N302KH

Part: NONE — NONE · airframe 53,545 hrs · 58,957 cycles

FLOOR SUPPORT CRACKED AT BS 665L. CORRECTIVE ACTION IN WORK, AC STILL DOWN AT THIS TIME.

Part: NOT REPORTED — NOT REPORTED · airframe 52,696 hrs · 57,515 cycles

CRACK FOUND AT BS 867 + 10", STR 3R. 3" LENGTH. CORRECTIVE ACTION PENDING AMOC SIGNOFF.

Part: NONE — NONE · airframe 52,459 hrs · 57,329 cycles

FOUND DENT BELOW SERVICE DOOR AFT OF LAV PANEL. CERTIFIED AVIATION SERVICES REPAIRED DAMAGE IAW SRM 53-00-01 REPAIR 31 DETAIL 19 PER CAS WO ALOHA302.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,287 hrs · 56,264 cycles

DURING SCHEDULED INSPECTION AT HAECO LAKE CITY, FLORIDA FOUND FUSELAGE SKIN FWD OF FWD GALLEY DOOR ADJACENT TO UPPER DOOR HINGE CUTOUT 3RD HOLE UP FROM S-10R AT BS 291 HAS CRACK INDICATION IN BEAR STRAP LAYER. S/O 660004 N/R 44997

Part: FLOORBEAM — CORRODED (BS 907) · corrosion level 2 · airframe 51,287 hrs · 56,264 cycles

DURING SCHEDULED INSPECTION AT HAECO LAKE CITY, FLORIDA FOUND FLOOR BEAM UNDER MAIN CABIN HAS EVIDENCE OF CORROSION AT BS 907, LBL 70.53 TO RBL 70.53. S/O 660004 N/R 44835.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 51,287 hrs · 56,264 cycles

DURING SCHEDULED INSPECTION AT HAECO LAKE CITY, FLORIDA FOUND NUMEROUS BULBS INOPERATIVE IN THE EMERGENCY LIGHTS OVER THE FLIGHT DECK DOOR AND THE L1 DOOR. S/O 660004 N/R 44152

Part: SKIN — CRACKED (RT WING SLAT) · airframe 51,287 hrs · 56,264 cycles

DURING SCHEDULED INSPECTION, FOUND R/H WING #6 SLAT O/B END OF LOWER T/E HAS CRACK ALONG FASTENER ROW OF 3 EACH FASTENERS. S/O 660004 N/R 45081.

Part: FITTING — CRACKED (LT WING SPOILER) · airframe 51,287 hrs · 56,264 cycles

DURING SCHEDULED INSPECTION AT HAECO LAKE CITY, FLORIDA FOUND L/H WING SPOILER #5 GROUND SPOILER FITTING HAS A CRACKED LUG. S/O 660004 N/R 45085

Part: SEAT TRACK — GOUGED (BS 540-706) · corrosion level 2 · airframe 51,287 hrs · 56,264 cycles

DURING SCHEDULED INSPECTION AT HAECO LAKE CITY, FLORIDA FOUND MAIN CABIN SEAT TRACK LBL 45.50 BS 540 - 706 O/B FLANGE HAS AREAS WITH GOUGES AND CORROSION. S/O 660004 N/R 44658

Part: FLOORBEAM — CORRODED (MAIN CABIN) · corrosion level 2 · airframe 51,287 hrs · 56,264 cycles

DURING SCHEDULED INSPECTION AT HAECO, LAKE CITY, FLORIDA FOUND MAIN CABIN UNDER FLOOR BEAM HAS EVIDENCE OF CORROSION AT BS 827, LBL 70.53 - RBL 70.53. S/O 660004 N/R 44833

Part: FITTING — CRACKED (LT MAIN LG) · airframe 51,287 hrs · 56,264 cycles

DURING SCHEDULED INSPECTION AT HAECO LAKE CITY, FLORIDA FOUND LMLG SUPPORT BEAM AT RSS 224.14 FITTING FASTENER HOLE #12 HAS REJECTABLE INDICATION IN WEB LAYER. S/O 660004 N/R 44918

Part: SUPPORT BEAM — CRACKED (LT MLG) · airframe 51,287 hrs · 56,264 cycles

DURING SCHEDULED INSPECTION AT HAECO LAKE CITY, FLORIDA FOUND LMLG SUPPORT BEAM AT RSS 224.14 FITTING FASTENER HOLE #5 HAS CRACK INDICATION IN CHORD LAYER. S/O 660004 N/R 44913

Part: SUPPORT BEAM — CRACKED (LT MLG) · airframe 51,287 hrs · 56,264 cycles

DURING SCHEDULED INSPECTION AT HAECO LAKE CITY, FLORIDA FOUND LMLG SUPPORT BEAM AT RSS 224.14 FITTING FASTENER HOLE #10 HAS CRACK INDICATION IN WEB LAYER. S/O 660004 N/R 44917

Part: PAN — CRACKED (CARGO DOORWAY) · airframe 51,287 hrs · 56,264 cycles

DURING SCHEDULED INSPECTION AT HAECO LAKE CITY, FLORIDA FOUND THE I/B LOWER ATTACH HOLE IN DOOR PAN WAS CRACKED THROUGH. S/O 660004 N/R 45026

Part: SUPPORT BEAM — CRACKED (LT MLG) · airframe 51,287 hrs · 56,264 cycles

DURING SCHEDULED INSPECTION AT HAECO LAKE CITY, FLORIDA FOUND LMLG SUPPORT BEAM AT RSS 224.14 FITTING FASTENER HOLE #4 HAS CRACK INDICATION IN CHORD LAYER. S/O 660004 N/R 44912

Part: SUPPORT BEAM — CRACKED (LT MLG) · airframe 51,287 hrs · 56,264 cycles

DURING SCHEDULED INSPECTION AT HAECO LAKE CITY, FLORIDA FOUND LMLG SUPPORT BEAM AT RSS 224.14 FITTING FASTENER HOLE #7 HAS CRACK INDICATION IN WEB LAYER. S/O 660004 N/R 44914

Part: SUPPORT BEAM — CRACKED (LT MLG) · airframe 51,287 hrs · 56,264 cycles

DURING SCHEDULED INSPECTION AT HAECO LAKE CITY, FLORIDA FOUND LMLG SUPPORT BEAM AT RSS 224.14 FITTING FASTENER HOLE #3 HAS CRACK INDICATION IN WEB LAYER. S/O 660004 N/R 44911

Part: SUPPORT BEAM — CRACKED (LT MLG) · airframe 51,287 hrs · 56,264 cycles

DURING SCHEDULED INSPECTION AT HAECO LAKE CITY, FLORIDA FOUND LMLG SUPPORT BEAM AT RSS 224.14 FITTING FASTENER HOLE #8 HAS CRACK INDICATION IN CHORD LAYER. S/O 660004 N/R 44915

Part: SUPPORT BEAM — CRACKED (LT MLG) · airframe 51,287 hrs · 56,264 cycles

DURING SCHEDULED INSPECTION AT HAECO LAKE CITY, FLORIDA FOUND LMLG SUPPORT BEAM AT RSS 224.14 FITTING FASTENER HOLE #9 HAS CRACK INDICATION IN FWD FITTING LAYER. S/O 660004 N/R 44916

Part: SUPPORT BEAM — CRACKED (LT MLG) · airframe 51,287 hrs · 56,264 cycles

DURING SCHEDULED INSPECTION AT HAECO LAKE CITY, FLORIDA FOUND LMLG SUPPORT BEAM AT RSS 224.14 FITTING FASTENER HOLE #2 HAS CRACK INDICATION IN CHORD LAYER. S/O 660004 N/R 44910

