N589NN

Part: ACTUATOR — FAILED (ZONE 500 FLAPS) · airframe 21,418 hrs · 18,979 cycles

FLAPS FAIL ON TAKE OFF. COMPLETED INSTALL OF LH #3 FLAP ACTUATOR IAW CRJ 900 AMM 27-52-09-400-803 AND LH #4 FLAP ACTUATOR IAW AMM 27-52-09-400-804. OPS CHECK GOOD.

Part: ACTUATOR — TRIPPED (ZONE 500 FLAPS) · airframe 21,336 hrs · 18,918 cycles

RTF-FLAPS FAIL CAUTION MSG ON TAKE OFF. / FOUND B1 CODE 006551. CLEARED INHIBITS AND SELF TEST FOR SFECU PASSED IAW CRJ 900 AMM 45-45-00-970-821. FOUND LH OB INB FLAP ACTUATOR TRIPPED. RESET THE TRIPPED ACTUATOR IAW CRJ 900 AMM 27-52-09-610-802. PERFORMED OPS TEST OF SLATS AND FLAPS IAW CRJ 900 AMM 27-50-00-710-801 MULTIPLE TIMES AND DID NOT HARD FAULT. CAUTION MESSAGE IS GONE. OPS CHECK GOOD.

Part: FLAP SYSTEM — MALFUNCTIONED · airframe 20,417 hrs · 18,195 cycles

ON APPROACH TO GPT, PILOTS MOVED THE FLAP LEVER TO 8 AND GOT A STICK SHAKER FOLLOWED BY A STICK PUSHER. PILOTS WERE ABLE TO MANUALLY PULL THE NOSE UP FROM A DIVE DOWN SCENARIO. PILOTS DISCONNECTED THE STICK PUSHER SWITCHES AND BEGAN TO CLIMB PERFORMING A GO AROUND RETRACTING FLAPS. READ QRH FOR STICK PUSHER FAIL AND TRY ONE MORE APPROACH AT 210KTS AND BOTH STICK PUSHER SWITCHES IN THE OFF POSITION. THE STICK SHAKER AND PUSHER WENT OFF AGAIN AND WE WERE IN THE SAME SCENARIO. WE REALIZED FLAPS OUT OF ZERO WERE SOMEHOW ASSOCIATED AND DIVERTED FOR A FLAP ZERO LANDING. NO FURTHER ISSUES AFTER THAT / C/W INSTRUCTIONS LISTED IN RIL# 12219.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 19,556 hrs · 17,466 cycles

CORROSION ON SEAT RAILS FROM STA 847 TO 977, RBL9. SEAT RAIL FROM STA 847 TO 977, RBL 9 WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-51-49-101-001-A02 AND WAS REPLACED PER CRJ900 SRM 53-00-49-201-002-A01 AND PER CRJ900 AMM 53-00-49 (CONFIG A12).

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 19,556 hrs · 17,466 cycles

CORROSION ON FLOOR SUPPORT SPLICE LOWER CHORD BTW STA 865-881 AND 9RBL AT FLOOR STRUCTURE OF PASSENGER CABIN (CPAX). FLOOR SUPPORT SPLICE WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-51-43-101-001-A02; FABRICATED PER DWG NO. SH670-32161 REV. NC AND WAS REPLACED PER CRJ900 SRM 51-42-21-001-001-A01"

Part: RIB — CRACKED (ZONE 500) · airframe 19,556 hrs · 17,466 cycles

CRACK ON OUTB MACHINED RIB OF WS 163.00 TRAILING EDGE AT LH WING. RIB OF WS 163.00 TRAILING EDGE AT LH WING WAS REPAIRED PER REO 690-57-51-381 REV.

Part: SKIN — DENTED (ZONE 200) · airframe 19,556 hrs · 17,466 cycles

" SEVERAL DENTS ON FUSELAGE SKIN SETTLEMENT AREA OF VENTRAL FIN FAIRING RH. SEVERAL DENTS ON FUSELAGE SKIN SETTLEMENT AREA OF VENTRAL FIN FAIRING RH.WERE REPAIRED PER REO 670-51-00-085 REV -A AND PER REO 690-53-00-580 REV."

