 51-40-11, SRM 51-21-11 AND MHIRJ REO 601R-57-41-1124 REV -- DATE: 2021-05-04

Part: SUPPORT ANGLE — CORRODED (SEAL RETAINER) · airframe 34,764 hrs · 33,747 cycles

LH FWD AVIONICS BAY DOOR SEAL RETAINER SUPPORT ANGLE HAS CORROSION. (C-CHECK RO 5/16/2021) VALUATE LH FWD AVIONICS BAY DOOR SEAL RETAINER SUPPORT ANGLE CORRECTIVE ACTION: LH FWD ANGLE IS 100% EXFOLIATED, FOUND TO BE OUT OF LIMITS. REF CRJ 200 SRM 52-00-00.. INSTALLED NEW L/H FWD SEAL RETAINER SUPPORT ANGLE ON AVIONICS BAY DOOR REF. CRJ200 SRM 51-42-06. SEE CONTINUATION CARD FOR DETAILS

Part: CUP — DAMAGED (HAND RAIL) · airframe 34,764 hrs · 33,747 cycles

PAX DOOR UNDER FLOOR AFT HAND RAIL CUP REQUIRES REPLACEMENT. (C-CHECK RO 5/16/2021) REMOVED AND REPLACED THE PAX DOOR AFT HANDRAIL CUP ASSY WITH 1EA. NEW PART REF. CRJ200 SRM 51-42-06 , CRJ200 SRM 51-42-13, & BOMBARDIER DWG 601R31527 REV W. COMPLIED WITH 51-900-1003-SKY.

Part: BULKHEAD WEB — CRACKED (BS 621) · airframe 34,764 hrs · 33,747 cycles

FS.621 PRESS BULKHEAD LWR WEB AFT STIFFENER LOCATED OUTBD OF LBL36 ABOVE FLOOR AT WL80 FOUND CRACKED . (C-CHECK RO 5/16/2021) REMOVED AND INSTALLED REPLACEMENT FS.621 PRESS. BULKHEAD WEB AFT SIDE STIFFENER P/N 601R36008-51 AT WL.79 OUTBD OF LBL36 PER CRJ200 SRM 51-42-06 REF. BOMBARDIER. DWG. 601R36008 REV. W . COMPLIED WITH 51-900-1003-SKY AND PRESSUE CHECK GOOD . SEE CONTINUATION CARD FOR DETAILS

Part: ANGLE — CRACKED (BS 280 RBL 9) · airframe 34,764 hrs · 33,747 cycles

FS 280 RBL 9, INBOARD VERTICAL ANGLE APPEARS CRACKED AT TOP END. (C-CHECK RO 5/16/2021) REMOVED AND REPLACED VERTICAL ANGLE UNDER FLOOR LEVEL AT FS.280 RBL.9 (INBD) REF REO 601R-53-11-171 REV.-D DATED 13 FEB 07 AND CRJ 200 SRM 51-42-21 AND COMPLIED WITH SKY CARD 51-900-1003-SKY AND SEE CONTINUATION CARD FRO DETAILS / PREVIOUSLY REPAIRED ANGLE REPLACEMENT ONLY

Part: ANGLE — CRACKED (BS 280 LBL9) · airframe 34,764 hrs · 33,747 cycles

FS 280 LBL 9, INBOARD VERTICAL ANGLE APPEARS CRACKED AT TOP END. (C-CHECK RO 5/16/2021) REMOVED AND REPLACED VERTICAL ANGLE UNDER FLOOR LEVEL AT FS.280 LBL.9 (INBD) REF REO 601R-53-11-171 REV.-D DATED 13 FEB 07 AND CRJ 200 SRM 51-42-21 COMPLIED WITH 51-900-1003-SKY AND SEE CONTINUATION CARD FOR DETAILS PREVIOUSLY REPAIRED ANGLE REPLACEMENT ONLY

Part: FRAME — CRACKED (BS 333) · airframe 34,764 hrs · 33,747 cycles

*FS333 FRAME CRACKED BETWEEN STR1L AND STR2L (C-CHECK RO 5/16/2021) REMOVED AND INSTALLED FRAME SECTOR 601R32004-41 REF. CRJ 200 SRM 51-42-06, CRJ-200-SRM 51-42-21. DRAWING 601R31522 REV AC AND DRAWING 601R31016 REV D. COMPILED WITH 51-900-1003-SKY AND PRESSURE CHECK GOOD . SEE CONTINUATION CARD FOR DETAILS

Part: SKIN — CHAFED (FUSELAGE) · airframe 34,764 hrs · 33,747 cycles

* THE CENTER WING LOWER PLANK IS CHAFED AT 2 LOCATIONS ALONG ITS AFT END, JUST INBOARD OF LBL 45 AND JUST INBOARD OF RBL 45, BOTH LOCATIONS ARE BELOW THE AFT SPAR. (C-CHECK RO 5/16/2021) REPAIRED THE CENTER WING LOWER PLANK CHAFE AT 2 LOCATIONS ALONG ITS AFT END, JUST INBOARD OF LBL 45 AND JUST INBOARD OF RBL 45, BOTH LOCATIONS ARE BELOW THE AFT SPAR. REF REO 601R-57-21-3459 REV -- DATED 2021-04-13 COMPLIED WITH 28-900-1000-SKY AND 51-900-1003-SKY .LEAK CHECKS GOOD AND SEE CONTINUATION CARD FOR DETAILS

Part: HINGE — GOUGED (RT AILERON) · airframe 34,764 hrs · 33,747 cycles

*RIGHT WING, AILERON HINGE FITTING #2 (CENTER INBD), HAS GOUGING (MARKED) (C-CHECK RO 5/16/2021) REMOVED GOUGE ON *RIGHT WING, AILERON HINGE FITTING #2 (CENTER OTBD) REF CRJ-200-SRM 51-12-00. BLENDED AREA FOR TO BE OUT OF LIMITS REF CRJ-200-SRM 57-51-14. REPAIRED RIGHT WING, AILERON HINGE FITTING #2 REF REO 601R-57-51-946 REV -- DATED 2021-04-13. SEE CONTINUTION CARD FOR DETAILS

Part: HINGE — CORRODED (RT AILERON) · airframe 34,764 hrs · 33,747 cycles

*RIGHT WING, AILERON HINGE FITTING #1 (MOST INBD), HAS GOUGING (MARKED) (C-CHECK RO 5/16/2021) REMOVED GOUGE ON *RIGHT WING, AILERON HINGE FITTING #1 (CENTER OTBD) REF CRJ-200-SRM 51-12-00. BLENDED AREA FOR TO BE OUT OF LIMITS REF CRJ-200-SRM 57-51-14. REPAIRED RIGHT WING, AILERON HINGE FITTING #1 REF REO 601R-57-51-946 REV -- DATED 2021-04-13. SEE CONTINUTION CARD FOR DETAILS

Part: HINGE — GOUGED (RT AILERON) · airframe 34,764 hrs · 33,747 cycles

*RIGHT WING, AILERON HINGE FITTING #3 (CENTER OTBD), HAS GOUGING (MARKED) (C-CHECK RO 5/16/2021) REMOVED GOUGE ON *RIGHT WING, AILERON HINGE FITTING #3 (CENTER OTBD) REF CRJ-200-SRM 51-12-00. BLENDED AREA FOR TO BE OUT OF LIMITS REF CRJ-200-SRM 57-51-14. REPAIRED *RIGHT WING, AILERON HINGE FITTING #3 REF REO 601R-57-51-946 REV -- DATED 2021-04-13. SEE CONTINUTION CARD FOR DETAILS

Part: SEAT TRACK — CORRODED (BS 364-394) · airframe 34,764 hrs · 33,747 cycles

* CORROSION IN MULTIPLE SPOTS ON LBL9.00 FLOOR SEAT TRACK BETWEEN FS364.00 & FS394.00 (C-CHECK RO 5/16/2021) REMOVED DISCREPANT SEAT TRACK REF CRJ 200 SRM 51-41-02, FABRICATED AND INSTALLED NEW LBL 9 SEAT TRACK BETWEEN FS364.00 & FS394.00 , REF REO 601R-53-00-485 REV D DATED 2018-01-29

Part: SEAT TRACK — CORRODED (BS 364-394) · airframe 34,764 hrs · 33,747 cycles

* CORROSION IN MULTIPLE SPOTS ON RBL9.00 FLOOR SEAT TRACK BETWEEN FS364.00 & FS394.00 (C-CHECK RO 5/16/2021) REMOVED AND INSTALLED NEW SEAT TRACK WITH RTV 157 ON FAYING SURFACE BETWEEN FS364 TO FS399 REF CRJ 200 AMM 53-01-11-400-802

Part: FRAME — CORRODED (BS 409 S26L-26R) · airframe 34,764 hrs · 33,747 cycles

* CORROSION ON FRAME 409+16 FORWARD SIDE AND ATTACH FLANGE BETWEEN STR26R AND STR26L. (C-CHECK RO 5/16/2021) REPAIRED FRAME 409+16 FORWARD SIDE AND ATTACH FLANGE BETWEEN STR25R AND STR25L REF CRJ-200-SRM 53-00-15. PREESURE CHECK GOOD AND COMPLIED WITH 51-900-1003-SKY

Part: FLOORBEAM — CORRODED (BS 280 L/RBL 9) · airframe 34,764 hrs · 33,747 cycles

* CORROSION ON FS280.00 BEAM BETWEEN RBL9.00 & LBL9.00 (MARKED WITH ORANGE STREAMER) (C-CHECK RO 5/16/2021) REMOVED CORROSION ON FS280 BEAM BETWEEN RBL9 & LBL9, REF CRJ 200 SRM 51-21-06, FWD ANGLE IS OUT OF LIMITS PER REF CRJ 200 SRM 53-00-00, AFT ANGLE IS WITHIN LIMITS PER REF CRJ 200 SRM 53-00-00,REMOVED AND REPLACED FWD ANGLE REF CRJ 200 SRM 51-42-06, & REF CRJ 200 SRM 51-42-21, & BOMBARDIER DWG# 600-34017, REV AC. SEE CONTINUATION CARD FOR MORE DETAILS.COMPLIED WITH 51-900-1003-SKY.

Part: FLOOR SUPPORT — CORRODED (PRESSURE DECK) · airframe 34,764 hrs · 33,747 cycles

* LH PRESSURE FLOOR SILL CORRODED IN MULTIPLE SPOTS (MARKED). (C-CHECK RO 5/16/2021) REPAIRED LH PRESSURE FLOOR SILL REF REO 601R-53-41-2901 REV-- DATED 2021-04-16 AND REO 601R-53-41-666 REV C DATED 2012-11-06. PRESSURE CHECK GOOD AND COMPLIED WITH 51-900-1003-SKY. SEE CONTINUATION CARD FOR DETAILS

Part: FLOORBEAM — CORRODED (BS 621 LBL 27) · airframe 34,764 hrs · 33,747 cycles

* CORROSION ON FLOOR SUPPORT ANGLE AT FS621 OUTBOARD OF LBL27. (C-CHECK RO 5/16/2021) REMOVED AND REPLACED FLOOR SUPPORT ANGLE AT FS621 OUTBOARD OF LBL27 REF REO 601R-53-61-117 REV -E DATED 2018-01-15, CRJ 200 SRM 51-42-06 AND CRJ 200 SRM 51-42-21. PRESSURE CHECK GOOD AND COMPLIED WITH 51-900-1003-SKY . SEE CONTINUATION CARD FOR DETAILS

Part: FRAME — CRACKED (BS 605 S24L) · airframe 34,764 hrs · 33,747 cycles

* FS605 FRAME LOWER FLANGE CRACKED AT STR24L. (C-CHECK RO 5/16/2021) REMOVED AND INSTALLED NEW LOWER FRAME SECTOR, 4(EA) SPLICES AND 2(EA) SUPPORT CLIPS OF FS605 REF. CRJ200 SRM 51-42-06, CRJ200 SRM 51-42-21 AND DWG601R36026 REV.AF. COMPLIED WITH 51-900-1003-SKY AND PRESSURE CHECK GOOD . SEE CONTINUATION CARD FOR DETAILS