Part: FRAME — DENTED (BS 500) · airframe 51,287 hrs · 56,264 cycles

DURING SCHEDULED INSPECTION AT HAECO LAKE CITY, FLORIDA FOUND MAIN CABIN R/H FRAME HAS DENT 4 - 5" ABOVE FLOOR LEVEL AT BS 500. S/O 660004 N/R 44351

Part: FRAME — DENTED (BS 480) · airframe 51,287 hrs · 56,264 cycles

DURING SCHEDULED INSPECTION AT HAECO LAKE CITY, FLORIDA FOUND MAIN CABIN R/H FRAME HAS DENT 4 - 5" ABOVE FLOOR LEVEL BS 480. S/O 660004 N/R 44350

Part: SEAT TRACK — GOUGED (MAIN CABIN) · airframe 51,287 hrs · 56,264 cycles

DURING SCHEDULED INSPECTION AT HAECO LAKE CITY, FLORIDA FOUND MAIN CABIN SEAT TRACK UPPER LOBES GOUGED AT BS 400, LBL 7053. S/O 660004 N/R 44755

Part: ATTACH FITTING — CORRODED (RT WING SKIN) · corrosion level 2 · airframe 51,287 hrs · 56,264 cycles

DURING SCHEDULED INSPECTION AT HAECO, LAKE CITY, FLORIDA FOUND EXFOLIATED CORROSION ON ATTACH FITTING OF R/H UNDER WING SKIN PANEL O/B OF LANDING GEAR. S/O 660004 N/R 45078

Part: FLOORBEAM — CRACKED (MAIN CABIN) · airframe 51,287 hrs · 56,264 cycles

DURING SCHEDULED INSPECTION AT HAECO LAKE CITY, FLORIDA FOUND A CRACK INDICATION IN FLOOR BEAM LAYER OF MAIN CABIN, FLOOR BEAM LBL 24.82, HOLE AT BS 660 4TH OPEN HOLE. S/O 660004 N/R 44935

Part: FLOORBEAM — CORRODED (MAIN CABIN) · corrosion level 2 · airframe 51,287 hrs · 56,264 cycles

DURING SCHEDULED INSPECTION AT HAECO, LAKE CITY, FLORIDA FOUND EXFOLIATED CORROSION IN MAIN CABIN FLOOR STRUCTURE LATERAL CROSSBEAM AT BS 767, RBL 35.00. S/O 660004 N/R 44993

Part: SEAT TRACK — GOUGED (MAIN CABIN) · airframe 51,287 hrs · 56,264 cycles

DURING SCHEDULED INSPECTION AT HAECO LAKE CITY, FLORIDA FOUND MAIN CABIN SEAT TRACK HAS VIBRATORY GOUGES BS 520-560 LBL 45.50. S/O 660004 N/R 44754

Part: FLOOR SUPPORT — CRACKED (FWD CARGO) · airframe 51,287 hrs · 56,264 cycles

DURING SCHEDULED INSPECTION AT HAECO LAKE CITY, FLORIDA FOUND FORWARD CARGO COMPARTMENT, MAIN DECK, BL 0 FLOOR BEAM, BETWEEN BS 500A - 500B, SIX (6) EACH SCREW HOLES HAVE CORROSION AND CRACKS. S/O 660004 N/R 44449

Part: FLOORBEAM — CORRODED (MAIN CABIN) · corrosion level 2 · airframe 51,287 hrs · 56,264 cycles

DURING SCHEDULED INSPECTION AT HAECO LAKE CITY, FLORIDA FOUND MAIN CABIN UNDER FLOOR BEAM HAS EVIDENCE OF CORROSION AT BS 887 LBL 70.53 - RBL 70.53. S/O 660004 N/R 44834

Part: FRAME — DENTED (BS 460) · airframe 51,287 hrs · 56,264 cycles

DURING SCHEDULED INSPECTION AT HAECO LAKE CITY, FLORIDA FOUND MAIN CABIN R/H FRAME HAS A DENT 4-5" ABOVE FLOOR LEVEL AT BS 460. S/O 660004 N/R 44349

Part: FITTING — DAMAGED (RT MLG) · airframe 41,287 hrs · 56,264 cycles

DURING SCHEDULED INSPECTION AT HAECO LAKE CITY, FLORIDA FOUND RMLG SUPPORT BEAM AT RSS 224.14 FITTING FASTENERS HOLE #5 HAS REJECTABLE INDICATION IN AFT FITTING LAYER. S/O 660004 N/R 44921

Part: FITTING — DAMAGED (RT MLG) · airframe 41,287 hrs · 56,264 cycles

DURING SCHEDULED INSPECTION AT HAECO LAKE CITY, FLORIDA FOUND RMLG SUPPORT BEAM AT RSS 224.14 FITTING FASTENER HOLE #8 HAS REJECTABLE INDICATION IN ALL LAYERS. S/O 660004 N/R 44920

Part: SEAT TRACK — WORN (MAIN CABIN) · airframe 51,287 hrs · 56,264 cycles

DURING SCHEDULED INSPECTION AT HAECO LAKE CITY, FLORIDA FOUND MAIN CABIN SEAT TRACK HAS WEAR MARKS AT STA. 380-480 LBL 45.50. S/O 660004 N/R 44756

Part: SEAT TRACK — CORRODED (BS 727B-927) · corrosion level 2 · airframe 41,287 hrs · 56,264 cycles

DURING SCHEDULED INSPECTION AT HAECO, LAKE CITY, FLORIDA FOUND MAIN CABIN SEAT TRACK AND TRACK FLANGES HAVE VIBRATION GOUGES AND EVIDENCE OF CORROSION STA. 727B - 927 BBL 0.0. S/O 660004 N/R 44799

Part: SEAT TRACK — GOUGED (MAIN CABIN) · corrosion level 2 · airframe 41,287 hrs · 56,264 cycles

DURING SCHEDULED INSPECTION AT HAECO LAKE CITY, FLORIDA FOUND MAIN CABIN SEAT TRACK AND TRACK FLANGES HAVE CHATTER MARKS AND EVIDENCE OF CORROSION AT BS 727-727B LBL 45.50. SO 660004 N/R 44660

Part: SEAT TRACK — CORRODED (MAIN CABIN) · corrosion level 2 · airframe 41,287 hrs · 56,264 cycles

DURING SCHEDULED INSPECTION AT HAECO LAKE CITY, FLORIDA FOUND MAIN CABIN SEAT TRACK HAS CHATTER MARKS AND EVIDENCE OF CORROSION STA. 867-887 RBL 46.50. S/O 660004 N/R 44841

Part: SUPPORT BEAM — CRACKED (RT MLG) · airframe 51,287 hrs · 56,264 cycles

DURING SCHEDULED INSPECTION AT HAECO LAKE CITY, FLORIDA FOUND RMLG SUPPORT BEAM AT RSS 224.14 FITTING FASTENER HOLE #11 HAS A CRACK INDICATION IN FWD FITTING LAYER. S/O 660004 N/R 44925

Part: SEAT TRACK — CORRODED (BS 727-727B) · corrosion level 2 · airframe 41,287 hrs · 56,264 cycles

DURING SCHEDULED INSPECTION AT HAECO LAKE CITY, FLORIDA FOUND MAIN CABIN SEAT TRACK AND TRACK FLANGES HAVE CHATTER MARKS AND EVIDENCE OF CORROSION STA. 727-727B, RBL 45.50. S/O 660004 N/R 44796

