N244PS

Part: SUPPORT BRACKET — BROKEN (PYLON) · airframe 34,226 hrs · 341,264 cycles

SUPPORT BRACKET AND CLIP FOR LH UPPER STANG FAIRING IS BROKEN ON PYLON TRACK. C/A: REMOVED AND REPLACED SUPPORT ASSY IAW CRJ200 SRM 51-42-06.

Part: CARGO TRACK — CORRODED (BS 559) · airframe 34,226 hrs · 341,264 cycles

AFT CARGO COMPARTMENT, SEAT TRACK @ LBL9, APPROX. F.S. 559.00+80 CORRODED. C/A: REMOVED AN REPLACED DAMAGED SEAT TRACK AT @FS559.00+80 LBL 9 NEW SEAT TRACK IAW CRJ 200 AMM 53-01-11-000-802.

Part: CARGO TRACK — CORRODED (BS 559) · airframe 34,226 hrs · 341,264 cycles

AFT CARGO COMPARTMENT, SEAT TRACK @ RBL9, APPROX. F.S.559.00+112 CORRODED. C/A: REMOVED SEAT TRACK AND INSTALLED NEW SEAT TRACK P/N: 601R38779-49 IAW CRJ200 AMM 53-01-11-000-802.

Part: CARGO TRACK — CORRODED (BS 559) · airframe 34,226 hrs · 341,264 cycles

AFT CARGO COMPARTMENT SEAT TRACK @ LBL9, APPROX. F.S. 559.00+112 CORRODED. C/A: REMOVED SEAT TRACK AND REPLACED SEAT TRACK, P/N 601R38779-S, IAW CRJ200 AMM 53-01-11-400-802

Part: SEAT TRACK — CORRODED (BS 559) · airframe 34,226 hrs · 341,264 cycles

SEAT RAIL AT LBL27, APPROX F.S. 559.00+80 CORRODED. C/A: REMOVED AND REPLACED DAMAGED SEAT TRACK AT F 559.00+80 LBL 27. INSTALLED NEW SEAT TRACK IAW CRJ 200 AMM 53-01-11-400-802.

Part: DOOR FRAME — CRACKED (RT OVERWING) · airframe 34,226 hrs · 341,264 cycles

R/H OVERWING DOOR CUTOUT HAS CRACKED/ MISSING STRUCTUAL FILLER FOR DOOR SEAL LANDING. C/A: REPAIRED RH OVERWING DOOR CUTOUT MISSING STRUCTURAL FILLER IAW SRM 51-12-00 P14 STEP 9.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 34,226 hrs · 341,264 cycles

SEAT TRACK ON RBL9 BETWEEN FS.559+16 TO FS.559+80 IS CORRODED. C/A: NSTALLED NEW SERVICEABLE SEAT TRACK ON RBL9 BETWEEN FS559.00+16 - FS559.00+80 IAW CRJ200 AMM 53-01-11-400-802.

Part: CARGO TRACK — CORRODED (BS 559) · airframe 34,226 hrs · 341,264 cycles

AFT CARGO COMPARTMENT, SEAT TRACK @ RBL9, APPROX. F.S. 559.00+80 CORRODED. C/A: REMOVED AN REPLACED DAMAGED SEAT TRACK AT @FS559.00+80 LBL 9 NEW SEAT TRACK IAW CRJ 200 AMM 53-01-11-000-802.

Part: ANGLE — CRACKED (BS 280 FLOORBEAM) · airframe 34,226 hrs · 341,264 cycles

FS.280 CROSSBEAM IS CORRODED BETWEEN LBL9 AND RBL9. FOUND 4EA FS280 CLIPS TO BE CRACKED BETWEEN LBL9 AND RBL9. C/A: FABRICATED 4 EA F.S. 280 CLIPS REFERENCING REO 601R-53-11-926 FOR MATERIAL SPEC IAW CRJ200 SRM 51-24-36-AND 51-40-11 REF. JOB:27912111 OP:134 FOR INSTALL.

Part: FITTING — CRACKED (WINDOW FRAME) · airframe 34,226 hrs · 341,264 cycles

WINDSHIELD CNTR POST R/H BOTTOM FITTING CRACKED FROM LOWER FASTENER HOLE TO EDGE OF FITTING. C/A:REMOVED UNSERVICEABLE CENTER POST IAW CRJ 200 SRM 51-42-21. RECEIVED NEW CENTER POST RH BOTOTM FITTING. LOCATED AND DRILLED CENTER POST RH BOTTOM FITTING PN IAW CRJ 200 SRM 51-40-11-00 AND INSTALLED FITTING IAW CRJ 200 SRM 51-42-21.

Part: CARGO TRACK — BROKEN (NOT REPORTED) · airframe 34,226 hrs · 341,264 cycles

AFT CARGO COMPARTMENT TWO SEAT TRACK FILLERS BROKEN. K.LONG 10/22/18. C/A: INSTALLED 3 EACH NEW SERVICEABLE SEAT TRACK FILLERS P/N:601R38731-7, 601R38731-17 AND 601R38731-19 IAW CRJ200 AMM 20-21-00-910-801.

