N906SW

Part: ACTUATOR — FAILED (TE FLAPS) · airframe 42,531 hrs · 39,899 cycles

ON APPROACH TO SLC WITH FLAPS SET 20 WHEN SELECTED GEAR DOWN AND FLAPS 30 RECEIVED FLAP FAIL MESSAGE, COMPLETED QRH AND LANDED WITH FLAPS AT 20. REMOVED AND REPLACED R/H OUTBOARD FLAP OUTBOARD ACTUATOR. OPS CHECK GOOD.

Part: BRACKET — FAILED (NLG DOOR) · airframe 42,216 hrs · 39,536 cycles

GEAR DISAGREE, FLT 3742, REMOVED AND REPLACED BRACKET IAW AMM. NO DEFECTS NOTED AT THIS TIME.

Part: FLOOR SUPPORT — CORRODED (BS 295-310) · airframe 41,014 hrs · 38,141 cycles

AT APPROX FS 295 TO FS 310 €“ LEFT HAND CABIN FLOOR SILL HAS SIGNS OF CORROSION AROUND NUT PLATES. (C-CHECK) RO: 11/20/2018 REMOVED AND BLENDED OUT CORROSION AROUND NUT PLATES IAW REO.

Part: FLOOR SUPPORT — CORRODED (BS 559) · airframe 41,014 hrs · 38,141 cycles

FS559 TO FS559+80 RH FLOOR SILL HAS MULTIPLE AREAS OF CORROSION. (C-CHECK) RO: 11/20/2018 REMOVED AND REPLACED R/H FLOOR SILL FROM FS559 TO FS559+80 IAW SRM. PERFORMED PRESSURE CHECK OF REPAIR AREA IAW AMM. PRESSURE CHECKED GOOD.

Part: FRAME — CORRODED (BS 349) · airframe 41,014 hrs · 38,141 cycles

FS 349.00 FRAME CORRODED AFT SIDE BETWEEN STGR 26L AND STGR 26R. (C-CHECK) RO: 11/20/2018 REMOVED AND INSTALLED NEW SERVICEABLE LOWER FRAME SECTOR P/N 601R32005-69 AT FS349.00 BETWEEN STGR 23L AND STGR 23R IAW SRM. PERFORMED PRESSURE CHECK OF REPAIR AREA IAW AMM. PRESSURE CHECK GOOD.

Part: BEAM — GOUGED (LT WING) · airframe 37,544 hrs · 34,238 cycles

LEFT INBOARD FLAP INBOARD VANE ACTUATOR BEAM HAS A GOUGE. REPLACED THE LT INBD FLAP AND TRANSFERED HINGE ARMS TO NEW FLAP IAW AMM.

Part: BEAM — GOUGED (RT WING) · airframe 37,544 hrs · 34,238 cycles

RIGHT INBOARD FLAP INBOARD VANE ACTUATOR BEAM HAS A GOUGE. REPLACED RT INBD FLAP AND TRANSFERED HINGE ARMS TO NEW FLAP IAW AMM.

Part: PROXIMITY SENSOR — OUT OF ADJUST (NLG) · airframe 35,818 hrs · 32,234 cycles

RETURN TO FIELD NLG GEAR WOULD NOT RETRACT. ADJUSTED NOSE GEAR OLEO STRUT EXT PROXIMITY SENSOR TO LIMITS. SWUNG GEAR, OPS CHECK GOOD IAW AMM.

Part: FUEL NOZZLE — OUT OF POSITION (APU) · airframe 35,676 hrs · 32,069 cycles

AFTER LANDING, STARTED APU AND RECEIVED AN ITT SPIKE. ATC REPORTED TO THE CREW THEY SAW FLAMES FROM THE RT ENGINE. RT ENGINE PARAMETERS NORMAL. REINSTALLED APU NOZZLE IN CORRECT POSITION, LEAK CHECKED GOOD.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 34,058 hrs · 30,147 cycles

DAMAGE ON FUSELAGE SKIN UNDER ADF ANTENNA, LIGHTNING STRIKE. C-CHECK, REPAIRED DAMAGE ON FUSELAGE SKIN UNDER ADF ANTENNA, LIGHTNING STRIKE IAW REO.

Part: WINDOW FRAME — DAMAGED (COCKPIT) · airframe 34,058 hrs · 30,147 cycles

DAMAGE ON WINDSHIELD LOWER FWD FRAME FWD SIDE, RT OF CENTER POST. C-CHECK, REMOVED DAMAGE IAW REO.

Part: HINGE — MISALIGNED (HORIZONTAL STAB) · airframe 34,058 hrs · 30,147 cycles

HORIZONTAL STABILIZER HAS MISALIGNED HINGE BUSHINGS HOLES. C-CHECK, R & R BUSHINGS FOR HORIZONTAL STABILIZER HINGE AND BUSHINGS FOR VERTICAL STABILIZER HINGE IAW REO.

Part: SKIN — DENTED (RT AILERON) · airframe 34,058 hrs · 30,147 cycles

RIGHT AILERON HAS A DENT ON THE TOP SIDE. REPAIRED RT AILERON DENT ON UPPER SKIN IAW EA.

Part: FLOOR SUPPORT — CORRODED (BS 544-550) · airframe 34,058 hrs · 30,147 cycles

LEFT PRESSURE FLOOR SUPPORT ANGLE UPPER SURFACE CORRODED FROM BS 544 - 550, LBL 36. BLENDED OUT CORROSION IAW REO.

Part: FLOORBEAM — CORRODED (BS 449) · airframe 34,058 hrs · 30,147 cycles

LT PRESSURE FLOORBEAM ANGLE UPPER SURFACE CORRODED AT BS 449.85, LBL 36. C-CHECK BLENDED OUT CORROSION AT LT PRESSURE FLOORBEAM ANGLE IAW REO.

Part: FLOOR SUPPORT — CORRODED (BS 358-344) · airframe 34,058 hrs · 30,147 cycles

LEFT PRESSURE FLOOR SUPPORT ANGLE UPPER SURFACE CORRODED FROM BS 538 - 544, LBL 36. C-CHECK, BLENDED OUT CORROSION IAW REO.

Part: FLOOR SUPPORT — CORRODED (BS 449) · airframe 34,058 hrs · 30,147 cycles

RIGHT PRESSURE FLOOR SUPPORT ANGLE UPPER SURFACE CORRODED AT BS 449.85 RBL 36. C-CHECK, BLENDED OUT CORROSION AT RT PRESSURE FLOOR SILL ANGLE UPPER SURFACE CORRODED AT FS449.85, RBL36 IAW REO.

