N202PS

Part: FRAME — CORRODED (BS 364) · airframe 35,441 hrs · 35,246 cycles

F.S. 364 FRAME CORRODED AT STINGER 23R. C/A: SPLICE REPAIRED FS 264 FRAME IAW BBD REO 601R-53-21-3055

Part: WARNING MESSAGE — FALSE ACTIVATION (STALL WARNING) · airframe 33,875 hrs · 33,778 cycles

THE AIRCRAFT RECEIVED A STALL FAIL 1 MESSAGE AT 5000 FEET. DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. MAINTENANCE COMPLIED WITH A SYS RESET OF STALL COMPUTER, MESSAGE CLEARED.

Part: STIFFENER — CRACKED (BS 621 BULKHEAD) · airframe 32,778 hrs · 32,793 cycles

LOWER STIFFENER ON AFT SIDE OF THE BS 621 BULKHEAD, LBL 36 FOUND CRACKED. REMOVED AND REPLACED THE STIFFENER IAW SRM 51-40-11, AND 51-42-06.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 32,778 hrs · 32,793 cycles

FS 621 REAR PRESSURE BULKHEAD WEB CRACKED AT LBL 18.0 / WL 132, LBL 27.50 / WL 112, BL 0.0 / WL 112, BL 0.0 / WL 134, RBL 9.50 / WL103, RBL 9.50 / WL110, RBL 9.50 / WL127, RBL 18.00 / WL110, RBL 27.50 / WL101 AND RBL 27.50 / WL111. REPAIRED CRACKS IN REAR PRESSURE BULKHEAD IAW REO 601R-53-61-1240 REV D.

Part: FLOOR SUPPORT — CORRODED (BS 559-595) · corrosion level 2 · airframe 32,778 hrs · 32,793 cycles

RIGHT FLOOR SUPPORT CORRODED FROM BS 559+96 TO 595. REPAIRED THE FLOOR SUPPORT IAW REO 601R-53-00-526.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 32,778 hrs · 32,793 cycles

FS 280.00 FLOORBEAM CRACKED AT RBL 9. REPAIRED IAW REO 601R-53-11-171 REV D.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,778 hrs · 32,793 cycles

RT FLOOR SILL DOUBLER AT FS 319.70 IS CORRODED ON I/B CORNER RBL 36. REMOVED AND REPLACED W/NEW SERVICEABLE P/N 601R38669-49 IAW SRM 51-42-06, 51-40-11 AND 51-42-15.

Part: FLOOR SUPPORT — CORRODED (BS 473-559) · corrosion level 2 · airframe 32,778 hrs · 32,793 cycles

LEFT FLOOR SUPPORT IS CORRODED AT BS 473.15 AND 559. COMPLIED WITH REO 601R-53-41-666.

Part: FRAME — CORRODED (BS 605) · corrosion level 2 · airframe 32,778 hrs · 32,793 cycles

FUSELAGE FRAME AT BS 605 IS CORRODED FROM STRINGERS 24L TO 24R. INSTALLED A NEW FRAME.

Part: FLOOR SUPPORT — CORRODED (BS 574-621) · corrosion level 2 · airframe 32,778 hrs · 32,793 cycles

LEFT FLOOR SUPPORT IS CORRODED FROM BS 574 TO 621. REPAIRED IAW REO 601R-53-00-526.

Part: FLOOR SUPPORT — CORRODED (BS 499-513) · corrosion level 2 · airframe 32,778 hrs · 32,793 cycles

RIGHT SIDE FLOOR SUPPORT CORRODED AT BS 499 AND 513 . COMPLIED WITH REO 601R-53-41-666.

Part: DOOR FRAME — CORRODED (BS 333) · airframe 32,778 hrs · 32,793 cycles

PASSENGER DOOR UPPER FRAME AT BS 333 IS CRACKED AT THE STANDOFF. REMOVED & REPLACED THE UPPER DOOR FRAME,

Part: BEAM — LEAKING (WINDOWS) · airframe 31,647 hrs · 31,689 cycles

LOUD HIGH PRESSURE HISS EMINATING FROM FRONT LEFT SIDE OF COCKPIT. RESEALED LEFT WINDSHIELD I-BEAM.

Part: LIGHT — PEELING (CABIN) · airframe 31,084 hrs · 31,158 cycles

EMERGENCY LIGHT STRIP AT ROW 1D PEELING UP. MAINTENANCE INSPECTED, R & R THE LIGHT STRIP COVER AT ROW 1D AND PERFORMED CHECKS IAW THE AMM. THE ACFT WAS RELEASED FOR SERVICE.

Part: SHUTOFF VALVE — MALFUNCTIONED (PNEUMATIC SYSTEM) · airframe 30,461 hrs · 30,544 cycles

RIGHT BLEED AIR SHUTOFF VALVE FAILED TO OPEN. THE CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED, AND PERFORMED OPS CHECKS IAW THE AMM. THE ACFT WAS RELEASED FOR SERVICE.

