N878RW

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 34,911 hrs · 26,662 cycles

SPRAY PATTERN ON WINDSHIELD SUGGESTS BIRD STRIKE JUST LEFT OF CENTERLINE OF RADOME/SUPPORT STRUCTURE. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. PERFORMED BIRD STRIKE INSPECTION, NO DAMAGE FOUND.

Part: GCU — FAULTED (ZONE 100) · airframe 33,082 hrs · 25,055 cycles

CENTER EBAY FAN FAIL. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. R&R GCU 1.

Part: BEAM — CRACKED (NLG) · airframe 31,348 hrs · 23,857 cycles

(MAJOR) NOSE LANDING GEAR I BEAM REINFORCEMENT. DURING AIRCRAFT FULL SCALE FATIGUE TEST, CRACKS WERE DETECTED IN THE I-SHAPED BEAM TO WHICH THE NOSE LANDING GEAR MANEUVER ACTUATOR FITTING IS CONNECTED, IN THE UPPER PART OF THE NLG BAY. REINFORCEMENTS TO THE I-SHAPED BEAM AND IMPROVEMENTS TO THE RELATED ATTACHING POINTS ARE BEING IMPLEMENTED

Part: BUSHING — CRACKED · airframe 31,348 hrs · 23,857 cycles

RH IB TRUST REVERSER FWD MOUNTING LUG BUSHING CRACKED. REMOVED AND REPLACED RH IB THRUST REVERSER FWD MOUNT LUG BUSHING IAW CMM 78-30-02

Part: ANGLE — CRACKED · airframe 31,348 hrs · 23,857 cycles

FWD FUSELAGE CRACK FOUND ON ANGLE SUPPORT AT FR 12 BL 0. REPLACED ANGLE SUPPORT @ FR 12 BL 0 IAW SRM 51-41-01

Part: SUPPORT BRACKET — CORRODED (ZONE 100) · corrosion level 2 · airframe 31,348 hrs · 23,857 cycles

WHILE AC WAS IN FOR HVY CK FOUND CENTER FUSELAGE 3 FLOOR BOARD SUPPORT BRACKET AT FR 86 LBL FOUND CORRODED. REPLACED SUPPORT BRACKET PN 170-66797-001 IAW SRM 51-41-01 FOR DETAILS OF WORK PERFORMED SEE AAR NRC # 4500928-1000-0058. AC REMAINS IN YQU FOR COMPLETION.

Part: SUPPORT BRACKET — CORRODED (ZONE 100) · corrosion level 2

WHILE AC WAS IN FOR HVY CK FOUND CENTER FUSELAGE 3 FLOOR BOARD SUPPORT BRACKET AT FR 86 RBL 29 FOUND CORRODED. REPLACED SUPPORT BRACKET PN 170-66797-001 IAW SRM 51-41-01 FOR DETAILS OF WORK PERFORMED SEE AAR NRC# 4500928-1000-0059. AC REMAINS IN YQG FOR COMPLETION.

Part: STAB SYSTEM — CRACKED (ZONE 300) · airframe 31,348 hrs · 23,857 cycles

LH HORIZONTAL STAB LEADING EDGE, CRACK FOUND ON RIB 4. L/H HORIZONTAL STAB LEADING EDGE, RIB HAS BEEN REPAIRED I/A/W SRM 55-10-07 ROI. HFEC C/W NO FAULTS FOUND. SEE AWS AND NDT REPAIR TWO34095-1 FOR DETAILS

Part: DOUBLER — CORRODED (ZONE 200) · airframe 31,348 hrs · 23,857 cycles

FORWARD FUSELAGE, SHEAR DOUBLER AT FR 16 LBL 12 FOUND CORRODED. FWD FUSELAGE, SHEAR DOUBLER AT FR 16 LBL 12 HAS BEEN REPAIRED I/A/W SRM 53-10-10-A006. DOUBLER WITHIN LIMITS. HFEC C/W NO FAULTS FOUND, SEE AWS AND NDT REPAIR TWO 34095-G FOR DETAILS AND WORK PERFORMED. P/N 170-12118-001. MAX REMOVED 0.004" P.S.E 53-10-027

Part: BONDING PLATE — CORRODED (ZONE 100) · corrosion level 2 · airframe 31,348 hrs · 23,857 cycles

WHILE AC WAS IN FOR HVY CK FOUND AFT WTBF FOUND BONDING PLATE CORRODED ON ACCESS PANEL 195CR, 195FR AND 195DR REPAIRED IAW SRM 51-73-00 REV 48. FOR DETAILS OF WORK PERFORMED SEE NRC# 4500928-1000-0028. AC REMAINS IN YQG FOR COMPLETION.

Part: HINGE — CORRODED (ZONE 100) · corrosion level 2 · airframe 31,348 hrs · 23,857 cycles

WHILE AC WAS IN FOR HVY CK FOUND CF3 LAV WASTE ACCESS DOOR HINGE PN 170-85090-003 HAS CORROSION. REPLACED DOOR HINGE IAW SRM 51-41-02 SEE AAR NRC# 4500928-1000-0042 FOR DETAILS OF WORK PERFORMED. AC REMAINS IN YQG FOR COMPLETION.

Part: SIGN — CRACKED (EMERGENCY LIGHT) · airframe 30,792 hrs · 23,438 cycles

EXIT SIGN NEAR FWD FA JUMPSEAT FRAME IS CRACKED, PARTIALLY MISSING. R&R L1 DOOR EXIT INDICATOR SIGN IAW AMM 33-50-15.

Part: DOUBLER — CRACKED (LT WING SLT TRK) · airframe 31,348 hrs · 23,857 cycles

L/H WING, #5 SLAT TRACK CUT OUT DOUBLER FOUND CRACK. L/H WING, #5 SLAT TRACK CUT OUT DOUBLER REPLACED WITH MADE REPAIR PART I/A/W DRW# 170-31084-001 INSTALLED I/A/W SRM 51-41-02

Part: UNKNOWN — ODOR (CABIN) · airframe 30,081 hrs · 22,896 cycles

BURNING SMELL IS STILL COMING FROM FORWARD GALLEY. RAN BOTH PACKS FOR A WHILE. INSPECTED FWD GALLEY AREA COFFEE MAKERS, FWD EBAY. NO SIGN OF SMOKE NOR SMELL. PACKS OPS CHECK GOOD IAW AMM 21-00-00.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHTS) · airframe 28,776 hrs · 21,782 cycles

#3 EMERGENCY LIGHT INOP. SECURED THE CONNECTOR ON OVERHEAD PANEL IAW SWPM 20-52-00.

Part: SPLICE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 27,818 hrs · 21,049 cycles

WHILE IN HEAVY CHECK - CORROSION ON LT BEAM SPLICE AT FR 90. REMOVED AND REPLACED LT BEAM SPLICE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 27,818 hrs · 21,049 cycles

WHILE IN HEAVY CHECK - CORROSION STRUCTURAL CENTER FUSELAGE III WET AREA 53-23 LT BEAM Y=-10.748" AS MARKED NEXT TO RIVET. REPLACED CENTER FUSELAGE III WET AREA 53-23 LT BEAM Y=-10.748", REF SRM 51-40-08.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 27,818 hrs · 21,049 cycles

WHILE IN HEAVY CHECK - FWD WET AREA 9 HOLE DOUBLER P/N 170-12118-001 IS CORRODED AS MARKED. REPLACED FWD WET AREA 9 HOLE DOUBLER P/N 170-12118-001 REF SRM 51-40-08.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 27,818 hrs · 21,049 cycles

WHILE IN HEAVY CHECK - FWD WET AREA LT SILL P/N 170-05662-001 IS CORRODED AS MARKED. REPLACED SILL.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 27,818 hrs · 21,049 cycles

WHILE IN HEAVY CHECK - FWD WET AREA LT SIDE DOUBLER P/N 170-07311-001 IS CORRODED AS MARKED. REMOVED AND REPLACED DOUBLER REF SRM 51-40-08, 51-40-02.

Part: GUSSET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 27,818 hrs · 21,049 cycles

WHILE IN HEAVY CHECK - CORROSION ON RT INTERCOSTAL GUSSET PLATE AT FR 90. REMOVED AND REPLACED RT INTERCOSTAL GUSSET PLATE.

Part: SHEAR PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 27,818 hrs · 21,049 cycles

WHILE IN HEAVY CHECK - CORROSION ON RT SHEAR PANEL FR 87-88. REMOVED AND REPLACED RT SHEAR PANEL FR 87-88.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 27,818 hrs · 21,049 cycles

WHILE IN HEAVY CHECK - FWD WET AREA RT TRACK P/N 170-03263-001 IS CORRODED AS MARKED. REMOVED & REPLACED FWD WET AREA RT TRACK REF SRM 51-40-08.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 27,818 hrs · 21,049 cycles

WHILE IN HEAVY CHECK - CORROSION ON LT FLOORBEAM BETWEEN FR 90-90A AS MARKED. REMOVED AND REPLACED LT FLOORBEAM.

Part: SHEAR PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 27,818 hrs · 21,049 cycles

WHILE IN HEAVY CHECK - CORROSION ON LT SHEAR PANEL FR 87-88. LOCATED, DRILLED AND INSTALLED NEW LT SHEAR PANEL FR 87-88. REF SRM 51-40-02, 51-21-01, 51-40-08.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 27,818 hrs · 21,049 cycles

WHILE IN HEAVY CHECK - CORROSION ON RT FLOORBEAM BETWEEN FR 87-89 AS MARKED. REMOVED AND REPLACED RT FLOORBEAM P/N 170-65669-004 REF SRM 51-40-08, 51-23-04, 51-40-08.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 27,818 hrs · 21,049 cycles

WHILE IN HEAVY CHECK - FWD WET AREA RT SILL P/N 170-05663-003 (3 HOLE DOUBLER) IS CORRODED AS MARKED. REMOVED FWD WET AREA RT SILL P/N 170-05663-003 (3 HOLE DOUBLER) REF SRM 51-40-08.

Part: THRESHOLD — CORRODED (FUSELAGE) · corrosion level 2 · airframe 27,818 hrs · 21,049 cycles

MAJOR: CORROSION FOUND AT FASTENER HOLES AND GIRT BAR FITTING EDGE ON FWD/AFT R1 DOOR LOWER BEAM THRESHOLD. REMOVED AND REPLACED R1 DOOR THRESHOLD PN: 170-03599-005 REF 51-40-08. SEE W/O H6663 SN 379 FOR WORK DETAILS

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 27,818 hrs · 21,049 cycles

FWD WET AREA LT TRACK P/N 170-03264-001 IS CORRODED AS MARKED. REMOVED AND REPLACED SEAT TRACK PN: 170-03264-001 REF EMB SRM 51-40-01, 51-41-02, 51-43-03. SEE W/O H6663 SN 325 FOR WORK DETAILS