N510AE

Part: FORMER — CORRODED (ZONE 200) · airframe 47,853 hrs · 37,581 cycles

PASSENGER DOOR FWD FORMER IS CORRODED. CORROSION IS LOCATED UNDER PANEL 832FL. REMOVED CORROSION AND TREATED AFFECTED AREA IAW MHIRJ REO 670-52-11-1468 REV. --.

Part: COVER — MISSING (ZONE 100) · airframe 46,834 hrs · 36,728 cycles

LOW PRESSURE GROUND AIR ACTUAL COVER MISSING / REMOVED AND REPLACED LOW PRESSURE GROUND AIR LOCKING PIN AND INSTALLED NEW COVER AND PIN IAW CRJ 700 AMM 21-20-02-000/400-801-A01-PSA.

Part: STEERING SYS — UNKNOWN (NLG) · airframe 46,400 hrs · 36,347 cycles

NOSE WHEEL STEERING INOP CAUTION MSG IN FLIGHT / PERFORMED SYS RESET PER MIPM PROCEDURES FAULT DID NOT CONTINUE. PERFORMED OPS CHECK OF NLG STEERING SYSTEM IAW CRJ 700 AMM 32-51-00-710-801. OPS CHECK GOOD AT THIS TIME.

Part: ANGLE — CORRODED (ZONE 100) · corrosion level 2 · airframe 44,704 hrs · 34,880 cycles

GALLEY SERVICE DOOR O/B SILL ANGLE IS CORRODED AROUND THE SCREW HOLES.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 44,704 hrs · 34,880 cycles

WVAC CO # 10105723 JOB # 21010571, OP # 138: STRINGER 26R IS CORRODED BETWEEN FS 333.00 AND 349.00.

Part: DOOR SILL — CORRODED (ZONE 100) · corrosion level 2 · airframe 44,704 hrs · 34,880 cycles

GALLEY SERVICE DOOR I/B SILL ANGLE IS CORRODED.

Part: INTERCOSTAL — CORRODED (ZONE 100) · corrosion level 2 · airframe 44,704 hrs · 34,880 cycles

INTERCOSTAL AT STGR 20L FS 333 TO FS 349 HAS CORROSION

Part: INTERCOSTAL — CORRODED (ZONE 100) · corrosion level 2 · airframe 44,704 hrs · 34,880 cycles

UPON REMOVING INTERCOSTAL AT FS 319.00 TO FS 333.00 FOUND FRAME AT FS 319.00 TO HAVE HEAVY CORROSION

Part: INTERCOSTAL — CORRODED (ZONE 100) · corrosion level 2 · airframe 44,704 hrs · 34,880 cycles

INTERCOSTAL AT STGR 19R IS CORRODED BETWEEN FS 319.00 AND 333.00.

Part: INTERCOSTAL — CORRODED (ZONE 100) · corrosion level 2 · airframe 44,704 hrs · 34,880 cycles

INTERCOSTAL AT STGR 20L IS CORRODED BETWEEN FS 319.00 AND 333.00.

Part: STRINGER SPLICE — CORRODED (ZONE 100) · corrosion level 2 · airframe 44,704 hrs · 34,880 cycles

STRINGER 25R SPLICE IS CORRODED BETWEEN FS 333.00 AND 349.00

Part: FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 44,704 hrs · 34,880 cycles

FRAME IS CORRODED AT FS 517.00 BETWEEN STGR 18L AND 19L

Part: SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 44,704 hrs · 34,880 cycles

AVI DOOR SUPPORT INTERCOSTAL LEFT OF STGR 27 IS CORRODED BETWEEN FS 394.00 AND 409.00

Part: GLAND NUT — CORRODED (ZONE 700) · corrosion level 2 · airframe 44,704 hrs · 34,880 cycles

DISCREPANCY: RH MLG GLAND NUT THREADS ARE CORRODED.

Part: TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 44,704 hrs · 34,880 cycles

DISCREPANCY: FWD CARGO MIDDLE FWD FLOOR TRACK CORRODED REQUIRES REPAIR OR REPLACE.

Part: PCU — JAMMED · airframe 44,388 hrs · 34,588 cycles

OB SPOLILERSON AND OB FLT SPOILERS CAUTION MSG AFTER EXTENDING SPOILERS THROUGH 5K FEET. DIVERTED TO KIAD / INTEROGATED MDC AND FOUND B1 CODE 007920(R OB MFS PCU / PCU JAM) POSTED AND PERFORMED CRJ700FIM 27ˆ’64ˆ’01ˆ’810ˆ’817-A01 CYCLED AIRCRAFT POWER, FAULT CLEARED AND DID NOT RETURN, SYSTEM RESET WAS SUCCESSFUL, OPENED TEMP REPAIR TO MONITOR THE SPECIFIC PCU. UPON A REPEAT EVENT WITHIN APPROX. 30 DAYS, SCHEDULE THE AFFECTED MFS PCU TO BE REPLACED AT THE NEXT MAINTENANCE OPPORTUNITY NO FURTHER MX ACTION REQUIRED AT THIS TIME AIRCRAFT OK FOR SERVICE.