Part: CASCADE — CRACKED (THRUST REVERSER) · airframe 34,226 hrs · 341,264 cycles

UPPER CENTER CASCADE CRACKED ON LH THRUST REVERSER ASSY MARKED WITH TAPE. C/A: REMOVED L/H TR UPPER CENTER CASCADE IAR CRJ200 AMM 78-33-01-000-801. INSTALLED L/H TR UPPER CENTER CASCADE IAW CRJ200 AMM 78-33-01-400-801.

Part: FRAME — CRACKED (BS 718) · airframe 34,226 hrs · 34,126 cycles

FS718 FRAME IS CRACKED AT STGR 11R. C/A: REMOVED FRAME AT R/H FS718 AND COMPLETED INSTALLATION OF FRAME AT FS718 IAW CRJ 200 SRM 51-42-06 AND 51-42-21.

Part: WINDSHIELD — FAILED (COCKPIT) · airframe 33,920 hrs · 33,884 cycles

THE CREW REPORTED THE FIRST OFFICER'S WINDSHIELD SHATTERED IN FLIGHT, AFTER THEY RECEIVED A WINDSHIELD HEAT CUATION MESSAGE. DECLARED AN EMERGENCY AND DIVERTED. THE AIRCRAFT LANDED WITHOUT INCIDENT.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 33,920 hrs · 33,884 cycles

SUPPLEMENTAL INFORMATION: MX REPLACED FO WINDSHIELD. REMOVED & REPLACED RH WINDSHIELD HEAT CONTROLLER. OPS CHECK GOOD. P/N 1659-1 S/N 4643

Part: WARNING MESSAGE — FALSE ACTIVATION (BLEED LEAK) · airframe 33,140 hrs · 33,098 cycles

DECLARED AN EMERGENCY ON APPROACH FOR A 14TH STAGE BLEED AIR WARNING. MAINTENANCE INSPECTED LOOPS AND NO DEFECTS WERE FOUND, OPS CHECKED GOOD. NO ABNORMAL INDICATIONS FOUND.

Part: OIL SYSTEM — FLUCTUATES (RT ENGINE) · airframe 31,290 hrs · 31,395 cycles

ON APPROACH, CREW DECLARED AN EMERGENCY DUE TO RT ENGINE OIL PRESSURE FLUCUATED AND JUST BEFORE TOUCHDOWN GOT A RT ENGINE OIL LOW PRESSURE WARNING MESSAGE.

Part: COVER — BROKEN (EMERGENCY LIGHT) · airframe 30,579 hrs · 30,655 cycles

ROW 1 EMERGENCY LIGHT COVER BROKEN. REPLACED THE TRACK COVER, STRAIGHTENED PINS ON FORWARD EMERGENCY TRACK LIGHTING CONNECTOR AND CONNECTED.

Part: WIRE HARNESS — DEFECTIVE (PAX DOOR) · airframe 30,539 hrs · 30,619 cycles

PASSENGER DOOR LATCH CAUTION MESSAGE DURING FLIGHT. REMOVED AND REPLACED THE PASSENGER DOOR WIRE HARNESS, OPS CHECKED GOOD.

Part: BULKHEAD WEB — CRACKED (BS 621) · airframe 30,185 hrs · 30,267 cycles

BS 621 PRESSURE BULKHEAD WEB IS CRACKED IN 4 PLACES. MAINTENANCE PERFORMED A MAJOR REPAIR.

Part: SENSOR — FAULTY (BLEED SYSTEM) · airframe 29,998 hrs · 30,094 cycles

RIGHT ENGINE 14TH STAGE BLEED WARNING MESSAGE. THE CREW DECLARED AN EMERGENCY, CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, REMOVED AND REPLACED THE RIGHT HAND PYLON SENSING ELEMENT AND PERFORMED CHECKS IAW THE AMM. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: ANTI-ICE VALVE — FAILED (RT NACELLE) · airframe 27,807 hrs · 27,867 cycles

CREW REPORTED RT COWL ANTI-ICE CAUTION MESSAGE. CREW RAN QRH, MESSAGE PERSISTED IN FLIGHT WITH COWL ANTI-ICE SELECTED OFF. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, R & R RT ENGINE COWL ANTI-ICE VALVE AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: PRESSURE SWITCH — FAILED (COWL ANTI-ICE SY) · airframe 27,806 hrs · 27,866 cycles

CREW REPORTED RT COWL ANTI-ICE CAUTION MESSAGE IN FLIGHT WITH ANTI-ICE SELECTED OFF. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, R & R RT COWL ANTI-ICE PRESSURE SWITCH AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: WARNING MESSAGE — FALSE ACTIVATION (APU OIL SYS) · airframe 27,803 hrs · 27,863 cycles

CREW REPORTED APU OIL PRESSURE CAS MESSAGE DURING CRUISE FLIGHT. CREW DIVERTED AND LANDED WITHOUT INCIDENT. MAINTENANCE VERIFIED APU OIL LEVEL AS FULL AND OIL PRESSURE SENSOR CONNECTOR. NO DEFECT FOUND. CHECKS PERFORMED BY MAINTENANCE IAW AMM. COULD NOT DUPLICATE MESSAGE. ACFT RELEASED FOR SERVICE.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHT) · airframe 26,101 hrs · 26,198 cycles

CREW REPORTED ROW 6-8 EMERGENCY LIGHTS AND EMERGENCY DOOR LIGHT INOPERATIVE. MAINTENANCE INSPECTED AND SECURED CONNECTOR AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: STRINGER — CRACKED (BS 379) · airframe 26,009 hrs · 26,105 cycles

STRINGER 3L FWD OF BS 379 HAS .500 INCH CRACK. REPAIRED THE STRINGER IAW SRM, 53-00-03, SPLICE REPAIR FIG 202, SHEET 1.

