N917EV

Part: ENGINE — FAILED · airframe 39,321 hrs · 39,877 cycles

ENGINE FAILURE ON CLIMB OUT.

Part: LANDING GEAR — DID NOT STOW (NOSE) · airframe 38,663 hrs · 39,154 cycles

GEAR DISAGREE AND NOSE DOOR WARNINGS AFTER ATTEMPTING TO RETRACT GEAR AFTER TAKEOFF. NOSE GEAR DID NOT RETRACT. RAN QRH AND ALL GEAR EXTENDED CORRECTLY, CLEARING WARNINGS. RETURNED TO FIELD WITHOUT INCIDENT. (FLIGHT 5437 - FILED CLOSED)THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 28552545 WITH THE FOLLOWING CORRECTIVE ACTION: "REF CP 28553275 FOR TROUBLESHOOTING GEAR DISAGREE. REF CP 28553316 FOR CORRECTIVE ACTIONS.REF CP 28556342 FOR NLG WOW2 AND CENTERED HARNESS ASSEMBLY."

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 38,053 hrs · 38,505 cycles

FLOOR BEAM AT RBL 9.00 BETWEEN FS409.00 + 112 AND FS409.00 + 128 HAS 2 AREAS OF CORROSION NEAR THE FWD SPLICE. (C-CHECK RO 2/12/2024) REPAIRED 2 AREAS OF CORROSION NEAR THE FWD SPLICE OF THE FLOOR BEAM AT RBL 9.00 BETWEEN FS409.00 + 112 AND FS409.00 + 128 IN REF TO REO 601R-53-41-3211, REV--, DATED 2024-01-18. TASK CARD 51-900-1003-SKY. COMPLETED M-337.

Part: BRACKET — CRACKED (BS 621) · airframe 38,053 hrs · 38,505 cycles

STRINGER CLEAT CRACKED ON THE AFT SIDE OF THE REAR PRESURE BULKHEAD AT STGR 14R. (C-CHECK RO 2/12/2024) REMOVED AND REPLACED STRINGER CLEAT ON THE AFT SIDE OF THE REAR PRESURE BULKHEAD AT STGR 14R IN REF TO SRM 51-42-06. COMPLIED WITH FORM M-337 AND TASK CARD 51-900-1003-SKY

Part: BRACKET — CRACKED (BS 621) · airframe 38,053 hrs · 38,505 cycles

STRINGER CLEET CRACKED ON THE AFT SIDE OF THE REAR PRESURE BULKHEAD AT STGR 14L . (C-CHECK RO 2/12/2024) REMOVED AND REPLACED STINGER CLEAT ON THE AFT SIDE OF THE REAR PRESURE BULKHEAD AT STGR 14L IN REF TO SRM 51-42-06. COMPLIED WITH FORM M-337 AND TASK CARD 51-900-1003-SKY

Part: PRESSURE BLKHD — GOUGED (BS 621) · airframe 38,053 hrs · 38,505 cycles

AFT PRESSURE BULKHEAD (FS621.00) FWD FACE HAS 8 GOUGES AND 7 GOUGED RIVET HEADS IN THE WEB DOUBLERS AT RBL 36.20, RBL 27.50, RBL 18.00, LBL 9.50, LBL 18.00, LBL 27.50, AND LBL 36.20. (C-CHECK RO 2/12/2024) REPAIRED 8 GOUGES AND REPLACED 7 GOUGED RIVETS IN THE WEB DOUBLERS OF THE AFT PRESSURE BULKHEAD (FS621.00) FWD FACE AT RBL 36.20, RBL 27.50, RBL 18.00, LBL 9.50, LBL 18.00, LBL 27.50, AND LBL 36.20. IN REF TO REO 601R-53-61-8145, REV--, DATED 2024-01-11. COMPLETED TASK CARD 51-900-1003-SKY AS WELL AS FORM M-337

Part: PRESSURE DECK — DAMAGED (BS 500) · airframe 38,053 hrs · 38,505 cycles

PRESSURE FLOOR AT APPROX. FS. 500, OUTBOARD OF LBL 9.00 AND CENTERED BETWEEN SUPPORT BEAM AND JUST AFT OF CABLE SUPPORT BRACKET, SKIN HAS SMALL NICK. (C-CHECK RO 2/12/2024) REPAIRED GOUGE DAMAGE TO PRESSURE FLOOR AT APPROX. FS. 500, OUTBOARD OF LBL 9.00 AND CENTERED BETWEEN SUPPORT BEAM AND JUST AFT OF CABLE SUPPORT BRACKET IN REF TO REO 601R-53-41-3209, REV--, DATED 2024-01-16. COMPLETED TASK CARD 51-900-1003-SKY AND FORM M-337

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 38,053 hrs · 38,505 cycles

FLOOR BEAM RBL9.00 BETWEEN FS. 409.00 +48 - 409.00 +128 HAS MULITPLE AREAS OF SURFACE CORROSION ON INBOARD FLOORBOARD LANDING. (C-CHECK RO 2/12/2024) REMOVED AND REPLACED FLOOR BEAM RBL9.00 BETWEEN FS. 409.00 +48 - 409.00 +128 IN REF TO SRM 51-42-34, 51-42-21, AND 51-42-11. COMPLETED TASK CARD 51-900-1003-SKY. COMPLETED M-337.

Part: NONE — DAMAGED · airframe 36,137 hrs · 36,252 cycles

TRANSFER FROM EAML 778862 : TRANSFERRED FROM CAMP 23817432. DAMAGE FOUND TO BE ON RIGHT SIDE OF AIRCRAFT BETWEEN FS 379.00 AND FS 394.00 TO BE AS FOLLOWS: / (1-OFF) DENT DAMAGE MEASUREING 1.25" LENGTH X .075" WIDTH X 0.060" MAX DEPTH & (1-OFF) GOUGE DAMAGE MEASURING 0.125" LENGTH X 0.050" WIDTH X 0.026" MAX DEPTH TO FUSELAGE SKIN PANEL (DWG 601R31019, REF). DAMAGE ALSO AFFECTS INTERNAL STRINGER 15R (DWG: 601R31111, REF) AND (1-OFF) DAMAGED FASTENER WITHIN DISCREPANT AREA. / DAMAGE FOUND TO BE OUT OF LIMITS PER CRJ200 SRM 53-00-31. (FILED CLOSED) DAMAGE FOUND TO BE ON RIGHT SIDE OF AIRCRAFT BETWEEN FS 379.00 AND FS 394.00 AT SRT 15R. REPAIRED DAMAGE PER REO 601R-53-21-3509 REV: -- DATED 2021-11-19. COMPLIED WITH TASK CARD 51-900-1003-SKY AND COMPLETED M-337.

Part: NONE — DAMAGED · airframe 35,950 hrs · 36,027 cycles

COMPLY WITH FORM M-337 FOR MAJOR REPAIR TO SCREW HOLE FOR ACCES PANEL 131AL SEE PARENT. (FILED CLOSED) COMPLIED WITH FORM M-337 FOR REPAIR TO SCREW HOLE SURROUND STRUCTURE FOR ACCESS PANEL 131AL

Part: FRAME — CORRODED (BS 333) · airframe 34,755 hrs · 34,476 cycles

F.S. 333 FRAME IS CORRODED FROM STRINGER 18R TO 17R. C-CHECK RO 8/29/2020. REMOVED AND INSTALLED NEW FRAME SECTORS AT FS333.00 STRINGER 18R TO 23R IAW CRJ-200 SRM, DRAWING AND SKYWEST CARD. COMPLETED FORM M-337. WEIGHT AND BALANCE NOT AFFECTED.

Part: FRAME — CORRODED (BS 333) · airframe 34,755 hrs · 34,476 cycles

F.S. 333 FRAME IS CORRODED FROM 23L-17L. C-CHECK RO 8/29/2020. REMOVED AND INSTALLED NEW FRAME SECTORS AT FS333.00 STRINGER 18R TO 23R IAW CRJ-200 SRM, BOMBARDIER DRAWING, AND SKYWEST CARD. COMPLETED M-337 AND M-131. WEIGHT AND BALANCE NOT AFFECTED PART FOR PART REPLACEMENT.

Part: FLOORBEAM — CRACKED (BS 484) · airframe 34,755 hrs · 34,476 cycles

F.S. 484 LT INTERCOSTAL BETWEEN LBL 27 AND LBL 36 IS CRACKED AT THE LOWER OUTBOARD CORNER. C-CHECK RO 8/29/2020. REPAIRED DAMAGED F.S.484 LT INTERCOSTAL BETWEEN LBL 27 AND LBL 36 LWR CORNER IAW MHIRJ REO AS DOCUMENTED ON CONTINUATION CARD. FORM M-337 COMPLETED. WEIGHT AND BALANCE NOT AFFECTED.

Part: FLOOR SUPPORT — ELONGATED (BS 464) · airframe 34,755 hrs · 34,476 cycles

NUTPLATE HOLE ON LT CABIN FLOOR SILL AT F.S.464 IS ELONGATED. C-CHECK RO 8/29/2020. PERFORMED A MAJOR REPAIR TO THE LT PRESSURE FLOOR SKIN IAW MHIRJ REO. COMPLETED SKYWEST TASK. COMPLETED FORM M-337. NO WEIGHT CHANGE.

Part: BUTTSTRAP — CORRODED (BS 333) · airframe 34,755 hrs · 34,476 cycles

CORROSION FOUND ON BUTT STRAP AT F.S. 333 STRINGER 27-26L. C-CHECK RO 8/29/2020. REMOVED AND INSTALLED NEW BUTT STRAP IAW CRJ 200 SRM AND BOMBARDIER DWG. COMPLIED WITH TASK CARD, M-337 COMPLETED. WEIGHT AND BALANCE NOT AFFECTED.

Part: FLOOR SUPPORT — CORRODED (BS 409-559) · airframe 34,755 hrs · 34,476 cycles

RT CABIN PRESSURE FLOOR SILL PANEL HAS CORROSION FROM F.S. 409+128 TO F.S. 559.00. C-CHECK RO 8/29/2020. REPAIRED RT FLOOR SILL FROM FS 409.128 TO FS 559.00 IAW REO. COMPLIED WITH SKY CARD AND FORM M-337. SEE CONTINUATION CARD FOR DETAILS OF WORK PREFORMED. WEIGHT AND BALANCE NOT AFFECTED.

Part: INTERCOSTAL — CORRODED (BS 349) · airframe 34,755 hrs · 34,476 cycles

F.S. 349 INTERCOSTAL AT STRINGER 20R IS CORRODED. C-CHECK RO 8/29/2020. REMOVED AND INSTALLED NEW INTERCOSTAL AT FS 349 AT STRINGER 20R IAW CRJ 200 SRM AND DRAWING 601R38303. COMPLIED WITH SKYCARD AND FORM M-337. SEE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED. WEIGHT AND BALANCE NOT AFFECTED.