Part: CONTROL PANEL — FAILED (GENERATOR) · airframe 29,082 hrs · 29,159 cycles

CREW REPORTED AIR DRIVEN GENERATOR INADVERTENTLY DEPLOYED DURING TAKEOFF ROTATION. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, R & R AIR DRIVEN GENERATOR AUTO DEPLOYMENT CONTROL PANEL AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHT) · airframe 28,633 hrs · 28,745 cycles

PRIOR TO FIRST FLIGHT OF THE DAY, CREW REPORTED THE FOLLOWING EMERGENCY LIGHTS INOPERATIVE: FLOOR LEVEL AFT OF ROW 5, LT OVERWING EXIT, TOP, RT OVERWING EXIT, LOWER, AFT 2 LT EXTERIOR OVERWING EXIT LIGHTS AND AFT 2 RT EXTERIOR OVERWING EXIT LIGHTS. MAINTENANCE INSPECTED, R & R NR 4 EMERGENCY BATTERY AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHT) · airframe 28,633 hrs · 28,745 cycles

PRIOR TO FIRST FLIGHT OF THE DAY, CREW REPORTED THE FOLLOWING EMERGENCY LIGHTS INOPERATIVE: FLOOR LEVEL AFT OF ROW FIVE, LEFT OVERWING EXIT - TOP, RT OVERWING EXIT - LOWER, AFT 2 LT EXTERIOR OVERWING EXIT LIGHTS AND AFT 2 RT EXTERIOR OVERWING EXIT LIGHTS. MAINTENANCE INSPECTED, R & R NR 3 EMERGENCY BATTERY AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: ENGINE — FLUCTUATES (RIGHT) · airframe 28,006 hrs · 28,126 cycles

CREW REPORTED RT ENGINE N1 FLUCTUATING FROM 80.8 TO 93.0 IN CLIMB AT FL190. CREW LANDED AT DESTINATION AIRPORT WITHOUT INCIDENT. MAINTENANCE INSPECTED AND DEFERRED ENGINE SPEED CONTROL SYS IAW MINIMUM EQUIPMENT LIST, MEL. ACFT RELEASED FOR SERVICE.

Part: CONTROL UNIT — FAILED (FLAP SYS) · airframe 25,820 hrs · 25,917 cycles

CREW REPORTED FLAPS FAIL AMBER MESSAGE AT FLAPS 8 DEGREES AFTER TAKEOFF. FLAPS WOULD NOT RETRACT TO ZERO DEGREES. CREW DECLARED EMERGENCY, RETURNED TO FIELD AND LANDED SAFELY. MAINTENANCE TROUBLESHOT FLAP SYS, R & R FLAP ELECTRONIC CONTROL UNIT, FECU, AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: FEEDER CABLE — DAMAGED (LT ENGINE) · airframe 25,732 hrs · 25,824 cycles

CREW REPORTED LT ENGINE SURGING AT MAXIMUM CLIMB THRUST (MCT) 86.0 TO 91.0 PERCENT N1 AND LT ENGINE FUEL FLOW SURGE 2,300-2,500 AT MCT. NO SURGE BELOW 76 PERCENT N1. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT LT ENGINE SPEED CONTROL SYS, R & R W9 BROWN ELECTRICAL CABLE FOR T2 TRANSMITTER AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: SENSOR — FAILED (LT ENGINE) · airframe 25,413 hrs · 25,513 cycles

CREW REPORTED LT N1 PLUS OR MINUS 5 PERCENT UNCOMMANDED POWER ADJUSTMENTS DURING FLIGHT, N1, ITT, N2 AND FUEL FLOW ALL UNCOMMANDED MOVEMENT. UNABLE TO SET AND MAINTAIN POWER SETTING AT HIGHER SETTING. NO ISSUES AT IDLE. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, R & R LT FAN INLET TEMPERATURE, T2, SENSOR AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: CONNECTOR — DIRTY (EMERGENCY LIGHT) · airframe 24,999 hrs · 25,092 cycles

CREW REPORTED LIGHTS ON WITH EMERGENCY LIGHT SWITCH IN ARM POSITION. MAINTENANCE INSPECTED, CLEANED CONNECTOR AND PERFORMED CHECKS IAW AMM. AIRCRAFT RELEASED FOR SERVICE.