Part: HARNESS — FALSE INDICATION · airframe 43,229 hrs · 33,541 cycles

ATC DECLARED AN EMERGENCY FOR THE AIRCRAFT AFTER A LOSS OF STEERING EVENT. CA DID NOT FEEL THE NEED TO DECLARE AN EMERGENCY HIMSELF. NO ADDITIONAL ISSUES. STEERING INOP CAUTION ILLUMINATED AFTER GEAR RETRACTION / CLEANED HARNESS MT129P1 IAW CRJ 700 RIL 8574 AND REASSEMBLED IAW CRJ 700 ESPM 20-14-01. REINSTALLED IAW CRJ 700 AMM 29-34-01-400-802 STEPS 4.A.7-5I. OPS CHECK GOOD NO DEFECTS NOTED AT THIS TIME.

Part: SHUTOFF VALVE — UNSERVICEABLE (RT ENGINE BLEED) · airframe 41,433 hrs · 31,938 cycles

MAINTENANCE AIR RETURN DUE RIGHT ENGINE BLEED CAUTION MESSAGE ON TAKEOFF DID NOT LAND OVER WEIGHT AND DID NOT DECLARE AN EMERGENCY. REMOVED AND REPLACED PRSOV, IAW CRJ 700 AAM 36-12-01-000\400-801-A01.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 40,596 hrs · 31,128 cycles

REMOVED AND REPLACED THE PSU BATTERY PACKS. OPS CHECK GOOD AT THIS TIME. POSITION 1. MPN OFF - 2013-1A / MSN OFF 79939. MPN ON 2013-1A / MSN ON 206909 POSITION 2 MPN OFF 2013-1A / MSN OFF 125181. MPN ON 2013-1A MSN ON 76501. POSITION 3 MPN OFF 2013-1A / MSN OFF 104542 MPN ON 2013-1A MSN ON 99189. POSITION 4 MPN OFF 2013-1A MSN OFF 124849 MPN ON 2013-1A MSN ON 69714.

Part: ANGLE — CORRODED (PAX DOOR) · corrosion level 2 · airframe 40,573 hrs · 31,107 cycles

PAX DOOR MID CAP ANGLE CORRODED AROUND FASTENER HOLES. LOCATED,DRILLED,AND INSTALLED NEW SERVICEABLE PAX DOOR MID CAP ANGLE P/N SH67031825-9S IAW CRJ 700 SRM 51-40-11-001-001-A01 AND SRM 51-42-06-001-001-A01.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 40,573 hrs · 31,107 cycles

PAX DOOR AFT DRAG ANGLE CRACKED. REPAIRED IAW STS EA 70-2020-095.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,573 hrs · 31,107 cycles

PASSENGER DOOR LOWER SILL ANGLE IS CORRODED. INSTALL NEW SERVICEABLE PAX DOOR LOWER SILL ANGLE P/N SH670-31875-3 IAW CRJ 700 SRM 51-42-06-001-001-A01 AND SRM 57-42-21-001-001-A01.

Part: BRACKET — CRACKED (PAX DOOR) · airframe 40,573 hrs · 31,107 cycles

PAX DOOR ASSIST MOTOR LOWER BRACKET CRACKED. LOCATED, DRILLED AND INSTALLED NEW SERVICEABLE PAX DOOR ASSIST MOTOR BRACKET IAW CRJ 700 SRM 51-40-11-001-010-A01, 51-42-06-001-001-A01 AND 51-42-13-001-001-A01.

