N245LR

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 26,496 hrs · 20,231 cycles

L1 DOOR LOWER EXIT SIGN SEVERAL LED OUT. CURRENTLY OUT OF SERVICE. REPLACED 2 BULBS IN SIGN.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 26,045 hrs · 19,854 cycles

INTERIOR EME LIGHTS EVEY OTHR LIGHT INOP- OP CHECK FOUND TO BE NORMAL CONFIGURATION

Part: SMOKE DETECTOR — FAILED (ZONE 200) · airframe 25,480 hrs · 19,408 cycles

SMOKE FWD LAV WARN (NOT ACTUAL SMOKE) PLACED ON MEL

Part: BATTERY PACK — DEPLETED (ZONE 200) · airframe 24,826 hrs · 18,875 cycles

EMERGENCY LIGHTS INOP - CHARGED EMER BATT PACKS

Part: NONE — NONE · airframe 24,483 hrs · 18,602 cycles

EMER LITES ROW 4 BACK INOP. MX CHARGED EMER BATTERY PACKS.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 24,431 hrs · 18,566 cycles

EMER LT ROW 12 & 13 WN ILLUM. CHARGED EMER LT OPS CK NO DEFECT NOTED.

Part: NONE — UNKNOWN · airframe 24,353 hrs · 18,515 cycles

EMERGENCY LIGHTS INOP RH/LH ROWS 3 AND 13. PERFORMED OPERATIONAL CHECK OF EMERGENCY LIGHTS, OPS CHECK NORMAL, NO DEFECTS NOTED.

Part: LIGHT — INOPERATIVE · airframe 24,287 hrs · 18,470 cycles

CEILING ORDINANCE EMER SIGNS INOP. CURRENTLY OUT OF SERVICE TROUBLE SHOOTING.

Part: NONE — NONE · airframe 24,186 hrs · 18,383 cycles

ALL OVR WING EMER EXIT LIGHS INOP. AIRCRAFT IS STILL CURRENTLY OOS.

Part: NONE — NONE · airframe 24,150 hrs · 18,359 cycles

ALL OVR WING EXIT ROW EMER LIGHTS INOP. CURRENTLY OOS.

Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 24,148 hrs · 18,358 cycles

MID CABIN - ROW 13 LH/RH EMER LTS INOP

Part: NONE — NONE · airframe 24,081 hrs · 18,310 cycles

CABIN EMER LIGHTS COME ON INTERMITTENTLY. CURRENTLY OOS TROUBLE SHOOTING.

Part: NONE — NONE · airframe 24,080 hrs · 18,309 cycles

CABIN EMER LIGHT AFT 1ST CLASS INOP. CURRENTLY OOS.

Part: BULB — INOPERATIVE (ZONE 200) · airframe 23,686 hrs · 18,033 cycles

OW LH-RH OUTSIDE EMER LIGHTS INOP

Part: NONE — NONE (LH THRUST REVERS) · airframe 23,616 hrs · 17,984 cycles

THE LH THRUST REVERSER HINGE LINE FAIRING SKIN WAS FOUND TO HAVE WEAR DAMAGE NEAR AN EXISTING SPLICE REPAIR. PERFORM PERMANENT REPAIR IAW CRJ7/9 STRUCTURAL REPAIR MANUAL (SRM) A) 54-12-01, FIGURE 54-12-01-991-808, ITEM 8 (REV. 38 DATED JUL. 25 2020) B) ILLUSTRATED PARTS CATALOG (IPC) 54-12-01, FIGURE 5, ITEM 10A (REV. 71 DATED OCT 25, 2021 ).

Part: NONE — NONE (BLKHD FS280-RBL1) · airframe 23,616 hrs · 17,984 cycles

THE BULKHEAD FLOOR POST (P/N: CC670-34180-6) AT FS280.00 AND RBL 11.16 WAS FOUND TO HAVE A CORROSION DAMAGE. PERFORM PERMANENT REPAIR IAW CRJ7/9 STRUCTURAL REPAIR MANUAL (SRM) 53-11-10-001-003-A01, FIGURE 53-11-10-991-803 (SHEET 4 OF 7), ITEM 57_8 (REV.33 DATED JUN. 25, 2017).

