N809CA

Part: NUT PLATE — BROKEN (LT WING) · airframe 41,109 hrs · 38,383 cycles

PANEL 571LL ON L/H WING HAS ONE BROKEN NUTPLATE. (C CHECK) RO 3/27/2020 REMOVED BROKEN NUTPLATE AND INSTALLED NEW P/N NAS1789-3 NUTPLATE IAW CRJ 200 SRM.

Part: FITTING — BROKEN (E&E DOOR) · airframe 41,109 hrs · 38,383 cycles

AVIONICS BAY DOOR FWD R/H NYLON GUIDE FITTING BROKEN. (C CHECK) RO 3/27/2020 REMOVED BROKEN AVIONICS BAY DOOR FWD R/H NYLON GUIDE FITTING. LOCATED AND DRILLED NEWAVIONICS BAY DOOR FWD R/H NYLON GUIDE FITTING REF. CRJ-200 [TR51-42] SRM. INSTALLATION PERFORMED ON JOB 2736661, OP: 381, STEP 3 OF CORRECTIVE ACTION.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 41,109 hrs · 38,383 cycles

*ANGLE ATTACHED TO TOP AFT EDGE OF FRAME AT FS 682 IS CRACKED BETWEEN STGR25R AND STGR26R. (C CHECK) RO 3/27/2020 REPAIRED ANGLE ATTACHED TO TOP AFT EDGE OF FRAME AT FS 682 BETWEEN STGR25R AND STGR26R PER BOMBARDIER REO COMPLIED WITH ALL STEP OF REO.

Part: FITTING — CRACKED (WINDSHIELD) · airframe 41,109 hrs · 38,383 cycles

*R/H WINDSHIELD SIDE POST AFT LWR CLIP (FITTING) IS CRACKED. (C CHECK) RO 3/27/2020 REMOVED AND REPLACED R/H WINDSHIELD SIDE POST FITTING REFERENCE CRJ 200 SRM AND DRAWING. COMPLIED WITH. SEE CONTINUATION FOR DETAILS.

Part: FITTING — CRACKED (WINDSHIELD) · airframe 41,109 hrs · 38,383 cycles

*L/H WINDSHIELD SIDE POST AFT LWR CLIP (FITTING) IS CRACKED. (C CHECK) RO 3/27/2020 REMOVED AND REPLACED CRACKED L/H WINDSHEILD SIDE POST AFT LOWER FITTING WITH NEW FITTING. REF DRAWING AND CRJ 200 SRM. SEE CONTINUATION FOR DETAILS.

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,109 hrs · 38,383 cycles

FS 605.0 FRAME FLANGE LEFT HAND SIDE, JUST OVER AFT CARGO DOOR HAS SUSPECT CRACK AT RIVET LOCATION JUST ABOVE AND BELOW STR 9. (MARKED) (C CHECK) RO 3/27/2020 REPAIRED DAMAGE AREA AND COMPLIED WITH ALL STEPS OF BOMBARDIER REO. PRESSURE CHECK GOOD. SEE CONTINUATION FOR FURTHER DETAILS.

Part: RIB — DAMAGED (TE FLAP VANE) · airframe 41,109 hrs · 38,383 cycles

RH INBOARD FLAP VANE LEADING EDGE INBOARD RIB REQUIRES REPLACEMENT (C CHECK) RO 3/27/2020 REMOVED AND REPLACED AND RESTORED FINISH ON RH INBOARD FLAP VANE LEADING EDGE INBOARD RIB. REF: CRJ200 SRM. FOUND TO BE OUT OF LIMITS ON CAMP 20427303 JOB 2736661 OP 186

Part: FLOOR SKIN — CRACKED (FUSELAGE) · airframe 41,109 hrs · 38,383 cycles

*PRESSURE FLOOR SKIN IS CRACKED AT 2EA LOCATIONS AT APPROX FS 461 BETWEEN BL0 AND LBL 9 AND BL0 TO RBL9. SUSPECT AREAS ARE MARKED WITH RED GREASE PENCIL. (C CHECK) RO 3/27/2020 REPAIRED PRESSURE FLOOR SKIN @ 2EA LOCATIONS AT APPROX FS.461.00 BETWEEN BL0 AND LBL 9 AND BL0 TO RBL9 REF REO. COMPLIED WITH ALL APPLICABLE STEPS OF REO. COMPLIED WITH TASK CARD. PRESSURE CHECK GOOD. SEE CONTINUATION FOR FURTHER DETAILS,

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 41,109 hrs · 38,383 cycles

CORROSION FOUND ON AVIONICS BAY DOOR POSITION SENSOR MOUNTING CHANNEL AT FS.364.00, STGR 27. (MARKED) (C CHECK) RO 3/27/2020 REMOVED CORROSION FROM AVIONICS BAY DOOR POSITION SENSOR CHANNELS AT FS364.00 REF CRJ200 SRM. FOUND TO BE OUT OF LIMITS. RECEIVED NEW REO. COMPLIED WITH ALL STEPS OF REO. SEE CONTINUE CARD FOR DETAILS.

Part: FRAME SPLICE — CORRODED (FUSELAGE) · airframe 41,109 hrs · 38,383 cycles

CORROSION FOUND ON UPPER SPLICE ANGLE FOR LOWER FRAME SECTOR AT FS.364.00 AND STGR 27. (MARKED) (C CHECK) RO 3/27/2020 REMOVED CORROSION ON UPPER SPLICE ANGLE FOR LOWER FRAME SECTOR AT FS364.00 STGR 27 REF CRJ200 SRM. FOUND TO BE OUT OF LIMITS. RECEIVED NEW REO. COMPLIED WITH ALL STEPS OF REO. SEE CONTINUE CARD FOR DETAILS.

Part: FITTING — CRACKED (FUSELAGE) · airframe 41,109 hrs · 38,383 cycles

*AFT LINTEL CLIP IS POSSIBLY CRACKED. FLAGGED (C CHECK) RO 3/27/2020 REMOVED AND REPLACED AFT LINTEL CLIP REF. CRJ-200 SRM AND BOMBARDIER DWG. PRESSURE CHECK GOOD. SEE CONTINUATION CARD FOR DETAILS.

Part: DOOR SILL — CRACKED (FUSELAGE) · airframe 41,109 hrs · 38,383 cycles

*FRAME FROM PAX DOOR UPPER SILL TO STGR 0 AT FS 333 IS CRACKED. (C CHECK) RO 3/27/2020 REMOVED AND INSTALLED A NEW FRAME @ FS.333.00 FROM PAX DOOR UPPER SILL TO STRG 0 REF CRJ 200 SRM AND BOMBARDIER DWG. PRESSURE CHECK GOOD. COMPLIED WITH TASK CARD. SEE CONTINUATION FOR FURTHER DETAILS.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 41,109 hrs · 38,383 cycles

*CORROSION FOUND ON INTERCOSTAL AFT OF AVIONICS BAY DOOR ON R/H SIDE OF STGR27. (C CHECK) RO 3/27/2020 REMOVED AND REINSTALLED A NEW INTERCOSTAL AT STRG 27 RH FROM FS.394.00 TO FS.409.00 REF CRJ 200 SRM AND BOMBARDIER DWG. PRESSURE CHECK GOOD. COMPLIED WITH TASK CARD. SEE CONTINUATION FOR FURTHER DETAILS.

Part: NOT REPORTED — CORRODED (FUSELAGE) · airframe 41,109 hrs · 38,383 cycles

*FS559.00+80 €“ 559.00+112 STGR 26L €“ 26R CORROSION AROUND SEVERAL FASTENERS (MARKED) (C CHECK) RO 3/27/2020 REPAIRED CORROSION DAMAGE AT FS559+80 TO FS574 STGR25L TO STGR26R COMPLIED WITH ALL APPLICABLE STEPS OF BOMBARDIER REO. LEAK CHECK GOOD. SEE CONTINUATION FOR FURTHER DETAILS.

Part: PANEL — CORRODED (FUSELAGE) · airframe 41,109 hrs · 38,383 cycles

THE RH FLOOR SILL PANEL HAS MULTIPLE LOCATIONS OF CORROSION FROM FS409.00+128 TO FS559.00. (MARKED) (C CHECK) RO 3/27/2020 BLENDED MULTIPLE AREAS OF CORROSION FROM R/H FLOOR SILL PANEL FROM FS. 409.00+128 TO FS. 559.00 IAW REO CRJ-200 SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 41,109 hrs · 38,383 cycles

FRAME AT L/H FS 513 WL73 (FLOOR LEVEL) HAS SMALL AREA OF CORROSION. (C CHECK) RO 3/27/2020 REMOVED CORROSION ON FRAME @ FS.513 WL.73. FOUND TO BE OUT OF LIMITS. COMPLIED WITH ALL APPLICABLE STEPS OF REO. SEE CONTINUATION FOR FURTHER DETAILS.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 41,109 hrs · 38,383 cycles

FWD CABIN - APPROX.€¦ FS280.00 STGR 3 €“ STRINGER CLIP HAS SIGNS OF A CRACK AND WORKING RIVETS (MARKED) (C CHECK) RO 3/27/2020 REMOVED AND INSTALLED A NEW FWD CABIN STRINGER CLIP ON RH STRG 3 @ FS.280.00 REF CRJ 200 SRM AND BOMBARDIER DWG.LEAK CHECK GOOD. COMPLIED WITH TASK CARD. SEE CONTINUATION FOR FURTHER DETAILS.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 41,109 hrs · 38,383 cycles

*CORROSION FOUND ON INTERCOSTAL AFT OF AVIONICS BAY DOOR ON L/H SIDE OF STGR27. (C CHECK) RO 3/27/2020 REMOVED AND INSTALLED A NEW INTERCOSTAL AFT OF AVIONICS BAY DOOR ON THE LH SIDE OF STRG 27 REF BOMBARDIER DWG AND CRJ 200 SRM. COMPLIED WITH TASK CARD. PRESSURE CHECK GOOD. SEE CONTINUATION FOR FURTHER DETAILS.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 41,109 hrs · 38,383 cycles

*FS621.00 - 625.30 STGR APPROX. 14R ANGLE CRACKED (MARKED) (C CHECK) RO 3/27/2020 REMOVED CRACKED ANGLE BRACKET FROM FS. 625.30 STRINGER 14R AND INSTALLED NEW ANGLE BRACKET IAW CRJ 200 SRM. COMPLIED WITH TASK CARD.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 41,109 hrs · 38,383 cycles

THE FLOORBEAM AT LBL9.00 FROM FS409.00 TO FS409.00+128 HAS MULTIPLE LOCATIONS OF CORROSION. (MARKED) (C CHECK) RO 3/27/2020 REMOVED CORROSION FROM FLOOR BEAM AT LBL 9.00 FROM FS. 409.00 TO FS. 409.00+128 IAW REO ( SEE CONTINUATION CARD FOR DETAILS ).