Part: STRUCTURE — CRACKED (FLOOR WEB) · airframe 34,058 hrs · 30,147 cycles

PRESSURE FLOOR CRACKED AT FS 460, RBL 4. C-CHECK, REPAIRED PRESSURE FLOOR CRACKED AT FS 460, RBL 4 IAW REO.

Part: TRAY — CRACKED (COCKPIT) · airframe 34,058 hrs · 30,147 cycles

ELECTRICAL SUPPORT TRAY INSIDE AFT SECTION OF PILOT'S SIDE CONSOL HAS A CRACK IN THE OTBD EDGE. REPAIRED ELECTRICAL EQUIPMENT TRAY IAW STS EA.

Part: STRIKER — DENTED (PAX DOOR) · airframe 34,058 hrs · 30,147 cycles

PAX DOOR SEAL STRIKER FWD UPPER SIDE DENTED. C-CHECK, R & R PAX DOOR SEAL STRIKER FWD UPPER SIDE, IAW SRM AND REO.

Part: VANE — CHAFED (LT WING TE FLAP) · airframe 34,058 hrs · 30,147 cycles

LEFT INBD FLAP VANE L/E IS CHAFED AT OTBD SIDE. C-CHECK, BLENDED, FOUND WITHIN LIMITS AND RESTORED FINISH TO LT INBD FLAP VANE L/E OTBD SIDE IAW REO.

Part: VANE — CHAFED (LT WING TE FLAP) · airframe 34,058 hrs · 30,147 cycles

LEFT INBD FLAP VANE L/E IS CHAFED AT CENTER OF VANE. C-CHECK, BLENDED, FOUND WITHIN LIMITS AND RESTORED FINISH TO LT INBD FLAP VANE L/E CENTER SIDE IAW REO.

Part: SKIN — BENT (RT WING) · airframe 34,058 hrs · 30,147 cycles

RIGHT WING OTBD L/E SEGMENT 630KL, UPPER FLANGE INTERNAL SKIN IS BENT/DISTORTED AND DISBONDED AT THE OTBD END. C-CHECK, REPAIRED RT WING OTBD L/E SEGMENT 630KL, UPPER FLANGE INTERNAL SKIN IAW REO.

Part: VANE — CHAFED (LT WING TE FLAP) · airframe 34,058 hrs · 30,147 cycles

LEFT INBD FLAP VANE L/E IS CHAFED AT INBD SIDE. C-CHECK BLENDED, FOUND WITHIN LIMITS AND RESTORED FINISH TO LT INBD FLAP VANE L/E INBD SIDE IAW REO.

Part: SUPPORT — CHAFED (LT MLG) · airframe 34,058 hrs · 30,147 cycles

LT MLG UPLOCK STRUCTURE HAS A CHAFE ON EDGE OF FWD INBD FLANGE ON BOTTOM SUPPORT. C-CHECK, BLENDED CHAFE AND REROUTED INBD WIRING HARNESS ON LT MLG IAW STS EA.

Part: VANE — LOOSE (EXHAUST DUCT) · airframe 34,058 hrs · 30,147 cycles

RIGHT ACM EXHAUST DUCT HAS A LOOSE VANE. C-CHECK, REBONDED LOOSE VAIN IN RT ACM EXHAUST DUCT IAW REO.

Part: HOUSING — CHAFED (CARGO DOOR) · airframe 34,058 hrs · 30,147 cycles

CARGO DOOR EXTERNAL HANDLE HOUSING IS CHAFED AT THE BOTTOM FWD EDGE. REPAIRED THE CARGO DOOR HANDLE HOUSING IAW REO.

Part: SKIN — CHAFED (RT AILERON) · airframe 34,058 hrs · 30,147 cycles

RIGHT AILERON, L/E UNDER SHROUDS, CHAFED FROM WS 282.00- WS 353.00. C-CHECK, BLENDED OUT DAMAGE RT AILERON, L/E UNDER SHROUDS WS 282.00- WS 353.00 IAW REO.

Part: CHANNEL — CRACKED (BS 682) · airframe 34,058 hrs · 30,147 cycles

LT ENGINE, FIXED CORE COWL AFT CHANNEL CRACKED AT UPPER FWD SIDE STA FS682, STA XN208.39. C-CHECK, R & R DUCT ON LT FIXED CORE COWL AFT SIDE IAW SRM AND STS EA.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 33,772 hrs · 29,841 cycles

ROWS 9-13 FLOOR EMERGENCY LIGHTS INOPERATIVE. REPLACED NR 4 BATTERY PACK. OPS CHECKED GOOD IAW AMM.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 33,440 hrs · 29,485 cycles

INTERIOR REAR FWD & AFT FACING EMERGENCY EXIT SIGNS ARE BURNED OUT. REPLACED THE LAMPS.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 33,440 hrs · 29,485 cycles

LEFT SIDE MOST FWD EXIT EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMP.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 33,341 hrs · 29,379 cycles

SEVERAL LIGHTS BURNED OUT ON THE OVER WING EMERGENCY DOOR EXIT LIGHT. REPLACED THE LAMPS.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 33,341 hrs · 29,379 cycles

MIDDLE OVERHEAD EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMPS.

Part: BOLT — GALLED (ENGINE MOUNT) · airframe 33,286 hrs · 29,319 cycles

LT ENGINE FWD MOUNT LOWER BOLT ASSY GALLED. SERVICE, R & R LT ENGINE FWD MOUNT LOWER BOLT ASSEMBLY IAW AMM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 33,233 hrs · 29,261 cycles

LEFT AND RIGHT OVERWING EXIT LIGHTED EXIT SIGNS HAVE LAMPS INOPERATIVE, REPLACED THE LAMP IAW AMM.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 33,233 hrs · 29,261 cycles

FWD CEILING LIGHTED EXIT SIGN NEAR THE OVERWING EXIT IS BURNED OUT, REPLACED THE LAMP IAW AMM.

Part: INVERTER — FAILED (EMERGENCY LIGHTS) · airframe 32,913 hrs · 28,914 cycles

LESS THAN 10 FT OF EMERGENCY FLOOR STRIP LIGHTING BETWEEN ROWS 6 & 8 ON ACFT RT SIDE DOES NOT ILLUMINATE. REPLACED THE NR 3 INVERTER FOR THE EMERGENCY LIGHT SYS IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,821 hrs · 28,820 cycles

CABIN EMERGENCY EXIT LIGHT AT 8F DOES NOT ILLUMINATE. FLT 2907 RELAMPED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,806 hrs · 28,808 cycles

ROW 8 EMERGENCY LIGHT LOWER PANEL IS BURNED OUT. FLT 2948 RELAMPED.

