N866AS

Part: BULKHEAD WEB — CRACKED (BS 280) · airframe 40,277 hrs · 36,015 cycles

FS.280.00 LOWER WEB HAS CRACKS AT LBL9 AND RBL9. (C-CHECK) RO: 11/12/2018 COMPLIED WITH REPAIR OF THE FS280 BULKHEAD WEB. PERFORMED ALL STEPS IAW REO.

Part: FRAME — CORRODED (BS 589) · airframe 40,277 hrs · 36,015 cycles

FS589.00, STGR27 AND STGR26R €“ FRAME SHOWS SIGNS OF CORROSION ON THE FWD SIDE. (C-CHECK) RO: 11/12/2018REPLACED CORRODED FRAME SECTION AT FS 589.00 @STGR 20L IAW REO. PRESSURE LEAK CHECK GOOD.

Part: STRINGER — CRACKED (BS 282) · airframe 40,277 hrs · 36,015 cycles

CLIP ON THE UPPER SIDE OF STGR3L, FS282.00 IS CRACKED. (C-CHECK) RO: 11/12/2018 REMOVED AND INSTALLED NEW CLIP ON THE UPPER SIDE OF STGR3L, FS282.00. IAW SRM. PRESSURE LEAK CHECK GOOD.

Part: DOUBLER — CORRODED (BS 349) · airframe 40,277 hrs · 36,015 cycles

CORROSION ON DOUBLER FOR THE PASSENGER DOOR LOWER SILL FS349.00. (C-CHECK) RO: 11/12/2018 REMOVED CORROSION FROM DOUBLER LOCATED UNDER FLOOR SILL JUST AFT OF PAX DOOR CUTOUT IAW SRM.

Part: SKIN — DENTED (BS 369) · airframe 40,277 hrs · 36,015 cycles

DENT IN FUSELAGE SKIN AT FS639.00 JUST BELOW STGR2R. (C-CHECK) RO: 11/12/2018 DRESSED BACK DENT IN FUSELAGE SKIN AT FS639.00 JUST BELOW STGR2R IAW REO.

Part: BRACKET — FAILED (MLG) · airframe 38,841 hrs · 34,595 cycles

GEAR DISAGREE NOSE GEAR WOULD NOT RETRACT. (FLT#2944) CLOSED REMOVED AND REPLACED BRACKET IAW AMM. SWUNG GEAR OPS GOOD.

Part: BRACKET — DAMAGED (NLG) · airframe 38,734 hrs · 34,480 cycles

NOSE GEAR DISAGREE. REMOVED AND REPLACED THE NR 2 WOW AND CENTERED HARNESS ASSY IAW AMM. OPS CHECKED GOOD. REMOVED AND REPLACED CENTERING SENSOR BRACKET IAW CMM. OPS CHECKED GOOD.

Part: CONTROL UNIT — FAILED (TE FLAPS) · airframe 38,005 hrs · 33,668 cycles

FLAP FAIL, RETURNED TO THE FIELD. EMERGENCY DECLARED. REPLACED THE FLAP LEVER AND FECU. AND RERIGGED THE RIGHT BPSU. SYSTEM OP CHECKS GOOD.

Part: UNKNOWN — SMOKE (COCKPIT) · airframe 37,510 hrs · 33,094 cycles

SMOKE IN COCKPIT AND SMOKE CARGO WARNING MESSAGE, DIVERTED. OPEN.

Part: CARBON SEAL — LEAKING (NR 1) · airframe 38,182 hrs · 33,869 cycles

SMOKE IN THE COCKPIT AND A SMOKE CARGO WARNING MESSAGE. DIVERTED. REMOVED AND REPLACED THE NR 1 CARBON SEAL. LEAK CHECKED AND OIL CONSUMPTION CHECKED GOOD.

Part: PANEL — CHAFED (RT WING) · airframe 36,646 hrs · 32,139 cycles

PANEL 684BB CHAFED ON FWD EDGE. REPAIRED IAW EA.

Part: PLATE — CRACKED (CARGO BAY) · airframe 36,646 hrs · 32,139 cycles

CARGO SKIN PROTECTIVE PLATE HAS CRACKS AROUND FASTENER HOLES. ( LOCATED & DRILLED HOLES ON NEW CARGO PROTECTIVE PLATE IAW SRM.

Part: SKIN — WORN (RT NACELLE) · airframe 36,646 hrs · 32,139 cycles

RIGHT NACELLE CORE COWL HAS WEAR AT LATCH AREA CAUSED BY BLOCKER DOOR. FABRICATED AND INSTALLED REPAIR PLATE IAW CMM. BLENDED NR 6 BLOCKER DOOR TO OBTAIN THE CORRECT CLEARENCE IAW CMM, CLEARANCE CHECKED GOOD.

Part: LANDING GEAR — MALFUNCTIONED (NOSE) · airframe 34,465 hrs · 29,690 cycles

GEAR DISAGREE MESSAGE WITH WOW MESSAGE. RETURNED TO DEPARTURE. SERVICED NLG, BLED SYSTEM. OPS CHECKED GOOD.

Part: WARNING MESSAGE — FALSE ACTIVATION (THRUST REVERSER) · airframe 33,283 hrs · 28,511 cycles

"RT REV UNLOCKED" CAUTION MSG IN FLIGHT. COMPLIED WITH QRH PROCEDURE ON EMER1-16, LANDED NEAREST SUITABLE AIRPORT. TROUBLESHOT RIGHT THRUST REVERSER UNLOCK MESSAGE DURING FLIGHT IN REFERENCE TO FIM, CHECK FOR GROUND ONTHROTTLE LOCKOUT GEARBOX SOLENOID, NO DEFECTS NOTED, CHECKED RIGGING OF STOW AND THROTTLE LOCKOUT SWITCHES, NO DEFECTS NOTED. CHECKED RIGGING OF PDU AND OPERATION OF FLEXSHAFT SWITCH AND BRAKE SWITCH NO DEFECTS.

Part: TUBE — DAMAGED (SERVICE DOOR) · airframe 32,212 hrs · 27,461 cycles

SERVICE DOOR CONVOLEX DAMAGED. C-CHECK, R & R CONVOLEX TUBING WITH NEW, IAW REO.