Part: HINGE — CORRODED (RUDDER) · airframe 41,109 hrs · 38,383 cycles

*RUDDER CENTER HINGE AREA, UPPER AND LOWER GROUND STUD AND HARDWARE ON RUDDER, CORRODED (MARKED, OUT OF SCOPE) (C CHECK) RO 3/27/2020 REMOVED AND INSTALLED NEW RUDDER CENTER HINGE, UPPER AND LOWER GROUND STUD AND HARDWARE REF CRJ 200 AMM.

Part: STAND OFF — CORRODED (FUSELAGE) · airframe 41,109 hrs · 38,383 cycles

* THE LH FLOOR SILL HAS 3EA ELECTRICAL STANDOFFS THAT ARE CORRODED BETWEEN FS409.00+64 TO FS409.00+80. (MARKED) (C CHECK) RO 3/27/2020 REMOVED AND REPLACED 3 EACH STAND OFFS PER REFERENCE CRJ 200 SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 41,109 hrs · 38,383 cycles

AFT CARGO APPROX.€¦ FS.559.00+118 TO FS. 621.00 LEFT HAND LBL 27.00 FLOOR BEAM HAS NUMEROUS SPOTS OF CORROSION (MARKED) (C CHECK) RO 3/27/2020 COMPLIED WITH REO FOR THE REMOVAL OF CORROSION FROM FLOOR BEAM FS. 559.00+118 TO FS. 621.00 LBL 27.

Part: NOT REPORTED — CORRODED (FUSELAGE) · airframe 41,109 hrs · 38,383 cycles

*FS559.00 STGR 26L €“ 26R HAS CORROSION ON FASTENERS AND AROUND THE FASTENERS(MARKED) (C CHECK) RO 3/27/2020 REPAIRED FS559.00 STR26L -26R REFERENCING REO. ALL STEPS COMPLIED WITH.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 41,109 hrs · 38,383 cycles

THE SEAT TRACK AT RBL9.00 FROM FS409.00+128 TO FS559.00 HAS MULTIPLE LOCATIONS OF CORROSION. (MARKED) (C CHECK) RO 3/27/2020 BLENDED SEAT TRACK AT RBL9 FS409+128 TO FS559.00 REF CRJ200 SRM. FOUND TO BE OUT OF LIMITS. FABRICATED NEW SEAT TRACK. REF: BOMBARDIER REO. REMOVED AND INSTALLED NEW FABRICATED SEAT TRACK AT RBL 9.00 FROM FS 409+128 TO FS 559+4. REF: CRJ-200 AMM. SEE CONTINUATION CARD FOR DETAILS.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 41,109 hrs · 38,383 cycles

*FS621.00 - 625.30 STGR APPROX. 14L ANGLE CRACKED (MARKED) (C CHECK) RO 3/27/2020 REMOVED CRACKED ANGLE BRACKET FROM FS. 625.3.0 STRINGER 14L AND INSTALLED NEW ANGLE BRACKET IAW CRJ 200 SRM. COMPLIED WITH TASK CARD.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 41,109 hrs · 38,383 cycles

THE SEAT TRACK AT LBL9.00 FROM FS409.00+128 TO FS559.00 HAS MULTIPLE LOCATIONS OF CORROSION. (MARKED) (C CHECK) RO 3/27/2020 REMOVED CORRODED SET TRACK LBL BETWEEN FS. 409.00+128 AND FS. 559.00 AND INSTALLED NEWLY FABRICATED SEAT TRACK IAW CRJ 200 AMM AND REO.

Part: STRAP — CORRODED (FUSELAGE) · airframe 41,109 hrs · 38,383 cycles

AFT CABIN APPROX. FS 559.00 RIGHT HAND RBL 42.90 TO RBL27.00- INTERCOSTAL STRAP HAS SIGNS OF CORROSION (MARKED) (C CHECK) RO 3/27/2020 REPLACED AFT CABIN APPROX FS559.00 RIGHT HAND RBL 42.90 INTERCOSTAL STRAP WITH NEW REF BOMBARDIER DWG, CRJ 200 SRM. SEE CONTINUATION CARD FOR DETAILS.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 41,109 hrs · 38,383 cycles

AFT CABIN APPROX. FS 559.00 TO 559.00 +96 RIGHT HAND FLOOR SILL BL 42.90 HAS NUMEROUS SPOTS OF CORROSION (MARKED) (C CHECK) RO 3/27/2020 REPLACED AFT CABIN APPROX FS559.00 TO FS559.00+16 RIGHT HAND FLOOR SILL INTERCOSTAL BL42.90 REF BOMBARDIER DWG, CRJ 200 SRM, SEE CONTINUATION CARD FOR DETAILS. FOUND THE RIGHT FLOOR SILL FROM 559+16 TO 559+96 AT BL 42.90 TO BE IN LIMITS.

Part: FRAME — CORRODED (FUSELAGE) · airframe 41,109 hrs · 38,383 cycles

AFT CARGO APPROX.€¦ FS.574.00 LEFT HAND STGR 25 TO STGR 18 - FRAME HAS NUMEROUS SPOTS OF CORROSION (MARKED) (C CHECK) RO 3/27/2020 REPLACED AFT CARGO APPROX FS574.00 LEFT HAND STGR25 TO STGR18 FRAME REF CRJ 200 SRM AND BOMBARDIER DWG LEAK TEST GOOD. SEE CONTINUATION CARD FOR DETAILS.

Part: NUT — CORRODED (LT SPOILER) · airframe 41,109 hrs · 38,383 cycles

*LH OUTBD GROUND SPOILER HINGES ATTACH HARDWARE NUTS CORRODED (MARKED) (C CHECK) RO 3/27/2020 REMOVED AND INSTALLED NEW HARDWARE (NUTS) ON LH OUTBOARD GROUND SPOILER HINGES REF CRJ200 AMM. OPS TEST GOOD. SEE CONTINUE CARD FOR DETAILS.

Part: FASTENER — CORRODED (LT SPOILER) · airframe 41,109 hrs · 38,383 cycles

*LH FLIGHT SPOILER BOTH PCU, BOTTOM ATTACH HARDWARE CORRODED (MARKED) (C CHECK) RO 3/27/2020 REMOVED AND INSTALLED NEW HARDWARE AT BOTTOM ATTACHING POINTS OF THE LH FLIGHT SPOILER PCU'S REF CRJ200 AMM. OPS TEST GOOD. SEE CONTINUE CARD FOR DETAILS.

Part: NUT — CORRODED (RT SPOILER) · airframe 41,109 hrs · 38,383 cycles

*RH OUTBD GROUND SPOILER INBD/OUTBD HINGE ATTACH HARDWARE NUTS CORRODED (MARKED) (C CHECK) RO 3/27/2020 REMOVED AND REPLACED THE ATTACHING HARDWARE ON THE RIGHT OUTBOARD GROUND SPOILER HINGES, REF CRJ 200 AMM. OPERATIONAL TEST OF GROUND SPOILERS CHECKED GOOD. SEE CONTINUE CARD FOR DETAILS.

Part: SEAT TRACK — CHAFED (FUSELAGE) · airframe 41,109 hrs · 38,383 cycles

*NUMEROUS AREAS OF CHAFEING, FRETTING, AND CORROSION ON SEAT RAIL FROM FS409 TO FS409+128 AT RBL9 (C CHECK) RO 3/27/2020 REPLACED SEAT RAIL FROM FS409 TO FS409+128 AT RBL9 WITH A NEW FABRICATED PART REF REO, SEE CONTINUATION CARD FOR DETAILS.

Part: FASTENER — CORRODED (RT SPOILER) · airframe 41,109 hrs · 38,383 cycles

*RH FLIGHT SPOILER BOTH PCU, BOTTOM ATTACH HARDWARE CORRODED (MARKED) (C CHECK) RO 3/27/2020 REMOVED AND INSTALLED NEW HARDWARE ON BOTTOM ATTACHING OINTS ON RH FLIGHT SPOILER PCU REF CRJ200 AMM. OPS TEST GOOD. SEE CONTINUE CARD FOR DETAILS.