Part: CARGO TRACK — CRACKED (BS 621) · airframe 34,764 hrs · 33,747 cycles

* BRACKET ON BOTTOM OF CARGO TRACK SUPPORT AT FS621 CRACKED. (C-CHECK RO 5/16/2021) REMOVED AND REPLACED 1EA. NEW SUPPORT BRACKET FOR CARGO DOOR TRACK, LOCATED AT BOTTOM OF DOOR SUPPORT TRACK AT FS621 REF. BOMBARDIER DWG#601R35050 REV Y. & SRM 51-42-21. COMPLIED WITH 51-900-1003-SKY. PRESSURE CHECK GOOD

Part: WEB — CORRODED (PAX DOOR) · airframe 34,764 hrs · 33,747 cycles

* PASSENGER DOOR AFT WEB NEAR PULLEY BRACKET FOR SUPPORT WHEEL CABLE HAS CORROSION (MARKED). (C-CHECK RO 5/16/2021) REMOVED AND REPLACED WITH NEW PAX DOOR AFT WEB REF CRJ 200 SRM 51-42-06 SEE CONTINUE CARD FO DETAILS

Part: TIE DOWN — CORRODED (BS 574-621) · airframe 34,764 hrs · 33,747 cycles

* CORROSION ON PLATES FOR CARGO NET TIE DOWNS BETWEEN FS574 AND FS621. (C-CHECK RO 5/16/2021) REMOVED AND REPLACED FWD, MID, AND AFT TIE DOWN PLATES FLOOR SUPPORTS. IAW CRJ200 SRM 51-42-06, 51-45-00, AND BOMBARDIER INC. CANADAIR ENGINEER DWG NO. 601R35031 REV Y. COMPLIED WITH 51-900-1003-SKY

Part: ANGLE — CORRODED (PAX DOOR) · airframe 34,764 hrs · 33,747 cycles

* PASSENGER DOOR ANGLE ATTACHED TO INNER SKIN FOR PANEL 832AT HAS CORROSION (MARKED). (C-CHECK RO 5/16/2021) REMOVED AND REPLACED PAX DOOR ANGLE ATTACHED TO INNER SKIN FOR PANEL 832AT REF. CRJ200 SRM 51-42-13.

Part: HINGE — CORRODED (RT SPOILER) · airframe 34,764 hrs · 33,747 cycles

RH FLIGHT SPOILER INBD AND MIDDLE HINGE POINT HARDWARE AND INBD COVER PLATE HARDWARE CORRODED (C-CHECK RO 5/16/2021) REMOVED AND REPLACED FLIGHT SPOILER INBD AND MIDDLE HINGE POINT HARDWARE & INBD COVER PLATE HARDWARE REF CRJ200 AMM 27-64-05-400-801

Part: SKIN — DAMAGED (LT WING) · airframe 34,764 hrs · 33,747 cycles

WHILE COMPLYING WITH SB 601R-57-046 REV C ( PART A) LHS 1EA O/S FASTENER FOUND INSTALLED IN HOLE #14. FASTENER TYPE IS (HST411-10, HOLE DIA. IS .340". (C-CHECK RO 5/16/2021) REPAIRED L/H SIDE 1 EA OVERSIZE FASTENER HOLE IN WING PLANK ASSY ( STEEL STRAP,LOWER WING PLANK AND TRUNNION FLAGE ) AT WS 65.75 BETWEEN REAR SPAR AND AUX SPAR REF REO 601R-57-21-3456 REV -- DATED 2021-04-09. COMPLIED WITH ALL STEPS OF REO 601R-57-21-3456 REV -- DATED 2021-04-09 AND 51-900-1003-SKY. SEE CONTINUATION CARD FOR DETAILS

Part: ATTACH FITTING — CORRODED (RT SPOILER) · airframe 34,764 hrs · 33,747 cycles

RH OTBD GROUND SPOILER INBD, MIDDLE, OTBD AND PCU CONNECT HARDWARE CORRODED (C-CHECK RO 5/16/2021) REMOVED AND REPLACE CORRODED HARDWARE WITH NEW HARDWARE ON RH OTBD GROUND SPOILER AT INBD, MIDDLE, OTBD, AND PCU ATTATCHING POINTS. REF CRJ 200 AMM 27-65-01-400-801

Part: HINGE — CORRODED (RT SPOILERON) · airframe 34,764 hrs · 33,747 cycles

RH SPOILERON INBD AND OTBD HINGE POINT COVER PLATE HARDWARE CORRODED (C-CHECK RO 5/16/2021) REMOVED AND REPLACED INBD AND OTBD HINGE POINT COVER PLATE HARDWARE REF CRJ 200 AMM 27-64-01-400-801

Part: SEAT TRACK — CORRODED (BS 409-559 LBL 9) · airframe 34,764 hrs · 33,747 cycles

CORROSION ON THE SEAT RAIL SUPPORT BEAM FS409+118 TO FS559-10 LBL9.0 (C-CHECK RO 5/16/2021) / REMOVED CORROSION ON THE SEAT RAIL SUPPORT BEAM FROM FS409+118 TO FS559+10 LBL9, & FOUND TO BE OUT OF LIMITS PER REF REO 601R-53-00-005, REV -B, DATE 2011-01-06. REPAIRED SEAT RAIL PER MHIRJ REO 601R-53-41-2906, REV -- , DATED 2021-05-07 AND COMPLIED WITH ALL STEPS OF THE REO. SEE CONTIUATION CARD FOR FURTHER DETAILS. COMPLIED WITH TASK CARD 51-900-1003-SKY.

Part: SEAT TRACK — CORRODED (BS 424-513 RBL 9) · airframe 34,764 hrs · 33,747 cycles

CORROSION ON THE SEAT RAIL SUPPORT BEAM FS424 TO FS513 RBL9.0 / 783161$M255 (C-CHECK RO 5/16/2021) REPAIRED SEAT RAIL PER MHIRJ REO 601R-53-41-2907, REV -- , DATED 2021-05-07 AND COMPLIED WITH ALL STEPS OF THE REO. SEE CONTIUATION CARD FOR FURTHER DETAILS. COMPLIED WITH TASK CARD 51-900-1003-SKY.

Part: HINGE — CORRODED (RT SPOILER) · airframe 34,764 hrs · 33,747 cycles

RH INBD GROUND SPOILER OTBD HINGE HARDWARE CORRODED (C-CHECK RO 5/16/2021) REMOVED AND REPLACED HARDWARE ON RH INBD GROUND SPOILER OTBD HINGE REF CRJ 200 AMM 27-65-01-000-801

Part: FLOOR SUPPORT — CORRODED (PRESSURE DECK) · airframe 34,764 hrs · 33,747 cycles

* RH PRESSURE FLOOR SILL CORRODED IN MULTIPLE SPOTS (MARKED). (C-CHECK RO 5/16/2021) REPAIRED RH PRESSURE FLOOR SILL REF REO 601R-53-41-2902 REV-- DATED: 2021-04-16 AND REO 601R-53-41-666 REV. €“C DATE 2012-11-06. . PRESSURE CHECK GOOD AND COMPLIED WITH 51-900-1003-SKY. SEE CONTINUATION CARD FOR DETAILS

Part: FLOOR SUPPORT — CORRODED (PRESSURE DECK) · airframe 34,764 hrs · 33,747 cycles

* RH PRESSURE FLOOR SILL ANGLE CORRODED IN MULTIPLE SPOTS (MARKED). (C-CHECK RO 5/16/2021) REMOVED CORROSION FROM R/H PRESSURE FLOOR SILL ANGLE AT MULTIPLE LOCATIONS REF REO 601R-53-41-666, REV -C, 2012-11-06 AND REO 601R-53-41-2902 REV-- DATED: 2021-04-16 . COMPLIED WITH TASK CARD 51-900-1003-SKY.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 34,764 hrs · 33,747 cycles

* LH SIDE SEAT TRACK RETAINER CORRODED FROM 559+16 TO 559+80 (MARKED). (C-CHECK RO 5/16/2021) REMOVED CORROSION FROM LH SIDE SEAT TRACK RETAINER FROM FS559+16 TO FS559+80 REF CRJ 200 SRM 51-21-06. NDT IAW CRJ 200 NDT M PART 1 REV 42 10-10 -20 51-20-04, 51-20-06 NO DEFECTS. LH SIDE DEAT TRACK RETAINER FOUND OUT OF LIMITS IAW CRJ200 SRM 53-00-00. REPLACED LH SIDE SEAT TRACK RETAINER FROM FS559+16 TO 559+80 WITH NEW RETAINER P/N: 601R38312-97 REF CRJ 200 AMM 53-01-11-400-802.

Part: STRAP — CORRODED (BS 559 LBL24-40) · airframe 34,764 hrs · 33,747 cycles

* THE LH FLOOR SUPPORT STRAP AT FS 559 THAT EXTENDS BETWEEN LBL 24 AND LBL 40 HAS CORROSION ALONG ITS SURFACE. (C-CHECK RO 5/16/2021) REMOVED AND INSTALLED NEW L/H FLOOR SUPPORT STRAP AT FS559 THAT EXTENDS BETWEEN LBL24 & LBL40, REF CRJ 200 SRM 51-42-06, & BOMBARDIER DWG# 601R31025, REV N. PRESSURE CHECK GOOD AND COMPLIED WITH 51-900-1003-SKY. SEE CONTINUATION CARD FOR DETAIL S

Part: STRINGER — CORRODED (BS 310 S16L) · airframe 34,764 hrs · 33,747 cycles

* STR16L CORRODED AT FS310.00 (MARKED). (C-CHECK RO 5/16/2021) REMOVED CORROSION ON STGR16L INTERCOSTAL AT FS310, REF CRJ 200 SRM 51-21-06. EVALUATED AND FOUND TO BE OUT OF LIMITS. SUBMITTED TO ENGINEERING AND RECEIVED MHIRJ REO 601R-53-21-3439 REV-- DATED:2021-4-23 AND MHIRJ REO 601R-53-21-3445 REV -- DATED 2021-04-29. ALL STEPS OF REO COMPLIED WITH. COMPLIED WITH 51-900-1003-SKY.

Part: SEAT TRACK — CORRODED (BS 449-499) · airframe 34,764 hrs · 33,747 cycles

* RH SIDE SEAT TRACK EXTRUSION CORRODED IN MULTIPLE SPOTS FROM FS 449.00 TO FS499.00 (MARKED). (C-CHECK RO 5/16/2021) REMOVED AND INSTALLED NEW SEAT TRACK AT FS449 TO FS501 RBL9.0 PART # 601R38312-119 REF. CRJ200 AMM 53-01-11-400-802.

Part: STRAP — CORRODED (BS 559 RBL 24-40) · airframe 34,764 hrs · 33,747 cycles

* THE RH FLOOR SUPPORT STRAP AT FS 559 THAT EXTENDS BETWEEN RBL 24 AND RBL 40 HAS CORROSION ALONG ITS SURFACE. (C-CHECK RO 5/16/2021) REMOVED AND INSTALLED NEW R/H FLOOR SUPPORT STRAP AT FS559, BETWEEN RBL27 AND RBL40. REF: CRJ 200, DRW 601R31025, REV N, CRJ-200 SRM 51-42-06 . COMPLIED WITH 51-900-1003-SKY AND PRESSURE CHECK GOOD . SEE CONTINUATION CARD FOR DETAILS

Part: SEAT TRACK — CORRODED (BS 409-559) · airframe 34,764 hrs · 33,747 cycles

* THE CABIN FLOOR SEAT RAIL/TRACK ON LBL 9.0 BETWEEN FS 409+128 AND FS 559 HAS MULTIPLE SPOTS OF CORROSION, SCRATCHES AND NICKS. (C-CHECK RO 5/16/2021) REMOVED THE CORROSION AND OTHER DAMAGE FROM THE SEAT TRACK, FS409+126 TO FS559+4 LBL9.0 PART # 601R31032-7 REF. CRJ200 SRM 51-12-00 AND CRJ200 SRM 51-21-06. THE BLEND ON THE SEAT TRACK AT FS409+126 TO FS559+4 LBL9.0 PART # 601R31032-7 IS OUT OF LIMITS REF. CRJ200 SRM 53-21-49. REMOVED THE SEAT TRACK AT FS409+126 TO FS559+4 LBL9.0 PART # 601R31032-7 REF. CRJ200 AMM 53-01-11-000-802. REPLACED SEAT TRACK FROM FS409+126 TO FS559+4 LBL9.0 PART #601R31032-7 WITH NEW PART REF CRJ 200 AMM 53-01-11-400-802.