Part: SKIN — DENTED (LT SPOILER) · airframe 26,009 hrs · 26,105 cycles

LEFT INBD GROUND SPOILER, INBD LOWER CORNER DENTED 5" LONG AND 2" WIDE. REPAIRED IAW EO CL600-2B19-57-L02986.

Part: PUMP — FAILED (HYDRAULIC SYSTEM) · airframe 24,910 hrs · 24,989 cycles

CREW REPORTED, NR 1 HYD SYSTEM FAILED IN FLIGHT WITH NO PRESSURE AND NO FLUID LEVELS. CREW DIVERTED AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND PERFORMED REPAIR TO PRESSURE LINE FROM NR 1 ENGINE DRIVEN PUMP AFTER FINDING LINE CHAFED THROUGH AT CLAMPING POSITION. HYD SYS NR 1 EDP AND CASE DRAIN MANIFOLD ASSY FILTER ELEMENT WERE R & R DUE TO EXTENDED OPERATION WITHOUT FLUID. SEVERAL BLOCK CLAMPS ON NR 1 HYD SYS PLUMBING LINES WERE R & R FOR BEING WORN BEYOND SERVICEABLE LIMITS. MAINTENANCE SERVICED NR 1 HYD SYS AND PERFORMED CHECKS. ACFT RELEASED FOR SERVICE. ALL WORK ACCOMPLISHED BY MAINTENANCE IAW AMM.

Part: CONTROL UNIT — FAILED (STAB TRIM) · airframe 24,686 hrs · 24,756 cycles

CREW REPORTED STAB CHANNEL ONE INOPERATIVE MESSAGE DURING FLIGHT. ENGAGED SYSTEM AND BOTH STAB TRIM AND MACH TRIM WENT INOPERATIVE. CREW FOLLOWED QRH TO RE-ENGAGE SYSTEMS. STABILIZER CHANNEL, 1 INOPERATIVE MESSAGE OCCURRED AGAIN, FOLLOWED BY STAB TRIM AND MACH TRIM OFF AND THEN AUTOPILOT NOSE UP MESSAGE. CREW FOLLOWED QRH TO DISCONNECT AUTOPILOT. CREW ENGAGED ALL SYSTEMS EXCEPT STAB TRIM ONE, RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED, R & R HORIZONTAL STABILIZER MOTOR CONTROL UNIT (MCU) AND PERFORMED CHECKS IAW AMM. OPS CHECK FLIGHT (OCF) PERFORMED SATISFACTORILY. ACFT RELEASED FOR SERVICE.

Part: OIL SYSTEM — LOW PRESSURE (LT ENGINE) · airframe 23,087 hrs · 23,277 cycles

CREW REPORTED LT ENGINE OIL PRESSURE AMBER DURING TAKEOFF ABOVE 80 KTS AND FOR FIRST 3 MINUTES AFTER TAKEOFF. MAXIMUM PSI OBSERVED WAS 150 PSI. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MX INSPECTED, R & R LT ENGINE AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: SKIN — DAMAGED (RT WING) · airframe 22,953 hrs · 23,153 cycles

DURING SCHEDULED MX, THE RT LOWER WING PLANK CHAFE DAMAGE WAS FOUND. THE AREA WAS INSPECTED AND REPAIRED USING AMM. ACFT WAS RELEASED FOR SERVICE.

Part: SKIN — DAMAGED (LT WING) · airframe 22,953 hrs · 23,153 cycles

DURING SCHEDULED MX, THE LT LOWER WING PLANK CHAFE DAMAGE WAS FOUND. THE AREA WAS INSPECTED AND REPAIRED USING AMM. ACFT WAS RELEASED FOR SERVICE.

Part: CONTROL UNIT — FAILED (HORIZ STAB) · airframe 22,570 hrs · 22,802 cycles

CREW REPORTED STAB TRIM CAUTION MESSAGE AND RUNAWAY DURING CLIMB. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, REMOVED AND REPLACED HSTCU (HORIZONTAL STABILIZER TRIM CONTROL UNIT), CLEANED MACH TRIM SWITCH AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.

Part: RING — DAMAGED (NAV LIGHT) · airframe 21,753 hrs · 22,087 cycles

CREW REPORTED POSSIBLE LIGHTNING STRIKE IN FLIGHT AT 17,000 FEET. AIRCRAFT IN CLEAN CONFIGURATION. CREW LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE PERFORMED LIGHTNING STRIKE INSPECTION, REMOVED AND REPLACED LOWER TAIL NAV LIGHT LENS RING DUE TO MULTIPLE MINOR BURN MARKS AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 21,469 hrs · 21,849 cycles

CREW REPORTED GEN 2 AMBER CAS MESSAGE ON CLIMBOUT. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT USING FIM (FAULT ISOLATION MANUAL). MAINTENANCE FOUND IDG (INTEGRATED DRIVE GENERATOR) OIL LEVEL FULL, INSPECTED WIRING AND PERFORMED CHECKS OF RIGHT IDG USING AIRCRAFT MAINTENANCE MANUALS. NO FAULTS FOUND. AIRCRAFT RELEASED FOR SERVICE.

