N246LR

Part: SKIN — CHAFED (ZONE 100) · airframe 27,999 hrs · 21,176 cycles

AFT FUSELAGE SKIN CHAFED AT FS920 STR27. REPAIRED AFT FUSELAGE SKIN AT FS920 STR27 IN REF TO REO 670-53-00-290 REV. -F AND REO 690-53-00-649 REV. -. COMPLIED WITH TASK CARD 51-900-1002-SKY. PRESSURIZATION LEAK CHECKED GOOD.

Part: ROLLER — WORN (SLAT TRACK) · airframe 27,999 hrs · 21,176 cycles

LH SLAT TRACK 2-2 FWD AND AFT IB SIDE ROLLERS AND FWD OB SIDE ROLLER WORN OUT OF LIMITS. REMOVED AND REPLACE LH SLAT TRACK 2-2 FWD IB AND OB ROLLERS PER AMM 27-81-44-400-802 (CONFIG A01) AND REEVALUATED AFT IB ROLLER FOUND TO WITHIN LIMMITS PER AMM 27-81-43-220-801 (CONFIG A01) STEP 4. E. (1) - (7) AND REINSTALLED PER AMM 27-81-44-400-802 (CONFIG A01)

Part: ROLLER — WORN (RT SLAT TRACK) · airframe 27,999 hrs · 21,176 cycles

RH SLAT TRACK 2-2 AFT IB SIDE ROLLER WORN OUT OF LIMITS. REEVALUEATED RH SLAT TRACK 2-2 AFT SIDE ROLLER FOUND TO BE WITHIN LIMITS PER CRJ 900 AMM 27-81-43-220-801 (CONFIG A01) STEP 4. E. (1) - (7) AND REINSTALLED PER CRJ 900 AMM 27-81-44-400-802 (CONFIG A01)

Part: ROLLER — WORN (RT SLAT TRACK) · airframe 27,999 hrs · 21,176 cycles

RH SLAT TRACK 3-2 FWD IB AND FWD OB SIDE ROLLERS WORN OUT OF LIMITS. REMOVED AND REPLACED RH SLAT TRACK 3-2 FWD OB ROLLER PER CRJ 900 AMM 27-81-44-400-803 (CONFIG A01) AND REEVALUATED RH SLAT TRACK 3-2 FWD IB ROLLER FOUND TO BE WITHIN LIMITS PER CRJ 900 AMM 27-81-43-220-801 (CONFIG A01) STEP 4. E. (1) - (7) AND REINSTALLED PER CRJ 900 AMM 27-81-44-400-802 (CONFIG A01)

Part: ROLLER — WORN (SLAT TRACK) · airframe 27,999 hrs · 21,176 cycles

LH SLAT TRACK 3-2 FWD OB SIDE ROLLER AND AFT IB SIDE ROLLER WORN OT OF LIMITS. REEVALUATED LH SLAT TRACK 3-2 FWD OB SIDE ROLLER AND AFT IB SIDE ROLLER AND FOUND TO BE IN LIMITS PER CRJ 900 AMM 27-81-43-220-801 STEP 4. E. (1) - (7) REINSTALLED PER CRJ 900 AMM 27-81-44-400-803 (CONFIG A01)

Part: ROLLER — WORN (RT SLAT TRACK) · airframe 27,999 hrs · 21,176 cycles

RH SLAT TRACK 1-2 FWD AND AFT IB SIDE ROLLERS AND AFT OB SIDE ROLLER WORN OUT OF LIMITS (C-CHECK RO 04/17/2026)REMOVED AND REPLACED RH SLAT TRACK 1-2 FWD IB ROLLER PER CRJ 900 AMM 27-81-44-400-801 (CONFIG A01) AND REEVALUATED RH SLAT TRACK 1-2 AFT OB ROLLER AND FOUND TO BE WITHIN LIMITS PER CRJ 900 AMM 27-81-43-220-801 (CONFIG A01) STEP 4. E. (1) - (7) AND REINSTALLED PER CRJ 900 AMM 27-81-44-400-801 (CONFIG A01)

Part: ROLLER — WORN (SLAT TRACK) · airframe 27,999 hrs · 21,176 cycles

LH SLAT TRACK 1-2 FWD AND AFT OB SIDE ROLLERS AND FWD IB SIDE ROLLER WORN OUT OF LIMITS. REMOVED AND REPLACED LH SLAT TRACK 1-2 IB AND OB FWD ROLLERS PER AMM 27-81-44-400-801 (CONFIG A01) REEVALUATED LH SLAT TRACK 1-2 AFT OB SIDE ROLLER FOUND TO BE WITHIN LIMITS IAW AMM 27-81-43-220-801 (CONFIG A01) STEP 4. E. (1) - (7) AND REINSTALLED PER CRJ 900 AMM 27-81-44-400-801 (CONFIG A01)

Part: SKIN — CORRODED (ZONE 200) · airframe 27,999 hrs · 21,176 cycles

CORROSION FOUND ON SKIN @ R1 DOOR SKIN CUTOUT 2 INCHES BELOW LWR EDGE (C-CHECK RO 04/17/2026)BLENDED OUT CORROSION IN DICREPANT AREA. AREA WAS BLESSED WITHIN LIMITS AS PER MHIRJ REO 690-53-21-2046 REV. -- DATED: 2025-11-04. COMPLIED WITH ALL STEPS OF REO. SEE CONTINUATON CARD FOR DETAILS OF WORK PERFORMED. (INSTALLATION OF SCUFF PLATE WILL BE C.W ON HT461/10983)COMPLIED WITH TASK CARD 51-900-1002-SKY "STRUCTURAL MAJOR REPAIR (**RII**). BLEND OUT ONLY NOW WEIGHT DIFFERENCE.COMPLIED WITH M-337. PRESSURE LEAK CHECK PERFORMED ON HT 461 / 20376, CAMP # 31744928.