Part: FLOOR SUPPORT — CORRODED (BS 409) · airframe 34,755 hrs · 34,476 cycles

LBL 9 FLOOR BEAM CAP IS CORRODED BETWEEN F.S. 409 TO F.S. 409+96 ON THE INBOARD SIDE. C-CHECK RO 8/29/2020. PERFORMED A MAJOR REPAIR TO FS 409 TO FS 409+96 LBL9 FLOOR BEAM CAP IAW CRJ-200 SRM AND REO. REFERENCE BOMBARDIER DRAWING. COMPLIED WITH SKYWEST TASK CARD. COMPLETED M-337 AND SDR M-131. NO WEIGHT CHANGE PART FOR PART REPLACEMENT.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 34,755 hrs · 34,476 cycles

F.S. 280 RBL9 SUPPORT CLIP IS CRACKED. C-CHECK RO 8/29/2020. REMOVED AND REPLACED CRACKED SUPPORT CLIP AT FS.280 RBL9 OUTBOARD IAW CRJ 200SRM.

Part: STIFFENER — CRACKED (RT MLG WW) · airframe 34,755 hrs · 34,476 cycles

RT MAIN LANDING GEAR WHEEL WELL UPPER I/B BATT RIB ANGLE IS CRACKED. C-CHECK RO 8/29/2020. REMOVED AND REPLACED BATT RIBB ANGLE PN: 600-10389-2 IAW CRJ-200 SRM.

Part: FLOOR SUPPORT — CORRODED (BS 409-559) · airframe 34,755 hrs · 34,476 cycles

LT CABIN FLOOR SILL IS CORRODED IN SEVERAL AREAS BETWEEN F.S. 409.00+128 AND F.S. 559.00. C-CHECK RO 8/29/2020. REPAIRED LT SILL PANEL FROM FS 409.00+128 TO FS 559.00 IAW BOMBARDIER REO. TASK CARD COMPLIED WITH, FORM M-337 ATTACHED. WEIGHT AND BALANCE NOT EFFECTED.

Part: SEAT TRACK — CORRODED (BS 544-559) · airframe 34,755 hrs · 34,476 cycles

RT SIDE SEAT RAIL BETWEEN F.S. 544.00 AND F.S. 559.00 +96 IS CORRODED. C-CHECK RO 8/29/2020. REMOVED AND REPLACED RT SIDE SEAT RAIL BETWEEN F.S. 544.00 - F.S. 559.00+96 IAW CRJ-200 AMM.

Part: FLOORBEAM — CRACKED (BS 484) · airframe 34,755 hrs · 34,476 cycles

LT F.S. 484.00 ANGLES AT LBL 36 AND LBL 27 ARE CRACKED. C-CHECK RO 8/29/2020. REMOVED AND REPLACED CRACKED ANGLE AT F.S. 484 LBL27 IAW CRJ 200 SRM. REFERENCE CAMP #21306170 FOR REPAIR OF LBL 36 ANGLE AT F.S. #84.

Part: SEAT TRACK — CORRODED (BS 364) · airframe 34,755 hrs · 34,476 cycles

LBL9 FLOOR SEAT TRACK IS CORRODED AT F.S. 364. C-CHECK RO 8/29/2020. REMOVED AND REPLACED SEAT TRACK AT FS 364 LBL9 IAW: CRJ200-AMM.

Part: SEAT TRACK — CORRODED (BS 499-544) · airframe 34,755 hrs · 34,476 cycles

RT SIDE SEAT RAIL BETWEEN F.S. 499.00 AND F.S. 544.00 IS CORRODED. C-CHECK RO 8/29/2020. REMOVED CORRODED SEAT RAIL AND INSTALLED NEWLY FABRICATED SEAT RAIL (REFERENCE CAMP #21262560 FOR FABRICATION) BETWEEN F.S. 499.00 AND F.S 544.00 IAW CRJ 200 AMM.

Part: SEAT TRACK — CORRODED (BS 449) · airframe 34,755 hrs · 34,476 cycles

RT SIDE SEAT RAIL BETWEEN F.S. 449.85 AND F.S. 499.00 IS CORRODED. C-CHECK RO 8/29/2020. REMOVED AND REPLACED RT SIDE SEAT RAIL BETWEEN F.S. 449.85 AND F.S. 499.00 IAW CRJ 200 AMM.

Part: ANGLE — CORRODED (BS 280) · airframe 34,755 hrs · 34,476 cycles

F.S. 280 FWD J ANGLE IS CORRODED. C-CHECK RO 8/29/2020. REMOVED CORRODED FORWARD FLOOR ANGLE ( "J" ANGLE), AND REPLACED WITH NEW P/N 600-34017-351 IAW CRJ-200 SRM.

Part: ANGLE — CRACKED (LT MLG WW) · airframe 34,755 hrs · 34,476 cycles

LT MAIN LANDING GEAR WHEELWELL UPPER I/B BATT RIB ANGLE IS CRACKED. C-CHECK RO 8/29/2020. REMOVED AND INSTALLED SERVICEABLE LT MAIN LANDING GEAR WHEEL WELL UPPER I/B BATT RIB ANGLE IAW CRJ 200 SRM AND MHIRJ REO. COMPLIED WITH SKYWEST TASK CARD, SCANNED M-337. NO WEIGHT CHANGE PART FOR PART REPLACEMENT.

Part: PLATE — CORRODED (PAX DOOR) · airframe 34,755 hrs · 34,476 cycles

PASSENGER DOOR AFT ANCHOR FITTING SERRATED PLATE IS CORRODED. C-CHECK RO 8/29/2020. REMOVED AND REPLACED PASSENGER DOOR ANCHOR FITTING SERRATED PLATE IAW CRJ 200 AMM. ADJUSTMENT AND OPS CHECKS "GOOD".

Part: ATTACH ANGLE — CORRODED (PAX DOORWAY) · airframe 34,755 hrs · 34,476 cycles

ON AIRCRAFT PASSENGER DOOR FRAME WHILE REMOVING ANGLE 601R31527-205 FOUND THAT ATTACHING ANGLE 601R31527-179 IS HEAVILY CORRODED AND NEEDS REPLACED. C-CHECK RO 8/29/2020. REMOVED ANGLE 601R31527-205, FOUND ATTACHING ANGLE 601R31527-179 IS HEAVILY CORRODED AND REPLACED IAW CRJ 200 SRM. COMPLIED WITH SKYCARD AND FORM M-337. SEE CONTINUATION CARD FOR DETAILS OF WORK PREFORMED. WEIGHT AND BALANCE NOT AFFECTED.

Part: BRACKET — CORRODED (PAX DOOR) · airframe 34,755 hrs · 34,476 cycles

FWD AND AFT PASSENGER DOOR BRACKET ASSEMBLIES ARE CORRODED. C-CHECK RO 8/29/2020. REMOVED AND REPLACED FWD AND AFT PASSENGER DOOR BRACKET ASSEMBLIES PT# 601R31527-217 IAW CRJ 200 SRM.

Part: GUSSET — CORRODED (BS 310) · airframe 34,755 hrs · 34,476 cycles

PASSENGER DOOR GUSSET AT FS310.00 AND BETWEEN STRINGER 15L AND STRINGER16L CORRODED AND REQUIRES EVALUATION. C-CHECK RO 8/29/2020. REMOVED AND INSTALLED NEW GUSSET IAW CRJ 200. SEE CONTINUATION CARD FOR DETAILS OF WORK PREFORMED.

Part: BRACKET — CHAFED (RT WING TE FLAP) · airframe 34,755 hrs · 34,476 cycles

RT WING INBOARD TRAILING EDGE, I/B FLAP STUB FAIRING MOUNTING BRACKET CHAFED APPOX. 0.025 DEEP. C-CHECK RO 8/29/2020. REMOVED DAMAGED RT WING I/B TRAILING EDGE FLAP STUB FAIRING MOUNTING BRACKET AND INSTALLED NEW SERVICEABLE MOUNT BRACKET IAW CRJ 200 SRM.

Part: INTERCOSTAL — CORRODED (BS 295-310) · airframe 34,755 hrs · 34,476 cycles

INTERCOSTAL LOWER CORRODED BETWEEN FS 295.00 AND FS310.00 AND BETWEEN STRINGER 16L AND STRINGER 17L. C-CHECK RO 8/29/2020. REMOVED AND INSTALLED NEW INTERCOSTAL IAW CRJ 200 SRM AND DRAWING. COMPLIED WITH SKYCARD AND FORM M-337. WEIGHT AND BALANCE NOT AFFECTED.

Part: FITTING — CRACKED (WINDOW POST) · airframe 34,755 hrs · 34,476 cycles

WINDSHIELD CENTER POST LOWER FITTING IS CRACKED THRU THE LOWER FASTENER LOCATIONS ON THE AFT SIDE OF FITTING. C-CHECK RO 8/29/2020. REMOVED UNSERVICEABLE POST FITTING AND INSTALLED SERVICEABLE POST FITTING IAW CRJ 200 SRM.

Part: FRAME — CORRODED (BS 319) · airframe 34,755 hrs · 34,476 cycles

F.S. 319 FRAME IS CORRODED BETWEEN STRINGER 27 TO 26L. C-CHECK RO 8/29/2020. REMOVED AND INSTALLED NEW FRAME SECTION AND SPLICES IAW CRJ 200 SRM AND SKYWEST CARD. COMPLETED FORM M-337 AND M-131. WEIGHT REMOVED .35 WEIGHT INSTALLED .6 TOTAL WEIGHT INSTALLED IS .25.

Part: FLOOR SUPPORT — CORRODED (BS 589) · airframe 34,755 hrs · 34,476 cycles

LT CARGO FLOOR SILL IS CRACKED AT FS 589 AND CORRODED AROUND SEVERAL NUTPLATE HOLES. C-CHECK RO 8/29/2020. REMOVED DAMAGED LT SILL AND INSTALLED NEW SERVICEABLE FLOOR SILL IAW CRJ 200 SRM AND BOMBARDIER REO. WEIGHT AND BALANCE NOT EFFECTED. COMPLIED WITH M-337.

Part: INTERCOSTAL — CORRODED (E/E BAY DOOR) · airframe 34,755 hrs · 34,476 cycles

FWD AVIONICS BAY DOOR INTERCOSTAL IS CORRODED AT F.S. 364 BETWEEN STRINGER 27 TO STRINGER 26R. C-CHECK RO 8/29/2020. REMOVED AND REPLACED FS364 BETWEEN STRINGER 27 AND STRINGER 26R CRJ-200 SRM.

Part: CHANNEL — CRACKED (BS 574) · airframe 34,755 hrs · 34,476 cycles

CARGO DOOR CUTOUT SURROUND HAT CHANNEL FS 574 IS CRACKED IN TWO LOCATIONS. (C-CHECK) RO 8/29/2020. REMOVED OLD PART AND INSTALLED SERVICABLE PART IAW CRJ 200 SRM. CALIBRATED TOOL USED 204368 CAL DUE 10-31-20.

