N427SW

Part: SKIN — DAMAGED (RT AILERON LE) · airframe 40,179 hrs · 34,776 cycles

RIGHT AILERON ASSEMBLY €“ UPPER LEADING EDGE FOUND TO BE OUT OF LIMITS. (C-CHECK) RO: 12/11/2018 REMOVED AND REPLACED RH AILERON UPPER LEADING EDGE SKIN IAW SRM.

Part: DOOR SILL — CORRODED (BS 310-319) · airframe 40,179 hrs · 34,776 cycles

THE SERVICE DOOR FWD SILL FROM FS310.0 TO FS319.0 HAS CORROSION. (C-CHECK) RO: 12/11/2018 REMOVED AND REPLACED FLOOR SILL IAW SRM.

Part: ATTACH ANGLE — CORRODED (BS 605) · airframe 40,179 hrs · 34,776 cycles

FOUND CORRODED SPLICE ANGLE ATTACHED TO THE LH SIDE OF LOWER FRAME SPLICE @ FS.605. (C-CHECK) RO: 12/11/2018 REMOVED AND REPLACED SPLICE ANGLE AT FS 605.00 ON THE LH SIDE IAW SRM.

Part: ATTACH BRACKET — CORRODED (BS 319) · airframe 40,179 hrs · 34,776 cycles

THE FRAME TO FLOOR BEAM ATTACH BRACKET (€ŒT€? FITTING) AT FS 319.0 HAS CORROSION. (C-CHECK) RO: 12/11/2018 REMOVED AND REPLACED FRAME TO FLOOR BEAM ATTACH BRACKET (€ŒT€? FITTING) AT FS 319.0 IAW SRM.

Part: DRAIN — CORRODED (THRESHOLD) · airframe 40,179 hrs · 34,776 cycles

CORROSION ON THE FORWARD PASSENGER DOOR LOWER SILL DRAIN TUBE SUPPORT BRACKET. LOCATED ON THE LOWER SIDE OF THE DOOR SILL. FS312.00 (C-CHECK) RO: 12/11/2018 REMOVED AND REPLACED DRAIN TUBE BRACKET IAW SRM.

Part: PRESSURE DECK — CORRODED (BS 445-559) · airframe 40,179 hrs · 34,776 cycles

RIGHT HAND UPPER SURFACE OF PRESSURE FLOOR SILL HAS CORROSION MARKED FROM FS 445.0 TO 559.0. (C-CHECK) RO: 12/11/2018 BLENDED 11 EA LOCATIONS ON RIGHT HAND UPPER SURFACE OF PRESSURE FLOOR SILL FROM FS 445.0 TO 559.0. COMPLIED WITH ALL STEPS OF THE REPAIRS IAW REO AND SRM.

Part: PRESSURE DECK — CORRODED (BS 445-559) · airframe 40,179 hrs · 34,776 cycles

LEFT HAND UPPER SURFACE OF PRESSURE FLOOR SILL HAS CORROSION MARKED FROM FS 445.0 TO 559.0. (C-CHECK) RO: 12/11/2018 BLENDED THE LEFT HAND UPPER SURFACE OF PRESSURE FLOOR SILL FROM FS 445.0 TO 559.0. COMPLIED WITH ALL STEPS OF THE REPAIRS IAW REO AND SRM.

Part: FLOOR SUPPORT — CORRODED (BS 559) · airframe 40,179 hrs · 34,776 cycles

RIGHT SIDE SILL BETWEEN FS559-FS559+80 HAS SEVERAL SPOTS OF CORROSION. (C-CHECK) RO: 12/11/2018 REPLACED 2EA SECTIONS OF RH FLOOR SILL FROM FS559 TO FS559+80 IAW REO AND SRM.

Part: VANE — CHAFED (LT WING TE FLAP) · airframe 40,179 hrs · 34,776 cycles

REPLACE LH INBOARD FLAP VANE L/E SKIN, CENTER LOCATION DUE TO OUT OF LIMITS CHAFE DAMAGE. (C-CHECK) RO: 12/11/2018 REMOVED AND REPLACED LH INBOARD FLAP VANE L/E SKIN, CENTER LOCATION IAW SRM.

Part: HINGE — CORRODED (LAV SERVICE DOOR) · airframe 40,179 hrs · 34,776 cycles

LAVATORY SERVICE DOOR ( 196AR ) UPPER AND LOWER HINGES CORRODED. (C-CHECK) RO: 12/11/2018 REPLACED THE AFT LAVATORY SERVICE DOOR WITH NEW UPPER AND LOWER HINGES IAW SRM.

Part: VANE — CHAFED (LT WING TE FLAP) · airframe 40,179 hrs · 34,776 cycles

REPLACE LH INBOARD FLAP VANE L/E SKIN, OUTBOARD LOCATION DUE TO OUT OF LIMITS CHAFE DAMAGE. (C-CHECK) RO: 12/11/2018 REMOVED AND REPLACED LH INBOARD FLAP VANE L/E SKIN, OUTBOARD LOCATION IAW SRM.

Part: FRAME — CORRODED (BS 394) · airframe 40,179 hrs · 34,776 cycles

FS 394.0 AVIONICS BAY AFT FRAME HAS CORROSION. (C-CHECK) RO: 12/11/2018 REMOVED CORROSION FROM LOWER FRAME AT FS394.0 IAW SRM. PRESSURE CHECKS GOOD.

Part: INTERCOSTAL — CORRODED (BS 349-364) · airframe 40,179 hrs · 34,776 cycles

AVIONICS BETWEEN FS 349.0 TO FS 364.0 HAS CORROSION AT INTERCOSTAL ON STR 26 R. (C-CHECK) RO: 12/11/2018 REPLACED INTERCOSTAL AT FS349 TO FS364 NEAR STR26R IAW SRM. PRESSURIZATION LEAK CHECK GOOD.

Part: INTERCOSTAL — CORRODED (BS 349-364) · airframe 40,179 hrs · 34,776 cycles

AVIONICS BAY IN BETWEEN FS 364 AND FS 349.0 AT STR 26L INTERCOSTAL HAS CORROSION. (C-CHECK) RO: 12/11/2018 INSTALLED NEW SERVICABLE L/H LATCH PIN INTERCOSTAL BETWEEN FS349.00-FS364.00 AND BETWEEN STGE 26L TO STGR 27 IAW SRM, LEAK CHECK GOOD.

Part: SKIN — SCRATCHED (AFT CARGO DOOR) · airframe 40,179 hrs · 34,776 cycles

ABOVE AFT CARGO DOOR A/C OUTER SKIN THERE IS DEEP SCRATCHES. (C-CHECK) RO: 12/11/2018 REMOVED CARGO DOOR A/C OUTER SKIN SCRATCHES IAW SRM. NO DEFECTS NOTED.

