N534AE

Part: SKIN — DENTED (ZONE 100) · airframe 31,556 hrs · 24,746 cycles

LH SIDE FWD FUSELAGE DENT (REO) 670-53-11-2108 / C/W REO 670-53-11-2108 REPAIR FOR DENT DAMAGE TO UPPER FUSELAGE SKIN PANEL BETWEEN FS 220.00 - FS250.00 AND STR12L - STR15L

Part: SKIN — DAMAGED (ZONE 100) · airframe 31,556 hrs · 24,746 cycles

(RH) NOSE SKIN DAMAGED AFT OF TRU ACCESS PANEL / C/W REO 670-53-11-815 REPAIR TO UPPER SECTOR FS193.00.

Part: STRINGER SPLICE — CORRODED (ZONE 500) · airframe 28,876 hrs · 22,491 cycles

CORROSION FOUND ON STR 25R @ MULTIPLE LOCATIONS FROM F.S 280 THRU F.S 333. 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: SKIN — CHAFED (ZONE 500) · airframe 28,876 hrs · 22,491 cycles

L/H WING, LOWER WING SKIN IS CHAFED JUST FORWARD OF OUTBOARD FLAP, MID HINGE BOX. DAMAGE IS FROM CONTACT WITH HINGE BOX. REPAIRED IAW OLIVER WYMAN EA 23-C7-57-1297 REV IR DATED 09/20/2023.

Part: SKIN — CHAFED (ZONE 600) · airframe 28,876 hrs · 22,491 cycles

R/H WING, LOWER WING SKIN HAS CHAFE DAMAGE JUST FORWARD OF THE OUTBOARD FLAP, MIDDLE HINGE BOX. DAMAGE IS FROM CONTACT WITH HINGE BOX FAIRING. REPAIRED IAW EA 23-C7-57-1290 REV IR DATED 09/19/2023.

Part: SKIN — CHAFED (ZONE 500) · airframe 28,876 hrs · 22,491 cycles

L/H WING, LOWER WING SKIN IS CHAFED JUST FORWARD OF OUTBOARD FLAP, MID HINGE BOX. DAMAGE IS FROM CONTACT WITH HINGE BOX FAIRING. REPAIRED IAW EA 23-C7-57-1297 REV IR DATED 09/20/2023.

Part: SKIN — CHAFED (ZONE 500) · airframe 28,876 hrs · 22,491 cycles

/H WING, LOWER WING SKIN IS CHAFED JUST FORWARD OF INBOARD FLAP, OUTBOARD HINGE BOX. DAMAGE IS FROM CONTACT WITH HINGE BOX FAIRING. REPAIRED IAW EA 23-C7-57-1251 REV IR DATED 09/20/2023.

Part: SKIN — CHAFED (ZONE 600) · airframe 28,876 hrs · 22,491 cycles

R/H WING, LOWER WING SKIN HAS CHAFE DAMAGE JUST FORWARD OF THE OUTBOARD FLAP, OUTBOARD HINGE BOX. DAMAGE IS FROM CONTACT WITH HINGE BOX FAIRING. REPAIRED IAW EA 23-C7-57-1291 REV IR DATED 09/19/2023.

Part: FRAME — CHAFED (ZONE 100) · airframe 28,876 hrs · 22,491 cycles

FRAME @ F.S 319 STR 25 R HAS CORROSION. REPAIRED IAW CRJ 700 SRM 53-00-06-201-006-A01.

Part: SKIN — CHAFED (ZONE 600) · airframe 28,876 hrs · 22,491 cycles

R/H WING, LOWER WING SKIN HAS CHAFE DAMAGE JUST FORWARD OF THE OUTBOARD FLAP, INBOARD HINGE BOX. DAMAGE IS FROM CONTACT WITH HINGE BOX FAIRING. REPAIRED IAW EA 23-C7-57-1245 REV IR DATED 09/19/2023.

