N536EA

Part: ACM — UNSERVICEABLE (LH ACM) · airframe 29,457 hrs · 22,930 cycles

SMOKE IN COCKPIT AND CABIN WHEN ENGINE WAS SHUT OFF. PILOTS SAID SMELLS LIKE €ŒPACK RELATED SMOKE ISSUE€?. THE LOCATION OF THE SMOKE WAS LOCATED IN BOTH THE COCKPIT AND THE CABIN. THE SOURCE OF THE SMOKE WAS THE LH ACM. THE DURATION OF THE SMOKE LASTED NO MORE THAN 5 MINUTES. NO MEDICAL ATTENTION REQUIRED./ REMOVED AND REPLACED LH ACM IAW CRJ 700 AMM 21-51-08-000/400-801-A01. OPS CHECK GOOD. LEAK CHECKS GOOD.

Part: WIRE HARNESS — FAULTED (NLG STEERING) · airframe 28,857 hrs · 22,396 cycles

NOSEWHEEL STEERING FAILED COULD NOT RESET IN THE AIR OR ON THE GROUND. / REMOVED AND REPLACED THE NOSEWHEEL STEERING HARNESS IAW CRJ 700 AMM 32-21-01-000/400-803. BITE GOOD. OPS TEST GOOD.

Part: WINDOW — CRACKED (200) · airframe 26,647 hrs · 20,524 cycles

LH WINDOW HEAT CAUTION MSG CYCLED SWITCH MSG CLEARED ,BUT SPARKS CAME FROM TERMINAL AND WINDOW BEGAN SHATTERING. REMOVED AND REPLACED LH FLIGHT COMPARTMENT SIDE WINDOW IAW CRJ-700 AMM 56-12-01-000/400-801-A01-PSA. OPS TEST AND LEAK CK GOOD.

Part: STRINGER — CORRODED · corrosion level 2 · airframe 26,548 hrs · 20,427 cycles

STRINGER 26L IS CORRODED BETWEEN FS 310.00 AND 333.00.

Part: DOOR — GOUGED · airframe 26,548 hrs · 20,427 cycles

FWD CARGO DOOR LOWER OUTER SEAL RETAINER IS GOUGED AND BENT AT SEVERAL LOCATIONS.

Part: FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 26,548 hrs · 20,427 cycles

UPON REMOVAL OF FRAME SECTION 319 FOUND EXCESSIVE CORROSION ON ATTACH FLANGE REQUIRES REPAIR

Part: DOOR — CHAFED · airframe 26,548 hrs · 20,427 cycles

RH OVERWING EMERGENCY EXIT DOOR OUTER SKIN HAS THREE GOUGED AREAS ON EDGE OF THE SKIN AT THE UPPER MID SECTION OF THE DOOR

Part: DOOR — CHAFED · airframe 26,548 hrs · 20,427 cycles

FORWARD BAGGAGE BAY DOOR INNER SKIN IS CHAFED AT (2EA) LOCATIONS.

Part: HINGE — WORN (ZONE 800) · airframe 26,548 hrs · 20,427 cycles

DURING INSTALLATION OF THE PASSENGER DOOR, FOUND EXCESSIVE DOOR PLAY AT THE HINGE ATTACHMENT POINT WITH NEW PIN INSTALLED.

Part: DRAG ANGLE — CRACKED · airframe 26,548 hrs · 20,427 cycles

LH AFT VERTICAL STAB DRAG ANGLE SUSPECTED POSSIBLE CRACK

Part: SUPPORT ANGLE — CORRODED · corrosion level 2 · airframe 26,548 hrs · 20,427 cycles

BELLY FAIRING SUPPORT ANGLE IS CORRODED AT FS939.00 STGR 27.

Part: DOOR — UNKNOWN · airframe 26,548 hrs · 20,427 cycles

SB 670BA-52-042 PAX DOOR MODIFICATION TO THE INSTALLATION OF ACCESS PANELS AND COVERS, REQUIRES COMPLETION.

Part: DOOR — UNKNOWN · airframe 26,548 hrs · 20,427 cycles

IS67052110200 IMPROVED CORROSION RESISTANCE OF PHASE IV PAX DOOR, REQUIRES COMPLETION.