Part: DISPLAY — DIRTY (COCKPIT) · airframe 19,364 hrs · 19,935 cycles

CREW REPORTED CAPTAIN’S PFD DISPLAY TEMP MESSAGE AND FIRST OFFICER’S PFD AND MFD DISPLAY TEMP MESSAGES DURING FLIGHT. CREW DIVERTED AND LANDED WITHOUT INCIDENT. MAINTENANCE CLEANED AND INSPECTED FLIGHT DISPLAY DUCTS, PFD’S (PRIMARY FLIGHT DISPLAY) AND MFD (MULTIFUNCTION DISPLAY) AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT RELEASED FOR SERVICE.

Part: RADOME — DAMAGED (FUSELAGE) · airframe 19,329 hrs · 19,901 cycles

CREW REPORTED TOP STATIC WICK ON LEFT WINGLET MISSING, WITH SOME BURN DAMAGE VISIBLE. CREW ALSO REPORTED POSSIBLE LIGHTNING STRIKE DAMAGE TO TAIL CONE. MAINTENANCE PERFORMED LIGHTNING STRIKE INSPECTION, REMOVED AND REPLACED RADOME AND LEFT WINGLET TIP FAIRING AND INSTALLED NEW WINGLET LIGHTNING PROTECTION KIT ON LEFT WINGLET. MAINTENANCE REPAIRED DAMAGE TO TAIL CONE, REMOVED AND REPLACED TAIL CONE STATIC DISCHARGER AND PERFORMED CHECKS. ALL WORK ACCOMPLISHED BY MAINTENANCE USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 18,108 hrs · 18,733 cycles

DURING SCHEDULED MAINTENANCE THE FS 621 BULKHEAD WEB WAS FOUND CRACKED. THE FS 621.0 BULKHEAD WEB WAS INSPECTED AND REPAIRED USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 18,108 hrs · 18,733 cycles

DURING SCHEDULED MAINTENANCE THE FS 280.0 FLOOR TRAVERSE BEAM WAS FOUND CRACKED. THE FS 280.0 FLOOR TRAVERSE BEAM WAS INSPECTED AND REPAIRED USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: TRANSDUCER — MALFUNCTIONED (OIL SYSTEM) · airframe 18,020 hrs · 18,654 cycles

CREW REPORTED LEFT ENGINE LOW OIL PRESSURE 40 TO 22 PSI AT ALL POWER SETTINGS AFTER DEPARTURE FROM DAY. CREW RETURNED TO DAY AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND TROUBLESHOT AIRCRAFT, REMOVED AND REPLACED LEFT ENGINE OIL PRESSURE TRANSDUCER AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.

Part: SCAVENGE PUMP — MALFUNCTIONED (LT ENGINE) · airframe 17,999 hrs · 18,630 cycles

CREW REPORTED LEFT OIL PRESSURE DROPPED FROM 70 PSI TO 48 PSI ON TAKEOFF ROLL ON DEPARTURE FROM CLT. LEFT HAND OIL PRESSURE DROPPED TO 39 PSI AT 2,000 FEET. CREW RETURNED TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AIRCRAFT, REMOVED AND REPLACED LEFT ENGINE LUBE AND SCAVENGE PUMP AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.

Part: BPSU — FAILED (TE FLAP) · airframe 17,884 hrs · 18,519 cycles

CREW REPORTED FLAPS FAIL AMBER CAS MESSAGE IN FLIGHT EN ROUTE FROM CAK TO CLT. CREW DIVERTED TO GSO AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT FLAP SYSTEM, REMOVED AND REPLACED LEFT BPSU (BRAKE AND POSITION SENSOR UNIT) AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.

Part: ECU — FAILED (TE FLAP) · airframe 17,872 hrs · 18,507 cycles

CREW REPORTED FLAPS FAIL CAUTION MESSAGE AT ZERO DEGREES ON DESCENT INTO SDF. AIRCRAFT LANDED IN SDF 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: BPSU — FAILED (TE FLAP) · airframe 17,816 hrs · 18,453 cycles

CREW REPORTED FLAPS FAIL CAUTION MESSAGE IN FLIGHT ON DESCENT INTO CLT. CREW COMPLETED QRH AND AIRCRAFT LANDED IN CLT WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT FLAP SYSTEM, REMOVED AND REPLACED RIGHT BPSU (BRAKE AND POSITION SENSOR UNIT) AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.

Part: BPSU — FAILED (TE FLAP) · airframe 17,811 hrs · 18,447 cycles

CREW REPORTED FLAPS FAIL CAS MESSAGE IN FLIGHT ON RETRACTION UPON DEPARTURE FROM FAY EN ROUTE TO CLT. FLAPS FAILED AT ZERO DEGREES. AIRCRAFT LANDED IN CLT WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT FLAP SYSTEM, REMOVED AND REPLACED RIGHT FLAP BPSU (BRAKE AND POSITION SENSOR UNIT) AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.

