N913SW

Part: CONTROL HANDLE — FAILED (MLG) · airframe 43,968 hrs · 37,382 cycles

AFTER TAKEOFF, THE LANDING GEAR FAILED TO RETRACT; FOLLOWED BY A/SKID INBD AND PARK BRAKE SOV CAUTION MESSAGES. RETURNED TO FIELD. (FLT#5399) REMOVED AND REPLACED LANDING GEAR CONTROL HANDLE ASSY IAW AMM. PERFORMED LANDING GEAR EXTENSION AND RETRACTION SEVERAL TIMES IAW AMM. OPS CHECK GOOD AT THIS TIME.

Part: SERVO VALVE — FAILED (NLG STEERING) · airframe 43,726 hrs · 37,168 cycles

STEERING INOP CAUTION IN FLIGHT. COMPLIED WITH QRH. (FLT#5311) CLOSED REMOVED AND REPLACED SERVO VALVE IAW AMM.

Part: SKIN — DENTED (RT WING TE FLAP) · airframe 42,629 hrs · 36,146 cycles

A DENT WAS FOUND ON THE RT INBD FLAP LOWER SKIN. REPAIRED THE SKIN IAW SRM 57-52-00.

Part: FRAME — CORRODED (BS 605) · airframe 42,629 hrs · 36,146 cycles

BS 605 FRAME FOUND CORRODED. REMOVED AND REPLACED THE ENTIRE FRAME SECTOR IAW SRM 51-42-06.

Part: FLOOR SUPPORT — CORRODED (BS 559) · airframe 42,629 hrs · 36,146 cycles

FLOOR SUPPORT CORRODED AT BS 559. REMOVED AND REPLACED IAW SRM 51-42-06.

Part: FLOOR SUPPORT — CORRODED (BS 559) · airframe 42,629 hrs · 36,146 cycles

RIGHT FLOOR SUPPORT CORRODE AT BS 559. REMOVED AND REPLACED IAW SRM 51-42-06.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 42,629 hrs · 36,146 cycles

COCKPIT FLOORBEAM, BS 280 WAS CORRODED. REMOVED AND REPLACED THE COCKPIT FLOORBEAM ANGLE.

Part: VANE — WORN (LT WING TE FLAP) · airframe 42,629 hrs · 36,146 cycles

LEFT OUTBOARD FLAP, OUTBOARD VANE MOUNT STRUCTURE WAS WORN. MEASURED REMAINING MATERIAL AND FOUND WITHIN LIMITS IAW REO 601R-57-53-195.

Part: VANE — GOUGED (RT WING TE FLAP) · airframe 42,629 hrs · 36,146 cycles

RIGHT INBOARD FLAP VANE WAS GOUGED. REPAIRED IAW SRM 51-21-06.

Part: STRINGER SPLICE — CRACKED (BS 379) · airframe 42,629 hrs · 36,146 cycles

STRINGER SPLICE WAS CRACKED AT ITS ATTACH POINT TO PASSENGER DOOR UPPER SILL, BS 379. REPAIRED THE STRINGER SPLICE IAW SRM 53-00-03.

Part: FRAME — CORRODED (BS 333) · airframe 42,629 hrs · 36,146 cycles

CORROSION FOUND ON THE FWD AND AFT FACES OF THE FRAME AT BS 333. REMOVED THE CORROSION IAW SRM 51-21-06.

Part: PANEL — GOUGED (NOT REPORTED) · airframe 42,629 hrs · 36,146 cycles

PANEL 326CR GOUGED. REPAIRED THE PANEL IAW REO 601R-55-32-384.

Part: HINGE — CHAFED (SERVICE DOOR) · airframe 42,629 hrs · 36,146 cycles

SERVICE DOOR INTERIOR HINGE CHAFED. REMOVED AND REPLACED THE SERVICE DOOR HINGE PLATE IAW SRM 51-41-21. OPS CHECKED GOOD

Part: BRACKET — CORRODED (BS 319) · airframe 42,629 hrs · 36,146 cycles

CORROSION FOUND ON THE BRACKET ATTACHED TO FRAME AT BS 319. REMOVED AND REPLACED THE BRACKET IAW SRM 51-42-21.

Part: STRAP — CORRODED (BS 333) · airframe 42,629 hrs · 36,146 cycles

CORROSION FOUND ONTHE CIRCUMFERENTIAL STRAP BELOW FRAME BS 333. BLENDED THE STRAP IAW SRM 51-21-06.

Part: SKIN PANEL — CHAFED (LT WING) · airframe 42,629 hrs · 36,146 cycles

LEFT WING SKIN PANEL WAS CHAFED. BLENDED THE PANEL IAW SRM 51-41-02.

Part: SKIN — CHAFED (LT ELEVATOR) · airframe 42,629 hrs · 36,146 cycles

LEFT ELEVATOR SKIN PANEL WAS CHAFED. REPAIRED THE DAMAGE IAW SRM 51-12-00.

Part: SKIN — CHAFED (HORIZONTAL STAB) · airframe 42,629 hrs · 36,146 cycles

RIGHT HORIZONTAL STAB PANEL WAS CHAFED ON THE INNER SKIN. R & R THE SKIN PANEL IAW SRM 51-12-00.

Part: SKIN — CHAFED (LT NACELLE) · airframe 42,629 hrs · 36,146 cycles

LEFT NACELLE SKIN PANEL WAS CHAFED AT MULTIPLE PLACES. REMOVED AND REPLACED THE SKIN IAW SRM 51-42-06.

Part: SKIN — CORRODED (PAX DOOR) · airframe 42,629 hrs · 36,146 cycles

CORROSION FOUND ON THE INNER SKIN, AROUND FORWARD AND AFT ACCESS DOOR CUT-OUTS. REMOVED AND REPLACED THE PAX DOOR SKIN IAW SRM 51-42-06.

Part: SKIN — DENTED (FUSELAGE) · airframe 42,629 hrs · 36,146 cycles

A DENT WAS FOUND AFT AND ABOVE THE LT ACM EXHAUST OPENING. REPAIRED THE DENT IAW REO 601R-51-00-309.

Part: SKIN — DENTED (CARGO DOOR) · airframe 42,629 hrs · 36,146 cycles

A DENT WAS FOUND ON THE CARGO DOOR SKIN, AT THE BOTTOM CORNER. REPAIRED THE CARGO DOOR SKIN IAW REO 601R-52-31-299.

Part: COVER — NICKED (NOT REPORTED) · airframe 42,629 hrs · 36,146 cycles

TWO NICKS FOUND JUST AFT OF GROUND AIR LOW PRESSURE COVER. COMPLIED WITH PERMANENT REPAIR OF THE AREA IAW REO 601R-53-61-6734.

Part: SKIN — DENTED (FUSELAGE) · airframe 42,629 hrs · 36,146 cycles

A DENT WAS FOUND ON THE RT BOTTOM FUSELAGE JUST OUTBOARD FROM NLG. REPAIRED IAW REO 601R-53-11-3333.

Part: STRUCTURE — DENTED (NOT REPORTED) · airframe 42,629 hrs · 36,146 cycles

A DENT WAS FOUND ON THE AFT FUSELAGE TAIL. REPAIRED.