Part: SKIN — CRACKED (ZONE 100) · airframe 27,999 hrs · 21,176 cycles

RIGHT FUSELAGE ADG SKIN HAS POSSIBLE CRACK AT AFT LOWER CORNER OF TRU BAY DOOR OPENING (C-CHECK RO 04/17/2026)REMOVED AND REPLACED ADG SKIN AT RH FUSELAGE IN REF. TO CRJ-900 SRM 51-42-06-001-001-A01 PAR. 6.B, 51-42-13-001-001-A01 PAR. 6.B AND REO #690-53-11-2150 REV. -A DATE 2026-03-16 AND DWG PL CC670-33109-5 REV. -DCOMP[L;IED WITH TASK 51-900-1002-SKY.

Part: LANDING — CRACKED (ZONE 100) · airframe 27,999 hrs · 21,176 cycles

R/H TRU BAY DOOR LAND HAS POSSIBLE CRACK AT AFT LATCH CUTOUT. REMOVED AND RAPLACED TRU BAY DOOR LANDING R/H P/N CC670-33151-6 P.O. # CPT837 IAW SRM 51-42-06-001-001-A01 PG 7 PARA 6 (A) AND SRM 51-42-13-001-001-A01 PG 8 PARA 6 (A). NO WEIGHT CHANGES NOTED, REMOVED AND REPLACED LANDING. COMPLIED WITH TASK CARD 51-900-1002-SKY (CL600-2D24)

Part: ROLLER — OUT OF LIMITS (ZONE 600 SLAT) · airframe 27,999 hrs · 21,176 cycles

COMPLY WITH SCHEDULED MAINTENANCE CODE: TRACK ROLLER SLAT 1-2 900 RH - COMPLY WITH TASK CARD 27-630-809 RH TRACK ROLLER SEALED, TRACK 1-2, TOP FORWARD - SLAT 1 ( REMOVED AND REPLACED RH TRACK ROLLER SEALED TRACK 1-2 , TOP FORWARD SLAT 1 IAW AMM CRJ900 27-81-43-400-801COMPLIED WITH TASK CARD 27-630-809TW:DKJ2023 DUE: 05/31/2026

Part: WINDOW — FAILED (COCKPIT) · airframe 27,994 hrs · 21,172 cycles

FO WINDSHEILD SHATTERED RTF EMERGENCY DECLARED. CURRENTLY OOS - REPLACE WINDOW IN WORK.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 26,181 hrs · 19,732 cycles

ROW 18 OVRHD CEILING EMER FLOOD LT INOP. RELAMPED.

Part: NONE — NONE · airframe 25,927 hrs · 19,532 cycles

LWR GLY EXT SGN LITE BULBS INOP. RELAMPED.

Part: SWITCH — NONE (ZONE 200) · airframe 27,799 hrs · 19,438 cycles

EMR LTS ON W SW IN ARMD POSTN RESET CIRCUIT BREAKER. PERFORMED OPERATION CHECK OF THE EMERGENCY LIGHTS. OPS CHECK GOOD.

Part: NONE — NONE · airframe 24,824 hrs · 18,733 cycles

SVC DOOR EXIT SIGN 1 BULB INOP. REPLACED BULB.

Part: NONE — NONE · airframe 24,824 hrs · 18,733 cycles

PAX DOOR EXIT SIGN 1 BULB INOP. REPLACED BULB

Part: NONE — NONE · airframe 24,814 hrs · 18,725 cycles

LH FWD OVERWING EXTERNAL EMERGENCY EXIT WING LT INOPERATIVE.- PLACED ON MEL

Part: NONE — NONE · airframe 24,814 hrs · 18,725 cycles

LH AFT EXTERNAL OVERWING EXIT LIGHT INOPERATIVE. -PLACED ON MEL

Part: NONE — NONE · airframe 24,544 hrs · 18,510 cycles

AFT LAV SMOKE DETECTOR WENT OFF IN FLIGHT (FALSE INDICATION). CLEANED SMOKE DETECTOR, OPS CHECK GOOD.

Part: NONE — NONE (AFT EDGE Z MEMBE) · airframe 24,140 hrs · 18,231 cycles

RH LOWER FORWARD CORE COWL Z MEMBER ON THE AFT EDGE WAS FOUND WITH WEAR DAMAGE. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 54-23-10, FIGURE 4-23-10-991-801, ITEM 10, EA 69-2021-196.

Part: NONE — NONE (RH FAN COWL DOOR) · airframe 24,140 hrs · 18,231 cycles

RH UPPER FAN COWL DOOR HINGE FITTING (PN -CN622-0306-206) AND ITS MATING STRUCTURE, THE PYLON TIE BAR (PN -CN624-4203-207) WERE FOUND TO HAVE CORROSION DAMAGE. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 54-14-05-001-001-A01, 54-24-01-001-002-A01, EA12-2021-267

Part: NONE — NONE (RH FWD CORE COWL) · airframe 24,140 hrs · 18,231 cycles

OUTBOARD LOWER FACING SHEET OF THE RH UPPER CORE COWL BONDMENT ASSEMBLY WAS FOUND TO HAVE 2EA GOUGES. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 54-23-15, 54-23-15-991-801, ITEM 2, EA 72-2021-212. DEFECT LOCATION: RH FWD CORE COWL BONDMENT ASSEMBLY

Part: NONE — NONE (ANGLE LOWER SUPP) · airframe 24,140 hrs · 18,231 cycles

LOWER SUPPORT ANGLE OF THE FWD BAGGAGE BAY DOOR SURROUND STRUCTURE WAS FOUND BENT. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 53-31-23, FIGURE 53-31-2-991-802, ITEM 74 EA 72-2021-203.

Part: NONE — NONE (FS629-661+16.00) · airframe 24,140 hrs · 18,231 cycles

FUSELAGE SKIN AT FS629.00-FS661.00+16.00 AND STGR21L-STGR25L WAS FOUND TO HAVE NICKS. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 53-31-01, FIGURE 53-31-01-991-806, ITEM 1B, EA 72-2021-209.

