N577NN
Registered owner: AMERICAN AIRLINES INC, TX (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
CORROSION FOUND ON THE AFT BOTTOM SIDE OF FRAME SECTION 295 BETWEEN THE BOTTOM CENTER STRINGER 27 AND RIGHT HAND 26 / BLENDED DAMAGE AREAS. PERFORMED NDT (LPI & EDDY CURRENT) WITH NO DEFECTS AND RESTORED FINISH IAW REO 690-53-21-2151.
CORROSION FOUND ON THE FORWARD SIDE OF FRAME SECTION 310 BETWEEN THE BOTTOM CENTER STRINGER 27 AND LEFT HAND 26 / BLENDED DAMAGE AREAS. PERFORMED NDT (LPI & EDDY CURRENT) WITH NO DEFECTS AND RESTORED FINISH IAW REO 690-53-21-2151.
CORROSION FOUND ON THE FORWARD BOTTOM SIDE OF FRAME SECTION 310 BETWEEN THE BOTTOM CENTER STRINGER 27 AND RIGHT HAND 26. BLENDED DAMAGE AREAS. PERFORMED NDT (LPI & EDDY CURRENT) WITH NO DEFECTS AND RESTORED FINISH IAW REO 690-53-21-2151.
RH MLG TIRES BLOWN ON TAXI. / RH IB TIRE + WHEEL ASSY REMOVED AND REPLACED IAW CRJ 900 AMM 32-41-01-000/400-801-A01-PSA
FOS WINDSHIELD ARCING IN FLIGHT QRH COMPLETED. REMOVED AND REPLACED FO SIDE WINDSHIELD IAW AMM 56-11-01-000/400-801-A01-PSA. OPS TEST OF FO SIDE WINDSHIELD TEMPERATURE CONTROL PASSED IAW AMM 30-41-06-710-801-A01. PRESSURIZED THE AIRCRAFT FOR LEAK TEST OF THE WINDSHIELD IAW AMM 21-31-00-910-801-A02-PSA AND LEAK TEST PASSED.
R PACK AUTO FAIL CAUTION MSG. FA'S REPORTED SMOKE IN CABIN. PACK TEMP HIT 99C / TROUBLESHOT AND FOUND RH ACM TO BE SEIZED UP. REMOVED AND REPLACED RH ACM IAW CRJ 900 AMM 21-51-08-000/400-801-A01. RH PACKS SYSTEM OPS AND LEAKS CHECKS GOOD IAW CRJ 900 AMM 21-51-00-710/790-801.
CORROSION ON SILL STRIKER AT FWD SURROUND STRUCTURE OF GALLEY SERVICE DOOR BTW STA FS 319.70 TO FS 349.00 WAS FOUND. SILL STRIKER AT FWD SURROUND STRUCTURE OF GALLEY SERVICE DOOR BTW STA FS 319.70 TO FS 349.00 WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-21-23-101-002-A02 AND WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01.
CORROSION ON KICKPLATE AND MID CAP BTW FS 310.00 TO FS 349.00 AT SURROUND STRUCTURE PASSENGER DOOR. KICKPLATE AND MID CAP BTW FS 310.00 TO FS 349.00 AT SURROUND STRUCTURE PASSENGER DOOR WERE EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-21-23-101-001-A02 AND WERE REPLACED PER CRJ900 SRM 51-42-06-001-001-A01 AND CRJ900 SRM 51-41-02-001-001-A01
CORROSION ON SEAT RAIL (SEVERAL LOCATIONS) BTW FS477.40 TO FS693.00 LBL/RBL 9.00 AT PASSENGER CABIN. CORROSION ON SEAT RAIL (SEVERAL LOCATIONS) BTW FS477.40 TO FS693.00 LBL/RBL 9.00 AT PASSENGER CABIN WAS EVALUATED OUT OF LIMITS PER CRJ-900 SRM 53-31-49-101-001-A02 AND WERE REPLACED PER CRJ900 AMM 53-00-49 (CONFIG A12)
CORROSION ON WINGLET LOWER CLOSING RIB AT RH WINGLET CORROSION ON WINGLET LOWER CLOSING RIB AT RH WINGLET WAS REPAIRED PER REO 690-57-31-229 REV. --
CORROSION ON AFT CARGO COMPARTMENT DOOR SILL BTW FS 1000.00 TO FS 1047.00. AFT CARGO COMPARTMENT DOOR SILL BTW FS 1000.00 TO FS 1047.00 WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-61-23-201-001-A01 AND WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01, CRJ900 SRM 51-42-13-001-001-A01 AND CRJ900 SRM 51-42-21-001-001-A01
CORROSION ON LOWER FACE OF PLATES LBL 3.4 (PLATE 1) BTW FS533.00 AND FS 549.00 (PLATE 2) BTW FS 645.00 AND FS 661.00 AT FWD CARGO COMPARTMENT. DUE TO NO DAMAGE IS ALLOWED ON THE FORWARD BAGGAGE BAY STRUCTURE, PLATES LBL 3.4 (PLATE 1) BTW FS533.00 AND FS 549.00 (PLATE 2) BTW FS 645.00 AND FS 661.00 AT FWD CARGO COMPARTMENT PER CRJ 900 SRM 53-32-58-101-001-A01 WERE REPLACED PER CRJ900 SRM 51-42-21-001-001-A01.
