N516AE

Part: FAIRING — MISSING (ZONE 600 FLAP) · airframe 47,757 hrs · 36,662 cycles

RH INBOARD 2ND FLAP FAIRING MISSING, LOST IN FLIGHT / REMOVED WHAT WAS LEFT OF PANEL 686BB ON RH WING INBD FLAP IAW CRJ 700 AMM 57-51-84-000-802-A01.

Part: PCU — FAULTED (SPOILERS) · airframe 45,273 hrs · 34,591 cycles

OB FLT SPLRS AND OB SPOILERONS CAUTION MSG IN FLIGHT / T/S PER CRJ 700 FIM 27-64-01-810-807-A01-PSA, FAULT DID NOT RETURN. OPS TEST GOOD IAW CRJ 700 AMM 27-64-00-710-801-A01. REMOVED AND REPLACED LH OB MFS PCU IAW CRJ700 AMM27-62-01-000/400-801-A01-PSA. OPS AND LEAK CHECK GOOD

Part: COMPENSATOR — UNSERVICEABLE (100) · airframe 44,630 hrs · 34,051 cycles

AUTO XFLOW INHIB STATUS CLIMBING THRUGH 16000 FT. LOST LEFT FUEL TANK AND TOTAL FUEL INDICATION. / REMOVED AND REPLACED LH WING FUEL QUANITY PROBE 6 IAW CRJ AMM 28-41-09-000/400-801

Part: TRACK — BROKEN · airframe 42,898 hrs · 32,523 cycles

RH UPPER IB TRANSCOWL NYLON TRACK IS BROKEN. PERFORMED EA21-C7-78-710 AS TEMPORARY CORRECTIVE ACTION WITH EDDY CURRENT INSPECTION OF RH UPPER HINGE BEAM TRACK INSERT FASTENER HOLES IN ACCORDANCE WITH NDTM 51-20-006. NO CRACKS FOUND. PERFORMED REO 670-78-30-921 ON THE RH UPPER HINGE BEAM TRACK FASTENER HOLES IAW REO INSTRUCTIONS. THIS TERMINATES EA21-C7-78-710. NO FURTHER ACTION REQUIRED.

Part: SPOILER SYS — MALFUNCTIONED · airframe 41,832 hrs · 31,591 cycles

ON FINAL APPROACH INTO CLT, THE AIRCRAFT OB SPOILERONS AND OB FLIGHT SPOILERS FAILED. THE FLIGHT CREW DECLARED EMERGENCY, AND LANDED THE AIRCRAFT SAFELY. EMERGENCY VEHICLES ROLLED, HOWEVER THEY WERE NOT NEEDED AS THE CREW CANCELLED THE EMERGENCY ONCE THEY WERE ON THE GROUND SAFELY. MX IS INBOUND TO INSPECT THE PROBLEM SYSTEMS, NOTHING FURTHER TO REPORT. RECEIVED OUTBOARD SPOILERONS AND OUTBOARD FLIGHT SPOILERON CAUTION WHEN DEPLOYING FLIGHT SPOILERS. / TROUBLESHOT SSCU 1 PER FIM CRJ 700 FIM 27-61-05-810-818. NO FAULTS SHOWN. OPS CHECK GOOD. PERFORMED SPOST 1 & 2 IAW CRJ 700 AMM 27-61-05-740-801. OPS CHECK GOOD.

Part: VALVE — STUCK (PRESSURE RELIEF) · airframe 41,627 hrs · 31,393 cycles

AFTER TAKE OFF FROM CLT THE CREW REPORTED A FUEL LEAK TO DISPATCH. THE CREW RETURNED THE FLIGHT TO CLT AND DECLARED A FUEL EMERGENCY. THEY LANDED SAFELY AND TAXIED TO THE GATE. THEY DID NOT LAND OVERWEIGHT. THE AIRCRAFT IS CURRENTLY IN MAINTENANCE. / CREW REPORTS A RAPID LOSS OF FUEL AFTER TAKE OFF / UPON INSPECTION FOUND THE L/H WING MAIN TANK RELIEF VALVE STUCK OPEN. R&R RELIEF VALVE.

Part: WINDSHIELD — SMOKE (COCKPIT) · airframe 41,421 hrs · 31,213 cycles

SINGLE PUFF OF SMOKE FROM CENTER FRONT WINDSHIELD. PERFORMED GVI/DAMAGE CHECK OF WINDSHIELDS IAW CRJ 700 AMM 56-11-01-210-801-PSA AND OPS CHECKED WINDSHIELD HEAT IAW CRJ 700 AMM 30-41-06-710-801, NO SIGNS OF DAMAGE OR FAULTS FOUND.

Part: WINDSHIELD — UNSERVICEABLE (COCKPIT) · airframe 41,421 hrs · 31,214 cycles

AFTER TAKEOFF THE CREW STARTED TO SEE SMOKE ALONG THE FLIGHT DECK WINDOWS. THEY DECLARED EMERGENCY AND TURNED AROUND TO RETURN TO CLT. CAPTAIN DID NOT SPECIFY WHETHER OR NOT THEY WERE OVERWEIGHT ON LANDING. PASSENGERS DID NOT BRACE. FLIGHT RETURNED TO E19 AND PASSENGERS ARE DEPLANING NORMALLY. NO FURTHER INFORMATION AT THIS TIME. / INSPECTED WINDSHIELD AND WINDOW TERMINAL BLOCKS FOR EVIDENCE OF BURNS. NO DEFECTS NOTED. PERFORMED WIRING INTEGRITY CHECK OF LH SIDE IAW TO 30-079-005-21. C/W WIRING INTEGRITY CHECK OF RH SIDE IAW TO 30-079-006-21. NO DEFECTS NOTED. REMOVED AND REPLACED WINDSHIELD TEMPERATURE CONTROLLER IAW CRJ 700 AMM 30-41-06-000/400-801. OPS TEST GOOD.REMOVED AND REPLACED CAPTAIN'S WINDSHIELD IAW CRJ700 AMM 56-11-01-000/400-801. OPS CHECKED GOOD NO DEFECTS NOTED. WINDOW HEAT CONTROLLER 1659-1-1 SN: 3684 LH WINDSHIELD 601R33033-27 SN: 19091H8549