Part: PICCOLO TUBE — DENTED (LT WING) · airframe 32,212 hrs · 27,461 cycles

LT WING OTBD PICCOLO TUBE HAS A DENT 38.5" FROM OTBD EDGE. C-CHECK, REPAIRED DENT IN OTBD PICCOLO TUBE IAW STS EA.

Part: PICCOLO TUBE — GOUGED (LT WING) · airframe 32,212 hrs · 27,461 cycles

LEFT WING OTBD PICCOLO TUBE HAS GOUGE NEAR WELD AT INBD FLANGE. C-CHECK, REPAIRED GOUGE ON INBD FLANGE IAW STS EA.

Part: PICCOLO TUBE — CHAFED (LT WING) · airframe 32,212 hrs · 27,461 cycles

LEFT WING OTBD PICCOLO TUBE HAS CHAFING FROM L/E RIB BETWEEN 530JZ AND 530KZ. C-CHECK, REPAIRED CHAFE ON OTBD PICCOLO TUBE IAW STS EA.

Part: PICCOLO TUBE — DAMAGED (LT WING) · airframe 32,212 hrs · 27,461 cycles

LT WING OTBD PICCOLO TUBE HAS DRILL START 38.5" FROM OTBD EDGE. C-CHECK, CLEANED AND WELDED DRILL START IAW STS EA.

Part: SKIN — GOUGED (BS 409) · airframe 32,212 hrs · 27,461 cycles

FUSELAGE SKIN, LOWER FORWARD AREA, RT LOWER DME ANTENNA FOOT PRINT HAS A MINOR GOUGE. C-CHECK, REPAIRED LWR FUSELAGE BETWEEN FS 409.0+48 & 409.00+64, S25R-S26R IAW STS EA.

Part: SKIN — GOUGED (BS 409) · airframe 32,212 hrs · 27,461 cycles

ON FUSELAGE SKIN LOWER FORWARD AREA, LT LOWER DME ANTENNA FOOT PRINTS HAS MINOR GOUGES 2 LOCATIONS. C-CHECK, REPAIRED LWR FUSELAGE BETWEEN FS 409.0+48 & 409.00+64, S25L-S26L IAW STS EA.

Part: SKIN — NICKED (FUSELAGE) · airframe 32,212 hrs · 27,461 cycles

FWD LOWER CORNER OF PAX DOOR CUT OUT HAS NICKS. C-CHECK, BLENDED FWD LOWER CORNER FUSELAGE SKIN AT PAX DOOR CUT OUT TO A SMOOTH FINISH, IAW STS EA.

Part: HINGE — GOUGED (PAX DOOR) · airframe 32,212 hrs · 27,461 cycles

FUSELAGE MOUNTED PAX DOOR PIANO HINGE HALF HAS A GOUGE ON LUG, 6TH FROM AFT END. C-CHECK, BLENDED DAMAGED AREA TO A SMOOTH FINISH, IAW REO.

Part: HINGE — GOUGED (PAX DOOR) · airframe 32,212 hrs · 27,461 cycles

PAX DOOR MOUNTED PIANO HINGE HALF HAS WEAR GROOVES AND GOUGES ON LUGS 12 LOCATIONS SEEN WITH DOOR OPENED AND CLOSED. BLENDED DAMAGED AREA TO A SMOOTH FINISH, IAW REO.

Part: FLOOR SUPPORT — CORRODED (BS 461) · airframe 32,212 hrs · 27,461 cycles

LEFT FUSELAGE FLOOR ANGLE CORRODED AT FS461, LBL 47. C-CHECK, REMOVED CORROSION ON LT FUSELAGE FLOOR ANGLE AT FS 461, LBL47 IAW REO.

Part: SEAT TRACK — CORRODED (BS 612-617) · airframe 32,212 hrs · 27,461 cycles

LEFT FUSELAGE SEAT TRACK CORRODED AT BS 612 - 617 LBL 9. R & R THE SEAT TRACK SECTION, IAW REO AND SRM.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 32,212 hrs · 27,461 cycles

LEFT FUSELAGE SEAT TRACK CORRODED AT BS 559+112 LBL 9. REPLACED THE SEAT TRACK IAW REO.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 32,212 hrs · 27,461 cycles

RT FUSELAGE SEAT TRACK CORRODED BS 559+80 - 559+96. R & R THE SEAT TRACK SECTION IAW REO.

Part: FLOOR SUPPORT — CORRODED (BS 605-621) · airframe 32,212 hrs · 27,461 cycles

RT FUSELAGE FLOOR SUPPORT IS CORRODED AROUND NUTPLATE HOLE BS 605 - 621. REMOVED CORROSION IAW REO.

Part: LINE — CRACKED (APU FUEL) · airframe 32,212 hrs · 27,461 cycles

APU FUEL LINE HAS A CRACKED WELD AT SUPPORT BRACKET INSIDE PRESSURE BOX. C-CHECK, REINFORCED FUEL LINES FUEL PRESSURE BOX IAW REO.

Part: FLOOR SUPPORT — CORRODED (BS 529) · airframe 32,212 hrs · 27,461 cycles

RIGHT FUSELAGE FLOOR ANGLE HAS CORROSION AT FS529.00, RBL 47. C-CHECK, CORROSION ON RT FLOOR ANGLE AT FS 529.00, RBL 47, WAS BLENDED IAW REO.

Part: FLOOR SUPPORT — CORRODED (BS 544) · airframe 32,212 hrs · 27,461 cycles

LEFT FUSELAGE FLOOR ANGLE HAS CORROSION AT FS 544, LBL47. C-CHECK, BLENDED CORROSION IAW REO.

Part: FLOOR SUPPORT — CORRODED (BS 449) · airframe 32,212 hrs · 27,461 cycles

LEFT FUSELAGE FLOOR ANGLE CORRODED AT BS 449.85, LBL 47. REMOVED CORROSION BY BLENDING IAW REO.

Part: FLOOR SUPPORT — CORRODED (BS 461) · airframe 32,212 hrs · 27,461 cycles

RIGHT FUSELAGE FLOOR ANGLE HAS CORROSION AT FS 461, RBL 47. BLENDED OUT CORROSION IAW REO.

