N529EA

Part: COFFEEMAKER — ODOR (ZONE 900) · airframe 32,775 hrs · 25,305 cycles

THE FLIGHT CREW REPORTED A BURNING POPCORN SMELL WHILE ENROUTE. THE SMELL DISSIPATED. NO MEDICAL ATTENTION REQUIRED. PERFORMED OPS CHECK OF THE TEMPERATURE CONTROL SYSTEM IAW AMM 21-60-00-710-801. OPS CHECK GOOD AT THIS TIME. DURING OPS CHECK, NO ODORS WERE NOTED. AFTERWARDS, NOTED BURNING SMELL IN GALLEY, COMING FROM LH COFFEE MAKER. REMOVED AND REPLACED IAW VCMM 25-33-21. NO ODOR NOTED WHEN OPERATING COFFEE MAKER.

Part: ANGLE — CORRODED (ZONE 200) · airframe 32,516 hrs · 25,083 cycles

PASSENGER DOOR LOWER SILL CAP ANGLE IS CORRODED ADJACENT TO THE PROX SWITCH. REMOVED UNSERVICEABLE PAX DOOR LOWER SILL CAP (P/N: SH670-31825-9S) IAW CRJ700 SRM 51-41-02-001-001-A01. LOCATED, DRILLED, AND INSTALLED NEW SERVICEABLE PAX DOOR LOWER SILL CAP (P/N: SH670-31825-9S) IAW CRJ700 SRM 51-40-11-001-001-A01, 51-41-02-001-001-A01, 51-42-13-001-001-A01, AND 51-45-00-001-001-A01

Part: ANGLE — CORRODED (ZONE 200) · airframe 32,516 hrs · 25,083 cycles

THE FWD J ANGLE ON FS 280 IS CORRODED. REMOVED AND REPLACED IAW CRJ 700 SRMS 51-40-11-001-001-A01, 51-42-06-001-001-A01, AND 51-42-21-001-001-A01.

Part: FRAME — CORRODED (ZONE 100) · airframe 32,516 hrs · 25,083 cycles

F.S. 319.70 FRAME FROM STRG. 26 R/H TO STRG. 27 HAS PATCH OF CORROSION. CUT AWAY DAMAGED FRAME SECTION AND SPLICED IN REPAIR FRAME IAW CRJ 700 SRM 53-00-06-201-006-A01.

Part: CONNECTOR — DAMAGED (ASCU) · airframe 29,833 hrs · 22,866 cycles

BRAKE OVHT MASTER CAUTION IN FLIGHT / REMOVED ASCU MOUNTING TRAY AND FOUND CONNECTOR THREADED MOUNTING NUT MISSING, REINSTALLED ASCU MOUNTING TRAY WITH CONNECTOR ON CORRECT SIDE OF TRAY WITH NUT AND WASHER PER REO 670-32-48-002 PERMANENT REPAIR AND AMM 32-44-07-000/400-801. PERFORMED ACSU BITE TEST AND SELF-TEST OF BRAKE TEMP SENSOR IAW CRJ700 32-46-01-740-801-A01. TAXID A/C TO RUN UP PAD FOR BRAKE TEMPERATURE IAW CRJ 700 AMM 09-20-585-801. OPS CHECK GOOD AT THIS TIME.

Part: DIAPHRAGM — OBSTRUCTED (CABIN PRESSURE) · airframe 29,779 hrs · 22,817 cycles

CABIN ALT CAUTION MSG, AT FLT LEVEL 360, CABIN ALT WENT TO 9000FLT / INSPECTED THE #2 SAFETY VALVE AND FOUND LOOSE INSULATION STUCK BETWEEN THE DIAPHRAGM AND IT€™S SEAT. REMOVED INSULATION AND PERFORMED A FUNCTIONAL TEST OF THE SAFETY VALVE IAW CRJ 700 AMM 21-32-03-720-802-A01. PERFORMED A PRESSURIZATION CHECK OF THE AIRCRAFT IAW CRJ 700 AMM 21-31-00-910-801-A01-PSA. OPS CHECKS GOOD.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 13,409 hrs · 12,107 cycles

CORROSION AT SEAT RAIL RBL9 BETWEEN FS661+98 – FS677+8. SECTION OF SEAT RAIL WAS REPLACED, AT RBL9 ,BETWEEN FS=661+98 TO FS=677+8, PER CRJ-900 AMM 53-00-49 (CONFIG. A12).

Part: SKIN — CORRODED · corrosion level 2 · airframe 26,888 hrs · 20,230 cycles

CORROSION AT SETTLEMENT AREA OF MAIN AVIONICS COMPARTMENT DOOR SURROUND STRUCTURE.

