N209PS

Part: BATTERY — DISCHARGED (EMERGENCY LIGHTS) · airframe 37,156 hrs · 36,739 cycles

EMERGENCY LIGHTS ASSOCIATED WITH BATTERY PACK 4 ILLUMINATE FOR A FEW SECONDS THEN EXTINGUISH. R/R NUMBER 4 EMERGENCY LIGHT BATTERY PACK IAW CRJ-200 AMM 33-51-04-000/400-801 OPS CHECK GOOD

Part: TRANSDUCER — FAILED (WHEEL SPEED) · airframe 36,800 hrs · 36,410 cycles

JUST AS THEY STARTED THEIR TAKE OFF RUN, AT APPROX 20-30KTS CREW RECEIVED ANTI SKID OUTBOARD CAUTION MESSAGE. THEY ABORTED THE TAKE OFF AND SAFELY TAXI OFF OF THE RUNWAY AND CONTACTED MAINTENANCE. THEY WERE UNABLE TO CORRECT THE ISSUE AND RETURNED TO THE GATE. REMOVED AND REPLACED RIGHT OUTBOARD WHEEL SPEED TRANSDUCER PLUG IN ACCORDANCE WITH ESPM 20-17-10 CHECK GOOD IN ACCORDANCE WITH AMM CRJ200 32-44-06-740-801 THIS CLEARS MEL

Part: CONTROL HANDLE — FAULTY (COCKPIT) · airframe 36,649 hrs · 36,267 cycles

DURING INITIAL CLIMB, THE AIRCRAFT'S LANDING GEAR WOULD NOT RETRACT. THE CREW DECLARED AN EMERGENCY AND DECIDED TO DIVERT TO IAD. AS THE CREW WAS BEING VECTORED TO IAD, THE GEAR THEN DID RETRACT. THE CREW WAS ABLE TO RE-EXTEND LANDING GEAR FOR THE LANDING. THE AIRCRAFT LANDED AND TAXIED INTO IAD WITHOUT FURTHER INCIDENT. FERRIED AIRCRAFT TO ORF. REMOVED AND REPLACED LANDING GEAR CONTROL HANDLE AND PERFORMED OPERATIONAL CHECK FLIGHT, OPS CHECK GOOD.

Part: HYDRAULIC SYSTEM — LOW (NR 1) · airframe 36,646 hrs · 36,263 cycles

ON CLIMB OUT FROM BUF, CREW RECEIVED A GEAR DISAGREE MESSAGE AND THE LANDING GEAR WOULD NOT RETRACT. EMERGENCY WAS DECLARED. FLIGHT LANDED WITH OUT FURTHER INCIDENT AND TAXIED BACK TO GATE. DEFERRED LANDING GEAR RETRACTION SYSTEM. SERVICED #1, 2, 3 HYDRAALICS & BLEED SYSTEM JACKED AND CYCLED AIRCRAFT, FUNCTION TEST GOOD. THIS CLEARS MEL.

Part: BATTERY PACK — FAILED (CABIN) · airframe 35,625 hrs · 35,292 cycles

EMERGENCY BATTERY WILL NOT STAY ON. REMOVED AND REPLACED 4 BATTERY PACKS IAW CRJ 200 AMM 33-51-04-000/400-801 OPS CK GOOD. #1 P/N AD2013-1A S/N 69914, #2 S/N 122491, #3 S/N 89779, #4 S/N 187402

Part: PROXIMITY SENSOR — OUT OF ADJUST (NLG) · airframe 34,706 hrs · 34,502 cycles

AFTER TAKEOFF, THE CREW REPORTED A GEAR DISAGREE, THE NLG WOULD NOT RETRACT, BOTH MAINS RETRACTED WITHOUT ISSUE. WE DEFERRED THE LANDING GEAR RETRACTION SYSTEM AND THE AIRCRAFT FLEW ON TO CLT. ADJUSTED PROX SENSOR PS13 IAW CRJ 200 AMM OPS CHECK GOOD.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 34,515 hrs · 34,320 cycles

THE CREW RECEIVED AN APU OIL TEMP CAUTION WITH THE NR 2 IDG ON DEFERRAL. THE AIRCRAFT DIVERTED AND DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. MAINTENANCE CHECKED THE APU OIL LEVEL AND DELTA P WITH NO DEFECTS. OPERATIONAL CHECK GOOD. / 209

Part: SHUTOFF VALVE — LEAKING (APU) · airframe 34,016 hrs · 33,818 cycles

FUEL SMELL FROM BOTH PACKS AT FL18. R&R APU SOV, OPS AND LEAK CK GOOD.

Part: BULKHEAD WEB — CRACKED (BS 621) · airframe 33,792 hrs · 33,582 cycles

FOUND REAR PRESSURE BULKHEAD WEB, BS 621, RBL 18.00, WL 110 HAD MULITPLE INDICATIONS NOTED, APPROXIMATELY 4 INCHES LONG, 50% FSH. FAILED NDT INSPECTION. REPAIRED THE BULKHEAD WEB IAW REO 601R-53-61-1285, REV E.