Part: SUPPORT PLATE — CORRODED (BS 310-319) · airframe 34,755 hrs · 34,476 cycles

RT CABIN FLOOR SUPPORT PLATE FOR GALLEY 1 IS CORRODED AT RBL 36 BETWEEN FS310 AND FS 319. C-CHECK RO 8/29/2020. REMOVED AND REPLACED RT CABIN FLOOR SUPPORT IAW CRJ-200 SRM.

Part: FRAME — CORRODED (BS 333) · airframe 34,755 hrs · 34,476 cycles

F.S.333 FRAME IS CORRODED BETWEEN STRINGER 27 TO STRINGER 26L AND 23L TO 22L. C-CHECK RO 8/29/2020. REMOVED AND INSTALLED NEW FRAME SECTORS AT FS 333 STRINGER 18L-23R IAW CRJ 200 SRM, AND DWG. COMPLIED WITH SKY CARD FORM M-337 COMPLETED. WEIGHT AND BALANCE NOT AFFECTED.

Part: BULKHEAD — CHAFED (BS 280) · airframe 34,755 hrs · 34,476 cycles

FS 280 BULKHEAD IS CHAFED ON AFT FACE BETWEEN RBL 11.00 AND RBL 18.80 APPROXIMATELY 16 INCHES ABOVE FLOOR LEVEL. C-CHECK RO 8/29/2020. PERFORMED A MAJOR REPAIR TO FS 280 BULKHEAD CHAFE IAW REO. COMPLETED SKYWEST TASK CARD. COMPLETED FORM M-337 IS ATTACHED. WEIGHT CHANGE TOTAL WEIGHT REMOVED .007LBS, TOTAL WEIGHT ON .059 LBS, TOTAL WEIGHT ADDED .052 LBS.

Part: FLOORBEAM — CRACKED (BS 484) · airframe 34,755 hrs · 34,476 cycles

FS 484 ANGLE CLIP ON OB SIDE OF RBL 27 FLOOR BEAM IS CRACKED. C-CHECK RO 8/29/2020. R & R ANGLE CLIP ON OB SIDE OF RBL 27 IAW CRJ-200 SRM. REFERENCE CONTINUATION CARD FOR WORK PERFORMED.

Part: FLOOR SUPPORT — CORRODED (BS 589-612) · airframe 34,755 hrs · 34,476 cycles

CARGO FLOOR BEAM LBL 27 HAS CORROSION AROUND 3EA NUTPLATES ON OB FLANGE BETWEEN FS 589 AND FS 612. C-CHECK RO 8/29/2020. PERFORMED A MAJOR REPAIR BY REPLACING THE CARGO FLOOR BEAM AT LBL 27 BETWEEN FS 589 AND FS 612 IAW CRJ 200 SRM COMPLETED SDR AND CPCP. NO WEIGHT CHANGE PART FOR PART REPLACEMENT.

Part: INTERCOSTAL — CORRODED (BS 364) · airframe 34,755 hrs · 34,476 cycles

FWD AVIONICS BAY DOOR INTERCOSTAL IS CORRODED AT F.S. 364 BETWEEN STRINGER 27 TO 26L IS CORRODED. C-CHECK RO 8/29/2020. REMOVED AND REPLACED INTERCOSTAL AT FS 364 BETWEEN STRINGER 27.0 TO 26L IAW CRJ-200 SRM.

Part: FLOOR SUPPORT — CORRODED (BS 409-559) · airframe 34,755 hrs · 34,476 cycles

RT CABIN PRESSURE FLOOR SILL HAS CORROSION FROM FS409+128 TO FS 559.00 ON BOTH THE FLOOR SILL PANEL AND FLOOR ANGLES. C-CHECK RO 8/29/2020. REPAIRED RT CABIN FLOOR SILL IAW MHIRJ REO AND CRJ 200 SRM. COMPLIED WITH SKYCARD AND FORM M-337. SEE CONTINUATION CARD FOR DETAILS OF WORK PREFORMED. WEIGHT AND BALANCE NOT AFFECTED.

Part: SKIN — DAMAGED · airframe 34,755 hrs · 34,476 cycles

AFTER DETAILED INSPECTION ON THE FUSELAGE SKIN SURROUND FOR ATTACHING PNL. 131 AL, FOUND ONE EACH REPAIRED HOLE'S FREEZE PLUG NOT SEATED. REQUIRES REPAIR. C-CHECK RO 8/29/2020. PANEL 131AL HAD A DAMAGED/LOOSE FREEZE PLUG AND REPAIRED IAW BOMBARDIER REO. COMPLIED WITH SKYCARD AND FORM M-337. SEE CONTINUATION CARD FOR DETAILS OF WORK PREFORMED. WEIGHT AND BALANCE NOT AFFECTED.

Part: CONTROL UNIT — CORRODED (RT AILERON) · airframe 34,755 hrs · 34,476 cycles

RT WING AILERON OUBOARD PCU ATTACHMENT LUG APPEARS CORRODED. REMOVED AND REPLACED RT O/B AILERON PCU IAW CRJ 200 MIP.

Part: SKIN — DENTED (RT WING TE FLAP) · airframe 34,755 hrs · 34,476 cycles

RIGHT INBOARD FLAP HAS FOUR SHARP DENTS ON THE LOWER SKIN. FIRST DENT .015" DEEP .250" LONG, 14.625" FROM TRAILING EDGE 5.25" FROM INBOARD RIB. SECOND DENT .008" DEEP .375" LONG, 15.375" FROM TRAILING EDGE 19.5" FROM INBOARD RIB. THIRD DENT .008" DEEP .375" LONG, 3" FROM TRAILING EDGE 22" FROM INBOARD RIB. FOURTH DENT .014" DEEP .5" LONG, 1" FROM TRAILING EDGE 45.5" FROM INBOARD RIB. DENTS ARE OUT OF LIMITS IAW CRJ 200 SRM. C-CHECK RO 8/29/2020. REMOVED AND REPLACED RT INBOARD FLAP LOWER SKIN IAW CRJ-200 SRM AND BOMBARDIER DRAWING. COMPLETED SKYCARD, FORM M-337 ATTACHED. WEIGHT AND BALANCE NOT AFFECTED.

Part: STOP FITTING — CORRODED (E/E BAY DOOR) · airframe 34,755 hrs · 34,476 cycles

MAIN AVIONICS COMPARTMENT DOOR SIDE FITTINGS ON FUSELAGE HAVE CORRODED STOPS. C-CHECK RO 8/29/2020. REMOVED AND REPLACED CORRODED STOPS (PADS) WITH NEW/SERVICEABLE ONES.

Part: NUT — CORRODED (SPOILER PCU) · airframe 34,755 hrs · 34,476 cycles

LEFT WING SPOILERON AND FLIGHT SPOILER INBOARD AND OUTBOARD PCU MOUNTING HARDWARE (NUTS) ARE CORRODED. C-CHECK RO 8/29/2020. REMOVED AND REPLACED CORRODED NUTS IAW CRJ-200-AMM.

Part: NUT — CORRODED (SPOILER PCU) · airframe 34,755 hrs · 34,476 cycles

RIGHT WING SPOILERON AND FLIGHT SPOILER INBOARD AND OUTBOARD PCU MOUNTING HARDWARE (NUTS) ARE CORRODED. C-CHECK RO 8/29/2020. REPLACED CORRODED NUTS ON THE RT WING SPOILERON AND FLIGHT SPOILER INBOARD AND OUTBOARD PCU TO WING ATTACHMENT POINT WITH NEW SERVICEABLE NUTS IAW CRJ 200 AMM.

Part: BOLT — CORRODED (SPOILER PCU) · airframe 34,755 hrs · 34,476 cycles

RIGHT WING INBOARD AND OUTBOARD GROUND SPOILER PCU MOUNTING HARDWARE CORRODED. REPLACED THE RT INBOARD AND OUTBOARD GROUND SPOILER ACTUATOR MOUNTING HARDWARE WITH NEW SERVICABLE HARDWARE IAW CRJ 200 AMM. OPERATIONAL TEST CHECKS GOOD IAW CRJ 200 AMM.

Part: MOUNT — CORRODED (SPOILER PCU) · airframe 34,755 hrs · 34,476 cycles

LEFT WING INBOARD AND OUTBOARD GROUND SPOILER PCU MOUNTING HARDWARE CORRODED. C-CHECK RO 8/29/2020. INSTALLED SERVICEABLE MOUNTING AND ATTACHING HARDWARE TO LT WING INBOARD AND OUTBOARD GROUND SPOILERS PCU IAW CRJ 200 AMM. OPERATIONAL TEST CHECKS GOOD IAW CRJ 200 AMM.

Part: SKIN — DENTED · airframe 34,755 hrs · 34,476 cycles

COMPLY WITH SCHEDULED MAINTENANCE CODE: DENT FOUND RT FWD FUSELAGE BETWEEN STRINGERS R25 & R24. REINSPECT NEEDED EVERY 600 HOURS PER REO. PERMANENT REPAIR DUE IN 5300 FLIGHT HOURS BY 38018.2 TAT., PART NUMBER: - , SERIAL NUMBER: 7769, POSITION: C-CHECK RO 8/29/2020. DENT FOUND RT FWD FUSELAGE BETWEEN STRINGERS R25 & R24. REPAIRED IAW MHIRJ REO. COMPLIED WITH SKYCARD AND FORM M-337. SEE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED. WEIGHT AND BALANCE NOT AFFECTED.

Part: SKIN — DAMAGED · airframe 34,755 hrs · 34,476 cycles

COMPLY WITH SCHEDULED MAINTENANCE CODE: REPAIRED 2 ELONGATED FASTENER HOLES ON FWD FUSE SKIN USED FOR ATTACHING PANEL 131AL PER REO. PERFORM DETAILED VISUAL INSPECTION, PART NUMBER: - SERIAL NUMBER: 7769, POSITION: C-CHECK RO 8/29/2020. PERFORMED DETAILED VISUAL INSPECTION PER SCHEDULED MAINTENANCE CODE, REFERENCE JOB 9776985 OPERATION 16 FOR NOTED DEFECTS.

Part: CLAMP — LOOSE (BLEED AIR SYS) · airframe 32,730 hrs · 32,130 cycles

CARGO BTL LOW CAUTION MESSAGE IN CRUISE. RAN QRH AND LANDED AT NEAREST SUITABLE AIRPORT. (FLT#3500) CLOSED UPON INVESTIGATION OF RIGHT HAND CARGO FIRE BOTTLE BEING RELEASED, ALSO FOUND THE RIGHT HAND 14TH STAGE DUCT ASSY INSULATION WAS BLOWN APART DUE TO THE AFT CLAMP OF THE 14TH STAGE SHUTOFF VALVE BEING LOOSE. REMOVED AND REPLACED THE 14TH STAGE DUCT ASSY IAW AMM. LEAK AND OPS CHECK GOOD, NO DEFECTS NOTED. A/C OK FOR SERVICE.