Part: FLOOR SUPPORT — CORRODED (BS 559) · airframe 32,212 hrs · 27,461 cycles

RT FLOOR SUPPORT BS 559+80 - 559+112 IS CORRODED. CORROSION WAS BLENDED AND FOUND WITHIN LIMITS IAW REO AND SRM.

Part: FLOOR SUPPORT — CORRODED (BS 499-513) · airframe 32,212 hrs · 27,461 cycles

RIGHT FUSELAGE FLOOR ANGLE HAS CORROSION AT FS 499 TO 513, RBL 47. C-CHECK, CORROSION ON RT FLOOR ANGLE AT FS 499 TO FS 513, RBL 47, WAS BLENDED IAW REO.

Part: FLOOR SUPPORT — CORRODED (BS 473) · airframe 32,212 hrs · 27,461 cycles

RIGHT FUSELAGE FLOOR ANGLE HAS CORROSION AT FS 473.15 RBL 47. REMOVED CORROSION BY BLENDING IAW REO.

Part: FLOOR SUPPORT — CORRODED (BS 513) · airframe 32,212 hrs · 27,461 cycles

LEFT FUSELAGE FLOOR ANGLE HAS CORROSION AT AFT SIDE OF FS 513. C-CHECK, CORROSION ON LEFT FLOOR ANGLE AFT OF FS 513 WAS BLENDED IAW REO.

Part: FLOOR SUPPORT — CORRODED (BS 499-513) · airframe 32,212 hrs · 27,461 cycles

LEFT FLOOR ANGLE HAS CORROSION AT FS499 TO 513 LBL47. C-CHECK, CORROSION ON LT FLOOR ANGLE FS 499-FS 513 AT LBL 47 WAS BLENDED IAW REO.

Part: FLOOR SUPPORT — CORRODED (BS 449) · airframe 32,212 hrs · 27,461 cycles

RIGHT FUSELAGE FLOOR ANGLE HAS CORROSION AT FS449.85, RBL 47. C-CHECK CORROSION ON RIGHT FLOOR ANGLE AT FS 449.85, RBL 47, WAS BLENDED IAW REO.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 32,212 hrs · 27,461 cycles

LEFT FUSELAGE SEAT TRACK CORRODED AT BS 559+80 - 559+96 LBL 9. R & R THE SEAT TRACK SECTION IAW REO.

Part: ATTACH ANGLE — GOUGED (BS 621) · airframe 32,212 hrs · 27,461 cycles

AFT CARGO FLOORBEAM ATTACHMENT TO THE BS 621 PRESSURE BULKHEAD AT LBL27 HAS GOUGE. C-CHECK, REPAIRED AFT CARGO FLOOR RAIL FITTING ON FS 621 LBL 27.00 IAW REO.

Part: ANGLE — CRACKED (BS 484) · airframe 32,212 hrs · 27,461 cycles

FS 484, RBL 36, OTBD CLIP IS CRACKED. C-CHECK, INSTALLED REPAIR ANGLE IAW REO.

Part: SKIN — CHAFED (LT WING TE FLAP) · airframe 32,212 hrs · 27,461 cycles

LT INBD FLAP INNER SKIN IS CHAFED FROM GROUND WIRE UNDER PANEL 584CB. C-CHECK, BLENDED THE LT, INBD FLAP INNER SKIN UNDER PANEL 584CB IAW STS EA.

Part: DOOR — DAMAGED · airframe 32,212 hrs · 27,461 cycles

BUTTE DOOR 594LB HAS A NICK NEAR SCREW HOLE ON INBD SIDE. C-CHECK, REPAIRED BUTTE DOOR 594LB IAW EA.

Part: SKIN — CHAFED (RT AILERON) · airframe 32,212 hrs · 27,461 cycles

RT AILERON UPPER SKIN SHROUD CHAFED IN 2 LOCATION, BOTH SIDES OF OTBD HINGE. C-CHECK, BLENDED RT AILERON UPPER SKIN SHROUD IN 2EA LOCATIONS, BOTH SIDES OF OTBD HINGE IAW REO.

Part: POST — CRACKED (BS 409) · airframe 32,212 hrs · 27,461 cycles

VERTICAL POST AT FS 409+128, LBL 27 INBD SIDE IS CRACKED. C-CHECK, R & R CRACKED POST AT FS 409+128 LBL 27 INBD SIDE IAW EA.

Part: SKIN — CHAFED (LT AILERON) · airframe 32,212 hrs · 27,461 cycles

LEFT AILERON UPPER SKIN SHROUD CHAFED IN 2 LOCATION, INBD OF INBD HINGE AND OTBD OF CENTER HINGE. C-CHECK, BLENDED THE LT AILERON UPPER SKIN SHROUD, 2EA, CHAFES, INBD OF INBD HINGE AND OT OTBD CENTER HINGE IAW REO.

Part: LINK — CHAFED (THRUST REVERSER) · airframe 32,212 hrs · 27,461 cycles

LEFT ENGINE BLOCKER BLOCKER DOOR LINKS HAVE CHAFE DAMAGE AT FORWARD END. REPAIRED DAMAGE ON LT ENG BLOCKER DOOR LINKS IAW REO.

Part: POST — CRACKED (BS 409) · airframe 32,212 hrs · 27,461 cycles

VERTICAL POST AT FS 409+128, RBL 18 OBD SIDE IS CRACKED. C-CHECK R & R THE VERTICAL POST AT FS409+128, RBL18 OTBD IAW REO.

Part: POST — CRACKED (BS 409) · airframe 32,212 hrs · 27,461 cycles

VERTICAL POST AT FS 409+128, RBL 27 INBD SIDE IS CRACKED. C-CHECK, R & R CRACKED POST AT FS 409+128 RBL 27 INBD SIDE IAW STS EA.

Part: POST — CRACKED (BS 409) · airframe 32,212 hrs · 27,461 cycles

VERTICAL POST AT FS 409+128, LBL 18 OTBD IS CRACKED. C-CHECK, R & R FS 409+128, LBL 18 OTBD VERTICAL POST IAW REO.

Part: SKIN — CHAFED (RT WING TE FLAP) · airframe 32,212 hrs · 27,461 cycles

RT WING INBD FLAP HAS INNER SKIN CHAFE FROM BONDING WIRE UNDER PANEL 684BB. C-CHECK, BLENDED OUT CHAFE ON RT INBD FLAP INNER SKIN UNDER PANEL 684BB IAW STS EA.