CORROSION ON SEAT RAIL (SEVERAL LOCATIONS) BTW FS693.00 TO FS847+16.00 RBL 9.00 AND CORROSION ON SEAT RAIL BTW FS693.00 TO FS720.85 LBL 9.00 AT PASSENGER CABIN CORROSION ON SEAT RAIL (SEVERAL LOCATIONS) BTW FS693.00 TO FS847+16.00 RBL 9.00 AND CORROSION ON SEAT RAIL BTW FS693.00 TO FS720.85 LBL 9.00 AT PASSENGER CABIN WAS EVALUATED OUT OF LIMITS AND PER CRJ900 SRM CRJ- 900 SM 53-41-49-101-001-A02 AND CRJ900 SRM 53-- 51-49-101-001-A02 AND WERE REPLACED PER CRJ900 AMM 53-00-49 (CONFIG A12)
DURING INSPECTION OF THE TASK CARD 500-08E2-JIC IT WAS DETECTED CRACK IN CANISTER WELDED NO.3 IN, STA. WS148 OF INTERNAL LH MAIN FUEL TANK. CANISTER WELDED NO.3 IN, STA. WS148 OF INTERNAL LH MAIN FUEL TANK WAS REPAIRED PER REO 670-57-42-577 REV. - -
WEAR ON AREA OF SETTLEMENT OF FAIRINGS (583AB, 586AB, 592AB, 595AB AND 597AB) AT LH WING LOWER SKIN. SETTLEMENT AREA OF FAIRINGS (583AB, 586AB, 592AB, 595AB AND 597AB) AT LH WING LOWER SKIN WAS REPAIRED PER REO 690-57-21-453 REV - -.
WEAR ON AREA OF SETTLEMENT OF FAIRINGS (683AB, 686AB, 692AB, 695AB AND 697AB) AT RH WING LOWER SKIN. SETTLEMENT AREA OF FAIRINGS (683AB, 686AB, 692AB, 695AB AND 697AB) AT RH WING LOWER SKIN WAS REPAIRED PER REO 690-57-21-452 REV - -.