Part: ANGLE — CRACKED · airframe 26,888 hrs · 20,230 cycles

CRACK ON ATTATCHMENT ANGLE OF ACCESS PANEL 542AZ ON LH MLG SHOCK STRUT BAY

Part: STRINGER SPLICE — CORRODED · corrosion level 2 · airframe 26,888 hrs · 20,230 cycles

CORROSION ON STRINGER SPLICE ON FS 333.00, STGR 26RH. (SM)

Part: FRAME — CORRODED · corrosion level 2 · airframe 26,888 hrs · 20,230 cycles

CORROSION ON FRAME FS613 BETWEEN STGR 27 TO 26LH INTERNAL STRUCTURE AT CARGO COMPARTMENT FWD (CCF)

Part: SKIN — CORRODED · airframe 26,888 hrs · 20,230 cycles

CORROSION AT SETTLEMENT AREA OF MAIN AVIONICS COMPARTMENT DOOR SURROUND STRUCTURE

Part: FLOOR SUPPORT — CORRODED · corrosion level 2 · airframe 26,888 hrs · 20,230 cycles

CORROSION AT FLOOR ANGLE SUPPORT OF FS280.0 BETWEEN RBL9 AND LBL9

Part: SEAT TRACK — CORRODED · airframe 26,888 hrs · 20,230 cycles

CORROSION ON SEAT RAIL 9RBL FROM FS 421.00 TO 477.40

Part: SWITCH — UNSERVICEABLE (600) · airframe 26,712 hrs · 20,073 cycles

IB GND SPLRS AND GND SPLR DEPLOY CAUTION MSGS IN FLIGHT, RH IB SPLR SHOWED DEPLOYED ON FLT/CTL PAGE / INTERROGATED MDC FOR B1 CODE 156704. ADVANCED DIAGNOSTICS SHOWED BIT FOR R IB GROUND SPOILER SENSOR SET TO 1. REMOVED AND REPLACED RH IB GROUND PROXIMITY SWITCH IAW AMM TASK 27-63-07-000/400-801-A01. OPS/RIG CHECK GOOD.

Part: SPOILERON — FALSE INDICATION · airframe 26,390 hrs · 19,794 cycles

OB SPOILERONS CAUTION MESSAGE / CYCLED SYSTEM CBS MESSAGES CLEARED PROBLEM DID NOT REOCCUR.

Part: UNKNOWN — ODOR (CABIN) · airframe 25,624 hrs · 19,118 cycles

BURNING ODOR WHEN BLEEDS TRANSFERRED TO APU AFTER LANDING DISSIPATED AFTER A FEW MOMENTS / DEFERRED BOTH PACKS PER MEL 21-51-1-2 OPTION 3. PERFORMED OPS TEST OF AIR CONDITIONING DISTRIBUTION SYSTEM IAW CRJ 700 AMM 21-51-00-710-801. SMOKE ODOR NOT PRESENT FOR THE HOUR PACKS WERE RAN. OPS TEST GOOD. THIS CLEARS MEL.

Part: SKIN — DENTED (BS 202-210) · airframe 25,492 hrs · 18,995 cycles

DURING MAINTENANCE OPERATIONS AT DAYTON INTERNATIONAL AIRPORT (DAY) FACILITIES IN DAYTON, OH, MAINTENANCE IDENTIFIED ONE SLIGHT DENT, IN THE FUSELAGE SKIN PANEL (P/N CC670ˆ’33101ˆ’5) AFT OF FS202.75, BELOW STGR12A LH SIDE. THE DENT MEASURES APPROX. 1.75"" LONG, 2.5"" WIDE, .0025€? DEPTH. / TEMPORARY REPAIR WAS PERFORMED AS FOLLOWS: MAY 12TH,2021 SECTION 1 STEPS 1-4 PERFORMED WITH NO DEFECTS NOTED, JUNE 19TH, 2021 SECTION 1 STEPS 5 & 6 PERFORMED AND PSA AIRLINES ENGINEERING NOTIFIED. ALL TEMPORARY REPAIR STEPS COMPLETED AT PSA AIRLINES MAINTENANCE FACILITY IN DAYTON, OH. REVISION C/D (07/21/2021) OF EA CHANGED IT TO THE TEMPORARY REPAIR CAN BE UTILIZED AS THE PERMANENT REPAIR. ENGINEERING MARKED AS MAJOR REPAIR. EA21-C7-53-417-F (PERMANENT REPAIR - FUSELAGE SKIN PANEL - FS202.75 - FS281.65)"