Part: SEAT TRACK — CORRODED (BS 727B-887) · corrosion level 2 · airframe 41,287 hrs · 56,264 cycles

DURING SCHEDULED INSPECTION AT HAECO LAKE CITY, FLORIDA FOUND MAIN CABIN SEAT TRACK AND TRACK FLANGES HAVE CHATTER MARKS AND EVIDENCE OF CORROSION STA. 727B-887 LBL 45.50. S/O 660004 N/R 44800

Part: SEAT TRACK — CORRODED (BS 727B-947) · corrosion level 2 · airframe 41,287 hrs · 56,264 cycles

DURING SCHEDULED INSPECTION AT HAECO LAKE CITY, FLORIDA FOUND MAIN CABIN SEAT TRACK AND TRACK FLANGES HAVE CHATTER MARKS AND EVIDENCE OF CORROSION STA. 727B-947 RBL 24.50. S/O 660004 N/R 44803

Part: SEAT TRACK — CORRODED (MAIN CABIN) · corrosion level 2 · airframe 41,287 hrs · 56,264 cycles

DURING SCHEDULED INSPECTION AT HAECO LAKE CITY, FLORIDA FOUND MAIN CABIN SEAT TRACK HAS VIBRATION GOUGES AND EVIDENCE OF CORROSION STA. 887-1016 RBL 45.40. S/O 660004 N/R 44849

Part: SEAT TRACK — CORRODED (BS 727-727B) · corrosion level 2 · airframe 41,287 hrs · 56,264 cycles

DURING SCHEDULED INSPECTION AT HAECO LAKE CITY, FLORIDA FOUND MAIN CABIN SEAT TRACK AND TRACK FLANGES HAVE CHATTER MARKS AND EVIDENCE OF CORROSION STA. 727-727B RBL.24.50. S/O 660004 N/R 44797

Part: SUPPORT BEAM — DAMAGED (RT MLG) · airframe 51,287 hrs · 56,264 cycles

DURING SCHEDULED INSPECTION AT HAECO LAKE CITY, FLORIDA FOUND RMLG SUPPORT BEAM AT RSS 224.14 FITTING FASTENER HOLE #9 HAS REJECTABLE INDICATION IN FWD FITTING LAYER. S/O 660004 N/R 44927

Part: SEAT TRACK — CORRODED (BS 500B-550A) · corrosion level 2 · airframe 51,287 hrs · 56,264 cycles

DURING SCHEDULED INSPECTION AT HAECO LAKE CITY, FLORIDA FOUND FWD CARGO COMPARTMENT MAIN DECK LBL 24.5 SEAT TRACK BETWEEN FS 500A-500B HAS A SCREW HOLE WITH CORROSION. S/O 660004 N/R 44446

Part: FITTING — DAMAGED (RT MLG) · airframe 41,287 hrs · 56,264 cycles

DURING SCHEDULED INSPECTION AT HAECO LAKE CITY, FLORIDA FOUND RMLG SUPPORT BEAM AT RSS 224.14 FITTING FASTENER HOLE #3 HAS REJECTABLE INDICATION IN FWD AND AFT FITTING LAYER.

Part: SUPPORT BEAM — DAMAGED (RT MLG) · airframe 41,287 hrs · 56,264 cycles

DURING SCHEDULED INSPECTION AT HAECO LAKE CITY, FLORIDA FOUND RMLG SUPPORT BEAM AT RSS 224.14 FITTING FASTENER HOLE #1 HAS REJECTABLE INDICATION IN FWD AND AFT FITTING LAYER. S/O 660004 N/R 44924

Part: SUPPORT BEAM — DAMAGED (RT MLG) · airframe 51,287 hrs · 56,264 cycles

DURING SCHEDULED INSPECTION AT HAECO LAKE CITY, FLORIDA FOUND RMLG SUPPORT BEAM AT RSS 224.14 FITTING FASTENER HOLE #10 HAS REJECTABLE INDICATION IN AFT FITTING LAYER. S/O 660004 N/R 44926

Part: FRAME — DENTED (BS 440) · airframe 51,287 hrs · 56,264 cycles

DURING SCHEDULED INSPECTION AT HAECO LAKE CITY, FLORIDA FOUND MAIN CABIN R/H FRAME HAS A DENT 4 - 5" ABOVE FLOOR LEVEL BS 440. S/O 660004 N/R 44348

Part: FITTING — DAMAGED (RT MLG) · airframe 41,287 hrs · 56,264 cycles

DURING SCHEDULED INSPECTION AT HAECO LAKE CITY, FLORIDA FOUND RMLG SUPPORT BEAM AT RSS 224.14 FITTING FASTENER HOLE #2 HAS REJECTABLE INDICATION IN CHORD LAYER AND CRACK INDICATION IN WEB LAYER. S/O 660004 N/R 44923

Part: WEB — CRACKED (AFT CABIN R/H) · airframe 41,287 hrs · 56,264 cycles

DURING SCHEDULED INSPECTION AT HAECO LAKE CITY, FLORIDA FOUND AFT CABIN AT STA. 986.5 WL 208 R/H WEB CRACKED . S/O 660004 N/R 44494

Part: ATTACH ANGLE — WORN (R/H WING ROOT) · airframe 41,287 hrs · 56,264 cycles

DURING SCHEDULED INSPECTION AT HAECO LAKE CITY, FLORIDA FOUND R/H WING, AFT UPPER T/E, WING ROOT PANEL AT 71.24, LOWER ATTACH ANGLE AFT HOLE IS WORN OUT. S/O 660004 N/R 45017

Part: GUSSET — CRACKED (MLG W/W FWD BULK) · airframe 41,287 hrs · 56,264 cycles

DURING SCHEDULED INSPECTION AT HAECO, LAKE CITY, FLORIDA FOUND CRACK INDICATION IN BOTH LAYERS OF MLG W/W FWD BULKHEAD RBL6.15 GUSSET HOLE. S/O 660004, N/R 44951

Part: SUPPORT ANGLE — CORRODED (L/H W/W AFT WALL) · corrosion level 2 · airframe 41,287 hrs · 56,264 cycles

DURING SCHEDULED INSPECTION AT HAECO LAKE CITY, FLORIDA FOUND CORROSION ON BELLY PANEL SUPPORT ANGLE OF L/H W/H AFT WALL STA. 727. S/O 660004, N/R 44334.

Part: THRESHOLD — CORRODED (R/H CARGO DOOR) · corrosion level 2 · airframe 41,287 hrs · 56,264 cycles

DURING SCHEDULED INSPECTION AT HAECO LAKE CITY, FLORIDA FOUND CRACK IN DOOR JAMB THRESHOLD OF AFT CARGO R/H. S/O 660004, N/R 44722

Part: SUPPORT ANGLE — CORRODED (R/H W/W AFT WALL) · corrosion level 2 · airframe 41,287 hrs · 56,264 cycles

DURING SCHEDULED INSPECTION AT HAECO LAKE CITY, FLORIDA FOUND CORRODED BELLY PANEL SUPPORT ANGLE AT R/H W/W AFT WALL STA. 727. S/O 660004, N/R 44329

Part: STRINGER — CRACKED (ZONE 200) · airframe 41,287 hrs · 56,264 cycles

DURING SCHEDULED INSPECTION, FOUND STRINGER ANGLE CRACKED IN THE RADIUS AT MAIN CABIN R/H SIDE, FS 291.3, STR. 13A-R. S/O 660004, N/R 44805

Part: FRAME — DENTED (FUSELAGE) · airframe 41,287 hrs · 56,264 cycles

DURING SCHEDULED INSPECTION, FOUND MAIN CABIN R/H FRAME HAS A DENT 4-5" INCHES ABOVE FLOOR LEVEL AT STA. 500A. S/O 660004, N/R 44352

Part: SKIN — DAMAGED (PAX DOOR) · airframe 41,287 hrs · 56,264 cycles

DURING SCHEDULED INSPECTION, FOUND BLEND IN DOOR SKIN UPPER CORNER AT LT FWD CABIN DOOR. S/O 660004 N/R 44380.