Part: BATTERY — DISCHARGED (CABIN) · airframe 40,353 hrs · 30,932 cycles

LEFT OVERWING EXIT LOCATING SIGN IN ROW 16 OUT. REMOVED AND REPLACED EXIT SIGN. OPS CHECK BAD. REMOVED AND REPLACED 4 EMERGENCY BATTERIES P/N 2013-1A. #1 S/N 122464 11276 HR 10345 CYCLES 1525 OVERHAUL. #2 S/N 122516 10318 HR 9356 CYCLES 249 INSPECTED. #3 S/N 98260 21162 HR 17350 CYCLES 1525 OVERHAUL. #4 S/N 104852 20091 HR 17106 CYCLES 1525 OVERHAUL. OPS CHECK GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 38,829 hrs · 29,586 cycles

EMERGENCY LIGHTS IN FLIGHT DECK LEFT IN ON POSITION. REPLACED 4 BATTERY PACKS P/N 2013-1A S/N 122525, 122912, 122512, 73206. OPS CHECK GOOD.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 38,402 hrs · 29,202 cycles

STR 26L IS CORRODED BETWEEN FS333 AND FS349. REMOVED CORROSION STRINGER 26L/LOCATED AND DRILLED SERVICEABLE STRINGER P/N SH670-31372-3S IAW SRM 51-40-11-001-001-A01.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 38,402 hrs · 29,202 cycles

FWD JACK FITTING SUPPORT INTERCOSTALS BETWEEN FS265 AND FS280 ARE CORRODED. INSTALLED 2A NEW INTERCOSTALS AT FS265-280 STRINGER 27 P/N: CC670-32179-1 AND CC670-32179-2 IAW SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 38,402 hrs · 29,202 cycles

STR 24R IS CORRODED BETWEEN FS333 AND FS349. COMPLIED WITH STRINGER 24R SPLICE REPAIR IAW SRM 53-21-03-201-006-A01.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 38,402 hrs · 29,202 cycles

INTERCOSTALS BETWEEN FS349 AND FS364 BETWEEN STR 26L AND STGR 26R ARE CORRODED. REMOVED UNSERVICEABLE INTERCOSTALS IAW SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01. LOCATED, DRILLED AND INSTALLED NEW SERVICEABLE INTERCOSTALS BETWEEN FS 349 AND FS 364 FROM STR 26L - 26R IAW SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.

Part: HINGE — WORN (PAX DOOR) · airframe 38,392 hrs · 28,862 cycles

PAX DOOR HINGE WORN. REMOVED AND REPLACED THE DOOR HINGE IAW SRM 52-11-01-201-002-A01.

Part: HINGE — WORN (PAX DOOR) · airframe 38,392 hrs · 28,862 cycles

PAX DOOR HINGE WORN. REMOVED AND REPLACED THE DOOR HINGE IAW SRM 51-40-11-001-001-A01, AND 52-11-01-201-A01.

Part: REHEATER — MALFUNCTIONED (LT A/C PACK) · airframe 37,048 hrs · 27,953 cycles

CREW REPORTED THE LT PACK WAS SURGING AND CAUSING A SLIGHT BURNING SMELL. REMOVED AND REPLACED LT REHEATER. OPS AND LEAK CHECKS GOOD.

Part: FLOORBEAM — CORRODED (BS 1031) · corrosion level 2 · airframe 34,787 hrs · 25,822 cycles

FLOORBEAM CAP AT BS 1031, LBL 27 IS CORORDED AT A COUPLE LOCATIONS. REPAIRED THE FLOORBEAM CAP IAW SRM 53-00-41-201-001-A01.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 34,787 hrs · 25,822 cycles

J-ANGLE GUSSET IS CRACKED AT BS 280, LBL 9. THE FLOORBEAM ANGLE WAS REPLACED

Part: FLOORBEAM — CORRODED (BS 280) · corrosion level 2 · airframe 34,787 hrs · 25,822 cycles

J-ANGLE IS CORRODED AROUND FASTENER HOLES AT THE BS 280 FLOORBEAM BETWEEN LBL 9 AND RBL 9. REPLACED THE FLOORBEAM ANGLE IAW SB 670BA-53-041

Part: FLOORBEAM — CRACKED (BS 280) · airframe 34,787 hrs · 25,822 cycles

FLOORBEAM ANGLE IS CRACKED AT BS 280, RBL 9. REPAIRED IAW MWC 21010535, SB 670BA-53-041.

Part: FLOORBEAM — CORRODED (BS 1031) · corrosion level 2 · airframe 34,787 hrs · 25,822 cycles

FLOORBEAM CAP AT BS 1031, LBL 27 IS CORRODED AT A COUPLE OF LOCATIONS. REPAIRED THE FLOORBEAM CAP IAW SRM 53-00-41-201-001-A01.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 34,787 hrs · 25,822 cycles

THE BS 280 FLOORBEAM FOUND CRACKED AT RBL 9.. REPLACED THE FLOORBEAM IAW SB 670BA-53-041.

Part: BALLAST — ODOR (CABIN LIGHTS) · airframe 34,266 hrs · 25,399 cycles

ELECTRICAL ODOR IN CARGO BIN ABOVE 21 ABC. REMOVED AND REPLACED THE BALLAST.