Part: NONE — NONE (FS565.00 STR16L&) · airframe 24,140 hrs · 18,231 cycles

FUSELAGE SKIN AND JOINT PANEL LOCATED IN THE UPPER CORNER OF THE FORWARD BAGGAGE DOOR SURROUND STRUCTURE AT FS571.300 WAS FOUND WITH WEAR DAMAGE. PERFORMED PERMANENT REPAIR IAW CRJ700/900 SRM 53-31-01, FIGURE 53-31-01-995-801, ITEM 1A AND 53-31-23, FIGURE 53-31-23-991-802, ITEM 45A, EA 69-2021-186 PART NUMBER: SH690-33102-19/SH670-33832-5

Part: NONE — NONE (FLS15.00 TO FLS3) · airframe 24,140 hrs · 18,231 cycles

SEVEN DENTS WERE FOUND AFFECTING THE LOWER SKIN OF LEFT INBOARD FLAP LOCATED AT APPROXIMATELY FSL 20. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 57-52-01, FIGURE 57-52-01-991-801, ITEM 27A.

Part: NONE — NONE (REINFORCE LATCH/) · airframe 24,140 hrs · 18,231 cycles

R/H LOWER FORWARD CORE COWL REINFORCING LATCH WAS FOUND TO HAVE WEAR DAMAGE, WHICH IS LOCATED AT THE FREE EDGE AT THE LATCH, LOCATED ALONG THE EDGE WHERE THE DOOR LATCH ENGAGES AND CAUSES WEAR DAMAGE. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 54-23-10-001-002-A01, EA 20-2021-200. DEFECT LOCATION: REINFORCING LATCH/FREE EDGE

Part: NONE — DENTED (FLS 24.00) · airframe 24,140 hrs · 18,231 cycles

NBOARD FLAP LOWER SKIN OF THE RH WING WAS FOUND TO HAVE (2) DENTS AT FLS 24.00. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM57-52-01, ITEM 28A, B, EA 80-2021-153

Part: NONE — NONE (PANEL 584EB/FWD) · airframe 24,140 hrs · 18,231 cycles

WEAR DAMAGE WAS FOUND ON THE L/H INBOARD FLAP UPPER ACCESS PANEL 584EB, THE DAMAGE IS LOCATED IN THE FORWARD EDGE. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 57-52-01-001-001-A01, DATED AUG-20-2010, EA 20-2021-199.

Part: NONE — NONE (FWD BAG BAY DOOR) · airframe 24,140 hrs · 18,231 cycles

OUTER SKIN AND DOUBLER OF THE FORWARD BAGGAGE BAY DOOR WERE FOUND TO HAVE GOUGE DAMAGE AT THE FORWARD EDGE. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 52-35-01, FIGURE 52-35-01-991-801, ITEMS 1, 2, EA 72-2021-194. DEFECT LOCATION: FWD BAG BAY DOOR. FWD EDGE

Part: NONE — NONE (SEE DESCRIPTION) · airframe 24,140 hrs · 18,231 cycles

LH OUTBOARD FLAP UPPER AND LOWER SKINS FROM LIGTHNING STRIKES ON THE TRAILING EDGE AFTER REMOVING A TEMPORARY REPAIR INSTALLED PER AN OEM REO, THE DAMAGE HAS 8 LOCATIONS, AT WS266, WS256, WS243, WS235, WS227, WS219, WS213 AND WS207. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 57-53-02, FIGURE 57-53-02-991-809, EA 69-2021-187.

Part: NONE — DAMAGED (WINGTOBODYFRNG19) · airframe 24,140 hrs · 18,231 cycles

AFT LAVATORY SERVICE DOOR.(196ER) INSTALLED ON THE WING-TO-BODY FAIRING PANEL 196DR WAS FOUND TO HAVE DAMAGE ON ONE OF THE TWO HINGES. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 IPC 52-45-01, FIGURE 1, ITEM 30, EA 81-2021-084.

Part: NONE — DAMAGED (PANELS 699AB&699) · airframe 24,140 hrs · 18,231 cycles

DAMAGE TO THE RH AILERON LOWER LEADING EDGE ACCESS PANEL 699AB AND 699BB WAS FOUND. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 57-61-02-001-001-A02 ITEMS 16, 34, AND 36, EA 81-2021-087.

Part: NONE — DENTED (LH SIDE, FS169-F) · airframe 24,140 hrs · 18,231 cycles

FUSELAGE SKIN PANEL BETWEEN FS 169 -FS 173 WAS FOUND WITH A DENT. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 53-11-01, 53-00-01-101-001-A01, EA 20-2021-195.

Part: NONE — NONE (FS1015.00 & LBL) · airframe 24,140 hrs · 18,231 cycles

WEAR DAMAGE WAS ACCIDENTALLY CAUSED TO CROSS BEAMS (P/N MM670-35314-009 AND MM670-35319-001} AT THE JOINT WITH CLIP (P/N MM670-35335- 001} LOCATED AT FS1015.00 DURING MTC ACTIVITIES WHEN FLOOR BEAM WAS REMOVED. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 53-61-43-001-001-A01, FIGURE 53-61-43-991-801, ITEM 29A,21B, EA 81-2021-085 .