Part: STRINGER — CORRODED · corrosion level 2 · airframe 26,548 hrs · 20,427 cycles

STRINGER 25R IS CORRODED IN MULTIPLE LOCATIONS BETWEEN FS 280.00 AND 333.00.

Part: FRAME — CORRODED · corrosion level 2 · airframe 26,548 hrs · 20,427 cycles

FRAME AT FS 310.00 IS CORRODED BETWEEN STGR 24L AND 26R.

Part: NONE — CORRODED (ZONE 800) · airframe 22,122 hrs · 19,956 cycles

C.O. 10315122 JOB21031511, OP 90 AFT CARGO DOOR SILL PLATE HAS MINOR CORROSION WITH ATTENTION TO BE AROUND THE CARGO DOOR STOP FITTINGS CORRECTIVE ACTION: . REMOVED AND REPLACED AFT CARGO SILL PLATE IAW CRJ700 SRM 51-42-06-001-001-A01, 51-42-13-001-001-A01, 51-42-21-001-001-A01, AND MHIRJ REO 670-53-61-2101 REV -- DATED 2022-10-13.

Part: ENGINE — VIBRATION (LEFT) · airframe 25,159 hrs · 19,199 cycles

5206/22MAR CLT-LFT TAIL 536 ENGINE VIBE WARNING, FOLLOWED QRH, UNABLE TO CLIMB FURTHER. RETURNING TO CLT. EMERGENCY DECLARED 0235Z ENGINE VIBE WENT UP TO 2.0 LANDED OVERWEIGHT, BUT WITHOUT FURTHER/OTHER ISSUE 70.4 - 70 LANDING WEIGHT. L ENGINE VIB WENT TO 2.0 ON CLIMB / REMOVED FAN BLADES , SPINNER AND BLADEPORT PLUG TO FOM. CLEANED AND LUBED FAN BLADES IAW CRJ 700 AMM 72-21-02-640-801. REPLACED FAN RETAINING PINS IAW CRJ 700 AMM 72-21-02-400-801-A01-PSA. PERFORMED LH ENG BLADE SHAKER LIMIT AND BLADE RETAINING RING TORQUE CHECK AND REPLACED BUMPERS AS NEEDED IAW CRJ700 AMM 72-21-02-400-801-A01-PSA. VIBRATION CHECK GOOD. PERFORMED LH ENGINE VIBE CHECK IAW CRJ900 AMM 71ˆ’00ˆ’00ˆ’720ˆ’806 . VIBE CHECK GOOD"

Part: PROXIMITY SENSOR — OUT OF RIG · airframe 25,097 hrs · 19,151 cycles

SHORTLY AFTER TAKE OFF THE CREW RECEIVED A GEAR DISAGREE MESSAGE. THEY RAN THE QRH AND RETURNED TO DAY. CLIMB GEAR DISAGREE WARNING RAN QRC/QRH MESSAGE EXTINGUISHED RTF . INITIAL MSG APPEARED AROUND 600 FT WITH A PROX SYS 1 FAULT S MSG. THEY WERE NOT OVERWEIGHT AT LANDING. THEY DID NOT DECLARE AN EMERGENCY THEMSELVES, HOWEVER ATC DECLARED FOR THEM AND ROLLED THE TRUCKS. THE PASSENGERS DID NOT BRACE. THE AIRCRAFT LANDED SAFELY AND TAXIED TO THE GATE. THE AIRCRAFT IS CURRENTLY IN MAINTENANCE. INTERROGATED MDC AND FOUND B1- 007697 007249 007437 005968 007412. TROUBLESHOT B1-007412 IAW CRJ 700 FIM 32-61-05-810-828-A01, FOUND PX37 TO BE OUT OF RIG. ADJUSTED PX37 IAW CRJ 700 AMM 32-61-05-820-805-A01. RIG CHECK GOOD AT THIS TIME. GEAR SWING GOOD AT THIS TIME IAW CRJ 700 AMM 32-30-00-865-801-A01.