Part: SKIN — DENTED (BS 589-605) · airframe 42,629 hrs · 36,146 cycles

TWO SMALL DENTS FOUND ON THE RT FUSELAGE BETWEEN BS 589 TO 605. REPAIRED IAW REO 601R-53-61-6734.

Part: SKIN — DAMAGED (LT WING) · airframe 42,253 hrs · 35,801 cycles

FOUND ELONGATED DAMAGED SCREW HOLE UNDER THE LT MLG ACCESS PANEL ADJACENT TO THE MLG OPENING. BETWEEN LT WS 53.60 - 65.75. REPAIRED WING PLANK IAW REO.

Part: ENGINE — FLAMED OUT (RIGHT) · airframe 41,715 hrs · 35,326 cycles

CAPTAIN REPORTED THAT DURING APPROACH, RECEIVED A RT MAIN EJECTOR AND RT SCAVENGE EJECTOR CAUTION MESSAGES AND RIGHT AFTER TOUCH DOWN THE RT ENGINE FLAMED OUT. ENGINE SHUT DOWN AFTER THRUST REVERSER ACTIVATION. REMOVED AND REPLACED THE RT ENGINE ASSY IAW AMM. OPS CHECKED GOOD

Part: STRINGER — DAMAGED (BS 409) · airframe 38,037 hrs · 31,842 cycles

DAMAGE TO STRINGER 16R BETWEEN BS 409 - 409 + 32. REMOVED AND REPLACED THE STRINGER IAW SRM.

Part: STRINGER — DAMAGED (BS 409) · airframe 38,037 hrs · 31,842 cycles

DAMAGE TO STR 0 BETWEEN BS 409+80 AND 409.00+96. REMOVED AND INSTALLED THE STRINGER IAW SRM.

Part: VANE — CHAFED (LT WING TE FLAP) · airframe 38,037 hrs · 31,842 cycles

LEFT FLAP VANE INBD LEADING EDGE IS CHAFED. REMOVED AND REPLACED LT FLAP VANE INBD LEADING EDGE IAW SRM.

Part: VANE — CHAFED (RT WING TE FLAP) · airframe 38,037 hrs · 31,842 cycles

RIGHT FLAP VANE OTBD LEADING EDGE IS CHAFED. REMOVED AND REPLACED THE FLAP VANE OTBD LEADING EDGE IAW SRM.

Part: VANE — CHAFED (RT WING TE FLAP) · airframe 38,037 hrs · 31,842 cycles

RIGHT FLAP VANE CENTER OF LEADING EDGE IS CHAFED. REMOVED AND REPLACED THE FLAP VANE CENTER LEADING EDGE IAW SRM.

Part: VANE — CHAFED (RT WING TE FLAP) · airframe 38,037 hrs · 31,842 cycles

RIGHT FLAP VANE INBD LEADING EDGE IS CHAFED. REMOVED AND REPLACED THE FLAP VANE INBD LEADING EDGE IAW SRM.

Part: SKIN — GOUGED (BS 627) · airframe 33,832 hrs · 28,087 cycles

BS 627, OTBD OF STRINGER 4L, TWO GOUGES ON SKIN. REPAIRED IAW EA

Part: PANEL — CRACKED · airframe 33,832 hrs · 28,087 cycles

PANEL 221BLC CRACKED AND MISSING 6 EA SPACERS. REPAIRED CRACKED PANEL IAW EA AND SRM.

Part: DOOR — CHAFED (RT MLG) · airframe 33,832 hrs · 28,087 cycles

RIGHT MLG DOOR HAS CHAFE ON AFT EDGE THRU INNER SKIN NEAR BRUSH. RT MLG DOOR WORKED IAW STS EA COMPLIED WITH STEPS 1 THRU END, IAW SRM, REPAIR COMPLETED. THIS IS A PERMANANT REPAIR.

Part: VANE — DAMAGED (LT WING TE FLAP) · airframe 33,832 hrs · 28,087 cycles

LT INBD FLAP VANE CENTER CAP FOUND TO BE OUT OF LIMITS. R & R LT INBD FLAP VANE CENTER L/E SKIN, CAP, IAW SRM AND DWG 601R14303, REV J.

Part: BULKHEAD — DAMAGED (BS 621) · airframe 33,832 hrs · 28,087 cycles

FWD FACE OF FS 621 REAR PRESSURE BULKHEAD HAS SCREW STRIKES BETWEEN ISOLATOR MOUNTS AS MARKED. C-CHECK, RO 12/10/14. BLENDED SEVERAL AREAS OF SCREW NICKS ON FS 621 AT ISOLATOR MOUNTS REF SRM. FOUND TO BE WITHIN LIMITS REF REO.

Part: FAIRING — DAMAGED (HORIZONTAL) · airframe 33,832 hrs · 28,087 cycles

LEFT HORIZONTAL TIP FAIRING 333AL HAS MULTIPLE ELONGATED HOLES. REPAIRED IAW EA.

Part: PRESSURE PANEL — CRACKED (BS 460) · airframe 33,832 hrs · 28,087 cycles

PRESSURE FLOOR CRACKED IN 2 PLACES AT FS 460 OTBD OF LBL 0.0 AND RBL 0.0. COMPLIED WITH REPAIR OF PRESSURE FLOOR 2 PLACES AT FS 460 OTBD OF BL 0.0. RT & LT SIDES REF REO. PRESSURE LEAK CHECK GOOD. COMPLIED WITH ST CARD LEAK CHECK GOOD. MATERIAL REMOVED WEIGHT IS .5 LBS, ADDED MATERIAL WEIGHT IS 3.8 LBS FOR A TOTAL WEIGHT INCREASE OF 3.3 LBS.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 33,832 hrs · 28,087 cycles

SEAT TRACK RBL9 FS 559+86 TO 559+112 CORRODED. REPLACED THE SEAT TRACK IAW AMM AND REO.

Part: PANEL — CRACKED (COCKPIT) · airframe 33,832 hrs · 28,087 cycles

CREW ESCAPE HATCH TRIM PANEL 831BZ IS CRACKED AT THE "STOW HANDLE" SLOT. REPAIRED THE TRIM PANEL IAW EA.

Part: LEVER — WORN (PAX DOOR) · airframe 33,832 hrs · 28,087 cycles

PAX DOOR PULL IN LEVER IS WORN. REPAIRED THE PASSENGER DOOR PULL IN LEVER IAW REO.

Part: FRAME — CRACKED (BS 605) · airframe 33,832 hrs · 28,087 cycles

AFT CARGO BAY JUST ABOVE CARGO DOOR ENTRYWAY STRINGER 9L, FS 605.0 FRAME IS CRACKED. REPAIRED THE FRAME IAW REO. PRESSURE CHECKED GOOD.

Part: TRUNNION — DAMAGED (LEFT) · airframe 33,832 hrs · 28,087 cycles

FOUND AN OVERSIZED HOLE ON LT TRUNNION. REPAIRED THE LT TRUNION IAW REO.

Part: DOOR SILL — CORRODED (BS 574-621) · airframe 33,832 hrs · 28,087 cycles

LEFT CARGO DOOR SILL HAS CORROSION AROUND NUTPLATE HOLES FS 574 TO 621. C-CHECK, RO 12/10/14, BLENDED LT CARGO DOOR SILL CORROSION AROUND NUTPLATE HOLES FS 574 TO 621 REF SRM , BLEND OUT OF LIMITS. R & R LT CARGO DOOR SILL REF SRM & REO.