Part: CROSSBEAM — CRACKED (ZONE 200) · airframe 19,556 hrs · 17,466 cycles

"I"INITIAL INSPECTION: CRACK ON COCKPIT FLOOR LONGITUDINAL BEAM RBL12 AT CROSSBEAM FS 280. FLOOR STRUCTURE BELOW FLIGHT COMPARTMENT. COCKPIT FLOOR LONGITUDINAL BEAM RBL12 AT CROSSBEAM FS 280. FLOOR STRUCTURE BELOW FLIGHT COMPARTMENT. WAS REPAIRED PER REO 690-53-11-1854 REV. "

Part: INTERCOSTAL — CORRODED (ZONE 100) · corrosion level 2 · airframe 19,556 hrs · 17,466 cycles

"INITIAL INSPECTION: CORROSION ON INTERCOSTALS (2EAS) BTW FS349.00 TO FS364.00 NEAR STGR 27 AT MAIN AVIONICS COMPARTMENT. EVALUATED, DUE TO NOT ALLOWED DAMAGE ON INTERCOSTALS (2EAS) BTW FS349.00 TO FS364.00 NEAR STGR 27 AT MAIN AVIONICS COMPARTMENT,THEREFORE FOUND OUT OF LIMITS PER CRJ-900 SRM 53-21-23-101-003-A02 AND REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 AND CRJ-900 SRM 51-42-21-001-001-A01."

Part: FLOORBEAM — CRACKED (ZONE 200) · airframe 19,556 hrs · 17,466 cycles

"INITIAL INSPECTION: CRACK ON COCKPIT FLOOR LONGITUDINAL BEAM LBL12 AT CROSSBEAM FS 280. FLOOR STRUCTURE BELOW FLIGHT COMPARTMENT. COCKPIT FLOOR LONGITUDINAL BEAM LBL12 AT CROSSBEAM FS 280. FLOOR STRUCTURE BELOW FLIGHT COMPARTMENT WAS REPAIRED PER REO 690-53-11-1853 REV."

Part: DOOR SILL — CORRODED (ZONE 100) · corrosion level 2 · airframe 19,556 hrs · 17,466 cycles

"INITIAL INSPECTION: CORROSION ON LOWER SILL AT AFT BAGGAGE-BAY DOOR CUT OUT. EVALUATED, DUE TO EXCESSIVE CORROSION ON LOWER SILL AT AFT BAGGAGE-BAY DOOR CUT OUT,THEREFORE OUT OF LIMIT PER CRJ 900 SRM 53-61-23-201-001-A01 AND REPLACED PER CRJ 900 SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01 AND SRM 51-42-10-001-001-A01."

Part: FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 19,556 hrs · 17,466 cycles

" CORROSION ON JACK FITTING SUPPORT RH BTW FS 265.00 AND FS 280.00 AT MAIN AVIONICS COMPARTMENT. CORROSION ON JACK FITTING SUPPORT RH BTW FS 265.00 AND FS 280.00 AT MAIN AVIONICS COMPARTMENT WAS FOUND OUT OF LIMITS PER CRJ900 SRM 53-00-00-101-001-A01 THEREFORE WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01 "

Part: FLOOR SUPPORT — CRACKED (ZONE 100) · airframe 19,556 hrs · 17,466 cycles

"CRACK ON FLOOR SUPPORT RBL12.0 BTW FS 221.73 TO FS 229.00 AT FWD FUSELAGE INTERNAL STRUCTURE, FLOOR SUPPORT RBL 12 TBW FS221.73 TO FS229 FWD FUSELAGE INTERNAL STRUCTURE WAS REPAIRED PER REO 690-53-11-1855 REV."

Part: FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 19,556 hrs · 17,466 cycles

"CORROSION ON FRAME FS364.00 NEAR STGR 27 BEHIND OF SENSOR PX41 AT MAIN AVIONICS COMPARTMENT. FRAME FS364 WAS RE INSPECTED PER CRJ900 NDTM PART 01 51-20-009-210-A01 AND ONLY NUTPLATE BRACKET WAS FOUND WITH CORROSION, WAS FABRICATED PER DWG SH670-32456 REV. NC AND WAS REPLACED PER CRJ-900 SRM 51-41-02-001-001-A01"

