N591ML

Part: UPLOCK — MISRIGGED (RT MLG) · airframe 20,647 hrs · 19,021 cycles

ACFT RETURNED TO BASE AFTER THE CREW RECIEVED A RT MLG DISAGREE ON RETRACTION WHILE DEPARTING. THE CREW FOLLOWED THE EMERGENCY PROCEDURE IN THE QRH AND CONDUCTED AN ALTERNATE EXTENSION. SUBSEQUENTLY, THE GEAR EXTENDED, INDICATED DOWN AND LOCKED, AND A NORMAL LANDING WAS PERFORMED. UPON INSPECTION, FOUND THE SENSOR/ TARGET GAP WAS SLIGHTLY OUT OF TOLERANCE AND THE TARGET PLATE HAD MINOR FREE PLAY. THE SNAG COULD BE INTERMITTENTLY DUPLICATED IN THE HANGAR. THE TARGET PLATE WAS ADJUSTED IAW THE CMM AND THE PROXIMITY SWITCH WAS ADJUSTED IAW THE ACFT AMM. FUNCTIONAL TESTS WERE DEFECT FREE. MFG HAS ISSUED AOM 1362B DATED 7-NOV-2012 THAT ADDRESSES THIS AS A FLEET ISSUE. AN AOM IS NOT REGULTORY MATERIAL AND DOES NOT MANDATE COMPLIANCE.

Part: A/C PACK — FAILED (LEFT) · airframe 20,266 hrs · 18,863 cycles

ACFT EXPERIENCED A LT ACM FAILURE ON SHORT FINAL. CREW REPORTED A STRONG BURNED OIL ODOR OR VAPOR ENTERING THE COCKPIT THROUGH THE ECS SYSTEM. BOTH PACKS WERE TURNED OFF AND THE ODOR DISSIPATED. MX CONFIRMED THAT THE LT PACK HAD LOST OIL QUANTITY AND FAILED. NO OTHER DAMAGE WAS NOTED.

Part: SKIN — CRACKED (ZONE 100) · airframe 19,928 hrs · 18,738 cycles

A 1 INCH PRESSURE SKIN CRACK WAS FOUND BETWEEN THE LOWER BEACON AND THE NR 2 VHF ANTENNA. LOCATED AT FS 409+32, STR 26L TO STR 26R. REPAIRED WITH REO 601R-53-31-759.

Part: HOUSING — ARCED (GALLEY LIGHTS) · airframe 18,605 hrs · 18,207 cycles

DURING DESCENT, THE F/A REPORTED A FAINT SMOKE OR ELECTRICAL ORDER AND FLICKERING LIGHTS IN THE GALLEY AREA. INSPECTED ON GROUND FOUND SIGNIFICANT DAMAGE TO A LIGHT ASSY DUE TO ELECTRICAL ARCING. NO RECENT MAINTENANCE HAS BEEN PREFORMED ON THE LIGHT ASSY. DAMAGE WAS CONTAINED TO THE LIGHT ASSY ITSELF.

Part: O-RING — FAILED (IDG) · airframe 18,353 hrs · 18,102 cycles

ON APPROACH, THE CREW RECIEVED A "IDG 2" CAS MESSAGE. THE CREW LANDED WITHOUT INCIDENT. I NSP OF THE GENERATOR FOUND THAT THE FILTER DELTA P INDICATOR O-RING HAD FAILED RESULTING IN TOTAL FLUID LOSS. OPS WERE CONTINUED IAW MEL.

Part: O-RING — FAILED (IDG) · airframe 18,422 hrs · 18,131 cycles

DURING AN UNRELATED MX GROUND RUN, THE NR1 IDG OVERHEATED, A BOLT AND A O-RING ON THE GENRERATOR MODULE FAILED, AND THE LUBRICATING OIL SPRAYED UNDER HIGH PRESSURE ONTO THE CORE OF AN OPERATING ENGINE. THE ENGINE WAS IMMEDIATELY SHUTDOWN. THERE WAS A LARGE SMOKE CLOUD BUT NO FIRE NOTED VISUALLY OR BY INDICATION.

