N439SW

Part: ANGLE — CRACKED (WINDSHIELD) · airframe 39,717 hrs · 34,802 cycles

*RIGHT HAND - CRACK IN STRUCTURE BELOW THE WINSHIELD POST. (MARKED & FLAGGED) (C-CHECK) RO 1/28/2020 REMOVED AND REPLACED ANGLE. REF CRJ200 SRM, DRW. COMPLIED WITH SKYCARD. SEE CONTINUATION FOR DETAILS.

Part: FRAME — CRACKED (BS 333) · airframe 39,717 hrs · 34,802 cycles

* SUSPECTED CRACK AT FS 333 LBL 5 MARKED (C-CHECK) RO 1/28/2020 VERIFIED CRACK, REMOVED CRACKED FRAME SECTOR AT FS 333 LBL 5 REF CRJ 200 SRM. - INSTALLED NEW FRAME SECTOR PN 601R32004-41 AT FS 333 REF DRAWINGS AND CRJ 200 SRM. RESTORED FINISH AND APPLIED CIC.

Part: SPAR — CORRODED (HORIZONTAL STAB) · airframe 39,717 hrs · 34,802 cycles

RH HORIZONTAL STAB REAR SPAR HAS CORROSION FWD OF OUTBOARD HINGE FITTING (C-CHECK) RO 1/28/2020 REMOVED CORROSION, RH HORIZONTAL STAB REAR SPAR NEAR OUTBOARD HINGE FITTING, REFERENCE CRJ200 SRM. CORROSION REMOVAL STRUCTURALLY ACCEPTABLE REFERENCE REO.

Part: FRAME — CORRODED (BS 605) · airframe 39,717 hrs · 34,802 cycles

*FS 605 FRAME CORRODED ON FWD SIDE LOWER FLANGE STR 26R-23L (C-CHECK) RO 1/28/2020 BLENDED CORROSION ON FRAME AT FS 605 BETWEEN STGR 26R AND STGR 23L. FOUND TO BE OUT OF LIMITS. REMOVED AND INSTALLED NEW FS 605.00 FRAME LOWER SECTOR AND REINFORCING ANGLE. REF: CRJ-200 SRM AND BOMBARDIER DWG. SEE CONTINUATION FOR DETAILS.

Part: FLOOR SUPPORT — CORRODED (PRESSURE DECK) · airframe 39,717 hrs · 34,802 cycles

*LH PRESSURE FLOOR SILL HAS SEVERAL AREAS OF CORROSION (MARKED) (C-CHECK) RO 1/28/2020 REPAIRED LH FLOOR PRESSURE SILL REF REO. ALL STEPS APPLICABLE STEPS COMPLIED WITH. SEE CONTINUATION CARD FOR DETAILS.

Part: FLOOR SUPPORT — CORRODED (PRESSURE DECK) · airframe 39,717 hrs · 34,802 cycles

*RH PRESSURE FLOOR SILL HAS SEVERAL AREAS OF CORROSION ( MARKED ) (C-CHECK) RO 1/28/2020 REPAIRED RH FLOOR PRESSURE SILL REF REO. ALL STEPS COMPLIED WITH. SEE CONTINUATION CARD FOR DETAILS. NO WEIGHT CHANGE AS THESE WERE MINIMAL BLENDS.

Part: FRAME — CRACKED (BS 379) · airframe 39,717 hrs · 34,802 cycles

* STRGR 3L CRACKED AT FRAME 379 MARKED (C-CHECK) RO 1/28/2020 CUT AWAY DAMAGED SECTION OF STRINGER 3L BETWEEN FS 379 AND 394 REF CRJ 200 SRM. INSTALLED STRINGER 3L REPAIR PARTS REF CRJ 200 SRM. WEIGHT OF PART REMOVED IS .12LBS AND WEIGHT OF REPAIR PARTS ARE .24LBS FOR A NET INCREASE OF +.12LBS . RESTORED FINISH. PRESSURE CHECKS GOOD. REFERENCE THE CONTINUE CARD FOR DETAILS.

Part: FLOOR SUPPORT — CORRODED (PRESSURE DECK) · airframe 39,717 hrs · 34,802 cycles

*LH FLOOR SILL ANGLE HAS SEVERAL AREAS OF CORROSION (MARKED ) (C-CHECK) RO 1/28/2020 REPAIRED LH FLOOR PRESSURE SILL ANGLE REF REO. ALL STEPS COMPLIED WITH. SEE CONTINUATION CARD FOR DETAILS. PRESSURE CHECK IS GOOD.

Part: FRAME — CORRODED (BS 589) · airframe 39,717 hrs · 34,802 cycles

*FS 589 FRAME ON FWD SIDE LOWER FLANGE CORRODED FROM STR 25R-23L (C-CHECK) RO 1/28/2020 REPAIRED FRAME AT FS 589. REF BOMBARDIER REO AND BOMBARDIER DWG. REFERENCE THE CONTINUE CARD FOR DETAILS. PRESSURE LEAK CHECKS GOOD.

Part: SEAT TRACK — CORRODED (BS 559-574) · airframe 39,717 hrs · 34,802 cycles

CARGO SEAT TRACK STRUCTURE BETWEEN FS559+112 - FS574.00, LBL27 CORROSION AROUND SCREWHOLES MARKED (C-CHECK) RO 1/28/2020 LBL 27 FLOOR BEAM CAP FOR THE SEAT TRACK CORRODED 100% THRU FLANGE AND INSTALLED A NEW FLOORBEAM CAP FROM APPRX FS 559+10 TO FS 583 REF DRAWING AND REO. COMPLIED WITH TASK CARD.

Part: ANGLE — CRACKED (BS 484) · airframe 39,717 hrs · 34,802 cycles

INBD CLIP AT FS484.00 RH SIDE PRESSURE FLOOR CRACKED, FLAGGED AND MARKED (C-CHECK) RO 1/28/2020 REMOVED CRACKED AND INSTALLED NEW CLIP REF CRJ 200 SRM WITH REO FOR FASTENERS SIZE AND TYPE.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 39,717 hrs · 34,802 cycles

FS280 FLOORBEAM CLIP RBL9 OUTBOARD IS CRACKED (C-CHECK) RO 1/28/2020 REMOVED AND REPLACED FS280 FLOORBEAM CLIP RBL9 OUTBOARD REF. CRJ 200 SRM AND REO. C/W TASK CARD.

Part: SEAT TRACK — CORRODED (BS 574-621) · airframe 39,717 hrs · 34,802 cycles

CARGO SEAT TRACK STRUCTURE BETWEEN FS574.00 - FS621.00, LBL27 CORROSION AROUND SCREWHOLES MARKED (C-CHECK) RO 1/28/2020 REMOVED CORROSION AT CARGO SEAT TRACK STRUCTURE BETWEEN FS574.00 - FS621.00, LBL27 REF CRJ200 SRM. FOUND TO BE OUT OF LIMITS. REMOVED AND INSTALLED NEW FABRICATED FLOOR BEAM CAP FROM FS574 TO FS621 AT LBL27 REF BOMBARDIER DWG, AND REO. COMPLIED WITH TASK CARD. SEE CONTINUE CARD FOR DETAILS.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 39,717 hrs · 34,802 cycles

FS280 FLOORBEAM CLIP LBL9 OUTBOARD IS CRACKED (C-CHECK) RO 1/28/2020 REMOVED CRACKED FLOOR BEAM CLIP FS280 LBL9 OUTBOARD REF. CRJ 200 SRM . - INSTALLED NEW FLOOR BEAM CLIP FS280 LBL9 OUTBOARD P/N 601R-53-11-3529-1 REF. REO. PERFORMED FUNCTIONAL TEST OF THE MLG MANUAL RELEASE SYSTEM REF CRJ 200 AMM FUNCTIONAL TEST GOOD. CALIBRATED TOOL USED TUC4748 CAL DUE DATE 30-APR-20

Part: ANGLE — CRACKED (BS 484) · airframe 39,717 hrs · 34,802 cycles

OTBD CLIP AT FS484.00 RH SIDE PRESSURE FLOOR CRACKED, FLAGGED AND MARKED (C-CHECK) RO 1/28/2020 REMOVED CRACKED CLIP REF CRJ 200 SRM. INSTALLED NEW CLIP REF CRJ 200 SRM WITH REO FOR FASTENERS SIZE AND TYPE. PRESSURE LEAK CHECKS GOOD.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 39,717 hrs · 34,802 cycles

FS280 FLOORBEAM CLIP LBL9 INBOARD IS CRACKED (C-CHECK) RO 1/28/2020 REMOVED AND REPLACED FS280 FLOORBEAM CLIP LBL9 INBOARD REF. CRJ 200 SRM AND REO. C/W TASK CARD. NOTE: REO PREVIOUSLY COMPLIED WITH, AND USED FOR FABRICATION AND INSTALLATION ONLY.