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 19,556 hrs · 17,466 cycles

"INITIAL INSPECTION: CORROSION ON SIDE SEAT RAIL STGR 15 (5EAS) RH AND (5EAS) LH BTW FS 379.00 TO FS 669.40. EVALUATED,SIDE SEAT RAIL STGR 15 (5EAS) RH AND (5EAS) LH BTW FS 379.00 TO FS 669.40 DUE TO EXCESIVE DAMAGE, THEREFORE ARE OUT OF LIMITS PER CRJ-900 SRM 53-21-49-101-001-A01,CRJ-900 SRM 53-31-49-101-001-A02 AND REPLACED PER CRJ-900 AMM 53-00-49 CONF(A12)"

Part: CANISTER — CRACKED (ZONE 500) · airframe 19,556 hrs · 17,466 cycles

CRACK ON CANISTER WELDED NO. 3 IN STA WS 148.00 OF INTERNAL LH MAIN FUEL TANK. CANISTER WELDED NO. 3 IN STA WS 148.00 LH FUEL TANK WAS REPAIRED PER REO 670-57-42-577 REV.

Part: BRACKET — CORRODED (ZONE 100) · corrosion level 2 · airframe 19,556 hrs · 17,466 cycles

"CORROSION ON BRACKETS, MACHINED (3EAS) AND PLATE (2 EAS) OF INTERNAL STRUCTURE AT FWD CARGO COMPARTMENT BRACKETS, MACHINED (3EAS) AND PLATE (2 EAS) OF INTERNAL STRUCTURE AT FWD CARGO COMPARTMENT WERE EVALUATED OUT OF LIMITS AND WERE REPLACED PER CRJ-900 SRM 53-32-58-101-001-A01 AND SRM 51-42-22-001-001-A01, SRM 51-42-10-001-001-A01 AND SRM 51-42-21-001-001-A01"

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 19,556 hrs · 17,466 cycles

"DESCRIPTION: CORROSION ON SEAT RAIL ON LBL 9 (5EAS) AND RBL9 (6EAS) BTW FS349.00 TO FS847. SEAT RAIL ON LBL 9 (5EAS) AND RBL9 (6EAS) BTW FS349.00 TO FS847.00 WERE EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-21-49-101-001-A01, CRJ900 SRM 53-31-49-101-001-A02 AND CRJ900 SRM 53-41-49-101-001-A02 AND WERE REPLACED PER CRJ900 AMM 53-00-49 CONF (A12)"

Part: ANGLE — CORRODED (ZONE 100) · corrosion level 2 · airframe 19,556 hrs · 17,466 cycles

"CORROSION ON FLOOR PANEL SUPPORT ANGLE FS280.00 AT CABIN FLOOR STRUCTURE. FLOOR PANEL SUPPORT ANGLE FS280.00 AT CABIN FLOOR STRUCTURE WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-00-00-101-001-A01 AND WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01 PAR.6 C AND CRJ900 SRM 51-42-21-001-001-A01 PAR.6 C"

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 19,556 hrs · 17,466 cycles

"AFTER REMOVAL OF FLOOR SUPPORT ANGLE, CORROSION ON RH SIDE FLOOR BEAM AT FS 280.00. RH SIDE FLOOR BEAM AT FS280.00 WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-00-01-101-001-A01 AND WAS REPLACED PER CRJ900 SRM 51-42-21-001-001-A01 AND CRJ900 SRM 51-42-06-001-001-A01"

Part: DRAG ANGLE — CRACKED (ZONE 300) · airframe 19,556 hrs · 17,466 cycles

"INITIAL INSPECTION: CRACK ON RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TR RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00) WAS REPAIRED PER CRJ-900 SRM 55-31-00-201-001-A01"

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 19,556 hrs · 17,466 cycles

"INITIAL INSPECTION: CORROSION ON SIDE SEAT RAIL STGR 15 (6EAS) LH AND (6EAS) RH BTW FS 669.40 TO FS 977. EVALUATED, SIDE SEAT RAIL STGR 15 (6EAS) LH AND (6EAS) RH BTW FS 669.40 TO FS 977.00 ARE OUT OF LIMITS PER CRJ-900 SRM 53-41-49-101-001-A02, CRJ-900 SRM 53-51-49-101-001-A02 AND REPLACED PER CRJ-900 AMM 53-00-49 (CONFIG A12)"