Part: BULKHEAD — CHAFED (BS 621) · airframe 24,945 hrs · 25,045 cycles

DURING SCHEDULED MAINTENANCE, THE BS 621 PRESSURE BULKHEAD WAS FOUND CHAFED AT BL 0.0 AFT FACE ZEE MEMBER. THE AREA WAS INSPECTED AND REPAIRED USING AMM. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: STRINGER — CRACKED (BS 379) · airframe 24,945 hrs · 25,045 cycles

DURING SCHEDULED MAINTENANCE, BS 379.0 AT STRINGER 3L WAS FOUND CRACKED WHERE IT CONNECTS TO THE PASSENGER DOOR UPPER SILL. THE AREA WAS INSPECTED AND REPAIRED USING AMM. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: SKIN — CRACKED (CARGO DOOR) · airframe 24,945 hrs · 25,045 cycles

DURING SCHEDULED MAINTENANCE, THE INTERIOR SKIN OF THE CARGO DOOR WAS FOUND CRACKED FORWARD SIDE OF HANDLE CUTOUT. THE AREA WAS INSPECTED AND REPAIRED USING AMM. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 23,956 hrs · 24,124 cycles

CREW REPORTED EMERGENCY LIGHT STRIP ON RT SIDE, FROM SEAT 2D TO 5D, WILL NOT LIGHT UP. MX INSPECTED, R & R NR 2 EMERGENCY LIGHT BATTERY AND INVERTER AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: FUEL CONTROL — FAILED (ENGINE) · airframe 23,494 hrs · 23,696 cycles

CREW REPORTED RT ENGINE WOULD NOT PRODUCE TAKEOFF THRUST AT TAKEOFF ROLL. ABORTED TAKEOFF AND RETURNED TO GATE. MX TROUBLESHOT, R & R RT ENGINE FUEL CONTROL AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: POSITION SENSOR — FAILED (TE FLAP) · airframe 23,147 hrs · 23,379 cycles

CREW REPORTED FLAPS DEGRADED MESSAGE IN FLIGHT AND THAT LEFT FLAP INDICATES ZERO TO 20 DEGREES WITH CONTROLLABILITY ISSUE. AIRCRAFT PITCH REFLECTED MOVEMENT. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED, REMOVED AND REPLACED LEFT FLAP POSITION TRANSMITTER AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.

Part: PRESSURE SWITCH — DEFECTIVE (ANTI-ICE SYS) · airframe 22,227 hrs · 22,551 cycles

CREW REPORTED LEFT COWL ANTI-ICE CAS MESSAGE AFTER TAKEOFF WITH ANTI-ICE SELECTED OFF. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT USING FIM (FAULT ISOLATION MANUAL), REMOVED AND REPLACED LEFT ENGINE COWL ANTI-ICE PRESSURE SWITCH AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 21,465 hrs · 21,877 cycles

DURING SCHEDULED MAINTENANCE FOUND FS 202.75 PRESSURE BULKHEAD WEB CRACKED AROUND THE PARKING BRAKE CUTOUT. FS 202.75 PRESSURE BULKHEAD WEB AT THE PARKING BRAKE CUTOUT WAS INSPECTED AND REPAIRED USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 21,465 hrs · 21,877 cycles

DURING SCHEDULED MAINTENANCE THE REAR PRESSURE BULKHEAD WEB INDICATED CRACKED. THE REAR PRESSURE BULKHEAD WAS INSPECTED AND REPAIRED USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: TRIM SYSTEM — DISCONNECTED (HORIZ STAB) · airframe 21,133 hrs · 21,574 cycles

DURING INITIAL CLIMB, CREW REPORTED STAB TRIM DISCONNECTED TWICE AND WAS RESET. AUTOPILOT SELF-CANCELLED AFTER 30 SECONDS OPERATION AND WOULD NOT STAY ON. WHILE ON, YOKE MOVED FRONT AND BACK IN VIBRATING PATTERN IN SMOOTH AIR. LOW FREQUENCY VIBRATION OF TAIL DISCERNABLE FROM COCKPIT. CREW RETURNED TO FIELD AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND PERFORMED CHECKS ON HORIZONTAL STAB TRIM, ELEVATOR CONTROL AND RUDDER CONTROL SYSTEMS USING AIRCRAFT MAINTENANCE MANUALS. NO DEFECTS NOTED. AIRCRAFT RELEASED FOR SERVICE.

Part: WIRE HARNESS — DEFECTIVE (NLG) · airframe 21,021 hrs · 21,470 cycles

CREW REPORTED THE LANDING GEAR WAS SLOW TO RETRACT. AIRCRAFT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, REMOVED, AND REPLACED THE NOSE LANDING GEAR HARNESS USING AIRCRAFT MAINTENANCE MANUALS. OPERATIONAL CHECKS WERE ACCOMPLISHED USING THE AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: CONTROL LEVER — FAILED (FLAP SYSTEM) · airframe 20,692 hrs · 21,168 cycles

CREW REPORTED FLAPS FAIL AT 30 DEGREES WHILE COMING IN TO LAND. CREW LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE TROUBLESHOT FLAP SYSTEM, REMOVED AND REPLACED FLAP CONTROL LEVER AND PERFORMED CHECKS USING FIM. AIRCRAFT RELEASED FOR SERVICE.