Part: NONE — DAMAGED (AFT LAV SVC DR,) · airframe 24,140 hrs · 18,231 cycles

THE AFT LAVATORY SERVICE DOOR(196ER) INSTALLED ON THE WING-TO-BODY FAIRING PANEL 196DR WAS FOUND TO HAVE DAMAGE ON ONE OF THE TWO HNGES. PERFORMED PERMANENT REPAIR IAW CRJ700/900 IPC 52-45-01, FIGURE 1, ITEM 30, EA 81-2021-084 | DEFECT LOCATION:AFT LAV SERVICE DOOR (196ER), FAIR PANEL 196DR)

Part: NONE — CORRODED (FS1000/STR23R&ST) · airframe 24,140 hrs · 18,231 cycles

FUSELAGE FRAME AT FS 1000 WAS FOUND WITH CORROSION DAMAGE AT THE THREE LOCATIONS BETWEEN STR 23R AND STR 25L. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 53-61-06-003-A01, FIGURE 5453-61-06-991-804, ITEM 2, EA 69-2021-185

Part: NONE — CORRODED (FS311.75) · airframe 24,140 hrs · 18,231 cycles

PASSENGER DOOR INTERCOSTAL DD6 WEB AND AN ATTACH BRACKET AT FS 311.75, BETWEEN INTERCOSTALS DD5 AND DD06, WERE FOUND WITH CORROSION DAMAGE. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 52-11-06-001-001-A01, " PASSENGER DOOR STRUCTURE".

Part: NONE — NONE (PAX DR LATCH MCH) · airframe 24,140 hrs · 18,231 cycles

PASSENGER DOOR LATCH MECHANISM HOUSING STOP WAS FOUND WITH WEAR DAMAGE. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 IPC 52-11-02-05-PSA REV B, FIGURE 5, ITEM 410, EA 79-2021-245. DEFECT LOCATION: LATCH MECHANISM, PAX DOOR

Part: NONE — CRACKED (PAX DOOR-AFT) · airframe 24,140 hrs · 18,231 cycles

PASSENGER DOOR AFT SIDE PANEL COMMON TO THE AIRSTAIR WAS FOUND TO HAVE A CRACK. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 52-11-04, FIGURE 52-11-04-991-801, ITEM 1B, EA 32-2021-021.

Part: NONE — CORRODED (FS985 STR25R&STR) · airframe 24,140 hrs · 18,231 cycles

FUSELAGE FRAME AT FS 985 WAS FOUND WITH CORROSION DAMAGE BETWEEN STR 25R AND STR 26R, THE DAMAGE IS ON THE OUTBOARD FLANGE INTERNAL SURFACE. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 53-61-06-003-A01, FIGURE 5453-61-06-991-804, ITEM 2, EA 69-2021-189.

Part: DOUBLER — CORRODED (POT WATER SVC SS) · airframe 24,140 hrs · 18,231 cycles

DOUBLER FOR THE POTABLE WATER SERVICING SURROUND STRUCTURE OF THE CENTER FUSELAGE WAS FOUND TO HAVE CORROSION DAMAGE AT 33 LOCATIONS. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 53-51-23-001-002-A01, FIGURE 53-51-23-991-803, ITEM 3A, EA 48-2021-049. DEECT LOCATION: POTABLE WATER SERVICING SUR STRUCTURE

Part: DOUBLER — CORRODED (POT WATER SERVIC) · airframe 24,140 hrs · 18,231 cycles

DOUBLER FOR THE POTABLE WATER SERVICING SURROUND STRUCTURE OF THE CENTER FUSELAGE WAS FOUND TO HAVE CORROSION DAMAGE AT 33 LOCATIONS. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 53-51-23-001-002-A01, FIGURE 53-51-23-991-803, ITEM 3A, EA 48-2021-049. DEFECT LOCATION: POTABLE WATER SERVICING SURROUND STRUCTURE

Part: NONE — CORRODED (GALLEY SVC DOOR) · airframe 24,140 hrs · 18,231 cycles

CORROSION ON ANGLE MOUNTING OF LOWER SILL AT GALLEY SERVICE DOOR. ANGLE MOUNTING OF LOWER SILL AT GALLEY SERVICE DOOR WAS REPLACED PER CRJ 900 SRM 51-42-06-001-001-A01

Part: INTERCOSTAL — CORRODED (VIONICS COMPARME) · airframe 24,140 hrs · 18,231 cycles

CORROSION ON INTERCOSTAL 20RH BETWEEN FS310 AND FS319 AT MAIN AVIONICS COMPARMENT. NTERCOSTAL 20RH BETWEEN FS310 AND FS319 WAS REMPLACED PER CRJ/900 SRM 51-42-21.

Part: NONE — CORRODED (AVIONICS COMPARM) · airframe 24,140 hrs · 18,231 cycles

CORROSION WERE FOUND ON SPLICES FS 333, STRGR.25R AND 26L IN REF SB 53-057C AT MAIN AVIONICS COMP| SPLICE WAS INSTALLED PER. CRJ-900 SRM 51-42-06

Part: SKIN — CRACKED (SS144.94 & SS249) · airframe 24,140 hrs · 18,231 cycles

LEADING EDGE SKIN BETWEEN SS144.94 AND SS210.69, WAS FOUND WITH A CRACK. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 57-41-01, FIGURE 57-41-01-991-801, ITEM 35D, EA 83-2021-048

Part: NONE — CORRODED (CABIN PAX) · airframe 24,140 hrs · 18,231 cycles

CORROSION ON LEFT FLOOR SEAT RAIL FS374-FS485 BL 9.0 AT PAX CABIN LEFT FLOOR SEAT RAIL FS374-FS485 BL 9.0 AT PAX CABIN WAS REPLACED PER AMM 53-00-49

Part: NONE — CORRODED (CABIN PAX) · airframe 24,140 hrs · 18,231 cycles

CORROSION ON RIGHT FLOOR SEAT RAIL FS349-FS485 BL 9.0 AT PAX CABIN | FLOOR SEAT RAIL FS349-FS485 BL 9.0 AT PAX CABIN WAS REPLACED PER CRJ-900 SRM 53- 00-49.