Part: SEAT TRACK — CORRODED (UNKNOWN) · corrosion level 2 · airframe 22,461 hrs · 28,846 cycles

LH #5 SEAT TRACK IS CORRODED AT LBL 9.

Part: SKIN — DAMAGED (LT WING TE FLAP) · airframe 22,461 hrs · 28,846 cycles

LH I/B FLAP PANEL 584KB & UNDERLYING STRUCTURE HAS 1EA ELONGATED HOLE.

Part: SEAT TRACK — CORRODED (UNKNOWN) · corrosion level 2 · airframe 22,461 hrs · 28,846 cycles

.LH #2 SEAT TRACK IS CORRODED AT LBL 9

Part: CLEAT — CORRODED (UNKNOWN) · corrosion level 2 · airframe 22,461 hrs · 28,846 cycles

PAX DOOR CLIPS THAT ATTACH TO THE FWD AND AFT ENDS OF "ANGLE C" LOCATED ON INNER PORTION OF OUTER HANDLE BOX BELOW HINGE ARE CORRODED.

Part: SEAT TRACK — CORRODED (UNKNOWN) · corrosion level 2 · airframe 22,461 hrs · 28,846 cycles

REMOVED AND REPLACED IAW CRJ 700 AMM 53-00-49-000/400-801-A01 AND CRJ 700 SRM 51-40-11-001-001-A01.

Part: STRINGER SPLICE — CORRODED (UNKNOWN) · corrosion level 2 · airframe 22,461 hrs · 28,846 cycles

STRINGER 26R SPLICE AT F.S. 333.00 IS CORRODED

Part: STRINGER — CORRODED (UNKNOWN) · corrosion level 2 · airframe 22,461 hrs · 28,846 cycles

STRINGER 26R AT F.S. 300.00 HAS CORROSION AROUND FASTENER HOLE.

Part: FORMER — CORRODED (UNKNOWN) · corrosion level 2 · airframe 22,461 hrs · 28,846 cycles

REMOVED AND REPLACED IAW CRJ700 SRMS 51-40-11-001-001-A01, 51-42-06-001-001-A01, 51-42-13-001-001-A01, AND 51-42-21-001-001-A01.

Part: STRAP — CORRODED (UNKNOWN) · airframe 22,461 hrs · 28,846 cycles

670-57-21-867_REV-A (PERM REPAIR-LOWER SKIN ASSY AND INSTL WINGBOX) REPAIR IAW REO-670-57-21-867 WITHIN 8000 FH OR NEXT "C" CHECK.

Part: STIFFENER — CRACKED (UNKNOWN) · airframe 22,461 hrs · 28,846 cycles

FWD PAX DOOR WEB STIFFENER IS CRACKED.

Part: SKIN — CRACKED (PAX DOOR) · airframe 22,461 hrs · 28,846 cycles

FOUND CRACK ON PAX DOOR INNER SKIN AT PANEL CUTOUT.

Part: DOOR SILL — CORRODED (UNKNOWN) · corrosion level 2 · airframe 22,461 hrs · 28,846 cycles

AFT CARGO DOOR SILL IS CORRODED BEYOND REPAIRABLE LIMITS

Part: INTERCOSTAL — CORRODED (UNKNOWN) · corrosion level 2 · airframe 22,461 hrs · 28,846 cycles

STRINGER 27 RH INTERCOSTAL IS CORRODED BETWEEN FS 349.00 AND 364.00.

Part: ANGLE — CORRODED (UNKNOWN) · corrosion level 2 · airframe 22,461 hrs · 28,846 cycles

PAX DOOR SILL ANGLE IS CORRODED.

Part: ANGLE — CORRODED (UNKNOWN) · corrosion level 2 · airframe 22,461 hrs · 28,846 cycles

PAX DOOR LOWER SILL MID CAP ANGLE IS CORRODED.