Part: SUPPORT FITTING — CRACKED (LT WING) · airframe 33,792 hrs · 33,582 cycles

LEFT MLG LOWER WING PLANK HAD AN INDICATION 100% FSH AT THE LOWER EDGE OF THE MOST AFT FASTENER HOLE, INBD. FAILED NDT. REPAIRED THE DAMAGE IAW REO 601R-57-21-2793

Part: FLOORBEAM — CORRODED (BS 280) · corrosion level 2 · airframe 33,792 hrs · 33,582 cycles

BS 280 FLOORBEAM ANGLE WAS CORRODED AROUND 2 EA FASTENER HOLES, BETWEEN LBL 9 AND RBL 9. FABRICATED AND FIT A NEW FLOORBEAM ANGLE IAW REO 601R-53-11-926.

Part: FLOOR SUPPORT — CORRODED (BS 574-621) · corrosion level 2 · airframe 33,792 hrs · 33,582 cycles

LEFT FLOOR SUPPORT WAS CORRODED, BS 574 TO 621 ON UPPER AND LOWER SURFACE. REPAIRED THE FLOOR SUPPORT IAW REO 601R-53-61-1574, REV B.

Part: STRAP — CORRODED (BS 559) · corrosion level 2 · airframe 33,792 hrs · 33,582 cycles

LT & RT FLOORBEAM STRAP AT BS 559 BETWEEN RBL 27 AND RBL 43 WAS CORRODED. REPLACED THE STRAP.

Part: STRINGER — CORRODED (BS 379) · corrosion level 2 · airframe 33,792 hrs · 33,582 cycles

STRINGER 3L WAS CRACKED AT BS 379. REPAIRED THE STRINGER IAW SRM 53-00-03.

Part: SEAT TRACK — CORRODED (BS 559-621) · corrosion level 2 · airframe 33,792 hrs · 33,582 cycles

SEAT TRACK CORRODED FROM BS 559+80 TO 621. REPLACED THE SEAT TRACK.

Part: STRINGER — CORRODED (BS 379) · corrosion level 2 · airframe 33,792 hrs · 33,582 cycles

STRINGER 3L WAS CRACKED AT BS 379. REPAIRED THE STRINGER IAW SRM 53-00-03.

Part: SEAT TRACK — CORRODED (BS 364-409) · corrosion level 2 · airframe 33,792 hrs · 33,582 cycles

SEAT TRACK CORRODED. REPLACED THE SEAT TRACK.

Part: FLOORBEAM — CORRODED (BS 615) · corrosion level 2 · airframe 33,792 hrs · 33,582 cycles

LBL 27, FLOORBEAM ANGLE HAD CORROSION AT BS 615. REPLACED THE FLOORBEAM ANGLE.

Part: WIRE HARNESS — MALFUNCTIONED (NLG DOWLOCK) · airframe 32,597 hrs · 32,487 cycles

DURING CRUISE, AT 27,000 FEET, GEAR INDICATIONS APPEARED ON THE EICAS WITH AMBER DASHED LINES FOR NOSE GEAR FLUCTUATING THEN CAME ON SOLID RED THEN GEAR DISAGREE MESSAGE APPEARED ON EICAS CREW REPORTED GEAR RETRACTION HAD BEEN NORMAL, AND AFTER FOLLOWING QRH THE GEAR INDICATIONS WERE NORMAL. LANDED WITHOUT INCIDENT, NO OTHER MESSAGES NOTED. THE ACFT RETUNED TO DEPARTURE, MX REPLACED THE NLG NR 2 DOWNLOCK SENSOR AND WIRING HARNESS.

Part: PRIORITY VALVE — FAILED (MLG) · airframe 32,547 hrs · 32,440 cycles

GEAR DISSAGREE MESSAGE AFTER TAKE OFF. DECLARED EMERGENCY AND RETURNED TO DEPARTURE. MX R & R THE NLG PRIORITY VALVE OPS CHECKED GOOD.

Part: SWITCH — FAULTY (COCKPIT) · airframe 32,410 hrs · 32,307 cycles

AFTER LANDING, CREW REPORTED SMOKE FROM AROUND THE STANDBY COMPASS AND THE FO WAS SHOCKED BY THE OVERHEAD PANEL. REMOVED AND REPLACED NOSE LANDING LIGHT SWITCH IAW CMM 33-41-07-OPS CHECKS GOOD AT THIS TIME.

Part: PROXIMITY SWITCH — FAULTY (SERVICE DOOR) · airframe 31,581 hrs · 31,504 cycles

SERVICE DOOR INDICATION SYSTEM INOPERATIVE. REMOVED AND REPLACED THE SERVICE DOOR OUTER HANDLE PROXIMITY SWITCH.

Part: STIFFENER — CRACKED (FS 409) · airframe 29,998 hrs · 7,874 cycles

BS 409+128 RBL 18 INBOARD AND OUTBOARD SIDE VERTICAL STIFFENERS CRACKED. MAINTENANCE PERFORMED A MAJOR REPAIR TO FS 409+128 RBL 18 INBOARD AND OUTBOARD VERTICAL STIFFENERS IAW THE AMM. THE AIRCRAFT CONTINUES HEAVY CHECK MAINTENANCE.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 29,998 hrs · 29,982 cycles

FRAME FS 349 CORRODED BETWEEN STR 26L AND STR 26R. MAINTENANCE R & R FS 349 FRAME SEGMENT BETWEEN STR 26L AND STR 26R AND PERFORMED CHECKS IAW THE AMM. THE ACFT CONTINUES HEAVY CHECK MAINTENANCE.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 29,998 hrs · 29,982 cycles

FRAME, FS 333 CORRODED BETWEEN 26L AND 25R. MAINTENANCE R & R FS 333 SEGMENT BETWEEN STR 26L AND 25R AND PERFORMED CHECKS IAW THE AMM. THE ACFT CONTINUES HEAVY CHECK MAINTENANCE.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 29,998 hrs · 29,982 cycles