Part: FLOORBEAM — CRACKED (BS 414 LBL27-36) · airframe 34,764 hrs · 33,747 cycles

* THE FS 484 BELOW FLOOR INTERCOSTAL BETWEEN LBL 27 AND LBL 36 HAS A CRACKED OUTBOARD CLIP. (C-CHECK RO 5/16/2021) REMOVED THE OTBD BRACKET AT FS484 BETWEEN LBL27 & LBL36 REF. CRJ200 SRM 51-42-21. FABRICATED NEW REPLACEMENT BRACKET PN# S6144-14, PO T000057813/7, STEPS 5.REF: CRJ 200, BOMBARDIER REO 601R-53-41-059, REV-B, DATE: 2009-09-16. REPLACED NEW BRACKET LOCATED AT FS484. BELOW FLOOR INTERCOSTAL AT LBL36, REF: CRJ 200, SRM 51-42-21 AND IN REFERENCE TO PREVIOUSLY INCORPERATED BOMBARDIER REO 601R-53-41-059, REV-B, DATE: 2009-09-16. COMPLIED WITH 51-900-1003-SKY. PRESSURE CHECK GOOD

Part: SEAT TRACK — CORRODED (BS 409-559) · airframe 34,764 hrs · 33,747 cycles

* THE CABIN FLOOR SEAT RAIL/TRACK ON RBL 9.0 BETWEEN FS 409+128 AND FS 559 HAS MULTIPLE SPOTS OF CORROSION, SCRATCHES AND NICKS. (C-CHECK RO 5/16/2021) REMOVED THE CORROSION AND OTHER DAMAGE FROM THE SEAT TRACK, FS409+126 TO FS559+4 RBL9.0 PART # 601R31032-7 REF. CRJ200 SRM 51-12-00 AND CRJ200 SRM 51-21-06. EVALUATED AND FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED SEAT TRACK WITH NEW PART ON RBL9 BETWEEN FS409+128 AND FS559. REF: CRJ 200, AMM 53-01-11-400-802, TOOL USED: TUC7824, CAL DUE DATE: 31-DEC-21

Part: FLOORBEAM — CORRODED (BS 559 RBL 9) · airframe 34,764 hrs · 33,747 cycles

* THE FLOOR BEAM AT RBL 9 HAS A SHEARED NUTPLATE ON ITS INBOARD FLANGE AT APPROX. FS 559+6 AND CORROSION AROUND THE NUTPLATE ON ITS OUTBOARD FLANGE AT APPROX. FS 559+6. (MARKED WITH RED GREASE PENCIL) (C-CHECK RO 5/16/2021) REMOVED CORROSION ON FLOOR BEAM ON RBL9 O/B FLANG AT APPROX FS559+6, REF CRJ 200 SRM 51-21-06. EVALUATED AND FOUND TO BE OUT OF LIMITS. SUBMITTED TO ENGINEERING AND RECEIVED REO 601R-53-51-577 REV--P1, 2021-04-13. REPAIRED PER REO 601R-53-51-577 REV--, 2021-04-26. ALL STEPS COMPLIED WITH. COMPLIED WITH 51-900-1003-SKY.

Part: FLOORBEAM — CRACKED (BS 484 RBL27-36) · airframe 34,764 hrs · 33,747 cycles

* THE FS 484 BELOW FLOOR INTERCOSTAL BETWEEN RBL 27 AND RBL 36 HAS A SUSPECTED CRACK ON ITS INBOARD CLIP IN THE TOP RADIUS. (C-CHECK RO 5/16/2021) REMOVED AND REPLACED THE INBD CLIP AT FS 484.00 BELOW FLOOR INTERCOSTAL BETWEEN RBL 27 AND RBL 36 WITH NEW PART , REF DWG 601R31171 REV A AND CRJ200 SRM 51-42-21. COMPLIED WITH 51-900-1003-SKY.

Part: SEAT TRACK — CORRODED (BS 364-409) · airframe 34,764 hrs · 33,747 cycles

* RH SIDE SEAT TRACK CORRODED IN MULTIPLE SPOTS FROM FS 364.00 TO FS409.00 (MARKED). (C-CHECK RO 5/16/2021) REMOVED AND INSTALLED NEW SEAT TRACK AT FS364 TO FS409+18 RBL9.0 PART # 601R38312-31 REF. CRJ200 AMM 53-01-11-400-802.

Part: FLOORBEAM — CORRODED (BS 621) · airframe 34,764 hrs · 33,747 cycles

* THE LBL 9.0 FLOOR BEAM ATTACHMENT TO THE FS 621 BULKHEAD'S SEAT TRACK HAS CORROSION AROUND ITS SCREW HOLES. (C-CHECK RO 5/16/2021) REMOVED AND INSTALLED NEW CARGO TIE-DOWN TRACK AT LBL9 APPROX. FS621 REF CRJ200 AMM 53-00-49-000-801 & 53-00-49-400-801. CAL TOOL: TUC7826 DUE: 31-MAR-22

Part: CAM — CHAFED (PAX DOOR FRAME) · airframe 34,764 hrs · 33,747 cycles

* PAX DOOR SURROUND UPPER AFT CAM FITTING CHAFED (FLAGGED). (C-CHECK RO 5/16/2021) BLENDED CHAFE ON PAX DOOR SURROUND UPPER AFT CAM FITTING REF CRJ200 SRM 51-12-00. EVALUATED AND FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED THE PAX DOOR SURROUND UPPER AFT CAM FITTING WITH 1EA. NEW PART REF. CRJ200 SRM 51-42-21.

Part: ANCHOR FITTING — CORRODED (PAX DOOR FRAME) · airframe 34,764 hrs · 33,747 cycles

* PAX DOOR SURROUND FWD AND AFT ANCHOR FITTINGS HAVE CORRODED HARDWARE. (C-CHECK RO 5/16/2021) REMOVED AND REPLACED PAX DOOR SURROUND FWD AND AFT ANCHOR FITTINGS HARDWARE WITH NEW 8EA BOLTS 12EA SCREWS, 28EA WASHERS, AND 20EA NUTS REF CRJ 200 SRM 51-41-02

Part: CUP — CORRODED (HAND RAIL) · airframe 34,764 hrs · 33,747 cycles

* PAX DOOR UNDERFLOOR FWD AND AFT HAND RAIL RECIEVING CUPS CORRODED IN MULTIPLE SPOTS (MARKED). (C-CHECK RO 5/16/2021) BLENDED CORROSION FROM FWD AND AFT PAX DOOR UNDERFLOOR HAND RAIL RECEIVING CUPS, (MULTIPLE AREAS). REF: CRJ 200, SRM 51-21-06. EVALUATED AND FOUND TO BE OUT OF LIMITS. :INSTALLED NEW FWD PAX DOOR HANDLE CUP. REF: CRJ 200, SRM 51-42-06, SRM 51-42-13 & BOMBARDIER DWG 601R31527 REV W. SEE JOB: 2783161 OP:362 MXTRANS# 22654106 FOR REPLACEMENT OF AFT HANDRAIL CUP. COMPLIED WITH 51-900-1003-SKY.

Part: RIB — CRACKED (RT MLG WW) · airframe 34,764 hrs · 33,747 cycles

*RH MLG BATT RIB AT APPROX RBL 45 HAS A CRACK. AREA MARKED (C-CHECK RO 5/16/2021) REMOVED AND REPLACED THE RH MLG BATT RIB CAP ANGLE AT APPROX RBL 45 REF DWG 601R10204 REV J, DWG 601R10212 REV A, CRJ200 SRM 51-42-06 AND 51-42-21. / COMPLIED WITH 51-900-1003 SKY

Part: SKIN — DENTED (BS295-310) · airframe 34,764 hrs · 33,747 cycles

* DENT ON FUSELAGE BETWEEN FS295 AND FS310 BETWEEN STR25R AND STR26R (C-CHECK RO 5/16/2021) EVALUATED DENT DIMENSION AND FOUND TO BE OUT OF LIMITS. DENT IS LESS THEN 1 INCH FROM FASTENER REF CRJ200 SRM 53-00-31. SUBMITTED TO ENGINEERING AND RECEIVED MHIRJ REO 601R-53-21-3435 REV -- DATED 2021-04-13. (ALL STEPS COMPLIED WITH). RESTORED FINISH.

Part: ANGLE — CORRODED (RT AFT DOOR SEAL) · airframe 34,764 hrs · 33,747 cycles

* RH AFT ANGLE FOR AVIONICS BAY DOOR SEAL RETAINER HAS CORROSION. (C-CHECK RO 5/16/2021) REMOVED AND INSTALLED REPLACEMENT R/H AFT AVIONICS BAY DOOR SEAL RETAINER SUPPORT ANGLE CC670-38660-1 REF CRJ 200 SRM 51-42-06 . COMPLIED WITH 51-900-1003-SKY AND SEE CONTINUATION CARD FOR DETAILS

Part: STOP FITTING — GOUGED (E/E BAY DOOR) · airframe 34,764 hrs · 33,747 cycles

* AVIONICS BAY DOOR RH AFT STOP FITTING ON FUSELAGE GOUGED. (C-CHECK RO 5/16/2021) AVIONICS BAY DOOR RH AFT STOP FITTING FOUND TO BE OUT OF LIMITS, REMOVED AND REPLACED WITH NEW AVIONICS BAY DOOR STOP FITTING REF CRJ200 SRM 51-41-02

Part: HOUSING — CHAFED (CARGO DOOR HANDL) · airframe 34,764 hrs · 33,747 cycles

CARGO DOOR HANDLE HOUSING IS CHAFED (C-CHECK RO 5/16/2021) REMOVED AND INSTALLED NEW CARGO HANDLE HOUSING ON CARGO DOOR REF DWG 601R35027 REV -AY AND CRJ200 SRM 51-42-21. COMPLIED WITH 51-900-1003-SKY AND PRESSURE CHECK GOOD

Part: ANGLE — CORRODED (E/E SEAL RETAINE) · airframe 34,764 hrs · 33,747 cycles

* RH FWD ANGLE FOR AVIONICS BAY DOOR SEAL RETAINER HAS CORROSION. (C-CHECK RO 5/16/2021) REMOVED CORROSION ON RH FWD ANGLE FOR AVIONICS BAY DOOR SEAL RETAINER REF CRJ200 SRM 51-21-06. RH FWD ANGLE IS 100% EXFOLIATED, FOUND TO BE OUT OF LIMITS REF CRJ200 SRM 52-00-00.INSTALLED NEW R/H FWD SEAL RETAINER SUPPORT ANGLE ON AVIONICS BAY DOOR REF. CRJ200 SRM 51-42-06.

Part: RETAINER — CORRODED (E/E DOOR SEAL) · airframe 34,764 hrs · 33,747 cycles

* LH AFT ANGLE FOR AVIONICS BAY DOOR SEAL RETAINER HAS CORROSION. (C-CHECK RO 5/16/2021) REMOVED CORROSION ON LH AFT ANGLE FOR AVIONICS BAY DOOR SEAL RETAINER REF CRJ200 SRM 51-21-06. LH AFT ANGLE IS 100% EXFOLIATED, FOUND TO BE OUT OF LIMITS REF CRJ200 SRM 52-00-00. INSTALLED NEW L/H AFT SEAL RETAINER SUPPORT ANGLE ON AVIONICS BAY DOOR REF. CRJ200 SRM 51-42-06.

Part: SKIN — CHAFED (RT WING TE FLAP) · airframe 34,764 hrs · 33,747 cycles

* R/H INBOARD FLAP VANE SKIN IS CHAFED AT THE OUTBOARD LEADING EDGE. (C-CHECK RO 5/16/2021) BLENDED CHAFE ON R/H INBOARD FLAP VANE LEADING EDGE SKIN, OUTBOARD LOCATION. REF: CRJ 200, BOMBARDIER REO 601R-57-52-004, REV-D, DATE: 2012-12-19. EVALUATED AND FOUND TO BE OUT OF LIMITS. REPLACED R/H INBOARD FLAP VANE SKIN, LOCATED AT THE OUTBOARD EDGE. WITH NEW PART REF: BOMBARDIER DRW# 601R14303, REV J, CRJ 200, SRM 51-42-13. COMPLIED WITH 51-900-1003-SKY.