Part: NUT — CORRODED (RT SPOILER) · airframe 41,109 hrs · 38,383 cycles

*RH INBD GROUND SPOILER OUTBD HINGE ATTACH HARDWARE NUT CORRODED (MARKED) (C CHECK) RO 3/27/2020 REMOVED AND REPLACED HARDWARE OF THE RH INBOARD GROUND SPOILER OUTBOARD HINGE WITH NEW, REF CRJ 200 AMM. OPERATIONAL TEST OF THE GROUND SPOILERS CHECKED GOOD. SEE CONTINUE CARD FOR DETAILS.

Part: FASTENER — CORRODED (LT SPOILERON) · airframe 41,109 hrs · 38,383 cycles

*LH SPOILERON BOTH PCU, BOTTOM ATTACH HARDWARE CORRODED (MARKED) (C CHECK) RO 3/27/2020 REMOVED AND INSTALLED NEW HARDWARE ON LH INBOARD SPOILER PCU BOTTOM ATTACH POINT REF CRJ200 AMM. OPS TEST GOOD. SEE CONTINUE CARD FOR DETAILS.

Part: SEAT TRACK — CHAFED (FUSELAGE) · airframe 41,109 hrs · 38,383 cycles

*NUMEROUS AREAS OF CHAFEING, FRETTING, AND CORROSION ON SEAT RAIL FROM FS364 TO FS409 AT RBL9. (C CHECK) RO 3/27/2020 BLENDED SEAT TRACK AT RBL 9.00 FROM FS 364.00 TO FS 409.00 . REF: CRJ-200 SRM. FOUND TO BE OUT OF LIMITS. FABRICATED NEW SEAT TRACK. REF: BOMBARDIER REO. REMOVED AND NSTALLED NEW FABRICATED SEAT TRACK AT RBL 9.00 FROM FS 364.00 TO FS 409.00 . REF: CRJ-200 AMM. SEE CONTINUATION CARD FOR DETAILS.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 41,109 hrs · 38,383 cycles

*R/H FLOOR SILL HAS 4EA AREAS OF CORROSION BETWEEN FS310 AND FS319.70. AREAS MARKED WITH RED GREASE PENCIL. (C CHECK) RO 3/27/2020 REMOVED AND REPLACE RH FLOOR SILL BETWEEN FS310 AND FS319.70 REF DWG 601R31148 REV Y. SEE CONTINUATION CARD FOR DETAILS

Part: NUT — CORRODED (LT SPOILER) · airframe 41,109 hrs · 38,383 cycles

*LH FLIGHT SPOILER HINGES ATTACH HARDWARE NUTS CORRODED (MARKED) (C CHECK) RO 3/27/2020 LEFT FLIGHT SPOILER CENTER HINGES HARDWARE REMOVED AND REPLACED WITH NEW, REF CRJ 200 AMM. OPERATIONAL TEST CHECKED GOOD. SEE CONTINUE CARD FOR DETAILS.

Part: NUT — CORRODED (RT SPOILERON) · airframe 41,109 hrs · 38,383 cycles

*RH SPOILERON HINGES ATTACH HARDWARE NUTS CORRODED (MARKED) (C CHECK) RO 3/27/2020 REMOVED AND REPLACED THE HARDWARE WITH NEW ON THE RH SPOILERON HINGE ATTACH POINTS. REF CRJ 200 AMM. OPERATIONAL TEST CHECKED GOOD. SEE CONTINUE CARD FOR DETAILS.

Part: NUT — CORRODED (RT SPOILER) · airframe 41,109 hrs · 38,383 cycles

*RH FLIGHT SPOILER HINGES ATTACH HARDWARE NUTS CORRODED (MARKED) (C CHECK) RO 3/27/2020 REMOVED AND INSTALLED NEW HARDWARE ON RH FLIGHT SPOILER HINGES REF CRJ200 AMM. OPS TEST GOOD. SEE CONTINUE CARD FOR DETAILS.

Part: NUT — CORRODED (LT SPOILERON) · airframe 41,109 hrs · 38,383 cycles

*LH SPOILERON HINGES ATTACH HARDWARE NUTS CORRODED (MARKED) (C CHECK) RO 3/27/2020 REMOVED AND INSTALLED NEW HARDWARE (NUTS) ON LH SPOILERON END HINGES REF CRJ200 AMM. OPS TEST GOOD. SEE CONTINUE CARD FOR DETAILS.

Part: PLATE — CORRODED (FUSELAGE) · airframe 41,109 hrs · 38,383 cycles

THE PLATE UNDER THE TRANSMITTER ANTENNA NO.2 HAS CORROSION. (MARKED) (C CHECK) RO 3/27/2020 REMOVED CORROSION FROM PLATE UNDER TRANSMITTER ANTENNA #2 REF CRJ 200 SRM. FOUND TO BE OUT OF LIMITS. REMOVED AND INSTALLED A NEW PLATE UNDER THE TRANSMITTER ANTENNA #2 REF CRJ 200 SRM. PRESSURE LEAK CHECK AND OPS GOOD. COMPLIED WITH TASK CARD. SEE CONTINUATION FOR FURTHER DETAILS.

Part: NUT — CORRODED (LT SPOILER) · airframe 41,109 hrs · 38,383 cycles

*LH INBD GROUND SPOILER HINGES ATTACH HARDWARE NUTS CORRODED (MARKED) (C CHECK) RO 3/27/2020 REMOVED AND INSTALLED NEW HARDWARE (NUTS) ON LH INBOARD GROUND SPOILER HINGES REF CRJ200 AMM. OPS TEST GOOD. SEE CONTINUE CARD FOR DETAILS.

Part: HINGE FITTING — GOUGED (LT SPOILERON) · airframe 41,109 hrs · 38,383 cycles

*LH SPOILERON THIRD HINGE FITTING GOUGED ON THE OUTBD UPPER AFT EDGE (MARKED) (C CHECK) RO 3/27/2020 REMOVED GOUGE ON THE LH SPOILERON THIRD HINGE FITTING OUTBD UPPER AFT EDGE. FOUND TO BE OUT OF LIMITS. RECEIVED REO. FOUND TO BE IN LIMITS . COMPLIED WITH ALL APPLICABLE STEPS OF REO. SEE CONTINUATION CARD FOR DETAILS.

Part: FASTENER — CORRODED (RT SPOILERON) · airframe 41,109 hrs · 38,383 cycles

*RH SPOILERON BOTH PCU, BOTTOM ATTACH HARDWARE CORRODED (MARKED) (C CHECK) RO 3/27/2020 REMOVED AND INSTALLED NEW HARDWARE AT BOTTOM ATTACH POINT AT RH SPOILERON OUTBOARD PCU REF CRJ200 AMM. OPS TEST GOOD, SEE CONTINUE CARD FOR DETAILS.

Part: VANE — DAMAGED (TE FLAP) · airframe 41,109 hrs · 38,383 cycles

RIGHT I/B FLAP MIDDLE VANE NEEDS TO BE REPLACED. (C CHECK) RO 3/27/2020 REMOVED AND REPLACED RH INBOARD FLAP, MIDDLE VANE CAP PER REFERENCE CRJ 200 SRM SEE CONTINUATION CARD FOR DETAILS

Part: TRACK — DAMAGED (CARGO DOOR) · airframe 41,109 hrs · 38,383 cycles

CARGO DOOR AFT TRACK DAMAGE IS OUT OF LIMITS DUE TO DENT IN TRACK IAW CRJ 200 SRM THIS CARD GENERATED FROM JOB 2736661 OP. 231 MX TRANS 20453161 (C CHECK) RO 3/27/2020 REPLACED CARGO DOOR AFT TRACK WITH NEW REF CRJ 200 SRM. SEE CONTINUE CARD FOR DETAILS, REF REO USED TO MACHINE DOWN TRACK ONLY.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 41,109 hrs · 38,383 cycles

*PAX DOOR AFT CUP ON SILL ANGLE HAS CORROSION AROUND SEVERAL OF THE FASTENER HOLES (MARKED) (C CHECK) RO 3/27/2020 BLENDED CORROSION ON PAX DOOR AFT CUP ON SILL ANGLE AROUND FASTENER HOLES FOUND TO HAVE SEVERE EXFOLIATION 100% MATERIAL LOSS. REF: CRJ200 SRM. REMOVED AND REPLACED ON PAX DOOR SILL ANGLE THE AFT CUP AND RESTORED FINISH. REF: CRJ200 SRM.

Part: TRIM PANEL — CRACKED (ESCAPE HATCH) · airframe 41,109 hrs · 38,383 cycles

CREW ESCAPE HATCH TRIM ASSY CRACKED IN SEVERAL AREAS (C CHECK) RO 3/27/2020 REPAIRED THE CREW ESCAPE HATCH TRIM ASSEMBLY USING PO# 24268 PER BOMBARDIER REO.

Part: RIB — CRACKED (RT WING) · airframe 41,109 hrs · 38,383 cycles

*R/H BATT BIB LOCATED AT WS 48.30 HAS A POSSIBLE CRACK AT THE AFT END. AREA MARKED WITH RED GREASE PENCIL. (C CHECK) RO 3/27/2020 REMOVED CRACKED CAP ANGLE AT RH BATT RIB LOCATED WS 48.30 AND INSTALLED NEW CAP ANGLE REF CRJ200 SRM. SEE CONTINUE CARD FOR DETAILS. COMPLIED TASK CARD.