Part: LIGHT — MALFUNCTIONED (CABIN/EXTERIOR) · airframe 34,140 hrs · 2,594 cycles

EMERGENCY LIGHTS FLASHING IN CABIN AND EXTERIOR.

Part: CONTROL PANEL — FAILED (AILERON TRIM) · airframe 33,232 hrs · 24,440 cycles

AILERON TRIM INOPERATIVE IN FLIGHT. THE CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED AILERON/RUDDER CONTROL PANEL IAW AMM. OPS CHECKED GOOD, THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 30,095 hrs · 21,565 cycles

PRIOR TO FIRST FLIGHT OF THE DAY, CREW REPORTED FLIGHT DECK EMERGENCY LIGHT SWITCH WAS LEFT ON AND BATTERY DEAD. MAINTENANCE INSPECTED, R & R NR 4 BATTERY PACK AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 30,095 hrs · 21,565 cycles

PRIOR TO FIRST FLIGHT OF THE DAY, CREW REPORTED FLIGHT DECK EMERGENCY LIGHT SWITCH WAS LEFT ON AND BATTERY DEAD. MAINTENANCE INSPECTED, R & R NR 2 BATTERY PACK AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 30,095 hrs · 21,565 cycles

PRIOR TO FIRST FLIGHT OF THE DAY, CREW REPORTED FLIGHT DECK EMERGENCY LIGHT SWITCH WAS LEFT ON AND BATTERY DEAD. MAINTENANCE INSPECTED, R & R NR 1 BATTERY PACK AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 30,095 hrs · 21,565 cycles

PRIOR TO FIRST FLIGHT OF THE DAY, CREW REPORTED FLIGHT DECK EMERGENCY LIGHT SWITCH WAS LEFT ON AND BATTERY DEAD. MAINTENANCE INSPECTED, R & R NR 3 BATTERY PACK AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: DOUBLER — CHAFED (FUSELAGE) · airframe 30,086 hrs · 21,556 cycles

DOUBLER ON FUSELAGE SKIN AT FS 969.00 & STRINGER 27 IS CHAFED. REPAIRED CHAFE IAW ERS CR-53MR-1511.

Part: SIGN — INOPERATIVE (PAX DOOR) · airframe 30,086 hrs · 21,556 cycles

PASSENGER EXIT DOOR HANDLE BETA LIGHT FAILED THE LUMINOSITY CHECK IAW WC 000-33-900-703. R & R SELF-ILLUMINATING SIGN IAW AMM 33-51-13.

Part: CROSSBEAM — CORRODED (FUSELAGE) · airframe 30,086 hrs · 21,556 cycles

LEFT SIDE OF FS 280.00 CROSSBEAM HAS EVIDENCE OF CORROSION. COMPLIED WITH REPAIR OF FS 280.00 IAW SRM 53--11-41. REFERENCE NRWC 460940 FOR INSTALLATION OF SUPPORT.

Part: BULKHEAD — CORRODED (FUSELAGE) · airframe 30,086 hrs · 21,556 cycles

LEFT COCKPIT BULKHEAD JUST FWD OF FS 280.00 HAS EVIDENCE OF CORROSION, LOWER INBD SIDE. REPAIR TO FS 280 LT LOWER WEB COMPLIED WITH IAW EO CR-53MR-174.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 30,086 hrs · 21,556 cycles

RIGHT SIDE LT BRACKET FOR FS 280.00, CROSSBEAM HAS 3/8" CRACK. COMPLIED WITH INSTALLATION OF RT T BRACKET IAW SRM 51-42-21 & 51-42-06.

Part: WEB — CRACKED (FUSELAGE) · airframe 30,086 hrs · 21,556 cycles

LEFT FWD EQUIP COMPARTMENT FLOOR WEB AT FS 202-75 IS CRACKED, APPROX. 3/8" LONG. REPAIRED LT FWD EQUIP COMPARTMENT FLOOR WEB IAW ETN CR-53-099.

Part: WEB — CRACKED (FUSELAGE) · airframe 30,086 hrs · 21,556 cycles

RIGHT FORWARD EQUIPMENT COMPARTMENT FLOOR WEB IS CRACKED, APPROXIMATELY 3/8" LONG & GOES UNDER THE ADG PUMP AT FS 202.75. REPAIRED RIGHT FORWARD EQUIPMENT COMPARTMENT FLOOR WEB CRACK IAW ERS-CR-5300-1506.

Part: SKIN — CHAFED (LT AILERON) · airframe 30,086 hrs · 21,556 cycles

LEFT AILERON TOP LEADING EDGE SKIN IS CHAFFED. R & R OF NEW UPPER LEADING EDGE IAW CRJ SRM 51-42-20. LOWER SKIN PN CC670-1354-1.