Part: SKIN — CHAFED (RT WING TE FLAP) · airframe 34,764 hrs · 33,747 cycles

* R/H INBOARD FLAP VANE SKIN IS CHAFED AT THE CENTER LEADING EDGE. (C-CHECK RO 5/16/2021) BLENDED CHAFE, BLENDED AREA IS FOUND TO BE OUT OF LIMITS REF REO 601R-57-52-004 REV D DATED 2012-12-19. INSTALLED NEW FLAP VAIN SKIN PN 601R14303-10. REF. CRJ200 SRM 51-42-10 AND DWG 601R14302 REV. D. / COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY

Part: SKIN — CHAFED (RT WING TE FLAP) · airframe 34,764 hrs · 33,747 cycles

* R/H INBOARD FLAP VANE SKIN IS CHAFED AT THE INBOARD SIDE LEADING EDGE. (C-CHECK RO 5/16/2021) REMOVED CHAFE ON R/H I/B FLAP I/B SIDE LEADING EDGE SKIN, & FOUND TO BE OUT OF LIMIT PER REF BOMBARDIER REO 601R-57-52-004, REV -D, DATE 2012-12-19, REMOVED AND REPLACED PART REF CRJ 200 SRM 51-42-13 & REF BOMBARDIER DWG# 601R14303, REV J. SEE CONTINUATION CARD FOR MORE DETAILS. COMPLIED WITH 51-900-1003-SKY.

Part: SKIN — ERODED (RT WING LE) · airframe 34,764 hrs · 33,747 cycles

* RH WING CENTER LEADING EDGE PANEL (630JL) HAS EROSION. (C-CHECK RO 5/16/2021) COMPLIED WITH REO 601R-57-41-1120, REV. --, 2021-04-26 IN ITS ENTIRETY (STEPS 1-5). COMPLIED WITH 51-900-1003-SKY. REMOVED AND INSTALLED R/H WING CENTER L/E PICCOLO TUBE, REF. CRJ200 AMM 30-11-41-400-801. TORQUE WRENCH USED TUC6225, CAL DUE 31-MAR.-22. ALL CHECKS GOOD COMPLIED WITH 51-900-1003-SKY.

Part: SKIN — ERODED (LT WING LE) · airframe 34,764 hrs · 33,747 cycles

* LH WING CENTER LEADING EDGE PANEL (530JL) HAS EROSION. (C-CHECK RO 5/16/2021) REMOVED EROSION DAMAGE ON L/H WING CENTER LEADING EDGE PANEL 530JL REF CRJ 200 SRM 51-12-00. COMPLIED WITH REO 601R-57-41-1119 REV (--) 2021-04-26 STEPS 1-5 DUE TO EROSION DAMAGE REMOVAL BEING OUT OF LIMITS REF CRJ 200 SRM 57-41-31.COMPLIED WITH 51-900-1003-SKY

Part: BULKHEAD WEB — CRACKED (BS 621) · airframe 34,764 hrs · 33,747 cycles

TRANSFER FROM EAML 597316 : TRANSFER FROM EAML 427961 : WHILE PERFORMING THE NDT EDDY CURRENT INSPECTION OF THE AFT PRESS BULHEAD FWD FACE DISCOVERED CRACKS AT STATIONS: / RBL 36.20-WL 103.18 / RBL 27.50-WL 103.68 / RBL 18.00-WL 103.68 / RBL 9.50-WL 103.68 / LBL 18.00-WL 103.18 / LBL 27.50-WL 103.43 / LBL 36.20-WL 103.18 (C-CHECK RO 5/16/2021) REPAIRED 7EA. CRACKED LOCATIONS ON THE FS621 BULKEAD REF. BOMBARDIER REO 601R-53-61-1240 REV -D DATED 2016-10-31. COMPLIED WIWTH 51-900-1003-SKY ADN PRESSURE CHECK GOOD . SEE CONTINUATION CARD FOR DETAILS

Part: BRACKET — FAILED (NLG) · airframe 32,823 hrs · 32,062 cycles

GEAR DISAGREE ON CLIMB OUT RAN QRH AND RETURNED TO FIELD. (FLT#5326) CLOSED REMOVED AND REPLACED BENT NLG CENTERED/EXTENDED PROXIMITY SENSOR BRACKET IAW CMM. ADJUSTED NLG CENTERED/EXTENDED PROXIMITY SENSOR AND PERFORMED GEAR SWINGS IAW AMM. OPS CHECK GOOD.

Part: SELECTOR VALVE — FAILED (NLG) · airframe 32,306 hrs · 31,609 cycles

GEAR DISAGREE AFTER TAKEOFF. NOSE GEAR WOULD NOT RETRACT. (FLT#5749) FO: 03/05/2019 CLOSED REMOVED AND REPLACED NLG SELECTOR VALVE IAW AMM. OPS CHECK GOOD AT THIS TIME. LEAK CHECK GOOD.

Part: LANDING GEAR — ICED (NOSE) · airframe 32,222 hrs · 31,536 cycles

NOSE DOOR AND GEAR DISAGREE MSG ON TAKEOFF. MSG CLEARED AND GEAR CAME UP AFTER 5 SECONDS. NORMAL GEAR EXTENSION AND INDICATIONS ON LANDING. (FLT#5974) PSEU INDICATES ONLY NOSE DOOR SENSORS BEING FLAGGED. TALKED TO AIR CREW AND LEARNED GEAR WAS ICE COVERED PRIOR TO TAKEOFF. ICE ON THE NOSE LANDING GEAR DOORS IS CAUSE. OPERATED THE NOSE LANDING GEAR DOORS SEVERAL TIMES WITH BOTH SYSTEM 3 HYDRAULIC PUMPS INDEPENDENTLY AND COMBINED WITH NO DEFECTS NOTED. AIRCRAFT IS GOOD FOR CONTINUED SERVICE AT THIS TIME.

Part: PROXIMITY SENSOR — FAILED (LANDING GEAR) · airframe 30,851 hrs · 30,307 cycles

WHEN GEAR WAS EXTENDED DURING APPROACH RECEIVED WOW INPUT CAUTION MESSAGE AND A DOWN AND LOCKED 3 GREEN INDICATION. EXECUTED GO AROUND PROCEDURE TO INCLUDE GEAR RETRACTION. COMPLIED WITH QRH. ON SECOND APPROACH GEAR EXTENSION WAS NORMAL. RECEIVED NO WOW INPUT CAUTION MESSAGE AND A DOWN AND LOCKED 3 GREEN INDICATION. (FLT 3265) FO: 07/02/2018 CLOSED REMOVED AND REPLACED UPPER AND WOW SUB-ASSY IAW AMM. PERFORMED RETRACTION/EXTENSION OPERATIONAL TEST. NO FAULTS NOTED.

Part: PRIORITY VALVE — FAILED (NLG) · airframe 30,634 hrs · 30,114 cycles

AFTER TAKE OFF, DURING GEAR RETRACTION, NOSE GEAR FAILED TO RETRACT. NOSE GEAR INDICATION SHOWED DOWN WITH MAINS UP. FOLLOWED QRH PROCEDURE, ALL THREE GEAR SHOWED DOWN AND LOCKED. REMOVED AND REPLACED THE MLG SELECTOR VALVE AND MLG PRIORITY VALVE PN 4619-3, SN 1137B AND LT MLG UP-LOCK PN 17051-101, SN CWDD2346-02. OPS CHECKED GOOD.

Part: UNKNOWN — MALFUNCTIONED (NLG) · airframe 30,517 hrs · 30,004 cycles

AFTER TAKE OFF, DURING GEAR RETRACTION, NOSE GEAR FAILED TO RETRACT. NOSE GEAR INDICATION SHOWED DOWN WITH MAINS UP. FOLLOWED QRH PROCEDURE, ALL 3 GEAR SHOWED DOWN AND LOCKED. (FLT 5195) FO: 05/14/2018 WORK IN PROGRESS.

Part: SKIN — DENTED (FUSELAGE) · airframe 29,924 hrs · 29,473 cycles

RIGHT FUSELAGE SKIN DENTED. APPLIED AERODYNAMIC FILLER TO DENT IAW SRM.

Part: SEAL — CORRODED (PAX DOOR) · airframe 29,924 hrs · 29,473 cycles

CORROSION ON PASSENGER DOOR SEALS. REMOVED CORROSION IAW SRM 51-21-06.

Part: THRUST REVERSER — CHAFED (UNREPORTED ENG) · airframe 29,924 hrs · 29,473 cycles

ENGINE THRUST REVERSER CHAFED. R & R THE THRUST REVERSER IAW AMM.

Part: FLOORBEAM — CORRODED (NOT REPORTED) · airframe 29,924 hrs · 29,473 cycles

CORROSION ON FLOORBEAM. R & R THE FLOORBEAM IAW SRM.

Part: FLOORBEAM — CORRODED (NOT REPORTED) · airframe 29,924 hrs · 29,473 cycles

FLOORBEAM CORRODED. R & R THE FLOORBEAM IAW REO.

Part: FLOOR SUPPORT — CORRODED (NOT REPORTED) · airframe 29,924 hrs · 29,473 cycles

FLOOR SUPPORT CAP CORRODED. R & R THE FLOOR SUPPORT IAW REO.

Part: SKIN — CHAFED (RIGHT AILERON) · airframe 29,924 hrs · 29,473 cycles

RIGHT AILERON SURFACE CHAFED. R & R THE AILERON SKIN IAW SRM.

Part: OIL SYSTEM — OVERSERVICED (RT ENGINE) · airframe 25,833 hrs · 24,962 cycles

HOT RT ENGINE OIL TEMP 170-175 ON DEPARTURE. COMPLIED WITH QRH. TEMP DID NOT DECREASE WITH THRUST REDUCTION. SHUTDOWN RT ENGINE TO COMPLY WITH QRH. LANDING WEIGHT APPROXIMATELY 46,000 LBS RT OIL PRESSURE 50-42 PSI. LANDING A/S 154 KTS, ACFT RETURNED TO DEPARTURE AFTER T/O, EMERGENCY DECLARED. TROUBLESHOT HOT RT ENGINE OIL TEMP IAW FIM 79-20-05 AND ENGINE MANUAL 72-00-00, FOUND ENGINE OVERSERVICED. SERVICED RT ENGINE IAW AMM 12-13-79. OPS AND LEAK CHECK IAW AMM 71-00-00. NO DEFECTS NOTED AT THIS TIME.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 25,726 hrs · 24,851 cycles

FWD RT EMGERGENCY LIGHT INOPERATIVE. TROUBLESHOT AND FOUND FWD RT EMERGENCY LIGHT BULB BLOWN. R & R LAMP IAW AMM 33-51-21-400-801. PERFORMED OPS CHECK OF RT FWD EXTERNAL EMERGENCY LIGHT IAW AMM 33-51-00-710-801. OPS TEST GOOD.

Part: SIGN — MISINSTALLED (CABIN) · airframe 25,717 hrs · 24,843 cycles

LEFT AND RT LIGHTED FLOOR LEVEL EXIT SIGN FOR LT AND RT EMERGENCY OVERWING EXIT INSTALLED ON WRONG SIDE. REMOVED LT & RT LIGHTED EXIT SIGNS BY OVERWING EXITS IAW AMM 33-51-10-000-801. REINSTALLED ON CORRECT SIDES THE LT & RT LIGHTED FLOOR LEVEL EXIT SIGN IAW 33-51-10-400-801. OPS TEST OF LIGHTS IS GOOD.

Part: FITTING — CRACKED (BS 319) · airframe 25,716 hrs · 24,842 cycles

CRACKED FITTING FOUND AT FS 319. REMOVED FITTING AT FS 319, STR 18 RT IAW SRM 51-42-21. LOCATED AND DRILLED FITTING AT FS 319, STR 18 RT IAW SRM TASK 51-40-11. INSTALLED NEW FITTING AT FS 319, STR 18, RT, PN: 601R38335-15 IAW SRM 51-77-00-00 T/R 51-32 AND 51-42-21.