Part: WARNING MESSAGE — FALSE INDICATION (NLG STEERING) · airframe 25,006 hrs · 18,544 cycles

NOSEWHEEL STEERING INOP MESSEGE DURING FLIGHT. EMERGENCY WAS DECLARED BEFORE LANDING IN LEX TO ENSURE TRUCKS WERE ROLLED. THE AIRCRAFT WAS ABLE TO COME TO A COMPLETE STOP, RESET THE SYSTEM, AND TAXI TO THE GATE UNDER THEIR OWN POWER. THERE WAS NO CALL FOR PAX TO BRACE. / CYCLED SYSTEM CBS AT THE GATE AND PERFORMED SYSTEM OPS CHECK OF THE NLG STEERING SYSTEM IAW CRJ700 AMM 32ˆ’51ˆ’00ˆ’710ˆ’801-A01 FAULT CLEARED AND DID NOT RETURN SYSTEM RESET WAS SUCCESSFUL.

Part: PCU — FAILED (SPOILER SYSTEM) · airframe 24,063 hrs · 17,721 cycles

OUTBOARD SPOILERON/OUTBOARD FLT SPOILERS CAUTION MESSAGE DURING FLIGHT. REMOVED AND REPLACED RT OUTBOARD MULTI-FUNCTION SPOILERON PCU. LEAK CHECK AND OPS CHECK GOOD.

Part: WARNING MESSAGE — FALSE ACTIVATION (SPOILERS) · airframe 23,769 hrs · 17,455 cycles

DURING APPROACH TO DCA THE CREW RECEIVED AN OB SPOILERON AND FLIGHT SPOILER CAUTION MESSAGE. THEY DECLARED AN EMERGENCY, LANDED SAFELY AND TAXIED TO THE GATE WITH NO ISSUES. TRUCKS ROLLED. PASSENGERS DID NOT BRACE. AIRCRAFT IS CURRENTLY WAITING FOR A MAINTENANCE INSPECTION.C/W CRJ 700 MEL SYSTEM RESET PG. 1-3 MESSAGES CLEARED SYS CK GOOD.

Part: ANGLE — CRACKED (BS 280) · airframe 22,070 hrs · 15,977 cycles

RBL 12 ANGLE IS CRACKED JUST FWD OF BS 280. REPAIRED RBL 12 IAW SRM 53-11-43.

Part: ANGLE — CRACKED (BS 280) · airframe 22,070 hrs · 15,977 cycles

LBL 12 ANGLE IS CRACKED JUST FWD OF BS 280. REPAIREDTHE ANGLE IAW SRM 53-11-43.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 22,070 hrs · 15,977 cycles

FLOORBEAM AT FS280.OO RIGHT UPPER FLANGE IS CORRODED, BETWEEN UPPER L ANGLE DRIP TRAY. INSTALLED NEW RH FS280.00 CROSSBEAM IAW SRM 51-42-06 AND 51-42-13.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 22,070 hrs · 15,977 cycles

FLOORBEAM AT FS280.00 LEFT UPPER FLANGE IS CORRODED, BETWEEN UPPER L ANGLE DRIP TRAY. (FS280 CROSSBEAM)-C/A-REMOVED AND REPLACED LH FS280.00 CROSSBEAM IAW SRM 51-42-06 AND 51-42-13.

Part: CROSSBEAM — CORRODED (BS 280) · airframe 22,070 hrs · 15,977 cycles

LEFT HAND SIDE OF FS280. CROOSBEAM IS CORRODED AT WALL CONNECTION. (BULKHEAD REPAIR)-C/A-REMOVED AND REPLACED LHS LOWER BULKHEAD WEB AT FS-2800.00 IAW SRM 53-11-10 AND 51-42-06.

Part: ATTACH ANGLE — CRACKED (VERTICAL STAB) · airframe 22,070 hrs · 15,977 cycles

LEFT VERTICAL STAB TO FUSELAGE ATTACH ANGLE HAS AN APPROX. 1" CRACK EXTENDING FROM UNDER PREVIOUS REPAIR DOUBLER. REPAIRED LEFT VERTICAL STAB TO FUSEALGE ATTACH ANGLE IAW SRM 55-31-00.

Part: FLOOR PANEL — CRACKED (EQUIP BAY) · airframe 22,070 hrs · 15,977 cycles

FWD EQUIPMENT COMPARTMENT FLOOR HAS AN 1/8" CRACK AT FS202.75 BY THE AFT CORNER OF CUTOUT FOR 211AL. REPAIRED LH FWD EQUIPMENT COMPARTMENT FLOOR IAW ETN-CR-53-099.