Part: CONTROL UNIT — FAILED (TE FLAP) · airframe 17,747 hrs · 18,388 cycles

CREW REPORTED FLAPS FAIL CAS MESSAGE UPON SELECTING FLAPS EIGHT (8) DEGREES DURING APPROACH TO HSV. FLAPS EXTENDED TO EIGHT (8) DEGREES, THEN FAILED. AIRCRAFT LANDED IN HSV 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: ELEVATOR — DAMAGED (LEFT) · airframe 17,187 hrs · 17,845 cycles

CREW REPORTED HYD 2 AMBER MESSAGE. CREW ELECTED TO DIVERT TO RDU. DURING THE DIVERSION A LIGHTNING STRIKE WAS REPORTED. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND A HOLE IN THE HYDRAULIC RETURN LINE. LINE WAS REPAIRED. DAMAGE WAS FOUND TO THE LT ELEVATOR AND WAS REPLACED. INSPECTIONS AND REPAIRS WERE ACCOMPLISHED USING THE AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: STRUCTURE — DAMAGED (FUSLEAGE) · airframe 16,870 hrs · 17,546 cycles

WHILE DIVERTING DUE TO WEATHER, CREW REPORTED LIGHTNING STRIKE ON RT SIDE OF ACFT. CREW LANDED WITHOUT INCIDENT. MX INSPECTED ACFT, R & R GROUND SCREW ON TAIL CONE, REPLACED STATIC WICK ON LT HORIZ STAB TIP FAIRING, APPLIED TOPCOAT TO SEVERAL LOCATIONS ON RT FUSELAGE AND PERFORMED CHECKS USING ACFT MM AND REO. ACFT RELEASED FOR SERVICE.

Part: RADOME — DAMAGED (FUSELAGE) · airframe 16,738 hrs · 17,422 cycles

AT CLT, CREW REPORTED LIGHTNING STRIKE. MAINTENANCE INSPECTED AIRCRAFT AND REMOVED AND REPLACED RADOME, LOWER VHF ANTENNA, RIGHT LANDING LIGHT, FCC NR 1 (FLIGHT CONTROL COMPUTER), LOWER TAIL NAV LIGHT LENS AND RING, AFT DRAIN MAST, RIGHT STROBE POWER SUPPLY AND STATIC DISCHARGERS. MAINTENANCE REPAIRED BURN MARKS ON RIGHT NOSE GEAR DOOR. CHECKS WERE PERFORMED. ALL WORK WAS ACCOMPLISHED USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: PROXIMITY SENSOR — ICED (NLG) · airframe 16,257 hrs · 16,966 cycles

CREW REPORTED AFTER LANDING GEAR HANDLE SELECTED TO THE UP POSITION, RECEIVED A GEAR DISAGREE CAS MESSAGE. AIRCRAFT RETURNED TO DAY LANDING WITHOUT INCIDENT. MAINTENANCE FOUND ICE ON THE NOSE GEAR PROXIMITY SENSOR. THE ICE WAS REMOVED AND USING THE AIRCRAFT MAINTENANCE MANUAL, INSPECTIONS AND CHECKS WERE PERFORMED. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: UNKNOWN — MALFUNCTIONED (AUTOPILOT SYS) · airframe 14,736 hrs · 15,440 cycles

CREW REPORTED AFTER ENGAGING AUTOPILOT THE AIRCRAFT ROLLS TO RIGHT. AIRCRAFT RETURNED TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE CHECKED THE AUTOPILOT AND AILERON CONTROL SYSTEMS USING AIRCRAFT MAINTENANCE MANUAL. NO DEFECTS WERE NOTED AND AIRCRAFT WAS RELEASED FOR SERVICE.

Part: TIRE — BLOWN (LT MLG) · airframe 14,574 hrs · 15,281 cycles

CREW REPORTED A LOUD BANG ON ROTATION, ALONG WITH WEIGHT-ON-WHEELS (WOW) INPUT AND ANTI-SKID INBOARD MESSAGES, DURING TAKEOFF FROM CLT. AIRCRAFT RETURNED TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE LEFT INBOARD MAIN LANDING GEAR (MLG) TIRE BLOWN AND ASSOCIATED DAMAGE. MAINTENANCE REMOVED AND REPLACED THE LEFT INBOARD AND LEFT OUTBOARD MLG WHEEL ASSEMBLIES, THE LEFT INBOARD FLAP AND THE LEFT INBOARD MLG HARNESS. THE LEFT FLAP STUB FAIRING WAS REPAIRED AND HYDRAULIC LINES WERE REPAIRED / REPLACED. CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. ALL WORK WAS ACCOMPLISHED USING THE AIRCRAFT MAINTENANCE MANUALS.

Part: SELECTOR VALVE — MALFUNCTIONED (MLG) · airframe 14,528 hrs · 15,235 cycles

CREW REPORTED ANTI-SKID OUTBOARD AND GEAR DISAGREE MESSAGE ILLUMINATED RIGHT AFTER TAKEOFF FROM CLT. AIRCRAFT RETURNED TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT THE AIRCRAFT, REMOVED AND REPLACED THE MAIN LANDING GEAR SELECTOR VALVE, AND PERFORMED CHECKS USING THE AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: ACTUATOR — LEAKING (NLG) · airframe 14,528 hrs · 15,235 cycles

CREW REPORTED AN ANTI-SKID INBOARD AMBER MESSAGE, THEN A GEAR DISAGREE RED MESSAGE AFTER TAKEOFF FROM CLT. AIRCRAFT RETURNED TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT AND INSPECTED THE AIRCRAFT, REMOVED AND REPLACED THE NOSE LANDING GEAR DOOR ACTUATOR AND PERFORMED CHECKS USING THE AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: SWITCH — MALFUNCTIONED (ANTI-ICE SYS) · airframe 14,300 hrs · 14,994 cycles

CREW REPORTED A WING OVERHEAT RED WARNING MESSAGE AFTER TAKEOFF FROM DAY. AIRCRAFT RETURNED TO DAY AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT THE AIRCRAFT, REMOVED AND REPLACED THE RIGHT WING BACK-UP OVERHEAT SWITCH AND PERFORMED CHECKS USING THE AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 14,214 hrs · 14,898 cycles

DURING SCHEDULED MAINTENANCE A CRACK WAS FOUND ON THE PRESSURE BULKHEAD RT WEB AT FS 559.00. REPAIRS WERE DONE PER MAINTENANCE MANUALS AND AIRCRAFT RELEASED FOR SERVICE.

