N535EA

Part: DRAG ANGLE — CRACKED (UNKNOWN) · airframe 40,725 hrs · 30,328 cycles

HN 115604 DISCREPANCY: PASSENGER DOOR AFT DRAG ANGLE CRACKED AT MOTOR ASSIST CABLE PULLEY MOUNT CORRECTIVE ACTION: REMOVED AND REPLACED IAW CRJ 700 SRMS 51-40-11-001-001-A01, 51-42-06-001-001-A01, AND 51-42-14-001-001-A01.

Part: STRINGER SPLICE — CRACKED (UNKNOWN) · airframe 40,725 hrs · 30,328 cycles

HN 118006 DISCREPANCY: STRINGER 24R SPLICE AT F.S. 333.00 HAS CORROSION. CORRECTIVE ACTION: REMOVED AND REPLACED SPLICE I.A.W. BOMBARDIER CRJ700 SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01

Part: CLEAT — CORRODED (UNKNOWN) · airframe 40,725 hrs · 30,328 cycles

HN 116511 DISCREPANCY: CLEAT AT DATUM 7, F.S. 338.00 IS CORRODED. CORRECTIVE ACTION: REMOVED AND REPLACED CLEAT I.A.W. BOMBARDIER CRJ700 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.

Part: FRAME — CORRODED · airframe 40,725 hrs · 30,328 cycles

HN116508 DISCREPANCY: FS 280 CIRCUMFERENTIAL JOINT IS CORRODED BETWEEN STGR 25L AND STGR 26R. CORRECTIVE ACTION: REPAIRED F.S. 280 CIRCUMFERENTIAL SPLICE STRAP IAW EA 23-C7-53-1582, REV IR, DATED 10/31/2023.

Part: INTERCOSTAL — CORRODED · airframe 40,725 hrs · 30,328 cycles

HN 116505 DISCREPANCY: INTERCOSTAL AT DATUM 6 BETWEEN F.S. 320 AND F.S. 338 IS CORRODED. CORRECTIVE ACTION: REMOVED AND REPLACED INTERCOSTAL I.A.W. BOMBARDIER CRJ700 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.

Part: STIFFENER — CRACKED (UNKNOWN) · airframe 40,725 hrs · 30,328 cycles

HN 117741 DISCREPANCY: FOUND PAX DOOR STAIR AFT WEB SIDEWALL STIFFENER PN: 601R317745-7 FOR POWER ASSIST PULLEY MOTOR TO BE CRACKED. CORRECTIVE ACTION: REMOVED DAMAGED STIFFENER PN: 601R317745-7 IAW CRJ-700 SRM 51-42-06-001-001-A01 AND INSTALLED NEW STIFFENER PN 601R317745-7 IAW CRJ700 SRM 51-42-06-001-001-A01.

Part: ACCESS PANEL — CORRODED (UNKNOWN) · airframe 40,725 hrs · 30,328 cycles

HN 116286 DISCREPANCY: PANEL 542BZ HAS LIGHT CORROSION. CORRECTIVE ACTION: REMOVED AND REPLACED PANEL.

Part: STRINGER — CORRODED (UNKNOWN) · airframe 40,725 hrs · 30,328 cycles

HN 116984 DISCREPANCY: STGR 23R IS CORRODED BETWEEN FS 333 AND FS 349. CORRECTIVE ACTION: REMOVED CORRODED STRINGER AND SPLICE. FABRICATED NEW STRINGER AND SPLICE AND INSTALLED NEW PARTS IAW CRJ 700 SRM 53-00-03-201-001-A01.

Part: CLEAT — CORRODED (UNKNOWN) · airframe 40,725 hrs · 30,328 cycles

HN 116510 DISCREPANCY: CLEAT AT DATUM 7, F.S.327 IS CORRODED. CORRECTIVE ACTION: REMOVED AND REPLACED CLEAT I.A.W. BOMBARDIER CRJ700 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.

Part: SUPPORT WEB — CRACKED (UNKNOWN) · airframe 40,725 hrs · 30,328 cycles

HN00116233 DISCREPANCY: PAX DOOR STAIR AFT WEB HAS MULTIPLE CRACKS AND PREVIOUS REPAIRS THAT INTERFERE WITH INTEGRATION OF STRUCTURAL MODIFICATIONS. REQUIRES REPLACEMENT. CORRECTIVE ACTION: REMOVED PAX DOOR AFT WEB, INSTALLED A SERVICEABLE PAX DOOR AFT WEB IAW CRJ 700 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, 51-42-14-001-001-A01.

Part: ANGLE — CORRODED (UNKNOWN) · airframe 40,725 hrs · 30,328 cycles

HN116508 DISCREPANCY: TOP ANGLE AT INTERCOSTAL AT DATUM 7 BETWEEN FS 327 AND FS 338 IS CORRODED CORRECTIVE ACTION: REMOVED AND REPLACED IAW CRJ 700 SRMS 51-40-11-001-001-A01 AND 51-42-021-001-001-A01.

