N615NN

Part: MANIFOLD — UNSERVICEABLE (NLG STEERING) · airframe 11,639 hrs · 10,125 cycles

NOSE WHEEL STEERING CAUTION MESSAGE IN FLIGHT. REMOVED AND REPLACED NOSEWHEEL STEERING MANIFOLD IAW AMM 32-51-50-000/400-801. PERFORMED OPS AND LEAK TEST IAW AMM 32-51-00-710-801. OPS TEST AND LEAK TEST GOOD AT THIS TIME.

Part: STEERING SYS — MALFUNCTIONED (NLG) · airframe 9,036 hrs · 7,874 cycles

STEERING INOP CAUTION MSG. / COMPLIED WITH MIPM RESET FOR STEERING CAUTION MSG, FAULT EXTINGUISHED.

Part: ACM — ODOR (ZONE 200) · airframe 9,032 hrs · 7,870 cycles

AFT FA SMELLED ODOR OF BURNING ON TO ROLL FROM ROW 16 BACK. / REMOVED AND REPLACED RH ACM IAW CRJ 900 AMM 21-51-08-000/400-801-A01. OPS CHECKED GOOD, LEAK CHECKED GOOD.

Part: MANIFOLD — UNSERVICEABLE (NLG STEERING) · airframe 8,814 hrs · 7,672 cycles

STEERING INOP CAUTION MSG IN AIR AFTER GEAR UP / TROUBLESHOT STEERING MANIFOLD IAW CRJ 900 FIM 32-51-50-810-801. REMOVED AND REPLACED STEERING MANIFOLD IAW CRJ 900 AMM 32-51ˆ’50-000/400-801. COMPLETED INSTALLATION OF STEERING MANIFOLD IAW CRJ 900 AMM 32-51-50-400-801. OPS CHECK/BITE CHECK GOOD.

Part: CONTROL PANEL — NOT REPORTED (FLT CONTROLS) · airframe 8,224 hrs · 7,143 cycles

FMS 1 FAILED / REMOVED AND REPLACED FLIGHT CONTROL PANEL IAW CRJ 900 AMM 22-11-07-000/400-801. OPS CHECK GOOD.

Part: ACCESS PANEL — WORN (RT WING) · airframe 7,876 hrs · 6,810 cycles

LH AILERON FLUTTER DAMPER ACCESS PANEL (552KB) WITHIN 1,892.85 FHS FROM IR (BEFORE 8000 FH), REPAIR, OR REPLACE THE DISCREPANT ITEM IN ACCORDANCE WITH APPROVED PROCEDURES. LH AILERON FLUTTER DAMPER ACCESS PANEL (552KB) WAS REPAIRED PER REO 690-57-22-077 REV - -

Part: SHUTOFF VALVE — UNSERVICEABLE (ANTI-SKID SYS) · airframe 7,871 hrs · 6,808 cycles

THE CREW REPORTED A NORMAL CONFIGURATION FOR T/O. SHORTLY AFTER THEY RECEIVED A A/SKID INBD CAUTION MESSAGE. / REMOVED AND REPLACED THE PBSOV IAW CRJ 900 AMM 32-45-13-000/400-801. OPS CHECK GOOD. PERFORMED OPS TEST AND FUNCTIONAL CHECK OF THE ASCS IAW CRJ 900 AMM 32-44-00-710-801 AND 32-44-00-720-801. ALL CHECKED GOOD. FAULT DID NOT RETURN AT THIS TIME.