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,077 hrs · 30,697 cycles

REMOVED CORROSION AT F.S. 319 STR 27 MATERIAL LOST .001 FOUND WITHIN LIMITS IAW CRJ-700 SRM 53-21-06. TREAT AND PRIME IAW SRM 51-21-11 (LEVEL 2 CPCP)

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,077 hrs · 30,697 cycles

REPAIRED FRAME AT F.S. 517 BETWEEN STR 24L - 24R IAW EA21-C7-53-111. (LEVEL 2 CPCP) LEVEL 2 CORROSION.

Part: DRAG ANGLE — CORRODED (VERTICAL STAB) · airframe 40,837 hrs · 30,697 cycles

REPAIRED L/H DRAG ANGLE/AFT END @VERTICAL STABILIZER IAW BEMBARDRER REO 670-55-31-018

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,837 hrs · 30,697 cycles

BLEND OUT CORROSION IAW CRJ-700 SRM 51-21-06 AND EA 21-C7-53-139. RESTORED FINISH IAW CRJ-700 SRM 51-21-11, 51-25-01 & EA 21-C7-53-139. LEVEL 2 CORROSION.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 40,832 hrs · 30,692 cycles

IN FLIGHT TOXIC ODOR WAS NOTICED MAKING IT DIFFICULT TO BREATH ODOR CONTINUED THROUGHOUT ENTIRE FLIGHT FLIGHT DECK ONLY. PRESSURIZED LT AND RT PACK WITH APU AND RT ENGINE, IAW CRJ 700 AMM 21-50-00-862-801-A02 AND 21-50-00-862-805-A01, NO ABNORMAL SMELL NOTED. SEE LOGBOOK 18748 06 1 FOM.

Part: CONTROL VALVE — ABNORMAL (THRUS REVERSERS) · airframe 40,742 hrs · 30,606 cycles

RTO-TAKING OFF RWY 6 IN ERI AT 40KTS THE CREW RECEIVED A RT THRUST REVERSER UNSAFE AMBER MESSAGE AND ABORTED TAKEOFF. CREW RETURNED TO GATE.

Part: RELAY — ABNORMAL (THRUST REVERSERS) · airframe 40,688 hrs · 30,556 cycles

THE FLIGHT WAS TAKING OFF RWY 31 IN PIA AT 30KTS THE CREW RECEIVED A RT REVERSE UNSAFE CAUTION MESSAGE AND ABORTED TAKEOFF AND RETURNED TO GATE. DEF RT THRUST REVERSER SYSTEM, PER MEL 78-30-01 CAT C. M/FUNCTION C/W. DEACTIVATED THE RT THRUST REVERSER, IAW CRJ 700 AMM 78-30-00-040-801-A01 AND ISOLATED THE TRAS, IAW CRJ 700 AMM 78-32-00-910-801-A01. REMOVED AND REPLACED K28, JB-5 RELAY, IAW CRJ 700 AMM 24-03-09-000/400-801-A02. OPERATIONS TEST GOOD AT THIS TIME. THIS CLEARS MEL. PERFORMED OPERATIONS CHECK OF RT THRUST REVERSER, IAW CRJ700 AMM 78-30-00-720-801-A01. OPERATIONS CHECK GOOD.

Part: WARNING MESSAGE — ILLUMINATED (THRUST REVERSERS) · airframe 40,638 hrs · 30,509 cycles

REJECTED TAKEOFF FOR A RT THRUST REV UNSAFE CAUTION MESSAGE AT THE VERY BEGINNING OF THE TAKEOFF ROLL, LESS THAN 10 KNOTS. AIRCRAFT EXITED THE RUNWAY WITHOUT ISSUE AND RETURNED TO GATE WHERE MAINTENANCE HAS BEEN CALLED TO INSPECT AND TO POTENTIALLY DEFER THE RT THRUST REVERSER.

Part: LOOP — UNSECURE (RT WG ANTI ICE V) · airframe 40,492 hrs · 30,380 cycles

RESECURED BLEED LOOP AROUND RT WING ANTI-ICE VALVE. OPERATIONS AND LEAK CHECK GOOD, IAW CRJ 700 AMM 30-12-00-710-802-A02 AND AMM 36-21-00-710-801-A01.

Part: SEAL — LEAKING (HEAT EXCHANGER) · airframe 40,453 hrs · 30,343 cycles

FOUL SMELL FROM VENT IN COCKPIT. PERFORMED GVI OF RT AC PACK. FOUND AIR LEAK ON HEAT EXCHANGER PERI-SEAL/CONNECTOR. REPLACED PERI-SEAL. OPERATIONS AND LEAK CHECK GOOD. NO FURTHER DEFECTS NOTED AT THIS TIME.