Part: FRAME — CORRODED · airframe 40,725 hrs · 30,328 cycles

HN 116919 DISCREPANCY: FRAME AT FS863 CORRODED ON AFT FACE BETWEEN STR26L-STR26R. CORRECTIVE ACTION: REPAIRED DAMAGE I.A.W. OLIVER WYMAN CAVOK EA 23-C7-53-1520 REV.IR, DATED 11/09/2023

Part: FRAME — CORRODED (UNKNOWN) · airframe 40,725 hrs · 30,328 cycles

HN 116920 DISCREPANCY: FRAME AT FS879 CORRODED ON FWD AND AFT FACE BETWEEN STR25L-STR26R. CORRECTIVE ACTION: REPAIRED FRAME AT F.S. 879 BETWEEN STGR 25L TO STGR 26R IAW OLIVER WYMAN EA 23-C7-53-1519, REV IR, DATED 11/01/2023

Part: FRAME — CORRODED (UNKNOWN) · airframe 40,725 hrs · 30,328 cycles

HN 116921 DISCREPANCY: FRAME AT F.S. 909.00 IS CORRODED AT THE FORWARD SIDE AT STRINGER 26R. CORRECTIVE ACTION: REPAIRED DAMAGE I.A.W. MHIRJ REO 670-53-51-269 REV.--, DATED 2023-10-3

Part: STRINGER SPLICE — CORRODED (UNKNOWN) · airframe 40,725 hrs · 30,328 cycles

HN 116965 DISCREPANCY: STRINGER 24R SPLICE IS CORRODED BETWEEN FS 469 AND FS 485. CORRECTIVE ACTION: REMOVED AND REPLACED CORRODED STGR 24R SPLICE WITH NEW SERVICEABLE SPLICE (PN SH670-33241-1) IAW CRJ700 SRM 51-40-11-001-001-A01, 51-25-01-001-001-A01, & 51-21-11-001-001-A01.

Part: STRINGER SPLICE — CORRODED (UNKNOWN) · airframe 40,725 hrs · 30,328 cycles

HN 116978 DISCREPANCY: STRINGER 25R STRINGER SPLICE IS CORRODED BETWEEN F.S.319.70 AND F.S. 333.00. CORRECTIVE ACTION: REMOVED AND REPLACED STRINGER SPLICE I.A.W. BOMBARDIER CRJ700 SRM 51-42-06-001-001-A01 AND 51-40-11-001-001-A01.

Part: DRAIN LINE — CORRODED (UNKNOWN) · airframe 40,725 hrs · 30,328 cycles

HN 116258 DISCREPANCY: PAX DOOR AFT DRAIN TUBE IS CORRODED. CORRECTIVE ACTION: REMOVED AND REPLACED PAX DOOR DRAIN TUBE I.A.W. BOMBARDIER CRJ700 SRM 51-42-06-001-001-A01.

Part: STRINGER SPLICE — CRACKED (UNKNOWN) · airframe 40,725 hrs · 30,328 cycles

HN 118006 DISCREPANCY: STRINGER 24R SPLICE AT F.S. 333.00 HAS CORROSION. CORRECTIVE ACTION: REMOVED AND REPLACED SPLICE I.A.W. BOMBARDIER CRJ700 SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01

Part: FRAME — CORRODED (UNKNOWN) · airframe 40,725 hrs · 30,328 cycles

HN 118731 DISCREPANCY: FRAME 333 IS CORRODED BETWEEN STGR 26R TO 26L. CORRECTIVE ACTION: REMOVED CORRODED SECTION OF FRAME AND INSTALLED REPAIR PARTS IAW CRJ 700 SRM 53-00-06-201-006-A01.

Part: INTERCOSTAL — CORRODED (UNKNOWN) · airframe 40,725 hrs · 30,328 cycles

HN 116974 DISCREPANCY: INTERCOSTAL AT STGR 21L IS CORRODED BETWEEN FS 333 AND FS 349. CORRECTIVE ACTION: INSTALLED NEW SERVICEABLE INTERCOSTAL AT 21L FS 333 TO FS 349 IAW CRJ 700 SRM 51-42-06-001-001-A01.

Part: CLEAT — CORRODED · airframe 40,725 hrs · 30,328 cycles

HN 116507 DISCREPANCY: INTERCOSTAL BETWEEN DATUM 7 AND 8 BETWEEN F.S. 320.00 AND F.S. 327.00 IS CORRODED. CORRECTIVE ACTION: REMOVED AND REPLACED CLEAT I.A.W. BOMBARDIER CRJ700 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.