Part: VANE — CHAFED (LT WING TE FLAP) · airframe 33,832 hrs · 28,087 cycles

LEFT INBD FLAP VANE INBD CAP CHAFED. FOUND WITHIN LIMITS. COMPLETED AND COMPLIED WITH PERMANENT REPAIR IAW REO.

Part: LINK — CHAFED (LT MLG DOOR) · airframe 33,832 hrs · 28,087 cycles

LEFT MLG DOOR HAS A CHAFED ATTACHMENT LINK. BLENDED AND REPAIRED THE LT MLG DOOR CENTER ATTACHMENT LINK, IAW REO AND DWG.

Part: STRUCTURE — CHAFED (LT MLG) · airframe 33,832 hrs · 28,087 cycles

LEFT MLG DOOR HAS CHAFING AT FWD AND AFT EDGES. REPLACED FILLER ON PRIVIOUS REPAIR ON FWD EDGE OF LT MLG DOOR IAW REO. BLENDED AND FOUND TO BE WITHIN LIMITS IAW REO.

Part: VANE — CHAFED (RT WING TE FLAP) · airframe 33,832 hrs · 28,087 cycles

RIGHT INBD FLAP VANE OTBD CAP CHAFED. EVALUATED RT INBD FLAP VANE OTBD CAP AND FOUND TO BE WITHIN LIMITS. REPAIRED IAW REO COMPLIED WITH PERMANANT REPAIR, BLENDED AND RESTORED FINISH.

Part: VANE — CHAFED (RT WING TE FLAP) · airframe 33,832 hrs · 28,087 cycles

RIGHT INBD FLAP VANE CENTER CAP CHAFED. EVALUATED RT INBD FLAP VANE CENTER CAP AND FOUND TO BE WITHIN LIMITS. COMPLETED AND COMPLIED WITH PERMANENT REPAIR REF REO.

Part: VANE — CHAFED (RT WING TE FLAP) · airframe 33,832 hrs · 28,087 cycles

RIGHT INBD FLAP VANE INBD CAP CHAFED, C-CHECK RO 12/10/14, EVALUATED RT INBD FLAP VANE INBD CAP, ORIGINAL MATERIAL THICKNESS IS .050", REMAINING MATERIAL=.045", REMOVAL .005", MAX ALLOWABLE IS .020". FOUND TO BE WITHIN LIMITS. REF REO COMPLIED WIT PERMANENT REPAIR. BLENDED AND RESTORED FINISH.

Part: VANE — CHAFED (LT WING TE FLAP) · airframe 33,832 hrs · 28,087 cycles

LEFT INBD FLAP VANE OTBD CAP CHAFED. REPLACED LT INBD FLAP VANE DAMAGED OTBD CAP WITH NEW IAW REO AND SRM.

Part: DOOR — CHAFED (RT MLG) · airframe 33,832 hrs · 28,087 cycles

RIGHT MLG DOOR HAS CHAFING AT FWD AND AFT EDGES. RT MLG FWD CHAFE REPAIRED IAW REO. RT MLG DOOR AFT CHAFE FOUND OUT OF LIMITS. REPAIRED THE RT MLG DOOR.

Part: VANE — CHAFED (LT WING TE FLAP) · airframe 33,832 hrs · 28,087 cycles

LEFT INBD FLAP VANE CENTER CAP CHAFED. FOUND TO BE OUT OF LIMITS AND REPAIRED IAW REO

Part: VANE — LOOSE (EXHAUST DUCT) · airframe 33,832 hrs · 28,087 cycles

LEFT RAM AIR EXHAUST DUCT HAS THREE LOOSE VANES. REPAIRED THE VANES IAW REO.

Part: TUBE — DAMAGED (SERVICE DOOR) · airframe 33,832 hrs · 28,087 cycles

SERVICE DOOR HARNESS CONVOLEX TUBING DAMAGED. R & R THE SERVICE DOOR HARNESS CONVOLEX TUBING IAW REO .

Part: FASTENER — MISSING (SEAT TRACK) · airframe 33,832 hrs · 28,087 cycles

CO-PILOT'S INBD SEAT TRACK IS MISSING A RIVET. INSTALLED THE RIVET IAW REO.

Part: FASTENER — MISSING (SEAT TRACK) · airframe 33,832 hrs · 28,087 cycles

PILOT'S INBD SEAT TRACK IS MISSING A RIVET. INSTALLED THE MISSING RIVET ON PILOTS INBD SEAT TRACK IAW REO.

Part: LEVER — LOOSE (THROTTLE) · airframe 33,735 hrs · 28,017 cycles

LEFT ENGINE THRUST LEVER JAMMED AFTER TAKE OFF. RETURNED TO FIELD. SECURED THE LT ENGINE FUEL THROTTLE CONTROL GEAR BOX INPUT LEVER HARDWARE.

Part: SKIN — DAMAGED (BS 718) · airframe 33,646 hrs · 27,938 cycles

DAMAGE TO SKIN SPLICE BS 718 STRINGER 26R. REPAIRED SKIN IAW REO.

Part: IDG — FAILED (RIGHT) · airframe 33,490 hrs · 27,825 cycles

NR 2 IDG CAUTION MESSAGE. RETURNED TO FIELD. REMOVED AND REPLACED THE RT IDG IAW AMM. LEAK AND OPS CHECKED GOOD.

Part: A/C PACK — OVERPRESSURED (RIGHT) · airframe 33,422 hrs · 27,771 cycles

DURING BLEED SWAP DURING CLIMBOUT, BOTH PACKS OVER PRESSURED. LEFT SIDE RESET BUT RT PACK PSI WOULD NOT REDUCE BELOW 80 PSI WITH ENGINE BLEEDS ON. DID RESET WITH APU BLEED ONLY. PERFORMED HIGH POWER ENGINE RUN, AND OPERATED BOTH PACKS ON APU BLEED AND BOTH ENGINES BLEED PER NORMAL OPERATIONS. NO DEFECTS NOTED AT THIS TIME IAW AMM.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 32,289 hrs · 26,881 cycles

NR 2 EMERGENCY LIGHT CEILING POD BURNED OUT, REPLACED LAMP.

Part: PUMP — FAILED (HYDRAULIC SYS) · airframe 32,088 hrs · 26,741 cycles

AFTER SELECTING LG DOWN, RECEIVED HYD 3 LOW PRESS CAUTION, FOLLOWED BY GEAR DISAGREE & NOSE DOOR WARNING MESSAGE. AFTER 5 SECONDS ALL MESSAGES CLEARED ON THEIR OWN, ALL GEAR DOWN & GREEN. FLT 5253 REPLACED HYD SYS NR 3 PUMP 3A. PN ON OFF 848847, SN ON MX605967, SN OFF MX679140, PN ON OFF 848847 SN ON MX572952 & SN OFF MX563539.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,986 hrs · 26,658 cycles

REAR EMERGENCY OVERHEAD LIGHT IS BURNED OUT. FLT 6478 RELAMPED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,777 hrs · 26,500 cycles

NR 3 EMERGENCY OVERHEAD LIGHT IS BURNED OUT. FLT 6299 RELAMPED.