Part: FRAME — CORRODED (BS 349) · airframe 40,179 hrs · 34,776 cycles

AVIONICS BAY LOWER FRAME AT FS 349.0 HAS CORROSION. (C-CHECK) RO: 12/11/2018 REMOVED AND REPLACED 349 FRAME IAW SRM. ALL CHECKS OKAY.

Part: THRESHOLD — CORRODED (SERVICE DOOR) · airframe 40,179 hrs · 34,776 cycles

SERVICE DOOR THRESHOLD CORRODED. (C-CHECK) RO: 12/11/2018 INSTALLED NEW SERVICE DOOR STEP PLATE P/N 601R38957-31 IAW REO.

Part: FITTING — GOUGED (LT OVERWING DOOR) · airframe 40,179 hrs · 34,776 cycles

LH OVERWING EMERGENCY DOOR FITTINGS GOUGED 2EA. (C-CHECK) RO: 12/11/2018 REMOVED DAMAGE FROM THE LH EMERGENCY DOOR FITTINGS 2EA. IAW REO.

Part: FITTING — GOUGED (RT OVERWING DOOR) · airframe 40,179 hrs · 34,776 cycles

RH OVERWING EMERGENCY DOOR FITTINGS GOUGED 2EA. (C-CHECK) RO: 12/11/2018 REMOVED DAMAGE FROM THE RH EMERGENCY DOOR FITTINGS 2EA. IAW REO.

Part: STRINGER — DENTED (BS 589) · airframe 40,179 hrs · 34,776 cycles

DENT FOUND BETWEEN STR 21L AND 22L, 1 1/8" ABOVE 22L, 5.5" FORWARD OF FS 589.00. (C-CHECK) RO: 12/11/2018 COMPLIED WITH PERMANENT REPAIR OF DENT FOUND AT FS 589.00 AND ADDITIONAL DENT FOUND AT FS 580.00 IAW REO.

Part: FLAP — FAILED (WING) · airframe 38,336 hrs · 32,760 cycles

FLAP FAIL. EMERGENCY DECLARED. (FLT 4871). CLOSED. RESET IAW FIM.

Part: SKIN — CHAFED (RT AILERON) · airframe 36,652 hrs · 30,907 cycles

RIGHT AILERON PANEL 699BB IS CHAFED. INSTALLED A NEW PANEL IAW SRM.

Part: BRACKET — CORRODED (PAX DOOR) · airframe 36,652 hrs · 30,907 cycles

PAX DOOR LOWER SILL BRACKET CONNECTORS HAVE CORROSION. REMOVED AND REPLACED 2 EACH PAX DOOR LOWER SILL BRACKETS CONNECTORS IAW SRM.

Part: VISOR — FAILED · airframe 32,913 hrs · 26,995 cycles

VISOR PANEL 326AR FAILED GAP CHECK, C-CHECK, RECOUNTERED VISOR PANEL 326AR REF REO. GAP CHECKS GOOD.

Part: STEP — CRACKED (PAX DOOR) · airframe 32,913 hrs · 26,995 cycles

CRACK ON PAX DOOR FWD SIDE PANEL BOTTOM STEP. REPAIRED PAX DOOR BOTTOM STEP, PERFORMED NDT, NO DEFECTS NOTED. FABRICATED AND INSTALLED REPAIR AND RESTORED FINISH IAW EA.

Part: FRAME — CORRODED (BS 333) · airframe 32,913 hrs · 26,995 cycles

CORROSION FOUND BS 333 FRAME LOWER FLANGE BETWEEN S25L - 26R. REMOVED CORROSION AND FOUND TO BE WITHIN LIMITS AND RESTORED FINISH IAW EA.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 32,913 hrs · 26,995 cycles

FS 280 FLOORBEAM IS CRACKED LBL 11. THE FLOORBEAM REPAIRED IAW REO.

Part: FLOORBEAM — CORRODED (BS 353) · airframe 32,913 hrs · 26,995 cycles

CORROSION ON FLOORBEAM BS 353, RBL 44. BLENDED CORROSION AND FOUND TO BE IN LIMITS IAW REO.

Part: STRUCTURE — DAMAGED (BS 559) · airframe 32,913 hrs · 26,995 cycles

UPON REMOVAL OF FASTENERS FOR CORROSION REMOVAL FOUND ONE HOLE ELONGATED LOCATED ON LOWER AFT FUSELAGE, BS 559.47, RIGHT OF STR 27. REPAIRED.

Part: TRUNNION — CRACKED (RT MLG) · airframe 32,913 hrs · 26,995 cycles

RT MLG TRUNNION WAS FOUND CRACKED. REPAIRED THE TRUNNION IAW REO.

Part: TRUNNION — CRACKED (LT MLG) · airframe 32,913 hrs · 26,995 cycles

LT TRUNNION WAS FOUND CRACKED. REPAIRED THE LT TRUNNION IAW REO.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 32,913 hrs · 26,995 cycles

FLOORBEAM ANGLE AT BS 280, RBL 11 IS CRACKED. R & R THE FLOORBEAM ANGLE.

Part: FLOOR SUPPORT — CORRODED (BS 409) · airframe 32,913 hrs · 26,995 cycles

FLOOR SUPPORT HAS CORROSION AT BS 409.126 RBL 44. REMOVED CORROSION AND FOUND WITHIN LIMITS.

Part: FLOOR SUPPORT — CORRODED (BS 409) · airframe 32,913 hrs · 26,995 cycles

FLOOR SUPPORT HAS CORROSION AT FS 409.44 APPROXIMATELY, LBL 44. FLOOR SUPPORT REPAIRED IAW REO.

Part: FLOOR SUPPORT — CORRODED (BS 353) · airframe 32,913 hrs · 26,995 cycles

CORROSION ON FLOOR SUPPORT BS 353 LBL 44. REMOVED CORROSION AND FOUND WITHIN LIMITS IAW REO.

Part: STRINGER — CORRODED (BS 326) · airframe 32,913 hrs · 26,995 cycles

STRINGER 26L HAS CORROSION ON FLANGE AT FS 326 APPROXIMATELY, C-CHECK, BLENDED CORROSION. FOUND TO BE OUT OF LIMITS. CUT AND REMOVED DAMAGED SECTION OF STRINGER 26L FROM FS 325-FS 340 AND INSTALLED NEW STRINGER SECTION IAW SRM. COMPLIED WITH ST CARD. MAJOR REPAIR REPORTED IAW M337.