Part: STRINGER SPLICE — CORRODED (UNKNOWN) · airframe 40,725 hrs · 30,328 cycles

HN 119545 DISCREPANCY: FOUND MULTIPLE AREAS OF CORROSION ON F.S. 333.00 SPLICE AT STRINGER 26R. CORRECTIVE ACTION: REMOVED AND REPLACED SPLICE I.A.W. BOMBARDIER CRJ700 SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01.

Part: FORMER — CORRODED · airframe 40,725 hrs · 30,328 cycles

HN116503 DISCREPANCY: FWD FORMER AT PAX DOOR IS CORRODED. CORRECTIVE ACTION: REMOVED AND REPLACED IAW CRJ 700 SRMS 51-40-11-001-001-A01, 51-42-06-001-001-A01, 51-42-13-001-001-A01, AND 51-42-021-001-001-A01.

Part: HINGE — CHAFED (UNKNOWN) · airframe 40,725 hrs · 30,328 cycles

HN 116211 DISCREPANCY: PAX DOOR HINGE ON FUSELAGE HAS GOUGE/CHAFE DAMAGE ALONG THE AFT HALF OF HINGE AND (2) LOCATIONS ON FORWARD END. CORRECTIVE ACTION: REMOVED AND REPLACED IAW CRJ 700 SRM 53-21-23-201-007-A01.

Part: STRINGER — CORRODED (UNKNOWN) · airframe 40,725 hrs · 30,328 cycles

HN 118512 DISCREPANCY: STRINGER 24R IS CORRODED BETWEEN F.S. 333.00 AND F.S. 349.00. CORRECTIVE ACTION: REMOVED AND REPLACED STRINGER I.A.W. BOMBARDIER CRJ700 SRM REPAIR 53-00-03-201-001-A01.

Part: SKIN — CHAFED (UNKNOWN) · airframe 40,725 hrs · 30,328 cycles

HN116207 DISCREPANCY: FORWARD CARGO DOOR INNER SKIN IS CHAFED AT LOWER FORWARD AND AFT CORNERS. ASSOCIATED FRAMES ARE ALSO CHAFED. CORRECTIVE ACTION: REPAIRED FORWARD CARGO DOOR INNER SKIN CHAFES AT LOWER FWD AND AFT CORNERS IAW EA23-C7-52-1500, REV IR, DATED 10/24/2023

Part: FRAME — CORRODED (UNKNOWN) · airframe 40,725 hrs · 30,328 cycles

HN 119234 DISCREPANCY: FS 319 FRAME IS CORRODED BETWEEN STGR 27 AND STGR 24R CORRECTIVE ACTION: REPAIRED FS 319 FRAME IAW CRJ-700 SRM 53-00-06-201-006-A01.

Part: STRINGER — CORRODED (UNKNOWN) · airframe 40,725 hrs · 30,328 cycles

HN 116988 DISCREPANCY: STRINGER 25R IS CORRODED BETWEEN F.S. 280.00 AND F.S. 310.00. CORRECTIVE ACTION: REMOVED STRINGER 25R FROM FS 280 TO FS 333 IAW CRJ 700 SRM 51-42-06-001-001-A01. INSTALLED NEW STRINGER 25R P/N SH670-31212-2 FROM FS 280 TO FS 333 IAW CRJ 700 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.

Part: STRINGER — CORRODED (UNKNOWN) · airframe 40,725 hrs · 30,328 cycles

HN 116985 DISCREPANCY: STGR 24R IS CORRODED BETWEEN FS 310 AND FS 349. CORRECTIVE ACTION: REMOVED AND REPLACED STGR 24R BETWEEN FS 310 AND FS 349 IAW CRJ-700 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, AND 51-42-21-001-001-A01.

Part: STRINGER — CORRODED (UNKNOWN) · airframe 40,725 hrs · 30,328 cycles

HN 116987 DISCREPANCY: STRINGER 26R IS CORRODED BETWEEN F.S. 280.00 AND F.S. 310.00. CORRECTIVE ACTION: REMOVED AND REPLACED STRINGER I.A.W. BOMBARDIER CRJ700 SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01.

Part: STRINGER — CORRODED (UNKNOWN) · airframe 40,725 hrs · 30,328 cycles

HN 116986 DISCREPANCY: STGR 27 IS CORRODED BETWEEN FS 319.70 AND FS 333. CORRECTIVE ACTION: REPAIRED DAMAGE I.A.W. OLIVER WYMAN CAVOK EA 23-C7-53-1568 REV.IR, DATED 10/31/2023.

Part: SKIN — DAMAGED (UNKNOWN) · airframe 40,725 hrs · 30,328 cycles

HN 119205 DISCREPANCY: 1EA MISDRILLED HOLE ON FS 863 BETWEEN STGR 24L AND STGR25L. CORRECTIVE ACTION: REPAIRED FUSELAGE SKIN IAW OLIVER WYMAN EA 23-C7-53-1632 REV IR DATED 11-06-2023.