Part: ANGLE — CRACKED (BS 484) · airframe 39,717 hrs · 34,802 cycles

INBD CLIP AT FS484.00 LH SIDE PRESSURE FLOOR CRACKED, FLAGGED AND MARKED (C-CHECK) RO 1/28/2020 REMOVED CRACKED AND INSTALLED NEW CLIP REF CRJ 200 SRM WITH REO FOR FASTENERS SIZE AND TYPE.

Part: ANGLE — CRACKED (BS 484) · airframe 39,717 hrs · 34,802 cycles

OTBD CLIP AT FS484.00 LH SIDE PRESSURE FLOOR CRACKED, FLAGGED AND MARKED (C-CHECK) RO 1/28/2020 REMOVED CRACKED CLIP REF CRJ 200 SRM AND CRJ 200 SRM. INSTALLED NEW CLIP REF CRJ 200 SRM WITH REO FOR FASTENERS SIZE AND TYPE.

Part: STRAP — CORRODED (BS 559) · airframe 39,717 hrs · 34,802 cycles

LH FLOOR STRAP AT FS559.00 CORROSION SPOTS MARKED (C-CHECK) RO 1/28/2020 REMOVED CORROSION FORM LH FLOOR STRAP AT FS559 CRJ 200 SRM. FOUND TO BE OUT OF LIMITS. REMOVED AND INSTALLED NEW LH FLOOR STRAP AT FS559.00 REF CRJ200 SRM AND DWG. PRESSURE CHECK GOOD. COMPLIED WITH TASK CARD. SEE CONTINUE CARD FOR DETAILS.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 39,717 hrs · 34,802 cycles

FS280 FLOORBEAM CLIP RBL9 INBOARD IS CRACKED (C-CHECK) RO 1/28/2020 REMOVED AND REPLACED FS280 FLOORBEAM CLIP RBL9 INBOARD REF. CRJ 200 SRM AND REO. C/W TASK CARD.

Part: MOUNT — CORRODED · airframe 39,717 hrs · 34,802 cycles

BOTH INBD FWD AND AFT FLOOR MOUNT BOLT HOLES FOR THE WARDROBE HAVE CORROSION, MARKED (C-CHECK) RO 1/28/2020 REMOVED CORROSION ON BOTH IB= FWD AND IB-AFT WARDROBE MOUNT PLATES PER CRJ 200 SRM.,CHECKED AND FOUND IB- FWD PLATE WITHIN LIMIT PER CRJ 200 SRM. ORIGINAL THICKNESS OF IB-FWD PLATE .050" ,REMAINING .046" MATERIAL LOSS .004". CHECKED AND FOUND IB-AFT PLATE OUT OF LIMIT . REPLACED WITH NEW PN 601R38670-31 PER CRJ 200 SRM. COMPLIED WITH SKY WEST FORM.

Part: MOUNT — CORRODED · airframe 39,717 hrs · 34,802 cycles

BOTH INBD FWD AND AFT FLOOR MOUNT BOLT HOLES FOR THE GALLEY HAVE CORROSION, MARKED (C-CHECK) RO 1/28/2020 REMOVED CORROSION ON THE GALLEY INBD FWD AND AFT FLOOR MOUNT PLATES PER CRJ 200 SRM. CHECKED AND FOUND AFT PLATE WITHIN LIMIT PER CRJ 200 SRM, ORIGINAL THICHNESS .050" REMAINING .047" ,MATERIAL LOSS .003" . FOUND FWD PLATE OUT OF LIMIT AND REPLACED WITH NEW FABRICATED PLATE 601R38669-55 REF BOMBARDIER DWG AND CRJ 200 SRM. COMPLIED WITH SKY WEST FORM.

Part: SHEAR TIE — CORRODED (BS 394) · airframe 39,717 hrs · 34,802 cycles

*FS 394 FRAME LOWER FLANGE ON FWD SIDE HAS CORROSION BETWEEN STR 25R-25L (C-CHECK) RO 1/28/2020 REMOVED CORROSION ON FRAME FS394 LOWER FWD FLANGE BETWEEN STGR25R TO STGR25L REF CRJ200 SRM. FOUND TO BE OUT OF LIMITS REF CRJ 200 SRM. MEASURED THICKNESS .039. ORIGINAL THICKNESS .080. MATERAL LOSS .014 MAX ALLOWED .008. REMOVED CORRODED ANGLE. REF: CRJ-200 SRM. - INSTALLED THE NEW ANGLE 601R32011-45 TO THE FS 394 LOWER FRAME REF DRAWING AND CRJ 200 SRM. ALL CHECKS GOOD

Part: FLOORBEAM — CORRODED (BS 349) · airframe 39,717 hrs · 34,802 cycles

CORROSION ON FLOOR BEAM SUPPORT ANGLE FS349.00 LH SIDE AT WINDSCREEN TIEDOWN POST, MARKED (C-CHECK) RO 1/28/2020 CORROSION ON FLOOR BEAM SUPPORT ANGLE 100% EXFOILIATED, FABRICATED NEW ANGLE AND INSTALLED IT REF DRAWING, AND COMPLIED WITH SKYCARD STRUCTURAL MAJOR REPAIR.

Part: FLOOR SUPPORT — CORRODED (BS 349-379) · airframe 39,717 hrs · 34,802 cycles

RH FLOOR SILL CORROSION SPOTS AROUND SCREWHOLES FROM FS349.00 - FS379.00, MARKED (C-CHECK) RO 1/28/2020 REMOVED BAD AND INSTALLED REPLACEMENT RH FLOOR SILL FROM FS349.00 €“ FS409.00 WITH REPLACEMENT HARDWARE REF CRJ200 SRM. COMPLIED WITH TASK CARD. SEE CONTINUATION CARD FOR DETAILS.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 39,717 hrs · 34,802 cycles

FS280.00 BEAM HAS CORROSION AROUND SCREW HOLES, COCKPIT ENTRYWAY, MARKED (C-CHECK) RO 1/28/2020 REMOVED AND REPLACED AFT COCKPIT FLOOR SUPPORT AT FS280 REF. CRJ 200 SRM, BOMBARDIER DWG, AND REO. COMPLIED WITH TASK CARD.

Part: SKIN — CORRODED (BS 295-310) · airframe 39,717 hrs · 34,802 cycles

CORROSION ON SKIN DOUBLER FOR ANTENNA BETWEEN FS295.00 - FS310.00, STGR27 - STGR26R, MARKED (C-CHECK) RO 1/28/2020 REMOVED CORROSION FROM SKIN DOUBLER FOR TCAS ANTENNA BETWEEN FS295.00- FS310.00, STGR27-STGR26R REF CRJ200 SRM. FOUND TO BE OUT OF LIMITS. INSTALLED NEW DOUBLER REF CRJ200 SRM AND DWG. PRESSURE CHECK GOOD. SEE CONTINUE CARD FOR DETAILS. COMPLIED WITH TASK CARD.