Part: FLOOR SUPPORT — CORRODED (ZOEN 200) · corrosion level 2 · airframe 19,556 hrs · 17,466 cycles

CORROSION ON FLOOR SUPPORTS FROM STA 1000 TO STA 1069 LBL9 & LBL27 OF FLOOR STRUCTURE (C2). FLOOR SUPPORTS LBL27 ANT LBL9 AT FS1000 TO FS1069 WERE EVALUATED OUT OF LIMITS AND WERE REPAIRED PER CRJ900 SRM 53-61-43-101-001-A02 AND CRJ900 SRM 53-00-41-201-001-A03.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 19,556 hrs · 17,466 cycles

CORROSION ON SEAT RAILS FROM STA 847 TO 977 AND LBL9. SEAT RAILS FROM STA 847 TO 977 AND LBL9 WERE EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-51-49-101-001-A01 AND WERE REPLACED PER CRJ900 AMM 53-00-49 CONF (A12)"

Part: RIB — CRACKED (ZONE 600) · airframe 19,556 hrs · 17,466 cycles

"CRACK ON OUTB MACHINED RIB OF WS 163.00 TRAILING EDGE AT RH WING. OUTB MACHINED RIB OF WS 163.00 TRAILING EDGE RH WING WAS REPAIRED PER REO 690-57-51-380 REV."

Part: ANGLE — CORRODED (ZONE 200) · corrosion level 2 · airframe 19,556 hrs · 17,466 cycles

"CORROSION ON MOUNTING ANGLE OF GALLEY SERVICE DOOR LOWER SURROUND STRUCTURE. MOUNTING ANGLE WAS EVALAUTED OUT OF LIMITS PER CRJ900 SRM 53-21-23-101-002-A02 AND WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01 AND CRJ900 SRM 51-42-21-001-001-A01"

Part: LUG — CORRODED (ZONE 500 AILERON) · corrosion level 2 · airframe 19,556 hrs · 17,466 cycles

"DESCRIPTION: CORROSION ON HOUSING OF LUG 1, LUG 2, LUG 5 AND LUG 6 AT LH AILERON WAS FOUND. HOUSING OF LUG 1, LUG 2, LUG 5 AND LUG 6 AT LH AILERON WERE REPAIRED PER REO 670-57-61-237 REV--"

Part: PLATE — CORRODED (ZONE 200) · corrosion level 2 · airframe 19,556 hrs · 17,466 cycles

"INITIAL INSPECTION: CORROSION ON KICK PLATE AND MID CAP ANGLE OF PASSANGER DOOR LOWER SURROUND STRUCTURE. CORROSION WAS REMOVED ON KICK PLATE PER CRJ-900 SRM 51-21-06-001-001-A01, EVALUATED,THEREFORE IS WHITHIN OF LIMITS AND DUE TO EXCESSIVE DAMAGE MID CAP ANGLE, THEREFORE IS OUT LIMITS AT PASSENGER DOOR LOWER SURROUND STRUCTURE PER CRJ900 SRM53-21-23-101-001-A02 AND MID CAP ANGLE WAS REPLACE PER CRJ-900 SRM 51-41-02-001-001-A01"

Part: DOUBLER — CORRODED (ZONE 100) · corrosion level 2 · airframe 19,556 hrs · 17,466 cycles

CORROSION ON PRODUCTION DOUBLER OF ANTENNA AND ATTACH ANLGES BTW STA 1000-1015 AND STRINGERS 25RH-26RH AT AFT CARGO COMPARTMENT. PRODUCTION DOUBLER OF ANTENNA AND ATTACH ANLGES BTW STA 1000-1015 AND STRINGERS 25RH-26RH AT WERE EVALUATED OUT OR LIMITS PER CRJ900 SRM 53-00-00-101-001-A01 AND WERE REPLACED PER CRJ900 SRM 51-42-21-001-001-A01 AND CRJ900 SRM 51-42-06-001-001-A01.

Part: HINGE FITTING — CORRODED (ZONE 300) · corrosion level 2 · airframe 19,556 hrs · 17,466 cycles

"AFTER RUDDER REMOVAL, FREE PLAY ON SELF-ALIGN SELF-LUB BEARING PLAIN ON HINGE FITTING NO. 2 AND NO. 3 AT VERTICAL STABILIZER REAR SPAR MIDDLE SECTION. HINGE FITTING NO. 2 Y NO. 3 AT VERTICAL STABILIZER REAR SPAR WERE REPLACED PER RIL #2103 REV. B."