Part: LIFE VEST — MISSING (CABIN) · airframe 18,218 hrs · 17,849 cycles

TWO (2) INFANT LIFE VESTS MISSING. MX REPLACED BOTH VESTS.

Part: LIFE VEST — MISSING (CABIN) · airframe 18,124 hrs · 17,637 cycles

TWO LIFE VESTS MISSING. MX REPLACED THE VESTS.

Part: LIFE VEST — MISSING (CABIN) · airframe 18,046 hrs · 17,468 cycles

LIFE MISSING FROM 11D. REPLACED THE LIFE VEST.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,946 hrs · 17,240 cycles

FLOOR EMERGENCY LIGHTING ROW 1 TO 5 INOP. REPLACED LIGHT STRIP, OP GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,939 hrs · 17,224 cycles

FLOOR EMERGENCY LIGHTING ROW 1 TO 5 INOP. REPLACED LIGHT STRIP, OPS GOOD.

Part: LIFE VEST — MISSING (CABIN) · airframe 17,900 hrs · 17,139 cycles

ONE INFANT LIFE VEST MISSING. MX INSTALLED LIFE VEST.

Part: LIFE VEST — MISSING (CABIN) · airframe 17,829 hrs · 16,977 cycles

INFANT LIFE VEST MISSING. REPLACED VEST.

Part: LIFE VEST — MISSING (CABIN) · airframe 17,819 hrs · 16,954 cycles

TWO LIFE VESTS MISSING AT ROW 8 AC. R2 LIFE VESTS.

Part: STALL WARNING — MALFUNCTIONED (COCKPIT) · airframe 17,696 hrs · 16,687 cycles

MIS RTG STALL FAIL CAUTION ON T/O 90KT. RESET STALL PROTECTION SYSTEM.

Part: SMOKE DETECTOR — MALFUNCTIONED (CARGO BAY) · airframe 17,676 hrs · 16,642 cycles

ERRONEOUS CARGO SMOKE INDICATION DURING BAGGAGE UPLOAD. MX REPLACED THE AFT SMOKE DETECTOR.

Part: STALL WARNING — FALSE ACTIVATION (COCKPIT) · airframe 17,509 hrs · 16,280 cycles

ABORTED TAKEOFF FOR STALL FAIL CAUTION DURING HIGH WIND GUSTS. WIND GUSTS WERE DETERMINED TO BE THE CAUSE OF THE STALL FAIL INDICATION. STALL SYSTEM TEST OPS NORMAL, NO FURTHER ACTION IS REQUIRED.

Part: LIFE VEST — MISSING (CABIN) · airframe 17,233 hrs · 15,672 cycles

ASH FLT 1007 HNL-KOA. CREW REPORTED AN INFANT LIFE VEST WAS MISSING. MX INSTALLED A NEW LIFE VEST.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 14,401 hrs · 12,964 cycles

PERMANENT REPAIR TO FUSELAGE SKIN FS 349.00 TO 364.00 STR 13 TO 15 RIGHT HAND SIDE.

Part: SUPPORT BEAM — CRACKED (ENGINE) · airframe 14,396 hrs · 12,960 cycles

REPAIRED ENGINE SUPPORT BEAM, UPPER WEB WAS CRACKED.

Part: HANDLE — LACK OF LUBE (SERVICE DOOR) · airframe 14,366 hrs · 12,939 cycles

ASH 7171 ORD SERVICE DOOR OUTER HANDLE HARD TO CLOSE. MX CLEANED AND LUBED OUTER HANDLE.

Part: ENGINE — SMOKE (NR 1) · airframe 13,888 hrs · 12,440 cycles

ASH FLT 7223, TUC - CREW WAS MADE AWARE OF WHITE SMOKE COMING FROM NR 1 ENGINE DURING TAXI AFTER ENGINE WAS S/D. MX TROUBLESHOT AND FOUND OPS NORMAL.