Part: WIRE HARNESS — UNSERVICEABLE (700) · airframe 25,089 hrs · 19,144 cycles

RETURN TO FIELD FOR GEAR DISAGREE ON TAKEOFF. EMERGENCY DECLARED. CONTINUED TROUBLESHOOTING GEAR DISAGREED MASTER WARNING IAW CRJ 700 FIM 32-61-05-810-828 B1-007412. REMOVED AND REPLACED WOW CENTER HARNESS ASSY (RH) IAW CRJ 700 AMM 32-61-05-000/400-805. RIGGING PASSED AND OPS CHECKS GOOD NO CURRENT FAULTS AT THIS TIME.

Part: PANEL — SCRATCHED (ZONE 100) · airframe 23,922 hrs · 18,099 cycles

DURING ROUTINE OPERATIONS, MAINTENANCE DISCOVERED MULTIPLE SCRATCHES TO THE ADG PANEL (P/N CC670-33109-3). THE PANEL IS FABRICATED FROM 2024-T42 .100€? AND IS MILLED DOWN TO .058€? IN THE DAMAGED AREA. THE REPORTED SCRATCH DEPTHS ARE 0.003€? €“ 0.007€? / PERFORMED LPI INSPECTION ON FUSELAGE BELOW EXT AC SERVICE PANEL IAW CRJ 700 NDTM 51-20-008-230 A01. ALSO PERFORMED VISUAL INSPECTION IAW NDTM 51-20-009-210 A01 TO DEFER UT THICKNESS MEASUREMENTS. NO FURTHER DAMAGE NOTED FROM EITHER INSPECTION. PERFORMED BLEND AND PAINT RESTORATION OF AREA IAW CRJ 700 EA 21-C7-53-302 IR SECTION I. UT INSPECTION DEFERRED FOR 25 FLIGHT HOURS. REPEAT INSPECTIONS REQUIRE ACCOMPLISHED EVERY 140 FLIGHT HOURS. PERM REPAIR REQUIRES ACCOMPLISHED IN 250 FLIGHT HOURS. PERFORMED EA 21-C7-53-302 REV B SECTION II- REPETITIVE INSPECTIONS BY DVI AND NDTM 51-20-006 ECI. NO ADDITIONAL DAMAGE FOUND, NO CRACKS FOUND. PERFORMED BLEND REPAIR TO SKIN PANEL CC670-33109-3 IAW EA21-C7-53-302 REV C SEE BARCODE TRFKE006NS1D FOR WORK PERFORMED. FOR LAST NDT INSPECT PERFORMED SEE TRFKE007B2DW. SEE FAA FORM 337 DATED 8/10/21 THIS TERMINATES PERM REPAIR."

Part: SKIN — CRACKED (PAX DOOR) · airframe 21,625 hrs · 16,054 cycles

PASSENGER DOOR AFT SIDE SKIN HAS MULTIPLE CRACKS AT THE DOOR ASSIST MOTOR SUPPORT WEB-C/A-REMOVED AND REPLACED PASSENGER DOOR AFT SKIN IAW SRM 51-42-06.

Part: STRINGER — CORRODED (BS 280-293) · corrosion level 2 · airframe 21,625 hrs · 16,054 cycles

STR 25R IS CORRODED BETWEEN FS 280.00 AND 293.00-C/A-REMOVED AND REPLACED STR 25R BETWEEN FS280 AND FS-293 IAW SRM 51-42-06.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 21,625 hrs · 16,054 cycles

RH CROSSBEAM AT FS 280.00 IS CORRODED IN NUMEROUS AREAS BEWTEEN DRIP TRAY AND THE UPPER L ANGLE.-C/A-RH FS280.00 CROSSBEAM INSTALLATION IAW SRM 53-11-10 AND 51-42-06

Part: FLOORBEAM — CORRODED (BS 280) · airframe 21,625 hrs · 16,054 cycles

LH CROSSBEAM AT FS 280.00 IS CORRODED IN NUMEROUS AREAS BEWTEEN DRIP TRAY AND THE UPPER L ANGLE.-C/A-COMPLETED LH FS280.00 CROSSBEAM INSTALLATION IAW SRM 53-11-10 AND 51-42-06

Part: FLOORBEAM — CRACKED (BS 280) · airframe 21,625 hrs · 16,054 cycles

RH CENTER COCKPIT FLOOR BEAM AT BL12.00 IS CRACKED, LOCATED JUST FWD OF CROSSBEAM AT FS280.OO-C/A-REPAIRED R/H CENTER COCKPIT FLOOR BEAM AT BL 12.00 JUST FWD OF FS 280.-00 IAW SRM 53-11-43 AND ETN CR-53-088.