Part: UNKNOWN — OSCILLATES · airframe 21,811 hrs · 15,729 cycles

MAX ABORT T.O AIRCRAFT OSCILLATING ABOVE 90-100 MPH, A/C PULLS TO THE RIGHT DURING TAXI. PERFORMED GVI OF MLG IAW AMM 32-11-00 PERFORMED OPS CHECK OF BRAKES IAW AMM 32-43-00.OPS CHECK GOOD. INSPECTED NLG TORQUE LINKS AND TIRES IAW CRJ 700 AMM 32-42-01 AND 32-21-00 NO DEFECTS NOTED AT THIS TIME

Part: COMPUTER — INOPERATIVE (STALL) · airframe 19,621 hrs · 13,905 cycles

AT FLIGHT LEVEL AT FL270, STALL FAIL CAUTION POSTED. A SHORT TIME LATER A WARBLER TONE WAS HEARD. CA'S PFD SHOWED LOW SPEED RED RISING UP TO CURRENT SPEED OF 300. STICK SHAKER ACTIVATED AND STOPPED. ANOTHER ACTIVATION OF THE SHAKER HAPPENED AGAIN A MINUTE LATER. WE DISCONNECTED THE AUTO PILOT AND TRANSFERED CONTROL TO FO SIDE AND DECLARED EMERGENCY. PRIOR TO STICK SHAKER ACTIVATION WE COMPLIED WITH AOM1 STALL FAIL CAUTION. R AND L FADEC FAULT 2 ALSO POSTED DURING THE EVENT. TROUBLESHOT IAW FIM 27-35-05-810-805 LAOA/RESOLVER 1 AND 2 MDC MESS. FOUND STALL PROTECTION COMPUTER INOPERATIVE. REMOVED AND REPLACED THE STALL PROTECTION COMPUTER IAW AMM 27-35-01. OPS CHECKED GOOD. NO FADEC MESSAGES NOTED

Part: ACTUATOR — TRIPPED (SLATS) · airframe 18,844 hrs · 13,237 cycles

SLATS FAIL CAUTION MESSAGE. THE SLAT ACTUATOR HAD TRIP INDICATORS. FOUND THE LT NR 6 AND RT NR 5 TRIPPED. RESET THE LT NR 6 IAW ETN-CR-27-084R8 BUT THE RT NR 5 INDICATOR WILL NOT RESET. AFTER FURTHER INSPECTION OF SLAT ACTUATOR TRIP INDICATORS FOUND THE LT NR 1 AND LT NR 3 TRIPPED. RESET THE NR 1 AND 3 IAW ETN-CR-27-084 AND ALL TRIP INDICATORS REMAINED RESET AFTER MULTIPLE OPS CHECKS OF THE SLATS SYSTEM. OPS CHECKED GOOD. AIRCRAFT CAN RETURN TO SERVICE.

Part: DOOR — OUT OF ADJUST (PAX DOOR) · airframe 18,083 hrs · 12,653 cycles

PAX DOOR WAS HARD TO CLOSE. WAS ABLE TO CLOSE IT. THEN ON ARRIVAL, HAD TO CYCLE THE HANDLE 5 TIMES TO GET DOOR TO OPEN. GROUND WAS UNABLE TO OPEN FROM OUTSIDE. GAVE PROX SYST 1 FAULT DURING THE PROCESS. AIRCRAFT HAD SIMILAR WRITEUPS IN THE PAST. ADJUSTED DOOR IAW EA-ORD-02155 AND INSPECTED DOOR. THIS AIRCRAFT BEING FERRIED TO MQT FOR MAIN PAX DOOR RIG CHECK AND OR ADJUSTMENT.

Part: ACM — SEIZED (NR 2) · airframe 17,963 hrs · 12,558 cycles

F/A REPORTED A SMOKE ODOR IN CABIN DURING SHORT FINAL. COULDN`T DETERMAIN WHERE THE ODOR WAS FROM. AFTER TOUCHDOWN, THE RT PACK AUTOFAIL CAUTION MESSAGE APPEARED ON EICAS. TROUBLESHOT DISCREPANCY TO A SEIZED NR 2 ACM.

Part: DRAG ANGLE — CRACKED (VERTICAL STAB) · airframe 16,798 hrs · 11,660 cycles

RIGHT VERTICAL STAB TO FUSELAGE AFT DRAG ANGLE APPEARS TO BE CRACKED APPROX. ONE INCH IN LENGTH. REPAIRED IAW EO-CR-55MR-038.