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 19,556 hrs · 17,466 cycles

"CORROSION ON STRINGER 21RH FS 319.70 TO FS 333 . STGR21 RH BTW FS319 TO FS333 WAS EVALUATED PER CRJ900 SRM 53-21-03-101-002-A04 AND WAS REPLACED PER CRJ900 SRM 51-42-21-001-001-A01 AND CRJ900 SRM 51-42-06-001-001-A01"

Part: FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 19,556 hrs · 17,466 cycles

"DURING INSPECTION OF THE TASK CARD 53-21-301-JIC IT WAS DETECTED CORROSION ON FRAME FS 295.00 BTW STGR 24RH AND STGR 26LH AT MAIN AVIONICS COMPARTMENT. SUMMARY CORROSION ON FRAME FS 295.00 BTW STGR 25RH AND STGR 26LH THIS WAS FOUND ITS OUT LIMITS PER CRJ-900 SRM 53-21-06-101-002-A04 THEREFORE WAS REPAIRED PER CRJ-900 SRM 53-00-06-201-006-A01 AND CORROSION ON FRAME FS295 BTW STGR 25RH TO STGR 24RH WAS REMOVED AND WAS EVALUATED WIHTHIN LIMITS PER CRJ900 SRM 53-00-06-201-005-A01"

Part: DRIP TRAY — CORRODED (ZONE 100) · corrosion level 2 · airframe 19,556 hrs · 17,466 cycles

CORROSION ON RH TRAY DRIP ASSY. RH TRAY DRIP ASSY WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-00-00-101-001-A01 AND WAS REPLACED PER CRJ900 SRM 51-42-13-001-001-A01.

Part: SKIN — DENTED (ZONE 200) · airframe 19,556 hrs · 17,466 cycles

"SEVERAL DENTS ON FUSELAGE SKIN SETTLEMENT AREA OF VENTRAL FIN FAIRING LH. SEVERAL DENTS ON FUSELAGE SKIN SETTLEMENT AREA OF VENTRAL FIN FAIRING LH WERE REPAIRED PER REO 670-51-00-085 REV -A AND PER REO 690-53-00-579 REV."

Part: FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 19,556 hrs · 17,466 cycles

"DURING INSPECTION OF THE TASK CARD 53-21-301-JIC IT WAS DETECTED CORROSION ON FRAME FS 295.00 BTW STGR 24RH AND STGR 26LH AT MAIN AVIONICS COMPARTMENT. SUMMARY CORROSION ON FRAME FS 295.00 BTW STGR 25RH AND STGR 26LH THIS WAS FOUND ITS OUT LIMITS PER CRJ-900 SRM 53-21-06-101-002-A04 THEREFORE WAS REPAIRED PER CRJ-900 SRM 53-00-06-201-006-A01 AND CORROSION ON FRAME FS295 BTW STGR 25RH TO STGR 24RH WAS REMOVED AND WAS EVALUATED WIHTHIN LIMITS PER CRJ900 SRM 53-00-06-201-005-A01"

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 19,556 hrs · 17,466 cycles

"AFTER REMOVAL OF FLOOR SUPPORT ANGLE, CORROSION ON LH SIDE FLOOR BEAM AT FS 280.00. LH SIDE FLOOR BEAM AT FS280.00 WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-00-01-101-001-A01 AND WAS REPLACED PER CRJ900 SRM 51-42-21-001-001-A01 AND CRJ900 SRM 51-42-06-001-001-A01"

Part: LUG — CORRODED (ZONE 600 AILERON) · corrosion level 2 · airframe 19,556 hrs · 17,466 cycles

CORROSION ON HOUSING OF LUG 1, LUG 2, LUG 5 AND LUG 6 AT RH AILERON WAS FOUND. CORROSION ON HOUSING OF LUG 1, LUG 2, LUG 5 AND LUG 6 AT RH AILERON WERE REPAIRED PER REO 670-57-61-237 REV-.