Part: CUP — CORRODED (DOOR HANDRAIL) · airframe 39,717 hrs · 34,802 cycles

*PAX DOOR FWD AND AFT HANDRAIL CUPS CORRODED (C-CHECK) RO 1/28/2020 BLENDED OUT CORROSION ON THE FWD AND AFT PAX DOOR HANDRAIL CUPS REF CRJ 200 SRM, AFT CUP IN LIMITS AND FWD CUP OUT OF LIMITS REF CRJ 200 SRM, REPLACED FWD CUP REF CRJ 200 SRM AND DRAWING.

Part: FRAME — CORRODED (BS 319.7) · airframe 39,717 hrs · 34,802 cycles

CORROSION FWD SIDE FRAME FLANGE ON FRAME AT FS319.70 BETWEEN STGR24L - STGR25R, MARKED (C-CHECK) RO 1/28/2020 REPAIRED FRAME FS319.70 BETWEEN STGR24L TO STGR25R PER COMPLIED WITH ALL STEPS OF BOMBARDIER REO.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 39,717 hrs · 34,802 cycles

COCKPIT ENTRYWAY AFT FLOOR SILL ANGLE CORROSION, MARKED, FS280.00 (C-CHECK) RO 1/28/2020 REPAIRED CORRODED COCKPIT ENTRYWAY AFT FLOOR SILL ANGLE FS280.00 REF. REO, ALL STEPS COMPLIED WITH.

Part: FRAME — CORRODED (BS 349) · airframe 39,717 hrs · 34,802 cycles

*FS 349 FRAME OPPER FLANGE HAS CORROSION AT STR 26R (C-CHECK) RO 1/28/2020 REMOVED CORROSION ON FRAME AT FS349 UPPER FLANGE STGR26R CRJ200 SRM, REPAIRED FRAME REF REO. COMPLIED WITH ALL STEPS OF REO, SEE CONTINUATION CARDE FOR DETAILS.

Part: SKIN — CRACKED (NLG DOOR FRAME) · airframe 39,717 hrs · 34,802 cycles

* THE NLG WHEEL WELL SKIN CUTOUT ON LH SIDE JUST BEHIND THE AFT NLG DOOR IS CRACKED. (C-CHECK) RO 1/28/2020 REPAIRED THE CRACK AT THE NLG CUTOUT (LH) SIDE. REF BOMBARDIER REO AND REO. REFERENCE THE CONTINUE CARD FOR DETAILS.

Part: RIB — CORRODED (LT WING) · airframe 39,717 hrs · 34,802 cycles

*AT WS 50.00 BATT RIB HAS CORROSION AT CANNON PLUG CONNECTIONS R/H INSIDE WHEEL WELL (C-CHECK) RO 1/28/2020 BLENDED CORROSION AT RIGHT BATT RIB.AT WS 53.60 FOUND TO BE WITHIN LIMITS REF REO. COMPLIED WITH ALL APPLICABLE STEPS ON REO. COMPLIED WITH TASK CARD. SEE CONTINUATION FOR FURTHER DETAILS.

Part: SKIN — CORRODED (BS 559-574) · airframe 39,717 hrs · 34,802 cycles

*FS559.00 €“ FS574.00 BETWEEN STRG 26L AND 26R EXTERNAL SKIN CORROSION AT NUMEROUS AREAS (MARKED) (C-CHECK) RO 1/28/2020 BLENDED CORROSION BETWEEN FASTENER ROWS @ FS.559 TO FS.559+32, FS.559+32 TO FS559+80, AND FS.559+80 TO FS.574 ON STRG 26L TO STRG 26R. FOUND TO BE WITHIN LIMITS REF REO, DWG, AND CRJ200 SRM. COMPLIED WITH ALL APPLICABLE STEPS OF REO. COMPLIED WITH TASK CARD. COMPLETED SKYWEST FORM M-337.

Part: VANE — CHAFED (RT WING TE FLAP) · airframe 39,717 hrs · 34,802 cycles

* R/H INBD FLAP VANE INBD L/E CAP IS CHAFFED, (FLAGGED (C-CHECK) RO 1/28/2020 BLENDED RH INBOARD FLAP VANE INBOARD LE CAP CHAFE REF REO. FOUND TO BE OUT OF LIMITS. REMOVED AND INSTALLED NEW RH INBOARD FLAP VANE INBOARD LE CAP REF BOMBARDIER DWG AND CRJ200 SRM. SEE CONTINUE CARD FOR DETAILS. COMPLIED WITH TASK CARD.

Part: VANE — CHAFED (RT WING TE FLAP) · airframe 39,717 hrs · 34,802 cycles

* R/H INBD FLAP VANE MIDDLE L/E CAP IS CHAFFED, (FLAGGED) (C-CHECK) RO 1/28/2020 BLENDED RH INBOARD FLAP VANE MIDDLE LE CAP CHAFE REF REO. FOUND TO BE OUT OF LIMITS. REMOVED AND INSTALLED NEW RH INBOARD FLAP VANE MIDDLE LE CAP REF BOMBARDIER DWG AND CRJ200 SRM. SEE CONTINUE CARD FOR DETAILS. COMPLIED WITH TASK CARD.

Part: VANE — CHAFED (RT WING TE FLAP) · airframe 39,717 hrs · 34,802 cycles

* R/H INBD FLAP VANE OUTBD L/E CAP IS CHAFFED, (FLAGGED) (C-CHECK) RO 1/28/2020 BLENDED RH INBOARD FLAP VANE OUTBOARD LE CAP CHAFE REF. FOUND TO BE OUT OF LIMITS. REMOVED AND INSTALLED NEW RH INBOARD FLAP VANE OUTBOARD LE CAP REF BOMBARDIER DWG AND CRJ200 SRM. SEE CONTINUE CARD FOR DETAILS. COMPLIED WITH TASK CARD.

Part: VANE — CHAFED (LT WING TE FLAP) · airframe 39,717 hrs · 34,802 cycles

* L/H INBD FLAP VANE OUTBD L/E CAP IS CHAFFED, (FLAGGED) (C-CHECK) RO 1/28/2020 BLEND LEFT I/B FLAP VANE O/B CAP REF REO. FOUND TO BE OUT OF LIMITS REF REO. REMOVED AND REPLACED VANE CAP REF CRJ200 SRM, BOMBARDIER DRAWING. COMPLIED WITH SKY CARD.

Part: SKIN — CHAFED (LT WING TE FLAP) · airframe 39,717 hrs · 34,802 cycles

* L/H INBD FLAP VANE MIDDLE L/E CAP IS CHAFFED, (FLAGGED) (C-CHECK) RO 1/28/2020 REMOVED AND REPLACED WITH NEW 1EA. L/H I/B FLAP MIDDLE L/E VANE CAP (P/N 601R14303-51S). REF CRJ200 SRM AND BOMBARDIER DWG. COMPLIED WITH TASK CARD.

Part: BULKHEAD WEB — CRACKED (BS 621) · airframe 39,717 hrs · 34,802 cycles

COMPLY WITH SCHEDULED MAINTENANCE CODE: AD - COMPLY WITH PARAGRAPH (J) OF AD (J)(1) DOING A NONDESTRUCTIVE INSPECTION FOR CRACKING OF THE FORWARD FACE OF THE FUSELAGE STATION (FS) 621 PRESSURE BULKHEAD, IN ACCORDANCE WITH AWL OF BOMBARDIER TR, TO APPENDIX B€“AIRWORTHINESS LIMITATIONS, OF PART 2 OF THE BOMBARDIER. (J)(2) MODIFYING THE RPB AND DOING A NONDESTRUCTIVE INSPECTION FOR CRACKING OF THE FS 621 PRESSURE BULKHEAD WEB, IN ACCORDANCE WITH BOMBARDIER REPAIR ENGINEERING ORDER (REO). AND MARKING THIS CAMP AS "STRUCTURAL REPAIR," WHICH WILL GENERATE AN RA FOR TRACKING THE SDIR FOR THIS REO ON THIS AIRPLANE, PART NUMBER: - , SERIAL NUMBER: 7578, POSITION: (C-CHECK) RO 1/28/2020 COMPLIED WITH PARAGRAPH (J) OF AD BY: / (J)(1) DOING A NONDESTRUCTIVE INSPECTION FOR CRACKING OF THE FORWARD FACE OF THE FUSELAGE STATION (FS) 621 PRESSURE BULKHEAD, IN ACCORDANCE WITH AWL OF BOMBARDIER, TO APPENDIX B€“AIRWORTHINESS LIMITATIONS, OF PART 2 OF THE BOMBARDIER. / (J)(2) MODIFYING THE RPB AND DOING A NONDESTRUCTIVE INSPECTION FOR CRACKING OF THE FS 621 PRESSURE BULKHEAD WEB, IN ACCORDANCE WITH BOMBARDIER REPAIR ENGINEERING ORDER (REO). AND;MARKING THIS CAMP AS "STRUCTURAL REPAIR," WHICH WILL GENERATE AN RA FOR TRACKING THE SDIR FOR THIS REO ON THIS AIRPLANE.COMPLIED WITH SKY CARD.

