N417SW

Part: CAP — CRACKED (BS 409) · airframe 45,492 hrs · 39,255 cycles

LBL 9 BEAM CAP FROM FS409+4 TO FS409+118 CRACKED. REPLACED FLOOR BEAM CAP FROM FS409+4 TO FS409+118 IAW REO.

Part: FLOOR SUPPORT — CORRODED (BS 409) · airframe 45,492 hrs · 39,255 cycles

CORROSION ON THE LEFT HAND FLOOR SILL FS409.00+96 - FS409.00+128. C-CHECK. REPAIRED LEFT HAND FLOOR SILL IAW REO AND SRM.

Part: SKIN — CHAFED (FUSELAGE) · airframe 45,492 hrs · 39,255 cycles

FUSELAGE EXTERIOR SKIN HAS SEVERAL CHAFES/SCRATCHES AT APU EXHAUST OPENING AFT END. REPAIRED IAW REO.

Part: PLATE — CORRODED (SERVICE DOOR) · airframe 45,492 hrs · 39,255 cycles

SERVICE DOOR BOTTOM PLATE ASSEMBLY CORRODED. INSTALLED NEW SERVICE DOOR BOTTOM PLATE ASSEMBLY IAW SRM.

Part: BRACKET — FAILED (NLG) · airframe 45,330 hrs · 39,100 cycles

GEAR DISAGREE WITH NOSE GEAR UNSAFE. PERFORMED QRH PROCEDURE AND LANDING GEAR CAME DOWN WITH NOSE DOOR UNSAFE MESSAGE ON. RECEIVED HYD 3 HI TEMP MESSAGE ON FINAL APPROACH. (FLT#5723) CLOSED REPLACED NOSE LANDING GEAR CENTERING SENSOR BRACKET IAW AMM AND PERFORMED GEAR SWING IAW AMM. OPS CHECK GOOD AT THIS TIME.

Part: UNKNOWN — NOISY (LANDING GEAR) · airframe 44,895 hrs · 38,716 cycles

GEAR DISAGREE UPON T/O WITH LOUD CLANKING NOISES. WHEN BRINGING THE GEAR DOWN FOR LANDING, LOUD CLANKING SOUND COULD BE HEARD AGAIN. (FLT#5011) CLOSED PERFORMED OPERATIONAL CHECK IAW AMM. SWUNG ALL LANDING GEARS MULTIPLE TIMES. COULD NOT DUPLICATE PROBLEM. OPS CHECK GOOD AT THIS TIME.

Part: UPLOCK — FAILED (NLG) · airframe 44,070 hrs · 37,951 cycles

ON CLIMB OUT WE SELECTED GEAR UP. NOSE GEAR DID NOT COME UP AND WE GOT A GEAR DISAGREE WARNING MSG. RAN QRH AND ABOUT 30 SECONDS AFTER TURNING ON HYDRAULIC PUMPS, NOSE GEAR CAME UP. ON LANDING, GEAR CAME DOWN NORMALLY. REPOSITION FLIGHT - NO PAX (FLT 1357) CLOSED REMOVED AND REPLACED THE NLG UPLOCK IAW AMM. LEAK CHECK AND OPS CHECK GOOD AT THIS TIME. ALL LANDING GEAR RETRACTED AND LOCKED WITH NO ISSUES.

Part: COALESCER BAG — ODOR (AC BAY) · airframe 43,905 hrs · 37,761 cycles

PACKS GAVE OFF A BURNING SMELL IN FLIGHT IN BOTH THE CABIN AND COCKPIT. (FLT 3134) CLOSED REMOVED AND REPLACED RT AND LT WATER SEPARATOR COALESCERS, IAW AMM. UPON OPERATIONAL TEST OF THE PACKS, FOUND NO SMELL PRESENT IN COCKPIT OR GALLEY. ALSO REMOVED AND REPLACED CEILING LIGHT BALLAST AT ROW 10C/D IAW AMM.

Part: ANGLE — CORRODED (DOOR SILL) · airframe 41,872 hrs · 35,362 cycles

SERVICE DOOR LOWER SILL CORRODED. INSTALLED NEW DOOR SILL ANGLE IAW SRM.

Part: STIFFENER — GOUGED (BS 621 BULKHEAD) · airframe 41,872 hrs · 35,362 cycles

GOUGE LOCATED ON BACK SIDE OF REAR PRESSURE BULKHEAD ON UPPER VERTICAL STIFFENER AT BS 621, BL 0. REPAIRED THE STIFFENER IAW REO.

Part: FRAME — CORRODED (BS 333) · airframe 41,872 hrs · 35,362 cycles

AVIONICS BAY FRAME BS 333 CORRODED STRINGERS 25L - 26R. REMOVED AND REPLACED THE FRAME SECTOR IAW SRM.

Part: SKIN — CHAFED (RT WING TE FLAP) · airframe 41,872 hrs · 35,362 cycles

RIGHT INBD FLAP VANE CHAFED ON OTBD SIDE. REMOVED THE WORN OUT OF LIMITS LEADING EDGE SKIN CAP FROM THE RIGHT HAND INBOARD FLAP OUTBOARD SECTION AND INSTALLED NEW SKIN IAW SRM.

Part: PRESSURE DECK — CRACKED (BS 459) · airframe 41,872 hrs · 35,362 cycles

PRESSURE FLOOR SKIN CRACKED BS 459, RBL 3 & 7. REPAIRED PRESSURE FLOOR IAW REO. PRESSURE CHECKED OKAY.

Part: FITTING — WORN (FAIRING) · airframe 41,872 hrs · 35,362 cycles

MLG BAY FORWARD FAIRING RIGHT SIDE ATTACH FITTINGS WORN OUT OF LIMITS. REMOVED AND REPLACED THE FAIRING FITTINGS IAW SRM.

Part: SKIN — CHAFED (LT AILERON) · airframe 41,872 hrs · 35,362 cycles

LEFT AILERON UPPER SKIN LEADING EDGE CHAFED. REPLACED THE AILERON UPPER LE SKIN IAW SRM.

Part: BULKHEAD — CRACKED (BS 621) · airframe 41,872 hrs · 35,362 cycles

BS 621 REAR PRESSURE BULKHEAD FORWARD FACE CRACKED AT BL 0, 58 INCHES ABOVE FLOOR. REPAIRED THE PRESSURE BULKHEAD IAW REO.

