N411SW

Part: STRUT — DEFECTIVE (NLG) · airframe 47,020 hrs · 39,004 cycles

GEAR DISAGREE, NOSE GEAR DID NOT RETRACT. FLT 6215. REPACKED NOSE STRUT. PERFORMED MULTIPLE FUNCTIONAL CHECKS OF LANDING GEAR SYSTEM IAW AMM.

Part: COMPUTER — MALFUNCTIONED (NR 1 AHRS) · airframe 46,492 hrs · 38,569 cycles

AP DISCONNECTED & AIRCRAFT SLIGHTLY YAWED WITH SUBSEQUENT YD1 KICKING OFF LINE. FLT#4569 REPLACED THE NR 1 AHRS COMPUTER IAW AMM. PN ON OFF 622-9336-400, SN ON 1YLLK, SN OFF 1826.

Part: HANDLE — CORRODED (ESCAPE HATCH) · airframe 46,438 hrs · 38,522 cycles

CREW ESCAPE HATCH OUTER HANDLE RUSTED & DEFORMING. SERVICE REPLACED OUTER HANDLE IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 46,159 hrs · 38,324 cycles

GALLEY EMERGENCY LIGHT STRIP HAS A BULB BURNED OUT. FLT#5240 RELAMPED.

Part: UNKNOWN — MALFUNCTIONED (SPOILER SYS) · airframe 45,853 hrs · 38,108 cycles

RT SIDE FLIGHT SPOILER FAULT STATUS MESSAGE DURING DESCENT, AIRCRAFT BANKED UNCOMMANDED. FLT#6214 PERFORMED A FULL AIRCRAFT POWER DOWN & PWER BACK UP. PERFORMED FLIGHT SPOILER & SPOILERON IAW AMM.

Part: CONNECTOR — DISCONNECTED (NLG) · airframe 45,742 hrs · 38,013 cycles

RECEIVED A GEAR DISAGREE WARNING MESSAGE. COMPLIED WITH QRH & SUCCESSFULLY LOWERED LANDING GEAR. FLT#6192 REPOSITIONED SAFETY WIRE & RECONNECTED NOSE GEAR DOOR SELECTOR VALVE CANNON PLUG IAW AMM OPERATIONS CHECK OF NOSE GEAR DOORS GOOD AT THIS TIME. COMPLIED WITH REPEATED EXTENSION/RETRACTION CYCLES OF LANDING GEAR. OPERATIONS CHECKED GOOD.

Part: SKIN — CHAFED (TE FLAP) · airframe 45,638 hrs · 37,930 cycles

RIGHT SIDE INBD FLAP SKIN CHAFED UNDER PANEL 684CB. C-CHECK, BLENDED CHAFE ON INNER DOUBLER OF THE RIGHT SIDE INBD FLAP UPPER SKIN INNER DOUBLER UNDER LOWER ACCESS PANEL 684CB IAW REO.

Part: SKIN — CHAFED (TE FLAP) · airframe 45,638 hrs · 37,930 cycles

RT SIDE INBD FLAP SKIN CHAFED UNDER PANEL 684BB. C-CHECK, BLENDED CHAFE ON INNER DOUBLER OF THE RIGHT SIDE INBD FLAP SKIN UNDER THE LOWER ACCESS PANEL 684BB, IAW REO.

Part: SKIN — CHAFED (TE FLAP) · airframe 45,638 hrs · 37,930 cycles

RIGHT SIDE INBD FLAP SKIN CHAFED UNDER PANEL 684AB. C-CHECK, BLENDED CHAFE ON INNER DOUBLER OF THE RIGHT SIDE INBD FLAP UNDER LOWER ACCESS PANEL 684AB, IAW REO.

Part: SKIN — CHAFED (TE FLAP) · airframe 45,638 hrs · 37,930 cycles

LEFT SIDE INBD FLAP SKIN CHAFED UNDER PANEL 584AB. C-CHECK, BLENDED CHAFE ON INNER DOUBLER OF THE LEFT SIDE INBD FLAP UPPER SKIN INNER DOUBLER, UNDER LOWER ACCESS PANEL 584AB IAW REO.

Part: POST — CRACKED (FUSELAGE) · airframe 45,638 hrs · 37,930 cycles

FS 409.0+128 RBL 18.00 CRACK INDICATIONS NOTED ON INBD, OTBD VERTICAL POST AFT RADIUS. C-CHECK INSTALLED INBD, OTBD VERTICAL POST IAW SRM AND REO.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 45,638 hrs · 37,930 cycles

CRACKED LT FLOOR EDGE MEMBER SILL FLOOR SUPPORT AT FS 589 (C-CHECK)REPAIR TO CRACK ON THE LT FLOOR EDGE MEMBER SILL FLOOR SUPPORT IAW REO.

Part: SKIN — CHAFED (CARGO DOOR) · airframe 45,638 hrs · 37,930 cycles

CARGO DOOR CHAFED UPPER CENTER. C-CHECK BLENDED OUT CHAFING DAMAGE ON UPPER CENTER OUTSIDE SKIN OF CARGO DOOR IAW REO.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 44,248 hrs · 36,853 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5651) RELAMPED EMERGENCY LIGHT.

Part: CHARGER — FAILED (CABIN) · airframe 43,964 hrs · 36,545 cycles

EXTERIOR EMERGENCY LIGHTS ARE OUT. (FLT 4603) REPLACED NR 3 ELBP CHARGER IN REFERENCE TO AMM.

Part: INVERTER — FAILED (CABIN) · airframe 43,947 hrs · 36,528 cycles

LOWER EMERGENCY EXIT SIGN AT SEAT 8D IS INOPERATIVE. (FLT 4494) REPLACED INVERTER NR 3 IN REFERENCE TO CRJ200 AMM.