Part: ENGINE — FAILED (LEFT) · airframe 14,143 hrs · 14,814 cycles

CREW REPORTED A LEFT ENGINE FAILURE ON CLIMBOUT FROM CLT. AIRCRAFT RETURNED TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT AND REMOVED AND REPLACED THE LEFT ENGINE. MAINTENANCE ALSO REMOVED AND REPLACED DAMAGED CORE COWLS AND TRANSLATING COWLS. CHECKS WERE PERFORMED AND AIRCRAFT WAS RELEASED FOR SERVICE. ALL WORK WAS ACCOMPLISHED USING AIRCRAFT MAINTENANCE MANUALS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 13,993 hrs · 14,657 cycles

AT AVL, CREW REPORTED ROW 2 FLOOR EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE TROUBLESHOT, REMOVED AND REPLACED THE FLOOR-TRACK EMERGENCY LIGHT STRIP AND PERFORMED CHECKS USING THE AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: SENSING ELEMENT — DEFECTIVE (LT ENGINE) · airframe 13,952 hrs · 14,601 cycles

CREW REPORTED A LEFT TENTH STAGE DUCT RED MESSAGE IN FLIGHT EN ROUTE FROM HSV TO CLT. AIRCRAFT DIVERTED TO TYS AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT THE AIRCRAFT AND REMOVED AND REPLACED TWO (2) HEAT SENSING ELEMENTS IN THE LT TENTH STAGE DUCT LOOPS USING THE AIRCRAFT MAINTENANCE MANUAL. CHECKS WERE PERFORMED USING THE AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: NOZZLE — DAMAGED (ENGINE) · airframe 12,851 hrs · 13,425 cycles

CREW REPORTED A LIGHTNING STRIKE INSPECTION IN MOB. MAINTENANCE INSPECTED AIRCRAFT PER THE AIRCRAFT MAINTENANCE MANUAL. MAINTENANCE REMOVED AND REPLACED NOZZLE ASSY EXHAUST, TAILPIPE FAIRING ASSEMBLY AND STATIC WICKS. CHECKS WERE COMPLETED PER AIRCRAFT MAINTENANCE MANUAL AND AIRCRAFT RELEASED FOR SERVICE.

Part: LIGHT — DAMAGED (AFT POSITION) · airframe 12,818 hrs · 13,395 cycles

CREW REPORTED A LIGHTNING STRIKE AT 15,000 EN ROUTE BNA. MAINTENANCE INSPECTED, REMOVED AND REPLACED AFT POSITION LIGHT. ALSO, RIVETS AND STATIC WICKS WERE REPAIRED AND REPLACED. ALL WORK WAS ACCOMPLISHED PER THE AIRCRAFT MANUAL. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: WINDSHIELD — DELAMINATED (COCKPIT) · airframe 12,400 hrs · 12,958 cycles

CREW REPORTED POSSIBLE CAPTAINS WINDSHIELD DELAMINATION AND DIVERTED INTO TRI LANDING WITHOUT INCIDENT. MAINTENANCE INSPECTED PER THE AIRCRAFT MAINTENANCE MANUAL AND FOUND DELAMINATION AND WINDSHIELD WITHIN LIMITS. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: HANDLE — FAILED (COCKPIT) · airframe 10,511 hrs · 10,909 cycles

CREW REPORTED LANDING GEAR WOULD NOT RETRACT AFTER TAKE OFF. ANTI-SKID INBD AMBER AND PARKING BRAKE SOV AMBER MSG DISPLAYED. AFTER 3 MINUTES, MSG WENT AWAY AND LANDING GEAR RETRACTED. THE ACFT LANDED IN CLT WITHOUT INCIDENT. MX INSPECTED THE ACFT, PERFORMED ANTI-SKID TESTS AND R&R THE LANDING GEAR HANDLE ASSEMBLY. NO OTHER DEFECTS WERE NOTED. THE ACFT WAS RELEASED FOR SERVICE.