Part: ATTACH ANGLE — CORRODED (FWD CRGO FLOOR) · corrosion level 2 · airframe 41,287 hrs · 56,264 cycles

DURING SCHEDULED INSPECTION, FOUND FWD CARGO COMPARTMENT, BILGE AREA, LBL 21.8 FLOOR BEAM, FS 500D BULKHEAD ATTACH ANGLE HAS CORROSION. S/O 660004 N/R 44444.

Part: ATTACH ANGLE — CORRODED (FWD CARGO FLOOR) · corrosion level 2 · airframe 41,287 hrs · 56,264 cycles

DURING SCHEDULED INSPECTION AT HAECO LAKE CITY, FLORIDA FOUND FWD CARGO COMPARTMENT, BILGE AREA, RBL 21.8 FLOOR BEAM, FS 500D, BULKHEAD ATTACH ANGLE HAS CORROSION. S/O 660004 N/R 44445.

Part: ANGLE — CRACKED (ZONE 200) · airframe 41,287 hrs · 56,264 cycles

DURING SCHEDULED INSPECTION, FOUND FWD ENTRY DOOR AFT EDGE OF DOOR CUTOUT HAD A CRACKED ANGLE AT STA. 348 BETWEEN S8L - S9L.

Part: SEAT TRACK — GOUGED (MAIN CABIN) · airframe 41,287 hrs · 56,264 cycles

DURING SCHEDULED INSPECTION AT HAECO LAKE CITY, FLORIDA FOUND MAIN CABIN SEAT TRACK OUTBOARD FLANGE SPLICE GOUGED AT STA 420 RBL 45.50.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 41,287 hrs · 56,264 cycles

DURING SCHEDULED INSPECTION AT HAECO LAKE CITY, FLORIDA FOUND STIFFENER AT RBL6.15 AND WL 170.4 HAS A CRACKED HOLE. S/O 660004 N/R 44991.

Part: SKIN — GOUGED (HORIZONTAL STAB) · airframe 41,287 hrs · 56,264 cycles

DURING SCHEDULED INSPECTION AT HAECO LAKE CITY, FLORIDA FOUND RT HORIZONTAL STABILIZER, PANEL 92226R, STAINLESS ANGLE WAS GOUGED. S/O 6600004 N/R 44479.

Part: CAP — CORRODED (STA. 540) · corrosion level 2 · airframe 41,287 hrs · 56,264 cycles

DURING SCHEDULED INSPECTION AT HAECO LAKE CITY, FLORIDA FOUND MAIN CABIN FLOOR SUPPORT CAP HAS EVIDENCE OF CORROSION AND PUNCTURES AT STA. 540 RBL 24.50 - 45.50, LBL 24.50 - 45.50 AND LBL 70.53 - RBL 70.53. S/O 660004 N/R 44786

Part: FLOOR PANEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 41,287 hrs · 56,264 cycles

DURING SCHEDULED INSPECTION AT HAECO LAKE CITY, FLORIDA FOUND AFT CARGO FLOOR PANEL 1538, MIDDLE AREA, HAS PITTING CORROSION. S/O 660004 N/R 44977

Part: SKIN — CORRODED (RT WING) · airframe 50,580 hrs · 55,464 cycles

CORROSION ON WING LOWER SKIN AT STR7 WBL55R. REMOVED AND FOUND WITHIN LIMITS IAW DWG 5710D2830 REV IR, NO REMAINING DEFECTS FOUND.

Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 50,580 hrs · 55,464 cycles

CORROSION FOUND ON THE LOWER LEFT WING SKIN BETWEEN STRINGERS 5 & 6, WBL40L TO WBL60L. CORROSION REMOVED AND FOUND OUT OF LIMITS IAW DWG 5710D2830, REV IR. REPAIRED IAW DWG R27905.1-057-013-001, REV NC.

Part: PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,854 hrs · 52,373 cycles

DISCREPANCY: STA 380 - 420 RT FLOOR SIDE PLATE IN FWD CARGO PIT CORRODED AROUND NUT PLATES. CORRECTION: STA 380-420 RT FLOOR SIDEPLATE IN FWD CARGO PIT REPLACED IAW SRM 51-40-02 REV 118. SERVICEABLE. PART IDENTIFIED AS PER SRM REV 118 CH 53-30-53.

Part: HINGE — CRACKED (DOOR) · airframe 48,854 hrs · 52,373 cycles

DISCREPANCY: STA 500A IN STEEL HINGE ON DOOR SIDE, HAS 2 CRACK INDICATIONS IN DOOR SKIN ON DOOR FRAMES. CORRECTIVE ACTION: 2 CRACK INDICATIONS IN DOOR SKIN AND FRAMES AT STA 500A IN STEEL HINGE AREA ON DOOR SIDE REPAIRED IAW AEI EO 8331 REV IR, REFER TO FORM 8110-3. REFER TO NDT REPORT NDT19-3160 - NO CRACKS FOUND, NDT19-3067 - 2 CRACKS AS MARKED, NDT19- 3110 - FWD HOLE CRACKED IN SKIN AND FRAME AFT HOLE IN FRAME, NDT19-3148 - FWD HOLE NO CRACKS AFT HOLE 2 CRACKS.

Part: SKIN — CORRODED (LT WING) · airframe 48,854 hrs · 52,373 cycles

UPPER LT WING SURFACE BETWEEN WBL 71-200 HAS MULTI PAINT BLISTERS BETWEEN FWD & AFT SPAR. UPPER LT WING SURFACE BETWEEN WBL 71-200 BETWEEN FWD AND AFT SPAR PAINT BLISTERS BLENDED IAW SRM 51-10-2 REV 119. BLEND OUTS FOUND TO BE WITHIN LIMITS AND REPAIRED IAW DWG NO.R279051-057-007-001 SHTS 1,6, DETAIL K, REV NC PAINT BLISTERS DETERMINED TO BE CORROSION.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,854 hrs · 52,373 cycles

DISCREPANCY: STA 986 MAIN CABIN RBL 24-45 FLOORBEAM HAS CORROSION. CORRECTIVE ACTION: STA 986 MAIN CABIN RBL 24-45 FLOORBEAM REPAIRED IAW AEI EO 8512 REV IR SEE FAA FORM 8110-3 FOR APPROVAL FOR THE REPAIR ACCOMPLISHED TO BS986 UPPER FLOORBEAM CAP.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,854 hrs · 52,373 cycles

DISCREPANCY: STA320, BL48 R1 DOOR ENTER WAY BUST SILL ANGLE CORRODED AROUND ANCHOR NUTS. CORRECTION: STA 320. BL 48 R1 DOOR ENTER WAY DUST STILL ANGLE REPLACED IAW DOCUMENT # 65-45875 REV J.