Part: TRIM PANEL — FAILED (COCKPIT) · airframe 43,097 hrs · 35,737 cycles

RUDDER TRIM TRIMMED TO THE LEFT ON IT'S OWN IN FLIGHT. (FLT 4551) REPLACED RUDDER/AILERON TRIM PANEL IN REFERENCE TO AMM. P/N OFF: 601R51226-23SW1

Part: LIGHT — INOPERATIVE (CABIN) · airframe 42,653 hrs · 35,352 cycles

NR 4 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4820) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 41,466 hrs · 34,238 cycles

FORWARD LEFT WING EXTERIOR EMERGENCY LIGHT IS OUT. (SERVICE) RELAMPED EMERGENCY LIGHT.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 41,818 hrs · 34,547 cycles

FLOORBEAM CORRODED AT OUTBOARD END AND WEB SECTION FS 349 RBL 36. (C-CHECK) REPAIRED PER SRM.

Part: GUSSET — CORRODED (FUSELAGE) · airframe 41,818 hrs · 34,547 cycles

FORWARD AND AFT GUSSETS AT FS 314.0, 340.0 ARE CORRODED. (C-CHECK) REPLACED FORWARD AND AFT GUSSETS AT FS 314 AND FS 340 PER SRM.

Part: POST — CRACKED (FUSELAGE) · airframe 41,818 hrs · 34,547 cycles

VERTICAL POST AT FS 409+128, LBL 18 CRACKED IN AFT RADIUS OF "C" CHANNEL. (C-CHECK) REPLACED FS 409+128 VERTICAL POST PER SRM.

Part: ALTIMETER — MALFUNCTIONED (COCKPIT) · airframe 40,894 hrs · 33,720 cycles

STANDBY ALTIMETER MORE THAN 300 FEET OFF OF FIELD ELEVATION. (SERVICE) REPLACED STANDBY ALTIMETER/AIRSPEED INDICATOR. P/N WL102AMS5, S/N ON AP333, S/N OFF AN957.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 40,001 hrs · 32,958 cycles

NR 2 EMERGENCY LIGHT ON MAIN CABIN DOOR STAIRS OUT. (FLT 4736) RELAMPED EMERGENCY LIGHT.

Part: BUSHING — DAMAGED (ENGINE MOUNT) · airframe 39,858 hrs · 32,833 cycles

RIGHT ENGINE AFT THRUST MOUNT SPHERICAL BUSHING IS PITTED. (ENGINE CHANGE) REMOVED AND REPLACED RIGHT ENGINE AFT THRUST MOUNT SPHERICAL BUSHING.

Part: BUSHING — GALLED (ENGINE MOUNT) · airframe 39,858 hrs · 32,833 cycles

RIGHT ENGINE FORWARD YOKE MOUNT SPHERICAL BEARINGS ARE GALLED. (ENGINE CHANGE) REMOVED AND REPLACED RIGHT ENGINE FORWARD YOKE MOUNT.

Part: PIN — GALLED (ENGINE MOUNT) · airframe 39,858 hrs · 32,833 cycles

RIGHT ENGINE, YOKE MOUNT PINS HAVE GALL MARKS. (ENGINE CHANGE) INSTALLED SERVICEABLE RIGHT ENGINE FORWARD YOKE MOUNT PINS.

Part: BUSHING — GALLED (ENGINE MOUNT) · airframe 39,858 hrs · 32,833 cycles

RIGHT ENGINE FORWARD YOKE MOUNT LINK BUSHINGS ARE GALLED. (ENGINE CHANGE) REMOVED AND REPLACED RIGHT ENGINE FWD MOUNT LINK ASSEMBLY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 39,321 hrs · 32,379 cycles

AFT CABIN CEILING EMERGENCY LIGHT INOP. (FLT 4656) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 37,880 hrs · 31,179 cycles

LAST OVERHEAD EMERGENCY LIGHT INOP. (FLT 4464) RELAMPED EMERGENCY LIGHT.

Part: WINDOW — CRACKED (COCKPIT) · airframe 37,037 hrs · 30,511 cycles

CAPTAINS SIDE WINDOW CRACKED. (FLT 1021) REPLACED SIDE WINDOW.

Part: DOOR FRAME — CRACKED (PAX DOOR) · airframe 37,320 hrs · 30,732 cycles

PASSENGER DOOR INTERNAL FRAME CRACKED. (C CHECK) REPAIRED PER REO.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 37,320 hrs · 30,732 cycles

FS 202 BULKHEAD CRACKED. (C CHECK) REPAIRED PER REO.

Part: POST — CRACKED (COCKPIT) · airframe 37,320 hrs · 30,732 cycles

RIGHT COCKPIT WINDOW SIDE POST FITTING CRACKED. (C CHECK) REPAIRED PER SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 37,320 hrs · 30,732 cycles

FS 484 INTERCOSTAL ANGLE CRACKED. (C CHECK) REPAIRED PER SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 37,320 hrs · 30,732 cycles

FS 621 WEB, CLIPS, AND ISOLATOR CRACKED. (C CHECK) REPAIRED PER REO AND SRM.

Part: STRUCTURE — GOUGED (FUSELAGE) · airframe 37,320 hrs · 30,732 cycles

FS280 GOUGED. (C CHECK)REPAIRED PER REO.

Part: LAMP — BURNED OUT (EMERGENCY LIGHTS) · airframe 36,914 hrs · 30,413 cycles

FLT 4400 - AFT CEILING EMERGENCY LIGHT INOP. RELAMPED.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 36,724 hrs · 30,271 cycles

FLT 4690 - ONE EXTERNAL EMERGENCY LIGHT INOP ON LEFT SIDE. RELAMPED.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 35,964 hrs · 29,696 cycles

FLT 4859 - AFT CEILING LEVEL EMERGENCY FLOODLIGHT INOP. RELAMPED.