CORROSION AT RH WINGLET LOWER AREA BTW WGLTS0.00./WS398.93 AND FS695.00 /FS794.50. RH WINGLET LOWER AREA BTW WGLTS0.00./WS398.93 AND FS695.00 /FS794.50 WAS REPAIRED PER REO 690-57-31-228 REV. --
SEVERAL NICKS ON FUSELAGE SKIN, ON STA 1000.00 TO STA 1047 BTW STGR 22RH TO STGR 27. NICKS ON FUSELAGE SKIN, ON STA 1000.00 TO STA 1047 BTW STGR 22RH TO STGR 27 WERE REPAIRED PER REO 690-53-61-1357 REV. - -
CRACK ON STRAP AT FAIRING PANEL 196DR. STRAP AT FAIRING PANEL 196DR WAS REPAIRED PER REO 690-53-82-052 REV. --
ELONGATED HOLES ON LH INBOARD FIXED L/E MACHINED RIB AT SLAT STA. 57.16, PERFORM PERM REPAIR IAW ENGINEERING DISPOSITION.L LH INBOARD FIXED L/E RIB AT STA 57.16 WAS REPAIRED PER REO 690-57-41-420 REV. --
CRACKED CENTER COCKPIT FLOOR BEAM LBL12 AT FS 280.00 FLOOR INTERNAL SUPPORT STRUCTURE BELOW FLIGHT COMPARTMENT. CENTER COCKPIT FLOOR BEAM LBL12 AT FS 280.00 FLOOR INTERNAL SUPPORT STRUCTURE BELOW FLIGHT COMPARTMENT WAS REPAIRED PER REO 690-53-11-1701 REV. - -
CORROSION ON BRACKETS, MACHINED (6EAS) OF INTERNAL STRUCTURE AT FWD CARGO COMPARTMENT. BRACKETS, MACHINED (6EAS) OF INTERNAL STRUCTURE AT FWD CARGO COMPARTMENT WERE EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-32-58-101-001-A01 AND WERE REPLACED PER CRJ-900 SRM 51-42-21-001-001-A01; CRJ900 SRM 51-42-10-001-001-A01 AND CRJ900 SRM 51-42-16-001-001-A01
CRACK ON ELECTRICAL BAY FLOOR WEB RIGHT SIDE (BELOW ADG SUPPORT DOUBLER) FS193.00. ELECTRICAL BAY FLOOR WEB RIGHT SIDE (BELOW ADG SUPPORT DOUBLER) FS193.00 WAS REPAIRED PER CRJ900 SRM 53-11-43-201-001-A01
CORROSION ON INTERCOSTAL ATTACHED TO STRINGER 20RH BTW STA. FS=310 TO FS=349 AT MAIN AVIONICS COMPARTMENT. CORROSION ON INTERCOSTAL ATTACHED TO STRINGER 20RH BTW STA. FS=310 TO FS=349 AT MAIN AVIONICS COMPARTMENT WAS REMOVED PER CRJ900 SRM 51-21-06-001-001-A01 AND BTW FS319 TO FS349 WAS EVALUATED. WITHIN LIMITS AND BTW FS310 TO FS319 WAS EVALUATED OUT OF LIMITS PER CRJ-900 SRM 53-21-23-101-002-A02 AND INTERCOSTAL OUT OF LIMITS WAS REPLACED PER CRJ900 SRM 51-42-21-001-001-A01
SPEED TAPE APPLIED - LH #2 SLAT AFT SKIN AT SS329.00 THE SUBJECT REWORKED CONDITION IS STRUCTURALLY ACCEPTABLE FOR 650 FH FROM THE EXPIRY OF THE E.A. 23-C9-57-1049 REVISION IR TIME VALIDITY (800 FH, REF) LH #2 SLAT AFT SKIN AT SS329.00 WAS REPAIRED PER REO 690-57-42-1036 REV. -
CRACKED CENTER COCKPIT FLOOR BEAM RBL12 AT FS 280.00 FLOOR INTERNAL SUPPORT STRUCTURE BELOW FLIGHT COMPARTMENT. CENTER COCKPIT FLOOR BEAM RBL12 AT FS 280.00 FLOOR INTERNAL SUPPORT STRUCTURE BELOW FLIGHT COMPARTMENT WAS REPAIRED PER REO 690-53-11-1702 REV. - -
CORROSION ON SILL AT FWD SURROUND STRUCTURE OF GALLEY SERVICE DOOR BTW FS319.70 / FS349.00. SILL AT FWD SURROUND STRUCTURE OF GALLEY SERVICE DOOR BTW FS319.70 / FS349.00 WAS EVALUATED OUT OF LIMITS AND WAS REPLACED PER CRJ-900 SRM 53-21-23-101-002-A02 AND CRJ900 SRM 51-42-06-001-001-A01
CORROSION ON STRAP INNER AT FS349.00 / STGR#17RH ON SURROUND STRUCTURE OF THE GALLEY SERVICE DOOR. STRAP INNER AT FS349.00 / STGR#17RH ON SURROUND STRUCTURE OF THE GALLEY SERVICE DOOR WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-21-23-101-002-A02 AND WAS REPLACED PER CRJ900 SRM 51-42-21-001-001-A01
CORROSION ON SIDE SEAT RAIL STGR 15 RH/LH (SEVERAL LOCATIONS) BTW FS669.40 TO FS977.00 AT PASSENGER CABIN. SIDE SEAT RAILS STGR 15 RH/LH BTW FS669.40 TO FS977.00 AT PASSENGER CABIN WERE EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-41-49-101-001-A02 AND CRJ900 SRM 53-51-49-101-001-A02 AND WERE REPLACED PER CRJ900 AMM 53-00-49 (CONFIG A12).