Part: SKIN — DAMAGED (BS 248-233) · airframe 7,876 hrs · 6,810 cycles

LIGHTNING STRIKE (2EA) ON EXTERNAL FWD FUSELAGE SKIN AREA STGR14 BTW FS248.5 - FS233.5. LIGHTNING STRIKE (2EA) ON EXTERNAL FWD FUSELAGE SKIN AREA STGR14 BTW FS248.5 - FS233.5 WAS REPAIRED PER PER CRJ-900 SRM 53-00-00-201-003-A03

Part: SKIN — DAMAGED (BS 596 S23R) · airframe 7,876 hrs · 6,810 cycles

LIGHTNING STRIKE ON FUSELAGE SKIN ON STGR 23 RH AT FS 596. LIGHTNING STRIKE ON FUSELAGE SKIN ON STGR 23 RH AT FS 596 WAS REPAIRED PER PER CRJ-900 SRM 53-00-00-201-003-A03

Part: SKIN — DAMAGED (BS 264-280) · airframe 7,876 hrs · 6,810 cycles

LIGHTNING STRIKE (1EA) ON EXTERNAL FWD FUSELAGE SKIN AREA STGR15 BTW FS280 - FS264. LIGHTNING STRIKE (1EA) ON EXTERNAL FWD FUSELAGE SKIN AREA STGR15 BTW FS280 - FS264 WAS REPAIRED PER PER CRJ-900 SRM 53-00-00-201-003-A03

Part: SKIN — DAMAGED (BS 549 S20R) · airframe 7,876 hrs · 6,810 cycles

LIGHTNING STRIKE ON FUSELAGE SKIN BTW STGR 19 RH TO STGR 20 RH AT FS 549. LIGHTNING STRIKE ON FUSELAGE SKIN BTW STGR 19 RH TO STGR 20 RH AT FS 549 WAS REPAIRED PER PER CRJ-900 SRM 53-00-00-201-003-A03

Part: SKIN — DAMAGED (BS 1051-1069) · airframe 7,876 hrs · 6,810 cycles

LIGHTNING STRIKE ( 1EA) ON FUSELAGE SKIN BTW STGR 14 RH TO STGR 15RH AND BTW FS 1051 TO FS 1069. LIGHTNING STRIKE ( 1EA) ON FUSELAGE SKIN BTW STGR 14 RH TO STGR 15RH AND BTW FS 1051 TO FS 1069. WAS BLEND OUT PER CRJ900 SRM 51-12-00-001-001-A01 AND WAS EVALUATED WITHIN LIMITS PER CRJ900 SRM 53-61-01-101-004-A02

Part: DRAG ANGLE — CRACKED (VERTICAL STAB) · airframe 7,876 hrs · 6,810 cycles

CRACK ON LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00). AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00) WAS REPAIRED PER CRJ900 SRM 55-31-00-201-001-A01.

Part: DRAG ANGLE — CRACKED (VERICAL STAB) · airframe 7,876 hrs · 6,810 cycles

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

Part: BEARING — UNSERVICEABLE

SUPPLEMENTAL RECORD CORRECTION: INSTALLED FWD AND AFT SPIGOT ASSEMBLIES AND SERRATED PLATES IAW CRJ 900 AMM 53-21-23-400-803-A03. ADJUSTED SERRATED PLATES BY ADDING SHIMS TO BOTH PLATES. INSTALLED FWD AND AFT SPIGOT BEARING ASSEMBLIES IAW CRJ 900 AMM 53-21-23-400-803. FWD AND AFT BEARING NOW SPINS FREELY WHEN DOOR IS FULLY LATCHED. PERFORMED FUNCTIONAL TEST OF THE PASSENGER DOOR AND ADJUSTED PULL-IN LEVER STOP IAW CRJ 900 AMM 52-11-00-720-802-A01. ALL CHECKS GOOD.

Part: ROLLER TRACK — UNSERVICEABLE · airframe 3,989 hrs · 3,464 cycles

MAIN CABIN DOOR NOT OPENING UPON PARKING. THIS AIRCRAFT IS BEING FERRIED. INSPECTED PAX DOOR SPIGOT FITTINGS & FOUND FWD FITTING ROLLER TO HAVE ROUGH AREAS WHEN BEING SPUN; REMOVED & REPLACED FWD SPIGOT FITTING ROLLER IAW 900 AMM 53-21-23-000/400-803-A03; ORIGINAL ISSUE STILL REMAINS; UPON DOING CLEARANCE/OPS CHECKS OF FWD SPIGOT ROLLER FOUND THAT THE ROLLER WILL NOT SPIN FREELY WHEN DOOR IS LATCHED; FWD SPIGOT FITTING NEEDS TO BE ADJUSTED DOWN FURTHER BUT IS UNABLE TO BE PHYSICALLY ADJUSTED ANY LOWER.