Part: SKIN — CORRODED (UNKNOWN) · airframe 40,725 hrs · 30,328 cycles

HN 116236 DISCREPANCY: PAX DOOR INNER SKIN HAS MULTIPLE AREAS OF CORROSION. CORRECTIVE ACTION: REMOVED AND REPLACED PAX DOOR INNER SKIN I.A.W. BOMBARDIER CRJ700 SRM 51-42-06-001-001-A01, 51-42-13-001-001-A01, 51-42-14-001-001-A01, 51-42-21-001-001-A01 AND 51-42-22-001-001-A01.

Part: STRINGER — CORRODED (UNKNOWN) · airframe 40,725 hrs · 30,328 cycles

HN 116983 DISCREPANCY: STGR 22R IS CORRODED BETWEEN FS 333 AND FS 349. CORRECTIVE ACTION: COMPLIED WITH MHIRJ REO 670-53-21-2333 REV -- DATED 2023-11-02

Part: FLOORBEAM — DAMAGED (ZONE 200) · airframe 27,746 hrs · 21,320 cycles

WHILE DRILLING L/H AND R/H 36 BEAM MISSED PILOT HOLE AND DOUBLE DRILLED HOLE INTO BUMP BEAM, FLOOR SKIN AND 36 BEAM FS 743.35 AND BL 36.00, LH AND RH SIDES.

Part: DOUBLER — CORRODED (ZONE 100) · airframe 27,746 hrs · 21,320 cycles

REMOVED UNSERVICBALE ANTENNA DOUBLER, DRILLED UP, INSTALLED SERVICABLE ANTENNA DOUBLER IAW CRJ 700 SRM 51-42-06-001-001-A01, 51-42-12-001-001-A01,SEE JOB 210313MOD7 OP 37 FOR REMOVAL AND INSTALL OF TCAS ANTENNA. REMOVED AND INSTALLED 10 FASNTERS FROM STR 22 IAW CRJ 900 SRM 51-42-06-001-001-A01 DISPLACED HYD LINES FOR ACCESS IAW CRJ 900 AMM 20-21-00-910-801-A01.

Part: FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 27,746 hrs · 21,320 cycles

FORWARD SIDE OF FRAME HAS CORROSION, LOCATED AT FS310, BETWEEN STRINGERS 26L AND 27.

Part: SELECTOR VALVE — FAILED (MLG) · airframe 27,424 hrs · 21,020 cycles

GEAR DISAGREE WARNING ON FINAL RAN QRH AND HAD TO MANUAL DEPLOY LANDING GEAR / REMOVED AND REPLACED LG SELECTOR VALVE IAW CRJ700 AMM 32-32-10-000/400-801-A01.

Part: DOOR LATCH — OUT OF ADJUST · airframe 26,827 hrs · 20,478 cycles

PAX DOOR HARD TO OPEN AND CLOSE. PERFORMED LUBRICATION OF PASSENGER DOOR IAW CRJ700 AMM 12-20-52-640-808. PERFORMED ADJUSTMENT OF LATCH MECHANISM IAW CRJ900 AMM 52-11-02-820-801-A02. MOVED AIRCRAFT AROUND TO LEVEL AND NON LEVEL GROUND AND PERFORMED OPS CHECK IN VARIOUS SPOTS. OPS CHECKS WERE GOOD IN ALL LOCATIONS.

Part: SKIN PANEL — ELONGATED (ZONE 500) · airframe 26,228 hrs · 19,922 cycles

UPON REMOVAL OF PANEL 521BL ON THE LEADING EDGE OF THE LH WING, 1 EA HOLE WAS FOUND TO BE ELONGATED

Part: INTERCOSTAL — CORRODED (ZONE 100) · airframe 26,228 hrs · 19,922 cycles

RH INTERCOSTAL ADJACENT TO STR 27 FS 349-364 HAS AREAS OF CORROSION

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 26,228 hrs · 19,922 cycles

SEAT TRACK SUPPORT CHANNELS LH AND RH AT FS 795 HAVE AREAS OF CORROSION

Part: TRANSDUCER — FAILED (WHEEL SPEED) · airframe 23,168 hrs · 17,186 cycles

INBOUND, THE CREW GOT AN ANTI-SKID OUTBOARD CAUTION MESSAGE. THE CREW RAN THE QRH AND DECIDED TO DECLARE A EMERGENCY. THE AIRCRAFT TAXIED TO A GATE UNDER THEIR OWN POWER WITHOUT INCIDENT. NO FURTHER ISSUES AT THIS TIME. R & R LEFT OUTBOARD WHEEL SPEED TRANSDUCER IAW AMM 32-44-01-400-801 (CONFIG A01.) OPS TESTED GOOD.