Part: A/C PACK — ODOR · airframe 40,420 hrs · 30,310 cycles

OILY SMELL COMING FROM THE PACKS. INVESTIGATED OIL SMELL COMING FROM PACKS. COULD NOT REPLICATE PROBLEM. FOUND NO DEFECTS AT THIS TIME. OPS CHK OF A/C SYS SOURCING FROM APU & BOTH ENG ABOVE IDLE. NO ODORS DETECTED AT THIS TIME.

Part: ACM — FAILED (LEFT) · airframe 40,411 hrs · 30,302 cycles

FOUL ODOR COMING FROM PACKS. TROUBLESHOT PER FIM. INSPECTED APU AND LOAD CONTROL VALVE, FOUND NO EVIDENCE OF OIL CONTAMINATION. RAN PACKS IN ALL BLEED CONFIGURATIONS WITH AND WITHOUT ENGINES AND DETERMINED SMELL TO BE PREVALENT WITH LT PACK. SUSPECT LT ACM TO BE FAULTY. DEFERRED LT PACK. REMOVED AND REPLACED LT ACM, IAW CRJ700 AMM. OPS AND LEAK CHECK GOOD. NO SMELL NOTED AT THIS TIME, THIS CLEARS MEL.

Part: ACM — FAILED (AC BAY) · airframe 40,022 hrs · 29,960 cycles

CABIN FILLED WITH SMOKE FOLLOWED BY RT PACK AUTO FAIL WHILE AT GATE. MAINTENANCE REMOVED AND REPLACED THE AIR CYCLE MACHINE.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 38,068 hrs · 28,238 cycles

DURING CRUISE AT FL330, CA WINDSHIELD CRACKED. EMERGENCY DECLARED FOR PRIORITY DESCENT AND FLIGHT DIVERTED INTO CLT. CA STATED THE INNER LAYER OF THE WINDSHIELD PEELED OFF AND LANDED ON HIS LAP. FLIGHT LANDED ON RWY 18L IN CLT AND CANCELLED THE EMERGENCY AFTER LANDING. FLIGHT WAS ABLE TO TAXI TO GATE E16. MX REPLACED LT WINDSHIELD.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 36,604 hrs · 26,875 cycles

LBL 9 FLOOR SEAT TRACK SEGMENTS FS 517 TO FS 581 AND FS 581 TO 683 ARE CORRODED. REMOVED SEAT TRACKS, FABRICATED NEW SEAT TRACKS AND INSTALLED IAW AMM 53-00-49 AND REO 670-53-00-343 REV M.

Part: FITTING — CRACKED (FUSELAGE) · airframe 36,604 hrs · 26,875 cycles

FS 280 CROSSBEAM TO RBL 9 FLOORBEAM T FITTING IS CRACKED ON IB SIDE. FABBED & REINSTALLED 2 EA NEW ATTACH ANGLES AT FS 280 RBL 9.0 IAW SRM 51-42-21-001-001-A01 AND REO 670-53-11-165 REV B.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 36,604 hrs · 26,875 cycles

PAX DOOR SURROUND STRUCTURE CENTER FLOORBOARD SUPPORT ANGLE AND SILL ANGLE HAS CORROSION AT SCREW HOLES. REMOVED AND REPLACED SILL ANGLE SH670-31875-3 IAW SRM 51-42-06-001-001-A01, AND 51-42-21-001-001-A01.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 36,604 hrs · 26,875 cycles

RBL 9 FLOOR SEAT TRACK SEGMENTS FS 349 TO FS 485 AND FS 581 TO 683 ARE CORRODED. REMOVED SEAT TRACKS, FABRICATED NEW SEAT TRACKS AND INSTALLED IAW AMM 53-00-49 AND REO 670-53-00-343 REV M.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 34,657 hrs · 25,107 cycles

CREW REPORTED AP LWD CAUTION MSG. CREW DIVERTED TO BMH. MAINTENANCE INSPECTED FLIGHT CONTROL CABLES NO DEFECTS NOTED. DEFERRED AUTO PILOT.

Part: SKIN — DAMAGED (BS 969-985) · airframe 34,480 hrs · 24,943 cycles

DURING HEAVY MAINTENANCE, DAMAGE WAS FOUND TO THE EXTERIOR FUSELAGE SKIN BETEWEEN BS 969 AND 985, STRINGER 27L. REPAIRED THE SKIN IAW ERS-CR-53MR-2905.

Part: CROSSBEAM — CRACKED (BS 280) · airframe 34,480 hrs · 24,943 cycles

FRAME BS 280 LT SIDE CROSSBEAM CRACKED ON FWD SIDE BELOW CENTER COCKPIT FLOORBOARD. A NEW CROSSBEAM WAS INSTALLED IAW SRM 51--42-06, SRM 51-42-10, AND SRM 51-42-13.

Part: LINE — DAMAGED (HYD SYSTEM) · airframe 33,068 hrs · 23,826 cycles

DURING TAXI IN, LOST OF NOSE WHEEL STEERING HYDRAULIC SYSTEM NR 3 LOW PRESSURE AND ZERO QUANITY IN THE SYSTEM NR 3 RESEVOIR. REMOVED AND REPLACED THE REAR FLEXIBLE HYD HOSE FOR NLG RETRACT ACTUATOR IAW AMM 32-32-09. OPS AND LEAK CHECKED GOOD.