Part: POST — CRACKED (BS 409) · airframe 32,212 hrs · 27,461 cycles

VERTICAL POST AT FS 409+128, LBL 18 INBD IS CRACKED. C-CHECK, RO: 11/06/2014. R & R THE VERTICAL POST AT FS409+128, LBL 18 OTBD IAW REO.

Part: BULKHEAD WEB — CRACKED (BS 621) · airframe 32,212 hrs · 27,461 cycles

CRACK NOTED ON FS 621 BULKHEAD WEB, FWD FACE, ALONG HEEL LINE AT RBL27.5, APPROXIMATELY WL90. C-CHECK, INSTALLED ALL REPAIR PARTS IAW REO.

Part: VANE — CHAFED (RT WING TE FLAP) · airframe 32,212 hrs · 27,461 cycles

RIGHT INBD FLAP VANE SKIN INBD CAP CHAFED. BLENDED RT INBD FLAP VANE SKIN INBD CAP IAW REO.

Part: FLOOR PANEL — CRACKED (BS 193) · airframe 32,212 hrs · 27,461 cycles

LEFT TRU BAY FLOOR CRACKED AT BS 193. INSTALLED REPAIR IAW REO.

Part: VANE CAP — CHAFED (LT WING TE FLAPS) · airframe 32,212 hrs · 27,461 cycles

LEFT INBD FLAP VANE SKIN MOST OTBD CAP CHAFED. BLENDED LT, INBD FLAP VANE SKIN OTBD CAP IAW REO.

Part: SKIN — DENTED (BS 605) · airframe 32,212 hrs · 27,461 cycles

SMALL DENT BELOW CARGO DOOR ON FUSELAGE, BEHIND BS 605.00 AND BELOW STINGER 20, REPAIRED IAW EA.

Part: END PLUG — DENTED (PAX DOOR) · airframe 32,212 hrs · 27,461 cycles

PAX DOOR AFT END CAP IS DENTED. C-CHECK, REMOVED, REPAIRED AND INSTALLED PAX DOOR AFT END CAP, IAW REO.

Part: VANE — CHAFED (RT WING TE FLAP) · airframe 32,212 hrs · 27,461 cycles

RIGHT INBD FLAP VANE SKIN CENTER OTBD CAP CHAFED. BLENDED THE RT, INBD FLAP VANE SKIN CENTER OTBD CAP IAW REO.

Part: ARM — CHAFED (PAX DOOR) · airframe 32,212 hrs · 27,461 cycles

PAX DOOR WHEEL SUPPORT ARM CHAFED. BLENDED DAMAGED AREA ON THE PAX DOOR WHEEL SUPPORT LEG TO A SMOOTH CONTOUR, IAW EA.

Part: SKIN — CHAFED (LT NACELLE) · airframe 32,212 hrs · 27,461 cycles

LEFT ENGINE CORE COWL, 435AB HAS 3.5 INCH CHAFE AFT OF FWD LATCH. C-CHECK, REPAIRED LT ENGINE CORE COWL 435AB IAW STS EA.

Part: SKIN — DENTED (LT WING TE FLAP) · airframe 32,212 hrs · 27,461 cycles

LEFT OTBD FLAP FIXED VANE SKIN DENTED APPROX 11" FROM MOST INBD EDGE. C-CHECK, INSTALLED NEW VANE SKIN IAW SRM AND REO.

Part: VANE CAP — CHAFED (LT WING TE FLAP) · airframe 32,212 hrs · 27,461 cycles

LEFT INBD FLAP VANE SKIN MOST INBD CAP CHAFED. BLENDED CHAFE ON THE LT, INBD FLAP VANE SKIN IAW REO.

Part: SKIN — DENTED (BS 333) · airframe 32,212 hrs · 27,461 cycles

SHALLOW DENT ONE INCH IN DIAMETER .044 DEEP, CENTERED 12 INCHES BELOW THE SERVICE DOOR. C-CHECK, REPAIRED DENT BELOW THE SERVICE DOOR AT BS 333 BETWEEN S20-21R IAW EA.

Part: VANE CAP — CHAFED (LT WING TE FLAP) · airframe 32,212 hrs · 27,461 cycles

LEFT INBD FLAP VANE SKIN CENTER OTBD CAP CHAFED. C-CHECK, RO: 11/06/2014 BLENDED THE LT, INBD FLAP VANE SKIN CENTER OTBD CAP IAW REO.

Part: SKIN — DENTED (RT WING) · airframe 32,212 hrs · 27,461 cycles

RIGHT WING LEADING EDGE PANEL 630JL HAS A DENT ABOUT THE MIDDLE, UPPER LEADING EDGE SURFACE. DRESSED DENT BACK TO ORIGINAL CONTOUR IAW REO.

Part: WEB — DENTED (PAX DOOR) · airframe 32,212 hrs · 27,461 cycles

PAX DOOR AFT WEB HAS A DENT BY POWER ASSISIT MOTOR BRACKET. DRESSED OUT THE DENT AT THE PAX DOOR AFT WEB BY POWER ASSIST MOTOR TO THE ORIGINAL CONTOUR IAW EA.

Part: END PLUG — DENTED (PAX DOOR) · airframe 32,212 hrs · 27,461 cycles

PAX DOOR FWD END CAP IS DENTED. REMOVED, REPAIRED AND INSTALLED PAX DOOR FWD END CAP, IAW REO.

Part: PANEL — FAILED · airframe 32,212 hrs · 27,461 cycles

RIGHT LOWER VISOR PANEL 326BR FAILED GAP CHECK. CONTOURED BY HAND THE AFFECTED VISOR PANEL 326BR. PART IS NOT BUCKLED OR CREASED IAW REO.

Part: SKIN — DENTED (BS 559) · airframe 32,212 hrs · 27,461 cycles

LEFT FUSELAGE DENT AT BS 559+50, APPROXIMATELY FOUR INCHES BELOW STRINGER 15L. C-CHECK, COMPLIED WITH EA.