Part: DRAG ANGLE — CRACKED (VERTICAL STAB) · airframe 16,798 hrs · 11,660 cycles

LEFT VERTICAL STAB TO FUSELAGE AFT DRAG ANGLE APPEARS TO BE CRACKED, ONE INCH IN LENGTH. REPAIRED IAW EO-CR-55MR-038.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 16,116 hrs · 11,093 cycles

RT EXTERIOR EMERGENCY LIGHT JUST AFT OF EMERGENCY EXIT DOOR INOPERATIVE. REMOVED AND REPLACED THE LAMP.

Part: SPOILER SYS — MALFUNCTIONED (WING) · airframe 15,014 hrs · 10,267 cycles

ON APPROACH, INBD FLT SPLRS, & INBD SPOILERONS, CAUTION MSG POSTED UPON SELECTION OF THE FLIGHT SPOILER HANDLE. AOM VOL 1 EMER & ABNORMAL PROCEDURES COMPLIED WITH. INTERROGATED MDC FOUND LT INBD MFS PCU & PCU JAM MDC MSG. PERFORMED SPOST 1 RESET. PERFORMED OPERATIONS CHECK IAW ETN-CR-27-093. OPERATIONS CHECKED GOOD.

Part: PANEL — CRACKED (PAX DOOR) · airframe 14,943 hrs · 10,218 cycles

PASSENGER DOOR AFT STEP SHELL SIDE PANEL HAS A CRACK BY SECOND STEP FROM BOTTOM WITH DOOR OPEN. REPAIRED IAW ERS-CR-5200-544.

Part: FRAME — CORRODED (FUSELAGE) · airframe 14,943 hrs · 10,218 cycles

FRAME AT FS 295.00 IS CORRODED, BETWEEN STRINGERS 25 LT - 25 RT. REPAIRED FRAME AT FS 295, BETWEEN STRINGER 25 LT - 25 RT IAW ERS-CR-53MR-2078.

Part: MARKER — WORN (CABIN) · airframe 14,943 hrs · 10,218 cycles

LEFT AFT AISLE EMER EXIT LIGHT RED MARKINGS ARE WORN OFF GOING INTO LT EMER EXIT SEATS. R & R LT AFT AISLE EMER EXIT LIGHT STRIP GOING INTO LT EMER EXIT SEATS IAW 33-51-01.

Part: SKIN — CORRODED (FUSELAGE) · airframe 14,943 hrs · 10,218 cycles

PASSENGER DOOR INNER SKIN HAS CORROSION ON LOWER EDGE WITH DOOR OPEN. REPAIRED CORROSION ON PAX DOOR INNER SKIN ALONG LOWER EDGE IAW SRM 52-00-01.

Part: HANDLE — LACK OF LUBE (CABIN DOOR) · airframe 14,835 hrs · 10,132 cycles

REF ITEM 1 MAIN CABIN DOOR WILL NOT OPEN FROM OUTSIDE. LUBRICATED MAIN DOOR HANDLE & PERFORMED OPERATIONS CHECK IAW AMM 52-11-03, FOUND WORKING GOOD.

Part: DOOR — STUCK (CABIN) · airframe 14,835 hrs · 10,132 cycles

GATE AGENT REPORTS MAIN CABIN DOOR WILL NOT OPEN. PERFORMED GVI INSPECTION OF MAIN CABIN DOOR, FOUND DOOR TO NOT OPEN FROM OUTSIDE. VERIFIED DOOR OPERATION OF CABIN DOOR FROM INSIDE TO OPERATE NORMAL IAW AMM 52-11-00 REF ITEM 2.

Part: PCU — FAILED (SPOILER) · airframe 14,754 hrs · 10,071 cycles

OUTBOARD SPOILERS & OUTBOARD FLIGHT SPLRS, CAUTION MSG DISPLAYED IN DESCENT. TRANSFERRED TO NRWC 9 EACH ORD 01764. R & R MULTI-FUNCTION SPOILER PCU IAW AMM 27-62-01. OPERATIONS CHECKED GOOD.

Part: UNKNOWN — NOT REPORTED (CABIN PRESSURE) · airframe 14,597 hrs · 9,951 cycles

AIRCRAFT WILL NOT PRESSURIZE IN AUTO OR MANUAL MODE. COMPLIED WITH M PROCEDURE FOR MEL 21-6 & COMPLIED WITH PRESSURIZATION SYS. OPERATIONS CHECKED IAW AMM 21-31-00. FOUND SATISFACTORY AT THIS TIME.