CORROSION ON SEAT RAIL (SEVERAL LOCATIONS) BTW FS847.00+16.00 TO FS977.00 LBL/RBL 9.00 AT PASSENGER CABIN. SEAT RAIL BTW FS847.00+16.00 TO FS977.00 LBL/RBL 9.00 AT PASSENGER CABIN WERE EVALUATED OUT OF LIMITS PER CRJ-900 SRM 53-31-49-101-001-A02 AND WERE REPLACED PER CRJ900 AMM 53-00-49 (CONFIG A12)
AFTER ACCESS PANEL 521BL REMOVAL , CRACK ON MACHINED RIB LEADING EDGE SS58.41 AT LEFT WING. LH INBOARD FIXED L/E RIB AT STA 57.16 WAS REPAIRED PER REO 690-57-41-420 REV. --
DURING INSPECTION OF THE TASK CARD 600-08E2-JIC IT WAS DETECTED CRACK IN CANISTER WELDED NO.3 INTO, STA. WS148 OF INTERNAL RH MAIN FUEL TANK. CANISTER WELDED NO.3 INTO, STA. WS148 OF INTERNAL RH MAIN FUEL TANK WAS REPAIRED PER REO 670-57-42-577. REV.--
FREE PLAY ON SELF-ALIGN SELF-LUB BEARING PLAIN ON HINGE FITTING NO. 3 AT VERTICAL STABILIZER REAR SPAR MIDDLE SECTION. HINGE FITTING NO. 3 AT VERTICAL STABILIZER REAR SPAR MIDDLE SECTION WAS REPLACED PER RIL #2103 REV. B
CORROSION ON SIDE SEAT RAIL STGR 15 RH/LH (SEVERAL LOCATIONS) BTW FS379.00 TO FS669.40 AT PASSENGER CABIN. SIDE SEAT RAIL STGR 15 RH/LH BTW FS379.00 TO FS669.40 AT PASSENGER CABIN WERE EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-41-49-101-001-A02; CRJ900 SRM 53-51-49-101-001-A02 AND WERE REPLACED PER CRJ900 AMM 53-00-49 (CONFIG A12)
AFT SILL REMOVAL IN REFERENCE TO NRC 0109, CORROSION ON MOUNTING ANGLE AT FWD SURROUND STRUCTURE OF GALLEY SERVICE DOOR BTW STA FS 319.70 TO FS 349.00 WAS FOUND MOUNTING ANGLE AT FWD SURROUND STRUCTURE OF GALLEY SERVICE DOOR BTW STA FS 319.70 TO FS 349.00 WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-21-23-101-002-A02 AND WAS REPLACED PER CRJ900 SRM 53-21-23-001-002-A01
CORROSION ON FITTING (4E/A) OF ATTACHMENT POINT AT GALLEY 1 AND CORROSION ON FITTING (2EA) OF ATTACHMENT POINT AT ENTRANCE COMPARTMENT. (FLOOR STRUCTURE AREA). FITTING (4E/A) OF ATTACHMENT POINT AT GALLEY 1 AND CORROSION ON FITTING (2EA) OF ATTACHMENT POINT AT ENTRANCE COMPARTMENT WERE EVALUATED PER CRJ900 SRM 53-21-43-101-001-A03 AND WERE REPLACED PER CRJ900 SRM 51-42-21-001-001-A01
AFT DOOR SILL REMOVAL IN REFERENCE TO NRC 0095, CORROSION ON FWD CHORD AT C2 BTW STA FS 1000.00TO FS 1015.00 WAS FOUND. FWD CHORD AT C2 BTW STA FS 1000.00TO FS 1015.00 WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-61-23-101-001-A01 AND WAS VERIFIED PER CRJ900 SRM 53-61-23-001-001-A01.