Part: VANE CAP — CHAFED (RT WING TE FLAP) · airframe 32,212 hrs · 27,461 cycles

RT INBD FLAP VANE SKIN MOST OTBD CAP CHAFED. BLENDED THE RT, INBD FLAP VANE SKIN MOST OTBD CAP IAW REO.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 32,212 hrs · 27,461 cycles

PAX DOOR AFT DRAG ANGLE CRACKED BY POWER ASSIST PULLEY BRACKET. R & R CRACKED PAX DOOR AFT DRAG ANGLE IAW SRM.

Part: BULKHEAD — CRACKED (BS 621) · airframe 31,684 hrs · 26,913 cycles

WHILE PERFORMING EDDY CURRENT NDT INSPECTION OF THE BS 621 AFT PRESSURE BULKHEAD, FOUND CRACK INDICATION AT THE FOLLOWING LOCATION: .5" LEFT, FWD-LOOKING-AFT, OF RBL 9.50, 24-.6250" UP FROM WL 73.50 AND 22.5" DOWN FROM WL 120.43. INDICATION RUNS VERTICAL APPROXIMATELY .5" IN LENGTH. C-CHECK, REPAIRED BULKHEAD IAW REO.

Part: WARNING MESSAGE — ILLUMINATED (MLG) · airframe 31,382 hrs · 26,613 cycles

RETURNED TO FIELD WITH RT MAIN GEAR DISAGREE WARNING AFTER TAKEOFF WHEN GEAR WAS RETRACTED.

Part: SEQUENCE VALVE — FAILED (MLG) · airframe 31,382 hrs · 26,614 cycles

RETURNED TO FIELD WITH RT MAIN GEAR DISAGREE WARNING AFTER TAKEOFF, WHEN GEAR RETRACTED. R & R MLG SELECTOR VALVE AND ADJUSTED RT LANDING GEAR PROXIMITY SENSOR IAW AMM, PN ON 750005000, SN ON 0057T; PN OFF 750005000, SN OFF 1030.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,233 hrs · 26,471 cycles

AFT CEILING EMERGENCY FLOOD LIGHT INOPERATIVE.

Part: SELECTOR VALVE — FAILED (NLG) · airframe 30,411 hrs · 25,662 cycles

GEAR DISAGREE MESSAGE. FLT 2612 REPLACED NLG SELECTOR VLV IAW AMM, PN 750006000, SN ON 1640 & SN OFF 1592.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,641 hrs · 24,875 cycles

AFT CABIN CEILING LEVEL EMERGENCY LIGHT IS BURNED OUT. FLT#2638 RELAMPED.

Part: TRUNNION — CRACKED (LANDING GEAR) · airframe 27,450 hrs · 22,511 cycles

ONE HOLE, SEVENTH FROM AFT, LEFT SIDE TRUNNION WAS FOUND TO BE CRACKED. (C-CHECK) REPAIRED ONE HOLE, SEVENTH FROM AFT ON LEFT TRUNNION PLANK IAW REO.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 27,450 hrs · 22,511 cycles

FS 621 BULKHEAD CRACKED. (C-CHECK) REPAIRED FS 621 BULKHEAD IAW REO.

Part: BUSHING — CORRODED (ENGINE MOUNT) · airframe 27,449 hrs · 22,510 cycles

THE RIGHT ENGINE FORWARD YOKE MOUNT HAS PITTING ON THE UPPER BUSHINGS. (ENGINE CHANGE) REPLACED THE RIGHT ENGINE FORWARD YOKE MOUNT.

Part: BOLT — GALLED (ENGINE MOUNT) · airframe 27,449 hrs · 22,510 cycles

THE RIGHT ENGINE FORWARD YOKE PIN BOLTS HAVE GALLING. (ENGINE CHANGE) REPLACED A NEW UPPER AND LOWER PIN BOLT ON THE RIGHT ENGINE.

Part: BUSHING — CORRODED (ENGINE MOUNT) · airframe 27,449 hrs · 22,510 cycles

THE RIGHT ENGINE FORWARD YOKE MOUNT UPPER LINK HAS PITTING ON THE BUSHINGS. (ENGINE CHANGE) REPLACED THE RIGHT ENGINE FORWARD YOKE MOUNT UPPER LINK ASSEMBLY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,236 hrs · 22,298 cycles

NR 4 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4488) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,074 hrs · 22,144 cycles

NR 1 AND NR 3 OVERHEAD EMERGENCY LIGHTS ARE OUT. (FLT 4494) RELAMPED EMERGENCY LIGHTS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,893 hrs · 21,960 cycles

NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4629) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,880 hrs · 21,948 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4659) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,559 hrs · 21,644 cycles

NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (SERVICE) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,171 hrs · 21,269 cycles

NR 3 AND 5 LEFT OVERWING EMERGENCY LIGHTS ARE OUT. (FLT 4734) RELAMPED EMERGENCY LIGHTS.

Part: CHARGER — FAILED (CABIN) · airframe 26,136 hrs · 21,235 cycles

NR 2 AND NR 5 OVERHEAD EMERGENCY LIGHTS ARE OUT. (FLT 4765) REPLACED THE NR 4 EMERGENCY BATTERY CHARGER ASSEMBLY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,031 hrs · 21,130 cycles

NR 2 CEILING EMERGENCY LIGHT IS OUT. (FLT 4562) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,870 hrs · 20,966 cycles

AFT OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4687) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,609 hrs · 20,726 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4670) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,486 hrs · 20,610 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4736) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,402 hrs · 20,528 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4702) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 25,355 hrs · 20,478 cycles

LEFT EXTERIOR OVERWING FORWARD EMERGENCY LIGHT IS OUT. (FLT 4750) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,355 hrs · 20,478 cycles

NR 1 AND NR 3 OVERHEAD EMERGENCY LIGHTS ARE OUT. (FLT 4473) RELAMPED EMERGENCY LIGHTS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,285 hrs · 20,414 cycles

NR 1 AND NR 2 OVERHEAD EMERGENCY LIGHTS ARE OUT. (FLT 7779) RELAMPED EMERGENCY LIGHTS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,210 hrs · 20,346 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4579) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,133 hrs · 20,276 cycles

RIGHT REAR OVERWING EMERGENCY LIGHT IS OUT. (FLT 4639) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 25,028 hrs · 20,179 cycles

LEFT 2 AFT EXTERNAL EMERGENCY LIGHTS ARE OUT. (SERVICE).