Part: HANDLE — CHAFED (SERVICE DOOR) · airframe 41,109 hrs · 38,383 cycles

*SERVICE DOOR INNER HANDLE HAS NUMEROUS CHAFFED AREAS (MARKED) (C CHECK) RO 3/27/2020 REPAIRED SERVICE DOOR INNER HANDLE PER BOMBARDIER REO REPAIR STEPS 1-3 COMPLIED WITH.

Part: VANE — DAMAGED (TE FLAP) · airframe 41,109 hrs · 38,383 cycles

RIGHT I/B FLAP O/B VANE CAP NEEDS TO BE CHANGED. (C CHECK) RO 3/27/2020 REMOVED AND REPLACED RH INBOARD FLAP OUTBOARD VANE CAP PER REFERENCE CRJ 200 SRM SEE CONTINUATION CARD FOR DETAILS

Part: STRINGER — CRACKED (FUSELAGE) · airframe 41,109 hrs · 38,383 cycles

STRINGER 3 POSSIBLE CRACK AT FWD END, JUST AFT OF FS379.00 (MARKED) (C CHECK) RO 3/27/2020 REMOVED AND INSTALLED A NEW STRINGER 3 L REPAIR @ FS.379.00 REF REO. PRESSURE LEAK CHECK GOOD. COMPLIED WITH TASK CARD. COMPLIED WITH ALL APPLICABLE STEPS OF REO. SEE CONTINUATION FOR FURTHER DETAILS.

Part: TRACK — GOUGED (CARGO DOOR) · airframe 41,109 hrs · 38,383 cycles

*CARGO DOOR FWD AND AFT TRACK ARE GOUGED AT THE OUTBD CENTER TRACK, TOWARD THE END (MARKED) (C CHECK) RO 3/27/2020 REPLACED CARGO DOOR FWD TRACK REF CRJ 200 SRM. GENERATED NEW CAMP FOR CARGO DOOR AFT TRACK, SEE CAMP # 20454774 JOB 2736661 OP 233 FOR TRACK REPLACEMENT. SEE CONTINUATION CARD FOR DETAILS.

Part: ROD END — CORRODED (AILERON PCU) · airframe 41,109 hrs · 38,383 cycles

R/H OBD AILERON PCU OUTPUT ROD END CORRODED. (C CHECK) RO 3/27/2020 REMOVED AND REPLACED RH OB AILERON PCU REF. CRJ200 AMM. RIGGING AND OPS CHECK GOOD AT THIS TIME. COMPLIED WITH TASK CARD.

Part: VANE — CHAFED (TE FLAP) · airframe 41,109 hrs · 38,383 cycles

LEFT HAND INBOARD FLAP VANE €“ LEADING EDGE MIDDLE €“ CHAFED (MARKED) (C CHECK) RO 3/27/2020 REPLACED LEFT HAND INBOARD FLAP VANE - LEADING EDGE MIDDLE CAP REF CRJ 200 SRM AND BOMBARDIER DWG. SEE CONTINUATION CARD FOR DETAILS.

Part: COWLING — DENTED (RT ENGINE) · airframe 41,109 hrs · 38,383 cycles

*RH ENGINE UPPER CORE COWL 445AT DENTED AT FWD INBD SIDE (MARKED) (C CHECK) RO 3/27/2020 REPAIRED DENT ON R/H ENGINE UPPER CORE COWL 445AT PER BOMBARDIER REO.

Part: VANE — CHAFED (TE FLAP) · airframe 41,109 hrs · 38,383 cycles

LEFT HAND INBOARD FLAP VANE €“ LEADING EDGE INBOARD €“ CHAFED (MARKED) (C CHECK) RO 3/27/2020 BLENDED, REMOVED, REPLACED AND RESTORED FINISH OF THE LEFT HAND INBOARD FLAP VANE LEADING EDGE CAP REF CRJ200 SRM.

Part: VANE — DAMAGED (TE FLAP) · airframe 41,109 hrs · 38,383 cycles

RH INBOARD FLAP VANE LEADING EDGE INBOARD, MID, OUTBOARD SIDE AND INBOARD END HAS ABRASION DAMAGE AS MARKED. (C CHECK) RO 3/27/2020 BLENDED OUT CHAFFING TO A SMOOTH CONTOUR ON THE RH FLAP VANE IB END 2 AREAS REF CRJ 200 SRM AND THE IB LEADING EDGE CAP REF REO. THE MID CAP AND OB END CAP REQUIRES REPLACEMENT DUE TO TEMP REPAIRS.FOUND THE I/B VANE CAP WITH IN LIMITS REF REO. RESTORED FINISH TO THE I/B CAP. RH O/B VANE CAP REPLACED ON CAMP 20451590 JOB 1 OP 216 AND R/H MIDDLE VANE CAP REPLACED ON CAMP 20452741 JOB 1 OP 222 ALSO THE RH I/B VANE RIB REPLACED ON CAMP 20508275 JOB 1 OP 397. SEE CONTINUATION CARD FOR DETAILS

Part: ACCESS PANEL — CHAFED (RT COWLING) · airframe 41,109 hrs · 38,383 cycles

*RH ENGINE UPPER NOSE COWL 442AT HAS NUMEROUS GOUGES/CHAFFES AT THE TRAILING EDGE (MARKED) (C CHECK) RO 3/27/2020 REMOVED DAMAGED R/H UPPER ENGINE NOSE COWL 442AT ACCESSS PANEL AFT EDGE STRIP, AND INSTALLED 1 EA. NEW STRIP REF. CRJ200 CMM REPAIR SRS091.

Part: STRIP — CHAFED (RT COWLING) · airframe 41,109 hrs · 38,383 cycles

*RH ENGINE LOWER NOSE COWL 442AB HAS NUMEROUS GOUGES/CHAFFES AT THE TRAILING EDGE (MARKED) (C CHECK) RO 3/27/2020 REMOVED DAMAGED R/H ENGINE LOWER NOSE COWL 442AB ACCESS PANEL AFT EDGE STRIP, AND INSTALLED 1 EA. NEW STRIP REF. CRJ200 CMM REPAIR SRS091.

Part: BRACKET — CHAFED (LT AILERON) · airframe 41,109 hrs · 38,383 cycles

LEFT AILERON FRONT LEADING EDGE €“ BRACKET GOUGED/CHAFED. (MARKED) (C CHECK) RO 3/27/2020 BLENDED OUT CHAFFE/GOUGE ON THE LH AILERON LE BRACKET REF CRJ200 SRM. FOUND OUT OF LIMITS. REMOVED AND REPLACED NEW LH AILERON FRONT LEADING EDGE BRACKET REF CRJ200 SRM. SEE CONTINUE CARD FOR DETAILS.

Part: HOUSING — CRACKED (PAX DOOR) · airframe 41,109 hrs · 38,383 cycles

*PASSENGER DOOR €“ INNER HANDLE HOUSING FOR THE CAM FOLLOWER ROLLER ASSEMBLY IS CRACKED. (MARKED) (C CHECK) RO 3/27/2020 REMOVED PASSENGER DOOR INNER HANDLE HOUSING FOR CAM FOLLOWER ROLLER ASSEMBLY REF CRJ 200 AMM AND INSTALLED NEW HOUSING REF CRJ 200 AMM. OPERATIONAL TEST GOOD REF CRJ 200 AMM.

Part: NUT CLIP — BROKEN (FUSELAGE) · airframe 41,109 hrs · 38,383 cycles

BROKEN NUT CLIP UNDER FLOOR BOARD PANEL 261 CLF (MARKED WITH GREEN TAPE). MULTIPLE STRIPPED SCREWS ON FLOOR BOARD 261 DLF (MARKED WITH GREEN TAPE). (C CHECK) RO 3/27/2020 REMOVED AND REPLACED 8EA NEW DOMENUTS ON PANEL 261DLF REF CRJ 200 SRM AND 2EA NEW NUTPLATES ON PANEL 261CLF REF CRJ 200 SRM. PRESSURE LEAK CHECKS GOOD. SEE CONTINUATION FOR FURTHER DETAILS.

Part: LEVER — CHAFED (PAX DOOR) · airframe 41,109 hrs · 38,383 cycles

* PASSENGER DOOR FWD PULL IN LEVER CHAFED (C CHECK) RO 3/27/2020 REMOVED AND EVALUATED ON CHAFED PULL-IN LEVER MEASUREMENTS ARE 0.060", MAX ALLOWABLE .050", OUT OF LIMITS, RECEIVED DRILLED AND INSTALLED BOLTS IN NEW PASSENGER DOOR FOWARD PULL-IN LEVER IN ALIGNMENT POSITION THROUGH DOOR STRUCTURE AND MOVING PULL-IN LEVER IN OPEN CLOSE POSITION, REF CRJ200 AMM, REO. OPERATIONAL CHECKS ARE GOOD AT THIS TIME. REF CRJ200 AMM.

Part: TRIM PANEL — BROKEN (ESCAPE HATCH) · airframe 41,109 hrs · 38,383 cycles

CREW ESCAPE HATCH FWD OUTER TRIM PANEL BROKEN AND CRACKED IN SEVERAL PLACES (C CHECK) RO 3/27/2020 REMOVED AND REPLACED WITH NEW PART THE CREW ESCAPE HATCH FWD OUTER TRIM ASSY. REF CRJ200 SRM.

Part: NUT PLATE — BROKEN (STABILIZER) · airframe 41,109 hrs · 38,383 cycles

STABILIZER INTAKE PANEL 323AT BROKEN NUT PLATE. (C CHECK) RO 3/27/2020 REMOVED AND REPLACED BROKEN NUTPLATE ON PANEL 323AT REF: CRJ200 SRM.