Part: SHUTOFF VALVE — LOOSE (CABIN PRESSURE) · airframe 31,379 hrs · 26,207 cycles

ON CLIMB OUT THE PLANE WOULD NOT PRESSURIZE. FLT 6362 INSPECTED & FOUND THE INBD EXHAUST SOV LOOSELY SAFETIED. RE-SECURED INBD EXHAUST VALVE IN OPEN POSITION. PERFORMED OPERATION CHECK OF THE PRESS SYSTEM IAW AMM. OPERATIONS CHECKED GOOD.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 30,878 hrs · 25,837 cycles

OIL FUEL SMELL DETECTED THROUGH THE FLIGHT DECK GASPER VENTS DURING CRUISE WITH A LT PACK DUCT TEMPERATURE OF AROUND 35-45°C. FLT#5520 RAN LT PACK TO FULL HOT TEMPERATURE, SMELL DISAPPEARED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,298 hrs · 25,380 cycles

ONE EMERGENCY LIGHT BURNED OUT AT THE RIGHT OVERWING EXIT. FLT# 6534 RELAMPED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,284 hrs · 25,370 cycles

CENTER OVERHEAD EMERGENCY LIGHT IS BURNED OUT. FLT#5385 RELAMPED.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 30,110 hrs · 25,244 cycles

LBL 27.0 FLOOR SUPPORT BEAM HAS NUMEROUS CRACKS AT FLOORBOARD ATTACH FLANGES (OTBD SIDE) BETWEEN FS 572-621. (C-CHECK)REPLACED FLOOR SUPPORT BEAM UPPER CAP LBL27.0, FS 572-621 IAW REO.

Part: VANE — CHAFED (TE FLAP) · airframe 30,110 hrs · 25,244 cycles

RIGHT WING INBD FLAP VANE CHAFE ON MIDDLE L/E VANE IS OUT OF LIMITS. (C-CHECK) REPLACED RT WING INBD FLAP VANE, MIDDLE L/E, WITH NEW PN 601R-14303-52 IAW SRM.

Part: VANE — CHAFED (TE FLAP) · airframe 30,110 hrs · 25,244 cycles

RIGHT WING INBD FLAP VANE HAS A CHAFE ON OTBD L/E OUT OF LIMITS. (C-CHECK) REPLACED RT WING INBD FLAP VANE ON OTBD L/E WITH A NEW FLAP VANE CAP IAW SRM.

Part: VANE — CHAFED (TE FLAP) · airframe 30,110 hrs · 25,244 cycles

RIGHT WING INBD FLAP VANE CHAFE ON MIDDLE L/E VANE IS OUT OF LIMITS. (C-CHECK) REPLACED RT WING INBD FLAP VANE, MIDDLE L/E, WITH NEW PN 601R-14303-52 IAW SRM.

Part: VANE — CHAFED (TE FLAP) · airframe 30,110 hrs · 25,244 cycles

RT WING INBD FLAP VANE HAS A CHAFE ON INBD L/E OF FLAP VANE. (C-CHECK) REWORKED RT WING INBD FLAP VANE INBD L/E IAW REO.

Part: VANE — CHAFED (TE FLAP) · airframe 30,110 hrs · 25,244 cycles

LEFT WING INBD FLAP VANE HAS A CHAFE ON INBD L/E OF FLAP VANE. (C-CHECK)REWORKED LT WING INBD FLAP VANE INBD L/E IAW REO.

Part: VANE — CHAFED (TE FLAP) · airframe 30,110 hrs · 25,244 cycles

LEFT WING INBD FLAP VANE HAS A CHAFE ON OTBD L/E OF FLAP VANE. (C-CHECK) REWORKED LT WING INBD FLAP VANE OTBD L/E IAW REO.

Part: POST — CRACKED (FUSELAGE) · airframe 30,110 hrs · 25,244 cycles

CRACK NOTED & MARKED ON FS409.0+128 VERT POST OTBD AFT RADIUS AT RBL18.00 WL71.00. (C-CHECK) R & R NEW POSTS IAW REO.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,876 hrs · 25,072 cycles

NR 3 EMERGENCY OVERHEAD LIGHT IS BURNED OUT. (FLT 5381) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,495 hrs · 24,786 cycles

LAST OVERHEAD EMERGENCY LIGHT IS BURNED OUT. (FLT 5351) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,397 hrs · 24,720 cycles

AFT OVERHEAD EMERGENCY LIGHT BURNED OUT. (FLT 6520) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,885 hrs · 24,355 cycles

LAST EMERGENCY OVERHEAD LIGHT IS BURNED OUT. (FLT 6202) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,484 hrs · 24,023 cycles

ONE OF THE EMERGENCY LIGHTS ON THE GALLEY SERVICE DOOR IS OUT. (FLT 5650) RELAMPED EMERGENCY LIGHTS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,285 hrs · 23,872 cycles

FLOOR LEVEL EMERGENCY LIGHT NEAR CABIN DOOR IS OUT. (FLT 5637) RELAMPED EMERGENCY LIGHT.

Part: PANEL — FAILED (COCKPIT) · airframe 28,237 hrs · 23,840 cycles

SPEED BUG RESET TO 40 KNOTS AND FLIGHT DIRECTION PITCHED UP TO FOLLOW. (FLT 6240) REPLACED CAPTAINS AIR DATA REFERENCE PANEL IN REFERENCE TO AMM. PART OFF: 622-9819-104 S/N: 1GFTL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,586 hrs · 23,335 cycles

NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5301) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,290 hrs · 23,098 cycles

OVERHEAD EMERGENCY LIGHT AT ROW 8 IS OUT. (FLT 5303) RELAMPED EMERGENCY LIGHT.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 26,836 hrs · 22,745 cycles

NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5304) RELAMPED EMERGENCY LIGHT.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 26,820 hrs · 22,729 cycles

FLT 6381, AFT OVERHEAD EMERGENCY LIGHT INOPERATIVE. RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,766 hrs · 22,690 cycles

AFT OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6308) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,766 hrs · 22,690 cycles

NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. (SERVICE) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,640 hrs · 22,583 cycles

NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6392) RELAMPED EMERGENCY LIGHT.