Part: SELECTOR VALVE — MALFUNCTIONED (NLG) · airframe 35,000 hrs · 28,941 cycles

WHILE SELECTING GEAR DOWN, RECEIVED A TRIPLE CHIME "GEAR DISAGREE" AND "NOSE GEAR DOOR" AURAL WARNING. (FLT 3812) REPLACED NOSE GEAR SELECTOR VALVE IAW AMM 32-33-01. OPS CHECKS GOOD.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 34,834 hrs · 28,809 cycles

FLT 3757 - RIGHT WING FORWARD EMERGENCY EXIT LIGHT IS INOP. REPLACED EMERGENCY BULB. OPS CHECK GOOD.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 34,513 hrs · 28,570 cycles

FLT 3951 - RIGHT WINDSHIELD CRACKED ON TAXI OUT. REPLACED THE FIRST OFFICER WINDSHIELD IAW AMM 56-11-01, P/N NP-139321-6, S/N OFF 016095H3873.

Part: WINDSHIELD — FAILED (COCKPIT) · airframe 34,335 hrs · 28,434 cycles

FLT 3774 - LEFT WINDSHIELD SHATTERED INFLIGHT. REPLACED LEFT WINDSHIELD IAW AMM 56-11-01. OPS CHECK GOOD, P/N OFF: NP-139321-9, S/N OFF: 01200H3576.

Part: SELECTOR VALVE — MALFUNCTIONED (NLG) · airframe 34,084 hrs · 28,237 cycles

FLT 3767 - NOSE GEAR WOULD NOT EXTEND. REPLACED NOSE GEAR DOOR SELECTOR VALVE IAW AMM 32-22-20.

Part: SMOKE WARNING — FALSE ACTIVATION (LAVATORY) · airframe 34,002 hrs · 28,174 cycles

FLT 4114 - SMOKE TOILET CAUTION MESSAGE APPEARED. INSPECTED RIGHT ENGINE, AIR CYCLE MACHINE AND ASSOCIATED DUCTING FOR SIGNS OF CONTAMINATION WITH NO DISCREPANCIES NOTED. RAN ENGINES AT FULL POWER FOR 30 MINUTES AND COULD NOT DUPLICATE. OPS CHECK OF LAV SMOKE DETECTOR GOOD.

Part: ACTUATOR — FAILED (THRUST REVERSER) · airframe 32,793 hrs · 27,257 cycles

RIGHT THRUST REVERSER UNLOCK CAUTION MESSAGE ILLUMINATED IN FLIGHT. RETURNED TO FIELD. REPLACED RIGHT LOWER INBOARD THRUST REVERSER BALLSCREW ACTUATOR IAW MM 78-32-01.

Part: HINGE — CORRODED (LT ELEVATOR) · airframe 33,025 hrs · 27,418 cycles

LEFT ELEVATOR OUTBOARD HINGE HARDWARE IS CORRODED, FOUND AT C-CHECK. REPLACED CORRODED HARDWARE AND BUSHINGS PER CRJ200 AMM 27-34-01-000-801 STEPS G THRU-1-5.

Part: INVERTER — MALFUNCTIONED (CABIN) · airframe 31,790 hrs · 26,478 cycles

FOUND FLOOR EMERGENCY LIGHT AT RIGHT EXIT INOP. REPLACED INVERTER. OPERATIONAL CHECKS GOOD.

Part: WINDSHIELD — MALFUNCTIONED (COCKPIT) · airframe 30,513 hrs · 25,543 cycles

SLIGHT ELECTRICAL BURNING SMELL, ON DESCENT. REPLACED FO'S WINDSHIELD IAW AMM 56-11-01 AND RII 56-220-1000. OPERATIONAL CHECKS GOOD.

Part: BPSU — OUT OF RIG (TE FLAPS) · airframe 29,330 hrs · 24,653 cycles

FLAPS FAIL CAUTION MESSAGE EN ROUTE. RIGGED BPSU'S IAW MM 27-51-10, OPERATIONAL CHECK GOOD.

Part: SENSOR — MALFUNCTIONED (BRAKE POSITION) · airframe 29,218 hrs · 24,565 cycles

AFTER T/O FLAPS FAIL AFTER MOVING FROM 8-0 FLAPS. REPLACED LEFT AND RIGHT BPSU'S IAW 27-51-10 AND 27-54-00. OPERATIONAL CHECK GOOD, PN 855D100-9, SN/OFF 1097B, PN 855D100-9, SN/OFF 1474B.

Part: PDU — MALFUNCTIONED (FLAPS) · airframe 28,808 hrs · 24,270 cycles

FLAPS HALFSPEED STATUS MSG DURING APPROACH . REPLACED FLAP PDU, OPERATIONAL CHECK GOOD REF MM 27-52-02.

Part: WIRE — BROKEN (STICK SHAKER) · airframe 28,703 hrs · 24,190 cycles

AFTER TAKEOFF, THE STALL FAIL MESSAGE CAME ON FOLLOWED BY YD1 INOP STATUS MESSAGE. REPAIRED BROKEN WIRE ON CAPTS STICK SHAKER. OPERATIONAL CHECK GOOD.

Part: INTERCOSTAL — CRACKED (BS 449) · airframe 29,381 hrs · 24,691 cycles

INTERCOSTAL FLANGE CHAFED ON LT SIDE FUSELAGE AT FS 449.85 BETWEEN STRINGER 8 AND 9. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED REF REO 601R-53-41-375.

Part: VERTICAL BEAM — CRACKED (BS 409) · airframe 28,609 hrs · 24,109 cycles

FUSELAGE; VERTICAL BEAM; LOWER I/B + O/B FLANGE IS CRACKED; FS 409.0 + 128; LBL 27.0, ITEM FOUND AT C-CHECK INSPECTION. REPAIR IAW CRJ REO 601R-53-41-056 REV "C" .

Part: SUPPORT ANGLE — CRACKED (BS 605) · airframe 28,609 hrs · 24,109 cycles

CRACKED SUPPORT ANGLE UNDER CARGO DOOR SILL AT STA 605 LBL 42, ITEM FOUND AT C-CHECK INSPECTION. REPLACED CLIP IAW CRJ REO 601R-53-61-100 REV NC & REO 601R-53-61-422 REV NC.