FRAME, FS 319 CORRODED BETWEEN 25R AND 26R. MAINTENANCE R & R FS 319, FRAME SEGMENT BETWEEN STR 25R AND 26R AND PERFORMED CHECKS IAW THE AMM. THE ACFT CONTINUES HEAVY CHECK MAINTENANCE.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 29,998 hrs · 29,982 cycles

STRINGER 27, CORRODED AT MULTIPLE LOCATIONS BETWEEN FS 319 AND FS 349. MAINTENANCE PERFORMED A SPLICE REPAIR TO STR 27 BETWEEN FS319 AND FS 349 IAW THE AMM. THE ACFT CONTINUES HEAVY CHECK MAINTENANCE.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 29,998 hrs · 29,982 cycles

REAR PRESSURE BULKHEAD WEB AROUND THE LINTEL ATTACHMENT FITTING FAILED NON-DESTRUCTIVE TESTING. MAINTENANCE PERFORMED A MAJOR REPAIR TO PRESSURE BULKHEAD WEB FS621, LINTEL INSTALLATION AND PERFORMED CHECKS IAW THE AMM. THE ACFT CONTINUES HEAVY CHECK MAINTENANCE.

Part: FLOOR SUPPORT — CORRODED (BS 569-621) · corrosion level 2 · airframe 29,998 hrs · 29,982 cycles

CARGO FLOOR SUPPORT LBL 27, BS 569 TO 621 CORRODED. MAINTENANCE REMOVED AND REPLACED THE FLOOR SUPPORT AND PERFORMED CHECKS IAW THE AMM. THE AIRCRAFT CONTINUES HEAVY CHECK MAINTNENANCE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,293 hrs · 29,287 cycles

CREW REPORTED ROW 1 FLOOR TRACK EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE INSPECTED, R & R ROW 1 EMERGENCY FLOOR LIGHT STRIP AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: SENSOR — FAILED (FLAP CONTROL SYS) · airframe 29,291 hrs · 29,284 cycles

CREW REPORTED RECEIVING A FLAP FAIL MESSAGE AT FL 290. THE CREW DECLARED AN EMERGENCY, CONTINUED TO DESTINATION AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE TROUBLESHOT, R & R THE BRAKE AND POSITIONING SENSOR UNIT. MAINTENANCE PERFORMED CHECKS IAW THE AMM AND THE ACFT WAS RELEASE FOR SERVICE.

Part: CONNECTOR — BROKEN (EMERGENCY LIGHTS) · airframe 29,034 hrs · 29,021 cycles

CREW REPORTED EMERGENCY FLOOR TRACK LIGHTING STRIP FROM ROW 9 AFT INOPERATIVE. MAINTENANCE INSPECTED, REPLACED BROKEN PIN CONNECTION AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: SHUTOFF VALVE — FAILED (BLEED AIR SYSTEM) · airframe 28,053 hrs · 28,039 cycles

CREW REPORTED LT PACK DID NOT PRESSURIZE AND LT PRESSURE REGULATING SHUTOFF VALVE DID NOT WORK AFTER TAKEOFF. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED, R & R TENTH STAGE SHUTOFF VALVE AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 24,682 hrs · 24,702 cycles

CREW REPORTED EXTERIOR, LT OVERWING AFT EMERGENCY LIGHT WOULD NOT ILLUMINATE. MAINTENANCE INSPECTED, REPLACED LAMPS AND PERFORMED CHECKS IAW AMM. AIRCRAFT RELEASED FOR SERVICE.

Part: RADOME — DAMAGED (FUSELAGE) · airframe 24,295 hrs · 24,347 cycles

CREW REPORTED LIGHTNING STRIKE TO NOSE OF ACFT DURING FLIGHT. MAINTENANCE PERFORMED LIGHTNING STRIKE INSPECTION AND R & R RADOME.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 24,149 hrs · 24,197 cycles

CREW REPORTED CRACKED WINDSHIELD. MAINTENANCE TROUBLESHOT, R & R THE LEFT WINDSHIELD USING AMM. ACFT WAS RELEASED FOR SERVICE.

Part: CONTROL UNIT — FAILED (MLG) · airframe 23,671 hrs · 23,759 cycles

CREW REPORTED WOW INPUT INOPERATIVE CAUTION MESSAGE ON INITIAL TAKEOFF ROLL AND NOSE WHEEL STEERING INOPERATIVE. CREW REJECTED TAKEOFF AND RETURNED TO GATE. MX TROUBLESHOT, R & R PSEU (PROXIMITY SENSOR ELECTRONIC UNIT) AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: CONNECTOR — DIRTY (NLG STEERING) · airframe 22,993 hrs · 23,121 cycles

STEERING INOPERATIVE MESSAGE AS ACFT TOOK RUNWAY FOR DEPARTURE. PULLED OFF RUNWAY AND RETURNED TO GATE. MX INSPECTED, REMOVED, CLEANED AND REINSTALLED NOSE WHEEL STEERING CONNECTORS AND PERFORMED CHECKS USING AMM. ACFT RELEASED FOR SERVICE.