Part: FLOORBEAM — CORRODED (BS 559) · airframe 32,003 hrs · 31,307 cycles

CORROSION ON FLOOR BEAM ON LBL9 BETWEEN FS559.0 - FS559+16 AROUND SCREW HOLES. (C-CHECK) RO: 09/27/2018 REPAIRED FLOOR BEAM BETWEEN FS559.0 - FS559+16 AROUND SCREW HOLES IAW REO.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 32,003 hrs · 31,307 cycles

CORRODED SEAT RAIL BEAM ON LBL28.00 NEAR FS559.00+112. (C-CHECK) RO: 09/27/2018 REMOVED CORROSION AROUND SCREW HOLE ON SEAT RAIL BEAM AT LBL28, FS559.00+110 IAW SRM.

Part: HINGE FITTING — GOUGED (PAX DOOR) · airframe 32,003 hrs · 31,307 cycles

FUSELAGE PASSENGER DOOR HINGE AFT LANDING HAS GOUGE FROM HINGE PIN ROLL PIN. (C-CHECK) RO: 09/27/2018 BLENDED FUSELAGE PAX DOOR HINGE AFT LANDING IAW REO.

Part: ANCHOR FITTING — GOUGED (GALLEY) · airframe 32,003 hrs · 31,307 cycles

GALLEY UPPER ANCHOR FITTING ON FUSELAGE IS GOUGED AT APPROXIMATELY FS 300. (C-CHECK) RO: 09/27/2018REMOVED DAMAGE ON GALLEY UPPER ANCHOR FITTING ON FUSELAGE AT FS295.00 TO FS310.00 STGR 4R. IAW REO AND SRM.

Part: FLOOR PANEL — CORRODED (COCKPIT) · airframe 32,003 hrs · 31,307 cycles

THERE IS AN AREA OF CORROSION ON THE L/H FLIGHT COMPARTMENT FLOOR PANEL AFT EDGE OUTBOARD OF THE PARKING BRAKE HANDLE. (C-CHECK) RO: 09/27/2018 REMOVED CORROSION ON THE L/H FLIGHT COMPARTMENT FLOOR PANEL AFT EDGE OUTBOARD OF THE PARKING BRAKE HANDLE IAW SRM.

Part: BRACKET — CORRODED (SERVICE DOOR) · airframe 32,003 hrs · 31,307 cycles

SERVICE DOOR AFT SILL & BRACKET IS CORRODED. (C-CHECK) RO: 09/27/2018 REMOVED AND REPLACED SERVICE DOOR SILL AND BRACKET IAW SRM.

Part: SKIN — DENTED (BS 767) · airframe 32,003 hrs · 31,307 cycles

REAR FUSELAGE LH SIDE DENTED APPROX FS767 LOCATED AFT OF LH PAC HEAT EXCHANGER EXHAUST. (C-CHECK) RO: 09/27/2018 REPAIRED LH SIDE DENT APROX FS767 AFT OF LH PAC HEAT EXCHANGER EXHAUST IAW REO.

Part: PUMP — FAILED (HYD SYSTEM) · airframe 30,274 hrs · 29,395 cycles

AFTER TAKEOFF, SELECTING GEAR UP, HAD A GEAR DISAGREE, AND NOSE DOOR OPEN WARNING MESSAGE. REMOVED AND REPLACED 3B HYDRAULIC PUMP IAW AMM. OPS AND LEAK CHECKED GOOD. PERFORMED GEAR SWINGS IAW AMM. NO DEFECTS NOTED.

Part: SKIN — DENTED (BS 424-439) · 29,288 cycles

EXTERNAL FUSELAGE SKIN IS DENTED AT STRINGER 7L BETWEEN BS 424 AND 439. REPAIRED THE SKIN IAW REO.

Part: SKIN — DENTED (BS 658) · 29,288 cycles

EXTERNAL FUSELAGE SKIN HAS ONE PROTRUDING DENT AT APPROX BS 658 BETWEEN STRINGERS 21L AND 22L. REPAIRED IAW REO.

Part: SKIN — DENTED (LT WING TE FLAP) · 29,288 cycles

LEFT WING INBD FLAP HAS TWO DENTD ON THE UPPER SURFACE. REPAIRED THE DAMAGE IAW REO.

Part: SKIN — DENTED (LT WING TE FLAP) · 29,288 cycles

LEFT WING OTBD FLAP HAS ONE DENT ON THE ON THE UPPER SURFACE. COMPLIED WITH REPAIR IAW SRM.

Part: CROSSBEAM — CRACKED (BS 280) · 29,288 cycles

BS 280 CROSSBEAM IS CRACKED JUST OTBD OF LBL 9 AND RBL 9. REPAIRED THE CROSSBEAM IAW REO.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 29,144 hrs · 28,145 cycles

FLOORBEAM RBL 9 CORRODED AT FS 409+130. REPAIRED RBL9 AT FS 409+130 PER REO 601R-53-41-2096 AND EC/TC REO 601R-53-41-2096. AIRCRAFT APPROVED FOR RETURN TO SERVICE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 29,144 hrs · 28,145 cycles

RBL 9 FLOORBEAM CAP SCREW HOLES CORRODED BTW FS 559+80-559+122. COMPLIED WITH ECTC/EO 600-53-0779 REV O REV DATE 2016-09-14. AIRCRAFT APPROVED FOR RETURN TO SERVICE.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 29,144 hrs · 28,145 cycles

CORRODED SEAT TRACK AT RBL9 AND FS 559.00 TO FS 559+112. REMOVED CORRODED SEAT TRACK, FABRICATED A NEW ONE AND INSTALLED AT RBL9 AND BETWEEN FS 559 TO 559+112 PER REO 601R-53-00-485 AND ECTC/REO 601R-53-00-485. AIRCRAFT APPROVED FOR RETURN TO SERVICE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 29,144 hrs

FLOORBEAM RBL 9 CORRODED AT FS 409+03, 409+28, 409+36. REPAIRED RBL9 FLOORBEAM BY REPLACING IT PER REO 601R-53-00-027 AND EC/TC REO EO 600-53-0778. AIRCRAFT APPROVED FOR RETURN TO SERVICE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 29,144 hrs · 28,145 cycles

LBL27 FLOORBEAM CAP SEGMENT AT FS 569.00 TO FS 609 HAS SEVERAL FLOOR PANEL SCREW HOLES CORRODED. REMOVED AND REPLACED CORRODED FLOORBEAM AT LBL27 AND BETWEEN FS 569 TO 609 PER REO 601R-53-61-3778 AND EC/TC REO 601R-53-61-3778.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 29,144 hrs · 28,145 cycles

LBL9 FLOORBEAM CAP SEGMENT FS 610-619 SCREW HOLES CORRODED. COMPLIED WITH ECTC/REO 601R-53-61-5823 REV 0.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 29,144 hrs · 28,145 cycles

CARGO COMPT RT FLOOR SILL CORRODED AT SEVERAL AREAS BETWEEN FS 559+112 TO FS 621. REPAIRED CORRODED CARGO COMPT RT FLOOR SILL BETWEEN FS 559+112 FS 621 PER REO 601R-53-00-526, REV AND EC/TC REO 601R-53-00-526 01.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 29,144 hrs · 28,145 cycles

LBL9 FLOORBEAM CAP SEGMENT BETWEEN FS 569.00 - 609.00 HAS SEVERAL FLOOR PANEL SCREW HOLES CORRODED. REMOVED CORRODED BEAM, DRILLED UP A NEW ONE AND INSTALLED PER REO 601R-53-61-3780 AND EC/TC 601R-53-61-3780 AND USED DWG 601R31030.

Part: HINGE — GOUGED (PAX DOOR) · airframe 29,144 hrs · 28,145 cycles

PAX DOOR PIANO HINGE HAS A GOUGE (FUSELAGE SIDE) (ANTI-ROTATION PIN MIGRATED OUT). REPAIRED GOUGE IN PAX DOOR PIANO HINGE PER BOMBARDIER REO 601R-53-21-2748 AND EXPRESSJET ECTC/REO 601R-53-21-2748. AIRCRAFT APPROVED FOR RETURN TO SERVOCE.

Part: STIFFENER — CRACKED (BS 409) · airframe 29,144 hrs · 28,145 cycles

BS 409+128 VERTICAL POST AT BL 0 CRACKED. CRACK IS IN THE RADIUS. REMOVED AND REPLACED STIFFENER IAW SRM 51-42-06, 51-40-06, 51-40-11, DRAWING 601R32208 AND ECTC/REO 601R-53-41-889 REV A. ECTC/REO 601R-53-41-889 REV A. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: PLUG — WORN (ZONE 100) · airframe 29,144 hrs · 28,145 cycles

PANEL 132AL 6 & 8 O'CLOCK SCREW HOLE FREEZE PLUGS ARE DISLODGED. REPAIRED AND REINSTALLED FREEZE PLUGS AT 6 & 8 O'CLOCK POSITIONS AT PANEL 132AL SURROUND STURCTURE PER REO 601R-53-11-162 REV C AND ECTC/ REO 601R-53-11-162. AIRCRAFT APPROVED FOR RETURN TO SERVICE.

Part: CARGO TRACK — CORRODED (BS 583-600) · airframe 29,144 hrs · 28,145 cycles

CARGO TRACK CORRODED AT BS 583 AND 600, LBL 9. REMOVED AND REPLACED THE CARGO TRACK IAW AMM 53-00-49-000 AND -400-801.

Part: CARGO TRACK — CORRODED (BS 559) · airframe 29,144 hrs · 28,145 cycles

CARGO TRACK CORRODED AT BS 559 AT LBL 27. REMOVED AND REPLACED THE CARGO TRACK IAW AMM 53-00-49-000 AND -400-801.

Part: STRAP — CORRODED (BS 559) · airframe 29,144 hrs · 28,145 cycles

CORRODED STRAP AND NUT PLATE CHANNEL AT BS 559 BETWEEN RBL 42 AND RBL 27. REMOVED AND INSTALLED NEW STRAP IAW SRM 51-42-06. AIRCRAFT APPROVED FOR RETURN TO SERVICE.

Part: CARGO TRACK — CORRODED (BS 559) · airframe 28,907 hrs · 27,879 cycles

CARGO BAY HAS THREE CARGO TRACKS CORRODED. REMOVED AND REPLACED THE CARGO TRACKS IAW AMM 53-00-49-000 / -400-801.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 27,595 hrs · 26,475 cycles

EXIT LIGHT COVER MISSING OVER SERVICE DOOR. REPAIRED IAW AMM 33-50-00.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 27,302 hrs · 26,159 cycles

F/O'S FLASHLIGHT INOPERATIVE. REPLACED FLASHLIGHT IAW CMM.