Part: CONNECTOR — LOOSE (CABIN) · airframe 32,671 hrs · 23,507 cycles

LAST TWO EMERGENCY DOME LIGHTS IN THE CABIN WILL NOT ILLUMINATE. FOUND LOOSE CONNECTOR ON EPSU 4. RE-SEATED CONNECTOR IAW ELECTRICAL STANDARD MTX PRACTICES. OPS CK GOOD. A/C OK FOR SERVICE

Part: PCU — MALFUNCTIONED (SPOILER) · airframe 31,438 hrs · 22,573 cycles

ON DESCENT, OTBD SPOILERONS, & OTBD FLIGHT SPOILERS", CAUTION MSGS. INTERROGATED MDC, FOUND, ROB MFS PCU FAILED PCU JAM. PERFORMED SPOST 1 RESET. PERFORMED OPERATIONS CHECK IAW ETN CR-27-093. OPERATIONS CHECKED GOOD. OPENED TDMI 516T2745 TA. R & R ROB MFS PCU IN 10 DAYS. TRANSFERRED TO MIC SHEET.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 31,246 hrs · 22,436 cycles

EMERGENCY LIGHTS AFT OF FIRST CLASS INOPERATIVE. R & R EPSU BATTERY PACK & CHARGER NR 3 IAW WC 33-002. OPERATIONAL TESTED GOOD. BATTERY CHARGER ASSEMBLY PN 11-0049 & SN 12337.

Part: HINGE FITTING — WORN (VERTICAL STAB) · airframe 31,074 hrs · 22,296 cycles

RUDDER 2, UPPER CTR, & NR 3, LOWER CENTER, HINGE FITTING BEARINGS ON VERTICAL STABILIZER HAS PLAY. R & R RUDDER NR 3, LOWER CTR, HINGE FITTING ON VERTICAL STAB IAW ETN CR-55-026 & NR 2, UPPER CTR, NR 2 RUDDER, PN AV670-21081-015.

Part: BULKHEAD — CORRODED (FUSELAGE) · airframe 31,074 hrs · 22,296 cycles

RIGHT LOWER BULKHEAD WEB AT FS 280.00 CORRODED. COMPLIED WITH EO CR-53MR-174 INSTALLATION OF CROSSBEAM AT FS 280.00.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 31,074 hrs · 22,296 cycles

STRINGER 19 LT CORRODED, BETWEEN FS 310.00 & 333.0. COMPLIED WITH REPAIR OF STRINGER 19 LT CORRODED, BETWEEN FS 310.00 & 333.00, IAW ERS-CR-53MR-1963.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 31,074 hrs · 22,296 cycles

L BRACKET OTBD OF RBL 9.00 & ATTACHED TO THE FWD SIDE OF FLOORBEAM FS-280.00 IS CRACKED, APPROX 1 INCH. REPLACED L BRACKET IAW SRM 51-42-06.

Part: PANEL — CRACKED (PAX DOOR) · airframe 31,074 hrs · 22,296 cycles

DURING REPAIR OF SECTION OF AFT DRAG ANGLE, FOUND PAX DOOR AFT SIDE PANEL TO BE CRACKED ON LOWER EDGE OF PANEL, AT THE OTBD STIFFENER FOR THE PAX DOOR POWER ASSIST MOTOR ASSEMBLY. CRACK IS APPROX 1/2" LONG. REPAIRED PAX DOOR AFT SIDE PANEL ON LOWER EDGE OF PANEL IAW ERS-CR-5200-505.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 31,074 hrs · 22,296 cycles

LEFT T BRACKET ON FLOORBEAM FS 280.00 CRACKED. R & R LT T BRACKET ON FLOORBEAM FS280.00 IAW SRM 53-11-41-201-001.

Part: ATTACH ANGLE — CRACKED (PAX DOOR) · airframe 31,074 hrs · 22,296 cycles

PASSENGER DOOR AFT STEP SKIN ATTACH ANGLE IS CRACKED BY PULLEY BRACKET. ATTACH ANGLE, DRAG ANGLE, REPAIR INCORPORATED INTO ANOTHER AREA REPAIR. REPAIRED PAX DOOR AFT SIDE PANEL ON LOWER EDGE OF PANEL IAW ERS-CR-5200-505.

Part: STEP — CRACKED (PAX DOOR) · airframe 31,074 hrs · 22,296 cycles

PASSENGER DOOR AFT STEP SKIN IS CRACKED AT STOW CUP, VERTICAL & HORIZONTAL FLANGES. REPAIRED IAW SRM 52-11-04.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 31,074 hrs · 22,296 cycles

FLOOR PANEL SUPPORT ON FLOORBEAM FS 280.00 IS CRACKED. DRILLED & INSTALLED NEW FLOOR PANEL SUPPORT ON FLOORBEAM FS 280.00 IAW SRM 51-42-06.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 31,074 hrs · 22,296 cycles

RIGHT T BRACKET ON FLOORBEAM FS 280.00 CRACKED. R & R RT T BRACKET ON FLOORBEAM FS 280.00 IAW SRM 53-11-41-201-001.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 31,074 hrs · 22,296 cycles

FLOORBEAM AT FS 280.00 CORRODED & RT SIDE CRACKED. R & R RT SECTION OF FLOORBEAM AT FS 280-00 IAW SRM 53-11-41.

Part: STEP — CRACKED (PAX DOOR) · airframe 31,074 hrs · 22,296 cycles

PASSENGER DOOR FWD STEP SKIN IS CRACKED AT STOW CUP, VERTICAL & HORIZONTAL FLANGE. REPAIRED IAW SRM 52-11-04.