Part: LIGHT — DAMAGED (TAIL) · airframe 22,923 hrs · 23,052 cycles

DURING APPROACH, A LIGHTNING STRIKE TO ACFT. ACFT LANDED WITHOUT INCIDENT. MX TROUBLESHOT, R & R THE UPPER TAIL NAVAGATION LIGHT ASSY, AND STATIC WICKS IAW ACFT MANUALS. CHECKS WERE PERFOMED IAW THE ACFT MANUALS AND ACFT WAS RELEASED FOR SERVICE.

Part: RADOME — DAMAGED (FUSELAGE) · airframe 22,916 hrs · 23,043 cycles

CREW REPORTED A LIGHTNING STRIKE TO AIRCRAFT. AIRCRAFT RETURNED TO AIRPORT AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, REMOVED AND REPLACED THE RADOME, RADAR ANTENNA, AND STATIC WICKS PER AIRCRAFT MANUALS. CHECKS WERE PERFOMED PER THE AIRCRAFT MANUALS AND AIRCRAFT WAS RELEASED FOR SERVICE.

Part: DOOR SEAL — DEFECTIVE (PAX DOOR) · airframe 22,502 hrs · 22,661 cycles

CREW REPORTED PASSENGER DOOR SQUEALING. AIRCRAFT RETURNED TO AIRPORT LANDING WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, REMOVED AND REPLACED THE DOOR SEAL PER AIRCRAFT MANUALS. CHECKS WERE PERFOMED PER THE AIRCRAFT MANUALS AND AIRCRAFT WAS RELEASED FOR SERVICE.

Part: MODULATING VALVE — FAILED (ANTI-ICE SYSTEM) · airframe 22,318 hrs · 22,491 cycles

CREW REPORTED WING OVERHEAT WARNING MESSAGE IN FLIGHT WITH WING ANTI-ICE SELECTED IN STANDBY MODE. NORMAL MODE WAS ON DEFERRAL PER MEL. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, REMOVED AND REPLACED LEFT MODULATING AND SHUTOFF VALVE USING AIRCRAFT MAINTENANCE MANUALS. THIS ALSO CLEARED PREVIOUS DEFERRAL. AIRCRAFT RELEASED FOR SERVICE.

Part: WIRE HARNESS — BROKEN (CARGO DOOR) · airframe 22,124 hrs · 22,311 cycles

CREW REPORTED PASSENGER DOOR WARNING AND SERVICE DOOR CAUTION MESSAGES AT 800 FEET AGL AFTER TAKEOFF. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND CARGO DOOR WIRING HARNESS BROKEN (CARGO DOOR INDICATION HAD PREVIOUSLY BEEN DEFERRED PER MEL). MAINTENANCE REMOVED CARGO DOOR WIRING HARNESS AND PERFORMED CHECKS. AIRCRAFT RELEASED FOR SERVICE. MAINTENANCE SUBSEQUENTLY REPLACED CARGO DOOR HARNESS AND CLEARED CARGO DOOR INDICATION DEFERRAL. ALL WORK ACCOMPLISHED BY MAINTENANCE USING AIRCRAFT MAINTENANCE MANUALS.

Part: BALLAST — DEFECTIVE (CABIN) · airframe 20,229 hrs · 20,640 cycles

CREW REPORTED SLIGHT BURNING SMELL IN AREA OF ROWS 1-3. MAINTENANCE INSPECTED, REMOVED AND REPLACED BALLAST AND BULBS FOR BOARDING LIGHTS AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT RELEASED FOR SERVICE.

Part: POWER UNIT — MALFUNCTIONED (CABIN) · airframe 20,213 hrs · 20,625 cycles

CREW REPORTED STRONG ODOR COMING FROM AROUND ROW 3, POSSIBLY BURNING PLASTIC. MAINTENANCE INSPECTED AND FOUND POWER UNIT DIMMER AT ROW 4A/C TO HAVE STRONG BURNING SMELL. MAINTENANCE REMOVED AND REPLACED POWER UNIT AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT RELEASED FOR SERVICE.

Part: TRANSCEIVER — FAULTY (WEATHER RADAR) · airframe 20,045 hrs · 20,454 cycles

CREW REPORTED WEATHER RADAR ON CAPTAIN’S AND FIRST OFFICER’S MFD (MULTIFUNCTION DISPLAY) WILL NOT DISPLAY IN FLIGHT. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, REMOVED AND REPLACED WEATHER RADAR RECEIVER / TRANSMITTER AND ANTENNA ASSEMBLY AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT RELEASED FOR SERVICE.

Part: APU — FAILED (APU BAY) · airframe 19,363 hrs · 19,803 cycles

CREW REPORTED SMOKE LAV CAS MESSAGE ON TAXI IN, ACCOMPANIED BY STRONG SMELL OF SMOKE. CREW STOPPED AIRCRAFT SHORT OF JETBRIDGE AND PASSENGERS EVACUATED AIRCRAFT THROUGH PASSENGER DOOR. MAINTENANCE INSPECTED LAVATORY AND FOUND NO EVIDENCE OF FIRE OR SMOKE. MAINTENANCE NOTED OIL SMELL WHEN BLEED SELECTED TO APU. MAINTENANCE REMOVED AND REPLACED APU AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.

Part: ENGINE — MALFUNCTIONED (RIGHT) · airframe 18,531 hrs · 19,002 cycles

CREW REPORTED RIGHT ENGINE OIL PRESSURE WARNING MESSAGE AND RIGHT ENGINE OIL INDICATION READ ZERO ON DESCENT INTO PHL. CREW COMPLIED WITH QRH AND SHUT DOWN RIGHT ENGINE. AIRCRAFT LANDED IN PHL WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED, REMOVED AND REPLACED RIGHT ENGINE AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.