Part: COMPUTER — MALFUNCTIONED (FUEL QUANTITY) · airframe 20,261 hrs · 20,749 cycles

CREW REPORTED FUEL CHANNEL 1/2 FAIL CAUTION MESSAGE IN FLIGHT FOR A FEW MINUTES, THEN MESSAGE DISAPPEARED. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT AIRCRAFT, REMOVED AND REPLACED FUEL QUANTITY GAUGE COMPUTER AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT RELEASED FOR SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,203 hrs · 20,688 cycles

CREW REPORTED EMERGENCY LIGHT STRIP ON FLOOR AT ROW 5D INOPERATIVE. MAINTENANCE INSPECTED, RE-INSTALLED ROW 5D EMERGENCY FLOOR LIGHT STRIP AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT RELEASED FOR SERVICE.

Part: CIRCUIT BREAKER — TRIPPED (DOOR WARNING) · airframe 20,044 hrs · 20,532 cycles

CREW REPORTED PASSENGER DOOR CAS MESSAGE, SERVICE DOOR MESSAGE AND CARGO DOOR MESSAGE ALL CAME ON AT 15,000 FEET ON CLIMBOUT. CREW RETURNED TO FIELD AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED, RESET A POPPED CIRCUIT BREAKER AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT RELEASED FOR SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,011 hrs · 20,500 cycles

CREW REPORTED FLOOR LEVEL EMERGENCY LIGHTING INOPERATIVE AT SEAT 3D. REMOVED AND REPLACED ROW THREE (3) RIGHT ELECTROLUMINESCENT FLOOR LIGHTING, PERFORMED CHECKS IAW MAINTENANCE MANUAL.

Part: B-NUT — LOOSE (HYDRAULIC SYS) · airframe 19,368 hrs · 19,865 cycles

CREW REPORTED HYD 1 LOW PRESSURE CAS MESSAGE IN FLIGHT EN ROUTE FROM CAK TO PHL. CREW DIVERTED TO PIT AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND TIGHTENED A LOOSE B-NUT ON NUMBER ONE HYDRAULIC SYSTEM PRESSURE MANIFOLD INLET LINE. MAINTENANCE ALSO REMOVED AND REPLACED NUMBER ONE EDP (ENGINE DRIVEN PUMP) BECAUSE OF DRY OPERATION DUE TO THE HYDRAULIC FLUID LOSS AND PERFORMED CHECKS. ALL WORK ACCOMPLISHED BY MAINTENANCE USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.

Part: COMPUTER — INTERMITTENT (FUEL SYSTEM) · airframe 19,230 hrs · 19,721 cycles

CREW REPORTED FUEL CHANNEL 1/2 FAIL CAUTION MESSAGE WITH YELLOW DASHED LINES IN ALL FUEL QUANTITY READINGS AFTER DEPARTURE FROM CLT. CREW RETURNED TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, REMOVED AND REPLACED FUEL SYSTEM COMPUTER AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.

Part: CONNECTOR — LOOSE (CABIN) · airframe 19,071 hrs · 19,573 cycles

AT CLT, CREW REPORTED FLOOR EMERGENCY PATH LIGHTING AT SEAT 5D HAD A LOOSE CONNECTION. MAINTENANCE INSPECTED, SECURED LOOSE CONNECTION AND PERFORMED CHECKS ON EMERGENCY LIGHTS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.

Part: LIGHT — DISCONNECTED (CABIN) · airframe 18,947 hrs · 19,448 cycles

AT CLT, EMERGENCY FLOOR LIGHT AT ROW 4 NOT ILLUMINATING. MAINTENANCE INSPECTED FLOOR EMERGENCY LIGHTING, FOUND ROW 4 UNPLUGGED AND TRACK COVER LOOSE, REINSTALLED LIGHT STRIP AND COVER AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT RELEASED FOR SERVICE.

Part: RADOME — DAMAGED (FUSELAGE) · airframe 18,409 hrs · 18,930 cycles

CREW REPORTED A LIGHTNING STRIKE IN FLIGHT EN ROUTE FROM CAK TO PHL. AIRCRAFT LANDED IN PHL WITHOUT INCIDENT. MAINTENANCE INSPECTED AIRCRAFT AND REMOVED AND REPLACED RADOME, TAT PROBE, ATC ANTENNA AND STATIC WICKS. DAMAGE (BURN MARKS) WAS REPAIRED ON LEFT AND RIGHT NOSE LANDING GEAR DOORS, LEFT FUSELAGE, LEFT HORIZONTAL STABILIZER TIP FAIRING AND TAIL CONE. ALL WORK WAS ACCOMPLISHED BY MAINTENANCE USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.