Part: STRIP — CHAFED (LT COWLING) · airframe 41,109 hrs · 38,383 cycles

THE LH ENGINE LOWER NOSE ACCESS COWL HAS MULTIPLE LOCATIONS OF CHAFFES ON INNER AFT SIDE. (C CHECK) RO 3/27/2020 REMOVER DAMAGED L/H LOWER ENGINE NOSE ACCESS COWL 432AB AFT EDGE STRIP, AND INSTALLED 1 EA. NEW STRIP REF. CRJ200 CMM REPAIR SRS091.

Part: COWLING — NICKED (LT ENGINE) · airframe 41,109 hrs · 38,383 cycles

THE LH ENGINE NOSE INLET LIP SKIN HAS MULTIPLE LOCATIONS OF NICKS (C CHECK) RO 3/27/2020 BLENDED THE LH ENGINE NOSE INLET LIP NICKS. BLENDS FOUND TO BE OUT OF LIMITS. REF CRJ200 CMM. REMOVED AND INSTALLED NEW SERVICEABLE LEFT ENGINE NOSE INLET COWL REF CRJ 200 AMM. ALL CHECKS GOOD. SEE CONTINUATION FOR DETAILS

Part: STRIP — CHAFED (LT COWLING) · airframe 41,109 hrs · 38,383 cycles

THE LH ENGINE UPPER NOSE ACCESS COWL 432AT IS CHAFFED IN MULTIPLE LOCATIONS ON INNER AFT SIDE. (C CHECK) RO 3/27/2020 REPLACED DAMAGED L/H UPPER NOSE ACCESS COWL 432AT AFT EDGE STRIP,AND INSTALLED 1 EA. NEW STRIP REF. CRJ200 CMM REPAIR SRS091.

Part: NUT PLATE — BROKEN (FUSELAGE) · airframe 41,109 hrs · 38,383 cycles

BROKEN NUTPLATES (2EA) UNDER CARGO FLOOR PANEL 281CLF (MARKED). (C CHECK) RO 3/27/2020 REMOVED AND REPLACED 2EA. NUTPLATES COMMON TO PANEL 281CLF. REF CRJ 200 SRM.

Part: SKIN PANEL — ERODED (LT WING) · airframe 41,109 hrs · 38,383 cycles

* L/H WING OBD LEADING EDGE PANEL ERODED/PITTED AT LEADING EDGE. (C CHECK) RO 3/27/2020 BLENDED OUT EROSION/PITTING FROM LH WING OTBD LEADING EDGE SKIN REF CRJ 200 SRM. FOUND TO BE OUT OF LIMITS AND REQUIRED TO BE RESKINNED. SEE JOB 2736665 OP 116 MX TRANS #20545737 FOR RESKINNING OF LEADING EDGE. ALL OPS CHECK GOOD. SEE CONTINUATION FOR FURTHER DETAILS.

Part: SKIN — CHAFED (RT MLG DOOR) · airframe 41,109 hrs · 38,383 cycles

R/H MLG DOOR INNER SKIN CHAFED NEAR CENTER OF DOOR. ( MARKED ) (C CHECK) RO 3/27/2020 BLENDED OUT TO A SMOOTH COUNTER CHAFED RH MLG DOOR INNER SKIN REF CRJ200 SRM FOUND OUT OF LIMITS RECEIVED REO. COMPLIED WITH ALL STEPS OF REO.

Part: BOLT — CORRODED (EMERGENCY EXIT) · airframe 41,109 hrs · 38,383 cycles

*LH OVRWNG DOOR HARDWARE IS CORRODED IN THE PULL IN HANDLE. (C CHECK) RO 3/27/2020 REMOVED CORRODED HARDWARE FROM PULL IN HANDLE ON LH OVER WING DOOR AND INSTALLED 2 EACH NEW BOLTS, EACH NEW NUTS AND 2 EACH NEW WASHERS REF BOMBARDIER CMM. USED TUC8619, CAL DUE 31-OCT-20.

Part: FILLER — CHAFED (RT MLG WW) · airframe 41,109 hrs · 38,383 cycles

R/H MLG DOOR INNER TRAILING EDGE CHAFED ON PREVIOUS REPAIR. ( FLAGGED ) (C CHECK) RO 3/27/2020 REMOVED AND REPLACED DAMAGED REPAIR FILLER FROM R/H MLG DOOR INNER T/E SKIN. REF: CRJ-200 SRM. SEE CONTINUATION CARD FOR DETAILS.

Part: NUT PLATE — BROKEN (FUSELAGE) · airframe 41,109 hrs · 38,383 cycles

BROKEN NUTPLATE (1EA) UNDER CARGO FLOOR PANEL 282FRF. (MARKED) (C CHECK) RO 3/27/2020 REMOVED AND REPLACED 1EA. NUTPLATES COMMON TO PANEL 282FRF. REF CRJ 200 SRM.

Part: BOLT — CORRODED (EMERGENCY EXIT) · airframe 41,109 hrs · 38,383 cycles

*RH OVRWNG DOOR HARDWARE IS CORRODED IN THE PULL IN HANDLE. (C CHECK) RO 3/27/2020 REMOVED CORRODED HARDWARE FROM PULL IN HANDLE ON RH OVER WING DOOR AND INSTALLED 2 EACH NEW BOLTS, 2 EACH NEW NUTS AND 2 EACH NEW WASHERS REF BOMBARDIER CMM. USED TUC8619, CAL DUE 31-OCT-20.

Part: ELEVATOR — DENTED (LEFT) · airframe 41,109 hrs · 38,383 cycles

ADM #1985. BOTTOM LEFT ELEVATOR. LOCATED APPROX. 3.5" INBOARD OF ES 69-10 AND APPROX 16" FWD OF TRAILING EDGE. .9" X .9" AND .004" DEEP. PLOT, MAP, AND EVALUATE DAMAGE IF WITHIN ACCEPTABLE LIMITS OR REWORKED, ELIMINATE EVIDENCE USING STANDARD ACFT PRACTICES. (C CHECK) RO 3/27/2020 REPAIRED LEFT ELEVATOR DENT REF REO. CUT AWAY DAMAGED AREA, FABRICATED AND INSTALLED ALL REPAIR PARTS. COMPLIED WITH ALL STEPS OF REO. SEE CONTINUATION CARD FOR DETAILS.

Part: SKIN — DENTED (FUSELAGE) · airframe 41,109 hrs · 38,383 cycles

ADM #1764. APPROX FS 654.5, APPROX 10IN BELOW THE GROUND AIR SUPPLY CONNECTION ACCESS PANEL ON THE LH SIDE OF THE AIRCRAFT. DENT APPROX .02045IN DEEP, 1/4IN WIDE AND APPROX 3/4IN LONG. PLOT, MAP, AND EVALUATE DAMAGE IF WITHIN ACCEPTABLE LIMITS OR REWORKED, ELIMINATE EVIDENCE USING STANDARD ACFT PRACTICES. (C CHECK) RO 3/27/2020 FOUND DENT TO BE OUT OF LIMITS REF CRJ 200 SRM. RECEIVED ENGINEERING AND WORKED THE DENT PER REO. COMPLIED WITH TASK CARD. SEE CONTINUATION FOR FURTHER DETAILS.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 41,109 hrs · 38,383 cycles

COMPLY WITH SCHEDULED MAINTENANCE CODE: AD COMPLY WITH PARAGRAPH (J) OF AD BY 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 MRM. 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: 7366, POSITION: (C CHECK) RO 3/27/2020 COMPLIED WITH PARAGRAPH (J) OF AD 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 MRM. 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). MARKING THIS CAMP AS "STRUCTURAL REPAIR," WHICH WILL GENERATE AN RA FOR TRACKING THE SDIR FOR THIS REO ON THIS AIRPLANE. COMPLIED WITH SERIAL NUMBER 7366. COMPLIED WITH TASK CARD.

Part: WARNING LIGHT — FALSE ACTIVATION (MLG) · airframe 39,792 hrs · 36,876 cycles

GEAR DISAGREE RED WARNING AFTER TAKEOFF. MESSAGE EXTINGUISHED AFTER APPROX 5 SECONDS. DID NOT RECEIVE WARNING ON LANDING. (FLT#4297) CLOSED DEFERRED LANDING GEAR RETRACTION SYSTEM IAW MEL

Part: BRACKET — FAILED (PAX DOOR) · airframe 39,367 hrs · 36,385 cycles

RECEIVED PAX DR LATCH CAUTION MESSAGE ON TAKE OFF. REMOVED AND REPLACED PS6MB AND PS5MB MOUNTING BRACKETS IAW AMM. RE-RIGGED SENSORS IAW AMM. OPS CHECK GOOD.

Part: PRIORITY VALVE — FAILED (NLG) · airframe 38,004 hrs · 34,844 cycles

CREW REPORTED A GEAR DISAGREE WARNING MESSAGE AFTER SELECTING THE GEAR DOWN. NOSE GEAR WOULD NOT COME DOWN. ALSO RECEIVED A NOSE DOOR OPEN, WARNING MESSAGE. CREW COMPLIED WITH AN EMERGENCY GEAR EXTENSION & ALL GEAR CAME DOWN & LOCKED. REMOVED AND REPLACED THE NLG PRIORITY VALVE, OPS AND LEAK CHECKED GOOD.