Part: JOINT — CHAFED (UNKNOWN) · airframe 22,461 hrs · 28,846 cycles

FS 280.00 CIRCUMFERENTIAL JOINT IS CORRODED BETWEEN STRINGER 27 AND 26R.

Part: COAMING — CHAFED (RT NACELLE) · airframe 22,461 hrs · 28,846 cycles

RH UPPER TRANSCOWL FWD HOOK LATCH (INNER DOUBLER) IS CHAFED.

Part: INTERCOSTAL — CORRODED (UNKNOWN) · corrosion level 2 · airframe 22,461 hrs · 28,846 cycles

STRINGER 20R INTERCOSTAL IS CORRODED BETWEEN FS 319.70 AND 349.00.

Part: STIFFENER — CRACKED · airframe 22,461 hrs · 28,846 cycles

FWD PAX DOOR WEB STIFFENER IS CRACKED.

Part: FLOOR SUPPORT — CORRODED (UNKNOWN) · corrosion level 2 · airframe 22,461 hrs · 28,846 cycles

RH FLOOR SILL IS CORRODED BETWEEN FS 280.00 AND 319.70.

Part: ANGLE — CORRODED (UNKNOWN) · corrosion level 2 · airframe 22,461 hrs · 28,846 cycles

GALLEY SERVICE DOOR SILL ANGLE IS CORRODED.

Part: FRAME — CORRODED (UNKNOWN) · corrosion level 2 · airframe 22,461 hrs · 28,846 cycles

F.S. 310.00 FRAME IS CORRODED BETWEEN STRINGER 26L AND STRINGER 26R.

Part: SELECTOR VALVE — FAULTED (MLG) · airframe 27,672 hrs · 21,427 cycles

ONCE IN GEAR UP POSITION GOT GEAR DISAGREE WITH IND. THREE GREEN WHILE HANDLE IN UP POSITION. ALSO GOT NWS INOP CAUT MSG. REMOVED AND REPLACED LANDING GEAR SELECTOR VALVE IAW CRJ 700 AMM 32-32-10-000/400-801-A01 OPS CHECK GOOD, GEAR SWING GOOD.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 22,762 hrs · 17,006 cycles

SLATS FAIL CAUTION WHEN DEPLOYING FLAPS FOR LANDING. FLAPS 45 SLATS 0. PERFORMED SELF TEST OF SFECU IAW CRJ 700 AMM 27-51-05-740-801. TEST PASSED. PERFORMED OPS TEST OF FLAPS / SLATS SYSTEM IAW 27-50-00-710-801. OPS TEST GOOD.

Part: SLAT SYSTEM — MALFUNCTIONED · airframe 22,598 hrs · 16,881 cycles

20 MIN OUT OF DCA THE CREW RECEIVED A SLAT FAIL MSG. THEY DIVERTED TO IAD FOR THE RW LENGTH. AC LANDED, AND TAXIED TO THE GATE SAFE. CLEARED SFECU INHIBITS IAW CRJ 700 AMM. PERFOMED SELF TEST OF SFECU AND OPS TEST OF SLATS AND FLAPS SYSTEM IAW CRJ 700 AMM. TESTS PASSED OPS CHECK GOOD.

Part: STRINGER — CRACKED (BS 280) · airframe 21,410 hrs · 15,830 cycles

AFT OF FS280 AT STR 3L, LINTEL IS CRACKED APPROX 1" LONG. REPAIRED PAX DOOR LINTEL (STR 3LZ) IAW REO 670-53-21-493 REV D DATE 2015-07-10 AND SB#670BA-53-040 PART B.

Part: FLOOR SUPPORT — CORRODED (BS 1000-1047) · corrosion level 2 · airframe 21,410 hrs · 15,830 cycles

AFT CARGO DOOR FLOOR SILL ANGLE IS CORRODED BETWEEN FS 1000 AND FS 1047.00. REPAIRED AFT CARGO DOOR FLOOR SILL ANGLE BETWEEN FS 1000 TO FS 1047 IAW BOMBARDIER REO #670-53-61-913 REV A DATE 2012-11-02.