Part: LANDING GEAR — MALFUNCTIONED (RIGHT) · airframe 24,969 hrs · 20,132 cycles

FLT 4443, RIGHT MAIN LANDING GEAR DID NOT EXTEND DURING LANDING. REMOVED AND REPLACED RT MAIN LANDING GEAR.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,893 hrs · 20,067 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (SERVICE) RELAMPED EMERGENCY LIGHT.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 24,339 hrs · 19,600 cycles

FS 280 FLOORBEAM LOWER FLANGE CRACKED ON RIGHT SIDE. (C-CHECK) REPAIR PER REO. REPLACED PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 24,339 hrs · 19,600 cycles

RIGHT SIDE FS 559 BULKHEAD CRACKED. (C-CHECK) REPAIR PER REO.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 24,577 hrs · 19,794 cycles

FS 202 BULKHEAD CRACKED AT PARKING BRAKE CABLE HOLE. (C-CHECK) REPAIRED PER REO.

Part: CHARGER — FAILED (CABIN) · airframe 23,501 hrs · 18,891 cycles

EMERGENCY LIGHT OVERHEAD SECOND FROM BACK DOES NOT WORK. (FLT 4847)REPLACED #3 ELBP CHARGER ASSEMBLY,

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,523 hrs · 18,032 cycles

TWO CEILING EMERGENCY FLOOD LIGHTS INOP. (FLT 4826) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,402 hrs · 17,937 cycles

EMERGENCY LIGHT OVER ROW 6 INOP. (FLT 4709) RELAMPED EMERGENCY LIGHT.

Part: SEALANT — OUT OF POSITION (TE FLAP) · airframe 21,794 hrs · 17,429 cycles

UNCOMMANDED ROLL WHEN FLAPS DEPLOYED TO 45 DEGREES. (FLT 4773) REMOVED PROTRUDING PAINT AND SEALANT ON RIGHT OUTBOARD LEADING EDGE FLAP VANE.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 21,181 hrs · 16,958 cycles

EN ROUTE AT FL350 NOTICED WINDSHIELD SPARKING. TURNED OFF WINDSHIELD HEAT, A COUPLE OF SECONDS LATER OUTER PLY OF WINDSHIELD SHATTERED. RAN QRH AND LANDED NORMALLY AT CVG. (FLT 4520) REMOVED AND REPLACED LT WINDSHIELD IAW AMM 56-11-01. S/N OFF: 01051H1362.

Part: SIGN — MALFUNCTIONED (CABIN) · airframe 21,155 hrs · 16,930 cycles

NR 3 EMERGENCY CEILING LIGHT AFT THE EXIT SIGN INOP. (FLT 4530) OPERATIONAL CHECK NORMAL.

Part: PIN — FAILED (LG UPLOCK) · airframe 21,092 hrs · 16,864 cycles

GEAR DISAGREE MESSAGE DISPLAYED. (FLT 4685) REPLACED UPLOCK PIN.

Part: SELECTOR VALVE — FAILED (MLG) · airframe 20,857 hrs · 16,677 cycles

GEAR DISAGREE MESSAGE DISPLAYED. (FLT 4758) REPLACED MLG SELECTOR AND PRIORITY VALVES.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,770 hrs · 16,608 cycles

LEFT AFT WING EMERGENCY LIGHT INOP. (SVC CHECK) RELAMPED EMERGENCY LIGHT.

Part: SEQUENCE VALVE — FAILED (NLG) · airframe 20,690 hrs · 16,542 cycles

NOSE GEAR DISAGREE MESSAGE. (FLT 4867) REPLACED NLG PRIORITY VALVE.

Part: ACTUATOR — FAILED (NLG) · airframe 20,529 hrs · 16,416 cycles

NOSE WHEEL DID NOT EXTEND. (FLT 4469)REPLACED NLG EXTEND/RETRACT ACTUATOR.

Part: SELECTOR VALVE — FAILED (NLG) · airframe 20,492 hrs · 16,386 cycles

NOSE GEAR DISAGREE MESSAGE DISPLAYED. (FLT 4368) REPLACED NOSE GEAR SELECTOR VALVE ASSEMBLY.

Part: BRACKET — CRACKED (CARGO DOOR) · airframe 20,201 hrs · 16,166 cycles

C-CHECK, CRACKED BRACKET AT CARGO DOOR SUPPORT BEAM ON FS 621 BULKHEAD. REPLACED PER SRM.

Part: FITTING — CRACKED (BS 621) · airframe 20,201 hrs · 16,166 cycles

C-CHECK, FS 621 BULKHEAD LINTEL FITTING CRACKED. REPAIRED PER REO.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 20,201 hrs · 16,166 cycles

C-CHECK, SERVICE DOOR THRESHOLD CORRODED. REPLACED THRESHOLD PER AMM.

Part: MOUNT — CRACKED (DOOR ASSIST) · airframe 20,201 hrs · 16,166 cycles

C-CHECK, PASSENGER DOOR ASSIST MOTOR MOUNT CRACKED. REPLACED PER SRM.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 19,573 hrs · 15,687 cycles

FLT 4852 - CABIN EMERGENCY CEILING LEVEL FLOOD LIGHT INOP. RELAMPED.

Part: LIGHT — BROKEN (EMERGENCY EXIT) · airframe 18,078 hrs · 14,523 cycles

FLT 3951 - MAIN CABIN EMERGENCY EXIT SIGN IS BROKEN. REPLACED MAIN CABIN EMERGENCY EXIT LIGHT ASSEMBLY.

Part: RELAY — FAULTY (THRUST REVERSER) · airframe 17,539 hrs · 14,107 cycles

FLT 3936 - LEFT REVERSER UNLOCKED CAUTION MESSAGE DURING CLIMB OUT. INSPECTED THRUST REVERSER RIGGING AND REPLACED RELAY 1K1KE AND 1K2KE. OPS CHECK GOOD.

Part: SWITCH — MALFUNCTIONED (THRUST REVERSER) · airframe 17,539 hrs · 14,107 cycles

FLT 3927 - AFTER TAKEOFF, RECEIVED A LEFT REVERSER UNLOCKED CAUTION MESSAGE. INSPECTED AND CHECKED GAP AND RIG OF STOW SWITCH IAW 78-32-01. OPS CHECK GOOD.