Part: HYDRAULIC LINE — CRACKED (HYDRAULIC SYS) · airframe 26,576 hrs · 22,533 cycles

HYDRAULIC SYSTEM 1 FLUID QUANTITY INDICATED 0 PERCENT. (FLT 6445) REPLACED CRACKED NR 1 HYDRAULIC PRESSURE SERVICE LINE.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 26,576 hrs · 22,533 cycles

NR 2 EXTERIOR AFT EMERGENCY LIGHT IS OUT. (FLT 6304) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,479 hrs · 22,459 cycles

NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5316) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,271 hrs · 22,290 cycles

THE 1ST OVERHEAD EMERGENCY LIGHT INOPERATIVE. (FLT 6190) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,139 hrs · 22,186 cycles

NR 4 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5571) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,081 hrs · 22,136 cycles

SECOND TO LAST OVERHEAD EMERGENCY LIGHT WILL NOT ILLUMINATE. (FLT 6398) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,062 hrs · 22,120 cycles

NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. (SERVICE) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 25,971 hrs · 22,030 cycles

NR 1 OVERHEAD EMERGENCY AND LEFT SIDE NR 2 EXTERIOR LIGHTS ARE OUT. (FLT 5566) RELAMPED EMERGENCY LIGHTS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,971 hrs · 22,030 cycles

AFT 2 OVERHEAD EMERGENCY LIGHTS ARE OUT. (FLT 6274) RELAMPED EMERGENCY LIGHTS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,821 hrs · 21,902 cycles

NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6447) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,772 hrs · 21,861 cycles

NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6517) RELAMPED EMERGENCY LIGHT.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 25,728 hrs · 21,827 cycles

C-CHECK, FS 621 AFT PRESSURE BULKHEAD AFT WEB CRACKED NEAR CARGO DOOR TRACK UPPER ATTACH POINT. REPAIR PER REO.

Part: SKIN — CHAFED (TE FLAP VANE) · airframe 25,728 hrs · 21,827 cycles

C-CHECK, LEFT INBOARD FLAP VANE CENTER LEADING EDGE SKIN CHAFED. REPLACED LEFT INBOARD FLAP VANE CENTER LEADING EDGE SKIN PER SRM.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 25,728 hrs · 21,827 cycles

C-CHECK, AVIONICS BAY DOOR CUTOUT STRUCTURE IS CORRODED. REPAIR PER MODSUM IS601R53210045.

Part: POST — CRACKED (FUSELAGE) · airframe 25,728 hrs · 21,827 cycles

C-CHECK, FS 409 +128 VERTICAL POST CRACKED ON LEFT AND RIGHT AFT RADIUS. REPLACE PER SRM.

Part: INTERCOSTAL — CRACKED (PAX DOOR) · airframe 25,728 hrs · 21,827 cycles

C-CHECK, PAX DOOR AFT INTERCOSTAL AT FS 340 CRACKED. REPAIR PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 25,728 hrs · 21,827 cycles

C-CHECK, FS 202 PRESSURE BULKHEAD CRACKED AT BRAKE CUTOUT. REPAIR PER REO.

Part: SKIN — CRACKED (FUSELAGE) · airframe 25,728 hrs · 21,827 cycles

C-CHECK, LEFT SIDE TRU DOOR LATCH LAND SKIN IS CRACKED. REPLACE SKIN PER SRM.

Part: VANE — CHAFED (TE FLAP) · airframe 27,325 hrs · 23,123 cycles

RIGHT INBOARD FLAP VANE LEADING EDGE CHAFED AT WS 140. (C-CHECK) REPAIRED PER REO.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,753 hrs · 21,845 cycles

CEILING EMERGENCY LIGHTS ARE OUT. (FLT 6262) RELAMPED ALL CEILING EMERGENCY LIGHTS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,753 hrs · 21,845 cycles

AFT OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6279) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,712 hrs · 21,817 cycles

ALL 4 CEILING LEVEL EMERGENCY FLOOD LIGHTS WILL NOT COME ON. (FLT 6350) RELAMPED EMERGENCY LIGHTS.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 25,676 hrs · 21,793 cycles

LEFT AFT EXTERIOR EMERGENCY LIGHT IS OUT. (FLT 5507) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,676 hrs · 21,793 cycles

NR 4 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5656) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,659 hrs · 21,781 cycles

NR 2 AND NR 4 OVERHEAD EMERGENCY LIGHTS ARE BURNED OUT. (FLT 6428) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,595 hrs · 21,729 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6280) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,595 hrs · 21,729 cycles

CEILING EMERGENCY LIGHT THIRD FROM AFT IS OUT. (FLT 6280) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,435 hrs · 21,599 cycles

FIRST AND LAST CEILING EMERGENCY LIGHTS ARE OUT. (FLT 5492) RELAMPED EMERGENCY LIGHTS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,352 hrs · 21,533 cycles

LEFT WING AFT EMERGENCY EXIT LIGHT IS OUT. (FLT 6490) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,248 hrs · 21,445 cycles

AFT OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5452) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,184 hrs · 21,399 cycles

NR 4 OVERHEAD EMERGENCY LIGHT IS BURNED OUT. (FLT 6403) REPLACED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,076 hrs · 21,304 cycles

AFT OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5458) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 24,629 hrs · 20,938 cycles

LEFT AFT EXTERIOR EMERGENCY LIGHT IS OUT. (FLT 6985) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,629 hrs · 20,938 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6985) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,295 hrs · 20,673 cycles

NR 4 OVERHEAD EMERGENCY LIGHT IS OUT. (SERVICE) RELAMPED EMERGENCY LIGHT.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 24,193 hrs · 20,588 cycles

BOTH LEFT AND RIGHT EMERGENCY OVERWING LIGHTS ARE OUT. (FLT 5844) REPLACED NR 1 AND NR 2 EMERGENCY LIGHT BATTERY PACKS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,098 hrs · 20,521 cycles

AFT CEILING MOUNTED EMERGENCY LIGHT IS OUT. (FLT 6605) RELAMPED EMERGENCY LIGHT.

Part: BATTERY — DISCHARGED (CABIN) · airframe 23,599 hrs · 20,130 cycles

ALL EXIT LIGHTS AND EMERGENCY LIGHTS WILL NOT ILLUMINATE. (FLT 6518) REPLACED ALL 4 EMERGENCY LIGHT BATTERIES.

Part: BALLAST — MALFUNCTIONED (LAVATORY) · airframe 22,962 hrs · 19,593 cycles

UNUSUAL ELECTRICAL ODOR IN LAV. (FLT 6590) REPLACED LAV LIGHT BALLAST PER AMM 33-25-07.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,712 hrs · 19,397 cycles

EMERGENCY LIGHT AT FA SERVICE DOOR INOPERATIVE. (FLT 6187)RELAMPED.

Part: GROUND WIRE — BROKEN (CABIN) · airframe 22,561 hrs · 19,276 cycles

EMERGENCY EXIT SIGN NEAR THE GALLEY SERVICE DOOR INOP. (FLT 6592) REPAIRED BROKEN GROUND WIRE.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 22,244 hrs · 19,015 cycles

FORWARD CEILING EMERGENCY CEILING LIGHT INOP. (FLT 6100) REPLACED NR 1 ELBP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,285 hrs · 18,182 cycles

CEILING EMERGENCY LIGHT OVER ROW 5 INOP. (FLT 6618) RELAMPED EMERGENCY LIGHT.

Part: INVERTER — FAILED (EMERGENCY LIGHT) · airframe 20,932 hrs · 17,874 cycles

FLT 6030 - FORWARD SECTION OF EMERGENCY FLOOR PATH LIGHTING INOP. REPLACED NR 2 INVERTER.

Part: LINK — CORRODED (ENGINE MOUNT) · airframe 20,894 hrs · 17,838 cycles

RIGHT ENGINE LINK AND BUSHING CORRODED, (ENG CHANGE). REPLACED LINK AND BUSHING.