Part: NONE — CORRODED (FS629-FS645) · airframe 23,615 hrs · 17,984 cycles

THE FUSELAGE SKIN (P/N: SH670-33003-11) BETWEEN FS629.00 - FS645.00 AT STGR0 WAS FOUND TO HAVE CORROSION, SCRATCH AND NICK DAMAGE. PERFORM PERMANENT REPAIR IAW CRJ7/9 STRUCTURAL REPAIR MANUAL (SRM) 53-31-01-001-001-A02, FIGURE 53-31-01-991-802, ITEM 1A, B (REV 33 DATED JUN 25, 2017)

Part: NONE — NONE (RH ENG INLET COW) · airframe 23,615 hrs · 17,984 cycles

THE RH INLET COWL LIPSKIN WAS FOUND TO HAVE CORROSION DAMAGE. THE MINIMUM REMAINING THICKNESSES IN THE BLENDED AREA ES 0.059. PERFORM PERMANENT REPAIR IAW CRJ7/9 STRUCTURAL REPAIR MANUAL (SRM) 54-11-05-001-001-A01, FIGURE 54-11-05-991-801, ITEM 1, (REV. 37 DATED AUG. 15, 2019)

Part: NONE — NONE (WING (LH) - SLAT) · airframe 23,615 hrs · 17,984 cycles

THE L/H WING LEADING EDGE SLAT NO. 3 TRAILING EDGE WEDGE WAS FOUND WITH WEAR DAMAGE AT SS407.75. PERFORM PERMANENT REPAIR IAW CRJ7/9 STRUCTURAL REPAIR MANUAL (SRM) 51-13-02 TABLE 1

Part: FLASHLIGHT — INOPERATIVE (ZONE 200) · airframe 23,359 hrs · 17,812 cycles

FO'S FLASHLIGHT INOP PLACED ON MEL

Part: SUPPORT BRACKET — CRACKED (LT SLAT TRACK) · airframe 26,379 hrs · 23,521 cycles

LT WING SLAT TRACK BOX 1-3 SUPPORT BRACKET CRACKED. REPAIRED LT WING SLAT BOX 1-3, CUT OUT DAMAGE. FABRICATED AND INSTALLED REPAIR PARTS, IAW BOMBARDIER REO 670-57-42-577 DATED: 2016-12-02.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 21,118 hrs · 16,197 cycles

GALLEY FLOOR LEVEL EXIT SIGN 2 BULBS INOPERABLE, PLACED ON MEL.

Part: BATTERY — INOPERATIVE (C/P FLASHLIGHT) · airframe 21,066 hrs · 16,151 cycles

CA FLASHLIGHT IND NOT BLINKING. REPLACED FLASHLIGHT BATTERY.

Part: CASCADE — CRACKED (THRUST REVERSER) · airframe 21,026 hrs · 16,119 cycles

LT THRUST REVERSER IN BOARD LOWER CASCADE CRACKED. CORRECTIVE ACTION TO BE ACCOMPLISHED ON AVMAX WORK ORDER 80892 WORK CARD 4019.

Part: STRINGER — CORRODED (ZONE 100) · airframe 21,026 hrs · 16,119 cycles

STRINGER 24R CORRODED BETWEEN FRAMES 333.00 AND 349.00. CORRECTIVE ACTION TO BE ACCOMPLISHED ON AVMAX WORK ORDER 80892 WORK CARD 1046.

Part: MOUNT — CORRODED (TCAS ANTENNA) · airframe 21,026 hrs · 16,119 cycles

TCAS ANTENNA MOUNT CORRODED. CORRECTIVE ACTION TO BE ACCOMPLISHED ON AVMAX WORK ORDER 80892 WORK CARD 1043.