Part: FLOOR SUPPORT — CORRODED (BS 319) · airframe 32,913 hrs · 26,995 cycles

FLOOR SUPPORT HAS CORROSION ON UPPER AND LOWER SURFACES AT NUTPLATE AT FS 319, RBL 44. REMOVED CORROSION IAW SRM AND FOUND TO BE WITHIN LIMITS IAW REO.

Part: FLOOR SUPPORT — CORRODED (BS 559) · airframe 32,913 hrs · 26,995 cycles

LT FLOOR SUPPORT IS CORRODED IN SEVERAL PLACES FROM BS 559 TO 559+16. FLOOR SUPPORT REPAIRED IAW REO, AND FOUND WITHIN LIMITS.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 32,913 hrs · 26,995 cycles

AFT RT FLOOR SUPPORT HAS CORROSION UNDER OTBD MATING SURFACE OF AFT RT CARGO FLOOR PANEL 282HRF. BLENDED CORROSION IAW REO.

Part: FLOOR SUPPORT — CORRODED (BS 409) · airframe 32,913 hrs · 26,995 cycles

FLOOR SUPPORT HAS CORROSION AT BS 409.87 LBL 44. REPAIRED IAW REO. UT INSPECTION REF NDTM. NO DEFECTS FOUND.

Part: FLOORBEAM — CRACKED (BS 409) · airframe 32,913 hrs · 26,995 cycles

FLOORBEAM CRACKED, BS 409+96, RBL 27. REPLACED THE CRACKED FLOORBEAM IAW SRM. PERMANENT REPAIR IAW EA.

Part: VANE — DAMAGED (LT WING TE FLAP) · airframe 32,913 hrs · 26,995 cycles

LT INBD FLAP VANE L/E SKIN, CENTER, WS 103 DAMGED. INSTALLED NEW FABRICATED CENTER CAP ONTO LT INBD FLAP VANE IAW SRM & EA.

Part: FLOOR SUPPORT — CORRODED (BS 445-559) · airframe 32,913 hrs · 26,995 cycles

LEFT UPPER SURFACE OF PRESSURE FLOOR SUPPORT FROM BS 445 TO 559 HAS CORROSION. BLENDED CORROSION IAW REO. ALL BLENDS WITHIN LIMITS.

Part: STRUCTURE — CHAFED (RT MLG DOOR) · airframe 32,913 hrs · 26,995 cycles

RT MLG DOOR AFT EDGE IS CHAFED. CHAFE BLENDED IAW SRM AND FOUND WITHIN LIMITS IAW SRM. REPAIRED IAW EA.

Part: STRUCTURE — CHAFED (LT MLG DOOR) · airframe 32,913 hrs · 26,995 cycles

LEFT MLG DOOR FWD EDGE CHAFED. BLENDED CHAFE IAW SRM AND FOUND TO BE WITHIN LIMITS. REPAIRED IAW REO.

Part: HINGE — CHAFED (PAX DOOR) · airframe 32,913 hrs · 26,995 cycles

PAX DOOR MOUNTED HINGE HALF HAS3 LUGS WITH CHAFED. BLENDED THE HINGE AND FOUND TO BE IN LIMITS IAW REO.

Part: HINGE — CHAFED (PAX DOOR) · airframe 32,913 hrs · 26,995 cycles

PAX DOOR FUSELAGE MOUNTED HINGE HAS FIVE LUGS WITH MINOR CHAFE. PAX DOOR HINGE REPAIRED IAW REO.

Part: FLOOR SUPPORT — CORRODED (BS 420-535) · airframe 32,913 hrs · 26,995 cycles

RIGHT UPPER SURFACE OF PRESSURE FLOOR SUPPORT FROM BS 420 - 535 HAS CORROSION. REPAIRED RT UPPER SURFACE OF PRESSURE FLOOR SUPPORT IAW REO. NO LEAKS NOTED.

Part: VANE — DAMAGED (RT WING TE FLAP) · airframe 32,913 hrs · 26,995 cycles

RT INBD FLAP VANE L/E SKIN, CENTER, WS 98.509 DAMAGED. INSTALLED NEW FABRICATED CENTER CAP ONTO RT INBD FLAP VANE, IAW SRM AND EA.

Part: SKIN — CORRODED (BS 559) · airframe 32,913 hrs · 26,995 cycles

EXTERNAL LOWER SKIN PANEL BS 559+48, STR 27 HAS CORROSION. FOUND TO BE WITHIN ALLOWABLE DAMAGE IAW EA,. BLENDED CORRODED AREA IAW SRM. NO LEAKS NOTED.

Part: SHROUD — CHAFED (LT AILERON) · airframe 32,913 hrs · 26,995 cycles

LEFT AILERON UPPER SHROUD CHAFED. BLENDED CHAFE ON LT AILERON UPPER SKIN SHROUD AND FOUND TO BE WITHIN LIMITS, IAW REO..

Part: RIB — GOUGED (BS 621) · airframe 32,913 hrs · 26,995 cycles

REAR PRESSURE BULKHEAD FORWARD FACE UPPER RIB BETWEEN DOOR TRACK AND FUSELAGE GOUGED. C-CHECK, RO 11/30/14, REPAIRED SUPPORT BRACKET, RIB, PN 601R36008-175 ON FS 621 BULKHEAD LT SIDE REF REO. ALL STEP COMPLIED WITH.

Part: CABLE — CRACKED (PARKING BRAKE) · airframe 32,913 hrs · 26,995 cycles

PARKING BRAKE CABLE HAS A CRACK AT 202 PRESSURE BULKHEAD, C-CHECK, RO 11/30/14, COMPLIED WITH CUT-AWAY DAMAGED AREA AND DOUBLER INSTALLED AT LT 202 PRESSURE BULKHEAD REF REO AND SR. NO LEAKS FOUND. COMPLIED WITH ST CARD.

Part: SKIN — CHAFED (RT WING) · airframe 32,913 hrs · 26,995 cycles

RIGHT SURFACE OF THE CENTER WING LOWER PLANK UNDER PANEL 193AB CHAFED. REPAIRED RIGHT SURFACE OF THE CENTER WING LOWER PLANK COMMON TO PANEL 193AB REF REO. ALL STEPS COMPLIED WITH.

Part: PRESSURE DECK — CRACKED (BS 460) · airframe 32,913 hrs · 26,995 cycles

PRESSURE FLOOR IS CRACKED AT BS 460 JUST INBD OF RBL 9. REPAIRED PRESSURE FLOOR CRACK AT FS460.0 JUST INBD RBL9.0 IAW REO, LEAK CHECK GOOD. COMPLIED WITH ST CARD.

Part: SKIN — CORRODED (BS 559) · airframe 32,913 hrs · 26,995 cycles

EXTERNAL LOWER SKIN PANEL AT BS 559+112, STR 27 HAS CORROSION. BLENDED CORROSION IAW SRM. FOUND TO BE WITHIN ALLOWABLE LIMITS IAW EA. RESTORED FINISH IAW SRM. NO LEAKS NOTED.