Part: DOOR — LACK OF LUBE (PAX DOOR) · airframe 13,729 hrs · 12,276 cycles

ASH FLT 7275 CAE-OVERNIGHT. FLIGHT DECK DOOR STICKING DURING OPENING AND CLOSING. MX LUBED AND ADJUSTED THE DOOR, OP CHECK GOOD.

Part: WIRE — DAMAGED (EMERGENCY LIGHTS) · airframe 13,624 hrs · 12,173 cycles

PAX DOOR EMERGENCY EXIT LIGHT INOP. REPAIRED BROKEN WIRE ON LIGHT.

Part: UNKNOWN — UNKNOWN (NLG STEERING) · airframe 13,409 hrs · 11,963 cycles

ASH 7284 ORD-SBN. DECLARED AN EMERGENCY DUE TO A NOSE WHEEL STEERING FAULT IN FLIGHT. MX INSPECTED THE NOSE WHEEL STEERING SYSTEM AND WERE UNABLE TO DUPLICATE THE FAULT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 12,430 hrs · 11,009 cycles

ASH 7285 PWM. LT FWD OVERWING EXTERIOR EMERGENCY LIGHT INOP. MX RELAMPED EMERGENCY LIGHT.

Part: CONNECTOR — DIRTY (SMOKE DETECTOR) · airframe 12,180 hrs · 10,763 cycles

ASH 7178 CLT - CREW REPORTED A LAV SMOKE CTN MSG. MX CLEANED SMOKE DETECTOR CONNECTIONS. OPS CHECKED NORMAL

Part: WARNING MESSAGE — ILLUMINATED · airframe 12,073 hrs · 10,654 cycles

ASH 7309 ORD - CREW REPORTED STALL FAIL FOLLOWED BY A TAKEOFF CONFIG WARNING ON TAKEOFF ROLL. MX CURRENTLY TROUBLESHOOTING.

Part: STALL WARNING — MALFUNCTIONED (COCKPIT) · airframe 11,929 hrs · 10,508 cycles

ASH 7300 ORD. PILOT ABORTED TAKEOFF DUE TO A STALL FAIL CTN. MX RESET SYSTEM.

Part: COALESCER BAG — UNKNOWN (A/C BAY) · airframe 11,965 hrs · 10,447 cycles

ASH 7323 LGA. RIGHTT PACK HIGH PRESSURE CAUTION, LT PACK WAS ALREADY DEFERRED. MX REPLACED COALESCER BAGS.

Part: MECHANISM — OUT OF ADJUST (FA SEAT) · airframe 11,416 hrs · 9,997 cycles

ASH 7156 GSP - "RTG" FWD FA SEAT WOULD NOT STOW PROPERLY. CONTRACT MX ADJUSTED THE SEAT MECHANISM. OP'S CHECK GOOD.

Part: GEARBOX — FAILED (NR 1 ENGINE) · airframe 11,235 hrs · 9,825 cycles

ASH 7112 DSM - CREW ABORTED TAKEOFF AND RTG. NR 1 ENGINE LOST N2 SPEED WITH A LOW OIL PRESSURE CAUTION ON TAKEOFF ROLL. ENGINE SHUTDOWN UNCOMMANDED. MAINTENANCE REMOVED AND REPLACED AGB AND LUBED SCAVENGE PUMP.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 11,228 hrs · 9,819 cycles

ASH 7392 OKC. THE CREW REPORTED A LT AFT EXTERIOR EMERGENCY LIGHT INOP. MAINTENANCE RELAMPED.

Part: ENGINE — HOT START (NR 1) · airframe 11,172 hrs · 9,760 cycles

ASH 7357 ORD. NR 1 ENGINE HOT START. PERFORMED SECOND START AND ENGINE STARTED NORMALLY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 11,085 hrs · 9,677 cycles

ASH 7255 IAD - RT OVERWING EXTERNAL EXIT LIGHT INOP. MX REPLACED THE LAMP AND IT OPS CHECKED GOOD.