Part: STRINGER SPLICE — CORRODED (ZONE 100) · airframe 21,026 hrs · 16,119 cycles

STRINGER 26R SPLICE AT FRAME 333.00 CORRODED. COERRECTIVE ACTION TO BE ACCOMPLISHED ON AVMAX WORK ORDER 80892 WORK CARD 1044.

Part: FRAME — CORRODED (ZONE 100) · airframe 21,026 hrs · 16,119 cycles

FRAME 319.00 CORRODED BETWEEN STRINGERS 25L AND 26R. CORRECTIVE ACTION TO BE ACCOMPLISHED ON AVMAX WORK ORDER 80892 WORK CARD 1039.

Part: FRAME — CORRODED (ZONE 100) · airframe 21,026 hrs · 16,119 cycles

FRAME 333.00 CORRODED BETWEEN STRINGERS 25L TO 24R. CORRECTIVE ACTION TO BE ACCOMPLISHED ON AVMAX WORK ORDER 80892 WORK CARD 1040.

Part: STRINGER — CORRODED (ZONE 100) · airframe 21,026 hrs · 16,119 cycles

STRINGER 25R CORRODED BETWEEN FRAMES 280.00 TO 310.00 AND 319.00 TO 349.00. CORRECTIVE ACTION TO BE ACCOMPLISHED ON AVMAX WORK ORDER 80892 WORK CARD 1035.

Part: FRAME — CORRODED (ZONE 100) · airframe 21,026 hrs · 16,119 cycles

FRAME 310.00 CORRODED BEWTEEN STRINGERS 25L TO 25R. CORRECTIVE ACTION TO BE ACCOMPLISHED ON AVMAX WORK ORDER 80892 WORK CARD 1037.

Part: TAIL CONE — DENTED (ZONE 300) · airframe 21,026 hrs · 16,119 cycles

APU TAILCONE DENTED ON RT SIDE. CORRECTIVE ACTION TO BE ACCOMPLISHED ON AVMAX WORK ORDER 80892 WORK CARD 3009.

Part: STRINGER — CORRODED (ZONE 100) · airframe 21,026 hrs · 16,119 cycles

STRINGER 27 CORRODED BETWEEN FRAMES 333.00 AND 349.00. CORRECTIVE ACTION TO BE ACCOMPLISHED ON AVMAX WORK ORDER 80892 WORK CARD 1048.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 21,026 hrs · 16,119 cycles

LT SIDE SEAT RAILS FROM FRAME STATIONS 693.00-813.00 AND 847.00-865.00 CORRODED. CORRECTIVE ACTION TO BE ACCOMPLISHED ON AVMAX WORK ORDER 80892 WORK CARD 2119. CORRODED SEAT TRACKS PART NUMBERS SH970-37543-3, SH690-36284-1, SH690-36285-2, AND SH670-36260-5.

Part: STRINGER — CORRODED (ZONE 100) · airframe 21,026 hrs · 16,119 cycles

STRINGER 26L CORRODED BETWEEN FRAMES 333.00 AND 364.00. CORRECTIVE ACTION TO BE ACCOMPLISHED ON AVMAX WORK ORDER 80892 WORK CARD 1041.

Part: STRINGER — CORRODED (ZONE 100) · airframe 21,026 hrs · 16,119 cycles

STRINGER 27 CORRODED BETWEEN FRAME 310.00 AND 333.00. CORRECTIVE ACTION TO BE ACCOMPLISHED ON AVMAX WORK ORDER 80892 WORK CARD 1070.

Part: STRINGER — CORRODED (ZONE 100) · airframe 21,026 hrs · 16,119 cycles

STRINGER 26R CORRODED BETWEEN FRAMES 319.00 AND 349.00. CORECCTIVE ACTION TO BE ACCOMPLISHED ON AVMAX WORK ORDER 80892 WORK CARD 1036.

Part: STRINGER SPLICE — CORRODED (ZONE 100) · airframe 21,026 hrs · 16,119 cycles

STRINGER 25R SPLICE AT FRAME 333.00 CORRODED. CORRECTIVE ACTION TO BE ACCOMPLISHED ON AVMAX WORK ORDER 80892 WORK CARD 1047.