Part: BRACKET — CRACKED (BS 625 BULKHEAD) · airframe 32,913 hrs · 26,995 cycles

REAR PRESSURE BULKHEAD WEB AFT SIDE BS 625 HAS A LT SIDE BRACKET CRACKED. R & R CRACKED BRACKET IAW SRM AND REO.

Part: SKIN — CORRODED (BS 364-394) · airframe 32,913 hrs · 26,995 cycles

AVIONICS BAY DOOR SURROUND HAS CORROSION. BLENDED AVIONICS BAY DOOR SURROUND, BS 364 - 394 AND S25L - 25R, FOUND TO BE IN LIMITS IAW REO.

Part: BRACKET — CRACKED (BS 625 BULKHEAD) · airframe 32,913 hrs · 26,995 cycles

REAR PRESSURE BULKHEAD WEB AFT SIDE S 625 HAS A RT SIDE BRACKET CRACKED. R & R CRACKED BRACKET IAW SRM AND REO.

Part: SKIN — CHAFED (RT WING TE FLAP) · airframe 32,913 hrs · 26,995 cycles

VANE SKIN, RIGHT INBD FLAP HAS CHAFING AT L/E CLOSE TO WS 98.509, C-CHECK, RT INBD FLAP VANE SKIN AT WS 98.509 OUT OF LIMITS. INSTALLED NEW FABRICATED CENTER CAP ONTO RT INBD FLAP VANE, PN 601R14303-52, REF SRM AND STS EA.

Part: SKIN — CHAFED (RT AILERON) · airframe 32,913 hrs · 26,995 cycles

RT AILERON ACCESS PANEL 699BB HAS CHAFING. , BLENDED DAMAGE AND FOUND TO BE WITHIN LIMITS IAW REO. REPAIR COMPLETE IAW REO.

Part: SKIN — CHAFED (RT WING TE FLAP) · airframe 32,913 hrs · 26,995 cycles

RIGHT INBD FLAP HAS CHAFING FROM GROUND WIRE UNDER PANEL 684AB. BLENDED CHAFE ON RT INBD FLAP UNDER PANEL IAW REO. FOUND TO BE WITHIN LIMITS.

Part: SKIN — CHAFED (LT MLG DOOR) · airframe 32,913 hrs · 26,995 cycles

LEFT MAIN LANDING GEAR DOOR HAS CHAFING AT INBD SIDE SKIN. REPAIRED THE CHAFE ON INBD SIDE OF LT MLG DOOR, REPAIRED IAW EA.

Part: SKIN — CHAFED (RT WING TE FLAP) · airframe 32,913 hrs · 26,995 cycles

VANE SKIN, RT INBD FLAP HAS CHAFING AT L/E CLOSE TO WS 137.012. R & R NEW L/E INBD FLAP VANE IAW SRM, IAW REO.

Part: VANE — CHAFED (RT WING TE FLAP) · airframe 32,913 hrs · 26,995 cycles

VANE SKIN, RIGHT INBD FLAP HAS CHAFING AT L/E CLOSE TO WS 60.005, C-CHECK, BLENDED CHAFE ON THE INBD END OF THE RT INBD FLAP VANE L/E CLOSE TO WS60.005, REF REO. FOUND TO BE WITHIN LIMITS.

Part: SKIN — CHAFED (RT AILERON) · airframe 32,913 hrs · 26,995 cycles

RT AILERON UPPER SHROUD CHAFED. BLENDED DAMAGE TO RT AILERON UPPER SHROUD, FOUND TO BE WITHIN LIMITS IAW REO.

Part: SKIN — CHAFED (RT WING TE FLAP) · airframe 32,913 hrs · 26,995 cycles

RT INBD FLAP HAS CHAFING FROM GROUND WIRE UNDER PANEL NR 684CB, BLENDED CHAFE ON RT INBD FLAP UNDER PANEL 684CB, IAW REO. FOUND TO BE WITHIN LIMITS.

Part: SHUTOFF VALVE — FAILED (LT A/C PACK) · airframe 32,860 hrs · 26,948 cycles

DURING CLIMBOUT, RECEIVED A LT PACK HIGH PRESSURE INDICATION. PERFORMED QRH PROCEDURE. PACK WOULD STILL OVER PRESSURE. R & R THE LT PRSOV IAW AMM. OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,981 hrs · 24,052 cycles

EMERGENCY OVERHEAD LIGHT IS BURNED OUT. (FLT 4674) RELAMPED EMERGENCY LIGHT.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 29,799 hrs · 23,880 cycles

AFT CEILING EMERGENCY EXIT SIGN BY OVERWING EXIT AND OVERHEAD EMERGENCY EXIT LIGHT AFT OF EXIT SIGN DO NOT ILLUMINATE. (FLT 4754) REPLACED EMERGENCY BATTERY PACK NR 3 P/N: AD-2013-1A S/N ON: 76608 S/N OFF: 41230

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 29,587 hrs · 23,682 cycles

AFT SIDE OF THE OVERHEAD EMERGENCY SIGN AT ROW 8 DOES NOT ILLUMINATE. (SERVICE) RELAMPED EMERGENCY SIGN.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,566 hrs · 23,657 cycles

NR 3 EMERGENCY OVERHEAD LIGHT IS BURNED OUT. (FLT 4681) RELAMPED EMERGENCY LIGHT.

Part: CONTROLLER — FAULTY (ADG) · airframe 29,487 hrs · 23,582 cycles

ON ROTATION, ADG DEPLOYED. BOTH MAIN GENERATORS REMAINED ONLINE WITH NO POWER INTERRUPTION. TAXIED OUT WITH BOTH MAIN GENERATORS ON-LINE. (FLT 4765) REPLACED ADG AUTO-DEPLOY CONTROLLER IAW AMM AND STOWED ADG. P/N: 82046-5 S/N: 407 S/N OFF: 1193.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 29,411 hrs · 23,517 cycles

FLOOR SUPPORT AT FS 559.0+112 TO FS 621.0 AT LBL 27 HAS CORROSION AROUND NUT PLATES. (C-CHECK) REPLACED FLOOR SUPPORT AT FS 559.0+112 TO FS 621.0 AT LBL 27 IAW REO.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 29,411 hrs · 23,517 cycles

CRACK NOTED AND MARKED ON FS 621 AFT PRESSURE BULKHEAD WEB FWD FACE AT LBL 27.50 WL 131.0 ABOVE AFT CARGO DOOR AFT TRACK. (C-CHECK) INSTALLED FABRICATED REPAIR PARTS ON FS 621 BULKHEAD IAW REO.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 29,411 hrs · 23,517 cycles

CRACK NOTED AND MARKED ON FS 621 AFT PRESSURE BULKHEAD WEB FWD FACE AT LBL 46.99 WL 108.64 AT LINTEL FITTING. (C-CHECK) INSTALLED FABRICATED REPAIR PARTS IAW REO.