Part: SEAT TRACK — CORRODED (BS 581-677) · corrosion level 2 · airframe 21,410 hrs · 15,830 cycles

LBL 9 SEAT RAIL, 3RD FROM FRONT, STARTING AT APPROX FS581.00 GOUGED/CORRODED IN MULTIPLE LOCATIONS. FABRICATED DRILLED AND INSTALLED NEW SERVICEABLE SEAT TRACK AMM 53-00-49-400-801-A03 SEAT TRACK LBL 9 FROM FS 581-FS 677 SRM 53-00-49-201-002-A01.

Part: FRAME — CORRODED (BS 349) · corrosion level 2 · airframe 21,410 hrs · 15,830 cycles

FS 349 FRAME IS CORRODED ON AFT SIDE BETWEEN STR27 & 26R. REPAIRED FS 349 AFT SIDE BETWEEN STR 27 AND 26R IAW REO 670-53-21-1308.

Part: DRAG ANGLE — CRACKED (NOT REPORTED) · airframe 21,410 hrs · 15,830 cycles

LEFT AFT FUSELAGE AFT DRAG ANGLE CRACKED. INSTALLED NEW L/H AFT FUSELAGE AFT DRAG ANGLE IAW CRJ700 SRM 51-42-10-001-001-A01, 51-42-21-001-A01.

Part: FRAME — CORRODED (BS 333) · corrosion level 2 · airframe 21,410 hrs · 15,830 cycles

FS333 FRAME IS CORRODED ON AFT SIDE BETWEEN STR 27 & 26R. REPAIRED FS 333 ON AFT SIDE BETWEEN STR 27 AND STR 26L AND STR 27 AND STR 26L IAW REO 670-53-21-1308.

Part: SEAT TRACK — CORRODED (BS 581-677) · corrosion level 2 · airframe 21,410 hrs · 15,830 cycles

RBL 9 SEAT RAIL, 3RD FROM FRONT, STARTING AT APPROX FS581.00 CORRODED. FABRICATED DRILLED AND INSTALLED NEW SERVICEABLE SEAT TRACK AMM 53-00-49-400-801-A03 SEAT TRACK RBL 9 FROM FS 581-FS 677 SRM 53-00-49-201-002-A01.

Part: SHUTOFF VALVE — FAILED (BLEED SYS) · airframe 21,348 hrs · 15,780 cycles

DURING CRUISE AT 35,800 FEET THE CREW RECEIVED A BLEED DUCT WARNING MESSAGE. THE OXYGEN MASKS DEPLOYED AND THE CREW FOLLOWED THE INSTRUCTIONS OF THE QRH AND LANDED AT THE NEAREST SUITABLE AIRPORT USING A DESCENT RATE OF 4200-4500 FPM. THE FLIGHT LANDED WITHOUT INCIDENT HOWEVER, AN EMERGENCY WAS DECLARED AND TRUCKS ROLLED. THE AIRCRAFT WILL FERRY TO CVG WHERE THEY REPLACED THE RH ENGINE HIGH PRESSURE SOV, PRSOV AND REPLACED A DAMAGED O-RING IN THE RH BLEED DUCT. OPS CHECKS AND LEAK CHECKS GOOD.

Part: CONTROLLER — FAILED (AILC) · airframe 21,284 hrs · 15,718 cycles

R BLEED DUCT (W/C) AND L BLEED DUCT (W/C) ALONG WITH RH/LH COWL A/I CAUTIONS. AS A RESULT BLEED VALVES CLOSED AND CABIN PRESSURE WAS LOST AIRCRAFT DIVERTED TO PITTSBURGH. GROUND RAN AIRCRAFT AND C/W LEAK CHECKS OF BLEED DUCTS AND A/C UNITS, NO LEAKS FOUND. FERRIED AIRCRAFT TO CAK. R&R AILC, OPS AND LEAK CHECKS ALL GOOD.