Part: STRUCTURE — CORRODED (PAX DOOR) · airframe 36,466 hrs · 31,187 cycles

CORROSION ON PAX DOOR AND BRACKET. REMOVED CORROSION AND REPLACED THE BRACKET IAW SRM.

Part: INTERCOSTAL — CORRODED (NOT REPORTED) · airframe 36,466 hrs · 31,187 cycles

INTERCOSTAL HAS CORROSION. INSTALLED A NEW INTERCOSTAL IAW SRM.

Part: CLEAT — CORRODED (PAX DOOR) · airframe 36,466 hrs · 31,187 cycles

PAX DOOR INTERCOSTAL CLEAT IS CORRODED. REMOVED AND REPLACED THE CLEAT IAW SRM 51-42-06.

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 36,466 hrs · 31,187 cycles

PAX DOOR INTERCOSTAL HAS CORROSION. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM.

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 36,466 hrs · 31,187 cycles

PAX DOOR INTERCOSTAL HAS CORROSION. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM.

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 36,466 hrs · 31,187 cycles

PAX DOOR INTERCOSTAL HAS CORROSION. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM.

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 36,466 hrs · 31,187 cycles

PAX DOOR INTERCOSTAL HAS CORROSION. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM.

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 36,466 hrs · 31,187 cycles

PAX DOOR INTERCOSTAL HAS CORROSION. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM.

Part: DOOR FRAME — CORRODED (PAX DOORWAY) · airframe 36,466 hrs · 31,187 cycles

PAX DOOR AFT FRAME HAS CORROSION. INSTALLED THE DOOR FRAME IAW SRM.

Part: DOOR SILL — CORRODED (SERVICE DOORWAY) · airframe 36,466 hrs · 31,187 cycles

SERVICE DOOR SILL HAS CORRODED. REMOVED AND REPLACED THE DOOR SILL IAW SRM.

Part: DOOR FRAME — CORRODED (PAX DOORWAY) · airframe 36,466 hrs · 31,187 cycles

PAX DOOR FWD FRAME HAS CORROSION. INSTALLED A NEW DOOR FRAME IAW SRM.

Part: STRUT — DISCHARGED (NLG) · airframe 35,337 hrs · 29,904 cycles

NOSE GEAR DISAGREE WARNING AFTER TAKE-OFF. RETURNED TO FIELD. SERVICED NLG STRUT IAW AMM. OPS CHECK GOOD. PERFORMED MULTIPLE GEAR SWINGS IAW AMM. OPS CHECKED GOOD.

Part: FLOOR SKIN — CRACKED (BS 461) · airframe 33,170 hrs · 27,554 cycles

PRESSURE FLOOR SKIN AT BS 461 HAS TWO CRACKS, TWO INCHES LONG, ONE BETWEEN BL 0 AND LBL 9 AND ONE BETWEEN BL 0 AND RBL 9. REPAIRED IAW SRM.

Part: FLOOR SKIN — DAMAGED (BS 461) · airframe 33,170 hrs · 27,554 cycles

FLOOR SKIN AT BS 461, RBL 9 CUT INTO DURING REPAIR. C-CHECK, NOT RELEASED YET REPAIRED IAW SRM.

Part: SKIN — CORRODED (BS 409) · airframe 33,169 hrs · 27,553 cycles

EXTERNAL FUSELAGE SKIN CORRODED UNDER ADF ANTENNA BETWEEN FS 409+64 AND FS 409+84, STRINGERS 1L AND 1R. C-CHECK, NOT RELEASED YET, WORK IN PROGRESS.

Part: STRUCTURE — CORRODED (BS 333) · airframe 33,169 hrs · 27,553 cycles

FS 333.00 IS CORRODED BETWEEN 25R AND 25L. R & R FS 333.00 IAW SRM.

Part: BULKHEAD WEB — CRACKED (BS 202) · airframe 33,169 hrs · 27,553 cycles

FS 202.75 BULKHEAD WEB IS CRACKED AROUND BRAKE CABLE PASS THROUGH. INSPECTION REPAIRED FS 202.75, BL 23.71 PRESSURE BULKHEAD IAW REO.

Part: STIFFENER — CRACKED (BS 409) · airframe 33,169 hrs · 27,553 cycles

FS 409+128, RBL 18 INBD VERTICAL POST HAS AN INDICATION NOTED IN THE AFT FLANGE RADIUS AT WL 69 APPROXIMATELY .265" LONG BY 55 PERCENT FSH AND OTBD POST HAS INDICATION IN THE AFT FLANGE RADIUS AT WL69 APPROXIMATELY .240" LONG BY 60 PERCENT FSH. C-CHECK NOT RELEASED YET. REPAIRED FS 409.00 + 128, RBL 18 INBD VERTICAL POST IAW REO.

Part: CONTROL PANEL — MALFUNCTIONED (CABIN PRESSURE) · airframe 30,645 hrs · 24,997 cycles

DURING CLIMBOUT, ACFT WOULD NOT PRESSUREIZE INITIALLY. AFTER REACHING 500 FT, AIRCRAFT FINALLY PRESSURIZED AFTER LEVELING OFF AND CONTINUED TO PERFORM NORMALLY. RETURNED TO FIELD. R & R CABIN PRESSURE CONTROL PANEL IAW AMM. OPS CHECKED GOOD.

Part: PCU — FAULTED (SPOILERS) · airframe 30,357 hrs · 24,699 cycles

FLT SPOILERONS FAULTED, UNCOMMANDED DEPLOYMENT OF FLIGHT SPOILERS, OTBD GROUND SPOILERS AND RT SPOILERON. R & R RT OTBD SPOILERON PCU IAW AMM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 30,233 hrs · 24,563 cycles

EXTERIOR EMERGENCY LIGHT NR 5 INOPERATIVE. REPLACED THE LAMP IAW AMM.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 30,075 hrs · 24,400 cycles

LT AND RT OVERWING EMERGENCY EXIT DOOR SIDEWALL EXIT SIGN HAVE SEVERAL LAMPS BURNED OUT. REPLACED LAMPS.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 29,878 hrs · 24,206 cycles

CABIN CEILING EXIT SIGN HAS A LIGHT BULB BURNED OUT. REPLACED BULB.

Part: SKIN — CHAFED (RT MLG DOOR) · airframe 29,601 hrs · 23,949 cycles

RT MLG DOOR INNER SKIN CHAFED AT THE LE. C-CHECK BLENDED CHAFFED ON RT MLG DOOR INNER SKIN AT LE IAW REO.

Part: VANE — CHAFED (TE FLAP) · airframe 29,601 hrs · 23,949 cycles

REPLACE RT INBD FLAP, INBD FLAP VANE LE. C-CHECK REPLACED RT INBD FLAP, INBD FLAP VANE LE IAW SRM.