Part: CONTROL UNIT — FAILED (TE FLAP) · airframe 18,499 hrs · 18,970 cycles

CREW REPORTED FLAPS FAIL AT 20 DEGREES DURING APPROACH TO CLT. AIRCRAFT LANDED IN CLT WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT FLAP SYSTEM, REMOVED AND REPLACED FECU (FLAP ELECTRONIC CONTROL UNIT) AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.

Part: REGULATOR VALVE — MALFUNCTIONED (AC BAY) · airframe 18,420 hrs · 18,893 cycles

CREW REPORTED RIGHT PACK OVERPRESSURE, WITH LEFT HAND PACK DEFERRED PER MEL, AFTER DEPARTURE FROM DAY. CREW RETURNED TO DAY AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT AIRCRAFT, REMOVED AND REPLACED RIGHT PRESSURE REGULATING / SHUTOFF VALVE AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 17,272 hrs · 17,780 cycles

DURING SCHEDULED MAINTENANCE REPAIRS WERE MADE TO THE RT BULKHEAD WEB AT FS 559.0 WHICH WAS CRACKED. INSPECTION AND REPAIR WAS ACCOMPLISHED USING THE AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 17,272 hrs · 17,780 cycles

DURING SCHEDULED MAINTENANCE REPAIRS WERE MADE TO THE LT PRESSURE BULKHEAD AT FS 202.75 BL 23.71 AT PARKING BRAKE CABLE PASS THROUGH THAT WAS CRACKED. INSPECTION AND REPAIR WAS ACCOMPLISHED USING THE AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 17,272 hrs · 17,780 cycles

DURING SCHEDULED MAINTENANCE REPAIRS WERE MADE TO FLOOR SUPPORT BEAM AT FS280.0 WHICH WAS CRACKED. INSPECTION AND REPAIR WAS ACCOMPLISHED USING THE AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: STIFFENER — CHAFED (FUSELAGE) · airframe 17,272 hrs · 17,780 cycles

DURING SCHEDULED MAINTENANCE REPAIRS WERE MADE TO A CHAFED BL 0 STIFFENER. INSPECTION AND REPAIR WAS ACCOMPLISHED USING THE AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: PUMP — SHEARED (RT ENGINE) · airframe 17,266 hrs · 17,773 cycles

CREW REPORTED AN OIL PRESSURE WARNING MESSAGE AT CRUISE. CREW SHUT DOWN ENGINE AND DIVERTED TO PHL. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT AND REMOVED, REPLACED, AND OPERATIONAL CHECKED THE SCAVAGE PUMP USING THE AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: PRIORITY VALVE — MALFUNCTIONED (NLG) · airframe 16,863 hrs · 17,395 cycles

CREW REPORTED THE NOSE WHEEL MADE A LOUD CLANGING NOISE ON GEAR EXTENSION ON APPROACH TO IND. GEAR EXTENSION TOOK LONGER THAN NORMAL. CREW LANDED IN IND WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT THE AIRCRAFT, REMOVED AND REPLACED THE NOSE LANDING GEAR (NLG) PRIORITY VALVE AND PERFORMED CHECKS USING THE AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: FUEL CONTROL — FAILED (APU) · airframe 16,108 hrs · 16,613 cycles

CREW REPORTED FUEL/OIL SMELL WHEN APU IS SUPPLYING BLEED AIR. MAINTENANCE TROUBLESHOT, REMOVED AND REPLACED THE APU FUEL CONTROL USING THE AIRCRAFT MAINTENANCE MANUALS. OPERATION CHECKS WERE PERFORMED USING THE AIRCARFT MAINTENANACE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: WARNING SYSTEM — FALSE ACTIVATION (BLEED AIR SYS) · airframe 16,083 hrs · 16,590 cycles

CREW REPORTED, RECEIVED A RED DUCT WARNING. AIRCRAFT DIVERTED TO IAD AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED SYSTEM USING THE AIRCRAFT MAINTENANCE MANUALS. NO DEFECTS NOTED. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: ENGINE — VIBRATION (RIGHT) · airframe 14,547 hrs · 15,082 cycles

CREW REPORTED VIBRATION FROM RIGHT ENGINE ON CLIMBOUT FROM CLT. AIRCRAFT RETURNED TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED CHECKS AND GROUND RAN THE ENGINE USING THE AIRCRAFT MAINTENANCE MANUALS. VIBRATION READINGS WERE WITHIN LIMITS. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: RADOME — DAMAGED (FUSELAGE) · airframe 13,596 hrs · 14,015 cycles

CREW REPORTED A BIRD STRIKE IN DCA. MAINTENANCE INSPECTED PER THE AIRCRAFT MAINTENANCE MANUAL. THE RADOME WAS REMOVED AND REPLACED AND CHECKS WERE MADE PER THE AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: THRUST REVERSER — WARNING MESSAGE (RIGHT) · airframe 13,341 hrs · 13,753 cycles

CREW REPORTED SHORTLY AFTER T/O, RT REV UNLOCKED AMBER MSG APPEARED AND RETURNED TO FIELD AFTER COMPLYING WITH QRH. AIRCRAFT LANDED WITHOUT INCIDENT AT DAY. MAINTENANCE DEFERRED THE RT THRUST REVERSER. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: SENSOR — OUT OF ADJUST (NLG) · airframe 13,259 hrs · 13,665 cycles