Part: CONTROL CABLE — BROKEN (LT THROTTLE) · airframe 32,479 hrs · 28,436 cycles

LT THRUST LEVER UNRESPONSIVE, PERFORMED QRH PROCEDURE & SHUTDOWN LT ENG. FLT 2901 REPLACED BROKEN LT ENG THROTTLE CONTROL CABLE IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,360 hrs · 28,300 cycles

NR 2 EMERGENCY OVERHEAD LIGHT IS BURNED OUT. FLT 2907 RELAMPED.

Part: TERMINAL — DIRTY (BATTERY PACK) · airframe 32,331 hrs · 28,270 cycles

EMERGENCY LIGHT IN CABIN UNDER RT OVERWING EXIT DOES NOT ILLUMINATE. FLT 2902 CLEAN TERMINALS TO BATTERY PACK NR 4.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 32,253 hrs · 28,189 cycles

EMERGENCY LIGHTS DON'T STAY ON. FLT 2951 EMERGENCY LIGHT BATTERY PACKS WERE CHARGED FOR APPROXIMATELY 1 HOUR. OPERATIONS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,791 hrs · 27,729 cycles

NR 2 EMERGENCY OVERHEAD LIGHT IS BURNED OUT. FLT#2973 RELAMPED.

Part: ROD — BROKEN (STAIRS) · airframe 31,659 hrs · 27,595 cycles

MAIN CABIN DOOR STAIR RETRACTION ROD BROKEN. FLT#2956 REPLACED FOLDING STEP & STEP RETRACTION ROD.

Part: ANCHOR FITTING — CRACKED (PAX DOOR) · airframe 31,559 hrs · 27,472 cycles

CRACK ON THE PAX DOOR LOWER AFT ANCHOR FITTING. C-CHECK REPLACED PAX DOOR AFT LOWER ANCHOR FITTING IAW REO & AMM.

Part: HOUSING — BROKEN (CABIN) · airframe 31,593 hrs · 27,504 cycles

EMERGENCY FLOOR FLOOD LIGHT HOUSING BROKEN. SERVICE REPLACED EMERGENCY FLOOD LIGHT ASSEMBLY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,503 hrs · 27,415 cycles

NR 2 EMERGENCY OVERHEAD LIGHT IS BURNED OUT. FLT#2950 RELAMPED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,416 hrs · 27,320 cycles

NR 1 EMERGENCY OVERHEAD LIGHT IS BURNED OUT. FLT#2969 R&R NR 1 EMERGENCY POD LIGHT WITH A SERVICEABLE UNIT. IAW REF AMM 33-51-16. OPERATIONS CHECKED GOOD AT THIS TIME.

Part: LIGHT — UNSECURE (CABIN) · airframe 30,698 hrs · 26,532 cycles

FLOOR LEVEL EMERGENCY LIGHT STRIP AT ROW 10 DOES NOT ILLUMINATE. (FLT 2960) RE-SECURED FLOOR EMERGENCY LIGHT STRIP.

Part: SKIN — DENTED (FUSELAGE) · airframe 30,416 hrs · 26,263 cycles

FUSELAGE SKIN DENTS FWD OF CARGO DOOR OUT OF LIMITS. (FLT 2977) COMPLIED WITH EXTERNAL PERMANENT REPAIR ON FUSELAGE SKIN FWD OF CARGO DOOR FS 559.00 AND FS 605.00 IAW SRM.

Part: POST — CRACKED (FUSELAGE) · airframe 29,862 hrs · 25,675 cycles

RBL 27 I/B POST HAS A CRACKED LOWER RADIUS. (C-CHECK) REPLACED INBOARD POST.

Part: POST — CRACKED (FUSELAGE) · airframe 29,862 hrs · 25,675 cycles

RBL 27.00 POST CRACKED LOWER RADIUS. (C-CHECK) REPLACED OUTBOARD POST.

Part: POST — CRACKED (FUSELAGE) · airframe 29,862 hrs · 25,675 cycles

RBL 18.00 POST CRACK LOWER RADIUS AROUND RIVET. (C-CHECK) REPLACED RBL 18.00 POST.

Part: POST — CRACKED (FUSELAGE) · airframe 29,862 hrs · 25,675 cycles

LBL 27.00 POST CRACK LOWER RADIUS AROUND RIVETS. (C-CHECK) REPAIRED LBL 27.00 POST IAW REO.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 29,862 hrs · 25,675 cycles

RBL 9 LOWER FLOOR SUPPORT CRACKED. (C-CHECK) REPLACED RBL 9 LOWER FLOOR SUPPORT REFERENCE REO.

Part: POST — CRACKED (FUSELAGE) · airframe 29,862 hrs · 25,675 cycles

LBL 18.00 OUTBOARD VERTICAL POST CRACK. (C-CHECK) REPLACED LBL 18 OUTBOARD POST IAW SRM.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 29,862 hrs · 25,675 cycles

RBL 9 UPPER FLOOR SUPPORT IS CRACKED. (C-CHECK) RBL 9 REPAIRED IAW WITH REO.

Part: HYDRAULIC SYSTEM — CONTAMINATED (NR 3) · airframe 29,383 hrs · 25,169 cycles

RECEIVED HYDRAULIC 3 LOW PRESSURE CAUTION MESSAGE FOLLOWED BY GEAR DISAGREE MESSAGE FOLLOWED BY NOSE DOOR MESSAGE. (FLT 2977) PURGED SYSTEM 3 HYDRAULIC 3A & 3B PUMPS ON ONE AT A TIME.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,255 hrs · 25,040 cycles

EMERGENCY EXIT LIGHT NOT ILLUMINATING. (SERVICE) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,208 hrs · 24,994 cycles

NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 2918) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,952 hrs · 24,732 cycles

THE FORWARD TWO OVERHEAD EMERGENCY LIGHTS ARE OUT. (FLT 2971) RELAMPED EMERGENCY LIGHTS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,826 hrs · 24,605 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 2986) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,772 hrs · 24,552 cycles

NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 2959) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,677 hrs · 24,454 cycles

NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 2948) RELAMPED EMERGENCY LIGHT.

Part: INVERTER — FAILED (CABIN) · airframe 28,533 hrs · 24,306 cycles

INTERIOR NR 4 EMERGENCY LIGHT STRIP FROM ROW 6 TO ROW 12 WON'T LIGHT UP. (SERVICE) REPLACED NR 4 EMERGENCY LIGHT INVERTER.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 28,505 hrs · 24,276 cycles

FLOOR LEVEL EMERGENCY LIGHTS INOP FROM EXIT ROW TO BACK OF CABIN. (FLT 2923) EMERGENCY LIGHT FLOOR STRIP CONNECTOR NOT CONNECTED. RE-CONNECTED FLOOR STRIP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,505 hrs · 24,276 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,446 hrs · 24,216 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 2974) RELAMPED EMERGENCY LIGHT.