Part: SKIN — CHAFED (TE FLAP VANE) · airframe 29,601 hrs · 23,949 cycles

REPLACE LT INBD FLAP, MIDDLE FLAP VANE LE SKIN. C-CHECK R & R LT INBD FLAP, MIDDLE FLAP VANE LE SKIN IAW SRM.

Part: SILL — CORRODED (FUSELAGE) · airframe 29,601 hrs · 23,949 cycles

UPPER SURFACE OF PRESS FLOOR SILL STRUCTURE HAS CORROSION THROUGHOUT FS 445.00 THRU FS 559.00, RBL36 THRU RBL45. C-CHECK REMOVED CORROSION IAW REO & SRM.

Part: SILL — CORRODED (FUSELAGE) · airframe 29,601 hrs · 23,949 cycles

UPPER SURFACE OF PRESS FLOOR SILL STRUCTURE HAS CORROSION THROUGHOUT FS 445.00 THRU FS 559.00, LBL 36 THRU LBL 45. C-CHECK REMOVED CORROSION IAW REO & SRM.

Part: VANE — CHAFED (TE FLAP) · airframe 29,601 hrs · 23,949 cycles

RT INBD FLAP, OTBD FLAP VANE HAS CHAFING. C-CHECK BLENDED & REPAIRED IAW REO & SRM.

Part: VANE — CHAFED (TE FLAP) · airframe 29,601 hrs · 23,949 cycles

LT INBD FLAP, OTBD FLAP VANE HAS CHAFING. C-CHECK BLENDED & REPAIRED IAW REO & SRM.

Part: VANE — CHAFED (TE FLAP) · airframe 29,601 hrs · 23,949 cycles

LT INBD FLAP, INBD FLAP VANE HAS CHAFING. C-CHECK REPAIRED IAW REO & SRM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 29,348 hrs · 23,699 cycles

THE EXTERIOR EMERGENCY EXIT LIGHT FOR THE SERVICE DOOR IS BURNED OUT. FLT 4762 RELAMPED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,272 hrs · 22,648 cycles

SECOND TO LAST EMERGENCY OVERHEAD LIGHT DOES NOT ILLUMINATE. RELAMPED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,479 hrs · 21,877 cycles

MAIN CABIN DOOR FLOOR LEVEL EMERGENCY LIGHT BURNED OUT. (FLT 4472) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,456 hrs · 21,854 cycles

AFT EMERGENCY CEILING LIGHT IS BURNED OUT. (FLT 4842) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,430 hrs · 21,829 cycles

EMERGENCY OVERHEAD LIGHT NR 2 BURNED OUT. (FLT 4455) RELAMPED EMERGENCY LIGHT.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 27,170 hrs · 21,558 cycles

RIGHT WINDSHIELD CRACKED. (FLT 4554) REPLACED WINDSHIELD IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,985 hrs · 21,394 cycles

NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4461) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,850 hrs · 21,267 cycles

NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4645) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,476 hrs · 20,903 cycles

NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4579) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,366 hrs · 20,797 cycles

EMERGENCY LIGHT IS OUT OVER RIGHT WING. (FLT 4510) RELAMPED EMERGENCY LIGHT.

Part: SPRING — OUT OF ADJUST (CABIN DOOR) · airframe 26,338 hrs · 20,769 cycles

MAIN CABIN DOOR LEVER IS HARD TO MOVE WHEN OPENING AND CLOSING DOOR. (FLT 4827) ADJUSTED MAIN CABIN DOOR CABLE SPRING BACK TENSION.

Part: PIN — LACK OF LUBE (NLG) · airframe 26,274 hrs · 20,705 cycles

GEAR DISAGREE IN DOWN POSITION WITH NOSE GEAR. (FLT 4670) LUBRICATED NLG UPLOCK PIN.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 26,108 hrs · 20,550 cycles

FLT 4501, NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. RELAMPED EMERGENCY LIGHT.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 26,108 hrs · 20,550 cycles

FLT 4745, NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. RELAMPED EMERGENCY LIGHT.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 25,972 hrs · 20,431 cycles

(C-CHECK) FS 280 BULKHEAD WEB CRACKED AT LBL 10 AND RBL 10 AT FLOOR SUPPORT. REPAIRED FS 280 BULKHEAD WEB AT LBL 10 AND RBL 10 AT FLOOR SUPPORT.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 25,972 hrs · 20,431 cycles

(C-CHECK) AREAS OF CORROSION FOUND ON LBL 27.00 BETWEEN FS 559+80 AND FS 539+112. REPAIRED CORROSION AT LBL 27.00 BETWEEN FS 559+80 AND FS 539+112.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,518 hrs · 20,000 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4523) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,418 hrs · 19,897 cycles

NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4549) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,252 hrs · 19,730 cycles

AFT OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4669) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,198 hrs · 19,681 cycles

AFT CEILING EMERGENCY LIGHT IS OUT. (FLT 4507) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,118 hrs · 19,598 cycles

NR 4 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4689) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 25,118 hrs · 19,598 cycles

RIGHT SIDE EXTERIOR FORWARD EMERGENCY LIGHT DOES NOT ILLUMINATE. (FLT 4551) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,118 hrs · 19,598 cycles

NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4456) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,030 hrs · 19,512 cycles

RIGHT FORWARD OVERWING EMERGENCY EXIT LIGHT IS OUT. (FLT 4554) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,030 hrs · 19,512 cycles

NR 2 AND NR 4 OVERHEAD EMERGENCY LIGHTS ARE OUT. (FLT 4649) RELAMPED EMERGENCY LIGHTS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,018 hrs · 19,500 cycles

NR 2 OVERHEAD EMERGENCY CEILING LIGHT IS OUT. (FLT 4549) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,939 hrs · 19,432 cycles

NR 2 CEILING EMERGENCY LIGHT IS OUT. (FLT 7771) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,870 hrs · 19,366 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4760) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,798 hrs · 19,306 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4613) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,355 hrs · 18,919 cycles

NR 4 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4511) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,017 hrs · 18,637 cycles

NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4504) RELAMPED EMERGENCY LIGHT.

Part: TIRE — FAILED (MLG) · airframe 23,945 hrs · 18,579 cycles

NR 4 TIRE BLEW ON LANDING. (FLT 4630) REPLACED NR 3 AND NR 4 MLG WHEEL ASSEMBLIES. NO OTHER DAMAGE NOTED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,839 hrs · 18,489 cycles

NR 1 OVERHEAD EMERGENCY LIGHT OUT. (FLT 4769) RELAMPED EMERGENCY LIGHT.

Part: YOKE — CORRODED (ENGINE MOUNT) · airframe 23,486 hrs · 18,195 cycles

LEFT ENGINE YOKE HAS CORROSION ON THE BUSHING FACES ON LINK ATTACH END. (ENGINE CHANGE) INSTALLED SERVICEABLE YOKE ASSEMBLY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,116 hrs · 17,892 cycles

THIRD AFT EMERGENCY LIGHT INOPERATIVE. (FLT 4523) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,087 hrs · 17,015 cycles

NR 1 OVERHEAD CABIN EMERGENCY FLOOD LIGHT INOP. (FLT 4581) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,087 hrs · 17,015 cycles

MAIN CABIN OVERHEAD EMERGENCY EXIT LIGHT INOP. (FLT 4718) RELAMPED EMERGENCY LIGHT.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 21,869 hrs · 16,827 cycles

PASSENGER DOOR THRESHOLD AND ATTACH STRUCTURE CORRODED. (C CHECK) REPAIRED PER SRM.

Part: ANGLE — CRACKED (MLG WW) · airframe 21,869 hrs · 16,827 cycles

RIGHT AND LEFT MAIN LANDING GEAR WHEEL WELL BAT ANGLES CRACKED. (C CHECK) REPAIRED PER REO.