Part: ANGLE — CRACKED (PAX DOOR) · airframe 21,625 hrs · 16,054 cycles

PAX DOOR HAS A CRACK ON THE AFT ANGLE, ON PREVIOUS REPAIR-C/A-REPAIRED AFT DRAG ANGLE IAW SRM 52-11-04-201-002-A01.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 21,625 hrs · 16,054 cycles

LH CENTER COCKPIT FLOOR BEAM AT BL12.00 IS CRACKED, LOCATED JUST FWD OF CROSSBEAM AT FS280.OO-C/A-REPAIRED L/H CENTER COCKPIT FLOOR BEAM AT BL 12.00 JUST FWD OF FS 280.-00 IAW SRM 53-11-43 AND ETN CR-53-088.

Part: INDICATION SYS — UNKNOWN (OIL TEMP) · airframe 21,223 hrs · 15,608 cycles

AT LEVEL OFF 13,000' 0 LEFT OIL TEMP WENT AMBER AND RED. WENT IDLE, TEMP WENT BACK AMBER, THEN WENT 147-149 AFTER 10 MIN TEMP STAYED 135 TO 137. TAXI, TAFF, CLIMB NORMAL OPS. CHECKED IAW FIM 79-30-00-810-810 RAR #1 ENGINE OIL LEVEL/OIL TEMPERATURE SENSOR IAW AMM 79-31-01; PERFORMED HIGH/CLIMB POWER OPS CHECK LEAK CHECK GOOD. ALL INDICATIONS NORMAL.

Part: HYDRAULIC SYSTEM — CONTAMINATED (NR 3) · airframe 20,207 hrs · 14,703 cycles

GEAR DISAGREE WARNING AFTER GEAR RETRACTION ON T/O-C/A-T/S AND FOUND B CODE B1-0060112 IN THE MDC FOUND A LARGE AMOUNT OF AIR IN THE #3 HYD SYSTEM PERFORMED BLEEDING OF THE #3 HYD SYSTEM IAW CRJ 700 AMM 29-10-00 OPT'S CHECKED LANDING GEAR IAW CRJ 700 AMM 32-30-00 OPTS CHECK GOOD

Part: SENSOR — OUT OF ADJUST (PX37) · airframe 20,157 hrs · 14,660 cycles

PROX SYS FAULT STATUS MSG. AFTER X-LIST FOR GEAR DISAGREE WARNING MSG. GEAR DISAGREE WARNING MSG. AFTER T/0.-C/A-FOUND NG CENTRD #2 SNSR/OUT-OF-RIG/REASON-FAR 007412. C/W CRJ-700 FIM 32-61-05-810-828. ADJUSTED PX37 SENSOR IAW CRJ-700 AMM 32-61-05. PERFORMED OPS CK OF LANDING GEAR EXTENSION /RETRACTION OPS CK GOOD IAW CRJ 700 AMM 32-30-00 AND FIM 32-31-00.

Part: UNKNOWN — SMOKE (CABIN) · airframe 19,511 hrs · 14,116 cycles

CABIN FILLED W/ SMOKE WITH BOTH ENGINES OFF. SMELL OF ELECTRICALSMOKE. -C/A-PERFORMED OPS CHECK OF CAIN INTERNAL LIGHTS IAW AMM 33-21-01 AND 33-2-09 OPS CHECKS GOOD NO DEFECTS NOTED PERFORMED OPS CHECK OF PACK SYSTEM IAW AMM 21-51-00 OPS CHECK GOOD NO DEFECTS NOTED.