Part: SKIN — CORRODED (BS 280-295) · airframe 22,269 hrs · 16,423 cycles

INNER FUSELAGE SKIN CORRODED BETWEEN FS280 & FS295 BETWEEN STGR 25R & 24R -C/A-C/W ERS-CR-53MR-3954 SKIN REPAIR(DOUBLER) AT F.S 295 STR 24R-25R

Part: DOOR SILL — CORRODED (BS 1000-1047) · airframe 22,269 hrs · 16,423 cycles

MULTIPLE SPOTS OF CORROSION ON THE AFT CARGO DOOR SILL BETWEEN FS1000.00 AND 1047.00.-C/A-INSTALLED NEW AFT CARGO DOOR SILL IAW SRM 51-42-06, 51-42-13 AND 51-42-21.

Part: CROSSBEAM — CORRODED (BS 280) · airframe 22,269 hrs · 16,423 cycles

CROSSBEAM AT FS280.00 RIGHT IS CORRODED-C/A-COMPLETED REPAIR OF THE RH CROSSBEAM AT FS280.00 IAW SRM 51-42-06 AND SRM 51-42-13.

Part: CROSSBEAM — CORRODED (BS 280) · airframe 22,269 hrs · 16,423 cycles

CROSSBEAM AT FS280.00 LEFT IS CORRODED-C/A-COMPLETED REPAIR OF THE LH CROSSBEAM AT FS280.00 IAW SRM 51-42-06 AND SRM 51-42-13.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 22,269 hrs · 16,423 cycles

LH CENTER COCKPIT FLOOR BEAM AT BL12.00 IS CRACKED, LOCATED JUST FWD OF CROSSBEAM AT FS280.00-C/A-COMPLETED REPAIR TO LH CENTER COCKPIT FLOOR BEAM AT BL12.00 IAW SRM 53-11-43.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 22,269 hrs · 16,423 cycles

RH CENTER COCKPIT FLOOR BEAM AT BL12.00 IS CRACKED, LOCATED JUST FWD OF CROSSBEAM AT FS280.00-C/A-COMPLETED REPAIR TO RH CENTER COCKPIT FLOOR BEAM AT BL12.00 IAW SRM 53-11-43.

Part: FRAME — GOUGED (FUSELAGE) · airframe 22,121 hrs · 16,253 cycles

GOUGE ON FRAME AT FS1162 BETWEEN STGR7L AND STGR8L. TRANSFERED FROM AML PAGE 4598770 BLOCK 2 T LEW 445258 MAJOR REPAIR-C/A-REPAIRED GOUGE ON FRAME AT FS1162 BETWEEN STR7L AND STR 8L IAW ERS-CR-53MR-1724.

Part: FRAME — GOUGED (FUSELAGE) · airframe 22,121 hrs · 16,253 cycles

GOUGE ON STGR 6L 8.0" FWD OF FRAME FS1162 AND IS 3/8" WIDE AND THROUGH THE EDGE OF MATERIAL NEAR BEND RADIUS. "TRANSFERRED TO NRWC 535-MQT-02998" EDWARD LAKANEN 148836 UPGRADED TO A MAJOR REPAIR-C/A-REPAIRED DAMAGE IAW ERS-CR-53MR-3901, REF NRWC 535-MQT-02998

Part: STRINGER — GOUGED (FUSELAGE) · airframe 22,121 hrs · 16,253 cycles

"TRANSFERRED FROM AML PAGE 4598770 ITEM 3" GOUGE ON STGR7L 7 5/8" FWD OF FS1162 AND 5/8" IN WIDTH. DEPTH IS THROUGH RADIUS OF BEND, AND THROUGH EDGE OF MATERIAL. MAJOR REPAIR.-C/A-COMPLETED REPAIR ON STGR 7L FWD OF FS1162 IAW CRJ SRM 53-00-03.

Part: PANEL — CRACKED (CARGO BAY WALL) · airframe 21,843 hrs · 15,970 cycles

AFT CARGO RH AFT WALL PANEL 282CRW HAS AN APPROXIMATELY 8" CRACKED. REPAIRED COMPOSITE DAMAGE ON AFT CARGO PANEL 282CRW IAW AMM 25-52-01.

Part: SEALANT — UNSECURE (WINDSHIELD) · airframe 21,044 hrs · 15,268 cycles

RT (FO SIDE) OUTER WINDSHIELD SEAL STARTING TO COME OFF. C/A-PERFORMED GVI OF RT SIDE WINDOW FOUND SMALL AMOUNT OF FILLET SEAL TRIMMED EXCESS SEALANT REF. AMM 56-12-01 A/C OK FOR SERVICE.