Part: PANEL — CORRODED (WING) · airframe 17,104 hrs · 17,662 cycles

DURING SCHEDULED MAINTENANCE ON THE RIGHT AND LEFT WING FUEL TANK ACESS PANELS, MINIOR CORROSION WAS FOUND. PANELS INSPECTED AND REPAIRED ARE 650DB, 650AB, 650BB, 550CB, 550DB, 550AB, AND 550BB. THE ABOVE INSPECTIONS AND REPAIRS WERE ACCOMPLISHED USING THE AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RETURNED TO SERVICE.

Part: BULKHEAD — CHAFED (FUSELAGE) · airframe 17,104 hrs · 17,662 cycles

DURING SCHEDULED MAINTENANCE CHAFE DAMAGE WAS FOUND ON THE REAR PRESSURE BULKHEAD. THIS WAS FROM THE ISOLATION VALVE. REPAIRS WERE MADE USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RETURNED TO SERVICE.

Part: COMPRESSOR — DAMAGED (LT ENGINE) · airframe 16,927 hrs · 17,482 cycles

ON CLIMBOUT FROM GNV, CREW REPORTED THE LEFT ENGINE FAILED AT ABOUT 3,000 FEET WITH SEVERE VIBRATION AND LOSS OF THRUST DOWN TO BELOW IDLE. ENGINE WOULD NOT RESPOND TO THRUST LEVER INPUTS. CREW SHUT DOWN THE LEFT ENGINE PER QRH, RETURNED TO GNV AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED, REMOVED AND REPLACED THE LEFT ENGINE DUE TO COMPRESSOR DAMAGE AND PERFORMED CHECKS USING THE AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: OUTFLOW VALVE — INOPERATIVE (CABIN PRESSURE) · airframe 16,623 hrs · 17,198 cycles

CREW REPORTED A CABIN ALTITUDE AMBER CAS MESSAGE. ACFT RETURNED AND LANDED WITHOUT INCIDENT. MX ,USING THE ACFT MM R & R THE OVERBOARD SHUTOFF VALVE. CHECKS WERE MADE AND ACFT WAS RELEASED FOR SERVICE.

Part: UNKNOWN — MALFUNCTIONED (CABIN PRESSURE) · airframe 16,556 hrs · 17,128 cycles

CREW REPORTED THE CABIN NOT PRESSURIZING AFTER TAKEOFF FROM CLT. CREW RETURNED TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND PERFORMED A PRESSURIZATION CHECK OF THE AIRCRAFT USING THE AIRCRAFT MAINTENANCE MANUAL. NO DEFECTS WERE NOTED. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 14,753 hrs · 15,327 cycles

AT PGV, CREW REPORTED FLOOR LEVEL EMERGENCY LIGHTS AFT OF ROW EIGHT (8) INOPERATIVE. MAINTENANCE TROUBLESHOT, RECONNECTED A FLOOR-TRACK EMERGENCY LIGHT CONNECTOR AND PERFORMED CHECKS USING THE AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: SENSING ELEMENT — DEFECTIVE (FUSELAGE) · airframe 14,636 hrs · 15,191 cycles

CREW REPORTED AN ANTI-ICE DUCT WARNING MESSAGE, WITH THE RT FUSELAGE INDICATING RED, AFTER DEPARTURE FROM TYS EN ROUTE TO CLT. AIRCRAFT DIVERTED TO TRI AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT THE AIRCRAFT AND REMOVED AND REPLACED A HEAT SENSING ELEMENT USING THE AIRCRAFT MAINTENANCE MANUAL. CHECKS WERE PERFORMED USING THE AIRCRAFT MAINTENANCE MANUAL AND NO FURTHER DEFECTS WERE NOTED. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 14,396 hrs · 14,907 cycles

DURING SCHEDULED MAINTENANCE IT WAS FOUND THAT THE REAR PRESSURE BULKHEAD WEB HAS A CRACK AT THE LINTEL ATTACHMENT. REPAIRS WERE MADE USING THE MANUFACTURERS MANUALS AND AIRCRAFT RELEASED FOR SERVICE.

Part: STRUCTURE — DENTED (FUSELAGE) · airframe 14,396 hrs · 14,907 cycles

DURING SCHEDULED MAINTENANCE IT WAS FOUND THAT A PROTRUDING DENT 4 X .75 X .015 INCH DEEP BETWEEN FS 682 - FS 700 AND BETWEEN STRINGERS 23-24 R. REPAIRS WERE MADE USING THE MANUFACTURERS MANUALS AND AIRCRAFT RELEASED FOR SERVICE.

Part: FRAME — CRACKED (FUSELAGE) · airframe 14,396 hrs · 14,907 cycles

DURING SCHEDULED MAINTENANCE IT WAS FOUND THAT A CRACK AT FRAME 559 FRAME CAP ANGLE BEND RADIUS LBL 18.0. ALSO, A WEB CRACK AT 559.0 INBOARD OF RBL 18.0 WL 59.10. REPAIRS WERE MADE USING THE MANUFACTURERS MANUALS AND AIRCRAFT RELEASED FOR SERVICE.

Part: LOOP — FAULTY (DETECTION SYS) · airframe 14,309 hrs · 14,805 cycles

CREW REPORTED ON TAKEOFF RECEIVED A RED ANTI ICE DUCT MESSAGE. AIRCRAFT RETURNED TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AIRCRAFT AND REMOVED AND REPLACED A FUSELAGE LOOP USING THE AIRCRAFT MAINTENANCE MANUAL. CHECKS WERE MADE USING THE MAINTENANCE MANUAL AND THE AIRCRAFT RELEASED FOR SERVICE.

Part: IDG — MALFUNCTIONED (NR 1) · airframe 12,521 hrs · 12,965 cycles

CREW RECEIVED NR 1 IDG DISCONNECT AND NR 1 GENERATOR OFF CAS MESSAGE ON TAKEOFF ROLL. THE CREW ABORTED THE TAKEOFF AND RETURNED TO GATE IN CLT. MAINTENANCE INSPECTED AND SERVICED THE NR 1 IDG AND LEAK CHECKED PER THE AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: RVDT — FAILED (NLG STEERING) · airframe 11,838 hrs · 12,226 cycles

CREW REPORTED AN ABORTED TAKEOFF AT ABOUT 80 KNOTS AND RETURN TO GATE IN CLT FOR NOSE WHEEL STEERING PULLING RIGHT. MAINTENANCE INSPECTED AIRCRAFT AND REPLACED THE RT RVDT. OPERATION CHECKS ACCOMPLISHED WITH NO OTHER DEFECTS. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: IDG — LOW (NR 2) · airframe 11,485 hrs · 11,828 cycles

CREW REPORTED GEN 2 TRIPS OFF LINE WHEN TAKEOFF POWER IS APPLIED. KVA, HZ AND V ALL READ ZERO. CREW ELECTED TO RETURN TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND NR 2 IDG OIL LEVEL LOW. MAINTENANCE SERVICED NR 2 IDG OIL LEVEL. CHECKS GOOD. NO FURTHER DEFECTS. AIRCRAFT RELEASED FOR SERVICE.

Part: IDG — LOW (NR 1) · airframe 11,485 hrs · 11,828 cycles

CREW REPORTED AMBER CAS MESSAGE IDG 1 AT 60 KNOTS. CREW ELECTED TO ABORT TAKEOFF AND RETURNED TO GATE WITHOUT INCIDENT. MAINTENANCE INSPECTED AND SERVICED NR 1 IDG. CHECKS GOOD. NO FURTHER DEFECTS. AIRCRAFT RELEASED FOR SERVICE.

Part: APU — MALFUNCTIONED · airframe 10,008 hrs · 10,217 cycles

CREW REPORTED THE APU FLAMED OUT AFTER ENGINE SHUTDOWN. GROUND CREW STATED SMOKE WAS COMING FROM THE RIGHT SIDE OF THE AIRCRAFT. MAINTENANCE INSPECTED AND FOUND SMOKE COMING FROM THE APU INTAKE DOOR, FUEL LEAKING FROM DRAIN ON TO THE AFT EQUIPMENT BAY. MAINTENANCE PERFORMED A GENERAL VISUAL CHECK OF THE APU, PERFORMED A GENERAL VISUAL INSPECTION OF THE APU FUEL SYSTEM COMPONENTS AND PERFORMED A START/STOP SEQUENCE OF THE APU IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL. OPERATIONAL CHECKS WERE PERFORMED. NO DEFECTS NOTED. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: OIL SYSTEM — LOW (APU) · airframe 9,702 hrs · 9,920 cycles

CREW REPORTED ON TAXI-OUT AN APU AUTO SHUTDOWN. CREW ELECTED TO RETURN TO THE GATE WITHOUT INCIDENT. MAINTENANCE INSPECTED AND DEFERRED THE APU PER MEL 49-10-01-1. MAINTENANCE PROPERLY SERVICED THE APU OIL LEVEL IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL. OPS CHECKS OF THE APU WERE GOOD, NO DEFECTS WERE NOTED. MEL WAS CLEARED. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: WINDSHIELD — DELAMINATED (COCKPIT) · airframe 9,162 hrs · 9,349 cycles