PERM REPAIR - LH PYLON ACCESS PANELS 412EB AND 412GB REF REO 690-54-51-050 WHITHIN 800 FH, REPAIR THE AFFECTED PARTS ACCORDING TO APPROVED PROCEDURES. LH PYLON ACCESS PANELS 412EB AND 412GB WERE REPAIRED PER REO 690-54-51-052 REV. - -
WEAR AND NICKS ON FWD/AFT COUNTERBALANCE ARM OF CENTER DOOR AT FWD CARGO COMPARTMENT. FWD/AFT COUNTERBALANCE ARM OF CENTER DOOR AT FWD CARGO COMPARTMENT WERE REPAIRED PER REO 690-52-35-388 REV. - - AND PER REO 690-52-35-390 REV. - -
WEAR AND NICKS ON FWD COUNTERBALANCE ARM OF FWD DOOR AT FWD CARGO COMPARTMENT. WEAR AND NICKS ON FWD COUNTERBALANCE ARM OF FWD DOOR AT FWD CARGO COMPARTMENT. WAS REPAIRED PER REO 690-52-35-389 REV. --
CRACK IN CANISTER WELDED NO.3 IN, STA. WS148 OF INTERNAL RH MAIN FUEL TANK. CRACK IN CANISTER WELDED NO.3 IN, STA. WS148 OF INTERNAL RH MAIN FUEL TANK WAS REPAIRED PER REO 670-57-42-577. REV.--
CABIN SMOKE ON TAKEOFF. RIGHT PACK AUTOFAIL ON LANDING / C/W OPS CHECK OF AIR-CONDITIONING SYSTEM IAW CRJ900 AMM 21-51-00-710-801 R/H PACK R/H PACK OVER TEMPED B-1 211943 C/W L/H AND R/H ENGINE START AND RUN AT IDLE IAW CRJ 900 AMM 71-00-00-866-806 NO INDICATION OF SMOKE IN COCKPIT OR CABIN T/S PER CRJ 900 FIM 21-22-00-810-806. REMOVED ACM, FOUND IT WAS SEIZED, AND REPLACED ACM IAW CRJ 900 AMM 21-51-08-000/400-801.
RUD LIMITER FAULT CAUTION MSG IN FLIGHT. / REMOVED AND REPLACED L/H FADEC IAW CRJ 900 AMM 73-21-01-000/400-801-A01. OPS CHECKS GOOD. PERFORMED RUDDER TRAVEL LIMITER OPS CHECK IAW CRJ 900 AMM 27-25-00-710-801-A01. OPS CHECK GOOD AT THIS TIME
L ENG SURGE CLOSED CAUTION MSG & L FADEC FAULT STATUS MSG IN FLIGHT / INSTALLED NEW LH ENG OBV IAW CRJ900 AMM 75-31-01-400-801. OPS CHECK/LEAK CHECK GOOD. IDLE SPEED CHECK GOOD IAW CRJ900 AMM 71-00-00-720-801. NO SURGING.
AFTER TAKE OFF THE CREW GOT BRAKE TEMP OVER HEAT INDICATOR MESSAGE. THEY RAN THE QRH AND MADE THE DECISION TO RETURN TO BGR. THEY WERE NOT OVERWEIGHT AND NO BRACE WAS CALLED. THE CREW DID DECLARED A EMERGENCY AND TRUCKS DID ROLL BUT THEY WERE NOT NEEDED. NO FURTHER INFORMATION HAS BEEN PROVIDED. BRAKE OVHT WARNING INFLIGHT.#1 INDICTOR IS INTERMITTENT ON EICAS. / DISCONNECTED LOB BRAKE TEMP SENSOR IAW MEL INSTRUCTIONS; M FUNCTION C/W. DEFERRED LOB SENSOR PER MEL 32-46-01 CAT C OPT 4. REMOVED AND REPLACED LH OB BRAKE THERMOCOUPLE SENSOR IAW CRJ 900 AMM 32-46-01-000/400-801-A01. OPERATIONAL CHECK GOOD. THIS CLEARS MEL. M FUNCTION REVERSED AND PLACARD REMOVED.