Part: PACKING — LEAKING (NLG STRUT) · airframe 18,598 hrs · 13,227 cycles

STEERING INOPERATIVE CAUTION MESSAGE IN FLIGHT. UNABLE TO RECOVER AFTER LANDING. TROUBLESHOT IAW FIM 32-50-00-810-802. PERFORMED NLG STRUT REPACKING IAW W/C 32-019. OPS & LEAK CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 17,683 hrs · 12,514 cycles

DURING A PS-1 INSPECTION, FOUND THE RT AFT EMERGENCY LIGHT ON FUSELAGE INOPERATIVE. R & R THE BULB IAW AMM 33-51-15. OPS CHECKED GOOD. NO FURTHER DEFECTS NOTED.

Part: WARNING MESSAGE — FALSE ACTIVATION (SPOILERS) · airframe 17,596 hrs · 12,450 cycles

ON APPROACH, DESCENDING FROM 6,000 FEET AND FLIGHT SPOILERS EXTENDED, OTBD SPOILERONS AND OTBD FLT SPOILER CAUTION MESSAGE POSTED ON ED1. INTERROGATED MDC FOUND LT OTBD MFS PCU JAM MDC MESSAGE. PERFORMED SPOST 1 RESET. PERFORMED OPS CHECK IAW ETN-CR-27-083. OPS CHECKED GOOD.

Part: SKIN — DENTED (BS 280-295) · airframe 16,926 hrs · 11,928 cycles

DENT FOUND ON THE FWD FUSELAGE AT BS 280 - 295, STRINGER 22 - 23R. PERFORMED A REPAIR IAW ERS-CR-53MR-2749.

Part: WEB — CRACKED (E/E BAY) · airframe 16,926 hrs · 11,928 cycles

LEFT FORWARD EQUIPMENT BAY FLOOR WEB HAS A .250 INCH CRACK. THE FLOOR WEB REPAIRED IAW ETN-CR-53-099.

Part: GAUGE — LEAKING (HYD SYSTEM) · airframe 16,417 hrs · 11,497 cycles

FOUND NR 2 HYD SYS BRAKE ACCUMULATOR PRESSURE GAUGE LEAKING. REMOVED AND REPLACED THE PRESSURE GAUGE IAW AMM 32-43-30. OPS CHECKED GOOD.

Part: UNKNOWN — SMOKE (CABIN) · airframe 15,514 hrs · 10,744 cycles

SMOKE IN CABIN STARTED REAR, APU ON, PACKS OFF. GVI OF CABIN AND COCKPIT PERFORMED RAN APU ALL NIGHT WITH ALTERNATING PACKS OFF AND ON, LIGHTS OFF AND ON, NO INDICATION OF SMOKE OR ODOR OF IT. INSPECTED AVIONICS BAY APU COWL, ENGINE AND COWL NO OIL LEAK.

Part: STAND OFF — CRACKED (RT TRANSCOWL) · airframe 15,512 hrs · 10,742 cycles

RIGHT LOWER TRANSCOWL INBD PROFILE IS CRACKED. C/W INSTALLATION OF SERVICEABLE STAND OFF ANGLE IAW ETN CR-54-015R1.

Part: PROFILE — CRACKED (THRUST REVERSER) · airframe 15,512 hrs · 10,742 cycles

RIGHT UPPER TRANSCOWL INBD PROFILE IS CRACKED. REPLACED THE PROFILE IAW ETN CR-54-051.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 15,512 hrs · 10,742 cycles

PAX DOOR AFT DRAG ANGLE IS CRACKED APPROXIMATELY 1/2 INCH IN A PREVIOUSLY REPAIRED AREA ABOVE THE POWER ASSIST PULLEY BRACKET. C/W INSTALLATION OF SERVICESABLE STAND OFF ANGLE IAW ETN CR-54-015R1.

Part: SKIN — CRACKED (PAX DOOR) · airframe 15,512 hrs · 10,742 cycles

PASSENGER DOOR AFT SIDE SKIN HAS 2 CRACKS APPROXIMATELY 3" IN LENGTH AT THE MID STEP LOCATION. REPAIRED IAW ETN ETN-CR-52-039.

Part: SKIN — DENTED (PAX DOOR) · airframe 15,512 hrs · 10,742 cycles

PASSENGER DOOR INNER SKIN HAS A DENT LOCATED BETWEEN FS 340-FS 349 & BETWEEN DOOR DATUM T/R 4 & 5. C/W ERS-CR-52DF-618 PART-A.