Part: SMOKE DETECTOR — FALSE ACTIVATION (AFT LAVATORY) · airframe 17,845 hrs · 12,585 cycles

THE CREW REPORTED AN AFT LAVATORY WARNING MESSAGE. THERE WAS NO PHYSICAL SMOKE OR ODOR OF SMOKE. THE SMOKE DETECTOR ALARM WILL NOT TURN OFF. MX R & R THE LAVATORY SMOKE DETECTOR. OPS CHECKED GOOD.

Part: BPSU — WARNING MESSAGE (FLAP SYSTEM) · airframe 17,354 hrs · 12,159 cycles

CREW RECEIVED FLAPS FAIL MESSAGE ON RETRACTION. RAN CHECKLIST AND DECLARED EMERGENCY. R & R THE LT BPSU, OPS CHECKED GOOD.

Part: FADEC — FAILED (LEFT) · airframe 16,748 hrs · 11,605 cycles

FLIGHT DIVERTED DUE TO AN AMBER LEFT FADEC CAUTION MESSAGE. WAS ABLE TO TAXI TO A GATE. MX REPLACED THE FADEC.

Part: DOUBLER — CRACKED (PAX DOOR) · airframe 16,737 hrs · 11,594 cycles

PAX DOOR PULL IN CAM DOUBLER CRACKED. REPLACED THE DOUBLER.

Part: STIFFENER — CRACKED (BS 202) · airframe 16,637 hrs · 11,503 cycles

FUSELAGE BULKHEAD AT BS 202.75 STIFFENER AT RBL 30 LOWER END FOUND BENT AND CRACKED. REPAIRED IAW ERS-CR-53MR-2412.

Part: SHUTOFF VALVE — MALFUNCTIONED (APU) · airframe 16,343 hrs · 11,268 cycles

APU SHUTOFF VALVE OPEN WITH APU OFF. PERFORMED AN OPS TEST OF THE APU FUEL FEED SYSTEM IAW AMM 28-24-00-710-801, OPS TESTED GOOD.

Part: SKIN — DENTED (BS 364-379) · airframe 15,955 hrs · 10,951 cycles

DENT LOCATED ON THE RT FUSELAGE SKIN BETWEEN BS 364 AND 379, STRINGERS 16 AND 17R. REPAIRED IAW SRM 53-00-01.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 15,867 hrs · 10,880 cycles

ILLUMINATED EXIT SIGNS AT PAX DOOR AND GALLEY CEILING, AND FWD 2 CABIN OVERHEAD EMERGENCY LIGHTS DO NOT ILLUMINATE. REMOVED AND REPLACED THE NR 1 EPSU BATTERY PACK AND CHARGER IAW AMM 33-51-17. OPS CHECKED GOOD.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHTS) · airframe 15,468 hrs · 10,543 cycles

TWO EMERGENCY LIGHTS RT AFT OVERWING INOPERATIVE. CONNECTED P876 CONNECTOR FOR RH O/W EMERGENCY EXIT LIGHT. OP TEST GOOD IAW 33-51-15-710-801.

Part: BRACKET — CRACKED (THRUST REVERSER) · airframe 15,436 hrs · 10,513 cycles

RIGHT UPPER TRANSCOWL INBD STANDOFF BRACKET IS CRACKED. REMOVED AND REPLACED THE STANDOFF BRACKET IAW ETN CR-54-015R1.

Part: SKIN — DAMAGED (BS 210-235) · airframe 15,428 hrs · 10,506 cycles

RT UPPER NOSE SKIN PANEL HAS FIVE DAMAGED AREAS BETWEEN BS 210 AND 235, STRINGERS 15AR AND SKIN SPLICE. REMOVED AND REPLACED THE SKIN PANEL IAW ERS-CR=53MR-2327. MAJOR REPAIR.