Part: BRACKET — CORRODED (DOOR SILL) · airframe 37,305 hrs · 34,078 cycles

PASSENGER DOOR LOWER SILL AFT CUP HAS CORROSION. REMOVED AND REPLACED THE DOOR SILL AFT CUP BRACKET IAW SRM.

Part: BULKHEAD — DAMAGED (BS 621) · airframe 37,305 hrs · 34,078 cycles

BS 621 BULKHEAD, RBL 27.5 DAMAGED. REPAIRED THE BULKHEAD IAW REO. LEAK CHECKED GOOD.

Part: ANGLE — CRACKED (BS 621) · airframe 37,305 hrs · 34,078 cycles

CRACK IN FLOORBEAM ANGLE ATTACHED TO BS 621 BULKHEAD, RBL 43. REPLACED THE ANGLE IAW REO AND SRM.

Part: ANGLE — CORRODED (DOOR SILL) · airframe 37,305 hrs · 34,078 cycles

PASSENGER DOOR LOWER SILL ANGLE HAS CORROSION AT SEVERAL LOCATIONS. REMOVED AND REPLACED THE DOOR SILL ANGLE IAW SRM. OPS CHECKS GOOD.

Part: BRACKET — CORRODED (DOOR SILL) · airframe 37,305 hrs · 34,078 cycles

PASSENGER DOOR LOWER SILL FWD CUP HAS CORROSION. REMOVED AND REPLACED THE PAX DOOR SILL FWD CUP BRACKET.

Part: VANE — CHAFED (LT WING TE FLAP) · airframe 37,305 hrs · 34,078 cycles

LEFT INBD FLAP L/E VANE CAP IS CHAFED AT CENTER SECTION. REMOVED AND REPLACED THE LT INBD FLAP CENTER VANE CAP IAW SRM.

Part: THRESHOLD — CORRODED (SERVICE DOOR) · airframe 37,305 hrs · 34,078 cycles

SERVICE DOOR STEP PLATE IS CORRODED ON BACKSIDE. INSTALLED A NEW SERVICEABLE THRESHOLD PLATE IAW SRM.

Part: HINGE — DAMAGED (PAX DOOR) · airframe 37,305 hrs · 34,078 cycles

PASSENGER DOOR PIANO HINGE HALF ON FUSELAGE SIDE HAS DEEP GROOVES WORN INTO LUGS. REMOVED AND REPLACED THE HINGE IAW SRM.

Part: BALLAST — FAILED (CABIN LIGHTS) · airframe 37,282 hrs · 34,055 cycles

SMOKE ODOR IN THE CABIN. EMERGENCY DECLARED. REMOVED AND REPLACED LIGHT BALLAST AT ROW 4CD.

Part: DOOR SILL — CORRODED (CARGO BAY) · airframe 33,716 hrs · 30,216 cycles

CARGO DOOR SILL PLACED HAD SURFACE CORROSION AROUND NUTPLATE HOLES FROM FS 589 TO FS 605. C-CHECK NOT RELEASED, R & R DOOR SILL IAW REO.

Part: FLOOR SUPPORT — CORRODED (BS 310-319) · airframe 33,716 hrs · 30,216 cycles

RT CABIN FLOOR SILL CORRODED BETWEEN FS 310.00 AND FS 319.00, RBL 47. C-CHECK, NOT RELEASED, BLENDED OUT DAMAGE TO RT CABIN FLOOR SILL BETWEEN FS 310.00 AND FS 319.00 AT RBL 47 IAW REO.

Part: ANGLE — CORRODED (BS 319-349) · airframe 33,716 hrs · 30,216 cycles

SERVICE DOOR SURROUND BOTTOM ANGLE CORRODED BETWEEN FS 319.70 AND FS 349.00, RBL 47. C-CHECK, NOT RELEASED. R & R LOWER SILL ANGLE, PN 601R38303-253 IAW SRM.

Part: BULKHEAD WEB — CRACKED (BS 621) · airframe 33,716 hrs · 30,216 cycles

REAR PRESSURE BULKHEAD WEB AT FS 621 HAS MULTIPLE INDICATIONS NOTED AT RBL 27.50, WL 110, APPROXIMATELY 1.0" IN LENGTH. 60 PERCENT FSH FAILED NDT INSPECTION.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 31,302 hrs · 27,801 cycles

EMERGENCY LIGHTS FAILED TO ILLUMINATE. CHARGED THE BATTERY PACKS IAW AMM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 31,148 hrs · 27,635 cycles

EXTERIOR EMERGENCY LIGHT FIVE IS INOPERATIVE, REPLACED THE LAMPS.

Part: HANDLE — BROKEN (PAX DOOR) · airframe 31,009 hrs · 27,471 cycles

MAIN CABIN DOOR DIFFICULT TO OPEN FROM INSIDE. REPLACED THE PASSENGER DOOR OUTER HANDLE ASSY IAW AMM.

Part: POST — CRACKED (BS 409) · airframe 30,920 hrs · 27,388 cycles

FS 409.0+128, VERTICAL POST RBL 18.0 OTBD SIDE HAS INDICATION NOTED AT AFT FLANGE RADIUS APPROXIMATELY .3" IN LENGTH 70 PERCENT FSH. C-CHECK, INSTALLED A NEW POST IAW REO.

Part: POST — CRACKED · airframe 30,906 hrs · 27,373 cycles

VERTICAL POST BL0.0, LT AND RT SIDES HAVE INDICATIONS NOTED AT AFT FLANGE RADIUS BOTH APPROXIMATELY .3" IN LENGTH 50 PERCENT FSH. REPAIRED IAW REO AND SRM.

Part: POST — CRACKED (BS 409) · airframe 30,906 hrs · 27,373 cycles

FOUND 409+128 VERTICAL POST, LBL 18.0 OTBD SIDE HAS INDICATION NOTED AT AFT FLANGE RADIUS APPROXIMATELY .3" LONG 50 PERCENT FSH. C-CHECK, REPLACED VERTICAL POST IAW REO AND SRM.

Part: INTERCOSTAL — CORRODED (BS 349-364) · airframe 31,113 hrs · 27,597 cycles

INTERCOSTAL STRINGER 27 BETWEEN BS 349-364 CORRODED. C-CHECK, R & R INTERCOSTAL IAW SRM.

Part: FRAME — CORRODED (BS 364) · airframe 31,113 hrs · 27,597 cycles

FRAME AT BS 364 CORRODED BETWEEN STRINGERS 26 -27L. C-CHECK. REPAIRED FRAME IAW EA.

Part: BULKHEAD WEB — CRACKED · airframe 30,822 hrs · 27,295 cycles

REAR PRESSURE BULKHEAD WEB HAS A CRACK INDICATION NOTED AT LBL 27.50, WL 130 APPROXIMATELY .3" IN LENGTH 100 PERCENT FSH. C-CHECK, REPAIRED IAW REO.

Part: FRAME — CORRODED (BS 605) · airframe 30,759 hrs · 27,237 cycles

FRAME IS CORRODED AT BS 605 BETWEEN STRINGER 26-27L, REPAIRED FRAME IAW REO.

Part: FRAME — CORRODED (BS 605) · airframe 31,113 hrs · 27,597 cycles

FRAME CORRODED AT BS 605 BETWEEN STRINGERS 26 - 27L. C-CHECK. REPAIRED FRAME IAW REO.

Part: INTERCOSTAL — CORRODED (BS 349-364) · airframe 30,770 hrs · 27,246 cycles

INTERCOSTAL AT STRINGER 27 BETWEEN FS 349 - 364 CORRODED. C-CHECK, REPLACED INTERCOSTAL IAW SRM.

Part: FRAME — CORRODED (BS 364) · airframe 30,759 hrs · 27,237 cycles

FRAME AT BS 364 IS CORRODED BETWEEN STRINGERS 26 AND 27L. REPAIRED FRAME IAW EA.

Part: FRAME — CORRODED (BS 349) · airframe 30,759 hrs · 27,237 cycles

FRAME AT BS 349 STRINGER 27 HAS CORROSION. REPLACED FRAME SECTOR IAW SRM.

Part: FRAME — CORRODED (BS 319) · airframe 31,113 hrs · 27,597 cycles

FRAME AT BS 319 CORRODED ON FWD SIDE AT STRINGER 27. C-CHECK. R & R FRAME SECTOR IAW SRM.

Part: FRAME — CORRODED (BS 319) · airframe 30,770 hrs · 27,246 cycles

FRAME BS 319 HAS CORROSION ON FWD SIDE AT S27. C-CHECK, REPLACED FRAME SECTOR IAW SRM.

Part: POST — CRACKED (BS 409) · airframe 30,759 hrs · 27,237 cycles

FOUND BS 409 + 128 VERTICAL POST, LBL 18.0 OTBD SIDE HAS INDICATION NOTED AT AFT FLANGE RADIUS APPROX 3 INCHES IN LENGTH 50 PERCENT FSH. REPLACED VERTICAL POST AT FS 409.0 +128 LBL 18 IAW SRM AND REO.

Part: SKIN — CORRODED (WING) · airframe 31,113 hrs · 27,597 cycles

WING PLANK ACCESS HOLE AT PANEL 550FB HAS PITTING CORROSION ON FWD AND AFT SIDES. C-CHECK. BLENDED DAMAGE IAW REO.

Part: SKIN — CORRODED (WING) · airframe 31,113 hrs · 27,597 cycles

WING PLANK ACCESS HOLE AT PANEL 550GB HAS PITTING CORROSION ON FWD SIDE OF OPENING. C-CHECK. BLENDED DAMAGE IAW REO.