Part: ENGINE — VIBRATION (NR 1) · airframe 15,333 hrs · 10,603 cycles

N1 FAN VIBRATION REMAINED IN AMBER DURING CLIMBOUT. COULD NOT GET ENGINE BACK TO GREEN RANGE DURING CLIMB MODE. PERFORMED FIM TASK 72-00-00, & FOUND NO MESSAGES IN CURRENT FAULTS & FAULT HISTORY. PERFORMED INSPECTION OF THE FAN BLADES FOR STIFFNESS IAW 72-21-02 & FOUND NO STIFFNESS. PERFORMED MUTLIPLE VIBRATION CHECKS FOR NR 1 ENGINE IAW AMM 71-00-00. INDICATION REMAINED IN THE GREEN RANGE AT 0.3 AT PEAK. OPS CHECKED GOOD.

Part: COOLING FAN — FAILED (COCKPIT) · airframe 14,490 hrs · 9,971 cycles

DISPLAY FAN FAILED, FOLLOWED BY BURNING SMELL IN COCKPIT. VERIFIED DISPLAY COOLING FAN NR 2 FAILED. SOURCE OF ODOR. DEFERRED COOLING NR 2. M PROCEDURE COMPLIED WITH. R & R NR 2 COCKPIT DISPLAY FAN IAW AMM 21-24-12. OPERATIONS CHECKED GOOD. MEL RESTORED.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 14,480 hrs · 9,962 cycles

UPON START UP NOTICED ELEC SMOKE SMELL & SOUNDED LIKE DISPLAY FAN WINDING DOWN. PERFORMED OPERATIONS CHECK OF THE DISPLAY COOLING SYS IAW AMM 21-24-00. NO DEFECTS NOTED.

Part: FLASHLIGHT — INTERMITTENT (COCKPIT) · airframe 14,381 hrs · 9,887 cycles

FIRST OFFICERS FLASHLIGHT WORKS INTERMITTENTLY, INDICATES CHARGING IN CRADLE. REPLACED FIRST OFFICERS FLASHLIGHT AS REQUIRED. OPERATIONS CHECKED GOOD.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 11,668 hrs · 7,692 cycles

COCKPIT FLASHLIGHT INOPERATIVE. R & R COCKPIT FLASHLIGHT IAW MM 25-61-02. OPERATIONS CHECKED GOOD.

Part: STEERING SYS — INOPERATIVE (NLG) · airframe 11,373 hrs · 7,450 cycles

STEERING INOPERATIVE IN FLIGHT UPON GEAR DOWN SELECTION. COMPLIED WITH ETN-CR-019.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 11,079 hrs · 7,185 cycles

FAIRING SUPPORT BRACKET IN THE RT MAIN WW BELOW THE SIDE BRACE PINTLE PIN IS CRACKED. R & R WEB BRACKET IAW AMM 20-21-00.

Part: STRUCTURE — CRACKED (E&E BAY) · airframe 11,079 hrs · 7,185 cycles

FORWARD RT ELEC COMPARTMENT FLOOR UNDER & OTBD OF THE ADG HYD HAND PUMP IS CRACKED. COMPLETED REPAIR IAW ETN-CR-53-099.

Part: ANGLE — CRACKED (PAX DOOR) · airframe 11,079 hrs · 7,185 cycles

PASSENGER DOOR AFT STEP SHELL ANGLE ATTACHMENT CRACKED BY THE DOOR ASSIST PULLEY BRACKET. REPAIRED PAX DOOR AFT STEP ANGLE IAW SRM 52-11-04.

Part: SKIN — CRACKED (PAX DOOR) · airframe 11,079 hrs · 7,185 cycles

PASSENGER DOOR INNER SKIN AFT UPPER CORNER DENTED & CRACKED. REPLACED ANGLE UNDER CORNER IAW SRM 51-42-06 & INSTALLED NEW PAX DOOR AFT UPPER CORNER IAW SRM 51-42-13. DIAPHRAGM PN 601R38122-1.

Part: AUTOPILOT SYS — MALFUNCTIONED (COCKPIT) · airframe 10,416 hrs · 6,720 cycles

IN CRUISE AT FL190 AUTO PILOT ENGAGED. AUTO PILOT LAGGED FLIGHT DIRECTOR RESULTING IN 400 FPM CLIMB & 500 FPM OSCILLATIONS, FROM CAPTURED ALTITUDE, 1/8 INCH GAP BETWEEN FLIGHT DIRECTOR & ACFT SYMBOL. LEVELED AT 2100 FT ON APPROACH & AGAIN WITH GLIDESLOPE CAPTURED, AURAL TRIM ELEVATOR WARNING WENT OFF. DEFERRED AUTO PILOT IAW MEL 22-1, ACFT IS NON-COMPLAINT FOR CAT II OPERATIONS, M PROCEDURE COMPLIED WITH MEL IS OPEN. T/S IAW FIM 22-12-14 RAR NR 1 LIGHTNING/HIRF IAW AMM 22-12-08 OPS CHECK GOOD MEL ITEM RESTORED.