Part: STRAP — CRACKED (WNG-BODY FAIRING) · airframe 21,026 hrs · 16,119 cycles

AFT WING TO BODY FAIRING STRAP CARCKED. CORRECTIVE ACTION TO BE ACCOMPLISHED ON AVMAX WORK ORDER 80892 WORK CARD 1051.

Part: SUPPORT BRACKET — CRACKED (ZONE 500) · airframe 21,026 hrs · 16,119 cycles

LT SLAT BOX 1-3 SUPPORT BRACKET CRACKED. CORRECTIVE ACTION TO BE ACCOMPLISHED ON AVAMX WORK ORDER 80892 WORK CARD 5041.

Part: SUPPORT BRACKET — CRACKED (RT SLAT BOX) · airframe 21,026 hrs · 16,119 cycles

RT SLAT BOX 1-3 SUPPORT BARCKET CRACKED. CORRECTIVE ACTION TO BE ACCOMPLISHED ON WORK ORDER 80892 WORK CARD 6036.

Part: STRIKER — CORRODED (SERVICE DOOR) · airframe 21,026 hrs · 16,119 cycles

STRICKER ANGLE AT GALLEY SERVICE DOOR CUT OUT CORRODED. CORRECTIVE ACTION TO BE PERFORMED ON AVMAX WORK ORDER 80892 WORK CARD 1050.

Part: DIAPHRAGM — CORRODED (ZONE 100) · airframe 21,026 hrs · 16,119 cycles

AFT WING TO BODY FAIRING SUPPORT DIAPHRAGM (LT SIDE) CRACKED. CORRECTIVE ACTION TO BE ACCOMPLISHED ON AVMAX WORK ORDER 80892 WORK CARD 1052.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 21,026 hrs · 16,119 cycles

LT CENTER SEAT RAIL CORRODED FROM FS 379.00 TO FS 409.00. CORRECTIVE ACTION TO BE ACCOMPLISHED ON AVMAX WORK ORDER 80892 WORK CARD 2116.

Part: ACCESS PANEL — CRACKED (ZONE 400) · airframe 21,026 hrs · 16,119 cycles

RT ENGINE PYLON PANEL 422CT CRACKED. CORRECTIVE ACTION TO BE ACCOMPLISHED ON AVAMX WORK ORDER 80892 WORK CARD 4022.

Part: SEAT TRACK — CORRODED (ZONE 100) · airframe 21,026 hrs · 16,119 cycles

SEAT TRACK AT RBL 9 BETWEEN FRAME STATION 661+32-693.00 CORRODED.

Part: ANGLE — CORRODED (PAX DOOR) · airframe 21,026 hrs · 16,119 cycles

PAX DOOR FLOOR SUPPORT KICK ANGLE CORRODED. ANGLE KICKPLATE REPLACED ON AVMAX WORK ORDER 80892 WORK CARD 1065.

Part: SUPPORT BRACKET — CRACKED (LT WING SLAT) · airframe 21,025 hrs · 16,119 cycles

RT SLAT BOX 1-3 SUPPORT BRACKET CRACKED ON SLAT BOX. CORRECTIVE ACTION TO BE ACCOMPLISHED ON AVMAX WORK ORDER: 80892 WORK CARD: 6036.

Part: SUPPORT BRACKET — CRACKED (LT SLAT TRACK) · airframe 21,025 hrs · 16,119 cycles

LT SLAT BOX 1-3 SUPPORT BRACKET CRACKED ON SLAT BOX. CORRECTIVE ACTION TO BE ACCOMPLISHED ON AVMAX WORK ORDER: 80892 WORK CARD: 5041.

Part: NOT REPORTED — MALFUNCTIONED (LANDING GEAR) · airframe 19,665 hrs · 15,078 cycles

GEAR DISAGREE W/N RETRACT. CURRENTLY OUT OF SERVICE

Part: ENGINE — FAILED (NR 2) · airframe 19,278 hrs · 14,777 cycles

RT ENGINE FAILED ON APPRCH/CREW SHUTDWN.