Part: LIGHT — DAMAGED (CABIN) · airframe 30,086 hrs · 21,556 cycles

LEFT EMERGENCY FLOOR LIGHT STRIP NR 1 HAS EVIDENCE OF IMPACT DAMAGE AT THE FWD EDGE. R & R LT EMERGENCY FLOOR LIGHT STRIP NR 1 IAW AMM 33-51-01.

Part: GLOWSTRIP — DELAMINATED (CABIN) · airframe 30,086 hrs · 21,556 cycles

LEFT EMERGENCY FLOOR LIGHT STRIP NR 11, PHOTO LUMINESCENT IS DELAMINATED AT ONE END. INSTALLED NEW EMERGENCY FLOOR LIGHT STRIP IAW AMM 33-51-01.

Part: STRIP — GOUGED (CABIN) · airframe 30,086 hrs · 21,556 cycles

LEFT EMERGENCY FLOOR LIGHT STRIP NR 2 HAS LARGE GOUGE OFF OF THE EDGE, NEAR THE FWD END. R & R LT EMERGENCY FLOOR LIGHT STRIP NR 2 IAW AMM 33-51-01.

Part: COVER — CRACKED (CABIN) · airframe 30,086 hrs · 21,556 cycles

RIGHT EMERGENCY FLOOR LIGHT STRIP NR 9, COVER IS CRACKED NEAR THE FWD EDGE. R & R RIGHT EMERGENCY FLOOR LIGHT STRIP NR 9 IAW AMM 33-51-01.

Part: GLOWSTRIP — DAMAGED (CABIN) · airframe 30,086 hrs · 21,556 cycles

LEFT EMERGENCY FLOOR LIGHT STRIP NR 4, PHOTO LUMINESCENT DAMAGED CAUSING A BLACK SECTION THAT IS NOT LUMINESCENT. R & R LEFT EMERGENCY FLOOR LIGHT STRIP NR 4 IAW AMM 33-51-01.

Part: SIGN — FAILED (EMERGENCY EXIT) · airframe 30,086 hrs · 21,556 cycles

LEFT EMERGENCY EXIT DOOR HANDLE, BETA LIGHT FAILED THE LUMINOSITY CHECK. R & R BETA LIGHT IAW AMM 33-51-13. HANDED FAILED BETA LIGHT TO STORES DEPARTMENT PERSONNEL FOR DISPOSAL IAW ETN-CR-33-018 & GPM SECTION 10-03.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 29,862 hrs · 21,372 cycles

DURING DESCENT, WHEN USING THE SPOILER LEVER, THE INBD FLIGHT SPOILER & INBD SPOILERONS CAUTION MSG APPEARED. PERFORMED SPOST TEST IAW AMM 27-60-00. OPERATIONS CHECKED GOOD AT THIS TIME.

Part: GCU — FAILED (LEFT) · airframe 29,697 hrs · 21,239 cycles

DURING CRUISE FLIGHT, ACCESS BUSS CAUTION MESSAGE. BUSS 1 & ENG 1 DISPLAYED AS MAGENTA ON SYNOPTIC PAGE. AFTER AOM1 CHECKLIST FAILED TO RESTORE FAILED SYS, APU WAS STARTED RESULTING IN PARTIAL RECOVERY OF LOST SYS, BUT NO FLOW BARS CONNECTING BUS 1 OR ESS BUS EVEN THOUGH ESS BUS APPEARED GREEN. R & R LT IDG GCU IAW AMM 24-11-07. OPERATIONS CHECKED GOOD.

Part: SHUTOFF VALVE — FAULTY (BLEED AIR SYS) · airframe 29,027 hrs · 20,683 cycles

AFTER TAKEOFF LT ENG BLEED CAUTION PRESENTED ON EICAS. R & R LT ENG PRSOV IAW AMM 36-12-01. OPERATIONS CHECKED GOOD.

Part: CHARGER — FAILED (EMERGENCY LIGHTS) · airframe 28,935 hrs · 20,609 cycles

EMERGENCY LIGHT INOPERATIVE. R & R BATTERY PACKS & CHARGERS IAW WC 33-002. OPS CHECKED GOOD,

Part: SENSOR — FAILED (RT SLAT) · airframe 28,832 hrs · 20,531 cycles

DURING DESCENT, CREW RECEIVED AN EICAS SLAT FAIL CAUTION MESSAGE. COMPLIED WITH AOM VOL 1 PROCEDURES, DECLARED AN EMERGENCY & LANDED WITHOUT INCIDENT. REMOVED AND REPLACED RT SLAT BPSU IAW AMM 27-81-03 OPERATION CHECK GOOD.