Part: SEAL — DETERIORATED (SERVICE DOOR) · airframe 26,053 hrs · 24,868 cycles

SERVICE DOOR WON'T OPEN. FOUND SERVICE DOOR PINCHING SEAL BETWEEN AIRFRAME AND DOOR R & R SERVICE DOOR SEAL AMM 52-41-07. PERFORMED OPS TEST OF SERVICE DOOR SEAL IAW AMM 52-41-074. ACFT RETURNED TO SERVICE.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 25,747 hrs · 24,545 cycles

F/A REPORT SERVICE DOOR EXIT SIGN COVER MISSING. R & R LIGHT COVER & ASSY IAW AMM 33-51-10, OP CK'S GOOD NO FURTHER DEFECTS NOTED.

Part: DOOR — LACK OF LUBE (SERVICE) · airframe 24,958 hrs · 23,756 cycles

SERVICE DOOR IS EXTREMELY DIFFICULT TO OPEN. LUBRICATED SERVICE DOOR IAW AMM 12-20-52, OPS CHECK GOOD, ACFT RETURN TO SERVICE.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 24,931 hrs · 23,729 cycles

1ST CENTER ISLE OVERHEAD EMERGENCY EXIT LIGHT OUT. SET THE EMERGENCY LIGHT SWITCH TO ARM AND LET THE BATTERIES CHARGE. PERFORMED OPS TEST OF THE EMERGENCY LIGHTS IAW AMM 33-51-00-710-801. OPS TEST CHECKS GOOD.

Part: WIRE — MISINSTALLED (EMERGENCY LIGHT) · airframe 24,931 hrs · 23,729 cycles

EMERGENCY EXIT LIGHT ON GALLEY NEXT TO SERVICE DOOR INOPERATIVE. FOUND WIRES SWAPPED ON EMERGENCY EXIT LIGHT BESIDE SERVICE DOOR. REMOVED WRONG WIRES AND INSTALLED IN CORRECT POSITION ON SPLICE IAW ESPM 20-16-00. PERFORMED OPS TEST OF THE EMERGENCY EXIT LIGHTS IAW AMM 33-51-00-710-801. OPS TEST CHECKED GOOD.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 24,931 hrs · 23,729 cycles

LT SIDE WALL SEAT TRACK AT STRINGER 15L HAS TWO AREAS OF CORROSION, BS 559+80. R & R SEAT TRACK IAW AMM 53-01-11-000-802, & 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (BS 426-549) · airframe 24,931 hrs · 23,729 cycles

CABIN SEAT TRACK RBL 9 HAS EIGHT AREAS OF CORROSION, BS 426 - 549. REMOVED AND REPLACED SEAT TRACK IAW AMM 53-01-11-000-802 AND AMM 53-01-11-400-802.

Part: DOUBLER — MISREPAIRED · airframe 24,931 hrs · 23,729 cycles

FOUND FASTENER COUNTER SUNK TOO DEEP IN THE DOUBLER ACCESS 132AL. REPAIRED IAW EC/TC REO 601R-53-11-162

Part: SKIN — CORRODED (LT WING) · airframe 24,931 hrs · 23,729 cycles

LEFT WING ACCESS HOLE LAND 550FB IS CORROED. REPAIRED IAW REO 601R-57-21-030. MAJOR REPAIR.

Part: SKIN — CORRODED (LT WING) · airframe 24,931 hrs · 23,729 cycles

LEFT WING ACCESS HOLE LAND 550DB IS CORRODED. REPAIRED IAW REO 601R-57-21-030, & ECTC EO 600-57-81. MAJOR REPAIR.

Part: SKIN — CORRODED (LT WING) · airframe 24,931 hrs · 23,729 cycles

LEFT WING ACCESS HOLE LAND 550EB IS CORRODED. REPAIRED IAW REO 601R-57-21-030, REV C. MAJOR REPAIR.

Part: SKIN — CORRODED (LT WING) · airframe 24,931 hrs · 23,729 cycles

LEFT WING ACCESS HOLE LAND 550GB IS CORRODED. REPAIRED IAW REO 601R-57-21-030. MAJOR REPAIR.

Part: ANGLE — CRACKED (BS 625) · airframe 24,931 hrs · 23,729 cycles

LT AND RT, FS 625, ANGLES ARE CRACKED. R & R LT & RT ANGLES IAW SRM 51-42-20.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 24,931 hrs · 23,729 cycles

RBL 27 SEAT TRACK SEGMENT BS 559+78 - 559+95 CORRODED. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11-000-801 & AMM 53-01-11-400-802.

Part: CROSSBEAM — CORRODED (BS 349) · airframe 24,931 hrs · 23,729 cycles

BS 349 CROSSBEAM CORRODED AT RBL 45. REMOVED SUPPORT ANGLE ATTACHED TO FS349 AND RBL27 IAW SRM 51-42-06 AND SRM 51-42-21-00. INSTALLED SUPPORT CLIP ATTACHED TO FS 349 & RBL 27 IAW SRM 51-42-06 & 51-42-21-00 & DWG 601R-53-21-2565. SUBMITTED TO THD AND RECEIVED REO 601R-53-21-2565 AND FORMED REPAIR ITEMS TO BE HEAT TREATED IAW STEP 10 OF REO 601R-53-21-2565. COMPLIED WITH STEP 1 OF REO PL601R 53-21-2565, CUT AWAY DAMAGE ON BEAM. RECEIVED AND COMPLIED WITH ECTC REO 601R-53-21-2565, REV A, REO 601R-21-2565, REV A.

Part: BUSHING — CORRODED (HORIZONTAL STAB) · airframe 24,931 hrs · 23,729 cycles

LEFT SIDE HORIZONTAL STABILIZER HINGE BUSHINGS HAVE CORROSION. REMOVED THE LT AND RT OTBD PIVOT BUSHINGS, INSPECTED THE BORES AND FOUND TO BE GALLED IAW RIL 3039, SB 601R-55-007, REV D, PART C. REMOVED GALLING WITH 1ST OVERSIZE REAMER 1.7151 DIA- 203-402 REAMER IAW SB601R-55-007, REV D, PART C ON LT AND RT OTBD HORIZONTAL LUGS A2A-C. INSTALLED LT AND RT OTBD PIVOT BUSHINGS AND FINAL REAM. INSTALLED LT AND RT OTBD BUSHINGS IN HORTIZONTAL STABILIZER AND FINAL REAMED TO SIZE IAW SB 601R-55-007, REV D, PART C 2D-E. REMOVED HORIZONTAL STABILIZER LT & RT INBD PIVOT BUSHINGS, INSPECTED BORES AND FOUND TO BE GALLED IAW RIL 3039, SB 601R-55-007, REV D, PART C. INSTALLED LT & RT INBD PIVOT BUSHINGS IN HORIZONTAL STABILIZER AND REAMED TO SIZE IAW SB601R-55-007, REV D, PART C, SUB D-W & RIL 3039. COMPLIED WITH REO 601R-55-11-02 AND EC/TC REO601R-55-11-022.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 24,931 hrs · 23,729 cycles

LBL 27, SEAT TRACK SEGMENT BS 559+78 - 559+95 IS CORRODED. REMOVED AND REPLACED THE SEAT TRACK SEGMENT IAW AMM TASK 53-01-11-000-802 AND AMM 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 24,931 hrs · 23,729 cycles

LBL 9 SEAT TRACK CORRODED AT 559+12.5. FOUND FOUND TO BE OUT OF LIMITS IAW SRM 53-51-49-01. R & R THE SEAT TRACK IAW EC/TC REO 601R-53-00-485 & REO 601R-53-00-485. C

Part: FLOOR SUPPORT — CORRODED (BS 559) · airframe 24,931 hrs · 23,729 cycles

CARGO RT FLOOR SUPPORT HAS SEVERAL SCREW HOLES CORRODED FROM BS 559+80 - 559+112. REMOVED CORROSION IAW SRM 51-21-06-00. REPAIRED IAW EC/TC REO 601R-53-00-526 01 AND REO 601R-53-00-526, REV. MAJOR REPAIR.

Part: FLOOR SUPPORT — CORRODED (BS 559) · airframe 24,931 hrs · 23,729 cycles

CARGO LT FLOOR SUPPORT HAS SEVERAL SCREW HOLES CORRODED FROM BS 559+80 - 559+112. REMOVED CORROSION IAW SRM 51-21-06-00. REPAIRED IAW EC/TC REO 601R-53-00-526 01 AND REO 601R-53-00-526, REV. MAJOR REPAIR.

Part: SEAT TRACK — CORRODED (BS 364-400) · airframe 24,931 hrs · 23,729 cycles

SEAT TRACK LBL 9, BS 364-400 IS CORRODED. R & R SEAT TRACK IAW 53-01-11-000-802 & 53-01-11-400-802.

Part: ANGLE — CRACKED (BS 280) · airframe 24,931 hrs · 23,729 cycles

ANGLE BRACKET CONNECTING BS 280 TO LBL 9 IS CRACKED. REMOVED BRACKET IAW SRM 51-42-00. LOCATED, DRILLED, AND INSTALLED NEW BRACKET IAW SRM 51-42-20 AND DWG NR 601R31113.

Part: BRACKET — CRACKED (BS 280) · airframe 24,931 hrs · 23,729 cycles

ANGLE BRACKET CONNECTING RBL 9 BS 280 IS CRACKED. REMOVED ANGLE BRACKET IAW SRM 51-42-21. DRILLED & INSTALLED NEW ANGLE BRACKET IAW SRM 51-40-11-00 & 51-42-21.

Part: SEAT TRACK — CORRODED (BS 400) · airframe 24,931 hrs · 23,729 cycles

SEAT TRACK LBL 9 BS 400-400+128 CORRODED. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11-080-802 AND AMM 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (BS 400) · airframe 24,931 hrs · 23,729 cycles

SEAT TRACK RBL 9, BS 400-400+128 CORRODED. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11-000-802, SRM 51-40-11, AND AMM 53-01-11-400-802.

Part: BUTT JOINT — CORRODED (BS 333) · airframe 24,931 hrs · 23,729 cycles

CORROSION FOUND ON BUTT STRAP AT BS 333 ON FWD AND AFT SIDE OF FRAME. REMOVED CORROSION BETWEEN STRINGERS 25L AND 26R IAW SRM 51-21-14. BLENDED AREAS FOUND TO BE OUT OF LIMITS IAW SRM 53-21-15, FIG 101. REPAIRED IAW EA 32-2014-047.

Part: FLOOR SUPPORT — CORRODED (BS 319) · airframe 24,931 hrs · 23,729 cycles

RT FLOOR SUPPORT T/E AT BS 319.7 CORRODED. REMOVED CORROSION DAMAGE IAW SRM 51-21-06-00. DAMAGE FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00-01. PART REPLACED IAW SRM 51-42-07 AND DWG 601R-31148.