Part: POST — CRACKED (FUSELAGE) · airframe 29,411 hrs · 23,517 cycles

CRACKS NOTED AND MARKED IN RIGHT FS 409+128 VERT POST AT RBL 18 AND I/B C-CHANNEL IN AFT RADIUS. (C-CHECK) INSTALLED NEW VERTICAL POST AT FS 409 +128 RBL 18 IAW SRM AND REO.

Part: POST — CRACKED (FUSELAGE) · airframe 29,411 hrs · 23,517 cycles

CRACKS NOTED AND MARKED IN LEFT FS 409+128 VERT POST AT LBL 18 AND O/B C-CHANNEL IN AFT RADIUS. (C-CHECK) INSTALLED NEW VERTICAL POST AT FS 409 +128 LBL 18 IAW SRM AND IAW REO.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,411 hrs · 23,517 cycles

EMERGENCY LIGHTS IN OVERHEAD EXIT SIGN DO NOT ILLUMINATE. (FLT 4495) RELAMPED EMERGENCY LIGHTS.

Part: PIN — UNSECURE (PROXIMITY SENSOR) · airframe 29,375 hrs · 23,486 cycles

CLIMBING THOUGH 11,000 FT. OVBD COOL, INBD COOL FAIL CAUTION MSG, CABIN ALTERNATIVE WARNING MSG, COULD NOT PRESSURIZE. (FLT 4734) RE-SECURED PIN ON PASSENGER DOOR OUTER HANDLE PROXIMITY SWITCH.

Part: RELAY — FAILED (HYDRAULIC SYS) · airframe 29,341 hrs · 23,455 cycles

GEAR DOWN WOULDN'T GO DOWN AND LOCK UNTIL PUMP 3B PUT IN - ON - POSITION. (FLT 4791) REPLACED RELAY K10D8 IAW AMM P/N: M83726/28-5000P.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,174 hrs · 23,277 cycles

EMERGENCY LIGHT OVER ROW 5 IS BURNED OUT. (FLT 5373) RELAMPED EMERGENCY LIGHT.

Part: COVER — MISSING (CABIN) · airframe 28,916 hrs · 23,037 cycles

FLOOR LEVEL EMERGENCY LIGHT COVER BY BOARDING DOOR IS MISSING. (FLT 4546) REPLACED EMERGENCY FLOOR LEVEL FLOOD LIGHT ASSEMBLY IN IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,645 hrs · 22,789 cycles

RIGHT OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. (FLT 4842) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,352 hrs · 22,516 cycles

NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4848) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,145 hrs · 22,307 cycles

NR 4 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4731) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 27,990 hrs · 22,157 cycles

NR 6 EXTERIOR EMERGENCY LIGHT ON RIGHT WING IS OUT. (FLT 7810) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,990 hrs · 22,157 cycles

FLOOR LEVEL EMERGENCY FLOOD LIGHT BY MAIN CABIN DOOR IS BURNED OUT. (FLT 4598) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,871 hrs · 22,035 cycles

NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4832) RELAMPED EMERGENCY LIGHT.

Part: WIRE — DAMAGED (COCKPIT) · airframe 27,683 hrs · 21,851 cycles

(FLT 4759) CAPTAIN'S FLOODLIGHT WIRES WERE EXPOSED, ARCED, AND POPPED CIRCUIT BREAKER. REPLACED PILOT SIDE CONSOLE FLOOD LIGHT.

Part: ACCUMULATOR — LEAKING (NR 3 BRAKE) · airframe 27,484 hrs · 21,656 cycles

GEAR DISAGREE AND "HYD 3 LO PRESS" MESSAGE. (FLT 4632) REPLACED NR 3 BRAKE ACCUMULATOR FOR LEAKING AIR INTO HYDRAULIC SYSTEM.

Part: HYDRAULIC SYSTEM — CONTAMINATED (NR 3) · airframe 27,207 hrs · 21,377 cycles

ON TAKEOFF WHEN GEAR SELECTED UP BOTH 3 HYDRAULIC PUMPS WERE CYCLING ON AND OFF. LANDING GEAR WAS SLOW TO RETRACT AND RECEIVED A GEAR DISAGREE MESSAGE. (FLT 4456) BLED A LARGE QUANTITY OF AIR IN SYSTEM HYDRAULIC SYSTEM 3.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,958 hrs · 21,126 cycles

NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4568) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,821 hrs · 20,994 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4493) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,675 hrs · 20,865 cycles

OVERHEAD EMERGENCY LIGHT AT ROW 4 IS OUT. (FLT 4635) RELAMPED EMERGENCY LIGHT.

Part: PROXIMITY SENSOR — FAILED (NLG) · airframe 26,620 hrs · 20,820 cycles

NOSE GEAR DISAGREE. (FLT 4604) REPLACE NR 1 NLG DOWNLOCK PROX SENSOR.

Part: WIRE HARNESS — DAMAGED (NLG) · airframe 26,566 hrs · 20,774 cycles

NOSE GEAR DISAGREE. (FLT 4521) REPLACED NLG HARNESS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,496 hrs · 20,707 cycles

NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4682) RELAMPED EMERGENCY LIGHT.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 25,897 hrs · 20,172 cycles

EMERGENCY FLOOR LIGHTING FROM ROW 9 AFT NOT ILLUMINATED. (FLT 4593) RECONNECTED FLOOR LEVEL LIGHTING CONNECTOR AT OVERWING EXIT.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 25,861 hrs · 20,144 cycles

STRINGER 11 AT FS 621 CRACKED AT SKIN ATTACH POINT. (C-CHECK) REPAIR PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 25,861 hrs · 20,144 cycles

FS 559.0 BULKHEAD CRACKED AT RIGHT SIDE. (C-CHECK) REPAIRED PER REO.

Part: DOOR — CRACKED (LT TRU) · airframe 25,861 hrs · 20,144 cycles

LEFT TRU DOOR AFT LATCH CUTOUT IS CRACKED. (C-CHECK) REPAIRED PER REO.

Part: BUSHING — CORRODED (ENGINE MOUNT) · airframe 25,578 hrs · 19,894 cycles

RIGHT ENGINE AFT MOUNT SPHERICAL BUSHING HOUSING ASSEMBLY HAS SOME PITTING. (ENGINE CHANGE) REPLACED RIGHT ENGINE AFT MOUNT SPHERICAL BUSHING ASSEMBLY.