Part: SPRING ASSY — OUT OF ADJUST · airframe 3,952 hrs · 3,434 cycles

UNABLE TO OPEN MAIN CABIN DOOR UPON ARRIVAL IN SRQ / INSPECTED MAIN PAX DOOR AND FOUND DOOR VERY DIFFICULT TO OPEN AND CLOSE, PLACED DOOR IN THE CLOSED AND LOCK POSITION FOR FERRY FLIGHT, AND VERIFIED ALL GREEN WITINESS MARKS ARE ALIGNED AND DEFERRED PER MEL52-21-01 CAT A, AND INSTALLED REQUIRED PLACARD. UPON FURTHER INSPECTION FOUND THE PRESSURE VENT FLAP SPRING ROD ASSEMBLY TO BE OUT OF ADJUSTMENT. RE-ADJUSTED SPRING ROD ASSEMBLY IAW CRJ 900 AMM 52-11-15-820-801. OPS CHECK GOOD, NO FURTHER DEFECTS FOUND AT THIS TIME. THIS CLEARS MEL

Part: DOOR — DIRTY · airframe 3,831 hrs · 3,332 cycles

MAIN CABIN DOOR WAS DIFFICULT TO OPEN UPON ARRIVAL AT GATE, REQUIRED MULTIPLE ATTEMPTS TO UNLATCH / OPERATED PAX DOOR MULTIPLE TIMES IAW CRJ 900 AMM 52-11-00-710-801 AND FOUND TORQUE TUBE ASSY AND LOCK PAWL TO BE CONTACTING WHEN TRYING TO CLOSE DOOR. T/S IAW CRJ 900 FIM 52-11-00-810-801/802. VISUALLY CHECKED FOR ANY DAMAGE TO THE OUTER HANDLE, VENT FLAP, AND SURROUNDING AREA. PERFORMED DETAILED INSPECTION OF PAX DOOR LATCH MECHANISM IAW CRJ 900 AMM 52ˆ’11ˆ’02ˆ’220ˆ’801. CLEANED AND LUBRICATED PAX DOOR, LATCH PINS, LATCH CAMS, AND SEAL IAW CRJ 900 AMM 12-20-52-640-808/809/812. OPS CHECKED IAW CRJ 900 AMM 52-11-00-710-801. OPS CHECK GOOD. NO FURTHER DEFECTS NOTED.

Part: WINDSHIELD — CRACKED (200) · airframe 3,640 hrs · 3,172 cycles

EN-ROUTE FROM CLT..CHS, AT FL220 IN OCCASIONAL LIGHT CHOP AND -RA, WHILE DEVIATING AROUND WEATHER. RADAR GAINS WERE UP AND WHILE FLYING AROUND STORM IN DEPICTED GREEN RADAR READING AIRCRAFT WINDSHIELD CRACKED ON CA SIDE. EMERGENCY WAS DECLARED. FO TOOK OVER FLYING RESPONSIBILITY. CREW RAN QRC AND QRH AND DESCENDED QUICKLY THROUGH ICING CONDITIONS WITH LEFT SIDE WINDSHIELD HEAT OFF DUE TO CRACK. AIRCRAFT LANDED SAFELY AT CHS WITHOUT FURTHER INCIDENT. NO INJURIES TO REPORT. REMOVED AND REPLACED CAPTAINS WINDSHIELD IAW CRJ 900 AMM 56-11-01-000/400-801-A01-PSA. WINDOW HEAT OPS CHECK GOOD. LEAK CHECK FAILED. REFER TO LGBK 20160 28 ITEM 1 FOR DISCREPANCY AND MAINTENANCE PERFORMED