Part: FLOOR SUPPORT — CORRODED (BS 349-364) · airframe 25,717 hrs · 24,843 cycles

RT FLOOR SILL AT FS 349 THROUGH FS 364 IS CORRODED. CUT FLOOR SILL AS SHOWN IN FIG 1 IAW GREO 601R-53-21-2633 AND IAW REO 601R-53-21-326. COMPLIED WITH REO 601R-53-21-2633, REV 10 & REO 601R-53-21-326, REV NC. REO 601R-53-21-2633 HAS BEEN ACCOMPLISHED AND ALL STEPS HAVE BEEN DOCUMENTED AND SIGNED FOR ON A NON-ROUTINE WORK CARD. COMPLIED WITH ECTC REO 601R-53-21-326.

Part: CHANNEL — CRACKED (BS 621-625) · airframe 25,726 hrs · 24,851 cycles

FS 621-FS 625 INTERCOSTAL "V CHANNEL" AT STR 13L IS CRACKED ON OTBD FLANGE THAT ATTACHES TO FUSELAGE SKIN IN AFT END OF RADIUS. REMOVED FS 621-625 INTERCOSTAL U-CHANNEL AT STR 13 IAW SRM'S 51-42-06 AND 51-42-21. INSTALLED QTY 3, HI-LITES IN INTERCOSTAL U-CHANNEL AT STR 13 BETWEEN FS 621-625 IAW SRM TASK 51-42-21. INSTALLED QTY 3 HI-LITES AND 3 SOLID RIVETS IN SERVICEABLE INTERCOSTAL U-CHANNEL AT STG 13L BETWEEN FS 621-625 IAW SRM TASKS 51-42-06 AND 51-42-21.

Part: CHANNEL — CRACKED (BS 409) · airframe 25,717 hrs · 24,843 cycles

INDICATIONS NOTED AT FS 409+128, WL 69.0, RBL 18, CHANNEL 50 PERCENT FULL SCREEN HEIGHT, APPROXIMATELY .200" LONG AND RBL 18 OTBD CHANNEL 50 PERCENT FULL SCREEN HEIGHT .100" LONG IN RADIUS, FAILING NDT INSPECTION. REMOVED FS 409+128 POST IAW SRM 51-42-06. FABRICATED STIFFENER, PN:601R32208-S1101, USING 7075-0 0.063", PO:W34348 IAW SNIEO S11 601R32208, STEP 1. COMPLIED WITH SNIEO 601R32208. FS 409+128 RBL 18 FABBED IAW SNIEO 601R32208. FABRICATED 1 EA 409 POST PN 601R32208-32, USING 7075-0 .063 MATERIAL PO W35756 IAW SNIEO 601R32208, S11, REF STEP 1. COMPLIED WITH EO SNIEO 601R32208 S11. FABRICATED STIFFENER, PN 601R32208-32 IAW SNIEO 601R32208 S11.

Part: INTERCOSTAL — CRACKED (BS 621-625) · airframe 25,717 hrs · 24,843 cycles

FS 621 - 625 INTERCOSTAL "V CHANNEL" AT STR 14L IS CRACKED ON OTBD FLANGE THAT ATTACHES TO FUSELAGE SKIN IN AFT END OF RADIUS. REMOVED "U" CHANNEL AT STR 14L IAW SRM 51-42-21. LOCATED NEW FASTENER HOLES ON NEW SERVICEABLE U-CHANNEL IAW SRM 51-40-11. INSTALLED "U-CHANNEL" IAW SRM 51-40-11. INSTALLED NEW SERVICEABLE U-CHANNEL, INTERCOSTAL AT STR 14L BETWEEN FS 621 AND 625 IAW SRM CH 51-42-21 AND SRM TR 51-32.

Part: CHANNEL — CRACKED (BS 409) · airframe 25,717 hrs · 24,843 cycles

INDICATION NOTED AT FS 409+128, WL 69.0, LBL 18 INBD CHANNEL 55 PERCENT FULL SCREEN HEIGHT APPROXIMATELY .250" LENGTH IN RADIUS, FAILING NDT. REMOVED POST ASSEMBLY AT FS 409+128 LBL 19 IAW SRM 51-42-06. INSTALLED POST ASSY AT FS 409+128, LBL 18 IAW SRM TASK 51-42-06 AND 601R-53-41-889. UPON FURTHER INVESTIGATION, FOUND OTBD CHANNEL AT FS 409+128, LBL 18 TO BE GOUGED IN MULTIPLE PLACES, REQUIRES REPLACEMENT. LOCATED AND DRILLED INBD CHANNEL, PN:601R32208-31S AND OTBD CHANNEL, PN:601R32208-155 IAW SRM 51-40-11. COMPLIED WITH EC/TC REO:601R-53-41-889 AND MET ALL REQUIREMENTS OF REO:601R-53-41-889, REV A.

Part: BULKHEAD WEB — CRACKED (BS 621) · airframe 25,717 hrs · 24,843 cycles

REAR PRESSURE BULKHEAD WEB THAT SURROUNDS THE LINTEL ATTACHMENT FITTING, HAS INDICATION NOTED, APPROXIMATELY .500" IN LENGTH 90 PERCENT FSH FAILED NDT INSPECTION. COMPLIED WITH EC/TC REO 601R-53-61-1230 & GREO 601R-53-61-1230, REV F.

Part: BULKHEAD WEB — CRACKED (BS 621) · airframe 25,717 hrs · 24,843 cycles

REAR PRESSURE BULKHEAD WEB HAS INDICATIONS NOTED AT BL 0.0, WL 112, APPROXIMATELY 3.0" IN LENGTH, 50 PERCENT FSH FAILED NDT INSPECTION. COMPLIED REO 601R-53-61-1285. FINISHED REPAIR PART IAW REO 601R-53-61-1285. COMPLIED WITH REO 601R-53-61-1285. REMOVED STIFFENING ANGLE FROM FWD SIDE OF PRESSURE BULKHEAD ALONG WATER LINE 120.43 IAW SRM 51-42-06 TO PERFORM REO 601R-53-61-1285. INSTALLED SAME SERVICEABLE STIFFENING ANGLE ON FWD SIDE OF PRESSURE BULKHEAD ALONG WL 120.43 IAW REO 601R-53-61-5508, 601R-53-61-1285. R & R 6 EACH FASTENERS IAW SRM 51-42-22. PAINTED REPAIR AREA IAW STEP 6 OF REO 601R-53-61-1285. COMPLIED WITH EC/TC REO 601R-53-61-1285 AND GREO 601R-53-61-1285, REV D.

Part: ANGLE — CORRODED · airframe 25,726 hrs · 24,851 cycles

SERVICE DOOR LOWER SILL ANGLE HAS SEVERAL AREAS OF CORROSION. REMOVED UNSERVICEABLE SERVICE DOOR LOWER SILL ANGLE, PN:601R38303-253 IAW SRM 51-42-13, 51-42-06 AND 51-42-21. LOCATED AND DRILLED NEW SERVICEABLE SERVICE DOOR LOWER SILL ANGLE, PN:601R38303-253 IAW SRM 51-40-11. INSTALLED NEW SERVICEABLE LOWER SILL ANGLE IAW SRM 51-42-06-00, 51-42-21-00, 51-42-11-00, 51-42-34-00 AND 51-77-00-00.

Part: SEAT TRACK — CORRODED (BS 398-409) · airframe 25,716 hrs · 24,842 cycles

IN PASSENGER COMPARTMENT, THE LT FLOOR SEAT TRACK AT SEVERAL LOCATIONS FROM FS 398.00 TO FS 409.00+124 HAS PITTING CORROSION. REMOVED UNSERVICEABLE CORRODED SEAT TRACK, FOUND TO BE OUT OF LIMITS, REQUIRED REPLACEMENT IAW SRM 53-21-49. FABRICATED NEW SERVICEABLE SEAT TRACK, PN N126-2075 IAW GREO 601R-53-00-485. LOCATED & DRILLED NEW SERVICEABLE SEAT TRACK, PN 601R-53-00-485-1 IAW AMM 53-01-11-400-802. FABRICATED SEAT TRACKS IAW GREO 601R-53-00-485, REV A.

Part: STRAP — CORRODED (BS 559) · airframe 25,716 hrs · 24,842 cycles

IN PASSENGER COMPARTMENT, UNDER FLOORBOARD, RT SIDE AT FS 559.00 BETWEEN RBL 27.00 TO RBL 45.00. THE FLOORBOARD ATTACHMENT STRAP HAS PITTING CORROSION. BLENDED OUT APPROXIMATELY .004" AT DAMAGE IAW SRM 53-41-43 AND 53-00-00, FIG 102, .046" OF MATERIAL REMAINING. ALODINED, PRIMED AND PAINTED REPAIR AREA IAW SRM 51-25-06 AND 51-25-16.

Part: SEAT TRACK — CORRODED (BS 364-398) · airframe 25,716 hrs · 24,842 cycles

IN PASSENGER COMPARTMENT THE RT FLOOR SEAT TRACK AT SEVERAL LOCATIONS FROM FS 364.00 TO FS 398.00 HAS PITTING CORROSION. REMOVED UNSERVICEABLE CORRODED SEAT TRACK, FOUND TO BE OUT OF LIMITS. REQUIRED REPLACEMENT IAW SRM 53-21-49, AMM 53-01-11 AT LOCATION FROM FS 364.00 TO FS 398.00. INSTALLED NEW SERVICEABLE SEAT RAIL AT FS 364.00 TO FS 398.00 RT SIDE IAW AMM 53-01-11-400-802. LOCATED & DRILLED NEW SERVICEABLE SEAT TRACK, PN N126-2075 IAW SRM 51-40-11. REPLACED NEW SERVICEABLE SEAT TRACK, PN N126-20752 IAW GREO 601R-53-00-485. FABRICATED SEAT RAILS IAW GREO 601R-53-00-485, REV A.

Part: FLOOR SUPPORT — CORRODED (CARGO BAY) · airframe 25,717 hrs · 24,843 cycles

CARGO BY LT FLOOR SILL HAS NUMEROUS AREAS OF CORROSION, FILIFORM. UPON REMOVAL OF CORROSION & FURTHER INVESTIGATION, FOUND SILL TO BE OUT OF LIMITS IAW SRM 53-00-00 AND LIMITS REF IN GREO 601R-53-00-526. REMOVED UNSERVICEABLE SILL IAW SRM 51-42-06, 51-42-21. COMPLETED IAW REO 601R-53-61-593, REV A DATED 2005/06/21. RECEIVED SERVICEABLE FLOOR LANDING NR 601R35011-63, REQ LOCATE & DRILL. LOCATED & DRILLED SERVICEABLE LANDING IAW SRM 51-40-11. INSTALLED FLOOR LANDING IAW REO STEPS 7-8 601R-53-61-593. COMPLIED WITH EC/TC REO 601R-53-61-593 IAW REO 601R-53-61-593.

Part: FLOOR SUPPORT — CORRODED (BS 424-535) · airframe 25,716 hrs · 24,842 cycles

IN PASSENGER COMPARTMENT UNDER FLOORBOARDS, THE LT PRESSURE FLOOR SILL FROM FS 424.00 TO FS 535.00 BETWEEN LBL 36.00 TO LBL 45.00. THE FLOOR SKIN AND FINGER WEB'S AT SEVERAL LOCATIONS HAVE PITTING CORROSION. BLENDED OUT SEVERAL AREAS OF CORROSION ON THE LT FLOOR SILL PANEL AREA, APPROXIMATELY .005" TO .010" OF DAMAGE REMOVED APPROXIMATELY .045" TO .050" OF MATERIAL REMAINING, BLENDED IAW REO 601R-53-41-666, REV C, STEPS 1.2, A-B. BLENDED SEVERAL AREAS OF CORROSION ON THE LT FLOOR SILL ANGLE, APRROXIMATELY .005" TO .020" OF DAMAGE REMOVED. APPROXIMATELY .060" TO .075" OF MATERIAL REMAINING. BLENDED IAW REO 601R-53-41-666, REV C, STEPS 2.2, A-B. C/W ECTC REO 601R-53-41-666, REV C.