Part: LIGHT — BROKEN (CABIN) · airframe 25,015 hrs · 19,408 cycles

FLOOR LEVEL EMERGENCY FLOOD LIGHT IS BROKEN. (FLT 4616) REPLACED FLOOD LIGHT.

Part: SELECTOR VALVE — INOPERATIVE (MLG) · airframe 24,114 hrs · 18,643 cycles

GEAR DISAGREE AFTER TAKEOFF WITH NO RETRACTION. (FLT 4562) REPLACED THE MLG SELECTOR VALVE. P/N 750005000, S/N OFF 0548.

Part: CONNECTOR — NOT SEATED (CABIN) · airframe 23,945 hrs · 18,493 cycles

FLOOR LEVEL EMERGENCY LIGHTING INOP BETWEEN ROWS 6 AND 8. (FLT 4731) RESEATED CONNECTOR.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,414 hrs · 18,025 cycles

LAST TWO OVERHEAD EMERGENCY LIGHTS INOP DURING TEST. (FLT 4698) RELAMPED EMERGENCY LIGHTS.

Part: WEB — CRACKED (WING LE) · airframe 22,120 hrs · 16,986 cycles

LEADING EDGE AT 630KL INNER WEB CRACKED. (C CHECK) REPAIRED PER REO.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 22,120 hrs · 16,986 cycles

PASSENGER DOOR AFT DRAG ANGLE CRACKED. (C CHECK) REPAIRED PER REO.

Part: STEP — CORRODED (PAX DOOR) · airframe 22,120 hrs · 16,986 cycles

PASSENGER DOOR STEP CORRODED. (C CHECK) REPLACED DOOR STEP.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 22,120 hrs · 16,986 cycles

FS 280 FLOORBEAM CRACKED. (C CHECK) REPAIRED PER REO.

Part: WINDOW — FRACTURED (COCKPIT) · airframe 20,401 hrs · 15,717 cycles

FLT 3768 - AT FL350, RIGHT WINDOW SHATTERED. REPLACED RIGHT SIDE WINDOW, PN ON NP-139322-12, PN OFF 601R33033-12, SN ON 08029H1712, SN OFF 00339H5276.

Part: WIRE HARNESS — FAULTY (NLG) · airframe 19,845 hrs · 15,279 cycles

UPON RETRACTION OF LANDING GEAR RECEIVED A "GEAR DISAGREE" WITH A "NOSE DOOR OPEN" MESSAGE. (FLIGHT NR 3805) INSPECTED AND CLEARED FAULTS IN PSEU. REPLACED BOTH NOSE GEAR HARNESSES. OPS CHECK GOOD IAW MM 32-61-05.

Part: WIRE HARNESS — MALFUNCTIONED (NLG) · airframe 19,828 hrs · 15,263 cycles

UPON GEAR RETRACTION, RECEIVED A GEAR DISAGREE. NOSE GEAR REMAINED DOWN AND LOCKED. (FLIGHT NR 3981) REPLACED GEAR DOOR SWITCH HARNESS. OPS CHECK GOOD.

Part: SELECTOR VALVE — FAILED (NLG) · airframe 19,818 hrs · 15,254 cycles

NOSE GEAR WOULD NOT EXTEND. CYCLED GEAR AGAIN TO GET THREE GREEN INDICATIONS. (FLIGHT NR 3803) REPLACED NOSE GEAR HYDRAULIC SELECTOR VALVE IAW MM 32-33-10. ALL OPS CHECK GOOD AT THIS TIME.

Part: SELECTOR VALVE — FAULTY (NLG DOOR) · airframe 19,776 hrs · 15,224 cycles

FLT 4083 - RECEIVED A "GEAR DISAGREE" AND "NOSE DOOR" WARNING MESSAGES. GEAR THEN LOCKED DOWN AND NOSE DOOR CLOSED. REPLACED THE NOSE LANDING GEAR HYDRAULIC SELECTOR VALVE IAW CRJ MM 32-33-10. OPS CHECK GOOD.

Part: DOOR — OUT OF RIG (MAIN PAX) · airframe 19,426 hrs · 14,957 cycles

FLT 3912 - PASSENGER DOOR IS VERY HARD TO OPEN. RESHIMMED AND RIGGED THE FORWARD LATCH CAMS IAW CRJ MM 52-11-23. OPS CHECK GOOD.

Part: ROD — OUT OF ADJUST (PAX DOOR) · airframe 19,038 hrs · 14,669 cycles

FLT 3789 - PAX DOOR IS DIFFICULT TO CLOSE. ADJUSTED PAX DOOR LATCH ROD IAW 52-11-21. OPS CHECK GOOD.

Part: LENS — CRACKED (EMERGENCY LIGHTS) · airframe 18,949 hrs · 14,604 cycles

FLT 3830 - LEFT FORWARD CABIN DOOR EMERGENCY EXIT SIGN LENS IS CRACKED. REPLACED FIXTURE BASE AND LENS COVER ASSEMBLY PER MM 33-51-19. OPS CHECK GOOD.

Part: HANDLE — STUCK (SERVICE DOOR) · airframe 18,308 hrs · 14,129 cycles

SERVICE DOOR OUTER HANDLE WILL NOT RELEASE. REPLACED OUTER HANDLE IAW CRJ SRM 51-40-11, 51-42-06 AND 51-42-21.

Part: AILERON — WORN (WING) · airframe 17,317 hrs · 13,372 cycles

REPLACE RIGHT AILERON DUE TO EXCESSIVE BACKLASH. REPLACED RIGHT AILERON WITH A SERVICEABLE UNIT IAW 27-15-01. OPS CHECK GOOD.

Part: BRACKET — CORRODED (BS 342) · airframe 17,317 hrs · 13,372 cycles

MAIN CABIN FS342.0 LBL41 HAS CORROSION, DISCOVERED AT C-CHECK. REPLACED SUPPORT BRACKET ASSEMBLY IAW CRJ200 SRM 51-42-06.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 17,317 hrs · 13,372 cycles

FOUND FS 280 FLOORBEAM IS CRACKED AT LBL9 UPPER ANGLE, DISCOVERED AT C-CHECK. INSTALLED REPAIR ANGLES IAW REO:601R-53-11-138.

Part: BRACKET — CRACKED (MLG WW) · airframe 17,317 hrs · 13,372 cycles

RIGHT BRAKE TRANSDUCER BRACKET IS CRACKED AT 3 PLACES, DISCOVERED AT C-CHECK. INSTALLED NEW BRACKET PER CRJ200 SRM 51-42-06.