Part: ANGLE — CORRODED (PAX DOOR SILL) · airframe 24,931 hrs · 23,729 cycles

PAX DOOR SILL ANGLE HAS CORROSION. REMOVED DAMAGE IAW SRM 51-21-06-00. INSTALLED NEW ANGLE IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (BS 364-400) · airframe 24,931 hrs · 23,729 cycles

SEAT TRACK RBL 9, BS 364-400 CORRODED. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11-04, AND AMM 53-01-11-400-802.

Part: FRAME — CORRODED (BS 319) · airframe 24,931 hrs · 23,729 cycles

CORROSION AT BS 319, FRAME BETWEEN STRINGERS 26 - 27L. REMOVED CORROSION IAW SRM 51-21-06.

Part: RUB STRIP — UNSECURE (LT AILERON) · airframe 24,931 hrs · 23,729 cycles

LT AILERON L/B PHENOLIC RUB STRIP UNSECURE. REPAIRED IAW REO 601R-57-61-503 PERMANENT REPAIR.

Part: FRAME — CORRODED (BS 333) · airframe 24,931 hrs · 23,729 cycles

CORROSION ON BS 333 FRAME FWD AND AFT SIDE BETWEEN STRINGER 25L - 26R. REMOVED CORROSION IAW SRM 51-21-06.

Part: HINGE — GOUGED (PAX DOOR) · airframe 24,931 hrs · 23,729 cycles

GOUGES ON PAX DOOR P1 AND HINGE HALF ON DOOR SIDE FWD END. BLENDED OUT DAMAGE ON PAX DOOR PIANO HINGE, HALF ON DOOR SIDE FWD END IAW REO 601R-52-11-134. MAJOR REPAIR.

Part: CAP — DENTED (PAX DOOR) · airframe 24,931 hrs · 23,729 cycles

DENT DISCOVERED ON BOTH LOWER END CAPS OF PAX DOOR. REPAIRED IAW REO 670-52-11-159.

Part: LIGHT — BROKEN (CABIN) · airframe 24,642 hrs · 23,445 cycles

EMERGENCY LIGHT AT 8C & D BENT, STICKING UP, AND BROKEN. SECURED EMERGENCY LIGHT IAW AMM 33-51-01. NO FURTHER DEFECTS NOTED. ACFT OK FOR SERVICE.

Part: BULKHEAD — CRACKED · airframe 24,170 hrs · 22,969 cycles

AFT PRESSURE BULKHEAD CRACKED AT LBL 27.50, UPPER END OF DOOR TRACK, APPROX. ONE INCH LONG.

Part: BULKHEAD — CRACKED · airframe 24,170 hrs · 22,969 cycles

AFT PRESSURE BULKHEAD CRACKED AT RBL 18.00, BELOW SECOND STANDOFF FROM FLOOR.

Part: DOOR — LACK OF LUBE (SERVICE) · airframe 23,548 hrs · 22,341 cycles

F/A SERVICE DOOR DIFFICULT TO OPEN FROM INSIDE AND UNABLE TO OPEN FROM OUTSIDE. LUBRICATED SERVICE DOOR IAW AMM 12-20-52. OPS CHECKED GOOD IAW AMM 52-41-00.

Part: THRESHOLD — DIRTY (SERVICE DOORWAY) · airframe 23,259 hrs · 22,043 cycles

SERVICE DOOR HARD TO OPEN AND CLOSE. CLEANED DEBRIS FROM BOTTOM OF DOOR THRESHOLD, OP'S CHECKED GOOD, REF MM 52-41-00.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 22,986 hrs · 21,772 cycles

NR 2 EXTERIOR EMERGENCY LIGHT INOP. REPLACED LAMPS IAW AMM 33-51-21. OPS CHECKED GOOD.

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 21,762 hrs · 20,508 cycles

LIGHTED EXIT SIGN COVER MISSING FROM INTERIOR WALL FORWARD OF PASSENGER DOOR INSTALLED NEW FLOOR FLOOD LIGHT IAW AMM 33-51-19.

Part: POST — CRACKED (BS 409) · airframe 21,261 hrs · 20,006 cycles

FS 409+128 VERTICAL POST BL 0 LT UPPER AFT RADIUS FAILS NDT WITH INDICATION GREATER THAN 50 PERCENT SCREEN HEIGHT. REMOVED VERTICAL POST IAW SRM 51-42-06 & 51-42-21. INSTALLED VERTICAL POST IAW REO 601R-53-41-889 AND SRM 51-42-06. LOCATED & DRILLED FASTENER HOLES ON LT POST IAW SRM 51-40-11.

Part: POST — CRACKED (BS 409) · airframe 21,261 hrs · 20,006 cycles

FS 409+128 VERTICAL POST, LBL 18 INBD AFT UPPER RADIUS FAILS NDT WITH INDICATION. GREATER THAN 50 PERCENT SCREEN HEIGHT. LOCATED AND INSTALLED NEW VERTICAL POST IAW SRM 51-42-06 AND REO 601R-53-41-889.

Part: SUPPORT ANGLE — CRACKED (BS 280) · airframe 21,244 hrs · 19,987 cycles

PASSENGER DOOR UPPER SILL JUST AFT OF FS 280 HAS CRACKED SUPPORT ANGLE, CRACK IS CRACKED 75 PERCENT THROUGH THE ANGLE. PASSENGER DOOR UPPER SILL FAILS INSPECTION IAW NDTM 53-21-126, PART 9, STEPS 5 THROUGH STEP 6. ALL SKINS OF CRACKS ON PASSENGER DOOR SILLS MEMBERS ARE CAUSE FOR REJECTION. REMOVED CRACKED SUPPORT ANGLE IAW SRM 51-42-06 & 51-42-21. INSTALLED NEW ANGLE IAW SRM 51-42-06.

Part: POST — CRACKED (BS 409) · airframe 21,261 hrs · 20,006 cycles

FS 409+128 VERTICAL POST RBL 18 OTBD UPPER AFT RADIUS FAILS NDT WITH AN INDICATION GREATER THAN 50 PERCENT SCREEN HEIGHT. REMOVED VERTICAL POST IAW SRM 51-42-06. LOCATED AND DRILLED NEW VERTICAL POST IAW SRM 51-40-11. INSTALLED NEW POST IAW SRM 51-42-06 & REO 601R-53-41-8899, REV A.

Part: SWITCH — BROKEN (FLASHLIGHT) · airframe 20,222 hrs · 18,839 cycles

CAPTAINS FLASHLIGHT ON/OFF SWITCH IS BROKEN. R & R CAPTAINS FLASHLIGHT IAW AMM 25-61-04.

Part: PLACARD — DETERIORATED (PAX DOOR) · airframe 20,111 hrs · 18,704 cycles

PASSENGER DOOR OPEN PLACARD, EXIT PLACARD AND TO OPEN PLACARD ARE WORN. R & R THE PASSENGER DOOR OPEN, EXIT, AND TO OPEN PLACARD IAW AMM 11-30-00. R & R THE PASSENGER DOOR OPEN, EXIT, AND TO OPEN PLACARD IAW AMM 11-30-00.

Part: FLASHLIGHT — MALFUNCTIONED (COCKPIT) · airframe 19,622 hrs · 18,141 cycles

CAPTAIN`S FLASHLIGHT WILL NOT STAY ON. R & R CAPTS FLASHLIGHT IAW AMM 25-61-04. OPS CHECKED GOOD.

Part: DOOR — INOPERATIVE (MAIN PAX) · airframe 18,670 hrs · 17,096 cycles

MAIN CABIN DOOR WILL NOT OPEN. R & R PAX DOOR ASSIST MOTOR IAW AMM 52-11-08.

Part: STRUCTURE — CRACKED (BS 559) · airframe 18,412 hrs · 16,811 cycles

CRACK INDICATION NOTED AT FS 559, RBL 9, WL 54.10 IN CHEM-MILL APPRO .100" LENGTH 50 PERCENT FULL SCREEN HEIGHT, FAILED NDT. REPAIRED IAW REO 601R-53-41-609 REV B.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 18,104 hrs · 16,467 cycles

RT AFT OVERWING EMERGENCY LIGHT INOP. REMOVED THE INOP BULB AND INSTALLED A NEW BULB IAW AMM 33-51-21. OPS CHECK GOOD. (CLOSED)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 17,149 hrs · 15,362 cycles

RT EXTERIOR NR1 EMERGENCY LIGHT INOP. R & R NR 1 EMERGENCY LIGHTING BATTERY IAW AMM 33-51-04, OPS CHECK GOOD. R & R NR1 EMERGENCY LIGHTING BATTERY IAW AMM 33-51-04, OPS CHECK GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 17,149 hrs · 15,362 cycles

LT EXTERIOR NR1 EMERGENCY LIGHT INOP. (RESOLVED ON W/O: 168312 TASKCARD: N/R-00005 ) R & R NR1 EMERGENCY LIGHTING BATTERY IAW AMM 33-51-04, OPS CHECK GOOD. R & R NR 1 EMERGENCY LIGHTING BATTERY IAW AMM 33-51-04, OPS CHECK GOOD. (CLOSED)

Part: LENS — CRACKED (EMERGENCY LIGHT) · airframe 16,463 hrs · 14,554 cycles

EMERGENCY EXIT LENS COVER ON LT WINDSCREEN IS CRACKED. REMOVED CRACKED EXIT LENS COVER FROM LT WINDSCREEN. INSTALLED NEW EXIT LENS COVER ON LT WINDSCREEN IAW AMM 33-51-13-400-801 STEP 3A (4).

Part: SUPPORT BEAM — CRACKED (FUSELAGE) · airframe 16,463 hrs · 14,554 cycles

FOUND CARGO DOOR SUPPORT BEAM AFT LOWER ANGLE IS CRACKED APPROX .4" IN LENGTH. R & R CARGO DOOR SUPPORT BEAM AFT LOWER ANGLE IAW SRM 51-42-21.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 16,463 hrs · 14,554 cycles

FOUND REAR PRESSURE BULKHEAD WEB THAT SURROUNDS THE LINTEL ATTACHMENT FITTING HAS INDICATION NOTED APPROX .2" IN LENGTH 50 PERCENT FSH. FAILED NDT INSP. REPAIR IAW REO EC/TC 601R-53-61-1230 HAS BEEN COMPLETE AND THE REPAIR COMPLIES WITH THE REQUIREMENTS OF EC/TC AND REO 601R-53-61-1230 REV D. REF MWC JOB 8776915, OP 209 FOR DEVIATION TO REO 601R-57-61-1230.

Part: SEAT TRACK — CORRODED (BS 394-409) · airframe 16,463 hrs · 14,554 cycles

RT FLOOR SEAT TRACK FROM FS 394 TO FS 409+128 IS CORRODED. R & R RT FLOOR SEAT TRACK FROM FS 394 TO FS 409+128 IAW AMM 53-01-11-000-802 & AMM 53-01-11-400-802.