Part: ACTUATOR — FAILED (LT MLG) · airframe 14,497 hrs · 9,878 cycles

MLG FAULT STATUS ON ED 2 FINAL APPROACH PREPARING TO LAND. TROUBLE SHOT IAW FIM 32-11-00-810-802. R & R LT MLG RETRACTION ACTUATOR IAW AMM 32-32-05. OPERATIONS & LEAK CHECKED GOOD.

Part: SENSOR — DEFECTIVE (LT MLG) · airframe 14,255 hrs · 9,705 cycles

BRAKE OVERHEAT, WARNING MSG OCCURRED AT ROTATION SPEED ON TAKEOFF. LT OTBD BRAKE TEMP CONTINUED RISING TO 18, BEFORE SLOWLY DROPPING BACK TO NORMAL. R & R THERMOCOUPLE SENSOR IAW AMM TASK 32-46-01. OPERATIONS CHECKED GOOD.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 13,285 hrs · 8,917 cycles

ON APPROACH, DECLARED EMER DUE INBD FLIGHT SPOILERS & SPOILERONS CAUTION MSG. EMER DECLARED & LANDED SAFELY. INTERROGATED MDC FOUND LT INBD MFS PCU & PCU JAM WAS NOTED. PERFORMED SPOST 1 RESET & PERFORMED OPERATIONS CHECK IAW ETN-CR-27-093. OPERATIONS CHECKED GOOD.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 13,186 hrs · 8,834 cycles

NUMBER 2 ENGINE N1 VIBRATION WENT INTO AMBER RANGE DURING CLIMB THROUGH FL 270. INSPECTED FAN BLADES FOR FREEDOM OF MOVEMENT WITH NO DEFECTS NOTED AND MAX VIBE AT .3 IPS AT TAKE OFF POWER. R & R BLADES IAW NRWC 9AE-DFW-01612.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 12,569 hrs · 8,334 cycles

BIRD STRIKE DAMAGE TO THE LT UPPER COCKPIT CANOPY. REPAIRED IAW ERS CR-53MR-1242. CANOPY SKIN PN CC670-33136-7S, FRAME PN CC670-33144-7.

Part: PULLEY — LACK OF LUBE (CABIN DOOR) · airframe 11,704 hrs · 7,665 cycles

MAIN CABIN DOOR WILL NOT OPEN FROM OUTSIDE. LUBRICATED DOOR PULLEYS & PERFORMED OPERATIONAL TEST OF PAX DOOR IAW AMM 52-11-00. OPERATIONS CHECKED OK.

Part: BRAKE — SMOKE (NR 2) · airframe 11,323 hrs · 7,310 cycles

NORMAL LANDING +TAXI LT BRAKE TEMP 5+8. LT BRAKE SMOKING ON POST FLIGHT. R & R NR 2 BRAKE ASSEMBLY IAW WC 32-007. TAXI CHECK COMPLIED WITH FOUND GOOD AT THIS TIME.

Part: LIGHT — BROKEN (CABIN) · airframe 11,018 hrs · 7,063 cycles

NUMBER 3 RT EMER LIGHT STRIP IS BROKEN & REQUIRES REPLACEMENT. RECEIVED FROM STORES, RT EMER LIGHT STRIP. SEE NRWC BOW160750 FOR INSTALLATION.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 11,000 hrs · 7,050 cycles

FIRST OFFICERS WINDSHIELD SHATTERED IN FLIGHT. R & R FIRST OFFICERS WINDSHIELD IAW AMM 56-11-01. OPERATIONS & LEAK CHECKED GOOD.

Part: RELAY — INOPERATIVE (DOOR ASSIST) · airframe 10,646 hrs · 6,781 cycles

PAX DOOR WILL NOT OPEN DUE TO DOOR MOTOR CONTINUOUSLY ON. PULLED CIRCUIT BREAKER 1 E1 PAX DOOR ASSIST. R & R PAX DOOR ASSIST MOTOR RELAY IAW AMM 20-42-00. OPS TESTED GOOD IAW AMM 52-11-08.

Part: STRUCTURE — DAMAGED (PAX DOOR) · airframe 10,605 hrs · 6,756 cycles

DAMAGE WAS FOUND ON THE PAX DOOR THAT HOLDS THE DOOR SEAL IN PLACE IN TWO AREAS. REPAIRED DAMAGED AREA IAW ERS-CR-5200-136 & AML 3373129 ITEM 3.

Part: STRUCTURE — BUCKLED (PAX DOOR) · airframe 10,604 hrs · 6,755 cycles

THERE IS EVIDENCE OF THE SIDE WALL BUCKLED JUST BELOW THE UPPER STEP ON THE LT & RT SIDE OF THE PAX DOOR. REPAIRED IAW ERS-CR-5200-137 IAW NRWC 9EA-MQT-01318 FOR BALANCING ENTRY.