Part: CLIP — CRACKED (BS 625) · airframe 28,609 hrs · 24,109 cycles

AFT EQUIPMENT COMP; INTERCOSTAL CLIP CRACKED; FS 625.00 STR 14L, ITEM FOUND AT C-CHECK INSPECTION. REPLACED CLIP IAW CRJ REO 601R-53-61-100 REV NC & REO 601R-53-61-422 REV NC.

Part: VERTICAL BEAM — CRACKED (BS 409) · airframe 28,609 hrs · 24,109 cycles

FUSELAGE; VERTICAL BEAM; LOWER O/B FLANGE IS CRACKED; FS 409.0 + 128; RBL - 18.0, ITEM FOUND AT C-CHECK INSPECTION. REPAIRED LOWER O/B FLANGE IAW CRJ REO 601R-53-41-056 REV "C".

Part: SUPPORT ANGLE — CRACKED (BS 589) · airframe 28,609 hrs · 24,109 cycles

CRACKED SUPPORT ANGLE UNDER CARGO DOOR SILL AT STA 589 LBL 42, ITEM FOUND AT C-CHECK INSPECTION.

Part: VERTICAL BEAM — CRACKED (BS 559) · airframe 29,381 hrs · 24,691 cycles

FUSELAGE; VERTICAL BEAM; LOWER I/B + O/B FLANGES ARE CRACKED FS 559.00; LBL 9.0. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED IAW REO 601R-53-41-377 AND 601R-53-41-057.

Part: PRESSURE PANEL — CRACKED (BS 621) · airframe 29,381 hrs · 24,691 cycles

CARGO COMPARTMENT AFT PRESSURE WEB FS 621 LINTEL INSTALLATION CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED WEB IAW CRJ REO 601R-53-61-1230 REV C.

Part: VERTICAL BEAM — CRACKED (BS 409) · airframe 28,609 hrs · 24,109 cycles

FUSELAGE; VERTICAL BEAM; LOWER I/B + O/B FLANGES ARE CRACKED; FS 409.0 + 128; RBL 27.0, ITEM FOUND AT C-CHECK INSPECTION. REPAIR LOWER I/B & OB FLANGES, FS 409.0 + 128; RBL 27.0 IAW CRJ REO 601R-53-41-056 REV "C".

Part: VERTICAL BEAM — CRACKED (BS 409) · airframe 28,609 hrs · 24,109 cycles

FUSELAGE; VERTICAL BEAM; LWR O/B FLANGE IS CRACKED; FS 409.0 + 128; LBL -18, ITEM FOUND AT C-CHECK INSPECTION. REPAIRED FUSELAGE, VERTICAL BEAM, LWR O/B FLANGE, FS 409.0 + 128, LBL -18 IAW CRJ REO 601R-53-41-379 REV "NC".

Part: FRAME — CRACKED (PAX DOOR) · airframe 29,381 hrs · 24,691 cycles

SUB FRAME CRACKED AT FS 323.6 ON PAX DOOR UPPER END. ITEM FOUND AT C-CHECK INSPECTION. PAX DOOR SUB-FRAME AT STA 323.6 REPLACED IAW CRJ SRM 51-40-11, 51-25-06, 51-23-00, 51-21-16, 51-42-06, 51-42-10 FIG 4, 51-42-13, 51-42-21.

Part: STEP — CRACKED (PAX DOOR) · airframe 29,381 hrs · 24,691 cycles

PAX DOOR, TOP STEP, AFT SIDE WEB, CRACKED ON INBOARD RETURN FLANGE, FS 340.0. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED IAW CRJ REO 601R-52-11-702 REV NC.

Part: WEB — CRACKED (BS 724) · airframe 28,609 hrs · 24,109 cycles

WEB CRACKED AT FS 724.0 AT STR 24L, ITEM FOUND AT C-CHECK INSPECTION. EDDY CURRENT INSP COMPLETED ON SUSPECT CRACK AREA IAW CRJ 200 NDTM PT 1 51-20-06. NO CRACK INDICATION NOTED. NO FURTHER ACTION REQUIRED.

Part: CLIP — CRACKED (BS 625) · airframe 28,609 hrs · 24,109 cycles

AFT EQUIPMENT COMP; INTERCOSTAL CLIP IS CRACKED; FS 625.00 STR 14R, ITEM FOUND AT C-CHECK INSPECTION. REPLACED CLIP IAW CRJ REO 601R-53-61-100, REV NC & REO 601R-53-61-422 REV NC.

Part: PRESSURE PANEL — CRACKED (BS 621) · airframe 29,381 hrs · 24,691 cycles

CARGO COMPARTMENT AFT PRESSURE WEB FS 621 LBL 27.5 WL 130 CRACKED. ITEM FOUND AT C-CHECK INSPECTION. WEB REPAIR CARRIED OUT REF RII 53-401 & M-337.

Part: BULKHEAD — CRACKED (BS 559) · airframe 28,609 hrs · 24,109 cycles

RT MLG BAY; REAR PRESSURE BULKHEAD IS CRACKED AT AILERON QUADRANT; FS 559.00; RBL 17.0 + RBL 10.0, ITEM FOUND AT C-CHECK INSPECTION. REPAIRED REAR PRESSURE BULKHEAD AT FS 559.00, RBL 17.0 & RBL 10.0 IAW CRJ REO 601R-53-41-260 REV "A".

Part: FRAME — CRACKED (BS 336) · airframe 28,609 hrs · 24,109 cycles

SUSPECT CRACK IN FRAME IN PAX DOOR AT APPROX STA 336 AT TOP OF DOOR, ITEM FOUND AT C-CHECK INSPECTION. PAX DOOR SUB-FRAME AT STQ 335.70 REPLACED IAW CRJ SRM 51-40-11, 51-25-06, 51-23-00, 51-21-16, 51-42-06, 51-42-10 FIG 4, 51-42-13, 51-42-21.