Part: MANIFOLD — FAILED (NLG STEERING) · airframe 18,782 hrs · 13,510 cycles

DECLARED AN EMERGENCY, NOSE WHEEL STEERING INOPERATIVE. R & R THE NLG STEERING MANIFOLD IAW AMM 32-51-50. OPS CHECKED GOOD

Part: CIRCUIT BOARD — DAMAGED · airframe 18,267 hrs · 13,079 cycles

STRONG ELECTRICAL BURNING ODOR IN THE FLIGHT DECK, ON ARRIVAL AT AC GPU WAS PLUGGED IN WITH BATTERY SWITCH OFF. REMOVED LT DCPC AND INSPECTED FOR DAMAGE TO THE BACK AND FACE OF BOARD. CLEANED AND REASSEMBLED IAW CMM 24-63-10. REINSTALLED THE LT DCPC IAW AMM 24-62-01. NO FURTHER ODOR NOTICED

Part: PCB — BURNED · airframe 18,265 hrs · 13,076 cycles

WHEN FO FIRST ARRIVED AT THE ACFT, NOTICED THE BATTERY MASTER SWITCH WAS LEFT ON. ELECTRICAL ODOR WAS PRESENT. GPU PLUGGED IN BUT NOT SELECTED. REMOVED AND REPLACED THE MAIN BATTERY AND APU BATTERY. ALL OPS CHECKED GOOD. REMOVED AND REPLACED THE LEFT DCPC PRINTED CIRCUIT BOARD 1 IAW AMM 24-62-17, OPS CHECKED GOOD. PCB SHOWED SIGN OF BURNING.

Part: TIRE — FAILED (NR 2) · airframe 17,299 hrs · 12,303 cycles

NR 2 TIRE TREAD SEPARATION, LEFT MAIN GEAR FLAT. REMOVED AND REPLACED THE NR 2 MAIN WHEEL ASSY IAW WORKCARD 32-002.

Part: FAN — FAILED (DISPLAY) · airframe 16,910 hrs · 11,987 cycles

STRONG BURNED ELECTRICAL LIKE ODOR WHEN ENTERING COCKPIT. DETERMINED SMELL COMING FROM AVIONICS DISPLAY FAN 2. REMOVED AND REPLACED DISPLAY SUPPLY FAN NR 2 IAW AMM 21-24-12. OPS CHECKED GOOD.

Part: LIGHT — INTERMITTENT (CABIN) · airframe 16,836 hrs · 11,920 cycles

EMERGENCY LIGHTS ON STATUS INTERMITTENT, EVEN WITH EMERGENCY LIGHTS SWITCH OFF. PERFORMED AND OPERATIONAL TEST OF THE EMERGENCY LIGHTS IAW AMM 33-51-00, OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 16,118 hrs · 11,347 cycles

LT EXTERIOR OVERWING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE BULB IAW 33-51-15. OPS CHECKED ALL EXTERIOR EMERGENCY LIGHTS, OPS CHECKED GOOD.

Part: TARGET — OUT OF ADJUST (NLG) · airframe 15,880 hrs · 11,146 cycles

GEAR DISAGREE, LANDING GEAR LEVER UP AFTER TAKE OFF. TROUBLESHOT TO RT NLG CENTERING PROX TARGET (PX37) AND HARDWARE. REPLACED HARDWARE WITH SERVICEABLE AND ADJUSTED TARGET IAW AMM32-61-05. OPS CHECK AND GEAR SWINGS GOOD.

Part: FRAME — CORRODED (BS 319) · corrosion level 2 · airframe 15,267 hrs · 10,640 cycles

FRAME BS 319.7 IS CORRODED BETWEEN STRINGERS 25L AND 26R. REPAIRED THE FRAME IAW ERS-CR-53MR-2365.

Part: FRAME — CORRODED (BS 310) · corrosion level 2 · airframe 15,267 hrs · 10,640 cycles

FRAME BS 310 IS CORRODED BETWEEN STRINGERS 24L AND 26R. REPAIRED THE FRAME BS 310 IAW ERS-CR-53MR-2366.

Part: FRAME — CORRODED (BS 295) · corrosion level 2 · airframe 15,267 hrs · 10,640 cycles

FRAME BS 295 IS CORRODED BETWEEN STRINGERS 25L AND 25R. REPAIRED THE FRAME IAW ERS-CR-53MR-2367.

Part: STAND OFF — CRACKED (LT NACELLE) · airframe 15,267 hrs · 10,640 cycles

LEFT UPPER TRANSCOWL FWD STANDOFF CRACKED. REMOVED AND REPLACED THE STANDOFF IAW ETN-CR-54-015R1 AND SRM 51-42-14 & 51-42-21.