Part: SEAT TRACK — CORRODED (BS 398-409) · airframe 25,716 hrs · 24,842 cycles

IN PASSENGER COMPARTMENT THE RT FLOOR SEAT TRACK AT SEVERAL LOCATIONS FROM FS 398.00 TO FS 409.00+124 HAS PITTING CORROSION. REMOVED UNSERVICEABLE CORRODED SEAT RAIL. FOUND TO BE OUT OF LIMITS. REQUIRED REPLACEMENT IAW SRM 53-21-49. FABRICATED NEW SERVICEABLE SEAT TRACK FROM N126-2075 MATERIAL IAW GREO 601R-53-00-485. DRILLED, LOCATED & INSTALLED NEW SERVICEABLE SEAT TRACK, PN 601R-53-00-485-1 IAW AMM 53-00-11-400-802. FABRICATED SEAT TRACK IAW GREO 601R-53-00-485, REV A.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 25,716 hrs · 24,842 cycles

INBD AND OTBD RBL 9 CLIPS ARE CRACKED AT FS 280.00. REMOVED INBD & OTBD CLIPS AT RBL 9, FS 280.00 IAW SRM 51-42-21. INSTALLED NEW INBD & OTBD CLIPS AT FS 280 RBL 9 IAW SRM 51-42-21 & 51-77-00-00 T/R 51-32. DRILLED & LOCATED, 2 EA, CLIPS OTBD & INBD IAW SRM 51-40-11.

Part: ATTACH ANGLE — CRACKED (BS 484) · airframe 25,716 hrs · 24,842 cycles

IN PASSENGER COMPARTMENT UNDER FLOORBOARDS AT FS 484.00 ON RBL 27.00, THE INTERCOSTAL ATTACHMENT ANGLE IS CRACKED. REMOVED ANGLE AT FS 484.0 RT RBL 27.00 IAW SRM 51-42-06. INSTALLED ANGLE AT FS 484.0, RBL 27.00 IAW SRM 51-42-21 AND 51-40-11.

Part: ANGLE — CRACKED (BS 484) · airframe 25,717 hrs · 24,843 cycles

IN PASSENGER COMPARTMENT UNDER FLOORBOARDS AT FS 484.00 ON LBL 36.00, THE INTERCOSTAL PEVIOUS REPAIR ATTACHMENT ANGLE IS CRACKED. C/W REO 601R-53-41-1917. REO 601R-53-41-1917 HAS BEEN ACCOMPLISHED.

Part: NOT REPORTED — CORRODED (BS 280) · airframe 25,716 hrs · 24,842 cycles

FS 280.00 IS CORRODED BETWEEN RBL 9-LBL 9. EVALUATED CORROSION AND FOUND CORROSION ON AFT J-CHANNEL WHICH WAS FOUND TO BE HEAVILY CORRODED AND PITTED AND REQUIRES REPAIR/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 REQUIREMENTS. COMPLIED WITH THE FABRICATION OF ATTACHMENT PARTS EO 600-53-91, C/W 01 IAW EO 600-53-91, CW AND MEETS ALL ITS REQUIREMENTS.

Part: CHANNEL — CORRODED (BS 280) · airframe 25,716 hrs · 24,842 cycles

FWD FS 280.00 J-CHANNEL IS CORRODED BETWEEN LBL 9-RBL 9. REMOVED FWD J-CHANNEL FROM FS 280, LBL 9 - RBL IAW SRM 51-42-06, FOUND TO BE HEAVILY PITTED, CORRODED & REQUIRES REPLACEMENT. DRILLED & LOCATED NEW FWD J-CHANNEL, 600-34017-21 IAW SRM 51-+40-11 & 51-40-06. INSTALLED NEW FWD J-CHANNEL IAW SRM 51-42-06 & 51-77-00-00, TR 51-32.

Part: SEAT TRACK — CORRODED (BS 364-398) · airframe 25,716 hrs · 24,842 cycles

IN PASSENGER COMPARTMENT THE LT FLOOR SEAT TRACK AT SEVERAL LOCATIONS FROM FS 364.00 TO FS 398.00 HAS PITTING CORROSION. REMOVED UNSERVICEABLE CORRODED SEAT RAIL AT FS 364.00 TO FS 398.00 LT, FOUND TO BE OUT OF LIMITS, REQ REPLACEMENT IAW SRM 53-21-49, AMM 53-01-11. INSTALLED NEW SERVICEABLE SEAT TRACK AT FS 364.00 TO FS 398.00 LT SIDE IAW AMM 53-01-11-400-802. LOCATED & DRILLED NEW SERVICEABLE SEAT TRACK, PN N126-2075 IAW SRM 51-40-11. REPLACED NEW SERVICEABLE SEAT TRACK, PN N126-2075 IAW GEN REO 601R-53-00-485. FABRICATED SEAT RAILS IAW GREO 601R-53-00-485, REV A.

Part: DOOR SILL — CORRODED (PAX DOORWAY) · airframe 25,717 hrs · 24,843 cycles

PAX DOOR LOWER SILL IS CORRODED. REMOVED PAX DOOR LOWER SILL ASSY IAW SRM 51-42-21, 51-41-00 AND 51-42-06. LOCATED & DRILLED NEW LOWER SILL ASSY IAW SRM 51-40-11-00. INSTALLED NEW LOWER SILL, PN 601R31527-221 IAW SRM 51-42-21, 51-42-06 AND 51-42-10. UPON REMOVAL OF LOWER SILL, FOUND 2 EA BRACKET CONNECTORS CRACKED DUE TO INTERGRANULAR CORROSION. LOCATED, DRILLED AND INSTALLED SERVICEABLE CONNECTOR BRACKET IAW SRM 51-42-06. INSTALLED 2 EA FASTENERS IN PAX DOOR LOWER SILL IAW SRM 51-41-00. INSTALLED NEW SERVICEABLE CONNECTOR BRACKET IAW SRM 51-42-06-00.

Part: CROSSBEAM — CORRODED (BS 349) · airframe 25,717 hrs · 24,843 cycles

CORROSION AT FS 349.00 AT SERVICE DOOR ON CROSSBEAM. COMPLIED WITH REO 601R-53-21-2635. COMPLIED WITH REO 601R-53-21-2635. REO 601R-53-21-2635 HAS BEEN ACCOMPLISHED.

Part: FRAME — CORRODED (BS 333) · airframe 25,716 hrs · 24,842 cycles

CORROSION ON FRAME AT FS 333.00 BETWEEN STR 25R AND 25L. FOUND LIGHT SURFACE CORROSION ON FRAME AT FS 333 FLANGE BETWEEN STR 26L-STR 27. REMOVED 6 OFF RIVETS IAW SRM 51-42-06 COMMON TO THIS AREA. REMOVED LIGHT SURFACE CORROSION FROM FRAME AT FS 333 ALONG FLANGE STR 26L - STR 27 USING SCOTCH PAD. NO PITTING FOUND IAW SRM 51-21-06, ITEM 3.

Part: ANGLE — CRACKED (BS 280) · airframe 25,716 hrs · 24,842 cycles

STGR 3L INBD ANGLE IS CRACKED AT FS 280.00. REMOVED CRACKED ANGLE. LOCATED AND DRILLED NEW PART IAW SRM 51-40-11, 51-42-06 AND 51-42-21. INSTALLED NEW ANGLE, PN:600-31057-19 IAW SRM 51-42-06, 51-42-21 AND TR 51-32.

Part: STRAP — CORRODED (BS 559) · airframe 25,716 hrs · 24,842 cycles

IN PASSENGER COMPARTMENT UNDER FLOORBOARDS, LT SIDE AT FS 559.00 BETWEEN LBL 27.00 TO LBL 45.00. THE FLOORBOARD ATTACHMENT STRAP HAS PITTING CORROSION. BLENDED OUT APPROXIMATELY .004" AT DAMAGE IAW SRM 53-41-43 AND 53-00-00, FIG 102. .046" OF MATERIAL REMAINING. ALODINED, PRIMED AND PAINTED REPAIR AREA IAW SRM 51-25-06 AND 51-25-16.

Part: SEAT TRACK — CORRODED (BS 409-559) · airframe 25,716 hrs · 24,842 cycles

IN PASSENGER COMPARTMENT THE RT FLOOR SEAT TRACK AT SEVERAL LOCATIONS FROM FS 409.00+124 TO FS 559.00+4 HAS PITTING CORROSION. REMOVED UNSERVICEABLE CORRODED SEAT RAIL. FOUND TO BE OUT OF LIMITS. REQUIRED REPLACEMENT IAW SRM 53-21-49. FABRICATED NEW SERVICEABLE SEAT TRACK FROM N126-2075 MATERIAL IAW GREO 601R-53-00-485. DRILLED, LOCATED & INSTALLED NEW SERVICEABLE SEAT RAIL, PN 601R-53-00-485-1 IAW AMM 53-00-11-400-802. FABRICATED SEAT RAILS GREO 601R-53-00-485, REV A.

Part: FLOOR SUPPORT — CORRODED (BS 422-548) · airframe 25,716 hrs · 24,842 cycles

IN PASSENGER COMPARTMENT UNDER FLOORBOARDS, THE RT PRESSURE FLOOR SILL FROM FS 422.00 TO FS 548.00 BETWEEN RBL 36.00 TO RBL 45.00. THE FLOOR SKIN AND FINGER WEBS AT SEVERAL LOCATIONS HAVE PITTING CORROSION. BLENDED OUT SEVERAL AREAS OF CORROSION ON THE RT FLOOR SILL PANEL AREA, APPROXIMATELY .005" TO .010" OF DAMAGE REMOVED APPROXIMTELY .045" TO .050" OF MATERIAL REMAINING, BLENDED IAW REO 601R-53-41-666, REV C, STEPS 1.2, A-B. BLENDED SEVERAL AREAS OF CORROSION ON THE RT FLOOR SILL ANGLE, APRROXIMATELY .005" TO .020" OF DAMAGE REMOVED. APPROXIMATELY .060" TO .075" OF MATERIAL REMAINING. BLENDED IAW REO 601R-53-41-666, REV C, STEPS 2.2, A-B. C/W ECTC REO 601R-53-41-666 AND REO 601R-53-41-666, REV C.

Part: ANGLE — CRACKED (BS 280) · airframe 25,726 hrs · 24,851 cycles

INBD AND OTBD LBL 9 CLIPS ARE CRACKED AT FS 280.00. REMOVED INBD AND OTBD CLIPS AT LBL 9 FS 280.00 IAW SRM 51-42-21. INSTALLED NEW INBD AND OTBD CLIPS AT FS 280, LBL 9 IAW SRM 51-42-21 AND 51-77-00-00, TR 51-32. LOCATED AND DRILLED 2 EA CLIPS INBD AND OTBD IAW SRM 51-40-11.

Part: TUBE — DETERIORATED (SERVICE DOOR) · airframe 25,716 hrs · 24,842 cycles

SERVICE WIRE HARNESS TUBE IS TORN AND HAS PIECES MISSING. COMPLIED WITH EC/TC REO 601R-52-70-008 01 FOR THE PERMANENT, ALTERNATE REPAIR OF REO 601R-52-70-008.

Part: GLOWSTRIP — NOT REPORTED · airframe 25,726 hrs · 24,851 cycles

PHOTOLUMINESCENT, NEED TO BE REPLACED ZONE 242 RT. REPLACED PHOTOLUMINESCENT, PN PL22-300LH00 IAW AMM 33-51-01-400-806.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 25,538 hrs · 24,657 cycles

EXTERIOR EMERGENCY LIGHT NR 1 INOPERATIVE. REPLACED THE LAMPS IAW AMM 33-51-21. SYSTEM OPS CHECKED GOOD. NO FURTHER ACTION.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 25,188 hrs · 24,312 cycles

L/H SIDE EMERGENCY LIGHT OVER THE WING INOPERATIVE. RELAMPED THE LT SIDE EMERGENCY LIGHT IAW AMM 33-51-21. OPS CHECK GOOD.