CREW REPORTED A BIRD STRIKE TO THE CAPTAIN SIDE WINDSHIELD ON SHORT FINAL. MAINTENANCE INSPECTED AND FOUND POSSIBLE DELAMINATION TO THE WINDOW. MAINTENANCE COMPLIED WITH INSPECTION OF LEFT HAND WINDSHIELD AND FOUND TO BE SURFACE DISCOLORATION ONLY IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL 56-11-01-210-801. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: FIRE BOTTLE — LOW (CARGO BAY) · airframe 9,025 hrs · 9,207 cycles

CREW REPORTED A CARGO BOTTLE LOW CAS MESSAGE IN FLIGHT. CREW ELECTED TO DIVERT AND LAND IN LYH WITHOUT INCIDENT. MAINTENANCE MEL'D THE CARGO FIRE BOTTLE PER MEL 26-25-01 -C-. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 7,705 hrs · 7,760 cycles

CREW REPORTED A FLAPS FAIL CAS MESSAGE ON DESCENT. MAINTENANCE INSPECTED AND COMPLIED WITH THE SERVICE LETTER 00-001. SYSTEM OPS CHECKED GOOD. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: STRUT — DISCHARGED (NLG) · airframe 7,612 hrs · 7,663 cycles

CREW REPORTED A GEAR DISAGREE MESSAGE AFTER TAKEOFF. CREW FOLLOWED THE QRH AND LANDED WITHOUT INCIDENT IN DAY. MAINTENANCE INSPECTED AND SERVICED THE NOSE LANDING GEAR SHOCK STRUT OIL AND NITROGEN IAW THE AIRCRAFT MAINTENANCE MANUAL. MAINTENANCE ALSO PERFORMED OPERATIONAL TESTS. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: CARBON SEAL — DAMAGED (NR 2 ENGINE) · airframe 7,122 hrs · 7,164 cycles

CREW REPORTED A RIGHT ENGINE LOW OIL PRESSURE MESSAGE ON CLIMBOUT. CREW RETURNED TO ATL WITHOUT INCIDENT. MAINTENANCE INSPECTED AND SERVICED THE ENGINE OIL. MAINTENANCE ALSO FOUND DAMAGED THE ENGINE CARBON SEAL. MAINTENANCE REMOVED AND REPLACED THE DAMAGED CARBON SEAL. OPERATIONAL CHECKS WERE PERFORMED. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: OIL SYSTEM — FLUCTUATES (NR 2 ENGINE) · airframe 7,114 hrs · 7,155 cycles

CREW REPORTED THE NR 2 ENGINE OIL PRESSURE INDICATION FLUCTUATED ON CLIMBOUT. CREW RETURNED TO MEM WITHOUT INCIDENT. MAINTENANCE INSPECTED AND PERFORMED OPERATIONAL CHECKS. MAINTENANCE ALSO SERVICED ENGINE OIL. OPERATIONAL CHECKS WERE GOOD. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: AUTOPILOT SYS — MALFUNCTIONED · airframe 6,458 hrs · 6,468 cycles

THE CREW REPORTED THE AUTO PILOT KICKED OFF WHEN GOING TO FLAPS 20, WENT BACK TO FLAPS 8 AND RE-ENGAGED AUTO PILOT, TRIED AGAIN WITH SAME RESULT. MAINTENANCE OPERATIONALLY CHECKED THE AUTO PILOT SYSTEM. OPS CHECKS GOOD. COULD NOT DUPLICATE ON THE GROUND. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: WARNING SYSTEM — MALFUNCTIONED (COCKPIT) · airframe 6,300 hrs · 6,307 cycles

AFTER TAKEOFF THE CREW REPORTED WHEN SWITCHING BLEED SOURCES THE RT PACK SHUT DOWN WITH A HIGH PRESSURE MESSAGE. MAINTENANCE PERFORMED AN OPERATIONAL CHECK OF THE RT PACK. OPS CHECKS GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: WARNING LIGHT — FALSE ACTIVATION (GRN SPOILERS) · airframe 6,113 hrs · 6,101 cycles

CREW REPORTED -O/B GROUND SPOILER FAULT- IN EN ROUTE. MAINTENANCE RESET AND OPERATIONALLY CHECKED SYSTEM. NO FAULTS FOUND. OPERATIONAL CHECKS WERE GOOD. AIRCRAFT WAS RETURNED FOR SERVICE.

