N330PQ

Part: DOOR — OUT OF ADJUST (ZONE 800) · airframe 22,555 hrs · 17,388 cycles

RH FWD AND AFT OVERWING EMERGENCY EXIT DOORS DO NOT CLEAR THE OVERHEAD BIN. ADJUSTED RODS OF THE OVERHEAD STORAGE BIN 11DC-13DC IAW CRJ 900 AMM 25-23-00-820-803-A01. CLEARANCE OF THE RH FWD AND AFT EMERGENCY EXIT DOORS GOOD AT THIS TIME.

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 22,555 hrs · 17,388 cycles

LH FS 280 CROSS BEAM HAS CORROSION PRESENT FOUND L/H F.S. 280 CROSS BEAM TO BE COMPLETELY CORRODED THROUGH AND OUT OF LIMITS IAW CRJ-900 SRM 53-00-00-101-001-A01. REMOVED CORRODED BEAM AND INSTALLED NEW SERVICEABLE L/H F.S. 280 CROSS BEAM P/N CC670-34094JP-1 IAW CRJ-900 SRM 51-42-06/13/21/22-001-001-A01.

Part: LUG — CORRODED (ZONE 800) · airframe 22,555 hrs · 17,388 cycles

LH FWD EMERGENCY EXIT DOOR SN: SB1509 IS CRACKED AT UPPER AFT LUG REPAIRED LH FWD EMERGENCY EXIT DOOR IAW ENDEAVOR EA CRJ952-17747 REV IR DATED 17747 REV IR DATED 11/19/24

Part: DOOR FRAME — CRACKED (ZONE 200) · airframe 22,555 hrs · 17,388 cycles

RH AFT EMERGENCY EXIT DOOR SN: SB1508 IS CRACKED AT UPPER AFT LUG REPAIRED RH AFT EMERGENCY EXIT DOOR IAW ENDEAVOR EA CRJ952-17749 REV IR DATED 11/19/24.

Part: LUG — CORRODED (ZONE 800) · airframe 22,555 hrs · 17,388 cycles

RH FWD EMERGENCY EXIT DOOR SN: SB1510 IS CRACKED AT UPPER AFT LUG REPAIRED RH FWD EMERGENCY EXIT DOOR IAW ENDEAVOR EA CRJ952-17748 REV IR DATED 11/19/24

Part: HINGE — CHAFED (ZONE 200) · airframe 22,555 hrs · 17,388 cycles

FOUND LUG ON PAX DOOR SIDE HINGE TO BE CHAFFED REMOVED CHAFE ON AFT LUG AT PAX DOOR IAW CRJ900 SRM 51-12-00-001-001-A01. MATERIAL REMAINING 0.87', FOUND TO BE OUT LIMITS IAW CRJ900 SRM 52-11-01-201-007-A01. COMPLIED WITH STEPS 3 AND 4 A-P IAW CRJ 900 SRM 52-11-- 01-201-002-A01 COMPLIED WITH STEP 4 Q THROUGH U IAW CRJ 900 SRM 52-11-01-201-002-A01 INSTALLED PAX DOOR FWD AND AFT HANDRAILS IAW CRJ900 AMM 52-11-05-400-801/801 A01 INSTALLED PAX DOOR MID STEP IAW CRJ900 SRM 51-42-21-001-001-A01

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 22,555 hrs · 17,388 cycles

RH FS 280 CROSS BEAM HAS CORROSION PRESENT FOUND R/H F.S. 280 CROSS BEAM TO BE COMPLETELY CORRODED THROUGH AND OUT OF LIMITS IAW CRJ-900 SRM 53-00-00-101-001-A01. REMOVED CORRODED BEAM AND INSTALLED NEW SERVICEABLE L/H F.S. 280 CROSS BEAM P/N CC670-34094JP-1 IAW CRJ-900 SRM 51-42-06/13/21/22-001-001-A01.

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 22,555 hrs · 17,388 cycles

R/H COCKPIT FLOORBEAM AT FS 280 RBL 9 IS CRACKED REPAIRED R/H COCKPIT FLOOR BEAM BY COMPLYING WITH ALL REPAIR STEPS PROVIDED IN MHIRJ REO 690-53-11-1891 REV-- DATED 2024-11-19.