Part: NONE — SCRATCHED (PASSENGER DOOR H) · airframe 24,140 hrs · 18,231 cycles

SCRATCHES ON PIANO HINGE AT L 1 PASSENGER DOOR SURROUND STRUCTURE PIANO HINGE AT PASSENGER DOOR FUSELAGE SURROUND STRUCTURE WAS BLEND OUT PER CRJ/900 SRM 53-21-23-201-010-A01 AND EVALUATED PER CRJ/900 SRM 53-21-23-201-010-A01

Part: WEB — CORRODED (E/E) · airframe 24,140 hrs · 18,231 cycles

CORROSION WAS FOUND ON AFT SIDE OF CABIN BULKHEAD WEB ON LOWER CORNER BTW 9RBL AND 12RBL APROX ON FS STA 280 | CORRECTIVE ACTION:WEB ON LOWER CORNER BTW 9RBL AND 12RBL APROX ON FS STA 280 WASREPLACED PER CRJ-900 SRM 53-11-10-201-003-A01.

Part: NONE — CRACKED (BTW VERT STAB &) · airframe 24,140 hrs · 18,231 cycles

CRACK ON RH/LH ANGLES BTW VERTICAL STAB AND EXTERNAL FUSELAGE (TAIL CONE STA 67.5%). CORRECTIVE ACTION: RH/LH ANGLES BTW VERTICAL STAB AND EXTERNAL FUSELAGE (TAIL CONE STA 67.5%) WERE REPAIRED PER CRJ-900 SRM 55-31-00-201-001-A01

Part: NONE — CORRODED (CABIN PAX) · airframe 24,140 hrs · 18,231 cycles

CORROSION ON LEFT SIDE SEAT RAIL FS785.15-FS847+14 AT PAX CABIN LEFT SIDE SEAT RAIL FS785.15 TO FS847+14 PAX CABIN WAS REPLACED PER CRJ-900 AMM 53-00-49

Part: NONE — CORRODED (CABIN PAX) · airframe 24,140 hrs · 18,231 cycles

CORROSION ON RIGHT SIDE SEAT RAIL FS847+14-FS868 AT PAX CABIN NEW RIGHT SIDE SEAT RAIL FS847+14-FS868 AT PAX CABIN WAS REPLACED PER.CRJ-900 SRM 53-00-49

Part: NONE — CORRODED (CABIN PAX) · airframe 24,140 hrs · 18,231 cycles

CORROSION ON LEFT SIDE SEAT RAIL FS847+14-FS905 AT PAX CABIN. | LEFT SIDE SEAT RAIL FS847+14-FS905 WAS REPLACED PER CRJ/900 AMM 53-00-49.

Part: NONE — CORRODED (CABIN PAX) · airframe 24,140 hrs · 18,231 cycles

CORROSION ON LEFT SIDE SEAT RAIL FS573-FS661+14 AT PAX CABIN LEFT SIDE SEAT RAIL FS573-FS661+14 WAS REPLACED PER CRJ-900 AMM 53-00-49

Part: NONE — WORN (CABIN PAX) · airframe 24,140 hrs · 18,231 cycles

WEAR ON LEFT SIDE SEAT RAIL FS483-FS517 AT PAX CABIN | LEFT SIDE SEAT RAIL FS483-FS573 AT PAX CABIN WAS REPLACED PER CRJ900 AMM 53-00-49

Part: NONE — CORRODED (CABIN PAX) · airframe 24,140 hrs · 18,231 cycles

CORROSION ON LEFT SIDE SEAT RAIL FS549-FS573 AT PAX CABIN | LEFT SIDE SEAT RAIL FS549-FS573 WAS REPLACED PER CRJ-900 AMM 53-00-49

Part: NONE — CORRODED (CABIN PAX) · airframe 24,140 hrs · 18,231 cycles

CORROSION ON RIGHT SIDE SEAT RAIL FS672-FS720.85 AT PAX CABIN| RIGHT SIDE SEAT RAIL FS672-FS722 AT PAX CABIN WAS REPLACED PER CRJ900 AMM 53-00-49

Part: NONE — CORRODED (CABIN PAX) · airframe 24,140 hrs · 18,231 cycles

CORROSION ON RIGHT SIDE SEAT RAIL FS661+14-FS672 AT PAX CABIN. RIGHT SIDE SEAT RAIL FS661+14-FS672 AT PAX CABIN WAS REPLACED PER CRJ-900 AMM 53-00-49.

Part: NONE — CORRODED (CABIN PAX) · airframe 24,140 hrs · 18,231 cycles

CORROSION ON RIGHT SIDE SEAT RAIL FS379-FS483 AT PAX CABIN. SEAT RAIL RIGHT SIDE FS379-FS483 AT PAX CABIN WAS INSTALLED PER CRJ900 AMM 53-00-49

Part: NONE — CORRODED (CABIN PAX) · airframe 24,140 hrs · 18,231 cycles

CORROSION ON RIGHT SIDE SEAT RAIL FS483-FS573 AT PAX CABIN | SEAT RAIL RIGHT SIDE FS483 - FS573 AT PAX CABIN WAS REPLACED PER AMM 53-00-49

Part: NONE — CORRODED (CABIN PAX) · airframe 24,140 hrs · 18,231 cycles

CORROSION ON RIGHT SIDE SEAT RAIL FS744.15-FS761.85 AT PAX CABIN. RIGHT SIDE SEAT RAIL FS744.15-FS761.85 AT PAX CABIN WAS REPLACED PER CRJ-900 AMM 53-00-49

Part: NONE — CORRODED (CABIN PAX) · airframe 24,140 hrs · 18,231 cycles

CORROSION ON LEFT SIDE SEAT RAIL FS661+14-FS672 AT PAX CABIN | LEFT SIDE SEAT RAIL FS661+14-FS672 AT PAX CABIN WAS REPLACED PER CRJ900 AMM 53-00-49.

Part: NONE — WORN (CABIN PAX) · airframe 24,140 hrs · 18,231 cycles

WEAR ON SEVERAL PLACES ON LEFT SIDE SEAT RAIL FS379-FS483 AT PAX CABIN. LEFT SIDE SEAT RAIL FS379-FS483 WAS INSTALLED PER CRJ-900 AMM 53-00-49.

Part: NONE — CORRODED (CABIN PAX) · airframe 24,140 hrs · 18,231 cycles

CORROSION ON LEFT FLOOR SEAT RAIL FS485-FS581 BL27.0 AT PAX CABIN | SEAT RAIL LEFT FLOOR FS485-FS581 BL 27.0 AT PAX CABIN REPLACED PER CRJ900 AMM 53-00-49

Part: NONE — CORRODED (AFT BAGGAGE BAY) · airframe 24,140 hrs · 18,231 cycles

CORROSION ON FLOOR BEAM 9LBL IN STA. FS= 985 TO FS= 1088 AT AFT BAGGAGE BAY |CORRECTIVE ACTION: SECTION FLOOR BEAM 9LBL IN STA. FS= 985 TO FS= 1088 AT AFT BAGGAGE BAY WAS REPLACED PER CRJ-900 SRM 53-00-41-201-001-A03.

Part: NONE — CORRODED (CABIN PAX) · airframe 24,140 hrs · 18,231 cycles

CORROSION ON LEFT FLOOR SEAT RAIL FS661+32-FS693 BL 9.0 AT PAX CABIN | LEFT FLOOR SEAT RAIL FS661+32-FS677 BL 9.0 AT PAX CABIN WAS REPLACED PER CRJ900 AMM 53-00-49

Part: NONE — CORRODED (CABIN PAX) · airframe 24,140 hrs · 18,231 cycles

CORROSION ON LEFT FLOOR SEAT RAIL FS581-FS661+32 BL 9.0 AT PAX CABIN | LEFT FLOOR SEAT RAIL FS581-FS661+32 BL 9.0 WAS REPLACED PER CRJ-900 AMM 53-00-49

Part: NONE — CORRODED (CABIN PAX) · airframe 24,140 hrs · 18,231 cycles

CORROSION ON RIGHT FLOOR SEAT RAIL FS581-FS661+32 BL 9.0 AT PAX CABIN | RIGHT FLOOR SEAT RAIL FS581-FS661+32 BL 9.0 WAS REPLACED PER CRJ-900 AMM 53-00-49

Part: NONE — CORRODED (CABIN PAX) · airframe 24,140 hrs · 18,231 cycles

WEAR ON SEVERAL PLACES ON LEFT FLOOR SEAT RAIL FS364-FS485 BL 27.0 AT PAX CABIN LEFT FLOOR SEAT RAIL FS364-FS485 BL 27.0 AT PAX CABIN WAS REPLACED PER CRJ900 AMM 53-00-49

Part: NONE — CORRODED (CABIN PAX) · airframe 24,140 hrs · 18,231 cycles

CORROSION ON RIGHT FLOOR SEAT RAIL FS485-FS581 BL 9.0 AT PAX CABIN. NEW RIGHT FLOOR SEAT RAIL FS485-FS581 BL 9.0 WAS REPLACED PER CRJ-900 AMM 53-00-49

Part: NONE — CORRODED (CABIN PAX) · airframe 24,140 hrs · 18,231 cycles

CORROSION ON LEFT FLOOR SEAT RAIL FS485-FS581 BL 9.0 AT PAX CABIN | SEAT RAIL LEFT FLOOR FS485-FS581 BL 9.0 AT PAX CABIN REPLACED PER CRJ900 AMM 53-00-49

Part: ANGLE — CORRODED (L 1 SURROUND DOO) · airframe 24,140 hrs · 18,231 cycles

CORROSION ON MID CAP ANGLE OF L 1 SURROUND STRUCTURE WAS FOUND. CORRECTIVE ACTION: MID CAP ANGLE OF L 1 SURROUND STRUCTURE WAS REPLACED PER CRJ-900 SRM 51-41-02-001-001-A01

Part: NONE — CORRODED (CABIN PAX) · airframe 24,140 hrs · 18,231 cycles

CORROSION ON LEFT SIDE SEAT RAIL FS905-FS969 AT PAX CABIN. LEFT SIDE SEAT RAIL FS905-FS969 AT PAX CABIN WAS REPLACED PER.CRJ-900 SRM 53-00-49.

Part: NONE — CORRODED (CABIN PAX) · airframe 24,140 hrs · 18,231 cycles

CORROSION ON RIGHT FLOOR SEAT RAIL FS661+32-FS684 BL 9.0 AT PAX CABIN RIGHT FLOOR SEAT RAIL FS661+32-FS677 BL 9.0 AT PAX CABIN WAS REPLACED PER.CRJ-900 SRM 53-00-49

Part: FRAME — CORRODED (COMPARTMENT.(E/E) · airframe 24,140 hrs · 18,231 cycles

CORROSION ON FRAME FS319 BETWEEN STRINGER 26L TO 26R AT MAIN AVIONICS COMPARTMENT.(E/E) CORROSION ON FRAME FS319 BETWEEN STRINGER 26L TO 26R WAS REPLACED PER CRJ-900 SRM 53-00-06

Part: INTERCOSTAL — CORRODED (BTWN FS349 & FS3) · airframe 24,140 hrs · 18,231 cycles

CORROSION WERE FOUND ON INTERCOSTALS (4 EIA)BETWEEN FS 349 AND FS364 AND STRGR.26R TO 26L IN REF SB 53-057C AT MAIN AVIONICS COMP.(EIE). INTERCOSTALS (2 EA) ON RBL 2 AND LBL 2 BETWEEN FS349 -FS364 WERE INSTALLED PER CRJ-900 SRM 51-42-06 AND CRJ-900 SRM 51-42-21 AND INTERCOSTALS (2EA) OF SIDE OF STGR 26RH AND 26LH BETWEEN FS349 - FS364 WAS MEASURED AND WERE FOUND WITH THE FOLLOW ORIGINAL THICNNESS IS = 0.063 IN. AND REMAINING THICKNESS IS= 0.060 IN. THEREFORE AREAS ARE WITHIN OF LIMITS PER CRJ/900 SRM 53-00-00

Part: NONE — GOUGED (CARGO/C1) · airframe 24,140 hrs · 18,231 cycles

GOUGES ON FWD/LWR AND AFT/LWR GUIDES FITTINGS AT BOTH FWD AND CENTER CARGO COMPARTMENT DOORS SURROUND STRUCTURES CORRECTIVE ACTION: DAMAGE WAS REMOVED AND WAS REPAIRED PER CRJ-900 SRM 53-31-23-201-002-A01

Part: NONE — NONE (FWD BAY DOOR) · airframe 24,140 hrs · 18,231 cycles

GOUGE ON SKIN LOCATED ON UP/FWD CORNER TO FWD BAGGAGE DOOR CORRECTIVE ACTION: GOUGE ON SKIN LOCATED ON UP/FWD CORNER TO FWD BAGGAGE DOOR WAS REPAIRED PER EA 72-2021-194 REV. IR.

Part: NONE — CRACKED (ADG COMPARTMENT) · airframe 24,140 hrs · 18,231 cycles

CRACK IN UPPER WEB OF INTERNAL ADG COMPARTMENT, BELOW OF SETTLEMENT AREA OF ADG PUMP. CRACK IN UPPER WEB OF INTERNAL ADG COMPARTMENT, BELOW OF SETTLEMENT AREA OF ADG PUMP WAS REPAIR PER CRJ-900 SRM 53-11-43-201-001-A01

Part: NONE — CRACKED (C/PAX) · airframe 24,140 hrs · 18,231 cycles

CRACK ON FLOOR BE AM 12 RBL IN STA. FS= 280 CPIL | CORRECTIVE ACTION : FLOOR BEAM SECTION 12 RBL BTW. FS STA= 265 AND FS STA= 280 CPIL WAS REPLACED PER CRJ/900 SRM 51-40-11-001-001-A01 AND CRJ-900 SRM 51-42-20-001-001- A01

Part: NONE — NONE (CARGO/C1) · airframe 24,140 hrs · 18,231 cycles

WEAR ON FWD/UP AND AFT/UP ROLLER GUIDES FITTINGS AT BOTH FWD AND CENTER CARGO COMPARTMENT DOORS SURROUND STRUCTURES CORRECTIVE ACTION: DAMAGE WAS REMOVED AND WAS REPAIRED PER CRJ-900 SRM 53-31-23-201-002-A01

Part: NONE — CRACKED (CIRCUNF SKIN JO) · airframe 24,140 hrs · 18,231 cycles

CRACKED STRINGER #3 [ LINTEL AREA] BTW STA. FS= 280 AND STA FS= 295 AT CIRCUNFERENTIAL SKIN JOINT. (CPAX). INSTALLATION OF REPAIR PER BOMBARDIER SERVICE BULLETIN 670BA-53-040 REV. C AND REO 670-53-21-493 REV D ---- DEFECT LOCATION: CIRCUNFERENTIAL SKIN JOINT. (CPAX).

Part: SMOKE WARNING — FALSE ACTIVATION (AFT LAVATORY) · airframe 24,027 hrs · 18,149 cycles

SMOKE AFT LAV WARNING IN FLT -FALSE INDICATION. PLACED AFT LAV SMOKE DET ON MEL.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 22,062 hrs · 16,737 cycles

SERVICE DOOR EXIT SIGN 1 BULB INOPERABLE. PLACED ON MEL.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 21,989 hrs · 16,680 cycles

GALLEY EXIT SIGN HAS 1 BULB INOPERABLE. PLACED ON MEL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,668 hrs · 16,454 cycles

PAX DOOR ENTRY EXIT SIGN 1 BULB INOP REPLACED BULB

Part: WARNING MESSAGE — ILLUMINATED · airframe 20,680 hrs · 15,733 cycles

LH BLEED DUCT WARNING WITH RT ON MEL.

Part: BATTERY — INOPERATIVE (FWD FLASHLIGHT) · airframe 20,470 hrs · 15,573 cycles

FWD FA FLASHLIGHT IND LIGHT INOP REPLACED BATTERY

Part: FLASHLIGHT — INOPERATIVE (AFT CABIN) · airframe 17,467 hrs · 13,315 cycles

AFT FA FLASHLIGHT INOPERATIVE.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 17,306 hrs · 13,189 cycles

FO'S FLASHLIGHT INOP. PLACED ON MEL.

Part: SIGN — INOPERATIVE (EMERGENCY LIGHT) · airframe 16,197 hrs · 12,343 cycles

ROW 4 REAR FACING EMERGENCY EXIT SIGN INOPERATIVE.

Part: FLASHLIGHT — INOPERATIVE (FWD CABIN) · airframe 16,147 hrs · 12,307 cycles

FWD FA FLASHLIGHT INOPERATIVE.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 16,147 hrs · 12,307 cycles

ROW 3/4 AFT FACING EMERGENCY EXIT SIGN INOPERATIVE. CHARGED THE BATTERY.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 16,147 hrs · 12,307 cycles

RT FWD OVER WING EMER EXIT SIGN INOP. REPLACED BATTERY PACK.

Part: SIGN — INOPERATIVE (CABIN) · airframe 16,144 hrs · 12,305 cycles

ROW 3/4 AFT FACING EMER EXIT SIGN INOP. CHARGED WITH EXTERNAL POWER.

Part: SEAT TRACK — CORRODED (BS 581-661) · corrosion level 2 · airframe 16,140 hrs · 12,303 cycles

RBL 9, BS 581 - 661+32 SEAT TRACK CORRODED.

Part: SEAT TRACK — CORRODED (BS 485-581) · corrosion level 2 · airframe 16,140 hrs · 12,303 cycles

RBL 9, BS 485 - 581 SEAT TRACK IS CORRODED.