Part: LATCH — BINDING (PAX DOOR) · airframe 28,478 hrs · 24,010 cycles

MAIN CABIN DOOR IS VERY DIFFICULT TO LATCH CLOSED OR OPEN USING THE INTERIOR HANDLE. LUBRICATED MAIN CABIN DOOR LATCH PINS, OPERATIONAL CHECKS GOOD.

Part: CONTROL UNIT — MALFUNCTIONED (HORIZONTAL STAB) · airframe 26,368 hrs · 22,375 cycles

CREW REPORTS STAB CHANNEL 1 WON'T STAY ENGAGED IN FLIGHT. REMOVED AND REPLACED MOTOR CONTROL UNIT AND HORIZONTAL STAB TRIM ACTUATOR IAW 27-42-05 AND 27-42-01. OPERATIONAL CHECK GOOD. P/N 7062-3, S/N OFF 704, P/N 8396-3, S/N OFF 693.

Part: CONTROL UNIT — MALFUNCTIONED (HORIZ STAB TRIM) · airframe 26,296 hrs · 22,319 cycles

MACH TRIM MESSAGE (AMBER) WHEN F/O USES YOKE SWITCH. REPLACED PITCH TRIM SWITCH IAW 27-41-05. REPLACED HSTCU IAW 27-41-01. OPERATIONAL CHECK GOOD.

Part: CONTROL UNIT — MALFUNCTIONED (HORIZ STAB TRIM) · airframe 26,280 hrs · 22,307 cycles

MACH TRIM DISENGAGES WHEN CAPTAINS PITCH TRIM IS ACTUATED. REPLACED MACH TRIM ENGAGE/DISENGAGE SWITCH IAW MM 27-41-25. REPLACED HSTCU IAW CRJ MM 27-41-01. OPERATIONAL CHECK GOOD.

Part: WINDOW — CRACKED (COCKPIT) · airframe 25,878 hrs · 21,991 cycles

ON POST FLIGHT INSPECTION, FIRST OFFICERS FORWARD WINDOW CRACKED ON OUTER PANE. REMOVED AND REPLACED RIGHT WINDSHIELD WITH SERVICEABLE UNIT IAW MM 56-11-01. P/N: NP-139321-12, S/N OFF: 94259H4059.

Part: CONNECTOR — CONTAMINATED (EMERGENCY LIGHT) · airframe 24,944 hrs · 21,261 cycles

FLOOR EMERGENCY LIGHTS BEHIND ROW 9 WILL NOT ILLUMINATE. CLEANED CONTAMINATED CONNECTION AT LAV. OPERATIONAL CHECK GOOD.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 24,731 hrs · 21,086 cycles

FS 484 ANGLE JUST OUTBOARD OF LBL 9 CRACKED. DISCOVERED DURING C-CHECK INSPECTION. INSTALLED ANGLE IAW BRAS EO 601R-53-4997 ON FS 484 LBL 9 STEPS 6-9.

Part: SERVO — FAILED (AUTOPILOT) · airframe 23,976 hrs · 20,508 cycles

AUTOPILOT JERKS LEFT AND RIGHT MAINLY IN TURNS AND MOST PRONOUNCED WHEN SELECTING AND DE-SELECTING TURBULENCE BUTTON. REMOVED AND REPLACED RIGHT AUTO PILOT SERVO IAW 22-11-21. OPS CHECK GOOD. P/N: 622-4404-101, S/N OFF: 122.

Part: PDU — MALFUNCTIONED (T/E FLAP) · airframe 22,597 hrs · 19,440 cycles

FLAPS HALF SPEED MESSAGE. REPLACED FLAP PDU WITH SERVICEABLE UNIT IAW MM 27-52-01. OPS CHECK GOOD. S/N OFF: 161.

Part: PCU — MALFUNCTIONED (SPOILER) · airframe 22,598 hrs · 19,440 cycles

DURING GLD FFOD WHEN (MAN ARM) IS SELECTED OR FLT SPOILERS EXTENDED THE (FLT SPOILERS FAULT) STATUS MSG IS DISPLAYED. RESET CB'S IAW, FAULT MSG. STILL CAME ON. REMOVED AND REPLACED LEFT INBOARD FLIGHT SPOILER PCU W/SERVICEABLE UNIT IAW MM 27-62-01. OPS CHECK GOOD . P/N: 27000-7

Part: ECU — MALFUNCTIONED (SPOILER) · airframe 22,501 hrs · 19,375 cycles

INFLIGHT SLIGHT ROLLING MOTION (UNCOMMANDED) LEFT ACCOMPANIED BY FLIGHT SPOILERS FAULT STATUS MESSAGE. LEFT INBD GRND SPOILER BOXED IN WHITE. REMOVED AND REPLACED NR 2 SECU IAW CRJ MM 27-61-00 & 21-61-05. OPS CHECK GOOD.

Part: COALESCER BAG — CONTAMINATED (AIR DISTRIBUTION) · airframe 22,119 hrs · 19,075 cycles

AFTER STARTING THE APU AND BRINGING ON BOTH PACKS, GOT SMOKE INTO THE FLIGHT DECK AND THE CABIN. SMOKE WAS COMING FROM THE AIR CONDITIONING SYSTEM. ALSO GOT A SMOKE CAUTION MESSAGE. REMOVED AND REPLACED BOTH RIGHT AND LEFT ACM WATER SEPARATOR SOCKS WITH SERVICEABLE UNITS IAW MM 21-51-13. CHECKS GOOD AT THIS TIME.

Part: ODOR — DETECTED (COCKPIT) · airframe 21,997 hrs · 18,976 cycles

AFTER LANDING AND CLEARING RUNWAY, TRANSFERED BLEEDS TO APU OPEN AND COCKPIT FILLED WITH SMOKE AND A STRONG BURNING ODOR. RAN ENGINES EXCESSIVELY WITH BOTH PACKS ON. NO SMOKE OR BURNING ODOR. TRANSFERRED BLEEDS OVER TO APU. RAN FOR 1/2 HR, NO SMOKE OR BURNING ODOR. OPS CHECK GOOD. UNABLE TO DUPLICATE.