Part: INVERTER — FAILED (CABIN) · airframe 28,298 hrs · 24,065 cycles

LEFT EMERGENCY EXIT SIDE WALL LIGHT AT EXIT ROW AND FLOOR LEVEL AT ROW 2 TO ROW 5 INOPERATIVE. (FLT 2993) REPLACED NR 2 INVERTER IN REFERENCE WITH AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,298 hrs · 24,065 cycles

FLOOR LEVEL EMERGENCY LIGHT STRIP ROWS 2 THROUGH 5 NOT ILLUMINATING. (FLT 2969) RE-RACKED POWER STRIP AT 5D.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,285 hrs · 24,049 cycles

NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 2974) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,269 hrs · 24,029 cycles

NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 2969) RELAMPED EMERGENCY LIGHT.

Part: BATTERY — DISCHARGED (CABIN) · airframe 28,256 hrs · 24,015 cycles

NR 2 TO NR 5 FLOOR EMERGENCY LIGHTS ARE OUT. (SERVICE) REPLACED NR 2 EMERGENCY BATTERY. PN: AD-2013-1A SN OFF: 65915.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,190 hrs · 23,945 cycles

NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 2987) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,799 hrs · 23,557 cycles

NR 1 AND 3 OVERHEAD EMERGENCY LIGHTS ARE OUT. (FLT 6420) RELAMPED EMERGENCY LIGHTS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,751 hrs · 23,509 cycles

THE 1ST AND 3RD OVERHEAD EMERGENCY LIGHT ARE OUT. (FLT 6418) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,634 hrs · 23,409 cycles

OVERHEAD EMERGENCY LIGHTS AT ROW 1 AND 10 ARE OUT. (FLT 5541) RELAMPED EMERGENCY LIGHTS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,593 hrs · 23,377 cycles

NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5438) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,516 hrs · 23,316 cycles

NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6474) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,473 hrs · 23,278 cycles

NR 1 EMERGENCY LIGHT INOPERATIVE. (FLT 5383) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,445 hrs · 23,245 cycles

NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6465) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,322 hrs · 23,129 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6278) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,245 hrs · 23,073 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6230) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,153 hrs · 22,995 cycles

EXTERIOR EMERGENCY LIGHT BY GALLEY SERVICE DOOR IS OUT. (FLT 6208) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — DISCONNECTED (CABIN) · airframe 26,921 hrs · 22,827 cycles

FLOOR LEVEL EMERGENCY LIGHT STRIP AT ROW 9 IS OUT. (SERVICE) RECONNECTED FLOOR EMERGENCY LIGHT STRIP AT ROW 9.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,783 hrs · 22,733 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5800) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 26,547 hrs · 22,555 cycles

EMERGENCY LIGHT ON LEFT SIDE OF FUSELAGE FORWARD OF MAIN CABIN DOOR IS OUT. (FLT 6350) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — BROKEN (CABIN) · airframe 26,547 hrs · 22,555 cycles

LAST THIRD OF EMERGENCY FLOOR LIGHTS DO NOT ILLUMINATE DURING TEST. (FLT 6847) REPLACED AFT FLOOR EMERGENCY LIGHT STRIP SECTION.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 26,401 hrs · 22,438 cycles

EXTERIOR EMERGENCY LIGHT NEAR SERVICE DOOR IS OUT. (SERVICE) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — DISCONNECTED (CABIN) · airframe 25,986 hrs · 22,089 cycles

AFT SECTION OF EMERGENCY LIGHT STRIP ON FLOOR DOES NOT ILLUMINATE. (FLT 6629) RECONNECTED AFT FLOOR EMERGENCY LIGHT STRIP.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 25,798 hrs · 21,936 cycles

FLOOR EMERGENCY LIGHTS AFT OF EMERGENCY EXIT DO NOT ILLUMINATE. (FLT 6606) RECONNECT FLOOR EMERGENCY LIGHT PLUG.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 25,661 hrs · 21,814 cycles

FS 559.0 BULKHEAD CRACKED ON RIGHT SIDE. (C-CHECK) REPAIR PER REO.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 25,986 hrs · 22,089 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,537 hrs · 21,719 cycles

NR 3 OVERHEAD EMERGENCY LIGHT INOPERATIVE. (FLT 6391) RELAMPED EMERGENCY LIGHT.

Part: WIRE — BROKEN (CABIN) · airframe 25,063 hrs · 21,319 cycles

EMERGENCY EXIT SIGN BY MAIN CABIN DOOR IS INOPERATIVE. (FLT 6900) REPAIRED WIRE AT EMERGENCY EXIT LIGHT CONNECTOR PIN.

Part: DOOR — OUT OF ADJUST (CABIN) · airframe 24,565 hrs · 20,906 cycles

COULD NOT OPEN MAIN CABIN DOOR FROM INSIDE OR OUTSIDE. (FLT 6735) ADJUSTED MAIN CABIN DOOR.

Part: COUNTERBALANCE — OUT OF RIG (CABIN DOOR) · airframe 24,521 hrs · 20,866 cycles

MAIN CABIN DOOR DIFFICULT TO OPEN. (FLT 6683) RIG PASSENGER DOOR COUNTERBALANCE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,232 hrs · 20,635 cycles

FORWARD EMERGENCY CEILING LIGHT INOP. (FLT 6377) RELAMPED EMERGENCY LIGHT.

Part: DOOR — MALFUNCTIONED (CABIN) · airframe 24,044 hrs · 20,481 cycles

MAIN CABIN DOOR WOULD NOT OPEN. (FLT 6540) CYCLED MAIN CABIN DOOR NUMEROUS TIMES, OPERATIONAL CHECK NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,696 hrs · 20,175 cycles

NR 1 CEILING EMERGENCY LIGHT INOP. (FLT 6644) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,262 hrs · 19,794 cycles

NR 2 OVERHEAD EMERGENCY LIGHT INOP. (FLT 6509) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,770 hrs · 19,330 cycles

EMERGENCY CEILING LIGHT NR 2 INOP. (FLT 6757) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,734 hrs · 19,296 cycles

NR 3 OVERHEAD DOME EMERGENCY LIGHT INOP. (FLT 6704) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,438 hrs · 19,067 cycles

NR 3 OVERHEAD EMERGENCY LIGHT INOP. (FLT 6518) `RELAMPED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,223 hrs · 18,893 cycles

NR 2 CEILING EMERGENCY LIGHT INOP. (FLT 6378) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,122 hrs · 18,819 cycles

NR 3 CABIN EMERGENCY FLOODLIGHT INOP. (FLT 6070) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,928 hrs · 18,661 cycles

EMERGENCY CEILING LIGHT NR 3 INOP. (FLT 6352) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,867 hrs · 18,609 cycles

CEILING EMERGENCY LIGHT AT ROW 5 INOP. (FLT 5922) RELAMPED EMERGENCY LIGHT.