Part: STRUCTURE — DAMAGED (LT MLG WW) · airframe 24,213 hrs · 23,337 cycles

DURING GEAR RETRACTION AND EXTENSION, FOUND LT MLG WHEEL WELL DAMAGED. REPAIRED IAW EA 20-2014-157 P1.

Part: DIODE — FAILED (EMERGENCY LIGHTS) · airframe 23,324 hrs · 22,444 cycles

DIODE CR4LF BROKEN. R & R DIODE IAW ESPM 20-16-00. OPS TESTED EMERGENCY EXTERIOR LIGHT IAW AMM 33-51-00. OPS CHECKED GOOD.

Part: BULKHEAD — CRACKED (AFT PRESSURE) · airframe 23,316 hrs · 22,435 cycles

AFT PRESSURE BULKHEAD CRACKED AT LBL 27.50, WL 130, ONE INCH ABOVE DOOR TRACK AND EXTENDING UNDER TRACK.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 22,396 hrs · 21,483 cycles

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

Part: ENGINE — OVERTEMP (RIGHT) · airframe 21,708 hrs · 20,764 cycles

AFTER TAKEOFF, RT ENGINE REACHED APPROX 926, N1 WAS SET AT .91-4. TARGET WAS 91-5 POWER WAS REDUCED & RECREASED INTO NORMAL RANGE. RETURNED TO DEPARTURE, EMERGENCY DECLARED. R & R RT ENGINE ASSY OPS AND LEAK CHECKED GOOD.

Part: FITTING — CRACKED (BS 460) · airframe 21,541 hrs · 20,583 cycles

RT FS 460 FLOOR SUPPORT FITTING, CRACKED AND TOP ATTACH RIVET SHEARED OFF AT OTBD SIDE OF RBL 9. REMOVED CRACKED FLOOR SUPPORT FITTING IAW SRM 51-42-06 AND 51-42-21. LOCATED, DRILLED AND INSTALLED NEW SERVICEABLE 460 SUPPORT FITTING IAW SRM 51-40-11, 51-42-06 AND 51-42-21.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 21,540 hrs · 20,582 cycles

CARGO TRACKS FROM FS 559+110 TO FS 559+122 AT LBL 9 AND RBL 9 ARE CORRODED BEYOND ALLOWABLE LIMITS IAW SRM 53-61-49. R & R CORRODED CARGO TRACKS WITH NEW SERVICEABLE TRACKS IAW SRM 51-40-11 & 51-41-04.

Part: ANGLE — CRACKED (BS 484) · airframe 21,533 hrs · 20,575 cycles

RIGHT SIDE FS 484.00 INTERCOSTAL ANGLE AT RBL 36.0 PREVIOUS REPAIR IS CRACKED IN UPPER END OF RADIUS APPROX 1.2" LONG. REMOVED DAMAGED ANGLE IAW SRM 51-42-21. FABRICATED NEW ANGLE IAW STEPS 5 AND 6 OF REO 601R-53-41-059 AND INSTALLED IAW SRM 51-42-21. REPAIRED IAW REO 601R-53-41-059, REV B.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 21,540 hrs · 20,582 cycles

CARGO TRACKS FROM FS 559+86 TO 559+96 AT LBL 9 AND RBL 9 ARE CORRODED BEYOND ALLOWABLE LIMITS IAW SRM 53-61-49. R & R CORRODED CARGO TRACKS WITH NEW SERVICEABLE TRACKS IAW SRM 51-40-11 & 51-41-04.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 21,540 hrs · 20,582 cycles

CARGO TRACKS FROM FS 559+78 TO 559+96 AT LBL 27 AND RBL 27 ARE CORRODED BEYOND ALLOWABLE LIMITS IAW SRM 53-61-49. R & R CORRODED CARGO TRACKS WITH NEW SERVICEABLE CARGO TRACKS IAW SRM 51-40-11 & 51-41-04.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 21,541 hrs · 20,583 cycles

CARGO TRACK FROM FS 612 TO 617 AT LBL 9 IS CORRODED BEYOND ALLOWABLE LIMITS IAW SRM 53-61-49. R & R CORRODED CARGO TRACK WITH NEW SERVICEABLE TRACKS IAW SRM 51-40-11 & 51-41-04.

Part: WEB — CRACKED (BS 193) · airframe 21,533 hrs · 20,575 cycles

WEB IS CRACKED AT FS 193.0 STRINGER 16A IN LT AFT OTBD SIDE OF TRU BAY. CRACK IS APPROX 1 INCH LONG. REPAIRED IAW GREO 601R-53-11-111.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 21,533 hrs · 20,575 cycles

PHOTOLUMINESCENT FLOOR TRACK LIGHTING CABIN ILLUMINATION FAILED FUNCTIONAL TEST. MEASURED AVERAGE OF LH 3 LUX, RT 3.5 LUX, MINIMUM OF 12 LUX REQUIRED. R & R ALL CABIN CEILING AND SIDEWALL LIGHT BULBS WITH NEW SERVICEABLE LIGHT BULBS (PN BR9805-007) IAW AMM 33-21-01-400-801 AND AMM 33-21-07-400-801. PERFORMED OPS TEST OF CABIN CEILING AND SIDEWALL LIGHTS IAW AMM 33-21-01-400-801. TESTED GOOD AT THIS TIME.

Part: BULB — BURNED OUT (LIGHT SWITCH) · airframe 21,319 hrs · 20,358 cycles

EMERGENCY LIGHT INOPERATIVE IN OVERHEAD. R & R EMERGENCY LIGHT SWITCH BULBS IAW ESPM 20-24-00. NO FURTHER DEFECT NOTED.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 20,938 hrs · 19,970 cycles

LT 1 EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED LT NR 1 EXTERIOR EMERGENCY LIGHT BULB IAW AMM 33-51-21. OP CHECKED GOOD.

Part: SIGN — DAMAGED (CABIN) · airframe 20,938 hrs · 19,970 cycles

EMERGENCY EXIT FLOOR FLOOD LIGHT DAMAGED AT SERVICE DOOR. REPLACED SERVICE DOOR LIGHTED EXIT SIGN IAW AMM 33-51-10. OPS CHECKED GOOD.

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 20,753 hrs · 19,782 cycles

CAPTAIN'S FLASHLIGHT INOPERATIVE. INSTALLED NEW BATTERY IN CAPTAIN'S FLASHLIGHT IAW AMM 25-60-00.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 20,186 hrs · 19,148 cycles

NR 5 EXTERIOR EMERGENCY LIGHT IS INOPERATIVE. RELAMPED EXTERIOR EMERGENCY LIGHT IAW AMM 33-51-21. OPS CHECKED GOOD.

Part: WIRE — DISCONNECTED (EMERGENCY LIGHT) · airframe 19,665 hrs · 18,563 cycles

F/A REPORTS LOOSE WIRE UNDER JUMPSEAT IN CLOSET. RESECURED EMERGENCY LIGHT WIRES UNDER F/A'S SEAT IAW AMM 33-51-10. OPS CHECKED GOOD.

Part: LIGHT — DISLODGED (CABIN) · airframe 19,289 hrs · 18,157 cycles

FLOOR LEVEL EMERGENCY EXIT LIGHT POPPED LOOSE ON FLOOR NET TO FORWARD CABIN DOOR. R & R FLOODLIGHT, FLOOR-LEVEL EMERGENCY. "BASE" IAW AMM 33-51-19. OPS CHECKED OK.

Part: UNKNOWN — ODOR (CABIN) · airframe 18,756 hrs · 17,580 cycles

F/A REPORTED STRONG ALCOHOL SMELL OR CHEMICAL ODOR COMING FROM ROW 9. EMERGENCY DECLARED AND RAN NR 1 & 2 ENGINES IAW AMM 71-00-00. OPS CHECKED BOTH PACKS ON ENGINES AND APU IAW AMM 21-50-00. NO DEFECTS NOTED.

Part: ELEMENT — MALFUNCTIONED · airframe 18,062 hrs · 16,830 cycles

LT 14TH STG DUCT PRIOR TO DECENT CW QRH MESSAGE DID NOT GO OUT IN THE DESIGNATED TIME PERIOD. EMERGENCY DECLARED AS A PRECAUTION. R & R LT 14TH STAGE PYLON LOOP ELEMENT ASSY IAW AMM 36-21-04, PERFORMED 2 HIGH POWER ENGINE RUNS OPERATIONALLY CHECKED LT 14TH STAGE LOOPS OPS CHECK GOOD AT THIS TIME. NO WARNING MESSAGES AT THIS TIME, A/C OK FOR SERVICE.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 17,193 hrs · 15,886 cycles

LT NR 2 EXT EMERGENCY LIGHT INOP. FOUND BROKEN WIRE AT DIODE CR2LF. R & R DIODE CR2LF IAW ESPM 20-16-00. CHECKS GOOD IAW AMM 33-51-00.

Part: FUSE — BLOWN (EMERGENCY LIGHT) · airframe 17,193 hrs · 15,886 cycles

WORKING DMIL 599378-2, LEFT NR 2 EXTERIOR EMERGENCY LIGHT INOP. R & R FUSE AT PS2LF AND PS3LF IAW VCMM 33-21-70. OPS IAW AMM 33-51-00 GOOD. DMIL CLEARED/PLACARD REMOVED.

Part: FUSE — BLOWN (EMERGENCY LIGHT) · airframe 17,193 hrs · 15,886 cycles

LT NR 2 EXTERIOR EMERGENCY LIGHT INOP. (EXTERIOR EMERGENCY LIGHTS - ACFT NOT OPERATED AT NIGHT) R & R FUSE AT PS2LF AND PS3LF IAW VCMM 33-21-70. OPS IAW AMM 33-51-00 GOOD. DMIL CLEARED/PLACARD REMOVED. (CLOSED)

Part: ATTACH FITTING — CORRODED (PAX DOOR) · airframe 16,522 hrs · 15,106 cycles

CLIP AT FS 336 ON BOTTOM OF PAX DOOR IS CORRODED. R & R CORRODED CLIP IAW SRM 51-40-11, 51-42-06, AND 51-42-21 SEE FORM 412 FOR FABRICATION AND INSTALLATION DETAILS.

Part: ATTACH FITTING — CORRODED (PAX DOOR) · airframe 16,522 hrs · 15,106 cycles

CLIP AT FS 321 ON BOTTOM OF PAX DOOR IS CORRODED. R & R CORRODED CLIP IAW SRM 51-40-11, 51-42-06, AND 51-42-21. SEE FORM 412 FOR FABRICATION AND INSTALLATION DETAILS.

Part: ATTACH FITTING — CORRODED (PAX DOOR) · airframe 16,522 hrs · 15,106 cycles

CLIP AT FS 322 ON BOTTOM OF PAX DOOR IS CORRODED. R & R CORRODED CLIP IAW SRM 51-40-11, 51-42-06, AND 51-42-21. SEE FORM 412 FOR FABRICATION AND INSTALLATION DETAILS.

Part: SKIN — CRACKED (PAX DOOR) · airframe 16,522 hrs · 15,106 cycles

PAX DOOR INNER SKIN TO STAIR SUPPORT AFT DRAG ANGLE IS CRACKED. REPAIRED AFT DRAG ANGLE IAW REO 601R-52-11-513. C/W ASA EC/TC REO 601R-52-11-513.

Part: RIB — CRACKED (RT WING WW) · airframe 16,522 hrs · 15,106 cycles

BATTERY RIB IN RT W/W IS CRACKED. REPAIRED BATTERY BIB RT IAW REO 601R-57-51-046, REV B. AND EC/TC 601R-57-51-046.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 16,522 hrs · 15,106 cycles

RT NR 1 FLOOR SEAT TRACK HAS FLAKING CORROSION. REMOVED DAMAGED SEAT FLOOR TRACK LOCATED DRILLED AND INSTALLED SERVICABLE FLOOR TRACK RT NR1 IAW SRM 51-40-11 AND AMM 53-01-11.