Part: BRACKET — DAMAGED (NLG) · airframe 10,974 hrs · 9,568 cycles

ASH 7159 IAD - NLG DOOR OPEN MESSAGE WITH GEAR DISAGREE. MX REPLACED THE PROXIMITY BRACKET.

Part: TARGET — OUT OF ADJUST (EMERGENCY EXIT) · airframe 10,924 hrs · 9,522 cycles

ASH 7248 ORD - RIGHT EMERGENCY EXIT DOOR CAUTION MESSAGE IN FLIGHT. MX ADJ TARGET.

Part: UNKNOWN — UNKNOWN · airframe 10,632 hrs · 9,244 cycles

ASH 7202 ORD - STALL FAIL CAUTION ON TAKEOFF ROLL. PILOT ABORTED TAKEOFF AND RETURNED TO GATE. MX RESET. OP'S CHECK GOOD.

Part: PROXIMITY SWITCH — DIRTY (EMERGENCY EXIT) · airframe 10,556 hrs · 9,170 cycles

ASH 7337 ORD - RIGHT OVERWING EMERGENCY EXIT DOOR CAUTION IN FLIGHT. MAINTENANCE REMOVED AND INSPECTED DOOR, CLEANED PROX SWITCH AND REINSTALLED DOOR AND NOTED NO FURTHER FAULT.

Part: ACTUATOR — MALFUNCTIONED · airframe 10,498 hrs · 9,109 cycles

ASH 9700 OKC - YAW DAMPER 2 DISENGAGED IN FLIGHT. MAINTENANCE REPLACED THE NR 2 ACTUATOR.

Part: CAUTION MESSAGE — ILLUMINATED · airframe 10,486 hrs · 9,098 cycles

ASH 7271 IAD - ABORTED TAKEOFF DUE TO STALL FAIL CAUTION MESSAGE AND CONFIG SPOILER WARNING MESSAGE. MX RESET BOTH SYSTEMS.

Part: SPOILER — OUT OF RIG · airframe 10,276 hrs · 8,888 cycles

ASH 7191 CLT - SPOILER FAULT. MX RIGGED RIGHT I/B SPOILER. OPS CHECK GOOD.

Part: ECU — WARNING LIGHT (SPOILERS) · airframe 10,275 hrs · 8,887 cycles

ASH 7372 DSM, CONFIG SPOILER MASTER WARNING. MX R&R SECU NR 2.

Part: WARNING MESSAGE — FALSE ACTIVATION (SPOILER SYS) · airframe 10,276 hrs · 8,890 cycles

ASH 7327 ORD - ABORTED TAKEOFF AND RETURNED TO THE GATE DUE TO A CONFIG SPOILERS MESSAGE. RESET SYSTEM. OPS CHECK GOOD.

Part: PCU — MALFUNCTIONED · airframe 10,274 hrs · 8,884 cycles

ASH 7013 OKC - GEAR SWING TEST FLIGHT WAS GOOD BUT RIGHT FLIGHT SPOILER W/N DEPLOY WHEN COMMANDED. MX REPLACED PCU'S.

Part: PRIORITY VALVE — MALFUNCTIONED (MLG) · airframe 10,268 hrs · 8,881 cycles

ASH 7291 ROC - RETURN TO FIELD DUE TO A NOSE DIS MESSAGE. MX INSPECTED THE A/C AND FERRIED TO OKC FOR REPAIR. MX REPLACED NOSE AND MAIN PRIORITY VALVES.

Part: PCU — MALFUNCTIONED (SPOILERS) · airframe 10,252 hrs · 8,865 cycles

ASH 7399 ATL - ABORTED TAKEOFF, SPOILER MISCONFIG AND CAUTION MESSAGE. RESET SECU AND DOWNGRADED TO STATUS MESSAGE. MAINTENANCE REPLACED FLIGHT SPOILER PCU NR 1 & NR 2.

Part: PCU — FAULTED (SPOILERS) · airframe 10,248 hrs · 8,855 cycles

ASH 7196 GSP - FLIGHT SPOILER FAULT. MAINTENANCE REMOVED AND REPLACED RT FLT SPOILER OB PCU.

Part: WARNING MESSAGE — ILLUMINATED (FLT SPOILERS) · airframe 10,212 hrs · 8,824 cycles

ASH 7142 BUF - ABORTED TAKEOFF. FLIGHT SPOILER STATUS MESSAGE. MAINTENANCE PLACED ON MEL. OPS CHECK GOOD.

Part: WARNING MESSAGE — ILLUMINATED (STALL WARNING) · airframe 10,207 hrs · 8,816 cycles

ASH 7215 BMI - ABORTED TAKEOFF AND RETURNED TO GATE. STALL FAIL CAUTION MESSAGE. MAINTENANCE RESET SPOILER SYSTEM, RAN ENGINES AT HIGH POWER. OPS CHECK GOOD.

Part: COMPUTER — FAULTED (STALL WARNING) · airframe 10,155 hrs · 8,758 cycles

ASH 7248 ORD - ABORTED TAKEOFF DUE TO A STALL FAIL EICAS MESSAGE. MAINTENANCE RESET STALL PROTECTION COMPUTER. NO FURTHER DEFECTS NOTED.

Part: B-NUT — LEAKING (APU FUEL LINE) · airframe 10,134 hrs · 8,742 cycles

ASH 7230 ORD - FUEL LEAKING FROM APU SHROUD. RESECURED TWO FUEL LINE B-NUTS. MAINTENANCE PLACED APU ON DEFERRAL SO SHROUD COULD COMPLETELY PURGE OF FUMES. AIRCRAFT RETURNED TO SERVICE. MAINTENANCE COULD NOT DUPLICATE LEAK.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHT) · airframe 10,012 hrs · 8,920 cycles

FORWARD FACING EXIT SIGN IN CABIN INOPERATIVE. MAINTENANCE SECURED THE CONNECTION AT THE EMERGENCY LIGHT POWER SUPPLY.

Part: SPOILER SYS — FAULTED · airframe 9,862 hrs · 8,480 cycles

ASH 7212 IAD - INBOARD/OUTBOARD GROUND SPOILER FAULT AFTER TAKEOFF. MAINTENANCE RESET THE SPOILER SYSTEM AND THE OPS CK WAS NORMAL.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 9,711 hrs · 8,334 cycles

ASH 2762 PHL - ONE FLOOR PATH LIGHTING SEGMENT BROKEN. MAINTENANCE REPLACED THE SEGMENT.

Part: STALL WARNING — UNKNOWN · airframe 9,685 hrs · 8,313 cycles

ASH 2699 PHL - ABORTED TAKEOFF DUE TO A STALL FAIL AND A CONFIG SPOILER MESSAGE. MX PERFORMED, OPS CHECK OF STALL SYSTEM. OPS CHECK GOOD.

Part: PROXIMITY SENSOR — OUT OF ADJUST (NLG DOOR) · airframe 9,488 hrs · 8,113 cycles

ASH 2621 PHL - NOSE GEAR DOOR OPEN MESSAGE IN FLIGHT. MX ADJUSTED PROXIMITY SENSOR, JACKED A/C AND DID GEAR SWINGS. NO FURTHER DEFECTS FOUND.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 9,281 hrs · 7,947 cycles

THE EMERGENCY PATH LIGHTS AFT OF ROW 9 WERE NOT ILLUMINATED. MX REPOSITIONED THE LAST FLOOR STRIP AND OPS WERE NORMAL.