Part: WARNING LIGHT — FALSE INDICATION (14TH STAGE DUCT) · airframe 21,355 hrs · 18,498 cycles

SHORTLY AFTER TAKEOFF RED L 14TH STAGE DUCT MESSAGE. MESSAGE WENT OUT WITH AFFECTED THRUST REDUCED TO IDLE. INSPECTED 14TH STAGE LT NAC DUCT AND LOOP. FOUND NO PROBLEMS. CHECKED LOOP CONNECTORS WITH NO PROBLEMS. LEAK CHECKED LT 14TH STAGE NAC DUCT, NO LEAKS. OPERATED SYSTEM. OPS CHECK GOOD.

Part: ANTI-ICE VALVE — MALFUNCTIONED (RIGHT) · airframe 21,030 hrs · 18,255 cycles

RIGHT COWL ANTI-ICE CAUTION MESSAGE WITH RIGHT COWL SWITCH IN THE ON POSITION AIRBORNE. RAN QRH PROCEDURE, NOT EFFECTIVE. RETURNED TO ELP. REMOVED AND REPLACED RIGHT ENGINE COWL ANTI-ICE VALVE IAW MM 30-22-01. OPS CHECK GOOD. S/N OFF: 2173.

Part: FRAME — CORRODED (FS 364) · airframe 20,700 hrs · 17,995 cycles

FRAME AT FS 364 BETWEEN STR 25P AND 25S CORRODED BEYOND LIMITS. FOUND DURING C CHECK INSPECTION. REPLACED FRAME SECTION IAW CRJ SRM 51-40-06, 51-40-11, 51-42-06, 51-42-21, 51-23-00.

Part: FLOOR PANEL — CRACKED (E/E BAY) · airframe 20,683 hrs · 17,982 cycles

ELECTRICAL BAY FLOOR FS 193.0 RIGHT AND LEFT SIDES CRACKED. FOUND DURING C CHECK INSPECTION. HFEC INSPECTION CARRIED OUT ON CUTOUT REPAIR EDGE AND AREA AS REQUIRED IAW REO 601R-53-11-245. NO CRACKS FOUND. REPAIRED DAMAGED AREA IAW CRJ REO 601R-53-11-245 REV. ''NC''. REINSTALLED ADG PUMP IAW CRJ AMM 24-23-19-401-801.

Part: FRAME — CRACKED (FS 640, STR 9S) · airframe 20,683 hrs · 17,982 cycles

FRAME AT FS 640 IS CRACKED AT STR 9S. FOUND DURING C CHECK INSPECTION. FRAMED REPAIRED IAW CRJ REO 601R-53-61-532. HFEC INSPECTION CARRIED OUT ON CUTOUT REPAIR EDGE AS REQUIRED IAW REO 601R-53-61-532/RJ NDTM 51-20-06. NO CRACKS FOUND.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 20,683 hrs · 17,982 cycles

FS 280 PILOT'S BULKHEAD FLOORBEAM CRACKED AT RBL 9.0 & LBL 9.0. FOUND DURING C CHECK INSPECTION. HFEC INSPECTION CARRIED OUT ON CUTOUT REPAIRS AS REQUIRED IAW RJ NDTM 51-20-06. NO CRACKS FOUND. REPAIRED DAMAGED AREA IAW CRJ REO 601R-53-11-171, REV. ''NC''.

Part: CHANNEL — CRACKED · airframe 20,683 hrs · 17,982 cycles

#2 PRESSURE AND RETURN MANIFOLD CHANNEL CRACKED THROUGH BOLT HOLE. FOUND DURING C CHECK INSPECTION. FITTED AND INSTALLED NEW CHANNEL IAW SRM 51-40-11, 51-42-06. RE-INSTALLED HYDRAULIC COMPONENTS IAW CRJ MM CH. 49-11-05. P/N: 600-75221-130

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 20,700 hrs · 17,995 cycles

FS 280 PILOT'S BULKHEAD RBL AND LBL 9.0 AFT UPPER FLOORBEAM CRACKED. FOUND DURING C CHECK INSPECTION.HFEC INSPECTION CARRIED OUT ON CUTOUT REPAIR AS REQUESTED IAW RJ NDTM 51-20-06. NO CRACKS FOUND. REPAIRED DAMAGED AREA IAW CRJ REO 601R-53-11-137 REV. ''NC''.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 20,683 hrs · 17,982 cycles

FS 280.0 RBL 9.0 INBOARD FLOOR SUPPORT ANGLE CRACKED. FOUND DURING C CHECK INSPECTION. FIT AND INSTALLED NEW ANGLE IAW CRJ SRM 51-40-11, 51-42-06, AND 51-42-21.

Part: ECU — FAULTY (APU) · airframe 19,721 hrs · 17,232 cycles

DURING START OF APU, APU HANGS AT 9 PERCENT. STARTED ON FOURTH ATTEMPT WHICH RESULTED IN FIRE IN THE TAILPIPE, CAUSING DELAMINATION TO THE LOWER SIDE OF RIGHT ENGINE PYLON. REMOVED AND REPLACED APU IAW MM 49-10-00 DUE TO HIGH EGT & METAL ON CHIP DETECTOR. APU PN/ ON 3800488-3, S/N OFF P-676. ALSO REMOVED AND REPLACED APU ECU S/N OFF 44-F001. (THE CAUSE OF THE HUNG STARTS). OPS CHECK GOOD. PYLON REPAIRED IAW REO 601R-54-62-037.