Part: SENSOR — UNSERVICEABLE (BRAKE TEMP) · airframe 19,364 hrs · 17,301 cycles

BRAKE OVHT WARNING MSG IN FLIGHT, LHOB BTMS EICAS INDICATION BOX SHOWED RED, AND INDICATED 20, IN CRUISE FLIGHT / REMOVED AND REPLACED ASCU IAW CRJ900 AMM 32-44-06-000/400-801-A01 AND REMOVED AND REPLACED LH OB BRAKE TEMP SENSOR IAW CRJ900 AMM 32-46-01-000/400-801-A01-PSA. ASCU BITE-TEST GOOD AT THIS TIME IAW CRJ900 AMM 32-44-06-740-801-A01 AND LH OB BRAKE TEMP SENSOR SELF-TEST GOOD AT THIS TIME IAW CRJ900 AMM 32-46-01-740-801-A01.

Part: WARNING MESSAGE — FALSE INDICATION (ELEVATOR SYS) · airframe 18,722 hrs · 16,766 cycles

ELEVATOR SPLIT CAUTION MSG IN FLT / TROUBLESHOOT AND PERFORMED OPERATIONAL TEST OF THE ELEVATOR CONTROL SYSTEM IAW CRJ 900 FIM 27-31-00-810-803-A02 AND AMM 27-31-00-710-801-A01. OPS CHECK GOOD AT THIS TIME. FAULT CLEARED AND FAULT DID NOT RE-APPEAR.

Part: DETECTOR — UNSERVICEABLE (600) · airframe 17,525 hrs · 15,728 cycles

DURING CRUISE, THE CREW NOTICED A FLAPS/STALL FAIL MESSAGE / REMOVED AND REPLACED RIB SKEW DETECTOR MT5 IAW CRJ900 AMM 27-52-45-000/400-802-A01. OPS CHECK GOOD. RIG CHECK GOOD.

Part: PSEU — UNSERVICEABLE (700) · airframe 17,404 hrs · 15,615 cycles

NLG DID NOT DEPLOY WHEN LEVER SELECTED DOWN, HAD TO MANUALLY EXTEND PER QRH. REMOVED & REPLACED PSEU I.A.W. CRJ900 AMM 32-61-01-000/400-801. PERFORMED MULTIPLE OPS CHECKS OF LANDING GEAR EXTENSION/RETRACTION I.A.W. CRJ900 AMM 32-30-00-865-801. OPS CHECKS GOOD.

Part: MANIFOLD — UNSERVICEABLE (700) · airframe 16,857 hrs · 15,125 cycles

STEERING INOP AFTER TAKE OFF AND GEAR UP / REMOVED AND REPLACED THE STEERING MANIFOLD IAW CRJ 900 AMM 32-51-50-000/400-801. OPS CHECK AND LEAK CHECK GOOD.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 16,680 hrs · 14,976 cycles

NOSE WHEEL STEERING INOP CAUTION MESSAGE 10 SECONDS AFTER TAKE OFF. NO MESSAGE SHOWN UPON MEET AND GREET PERFORMED. RESET OF NWS IAW CRJ 900 AMM 32-50-00-810-802. NO DEFECTS NOTED

Part: NOT ENTERED — NOT ENTERED · airframe 15,772 hrs · 14,201 cycles

RH RUDDER SKIN STA136.90 - STA148.86 DENTED. PERFORMED PERMANENT REPAIR IAW EA 23-C9-55-0029-IR_APPROVED.

Part: DRAIN MAST — MISSING (APU) · airframe 15,444 hrs · 13,894 cycles

AFT FUEL DRAIN MISSING. REMOVED REMAINING PIECE OF THE DRAIN MAST AND SEAL IAW AMM 28-20-03-000-801-A01. NO FURTHER DEFECTS NOTED. A/C OK FOR FERRY FLIGHT. FERRY FLT 9977. REMOVED AND REPLACED AFT FUEL DRAIN MAST IAW AMM 28-20-03-000/400-801-A01.