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 9,019 hrs · 7,718 cycles

OUT BOUND PILOT FOUND EMERGENCY FLOOR LIGHTS BETWEEN ROW 1 & 5 TO BE INOP. MX REPLACED CABLE ASSY & ACFT CONTINUED OPERATIONS.

Part: DOOR — LACK OF LUBE (MAIN PAX) · airframe 8,691 hrs · 7,433 cycles

ASH 2631 PHL TO ATL - THE CREW FOUND THE MAIN PASSENGER DOOR DIFFICULT TO OPEN. MAINTENANCE APPLIED LUBRICATION.

Part: CONTROL SYSTEM — MALFUNCTIONED (SPOILERS) · airframe 8,306 hrs · 7,092 cycles

REJECTED TAKEOFF FOR SPOILER CONFIG MESSAGE ON EICAS AT 70 KTS. MESSAGE CLEARED AT 80 KTS. MX INSP MDC FOR FAULTS. NONE NOTED. MX RESET SPOILER CONTROL SYSTEM AND PERFORMED OPS CHECK. SYSTEM OPERATED NORMALLY.

Part: ENGINE — LEAKING (NR 2) · airframe 8,092 hrs · 6,900 cycles

EMERGENCY DECLARED. SHUTDOWN NR 2 ENGINE AND DIVERTED TO IAD DUE TO LOSS OF OIL PRESSURE. MX IS IN THE PROCESS OF TROUBLESHOOTING.

Part: BULB — BURNED OUT (EMERGENCY LIGHTS) · airframe 7,949 hrs · 6,766 cycles

ONE EMERGENCY LIGHT IN OVERHEAD INOP. MAINTENANCE COMPLIED WITH MEL PROCEDURES. 2/7/05 MAINTENANCE RELAMPED, OPS CHECK GOOD.

Part: LAMP — BROKEN (EMERGENCY LIGHTS) · airframe 7,862 hrs · 6,683 cycles

EMERGENCY FLOOR LIGHTS INTERMITTENT AFT OF THE EXIT ROW. ACFT AOG FOR A POWER CABLE ASSY. 1/24/05 MAINTENANCE REPLACED EMERGENCY LIGHT CABLE STRIP, OPS CHECKED GOOD.

Part: APU — FIRE (APU BAY) · airframe 7,079 hrs · 5,941 cycles

AFTER LANDING IN YUL AND SHUTTING DOWN THE APU FOR THE NIGHT THE GROUND CREW NOTICED FLAMES EMITTING FROM THE APU EXHAUST AREA. AS GROUND CREW WAS MOVING TO NOTIFY THE CREW, THE APU FIRE WARNING ALERTED IN THE COCKPIT AND SIMULTANEOUSLY DISCHARGED THE FIRE BOTTLE AUTOMATICALLY. MAINTENANCE IS IN THE PROCESS OF LOOKING FOR THE SOURCE OF THE FIRE. INDICATIONS ARE POINTING TO THE FIRE BOTTLE CONTAINED IN THE APU ENCLOSURE. 9/11 MX REPLACED FIRE DETECTION CONTROL P/N 472597-02, S/N 0434, AND APU FIREX CONTAINER.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 6,457 hrs · 5,439 cycles

ASH 2810 YUL - CLT, EMERGENCY EXIT FLOOR STRIPS INOP. CONTRACT MX TROUBLESHOOTING, MX REPLACED LIGHTING STRIP AND BATTERY. BATTERY PART NR 2013-1A.