Part: HYDRAULIC LINE — LEAKING (HYD SYSTEM) · airframe 19,255 hrs · 16,868 cycles

HYDRAULIC SYSTEM NR 2 LOST ALL FLUID INFLIGHT. REMOVED AND REPLACED RIGHT ENGINE HYDRAULIC PUMP (EDP). PERMA SWAGGED PRESSURE LINE NR 2 SYSTEM AT ACCUMULATOR. RAN ENGINE AND ELECTRICAL PUMP. SERVICED SYSTEM. NO LEAKS NOTED. PERFORMED OPS CHECKS OF FLIGHT CONTROLS ASSOCIATED WITH NR 2 SYSTEM. OPS CHECKS GOOD.

Part: WARNING SYSTEM — MALFUNCTIONED (COCKPIT) · airframe 18,131 hrs · 16,020 cycles

LEFT PITOT, AOA, BASE HEAT, AND MACH TRIM CAUTION MESSAGES ON TAKEOFF. RETURNED TO DFW. POWERED DOWN/POWERED UP. REINITIALIZED COMPUTER. MESSAGES CLEARED. NO DEFECTS.

Part: CONTROLLER — MALFUNCTIONED (CABIN PRESSURE) · airframe 18,131 hrs · 16,020 cycles

AIRCRAFT WOULD NOT PRESSURIZE IN FLIGHT. RETURNED TO PHX. PERFORMED SINGLE PACK TRANSFER PROCEDURE IN MEL APPENDIX O-1A. CHECKS GOOD.

Part: PCU — MALFUNCTIONED (SPOILER) · airframe 17,674 hrs · 15,665 cycles

LEFT OUTBOARD FLIGHT SPOILER TURNS WHITE WHILE PERFORMING GROUND TEST, ALSO SPOILERON FAULT MESSAGE. REMOVED AND REPLACED LEFT INBOARD SPOILER PCU IAW CRJ MM 27-62-01. OPS AND LEAK CHECK GOOD. P/N: 27000-5 S/N OFF: MAL0566

Part: PCU — FAULTY (SPOILER) · airframe 16,488 hrs · 14,713 cycles

ABORTED TAKEOFF DUE TO FLIGHT SPOILER WARNING EICAS MESSAGE WITH TAKEOFF CONFIG OK. MESSAGE FOR FLIGHT SPOILER WARNING AT APPROX 80 N1. PERFORMED AN OPS CHECK OF THE FLIGHT SPOILER WARNING AT 80 PERCENT N1 AND TAKEOFF CONFIGURATION. OK, NO WARNING NOTED. REMOVED AND REPLACED LEFT FLIGHT SPOILER OUTBOARD PCU IAW MM 27-62-01. P/N ON 27000-7, S/N ON 0474, S/N OFF 0514.

Part: ACTUATOR — INOPERATIVE (HORIZ STAB) · airframe 16,153 hrs · 14,405 cycles

STAB TRIM WILL NOT OPERATE (PILOT OR COPILOTS) USING STAB TRIM CH-2. REMOVED AND REPLACED MOTOR CONTROL UNIT. REMOVED AND REPLACED HORIZONTAL STABILIZER ACTUATOR, REF MM 27-42-61, 27-42-05. OPS CHECK GOOD ON BOTH CHANNELS. MEETS CAT II STANDARDS. CONTROL UNIT (P/N: 7062-3) (S/N ON: 329) (S/N OFF: 215). ACTUATOR (P/N: 8396-3) (S/N ON: 177) (S/N OFF: 281).

Part: CONNECTOR — FAILED (EVAC LIGHTS) · airframe 16,046 hrs · 14,312 cycles

LOWER EXIT LIGHT AT SERVICE DOOR WILL NOT ILLUMINATE. FORWARD FLOOR ORANGE EMERGENCY STRIP LIGHTS WILL NOT ILLUMINATE AND FLOOR LEVEL EXIT SIGN AT PAX DOOR INOP. REMOVED AND REPLACED CONNECTOR AT LOWER EXIT LIGHT AT SERVICE DOOR ON WIRE NUMBER P10LY. OPS CHECKS GOOD. EMERGENCY LIGHTING OPS CHECKS GOOD.

Part: INDICATOR — MALFUNCTIONED (COCKPIT) · airframe 15,898 hrs · 14,182 cycles

EFIS COMP MONITOR HDG FLAGS BOTH SIDES, INDICATION LASTED ONE MINUTE. ABORTED TAKEOFF. PERFORMED OPS CHECK OF THE EFIS COMP MONITOR SYSTEM. OPS CHECK GOOD IAW CRJ MM 34-20-00.

Part: PROBE — FAILED (TAT) · airframe 15,898 hrs · 14,182 cycles

TAT PROBE HEAT CAUTION IN FLIGHT. REMOVED AND REPLACED TAT PROBE IAW CRJ MM 34-11-11. OPS CHECK GOOD. P/N: 102AH2AG, S/N ON: A2058, S/N OFF: A4036.

Part: GENERATOR — FAILED (LEFT) · airframe 15,072 hrs · 13,451 cycles

ON TAKEOFF FROM BTM, LOST LEFT GENERATOR. ABORTED TAKEOFF. FOUND LEFT IDG OIL LEVEL LOW. SERVICED OIL IAW 12-13-00, OPS CHECKS GOOD.

Part: WARNING SYSTEM — FALSE INDICATION (PAX DOOR) · airframe 14,839 hrs · 13,231 cycles

AFTER TAKEOFF, MAIN CABIN DOOR HANDLE POPPED OUT. RETURNED TO FAT. INSPECTED, FOUND FAULT AT PSEU D113, D116, D117. CLEARED FAULTS AND INSPECTED PASSENGER DOOR OPERATION. GROUND CHECKS NORMAL. NO DEFECTS NOTED.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 14,760 hrs · 13,158 cycles

AFTER LEAVING SLC, LEFT AND RIGHT AOA HEAT, RIGHT STATIC AND RIGHT PITOT HEAT AND TAT PROBE HEAT SENSORS (AMBER) MESSAGES APPEARED ON EICAS 1. RETURNED TO FIELD. RESET AFFECTED SYSTEMS BY POWER DOWN OF AC IAW GMPM VOL 1.