Part: SPRING — FAULTY (CABIN DOOR) · airframe 21,738 hrs · 18,504 cycles

UNABLE TO OPEN MAIN CABIN DOOR. (FLT 6154) REPLACED THE FORWARD AND AFT MAIN DOOR COUNTERBALANCE SPRINGS.

Part: COMPUTER — MALFUNCTIONED (FLIGHT CONTROL) · airframe 21,697 hrs · 18,473 cycles

UNCOMMANDED RUDDER INPUTS IN FLIGHT. (FLT 6730) REPLACED FCC CARDS.

Part: SUPPORT — CRACKED (BS 280) · airframe 21,449 hrs · 18,272 cycles

FS 280 SUPPORT IS CRACKED. (C CHECK) REPAIRED PER REO.

Part: ATTACH FITTING — CRACKED (BS 280) · airframe 21,449 hrs · 18,272 cycles

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

Part: ATTACH FITTING — CRACKED (BULKHEAD) · airframe 21,449 hrs · 18,272 cycles

FORWARD PRESSURE BULKHEAD CLIPS CRACKED. (C CHECK) REPLACED CLIPS.

Part: BLEED AIR SYS — CONTAMINATED · airframe 20,715 hrs · 17,678 cycles

FLT 6695 - SMOKE FILLED FLIGHT DECK AND CABIN AFTER TAKEOFF. BLEED SYSTEM GLYCOL CONTAMINATED. ACCOMPLISHED PACK BURN OUT.

Part: COVER — NOT SEATED (EMERGENCY LIGHT) · airframe 20,641 hrs · 17,623 cycles

FLT 6223 - EMERGENCY LIGHTING COVER AT PASSENGER DOOR CAME OFF. REPLACED COVER.

Part: LAMP — BURNED OUT (EMERGENCY LIGHTS) · airframe 20,541 hrs · 17,543 cycles

FLT 6018 - NR 1 AND NR 3 CEILING EMERGENCY LIGHTS INOP. RELAMPED.

Part: WINDSHIELD — CRACKED (CRACKED) · airframe 20,219 hrs · 17,280 cycles

FLT 6695 - LEFT WINDSHIELD CRACKED. REPLACED WINDSHIELD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,160 hrs · 17,236 cycles

FLT 6303 - EMERGENCY FLOODLIGHT ON CEILING ABOVE ROW 2 INOP. RELAMPED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,147 hrs · 17,226 cycles

FLT 6001 - CABIN OVERHEAD EMERGENCY LIGHT, SECOND AFT, INOP. RELAMPED.

Part: SELECTOR VALVE — MALFUNCTIONED (NLG) · airframe 19,762 hrs · 16,947 cycles

FLT 6629 - NOSE LANDING GEAR WOULD NOT EXTEND. REPLACED NLG SELECTOR VALVE.

Part: WIRE — DAMAGED (CABIN) · airframe 16,894 hrs · 14,501 cycles

AFT FLOOR EMERGENCY LIGHTS ARE INOP, FLIGHT NR 6523. REPAIRED WIRING IAW WM 20-10-00. OPERATIONAL CHECK GOOD.

Part: INTERCOSTAL — CRACKED (PAX DOOR) · airframe 16,894 hrs · 14,501 cycles

PAX DOOR INTERCOSTAL IS CRACKED, FOUND AT C-CHECK. INSTALLED NEW INTERCOSTAL IAW CRJ200 SRM 51-42-06.

Part: FITTING — CRACKED (FUSELAGE) · airframe 16,894 hrs · 14,501 cycles

FOUND AT C-CHECK, FS480 AT LBL36 CLIP IS CRACKED. INSTALLED CLIP PER REO:601R-53-41-059 REV.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 16,894 hrs · 14,501 cycles

PAX DOOR AFT DRAG ANGLE IS CRACKED, FOUND AT C-CHECK. INSTALLED UPPER AND LOWER AFT ANGLE SPLICES PER CRJ200 SRM 51-42-06 PAGE 4.

Part: FITTING — CRACKED (FUSELAGE) · airframe 16,894 hrs · 14,501 cycles

FS 480 AT RBL36 CLIP IS CRACKED, FOUND AT C-CHECK. INSTALLED CLIP PER REO 601R 53-41-059.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 16,894 hrs · 14,501 cycles

FS 280 FORWARD FLOOR SUPPORT IS CRACKED WITH SHEARED FASTENERS, FOUND AT C-CHECK. REPLACED FASTENERS AND FLOOR SUPPORT PER CRJ200 SRM 51-41-00, 51-40-11 AND 51-42-06.

Part: STRINGER — DAMAGED (BS 202-220 S24R) · airframe 15,757 hrs · 13,539 cycles

STRINGER 24R BETWEEN FS 202 AND FS 220 IS DAMAGED. REPAIRED STRINGER 24R BETWEEN FS 202 AND 220 IAW CRJ 200 SRM 53-00-03.

Part: SKIN — DAMAGED (BS 202-220) · airframe 15,757 hrs · 13,539 cycles

FUSELAGE DAMAGE BETWEEN FS 202.75 AND FS 220.00 AND BETWEEN STRINGERS 23R AND 24R. REPAIRED FUSELAGE BETWEEN FS 202.75 AND FS 220 AND BETWEEN STRINGERS 23R AND 24R IAW REO NR 601R-53-11-1191.

Part: BULB — FAILED (EMERGENCY LIGHTS) · airframe 14,295 hrs · 12,314 cycles

CEILING EMERGENCY LIGHT ROW 2 AISLE INOP. REPLACED BULB IN EMERGENCY LIGHT AT AISLE 2. OPERATIONAL CHECKS GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 13,280 hrs · 11,420 cycles

OVERHEAD FORWARD SIDE OF EMERGENCY EXIT LIGHT DOES NOT ILLUMINATE. REPLACED NR 2 EMERGENCY LIGHT BATTERY PER 32-51-00. OPERATIONAL CHECKS GOOD, SN OFF 83354.

Part: DOOR — STICKS (PAX DOOR) · airframe 13,007 hrs · 11,175 cycles

AT GATE, MAIN CABIN DOOR WOULD NOT OPEN. PERFORMED VISUAL INSPECTION OF PASSENGER DOOR WITH NO DEFECTS NOTED. OPERATIONAL CHECKS GOOD.

Part: TRIM SWITCH — INOPERATIVE (RT ELEVATOR) · airframe 12,404 hrs · 10,612 cycles

ON TO, FO NOTICED THAT THE RIGHT ELEVATOR TRIM SWTICH WAS INOP. REPLACED RT PITCH TRIM SWITCH AS REQUIRED IAW CRJ AMM 27-41-05.