Part: SENSOR — FAULT MESSAGE (700) · airframe 14,650 hrs · 13,198 cycles

MX DIVERSION DUE TO BRAKE OVERHEAT WARNING MESSAGE. CREW FOLLOWED QRH AND DECIDED TO DIVERT TO THE NEAREST SUITABLE AIRPORT. TRUCKS WERE ROLLED IN ATL TO CHECK FOR BRAKE FIRES. CREW DID NOT PERFORM AN OVERWEIGHT LANDING. CREW WAS ABLE TO TAXI TO THE GATE AND MX HAS BEEN ADVISED. LEFT OUTBOARD BRAKE TEMP SENSOR AMBER WITH DASHES / RECLASSIFIED LH OTBD BTMS TO MEL 32-46-01 'C' OPT 4. M'FUNCTION C/W BY DISCONNECTING AND CAPPING THERMOCOUPLE CONNECTOR. THIS CLEARS OPTION 2 MEL. TROUBLESHOT IAW CRJ 900 FIM 32-46-01-810-802. SHOT WIRES, FOUND NO DISCREPANCIES. REMOVED & REPLACED LH OB BRAKE THERMOCOUPLE SENSOR TC09. OPS TEST GOOD.

Part: STIFFENER — DENTED (CARGO DOOR) · airframe 14,548 hrs · 13,112 cycles

DURING OVERNIGHT MX AT GSP, FOUND 3/4"" CRACK AND 1 1/2"" DENT ON FORWARD BAGGAGE BAY DOOR FORWARD LOWER STABILIZER / PERFORMED PERM REPAIR OF THE FWD BAGGAGE DOOR LOWER FWD STIFFENER IAW REO 690-52-35-298, EA 22-C9-52-0853, CRJ 900 SRM 51-42-06, AND CRJ 900 SRM 51-42-20."

Part: ACM — UNSERVICEABLE (200) · airframe 14,508 hrs · 13,077 cycles

ON DEPARTURE AFT FA IMMEDIATELY SMELLED SMOKE AND CALLED FWD FA. IT WAS DETERMINED THAT THE SMOKE ODOR WAS STRONGER IN THE REAR OF THE AIRCRAFT (ROW 11 BACK TO AFT FA STATION). SLIGHT SMOKY ODOR IN THE COCKPIT. CREW DECLARED AN EMERGENCY AND DECIDED TO RETURN TO GSP. UPON LANDING AND CLEARING THE RUNWAY, THE MAIN CABIN DOOR WAS OPENED FOR A BRIEF INSPECTION BY EMERGENCY CREWS. IT WAS DETERMINED THAT THE FLIGHT WAS SAFE TO TAXI TO THE GATE. PAX DEPLANED NORMALLY AT THE GATE. NO INJURIES WERE REPORTED AND NO EMK OR OTHER FIRST AID SUPPLIES WERE USED. UPON RE-ENTERING THE AIRCRAFT THE CREW DISCOVERED THERE WAS A LH AUTO PACK FAIL MSG, WHICH WAS NOT PRESENT DURING FLIGHT, TAXI, OR AFTER ENGINE SHUTDOWN. PERFORMED TROUBLESHOOTING OF THE SMOKE IN THE CABIN IAW CRJ 900 FIM 21-22-00-810-806-A01. FOUND THAT THE L/H PACK AUTO-FAILED ON EICAS, OPERATED PACK, HEARD ACM MAKING ABNORMAL NOISE. NOTICED THAT THE ACM WAS MAKING A BURNING SMELL. REMOVED AND REPLACED LH ACM IAW CRJ 900 AMM 21-51-08-000/400-801-A01. OPS CHECK GOOD AT THIS TIME. LEAK CHECK GOOD AT THIS TIME. NO SMOKE IN CABIN."

Part: SEAT TRACK — CORRODED (BS 376-501) · corrosion level 2 · airframe 12,503 hrs · 11,432 cycles

SEAT RAIL AT LBL9 CORRODED BEYOND LIMITS

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHTS) · airframe 10,945 hrs · 9,952 cycles

INSPECTED AND FOUND BATTERY PACK NR 4 CONNECTOR DISCONNECTED. RECONNECTED CONNECTOR, IAW CRJ 900 AMM 33-51-17-400-802-A04. REINSTALLED CEILING PANEL, OPS CHECK GOOD, IAW AMM 33-51-00-710-802-A27 AND AMM 25-26-05-400-802-A39.

Part: BATTERY — DISCHARGED (CABIN) · airframe 10,220 hrs · 9,293 cycles

OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED #3 BATTERY IAW CRJ900 AMM. OPS CHECKED GOOD.