Part: ANGLE — CRACKED (MLG WW) · airframe 22,305 hrs · 17,188 cycles

LEFT AND RIGHT MLG WHEEL WELL BAT ANGLES CRACKED. (C CHECK) REPAIRED PER REO.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 22,305 hrs · 17,188 cycles

FS 621 AFT PRESSURE BULKHEAD CRACKED AT CARGO DOOR AFT ROLLER GUIDE TRACK. (C CHECK) REPAIRED PER REO.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,312 hrs · 16,363 cycles

NR 2 CEILING LEVEL EMERGENCY FLOODLIGHT INOP. (FLT 4517) RELAMPED EMERGENCY FLOODLIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,171 hrs · 16,253 cycles

OVERHEAD EMERGENCY FLOODLIGHT NR 3 INOP. (FLT 4620)RELAMPED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,925 hrs · 16,063 cycles

NR 2 CEILING EMERGENCY LIGHT INOP. (FLT 4765) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,887 hrs · 16,023 cycles

NR 4 EMERGENCY FLOOD LIGHT IN CABIN CEILING INOP. (FLT 4843) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,764 hrs · 15,913 cycles

NR 3 CEILING EMERGENCY LIGHT INOP. (FLT 4464) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,609 hrs · 15,777 cycles

OVERHEAD EMERGENCY LIGHTS NR 1 AND NR 2 INOP. (FLT 4754) RELAMPED EMERGENCY LIGHTS.

Part: HANDLE — INTERMITTENT (MLG) · airframe 20,030 hrs · 15,321 cycles

FLT 4903 - GEAR DISAGREE MESSAGE DISPLAYED. REPLACED GEAR HANDLE, PN 7-45502-5 SN OFF 1405.

Part: ACTUATOR — FAILED (MLG) · airframe 19,743 hrs · 15,087 cycles

FLT 4784 - LEFT MAIN LANDING GEAR DID NOT COME DOWN AND LOCK. REPLACED LEFT SIDE STAY ACTUATOR.

Part: RELIEF VALVE — FAILED (MLG) · airframe 19,802 hrs · 15,135 cycles

FLT 4436 - LEFT MAIN LANDING GEAR SLOW TO EXTEND. REPLACED BALANCED RELIEF VALVE.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 18,764 hrs · 14,344 cycles

FS 280 FLOORBEAM ATTACH CLIPS AT LBL 9 ARE CRACKED. C-CHECK, REPLACED CLIPS.

Part: FLOORBEAM — CRACKED (BS 625) · airframe 18,764 hrs · 14,344 cycles

LEFT FS 625 OBLIQUE ANGLE CRACKED. C-CHECK, REPLACED ANGLE.

Part: BEAM — CRACKED (BS 409) · airframe 18,764 hrs · 14,344 cycles

VERTICAL BEAM AT FS 409 LBL 27 CRACKED AT INBOARD LOWER RADIUS. C-CHECK, REPAIRED PER REO.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 18,764 hrs · 14,344 cycles

CRACKED WEB ON FLOOR ANGLE AT FS 280 LBL 9 LOWER FLANGE. C-CHECK, REPAIRED PER REO.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 18,764 hrs · 14,344 cycles

AFT CAP ANGLE ATTACHED TO FS 280 IS CRACKED AT OUTBOARD SIDE OF LBL9 AND RBL9. C-CHECK, REPAIRED PER REO.

Part: THROTTLE — BINDING (LEFT) · airframe 17,932 hrs · 13,707 cycles

LEFT THROTTLE OCCASSIONALLY BINDS AND IS STIFF. (FLT 3801) REPLACED ENGINE THROTTLE CABLE ON LEFT SIDE IAW AMM 76-11-09. ENGINE RUN CHECK GOOD.

Part: CONTROLLER — OUT OF ADJUST (LT ENGINE) · airframe 17,624 hrs · 13,480 cycles

FLT 3919 - THE LEFT ENGINE SHUT DOWN WHILE TAXIING TO THE GATE. ADJUSTED THE LEFT ENGINE CONTROL RIGGING. OPS CHECK GOOD.

Part: RESERVOIR — MALFUNCTIONED (HYDRAULIC SYSTEM) · airframe 16,801 hrs · 12,857 cycles

FLT 3896 - WHEN SELECTING GEAR DOWN ON FINAL, NOSE GEAR DIDN'T COME DOWN. CYCLED GEAR TWICE AND RECEIVED THREE GREEN INDICATIONS. REPLACED NR 3 HYDRAULIC RESERVOIR IAW AMM 29-12-30, AND PERFORMED EXTENSION/RETRACTION FUNCTIONAL TEST IAW AMM 32-30-00 OPS AND LEAK CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 15,946 hrs · 12,217 cycles

FORWARD FLOOR EMERGENCY LIGHTS ARE INOP, FLIGHT NR 3916. INSTALLED NEW EMERGENCY LIGHT FLOOR SEGMENT. OPS CHECKS GOOD.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 15,946 hrs · 12,217 cycles

FOUND FORWARD FLOOR EMERGENCY LIGHTS ARE INOP. REPLACED INVERTER IAW MM 55-51-04. OPS CHECK GOOD, P/N - 5925-2.

Part: ADC — MALFUNCTIONED (NR 1) · airframe 14,963 hrs · 11,457 cycles

EFIS COMP WITH MACH TRIM CAUTION MESSAGE ON DESCENT ALONG WITH ASSOCIATED FLAGS. REPLACED NR 1 ADC IAW MM 34-13-01. PURGED MAIN PITOT STATIC SYSTEM IAW MM 34-11-00.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 14,963 hrs · 11,457 cycles

FORWARD CEILING EMERGENCY LIGHT IS INOP. REPLACED LAMP IN FORWARD CEILING EMERGENCY LIGHT.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 14,430 hrs · 11,038 cycles

AFT CEILING EMERGENCY EXIT LIGHT INOP. RELAMPED AFT CEILING EMERGENCY EXIT LIGHT. OPERATIONAL CHECKS GOOD.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 13,663 hrs · 10,466 cycles

RT 280 STA RBL9 FLOORBEAM SUPPORT CLIPS 2 INBOARD AND OUTBOARD CRACKED, DISCOVERED DURING C-CHECK INSPECTION. REPLACED 2 FLOORBEAM SUPPORT CLIPS PER CRJ200 SRM 51-42-06 REO NR 601R-53-11-137 REV HC AND RII 51-900-1002.

Part: ATTACH BRACKET — CRACKED (APU OIL COOLER) · airframe 13,663 hrs · 10,466 cycles

APU OIL COOLER ATTACH BRACKET CRACKED, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED NEW APU OIL COOLER ATTACH BRACKET IAW CRJ200 AMM TASK 49-91-08-400-803.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 13,663 hrs · 10,466 cycles

RT FS 484 RBL 36 AND 27, BRACKET CRACKED, DISCOVERED DURING C-CHECK INSPECTION. NEW CLIPS INSTALLED IAW REO601R-53-41-059 REV A.

Part: FITTING — CRACKED (FUSELAGE) · airframe 13,663 hrs · 10,466 cycles

RT FS 625 BL 40 CLIP CRACKED, DISCOVERED DURING C-CHECK INSPECTION. REPLACED RT FS 625 BL40 CLIP PER SRM 51-42-06 PG 4 ITEM B.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 13,663 hrs · 10,466 cycles

LT FS 484, LBL 36 BRACKET CRACKED, DISCOVERED DURING C-CHECK INSPECTION. REPAIR ANGLE INSTALLED IAW REO601R-53-41-059.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 12,320 hrs · 9,469 cycles

LEFT OUTSIDE FWD EMERGENCY LIGHT IS INOP. RELAMPED LEFT OUTSIDE FORWARD EMERGENCY LIGHT. OPERATIONAL CHECK GOOD.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 11,873 hrs · 9,140 cycles

FWD CEILING EMERGENCY FLOOD LIGHT INOP. RELAMPED FWD CEILING EMERGENCY LIGHT. OPERATIONAL CHECK GOOD.