Part: DETECTOR — MALFUNCTIONED (TE FLAPS) · airframe 12,037 hrs · 10,273 cycles

FLAPS HALF-SPEED STATUS MESSAGE. REPLACED SKEW DETECTOR, OPERATIONAL CHECK GOOD REF CL 600 MM 27-50-04.

Part: ATTACH FITTING — CRACKED (INTERCOSTAL) · airframe 12,548 hrs · 10,739 cycles

AFT EQUIPMENT COMP, INTERCOSTAL CLIPS ARE CRACKED, LT & RT, FS 621.00 - FS 625.00, STR 14L & STR 14R. ITEM FOUND AT C-CHECK INSPECTION. CLIPS REPLACED IAW CRJ REO 601R-53-61-100 REV NC AND REO 601R-53-61-422 REV NC.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 12,548 hrs · 10,739 cycles

FUSELAGE, LOWER TRANSVERSE BEAM IS CRACKED, FS 280.00, LBL 11.0. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED REF REO 601R-53-11-171 REV C.

Part: ATTACH FITTING — CRACKED (BS 280) · airframe 12,548 hrs · 10,739 cycles

FUSELAGE, FLOORBEAM TO TRANSVERSE ATTACH CLIPS ARE CRACKED, I/B & O/B LOCATIONS, FS 280.0, RBL 9.0. ITEM FOUND AT C-CHECK INSPECTION. INBOARD CLIP REPLACED IAW SRM 51-40-11, 51-23-00, 51-42-06, 51-42-21, 51-21-11 AND 51-25-16. OUTBOARD CLIP REPLACED IAW CRJ REO 601R-53-11-171 REV C.

Part: SHAFT — CORRODED (E HATCH HANDLE) · airframe 12,548 hrs · 10,739 cycles

COCKPIT ESCAPE HATCH OUTER HANDLE SHAFT CORRODED. ITEM FOUND AT C-CHECK INSPECTION. REPLACED THE OUTER HANDLE ASSY & ASSOC SPRING IAW TASK 52-22-03-400-801 OF THE AMM & 52-22-01 PG 615. OPERATIONAL CHECK GOOD.

Part: PUMP — LEAKING (NR 1 ENGINE) · airframe 12,387 hrs · 10,594 cycles

CREW REPORTS IN FLT SHUT DOWN OF NR 1 ENG DUE TO LOW OIL PRESS MASTER WARNING MSG. INSPECTED LT ENG AND FOUND OIL LEAKING FROM SPLINE PLUG FOR NR 1 EDP DEACTIVATION. VERIFIED LPT AND HPT ROTATE FREE. INTERROGATED MDC ENG EXCEEDENCE AND FOUND LT ENG LOP/SEC IN LIMITS IAW CRJ MM 72-00-00-280-201. C/W CHIP DETECTOR AND OIL FILTER INSPECTION AND NO CONTAMINATION FOUND.

Part: SENSOR — MALFUNCTIONED (BRAKE POSITION) · airframe 11,934 hrs · 10,173 cycles

FLAP FAIL MSG AT 18000 FT. REPLACED LT BPSU IAW CRJ MM 27-51-10. OPERATIONAL CHECK GOOD.

Part: ACTUATOR — MALFUNCTIONED (HORIZONTAL STAB) · airframe 11,941 hrs · 10,177 cycles

STAB TRIM INOP. REPLACED HORIZONTAL STAB ACTUATOR AND MCU. OPERATIONAL CHECK GOOD. REF CRJ AMM 27-42-01, P/N: 7062-3, S/N OFF: 901, P/N: 8396-3, S/N OFF: 1152.

Part: LAMP — BURNED OUT (FLOOD LIGHT) · airframe 11,426 hrs · 9,718 cycles

ONE CEILING FLOODLIGHT INOP. RELAMPED CEILING EMERGENCY FLOOD LIGHT AND OPERATIONAL CHECK GOOD. REF AMM 33-51-16.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT) · airframe 11,274 hrs · 9,574 cycles

GALLEY/BOARDING AREA "EXIT" LIGHT DOES NOT ILLUMINATE, BULKHEAD FLOOR EXIT LIGHT. RESEATED AND RESECURED LIGHT PLUG. OPERATIONAL CHECK NORMAL IAW MM 20-00-00.

Part: CONTROL UNIT — OUT OF RIG (TE FLAPS) · airframe 10,745 hrs · 9,108 cycles

"FLAPS FAIL" CAUTION MESSAGE. FLAPS FAILED AT 0 DEGREES. INTERROGATED FECU AND FOUND BOTH LEFT AND RIGHT BPSU'S OUT OF TOLERANCE. RE-RIGGED BOTH LEFT AND RIGHT BPSU'S IAW CRJ 200 MM 27-51-10. OPERATIONAL CHECK GOOD.

Part: BULB — BURNED OUT (EXTERIOR) · airframe 10,642 hrs · 9,022 cycles

EXTERIOR EMERGENCY LIGHT, 2ND FROM FRONT RT SIDE, FAILS TO ILLUMINATE. REPLACED EMERGENCY LIGHT BULB (2ND FROM FRONT ON RT SIDE). OPERATIONAL CHECK GOOD.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 9,872 hrs · 8,385 cycles

CEILING EMERGENCY LIGHT NR 3 INOPERATIVE. RELAMPED CEILING EMERGENCY LIGHT NR 3 IAW CRJ 200 MM 33-51-16. OPERATIONAL CHECK GOOD.

Part: BATTERY PACK — MALFUNCTIONED (EMERGENCY LIGHT) · airframe 9,778 hrs · 8,312 cycles

SERVICE DOOR EMERGENCY EXIT SIGN WILL NOT ILLUMINATE WHEN SWITCHED ON. REPLACED BATTERY PACK PER CRJ MM 33-51-04. OPERATIONAL CHECK NORMAL.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 9,607 hrs · 8,170 cycles

AFT CABIN CEILING CEMERGENCY LIGHT INOPERATIVE. RELAMPED AFT CABIN CEILING EMERGENCY LIGHT IAW MM 33-51-16. OPERATIONAL CHECK GOOD.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHT) · airframe 8,435 hrs · 7,136 cycles

EMERGENCY FLOOR LIGHTING FROM ROW 18 BACK INOPERATIVE. REMOVED AND REPLACED NR 4 EMERGENCY LIGHT INVERTER IAW MM 33-61-00. OPERATIONAL CHECK GOOD.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 7,936 hrs · 6,693 cycles

CARGO PIT FLOORBEAM ANGLE IS CRACKED FS 621.00 LBL 42.0. DISCOVERED DURING C-CHECK INSPECTION. REPAIRED ANGLE IAW CRJ REO 601R-52-11-213. FLOOR SUPPORT ANGLE AT FS 621.00 LBL 42.0 REPAIRED IAW CRJ REO 601R-53-61-117 REV. B.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 7,936 hrs · 6,693 cycles

FUSELAGE FLOORBEAM TO TRANSVERSE BEAM ATTACH CLIP IS CRACKED O/B LOCATION FS 280.00 LBL 9.0. DISCOVERED DURING C-CHECK INSPECTION. REPLACED CLIP IAW CRJ SRM 51-40-11, 51-23-00, 51-42-06, 51-42-21, 51-42-13, 51-25-16, 51-21-11.