Part: SWITCH — FAULTY (THRUST REVERSER) · airframe 17,461 hrs · 14,050 cycles

RECEIVED A "LEFT THRUST REVERSER UNLOCK" CAUTION MESSAGE AFTER TAKEOFF, FLIGHT NR 3843. REPLACED THROTTLE LOCKOUT MICROSWITCH IAW AMM 78-37-01. OPS CHECK GOOD.

Part: SELECTOR VALVE — MALFUNCTIONED (MLG) · airframe 17,160 hrs · 13,815 cycles

FLT 3904 - GEAR DISAGREE WARNING ON APPROACH AND NOSE GEAR WAS NOT DOWN. REPLACED NOSE GEAR SELECTOR VALVE IAW AMM 32-33-10. REPLACED PRIORITY VALVE IAW AMM 32-33-15.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 15,598 hrs · 12,639 cycles

AFT FLOOR TRACK LIGHTING IS INOP. REPLACED EMERGENCY BATTERY PACK NR 4 IAW AMM 33-51-07.

Part: PUMP — FAILED (HYD SYSTEM) · airframe 15,350 hrs · 12,451 cycles

AFTER LANDING, HYDRAULIC PUMP 2B CAUTION MESSAGE APPEARED, FOLLOWED BY HYD 2 LO PRESS MESSAGE. NR 2 HYDRAULIC QUANTITY SHOWS 0 PERCENT. REPLACED NR 2 AC MOTOR PUMP IAW MM 29-11-03.

Part: STRINGER CLIP — CRACKED (BS 625 S14R) · airframe 15,275 hrs · 12,397 cycles

FS 625 BULKHEAD STRINGER 14 HAS CRACKED CLIP ON RIGHT AND LEFT SIDE, DISCOVERED AT C-CHECK INSPECTION. REPLACED FS 625 BULKHEAD CLIPS P/N 601-35012-51 AND P/N 601-35012-52 IAW CRJ200 SRM 51-40-11 AND CRJ200 SRM 51-42-21.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 15,275 hrs · 12,397 cycles

CORROSION EXISTS UNDER PAX DOOR THRESHOLD TOP FOLDING STEP ATTACH INTERCOSTAL, DISCOVERED AT C-CHECK INSPECTION. INSTALLED NEW INTERCOSTAL AND TOP CAP ANGLE AT PAX DOOR THRESHOLD PER CRJ200 SRM 51-42-06 PG 1-18 AND CRJ200 SRM 51-42-21 PG 1-9.

Part: BRACKET — CRACKED (LT MLG WW) · airframe 15,275 hrs · 12,397 cycles

LEFT WHEEL WELL TRANSDUCER BRACKET IS CRACKED, DISCOVERED AT C-CHECK INSPECTION. INSTALLED NEW TRANSDUCER BRACKET P/N 601R-75262-159 PER CRJ200 SRM 51-42-06.

Part: BOLT — CORRODED (LT ELEVATOR) · airframe 15,275 hrs · 12,397 cycles

LEFT ELEVATOR TRANSMITTER ARM HAS CORRODED BOLT AND NUT, DISCOVERED AT C-CHECK INSPECTION. REPLACED BOLT AND NUT ON LEFT ELEVATOR TRANSMITTER ARM IAW CRJ200 AMM 20-24-00-910-801.

Part: SEAT BACK — CRACKED (COCKPIT) · airframe 15,275 hrs · 12,397 cycles

CO-PILOTS SEAT BACK SUPPORTS CRACKED, DISCOVERED AT C-CHECK INSPECTION. INSTALLED NEW SEAT BACK SUPPORTS P/N1C3076-2AJT AND P/N1C3076-1AJT PER CRJ200 SRM 51-42-10.

Part: ANGLE — CRACKED (PAX DOOR) · airframe 15,275 hrs · 12,397 cycles

PAX DOOR AFT UPPER CORNER HAS CRACKED INTERIOR ANGLE, DISCOVERED AT C-CHECK. INSTALLED INTERIOR ANGLE P/N 601R31-8094-2 AT PAX DOOR UPPER CORNER PER CRJ200 SRM 51-42-06. RII 52-900-1001.

Part: YOKE — CORRODED (LT ENGINE) · airframe 15,275 hrs · 12,397 cycles

LEFT ENGINE FORWARD MOUNT YOKE UPPER AND LOWER BEARINGS HAVE EVIDENCE OF PITTING CORROSION. LOWER BEARING IS FROZEN, DISCOVERED AT C-CHECK INSPECTION. REPLACED LEFT ENGINE FORWARD MOUNT YOKE P/N 601-37015-7.

Part: AIRSTAIR — CRACKED (PAX DOOR) · airframe 15,275 hrs · 12,397 cycles

PAX DOOR STAIR CASE IS CRACKED FORWARD OF STEP 5, DISCOVERED AT C-CHECK INSPECTION. REPLACED PAX DOOR REPAIR PARTS PER CRJ200 REO 601R 52-11-702 REV 'A'.

Part: SEAT BACK — CRACKED (COCKPIT) · airframe 15,275 hrs · 12,397 cycles

PILOTS SEAT BACK SUPPORTS ARE CRACKED, DISCOVERED AT C-CHECK INSPECTION. INSTALLED NEW SUPPORT P/N1C3076-1AJT AND P/N1C3076-2AJT PER CRJ200 SRM 51-42-10.

Part: BRACKET — CRACKED (RT MLG WW) · airframe 15,275 hrs · 12,397 cycles

RIGHT WHEEL WELL TRANDUCER BRACKET IS CRACKED, DISCOVERED AT C-CHECK INSPECTION. INSTALLED NEW TRANSDUCER BRACKET P/N 601R-75262-157 PER CRJ200 SRM 51-42-06.