Part: ANGLE — CRACKED (BS 280) · airframe 17,317 hrs · 13,372 cycles

FOUND STA 280 RBL9 LOWER ANGLE IS CRACKED, DISCOVERED AT C-CHECK. PERFORMED REPAIR IAW REO 601R-53-11-171.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 17,317 hrs · 13,372 cycles

COCKPIT FLOORBOARD SUPPORT ANGLE AT STA 280 LBL9/RBL9 IS CRACKED, DISCOVERED AT C-CHECK. INSTALLED NEW REPAIR ANGLES AT STN 280, LBL9.0-RBL9.0 IAW CRJ200 SRM CH 51-42-06, SECTION 9, PG 11.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 17,317 hrs · 13,372 cycles

PAX DOOR FRAME IS CRACKED AT LOWER AFT CORNER RADIUS, DISCOVERED AT C-CHECK. INSTALLED REPAIR ANGLE AND FILLER PER CRJ 200 REO 601R-52-11-279 REV NC 10-18-01.

Part: CONTROL UNIT — MALFUNCTIONED (SPOILERS) · airframe 16,804 hrs · 12,977 cycles

AIRCRAFT ROLLED UNCOMMANDED TO THE LEFT ON SHORT FINAL AND LANDING FLARE WITH NO CROSSWINDS. REPLACED NR 2 SECU. OPERATIONAL CHECK AND BITE TEST GOOD, PN: 49-164-06, S/N OFF: 01501.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 14,362 hrs · 11,133 cycles

CABIN EMERGENCY LIGHTS DO NOT WORK DURING PREFLIGHT INSPECTION. REMOVED AND REPLACED NR 4 EMERGENCY LIGHT BATTERY PACK IAW AMM 33-51-04. OPERATIONAL CHECKS GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 14,155 hrs · 10,979 cycles

VARIOUS EMERGENCY LIGHTS DO NOT COME ON WHEN TESTED. REPLACED NR 3 BATTERY FOR EMERGENCY LIGHT IAW LL600 MM 33-51-04. OPERATIONAL CHECKS GOOD, SN OFF: 82705.

Part: TRIM PANEL — MALFUNCTIONED (RUDDER) · airframe 13,827 hrs · 10,734 cycles

RUDDER TRIM WORKS INTERMITTENTLY TO NOSE LEFT. REPLACED RUDDER TRIM PANEL IAW CL 600 MM 27-12-10. OPERATIONAL CHECK GOOD.

Part: STRINGER CLIP — CRACKED (BS 625) · airframe 13,617 hrs · 10,571 cycles

LT SIDE FS 625 STR 14L CLIP CRACKED, ITEM FOUND AT C-CHECK INSPECTION. INSTALLED NEW CLIP PART IAW CRJ200 SRM 51-42-06 PG 9-14 .

Part: STRINGER CLIP — CRACKED (BS 625) · airframe 13,617 hrs · 10,571 cycles

RT SIDE FS 625 STR 14R CLIP CRACKED, ITEM FOUND AT C-CHECK INSPECTION. INSTALLED NEW CLIP IAW CRJ200 SRM 51-42-06 PG 9-14.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 13,617 hrs · 10,571 cycles

FS 280 LBL 9 INNER AND OUTER FLOORBEAM ANGLES CRACKED, ITEM FOUND AT C-CHECK INSPECTION. INSTALLED NEW INNER FLOOR SPORT ANGLE AT FS 280.0 LBL9 IAW REO 601R F53-11-136.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 13,617 hrs · 10,571 cycles

FS 280 RBL 9 INNER AND OUTER FLOORBEAM ANGLES CRACKED, ITEM FOUND AT C-CHECK INSPECTION. INSTALLED NEW CLIPS AT FS 280 RBL 9 INNER AND OUTER FLOOR SUPPORT ANGLES IAW REO 601R-53-11-136.

Part: CONTROL UNIT — MALFUNCTIONED (STAB) · airframe 12,671 hrs · 9,839 cycles

STAB TRIM INOP MSG. REPLACED HSTA AND MOTOR CONTROL UNIT IAW MM 27-42-01 AND 27-42-05, HSTA PN: 839603, SN:OFF 868.

Part: CONTROL PANEL — MALFUNCTIONED (STAB TRIM) · airframe 12,301 hrs · 9,549 cycles

HORIZONTAL STAB CHANNEL 2 WILL NOT ENGAGE. REPLACED STAB/MACH TRIM ENGAGE PANEL. OPERATIONAL CHECK GOOD.

Part: CONTROL UNIT — MALFUNCTIONED (STAB TRIM) · airframe 10,870 hrs · 8,453 cycles

RECEIVED STAB TRIM MESSAGE CLIMBING THROUGH 1000 FT AGL. INSTALLED A SERVICEABLE HSTCU COMPUTER IAW CRJ MM27-70-00-720-801. OPERATIONAL CHECK GOOD.

Part: CONTROL PANEL — MALFUNCTIONED (STAB TRIM) · airframe 10,918 hrs · 8,491 cycles

MACH TRIM DISENGAGES EVERYTHING. REMOVED AND REPLACED STAB/MACH TRIM SWITCH PANEL. OPERATIONAL CHECK GOOD.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 9,027 hrs · 6,974 cycles

LEFT 484 OUTBOARD VERTICAL SUPPORT ANGLE IS CRACKED. ITEM FOUND AT C-CHECK. REMOVED AND INSTALLED SERVICEABLE REPAIR ANGLE IAW SRM 601R-53-0030 AND REO 601R-53-41-059.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 9,027 hrs · 6,974 cycles

RIGHTHAND 484 OUTBOARD VERTICAL SUPPORT ANGLE IS CRACKED. ITEM FOUND AT C-CHECK. INSTALLED SERVICEABLE REPAIR ANGLE IAW SRM 601R-53-0030 AND REO 601R-53-41-059.

Part: FITTING — CRACKED (FUSELAGE) · airframe 9,027 hrs · 6,974 cycles

FS 625 RIGHT OBLIQUE ANGLE IS CRACKED. ITEM FOUND AT C-CHECK. REMOVED 625 OBLIQUE ANGLE RIGHT SIDE, INSTALLED NEW ANGLE IAW CRJ SRM 51-42-06.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 9,027 hrs · 6,974 cycles

FLOOR SUPPORT ANGLE CRACKED AT FS 621.0, RBL 45, WS 73.5. ITEM FOUND AT C-CHECK. INSTALLED NEW ANGLES AT FS 621 RBL 45 WL 73 IAW BOMBARDIER REO 601R-53-61-117.

Part: TRIM SWITCH — DIRTY (COCKPIT) · airframe 8,739 hrs · 6,750 cycles

IN FLIGHT (STAB) AND (MACH) TRIM CAUTION MESSAGES ILLUMINATED. CLEANED CAPTAIN'S STAB TRIM DISCONNECT SWITCH. OPS CKS GOOD.