Part: LIGHT — INOPERATIVE (RT OVERWING) · airframe 18,595 hrs · 14,274 cycles

RH AFT OVERWING EMERGENCY LIGHT INOP. PLACED ON MEL

Part: CONTACT — DIRTY (MEGAPHONE) · airframe 17,935 hrs · 13,782 cycles

MEGAPHONE INOP / CLEANED BATTERY CONNECTION OPS CK GOOD

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 16,536 hrs · 12,703 cycles

FS 280 FWD "J" ANGLE CORRODED ON UPPER SURFACE, LBL - RBL 12.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 16,536 hrs · 12,703 cycles

GALLEY SERVICE DOOR, LOWER SUPPORT ANGLE CORRODED.

Part: FLASHLIGHT — INOPERATIVE (AFT CABIN) · airframe 16,463 hrs · 12,647 cycles

AFT FA FLASHLIGHT WAS INOPERATIVE.

Part: LIGHT — INTERMITTENT (CABIN) · airframe 14,514 hrs · 11,123 cycles

EVERY OTHER OVHD EMER LIGHT INOP. RESET SYSTEM, OPS NORMAL.

Part: FLASHLIGHT ASSY — INOPERATIVE (COCKPIT) · airframe 14,441 hrs · 11,058 cycles

FIRST OFFICER`S FLASHLIGHT NOT CHARGING.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 12,953 hrs · 9,904 cycles

LT FWD EXTERNAL EMERGENCY LIGHT INOP. REPLACED BULB.

Part: FLASHLIGHT — INOPERATIVE (FWD CABIN) · airframe 12,890 hrs · 9,851 cycles

FWD CABIN FLASHLIGHT INOPERATIVE.

Part: FLASHLIGHT — INOPERATIVE (FWD CABIN) · airframe 12,320 hrs · 9,422 cycles

FWD FA FLASHLIGHT INOPERATIVE.

Part: SKIN — DENTED (BS 1015-1047) · airframe 12,114 hrs · 9,264 cycles

MULTIPLE SCRATCHES AND GOUGES TO FUSELAGE SKIN BETWEEN BS 1015 - 1047, STRINGERS 21-25R, CAUSED BY LOW PRESSURE AIR CAP.

Part: SKIN — DENTED (BS 565) · airframe 12,114 hrs · 9,264 cycles

EXTERNAL FUSELAGE SKIN DENTED AT BS 565 BETWEEN STRINGERS 16 - 17L.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 12,114 hrs · 9,264 cycles

RBL 12, COCKPIT FLOORBEAM FWD OF FS 280 ON UPPER SIDE FOUND INDICATION APPROXIMATELY 1.3" LONG 100 PERCENT FCH, FAILED NDT INSPECTION.

Part: CROSSBEAM — CORRODED (BS 280) · corrosion level 2 · airframe 12,114 hrs · 9,264 cycles

FOUND RT BS 280 CROSSBEAM CORRODED BETWEEN RBL 9.0 AND RBL 12.0.

Part: CROSSBEAM — CRACKED (FUSELAGE) · corrosion level 2 · airframe 12,114 hrs · 9,264 cycles

FOUND LT FS 280.00 CROSSBEAM CRACKED AND CORRODED BETWEEN LBL9.0 AND LBL12.0.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 12,114 hrs · 9,264 cycles

LBL12 COCKPIT FLOORBEAM FWD OF FS 280 ON UPPER SIDE FOUND INDICATION APPROXIMATELY 1.3" LONG 100 PERCENT FCH, FAILED NDT INSPECTION.

Part: BULKHEAD WEB — CORRODED (BS 280) · corrosion level 2 · airframe 12,114 hrs · 9,264 cycles

RIGHT BS 280.00 LOWER BULKHEAD WEB IS CORRODED.