Part: SELECTOR VALVE — FAILED (LANDING GEAR) · airframe 30,297 hrs · 21,657 cycles

PROXIMITY SYSTEM CAUTION. R & R LG SELECTOR VLV IAW AMM 32-32-10. COMPLIED WITH LG OPERATIONS CHECK IAW AMM 32-30-00. FOUND SATISFACTORY AT THIS TIME.

Part: STRINGER — DAMAGED (PAX DOOR) · airframe 29,813 hrs · 21,254 cycles

REPAIR MAIN PAX DOOR TO LINTEL STRINGER 3. PERFORMED MAJOR REPAIR TO LINTEL STRINGER 3 OF MAIN PAX DOOR BY INCORPORATING SB 670BA-53-040 REV C.

Part: FLASHLIGHT — BROKEN (COCKPIT) · airframe 29,784 hrs · 21,235 cycles

FIRST OFFICERS FLASHLIGHT BROKEN. R & R FIRST OFFICERS FLASHLIGHT IAW SMP. OPERATIONS CHECKED GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 29,767 hrs · 21,219 cycles

EMERGENCY LIGHTS BATTERY PACK AT PS35P1 IS DISCHARGED. R & R BATTERY PACK AT PS35P1 IAW AMM 33-51-17. OPERATIONS CHECKED GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 29,767 hrs · 21,219 cycles

EMERGENCY LIGHTS BATTERY PACK AT PS38P1 IS DISCHARGED. R & R BATTERY PACK AT PS38P1 IAW AMM 33-51-17. OPERATIONS CHECKED GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 29,767 hrs · 21,219 cycles

EMERGENCY LIGHTS BATTERY PACK AT PS36P1 IS DISCHARGED. R & R BATTERY PACK AT PS36P1 IAW AMM 33-51-17. OPERATIONS CHECKED GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 29,767 hrs · 21,219 cycles

EMERGENCY LIGHTS BATTERY PACK AT PS37P1 IS DISCHARGED. R & R BATTERY PACK AT PS37P1 IAW AMM 33-51-17. OPERATIONS CHECKED GOOD.

Part: ACM — FAILED (RIGHT) · airframe 29,435 hrs · 20,962 cycles

RIGHT PACK AUTO FAIL CAUTION MESSAGE DISPLAYED MOMENTARILY, FOLLOWED BY CABIN FILLING WITH VISIBLE SMOKE. TROUBLESHOOT RT PACK IAW FIM 216100. FOUND RT ACM INOPERATIVE CAUSING SMOKE. COMPLETED INSTALLATION OF ACM IAW MM 21-51-08. OPS CHECKED GOOD, LEAK CHECKED GOOD.

Part: HOLDER — BROKEN (FLASHLIGHT) · airframe 28,545 hrs · 20,238 cycles

FWD FLIGHT ATTENDANT FLASHLIGHT HOLDER BROKEN. FLIGHT CREW PLACARDED IAW MEL 25-15 M PROCEDURES COMPLIED WITH. R & R FWD FLIGHT ATTENDANT FLASHLIGHT ASSEMBLY IAW AMM 25-61-02. MEL RESTORED.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 28,426 hrs · 20,154 cycles

FIRST OFFICER'S RED CHARGE LIGHT ON FLASHLIGHT IS INOPERATIVE. R & R THE FIRST OFFICER`S FLASHLIGHT IAW AMM 26-61-02. OPERATIONS CHECKED GOOD.

Part: BRAKE — MALFUNCTIONED (NR 3) · airframe 27,693 hrs · 19,563 cycles

AFTER HIGH SPEED TAXI & ABORT, BRAKE TEMPS FOR ALL FOUR BRAKES ROSE TO 04, AFTER APPROX 5 TO 10 MIN NR 3 BRAKE CONTINUED TO RISE TO INDICATION OF 10 ON EICAS. REMAINING BRAKES STAYED AT AN INDICATION OF 05 & LOWER. INSPECTION OF BRAKES NR 3 BRAKE FEELS HOTTER THAN ALL OTHER BRAKES. R & R NR 3 BRAKE ASSEMBLY IAW WC 32-700. OPERATIONS CHECKED & LEAK CHECKED GOOD AT THIS TIME.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 27,015 hrs · 19,145 cycles

FOUND LT REAR EXTERIOR EMERGENCY LAMP INOPERATIVE. R & R LT REAR EXTERIOR EMERGENCY LAMP IAW AMM 33-51-15, OPERATIONS CHECKED GOOD.

Part: STRINGER — CHAFED (FUSELAGE) · airframe 26,920 hrs · 19,080 cycles

TRANSFERRED FROM AML PAGE 3358971 ITEM 3. TRANSFERRED FROM NRWC 516-XNA-01631 ITEM 1. STRINGER 7L, 6 1/2 INCHES FWD OF FS 1162.00 HAS CHAFE DAMAGE. REPAIRED STRINGER 7L FWD OF FS 1162.00 IAW ERS CR-53MR-359.

Part: UNKNOWN — MALFUNCTIONED (CABIN PRESSURE) · airframe 26,547 hrs · 18,828 cycles

PRESSURE INOPERATIVE AT 340. PERFORMED OPERATIONAL & FUNCTIONAL TEST OF THE CABIN PRESS CONTROLLERS IAW MM CHAPTER 21-31-04 & OPERATIONAL CHECK OF CABIN PRESS CONTROL PANEL IAW MM CHAPTER 21-33-01. ALL OPERATIONAL & FUNCTIONAL CHECKS CHECKED GOOD. MEL ITEM RESTORED.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 26,553 hrs · 18,833 cycles

DURING PS 1 CHECK INSPECTION, FOUND RT AFT EXTERNAL EMERGENCY LIGHT WILL NOT ILLUMINATE. R & R BULB IN RT AFT EXTERNAL EMERGENCY LIGHT IAW CMM 33-52-06. OPERATIONS CHECKED GOOD IAW AMM 33-51-15.