Part: LIGHT — INOPERATIVE (EMERGENCY EXIT) · airframe 6,362 hrs · 5,365 cycles

EMERGENCY EXIT LIGHT SWITCH LEFT IN THE ON POSITION. LIGHTS WERE INOPERATIVE. MX FOUND NO FAULT WITH EMERGENCY EXIT LIGHTING SYSTEM. OPS GOOD NO PARTS USED.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 5,766 hrs · 4,886 cycles

RT FS 625 OBLIQUE ANGLE IS CRACKED. REPLACED CRACKED OBLIQUE ANGLE IAW BOMB CRJ SRM 51-42.21

Part: ANGLE — CRACKED (FUSELAGE) · airframe 5,766 hrs · 4,886 cycles

LT FS 625 OBLIQUE ANGLE IS CRACKED. REPLACED 625 OBLIQUE ANGLE IAW BOMB CRJ SRM 51-42-21.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 5,766 hrs · 4,886 cycles

FS 621, RBL 40, WL 73 UNDER FLOOR SUPPORT ANGLE FROM RBL 32 TO RBL 44. FABRICATED REPAIR ANGLES IAW BOMB REO 601R-53-61-117 REV B

Part: ANGLE — CRACKED (FUSELAGE) · airframe 5,766 hrs · 4,886 cycles

FS 621, LBL 40, WL 73 UNDER SUPPORT ANGLE IS CRACKED. FABRICATED REPAIR ANGLES FROM P/N 601R-53-61-004-1 AND 601R-53-61-004-5 AND INSTALLED IAW BOMB REO 601R-53-61-117 REV B

Part: TAIL CONE — CUT (RT ENGINE) · airframe 3,558 hrs · 3,076 cycles

AIRCRAFT'S RIGHT ENGINE JET PIPE MISSING INSPECTION COVER AND TAIL CONE HAS A 1.5 INCH CUT. REPLACED RIGHT ENGINE TAIL CONE ASSEMBLY. OPS CHECKS GOOD.

Part: FLAP — MALFUNCTIONED (WING) · airframe 2,686 hrs · 2,362 cycles

FLAPS FAIL AT 30 DEGREES ON SHORT FINAL. PERFORMED OPERATIONAL CHECK OF FLAP SYSTEM PER AMM 27-54-00. SYSTEM OPERATIONAL CHECKS NORMAL. OK FOR SERVICE.

Part: SELECTOR VALVE — FAILED (NLG WW) · airframe 2,330 hrs · 2,064 cycles

UPON APPROACH INTO LGA NOSE DIAGREE MESSAGE ON EICAS, NOSE GEAR FAILED TO EXTEND NORMALLY. A/C DIVERTED TO SWF WHERE EMERGENCY GEAR HANDLE WAS PULLED. A/C LANDED WITH OUT INCIDENT. LANDING GEAR WAS PINNED AND MAINTENANCE FERRIED TO RDU. TROUBLSHOOTING INDICATED NOSE LANDING GEAR SELECTOR TO BE FAULTY. REMOVED AND REPLACED NOSE LANDING GEAR SELECTOR VALVE IAW CL-65 AMM 32-33-10. JACKED NOSE GEAR, SWUNG NOSE GEAR SEVERAL TIMES AND NO FAULTS NOTED.

Part: HANDLE — DETACHED (MLG) · airframe 1,832 hrs · 1,623 cycles

LANDING GEAR HANDLE FELL OFF IN HAND ON CLIMBOUT. REMOVED AND REPLACED IAW AMM 32-31-01.

Part: CONTROLLER — FAILED (HYD SYSTEM) · airframe 1,135 hrs · 1,023 cycles

STAB CH1 INOP. STATUS MSG AND ASSOCIATED CB POPPED IN FLIGHT(2B8). REMOVED AND REPLACED HSTA IAW 27-42-01. REMOVED AND REPLACED HSMCU IAW CRJ AMM 27-42-05, OPS CK GOOD.

Part: ACTUATOR — INTERMITTENT (HORIZONTAL STAB) · airframe 683 hrs · 623 cycles

NO MANUAL OR AUTOPILOT STABILZER TRIM AFTER T/O. NO ASSOCIATED CAUTIONS. MOMENTARY STAB CH 1 INOP STATUS MESSAGE, F/O HAD MOMENTARY TRIM. REMOVED AND REPLACED STAB TRIM ACTUATOR IAW AMM 27-42-01. OPS CHECK GOOD.