Part: INTERCOSTAL — CRACKED (BS 621-625 S14L) · airframe 16,463 hrs · 14,554 cycles

LEFT FS 621-625 INTERCOSTAL ANGLE CRACKED AT STR 14L PREVIOUSLY REPLACED. R & R LT FS 621-625 INTERCOSTAL ANGLE IAW SRM 51-42-21, STEP 9.

Part: PLACARD — DAMAGED (EMERGENCY EXIT) · airframe 16,463 hrs · 14,554 cycles

CREW ESCAPE HATCH EXTERNAL OPEN, CLOSE AND EMERGENCY EXIT PLACARDS DAMAGED. REMOVED DAMAGE SILKSCREEN IAW AMM 11-10-03-010-801 AND APPLIED NEW SILKSCREENS IAW AMM 11-10-03-400-801 TO CREW ESCAPE HATCH.

Part: SEAT TRACK — CORRODED (BS 409-559) · airframe 16,463 hrs · 14,554 cycles

LT FLOOR SEAT TRACK FROM FS 409+128 TO FS 559 IS CORRODED. REMOVED DAMAGED FLOOR (LT) SEAT TRACK FROM FS 409+128 TO FS 559 IAW SRM 51-41-02. LOCATED AND INSTALLED NEW SERVICEABLE FLOOR SEAT TRACK IAW SRM 51-41-02.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 16,463 hrs · 14,554 cycles

RT FLOOR SEAT TRACK FROM FS 559.0 TO FS 559+112 IS CORRODED. REMOVED DAMAGED RT FLOOR SEAT TRACK FROM FS 559.0 TO FS 559+112, IAW AMM 53-01-11-000-802. INSTALLED NEW SERVICEABLE RT FLOOR SEAT TRACK FROM FS 559.0 TO FS 559+112, IAW AMM 53-01-11-400-802.

Part: FLOOR SUPPORT — CORRODED (BS 621-574) · airframe 16,463 hrs · 14,554 cycles

FLOOR SUPPORT CAP AT FS 621 TO FS 574 LBL 27 IS CORRODED. REMOVED FLOORBEAM CAP AT FS 621 TO FS 574, LBL 27 IAW SRM 51-42-06 AND 51-42-21. LOCATED AND DRILLED NEW FLOORBEAM CAP IAW SRM 51-42-21, 51-42-28. REMOVED FLOORBEAM FITTING IAW SRM 51-42-21. LOCATED AND DRILLED NEW FLOORBEAM FITTING IAW SRM 51-40-11. INSTALLED FASTENER THROUGH BULKHEAD AT FS 621 THROUGH NEW FLOORBEAM FITTING IAW SRM 51-42-21 AND SRM 51-41-02. COMPLIED WITH EC/TC REO 601R-53-61-3578 AND REO 601R-53-61-3578 REV. INSTALLED FLOOR CAP AND FLOORBEAM FITTING IAW SRM 51-42-21 AND EC/TC REO 601R-53-61-3578 AND SRM 51-42-06 FS 574 TO FS 621.

Part: DOOR FRAME — CORRODED · airframe 16,463 hrs · 14,554 cycles

DISCONNECTED PROXIMITY SENSOR FROM PAX DOOR SILL. DISCONNECTED 2 EA CONNECTOR PLUGS FOR PAX DOOR (P1MB) (P2MB). REMOVED PAX DOOR SILL ANGLE IAW SRM 51-42-06, 51-42-11. LOCATED AND INSTALLED NEW SERVICEABLE PAX DOOR LOWER SILL ANGLE IAW SRM 51-42-06 AND 51-42-21. CONNECTED CONNECTOR PLUGS P1MB AND P2MB IAW AMM 52-11-00-400-802 SUBTASK 52-11-00-430-004 D1 & 3 AND INSTALLED PROX SENSOR BY TIGHTENING 1 EA NUTS. PROX SENSOR REQUIRES ADJUSTMENT AND SAFETY AND OPS CHECK DUE ON PAX DOOR. ADJUSTED & SAFETIED THE PAX DOOR PROX SENSOR (PS9MB), IAW AMM 52-70-04-820-803, STEP 3F (1)(A) THRU (1). OPS TEST OF THE PAX DOOR WARNING SYS DUE. OP TEST OF PAX DOOR WARNING SYS IS GOOD, IAW AMM 52-70-04-710-803. ASA RII C/W 5300010.

Part: FLOOR SUPPORT — CRACKED (BS 280) · airframe 16,463 hrs · 14,554 cycles

FS 280, RBL 9 INBD FLOOR SUPPORT CUP IS CRACKED. REMOVED CLIP & INSTALLED NEW SERVICEABLE CLIP AT RBL 9 INBD IAW SRM 51-42-21.

Part: SEAT TRACK — CORRODED (BS 394-409) · airframe 16,463 hrs · 14,554 cycles

LEFT FLOOR SEAT TRACK FROM FS 394 TO 409+128 IS CORRODED. R & R LT FLOOR SEAT TRACK FROM STA 394 TO 409+128 IAW AMM 53-01-11-000-802 & AMM 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (BS 364-394) · airframe 16,463 hrs · 14,554 cycles

RT FLOOR SEAT TRACK FROM FS 364 TO FS 394 CORRODED. R & R RT FLOOR SEAT TRACK FROM FS 364 TO FS 394 IAW AMM 53-01-11-000-802 & AMM 53-01-11-400-802.

Part: PLACARD — DAMAGED (EMERGENCY EXIT) · airframe 16,463 hrs · 14,554 cycles

PAX DOOR EXTERNAL OPEN/CLOSE DECAL AND EMERGENCY EXIT DECALS DAMAGED. REMOVED OLD SILKSCREENS IAW AMM TASK 11-10-03-000-801. APPLIED NEW IAW AMM TASK 11-10-03-400-801.

Part: SILL — CORRODED (DOOR FRAME) · airframe 16,463 hrs · 14,554 cycles

PAX DOOR CUTOUT LOWER SILL IS CORRODED AT CONNECTOR PLUG P1MB AND AT GROUND STUD AT AFT HANDRAIL SUPPORT.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 15,339 hrs · 13,357 cycles

FS 202.75 AT BL 23.71 PRESSURE BULKHEAD CRACKED. NEED EDDY CURRENT TO VERIFY CRACK.

Part: BATTERY PACK — UNKNOWN (CABIN) · airframe 15,324 hrs · 13,346 cycles

EMERGENCY BATTERY PACK NR 1 INOP AND NEEDS TO BE REPLACED.

Part: FLAP SYSTEM — FAILED (WING) · airframe 15,308 hrs · 13,326 cycles

FLAP FAIL AT O (APPROX 12,000 MSL) THE FLAP LEVEL WAS NOT MOVED. REPEAT WRITE-UP. SECOND FLAP FAILURE ON THIS A/C TODAY. EMERGENCY DECLARED. ALL CORRECTIVE ACTIONS ARE UNDER WO 125262 AND WORK ORDER COMPLIED WITH.

Part: STEP — BROKEN (MAIN PAX DOOR) · airframe 14,862 hrs · 12,880 cycles

LOWER PAX DOOR STEP BROKEN.

Part: SIGN — INOPERATIVE (CABIN) · airframe 14,477 hrs · 12,508 cycles

LIGHTED EXIT SIGN BY ASD AND FWD LIGHTED EXIT SIGN ON CEILING AT ROW 8 INOP.

Part: UNKNOWN — ODOR (COCKPIT/ CABIN) · airframe 14,248 hrs · 12,297 cycles

DURING CRUISE STRONG FUEL ODOR IN COCKPIT CALLED FA. FA REPORTED BURNING ELECTRICAL ODOR FROM ROW 8 TO BACK OF PLANE ODOR DISSIPATED DURING DESCENT AND LANDING... ( AUXILIARY POWER UNIT APU -INTAKE DOOR DEACTIVATED CLOSED)

Part: STEP — BROKEN (PAX DOOR) · airframe 13,669 hrs · 11,758 cycles

CREW REPORTS, BOTTOM STEP ON PAX DOOR HAS BROKEN OFF FROM DOOR LINKAGE.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHT) · airframe 13,022 hrs · 11,182 cycles

FORWARD EMERGENCY EXIT LIGHT (CURVED) MOUNTED ON THE ADJACENT TO THE HATCHES IS INOP. REMOVED AND REPLACED NR 2 BATTERY CHARGER FOR EMERGENCY LT`S SYSTEM. CHECKS GOOD IAW RJ-200 33-51-00. (B)

Part: A/C PACK — MALFUNCTIONED (RIGHT) · airframe 12,411 hrs · 10,655 cycles

RIGHT PACK UNCONTROLLABLE, CAUSING SMOKE (AIR CONDITIONING PACK - RT SIDE).

Part: LIGHT — BROKEN (CABIN) · airframe 12,376 hrs · 10,623 cycles

EMERGENCY LIGHT ABOVE SERVICE DOOR, BASE IS BROKEN.

Part: FITTING — CRACKED (FUSELAGE) · airframe 12,376 hrs · 10,623 cycles

LEFT AND RIGHT SIDE CLIPS ARE CRACKED ON THE AFT SIDE OF THE PRESSURE BULKHEAD FS 625.3. LUBED PAX DOOR IAW CRJ MM 12-20-52. PERFORMED FUNCTIONAL TEST OF INNER HANDLE WITH NO DEFECTS NOTED IAW CRJ MM 52-11-00. SUPPLEMENTAL SDR CLOSED 4/3/08.

Part: FITTING — CRACKED (FUSELAGE) · airframe 12,376 hrs · 10,623 cycles

LEFT AND RIGHT SIDE CLIPS ARE CRACKED ON THE AFT SIDE OF THE PRESSURE BULKHEAD FS 625.3. DRILLED UP LEFT AND RIGHT CLIPS AND INSTALLED PER CRJ 200 SRM 51-42-20. SUPPLEMENTAL SDR CLOSED 3/19/08.

Part: FITTING — CRACKED (FUSELAGE) · airframe 12,376 hrs · 10,623 cycles

FS 280 RBL 9 OUTBOARD CLIP CRACKED.