Part: GCU — FAILED (NR 3) · airframe 9,375 hrs · 8,536 cycles

ALL ELECTRICAL POWER LOST WHILE AT GATE, FOLLOWED BY BURNING SMELL AND SMOKE IN COCKPIT. INSPECTED AC FOUND CB Q11 ON CPB1POPPED OPEN. INVESTIGATED AND FOUNDGCU#3 FOR APU IS BURNED ON THE INSIDE. GCU #3REQ REPLACEMENT. R&R #3 GCU IAW CRJ 900 AMM 24-22-03-000/400-801. OPS CHECK GOOD

Part: MANIFOLD — FAILED (NLG STEERING) · airframe 7,958 hrs · 7,276 cycles

CREW RECEIVED STEERING INOP CAUTION MSG WHEN LANDING IN CLT. ATC DECLARED EMERGENCY FOR CREW AND ROLLED TRUCKS. FLIGHT LANDED WITHOUT INCIDENT AND TAXIED TO GATE. MX REPLACED NOSEWHEEL STEERING MANIFOLD. OPS CHECK GOOD.

Part: WIRE HARNESS — ABNORMAL (NLG STEERING) · airframe 7,948 hrs · 7,266 cycles

NOSE WHEEL STEERING INOP CAUTION MSG INFLIGHT. R&R NLG STEERING MANIFOLD HARNESS IAW AMM 32-51-50-000/400-801 OPS CHECK GOOD

Part: WARNING MESSAGE — FALSE ACTIVATION (NLG STEERING) · airframe 7,921 hrs · 7,238 cycles

NOSE WHEEL STEERING INOP CAUTION MSG AT 800 AGL C/W RESET PRCEDURE P1-9 MSG CLEARED

Part: SENSOR — FAILED (NLG) · airframe 7,916 hrs · 7,233 cycles

CREW RECEIVED A NOSE STEERING INOP MESSAGE AND NOTIFIED ATC OF THE SITUATION. ATC DECLARED AN EMERGENCY. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. NWS INOP AMBER DISPLAYED INFLIGHT. RAN QRH. 1 CW RESET PROCEDURE. MESSAGE CLEARED. MX REPLACED RH OB BRAKE TEMP SENSOR. OPS CHECK GOOD.

Part: WARNING MESSAGE — FALSE ACTIVATION (NLG STEERING) · airframe 7,838 hrs · 7,165 cycles

NOSE WHEEL STEERING INOP CAUTION MSG IN FLIGHT C/W RESET PRCEDURE MSG CLEARED

Part: ACM — SMOKE (RIGHT) · airframe 3,809 hrs · 3,516 cycles

AT 2000 FEET, DURING INITIAL CLIMB, THE FLIGHT ATTENDENT REPORTED SMOKE IN THE CABIN. DECLARED AN EMERGENCY AND RETURNED TO THE FIELD. MAINTENANACE THE RIGHT AIR CONDITIONING PACK WAS THE SOURCE OF THE SMOKE.

Part: WARNING MESSAGE — FALSE ACTIVATION (NLG STEERING) · airframe 3,791 hrs · 3,502 cycles

THE AIRCRAFT RECEIVED A NOSE WHEEL STEERING INOPERATIVE MESSAGE AND DECLARED EMERGENCY. THE CREW FOLLOWED THE QUICK REFERENCE HANDBOOK AND CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. MAINTENANCE CYCLED SYSTEM CIRCUIT BREAKERS AND THE MESSAGE CLEARED. NO FURTHUR ACTION TAKEN AND THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WARNING MESSAGE — FALSE ACTIVATION (NLG STEERING) · airframe 3,591 hrs · 3,323 cycles

THE CREW RECEIVED A NOSE WHEEL STEERING CAUTION MESSAGE DURING APPROACH. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE SYSTEM OPERATIONAL CHECK GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SPOILER SYS — MALFUNCTIONED · airframe 1,652 hrs · 1,532 cycles

INBOARD SPOILERON AND INBOARD FLIGHT SPOILERS CAUTION MESSAGE. MAINTENANCE TROUBLESHOT AND PERFORMED SELF TEST OF THE SPOILER AND STABILIZER CONTROL UNITS, OPS CHECKED GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.