Part: SKIN — CORRODED (WING) · airframe 31,113 hrs · 27,597 cycles

WING PLANK ACCESS HOLE AT PANEL 540AB HAS PITTING CORROSION ON FWD AND AFT SIDES. C-CHECK. BLENDED DAMAGE IAW REO.

Part: CHANNEL — CRACKED (BS 621-625) · airframe 30,906 hrs · 27,373 cycles

FS 621- 625, THREE U-CHANNELS BETWEEN STRINGERS 13 & 14L ARE CRACKED. C-CHECK, REPAIRED IAW SRM.

Part: ACCESS PANEL — CORRODED (WING) · airframe 31,113 hrs · 27,597 cycles

WING PLANK ACCESS HOLE AT PANEL 640AB CORRODED AT FWD AND AFT SIDES. C-CHECK. REPAIRED IAW REO.

Part: SKIN — CORRODED (WING) · airframe 31,113 hrs · 27,597 cycles

WING PLANK ACCESS HOLE AT PANEL 650GB HAS PITTING CORROSION ON FWD AND AFT SIDES. C-CHECK, FILE NR 2014NM060066. BLENDED DAMAGE IAW REO.

Part: SELECTOR VALVE — FAILED (NLG) · airframe 27,952 hrs · 24,503 cycles

NOSE GEAR DID NOT COME DOWN. AFTER 2 MINUTES, GEAR CAME DOWN. (FLT 4519) REPLACED NOSE GEAR SELECTOR VALVE AND NOSE GEAR DOOR SELECTOR VALVE IN REFERENCE TO CRJ 200 MM. PN:750006000 SN OFF: 0625 AND SN OFF: 1142.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,806 hrs · 24,359 cycles

NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4743) RELAMPED EMERGENCY LIGHT.

Part: SUPPORT — DAMAGED (FUSELAGE) · airframe 26,998 hrs · 23,603 cycles

(C-CHECK) LEFT MLG DOWNLOCK SUPPORT STRUCTURE IS DAMAGED. REPAIRED PER REO.

Part: DOOR FRAME — CRACKED (PAX DOOR) · airframe 26,933 hrs · 23,552 cycles

PAX DOOR FRAME MEMBER AT FS 335.70 (FWD) IS CRACKED. REMOVED DAMAGED SECTION AND REPLACED FRAME IAW SRM 51-42-06.

Part: DOOR FRAME — CRACKED (PAX DOOR) · airframe 26,933 hrs · 23,552 cycles

PAX DOOR FRAME MEMBER AT FS 338.90 (AFT) IS CRACKED. REMOVED DAMAGED SECTION AND REPAIRED IAW REO 601R-52-11-402.

Part: DOOR FRAME — CRACKED (PAX DOOR) · airframe 26,933 hrs · 23,552 cycles

PAX DOOR FRAME MEMBER AT FS 323.30 (AFT) IS CRACKED. REMOVED DAMAGED SECTION AND REPLACED IAW SRM 51-42-06.

Part: DOOR FRAME — CRACKED (PAX DOOR) · airframe 26,933 hrs · 23,552 cycles

PAX DOOR FRAME MEMBER AT FS320.10 (FWD) IS CRACKED. REMOVED DAMAGED SECTION AND REPAIRED IAW REO 601R-52-11-402.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 3 · airframe 26,933 hrs · 23,552 cycles

FLOOR SILL CORRODED AFT OF SEVICE DOOR. CUT OUT DAMAGED SECTION AND INSTALLED FILLER AND DOUBLER IAW REO 601R-53-21-2199.

Part: BEAM — CRACKED (FUSELAGE) · airframe 19,820 hrs · 13,982 cycles

VERTICLE BEAM AT FS 409+128 RBL 18 IS CRACKED ON OUTBOARD SIDE LOWER CORNER. REMOVED DAMAGE ON RT 409+128 RBL 18 BEAM AND REPAIRED IAW BOMBARDIER REO 601R-53-41-056.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 19,820 hrs · 13,982 cycles

RT CAP ANGLE CRACKED AT RBL 18 AND WEB CRACKED AT RBL 18 AT NUT PLATE. COMPLIED WITH THE CAP ANGLE CUTOUT AND REPLACEMENT AND WEB REINFORCEMENT IAW REO 601R-53-41-260 AND REO 601R53-41-609.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 19,820 hrs · 13,982 cycles

FWD CARGO DOOR STOP FWD ANGLE BRACKET CRACKED. INSTALLED ANGLE AS REQUIRED 601R35011-11 IAW SRM 51-42-00.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 23,101 hrs · 20,060 cycles

BULKHEAD WEB CRACKED AROUND LINTEL ATTACH FITTING AT FS 621, LT SIDE. CUT OUT DAMAGED AREA AND INSTALLED REPAIR DOUBLER IAW REO 601R-53--61-1230 REV D AND REO 601R-53-61-3318.

Part: UPLOCK — FAILED (NLG) · airframe 22,115 hrs · 19,288 cycles

ON CLIMBOUT FROM CVG RECEIVED NOSE GEAR DISAGREE WARNING MSG. PERFORMED QRH, A/C RETURNED TO CVG LANDED SAFELY. FOUND NLG UPLOCK NOT LOCKING. REMOVED AND REPLACED NLG UPLOCK ASSY.

Part: SELECTOR VALVE — FAULTY (LANDING GEAR) · airframe 22,117 hrs · 19,287 cycles

ON CLIMBOUT FROM EWR TO CVG RECEIVED NOSE GEAR DISAGREE MSG. EMERGENCY DECLARED, A/C RETURNED TO EWR LANDED SAFELY. REMOVED AND REPLACED NOSE LANDING GEAR SELECTOR VALVE.

Part: PRIORITY VALVE — FAULTY (NLG) · airframe 22,115 hrs · 19,286 cycles

ON CLIMBOUT FROM CVG TO BOS RECEIVED NOSE GEAR DISAGREE MSG. EMERGENCY DECLARED, A/C RETURNED TO CVG LANDED SAFELY. REMOVED AND REPLACED NOSE LANDING GEAR PRIORITY VALVE.

Part: STRINGER CLIP — CRACKED (FS 625 S14L) · airframe 21,560 hrs · 18,851 cycles

CRACKED CLIP AT FS 625 STR 14 LT SIDE AFT EQUIPMENT COMPARTMENT. REPLACED CLIP IAW REO 601R-53-61-100 AND SR 99-5140-0001.

Part: STRINGER CLIP — CRACKED (FS625 RT) · airframe 21,560 hrs · 18,851 cycles

CRACKED STRINGER CLIP AT FS 625 STR 14 RT SIDE AFT EQUIPMENT COMPARTMENT. REPLACED CLIP IAW REO601R-53-61-100 AND SR99-5140-0001.

Part: SKIN — DENTED (BS 654-682) · airframe 19,333 hrs · 17,023 cycles

AIRCRAFT SKIN AT STA 654.50 TO 682.00 BETWEEN STR A8 AND A9 LEFT IS DENTED. MANUFACTURED AND INSTALLED REPAIR DOUBLER FOR DENT BETWEEN STA 654.50 AND 672.20 IAW EA 10-5361-01894 DATED 10-18-07.

Part: CABLE — FAILED (CABIN) · airframe 19,168 hrs · 16,890 cycles

FLIGHT 5259 - AFT 1/3RD OF EMERGENCY FLOOR LIGHTING INOP. REMOVED AND REPLACED CABLE JUMPER FOR EMERGENCY FLOOR LIGHTING.

Part: PDU — FAULTY (T/E FLAP) · airframe 18,944 hrs · 16,722 cycles

FLIGHT 5461 - FLAPS FAIL MESSAGE AT 30 DEGREES WHEN SELECTED TO 45 DEGREES. REMOVED AND REPLACED FLAP SYS PDU.

Part: BPSU — FAILED (T/E FLAP) · airframe 18,943 hrs · 16,721 cycles

FLIGHT 5460 - ON APPROACH INTO CVG, RECEIVED FLAPS FAIL CAUTION MESSAGE WITH FLAPS SELECTED TO 30 DEGREES. FLAPS FAILED AT 20 DEGREES. AIRCRAFT LANDED SAFELY. REMOVED AND REPLACED LEFT BPSU.

Part: SHAFT — DAMAGED (T/E FLAP) · airframe 18,940 hrs · 16,719 cycles

FLIGHT 5051 - ON APPROACH TO JAN, FLAPS SELECTED TO 45 DEGREES, FLAPS FAIL CAUTION MESSAGE AT 30 DEGREES. AIRCRAFT LANDED SAFELY. REMOVED AND REPLACED RIGHT SIDE NR 5 FLEX SHAFT.

Part: FLAP — MALFUNCTIONED (WING) · airframe 18,943 hrs · 16,721 cycles

FLIGHT 5367 - FLAP FAIL CAUTION MESSAGE. AIRCRAFT LANDED SAFELY ON SECOND APPROACH. COMPLIED WITH AD 2006-12-21 FLAP CAUTION MESSAGE -FIRST EVENT- MAINTENANCE ACTION, PARAGRAPH (G) 1, 2, 3, (A, B, C). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTION MESSAGES.

Part: PRIORITY VALVE — FAULTY (NOSE HYD BAY) · airframe 17,784 hrs · 15,811 cycles

FLIGHT 5389 - RECEIVED GEAR DISAGREE DURING EXTENSION INDICATION NOSE GEAR MALFUNCTION. PRIOR TO QRH COMPLETION, MESSAGE DISAPPEARED. DECLARED EMERGENCY AND LANDED WITHOUT INCIDENT. REPLACED NOSE GEAR PRIORITY VALVE, CLEANED AND LUBRICATED NOSE LANDING GEAR. NO FURTHER DEFECTS.