Part: SKIN — DENTED (BS 409) · airframe 41,872 hrs · 35,362 cycles

FUSELAGE SKIN DENTED BETWEEN BS 409+16 & 409+32, STRINGER 18 & 19L. REPAIRED IAW REO.

Part: SKIN — DAMAGED (BS 605) · airframe 41,349 hrs · 34,747 cycles

FOUND HOLE IN SKIN ON TOP OF FUSELAGE APPROXIMATELY BS 605 ABOUT 12 INCHES LT OF CENTERLINE. REPAIRED THE SKIN IAW SRM.

Part: SWITCH — FAILED (AC BAY) · airframe 40,384 hrs · 33,850 cycles

LEFT PACK DEFERRED. RIGHT PACK HIGH TEMP AND SHUTDOWN. CREW DEPLOYED O2 MASKS AND DECLARED EMERGENCY. RETURNED TO FIELD. R & R RT PACK OVER TEMPERATURE COMPRESSOR SWITCH IAW AMM. OPS CHECK GOOD AT THIS TIME. PN ON 750659-17AEC, SN ON 0093, PN OFF 750659-17AEC, SN OFF 000201.

Part: SHUTOFF VALVE — FAILED (AC BAY) · airframe 40,384 hrs · 33,850 cycles

LEFT PACK DEFERRED. RT PACK AUTO SHUTDOWN. CREW DECLARED EMERGENCY. RETURNED TO FIELD. R & R PRESSURE REGULATING/SHUTOFF VALVE IAW AMM. PN ON 979998-2 SNON 5336, PN OFF 979998-2, SN OFF 4453. R & R BLEED AIR SHUTOFF VALVE IAW AMM. PN ON 3215622-1, SN ON 1201, PN OFF 3215622-1, SN ON 942.

Part: OUTFLOW VALVE — OBSTRUCTED (CABIN PRESSURE) · airframe 39,020 hrs · 32,644 cycles

AT CABIN ALTITUDE CAUTION MESSAGE, DESCENDED TO FL 240 DURING DESCENT CABIN ALTITUDE CLIMBED QUICKLY AND MASK DROPPED. RAN QRH FOR EMERGENCY DESCENT. DIVERTED, FOUND A LARGE PIECE OF INSULATION BLANKET STUCK IN THE PRIMARY OUT FLOW VALVE, NOT ALLOWING IT TO MODULATE PROPERLY. REMOVED PIECE OF INSULATION BLANKET AND RESECURED INSULATION. PERFORMED PRESSURIZATION CHECK, PRESSURE CHECK GOOD AT THIS TIME.

Part: FRAME — CRACKED (BS 589) · airframe 38,044 hrs · 31,636 cycles

FUSELAGE FRAME AT BS 589 OUTER FLANGE IS CRACKED COMMON TO STRINGER 18L. REPAIRED THE FRAME IAW EA.

Part: BULKHEAD — CRACKED (BS 280) · airframe 38,044 hrs · 31,636 cycles

CRACKS ON FS 280 BULKHEAD WEB AT LBL 9 AND RBL 9. COMPLIED WITH REPAIR TO BULKHEAD WEB FS 280.00 LBL 20.75-RBL 20.75 IAW REO.

Part: FRAME — CRACKED (BS 605) · airframe 38,044 hrs · 31,636 cycles

FUSELAGE FRAME AT BS 605 OUTER FLANGE IS CRACKED AT FASTENERS COMMON TO STR 18L. REPAIRED THE FRAME IAW EA.

Part: PANEL — OUT OF TOLERANCE (HORIZONTAL STAB) · airframe 38,044 hrs · 31,636 cycles

HORIZONTAL STABILIZER VISOR PANEL 326AR FAILED GAP CHECK. RECONTOURED VISOR PANEL 326AR IAW REO AND AMM.

Part: ANGLE — DAMAGED (BS 559) · airframe 38,044 hrs · 31,636 cycles

BS 559 LOWER CAP ANGLES BL 9.00 AND 18.00 LT SIDE AND RT SIDE. REPAIR AND REINFORCEMENT FOR FS559.00 LOWER CAP ANGLES BL 9.00 AND 18.00 LT SIDE AND RT SIDE IAW REO.

Part: STRUCTURE — DAMAGED · airframe 37,248 hrs · 30,867 cycles

MULTIPLE BIRD STRIKE DAMAGING RT L/E AND LT NOSE AND FUSELAGE DURING LANDING. REPAIRED IAW REO.

Part: BATTERY PACK — INOPERATIVE (FLASHLIGHT) · airframe 36,526 hrs · 30,163 cycles

F/A FLASHLIGHT IS INOPERATIVE. REPLACED FLASHLIGHT BATTERIES.

Part: WIRE HARNESS — DAMAGED (NLG) · airframe 36,196 hrs · 29,829 cycles

EXTENDED GEAR AND IT TOOK ABNORMALLY LONG TIME TO COME DOWN. LOUD POPPING SOUND FROM NOSE WHEEL. OVERFLEW AIRPORT. ATC CONFIRMED GEAR DOWN BEFORE LANDING. COULD NOT DUPLICATE. R & R THE NLG DOWNLOCK WIRE HARNESS IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 36,117 hrs · 29,745 cycles

RIGHT AFT EMERGENCY LIGHT INOPERATIVE. R & R RT AFT EMERGENCY LIGHT IAW AMM.

Part: BUSHING — CORRODED (LT ENGINE MOUNT) · airframe 35,489 hrs · 29,136 cycles

DURING C-CHECK, LEFT ENGINE MOUNT LINK BUSHINGS FOUND PITTED AND WORN. , REPLACED LT ENGINE MOUNT LINK BUSHINGS IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 34,924 hrs · 28,584 cycles

OVERHEAD EMERGENCY LIGHT IN AFT CABIN IS BURNED OUT. FLT 2598 RELAMPED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 34,821 hrs · 28,476 cycles

NR 2 OVERHEAD EMERGENCY LIGHT IS BURNED OUT. SERVICE RELAMPED.

Part: CHARGER — FAILED (CABIN) · airframe 34,620 hrs · 28,268 cycles

FWD EMERGENCY OVERHEAD LIGHT DOES NOT ILLUMINATE. SERVICE REPLACED BATTERY CHARGER ASSEMBLY NR 1 IAW AMM.