Part: LOCK — DIRTY (THRUST REVERSER) · airframe 8,919 hrs · 9,213 cycles

CREW REPORTED A LEFT HAND THRUST REVERSER UNLOCKED CAS MESSAGE AFTER TAKEOFF. CREW FOLLOWED THE QRH AND RETURNED TO CAK WITHOUT INCIDENT. MAINTENANCE INSPECTED AND CLEANED THE FLEX SHAFT LOCK UNIT. MAINTENANCE OPS CHECKED THE LEFT HAND THRUST REVERSER IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: SKIN — DAMAGED (LT WING) · airframe 8,622 hrs · 8,890 cycles

CREW REPORTED WHILE LANDING IN CLT, THE LEFT WING STRUCK THE RUNWAY UPON TOUCHDOWN. THE AIRCRAFT TAXIED SAFELY TO THE GATE WHERE MAINTENANCE INSPECTED AND FOUND DAMAGE TO THE LEFT HAND WINGTIP AND LEFT HAND OUTBOARD FLAP. MAINTENANCE COMPLIED WITH AN EDDY CURRENT INSPECTION FOR THE DAMAGE. MAINTENANCE REPAIRED ALL DAMAGE PER REO 601R-57-00-055. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: ECU — FAILED (T/E FLAP) · airframe 7,964 hrs · 8,175 cycles

CREW REPORTED A FLAPS FAIL AT 20 DEGREES. CREW DIVERTED TO ILM AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND THE FLAP ELECTRONIC CONTROL UNIT TO BE CAUSING ERRATIC MESSAGES. MAINTENANCE REMOVED AND REPLACED THE FECU IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: SWITCH — FAILED (PITCH TRIM) · airframe 7,201 hrs · 7,358 cycles

CREW REPORTED A STAB TRIM AND MACH TRIM CAUTION MESSAGE ON TAKEOFF ROLL. CREW ABORTED TAKEOFF AND RETURNED TO THE GATE WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE PITCH TRIM DISCONNECT SWITCH IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL 27-41-30-000(400)-801. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: PSEU — FAILED (PAX DOOR) · airframe 6,880 hrs · 7,024 cycles

CREW REPORTED A PAX DOOR/SERVICE DOOR CAUTION MESSAGE IN FLIGHT. CREW DIVERTED TO TYS AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE PROX SENSOR ELECTRONIC UNIT IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: CONTROL UNIT — FAILED (LT BLEED SYS) · airframe 6,119 hrs · 6,211 cycles

CREW REPORTED AN ANTI-ICE DUCT MESSAGE ON TAKEOFF ROLL. CREW ABORTED TAKEOFF AND RETURNED TO GATE WITHOUT INCIDENT. MAINTENANCE INSPECTED AND REMOVED AND REPLACED THE LT BLEED CONTROL UNIT. MAINTENANCE PERFORMED OPERATIONAL CHECKS AND OPS CHECKED GOOD. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: PROXIMITY SENSOR — INTERMITTENT (PAX DOOR) · airframe 5,120 hrs · 5,152 cycles

ON CLIMBOUT (3000') CREW REPORTED PASSENGER DOOR EMERGENCY ANNUNCIATION (EICAS) MASTER WARNING AND AURAL FOLLOWED BY AMBER PAX DOOR OUT HANDLE THEN INTERMITTENT -PASSENGER DOOR-. AIRCRAFT RETURNED TO DCA WITHOUT INCIDENT. INSPECTION OF PAX DOOR, PSEU BOX AND SWITCH COMPLETED, ALL CHECKED GOOD. REMOVED AND REPLACED PROX SENSOR. OPERATIONAL CHECK GOOD. AIRCRAFT WAS RELEASED AND RETURNED TO SERVICE.

Part: STRUCTURE — UNDAMAGED · airframe 5,106 hrs · 5,138 cycles

CREW REPORTED ON APPROACH TO CLT POSSIBLE BIRD STRIKE IN LT NOSE AREA. MAINTENANCE INSPECTED AIRCRAFT AND NO DAMAGE WAS FOUND. AIRCRAFT WAS RETURNED TO SERVICE.

Part: STRUCTURE — LIGHTNING STRIKE (LT WING) · airframe 4,659 hrs · 4,664 cycles

THE CREW REPORTED A POSSIBLE LIGHTNING STRIKE DURING CLIMBOUT FROM TYS. THE FLIGHT LANDED IN CLT WITHOUT INCIDENT. MAINTENANCE PERFORMED EN ROUTE AND DETAILED LIGHTNING STRIKE INSPECTIONS. MINOR DAMAGE WAS FOUND ON THE LEFT WINGLET, RIGHT ELEVATOR, AND RIGHT SIDE OF THE RUDDER. ALL DAMAGE WAS REPAIRED AND THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: CARBON SEAL — LEAKING (LT ENGINE) · airframe 3,971 hrs · 3,963 cycles

THE CREW REPORTED A LT ENG OIL PRESS WARNING WITH PRESSURE FLUCTUATING BETWEEN 23-31 PSI. THE FLIGHT RETURNED TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED & REPLACED THE NR 1 ENGINE IDG CARBON SEAL. OIL PRESSURE, LEAK, AND CONSUMPTION CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: CARBON SEAL — LEAKING (NR 1 ENGINE) · airframe 3,926 hrs · 3,818 cycles

AFTER LANDING, THE CREW REPORTED THAT THE NR 1 ENGINE OIL PRESSURE DROPPED ON FINAL APPROACH TO 17 PSI WITH N1 AT 67 PERCENT. MAINTENANCE REMOVED AND REPLACED THE NR 1 ENGINE AGB/IDG CARBON SEAL. OIL LEAK AND CONSUMPTION CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: SKIN — GROUND DAMAGE (RT WING) · airframe 3,719 hrs · 3,731 cycles