CREW REPORTED THE NOSE GEAR WOULD NOT RETRACT AFTER TAKE OFF. AIRCRAFT RETURNED TO CLT LANDING WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT USING THE AIRCRAFT MAINTENANCE MANUAL. THE NLG SENSOR PS14GA WAS FOUND OUT OF LIMITS. THE SENSOR WAS ADJUSTED AND SYSTEM CHECKED PER THE AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: ENGINE — BIRD INGESTION (LEFT) · airframe 11,854 hrs · 12,171 cycles

CREW REPORTED POSSIBLE BIRD STRIKE ON FINAL TO DAY. MX INSPECTED ACFT FOR BIRD STRIKE AND FOUND IT TO BE CONTAINED TO LT ENGINE ONLY. MX COMPLIED WITH BIRD STRIKE INSPECTION ON LT ENGINE AND FOUND FAN BLADES DAMAGED. MULTIPLE FAN BLADES WERE CHANGED ALONG WITH OPPOSITE BLADES IF NEEDED, PER THE MFG MM. CHECKS WERE MADE PER THE ACFT MM AND THE ACFT WAS RELEASED FOR SERVICE.

Part: ENGINE — FAILED (RIGHT) · airframe 9,506 hrs · 9,689 cycles

CREW REPORTED A SMOKE TOILET CAUTION MESSAGE 5 SECONDS AFTER TAKEOFF. CREW ELECTED TO RETURN TO PHL AND LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED A VISUAL INSPECTION OF THE RIGHT HAND ENGINE. MAINTENANCE FOUND EXTERIOR OIL LEAKAGE AT STAGES 2-5 OF THE COMPRESSOR ON OUTBOARD SIDE OF THE ENGINE. MAINTENANCE PERFORMED A BORESCOPE INSPECTION AND FOUND OIL ON STAGE 2 AND 3 VG VANES AND BLADES. MAINTENANCE REMOVED AND REPLACED THE ENGINE IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: DOOR — DAMAGED (E&E BAY) · airframe 9,083 hrs · 9,253 cycles

CREW REPORTED A BIRD STRIKE FORWARD OF THE AVIONICS NOSE COMPARTMENT. MAINTENANCE INSPECTED AND FOUND DAMAGE TO THE LEFT HAND FORWARD AVIONICS DOOR. MAINTENANCE COMPLIED WITH THE BIRD STRIKE INSPECTION 05-51-25-210-801. MAINTENANCE REPAIRED ALL DAMAGE TO THE LEFT HAND FUSELAGE NOSE AREA IN ACCORDANCE WITH THE AIRCRAFT STRUCTURE REPAIR MANUAL 53-11-31. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: SCREW — DAMAGED (FLAP FAIRING) · airframe 8,139 hrs · 8,232 cycles

CREW REPORTED DURING DESCENT A LIGHTNING STRIKE. CREW LANDED IN CHA WITHOUT INCIDENT. MAINTENANCE INSPECTED AND PERFORMED AN EN ROUTE VISUAL LIGHTNING STRIKE INSPECTION IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL 05-51-05-210-801. DAMAGE WAS FOUND ON RIGHT HAND INBOARD FLAP FAIRING SCREW AND LEFT OUTBOARD ELEVATOR STATIC WICK. MAINTENANCE REPAIRED ALL DAMAGE. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: WINDOW — FAILED (COCKPIT) · airframe 8,073 hrs · 8,155 cycles

CREW REPORTED ON CLIMBOUT OF HSV THE RIGHT HAND SIDE WINDOW BROKE. CREW ELECTED TO RETURN TO HSV AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE RIGHT HAND SIDE WINDOW DUE TO INNER PANE SPIDER WEB CRACKS IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL 56-12-01-400-801. OPERATIONAL CHECKS WERE GOOD. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: A/C PACK — MALFUNCTIONED (A/C BAY) · airframe 6,842 hrs · 6,877 cycles

CREW REPORTED A RIGHT HAND PACK OVER PRESSURE INDICATION ON TAKEOFF. CREW RETURNED TO MGM WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND NO DEFECTS. MAINTENANCE PERFORMED OPERATIONAL CHECKS AND OPS CHECKED GOOD. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: ACCESS DOOR — OPEN (EXTERIOR) · airframe 5,460 hrs · 5,403 cycles

DURING CLIMBOUT THE CREW REPORTED THE EXTERNAL SERVICE PANEL ACCESS DOOR WAS OPEN. THE FLIGHT RETURNED TO ABE AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE DOOR AND FOUND NO DEFECTS. THE DOOR WAS PROPERLY SECURED AND THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: STRUCTURE — LIGHTNING STRIKE (RT WING) · airframe 5,381 hrs · 5,319 cycles

DURING POSTFLIGHT INSPECTION THE CREW REPORTED EVIDENCE OF A LIGHTNING STRIKE ON THE RIGHT WINGLET. MAINTENANCE PERFORMED EN ROUTE AND DETAILED LIGHTNING STRIKE INSPECTIONS. DAMAGE WAS FOUND ON THE RIGHT WINGLET, NR 2 VHF ANTENNA, AND THE LOWER TAIL NAVIGATION LIGHT ASSEMBLY. ALL DAMAGE WAS REPAIRED AND THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 4,894 hrs · 4,831 cycles