Part: WARNING LIGHT — FALSE INDICATION (PAX DOOR) · airframe 14,476 hrs · 12,893 cycles

RETURNED TO RNO WITH OUTER DOOR HANDLE MESSAGE. INSURED ALL OUTER DOOR HANDLES WERE SECURE. UNABLE TO DUPLICATE. OPS CHECKS GOOD.

Part: BULB — FAILED (CABIN) · airframe 14,391 hrs · 12,816 cycles

EXTERIOR EMERGENCY LIGHT RIGHT SIDE BURNED OUT. REPLACED 1317 LAMP IN RIGHT SIDE SECOND EMERGENCY LIGHT, OPS CHECKS GOOD.

Part: BPSU — FAILED (TE FLAP) · airframe 13,704 hrs · 12,186 cycles

FLAP FAIL MESSAGE AFTER TAKEOFF WHEN FLAPS RETRACTED TO 8. RETURNED TO RAP. REPLACED RIGHT BPSU IAW MM 275110, OPS CHECKS GOOD. (P/N 855D1009) (S/N 218A) ON, (S/N 277) OFF.

Part: POWER LEVER — MALFUNCTIONED (LT ENGINE)

LEFT ENGINE POWER LEVER UNABLE TO RETARD TO IDLE OR CUT OFF. SHUT LEFT ENG DOWN USING LEFT FIRE PUSH BUTTON. LANDED AT SLC UNEVENTFUL. N1 STUCK AT 90 DEGREES. REMOVED AND REPLACED LEFT ENGINE GEAR BOX ASSY FOR POWER THROTTLE LEVER PER MM 76-11-17. PERFORMED ENGINE ASSURANCE RUNS PER MM 71-00-00. OPS CHECKS OF THROTTLE LINKAGE GOOD.

Part: INDICATION — MALFUNCTIONED (NLG)

NOSE GEAR DISAGREE WARNING LIGHT AFTER GEAR RETRACTION. NOSE GEAR LIGHT STAYED GREEN. PERFORMED GEAR SWING IAW MM 32-30-00, NO PROBLEMS FOUND. COULD NOT DUPLICATE DISCREPANCY.

Part: COMPUTER — TRIPPED (STALL WARNING)

STALL FAIL MESSAGE ILLUMINATED EN ROUTE. RETURNED TO SLC. RESET MEMORY ON STALL COMPUTER. OPS CHECKS GOOD.

Part: COMPUTER — MALFUNCTIONED (STALL WARNING)

STALL FAIL MESSAGE ON RIGHT AFTER TAKEOFF. RETURNED TO SLC. INSTALLED SERVICEABLE STALL WARNING COMPUTER. OPS CHECK GOOD IAW 27-34-00.

Part: STALL UNIT — FAILED (E & E COMPT)

DURING CLIMBOUT, THE EICAS CAUTION MESSAGE STALL FAIL DISPLAYED. CONSULTED MAINTENANCE CONTROL, ADVISED RETURN TO SLC AFTER COMPLETING QRH. REMOVED AND REPLACED STALL PROTECTION UNIT, OPS CHECK GOOD ON GROUND.

Part: TIRE — FAILED (RT MLG)

RIGHT MAIN TIRE BLEW RIGHT AT ROTATION ON TAKEOFF NR 3 MAIN. RETURNED TO SLC. REPLACED NR 3 AND NR 4 MAIN WHEEL ASSEMBLIES.

Part: ENGINE — MALFUNCTIONED (LEFT)

ABOUT 20 MINUTES OUT OF EUGENE, LEFT OIL PRESS LIGHT AND WARNING CAME ON. DID PRECAUTIONARY ENGINE SHUT DOWN PROCEDURES. DIVERTED TO PDX DUE TO WEATHER IN EUG. REPLACED ENGINE AS REQUIRED.

Part: BULKHEAD — CRACKED (BS 409)

DISCOVERED CRACK IN PRESSURE BULKHEAD (P/N 601R3208-123), JUST FORWARD OF WING LEADING EDGE FS 409+128.

Part: N1 CONTL AMP — FAILED (RT ENGINE)

RIGHT ENGINE N1 AND N/FF FLUCTUATING AT CRUISE N1 96-88 PERCENT, NORMAL OPERATION AFTER RT ENGINE SPEED SWITCH TURNED OFF PER A/C ORH MANUAL MEL 26-11-1. RIGHT ENGINE SPEED SWITCH. RETURNED TO FIELD. REPLACED RT ENGINE N1, CONTROL AMP IAW MM 73-21-03. OPS CHECKS GOOD.

Part: BALLAST — FAILED (CABIN)

FLIGHT ATTENDANT REPORTED SMOKE COMING FROM ROW 8 OVERHEAD BIN AND VENTS. MOSTLY DISSIPATED BY LANDING. VERY STRONG ELECTRICAL SMELL, BURNING IN SEVERAL PLACES ABOVE OVERHEAD BINS. FOUND LIGHT BALLAST FOR UPPER CABIN LIGHTING OVER ROW 8 ON RT SIDE OVERHEATED AND BURNED. REPLACED LIGHTING BALLAST WITH NEW ONE, CKS GOOD.

Part: CAPACITOR — FAILED (CABIN)

BALLAST UNIT RECEIVED FOR INSP FOLLOWING REPORT OF CABIN SMOKE. FOUND CAPACITOR C1 FAILED.

Part: ENGINE — FAILED (RIGHT)

DURING TAKEOFF, RT ENGINE ITT WENT TO RED LINE. ABORTED TAKEOFF, TOWER REPORTED FLAMES FROM RT ENGINE. PERFORMED ENGINE FIRE PROCEDURE. REPLACED RT ENGINE WITH REPAIRED ASSY, OPS CKS AND LEAKS CKS GOOD.