Part: MOUNT — CORRODED (LT ENGINE) · airframe 20,871 hrs · 17,822 cycles

LEFT ENGINE FORWARD LINK AND BUSHING PITTED. (ENG CHANGE) REPLACED YOKE LINK AND BUSHING.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 21,328 hrs · 18,220 cycles

FS 559 BULKHEAD LOWER CAP ANGLE RADIUS CRACKED. (C CHECK) REPAIRED PER REO.

Part: WEB — CRACKED (FUSELAGE) · airframe 21,328 hrs · 18,220 cycles

FS 621 WEB CRACKED AT LINTEL FITTING. (C CHECK) REPAIRED PER REO.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,799 hrs · 17,765 cycles

REAR MOST CEILING EMERGENCY LIGHT INOP. (FLT 6752)RELAMPED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,161 hrs · 17,254 cycles

LAST TWO CEILING EMERGENCY LIGHTS INOP. (FLT 6217) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,768 hrs · 16,953 cycles

AFT EMERGENCY LIGHT INOP. (FLT 6509) RELAMPED EMERGENCY LIGHT.

Part: CONNECTOR — LOOSE (CABIN) · airframe 19,768 hrs · 16,953 cycles

FORWARD FLOOR EMERGENCY LIGHTS INOP. (FLT 6586) RESECURED CONNECTOR.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 19,584 hrs · 16,811 cycles

NR 2 EMERGENCY OVERHEAD LIGHT INOP. (FLT 5191) RELAMPED EMERGENCY LIGHT.

Part: LAMP — BURNED OUT (EMERGENCY LIGHTS) · airframe 18,971 hrs · 16,325 cycles

FLT 6123 - NR 2 EMERGENCY DOME LIGHT INOP. RELAMPED.

Part: DOOR — FROZEN (MAIN PAX) · airframe 18,432 hrs · 15,904 cycles

FLT 6014 - MAIN CABIN DOOR WOULD NOT OPEN. LUBRICATED AND PERFORMED OPS CHECK OF MAIN CABIN DOOR.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 18,432 hrs · 15,904 cycles

FLT 6674 - AFT OVERHEAD EMERGENCY LIGHT INOP. RELAMPED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,293 hrs · 15,799 cycles

FLT 6555 - THIRD AFT OVERHEAD EMERGENCY LIGHT ON CEILING INOP. RELAMPED.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHTS) · airframe 18,293 hrs · 15,799 cycles

FLT 6576 - BACK ROW EMERGENCY LIGHTS INOP. RESEATED CONNECTOR.

Part: CONTROL HANDLE — MALFUNCTIONED (COCKPIT) · airframe 17,717 hrs · 15,345 cycles

ON ROTATION AND GEAR UP, GEAR DID NOT RETRACT UNTIL FL100. FLT 6252. REPLACED LANDING GEAR CONTROL HANDLE ASSEMBLY.

Part: WARNING MESSAGE — ILLUMINATED (NLG STEERING) · airframe 17,458 hrs · 15,102 cycles

"STEERING INOP" FOLLOWED BY GEAR DISAGREE WARNING MSG. JACKED THE NOSE GEAR AND PERFORMED SEVERAL GEAR RETRACTIONS, NOSE GEAR OPERATES NORMALLY.

Part: SWITCH — FAULTY (FIRE BOTTLE) · airframe 17,376 hrs · 15,030 cycles

RECEIVED A "CARGO BTL LO" CAUTION MESSAGE. RETURNED TO FIELD. FLIGHT 5802. REPLACED LARGE CARGO BOTTLE DUE TO FAULTY BOTTLE PRESSURE SWITCH PER AMM 26-25-01. OPS CHECK GOOD AT THIS TIME. P/N 3460037-1, S/N OFF 229NBFI.

Part: FITTING — CRACKED (FUSELAGE) · airframe 17,760 hrs · 15,377 cycles

INTERCOSTAL TO FRAME CLIP AT LFS625 STR 14 CRACKED (C-CHECK). REPLACED PER REO.

Part: FITTING — CRACKED (FUSELAGE) · airframe 17,717 hrs · 15,345 cycles

FS 280 RIGHT SIDE TOP OUTBOARD CLIP IS CRACKED (C-CHECK). REPLACED CLIP.

Part: FITTING — CRACKED (FUSELAGE) · airframe 17,760 hrs · 15,377 cycles

INBOARD AND OUTBOARD CLIPS AT STA 484 UNDER PANEL 261DLF CRACKED (C-CHECK). REPLACED PER REO.

Part: FITTING — CORRODED (LT ENGINE MOUNT) · airframe 17,760 hrs · 15,377 cycles

LEFT ENGINE REAR MOUNT THRUST FITTING SPHERICAL BALL END CORRODED (C-CHECK). REPLACED BALL END.

Part: FITTING — CORRODED (RT ENGINE MOUNT) · airframe 17,760 hrs · 15,377 cycles

RIGHT ENGINE REAR MOUNT THRUST FITTING BALL END CORRODED (C-CHECK). REPLACED BALL END.

Part: FITTING — CRACKED (FUSELAGE) · airframe 17,717 hrs · 15,345 cycles

OUTBOARD CLIP UNDER PANEL 262DRF AT FS 484 IS CRACKED (C-CHECK). REPAIRED PER REO.

Part: FITTING — CRACKED (FUSELAGE) · airframe 17,717 hrs · 15,345 cycles

INTERCOSTAL TO FRAME CLIP CRACKED AT RT FS 625 (C-CHECK). REPAIRED PER REO.

Part: SPHERICAL BEARIN — CORRODED (LT ENGINE MOUNT) · airframe 17,760 hrs · 15,377 cycles

LEFT ENGINE FORWARD MOUNT UPPER LINK SPHERICAL BEARING IS CORRODED (C-CHECK). REPLACED BEARING.

Part: LAMP — BURNED OUT (EMERGENCY LIGHTS) · airframe 16,369 hrs · 14,141 cycles

OVERHEAD EMERGENCY FLOODLIGHT IS INOP. RELAMPED OVERHEAD FLOODLIGHT. OPS CHECK GOOD.

Part: WINDOW — CRACKED (COCKPIT) · airframe 16,056 hrs · 13,888 cycles

FLT 6657 - FIRST OFFICERS SIDE WINDOW SHATTERED IN FLIGHT. REPLACED RIGHT SIDE WINDOW IAW CRJ 200 MM 56-12-01, PN NP139322-12, SN OFF 03010H4039.

Part: LAMP — FAILED (EMERGENCY LIGHTS) · airframe 12,637 hrs · 10,987 cycles

EMERGENCY LIGHT BETWEEN ROW 10 INOP. RELAMPED OVERHEAD EMERGENCY LIGHT. OPERATIONAL CHECKS GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 12,351 hrs · 10,752 cycles

THRID AFT CABIN EMERGENCY CEILING LEVEL FLOOD LIGHT IS OUT. REPLACED LAMP IAW AMM TASK 33-51-16. OPERATIONAL CHECKS GOOD.

Part: WEB — CRACKED (PAX DOOR) · airframe 12,647 hrs · 10,993 cycles

PAX DOOR FWD WEB CRACKED IN RADIUS UNDER HANDRAIL SUPPORT BRACKET, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED DOUBLER AND REPAIR ANGLES PER REO 601R 52-11-702.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 12,647 hrs · 10,993 cycles

CRACK AT FS 280 FLOORBEAM APPROXIMATELY LBL11.0 BELOW FLOORBOARD 231BLF, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED REPAIR PARTS.