Part: STAND OFF — CRACKED (LT NACELLE) · airframe 15,267 hrs · 10,640 cycles

LT UPPER TRANSCOWL AFT STANDOFF CRACKED. REMOVED AND REPLACED STANDOFF IAW ETN-CR-54-015R1 AND SRM 51-42-14 & 51-42-21.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 15,267 hrs · 10,640 cycles

PAX DOOR AFT SIDE DRAG ANGLE HAS A 1.25 INCH CRACK. DRAG ANGLE REPAIRED IAW SRM 52-11-04

Part: STAND OFF — CRACKED (RT NACELLE) · airframe 15,267 hrs · 10,640 cycles

RT UPPER TRANSCOWL FWD INBD STANDOFF CRACKED. REPLACED THE STANDOFF IAW ETN-CR-54-015R1.

Part: CABLE — MALFUNCTIONED (PAX DOOR) · airframe 14,830 hrs · 10,270 cycles

CABIN DOOR HARD TO OPEN. R & R MAIN DOOR ICE BRAKE CABLE IAW AMM 52-11-15. OPS CHECKED GOOD.

Part: PITOT LINE — CONTAMINATED (PITOT/STATIC SYS) · airframe 10,714 hrs · 6,926 cycles

10 KT SPLIT BETWEEN CAPTAIN & FIRST OFFICER`S AIRSPEED INDICATIONS DURING APPROACH. INSPECTED DRAIN LINES FOR CONTAMINATION. FOUND WATER IN NR 1 PITOT DRAIN LINE. REMOVED WATER IAW MM 34-11-00. OPERATIONS CHECKED GOOD. NO PRIOR PIREPS NOTED. ACFT ELIGIBLE FOR RVSM & CAT II OPERATION.

Part: RISER — CRACKED (PAX DOOR) · airframe 10,680 hrs · 6,896 cycles

PAX DOOR FWD STEP RISER CRACKED. REPAIRED STEP RISER IAW SRM 52-11-04.

Part: RISER — CRACKED (PAX DOOR) · airframe 10,680 hrs · 6,896 cycles

PAX DOOR AFT STEP RISER CRACKED. REPAIRED STEP RISER IAW SRM 52-11-04.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 10,680 hrs · 6,896 cycles

FORWARD EQUIPMENT BAY FLOOR STRUCTURE IS CRACKED UNDER THE ADG PUMP. COMPLIED WITH SHELF REPAIR IAW ETN CR-53-099.

Part: PCU — MALFUNCTIONED (SPOILERS) · airframe 10,677 hrs · 6,894 cycles

WHEN FLIGHT SPOILERS WERE DEPLOYED, OTBD SPOILERONS & OTBD FLIGHT SPOILERS CAUTION MESSAGES POSTED. PERFORMED SPOST 2 RESET TEST IAW ETN CR-27-093. NO MESSAGES DISPLAYED. REMOVED AND REPLACED THE LT OUTBOARD MFS PCU IAW AMM 27-62-01. OPS AND LEAK CHECKED GOOD.

Part: STRUCTURE — CRACKED (NLG WW) · airframe 10,680 hrs · 6,896 cycles

CR-53MR-349 DENT & CRACK DAMAGE IN NLG WW STRUCTURE AT FS 202.75. REPAIRED IAW EO CR-53MR-349.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 10,660 hrs · 6,880 cycles

ON DESCENT WITH FLIGHT SPOILERS EXTENDED GOT OTBD SPOILERONS AND OTBD FLIGHT SPLRS CAUTION MSGS. LANDING LT OTBD MULTI-FUNCTION SPOILER ON FLIGHT CONTROL SYNOPTIC SHOWED AMBER. ITEM PREVIOUSLY DEFERRED. RESET IAW ETN-CR-27-093. OPERATIONS CHECKED GOOD. NO FURTHER MSGS DISPLAYED. TDMI REMAINS OPEN.

Part: ENGINE — VIBRATION (RIGHT) · airframe 10,367 hrs · 6,652 cycles

RIGHT ENGINE HIGH VIBRATION 2.2 PLUS AT FL250, 63 PERCENT N1. ALSO AT 8000 FT 47 PERCENT N1 1.8 VIBRATION. R & R OTBD MULTI-FUNCTIONAL SPOILER PCU. OPS & LEAK CHECKED IAW AMM 27-62-01.