Part: VORTEX GEN — CORRODED (LT WING) · corrosion level 2 · airframe 48,854 hrs · 52,373 cycles

DISCREPANCY: LT WING UPPER SURFACE VORTEX GENERATOR CORRODED AT WBL 369 #3 FROM OUTBOARD. CORRECTION: LT WING UPPER SURFACE VORTEX GENERATOR REPLACED AT WS 423, #3 FROM OB IAW AMM 57-32-00 REV 88.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,854 hrs · 52,373 cycles

DISCREPANCY: STA 927-1006 MAIN CABIN BLO SEAT TRACK HAS CORROSION ON BOTH FLOORBOARD FLANGES. CORRECTIVE ACTION: STA 927-1006 MAIN CABIN INSTALLED MADE REPAIR PART BLO SEAT TRACK IAW AEI DRAWING # AE5714 REV.

Part: PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,854 hrs · 52,373 cycles

DISCREPANCY: STA 500-500A S-26-R FLOOR SUPPORT CHANNEL SIDE PLATE HAS SURFACE CORROSION FWD PIT. CORRECTION: STA 500-500A 526R FLOOR SUPPORT CHANNEL SIDE PLATE REPLACED WITH MADE REPAIR PART IAW DRAWING 65-20726 REV F AND SRM REV 119 CH 51-30-01.

Part: SKIN PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 48,854 hrs · 52,373 cycles

DISCREPANCY: LWR RT WING SURFACE @ WBL 72 APPROX HAS BLISTERING PAINT. CORRECTIVE ACTION: LWR RT WING SURFACE @ WBL 72 APPROX BLISTERING PAINT DETERMINED TO BE CORROSION. REPAIRED IAW SR #4- 4400286260 ISSUED 22 MAR 2019.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,854 hrs · 52,373 cycles

DISCREPANCY: STA 500B - 500C S-26R HAD CORROSION ON INTERCOSTAL. CORRECTION: STA 500B - 500C S-26R INTERCOSTAL REPLACED WITH MADE REPAIR PART IAW DWG NR 69-41473 AND B737-300 SRM 51-40-02 REV 118. IDENTIFIED IAW SRM REV 118 53-30-04. SERVICEABLE.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,854 hrs · 52,373 cycles

DISCREPANCY:STA 500 - 500A INTERCOSTAL AT S-26L CORRODED AROUND NUT PLATES. CORRECTION: STA 500 - 500A INTERCOSTAL AT S-26L REPLACED WITH MADE REPAIR PART IAW DWG NR 69-41473 AND SRM 51- 40-02 REV 118. STRUCTURE IDENTIFIED IAW SRM REV 118 CH 53-30-04.

Part: SKIN — CORRODED (RT WING) · airframe 48,854 hrs · 52,373 cycles

UPPER RT WING SURFACE BETWEEN WBL 479-541 APPROX HAS MULTI PAINT BLISTERS. UPPER RT WING SURFACE BETWEEN WBL 479-541 APPROX MULTI PAINT BLISTERS DETERMINED TO BE CORRODED SKIN PANEL AT D1, D2 LOCATIONS. CORRODED SKIN PANEL AT D1, D2 LOCATIONS REPLACED WITH NEW PANELS IAW SRM REV 119 51-40-02 PARA 4.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,854 hrs · 52,373 cycles

DISCREPANCY: 986 MAIN CABIN RBL32 FLOOR WEB HAS LIGHT CORROSION. CORRECTIVE ACTION: MADE AND INSTALLED NEW MADE REPAIR PART OF FLOOR WEB @ SAT 986 MAIN CABIN RBL 32 IAW SRM 51-40-02 REV 119 AND CH 51-30-01.

Part: BELTFRAME — DAMAGED (FUSELAGE) · airframe 48,854 hrs · 52,373 cycles

DISCREPANCY: BS986 BELTFRAME RIGHT HAND SIDE @ S17R FLOORBEAM TO BELTFRAME ATTACH FASTENER HOLES DAMAGED. CORRECTIVE ACTION: STA 986 BELTFRAME RT SIDE @ STR 17R WITH DAMAGED FLOORBEAM TO BELTFRAME ATTACH FASTENER HOLES, REPLACED IAW DWG #65-46564 REV B. NEW BELTFRAME INSTALLED IAW DWG #65- 46564 REV B & SRM 51-40-02 PARA 4, 7 REV 119.

Part: CREASE BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,854 hrs · 52,373 cycles

DISCREPANCY: STA 986-1000 CREASE BEAM WEB HAS CORROSION STR 17R. CORRECTIVE ACTION: MADE AND INSTALLED NEW MADE REPAIR BEAM WEB @ STA 986-1000 STR 17R IAW DWG 65-52878 REVJ AND SRM 51-40-02 REV 119.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 48,854 hrs · 52,373 cycles

STA 320, BL48 RT, R1 DOOR ENTER WAY. FLOORBEAM TOP CAP CORRODED AROUND ANCHOR NUTS. STA 328 BL48 RT, R1 DOOR ENTRY WAY FLOORBEAM TOP CAP REPAIRED IAW SRM REV 119 CH 53-10-51.

Part: FRAME — DENTED (FUSELAGE) · airframe 48,854 hrs · 52,373 cycles

DISCREPANCY: STA 460 RT STR 17-16R DENT ON FRAME. CORRECTIVE ACTION: STA 460 RT STR 17-16R DENT ON FRAME REPAIRED BY REPLACING FRAME WITH MADE REPAIR PART IAW DWG #65-46532 REV 13 SRM REV 119 51-30-01 AND 51-40-02 PARA 4,7.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 48,854 hrs · 52,373 cycles

DISCREPANCY: STRINGER CLIP @FSTA 500D STR L27 CRACKED. CORRECTIVE ACTION: STR CLIP @ STA 500D STR 27 REPLACED WITH NEW STR CLIP AND INSTALLED IAW SRM REV 119 CH 51-40-02 PARA. 4.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,854 hrs · 52,373 cycles

DISCREPANCY: STA 500A- 500B S-26R CORROSION ON INTERCOSTAL. CORRECTION: STA 500A - 500B S-26R INTERCOSTAL REPLACED WITH MADE REPAIR PART IAW DRAWING NO 69-41473 AND SRM 51-40- 02 REV 118 AND 53-30-04 SERVICEABLE. DWG NO 69-41473 REV.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,854 hrs · 52,373 cycles

DISCREPANCY: STA 887-986 MAIN CABIN LBL 45 SEAT TRACK HAS CORROSION ON BOTH FLOORBOARD FLANGES. CORRECTIVE ACTION: INSTALLED MADE REPAIR SEAT TRACK STA 887-986 MAIN CABIN LBL 45 SEAT TRACK IAW AEI DRAWING 5714 REV G.

Part: SKIN PANEL — DENTED (FUSELAGE) · airframe 48,854 hrs · 52,373 cycles

DISCREPANCY: STA 388 BETWEEN STR 26R + 25R EXTERNAL SKIN DENTS 2 LOCATIONS AS MARKED. CORRECTIVE ACTION STA 388, BETWEEN STR 24+25R, EXTERNAL DENTS IN 2 LOCATIONS REPAIRED IAW SRM 53-00-01 REPAIR 35 REV 119:

Part: FITTING — CRACKED (LT MLG) · airframe 48,854 hrs · 52,373 cycles

LEFT HAND MAIN LANDING GEAR BEAM FITTING ON AFT SPAR WBL157, HAS A CRACK INDICATION ON THE FORWARD FITTING. LEFT HAND MAIN LANDING GEAR BEAM FITTING ON AFT SPAR WBL157 CRACK REMOVED IAW SB737-57A1334 REV IR SEPT 16 2017.