Part: SWITCH — MALFUNCTIONED (STAB DISCONNECT) · airframe 11,518 hrs · 8,863 cycles

"STAB TRIM" AND "MACH TRIM" CAUTION MESSAGES ILLUMINATED AFTER TAKE OFF (1500' AGL). REPLACED CO-PILOT STAB DISCONNECT SWITCH IAW MM 27-41-30. OPERATIONAL CHECK GOOD IAW MM 27-40-00.

Part: CONTROL UNIT — MALFUNCTIONED (HORIZ STAB TRIM) · airframe 11,480 hrs · 8,833 cycles

STAB TRIM AND MACH TRIM FAILED WILL NOT RE-ENGAGE. REPLACED THE HSTCU IAW MM 27-41-01, OPERATIONAL CHECK GOOD IAW MM 27-40-00.

Part: CONTROL UNIT — MALFUNCTIONED (TRIM ACTUATOR) · airframe 11,470 hrs · 8,828 cycles

STAB TRIM CHANNEL 2 DISCONNECTS. REPLACED HORIZONTAL STABLILIZER TRIM ACTUATOR AND MOTOR CONTROL UNIT IAW CRJMM 27-42-01 AND 27-42-05. OPERATIONAL CHECK GOOD, PN: 8396-3, SN: OFF 750.

Part: PCU — MALFUNCTIONED (SPOILERS) · airframe 11,010 hrs · 8,475 cycles

SPOILERON FAULT MSG. REPLACED LEFT INBOARD SPOILERON PCU IAW 27-61-01. OPERATIONAL CHECK GOOD.

Part: POWER SUPPLY — INTERMITTENT (EMERGENCY LIGHT) · airframe 10,896 hrs · 8,374 cycles

FLOOR EMERGENCY LIGHT STRIP INTERMITTENT. REPLACED FWD POWER SUPPLY LIGHTING SECTION ELECTRICAL SUPPLY IAW MM 33-51-00. OPERATIONAL CHECK GOOD.

Part: CONTROL PANEL — MALFUNCTIONED (RUDDER TRIM) · airframe 10,633 hrs · 8,174 cycles

RUDDER TRIM WILL NOT ACTUATE NOSE RIGHT. REPLACED RUDDER TRIM/AILERON TRIM CONTROL PANEL. OPERATIONAL CHECK GOOD REF MM 27-12-10.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 10,584 hrs · 8,137 cycles

FORWARD MOST OVERHEAD EMERGENCY FLOOD LIGHT INOP. REPLACED LAMP, OPERATIONAL CHECK GOOD.

Part: LIGHT — BROKEN (CABIN) · airframe 9,981 hrs · 7,663 cycles

FLOOR EMERGENCY FLOODLIGHT ON BACKWARD OF WARDROBE UNIT BROKEN. REPLACED FLOODLIGHT ASSY WITH NEW UNIT. OPERATIONAL CHECK GOOD.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 9,933 hrs · 7,627 cycles

RT WINDSHIELD CRACKED EN ROUTE. REPLACED RIGHT WINDSHIELD IN ACCORDANCE WITH 56-11-00, 56-11-01, 56-12-01. P/N OFF 601R33033-14, S/N OFF 01173H1516.

Part: COMPUTER — MALFUNCTIONED (STALL WARNING) · airframe 9,476 hrs · 7,270 cycles

STALL FAIL MSG IN FLIGHT. REPLACED STALL COMPUTER IAW 27-34-00 AND REPLACED LEFT AOA IAW 27-35-05. OPERATIONAL CHECK GOOD.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 9,388 hrs · 7,199 cycles

AFT OVERHEAD EMERGENCY LIGHT INOP. RELAMPED AFT OVERHEAD EMERGENCY LIGHT, OPERATIONAL CHECK GOOD.

Part: OXYGEN MASK — DEPLOYED (ROWS 8 A&B) · airframe 8,893 hrs · 6,823 cycles

THE O2 MASKS FELL, ROWS 8A & B. SECURED O2 MASKS AT 8A & B.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 9,345 hrs · 7,167 cycles

FS 280 BL 9 LT INBOARD AND OUTBOARD BRACKETS CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPLACED FS 280 BL 9 LT INBOARD AND OUTBOARD BRACKETS IAW CRJ 200 SRM 51-42-06 PG 18, 51-40-11 PG 1, 2, 51-42-06 PG 11.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 9,345 hrs · 7,167 cycles

FS 625 STRINGER 14, LT AND RT SIDE ANGLES CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPLACED LT AND RT STRINGER 14 SIDE-ANGLES IAW CRJ 200 SRM 51-10-6 PG 3 PARA D & CRJ 200 SRM 51-42-06.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 9,345 hrs · 7,167 cycles

FS 280 BL RIGHT INBOARD ANGLE BRACKET CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPLACED ANGLE IAW CRJ 200 SRM 51-42-06 PG 4 & 18 & 51-42-20 PG 3 & 16.

Part: CONTROL UNIT — MALFUNCTIONED (SPOILERS) · airframe 8,262 hrs · 6,343 cycles

IB AND OB GROUND SPOILER FAULT MESSAGE SPOILERON MESSAGE. REPLACED SECU, OPERATIONAL CHECK GOOD.

Part: CONTROL PANEL — MALFUNCTIONED (AILERON/RUDDER) · airframe 8,070 hrs · 6,193 cycles

AILERON WILL TRIM TO LT BUT NOT TO RT. REMOVED AND REPLACED AILERON/RUDDER TRIM CONTOL PANEL. OPERATIONAL CHECK GOOD. P/N: 601R51226-23SW.

Part: PCU — MALFUNCTIONED (FLIGHT SPOILER) · airframe 7,531 hrs · 5,770 cycles

FLIGHT SPOILERS FAULT MESSAGE DISPLAYED ON ED-2. REMOVED AND REPLACED RIGHT HAND FLIGHT SPOILER NR 2 PCU IAW CRJ MM 27-62-01. OPERATIONAL CHECK GOOD.

Part: DCU — MALFUNCTIONED (COCKPIT) · airframe 6,282 hrs · 4,821 cycles

NR 1 PFD WENT BLANK FOLLOWED BY A NR 1 YAW DAMPER DISCONNECT AND AUTO PILOT DISCONNECT. BOTH RE-ENGAGED. REMOVED AND REPLACED NR1 PFD IAW 31-61-4. OPS CHECK GOOD. RETURNED TO CAT II. REMOVED AND REPLACED NR 1 DCU FOR NUMEROUS DCU FAILS IN MDC IAW 31-41-04. PFD P/N: 622-9810-016, S/N OFF: 10DRR.

Part: SWITCH — FAILED (STAB TRIM) · airframe 5,589 hrs · 4,305 cycles

STAB TRIM AND MACH TRIM FAILED DURING FLT. REPLACED CAPTAIN'S TRIM DISCONNECT SWITCH. OPS CHECKS GOOD.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 4,602 hrs · 3,556 cycles

FS 621 LT FLOOR SUPPORT ANGLE LBL 42 CRACKED. DISCOVERED DURING C-CHECK. DAMAGE REPAIRED IAW CRJ REO 601R-53-61-117 REV A. P/N: 601R-53-6117-3.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 4,602 hrs · 3,556 cycles

FS 625 RT INTERCOSTAL ANGLE STR 14L CRACKED. DISCOVERED DURING C-CHECK. REPLACED ANGLE IAW CRJ SRM 51-40-11 AND 51-42-06. P/N: 601-35012-52.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 4,602 hrs · 3,556 cycles

FS 621 RT FLOOR SUPPORT ANGLE RBL 42 CRACKED. DISCOVERED DURING C-CHECK. REPAIRED DAMAGED AREA IAW CRJ REO 601R-53-61-117 REV A. P/N: 601R-53-61-117-4.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 4,602 hrs · 3,556 cycles

FS 280 FLOORBEAM O/B ATTACH ANGLE RBL 9.0 CRACKED. DISCOVERED DURING C-CHECK. REPLACED ANGLE IAW CRJ SRM 51-40-11. P/N: 601R31113-58.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 4,602 hrs · 3,556 cycles

FS 625 LT INTERCOSTAL ANGLE STR 14L CRACKED. DISCOVERED DURING C-CHECK. REPLACED ANGLE IAW CRJ SRM 51-40-11 AND 51-42-06. P/N: 601-35012-51.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 4,602 hrs · 3,556 cycles

FS 484 LT INTERCOSTAL O/B FLANGE CRACKED. DISCOVERED DURING C-CHECK. REPAIRED FLANGE IAW CRJ REO 601R-53-41-059 REV A.