Part: AIRSTAIR — CRACKED (PAX DOOR) · airframe 15,275 hrs · 12,397 cycles

PAX DOOR STAIR CASE IS CRACKED AFT OF STEP NR 3, DISCOVERED AT C-CHECK INSPECTION. INSTALLED REPAIR PARTS PER CRJ200 REO 601R 52-11-702 REV 'A' ZONE 2 REPAIR.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 14,636 hrs · 11,909 cycles

FORWARD OVERHEAD EMERGENCY LIGHT INOP. RELAMPED EMERGENCY LIGHT. OPERATIONAL CHECKS GOOD.

Part: CONNECTOR — SHORTED (EMERGENCY LIGHT) · airframe 14,196 hrs · 11,584 cycles

LT LOWER EMERGENCY EXIT ROW LIGHT AND ASSOCIATED FLOOR STRIP LIGHT OUT. FOUND MOISTURE IN LIGHT STRIP. DRIED AND APPLIED SEALER TO CONNECTORS. OPS CHECKS GOOD IAW MM 33-51-00.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 13,616 hrs · 11,136 cycles

AFT OVERHEAD EMERGENCY LIGHT IS INOP. RELAMPED AFT OVERHEAD EMERGENCY LIGHT. OPERATIONAL CHECKS GOOD.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 12,682 hrs · 10,425 cycles

CEILING LEVEL EMERGENCY FLOOR LIGHT INOP. RELAMPED 3RD AFT CEILING EMERGENCY LIGHT. OPERATIONAL CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 12,306 hrs · 10,155 cycles

EMERGENCY FLOOD LIGHT AT ROW 10 INOP. REPLACED ROW 10 EMERGENCY FLOOR LIGHT IAW 33-51-16. OPERATIONAL CHECK GOOD.

Part: LIGHT — INOPERATIVE (EXTERIOR)

DURING AN A-CHECK IN BTR, THE AFT EXTERIOR EMERGENCY LIGHT ON THE LEFT SIDE WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE AFT EXTERIOR EMERGENCY LIGHT ON THE LEFT SIDE. OPERATIONAL CHECKS GOOD. (M)

Part: HINGE — CORRODED (PAX DOOR)

FLT 4398 - DURING A GROUND INSPECTION IN SHV, THE TOP STEP HINGE ON THE PASSENGER DOOR WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE TOP STEP HINGE ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: STEP — CRACKED (PAX DOOR)

DURING HANGAR MAINTENANCE, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE.

Part: CLIP — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE CLIP AT FS 484, LBL APPROXIMATELY 28 AND 36 WAS FOUND CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE CLIP AT FS 484, LBL APPROXIMATELY 28 AND 36 AND ALSO REMOVED AND REPLACED THE INTERCOSTAL AT FS 484 ON THE LEFT SIDE AT BL 27 AND 36 IAW ASA EO 600-53-0098. (M)

Part: CLIP — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE CLIPS AT FS 484, RBL APPROXIMATELY 28 AND 36 WERE FOUND CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE CLIPS AT FS 484, RBL APPROXIMATELY 28 AND 36 AND AT FS 484, BL 27 IAW ASA EO 600-53-0098. (M)

Part: CLIP — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE CLIP AT FS 280, RBL 9 OUTBOARD WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE CLIP AT FS 280, RBL 9 OUTBOARD IAW SRM 51-40-00. (M)

Part: CLIP — CRACKED

DURING A C-CHECK IN MCN, THE CLIPS AT FS 280, RBL 9 AND LBL 9 INBOARD WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE CLIPS AT FS 280, RBL 9 AND LBL 9 INBOARD IAW SRM 51-40-00. (M)

Part: CLIP — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE CLIPS AT THE AFT EQUIPMENT BAY BELOW THE ENGINE BEAM ON THE LEFT AND RIGHT SIDES WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE CLIPS AT THE AFT EQUIPMENT BAY BELOW THE ENGINE BEAM ON THE LEFT AND RIGHT SIDES IAW SRM 53-42-02. (M)

Part: FLOOR SUPPORT — CRACKED (FUSELAGE)

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

Part: STEP — CRACKED (PAX DOOR)

DURINGA C-CHECK IN MCN, THE PASSENGER DOOR BOTTOM STEP WAS FOUND CRACKED. MAINTENANCE IS REMOVING AND REPLACING THE PASSENGER DOOR BOTTOM STEP. (M)

Part: LIGHT — INOPERATIVE (LT OVERWING)

DURING A C-CHECK IN MCN, THE LEFT OVERWING MIDDLE EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE CLEANED THE LEFT OVERWING MIDDLE EMERGENCY LIGHT LAMP SOCKET. OPS CHECKS GOOD. (M)

Part: PUMP — CLOGGED (RT ENGINE)

FLT 4553 - DURING CRUISE FROM DTW-DFW, AT APPROXIMATELY 31,000 FEET THE CREW RECEIVED A RIGHT ENGINE LOW OIL PRESSURE WARNING MESSAGE. THE OIL PRESSURE FLUCTUATED BETWEEN 25-33 PSI OCCASIONALLY DROPPING BELOW 25 PSI AND THEN SLOWLY DECREASING. OIL TEMPERATURE WAS SLIGHTLY ELEVATED ON THE RIGHT ENGINE TO AROUND 135 DEGREES. QRH PROCEDURES WERE COMPLIED WITH AND THE CREW SHUT DOWN THE RIGHT ENGINE. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT DIVERTED INTO CVG, LANDING SAFELY. MAINTENANCE REMOVED AND REPLACED THE LUBE AND SCAVENGER PUMP ON THE RIGHT ENGINE. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT)

FLT 4469 - DURING A GROUND INSPECTION IN ATL, THE EMERGENCY LIGHT OVER THE RIGHT WING WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT LAMP OVER THE RIGHT WING. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: LIGHT — INOPERATIVE (EXTERIOR)

DURING GROUND INSPECTION IN DFW, THE FORWARD MOST EXTERNAL EMERGENCY LIGHT ON THE RIGHT SIDE OF THE FUSELAGE WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BURNED OUT EXTERNAL EMERGENCY LIGHT BULB. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: LIGHT — INOPERATIVE (CABIN)

FLT 4669 - DURING GROUND INSPECTION IN ATL, THE LEFT MIDDLE OVERWING EMERGENCY EXIT LIGHT WAS FOUND BURNED OUT. MAINTENANCE REMOVED AND REPLACED THE LEFT MIDDLE OVERWING EMERGENCY LIGHT BULB. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)