Part: INTERCOSTAL — CRACKED (BS 621-625) · airframe 16,522 hrs · 15,106 cycles

RT SIDE INTERCOSTAL LOCATED BETWEEN THE 621 BULKHEAD AND 625 IS CRACKED. REMOVED CRACKED PART RT SIDE INTERCOSTAL BETWEEN 621 BULKHEAD AND 625 IAW SRM 51-41-02. FABRICATED PART IAW SRM 53-61-17 PG. 3 FIG 1. TREATED AND PRIMED AND APPLIED TOPCOAT IAW SRM 51-21-11. INSTALLED PART IAW SRM 51-41-02.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 16,522 hrs · 15,106 cycles

FOUND CRACK INDICATION APPROX .2500" IN LENGTH AT WL 58.7 AND RBL 9. COMPLIED WITH EC/TC REO 601R-53-41-260 AND REO 601R-53-41-260 REV E AND COMPLIED WITH EC/TC REO 601R-53-41-609 OR AND MET ALL THE REQUIREMENTS OF REO 601R-53-41-609 REV B (SHEET 3 TO 11 REV A) FOR DEVIATION E.

Part: ISOLATOR — CRACKED (BS 621 BULKHEAD) · airframe 16,522 hrs · 15,106 cycles

AFT PRESSURE BULKHEAD HAS 5 ISOLATORS WITH CRACKS. REMOVED UNSERVICEABLE NR5 ISOLATORS FROM 621AFT PRESSURE BULKHEAD AND INSTALLED SERVICEABLE 5 EA ISOLATORS IAW SRM 51-42-06.

Part: RIB — CRACKED (LT WING WW) · airframe 16,522 hrs · 15,106 cycles

BATTERY RIB IN LT W/W IS CRACKED. REPAIRED BATTERY RIB IN LT W/W WHICH WAS CRACKED IAW REO 601R-57-51-046, REPAIR NR 2.

Part: SKIN — CORRODED (FUSELAGE) · airframe 16,522 hrs · 15,106 cycles

EXTERIOR SKIN AT LOWER AFT CORNER OF PAX DOOR CUTOUT HAS CORROSION. REPAIRED EXTERIOR SKIN AT LOWER AFT CORNER OF PAX DOOR CUTOUT, BLENDED TO WITHIN SERVICEABLE LIMITS IAW SRM 51-21-06 AND SRM 53-00-31.

Part: HANDLE — OUT OF ADJUST (PAX DOOR) · airframe 16,522 hrs · 15,106 cycles

PAX DOOR FAILED FUNCTIONAL TEST ON HANDLE FORCE AND OPENING TIME. ADJUSTED PAX DOOR INNER HANDLE IAW AMM SUBTASK 52-11-25-820-003, STEPS AC.1 THRU 7 AND REACCOMPLISHED FUNCTIONAL TEST IAW AMM 52-11-00-720-802. NO DEFECTS NOTED.

Part: PLACARD — DETERIORATED (CABIN) · airframe 16,348 hrs · 14,920 cycles

PAX DOOR EXIT PLACARD DETERIORATED. R & R PAX DOOR EXIT PLACARD IAW AMM 11-30-02. OK FOR SVC. R & R PAX DOOR EXIT PLACARD IAW AMM 11-30-02. OK FOR SVC. (CLOSED)

Part: BULB — BURNED OUT (EMERGENCY LIGHTS) · airframe 16,348 hrs · 14,920 cycles

LT 2 EXTERNAL EMERGENCY LIGHT INOP. R & R LT NR 2 EXTERNAL EMERGENCY LIGHT BULB IAW AMM 33-51-21. OPS CHECK GOOD. ITEM: 1 R & R LT NR 2 EXTERNAL EMERGENCY LIGHT BULB IAW AMM 33-51-21. OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (LT OVERWING) · airframe 15,831 hrs · 14,320 cycles

LEFT OVERWING NR 4 EXTERIOR EMERGENCY LIGHT INOP. REMOVED AND REPLACED LT OVERWING NR 4 EXTERIOR EMERGENCY LIGHT IAW AMM 33-51-21. OPS CHECK GOOD.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 14,951 hrs · 13,323 cycles

F/O FLASHLIGHT INOP.

Part: ANCHOR FITTING — CRACKED (PAX DOOR) · airframe 14,784 hrs · 13,125 cycles

PAX DOOR FWD ANCHOR FITTING CRACKED. INSTALLED NEW PAX DOOR FWD ANCHOR FITTING IAW EC/TC EO600-52-66 C/W. REMOVED PAX DOOR FWD ANCHOR FITTING IAW AMM 52-11-17. INSTALLED NEW PAX DOOR FWD ANCHOR FITTING IAW EC/TC EO600-52-66 C/W.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 13,769 hrs · 12,104 cycles

FOUND CRACK ON 202 PRESS BULKHEAD AT PARKING BRAKE CABLE. REPAIRED IAW EC/TC EO600-53-217.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 13,093 hrs · 11,497 cycles

WITH THE EMERGENCY LIGHTS SWITCH IN THE OFF POS SOME OF THE EMERGENCY LIGHTS STAY ON WHEN POWER IS TURNED OFF.

Part: SUPPORT BEAM — CRACKED (CARGO BAY) · airframe 12,880 hrs · 11,308 cycles

CARGO DOOR SUPPORT BEAM LOWER ANGLE IS CRACKED APPROX 1.3 INCH IN LENGTH.

Part: ANGLE — CRACKED (PAX DOOR) · airframe 12,880 hrs · 11,308 cycles

PAX DOOR INNER HANDLE MEET STRUCTURE HAS CRACKED ANGLE. REMOVED THE PAX DOOR INNER HANDLE STRUCTURAL ANGLE. LOCATED, SEALED AND INSTALLED A NEW ANGLE IAW SRM 51-40-11 AND 51-42-06.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 9,788 hrs · 8,520 cycles

RIGHT WING EMERGENCY LIGHT IS INOP.

Part: UNKNOWN — UNKNOWN (NLG) · airframe 8,746 hrs · 7,522 cycles

FOUND BIRDSTRIKE ON NOSE GEAR, EMERGENCY DECLARED.

Part: PUMP — FAILED (HYD SYSTEM) · airframe 8,228 hrs · 7,062 cycles

HYD SYSTEM 2 QTY READS 5 PERCENT LOST HYD 2A PUMP IN FLIGHT (EMERGENCY DECLARED).

Part: ATTACH FITTING — CRACKED (BS 280) · airframe 7,937 hrs · 6,827 cycles

I/B CLIP CRACKED @ FS280 RBL9

Part: ATTACH FITTING — CRACKED (BS 280) · airframe 7,937 hrs · 6,827 cycles

IB AND OB CLIPS AT FS280 LBL 9 CRACKED.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 7,937 hrs · 6,827 cycles

AFT ANGLE CRACKED AT FS 280 FLOORBEAM JUST OB OF LBL 9.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 7,937 hrs · 6,827 cycles

AFT ANGLE CRACKED AT FS 280 FLOORBEAM JUST OB OF RBL 9.

Part: INTERCOSTAL — CRACKED (BS 484) · airframe 7,937 hrs · 6,827 cycles

LT OB FS 484 INTERCOSTAL CRACKED.

Part: INTERCOSTAL — CRACKED (BS 484) · airframe 7,937 hrs · 6,827 cycles

RT OB FS 484 INTERCOSTAL CRACKED.

Part: STRINGER CLIP — CRACKED (BS 625) · airframe 7,937 hrs · 6,827 cycles

RIGHT SIDE FS 625 CLIP CRACKED (MARKED).

Part: HANDLE — CRACKED (AIR STAIR DOOR) · airframe 7,202 hrs · 6,266 cycles

ASD HANDLE CRACKED.

Part: LIGHT — BROKEN (CABIN)

FLT 4287 - DURING A GROUND INSPECTION IN ATL, THE EMERGENCY EXIT LIGHT COVER AT THE PASSENGER DOOR WAS FOUND BROKEN OFF. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT ASSEMBLY AT THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: APU — OVERSERVICED (APU BAY)

FLT 4151 - DURING FINAL APPROACH TO ATL FROM FPO, THE CREW RECEIVED A SMOKE TOILET CAUTION MESSAGE. THE MESSAGE OCCURRED SIMULTANEOUSLY WHEN SHIFTING THE BLEEDS FROM THE ENG TO THE APU. A MILD ACRID ODOR WAS PRESENT BRIEFLY WITH NO HARD INDICATIONS OF SMOKE OR FIRE BEING PRESENT. THE QRH WAS COMPLIED WITH. EMERGENCY EQUIPMENT ASSISTANCE WAS REQUESTED AS A PRECAUTION. THE AIRCRAFT LANDED SAFELY IN ATL. UPON INSPECTION OF THE AFT EQUIPMENT BAY MAINTENANCE FOUND SMOKE IN THE APU ENCLOSURE. AN INSPECTION OF THE APU REVEALED IT TO HAVE BEEN OVERSERVICED. MAINTENANCE REMOVED THE EXCESS OIL AND RAN THE APU. OPERATIONAL AND LEAK CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: ANGLE — CRACKED (FUSELAGE)

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

Part: CLIP — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE FS 625 LEFT CLIP WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE FS 625 LT CLIP IAW CRJ-200 SRM 51-42. (M)

Part: CLIP — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE RIGHT OUTBOARD FS 280 CLIP WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE RIGHT OUTBOARD FS 280 CLIP. (M)

Part: VALVE — FAILED (FUEL SOLENOID)

FLT 4390 - DURING DESCENT INTO MSP FROM DFW, THE AUXILIARY POWER UNIT PERFORMED AN AUTOMATIC SHUTDOWN WITH NO WARNING MESSAGE, ACCOMPANIED BY A HEAVY FUEL ODOR UPON SHUTDOWN. THE AIRCRAFT LANDED SAFELY IN MSP. MAINTENANCE REMOVED AND REPLACED THE FUEL SOLENOID VALVE. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: LIGHT — ODOR (LAVATORY)

DURING CRUISE, THE CREW NOTICED A HOT PLASTIC TYPE SMELL FROM THE LAVATORY AREA. UPON INVESTIGATION THE CREW DETERMINED THE LAVATORY OCCUPIED LIGHT WOULD NOT EXTINGUISH WHICH WAS CAUSING THE SMELL. THE AIRCRAFT LANDED SAFELY. MAINTENANCE INSPECTED THE LAVATORY LIGHT WITH THE SWITCH IN THE ON AND OFF POSITIONS. NO DEFECTS WERE NOTED. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE.

Part: WIRE — BROKEN (EMERGENCY LIGHT)

DURING A GROUND INSPECTION, THE AFT EMERGENCY FLOOR LIGHT POWER CABLE WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE AFT EMERGENCY FLOOR LIGHT POWER STRIP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE.

Part: WINDOW — CRACKED (COCKPIT)

FLT 4266 - DURING DESCENT INTO DFW FROM CAE, AT APPROXIMATELY 20,000 FT THE INTERIOR PANE ON THE FIRST OFFICERS RIGHT WINDOW CRACKED. THE CRACK CONTINUED TO PROPAGATE AND AN EMERGENCY WAS DECLARED AS A PRECAUTION. NO PRESSURIZATION OR OTHER PROBLEMS OCCURRED. THE CREW COMPLIED WITH THE QRH AND THE AIRCRAFT LANDED SAFELY IN DFW. MAINTENANCE REMOVED AND REPLACED THE FIRST OFFICERS RIGHT WINDOW. OPS AND LEAK CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: O-RING — LEAKING (APU OIL CAP)

FLT 4768 - DURING DESCENT AND APPROACH INTO ATL FROM GTR, THE CREW SMELLED FUMES AFTER SELECTING THE BLEEDS TO THE APU. SMOKE FILLED THE COCKPIT AND CABIN ACCOMPANIED BY A SMOKE LAVATORY MESSAGE. THE CREW SWITCHED THE BLEEDS BACK TO THE ENGINES AND THE SMOKE DISSIPATED SHORTLY AFTERWARDS FOLLOWED BY THE SMOKE LAVATORY MESSAGE EXTINGUISHING. THE TOWER ROLLED EMERGENCY VEHICLES AS A PRECAUTION WITH THE AIRCRAFT LANDING SAFELY IN ATL. MAINTENANCE REMOVED EXCESS OIL FROM THE AUXILIARY POWER UNIT AND REPLACED THE CAP O-RING. OPS CHECKS GOOD. NO SMOKE WAS NOTED. AIRCRAFT OK FOR SERVICE. (M)