Part: WARNING LIGHT — FALSE ACTIVATION (STALL WARNING) · airframe 5,572 hrs · 5,536 cycles

AFTER TAKEOFF THE CREW REPORTED AN INTERMITTENT -STALL FAIL- WARNING MESSAGE. THE FLIGHT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE OXYGEN SERVICING ACCESS DOOR OPEN. INSPECTION OF THE DOOR REVEALED NO DEFECTS. THE DOOR WAS PROPERLY SECURED. THE STALL PROTECTION SYSTEM OPERATIONALLY CHECKED GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: FLAP — BIRD STRIKE (LT WING) · airframe 5,084 hrs · 5,032 cycles

DURING THE SERVICE CHECK, MAINTENANCE FOUND EVIDENCE OF BIRD STRIKE DAMAGE TO THE LEFT INBOARD FLAP. MAINTENANCE COMPLIED WITH A TEMPORARY REPAIR IAW BOMBARDIER REO 601R-57-52-517. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: VALVE — FAILED (RT ANTI ICE SYS) · airframe 4,896 hrs · 4,832 cycles

DURING CLIMB THE RT ENGINE COWL ANTI-ICE CAUTION MESSAGE ILLUMINATED. THE CREW FOLLOWED THE QRH AND RETURNED TO PHL. MAINTENANCE REMOVED AND REPLACED THE RT COWL ANTI-ICE VALVE WITH A SERVICEABLE UNIT. THE SYSTEM LEAK AND OPERATIONALLY CHECK GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 4,506 hrs · 4,469 cycles

THE FLAPS FAIL CAUTION MESSAGE ILLUMINATED WITH FLAPS AT 8 DEGREES. THE CREW FOLLOWED THE QRH AND LANDED WITHOUT INCIDENT. MAINTENANCE RESET AND OPERATIONALLY CHECKED THE FLAP SYSTEM. ALL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: SKIN — UNKNOWN (LT WING TIP) · airframe 4,491 hrs · 4,454 cycles

DURING AN FAA RAMP CHECK, THE INSPECTOR REPORTED EVIDENCE OF LIGHTNING DAMAGE ON THE LT WINGTIP. MAINTENANCE COMPLIED WITH EN ROUTE AND DETAILED LIGHTNING STRIKE INSPECTIONS. NO DAMAGE OR EVIDENCE OF A LIGHTNING STRIKE WAS FOUND. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: SKIN — LIGHTNING STRIKE (FUSELAGE) · airframe 3,521 hrs · 3,473 cycles

THE CREW REPORTED A LIGHTNING STRIKE DURING DESCENT. MAINTENANCE COMPLIED WITH A DETAILED LIGHTNING STRIKE INSPECTION IAW CRJ200 AMM 05-51-05-220-801. THE AIRCRAFT WAS FERRIED TO DAY WHERE MAINTENANCE REPAIRED THE LIGHTNING DAMAGE AND RELEASED THE AIRCRAFT FOR SERVICE.

Part: SEAL — LEAKING (PAX DOOR) · airframe 2,509 hrs · 2,453 cycles

DURING CLIMB AFTER TAKEOFF, AT 1000 FEET, THE CABIN STARTED CLIMBING WITH THE AIRCRAFT AND A LOUD SQUEAL WAS HEARD COMING FROM THE FORWARD CABIN. THE CREW OF FLIGHT 2321 RETURNED TO DAY AND MADE AN UNEVENTFUL LANDING. PSA MAINTENANCE FOUND THE PASSENGER DOOR SEAL DAMAGED. THE SEAL WAS REMOVED AND REPLACED IAW CRJ200 AMM 52-11-10-000-803 & 400-803. THE PRESSURIZATION OPERATIONAL TEST WAS GOOD IAW CRJ 200 AMM 21-31-00-863-005. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE.

Part: STRUCTURE — BIRD STRIKE (RT WING) · airframe 1,922 hrs · 1,907 cycles

AFTER SHUTDOWN IN DAY EVIDENCE OF A BIRD STRIKE ON THE RT WING INBOARD LEADING EDGE WAS REPORTED BY THE CREW OF FLIGHT 2461. PSA MAINTENANCE INSPECTED THE AREA AND FOUND THE DAMAGE TO BE OUT OF LIMITS FOR CONTINUED SERVICE. PSA MAINTENANCE THEN REMOVED & REPLACED THE DAMAGED RT WING INBOARD LEADING EDGE PANEL WITH A SERVICEABLE UNIT IAW CRJ200 AMM 57-41-01 AND THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: FIRE LOOP — FAILED (LT ENGINE) · airframe 1,377 hrs · 1,385 cycles

THE CREW REPORTED THAT THE LEFT HAND ENGINE FIRE LOOP-A WAS INOP. MAINTENANCE CONTROL DEFERRED THE LEFT HAND FIRE LOOP-A WITH THE CREW PER MEL 26-11-01 CODE-C. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE.

Part: TRANSMITTER — FAILED (TE FLAPS) · airframe 1,151 hrs · 1,157 cycles

DURING FLIGHT, THE CREW RECEIVED A FLAP DEGRADE STATUS MESSAGE AND DIVERTED TO BTV. MAINTENANCE WAS SENT TO BTV. MAINTENANCE THEN INSPECTED AND REPLACED THE LEFT HAND FLAP POSITION TRANSMITTER ASSEMBLY IN ACCORDANCE WITH DORNIER MAITNENANCE MANUAL 27-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE.