N362GT

Part: SKIN — CHAFED (TE FLAP) · airframe 46,841 hrs · 47,469 cycles

AIRCRAFT GROUNDED. LT WING OUTBD MID FLAP LOWER SKIN IS CHAFED NEAR INBD FLAP TRACK CUTOUT. REPLACED LT OUTBD MID FLAP. INSTALL AND ADJUSTMENTS TO BE ACCOMPLISHED ON CARD 8017551.

Part: SKIN — DENTED (RT WING TE FLAP) · airframe 46,841 hrs · 47,469 cycles

RH INBD MID FLAP DENTED, 18.0" FROM EXHAUST GATE AND 5.5" FROM TE.

Part: SKIN — CHAFED (LT WING TE FLAP) · airframe 46,841 hrs · 47,469 cycles

LH WING OB MID FLAP LOWER SKIN IS CHAFFED NEAR IB FLAP TRACK CUTOUT. FLAP REPLACED WITH P/N 65C26320-17, S/N 1953.

Part: SKIN — DELAMINATED (LT ELEVATOR) · airframe 46,841 hrs · 47,469 cycles

LH ELEVATOR DAMAGED AT STA 121.59

Part: FLAP — DENTED (RT WING) · airframe 46,841 hrs · 47,469 cycles

AIRCRAFT GROUNDED. RT INBD MID FLAP DENTED, 18Ï¿½ IN FROM EXHAUST GATE AND 5 Ï¿½ INCHES FROM THE T/E. OK TO INSTALL. REPAIRED R/H INBD MID FLAP IAW SRM 51-70-102R-2. SEE ATTACHED SHOP FOR WORK ACCOMPLISHED.

Part: SKIN — DENTED (RT WING TE FLAP) · airframe 46,841 hrs · 47,469 cycles

RH IB AFT FLAP DENTED 10.0" IN FROM EXHAUST GATE 1.5" FROM TE.

Part: SLIDE — DEFECTIVE (R1 DOOR) · airframe 46,841 hrs · 47,469 cycles

AIRCRAFT GROUNDED. RT EMERGENCY FWD ESCAPE SLIDE FAILED TO DEPLOY CORRECTLY. REMOVED AND REPLACED R1 EMERGENCY SLIDE IAW AMM 25-61-35.

Part: SLIDE — NO TEST · airframe 46,841 hrs · 47,469 cycles

RIGHT EMERGENCY FWD ESCAPE SLIDE FAILED TO DEPLOY CORRECTLY. REPLACED WITH P/N 10166-107, S/N PAB630.

Part: LIGHT — INOPERATIVE (EVAC SLIDE) · airframe 46,841 hrs · 47,469 cycles

AIRCRAFT GROUNDED. LT FWD EMERGENCY SLIDE WHEN DEPLOYED DID NOT TRIGGER THE INTEGRAL LIGHTS. INSTALLED LT FWD DOOR SLIDE IAW AMM 25-61-35 TOOL# 346 DUE 23 MAR 19.

Part: SLIDE — NO TEST (LEFT) · airframe 46,841 hrs · 47,469 cycles

LH FWD EMERGENCY SLIDE WHEN DEPLOYED DID NOT TRIGGER THE INTEGRAL LIGHTS. REPLACED WITH P/N 101660-107, S/N PAB626.

Part: BATTERY — DISCHARGED (CABIN) · airframe 46,841 hrs · 47,469 cycles

AIRCRAFT GROUNDED. ALL BATTERY PACKS FOR THE EMERGENCY LIGHTS FAILED DURING THE TESTS. REF TASK 3500444 2000-0105. REMOVED AND REPLACED ALL BATTERIES FOR THE EMERGENCY LIGHTING. REF TASK 33-51-51-962-015. OPS CHECKS PERFORMED - PASSED. REF TASK STEP 3E (4).

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 46,841 hrs · 47,469 cycles

BATTERY PACKS FOR THE EMERGENCY LIGHTS FAILED DURING THE TEST. PACKS REPLACED WITH P/N 2013-1A (9EA).

Part: FLAP — GOUGED (LT WING) · airframe 46,841 hrs · 47,469 cycles

AIRCRAFT GROUNDED. FLAP 2 BY STATION 235 HAS DEEP GOUGE BY MOUNT BRACKET LT INBD FORE FLAP. SEE EA180602 IR FOR REPAIR PROCESS AND SHOP FOR ANY ADDITIONAL WORK STEPS COMPLETED.

Part: STRUCTURE — GOUGED (FLAP NR 2) · airframe 46,841 hrs · 47,469 cycles

FLAP 2 BY STATION 235 HAS DEEP GOUGE BY MOUNT BRACKET L/H INBD FORE FLAP.

Part: STRAP — NOT REPORTED (FUSELAGE) · airframe 46,841 hrs · 47,469 cycles

AIRCRAFT GROUNDED. LOCATE AND FABRICATE AND DRILL UP, TREAT AND PRIME AND TOPCOAT NEW REPAIR STRAPS FOR SEAT TRACK LINK ASSEMBLIES. FABRICATED AND INSTALLED STRAPS ON CABIN DECK STA 520 TO 540 RBL 24.75, RBL 45.5, LBL 24.75, LBL 45.5 IAW EA180595 & EO 3753A156.

Part: FLOOR SUPPORT — CORRODED (BS 787-807) · corrosion level 2 · airframe 46,841 hrs · 47,469 cycles

CORROSION AT FLOOR SUPPORT IN SEVERAL AREAS ON UPPER FLANGE, JUST FWD OF CARGO DOOR ENTRANCE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 46,841 hrs · 47,469 cycles

AIRCRAFT GROUNDED. CORROSION AT FLOOR SUPPORT IN SEVERAL AREAS ON UPPER JUST FWD OF CARGO DOOR ENTRANCE. REMOVED AND REPLACED FLOOR SUPPORT ON RT B2 787-807 PER 737-400-51-40-02.

Part: SHEAR WEB — CORRODED (BS 986.5-1016) · corrosion level 2 · airframe 46,841 hrs · 47,469 cycles

CORROSION FOUND ON SHEAR WEB JUST INBD AND AFT OF R2 DOOR AT BS 986.5 TO 1016.

Part: SHEAR WEB — CORRODED (FUSELAGE) · airframe 46,841 hrs · 47,469 cycles

AIRCRAFT GROUNDED. CORROSION FOUND. SHEAR WEB JUST INBD AFT OF R2 DOOR AT BS 986.5 Ï¿½ BS 1016. REMOVED AND REPLACED WEB ON INBD AFT R2 DOOR AT BS 986.5 BS1016 IAW SRM 51-40-02.