Part: SUPPORT BEAM — CRACKED (FUSELAGE) · airframe 12,376 hrs · 10,623 cycles

ENGINE SUPPORT BEAM UPPER WEB CRACKED AT FS 640 LBL 9.5 WL 19.12. ALL REPAIRS PERFORMED IN ACCORDANCE WITH REO 601R-53-61-345 AND REO 601R-58-61-348.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 12,376 hrs · 10,623 cycles

FS 280 AFT FLOOR SUPPORT ANGLE IS CRACKED AT LBL 9. JOB COMPLETE. REFER TO M-234 FORM STEPS 2 THRU 9 FOR CORRECTIVE ACTION. CUT AWAY DAMAGED SECTION OF 280 AFT FLOOR SUPPORT ANGLE IAW REO 601R-53-11-138. PERFORMED NDT ON CUTLINE PER REO 601R-53-11-138 NO DEFECTS NOTED AT THIS TIME PER NDTM 51-20-08. FABRICATED -3 AND -5 REPAIR ANGLES IAW REO 601R-53-11-138. HEAT TREAT REQUIRED. HEAT TREATED FABRICATED -3 & -5 ANGLES TO T62 CONDITION AS PER CRJ 200 SRM 51-24-06. HARDNESS TEST GOOD. DRILLED AND FIT -3 & -5 REPAIR ANGLES IAW REO 601R-53-11-138 READY TO INSTALL. FABRICATED -1 FILLER ANGLE FROM NEW 600-3407-595 ANGLE IAW REO 601R-53-11-138. READY TO INSTALL. INSTALLED -1 FILLER ANGLE AND -3 & 5 REPAIR ANGLES IAW REO 601R-53-11-138 AND FS 280 CLIPS IAW CRJ SRM 51-42-21. JOB COMPLETE. SUPPLEMENTAL SDR CLOSED 3/12/08.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 12,376 hrs · 10,623 cycles

FLOORBEAM AT LBL 36 AND FS 621 HAS POSSIBLE CRACK ON OUTBOARD UNDERSIDE IN RADIUS.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 12,376 hrs · 10,623 cycles

FS 280 WEB IS CRACKED AT RBL 9. FS 280 WEB AT RBL 9 CLEANED OF CORROSION PREVENTATIVE COMPOUND PER CRJ200 AMM 51-26-00, INSPECTED DISCREPANT AREA NO DEFECTS NOTED, RE-APPLIED CORROSION PREVENTATIVE COMPOUND PER CRJ200 SRM 51-21-11. REFER TO ATTACHED M234 ITEMS 2 THRU 4 FOR WORK PERFORMED. CLEANED STA 280 PILOTS BULKHEAD WEB AT RBL 9 PER CRJ 200 AMM 51-26-00. VISUALLY INSPECTED BULKHEAD WEB, NO DEFECTS NOTED. PERFORMED EDDY CURRENT INSPECTION OF SUSPECT AREA AT RBL 9 FS 280 IAW CRJ 200 NDTM 51-20-06. NO DEFECTS NOTED. RE-APPLIED CORROSION - PREVENTIVE COMPOUND AS PER CRJ 200 SRM 51-21-11 TO 280 BULKHEAD WEB AT RBL 9. JOB COMPLETED. SUPPLEMENTAL SDR CLOSED3/11/08.

Part: SKIN — CORRODED (FUSELAGE) · airframe 12,376 hrs · 10,623 cycles

CARGO COMPT DOOR CUTOUT COAMING HAS PITTING AND CORROSION ALONG BOTTOM (MARKED).

Part: ANCHOR FITTING — CRACKED (AIRSTAIR DOOR) · airframe 12,376 hrs · 10,623 cycles

ASD AFT ANCHOR FITTING CRACKED.

Part: FLAP — FAILED (WING) · airframe 10,954 hrs · 9,295 cycles

FLAPS FAILED AT 8 DEG WHEN 20 DEG WAS SELECTED. EMERGENCY DECLARED.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 10,833 hrs · 9,153 cycles

RIGHT WING EXT FWD EMERGENCY LIGHT INOP.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 10,833 hrs · 9,153 cycles

CAPTAIN'S FLASHLIGHT INOP.

Part: WARNING MESSAGE — ACTIVATED (STEERING SYS) · airframe 10,111 hrs · 8,466 cycles

STEERING INOP MSG AFTER GEAR RETRACTION, COMPLIED WITH QRH, SYSTEM RESET AFTER LANDING. EMERGENCY DECLARED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 9,556 hrs · 7,982 cycles

EMERGENCY LIGHTS EXTERIOR LT WING AND RT WING FWD, AND CABIN CENTER CURVED LIGHTS INOP.

Part: FLASHLIGHT — MALFUNCTIONED (COCKPIT) · airframe 8,371 hrs · 7,020 cycles

F/A FORWARD FLASHLIGHT WILL NOT STAY OFF.

Part: STEP — BROKEN (AIR STAIR DOOR) · airframe 8,371 hrs · 7,020 cycles

TOP ASD STEP BROKEN.

Part: LAMP — BURNED OUT (CABIN)

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

Part: COALESCER BAG — DIRTY (FUSELAGE)

DURING CRUISE, THE CREW REPORTED AN ODOR EMITTING FROM THE ECS. THE AIRCRAFT LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED THE LT AND RT COALESCER BAGS AND RAN THE PACKS WITH NO DEFECTS NOTED. OPERATION CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)

Part: COALESCER BAG — DIRTY (FUSELAGE)

DURING CRUISE, THE CREW REPORTED AN ODOR EMITTING FROM THE PACKS. THE AIRCRAFT LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED THE LT AND RT COALESCER BAGS. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)

Part: SUPPORT — CRACKED (FUSELAGE)

DURING A C-CHECK, THE CARGO DOOR CAM TRACK SUPPORT ASSY AFT ANGLES AT FS 621 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE CARGO DOOR CAM TRACK SUPPORT ASSY IAW SRM. (K)

Part: DOUBLER — CRACKED (FUSELAGE)

DURING C-CHECK, THE LT AND RT 640 DOUBLERS WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE LT AND RT 640 DOUBLERS IAW SRM. (K)

Part: HANDLE — CRACKED (AVIONICSBAY DOOR)

DURING A C-CHECK, THE AVIONICS BAY DOOR HANDLE WAS FOUND TO BE CRACKED AROUND THE HANDLE SHAFT BOSS. THE MRR WILL REMAIN OPEN PENDING MAINTENANCE DETERMINATION OF THE APPROPRIATE CORRECTIVE ACTION. (K)

Part: WEB — CRACKED (FUSELAGE)

DURING C-CHECK, THE LT BOX BEAM LOWER WEB, AT THE FORWARD IB NUT PLATE FOR THE ACCESS PANEL, WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE LT BOX BEAM LOWER WEB, AT THE FWD IB NUT PLATE FOR THE ACCESS PANEL, IAW EO. (K)

Part: LENS — CRACKED (FUSELAGE)

DURING A C-CHECK, THE EMERGENCY EXIT LIGHT LENS, NEAR THE SERVICE DOOR, WAS FOUND TO BE CRACKED. THIS MRR WILL REMAIN OPEN PENDING MAINTENANCES DETERMINATION OF AN APPROPRIATE CORRECTIVE ACTION. (K)

Part: HANDLE — CRACKED (FUSELAGE)

DURING C-CHECK, THE PASSENGER DOOR EXTERNAL HANDLE WAS FOUND TO BE CRACKED. MAINTENANCE IS REMOVING AND REPLACING THE PASSENGER DOOR EXTERNAL HANDLE. (K)

Part: CLIP — CRACKED (FUSELAGE)

DURING A C-CHECK, THE LT AND RT 625 CLIPS, NEAR STR 14, IN AFT EQUIPMENT BAY, WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE LT AND RT 625 CLIPS, NEAR STR 14, IN THE AFT EQUIPMENT BAY, IAW SRM. (K)

Part: CLIP — CRACKED (FUSELAGE)

DURING A C-CHECK, THE FS 260 IB CLIP, AT RBL 9, WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE FS 280 IB CLIP, AT RBL 9 IAW SRM. (K)

Part: LIGHT — INOPERATIVE (EXTERIOR)

DURING A GROUND INSPECTION IN SHV, THE RIGHT SIDE EXTERIOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE RIGHT SIDE EXTERIOR EMERGENCY LIGHT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: LAMP — BURNED OUT (EMERGENCY LIGHT)

DURING A GROUND INSPECTION IN ATL, THE RIGHT OVERWING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE RIGHT OVERWING EMERGENCY LIGHT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: ODOR — DETECTED (CABIN)

FLT 4155 - DURING APPROACH INTO ATL FROM GTR, THE CREW NOTICED A STRONG FUEL SMELL IN THE COCKPIT. SUBSEQUENTLY THE FLIGHT ATTENDANT REPORTED A FUEL SMELL IN THE CABIN. THE AIRCRAFT LANDED SAFELY IN ATL. MAINTENANCE CHECKED THE LEFT AND RIGHT ENGINES FOR FUEL LEAKS AND NONE WERE NOTED. MAINTENANCE ALSO GROUND RAN THE AIRCRAFT ENGINES AND PACKS WITH NO SMELL REOCCURRING. MAINTENANCE DETERMINED THE FUEL SMELL TO BE RESIDUAL FUEL FROM REPLACEMENT OF THE AUXILIARY POWER UNIT SOLENOID VALVE AFTER THE PREVIOUS FLIGHT. (M)

Part: BRACKET — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE SPIDER DUCT BRACKET IN THE AFT EQUIPMENT BAY WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE SPIDER DUCT BRACKET IN THE AFT EQUIPMENT BAY. (M)

Part: BRACKET — CRACKED (PAX DOOR)

DURING A C-CHECK IN MCN, THE FORWARD AND AFT CABLE ANCHOR MOUNTING BRACKETS ON THE PASSENGER DOOR WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE FORWARD AND AFT CABLE ANCHOR MOUNTING BRACKETS ON THE PASSENGER DOOR. (M)

Part: SUPPORT BEAM — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE RIGHT SIDE ACCESS PANEL CORNER OF THE ENGINE SUPPORT BEAM AT BL 36.20 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE RIGHT SIDE ACCESS PANEL CORNER OF THE ENGINE SUPPORT BEAM AT BL 36.20 IAW ASA EO 600-53-0070. (M)

Part: FLOOR SUPPORT — CRACKED (FUSELAGE)

DUIRNG A C-CHECK IN MCN, THE FLOOR SUPPORT ANGLE ON THE RIGHT SIDE AT FS 621 WAS FOUND TO BE CRACKED AT THE CORNER BEYOND LIMITS. MAINTENANCE REPAIRED THE FLOOR SUPPORT ANGLE ON THE RIGHT SIDE AT FS 621 IAW ASA EO 600-53-0105. (M)

Part: CONNECTOR — INOPERATIVE (EMERGENCY LIGHT)

FLT 4157 - DUIRNG A GROUND INSPECTION IN HOU, THE EMERGENCY FLOOR LIGHTS FROM ROW 8 TO THE LAVATORY WERE FOUND INOPERATIVE. MAINTENANCE RESECURED A LOOSE CONNECTOR ON THE EMERGENCY FLOOR LIGHTS NEAR THE LAVATORY. OPS CHECKES GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT)

DURING HANGAR MAINTENANCE IN MCN, THE EXTERIOR EMERGENCY LIGHT ON THE RT MID FUSELAGE WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EXTERIOR EMERGENCY LIGHT LAMP ON THE RT MID FUSELAGE. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: STEP — CRACKED (PAX DOOR)

DURING HANGAR MAINTENANCE IN MCN, THE BOTTOM STEP AT THE BRACKET ON THE PASSENGER DOOR WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE MAIN PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)