THE -FLAPS FAIL- CAUTION MESSAGE ILLUMINATED ON FINAL APPROACH WITH FLAPS AT 20 DEGREES SELECTED TO 30 DEGREES. THE CREW FOLLOWED THE QRH AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT AND RESET THE FLAP SYSTEM IAW BOMBARDIER SL-27-084. NO FAULTS WERE FOUND AND ALL OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 4,695 hrs · 4,637 cycles

DURING APPROACH WITH FLAPS AT 20 DEGREES THE FLAPS FAIL CAUTION MESSAGE ILLUMINATED. THE CREW ABORTED THE APPROACH AND FOLLOWED THE QRH. THE APPROACH WAS RE-ESTABLISHED AND THE AIRCRAFT LANDED FLAPS 20 DEGREES WITH NO FURTHER INCIDENT. MAINTENANCE RESET AND OPERATIONALLY TESTED THE FLAP SYSTEM. THE FLAPS OPERATIONALLY CHECKED GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 4,580 hrs · 4,528 cycles

DURING APPROACH WITH FLAPS AT 20 DEGREES THE FLAPS FAIL CAUTION MESSAGE ILLUMINATED. THE CREW ABORTED THE APPROACH AND DECLARED AN EMERGENCY. THE APPROACH WAS RE-ESTABLISHED AND THE AIRCRAFT LANDED FLAPS 20 DEGREES WITH NO FURTHER INCIDENT. MAINTENANCE RESET AND OPERATIONALLY TESTED THE FLAP SYSTEM IAW BOMBARDIER CRJ 200 SL00-001. THE FLAPS OPERATIONALLY CHECKED GOOD. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE.

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 4,564 hrs · 4,512 cycles

THE FLAPS FAIL MESSAGE ILLUMINATED ON APPROACH WITH FLAPS AT 20 DEGREES. THE CREW FOLLOWED THE QRH AND LANDED WITHOUT INCIDENT. MAINTENANCE RESET AND TESTED THE FLAP SYSTEM IAW RJ-SL-27-084. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: WARNING LIGHT — ILLUMINATED (TE FLAPS) · airframe 4,422 hrs · 4,393 cycles

DURING APPROACH WHEN FLAPS WERE SELECTED FROM 20 TO 30 DEGREES THE FLAPS FAIL CAUTION MESSAGE ILLUMINATED. 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: RADOME — GROUND DAMAGE (FUSELAGE) · airframe 4,373 hrs · 4,350 cycles

WHILE PARKED FOR THE NIGHT THE RADOME WAS STRUCK AND DAMAGED BY A LAV SERVICING TRUCK. AFTER INSPECTING THE AIRCRAFT MAINTENANCE REMOVED AND INSTALLED A SERVICEABLE RADOME. NO OTHER DAMAGE WAS FOUND. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 4,117 hrs · 4,102 cycles

DURING APPROACH THE FLAPS FAIL CAUTION MESSAGE ILLUMINATED WITH FLAPS AT 20 DEGREES SELECTED TO 30 DEGREES. THE CREW ABORTED THE APPROACH, RECONFIGURED THE AIRCRAFT, AND LANDED WITHOUT INCIDENT. MAINTENANCE RECORDED FECU LRU & FAULT LOG CONTENTS PER THE FIM. AN OPERATIONAL TEST OF THE FLAP SYSTEM WAS PERFORMED IAW CRJ200 AMM 27-54-00-710-801. THE FLAP SYSTEM OPS CHECKED GOOD AND THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: WARNING LIGHT — FALSE ACTIVATION (PILOT ERROR) · airframe 4,002 hrs · 3,982 cycles

THE FLAPS FAIL CAUTION MESSAGE ILLUMINATED DURING LANDING APPROACH. THE CREW FOLLOWED THE QRH AND MADE AN UNEVENTFUL LANDING. THE CREW REPORTED THAT THE FLAP SELECTOR WAS NOT IN THE DETENT. MAINTENANCE RESET AND OPERATIONALLY CHECKED THE FLAP SYSTEM IAW CRJ200 SL-00-001. OPS CHECKS WERE GOOD AND THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: STEERING SYS — WARNING LIGHT (NLG) · airframe 3,941 hrs · 3,817 cycles

THE STEERING INOP CAUTION MESSAGE ILLUMINATED AFTER DEPARTURE. THE NWS SWITCH WAS CYCLED BUT THE SYSTEM WOULD NOT RESET. THE CREW FOLLOWED THE QRH AND MADE A PRECAUTIONARY LANDING WITH EQUIPMENT AT DESTINATION. MAINTENANCE PERFORMED AN OPERATIONAL TEST OF THE NOSE WHEEL STEERING SYSTEM IAW CRJ200 AMM 32-51-00-710-802. OPS CHECKS WERE GOOD. NO FAULTS WERE FOUND. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE.

Part: WIRE HARNESS — FAILED (NLG STEERING) · airframe 3,942 hrs · 3,818 cycles

THE STEERING INOP CAUTION MESSAGE ILLUMINATED AFTER DEPARTURE. THE NWS SWITCH WAS CYCLED BUT THE SYSTEM WOULD NOT RESET. THE CREW FOLLOWED THE QRH AND RETURNED TO PIT AND LANDED SAFELY. THE AIRCRAFT WAS FERRIED TO CAK WHERE AFTER TROUBLESHOOTING, MAINTENANCE REMOVED AND REPLACED THE NOSE LANDING GEAR HARNESS ASSEMBLY IAW CRJ200 AMM 32-61-25-000(400)-801. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE.