THE RIGHT WINGLET SUSTAINED LEADING EDGE DAMAGE AFTER HITTING A BAGGAGE CART WHILE AIRCRAFT WAS BEING MARSHALLED INTO THE GATE. MAINTENANCE REMOVED & REPLACED THE RIGHT WINGLET LEADING EDGE ASSEMBLY. NO FURTHER DAMAGE WAS FOUND. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: BOLT — FAILED (EXHAUST NOZZLE) · airframe 3,440 hrs · 3,447 cycles

AFTER POST FLIGHT INSPECTION THE CREW REPORTED THE LEFT ENGINE EXHAUST NOZZLE AND FAIRING WERE MISSING. MAINTENANCE INSPECTED THE AIRCRAFT AND DETERMINED ALL 31 ATTACH BOLTS HAD FAILED AND WERE ALSO MISSING. ALL MISSING AND DAMAGED PARTS WERE REPLACED WITH SERVICEABLE PARTS IAW BOMBARDIER AND GENERAL ELECTRIC MAINTENANCE MANUALS. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: FCU — FAILED (TE FLAPS) · airframe 3,190 hrs · 3,226 cycles

AFTER TAKEOFF FROM DCA WITH FLAPS AT 20 DEGREES THE FLAPS FAIL CAUTION MESSAGE ILLUMINATED. THE CREW FOLLOWED THE QRH AND DIVERTED TO PHL, LANDING SAFELY. MAINTENANCE REMOVED AND REPLACED THE FLAP ELECTRONIC CONTROL UNIT IAW CRJ200 AMM 27-51-05-000(400)-801. OPERATIONAL TEST OF FLAP SYSTEM WAS GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: FCU — MALFUNCTIONED (TE FLAPS) · airframe 3,170 hrs · 3,206 cycles

WITH FLAPS AT 45 DEGREES ON APPROACH THE FLAPS FAIL CAUTION MESSAGE ILLUMINATED. THE CREW MADE A NORMAL LANDING. MAINTENANCE RESET THE FECU IAW CRJ200 SL-00-001. OPERATIONAL CHECKS WERE PERFORMED 5 TIMES AND WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: FCU — MALFUNCTIONED (TE FLAPS) · airframe 3,167 hrs · 3,202 cycles

WITH FLAPS AT 20 DEGREES ON APPROACH THE FLAPS FAIL CAUTION MESSAGE ILLUMINATED. THE CREW FOLLOWED THE QRH AND MADE A FLAPS 20 DEGREES LANDING. MAINTENANCE RESET THE FECU IAW CRJ200 SL-00-001. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: FCU — MALFUNCTIONED (TE FLAPS) · airframe 3,158 hrs · 3,192 cycles

WITH FLAPS AT 45 DEGRESS ON FINAL APPROACH THE FLAPS FAIL CAUTION MESSAGE ILLUMINATED. THE CREW REPORTED NO ASYMMETRY AND MADE A NORMAL LANDING. MAINTENANCE RESET THE FECU IAW CRJ200 SL-00-001. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: FCU — MALFUNCTIONED (TE FLAPS) · airframe 3,103 hrs · 3,137 cycles

DURING APPROACH WITH FLAPS 30 DEGREES THE FLAPS HALFSPEED STATUS MESSAGE ILLUMINATED. AT FLAPS 45DEGREES THE FLAPS FAIL MESSAGE ILLUMINATED. THE CREW FOLLOWED THE QRH AND LANDED SAFELY. MAINTENANCE RESET THE FECU IAW CRJ200 SL-00-001. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: DETECTOR — FAILED (TE FLAPS) · airframe 3,084 hrs · 3,121 cycles

ON FINAL APPROACH THE CREW REPORTED A FLAPS FAIL MESSAGE AT 45 DEGREES. MAINTENANCE DETERMINED THAT THE SKEW DETECTION UNIT WAS INOPERATIVE. THE SKEW DETECTION SYSTEM WAS DEFERRED IAW CRJ200 MEL 27-51-03(C). THE AIRCRAFT WAS RELEASED FOR SERVICE. CAK MAINTENANCE INSTALLED A SERVICEABLE SKEW DETECTION UNIT ON 08/30/05 IAW CRJ200 AMM 27-51-15-400-801. OPERATIONAL CHECKS WERE GOOD. THE MEL WAS CLEARED AND THE AIRCRAFT WAS AGAIN RELEASED FOR SERVICE.

Part: SWITCH — STUCK (SEAT 11 D-F) · airframe 2,647 hrs · 2,662 cycles

DURING CLIMB THE FLIGHT ATTENDANT CALL SWITCH AT SEATS 11D/F BECAME STUCK IN THE ON POSITION CAUSING THE AURAL CHIME TO SOUND CONTINUOUSLY IN THE CABIN. WHEN THE FLIGHT ATTENDANT TRIED TO UNSTICK THE SWITCH THE OXYGEN MASKS ABOVE 11D/F DEPLOYED. THE CREW RETURNED TO CLT. MAINTENANCE STOWED THE OXYGEN MASKS AND DEFERRED THE PSU AT SEAT 11D/F PER MEL 25-70-01-4 CAT D. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE.

Part: WARNING LIGHT — FALSE ACTIVATION (CARGO DOOR) · airframe 955 hrs · 974 cycles

DURING CRUISE THE CREW REPORTED A CARGO DOOR CAS MESSAGE. MAINTENANCE CONTROL DEFERRED THE CARGO DOOR INDICATION SYSTEM WITH THE CREW PER MEL 52-70-04 CODE-C.