Part: PAINT — MISINSTALLED (TE FLAP) · airframe 34,412 hrs · 28,052 cycles

ON FINAL APPROACH AT APPROXIMATELY 1000' FT AGL, FLAPS 45°, ON SPEED, TRIMMED OUT. AIRCRAFT BEGAN SUDDEN LT ROLL WITH AUTOPILOT OFF. SIGNIFICANT RWD TRIM ADDED TO CORRECT & FLY AIRCRAFT. NO ASSOCIATED EICAS MESSAGES DISPLAYED. FLT#2583 FOUND EXCESSIVE PAINT RUNS & EXCESSIVE SEALANT ON FORE FLAP & FLAP LE ON LT INBD & OTBD FLAP. RESTORED AERODYNAMIC SMOOTHNESS IAW SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 34,397 hrs · 28,036 cycles

EMERGENCY CEILING POD LIGHT BURNED OUT. FLT#2636 RELAMPED.

Part: TRANSCEIVER — FAILED (RADIO ALTIMETER) · airframe 34,228 hrs · 27,855 cycles

CONFIGURE WARNING & GROUND SPOILER DEPLOY MESSAGE. FLT#2643 REPLACED NR 1 RAD ALT TRANSCEIVER ALT-55B & NR 1 SECU IAW AMM. PN ON OFF 49-164-20, SN ON 03377, SN OFF 03060, PN ON OFF 622-2855-011, SN ON 21DJR & SN OFF 4PHW.

Part: BULKHEAD — DAMAGED (FUSELAGE) · airframe 34,025 hrs · 27,646 cycles

HOLE IN FS621 BULKHEAD ON LBL 31.4 & 2.3" ABOVE CARGO FLOOR. C-CHECK REPAIR TO FS621 BULKHEAD WEB. CUT AWAY DAMAGED AREA ON FS621 BULKHEAD WEB AT LBL 31.4 & 2.3" ABOVE CARGO FLOOR & INSTALLED DOUBLER FROM 2024-T3 IAW REO.

Part: VANE — CHAFED (TE FLAP) · airframe 34,025 hrs · 27,646 cycles

LT INBD FLAP VANE CHAFED ON INBD END. C-CHECK BLENDED LT INBD FLAP VANE INBD END IAW REO.

Part: VANE — CHAFED (TE FLAP) · airframe 34,025 hrs · 27,646 cycles

LT INBD FLAP VANE CHAFED ON OTBD END.. C-CHECK BLENDED LT INBD FLAP VANE OTBD END IAW REO.

Part: POST — CRACKED (FUSELAGE) · airframe 34,025 hrs · 27,646 cycles

VERTICAL POST ON FS409.0 +128 RBL 18.0 HAS CRACK ON INBD SIDE OF POST. C-CHECK REPLACED VERTICAL POST AT FS409.0 + 128 RBL 18.0 INBD SIDE IAW REO.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 33,220 hrs · 26,789 cycles

F/O WINDSHIELD CRACKED IN CRUISE. (FLT 2611) REPLACED F/O WINDSHIELD IAW AMM. P/N: NP-139321-6 S/N ON: 2214H5385 S/N OFF: 2140R6529

Part: BUCKLE — OUT OF ADJUST (FA SEATBELT) · airframe 32,439 hrs · 25,910 cycles

FLIGHT ATTENDANT SEATBELT BUCKLE IS HARD TO UNLATCH. (FLT 6533) ADJUSTED FLIGHT ATTENDANT SEATBELT BUCKLE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,220 hrs · 25,755 cycles

NR 4 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5658) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,110 hrs · 25,668 cycles

NR 4 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5652) RELAMPED EMERGENCY LIGHT.

Part: DOOR — LACK OF LUBE (CABIN) · airframe 31,176 hrs · 24,901 cycles

MAIN CABIN DOOR DIFFICULT TO OPEN. (FLT 5232) LUBRICATED MAIN CABIN DOOR IN REF TO AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,695 hrs · 24,515 cycles

NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6190) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,545 hrs · 24,401 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5327) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,458 hrs · 24,342 cycles

NR 1 RIGHT SIDE OVERWING EMERGENCY LIGHT IS OUT. (FLT 5302) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 30,274 hrs · 24,190 cycles

NR 3 EXTERIOR EMERGENCY LIGHT OVER THE LEFT WING IS OUT. (FLT 6268) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,218 hrs · 24,150 cycles

THE 3RD EMERGENCY OVERHEAD LIGHT IS OUT. (FLT 5484) RELAMPED EMERGENCY LIGHT.

Part: POST — CRACKED (FUSELAGE) · airframe 31,295 hrs · 24,997 cycles

FS 409.0+128 LEFT VERTICAL POST AT LBL 18.0 ON THE OUTBOARD AFT RADIUS IS CRACKED. (C-CHECK) REPLACED SECTION OF POST AT FS 409+128 LBL 18.0 IN REFERENCE TO CRJ SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,972 hrs · 23,947 cycles

NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5472) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,750 hrs · 23,778 cycles

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

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 29,750 hrs · 23,778 cycles

FORWARD LEFT SIDE EXTERIOR EMERGENCY IS OUT. (FLT 6527) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,675 hrs · 23,699 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 2968) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,208 hrs · 23,259 cycles

NR 1 CEILING EMERGENCY LIGHT IS OUT. (FLT 4760) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,077 hrs · 23,140 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4625) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN DOOR) · airframe 28,697 hrs · 22,830 cycles

BOTTOM EMERGENCY LIGHT ON MAIN CABIN DOOR STAIRS IS OUT. (FLT 6752) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,011 hrs · 22,255 cycles

NR 4 OVERHEAD EMERGENCY LIGHT OUT. (FLT 6306) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,866 hrs · 22,140 cycles

EMERGENCY CEILING LIGHT CLOSEST TO LAV OUT. (FLT 6729) RELAMPED EMERGENCY LIGHT.

Part: PIN — JAMMED (CABIN DOOR) · airframe 27,288 hrs · 21,665 cycles

MAIN CABIN DOOR WILL NOT OPEN FROM OUTSIDE. (FLT 6674) RE-INSTALLED DOOR RAIL PIN.