Part: STRIKER — CRACKED (PAX DOOR) · airframe 8,280 hrs · 6,397 cycles

PASSENGER DOOR SEAL STRIKER CRACKED AT FORWARD AND AFT PIN RECEPTACLES. DISCOVERED DURING B003 INSPECTION. REPAIRED IAW REO 601R-52-11-008.

Part: CONTROL UNIT — MALFUNCTIONED (SPOILERS) · airframe 7,970 hrs · 6,156 cycles

FLIGHT SPOILER CAUTION MESSAGE. REMOVED AND REPLACED NR 1 SECU WITH A SERVICEABLE UNIT. OPS CHECKS GOOD. WORK PERFORMED IAW AMM 27-61-05.

Part: CIRCUIT CARD — MALFUNCTIONED (NR1 FLT COMPUTER) · airframe 4,935 hrs · 3,828 cycles

STAB TRIM/MACH TRIM FAIL MESSAGE AT FL330, WOULD NOT RESET. REMOVED AND REPLACED FCC 4000 NR 1 CARD WITH SERVICEABLE UNIT IAW MM 22-12-14. OPS CHECK GOOD AT THIS TIME.

Part: DOOR — OPEN (EXTERNAL COMM) · airframe 4,627 hrs · 3,588 cycles

NOSE ELECTRICAL/COMMUNICATIONS EXTERNAL DOOR WAS NOT SHUT PROPERLY. RETURNED TO PHX. SECURED DOOR AND INSPECTED FOR DAMAGE. NO DAMAGE FOUND.

Part: CONTROL UNIT — MALFUNCTIONED (NR 2 TRIM MOTOR) · airframe 4,581 hrs · 3,547 cycles

STAB TRIM CHANNEL NR 2 WHEN ENGAGED AND TRIM IS TRIED, IT DISCONNECTS. STAB TRIM CHANNEL NR 1 OK. REMOVED AND REPLACED TRIM ACTUATOR AND MOTOR CONTROL UNIT IAW MM 27-40-00, 27-42-01 & 27-42-05. OPS CHECKS GOOD. ACTUATOR PN OFF 8396-3 SN OFF 715.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 4,614 hrs · 3,575 cycles

FS 484 LEFT INTERCOSTAL OUTBOARD FLANGE FOUND CRACKED AT LBL 36.00. FOUND DURING C CHECK INSPECTION. DAMAGED AREA REPAIRED IAW CRJ REO 601R-53-41-059. NDT-HFEC CARRIED OUT IAW REO 601R-53-41-0059. NO OTHER CRACKS NOTED.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 4,614 hrs · 3,575 cycles

ANGLE BRACKETS AT LBL AND RBL 9 AND FS 280 FOUND CRACKED DURING C CHECK INSPECTION. REPLACED BRACKETS IAW CRJ SRM 51-40-11, 51-42-21, 51-42-06.

Part: SUPPORT ANGLE — CRACKED (FS 621, LEFT) · airframe 4,614 hrs · 3,575 cycles

FS 621 LEFT FLOOR SUPPORT ANGLE CRACKED. FOUND DURING C CHECK INSPECTION. REPAIRED DAMAGE IAW CRJ REO 601R-53-61-117 REV. ''A''. ANGLE P/N: 601R53-61-117-1.

Part: BPSU — FAILED (T/E FLAP) · airframe 4,399 hrs · 3,415 cycles

ON DESCENT INTO DES MOINES, GOT THE FLAPS FAIL MSG. PERFORMED QRH PROCEDURE. LANDED FLAPS 0 DEGREES. REMOVED AND REPLACED RIGHT BPSU WITH SERVICEABLE IAW MM 27-51-10. OPS CHECKS GOOD.

Part: BUSS TIE — DEFECTIVE (COCKPIT) · airframe 3,996 hrs · 3,102 cycles

TURNING ON BATT MASTER, THE AROMA OF ELECTRICAL SMOKE EXISTED. NO CIRCUIT BREAKERS HAD POPPED. REPLACED BUSS TIE NR 2 CONTACTOR. TURNED ON BATT MASTER & RAN ALL SYSTEMS. NO SMOKE AROMA NOTED.

Part: TRANSDUCER — MALFUNCTIONED (STALL WARNING) · airframe 3,158 hrs · 2,466 cycles

AFTER TAKEOFF, THE STALL FAIL CAUTION MESSAGE CAME ON. COMPLIED WITH QRH. RETURNED TO SLC. REMOVED AND REPLACED NR 1 MACH TRANSDUCER. OPS CHECKS GOOD IAW 27-35-25.

Part: DISPLAY — MALFUNCTIONED (COCKPIT) · airframe 2,272 hrs · 1,795 cycles

NR 1 PFD WENT BLANK INFLIGHT. COMPLIED WITH FAULT ISOLATION MANUAL. RESET ALL CB FOR DISPLAYS. NR 1 PFD OPERATIONAL. OPS CHECKED GOOD.

Part: COMPUTER — MALFUNCTIONED (COCKPIT) · airframe 1,716 hrs · 1,393 cycles

SMELL OF SMOKE. FMS UNIT WAS HOT TO TOUCH AND LOSS OF COLORS ON SCREEN. REMOVED AND REPLACED FMS UNIT PER CRJ MM 34-16-01.

Part: CONNECTOR — DIRTY (FUEL FLOW TRANSM) · airframe 980 hrs · 815 cycles

RIGHT FUEL FLOW READOUT FAILED ON TAKEOFF. CLEANED CANNON PLUG ON RIGHT ENGINE FUEL FLOW TRANSMITTER FOR TROUBLESHOOTING. RAN ENGINES, COULD NOT DUPLICATE FUEL FLOW FAIL. OPS CHECK GOOD.

Part: PRESSURE SWITCH — FAILED (FUEL SYSTEM) · airframe 582 hrs · 493 cycles

INFLIGHT LEFT SCAVENGER EJECTOR CAUTION MESSAGE REPEATELLY ILLUMINATES, INCREASES FREQUENCY WITH VERTICAL SPEED GREATER THAN 1,000 FPM. INSTALLED SCAVENGE EJECTOR PRESSURE SWITCH IAW 28-42-07.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 42 hrs · 29 cycles

ON DESCENT THROUGH 17,000, LEFT WINDSHIELD SHATTERED. NO LOSS OF PRESSURIZATION AND NO OTHER STRUCTURAL DAMAGE NOTED. REMOVED AND REPLACED LEFT WINDSHIELD IAW RII 56-401 AND MM 56-11-01. OPS CHECKS GOOD. P/N ON PPG-WP-139321-9, S/N ON 0103248940, P/N OFF 601R33033-13, S/N OFF 01008H7144.