Part: BEAM — CRACKED (FUSELAGE) · airframe 7,936 hrs · 6,693 cycles

FUSELAGE TRANSVERSE BEAM HAS A CRACK BY LOWER FLANGE FS 280.00 RBL 12.0. DISCOVERED DURING C-CHECK INSPECTION. DAMAGE REPAIRED IAW CRJ REO 601R-53-11-171. REV. "NC"

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 7,936 hrs · 6,693 cycles

FS 484 RIGHT INTERCOSTAL RBL 27 ANGLE CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REPLACED CLIP IAW CRJ SRM 51-40-11, 51-23-00, 51-42-06, 51-42-21, 51-42-13, 51-25-16, 51-21-11.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 7,918 hrs · 6,676 cycles

ONE CEILING EMERGENCY LIGHT INOP. REPLACED MAIN DOOR CEILING EMERGENCY LIGHT BULB. OPERATIONAL CHECK GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 6,932 hrs · 5,831 cycles

SECOND ROW OF CABIN EMERGENCY LIGHTS (CEILING) INOP. REMOVED AND REPLACED LIGHT BULB. OPS CHECK GOOD.

Part: ACTUATOR — MALFUNCTIONED (HORIZONTAL STAB) · airframe 6,970 hrs · 5,861 cycles

STAB CH 1 INOP STATUS MESSAGE WILL NOT GO OUT. REMOVED AND REPLACED HSTA AND MCU SYSTEM. OPS CHECK GOOD PER CRJ MM 27-12-01. MCU P/N: 7062-3, S/N OFF 1126.

Part: CONTROL UNIT — MALFUNCTIONED (H/STAB TRIM) · airframe 6,804 hrs · 5,714 cycles

STAB TRIM CH 1 WILL NOT ENGAGE. REMOVED AND REPLACED HSTCU IAW CRJ MM 27-41-01. OPS CHECK NORMAL. S/N OFF: 1057.

Part: CAPACITOR — BROKEN (MCV)

MOTOR CONTROL UNIT CAPACITOR BROKEN MAKING CHANNEL NR 1 INOPERATIVE.

Part: CONTROL UNIT — FAILED (STAB TRIM ACT) · airframe 6,733 hrs · 5,640 cycles

STAB TRIM CH 2 WILL NOT TEST AND DISCONNECTS WHEN STAB TRIM SWITCH IS EXERCISED. INSTALLED SERVICEABLE MCU AND HORIZONTAL STAB TRIM ACTUATOR IAW 27-42-01, REF RII CARD 27-415. HSTA P/N: 8396-3, S/N OFF: 278, OPS CHECKS GOOD.

Part: STICK SHAKER — MALFUNCTIONED (STALL WARNING) · airframe 6,680 hrs · 5,600 cycles

STALL STICK PUSHER DOES NOT TEST PROPERLY. REMOVED AND REPLACED STICK PUSHER. OPS CHECK GOOD PER CRJ MM 27-35-15.

Part: STICK SHAKER — WILL NOT TEST (STALL WARNING) · airframe 6,409 hrs · 5,380 cycles

STICK PUSHER WILL NOT TEST. REMOVED AND REPLACED STICK PUSHER IAW CRJ MM 27-35-15. OPS CHECKS GOOD. P/N: 600-59156-15, S/N OFF: 1649.

Part: ADC — MALFUNCTIONED (COCKPIT) · airframe 6,033 hrs · 5,067 cycles

STALL TEST WILL NOT TEST PROPERLY. REMOVED AND REPLACED NR 1 ADC. OPS CHECKS GOOD.

Part: LIGHT — INOPERATIVE (FORWARD CABIN) · airframe 5,588 hrs · 4,678 cycles

EMERGENCY LIGHTING SYSTEM INOPERATIVE ROWS 1 THROUGH 5. EXIT SIGN FOR ROW 8 ALSO INOPERATIVE, LOWER, LEFT HAND SIDE. REPLACED LIGHT STRIP AT FORWARD CABIN. OPS CHECK GOOD.

Part: WARNING LIGHT — ILLUMINATED (TE FLAPS) · airframe 5,228 hrs · 4,336 cycles

FLAPS FAIL CAUTION MESSAGE ON LANDING. FLAPS FAILED AT 0 DEGREES. INTERROGATED FECU PER FIM 27-50. ALL LRU'S PASSED ALL TESTS. OPS CHECK GOOD ON GROUND. OPERATED FLAPS SEVERAL TIMES ON GROUND. NO PROBLEMS NOTED.

Part: CONTROLLER — MALFUNCTIONED (TE FLAPS) · airframe 5,061 hrs · 4,187 cycles

DURING APPROACH TO FAT, ATTEMPTED TO EXTEND FLAPS. FLAPS FAIL CAUTION MESSAGE ILLUMINATED AND FLAPS REMAINED AT ZERO DEGREES. FOLLOWED QHR PROCEDURE. LANDED WITH FLAPS AT ZERO DEGREES. RESET CIRCUIT BREAKERS FOR FLAPS CONTROLLER CHANNELS 1 & 2 (CB1 & 2F4). FLAPS FAIL MESSAGE WENT AWAY. CYCLED FLAPS THROUGH SEVERAL CYCLES. OPS CHECK GOOD AT THIS TIME.

Part: CONTROL UNIT — MALFUNCTIONED (HORIZONTAL STAB) · airframe 4,412 hrs · 3,698 cycles

ON DESCENT INTO SMF, RECEIVED AN AP PITCH TRIM CAUTION MESSAGE AND A STAB TRIM 1 STATUS MESSAGE. COMPLIED WITH QRH AND RECONNECTED STAB TRIM NR 1. AFTER 5 MINUTES THE MESSAGE REOCCURED. RETURNED TO LAX. REPLACED HSTCU WITH SERVICEABLE UNIT. OPS CHECK GOOD AT THIS TIME. S/N OFF: 846.

Part: WARNING LIGHT — ILLUMINATED (STAB TRIM) · airframe 4,309 hrs · 3,613 cycles

STAB TRIM CH 1 MESSAGE ILLUMINATED IN FLIGHT. RETURNED TO DEN. INSTALLED SERVICEABLE HSTCU. OPS CHECK GOOD. NO DEFECTS NOTED.