Part: DOUBLER — CRACKED (PAX DOOR) · airframe 12,647 hrs · 10,993 cycles

PAX DOOR AFT SIDE (INSIDE ACCESS PNL 832AR) DOUBLER AT PULL IN CAM FRAME IS CRACKED AT CORNER RADIUS, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED NEW DOUBLER P/N 601R318094-2 ON PAX DOOR IAW CRJ200 SRM 51-42-06 PAGE 10-18, 51-42-13 PAGE 4, 51-42-21 PAGE 17.

Part: WEB — CRACKED (PAX DOOR) · airframe 12,647 hrs · 10,993 cycles

PAX DOOR AFT WEB CRACKED IN RADIUS UNDER HANDRAIL SUPPORT BRACKET, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED DOUBLER AND REPAIR ANGLES PER REO 601R 52-11-702.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 12,647 hrs · 10,993 cycles

FS 280 LOWER FLANGE OF FLOORBEAM CRACKED AT LBL9 AND RBL9, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED REPAIR PARTS P/N 601R-53-11-171-1 IAW REO 601R-53-11-171 BETWEEN LBL15 - RBL15, FS 280 LOWER FLANGE.

Part: WEB — CRACKED (PAX DOOR) · airframe 12,647 hrs · 10,993 cycles

PAX DOOR AFT SIDE EXTRUSION INSIDE DOOR WEB THAT HOLDS DOOR ASSIST MOTOR IS CRACKED AT LOWER RADIUS, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED STIFFENER PER DWG 601R 317745 AND CRJ200 SRM 51-42-06.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 12,647 hrs · 10,993 cycles

PASSENGER DOOR, DRAG ANGLE IS ON AFT SIDE OF DOOR IS CRACKED JUST ABOVE DOOR PULLEY, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED DRAG ANGLE SECTION P/N 601F5211513-1 AND SPLICE ANGLES IAW REO 601R-52-11-513.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 12,647 hrs · 10,993 cycles

CRACK AT FS 280 FLOORBEAM APPROXIMATELY LBL 11.0 BELOW FLOORBOARD 231BLF, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED REPAIR PARTS IAW REO 601R-53-11-136.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 11,945 hrs · 10,388 cycles

CAPTAINS WINDSHIELD SHATTERED AT FL350. INSTALLED SERVICEABLE WINDOW IAW 56-11-01, AND RII CARD RII 56-220-1000, OPERATIONAL CHECKS GOOD.

Part: PCU — MALFUNCTIONED (SPOILERS) · airframe 10,791 hrs · 9,384 cycles

SPOILERON FAULT STATUS MESSAGE DOES NOT CLEAR (RIGHT SPOILERON ICON STAYS WHITE). REPLACED INBOARD RIGHT SPOILERON PCU IAW MM 27-00-00. OPERATIONAL CHECK GOOD.

Part: CONTROL UNIT — MALFUNCTIONED (SPOILER) · airframe 10,778 hrs · 9,370 cycles

SPOILERONS FAULT STATUS MSG. REPLACED SECU 2 IAW CRJ 200 MM 27-61-05. OPERATIONAL CHECK GOOD.

Part: PCU — MALFUNCTIONED (FLT SPOILERS) · airframe 10,462 hrs · 9,100 cycles

FLT SPLRS FAULT STATUS MESSAGE ON ED2 RECEIVED DURING TAXI. REPLACED FLT SPLRS PCU ON THE OUTBOARD SIDE IAW MM 27-62-01. OPERATIONAL CHECK GOOD.

Part: PCU — OUT OF RIG · airframe 10,401 hrs · 9,056 cycles

NORMAL T/O ROLL EXCEEDING 80KTS RECEIVED "T/O CONFIGURATION WORKING" . ADJUSTED RIGHT INBOARD PCU IAW 27-62-01, OPERATIONAL CHECK GOOD.

Part: PCU — MALFUNCTIONED (FLT SPOILERS) · airframe 10,165 hrs · 8,848 cycles

SPOILERONS FAULT STATUS MESSAGE REMAINS ON. INSTALLED NEW LT SPOILERON PCU IAW AMM 27-62-01. OPERATIONAL CHECK GOOD.

Part: CONTROL UNIT — MALFUNCTIONED (SPOILERS) · airframe 10,141 hrs · 8,822 cycles

SPOILERS FAULT. REPLACED NR 1 AND NR 2 SECU'S. OPERATIONAL CHECK GOOD IAW CRJ 200 MM 27-61-05, PN OFF: 49-164-05, SN OFF: 1245 SN OFF: 1450.

Part: LAMP — BURNED OUT (EMERGENCY LIGHTS) · airframe 10,141 hrs · 8,822 cycles

CEILING EMERG LIGHT FLOORLIGHT (2) INOP. RELAMPED CEILING EMERGENCY LIGHT (2). OPERATIONAL TEST GOOD.

Part: SENSOR — MALFUNCTIONED (TE FLAPS) · airframe 9,970 hrs · 8,662 cycles

"FLAPS DEGRADED" STATUS MESSAGE. REPLACED SKEW DETECTION SENSOR AND OPERATIONAL CHECK GOOD IAW 27-51-15.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 9,573 hrs · 8,308 cycles

FURTHEST AFT CEILING LEVEL EMERGENCY FLOOD LIGHT INOP. RELAMPED EMERGENCY FLOODLIGHT. OPERATIONAL CHECK GOOD.

Part: TRIM SWITCH — MALFUNCTIONED (COCKPIT) · airframe 9,370 hrs · 8,125 cycles

CAPT'S TRIM SWITCH STICKS. REPLACED CAPT'S TRIM SWITCH. OPERATIONAL CHECK GOOD IAW MM 27-40-00.

Part: WIRE — BROKEN (FLT CONTROLS) · airframe 9,313 hrs · 8,077 cycles

"CPLT ROLL CMD" ADVISORY MESSAGE. CAPTAIN'S AILERONS WORK NORMAL, NO JAM. REPAIRED WIRE CN619A22 AND CN620A22 IAW WDM 20-11-00. OPERATIONAL CHECK GOOD IAW 27-61-20.

Part: ACM — ODOR (LEFT) · airframe 9,295 hrs · 8,060 cycles

BURNING SMELL IN COCKPIT AND CABIN. REPLACED LEFT AIR CYCLE MACHINE IAW 21-51-10. OPERATIONAL CHECK GOOD.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 9,205 hrs · 7,985 cycles

LAST OVERHEAD EMERGENCY LIGHT INOP. REPLACED LAST OVERHEAD EMERGENCY LIGHT BULB, OPERATIONAL CHECK GOOD PER CRJ MM 33-51-16.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 9,103 hrs · 7,911 cycles

NR 3 OVERHEAD EMERGENCY LIGHT INOP. RELAMPED NR 3 OVERHEAD EMERGENCY LIGHT AS REQUIRED. OPERATIONAL CHECK GOOD.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 8,608 hrs · 7,512 cycles

AFT EMERGENCY CEILING FLOOD LIGHT INOP. RELAMPED AFT EMERGENCY CEILING LIGHT AS REQUIRED. OPERATIONAL CHECK GOOD. ALL IAW 33-31-16.