Part: FLASHLIGHT — UNSECURE (CABIN) · airframe 28,324 hrs · 20,098 cycles

FLASHLIGHT IN AFT CABIN WILL NOT STAY SECURE IN HOLDER. DEFERRED AFT CABIN FLASHLIGHT IAW MEL 25-15. R & R AFT CABIN FLASHLIGHT ASSEMBLY IAW AMM 25-61-02. OPERATIONS CHECKED GOOD. MEL SYS RESTORED.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 27,514 hrs · 19,542 cycles

STRINGER 24L IS CRACKED AT FS 1108.00. REPLACED STRINGER 24L IAW SRM 51-42-06 & 51-42-21.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 27,514 hrs · 19,542 cycles

FRAME 1108.00 IS BENT, TWISTED & CRACKED FROM STRINGER 21R TO 21L. REPAIRED FRAME 1108:00 IAW ERS-CR-53MR-420.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 27,514 hrs · 19,542 cycles

STRINGER 23L IS CRACKED AT FS 1108.00. COMPLIED WITH REPAIR TO STRINGER 23L AT FS 1108.00 IAW ERS-CR-53MR-420.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 27,447 hrs · 19,501 cycles

EMERGENCY LIGHT AFT OF SERVICE DOOR FAIL TO ILLUMINATE. R & R EMERGENCY LIGHT BULB LIGHT AFT OF SERVICE DOOR IAW AMM 33-51-15, OPERATIONS CHECKED GOOD.

Part: CIRCUIT BREAKER — FAILED (ELECTRICAL SYS) · airframe 26,984 hrs · 19,205 cycles

TOTAL AIR TEMPERATURE PROBE HEAT CAUTION RIGHT AFTER TAKEOFF. GEAR IN TRANSIT WOW AOM VOL 1 EMERGENCY ABNORMAL PROCEDURES COMPLIED WITH. FOUND BAD CB A12 IN CBP1. R & R CB A12 IN CBP1 IAW CRJ ESPM 20-25-05.

Part: MOUNT BRACKET — BROKEN (FLASHLIGHT) · airframe 26,884 hrs · 19,148 cycles

AFT CABIN FLASHLIGHT MOUNTING BRACKET IS BROKEN. R & R FLIGHT ATTENDANT`S NR 1 FLASHLIGHT IAW CRJ-700 AMM-25-61-02.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 26,774 hrs · 19,078 cycles

SLATS FAIL CAUTION MESSAGE DECLARED EMERGENCY.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 25,675 hrs · 18,379 cycles

RIGHT EMERGENCY EXIT LIGHT INOPERATIVE. R & R BULBS IAW AMM 33-51-05; OPS CHECKED GOOD.

Part: DRAG ANGLE — CRACKED (VERTICAL STAB) · airframe 25,150 hrs · 18,035 cycles

DURING 3 C CHECK FOUND LEFT VERTICAL STABILIZER FORWARD AND AFT DRAG ANGLES AT FS1181.00 ARE CRACKED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED FORWARD AND AFT DRAG ANGLES IAW EO CR-53MR-164 AND CR-53MR-053. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CROSSMEMBER — CRACKED (FUSELAGE) · airframe 25,150 hrs · 18,035 cycles

DURING 3 C CHECK FOUND THE LEFT SIDE OF CROSSMEMBER AT FS 280.00 CRACKED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPLACED LEFT SIDE OF CROSSBEAM AT FS 280.00 IAW STRUCTURAL REPAIR MANUAL 51-42-06 AND 51-42-10. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 25,150 hrs · 18,035 cycles

DURING 3 C CHECK FOUND STRINGER 26 RIGHT CORRODED BETWEEN FS 333.00 AND FS 364.00. THE AIRCRAFT WAS REMOVED FROM SERVICE. LEVEL OF CORROSION NOT SPECIFIED. REMOVED AND REPLACED STRINGER 26 RIGHT FROM FS 333.00 TO 364.00 IAW SRM 51-42-06. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: DOOR — DAMAGED (CARGO BAY) · airframe 25,150 hrs · 25,150 cycles

DURING 3 C CHECK FOUND FRAME ON FORWARD CARGO DOOR TO HAVE SEVERAL MISDRILLED HOLES. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED FORWARD CARGO DOOR IAW EO CR-52MR-169. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 25,150 hrs · 18,035 cycles