Part: CABLE — DETACHED (CABIN DOOR) · airframe 10,244 hrs · 6,559 cycles

FLIGHT ATTENDANT REPORTS MAIN CABIN DOOR OPENED VERY ROUGH, NO SPRING ASSIST & HIT THE GND HARD. PERFORMED GVI OF OUTSIDE OF DOOR & FOUND NO DAMAGE. REATTACHED MOTOR ASSIST CABLE TO PULLEY IAW SMP. DOOR OPENS & CLOSES NORMALLY IAW MM 52-11-00.

Part: MANIFOLD — DEFECTIVE (NLG STEERING) · airframe 9,844 hrs · 6,294 cycles

DURING FLIGHT 3402 CREW REPORTED NOSE WHEEL STEERING INOPERABLE & DECLARED EMERGENCY. THE ACFT WAS REMOVE FROM SERVICE. R & R THE NWS MANIFOLD IAW AMM 32-51-50. OPERATIONAL & LEAK CHECKS GOOD. THE ACFT RETURNED TO SERVICE.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 9,804 hrs · 6,268 cycles

STEER INOPERATIVE CAUTION IN FLIGHT. STEERING INOPERATIVE CAUTION RESET IAW CRJ AOM VOL 1, RESET PROCEDURES PAGE 130.12, OPERATIONS CHECKED GOOD, NO DEFECTS NOTED.

Part: STRUCTURE — CRACKED (NLG WW) · airframe 9,268 hrs · 5,906 cycles

DENT & CRACK DAMAGE IN LT MLG WW STRUCTURE AT FS 202.75. CRJ 700 ACFT PN & SN J700 & 10315 TWD=9332:38 HRS. PERFORMED GVI 0F DAMAGE AREA IAW EO CR-53MR-349 PART B, NO FURTHER DAMAGE NOTED AT THIS TIME.

Part: UNKNOWN — MALFUNCTIONED (NLG STEERING) · airframe 9,124 hrs · 5,816 cycles

STEERING INOPERATIVE. EICAS CAUTION MSG IN FLIGHT. RESET ON THE GND IAW AOM PROCEDURE. OPERATIONS CHECKED GOOD IAW AMM 32-50-00.

Part: STRUCTURE — DAMAGED (LT MLG) · airframe 9,023 hrs · 5,742 cycles

DENT & CRACK DAMAGE IN LT MLG WW STRUCTURE AT FS 202.75. ACFT PN & SN CRJ700 10315 TWD 9067:46 HRS. ACCOMPLISHED CR-53MR-349 PART B. NO DAMAGE PROGRESSION NOTED.

Part: ADC — CONTAMINATED (NR 1) · airframe 8,858 hrs · 5,633 cycles

EMERGENCY WAS DECLARED DUE TO FAILURE OF CAPTAIN'S ADC. DURING MAINTENANCE INSPECTION ON FLIGHT 3433 FOUND FAILURE OF CAPTAIN'S ADC. AIRCRAFT WAS REMOVED FROM SERVICE. FOUND WATER ADC NR 1 WATER DRAIN FULL WITH WATER DRAINED IAW CRJ 700 AMM 34-11-00. OPS CK GOOD IAW CRJ AMM 34-13-01. NO FAULTS NOTED.

Part: BRACKET — BROKEN (FLASHLIGHT) · airframe 8,557 hrs · 5,441 cycles

FORWARD FLIGHT ATTENDANT EMERGENCY FLASHLIGHT BRACKET BROKEN. R & R FWD FLIGHT ATTENDANT`S EMERGENCY FLASHLIGHT ASSEMBLY IAW EEL 65-EEL-08-12. OPERATIONS CHECKED GOOD, NO FURTHER DEFECTS NOTED.

Part: UNKNOWN — ODOR (POTABLE WATER) · airframe 8,377 hrs · 5,334 cycles

PASSENGERS AND F/A COMPLAINING OF FOUL ODOR EMANATING FROM COFFEE SUSPECT FORWARD POTABLE WATER TANK CONTAMINATED. FLUSHED AND SERVICED FORWARD POTABLE WATER TANK IAW AMM 38-11-00. NO DEFECTS NOTED.