Part: FLOORBEAM — CRACKED (ZONE 200) · airframe 22,555 hrs · 17,388 cycles

L/H COCKPIT FLOORBEAM AT FS 280 LBL 9 IS CRACKED REPAIRED L/H COCKPIT FLOORBEAM AT LBL 9 BY COMPLYING WITH ALL REPAIR STEPS PROVIDED IN MHIRJ REO 690-53-11-1890 REV-- DATED 2024-11-19.

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 22,555 hrs · 17,388 cycles

"RH FLOOR SILL AT FS280 HAS CORROSION. REMOVED DAMAGE FROM RH FLOOR SILL AT FS 280 IAW CRJ 900 SRM 51-12-00-001-001-A01 NOMINAL THICKNESS OF THE FLOOR SILL FROM FS 280 TO FS 319 IS .050"", REMOVED .036"", MRT IS .014. DAMAGE IS OUT OF ALLOWABLE LIMITS IAW CRJ900 SRM 53-00-45-201-001-A01. UPON FURTHER INVESTIGATION FOUND RH FLOOR SILL TO REQUIRE REPLACEMENT BETWEEN FS 280 - FS 319.70. INSTALLED RH FLOOR SILL BETWEEN FS 280 - FS 319.70, 2 EA LIGHTNING DIVERTER MOUNT BRACKETS, SPLICE ANGLE FROM FLOOR SILL BETWEEN FS 295 - FS 310, ATTACH ANGLE (P/N: SH 670-31503-1) AND MOUNTING BRACKET (SH670-41526-5), BLANKING PLATE ( P/N: SH670-32187-1), DUCT MOUNT, PLATE (P/N SH670-33548-5), DOUBLER (P/N:SH670-32197-1) IAW CRJ 900 SRM 51-42-06-001-001-A01 , 51-42-13-001-001-A01 , 51-42-21-001-001-A01. RECEIVED, LOCATED, DRILLED AND INSTALLED SERVICEABLE RING DOUBLER (P/N: SH670-31524-1) IAW CRJ 900 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01. RECONNECTED HR19P2, HR19P1 AND INSTALLED HOSE CLAMP ON HEATED DRAIN TUBE RH FLOOR SILL BETWEEN FS 310 - FS 31970 IAW CRJ 900 SRM 51-41-04-001-001-A01. ROUTED AND SECURED WIRES FOR CANNON PLUGS MT76P1 AND PL104P1 BETWEEN FS 280 - FS 310 BY INSTALLING ZIP TIES. OPERATIONAL TEST OF THE OBSERVER AUDIO PANEL PREFORMED IAW CRJ 900 AMM TASK 23-51-06-710-801 (CONFIG A01) OPERATIONAL TEST OF THE OBSERVER AUDIO PANEL GOOD IAW CRJ 900 AMM TASK 23-51-06-710-801 (CONFIG A01). OPS TEST GOOD IAW CRJ-900 AMM 27-35-05-710-801-A01. INSTALLED GS376 AND GS326 IAW CRJ 900 AMM 51-80-00-910-805 (A01) ROUTED AND SECURED WIRE BUNDLES BETWEEN FS 295 - FS 310 AND STGR 14R - 17R BY INSTALLING ZIP TIES. RESTORED SURFACE FINISH ON EXTERNAL FASTENERS @ STGR 17R BETWEEN FS 280 - FS 319.70 IAW CRJ 900 SRM 51-25-06-001-001-A01, 51-25-16-001-001-A01."

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 18,323 hrs · 13,847 cycles

RH AFT EXTERIOR EMERGENCY LIGHT INOP. REMOVED AND REPLACED RH AFT EXTERIOR EMERGENCY LAMP IAW AMM 33-51-15, OP'S CHECK GOOD. PN OFF/ON: 8GH005123-06

Part: DOUBLER — CORRODED (TCAS ANTENNA) · airframe 15,401 hrs · 11,408 cycles

INTERNAL STRUCTURE LOWER TCAS ANTENNA DOUBLER AT FS 300.00, STR 27 AREA CORRODED. REMOVED TCAS ANTENNA DOUBLER AND DRAME CLEET, LOCATED DRILLED, INSTALLED AND SEALED DOUBLER AND FRAME CLEET IAW CRJ 900 SRM 51-42-06-001-001-A01, 51-40-11-001-001-A01, 51-42-21-001-001-A01, 51-21-11-001-001-A01 REMOVED LOWER TCAS ANTENNA IAW CRJ 900 AMM 34-43-07-000-801-A02 SEE JOB 1 OP:285 FOR INSTALL AND SEAL. REMOVED AND REPLACED 1 HILITE ON STR 27 IAW CRJ 900 SRM 51-42-06-001-001-A01.