Part: UNKNOWN — ODOR (CABIN) · airframe 10,432 hrs · 6,634 cycles

AFTER LANDING, FLIGHT ATTENDANT REPORTED BURNING SMELL IN CABIN. FOLLOWED & PERFORMED FIM TASK 21-22-00, IAW ITEMS 1-3 ON LOG PG 3559720, NO FAULTS NOTED. FOLLOWING FIM TASK 21-22-00, INSPECTED FOR CABIN LIGHTS FAILURE & SMELL CONCENTRATIONS IN GALLEY, CABIN & LAVATORY, NO FAULTS NOTED IAW FIM TASK 21-22-00. PERFORMED OPERATIONS TEST OF BOTH PACKS DURING ENG OPERATION IAW MM 71-00-00 & AMM 21-51-00, NO DISCREPANCIES NOTED. IAW FIM TASK 21-22-00, PERFORMED OPERATIONS TEST OF LT & RT PACK DURING APU START IAW AMM 21-51-00 & 49-10-00. DID NOT DUPLICATE PROBLEM.

Part: MANIFOLD — FAULTY (NLG STERING) · airframe 10,035 hrs · 6,372 cycles

S132 STEERING INOPERATIVE. AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE STEERING MANIFOLD IAW CRJ 700 AMM 32-51-50. LEAK CHECK, OPS CHECK AND BITE TEST GOOD.

Part: MOUNT BRACKET — BROKEN (FLASHLIGHT) · airframe 10,005 hrs · 6,354 cycles

FORWARD CABIN FLASHLIGHT MOUNTING BRACKET IS BROKEN. R & R FWD CABIN FLASHLIGHT IAW AMM 25-61-02. OPERATIONS CHECKED GOOD. NO FURTHER DEFECTS NOTED.

Part: PRESSURE SWITCH — FAULTY (NLG STEERING) · airframe 9,804 hrs · 6,219 cycles

ON FLIGHT 3129 CREW REPORTED STEERING INOPERATIVE. CAUTION MESSAGE AFTER GEAR RETRACTION. THE ACFT WAS REMOVED FROM SERVICE. DURING TROUBLESHOOTING MDC SHOWED NWS MANIFOLD PRESS SW FAULTY. R & R THE STEERING MANIFOLD PRESS SWITCH IAW AMM 32-51-35. OPERATIONS CHECKED GOOD AT THIS TIME.

Part: ACTUATOR — FAILED (LE SLAT) · airframe 9,542 hrs · 6,053 cycles

ON FLIGHT 3588 DURING APPROACH CREW SELECTED FLAPS 1 & RECEIVED AN EICAS SLATS FAIL MESSAGE WITH NO INDICATION THE SLATS HAD DEPLOYED. THE CREW RAN THE CHECKLIST & STILL NO SLATS. THE CREW COMPLIED WITH AOM VOL 1 PROCEDURES, DECLARED AN EMERGENCY & LANDED AT MSP WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. R & R THE SLAT ACTUATOR AT TRACK 3 3 LT SIDE IAW CRJ 700 AMM 27-81-09, OPERATIONS CHECKED GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SLAT SYSTEM — MALFUNCTIONED · airframe 9,478 hrs · 6,010 cycles

THE CREW REPORTED THAT ON DESCENT FOR APPROACH THEY RECEIVED A CAUTION MESSAGE ON EICAS FOR "SLATS FAIL" WHEN SELECTING SLATS/FLAPS 1 DEGREE. DECLARED AN EMERGENCY. LANDED WITHOUT INCIDENT AND REMOVED FROM SERVICE. PERFORMED SLAT TRIP INSPECTION IAW AMM 27-81-09-610-803. LEFT OTBD FOUND TRIPPED. INSPECTED FOR WATER IAW ETN-CR-27-084/SL 27-80. NO WATER NOTED. OPS CHECKED GOOD IAW AMM 27-50-00-701-801. THE ACFT WAS RETURNED TO SERVICE.

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 8,881 hrs · 5,637 cycles

CREW REPORTED THAT ON DESCENT DURING SELECTION OF FLAPS 8, RECEIVED A FLAPS & SLATS CAUTION MESSAGE. DECLARED AN EMERGENCY AND COMPLIED WITH AOM VOL 1 PROCEDURES. NOTICED THAT FLAP LEVER HAD STOPPED SHORT OF THE FLAPS 8 DETENT. ONCE FLAP HANDLE WAS REPOSITIONED, FLAPS OPERATED NORMALLY. ACFT LANDED WITHOUT INCIDENT AND REMOVED FROM SERVICE.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 8,090 hrs · 5,146 cycles

DURING B INSPECTION, FOUND THE AFT F/A FLASHLIGHT DOES NOT TURN ON. THE ACFT WAS REMOVED FROM SERVICE. R & R THE AFT F/A FLASHLIGHT AS REQUIRED. THE OPS TEST WAS GOOD IAW AMM 25-61-00. THE ACFT WAS RETURNED TO SERVICE.