Part: STRINGER CLIP — DAMAGED (FUSELAGE) · airframe 48,854 hrs · 52,373 cycles

AFT PIT STA 887 STR 18R DAMAGED. STRINGER CLIP REPLACED WITH NEW SERVICEABLE STRINGER CLIP IAW SRM REV 118 CH 51-40-02 PAR 7D.

Part: SKIN — CORRODED (RT WING) · airframe 48,854 hrs · 52,373 cycles

UPPER RT WING SURFACE @ WBL 522 APPROX HAS CORROSION. UPPER RT WING SURFACE @ WBL 522,608,613 APPROX, CORROSION BLENDED IAW SRM 51-10-02 PARA 14 REV 119. AREAS MARKED D3,D4,D5,D6,D7 REPAIRED IAW KF DWG NR R27905.1-057- 008-001 REV NC.

Part: ATTACH ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,854 hrs · 52,373 cycles

DISCREPANCY: 794 STR 25R CORROSION ON SCUFF PLATE ATTACH ANGLE AFT PIT. CORRECTION: 794 STR 25R CORROSION ON SCUFFPLATE ATTACH ANGLE AFT PIT FOUND TO BEYOND LIMITS. ATTACH ANGLE REPLACED WITH MADE REPAIR PART IAW SRM REV 118,CH 51-30-01 PARA 3,8. ANGLE IDENTIFIED AS 7075-063C BY NDT REPORT NDT 19-4041 AND MEASUREMENT.INSTALLED IAW SRM REV 118 CH 51-40-02 PARA 7.

Part: NOT REPORTED — CRACKED (FUSELAGE) · airframe 48,854 hrs · 52,373 cycles

DISCREPANCY: COMPLY WITH AEI EO8552 FOR THE CRACK AT BS727 BL0. CORRECTIVE ACTION: CRACK AT BS 727 BL 0 REPAIRED IAW AEI EO 8552 REV IR. REFER TO FAA FORM 8110-3. REFER TO NDT REPORTS NDT19-3023 - CRACK IN TITANIUM LAYER, NDT19-3231 - NO CRACKS FOUND, NDT19-3207 - NO CRACKS IN 5/16 HOLE, NDT19-3228 - 3 CRACKS AS MARKED.

Part: SKIN — CRACKED (FUSELAGE) · airframe 48,854 hrs · 52,373 cycles

BS 947 STR MAGER 17L CRACK ON FUSE SKIN AT L2 DOOR FOUND BY INSPECTION SB737-53A1350. BS967 STRINGER 17L CRACK, REMOVED & REPAIRED ON FUSE SKIN AT L2 DOOR IAW SERVICE REQUEST 3-4426422151, SEE FAA FORM 8100-9 FOR THE APPROVAL FOR THE REPAIR, ATTACHED.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,854 hrs · 52,373 cycles

DISCREPANCY: STA 500D CORROSION FOUND ON LOWER SILL IN FWD PIT. LBL 30 TO RBL 30. CORRECTION: STA 500D CORROSION FOUND ON LOWER SILL IN FWD PIT LBL 30 TO RBL 30 REPLACED WITH MADE REPAIR PART IAW SRM REV 119 CH 51-40-02 PARA 4. STRUCTURE IDENTIFIED IN SRM REV 119 CH 53-30-53 CORROSION ALL THE WAY THROUGH STRUCTURE - BEYOND LIMITS OF TOLERANCE .007.

Part: PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,854 hrs · 52,373 cycles

DISCREPANCY: STA 500A - 500D CORROSION ON FLOOR SUPPORT CHANNEL SIDE PLATE AND NUT PLATES. CORRECTION: STA 500A-500D FLOOR SUPPORT CHANNEL SIDE PLATE RT REPLACED IAW SRM 51-40-02 REV 118, CH 51-30-01 AND CH 53-30- 53.

Part: SKIN PANEL — CRACKED (FUSELAGE) · airframe 48,854 hrs · 52,373 cycles

DISCREPANCY: STA.219.8 PILOT SIDE #1 WINDOW EXTERIOR SKIN CRACKED AT UPPER AFT CORNER. CORRECTIVE ACTION: REPAIRED STA219.8 PILOT SIDE #1 WINDOW, EXTERIOR SKIN CRACK AT AFT UPPER CORNER IAW SRM REV 119 53-10-01, REPAIR 10 FIGURE 201.

Part: PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,854 hrs · 52,373 cycles

DISCREPANCY: STA 430 S-26-R FLOOR SUPPORT CHANNEL SIDE PLATE CORRODED IN FWD PIT. CORRECTION: STA 430 526R FLOOR SUPPORT CHANNEL SIDE PLATE IN FWD PIT REPLACED WITH MADE REPAIR PART IAW DRAWING 65-20726 REV F AND SRM REV 119 CH 51-30-01.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,854 hrs · 52,373 cycles

DISCREPANCY: STA 500C TO 500D INTERCOSTAL AT S-26L CORRODED AROUND NUT PLATES. CORRECTION: STA 500C TO 500D INTERCOSTAL AT S-26L REPLACED IAW DWG NR 69-41757 AND B737-300 SRM 51-40-02 REV 118 WITH MADE REPAIR PART IAW SRM REV 119 CH 51-30-01.

Part: CREASE BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,854 hrs · 52,373 cycles

DISCREPANCY: 967-986 MAIN CABIN RBL 50 CORROSION ON DUST SILL INB R2 DOOR. CORRECTIVE ACTION: NEW CREASE BEAM INNER CHORD @ R2 DOOR STA 967-986 RBL 50 IN MAIN CABIN INSTALLED IAW DWG G5-52878 REV 5 AND SRM 51-40-02 REV 119.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,854 hrs · 52,373 cycles

DISCREPANCY: STA 500C-500D INTERCOSTAL: FLANGE STA 500C-500D 5-26R HAS SURFACE CORROSION. CORRECTION:STA 500C-500D INTERCOSTAL AT S-26R REPLACED IAW DWG NR 69-41757 REV - AND SRM 51-40-02 REV 118 AND IAW SRM REV 119 CH 51-30-01.

Part: CREASE BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,854 hrs · 52,373 cycles

DISCREPANCY; STA 985 CORROSION FOUND ON CREASE BEAM INNER CHORD AT LBL 45; FOUND ON REMOVALS FOR W/O 1869638 CORRECTIVE ACTION: NEW CREASE BEAM INNER CHORD AT LBL 45 STA 985 INSTALLED IAW DWG 65-52878 REV J AND SRM 51-40-62 REV 119.

Part: SKIN PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,854 hrs · 52,373 cycles

DISCREPANCY: STA 500A & 10 BETWEEN STR 20R & 21R CORRODED FASTENERS X3 COMMON TO EXTERIOR SKIN REPAIR. CORRECTIVE ACTION: STA 500A + 10 BETWEEN STR 20R AND 21R CORRODED FASTENERS X3 COMMON TO EXTERIOR SKIN REPAIR REPAIRED IAW SRM REV 119 CH. 53-00-01 REPAIR 35 FIG 201 DETAIL 7 PAGE 22.

Part: SKIN — CORRODED (RT WING) · airframe 48,854 hrs · 52,373 cycles

UPPER RT WING SURFACE BETWEEN WBL 71-110 APPROX HAS MULTI CORROSION SPOTS. UPPER RT WING SURFACE BETWEEN WBL71-110 APPROX, MULTIPLE CORROSION SPOTS BLENDED IAW SRM 51-10-02 PARA 14 REV 119. AREAS MARKED A1-A20 REPAIRED IAW SR # 4- 4400528446.