Part: PCU — MALFUNCTIONED (SPOILERS) · airframe 7,883 hrs · 6,923 cycles

FLT SPOILERS FAULT (STATUS) ON LEFT WING SIDE. REPLACED NR 2 ACTUATOR FOR LEFT WING FLT SPOILER IAW CRJ MM 27-62-01. OPERATIONAL CHECK GOOD.

Part: WINDOW — CRACKED (COCKPIT) · airframe 7,774 hrs · 6,834 cycles

LEFT SIDE WINDOW ON FLIGHT DECK SHATTERED IN FLIGHT AT FL350, DELTA WAS 8.2. OUTER AND CORE SHATTERED. REMOVED AND REPLACED LT SIDE WINDOW ON FLIGHT DECK IAW CRJ 200 MM ATA CHPT 56-12-01. OPERATIONAL CHECK GOOD. P/N OFF 601R33033-11, S/N OFF 01176H1629.

Part: PCU — MALFUNCTIONED (FLIGHT SPOILERS) · airframe 6,802 hrs · 5,992 cycles

SPOILERONS FAULT STATUS MESSAGE DISPLAYED. REMOVED AND REPLACED RIGHT OUTBOARD PCU. OPERATIONAL CHECK GOOD IAW MM 27-60-00.

Part: LAMP — BURNED OUT (GALLEY EXIT SIGN) · airframe 6,710 hrs · 5,901 cycles

FA REPORTS, EXIT LIGHTS ON GALLEY EXIT SIGN BURNED OUT. REPLACED LAMPS AT GALLEY EXIT SIGN, OPERATIONAL CHECK GOOD.

Part: CONTROL UNIT — MALFUNCTIONED (MOTOR) · airframe 6,384 hrs · 5,627 cycles

STAB CHANEL 1 FALLS OFF LINE. REMOVED AND REPLACED MCU IAW MM 27-42-05. OPERATIONAL CHECK GOOD. PN 7062-3 SN OFF 331.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 5,416 hrs · 4,746 cycles

EMERGENCY LIGHT IN AFT OVERHEAD INOP. RELAMPED AFT OVERHEAD EMERGENCY LIGHT. OPS CHECK GOOD.

Part: SWITCH — STICKING (MACH TRIM) · airframe 4,685 hrs · 4,103 cycles

AFTER ROTATION, STAB TRIM CH 1 AND CH 2 AND MACH TRIM DISCONNECTED AND WOULDN'T RE-ENGAGE. PERFORMED QRH PROCEDURES AND RETURNED TO DENVER. FOUND CAPT'S DISCONNECT BUTTON WAS STICKY (ON YOKE). CLEANED AND CYCLED REPEATEDLY. SYSTEM FUNCTIONING NORMALLY NOW.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 4,088 hrs · 3,582 cycles

FS 484 RT INTERCOSTAL O/B FLANGE CRACKED RBL 36. DISCOVERED DURING C-CHECK. REPAIRED FLANGE IAW CRT REO 601R-53-41-059 REV. 'A'.

Part: SHAFT — CORRODED (ESCAPE HATCH) · airframe 4,088 hrs · 3,582 cycles

CREW ESCAPE HATCH OUTER HANDLE HAS CORROSION ON INNER SHAFT. DISCOVERED DURING C-CHECK. CREW ESCAPE HATCH OUTER HANDLE REPLACED AS PER HARTWELL CMM 52-22-03. P/N: H3419-33

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 4,088 hrs · 3,582 cycles

FS 484 LT INTERCOSTAL OUTBOARD FLANGE CRACKED LBL 36. DISCOVERED DURING C-CHECK. REPAIRED FLANGE IAW CRT REO 601R-53-41-059 REV. 'A'.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 4,088 hrs · 3,582 cycles

FS 621 RT FLOOR SUPPORT ANGLE RBL 42 CRACKED. DISCOVERED DURING C-CHECK. ANGLE REPAIR CARRIED OUT IAW CRJ REO 601R-53-61-117. P/N: 601R53-61-117-2

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 4,088 hrs · 3,582 cycles

FS 621 LT FLOOR SUPPORT ANGLE LBL 42 CRACKED. DISCOVERED DURING C-CHECK. ANGLE REPAIR CARRIED OUT IAW CRJ REO 601R-53-61-117 AND RII 53-401. P/N: 601R-53-61-117-3

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 4,088 hrs · 3,582 cycles

FS 280 RT FLOORBEAM RBL 9.0 INBOARD ATTACH ANGLE CRACKED. DISCOVERED DURING C-CHECK. REPLACED ANGLE IAW CRJ SRM 51-40-11. P/N: 601R-31113-58.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 4,088 hrs · 3,582 cycles

FS 280 LT FLOORBEAM LBL 9.0 INBD ATTACH ANGLE CRACKED. DISCOVERED DURING C-CHECK. REPLACED ANGLE IAW CRJ SRM 51-40-11. P/N: S6144-13

Part: WIRE — BROKEN (RUDDER TRIM) · airframe 3,119 hrs · 2,703 cycles

AFTER LANDING UNABLE TO RE-CENTER RUDDER TRIM, TRIMS ONLY TO THE LEFT, RIGHT TRIM INOP. REPAIRED BROKEN WIRES ON SWITCH. OPS CHECK GOOD.

Part: SHUTOFF VALVE — MALFUNCTIONED (HYD SYSTEM) · airframe 2,453 hrs · 2,156 cycles

HYDRAULIC SYSTEM NR 1 LOW PRESSURE AMBER MESSAGE AND HYD 1A AMBER MESSAGE ON SYNOPTIC PAGE. RETURNED TO DEN. INSTALLED NR 1 HYDRAULIC SHUT OFF VALVE IAW MM 29-11-36. OPS CHECK GOOD. NO DEFECTS NOTED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 2,453 hrs · 2,156 cycles

2ND OVERHEAD EMERGENCY LIGHT IS INOP. RELAMPED WITH 1 GE1317 LAMP. OPS CHECK GOOD.

Part: ACTUATOR — MALFUNCTIONED (HORIZ STAB) · airframe 967 hrs · 936 cycles

STAB CH 1 & 2 AND MACH TRIM FAILED SHORTLY AFTER TAKEOFF. RAN QRH, RESET AND IT FAILED AGAIN. WAS ABLE TO GET ALL TO WORK WHILE FLYING TO BURN OFF GAS. RETURNED TO BOI. REMOVED AND REPLACED MOTOR CONTROL UNIT IAW 27-42-05. REMOVED AND REPLACED HSTA IAW 27-42-01. OPS CHECK GOOD.

Part: POTENTIOMETER — MALFUNCTIONED (APU) · airframe 286 hrs · 295 cycles

APU AUTO SHUTDOWN ON THE INITIATION OF TAKEOFF ROLL. ABORTED TAKEOFF AND TAXIED AIRCRAFT BACK TO THE GATE. FOUND APU DOOR POTENTIOMETER BAD. INSTALLED NEW POTENTIOMETER IAW 49-14-01. RIGGED DOOR AND RAN APU. ALL CHECKS OK AT THIS TIME.