Part: STRUCTURE — DAMAGED (FUSELAGE) · airframe 26,431 hrs · 18,757 cycles

DURING MAINTENANCE INSPECTION ON FLIGHT 2776 FOUND DAMAGE IN RVSM AREA ON RT SIDE. AIRCRAFT WAS REMOVED FROM SERVICE. RVSM ADL WORK SHEET AND GEOMECTRIC CONTOUR ANALYSIS APPROVAL SHEET INSTALLED AS REQUIRED. MEL RESTORED.

Part: STRUCTURE — DAMAGED (FUSELAGE) · airframe 26,412 hrs · 18,743 cycles

DURING MAINTENANCE INSPECTION FOUND DAMAGES TO O2 SERVICE DOOR SURROUND AREA. AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED AREA AROUND O2 SERVICING DOOR SURROUNDING AREA IAW ERS-CR-53MR-154.

Part: TRU — FAULTY (NR 2) · airframe 26,412 hrs · 18,743 cycles

TRU 2, PS32, HAD SMOKE COMING OUT OF COOLING FAN. R & R TRU 2 IAW CRJ700 24-31-01-400-801. OPERATIONS CHECKED GOOD.

Part: COFFEEMAKER — ODOR (GALLEY) · airframe 26,076 hrs · 18,540 cycles

COFFEE MAKER EMITTING SUSPICIOUS ODOR. SPECIFICALLY THE RT COFFEE MAKER. REMOVED, CLEANED & REINSTALLED COFFEE MAKERS 1 & 2. OPS CK NORMAL REF AMM 25-32-06

Part: CROSSBEAM — CORRODED (BS 280) · corrosion level 2 · airframe 25,216 hrs · 25,216 cycles

DURING 3C CHECK, FOUND RT SIDE OF CROSSBEAM AT BS 280 TO BE CORRODED. THE ACFT WAS REMOVED FROM SERVICE. REPAIRED CROSSBEAM IAW SRM 51-42-06. ACFT RETURNED TO SERVICE.

Part: LIGHT — DAMAGED (CABIN) · airframe 25,211 hrs · 17,959 cycles

EMERGENCY LIGHT DAMAGED FROM FS 847 TO 939. R & R EMERGENCY LIGHT IAW ETN-CR-33-004.;

Part: TIRE — FAILED (MLG) · airframe 25,048 hrs · 17,842 cycles

DURING TAKEOFF ROTATION, LEFT ENGINE FAN VIBRATION WENT INTO AMBER RANGE. DECLARED AN EMERGENCY AND DIVERTED. LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. ON POST FLIGHT INSPECTION, FOUND THE LEFT INBD TIRE WAS MISSING TREAD. R & R TIRE NR 2 IAW 32-002. NO FURTHER DEFECTS NOTED.

Part: GUARD — BROKEN (GALLEY) · airframe 24,229 hrs · 17,326 cycles

ON FLIGHT 4600 THE CREW REPORTED THE EMERGENCY LIGHT GUARD IN THE FORWARD GALLEY WAS BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. INSTALLED NEW GUARD ON FLIGHT ATTENDANT PANEL EMERGENCY SWITCH IAW CRJ AMM 33-23-21. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: HOLDER — BROKEN (FLASHLIGHT) · airframe 24,202 hrs · 17,308 cycles

DURING MAINTENANCE INSPECTION FOUND THE FORWARD FLIGHT ATTENDANT FLASHLIGHT HOLDER BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FORWARD FLASHLIGHT HOLDER IAW CRJ 700 AMM 25-61-02. THE OPERATIONAL CHECK WAS GOOD IAW CRJ 700 AMM 25-61-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: MOUNT BRACKET — BROKEN (COCKPIT) · airframe 23,618 hrs · 16,940 cycles

DURING MAINTENANCE INSPECTION FOUND THE LOWER MOUNTING BRACKET OF CAPTAIN'S FLASHLIGHT HOLDER BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED CAPTAIN’S FLASHLIGHT AND HOLDER IAW CRJ 700 AMM 25-61-02. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: HOLDER — BROKEN (FLASHLIGHT) · airframe 23,315 hrs · 16,729 cycles

ON FLIGHT 2761 THE CREW REPORTED THE FLASHLIGHT HOLDER/BRACKET AT THE NR 2 FLIGHT ATTENDANT STATION WAS BROKEN. DEFERRED AFT F/A FLASHLIGHT HOLDER. REMOVED AND REPLACED THE AFT FLIGHT ATTENDANT FLASHLIGHT ASSEMBLY. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CRADLE — LOOSE (CABIN) · airframe 23,175 hrs · 16,643 cycles

ON FLIGHT 3796 THE CREW REPORTED THE NR 1 FLIGHT ATTENDANT FLASHLIGHT CRADLE WAS LOOSE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FLASHLIGHT CRADLE IAW AMM 25-61-00. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: MOTOR — DEFECTIVE (PAX DOOR) · airframe 23,071 hrs · 16,574 cycles

ON FLIGHT 3839 THE CREW REPORTED THE MAIN PASSENGER DOOR OPENS PART WAY THEN STICKS. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE PASSENGER DOOR MOTOR ASSIST IAW CRJ700 AMM 52-11-08. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SPIGOT — DAMAGED (PAX DOOR) · airframe 22,773 hrs · 16,389 cycles

FLIGHT 3885, CREW REPORTED PASSENGER DOOR IS HARD TO OPEN. AIRCRAFT REMOVED FROM SERVICE. ADJUSTED AND INSTALLED UPPER AFT PASSENGER DOOR LATCH SPIGOT ASSEMBLY IAW AMM 53-21-23. PASSENGER DOOR NOW OPERATES NORMALLY. AIRCRAFT RETURNED TO SERVICE.