DURING 3 C CHECK FOUND STRINGER 26 RIGHT CORRODED BETWEEN FS 319.70 AND FS 333.00. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED STRINGER IAW CRJ 700 STRUCTURAL REPAIR MANUAL 51-42-06, 51-42-20 AND EO CR-53MR-333. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 25,367 hrs · 18,175 cycles

DURING MX INSP FOUND THE EMERGENCY LIGHT IN CEILING IN FRONT OF THE LAV DOOR INOPERABLE. THE ACFT WAS REMOVED FROM SERVICE. REMOVED THE CEILING PANEL AND FOUND THE PLUG NOT CONNECTED TO THE PANEL. INSTALLED PLUG AND CEILING PANEL IAW AMM 25-26-05-400-804. THE OPS CHECK OF THE EMERGENCY LIGHT WAS GOOD IAW AMM 33-51-00-710-802. THE ACFT WAS RETURNED TO SERVICE.

Part: LENS — CRACKED (CABIN) · airframe 25,367 hrs · 18,175 cycles

DURING B INSP, FOUND THE EXIT EMERGENCY LIGHT JUST AFT OF PASSENGER DOOR HAS A CRACKED LENS. THE ACFT WAS REMOVED FROM SERVICE. R & R THE EXIT EMERGENCY LIGHT JUST AFT OF PASSENGER DOOR IAW AMM 33-51-15. THE ACFT WAS RETURNED TO SERVICE.

Part: HOLDER — BROKEN (COCKPIT) · airframe 24,232 hrs · 17,461 cycles

ON FLIGHT 3775 THE CREW REPORTED THE CAPTAINS EMERGENCY FLASHLIGHT HOLDER LOWER BRACKET BROKEN FLASHLIGHT WILL NOT REMAIN STOWED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CAPTAIN’S FLASHLIGHT HOLDER IAW CRJ700 MM 25-61-02. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BALLAST — FAILED (CABIN LIGHTS) · airframe 23,458 hrs · 16,949 cycles

ON FLIGHT 3753, THE CREW REPORTED A STRANGE ODOR IN THE FLIGHT DECK. IT SMELLED LIKE SOMETHING ELECTRIC WAS BURNING. THE ODOR WAS BURNING THE CAPTAIN’S AND FIRST OFFICER’S EYES. THE AIRCRAFT WAS REMOVED FROM SERVICE. INSPECTED AIRCRAFT AND FOUND ENTRANCE LIGHTS DIMMER INOPERABLE AND STRONGLY SMELLING OF BURNT ELECTRONICS. REMOVED AND REPLACED THE DIMMER IAW AMM 33-23-13. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ICE BREAKER — FAILED (MAIN DOOR) · airframe 23,229 hrs · 16,779 cycles

FLIGHT 3847, FLIGHT ATTENDANT REPORTED THE MAIN DOOR WAS HARD TO OPEN AND IT MADE A STRANGE NOISE INSIDE OF DOOR WHEN OPENING AND FELT LIKE SOMETHING WAS LOOSE OR BROKEN WHEN MOVING LEVER. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED MAIN CABIN DOOR ICE BREAK ASSEMBLY IAW AMM 52-11-15. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: ROLLER — LACK OF LUBE (MAIN PAX DOOR) · airframe 23,188 hrs · 16,755 cycles

FLIGHT 3827, PASSENGER DOOR HANDLE BINDING WHEN OPENING FROM INSIDE. AIRCRAFT REMOVED FROM SERVICE. LUBRICATED ROLLERS ON MAIN PASSENGER DOOR REF CMM 52-11-00. NO FURTHER FAULTS NOTED. AIRCRAFT RETURNED TO SERVICE.

Part: FLASHLIGHT — DEFECTIVE (CABIN) · airframe 21,764 hrs · 15,862 cycles

ON FLIGHT 3773 THE CREW REPORTED THE FLIGHT ATTENDANT’S FORWARD FLASHLIGHT WILL NOT STAY IN ITS HOLDER. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FLIGHT ATTENDANT’S FLASHLIGHT ASSEMBLY PER CRJ MM 25-61-02. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: STRIKER — CHAFED (FUSELAGE) · airframe 19,731 hrs · 14,520 cycles

DURING MAINTENANCE BASE VISIT FOUND THE PASSENGER DOOR FORWARD SEAL STRIKER CHAFED BELOW UPPER FRAME ROLLER. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED IAW EO CR-53MR-238. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,731 hrs · 14,520 cycles

DURING MAINTENANCE BASE VISIT FOUND THE LEFT LOWER WEB CORRODED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT LOWER WEB IAW EO CR-53MR 174. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,731 hrs · 14,520 cycles