Part: SKIN — GOUGED (BS 220) · airframe 15,428 hrs · 10,506 cycles

RIGHT MIDDLE SKIN PANEL GOUGED FS 220 ABOVE STRINGER 17R. REPAIRED IAW ERS-CR-53MR-2327. MAJOR REPAIR.

Part: SKIN — DENTED (BS 193) · airframe 15,427 hrs · 10,505 cycles

DENT LOCATED AT STRINGER 16 - 17R FWD OF BS 193. INSTALLED SERVICABLE SKIN PANEL IAW SRM 51-40-06. MAJOR REPAIR.

Part: UNKNOWN — MALFUNCTIONED (SPOILER SYS) · airframe 15,388 hrs · 10,474 cycles

OTBD SPOILERONS AND OTBD FLIGHT SPOILERS CAUTION MESSAGE DISPLAYED DURING FLIGHT SPOILER DEPLOYMENT DURING FLIGHT. INTERROGRATED MDC. FOUND RT OTBD MFS PCU JAM MDC MESSAGE. PERFORMED SPOST 1 RESET. PERFORMED OPS CHECK IAW ETN-CR-27-093. OPS CHECK GOOD.

Part: SENSOR — FAULTY (MLG BRAKE) · airframe 14,855 hrs · 10,088 cycles

BRAKE OVERHEAT WARNING DURING APPROACH. NR 4 INDICATION 20. RETURNED TO ZERO AFTER GEAR EXTENSION. R & R NR 4 MLG RT OTBD BRAKE IAW W/C 32-007. OPS CHECK GOOD. SUSPECT FAULTY HARNESS FROM PX09J1 TO P616. REMOVED AND REPLACED NR 4 BTMS IAW AMM 32-61-05 OPS CHECK GOOD MEL RESTORED.

Part: SENSOR — FAILED (BRAKE SYSTEM) · airframe 14,807 hrs · 10,056 cycles

BRAKE OVERHEAT WARNING IN FLIGHT, DECLARED EMER, ACFT TOWED TO GATE. ITEM 1 AML PG 4016169. MDC SHOWS RT OTBD TEMP SENSOR FAIL. DEFERRED RT OTBD BTMS M PROCEDURE COMPLIED WITH. R & R NR 4 BRAKE TEMP SENSOR IAW AMM 32-46-01. OPS CHECK GOOD. MEL ITEM RESTORED.

Part: TRIM SWITCH — MALFUNCTIONED (COCKPIT) · airframe 13,737 hrs · 9,242 cycles

AFTER TAKEOFF ROTATION CA PITCH TRIM NOSE DOWN INOPERATIVE. SERVICED PITCH TRIM SWITCHES CA IAW AMM 12-20-27. OPERATIONS CHECKED GOOD.

Part: SHUTOFF VALVE — FAILED (RT A/C PACK) · airframe 13,674 hrs · 9,198 cycles

WHILE CRUISING AT FL 370. THE RT PACK WOULD CYCLE OFF & ON. DESCENDED TO FL 310 & THE ISSUE CONTINUED. WE NOTICED THAT THE RT BLEED PSI FLUCTUATE, BETWEEN 49 & 29, WHILE THE PACK WAS ON. R & R RT PRSOV. OPERATIONS & LEAK CHECKED GOOD IAW AMM 36-12-01.

Part: O-RING — FAILED (HYD SYSTEM) · airframe 12,143 hrs · 7,975 cycles

JUST PRIOR TO LEVEL OFF, HYD 2 LOW PRESSURE CAUTION MESSAGE FOLLOWED BY, IB FLT SPOILERS, IB SPOILERONS, ON EDI. R & R O-RINGS ON HYD 2 DAMPENER & AFT HOSE ASSEMBLY ON HYD 2 DAMPENER IAW AMM 29-11-60.