Part: IDG — WARNING LIGHT (NR 1) · airframe 17,485 hrs · 15,583 cycles

FLIGHT 5073 - AS THRUST LEVERS WERE ADVANCED FOR TAKEOFF, RECEIVED IDG NR 1 CAUTION. ABORTED TAKEOFF AT 80 KTS. IDG CAUTION EXTINGUISHED AND GEN 1 OFF MESSAGE APPEARED. SERVICED NR 1 IDG IAW AMM 12-13-24, OPS CHECK GOOD, NO FURTHER DEFECTS.

Part: IDG — WARNING LIGHT (NR 1) · airframe 16,886 hrs · 15,096 cycles

FLIGHT 5304 - DURING TAKEOFF ROLL, RECEIVED AN IDG NR 1 CAUTION, ABORTED TAKEOFF AND FLIGHT RETURNED TO THE GATE. SERVICED THE NR 1 IDG.

Part: SERVO — MALFUNCTIONED (AILERON) · airframe 15,495 hrs · 13,953 cycles

FLIGHT 5657 - FLIGHT CONTROLS STUCK DURING LANDING APPROACH. REPLACED THE AILERON SERVO.

Part: FAN BLADE — VIBRATES (RT ENGINE) · airframe 15,459 hrs · 13,921 cycles

FLIGHT 5022 - RT ENGINE N1 VIBE INDICATED 2.5. REPLACED THE RT ENGINE FAN BLADES.

Part: RESERVOIR — MALFUNCTIONED (NR 3 HYD SYSTEM) · airframe 15,366 hrs · 13,840 cycles

FLIGHT 5299 - GEAR DISAGREE WARNING. REPLACED THE NR 3 HYDRAULIC SYSTEM RESERVOIR.

Part: COMPUTER — MALFUNCTIONED (DG) · airframe 15,316 hrs · 13,798 cycles

FLIGHT 5005 - PILOT AND CO-PILOT DG WHITE FLAG AND UNRELIABLE. REPLACED THE NR 1 AHC.

Part: DOOR — OPEN (POWER ACCESS) · airframe 15,136 hrs · 13,649 cycles

FLIGHT 5531 - GROUND POWER ACCESS DOOR OPEN DURING FLIGHT. INSPECTED DOOR, FOUND SERVICEABLE, CLOSED DOOR.

Part: PCU — MALFUNCTIONED (SPOILERS) · airframe 14,587 hrs · 13,171 cycles

FLIGHT 5432 - SPOILER CONFIG MESSAGE DURING T/O. REPLACED THE LT SPOILERON PCU.

Part: CONTROL UNIT — ACTIVE (TE FLAPS) · airframe 13,667 hrs · 12,351 cycles

FLIGHT 5366 FLAPS FAIL CAUTION. REPLACED THE FECU.

Part: BPSU — OUT OF RIG (TE FLAPS) · airframe 13,667 hrs · 12,351 cycles

FLIGHT 5349 FLAPS FAIL CAUTION. RERIGGED THE LT AND RT BPSU.

Part: ENGINE — MALFUNCTIONED (LEFT) · airframe 12,496 hrs · 11,334 cycles

FLIGHT 5212 LEFT ENGINE OIL PRESSURE WARNING. REPLACED THE LEFT ENGINE.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 10,266 hrs · 9,552 cycles

FLIGHT 5226 EMERGENCY LIGHTS AT CABIN AND SERVICE DOOR ARE INOP. REPAIRED BROKEN WIRES AND SYSTEM TEST SATISFACTORY.

Part: WIRE — DISCONNECTED (CABIN) · airframe 10,173 hrs · 9,477 cycles

FLIGHT 5600 EMERGENCY LIGHTS AT CABIN AND SERVICE DOORS ARE INOP. RECONNECTED LOOSE WIRE CONNECTION.

Part: ELEMENT — MALFUNCTIONED (ANTI ICE DUCT) · airframe 9,950 hrs · 9,308 cycles

FLIGHT 5359 ANTI ICE DUCT WARNING. REPLACED SENSING ELEMENT A46WK.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 9,529 hrs · 8,980 cycles

LEFT HAND 621 FLOOR SUPPORT ANGLE CRACKED. REPAIRED IN ACCORDANCE WITH REO 601R-53-61-117.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 9,529 hrs · 8,980 cycles

RIGHT HAND 621 FLOOR SUPPORT ANGLE CRACKED. REPAIRED IN ACCORDANCE WTIH REO 601R-53-61-117 AND CRJ SRM 51-25-16.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 8,802 hrs · 8,418 cycles

FLIGHT 5133 PILOTS WINDSHIELD SHATTERED DURING TAXI. REPLACED WINDSHIELD.

Part: SPOILER · airframe 6,328 hrs · 6,378 cycles

FLIGHT 5755 SPOILERS CAUTION MESSAGE DURING FLIGHT.COULD NOT DUPLICATE. NO FAULTS CODES IN COMPUTER.

Part: TRIM SWITCH — BROKEN (COCKPIT) · airframe 4,752 hrs · 4,828 cycles

FLIGHT 5674 RUDDER TRIM CONTROL IS BROKEN.REPLACED TRIM CONTROL PANEL.

Part: DOOR · airframe 4,298 hrs · 4,356 cycles

FLIGHT 5895 DOOR OUTER HANDLE CAUTION MESSAGE DURING T/O.COULD NOT DUPLICATE. DOOR OPERATION NORMAL, NO DEFECTS FOUND.

Part: ESCAPE HATCH · airframe 3,441 hrs · 3,475 cycles

FLIGHT #5354 - CREW ESCAPE HATCH EXTREMELY LOUD DURING T/O, AIRCRAFT RETURNED TO THE FIELD.REMOVED, INSPECTED AND REINSTALLED CREW ESCAPE HATCH. NO DEFECTS WERE FOUND. CABIN PRESSURE CHECK WAS NORMAL.

Part: DOOR · airframe 3,299 hrs · 3,325 cycles

FLIGHT #5506. DURING CLIMB OUT OF CHO RECEIVED A CABIN DOOR OUTER HANDLE CAUTION MESSAGE, AIRCRAFT RETURNED TO THE FIELD.CLEANED AND LUBRICATED THE CABIN DOOR OUTER HANDLE LOCKING MECHANISM.

Part: WARNING SYSTEM — MALFUNCTIONED (COCKPIT) · airframe 5,333 hrs · 3,260 cycles

FLIGHT 5420. DURING CLIMBOUT OF CVG RECEIVED A CABIN DOOR OUTER HANDLE CAUTION MESSAGE, CREW DECLARED AN EMERGENCY AND RETURNED TO THE FIELD. PERFORMED AN OPERATIONAL CHECK OF THE CABIN DOOR OUTER HANDLE WARNING SYSTEM, DISCREPANCY COULD NOT BE DUPLICATED BY MAINTENANCE, RELEASED AIRCRAFT BACK TO SERVICE.

Part: DOOR · airframe 3,024 hrs · 3,034 cycles

CABIN DOOR OUTER HANDLE CAUTION MESSAGE.DEFERRED MAINTENANCE PER M.E.L.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 2,991 hrs · 2,992 cycles

COPILOTS WINDSHIELD CRACKED DURING FLIGHT. REPLACED WINDSHIELD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 2,838 hrs · 2,836 cycles

EMERGENCY LIGHT AT CABIN ENTRANCE IS INOPERABLE. SECURED WIRE CONNECTION, LIGHT OPERATES NORMAL.

Part: SENSOR — MALFUNCTIONED (APU TEMP) · airframe 2,530 hrs · 2,524 cycles

APU OIL TEMP CAUTION MESSAGE. REPLACED THE OIL TEMP BULB.

Part: SENSOR — MALFUNCTIONED (APU) · airframe 2,501 hrs · 2,499 cycles

APU OIL TEMP CAUTION MESSAGE. REPLACED OIL TEMP SENSOR.

Part: LAMP — BURNED OUT (OVERWING) · airframe 2,496 hrs · 2,491 cycles

OVERWING EMERGENCY LIGHT IS INOPERABLE. REPLACED THE LIGHT BULB.

Part: BUSHING — WORN (VERTICAL STAB) · airframe 1,262 hrs · 1,328 cycles

HORIZONTAL AND VERTICAL STABILIZER BUSHINGS ARE WORN. REPAIRED HORIZONTAL AND VERTICAL STABILIZER BUSHINGS IAW REO 601R-55-11-22 REV A AND WVAC EO 601R-55-1521.

Part: HANDLE — MALFUNCTIONED (COCKPIT) · airframe 833 hrs · 872 cycles

LANDING GEAR DID NOT EXTEND WHEN SELECTED DOWN. REPLACED THE LANDING GEAR CONTROL HANDLE.

Part: SELECTOR — FAILED (MLG)

WHEN GEAR HANDLE SELECTED DOWN, GEAR DID NOT COME DOWN. EMERGENCY EXTENSION OF GEAR REQUIRED. REMOVED AND REPLACED LANDING GEAR CONTROL PANEL.

Part: PSEU — FAILED (E/E BAY)

WHEN GEAR HANDLE SELECTED DOWN, GEAR DID NOT COME DOWN. EMERGENCY EXTENSION OF GEAR REQUIRED. REMOVED AND REPLACED PSEU. AIRCRAFT RETURNED TO SERVICE.