Part: UNKNOWN — MALFUNCTIONED (FUEL SYSTEM) · airframe 7,428 hrs · 4,766 cycles

ON FLIGHT 3661 - THE CREW REPORTED THE XFLOW PUMP CONTINOUSLY TRANSFERRED. THE CREW DECLARED AN EMERGENCY AND DIVERTED TO SAT. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. INSPECTED AND OPS CHECKED FUEL XFLOW SYSTEM IAW CRJ700 AMM 28-13-00. ALL TESTS PASSED. NO FURTHER DEFECTS NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CRACKED (COCKPIT) · airframe 5,835 hrs · 3,781 cycles

DURING C CHECK INSPECTION, FOUND LEFT FLOOR SUPPORT ANGLE IN COCKPIT ENTRY CRACKED. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED FLOOR SUPPORT IAW EO CR-53MR-296. AIRCRAFT RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 5,835 hrs · 3,781 cycles

DURING C CHECK INSPECTION, FOUND RIGHT FLOOR SUPPORT ANGLE IN COCKPIT ENTRY CRACKED. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED FLOOR SUPPORT IAW EO CR-53MR-296. AIRCRAFT RETURNED TO SERVICE.

Part: CRADLE — DAMAGED (CABIN FLASHLIGHT) · airframe 4,326 hrs · 2,811 cycles

ON FLIGHT 3816, FLIGHT ATTENDANT REPORTED CLIP BROKEN OFF OF THE FLIGHT ATTENDANT FLASHLIGHT HOLDER. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE FLIGHT ATTENDANT’S NR 1 FLASHLIGHT AND HOLDER IAW AMM 25-61-02. THE OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: HOLDER — BROKEN (CABIN) · airframe 4,269 hrs · 2,779 cycles

ON FLIGHT 3738 THE CREW REPORTED THE FORWARD FLIGHT ATTENDANT FLASHLIGHT HOLDER WAS BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FLASHLIGHT BASE IAW CRJ 700 AMM 25-61-02 NO DEFECTS NOTED. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LATCH — LACK OF LUBE (COCKPIT DOOR) · airframe 3,725 hrs · 2,427 cycles

ON FLIGHT 3708 THE CREW REPORTED THE COCKPIT DOOR SLAM LATCH OPENED TWICE IN FLIGHT. THE AIRCRAFT WAS REMOVED FROM SERVICE. SUSPECT LATCH NOT CLOSED COMPLETELY DUE TO DIFFICULT OPERATION. LUBRICATED THE LATCH. THE OPERATIONAL CHECK WAS GOOD AS REQUIRED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ENGINE — VIBRATION (NR 1) · airframe 277 hrs · 176 cycles

ON FLIGHT 3703 THE CREW REPORTED THAT DURING CRUISE THE LEFT ENGINE NR 1 VIBRATIONS WERE HIGH. THE CREW FOLLOWED THE AIRCRAFT OPERATION AS MANUAL PROCEDURE AND COULD NOT MAINTAIN ALTITUDE WITH THRUST SETTING. THE CAPTAIN DECLARED AN EMERGENCY AND DIVERTED TO BNA WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED ENGINE RUNS FOR NR 1 ENGINE IAW CRJ AMM 71-00-00. FOUND TO BE WITHIN LIMITS. NO PARTS REMOVED OR REPLACED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WIRE — WRONG PART (CABIN) · airframe 182 hrs · 115 cycles

FOR FLIGHT 3859 DURING INSPECTION FOUND THE EMERGENCY EXIT LIGHT OVER SERVICE DOOR NOT ILLUMINATING WHEN THE EMERGENCY LIGHTS WERE SELECTED ON. THE AIRCRAFT WAS REMOVED FROM SERVICE. INSPECTED AIRCRAFT AND FOUND WIRE ENDS P330 AND J328 ON WRONG WIRES. REPAIRED WIRES IAW CRJ EECSPM 20-33-00. THE OPERATIONAL CHECK OF THE EMERGENCY LIGHTS WERE GOOD IAW CRJ MM 33-51-00. THE AIRCRAFT WAS RETURNED TO SERVICE.