Part: ACTUATOR — TRIPPED (LE SLAT) · airframe 11,418 hrs · 7,402 cycles

DURING APPROACH SLATS FAIL CAUTION POSTED WHEN TRYING TO EXTEND THE FLAPS 1. SLATS DID NOT MOVE. SLATS FAIL CAUTION REMAINS ON T0 PARKING. FOUND LT SLAT ACTUATOR 3-3 TO BE TRIPPED. RESET TRIP INDICATOR IAW AMM 27-81-09. ACCOMPLISHED ETN-CR-27-084. OPERATIONS CHECKED GOOD. 1ST OCCURRENCE.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 11,207 hrs · 7,246 cycles

FIRST OFFICER'S FLASHLIGHT WILL NOT HOLD CHARGE. R & R WITH SERVICEABLE FLASHLIGHT BATTERY ASSEMBLY. OPERATIONS CHECKED OK.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 11,088 hrs · 7,154 cycles

FOUND SUPPORT STIFFENER FOR BAGGAGE FIRE BOTTLE MOUNT CRACKED. MARKED WITH RED GREASE PENCIL. INSTALLED NEW SUPPORT STIFFENER FOR BAGGAGE FIRE BOTTLE MOUNT IAW SRM 51-42-06.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 11,088 hrs · 7,154 cycles

PASSENGER DOOR AFT DRAG ANGLE IS CRACKED BY THE ASSIST CABLE PULLEY. REPAIRED PAX DOOR AFT DRAG ANGLE IAW SRM 52-11-04.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 11,088 hrs · 7,154 cycles

STRAP & STIFFENER CRACKED BETWEEN PANELS 196DR & 196DL. R & R STRAP & STIFFENER FOR SPLICE BETWEEN PANELS 196DR & 195DL IAW AMM 51-42-13. PERFORMED ETN-CR-53-052 ON STIFFENER. APPLIED PROTECTIVE COATINGS TO ALL NEW PARTS IAW SRM 51-25-06 & 51-25-16.

Part: BRACKET — CRACKED (LT WING) · airframe 11,088 hrs · 7,154 cycles

LEFT WING TELESCOPIC DUCT CLOSING PLATE BRACKET IS CRACKED. REMOVED LT WING TELESCOPIC DUCT CLOSING PLATE TO EVALUATE CRACKED BRACKET. FOUND THERE TO BE NO CRACK IN THE CLOSING PLATE BRACKET OR ANY ASSOCIATED CLOSING PLATE PARTS. REINSTALLED CLOSING PLATE IAW AMM 57-41-05.

Part: WEB — CRACKED (FUSELAGE) · airframe 11,088 hrs · 7,154 cycles

FORWARD EQUIPMENT COMPARTMENT RT FLOOR WEB CRACKED. REPAIRED IAW ETN-CR-53-099.

Part: WEB — CRACKED (FUSELAGE) · airframe 11,088 hrs · 7,154 cycles

FORWARD EQUIPMENT COMPARTMENT LT FLOOR WEB CRACKED. REPAIRED IAW ETN-CR-53-099.

Part: PCU — FAILED (SPOILER) · airframe 10,598 hrs · 6,736 cycles

ON THE DESCENT OTBD SPOILERON MSG APPEARED, FLT CONTROL PAGE RT WING NR 4 BOX YELLOW, RT WING NR 1 BOX WHITE. PERFORMED SPOST TEST IAW AMM 27-61-05 ALL MSGS CLEARED IAW TDMI 534T2722. RT OTBD PCU R & R IAW ETN CR-27-093. TDMI REMAINS OPEN FOR 1 FLIGHT DAY. ACFT OK FOR SERVICE. R & R RT OTBD PCU IAW AMM 27-62-01. OPERATIONS CHECKED GOOD. TDMI ITEM RESTORED.