FLAPS FAILED ON APPROACH INTO VPS. THEY LANDED WITHOUT INCIDENT AND THE FIRE TRUCKS MET THE AIRCRAFT AND EXAMINED THE BRAKES FOR DAMAGE. INTERROGATED MDC TO FIND B1 CODES 007795/007794/006796/007812. T/S FAULTS IAW CRJ 900 FIM 27-51-01-810-803/802-A01, 27-52-45-810-812-A01, AND 27-51-05-810-814-A01. FAULTS FOLLOWED SFECU 2 WHEN SWAPPED. SUSPECT FAULTY SPECU 2. REMOVED AND REPLACED SFECU 2 IAW CRJ 900 AMM 27-51-05-000/400-801-A01. OPS CHECK GOOD. SELF -TEST GOOD. NO FURTHER FAULTS FOUND.
AFTER BLOCKING OUT IN HSV, FLIGHT GOT FLAPS FAIL CAUTION. FLIGHT RTG AND MX WAS ABLE TO GET MESSAGE TO CLEAR. ONCE IN FLIGHT, FLAPS FAIL MESSAGE APPEARED AGAIN. FLIGHT CONTINUED TO CLT. ONCE ON APPROACH, AN EMERGENCY WAS DECLARED DUE TO FLAPS FAIL MESSAGE. FLIGHT LANDED WITHOUT FURTHER ISSUES, AND WAS ABLE TO TAXI TO THE GATE. AIRCRAFT IS NOW OUT OF SERVICE. REMOVED AND REPLACED SFECU 2 IAW CRJ-900 AMM 27-51-05-000/400-801. OPS TEST AND SELF TEST GOOD. MESSAGE DID NOT REOCCUR
STEERING INOPERABLE CAUTION MESSAGE IN FLIGHT. REMOVED AND REPLACED NWS WIRE HARNESS. REMOVED AND REPLACED NWS MANIFOLD. OPERATIONS AND LEAK CHECK GOOD.
RT AFT EMERGENCY AND FWD PASSENGER DOOR EXIT SIGNS WILL NOT ILLUMINATE. RELAMPED RT AFT EMERGENCY LIGHT. OPERATIONS CHECK GOOD. PERFORMED OPERATIONS CHECK OF FWD EXIT SIGN. OPERATIONS CHECK GOOD.
CREW CALLED IN TO REPORT INCIDENT AT 1946L AFTER COMPLETING RDU-CLT CONTINUATION TO GIVE DISPATCH COORDINATOR NECESSARY INFORMATION TO COMPLETE THIS REPORT. WHILE ENROUTE FROM IAD-CLT CREW DECLARED EMERGENCY FOR NOSE WHEEL STEERING INOPERABLE. UPON GETTING CLOSER TO CLT, CLT ENTERED GROUND STOP AND PREVENTED AIRCRAFT FROM LANDING AT INTENDED DESTINATION. AIRCRAFT THEN DIVERTED DUE WEATHER IN CLT TO RDU. RDU WAS NOTIFIED OF DIVERSION AND EMERGENCY FIRE AND RESCUE TRUCKS AND AIRCRAFT TOW TEAM WERE STANDING BY UPON ARRIVAL IN RDU. FLIGHT 5320 IAD-RDU LANDED SAFELY IN RDU AS NORMAL, WAS UNABLE TO PULL OFF RUNWAY UNDER OWN POWER. AIRCRAFT SAT ON RUNWAY FOR 10 MINUTES AS TOW TEAM PREPARED AIRCRAFT FOR TOW TO GATE. NO OPERATIONS OR ATC INCIDENTS OCCURED DUE TO THE RUNWAY CLOSURE IN RDU FURTHER MORE NO GO AROUNDS OR ATC SPACING WAS INCIDENTS OCCURED DUE TO THE AIRCRAFT BLOCKING THE RUNWAY FOR ABOUT 10-15 MINS. CREW DID NOT CONTACT DISPATCH AFTER SAFELY ARRIVING AT GATE, DISPATCH WAS NOT CONTACTED AND UPDATED ABOUT THE INCIDENT UNTIL AFTER RDU-CLT DIVERSION CONTINUATION WAS COMPLETED AT 1946 LOCAL TIME. CW SYSTEM RESET. OPERATIONS CHECK OF NWS GOOD, IAW CRJ 900 AMM 32-51-00-710-801-A01.