Part: BRACKET — LOOSE (FLASHLIGHT) · airframe 22,179 hrs · 15,997 cycles

ON FLIGHT 3656 THE FLIGHT ATTENDANT REPORTED THAT THE FLASHLIGHT ASSEMBLY IN THE REAR CABIN WOULD NOT HOLD THE FLASHLIGHT IN PLACE FOR RECHARGE. THE FLASHLIGHT KEPT FALLING OUT ONTO FLOOR. THE AIRCRAFT WAS REMOVED FROM SERVICE. RE-SECURED AFT FLASHLIGHT AS REQUIRED. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — OUT OF POSITION (SMOKE DETECTOR) · airframe 21,752 hrs · 15,732 cycles

ON FLIGHT 4674 THE CREW REPORTED THE GREEN LIGHT FOR SMOKE DETECTOR IN LAVE DOES NOT LIGHT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPOSITIONED GREEN LED PERFORMED OPERATIONAL CHECK IAW CRJ 700 AMM 26-16-01. THE OPERATIONAL CHECK WAS GOOD NO FURTHER DEFECTS NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 21,610 hrs · 21,610 cycles

DURING MAINTENANCE INSPECTION FOUND THE AFT CABIN FLASHLIGHT INOPERABLE AFTER CHANGING BATTERY. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED FLASHLIGHT IAW CMM 25-60-11. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — MISSING (COCKPIT) · airframe 21,267 hrs · 15,426 cycles

ON FLIGHT 3752 THE CREW REPORTED THE FIRST OFFICER’S FLASHLIGHT WAS MISSING FROM BEHIND THE SEAT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPLACED THE FLASHLIGHT ASSEMBLY IAW CRJ 700 AMM 25-61-02. THE OPERATIONAL CHECK WAS GOOD AT THIS TIME. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: EPSU — INOPERATIVE (CABIN) · airframe 21,187 hrs · 21,187 cycles

DURING MAINTENANCE INSPECTION FOUND THE EMERGENCY LIGHTS ON EPSU NR 4 INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED NR 4 EPSU IAW W/C 33-00. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: PSEU — MALFUNCTIONED (LANDING GEAR) · airframe 20,595 hrs · 15,002 cycles

ON FLIGHT 3867 THE CREW REPORTED THAT UPON SELECTING GEAR UP ON TAKEOFF THEY RECEIVED A WARNING MESSAGE GEAR DISAGREE POSTED ON EICAS. THE CREW WORKED THE CHECKLIST AND ELECTED TO RETURN TO ORD. AN EMERGENCY WAS DECLARED. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE SENSOR PROXIMITY ELECTRICAL UNIT IAW CRJ AMM 32-61-01. THE OPERATIONAL CHECK WAS GOOD OF THE GEAR EXTENSION AND RETRACTION IAW CRJ AMM 32-30-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FITTING — FAULTY (PAX DOOR) · airframe 20,092 hrs · 14,653 cycles

ON FLIGHT 4591 THE NR 1 FLIGHT ATTENDANT WAS UNABLE TO CLOSE THE MAIN CABIN DOOR. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE PASSENGER DOOR HANDRAIL SPRING CLIP IAW AMM 52-11-05. PERFORMED OPERATIONAL CHECK OF THE MAIN DOOR IAW 52-11-00. THE OPERATIONAL CHECK WAS GOOD.

Part: FASTENER — OUT OF POSITION (PAX DOOR)

PAX DOOR HARD TO OPEN. REPOSITIONED HARDWARE OPS CHECK GOOD.

Part: DOOR — OUT OF RIG (CABIN) · airframe 20,030 hrs · 14,619 cycles

MAIN PAX DOOR WILL NOT LOCK. RIGGED DOOR, OPS CHECK GOOD.

Part: SKIN — DENTED (FUSELAGE) · airframe 19,960 hrs · 14,571 cycles

DURIING MAINTENANCE BASE VISIT FOUND A FUSELAGE SKIN DENT AT FS 1162, STRINGER 23 LEFT -24 LEFT. THE AIRCRAFT WAS REMOVED FROM SERVICE. INSTALLED DOUBLED ON AFFECTED AREA IAW EO CR-53MR-245. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,960 hrs · 14,571 cycles

DURING MAINTENANCE BASE VISIT FOUND THE LEFT FRAME 280 WEB HAS CORROSION. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED WITH A SERVICEABLE UNIT IAW EO CR-53MR-174. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BEAM — CRACKED (FUSELAGE) · airframe 19,960 hrs · 14,571 cycles

DURIING MAINTENANCE BASE VISIT FOUND THE LEFT FRAME 280 BEAM CRACKED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED A WITH SERVICEABLE UNIT IAW EO CR-53MR-219. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SPRING — DEFECTIVE (PAX DOOR) · airframe 19,846 hrs · 14,494 cycles