Part: DETECTOR — MALFUNCTIONED (TE FLAPS) · airframe 3,705 hrs · 3,671 cycles

CLIMBING OUT OF DCA THE FLAPS FAIL CAUTION MESSAGE ILLUMINATED. THE CREW FOLLOWED THE QRH AND LANDED WITHOUT INCIDENT AT IAD. MAINTENANCE RESET THE SKEW DETECTION UNIT, PERFORMED A BITE CHECK, AND OPERATIONALLY CHECKED THE FLAP CONTROL LEVER IAW CRJ200 AMM 27-51-01-740-801 AND 27-51-15-710-802. ALL OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE.

Part: FLAP — UNKNOWN · airframe 3,465 hrs · 3,430 cycles

ON APPROACH THE FLAPS FAIL CAUTION MESSAGE ILLUMINATED. MAINTENANCE CLEARED THE CAUTION MESSAGE IAW BOMBARDIER SERVICE LETTER RJ-SL-00-001. THE FLAPS OPERATIONALLY CHECKED GOOD. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE.

Part: WARNING LIGHT — ILLUMINATED (TE FLAPS) · airframe 2,788 hrs · 2,734 cycles

DURING APPROACH TO PHL THE FLAPS FAIL CAUTION MESSAGE ILLUMINATED WITH THE FLAPS AT 20 DEGREES. THE CREW OF FLIGHT 2542 REQUESTED A SECOND APPROACH TO RECONFIGURE THE AIRCRAFT FOR A FLAPS 20 DEGREES LANDING, FOLLOWED THE QRH, AND MADE AN UNEVENTFUL LANDING. PSA MAINTENANCE RESET THE FECU CIRCUIT BREAKERS IAW BOMBARDIER CRJ200 SL: 00-001. OPERATIONAL CHECKS WERE GOOD WITH NO FAULTS FOUND. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE.

Part: STALL WARNING — MALFUNCTIONED · airframe 2,679 hrs · 2,624 cycles

ON CLIMBOUT (PHL TO YOW) THE STALL FAIL CAUTION MESSAGE ILLUMINATED. THE CREW OF FLIGHT 2566 RETURNED TO PHL AND LANDED WITHOUT INCIDENT. PSA MAINTENANCE RESET POWER AND OPERATIONALLY TESTED THE STALL PROTECTION SYSTEM IAW CRJ 200 AMM 27-35-01-750-802. THE STALL SYSTEM TESTED GOOD. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE.

Part: PITOT LINE — OBSTRUCTED · airframe 2,186 hrs · 2,140 cycles

ON A REPOSITIONING FLIGHT, DURING TAKEOFF ROLL AT DAY, THE CAPTAIN LOST IAS READOUT ON HIS PRIMARY FLIGHT DISPLAY AND PREFORMED A REJECTED TAKEOFF AT 95 KTS. PSA MAINTENACE FOUND WATER IN THE PILOT'S AND COPILOT'S PITOT LINES. THE CONTAMINATION WAS REMOVED FROM THE PITOT LINES IAW CRJ 200 AMM 34-11-00-100-801 AND -802. BOTH SYSTEMS LEAK CHECKED GOOD IAW CRJ 200 AMM 34-11-00-790-802. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE.

Part: FIRE LOOP — FAILED (APU) · airframe 1,567 hrs · 1,534 cycles

THE CREW REPORTED RECEIVING A APU FIRE FAIL AMBER CAS MESSAGE. THE FIRE LOOP-A WAS FAILING TO TEST. MAINTENANCE CONTROL DEFERRED THE APU FIRE DETECTION SYSTEM WITH THE CREW WITH 26-12-01, CODE-C.

Part: POWER SUPPLY — FAILED (EMERGENCY LIGHT) · airframe 678 hrs · 623 cycles

AIRCRAFT N209PS WAS A SPARE AIRCRAFT IN DAY. THE NR 1 EMERGENCY BATTERY POWER SUPPLY WAS FOUND TO BE BAD. MAINTENANCE INSPECTED AND REPLACED THE NR 1 EMERGENCY BATTERY POWER SUPPLY IN ACCORDANCE WITH BOMBARDIER MAINTENANCE MANUAL 24-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: OUTFLOW VALVE — FAILED (CABIN PRESSURE) · airframe 323 hrs · 301 cycles

DURING CLIMB, CREW COULD NOT PRESURIZE AIRCRAFT. AIRCRAFT RETURNED TO PIT. MAINTENANCE INSPECTED AND REPLACED THE PRIMARY OUTFLOW VALVE IN ACCORDANCE WITH BOMBARDIER MAINTENANCE MANUAL 21-00-00. OPERATIONAL CHECKS WERE PERFORMED AND AIRCRAFT WAS RELEASED FOR SERVICE.

Part: CONTROLLER — MALFUNCTIONED (CABIN PRESSURE) · airframe 316 hrs · 295 cycles

DURING CLIMB, CREW COULD NOT PRESSURIZE AIRCRAFT. AIRCRAFT RETURNED TO YOW. MAINTENANCE DEFERRED BOTH AUTO CABIN PRESSURE CONTROLLERS 21-31-1 CODE C.

Part: WARNING LIGHT — ILLUMINATED (EMERGENCY EXIT) · airframe 81 hrs · 73 cycles

THE CREW RECEIVED A RIGHT HAND OVERWING EMERGENCY EXIT INDICATION. MAINTENANCE THEN DEFERRED THE RIGHT HAND OVERWING EMERGENCY EXIT INDICATION IN ACCORDANCE WITH 52-70-3C.