Part: LIGHT — BROKEN (CABIN) · airframe 26,962 hrs · 21,404 cycles

THE AFT CEILING EMERGENCY FLOOD LIGHT INOPERATIVE. (FLT 6046) REMOVED AND REPLACED EMERGENCY LIGHT.

Part: DOOR — MALFUNCTIONED (CABIN) · airframe 26,561 hrs · 21,064 cycles

MAIN CABIN DOOR WOULD NOT OPEN. (FLT 5985) COULD NOT DUPLICATE PROBLEM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,561 hrs · 21,064 cycles

AFT EMERGENCY LIGHT INOP. (FLT 6915) RELAMPED EMERGENCY LIGHT.

Part: TORQUE TUBE — OBSTRUCTED (CABIN DOOR) · airframe 25,660 hrs · 20,309 cycles

UNABLE TO OPEN MAIN CABIN DOOR. (FLT 6154) REMOVED EXCESS GREASE AT DOOR LATCH CAM TORQUE TUBE.

Part: DOOR — DIRTY (CABIN) · airframe 25,592 hrs · 20,259 cycles

CABIN DOOR IS DIFFICULT TO OPEN. (FLT 6741) CLEANED AND LUBED CABIN DOOR.

Part: LATCH — LACK OF LUBE (MAIN DOOR) · airframe 25,534 hrs · 20,215 cycles

MAIN CABIN DOOR DIFFICULT TO OPEN. (FLT 6445) LUBED PASSENGER DOOR SEAL AND LATCHES.

Part: LATCH — LACK OF LUBE (MAIN DOOR) · airframe 25,534 hrs · 20,215 cycles

MAIN CABIN DOOR DIFFICULT TO OPEN. (FLT 6762) LUBED LATCH ASSEMBLY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,372 hrs · 20,072 cycles

CEILING EMERGENCY FLOOD LIGHT AT ROW 10 INOP. (FLT 4626) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,324 hrs · 20,030 cycles

SECOND AFT EMERGENCY LIGHT INOP. (C CHECK) RELAMPED EMERGENCY LIGHT.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 25,283 hrs · 20,000 cycles

FS621 PRESSURE BULKHEAD WEB CRACKED AT AFT CARGO DOOR ROLLER GUIDE TRACK. (C-CHECK) REPAIRED PER REO 601R-53-61-1541.

Part: LANYARD — OUT OF POSITION (MAIN DOOR) · airframe 25,010 hrs · 19,753 cycles

UNABLE TO OPEN MAIN DOOR FULLY. (FLT 7556) REPOSITION FWD PAX DOOR HANDRAIL PIP PIN LANYARD AND RE-SECURED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,747 hrs · 19,512 cycles

FORWARD EMERGENCY CEILING FLOOD LIGHT INOP. (FLT 6586) RELAMPED EMERGENCY LIGHT.

Part: TORQUE TUBE — OUT OF ADJUST (CABIN DOOR) · airframe 24,562 hrs · 19,346 cycles

MAIN CABIN DOOR HARD TO OPEN FROM OUTSIDE. (FLT 4614) ADJUSTED TORQUE TUBES AND LATCH CAMS.

Part: GLOWSTRIP — MISSING (CABIN) · airframe 23,588 hrs · 18,596 cycles

FLT 6207 - 2 STRIPS OF PHOTO LUMINESCENT EXIT PATH LIGHTING MISSING. REINSTALLED MISSING SECTION OF PHOTO LUMINESCENT EXIT PATH LIGHTING.

Part: HANDLE — DIRTY (PAX DOOR) · airframe 23,272 hrs · 18,360 cycles

FLT 6505 - MAIN CABIN DOOR EXTERIOR HANDLE VERY HARD TO OPEN. CLEANED AND LUBED OUTER DOOR HANDLE.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 22,792 hrs · 18,002 cycles

FLT 5835 - ENTRANCE FLOOR EMERGENCY LAMP ONE LIGHT INOP. RELAMPED.

Part: DOOR — BINDING (MAIN PAX) · airframe 22,174 hrs · 17,504 cycles

CREW COULD NOT OPEN MAIN CABIN DOOR FROM OUTSIDE. INSPECTED AND OPERATED MAIN CABIN DOOR SEVERAL TIMES. OPS CHECK GOOD.

Part: HANDLE — BINDING (PAX DOOR) · airframe 22,021 hrs · 17,370 cycles

MAIN CABIN DOOR OUTER HANDLE WOULD NOT OPEN DOOR. (FLIGHT NR 5901) INSPECTED AND LUBED PAX DOOR IAW 52-11-00. CYCLED DOOR SEVERAL TIMES AND OPS CHECK GOOD.

Part: FITTING — OUT OF ADJUST (PAX DOOR) · airframe 21,967 hrs · 17,323 cycles

MAIN CABIN DOOR IS HARD TO OPEN. (FLIGHT NR 2813) ADJUSTED BOTH MAIN CABIN DOOR SPIGOT FITTINGS. OPS CHECK GOOD IAW 52-00-00.

Part: CAM — BINDING (PAX DOOR) · airframe 21,967 hrs · 17,323 cycles

THE PASSENGER DOOR WILL NOT OPEN OR CLOSE. (FLIGHT NR 2531) CLEANED AND INSPECTED PAX DOOR MECHANISM AND CAMS. CYCLED DOOR SEVERAL TIMES. OPS CHECK GOOD.

Part: SWITCH — DIRTY (THRUST REVERSER) · airframe 21,930 hrs · 17,286 cycles

FLT 2522 - RECEIVED 'L REV UNLOCKED' MESSAGE INFLIGHT. CLEANED AND INSPECTED ALL SWITCHES AND PDU ON LEFT REVERSER. OPS CHECK GOOD.

Part: CAM — LACK OF LUBE (PAX DOOR) · airframe 21,845 hrs · 17,196 cycles

FLT 2804 - PAX DOOR IS DIFFICULT TO OPEN. INSPECTED AND LUBRICATED DOOR CAMS AND DOOR ASSIST MECHANISM. OPS CHECK GOOD.

Part: ROLLER — BINDING (PAX DOOR) · airframe 21,796 hrs · 17,141 cycles

MAIN CABIN DOOR IS VERY DIFFICULT TO OPEN. (FLIGHTNR 2875) ADJUSTED PAX DOOR SPIGOT ROLLER ASSEMBLY AND AFT MIDDLE LATCH PIN IAW AMM CHAPTER 52-11-00. CABIN DOOR OPS CHECK GOOD AT THIS TIME.

Part: EXTINGUISHER — DISCHARGED (LAVATORY) · airframe 21,788 hrs · 17,129 cycles

LAVATORY TRASH FIRE EXTINGUISHING BOTTLE IS DISCHARGED. (FLT 2778) REMOVED AND REPLACED THE LAVATORY TRASH FIRE BOTTLE AS NEEDED PER MM 26-26-01.

Part: BULKHEAD — CRACKED (AFT) · airframe 22,451 hrs · 17,721 cycles

REAR PRESSURE BULKHEAD WEB HAS .5 INCH CRACK (C-CHECK). REPAIRED PER REO.

Part: BULKHEAD — CRACKED (AFT) · airframe 22,451 hrs · 17,721 cycles

REAR PRESSURE BULKHEAD WEB HAS .5 INCH CRACK (C-CHECK). REPAIRED PER REO.

Part: SUPPORT BEAM — CRACKED (CARGO DOOR) · airframe 22,451 hrs · 17,721 cycles

CARGO DOOR SUPPORT BEAM LOWER ANGLE IS CRACKED (C-CHECK). REPLACED CARGO DOOR SUPPORT ANGLE.

Part: BULKHEAD — CRACKED (AFT) · airframe 22,451 hrs · 17,721 cycles

REAR PRESSURE BULKHEAD WEB AT LINTEL ATTACHMENT HAS .2 INCH CRACK (C-CHECK). REPAIRED PER REO.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHTS) · airframe 21,448 hrs · 16,777 cycles

FLT 2522 - FLOOR LEVEL EMERGENCY LIGHT AT MAIN CABIN DOOR ENTRANCE IS INOP. RESECURED CONNECTOR TO EMERGENCY LIGHT. OPS CHECK GOOD.

Part: DOOR — LACK OF LUBE (PAX DOOR) · airframe 20,480 hrs · 16,090 cycles

FLT 2509 - MAIN CABIN DOOR HANDLE WOULD NOT OPEN FROM THE OUTSIDE. INSPECTED, CLEANED AND LUBED DOOR. NO DEFECTS NOTED AT THIS TIME.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHTS) · airframe 20,271 hrs · 15,939 cycles

FLT 2912 - FLOOR LEVEL EMERGENCY EXIT LIGHT NEAR PAX DOOR IS INOP. SECURED PIN IN CONNECTOR OF EMERGENCY LIGHT IAW MM 33-51-00.

Part: PUMP — LEAKING (HYD SYSTEM) · airframe 19,765 hrs · 15,583 cycles

RECEIVED HYDRAULIC SYSTEM 1 LOW PRESSURE CAUTION MESSAGE. RETURNED TO RDU, FLIGHT NR 2702. REPLACED FLEX LINE AND NR 1 EDP IAW 32-29-01. OPS AND LEAK CHECK GOOD, PN 88705, SN OFF MX-600582.

Part: SHUTOFF VALVE — ODOR (APU FUEL SYS) · airframe 18,304 hrs · 14,532 cycles

STRONG ODOR OF FUEL WHEN APU IS RUNNING ON GROUND. REPLACED METERED FUEL OUTLET TUBE AND FUEL SHUT OFF VALVE IAW 49-31-01. OPERATIONAL CHECKS GOOD.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 18,066 hrs · 14,358 cycles

EXIT LIGHT OUT NEXT TO GALLEY SERVICE DOOR. REPAIRED BROKEN WIRE AT LIGHT ASSEMBLY. OPERATIONAL CHECKS GOOD.

Part: STRINGER CLIP — CRACKED (BS 280) · airframe 18,179 hrs · 14,434 cycles

LBL9 FS 280 OTBD CLIP CRACKED AT UPPER RADIUS AT FLANGE ATTACHED TO 280 BEAMS, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED CLIP P/N 601R3113-57 (PO 40800) AS PER CRJ200 SRM 51-42-21.

Part: STRINGER CLIP — CRACKED (BS 625) · airframe 18,179 hrs · 14,434 cycles

STA 625 CLIP STR 13 RT SIDE CRACKED, DISCOVERED DURING C-CHECK INSPECTION. REPLACED SUPPORT CLIP AT FS 625 STR 13 RT SIDE WITH P/N 601-35012-52 (PO 68411) AS PER CRJ200 SRM REFERENCE 51-42-21 PAGE 17-21.

Part: STEP — CRACKED (PAX DOOR) · airframe 18,179 hrs · 14,434 cycles

PAX DOOR BELOW BOTTOM STEP SUPPORT BRACKETS (3 EA) FOUND TO BE CRACKED, DISCOVERED DURING C-CHECK INSPECTION. REMOVED AND REPLACED PAX DOOR SUPPORT BRACKETS P/N 601R 31902-147/601R31902-147/601R31902-544 PER CRJ 200 SRM 51-42-6 PG 11/51-40-11 PG 4/51-41-02 PG 1/2.

Part: STRINGER CLIP — CRACKED (BS 280) · airframe 18,179 hrs · 14,434 cycles

RBL9.0 FS280 INBD AND OTBD CLIP CRACKED AT UPPER RADIUS AT FLANGE ATTACHED TO 280 FLAIR BEAM, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED FABRICATED CLIPS AT FS 280 RBL9 AS PER CRJ200 SRM 51-42-21.

Part: FRAME — CRACKED (PAX DOOR) · airframe 18,179 hrs · 14,434 cycles

PAX DOOR AFT OUTER SKIN INTERNAL FRAME CRACKED, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED REPAIR PIECE PER REO 601R 52-11-402.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 18,179 hrs · 14,434 cycles

FS 280 FLOORBEAM HAS A 2" CRACK AT LBL 9-11 PROTRUDING FROM THE ALT EXT PULLEY MOUNT ON THE LOWER EDGE OF THE BEAMS WEB, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED REPAIR PARTS AND 2EA NEW CLIPS TO FS 280 LBL 9-11 LOWER EDGE PER CRJ200 SRM 51-42-06 PG 11/ 51-42-21; PG 17.

Part: STRINGER CLIP — CRACKED (BS 624 S14L) · airframe 18,179 hrs · 14,434 cycles

FS 624 STR 14 LT SIDE SUPPORT CLIP CRACKED, DISCOVERED DURING C-CHECK INSPECTION. REPLACED DAMAGED SUPPORT CLIP AT FS624 STR 14 LH SIDE WITH P/N 601-35012-51 AS PER CRJ200 SRM REFERENCE 51-42-21 PAGE 17-21.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 16,289 hrs · 13,008 cycles

ROW 13 OVERHEAD EMERGENCY LIGHT INOP. REPLACED OVERHEAD EMERGENCY LIGHT LAMP AT ROW 13. OPERATIONAL CHECK GOOD.

Part: DOOR — BINDING (MAIN PAX) · airframe 15,631 hrs · 12,515 cycles

MAIN CABIN DOOR DIFFICULT TO OPEN AND CLOSE/LOCK FROM OUTSIDE/INSIDE. REPLACED INTERNAL CENTER BELLCRANK AND ALL ASSOCIATED HARDWARE IAW MM 52-11-02. OPERATIONAL CHECK OK.

Part: WINDSHIELD — FAILED (COCKPIT) · airframe 15,539 hrs · 12,445 cycles

ON TAXI OUT, LEFT WINDSHIELD SHATTERED RETURNED TO GATE. REPLACED LEFT WINDSHIELD IAW MM 56-11-01, PN NP-139321-5 SN OFF 01130H7181.

Part: CONTROL UNIT — MALFUNCTIONED (TE FLAPS) · airframe 15,477 hrs · 12,399 cycles

ON SETTING FLAPS TO 8 DEG, FLAPS HALFSPEED STATUS MSG. INSTALLED A SERVICEABLE FECU IAW MM 27-51-05. OPERATIONAL CHECK GOOD. PN ON 860D100-18ABCD OFF 725

Part: LATCH — BINDING (PAX DOOR) · airframe 14,602 hrs · 11,717 cycles

MAIN CABIN DOOR WON'T OPEN FROM OUTSIDE. CLEANED PAX DOOR LATCH PINS. CYCLED PAX DOOR HANDLE NUMEROUS CYCLES. OPERATIONAL CHECK GOOD.

Part: RIB — CRACKED (LT WING) · airframe 14,950 hrs · 11,987 cycles

LEFT BATTERY RIB IN MLG BAY CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED IAW 601R-57-51-046.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 14,950 hrs · 11,987 cycles

FLOORBEAM AT FS 280 IS CRACKED AT O/B OF RBL 9.0 AND LBL 9.0. ITEM FOUND AT C-CHECK INSPECTION. INSTALLED REPAIR ANGLE IAW REO 601R 53-11-136.

Part: RIB — CRACKED (RT WING) · airframe 14,950 hrs · 11,987 cycles

RIGHT BATTERY RIB IN MLG BAY CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED IAW REO 601R-57-51-046.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 14,950 hrs · 11,987 cycles

PAX DOOR AFT DRAG ANGLE IS CRACKED ABOVE DOOR ASSIST PULLEY. ITEM FOUND AT C-CHECK INSPECTION. INSTALLED DRAG ANGLE AND SPLICES IAW REO 601R-52-11-513.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 14,950 hrs · 11,987 cycles

FLOORBEAM AT FS 280 IS CRACKED AT O/B OF RBL 9.0 AND LBL 9.0. ITEM FOUND AT C-CHECK INSPECTION. INSTALLED REPAIR ANGLE IAW REO 601R 53-11-136.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 14,950 hrs · 11,987 cycles

TRANSVERSE FLOORBEAM AT FS 280 IS CRACKED O/B OF RBL 9.0 AND LBL 9.0. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED IAW 51-42-06 PG 1-20 AND 51-42-21 PG 1-4 AND REO 601R-53-11-171.

Part: MECHANISM — DIRTY (PAX DOOR) · airframe 11,884 hrs · 9,594 cycles

FLIGHT ATTENDANT COULD NOT OPEN MAIN CABIN DOOR FROM INSIDE AIRCRAFT. CLEANED AND REMOVED DEBRIS FROM FUSELAGE CUTOUT. OPERATIONAL CHECK GOOD.

Part: SENSOR — MALFUNCTIONED (AOA) · airframe 10,527 hrs · 8,528 cycles

DURING TAXI OUT STALL FAIL MESSAGE INTERMITTENLY CYCLES ON AND OFF. REMOVED AND REPLACED RIGHT AOA VANE IAW MM 27-35-05. OPS CHECKS GOOD.

Part: CONTROL UNIT — MALFUNCTIONED (STAB TRIM) · airframe 10,416 hrs · 8,443 cycles

STAB TRIM 2 WILL NOT TEST CORRECTLY. ROCKER SWITCH DISENGAGES STAB 2. REMOVED AND REPLACED STAB MOTOR CONTROL UNIT AND HORIZONTAL ACTUATOR IAW MM 27-40-00, 27-48-00 & RII CARD 27-415.

Part: WIRE — BROKEN (STICK SHAKER) · airframe 10,325 hrs · 8,376 cycles

LEFT STICK SHAKER INOP. REPAIRED BROKEN WIRE AT CANNON PLUG ON LEFT SHAKER. OPS TESTED GOOD.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 9,030 hrs · 7,398 cycles

FS 484 RT INTERCOSTAL O/B FLANGE RBL 36 CRACKED. DISCOVERED DURING C-CHECK. INTERCOSTAL REPAIRED IAW CRJ REO 601R-53-41-059 REV. ''A''. P/N: S6144-14

Part: ANGLE — CRACKED (FUSELAGE) · airframe 9,030 hrs · 7,398 cycles

AFT EQUIPMENT COMPARTMENT DOOR CUTOUT FS 700 RT ANGLE CRACKED. DISCOVERED DURING C-CHECK. REPLACED ANGLE IAW 51-40-11. P/N: 601-35013-12

Part: SILL — CRACKED (FUSELAGE) · airframe 9,030 hrs · 7,398 cycles

CARGO FLOOR SILL PLATE CRACKED AT FS 576.00, LBL 36, WL 73.50. DISCOVERED DURING C-CHECK. REPAIRED DAMAGE IAW CRJ REO 601R-53-61-690 REV. ''A''.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 9,030 hrs · 7,398 cycles

FS 280 RT FLOORBEAM ATTACH ANGLE I/B & O/B CRACKED. DISCOVERED DURING C-CHECK. ANGLES REPLACED IAW CRJ SRM 51-40-11. P/N: 601R-31113-58

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 9,030 hrs · 7,398 cycles

FS 484 LT INTERCOSTAL I/B & O/B FLANGES LBL 27 + LBL 36 CRACKED. DISCOVERED DURING C-CHECK. INTERCOSTAL REPAIRED IAW CRJ REO 601R-53-41-059 REV. ''A''. P/N: S6144-14

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 9,030 hrs · 7,398 cycles

FS 280 LT FLOORBEAM ATTACH ANGLE LBL 9 IB AND OB CRACKED. DISCOVERED DURING C-CHECK. ANGLES REPLACED IAW CRJ SRM 51-40-11. P/N: 601R-31113-57

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 9,030 hrs · 7,398 cycles

FS 625 LT INTERCOSTAL ANGLE STR 14L CRACKED. DISCOVERED DURING C-CHECK. ANGLE REPLACED IAW CRJ SRM 51-40-11. P/N: 601-35012-51

Part: AXLE — CORRODED (NLG) · airframe 9,187 hrs · 7,511 cycles

NLG AXLE ASSY HAS PITTING CORROSION AROUND BOLT HOLES. DISCOVERED DURING C-CHECK INSPECTION. NLG AXLE ASSY REPLACED IAW CRJ MM 32-21-15-000-801 AND 32-21-15-400-801. OPS CHECKS GOOD.

Part: PCU — MALFUNCTIONED (SPOILERONS) · airframe 6,942 hrs · 5,790 cycles

SPOILERON FAULT MESSAGE (STATUS) APPEARED AFTER ENGINE START. REMOVED AND REPLACED SPOILERON PCU ASSEMBLY IAW 27-62-01. OPS AND LEAK CHECKS GOOD.

Part: CONTROL UNIT — MALFUNCTIONED (HORIZ STAB) · airframe 6,829 hrs · 5,702 cycles

STAB TRIM CH1 STATUS MESSAGE INTERMITTENTLY ON. ABLE TO RESET 1ST 2 TIMES, 3RD TIME TOOK SEVERAL TRIES TO RESET. REMOVED AND REPLACED MCU, HSTA AND HSTCU IAW 27-42-01 AND 27-42-05. SYSTEMS OPS CHECK GOOD IAW 27-41-00.

Part: SWITCH — DIRTY (HORIZ STAB) · airframe 6,766 hrs · 5,652 cycles

STAN CHANNEL NR 1 INOP MESSAGE CAME ON AND WOULD NOT RESET. CLEANED STAB TRIM ENGAGE SWITCHES. PERFORMED OPERATIONAL CHECK OF HSTCU IAW MM 27-10-00-710-801 AND SELF DIAGONOSTICS OF HSTCU IAW MM 27-41-00-790-801. OPERATIONAL CHECKS SATISFACTORY. NO DEFECTS NOTED AT THIS TIME.

Part: SENSOR — FAULTY (WING) · airframe 6,460 hrs · 5,423 cycles

ON CLIMBOUT, INTERMITTENT WING OVHT MSG ILLUMINATED. FOLLOWED QRH PROCEDURE. MESSAGE STAYED OUT AT LOWER POWER SETTINGS. RETURNED TO SLC. REPLACED SUFFICIENT/OVERHEAT SENSOR IAW MM 30-12-23. OPS CHECK GOOD.

Part: SCREW — LOOSE (WINDOW HEAT) · airframe 6,392 hrs · 5,368 cycles

F/O'S WINDSHIELD HEAT IS SPARKING IN THE TERMINAL BOX. TIGHTENED UPPER TERMINAL SCREW. OPS CHECK OK.

Part: TORQUE LINK — BENT (NLG) · airframe 6,304 hrs · 5,298 cycles

ON DEPARTURE OUT OF DFW, DURING GEAR RETRACTION, WARNING MESSAGES GEAR DISAGREE AND NOSE DOOR ANNUNCIATED. THE NOSE GEAR INDICATED DOWN AND LOCKED WITH GEAR SELECTED UP. COMPLETED QRH PROCEDURES AND AFTER BURNING OFF EXCESS FUEL, A NORMAL LANDING WAS MADE BACK AT DFW. STRAIGHTENED NOSE GEAR TORQUE LINK BRACKET AND CALIBRATED PROX SENSOR GAP. SWUNG GEAR 3 TIMES WITH NORMAL OPERATION.

Part: ADC — FAILED (NR 1) · airframe 4,517 hrs · 3,883 cycles

NR 1 ADC FAILED EN ROUTE. RECEIVED IAS FLAG ON CAPTAIN'S SIDE ASSOCIATED WITH EFIS COMP MON MESSAGE. REMOVED AND REPLACED NR 1 ADC. OPS CHECK GOOD IAW 34-13-01.

Part: CONTROL UNIT — MALFUNCTIONED (TE FLAPS) · airframe 3,735 hrs · 3,272 cycles

FLAP FAIL MESSAGE ON EICAS WHEN FLAPS SELECTED TO 30 DEGREES.COMPLIED WITH AD 98-20-01 BY COMPLYING WITH PARAGRAPH (B)(1) 1-4. NO DISCREPANCIES NOTED.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 3,460 hrs · 3,062 cycles

CLIMBING THROUGH 10,000 MSL - DISPLAY COOL CAUTION MESSAGE. FOLLOWED QRH PROCEDURE AND SWITCHED TO FLT ALT. MESSAGE BRIEFLY WENT AWAY THEN RETURNED. SWITCHED TO STANDBY POSITION - MESSAGE EXTINGUISHED. RETURNED TO SLC. REPLACED P196325 DISPLAY COOL INLET FILTER. OPS CHECK OK.

Part: WARNING SYSTEM — ACTIVATED (SPOILERS) · airframe 3,390 hrs · 3,009 cycles

WHITE SPOILERON FAULT MESSAGE ON EICAS. RETURN TO GATE AS PER QRH.DEFERRED AS PER MEL 27-65-3. COMPLIED WITH MAINTENANCE PROCEDURE PER MEL. SUPPLEMENTAL REPORT FORTHCOMING. UPDATE 7/26/2001: REMOVED AND REPLACED NR 2 SECU IAW MM 27-60-01. SPOILERS CHECK GOOD.