Part: PCU — MALFUNCTIONED (SPOILER) · airframe 10,308 hrs · 6,649 cycles

INBOARD FLT SPOILERS & IB SPOILERONS MSG PRESENTED IN FLIGHT. TRANSFERRED TO NRWC 535-ORD-01112. R & R MFS PCU RT INBD IAW AMM TASK 27-62-01. OPERATIONS CHECKED GOOD. RETURN ACFT TO SERVICE.

Part: PCU — MALFUNCTIONED (SPOILERS) · airframe 10,267 hrs · 6,616 cycles

AT 11,000 FT, DEPLOYED FLIGHT SPOILERS. INBD FLT SPOILERS & INBD SPOILERONS ILLUMINATED ON EICAS. REMOVED AND REPLACED RT INBD PCU IAW AMM 27-62-01.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 10,184 hrs · 6,551 cycles

INBD FLIGHT SPOILERS & INBD SPOILERONS CAUTION MSG DURING ARRIVAL TO APPROACH. PERFORMED SPOST 1 & 2 TEST IAW AMM 27-40-00 FIM 27-41-00. OPERATIONS CHECKED GOOD. NO FURTHER DEFECTS NOTED.

Part: TRANSCEIVER — DEFECTIVE (RADIO ALTIMETER) · airframe 10,112 hrs · 6,505 cycles

CLIMB OUT OF LGA GLD UNSAFE EICAS CAUTION PRESENTED. COMPLIED WITH EMER & ABNORMAL CHECKLIST, RETURNED TO LGA & LANDED UNEVENTFULLY. R & R NR 2 A43 RADIO ALTIMETER TRANSCEIVER IAW AMM 34-44-01, OPERATIONS TESTED GOOD.

Part: FLASHLIGHT — MALFUNCTIONED (COCKPIT) · airframe 9,828 hrs · 6,321 cycles

CAPTAIN`S FLASHLIGHT RED INDICATOR LIGHT MISSING. PERFORMED OPERATIONAL CHECK OF CAPTAIN'S EMERGENCY FLASHLIGHT IAW MM 25-61-02. OPS CHECKED GOOD.

Part: ACM — FAILED (LEFT) · airframe 8,769 hrs · 5,622 cycles

ON GROUND, PARKED AT GATE, APU RUNNING. TURNED ON LT & RT PACKS. SMOKE BEGAN COMING FROM VENTS IN COCKPIT AND LT PACK AUTOFAIL CAUTION MESSAGE WAS PRESENTED. REMOVED AND REPLACED THE LEFT HAND AIR CYCLE MACHINE ASSY. IAW MM 21-51-08 -PERFORMED OPS TEST OF AIR-COND. SYSTEM - OPS & LEAK CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: A/C PACK — SEIZED (RIGHT) · airframe 8,684 hrs · 5,568 cycles

CREW REPORTED DIRTY SOCK ODOR FROM RT PACK. FOUND RT PACK SEIZED.

Part: FLASHLIGHT ASSY — INOPERATIVE (COCKPIT) · airframe 8,483 hrs · 5,435 cycles

CAPTAIN`S FLASHLIGHT INOPERATIVE. REMOVED AND REPLACED FLASHLIGHT IAW 65-08-12. OPS CHECKED GOOD.

Part: PRINTER — MALFUNCTIONED (COCKPIT) · airframe 7,621 hrs · 4,877 cycles

THE CREW REPORTED A COCKPIT ODOR. THE ACFT WAS REMOVED FROM SERVICE, MEL 23-06. R & R PRINTER IAW MM 23-22-05. THE OPS CHECK WAS GOOD. MEL RESTORED. THE ACFT WAS RETURNED TO SERVICE.

Part: WARNING SYSTEM — MALFUNCTIONED (SPOILER SYS) · airframe 7,115 hrs · 4,563 cycles

ON FLIGHT 3743 THE CREW REPORTED THAT UPON DESCENT THEY RECEIVED AN EICAS I/B SPOILERON AND I/B FLT SPOILERS FAULT MESSAGE. THE CREW COMPLIED WITH AOM VOL 1 PROCDURES, DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. I/B SPOILERON AND I/B FLT SPOILERS CAUTION RESET PER CRJ AOM VOLUME 1 RESET PROCEDURES PAGE 130.6. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: THRUST REVERSER — MALFUNCTIONED (LT ENGINE) · airframe 209 hrs · 149 cycles

ON FLIGHT 3877 ON THE LANDING ROLL OUT THE CREW TRIED TO STOW THE THRUST REVERSERS BUT THE LEFT REVERSER STAYED DEPLOYED. THE CAPTAIN DECLARED AN EMERGENCY WITH AIR TRAFFIC CONTROL. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED AN OPERATIONAL CHECK IAW CRJ 700 MM 78-30-00. NO PARTS REMOVED OR REPLACED. THE OPERATIONAL CHECK WAS GOOD. NO DEFECTS NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE.