N186GJ

Part: HAND RAIL — OUT OF ADJUST (ZONE 800) · airframe 24,372 hrs · 19,699 cycles

MAIN CABIN DOOR STICKING CLOSED AND WOULD NOT OPEN UPON ARRIVAL. PERFORMED ADJUSTMENTS TO MAIN CABIN DOOR HAND RAIL IAW 900 AMM 52-11-05. PERFORMED MULTIPLE OPS TESTS IAW 900 AMM 52-11-00 OF MAIN CABIN DOOR, ALL OPS TESTS GOOD. NO FURTHER DEFECTS NOTED.

Part: DOOR — INOPERATIVE (MAIN) · airframe 21,743 hrs · 21,743 cycles

MAIN CABIN DOOR WOULD NOT OPEN, PAX DOOR OP, CHK IAW AMM 52-11-00, CAM ROLLERS ON PAX DOOR LUBRICATED, NO DEFECTS NOTED,

Part: BULB — INOPERATIVE (UNKNOWN) · airframe 20,313 hrs · 16,335 cycles

UPON EMERGENCY LIGHTS OPS TEST FOUND ALL EMERGENCY LIGHTS TO BE INOP ON ENTRANCE STORAGE COMPARTMENT PN: 3071BPEGPL REPLACED EMERGENCY LIGHT BULBS ON ENTRANCE STORAGE COMPARTMENT PN:WL3071BPEGPL IAW CRJ 900 AMM 33-51-05-960-801-A02. OPS TEST GOOD ON ENTRANCE STORAGE COMPARTMENT EMERGENCY LIGHTS IAW CRJ 900 AMM 33-51-00-710-802-A04

Part: BRACKET — CORRODED (MLG WW) · airframe 20,313 hrs · 16,335 cycles

UNDER BLOW OUT PANEL 642AZ HYDRAULICS BRACKET FOR IB BK, LG EX, LG RET CORRODED IN RH MLG WHEEL WELL. INSTALLED NEW SERVICEABLE PANEL 642AZ BRACKET (P/N: CC670-10337-2) IAW CRJ900 AMM 20-21-00-910-801(A01) & AMM 20-22-00-910-801(A01).

Part: SEAT TRACK — CORRODED (BS 661-693) · airframe 20,313 hrs · 16,335 cycles

RBL 9 SEAT RAIL IS CORRODED BETWEEN FS 661+32 AND FS 693. REMOVED RBL 9 SEAT RAIL BETWEEN FS 661+32 AND FS 693 IAW CRJ900 AMM 53-00-49-000-801-A07 INSTALLED A NEW RBL 9 SEAT RAIL BETWEEN FS 661+32 AND FS 693 IAW CRJ900 AMM 53-00-49-400-801-A07, REO 670-53-00-589 REV -C DATED 2022-12-19.

Part: SEAT TRACK — CORRODED (UNKNOWN) · airframe 20,313 hrs · 16,335 cycles

SIDE SEAT RAIL AT STGR 15R IS CORRODED BETWEEN FS 661+16 AND FS 661+90. REMOVED CORODED R/H SIDE SEAT RAIL FROM F.S.661+16 TO F.S.661+90 AND INSTALLED NEW SERVICABLE SEAT RAIL IAW MHIRJ REO 670-53-00-587 REV C DATED 2023-02-08 AND CRJ 900 AMM 53-00-49-400-801-A13.

Part: SEAT TRACK — CORRODED (UNKNOWN) · airframe 20,313 hrs · 16,335 cycles

SIDE SEAT RAIL AT STGR 15L IS CORRODED BETWEEN FS 379 AND FS 485. REMOVED CORODED L/H SIDE SEAT RAIL FROM F.S.379 TO F.S.485 AND INSTALLED NEW SERVICABLE SEAT RAIL IAW MHIRJ REO 670-53-00-587 REV C DATED 2023-02-08 AND CRJ 900 AMM 53-00-49-400-801-A13.

Part: STRINGER — CORRODED (UNKNOWN) · airframe 20,313 hrs · 16,335 cycles

STRINGER 25L CORRODED BETWEEN FS333 - FS364. REPAIRED STGR 25L FROM F.S.333 TO F.S.349 IAW ENDEAVOR AIR EA CRJ953-15452 REV IR DATED 9/15/2023.

Part: FLOORBEAM — CORRODED (UNKNOWN) · airframe 20,313 hrs · 16,335 cycles

S 280 CORROSION NOTED AT APPROXIMATELY LBL 15.0 BETWEEN ANGLE (CAP) AND TOP OF CROSSBEAM, AROUND NUTPLATE HOLE FOR CABIN FLOORBOARD LH FS 280 CROSSBEAM IS HEAVILY CORRODED IN MULTIPLE LOCATIONS AND IS CRACKED ON UPPER FLANGE. NO LIMITATIONS PROVIDED IN SRM, REQUIRES REPLACEMENT. LOCATED AND DRILLED LH FS 280 CROSSBEAM PN: CC670-34094-1 IAW CRJ 900 SRM 51-40-11-001-001-A01. INSTALLED LH FS 280 CROSSBEAM PN: CC670-34094-1 IAW CRJ 900 SRM 51-42-06-001-001-A01.

Part: ANGLE — CRACKED (UNKNOWN) · airframe 20,313 hrs · 16,335 cycles

RBL 26 (P/N: CC670-34117-6) STIFFENING ANGLE ON RH FS 280 LWR BULKHEAD WEB FOUND TO BE CRACKED. LOCATED AND DRILLED NEW SERVICEABLE STIFFENING ANGLE PN: CC670-34117-6 IAW CRJ 900 SRM 51-40-11-001-001-A01.INSTALLED NEW STIFFENING ANGLE PN: CC670-34117-6 AT RBL 26 AND FS 280 IAW CRJ 900 SRM 51-42-06-001-001-A01.

Part: SKIN — CORRODED (UNKNOWN) · airframe 20,313 hrs · 16,335 cycles

"FUSELAGE SKIN IS CORRODED UNDER AFT CARGO DOOR PROTECTOR PLATE BETWEEN F.S. 1031 TO F.S. 1051. REMOVED CORROSION IN FUSELAGE SKIN UNDER AFT CARGO DOOR PROTECTOR PLATE, STRG 19L BETWEEN FS. 1031.0 TO FS. 1051.0, IAW CRJ900 SRM 51-21-06-001-001-A01. ORIGINAL THICKNESS IS 0.150"" WITH A 0.009"" MATERIAL LOSS AND A REMAINING THICKNESS IS 0.141"" ON FUSELAGE SKIN, MAX DEPTH ALLOWED IS 0.025"" FOUND TO BE WITHIN LIMITS IAW CRJ900 SRM 53-61-01-101-002-A02. "

Part: FLOOR SUPPORT — CORRODED (UNKNOWN) · airframe 20,313 hrs · 16,335 cycles

"LH FLOOR SILL IS CORRODED AT FS 565. REMOVED CORROSION AT FS 565 IAW CRJ900 SRM 53-00-45-201-001-A01 STEPS 6 A-E. PERFORMED UT THICKNESS OF LH FLOOR SILL FS565 REWORKED AREA IAW CRJ 900 NDTM PART 1 51-20-004-270-A01 REV 36 DATED 2/8/22. FOUND LOWEST REMAINING THICKNESS TO BE 0.049"" OR GREATER, MARKED ON PART. BLENDED AREA ON FLOOR SILL P/N SH690-32174-5 AT FS 565 ORIGINAL MAT'L THK .050"" REMAINING MAT'L THK .049"" MAT'L LOSS .001 FOUND TO WITHIN LIMITS IAW CRJ900 SRM 53-00-45-201-001-A01 & 53-31-45-001-001-A02"

Part: SKIN — CORRODED (UNKNOWN) · airframe 20,313 hrs · 16,335 cycles

"LH FLOOR SILL IS CORRODED AT FS 661+16. LH FLOOR SILL IS CORRODED AT FS 661+16. CORROSION REQUIRES REMOVAL REMOVED CORROSION AT FS 661+16 IAW CRJ900 SRM 53-00-45-201-001-A01 STEPS 6A-E UT REQUIRED FOR MRT PERFORMED UT THICKNESS OF LH FLOOR SILL FS661+16 REWORKED AREA IAW CRJ 900 NDTM PART 1 51-20-004-270-A01 REV 36 DATED 2/8/22. FOUND LOWEST REMAINING THICKNESS TO BE 0.048"" OR GREATER, MARKED ON PART. NDT REQUIRED PER CRJ900 SRM 53-00-45-201-001-A01 STEP 6F PERFORMED HFEC OF LH FLOOR SILL FS661+16 REWORKED AREA IAW CRJ 900 SRM 53-00-45-201-001-A01 STEP 6F. NO INDICATIONS NOTED AT THIS TIME. REMOVED 1EA SOLID RIVET IAW CRJ900 SRM 51-42-06-001-001-A01 INSTALLED 1EA SOLID RIVET ON LH FLOOR SILL FS661+16 IAW CRJ900 SRM 51-42-06-001-001-A01. REQUIRES REMAINING STEPS OF CRJ 900 SRM 53-00-45-201-001-A01. APPLIED PROTECTIVE TREATMENT AND FINISH PAINT ON REWORKED AREA IAW CRJ900 SRM 51-25-00-001-001-A01. UT MEASUREMENTS REQUIRE EVALUATION. EVALUATED LH FLOOR SILL FS661+16, ORIGINAL THICKNESS 0.050, MATERIAL REMOVED 0.002, REMAINING THICKNESS 0.048 FOUND TO BE WITHIN LIMITS IAW CRJ900 SRM 53-00-45-201-001-A01. "

Part: SKIN — CORRODED (UNKNOWN) · airframe 20,313 hrs · 16,335 cycles

"AFT BAGGAGE BAY DOOR SILL CORRODED BETWEEN FS 1000 AND FS1047 AT STRG17L AFT BAGGAGE BAY DOOR SILL CORRODED BETWEEN FS 1000 AND FS1047 AT STRG17L. REMOVED CORROSION ON AFT BAGGAGE BAY DOOR SILL BETWEEN FS1000 AND FS1047 AT STRG17L IAW CRJ900 SRM 53-61-23-201-001-A01 REMOVED 55EA SOLID RIVETS AND 15EA NUTPLATES ON AFT BAGGAGE BAY DOOR SILL BETWEEN FS1000 AT FS1047 AT STGR 17L IAW CRJ900 SRM 51-42-06-001-001-A01 AND CRJ900 SRM 53-61-23-201-001-A01. INSTALLED 51EA SOLID RIVETS AND 15EA NUTPLATES ON AFT BAGGAGE BAY DOOR SILL BETWEEN FS1000 AT FS1047 AT STGR 17L IAW CRJ900 SRM 51-42-06-001-001-A01 AND CRJ900 SRM 53-61-23-201-001-A01. REQUIRE NDT (UT) FOR EVALS REMAINING THICKNESS. PERFORMED U.T. THICKNESS ON DOOR SILL, S17L FS1000-FS1047 REWORK AREAS IAW CRJ 900 NDTM PART 1 51-20-004-270-A01 REV 36 DATED 02/08/2022. FOUND LOWEST REMAINING THICKNESS TO BE .059"" OR GREATER. MEASUREMENTS RECORDED ON THE PART. UT MEASUREMENTS REQUIRE EVALUATION. EVALUATED AFT BAGGAGE BAY DOOR SILL BETWEEN FS 1000 AND FS1047 AT STRG17L, ORIGINAL THICKNESS 0.063, MATERIAL REMOVED 0.004, REMAINING THICKNESS 0.059, FOUND TO BE WITHIN LIMITS IAW CRJ900 SRM 53-61-23-201-001-A01. REQUIRE NDT FOR CHECK CRACK FREE IAW CRJ900 SRM 53-61-23-201-001-A01, 6. B. (3). PERFORMED H.F.E.C. ON DOOR SILL, S17L FS1000-FS1047 REWORK AREAS IAW CRJ 900 SRM 53-61-23-201-001-A01 STEP 6.B.3. NO INDICATIONS NOTED AT THIS TIME. APPLY PROTECTIVE TREATMENT AND FINISH PAINT. RESTORED TO FINISH REWORKED AREA IAW CRJ 900 SRM TR 51-0068 A023. REQUIRE INSTALL 4EA SOLID RIVETS ON AFT BAGGAGE BAY DOOR SILL BETWEEN FS1000 AT FS1047 AT STGR 17L. INSTALLED 4 EA. RIVETS ON AFT BAGGAGE BAY DOOR SILL BETWEEN FS 1000 AND FS 1047 AT STR17L IAW CRJ 900 SRM 51-42-06-001-001-A01."

Part: STRINGER — CORRODED (UNKNOWN) · airframe 20,313 hrs · 16,335 cycles

STRINGER 26R CORRODED BETWEEN FS319-FS333. REMOVED UNSERVICEABLE PART. LOCATED AND DRILLED NEW STRINGER 26R PN: SH670-31634-2S FROM FS 280-333 IAW CRJ 900 SRM 51-40-11-001-001-A01. INSTALLED NEW STRINGER 26R FROM FS280-333 IAW CRJ 900 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.

Part: STRINGER — CORRODED (UNKNOWN) · airframe 20,313 hrs · 16,335 cycles

STRINGER 26R SPLICE CORRODED AT FS333 LOCATED AND DRILLED NEW STINGER SPLICE P/N:SH670-32429-2, STR26R AT FS333 IAW CRJ-900 SRM 51-40-11-001-001-A01. INSTALLED STGR 26R SPLICE AT FS333 IAW CRJ 900 SRM 51-42-06-001-001-A01

Part: STRINGER — CORRODED (UNKNOWN) · airframe 20,313 hrs · 16,335 cycles

STRINGER 26L CORRODED BETWEEN FS319 - FS333 LOCATED AND DRILLED NEW STRINGER P/N: SH670-31634-1S AT STR 26L FROM FS 280 TO FS 333 IAW CRJ-900 SRM 51-40-11-001-001-A01. INSTALLED STGR 26L FROM FS 280-333 IAW CRJ 900 SRM 51-42-06-001-001-A01

Part: SPLICE — CORRODED (UNKNOWN) · airframe 20,313 hrs · 16,335 cycles

STRINGER 26L SPLICE CORRODED AT FS333 LOCATED AND DRILLED NEW STRINGER SPLICE PN: SH670-32429-3 IAW CRJ 900 SRM 51-40-11-001-001-A01 INSTALLED STGR26L SPLICE AT FS 333 IAW CRJ 900 SRM 51-42-06-001-001-A01

Part: STRINGER — CORRODED (UNKNOWN) · airframe 20,313 hrs · 16,335 cycles

STRINGER 26L CORRODED BETWEEN FS333 - FS349 LOCATED AND DRILLED NEW STRINGER 26L PN: SH670-31372-3S IAW CRJ 900 SRM 51-40-11-001-001-A01 INSTALLED STGR 26L FROM FS333-364 IAW CRJ 900 SRM 51-42-06-001-001-A01

Part: STRINGER — CORRODED (UNKNOWN) · airframe 20,313 hrs · 16,335 cycles

STRINGER 26R CORRODED BETWEEN FS333 - FS364 LOCATED AND DRILLED NEW STGR 26R PN: SH670-31372-4S IAW CRJ 900 SRM 51-40-11-001-001-A01 INSTALLED STGR 26R FROM FS 333-364 IAW CRJ 900 SRM 51-42-06-001-001-A01

Part: STRINGER SPLICE — CORRODED (UNKNOWN) · airframe 20,313 hrs · 16,335 cycles

STRINGER SPLICE AT 25R FS333 CORRODED. LOCATED AND DRILLED NEW STRINGER SPLICE 25R FS333 P/N: SH670-32429-4S IAW CRJ-900 SRM 51-40-11-001-001-A01.INSTALLED NEW STRINGER SPLICE P/N SH670-32429-4S AT STR 25R FS 333, IAW CRJ-900 SRM 51-42-06-001-001-A01.

Part: LONGERON — CORRODED (UNKNOWN) · airframe 20,313 hrs · 16,335 cycles

STGR 25R LONGERON IS CORRODED BETWEEN FS 333 AND FS 364 LOCATED AND DRILLED NEW STR 25R LONGERON P/N SH670-32103-4 BETWEEN FS 333 TO FS 364 IAW CRJ-900 SRM 51-40-11-001-001-A01 INSTALLED NEW STR 25R LONGERON P/N: SH670-32103-4 BETWEEN FS333 TO FS364, IAW CRJ-900 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.

Part: ANGLE — CRACKED (UNKNOWN) · airframe 20,313 hrs · 16,335 cycles

FS 280 FLOORBEAM TO CROSSBEAM ATTACH BRACKET LBL 9.0 CRACKED ON OUTBOARD SIDE. LOCATED AND DRILLED SERVICEABLE LBL9 O/B ANGLE P/N: CC670-34269-7 IAW CRJ 900 SRM 51-40-11-001-001-A01. REF. BAR-CODE IDENTIFIER HR00304343 FOR INSTALL OF REMOVED 2EA BRACKET (I/B & O/B SIDE) ON FS280 FLOOR BEAM TO CROSSBEAM LBL9.

Part: HANDLE — CRACKED (UNKNOWN) · airframe 20,313 hrs · 16,335 cycles

PAX DOOR OUTER HANDLE CHAFED AND FLAP HANDLE CRACKED. REPLACED PAX DOOR OUTER HANDLE FLAP IAW CRJ900 SRM TASK 51-42-06-001-001-A01

Part: FLOORBEAM — CORRODED (UNKNOWN) · airframe 20,313 hrs · 16,335 cycles

FS 280 CORROSION NOTED AT APPROXIMATELY RBL 15.0 BETWEEN ANGLE (CAP) AND TOP OF CROSSBEAM, AROUND NUTPLATE HOLE FOR CABIN FLOORBOARD LOCATED AND DRILLED RH FS 280 CROSSBEAM PN: CC670-34094-2 IAW CRJ 900 SRM 51-40-11-001-001-A01. INSTALLED O/B JO-BOLT FASTENERS AND I/B POST FASTENERS IAW CRJ-900 SRM 51-42-06-001-001-A01 51-42-22-001-001-A01. INSTALLED NEW SERVICEABLE RH CAP ANGLE PN: CC670-34096-2 AT FS 280 IAW CRJ 900 SRM 51-42-06-001-001-A01 AND 51-42-13-001-001-A01. LOCATED AND DRILLED NEW SERVICEABLE RH CAP ANGLE PN: CC670-34096-2 AT FS 280 IAW CRJ 900 SRM 51-40-11-001-001-A01. INSTALLED TITANIUM STRIP AT FS 280 BETWEEN RBL 9 TO LBL 9 IAW CRJ 900 SRM 51-42-13-001-001-A01

Part: ANGLE — CRACKED (UNKNOWN) · airframe 20,313 hrs · 16,335 cycles

FS 280 FLOORBEAM TO CROSSBEAM ATTACH BRACKET RBL 9.0 IS CRACKED. LOCATED AND DRILLED SERVICEABLE RBL9 O/B ANGLE P/N: CC670-34269-8 IAW CRJ 900 SRM 51-40-11-001-001-A01. REF. BAR-CODE IDENTIFIER HR00304343 FOR INSTALL OF REMOVED 2EA BRACKET (I/B & O/B SIDE) ON FS280 FLOOR BEAM TO CROSSBEAM RBL9.

Part: SEAT TRACK — CORRODED (FRMS 573-661) · airframe 20,313 hrs · 16,335 cycles

SIDE SEAT RAIL AT STGR 15L IS CORRODED BETWEEN FS 573 AND FS 661+16. REMOVED SIDE SEAT RAIL AT LEVEL STR15L BETWEEN FS 573 TO FS 661+16. INSTALLED A SERVICEABLE SIDE SEAT RAIL AT STGR 15L BETWEEN FS 573 TO FS 661+16 IAW MHIRJ REO 670-53-00-587 DATED 2023-02-08 REV -C.

Part: FLOOR SUPPORT — CORRODED · airframe 20,313 hrs · 16,335 cycles

CRAWLWAY FLOOR PANEL SUPPORT ANGLE CORRODED AT FS280 BETWEEN STGR26L AND STGR26R INSTALLED NEW CRAWLWAY FLOOR PANEL SUPPORT ANGLE IAW CRJ 900 SRM 51-42-06-001-001-A01 AND CRJ 900 SRM 51-42-21-001-001-A01, P/N CC670-34256-3.

Part: INTERCOSTAL — CORRODED (UNKNOWN) · airframe 20,313 hrs · 16,335 cycles

MAIN AVIONICS BAY DOOR SURROUND STRUCTURE, INTERCOSTAL BETWEEN FS349 AND FS364 AT STGR 27L CORRODED. LOCATED AND DRILLED NEW INTERCOSTAL STR 27L BETWEEN FS 349 TO FS 364, P/N SH670-32075-3S, IAW CRJ-900 SRM 51-40-11-001-001-A01 INSTALLED NEW INTERCOSTAL P/N SH670-32075-3S STR 27L BETWEEN FS 349 TO FS 364, IAW CRJ-900 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01

Part: INTERCOSTAL — CORRODED (UNKNOWN) · airframe 20,313 hrs · 16,335 cycles

MAIN AVIONICS BAY DOOR SURROUND STRUCTURE, INTERCOSTAL BETWEEN FS349 AND FS364 AT STGR 27R CORRODED. LOCATED AND DRILLED NEW INTERCOSTAL P/N SH670-32075-4S, STR27R BETWEEN FS 349 AND FS 364 IAW CRJ-900 SRM 51-40-11-001-001-A01 INSTALLED NEW INTERCOSTAL P/N SH670-32075-4S, STR 27R BETWEEN FS349 AND FS364, IAW CRJ-900 SRM 51-42-06-001-001-A01 & 51-42-21-001-001-A01

Part: SPACER — CORRODED · airframe 20,313 hrs · 16,335 cycles

CROSSBEAM SPACER IS CORRODED AT FS 333, ON THE O/B SIDE OF THE RBL 9 BEAM. REMOVED THE RBL9 O/B CROSSBEAM SPACER AT FS 333 TO FULLY REMOVE ALL CORROSION IAW CRJ-900 51-42-06-001-001-A01. LOCATED, DRILLED AND INSTALLED NEW SERVICEABLE SPACER P/N SH670-32167-3 AT FS 333 AND RBL 9 O/B LOCATION IAW CRJ 900 SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01.

Part: FRAME — CORRODED (UNKNOWN) · airframe 20,313 hrs · 16,335 cycles

FRAME AT FS310 CORRODED BETWEEN STGR25R AND STGR25L. REMOVED CORROSION FROM FRAME 310 STGR 25L - STGR 25R IAW CRJ900 SRM 53-00-06-201-005-A01

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 20,313 hrs · 16,335 cycles

SIDE SEAT RAIL AT STGR 15R IS CORRODED BETWEEN FS 744 AND FS 761. REMOVED AND REPLACED SEAT RAIL IAW CRJ900 AMM TASKS 53-00-49-000-801-A13 AND 53-00-49-400-801-A13. FABRICATED PART IAW MHIRJ REO 670-53-00-587 REV C DATED 2023-02-08 REPAIR (B).

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 20,313 hrs · 16,335 cycles

SIDE SEAT RAIL AT STGR 15R IS CORRODED BETWEEN FS 680 AND FS 722. REMOVED AND REPLACED SEAT RAIL IAW CRJ900 AMM TASKS 53-00-49-000-801-A13 AND 53-00-49-400-801-A13. FABRICATED PART IAW MHIRJ REO 670-53-00-587 REV C DATED 2023-02-08 REPAIR (B).

Part: SEAT TRACK — CORRODED (UNKNOWN) · airframe 20,313 hrs · 16,335 cycles

RBL 9 SEAT RAIL IS CORRODED BETWEEN FS 581 AND FS 661+32. INSTALLED RBL 9 SEAT RAIL (P/N SH69033404-1) BETWEEN FS 581 TO 661+32 IAW CRJ900 AMM 53-00-49-400-801-A07.

Part: SEAT TRACK — CORRODED (UNKNOWN) · airframe 20,313 hrs · 16,335 cycles

LBL 9 SEAT RAIL IS CORRODED BETWEEN FS 581 AND FS 661+32. FABRICATED LBL 9 SEAT RAIL BETWEEN FS 581- FS 661+32 (P/N SH690-33404-1) FROM SEAT TRACK EXTRUSION P/N 20276-288-0-0, PO# W77329 IAW MHIRJ REO 670-53-00-589 REV (-C) DATED 2023-02-08 REPAIR (B). LOCATED AND DRILLED IAW CRJ-900 SRM 51-40-11-001-001-A01 INSTALLED LBL 9 SEAT RAIL (P/N 670-53-00-589-1) BETWEEN FS 581 TO FS 661+32 IAW CRJ900 AMM 53-00-49-400-801-A13.

Part: SEAT TRACK — CORRODED · airframe 20,313 hrs · 16,335 cycles

LBL 9 SEAT RAIL IS CORRODED BETWEEN FS 661+32 AND FS 693. LBL 9 SEAT RAIL BETWEEN FS 661+32 AND FS 693 IS CORRODED OUT OF LIMITS IAW CRJ900 SRM 53-31-49-101-001-A02. REMOVED, FABBED AND REPLACED SEAT RAIL IAW CRJ900 MHIRJ REO 670-53-00-589 REV-C DATED 2023-02-08. PRIME, PAINTED, INK STAMPED, P/N 670-53-00-589-1, AND CIC, LBL 9 SEAT RAIL BETWEEN FS 661+32 AND FS 693 IAW MHIRJ REO 670-53-00-589 REV-C DATED 2023-02-08 PART NUMBER FOR EXTRUSION 20276-288-0-0A

Part: FLOOR PANEL — CRACKED (UNKNOWN) · airframe 20,313 hrs · 16,335 cycles

IN FORWARD EQUIPMENT BAY FLOOR, R/H F.S. 193.00 IS CRACKED. REPAIRED RH ELECTRICAL BAY FLOOR AT FS 193.00 IAW CRJ900 SRM REPAIR 53-11-43-201-001-A01 RHS REPAIR TYPE 2.

Part: BRACKET — CRACKED (UNKNOWN) · airframe 20,313 hrs · 16,335 cycles

IN AFT EQUIPMENT BAY, OUTBOARD OF LH ACM, BRACKET FOR ACM TOP WATER LINE BROKEN. LOCATED, DRILLED AND INSTALL NEW BRACKET ASSY P/N MM670-97111-005 ON STGR 9L BTWN FS 1144.0 & FS 1154.48, IAW CRJ900 SRM 51-40-11-001-001-A01 & 51-42-06-001-001-A01

Part: ANGLE — CORRODED (UNKNOWN) · airframe 20,313 hrs · 16,335 cycles

GALLEY SERVICE DOOR SILL ANGLE AND ANGLES FOR LOWER DOOR FITTINGS ARE CORRODED. LOCATED AND DRILLED NEW SILL ANGLE P/N SH670-31996-3S, AT LOWER SERVICE DOOR, IAW CRJ-900 SRM 51-40-11-001-001-A01. INSTALLED GALLEY SERVICE DOOR SILL ANGLE P/N: SH670-31996-3S IAW CRJ-900 SRM 51-42-06-001-001-A01

Part: BRACKET — CRACKED (UNKNOWN) · airframe 20,313 hrs · 16,335 cycles

IN AFT EQUIPMENT BAY, OUTBOARD OF LH ACM, BRACKET FOR ACM TOP WATER LINE BROKEN. RECEIVED, LOCATED, DRILLED AND DEBURRED, NEW BRACKET ASSY P/N MM670-97107-001, ON STRG 7L BTWN FS 1162 TO FS 1181, IAW CRJ900 SRM 51-40-11-001-001-A01 INSTALLED NEW BRACKET ASSY P/N MM670-97107-001 ON STGR 7L BTWN FS 1162 TO FS 1181, IAW CRJ900 SRM 51-42-06-001-001-A01

Part: ANGLE — CORRODED (UNKNOWN) · airframe 20,313 hrs · 16,335 cycles

RH MLG, UNDER BLOW OUT PANEL 642BZ, BRACKET CORRODED REMOVED UNSERVICEABLE RH MLG BLOW OUT PANEL 642BZ BRACKET (P/N: CC670-10338-2) IAW CRJ-900 SRM 51-42-21-001-001-A01. INSTALLED NEW RH MLG BLOW OUT PANEL 642BZ BRACKET (P/N: CC670-10338-2) IAW CRJ-900 SRM 51-42-21-001-001-A01.

Part: BRACKET — CORRODED (UNKNOWN) · airframe 20,313 hrs · 16,335 cycles

UNDER BLOW OUT PANEL 542AZ HYDRAULICS BRACKET FOR IB BK, LG EX, LG RET CORRODED IN LH MLG WHEEL WELL. UPON FURTHER INVESTIGATION, FOUND LH MLG BLOW OUT PANEL 542AZ BRACKET (P/N: CC670-10337-1) TO BE OUT OF LIMITS DUE TO NO ALLOWABLE LIMITS PROVIDED IN THE SRM. REPLACEMENT REQUIRED. RECEIVED NEW SERVICEABLE BRACKET P/N CC670-10337-1 LOCATED AND DRILLED IAW CRJ900 SRM 51-40-11-001-001-A01. DISCONNECTED AND INSTALLED 5EA HYDRAULIC LINES IAW CRJ900 AMM 20-22-00-910-801-A01. REMOVED AND INSTALLED NEW BRACKET IAW CRJ900 SRM 51-41-02-001-001-A01. PERFORMED EXTERNAL LEAK CHECK OF THE HYDRAULIC LINES ON BRACKET P/N CC670-10337-1, LEAK CHECK GOOD AT THIS TIME IAW CRJ 900 AMM 29-10-00-790-802-A01. PERFORMED BLEEDING OF THE BRAKES IAW CRJ 900 AMM 32-43-00-870-801-A01.

Part: BRACKET — CRACKED (UNKNOWN) · airframe 20,313 hrs · 16,335 cycles

NOSE HYDRAULICS COMPARTMENT UPPER BRAKE ACCUMULATOR FWD BRACKET (ATTACHED TO INTERCOSTAL) IS CRACKED INSTALLED NEW SERVICEABLE UPPER FWD BRACKET OF NOSE HYDRAULICS COMPARTMENT P/N: CC670-75604-2 IAW CRJ-900 STM 51-42-21-001-001-A01

Part: ACCESS PANEL — CHAFED (RT WING) · airframe 20,313 hrs · 16,335 cycles

R/H WING ACCESS PANEL 699AB HAS CHAFFING. LOCATED AND DRILLED 1EA NEW SERVICEABLE ACCESS PANEL IAW CRJ-900 SRM 51-40-11-001-001-A01. P/N REMOVED: 601R13440-2 NEW P/N: 601R13440-2

Part: WARNING LIGHT — FALSE ACTIVATION (DOOR) · airframe 17,725 hrs · 14,249 cycles

RH AFT EXIT DOOR CAUTION IN FLIGHT. CYCLED THE EMER EXIT DOOR AFT IAW CRJ 900 AMM 52-21-00. MESSAGE CLEARED. ACFT OK FOR SERVICE.

Part: DOOR — WARNING MESSAGE (LT EMERGENCY) · airframe 17,649 hrs · 14,193 cycles

FWD LEFT EMERGENCY EXIT DOOR SHOW CAUTION MSG.AS PER TELCOM DEFERRED FWD LEFT EMERGENCY EXIT DOOR INDICATION OCN 70048929 PER MEL 52-70-03 CAT C

Part: COVER — UNSECURE (EMERGENCY EXIT) · airframe 17,017 hrs · 13,687 cycles

EMERGENCY DOOR HANDLE COVER AT 12A NEEDS TO BE SECURED. RESECURED EMERGENCY DOOR HANDLE COVER AT 12A. OK FOR SERVICE.

Part: WARNING MESSAGE — ILLUMINATED (EMERGENCY EXIT) · airframe 15,976 hrs · 12,853 cycles

AFT RIGHT WING EMERGENCY EXIT CAUTION.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 15,545 hrs · 12,523 cycles

DAMAGE TO AFT FUSELAGE SKIN BETWEEN FS1031-FS1051 AND STGR20R-STGR27. ACCOMPLISHED REPAIR TO THE AFT FUSELAGE SKIN BETWEEN FS1031-FS1051 AND STGR20R-STGR27 BY CUTTING THE DAMAGED AREA, FABRICATING AND INSTALLING REPAIR PARTS IAW REO 690-53-61-740, REV - DATED 2018-02-01, NDT PERFORMED.

Part: CROSSBEAM — CRACKED (FUSELAGE) · airframe 15,545 hrs · 12,523 cycles

LT & RT FS 280 CROSSBEAMS CRACKED. REMOVED AND REPLACED LT & RT FS 280 CROSSBEAMS IAW SRM 51-25-16, 51-21-11, 51-40-11, 51-42-06, 51-42-13, 51-42-21, 51-42-22 AMM 20-70-00.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 15,545 hrs · 12,523 cycles

TCAS CHANNEL IN MAIN AVIONICS BAY HAS SIGNS OF CORROSION. REMOVED AND REPLACED TCAS CHANNEL IN MAIN AVIONICS BAY IAW SRM 51-42-06 AND 51-42-21.

Part: BRACKET — CRACKED (ASSIST MOTOR) · airframe 15,545 hrs · 12,523 cycles

PASSENGER DOOR POWER ASSIST MOTOR FWD BRACKET CRACKED. REMOVED AND REPLACED THE BRACKET IAW SRM 51-42-06, 51-40-11, AND AMM 20-70-00

Part: MOUNT BRACKET — CRACKED (PAX DOOR) · airframe 15,545 hrs · 12,523 cycles

PAX DOOR STRUT MOUNTING BRACKET CRACKED. REMOVED AND REPLACED PAX DOOR STRUT MOUNTING BRACKET IAW AMM 20-70-00, SRM 51-42-05, SRM 51-40-11.

Part: LIGHT — INOPERATIVE (CABIN FLOOR) · airframe 15,530 hrs · 12,511 cycles

FORWARD AISLE FLOOR EMERGENCY LIGHT INOPERATIVE.

Part: WARNING MESSAGE — FALSE ACTIVATION (SLAT SYSTEM) · airframe 15,312 hrs · 12,328 cycles

SLATS FAIL CAUTION MSG IN FLIGHT.PERFORM OPS CHECK OF SLAT SUBSYSTEM IAW CRJ 900 AMM 27-81-00 OPS CHECK GOOD AT THIS TIME.

Part: WARNING MESSAGE — FALSE ACTIVATION (SLAT SYS) · airframe 13,252 hrs · 10,730 cycles

SLAT FAIL CAUTION MESSAGE IN FLIGHT. PERFORMED SLAT/FLAP OPERATIONAL CHECK IAW CRJ900 AMM 27-50-00. NO MESSAGE AT THIS TIME. OK FOR SERVICE.

Part: SKIN — DENTED (FUSELAGE) · airframe 13,178 hrs · 10,675 cycles

FUSELAGE SKIN DENTED FWD OF FS280 AND AFT OF FS265, BETWEEN STGR 26R AND 25R. CORRECTIVE ACTION: REPAIRED DENT IN FUSELAGE SKIN IAW BOMBARDIER REO 690-53-11-946, DATED 2017-01-18.

Part: GLOWSTRIP — MISSING (CABIN) · airframe 12,865 hrs · 10,463 cycles

ESCAPE PATH STRIP IN FRONT OF FWD CLOSET MISSING, 4" IN GALLEY AREA AND 5" MISSING AT 12C/D. DEFERRED PHOTO LUMINESCENT FLOOR TAPE 4" IN GALLEY AREA AND 5" AT SEAT 12 C/D ON DMI 70011960 PER MEL 33-51-01G-3F CAT C.

Part: SLAT SYSTEM — MALFUNCTIONED · airframe 12,625 hrs · 10,298 cycles

SLATS FAILED ON APPROACH, CLEARED INHIBITS, PERFORMED OPS CHECK OF SLAT/FLAP SYSTEM IAW AMM 27-52-00, OPS CHECKED GOOD.

Part: LIGHT — MISSING · airframe 12,451 hrs · 10,160 cycles

EMERGENCY LIGHT MISSING IN GALLEY.

Part: LIGHT — MISSING (CABIN) · airframe 12,451 hrs · 10,160 cycles

EMERGENCY LIGHT MISSING AT ROW 7 LEFT SIDE AND ROW 9 RIGHT SIDE.

Part: TIRE — FAILED (RT MLG) · airframe 12,085 hrs · 9,889 cycles

RIGHT OTBD TIRE FAILED. REMOVED & REPLACED THE TIRE IAW AMM 32-41-01.