Part: ANGLE — CORRODED (PAX DOOR SILL) · airframe 15,401 hrs · 11,408 cycles

PAX DOOR UPPER SILL ANGLE CORRODED AT FS 319.00 TO FS 333.00. REMOVED,LOCATED,DRILLED AND INSTALLED PAX DOOR UPPER LH FLOOR SILL ANGLES IAW CRJ 900 SRM 51-40-11-001-001-A01, 51-42-20-000-A01, 51-42-06-001-001-A01, REMOVED/INSTALLED PROX SENSOR PX25 IAW CRJ 900 AMM 52-70-04-000/400-802-A02 OPS CHECK GOOD.

Part: ANGLE — CORRODED (DOOR SILL) · airframe 15,401 hrs · 11,408 cycles

PAX DOOR UPPER SILL ANGLE CORRODED AT FS 319.00 TO FS 333.00. REMOVED,LOCATED,DRILLED AND INSTALLED PAX DOOR UPPER LH FLOOR SILL ANGLES IAW CRJ 900 SRM 51-40-11-001-001-A01, 51-42-20-000-A01, 51-42-06-001-001-A01, REMOVED/INSTALLED PROX SENSOR PX25 IAW CRJ 900 AMM 52-70-04-000/400-802-A02 OPS CHECK GOOD.

Part: DIAPHRAGM — CRACKED (LT MLG) · airframe 15,401 hrs · 11,408 cycles

L/H MLG FAIRING DIAPHRAGM ASSEMBLY HAS APPROX 3"" CRACK IN FLANGE. REMOVED & REPLACED LH MLG DIAPHRAGM ASSY P/N:CC670-39205-5 IAW CRJ 900 SRM 51-41-02-001-001-A01 & 51-42-16-001-001-A01.

Part: HINGE — CORRODED (DOOR STAIR PANEL) · airframe 15,401 hrs · 11,408 cycles

UPPER STAIR PANEL ASSEMBLY HINGE HAS CORROSION. REPLACED CORRODED PAX DOOR UPPER STAIR PANEL ASSEMBLY HINGE WITH NEW SERVICEABLE HINGE P/N CC670-31981-3.

Part: RETAINER — BENT (FWD CARGO DOOR) · airframe 15,401 hrs · 11,408 cycles

FWD BAGGAGE BAY DOOR LOWER SEAL RETAINER IS BENT IN SEVERAL PLACES. REMOVED & REPLACED FWD BAGGAGE DOOR LOWER SEAL RETAINER IAW CRJ-900 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01 AND AMM 52-35-07-400-802-A02.

Part: SEAT TRACK — GOUGED (BS 661-677) · airframe 15,401 hrs · 11,408 cycles

RH SIDE SEAT RAIL AND SUPPORT STRUCTURE HAVE SCRATCHES, GOUGESBETWEEN FS 661+32 AND FS 661+46. REMOVE AND REPLACED SIDE SEAT RAIL AND BLENDED AREA ON SUPPORT STRUCTURE IAW CRJ900 AMM AND SRM 53-00-49-000-801-A12, 53-00-49-400-801-A12, 53-31-51-101-001-A02.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 15,401 hrs · 11,408 cycles

UPON REMOVAL OF ANGLE AT FS 280, FOUND CORROSION ON LH AT RH CROSSBEAM BETWEEN LBL 12 TO RBL 12. REMOVED AND REPLACED LH AND RH FS 280 CROSSBEAMS IAW CRJ900 SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01 AND 51-42-22-001-001-A01.