OVERHEAD BIN INSTALLED INCORRECTLY CAUSING INTERFERENCE WITH EMERGENCY EXIT. REMOVED OVER HEAD BIN AT ROW 15-16AC IAW CRJ 900 AMM 25-23-01-000-801-A50. FOUND FWD AND AFT ROD TO BE LOOSE. ADJUSTED RODS AND INSTALLED OVERHEAD BIN IAW CRJ 900 AMM 25-23-01-400-801-A50. DOOR NOW CLEARS OVERHEAD BIN OPS CHECK OF OVER WING EMERGENCY DOOR IAW CRJ 900 AMM 52-21-00-710-801. OPS CHECK GOOD AT THIS TIME.
L/H FWD VERTICAL STABILIZER DRAG ANGLE IS CRACKED IN AFT RADIUS. INSTALLED REPAIR ON LH FWD VERT STAB DRAG ANGLE IAW STEPS #5.B.9-14 OF CRJ900 SRM 55-31-00-201-001-A01 AND SUP #6.
RH VERT STAB AFT DRAG ANGLE, POSSIBLE CRACK. INSTALLED NEW VERT DRAG ANGLE IAW CRJ900 SRM 51-42-13-001-001-A01, 51-42-21-001-001-A01 AND 51-42-22-001-001-A01
CABIN RH SIDE SEAT RAIL HAS MINOR CORROSION FS 785 TO FS 813. FABRICATED NEW SEAT TRACK IAW REO 670-53-00-343 AT FS 785 TO FS 813. INSTALLED SEAT TRACK AT FS 785 TO FS 813 RH IAW CRJ 900 AMM 59-00-49-400-801-A01.
CABIN LH SIDE SEAT RAIL HAS MINOR CORROSION AT FS 811. REMOVED AND INSTALLED NEW SERVICEABLE L/H SIDE SEAT TRACK P/N: SH670-36260-5 AT FS 811 IAW AMM 53-00-49-00/400-801-A12.
INTERCOSTAL BETWEEN FS 349 - 364 AND STGR 26L - 27 IS CORRODED. INSTALLED NEW SERVICEABLE INTERCOSTAL PN SH670-32075-3 IAW SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01 AND 51-40-11-001-010-A01.
CARGO FLOOR SEAT TRACKS AT LB L 9.0, RBL 9.0 AND RBL 27.0 ARE CORRODED FS 990 TO FS 1005. INSTALLED NEW SERVICEABLE SEAT TRACK LBL 9 @ FS 990-1005 IAW AMM 53-00-49-400-802-A02.
L/H AFT VERTICAL STABILIZER DRAG ANGLE IS CRACKED. INSTALLED NEW SERVICEABLE L/H AFT VERTICAL STAB DRAG ANGLE IAW CRJ900 SRM 51-42-13-001-001-A01, 51-42-21-001-001-A01 AND 51-42-22-001-001-A01.
CABIN ALT MASTER WARN IN CLIMB FL 32000. PERFORMED OPERATIONAL TEST OF THE CABIN PRESSURE CONTROLLER, OPS CHECK GOOD. PERFORMED FUNCTIONAL TEST (BYTE) OF THE CPC, OPS CHECK GOOD. PERFORMED OPS TEST OF THE PRESSURE CONTROL SYSTEM IN MAN MODE, PERFORMED FUNCTIONAL TEST OF THE OUTFLOW VALVE, OPS CHECK GOOD. FOUND NO ASSOCIATED B1 CODES. NO DEFECTS NOTED AT THIS TIME.
SHORTLY AFTER T/O, THE CREW REPORTED SMOKE IN THE CABIN. THEY DECLARED AN EMERGENCY AND LANDED WITHOUT ISSUE. MAINTENANCE TROUBLESHOT AND FOUND THE RT PACK OVERTEMPED AND SIEZED. DEFERRED THE RT PACK. REMOVED AND REPLACED RH ACM OPS CHECK GOOD. THIS CLEARS MEL.