Part: CONTROL UNIT — FAILED (HORIZONTAL STAB) · airframe 3,750 hrs · 2,884 cycles

LOST STAB AND MACH TRIM EN ROUTE. REENGAGED AS PER QRH. AFTER 10 MINUTES, THE PROBLEM OCCURRED AGAIN. REENGAGED AND SLOWED TO 250 KIAS. MAINTENANCE DIAGNOSTIC COMPUTER INDICATED HSTCU FAILED. REMOVED AND REPLACED HSTCU IAW 27-41-01.

Part: LIGHT — INOPERATIVE (LEFT OVERWING) · airframe 3,750 hrs · 2,884 cycles

LEFT CENTER OVERWING EMERGENCY LIGHT INOP. REMOVED AND REPLACED LAMP ON LEFT CENTER OVERWING EMERGENCY LIGHT. OPS CHECK GOOD.

Part: COMPUTER — MALFUNCTIONED (STALL WARNING) · airframe 3,599 hrs · 2,762 cycles

ON ROTATION STALL FAIL MESSAGE DISPLAYED. WOULD NOT CLEAR. INSPECTED STALL PROTECTION SYSTEM AND PERFORMED TESTS. COULD NOT DUPLICATE. SYSTEM OPS CHECKS GOOD.

Part: CONTROL UNIT — MALFUNCTIONED (STAB TRIM) · airframe 3,310 hrs · 2,545 cycles

'STAB CHANNEL 1 INOP' STATUS MESSAGE, WILL NOT ENGAGE ON GROUND. REMOVED AND REPLACED HSTCU WITH SERVICEABLE UNIT IAW 27-41-01. OPS CHECK GOOD AND SELF-TEST GOOD AT THIS TIME.

Part: PCU — MALFUNCTIONED (LEFT SPOILER) · airframe 3,310 hrs · 2,545 cycles

WITH ALL EMHP'S ON, L SPOILERON MESSAGE APPEARS. LEFT SPOILERON IS AMBER ON THE FLIGHT CONTROLS PAGE. INSTALLED SERVICEABLE PCU ON LEFT INBOARD POSITION ON LEFT SPOILERON IAW 27-60-00. OPS CHECKS AND LEAK CHECKS GOOD.

Part: TRIM SWITCH — MALFUNCTIONED (COCKPIT) · airframe 2,279 hrs · 1,766 cycles

WHILE EN ROUTE TO LAS HAD A STAB TRIM RUNAWAY. PERFORMED MEMORY ITEMS FOLLOWED BY QRH. RETURNED TO SLC. REMOVED AND REPLACED CAPTAIN'S TRIM SWITCH. OPS CHECK GOOD.

Part: DAMPER — FAULTY (AUTOPILOT SYS) · airframe 2,279 hrs · 1,766 cycles

NR 1 YAW DAMPER WOULD ENGAGE UNTIL RUDDER MOVEMENT WAS INITIATED THEN NR 1 WOULD AGAIN DISCONNECT. REPLACED NR 1 YAW DAMPER LINEAR ACTUATOR IAW MM 22-22-01. OPS CHECK GOOD.

Part: ANTI-ICE VALVE — FAILED (RT COWLING) · airframe 2,123 hrs · 1,644 cycles

RIGHT COWL ANTI-ICE FAILED EN ROUTE. DIVERTED TO GJT DUE TO WEATHER. REMOVED AND REPLACED RIGHT ENGINE COWL ANTI-ICE VALVE WITH SERVICEABLE UNIT IAW MM 30-22-01. OPS CHECKS GOOD.

Part: CONTROL UNIT — MALFUNCTIONED (SPOILER) · airframe 1,755 hrs · 1,354 cycles

OUTBOARD GROUND SPOILER FAULT STATUS MESSAGE AND, AFTER ENGINE START, SPOILERONS AND FAULT SPOILER CAUTION MESSAGE. RESET SECU'S IAW FIM 27-61-00.

Part: COMPUTER — MALFUNCTIONED (COCKPIT) · airframe 1,411 hrs · 1,080 cycles

STALL FAIL MESSAGE INFLIGHT. RETURNED TO SLC. RESET MEMORY ON CH1 & CH2 IN STALL COMPUTER IAW MM 27-35-01. PERFORMED TEST OF STALL SYSTEM. OPS CHECK GOOD, NO FAULTS NOTED.

Part: PCU — MALFUNCTIONED (SPOILER) · airframe 1,196 hrs · 908 cycles

SPOILERON FAULT FOR RIGHT WING. REMOVED AND REPLACED RIGHT OUTBOARD SPOILERON PCU IAW MM 27-62-01. OPS CHECK AND LEAK CHECK GOOD. REMOVED AND REPLACED SECU NR 1 WITH SERVICEABLE UNIT IAW 27-61-05. OPS CHECK GOOD. SECU P/N: 49-164-05, S/N OFF: 01374.

Part: CIRCUIT BOARD — FAULTY (AUTOPILOT SYS) · airframe 677 hrs · 513 cycles

AFTER EXCEEDING 250 KTS IAS, RUDDER FLUTTERED UNTIL AIRCRAFT WAS IN LANDING CONFIGURATION. REMOVED AND REPLACED LEFT (UPPER) LHP-4000 CARD IAW A/C MM 22-12-01. OPS CHECKED GOOD ON GROUND.

Part: STALL WARNING — FALSE ACTIVATION (COCKPIT) · airframe 677 hrs · 513 cycles

ON ROTATION RECEIVED STALL FAIL CAUTION MESSAGE. PERFORMED APPROPRIATE QRH PROCEDURE. RETURNED TO SLC. RESET STALL COMPUTER CIRCUIT BREAKERS CBP-1 Q2 CBP-4 C7 AND CLEARED THE MEMORY. OPS CHECK GOOD.

Part: ACTUATOR — FAULTY (AUTOPILOT SYS) · airframe 114 hrs · 81 cycles

AIRCRAFT OSCILLATED ABOUT YAW AXIS INFLIGHT INTERMITTENTLY. AIRCRAFT OSCILLATING INFLIGHT AROUND YAW AXIS. REMOVED AND REPLACED NR 2 YAW DAMPER IAW 22-22-01. OPS CHECK GOOD. P/N: 622-9508-001 S/N OFF: 2761 REPLACED NR 1 YAW DAMPER ACTUATOR IAW 22-22-00. PERFORMED FUNCTIONAL CHECK OF YAW DAMPER IAW MM 22-22-01. OPS CHECK GOOD.

Part: COMPUTER — FAULTY (AUTOPILOT SYS) · airframe 89 hrs · 62 cycles

CLIMBING OUT OF ELP THE AIRCRAFT CONTINUALLY YAWED LEFT AND RIGHT, NO MESSAGES. PERFORMED TEST OF YAW DAMPENERS IAW 22-22-01 AND NOTED FAILURE. REMOVED AND REPLACED NR 2 FCC CARD IAW 22-12-14. OPS CHECK GOOD.

Part: TRIM TAB — MALFUNCTIONED (RUDDER) · airframe 100 hrs · 69 cycles

CLIMBING OUT OF SLC, THE A/C CONTINUALLY YAWED L/R, NO MESSAGES. THE ONLY WAY TO STOP THE YAW WAS TO ADD RT RUDDER. INSPECTED RUDDER TRIM SYSTEM IAW CRJ MM 27-22-00. NO DEFECTS NOTED. SYSTEM OPS CHECK GOOD.