Part: STOP FITTING — DAMAGED (L1 DOOR) · airframe 48,854 hrs · 52,373 cycles

DISCREPANCY: BS348.2 S14L L1 DOOR STOP FITTINGS X10 HAVE DAMAGE ON INNER FLANGE DUE TO ORIGINAL VENTURA 9G SLIDING DOOR INSTALLATION. CORRECTIVE ACTION: STA 348-2 STR 7L-14L L1 DOOR STOP FITTINGS X10 HAVE DAMAGE ON INNER FLANGE HOLES DUE TO ORIGINAL VENTURA 9G SLIDING DOOR INSTALLATION REPAIRED BY INSTALLING NEW REPLACEMENT FITTINGS IAW DRAWING # 65-17685 REV H AND DRAWING # 3100 REV B.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,854 hrs · 52,373 cycles

DISCREPANCY: STA 907-1006 MAIN CABIN LBL 24 SEAT TRACK HAS CORROSION ON BOTH FLOORBOARD FLANGES. CORRECTIVE ACTION: INSTALLED MADE REPAIR PART SEAT TRACK AT STA 907-1006 MAIN CABIN LBL 24 IAW AEI DRAWING # AE5714 REV G.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,854 hrs · 52,373 cycles

DISCREPANCY: STA 947-1006 MAIN CABIN RBL 24 SEAT TRACK HAS CORROSION ON BOTH FLOORBOARD FLANGES. CORRECTIVE ACTION: STA 947-1006 MAIN CABIN INSTALLED MADE REPAIR PART RBL24 SEAT TRACK IAW AEI DRAWING # AE5714 REV G.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 48,854 hrs · 52,373 cycles

STA 344 BL 30-25 RH FLOOR BEAM TOP LAP REPAIRS IAW AEI EO 8326 REV IR AND B737-300 SRM REV 119 CH 53-10-51, SEE ATTACHED FAA 8110-3 APPROVAL.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 48,854 hrs · 52,373 cycles

STA 669 RBL 24 2 CRACKS ON LONGITUDINAL FLOORBEAM UPPER CHORD REPAIRED BY CHORD REPLACEMENT ON W/O 1894410. PREVENTIVE MOD INSTALLED PER SB 737-57A1296 REV 2 FIG 3 REFER TO NDT19-1057 - CRACKS CONFIRMED. REFER TO NDT19-3152 - NO CRACKS IN OPEN HOLES. SB 737-STA1296 DATED 1 APRIL 2015 REV 2.

Part: STRINGER CLIP — GOUGED (BS 500C) · airframe 48,301 hrs · 51,265 cycles

GOUGED STRINGER CLIP AT BS 500C, STRINGER 3L. REPLACED THE STRINGER CLIP IAW SRM 51-40-02, REV 117, AND DWG 65-46533, REV H.

Part: STRINGER CLIP — NOT REPORTED (BS 500D) · airframe 48,301 hrs · 51,265 cycles

REPLACED THE STRINGER CLIP AT BS 500D, STRINGER 6L IAW SRM 51-40-02, REV 117, AND DWG 65C22910, REV E.

Part: STRINGER CLIP — CRACKED (BS 500D) · airframe 48,301 hrs · 51,265 cycles

CRACKED STRINGER CLIP AT BS 500D, STRINGER 3L. REMOVED AND REPLACED IAW SRM51-40-02, REV 117 AND DWG 65C22910, REV E.

Part: STRINGER CLIP — CRACKED (BS 520) · airframe 48,301 hrs · 51,265 cycles

CRACKED STRINGER CLIP AT BS 520, S2L. REPLACED THE STRINGER CLIP IAW SRM 51-40-02, SEC 4, SEC 7, REV 117, AND DWG 65-46534, REV G.

Part: STRINGER CLIP — NOT REPORTED (BS 520) · airframe 48,301 hrs · 51,265 cycles

REPLACED STRINGER CLIP BS BS 520, STRINGER 6L IAW SRM 51-40-02, REV 117, AND DWG 65-46534, REV G.

Part: FRAME — CUT (BS 663.75) · airframe 48,301 hrs · 51,265 cycles

CUT ON THE BELT FRAME AT BS 663.75, STRINGER 4L. REPLACED THE UPPER SECTION OF THE FRAME BETWEEN STRINGERS 11L TO 11R IAW DWG 65-46541, REV P, AND DWG R279051-053-003-001, REV NC.

Part: SKIN — CORRODED (LT WING) · airframe 48,301 hrs · 51,265 cycles

REMOVED CORROSION ON UPPER SURFACE OF LEFT WING NEAR TIP IAW SRM 51-10-02, REV 117. FOUND TO BE BEYOND LIMITS IAW SRM 57-20-01. REPAIRED IAW ENGINEERING DRAWING R27905.1-057-006-001, REV A.

Part: STRINGER — GOUGED (BS 520) · airframe 48,301 hrs · 51,265 cycles

GOUGED STRINGER 5L AT BS 520. REPAIRED THE STRINGER IAW SRM 53-00-03, REPAIR 3, TYPE III, REV 117.

Part: STRINGER CLIP — CRACKED (BS 520) · airframe 48,301 hrs · 51,265 cycles

CRACKED STRINGER CLIP AT BS 520, STRINGER 5L. REPLACED THE STRINGER CLIP IAW SRM 51-40-02, REV 117, AND DWG 65-46534, REV G.

Part: STRINGER CLIP — NOT REPORTED (BS 500D) · airframe 48,301 hrs · 51,265 cycles

REPLACED STRINGER CLIP AT BS 500D, S8L IAW SRM 51-40-02, REV 117, AND DWG 65C22910, REV E.

Part: STRINGER — GOUGED (BS 520) · airframe 48,301 hrs · 51,265 cycles

GOUGED STRINGER 3L, BS 520. REPAIRED THE STRINGER IAW SRM 53-00-03, REPAIR 3, TYPE III, REV 117.

Part: STRINGER CLIP — CRACKED (BS 500D) · airframe 48,301 hrs · 51,265 cycles

CRACKED STRINGER CLIP AT BS 500D, STRINGER 2L REPLACED THE STRINGER CLIP IAW SRM 51-40-02, REV 117 AND DWG 6JC22910, REV E.

Part: STRINGER CLIP — NOT REPORTED (BS 520) · airframe 48,301 hrs · 51,265 cycles

STRINGER CLIP AT BS 520, STRINGER 3L REPLACED IAW SRM 51-40-02, REV 117, AND DWG 65-46534, REV G.

Part: STRINGER CLIP — NOT REPORTED (BS 500D) · airframe 48,301 hrs · 51,265 cycles

REPLACED THE STRINGER CLIP AT BS 500D, STRINGER 5L IAW SRM 51-40-02, REV 117, AND DWG 65C22910, REV E.

Part: PROXIMITY SWITCH — MALFUNCTIONED (K FLAP) · airframe 47,995 hrs · 50,638 cycles

NR 1OTBD KRUEGER FLAP CAUSING A LEADING EDGE FLAP TRANSIT LIGHT, WITH THE FLAPS IN THE UP POSITION. MX REPLACED THE NR 1 KRUEGER FLAP RETRACT PROXIMITY SWITCH IAW AMM 27-88-11. OPS CHECKED OK.

Part: SUPPORT BEAM — CORRODED (RT WING) · airframe 47,081 hrs · 48,682 cycles

BLENDED CORROSION ON WING CENTER SECTION SUPPORT BEAM WEB RT B STA 570, RBL 40.875 IAW SRM 51-10-02 REV 114. REMAINING MATERIAL THICKNESS 0.021". DAMAGE FOUND TO BE OUT OF LIMITS IAW SRM 57-10-13 FIG 101 DETAIL III REV 114. REPAIRED DAMAGE IAW DWG NR 27905.1 -057-005-001 REV A.

Part: DUCT — PUNCTURED (NR 2 ENGINE) · airframe 47,081 hrs · 48,682 cycles

REPAIRED NR 2 ENG I/B C-DUCT PUNCTURE AT 9:00 POSITION ON INNER SURFACE 23" FROM FWD EDGE IAW REPAIR DWG NR R27905.1-078-003-001 REV NC.

Part: ATTACH ANGLE — NOT REPORTED (FUSELAGE) · airframe 47,081 hrs · 48,682 cycles

SEAT TRACK LOWER ATTACH ANGLE AT BSTA 927 + 11, LBBL 24.00, AFT CARGO PIT WAS MEASURED BEYOND ALLOWABLE LIMITS IAW SRM REV 113 CH 53-60-51. ORIGINAL THICKNESS 0.040 INCH DEPTH OF DAMAGE 0.036 INCH. MATERIAL REMAINING 0.004 INCH. MADE REPAIR PART IAW DWG 69-35371 REV A. INSTALLED NEW PART IAW SRM REV 113 CH 51-40-02 PARA 4 AND PARA 9.

Part: SPAR — CORRODED (VERTICAL STAB) · airframe 47,081 hrs · 48,682 cycles

REMOVED CORROSION ON RT VERTICAL STAB CHORD FIN STA 274.30, FOUND BEYOND ALLOWABLE DAMAGE LIMITS IAW SRM REV 114 CH 55-30-10 DETAIL IV. REPAIRED DAMAGED SPAR CHORD ON RT STAB CHORD FIN STA 274.30 IAW SERVICE REQUEST NUMBER 3-3907440289.

Part: DUCT — DAMAGED (NR 2 ENGINE) · airframe 47,081 hrs · 48,682 cycles

REPAIRED NR 2 ENGINE I/B C DUCT AT AFT TOP SIDEWALL OF BYPASS DUCT IAW DWG R27905.1 -078-002-001 REV A.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 47,081 hrs · 48,682 cycles

REPAIRED AFT ENTRY DOORWAY AFT UPPER CORNER FUSELAGE SKIN IAW SRM REV 114, 53-00-01, REPAIR 32.

Part: SKIN — CORRODED (FUSELAGE) · airframe 47,081 hrs · 48,682 cycles

REPAIRED CORROSION DAMAGE ON RT FUSELAGE SKIN FORWARD OF POWERED OUTFLOW VALVE AT STA 971, STR 22R TO 25R IAW ENG DRAWING R27905.1-053-002-001 REV NV DATED 2017 JUNE 27.

Part: SKIN — DAMAGED (LT WING) · airframe 47,081 hrs · 48,682 cycles

REPAIRED LT WING UPPER SKIN AT TRAILING EDGE FROM WBL 300-392 IAW ENG DWG NR R27905.1-57-004-001 REV NC DATED 2017 JUN 27.

Part: STRINGER — NOT REPORTED (FUSELAGE) · airframe 45,322 hrs · 44,828 cycles

REPAIRED TOP FLANGE ON STRINGER 23 LT, BETWEEN STATION 500B - 500C IAW SRM 53-00-03 REPAIR 1 REV 108.

Part: BEAR STRAP — NOT REPORTED (FUSELAGE) · airframe 45,322 hrs · 44,828 cycles

BEAR STRAP AT STATION 303.9, JUST ABOVE LOWER HINGE, AT WL 238 LT & REPAIRED IAW SRM 53-10-01 REPAIR 14 REV 108. BEAR STRAP REPAIR AREA AT STATION 303.9 RE-FINISHED AS REQUIRED IAW AMM 51-21-99 REV 82.

Part: SKIN — GOUGED (LT HORIZ STAB) · airframe 45,322 hrs · 44,828 cycles

GOUGE IN LT STAB LE, AT STATION 111. REPAIRED DOUBLER FOUND TO BE BEYOND LIMITS IAW SRM REV 108 SECTION 55-10-01 FIG 101. MADE REPAIR DOUBLER, INSTALLED SRM REV 108 SECTION 51-30-01 PARA 8 & 51-40-02. MATERIAL IDENTIFIED IAW SAME SRM SECTION 55-10-01.

Part: SPAR — CRACKED (RT WING) · airframe 45,322 hrs · 44,828 cycles

UPPER AFT SPAR CHORD ON RT WING. CRACK AT WING STATION 220 RSS. REPAIRED IAW SRM REV 108 57-20-10 REPAIR 4.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 45,322 hrs · 44,828 cycles

CRACKED BRACKET ON INBD SIDE OF STUB BEAM AT STATION 639, RBL 45.5 & LBL 45.5 IN CABIN. REPLACED IAW 53A1254 REV 1 FIG 2 PAGE 14 ITEM E.

Part: FLOORBEAM — NOT REPORTED (FUSELAGE) · airframe 45,322 hrs · 44,828 cycles

NEW WEB ON FLOORBEAM, STATION 727, LBL45 IN MAIN CABIN. FABRICATED & INSTALLED IAW DWG 65-45410 REV J.

Part: SPAR — CRACKED (LT WING) · airframe 45,322 hrs · 44,828 cycles

UPPER AFT SPAR CHORD ON LT WING. CRACK AT WING STATION 220 RSS. REPAIRED IAW SRM REV 108 57-20-10 REPAIR 4.

Part: SUPPORT FITTING — CRACKED (RT MLG) · airframe 45,322 hrs · 44,828 cycles

AFT SUPPORT FITTING FOR RT MLG BEAM AT RSS 224.14. CRACK REPAIRED IAW SERVICE REQUEST NR 4-3129261229.

Part: SUPPORT FITTING — CRACKED (LT MLG) · airframe 45,322 hrs · 44,828 cycles

AFT SUPPORT FITTING FOR LT MLG BEAM AT RSS 224.14. CRACK REPAIRED IAW SERVICE REQUEST NR 4-31292551.

Part: SPAR — CRACKED (RT WING) · airframe 45,322 hrs · 44,828 cycles

AFT SPAR WEB CRACKED AT RT WING, STATION 220 AT LG BEAM, FITTING CUT OUT & REPAIRED IAW SRM REV 108 57-20-10 REPAIR 5.

Part: SPAR — CRACKED (LT WING) · airframe 45,322 hrs · 44,828 cycles

AFT SPAR WEB CRACKED AT LT WING, STATION 220 AT LG BEAM, FITTING CUT OUT & REPAIRED IAW SRM REV 108 57-20-10 REPAIR 5.

Part: FLOORBEAM — DAMAGED (BS 344) · airframe 43,709 hrs · 41,210 cycles

MAIN CABIN BS 344, LBL 20, GALLEY ATTACH HOLES ELONGATED ON UPPER FLANGE OF FLOORBEAM.

Part: FLOOR SUPPORT — CORRODED (BS 986)

CARGO FLOOR BS 986.5, RBL 43.5 UPPER CHORD FWD FLANGE UNDERNEATH CLIPNUT HAS CORROSION.