Part: PCU — FAULTY (SPOILER) · airframe 3,300 hrs · 2,943 cycles

RIGHT SPOILERON WHITE MESSAGE ON MID FLIGHT TO LANDING. REMOVED RIGHT INBOARD SPOILERON PCU, REPLACED WITH SERVICEABLE PCU IAW MM 27-62-01. LEAK CHECK OK.

Part: ECU — FAILED (SPOILER) · airframe 3,294 hrs · 2,936 cycles

SPOILERON FAULT MESSAGE ON EICAS DURING TAXI WITH SPOILERON OUTLINED IN WHITE. RESET SECU SPOILER FAULT STATUS MESSAGE IN ACCORDANCE WITH CRJ AMM 27-61-00. INSTALLED SERVICEABLE SECU ON NR 1 SIDE. TEST GOOD IAW 27-60-00. OPS CHECK GOOD.

Part: CONNECTOR — LOOSE (HYD SYSTEM) · airframe 3,167 hrs · 2,837 cycles

DURING CLIMB OUT THROUGH 18,000 FT LEFT ENGINE HAD UNCOMMANDED ACCELERATION. N1 WENT INTO RED. REDUCED THRUST LEVERS ON LEFT ENGINE SUCESSFULLY AND RETURNED TO SLC. PERFORMED FAN ROTOR N1 OVERSPEED INSPECTION PER RJ MM 71-00-00 PG 504 TABLE 503. NO DEFECTS FOUND OF INLET AND TAILPIPE AREAS. PERFORMED UNCOMMANDED ACCELERATION FAULT ISOLATION PER GE MM 72-00-00 FAULT ISOLATION 12, FOUND YELLOW HARNESS CONNECTOR W8P1 TO AMPLIFIER E5 WAS NOT FULLY SECURED. ALL OTHER HARNESS CONNECTORS CHECKED AND FOUND SECURED. N1 AMPLIFIER DISABLE CHECK, ACCEL/DECEL CHECKS PERFORMED IAW RJ MM 71-00-00. ALL ENGINE PARAMETERS FOUND TO BE WITHIN LIMITS.

Part: WINDSHIELD — FAILED (COCKPIT) · airframe 3,084 hrs · 2,770 cycles

PASSING THROUGH 10000 FT AT 150 KIAS AND NORMAL RATE OF DESCENT THE CAPTAIN'S FORWARD WINDSHIELD SHATTERED. IT SHATTERED WITH A VERY LOUD BANG. REMOVED AND REPLACED PILOT'S WINDSHIELD WITH SERVICEABLE WINDSHIELD IAW CRJ MM 56-00-00. PN ON NP-13921-9 SN ON 01130H7681.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 2,748 hrs · 2,477 cycles

AT FL 330, THE CAPT''S WINDSHIELD SHATTERED. REMOVE AND REPLACE CAPTAIN''S WINDSHIELD IAW MM 56-11-01. PRESSURIZED AC IAW 21-31-00 FOR WINDSHIELD REPLACEMENT. OPS CHECK AND LEAK CHECK GOOD. P/N ON 601R33033-9, S/N ON 980048H7587, S/N OFF 00020H8018.

Part: BPSU — FAILED (TE FLAPS) · airframe 1,537 hrs · 1,429 cycles

FLAP FAIL MESSAGE ON APPROACH AT 42 DEGREES. REMOVED AND REPLACED RIGHT BPSU IAW MM 27-51-00. PN 855D100-9 SN ON 301B SN OFF 1150A. REMOVED AND REPLACED OUTBOARD FLAP INBOARD ACTUATOR IAW MM 27-53-05 PN 853D106-17 SN ON 332 SNOFF 0964. OPS CHECKS GOOD. COMPLIED WITH AD 98-20-01 IAW MAINTENANCE PROCEDURE ACTION. ALL CHECKS GOOD

Part: CONTROLLER — FAILED (AIR DATA SENSOR) · airframe 1,398 hrs · 1,300 cycles

ON CLIMBOUT, RIGHT AOA HEAT CAME ON. REMOVED AND REPLACED RIGHT AIR DATA SENSOR CONTROLLER IAW CRJ MM 30-31-15. OPS CHECKS GOOD. P/N ON: 785-806-2, S/N ON: 1377, S/N OFF: 218.

Part: COMPUTER — FAILED (STALL WARNING) · airframe 1,333 hrs · 1,246 cycles

STALL FAIL CAUTION MESSAGE CAME ON AFTER ROTATION. RETURNED TO FIELD. INTERROGATED FAULT HISTORY AND LRU DIAGNOSTICS. NO FAULTS LOGGED. REPLACED STALL COMPUTER IAW MM 27-35-01. STALL TEST CHECKS GOOD, FAIL MESSAGE CLEARED. P/N: 39-951-002-08, S/N ON: 162, S/N OFF: 589.

Part: CONTROLLER — FAILED (STAB TRIM) · airframe 1,011 hrs · 937 cycles

STAB TRIM CHANNEL 2 WILL NOT ENGAGE. FAILED TRIM TEST ON GROUND DURING PREFLIGHT. ON TWO STAB TRIM TESTS CHANNEL 2 FAILURE INDICATED ON HSTCU TEST PANEL. REPLACED HSTCU IAW CL600 MM 27-42-05. STAB CHANNELS AND MACH TRIM TEST GOOD ON GROUND. AIRCRAFT OK FOR CAT II.S/N: 165 S/N OFF: 796.

Part: TRANSDUCER — FAILED (NR MACH) · airframe 972 hrs · 900 cycles

JUST AFTER LIFT OFF ''''''''STALL FAIL'''''''' MESSAGE. RETURNED TO SLC. REPLACED STALL COMPUTER. FAILED TEST. (P/N 39-951-002-08) ON, (S/N 521) ON, (S/N 589) OFF. REMOVED AND REPLACED NUMBER ONE MACH TRANSDUCER IAW MM 27-35-25. OPS CHECKS GOOD AT THIS TIME. (P/N 60730-000-1) ON, (S/N 132) ON, (S/N 979) OFF.

Part: FAN BLADE — DIRTY (RT ENGINE) · airframe 498 hrs · 464 cycles

RIGHT ENGINE N1 VIBRATION 2.7 MLS AT 89 PECENT AT FL 180. RETURNED TO SLC. REMOVED AND CLEANED RIGHT ENGINE FAN BLADES. OPS CHECKS GOOD.