Part: CONTROL UNIT — INOPERATIVE (CHANNEL 1) · airframe 4,346 hrs · 3,635 cycles

STAB CHANNEL 1 INOP WHILE STAB IS INTRANIT (HSTCU BITE CHECK INDICATES HSTCU CHANNEL 1 FAILURE). FOUND DURING C-CHECK INSPECTION - INCOMING RUNS. REPLACED HSTCU IAW AMM TASKS 27-41-01-000-801 AND 27-41-01-400-801. TESTED HSTCU SYSTEM IAW CRJ AMM TASKS 27-40-00-710-801, TASK 27-40-00-720-801 AND TEST 27-41-00-740-801. TESTED SERVICEABLE.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 4,346 hrs · 3,635 cycles

FS 621 RIGHT FLOOR SUPPORT ANGLE CRACKED. FOUND DURING C-CHECK INSPECTION. REPAIRED DAMAGE IAW CRJ REO 601R-53-61-117 REV 'A'. ANGLE P/N: 601R-53-61-004-2 REPAIR ANGLE P/N: 601R-53-61-004-6.

Part: ANGLE — CRACKED (INTERCOSTAL) · airframe 4,346 hrs · 3,635 cycles

FS 625 STR 14 LT AND RT INTERCOSTAL ANGLES CRACKED. FOUND DURING C-CHECK INSPECTION. ANGLES REPLACED IAW CRJ SRM 51-40-11, 51-42-06. P/N: 601-35012-51.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 4,346 hrs · 3,635 cycles

FS 280 RBL AND LBL 9.0 FLOORBEAMS INBOARD AND OUTBOARD ANGLES CRACKED. FOUND DURING C-CHECK INSPECTION. REPLACED ANGLES IAW CRJ SRM 51-40-11, 51-42-06, 51-42-13 AND 51-42-21. P/N: 601R31113-58.

Part: SWITCH — CONTAMINATED (RUDDER) · airframe 3,367 hrs · 2,833 cycles

ABORTED T/O DUE TO A RUDDER MISCONFIG. RUDDER TRIM CONTROL KNOB MIS-RIGGED. REPLACED RUDDER AND AILERON TRIM PANEL. RUDDER TRIM OPS CHECK GOOD. FOUND FAULTY RUDDER SWITCH.

Part: BPSU — MALFUNCTIONED (T/E FLAP) · airframe 2,931 hrs · 2,438 cycles

FLAPS FAIL CAUTION MESSAGE APPEARED WHILE CLIMBING THROUGH 10,000 FEET. FLAPS IN ZERO POSITION. DIVERTED TO FAT WHILE EN ROUTE TO OAK. REPLACED LEFT BPSU IAW CRJ MM 27-51-10 AND COMPLETED AD FORM 98-20-01-02. OPS CHECK GOOD.

Part: WIRE HARNESS — FAULTY (RT ENGINE) · airframe 2,689 hrs · 2,254 cycles

LEVEL AT 27,000 FEET, AFTER COWL ANTI-ICE WAS TURNED ON AND ASSOCIATED THRUST REDUCTION WAS MADE, THE RIGHT ENGINE N1 FLUCTUATED UNCOMMANDED 89.0 TO 95 PERCENT. ALSO ON DESCENT, WITH THRUST LEVER REDUCTION, RIGHT N1 FROM 81 TO 83 PERCENT. NOTICED SOME N2 FLUCTUATION OF UP TO + -1 PERCENT. RETURNED TO DENVER. REMOVED AND REPLACED BLUE, BROWN AND YELLOW ENGINE HARNESS. OPS CHECKS GOOD DURING ENGINE RUN ON GROUND IAW 73-21-13, 77-11-03 AND 73-21-05.

Part: HYDRAULIC LINE — LEAKING (NR 1 SYSTEM) · airframe 964 hrs · 643 cycles

HYD 1 LO PRESS MESSAGE ON INFLIGHT. QUANTITY AND PRESSURE AT 0. EXECUTED APPROPRIATE CHECK LISTS. DIVERTED TO GJT. ENGINE DRIVEN PUMP RAN DRY FOR 37 MINUTES. REMOVED AND REPLACED NR 1 HYDRAULIC ENGINE DRIVEN PUMP IAW 29-13-00 DUE TO BEING RAN DRY. REMOVED AND REPLACED NR 1 SYSTEM RETURN LINE DUE TO PIN HOLE IAW 29-11-00. C/W ENGINE RUN AND NR 1 ELECTRIC PUMP. OPS CHECK GOOD, NO LEAKS NOTED. S/N OFF: MX637287 LINE P/N: 601R75286-1

Part: CONTROL UNIT — MALFUNCTIONED (GROUND SPOILERS) · airframe 858 hrs · 541 cycles

INBOARD GROUND SPOILER FAULT MESSAGE.REPLACED SECU. OPS CHECK GOOD.

Part: SMOKE — DETECTED (CABIN) · airframe 388 hrs · 243 cycles

STRONG SMELL OF SMOKE ON LANDING. AFTER STOWING THRUST REVERSERS SMELL SEEMED TO SUBSIDE. PERFORMED RUN CHECK ON BOTH PACKS. NO SMOKE SMELL NOTED. OPS CHECK GOOD.

Part: FAN — FAILED (AIR DIST) · airframe 433 hrs · 269 cycles

ON CLIMBOUT RECEIVED ARINC COOL CAUTION MESSAGE. USED QRH PROCEDURE, MESSAGE WOULD NOT CLEAR. ON RETURN TO FAT DESCENDING THROUGH 25,000 FT MESSAGE WENT AWAY AFTER APPROXIMATELY 20 MINUTES.REPLACED ARINC FAN NR 1 AND REPLACED LOW FLOW ARINC DETECTOR. PERFORMED OPS TEST IAW 21-24-25. GROUND CHECK GRD ALT NORMAL/FLT ALT CHECK NORMAL.

Part: CONTROLLER — INOPERATIVE (DEICE SYSTEM) · airframe 180 hrs · 110 cycles

SHORTLY AFTER TAKE OFF GOT LEFT WINDOW HEAT CAUTION MESSAGE. RETURNED TO FAT. AFTER TROUBLESHOOTING SYSTEM FOUND FORWARD TEMP CONTROLLER INOP AND CANNON PLUGS SWAPPED. PUT CANNON PLUGS IN CORRECT POSITION AND REPLACED FORWARD TEMP CONTROLLER IAW CRJ MM 30-41-00. ALL OPS CHECKS GOOD AT THIS TIME. SN ON FORWARD 2454 SN OFF 2464 SN ON AFT 609, PN ON 1659-1.