FOR FLIGHT 3601 AFTER THE FLIGHT MAINTENANCE FOUND THE MAIN CABIN DOOR HARD TO OPEN. THE PASSENGER DOOR WOULD NOT OPEN EASILY. FINALLY SEVERAL HARD TUGS ON HANDLE IT OPENED, BUT IT DID NOT CLOSE OR OPEN PROPERLY. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPLACED HOUSING ASSEMBLY PART NUMBER 600-38038-9, BEARING PART NUMBER 600-3840-33, SPRING PART NUMBER LC063F6M, BOLT PART NUMBER NAS565-57 AND NUT PART NUMBER MS21045-5 IAW CRJ 700 AMM 52-11-02-400-831. THE OPERATIONAL CHECK WAS GOOD IAW AMM 52-11-00-710-801. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 17,370 hrs · 12,840 cycles

ON FLIGHT 3728 THE CREW REPORTED THAT THE EMERGENCY LIGHTS WERE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMERGENCY POWER SUPPLY UNIT BATTERY PACKS 1, 2, 3 AND 4 IAW CRJ AMM 33-51-17. SERIAL NUMBERS OF THE BATTERIES ARE: 80165, 104960, 77291, 10493A. THE OPERATIONAL TEST WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: HOLDER — FAULTY (FLASHLIGHT) · airframe 15,476 hrs · 11,436 cycles

ON FLIGHT 3559 THE CREW REPORTED THE FLASHLIGHT AT THE FORWARD FLIGHT ATTENDANT STATION DOES NOT STAY IN THE HOLDER. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE FORWARD FLIGHT ATTENDANT FLASHLIGHT HOLDER ASSEMBLY. AIRCRAFT RETURNED TO SERVICE.

Part: A/C PACK — SMOKE (RIGHT) · airframe 14,031 hrs · 10,329 cycles

ON FLIGHT 3894, CREW REPORTED SMOKE IN THE CABIN. MAINTENANCE TROUBLESHOOT TO RIGHT PACK, ISSUED MEL 21-13.

Part: WINDOW — FAILED (COCKPIT) · airframe 11,890 hrs · 8,637 cycles

ON FLIGHT 3542 - CREW REPORTED THAT IN FLIGHT THAT THE FO’S FORWARD WINDOW SPIDER WEBBED. CREW ELECTED TO DIVERT TO XNA.

Part: DOOR — UNSECURE (CARGO BAY) · airframe 10,729 hrs · 7,777 cycles

CREW NOTED DURING CLIMB OUT THAT COULD NOT PRESSURIZE A/C AND NO WARNING INDICATION, THEY RETURNED TO BNA FOR MTX. AFTER LANDING FOUND THE AFT CARGO DOOR AFT SECTION WAS NOT CLOSED ALL THE WAY. RESECURED CARGO DOOR PERFORMED GVI OF CARGO DOOR AND PERFORMED. OPS CHECK OF DOOR IAW CRJ MM 52-31-00, OPS CHECK GOOD. NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 9,394 hrs · 6,801 cycles

PILOT FRONT WINDSHIELD CRACKED. REMOVED AND REPLACED PILOT FRONT WINDSHIELD IAW CRJ MM. OPERATIONAL CHECKS GOOD. RETURNED AIRCRAFT TO SERVICE.

Part: SENSOR — FAILED (NR 1 ENGINE) · airframe 9,016 hrs · 6,548 cycles

ON CLIMB-OUT RECEIVED AN LEFT ENGINE COWL ANTI-ICE DEGRADE MESSAGE, RETURNED TO ORD. REMOVED AND REPLACED NUMBER ONE ENGINE T2 SENSOR IAW CRJ AMM 77-21-01. OPERATIONAL CHECK GOOD, RETURNED AIRCRAFT TO SERVICE.

Part: WINDOW — CRACKED (COCKPIT) · airframe 8,521 hrs · 6,185 cycles

ON DESCENT, CAPTAIN'S SIDE WINDOW CRACKED NO PRESSURE LOSS. REMOVED AND REPLACED SIDE WINDOW IAW CRJ AMM 56-10-05. PRESSURIZATION CHECK GOOD, AIRCRAFT RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN)

EMERGENCY EXIT LIGHTING INOPERATIVE. REPLACED ALL 4 EMERGENCY EXIT BATTERIES, P/N 20131A FOR ALL S/N`S OFF NR 1 - 85646, NR 2 79267, NR 3 71822, NR 4 85642. (M)

Part: CONTROL UNIT — FAILED (LT THRUST REV)

LT REVERSER UNSAFE CAUTION MSG ILLUMINATED DURING TAKEOFF ROLL. REPLACED THRUST REVERSER ICU IAW AMM 78-32-09. OPERATIONAL CHECKS GOOD AIRCRAFT RETURNED TO SERVICE. (M)

Part: SERVO — MALFUNCTIONED (RT WING)

AIRCRAFT REQUIRED EXCESSIVE TRIM IN FLIGHT. ALSO, HAD AILERON COMPARATOR AND AP MIS-TRIM. RETRIM WITH AP OFF NOT SUCCESSFUL. THEN GOT AP COMPARATOR. WITH AP DISCONNECTED AIRCRAFT BANKED 60 DEGREES RT. IT WAS BROUGHT BACK TO CENTER AND THEN BANKED 60 DEGREES LT. AC WAS UNCONTROLLABLE FOR APPROX 15 SECONDS. REGAINED CONTROL AND DIVERTED. T/S SYS AND FOUND A BAD AILERON SERVO UNIT FOR THE RT SIDE AND THE ALSO COMPLETED A FCF AND PASSED ALL CHECKS. (K)