DURING MAINTENANCE BASE VISIT FOUND BOTH HALVES OF FRAME 280 CORRODED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED IAW EO-CR-53MR-219. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,731 hrs · 14,520 cycles

DURING MAINTENANCE BASE VISIT FOUND THE TOP FLANGE OF TRANSVERSE FLOORBEAM AT FRAME 280 CORRODED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED THE CORROSION IAW EO CR-53MR-219. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SEAL — BROKEN (RT ENGINE) · airframe 17,870 hrs · 13,384 cycles

ON FLIGHT 3830 UPON SINGLE ENGINE TAXI WITH THE LEFT ENGINE RUNNING SMOKE IN COCKPIT AND CABIN. AIRCRAFT REMOVED FROM SERVICE. FOUND NR 2 ENGINE HYDRAULIC PUMP SEAL BROKE AND LEAKING. REMOVED AND REPLACED NR 2 HYDRAULIC PUMP. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CABLE — FAILED (ALTIMETER) · airframe 10,567 hrs · 7,807 cycles

APPROXIMATELY 1500 FEET RECEIVED GROUND PROXIMITY AURAL DESCENT/SINK WARNING, RETURNED TO DFW. REMOVED AND REPLACED ALTIMETER CABLE IAW CRJ 34-44-00. OPERATIONAL CHECK GOOD - AIRCRAFT RETURNED TO SERVICES.

Part: CONTROL UNIT — FAILED (ANTI SKID SYS) · airframe 10,168 hrs · 7,454 cycles

ANTI-SKID INOP ON LANDING. REMOVED ANTI-SKID CONTROL UNIT. OPERATIONAL CHECKS GOOD IAW CRJ AMM. RETURNED AIRCRAFT TO SERVICE.

Part: DOOR — UNSECURE (GROUND POWER) · airframe 9,746 hrs · 7,177 cycles

HEARD DULL THUMP FOLLOWED BY SQUEAL DURING AIRCRAFT ROTATION, POST FLIGHT INSPECTION REVEALED GROUND POWER UNIT DOOR NOT SECURED. INSPECTED FUSELAGE AROUND EXTERNAL ELECTRICAL RECEPTACLE AND FOUND NO DAMAGE. SECURED DOOR, RETURNED AIRCRAFT TO SERVICE.

Part: SEAL — LEAKING (ESCAPE HATCH) · airframe 9,095 hrs · 6,742 cycles

MULTIPLE WARNING AND STATUS MESSAGE WITH STAB TRIM RUNAWAY. POST INSPECTION FOUND EMERGENCY ESCAPE HATCH LEAKING. RESEALED ESCAPE HATCH PER AMERICAN EAGLE ENGINEERING TECHNICAL NOTICE CR-52-018 WITH NO LEAKS NOTED. PERFORMED MULTIPLE SYSTEM OPERATIONAL CHECKS IAW CRJ AMM 28-23-02, 31-41-04, 27-50-00, 71-00-00 AND 27-61-05 WITH NO DEFECTS. AIRCRAFT PERFORMED FUNCTIONAL CHECK FLIGHT WITH NO DISCREPANCIES NOTED. AIRCRAFT RETURNED TO SERVICE.

Part: COFFEEMAKER — DIRTY (GALLEY)

RUBBER BURNING SMELL BY SEAT 1B. FOUND SMELL TO BE COMING FROM BURNED COFFEE ON COFFEE HOT PLATE. REMOVED BURNED COFFEE FROM HOT PLATE. OPERATIONAL CHECK GOOD. RETURNED AIRCRAFT TO SERVICE. (M)

Part: HOSE — RUPTURED (OXYGEN SYS)

FLT 3543 - DFW - AN OXYGEN LEAK FROM OBSERVERS MASK AND DEPLETED ALL THE OXYGEN. TROUBLESHOT, FOUND OXYGEN LINE BEHIND OBSERVERS 02 MASK RUPTURED. REPLACED LINE IAW MM 35-11-03. INSTALLED SERVICEABLE CREW 02 BOTTLE IAW MM 35-11-03. NO LEAKS NOTED AT THIS TIME. AIRCRAFT RETURNED TO SERVICE. (M)

Part: LIGHT — SHORTED (COCKPIT)

LIT - FLT 3774 - DURING CRUISE FLIGHT, THE CRWE REPORTED SMOKE IN THE COCKPIT COMING FROM THE CAPTAINS FLOODLIGHT. FLOODLIGHT STOPPED SMOKING WHEN IT WAS TURNED OFF. MAINTENANCE REPLACED THE FLOODLIGHT IAW CRJ MM. AIRCRAFT WAS THEN RETURNED TO SERVICE. (M)