Part: NOZZLE — LEAKING (APU FUEL) · airframe 8,174 hrs · 8,174 cycles

DURING TAXI, A STRONG ODOR PRESENT IN ACFT. DURING TROUBLESHOOTING, EXCESSIVE LEAK WAS FOUND COMING FROM THE APU FUEL MANIFOLD. LEAK WAS COMING FROM THE 3 O`CLOCK FUEL DISCHARGE NOZZLE AND FUEL MANIFOLD. R & R APU FUEL NOZZLE IAW AMM 49-31-51, OPS CHECKED GOOD. ACFT RETURNED TO SERVICE.

Part: STIFFENER — DAMAGED (BS 203 BULKHEAD) · airframe 7,842 hrs · 4,975 cycles

STIFFENER BENT AND CRACKED ON BULKHEAD AT FS203.75 IN NLG COMPT. NEAR STRINGER 26L. REPAIR ON STIFFNER AT BULKHEAD AT FS 203.75 IN NLG COMPT NEAR STR 26L IAW EO CR-53MR-349.

Part: ACM — ODOR (LEFT) · airframe 7,157 hrs · 4,547 cycles

THE CREW REPORTED THAT AT ABOUT 6 MILES SOUTHWEST OF AIRPORT, NOTICED A STRONG ODOR OF ELECTRICAL SMOKE IN THE COCKPIT WITH A MINIMAL AMOUNT OF SMOKE. THE F/A ALSO REPORTED THE ODOR OF SMOKE IN THE CABIN. THE CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. INSPECTED ACFT AND FOUND NO FIRE. ACFT REMOVED FROM SERVICE. R & R AIR CYCLE MACHINE, IAW AMM 21-51-08. OPS CHECKED GOOD. NO FURTHER DEFECTS NOTED. THE ACFT WAS RETURNED TO SERVICE.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 6,344 hrs · 4,039 cycles

ON FLIGHT 3655 THE CREW REPORTED THE FLIGHT ATTENDANT FLASHLIGHT WAS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE AFT FLASHLIGHT ASSEMBLY IAW CRJ AMM 25-61-03. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WIRE — BROKEN (CHART LIGHT) · airframe 4,386 hrs · 2,808 cycles

FLIGHT 3556, DURING CRUISE, FIRST OFFICER’S YOKE CHART LIGHT PRODUCE SEVERAL LARGE SPARKS. SWITCH WAS IN OFF AT TIME OF INCIDENT. ATTEMPTED TO ISOLATE POWER WITH HELP OF MAINTENANCE BUT WERE UNABLE TO. CIRCUIT BREAKER G6 POPPED. NOTICED CHART TRAY SHOWED SIGNS OF CHARING AND A SMOKE ODOR EMANATED FROM AREA. ELECTED TO DIVERT. AIRCRAFT LANDED WITHOUT INCIDENT. AIRCRAFT WA REMOVED FROM SERVICE. FOUND WIRES BEHIND CHART HOLDER BROKEN, REPAIRED WIRES TEF J001-22 AND TEF J002-22 IAW ESPM 20-33-00 AND ETN-CR-20-010. OPS TESTED GOOD IAW AMM 33-13-07. AIRCRAFT RETURNED TO SERVICE.

Part: DOOR — UNSECURE (COMMS) · airframe 3,964 hrs · 2,554 cycles

FLIGHT 3715, THE CREW REPORTED THEY HEARD A THUD FROM BELOW FLIGHT DECK AREA AT ROTATION. INCREASING INTENSITY NOISE ACCOMPANIED THE INCREASE IN AIRSPEED. THE CREW DECLARED AN EMERGENCY AND AS A PRECAUTIONARY MEASURE RETURNED TO DEPARTURE. AIRCRAFT LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. COMMS DOOR LEFT OPEN ON DEPARTURE. NO OTHER DEFECTS FOUND AT THIS TIME. INSPECTED DOOR IAW CRJ SRM 52-00-01. NO DEFECTS FOUND AT THIS TIME. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WHEEL — DEFECTIVE (NLG) · airframe 2,209 hrs · 1,426 cycles

ON FLIGHT 3602 THE CREW REPORTED, HAD SEVERE VIBRATION IN NOSE GEAR ON TAKEOFF ROLL AND DURING RETRACTION. THE CREW DECLARED AN EMERGENCY. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED NOSEWHEEL AND TIRE ASSY IAW WORK CARD 32-006. THE OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.