Part: FITTING — CORRODED (BS 349) · airframe 15,401 hrs · 11,408 cycles

PAX DOOR INTERNAL SURROUND STRUCTURE AT FS 349.00 WL 72.50 FITTING IS CORRODED. REMOVED/INSTALLED NEW FITTING IAW CRJ900 SRM 51-42-21-001-001-A01.

Part: ANGLE — CORRODED (SRVCE DOOR SILL) · airframe 15,401 hrs · 11,408 cycles

SERVICE DOOR SILL ANGLE BRACKET CORRODED AT FS 311.00 TO FS 347.00. REMOVED AND REPLACED SERVICE DOOR MOUNTING ANGLE IAW CRJ 900 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.

Part: FLOOR SUPPORT — CORRODED (BS 320) · airframe 15,401 hrs · 11,408 cycles

FLOOR SUPPORT STRUCTURE ANGLE AT GALLEY DOOR FS 320.00 NUTPLATE MISSING. REMOVED AND REPLACED NEW SERVICEABLE NUTPLATE AT FS 320.00 ON SERVICES DOOR (GALLEY) IAW CRJ 900 SRM 51-42-06-001-001-A01.

Part: ENGINE — CONTAMINATED (RIGHT) · airframe 8,878 hrs · 6,158 cycles

ODOR OF SMOKE IN CABIN AFTER TAKEOFF, THE ODOR WAS LIKE BURNED RUBBER IN FOR AND AFT OF CABIN. PERFORMED INSPECTION IAW FIM 21-22-00, AND DETERMINED ABNORMAL ODOR IN CABIN TO BE FROM RT ENGINE COMPRESSOR WASH PERFORMED THE PREVIOUS NIGHT. RISE ENGINE IAW AMM 72-00-00, NO ABNORMAL ODOR NOTED. ARICRAFT OK FOR SERVICE.

Part: WEB — CRACKED (PASSENGER DOOR) · airframe 7,657 hrs · 5,306 cycles

PAX DOOR FWD WEB IS CRACKED AT LOWER PART OF RISER. REPAIRED THE DOOR FWD WEB AT LOWER PART OF RISER IAW SRM 52-11-04.

Part: STIFFENER — CRACKED (ACCESS PANEL) · airframe 7,657 hrs · 5,306 cycles

ACCESS PANEL 195DL HAS A CRACKED STIFFENER. REMOVED AND REPLACED IAW SRM 51-42-13.

Part: BULKHEAD — CORRODED (BS 280) · airframe 7,657 hrs · 5,306 cycles

LEFT BS 280 BULKHEAD IS CORRODED, LBL10.5, BOTTOM CORNER. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS. REPAIRED IAW SRM 51-21-06, PG. 7, AND 53-11-10, PG 201.

Part: HOUSING — CRACKED (DOOR HANDLE) · airframe 7,657 hrs · 5,306 cycles

AVIONICS COMPARTMENT DOOR HANDLE HOUSING IS CRACKED. REMOVED AND REPLACED THE HANDLE HOUSING ASSEMBLY IAW AMM 52-42-03-000-801, AND AMM 52-42-03-400-801. OPS CHECKED GOOD IAW AMM 52-42-03-00-710-801.

Part: SMOKE DETECTOR — INOPERATIVE (FWD LAVATORY) · airframe 7,463 hrs · 5,161 cycles

DURING AN OPS CHECK OF THE FWD LAVATORY SMOKE DETECTION SYS. FOUND SMOKE DETECTOR INOPERATIVE. .R & R THE FWD LAVATORY SMOKE DETECTOR IAW AMM 26-10. THE SMOKE DETECTOR OPS CHECKED GOOD.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 3,224 hrs · 2,197 cycles

FORWARD ENTRANCE EMER FLASHLIGHT INOPERATIVE & STRAP BROKEN. R & R FWD ENTRANCE FLASHLIGHT & HOLDER IAW AMM 25-61-02. OPERATIONS CHECKED GOOD IAW AMM 25-61-00.

Part: FIRE BOTTLE — LEAKING · airframe 2,466 hrs · 1,683 cycles

WATER EXTINGUISHER IS LEAKING. R & R WATER FIRE EXTINGUISHER IAW TASK FCR 26001.