Part: SPOILER — MALFUNCTIONED (WING) · airframe 10,526 hrs · 6,690 cycles

OB SPOILERONS CAUTION MSGS POSTED ON DESCENT UPON ACTIVATION OF FLIGHT SPOILER HANDLE. RESET SPOILERON SYS IAW ETN-CR-27-093. MSGS CLEARED.

Part: INSULATOR — FAILED · airframe 10,521 hrs · 6,686 cycles

DUCT MON FAULT. FOUND INSULATOR AT MT205P1 BAD. REMOVED AND REPLACED INSULATOR IAW ETN-CR-36-016 OPS CHECKED IAW AMM 36-21-00 OPS CHECKED GOOD.

Part: SKIN — PUNCTURED (FUSELAGE) · airframe 8,468 hrs · 5,328 cycles

PUNCTURE REAR OF RT FUSELAGE BELOW 2 ENGINE. REPAIRED RT FUSELAGE IAW SRM 53-00-01.

Part: STRUT — DAMAGED (PAX DOOR) · airframe 7,195 hrs · 4,543 cycles

FLIGHT 3743. MAIN CABIN DOOR DIFFICULT TO OPEN. DOOR WENT DOWN QUICKLY. CABLES APPEARED TO BE LOOSE. AIRCRAFT REMOVED FROM SERVICE. REPLACED BOTH PASSENGER DOOR COUNTER BALANCE STRUTS IAW MM 52-11-17. OPS CHECKED GOOD. REMOVED AND REPLACED CABIN DOOR POWER ASSIST MOTOR IAW MM 52-11-08. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: FLASHLIGHT — UNSERVICEABLE (COCKPIT) · airframe 6,929 hrs · 4,376 cycles

ON FLIGHT 3725 THE CREW REPORTED THE FIRST OFFICER’S FLASHLIGHT WAS NOT CHARGING IN THE HOLDER. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FIRST OFFICER’S FLASHLIGHT IAW CRJ 700 AMM 25-61-02. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 5,255 hrs · 3,302 cycles

FLIGHT 3630, CREW REPORTED THAT ON PUSHBACK, FLIGHT ATTENDANT ADVISED PASSENGER "SMELLED SMOKE". AIRCRAFT REMOVED FROM SERVICE. RAN APU AND TURNED ON PACKS. OPENED GASPERS AND TURNED ON ALL LIGHTING. WALKED THROUGHOUT CABIN . NO ODOR OR SIGHT OF ANY SMOKE. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: COUNTERBALANCE — LOOSE (MAIN DOOR) · airframe 3,228 hrs · 2,084 cycles

ON FLIGHT 3873 THE CREW REPORTED THE MAIN DOOR WILL NOT CLOSE. THE HINGE PIECE APPEARS OUT OF ALIGNMENT AT FORWARD BOTTOM PART OF THE DOOR. THE AIRCRAFT WAS REMOVED FROM SERVICE. RE-SECURED PASSENGER DOOR FORWARD SWIVEL LEVER (COUNTER BALANCE) IAW CRJ 700 MM 52-11-17. NO PARTS REMOVED OR REPLACED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WARNING SYSTEM — FALSE ACTIVATION (FUEL SYSTEM) · airframe 1,297 hrs · 839 cycles

ON FLIGHT 3761 DURING CLIMB THE CREW REPORTED, RECEIVED AN X-FLOW PUMP FAIL CAUTION MESSAGE INFLIGHT WITH FUEL IMBALANCE CAUTION MESSAGE AND AS HIGH AS 1000 LBS IMBALANCE WITHIN MINUTES. INDICATIONS SHOWED 300 LBS INTO CENTER TANK. THE CAPTAIN DECLARED AN EMERGENCY AND ELECTED TO RETURN TO SLC. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. CLEARED XFLOW PUMP CAUTION MESSAGE IAW ETN CR-28-007. NO PARTS REMOVED OR REPLACED. NO MESSAGES NOTED ON EICAS AT THIS TIME. THE AIRCRAFT WAS RETURNED TO SERVICE.