Part: BULKHEAD WEB — CORRODED (BS 280) · corrosion level 2 · airframe 12,114 hrs · 9,264 cycles

LEFT BS 280 LOWER BULKHEAD WEB IS CORRODED.

Part: FLASHLIGHT — INOPERATIVE (AFT CABIN) · airframe 11,951 hrs · 9,139 cycles

AFT F/A FLASHLIGHT INOPERATIVE.

Part: FLASHLIGHT — INOPERATIVE (FWD CABIN) · airframe 11,899 hrs · 9,100 cycles

FWD F/A FLASHLIGHT INOPERATIVE.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 11,854 hrs · 9,057 cycles

EMERGENCY FLOOD LIGHT HAD ONE BULB INOPERATIVE.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 11,743 hrs · 8,967 cycles

EMERGENCY EXIT SIGN FLOOR LEVEL BY SERVICE DOOR, ONE BULB INOPERATIVE, REPLACED THE LAMP.

Part: SKIN — DAMAGED (BS 394-409) · airframe 10,581 hrs · 8,269 cycles

DAMAGE TO RT BELLY SKIN BETWEEN FS 394-409, STR 15-16R. C/W REPAIRS AS REQUIRED.

Part: SKIN — DAMAGED (BS 394-409) · airframe 10,852 hrs · 8,269 cycles

RT FUSELAGE SKIN DAMAGED BETWEEN FS 394-409, STRINGERS 15-16R. REPAIRED IAW REO 690-53-21-809, REV , DATED 2015-12-22.

Part: SKIN — PUNCTURED (BS 349-409) · airframe 10,582 hrs · 8,269 cycles

DAMAGE TO RT BELLY SKIN AT FS 394 TO FS 409 BETWEEN STRINGER 15R AND 16R.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 10,754 hrs · 8,196 cycles

CABIN ENTRY DOOR LEVEL EMERGENCY LIGHT HAS ONE BULB INOPERATIVE. REPLACED THE BULB IAW 33-51-11; OPS CHECKED GOOD IAW AMM 33-51-00.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 10,733 hrs · 8,180 cycles

FLOOR LEVEL EMERGENCY FLOOD LIGHT.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 10,347 hrs · 7,869 cycles

F/O'S FLASHLIGHT INOPERATIVE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 10,183 hrs · 7,726 cycles

SERVICE DOOR EMERGENCY LIGHTS FLICKER ON AND OFF, REPLACED THE LAMP.

Part: BATTERY PACK — INOPERATIVE (FLASHLIGHT) · airframe 9,476 hrs · 7,194 cycles

F/O FLASHLIGHT INOPERATIVE. REPLACED BATTERY.

Part: BALLAST — ODOR (CABIN LIGHTS) · airframe 9,336 hrs · 7,088 cycles

BURNING PLASTIC ODOR FROM FWD LAV. REPLACED FORWARD LAVATORY LIGHTING BALLAST.

Part: FLASHLIGHT — INOPERATIVE (FWD CABIN) · airframe 9,301 hrs · 7,063 cycles

FWD CABIN EMERGENCY FLASHLIGHT INOPERATIVE.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 9,092 hrs · 6,917 cycles

EMERGENCY SIGN BY PASSENGER DOOR HAS 2 BULBS INOPERATIVE. REPLACED BULBS.

Part: SLAT SYSTEM — FAILED · airframe 8,638 hrs · 6,584 cycles

SLATS FAILED CAUTION MESSAGE. PILOT DECLARED AN EMERGENCY. CLEARED INHIBITS AND OPERATED SLATS.

Part: UNKNOWN — ODOR (CABIN) · airframe 7,645 hrs · 5,876 cycles

ELECTRICAL ODOR AT EXIT ROW AREA. MAINTENANCE INSPECTED, NO ELECTRICAL ODOR NOTED.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 5,780 hrs · 4,367 cycles

AFT FLASHLIGHT INOPERATIVE.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 5,136 hrs · 3,823 cycles

GALLEY EXIT SIGNS INOPERATIVE, CHARGED BATTERIES.