Part: ANGLE — CORRODED (BS 280 FLOORBEAM) · corrosion level 2 · airframe 16,140 hrs · 12,303 cycles

BS 280 FLOORBEAM ANGLE IS CORRODED.

Part: DRAG ANGLE — CRACKED (VERTICAL STAB) · airframe 16,140 hrs · 12,303 cycles

PERFORMED A MAJOR REPAIR TO LT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FORWARD DRAG ANGLE IAW REO 670-55-31-018 REV A DATED 2016-11-10.

Part: DRAG ANGLE — CRACKED (VERTICAL STAB) · airframe 16,140 hrs · 12,303 cycles

PERFORMED A MAJOR REPAIR TO RT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FORWARD DRAG ANGLE IAW REO 670-55-31-018 REV A DATED 2016-11-10.

Part: SEAT TRACK — CORRODED (BS 661-677) · corrosion level 2 · airframe 16,140 hrs · 12,303 cycles

SEAT TRACKS CORRODED, RBL 9 BS 661+32 - 677.

Part: INTERCOSTAL — CORRODED (BS 349-364) · corrosion level 2 · airframe 16,140 hrs · 12,303 cycles

AVIONICS DOOR FWD INTERCOSTAL 27L CORRODED.

Part: BATTERY PACK — DISCHARGED (FLASHLIGHT) · airframe 14,747 hrs · 11,198 cycles

FWD FA FLASHLIGHT LED. REPLACED FLASHLIGHT BATTERY.

Part: FLASHLIGHT — INOPERATIVE (FWD CABIN) · airframe 14,565 hrs · 11,057 cycles

FWD FA FLASHLIGHT INOPERATIVE.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 14,461 hrs · 10,982 cycles

PAX DOOR FLOOR LEVEL EMER SIGN 2 BULBS INOP. REPLACED BULBS.

Part: BULB — INOPERATIVE (EMERGENCY LIGHTS) · airframe 13,772 hrs · 10,477 cycles

FWD FA SEAT EMERGENCY EXIT SIGN HAD ONE BULB INOPERATIVE.

Part: FLOORBEAM — CRACKED (BS 276) · airframe 11,918 hrs · 9,071 cycles

LBL 12.0 FLOORBEAM HAS AN INDICATION NOTED AT FS 276.0, WL 73.0 .3" LONG.

Part: FLOORBEAM — CRACKED (ZONE 100) · airframe 11,918 hrs · 9,071 cycles

RBL 12.0 FLOORBEAM HAS AN INDICATION AT FS 276.0, WL 73 .3" LONG.

Part: FLOORBEAM — CORRODED (BS 280) · corrosion level 2 · airframe 11,918 hrs · 9,071 cycles

FS 280 FLOORBEAM CORROSION ON UPPER SURFACE BETWEEN LBL 9 AND RBL 9.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 11,918 hrs · 9,071 cycles

COCKPIT FLOORBEAMS AT LBL 12 AND RBL 12 ARE CRACKED FORWARD OF FS 280.00.

Part: TRANSCOWL — DENTED (LEFT) · airframe 11,918 hrs · 9,071 cycles

DURING HEAVY CHECK INSPECTION, A DENT WAS DISCOVERED ON THE LT LOWER TRANSCOWL, LOWER OTBD AREA, MEASURING APPROXIMATELY 2" W X 2" L X .020" D. DENT WAS REPAIRED IAW BSC EO CL600-2D24-71-L03954.

Part: FLASHLIGHT — INOPERATIVE (AFT CABIN) · airframe 11,748 hrs · 8,938 cycles

AFT CABIN FLASHLIGHT WILL NOT TEST.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 985 hrs · 8,325 cycles

CEILING LEVEL EMERGENCY LIGHT EXIT STAYS ILLUMINATED.

Part: LIGHT — MISSING (ROWS 12-13) · airframe 10,583 hrs · 7,981 cycles

EMERGENCY LIGHT STRIP ROWS 12EF &13AC MISSING. REPLACED EMERGENCY LIGHT STRIPS.

Part: FLASHLIGHT — INOPERATIVE (AFT CABIN) · airframe 9,384 hrs · 7,092 cycles

AFT F/A FLASHLIGHT INOPERATIVE. R & R FLASHLIGHT, OPS CHECK GOOD.

Part: A/C PACK — ODOR (RIGHT) · airframe 8,427 hrs · 3,507 cycles

RIGHT PACK AUTO FAIL, ODOR LIKE A BURNED MATCH. MAINTENANCE IS TROUBLESHOOTING.

Part: PLACARD — WORN (PAX DOOR) · airframe 8,323 hrs · 6,371 cycles

FOUND PAX DOOR STEP OPEN PLACARD WORN. R & R PLACARD.

Part: CRADLE — BROKEN (FLASHLIGHT) · airframe 8,207 hrs · 6,274 cycles

FLASHLIGHT CHARGING INDICATOR BROKEN.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 7,989 hrs · 6,128 cycles

FLOOR LEVEL SERVICE DOOR EMERGENCY LIGHT LENS MISSING.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 7,031 hrs · 5,392 cycles

FOUND ONE PEANUT BULB OUT ON THE ENTRY WAY LOWER EMERGENCY LIGHT. REMOVED AND REPLACED THE BULB, OPS CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (FLASHLIGHT) · airframe 6,362 hrs · 4,821 cycles

FORWARD F/A FLASHLIGHT INOPERATIVE. MAINTENANCE REPLACED FLASHLIGHT BATTERY.

Part: BATTERY PACK — INOPERATIVE (FLASHLIGHT) · airframe 6,189 hrs · 4,684 cycles

FWD CABIN EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED NR 2 AND 3 BATTERY PACKS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 6,175 hrs · 4,673 cycles

EMERGENCY CEILING LIGHT FROM ROW 12 FWD INOPERATIVE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 6,022 hrs · 4,547 cycles

RIGHT FWD EXTERIOR EMERGENCY LIGHT INOPERATIVE.