N742AS

Part: BATTERY — DISCHARGED (EMERGENCY LIGHTS) · airframe 61,938 hrs · 55,409 cycles

SMOKE BARRIER NR 8 EMERGENCY EXIT LIGHT BATTERY LOW. REPLACED BATTERY PER AMM.

Part: LIGHT — INOPERATIVE (L-1 DOOR) · airframe 60,645 hrs · 54,143 cycles

L1 EMERGENCY LIGHT INOP. INSTALLED SERVICABLE EXIT LIGHT ABOVE L1 DOOR PER AMM.

Part: BATTERY — DISCHARGED (BS 950) · airframe 60,588 hrs · 54,084 cycles

EMERGENCY EXIT LIGHT ADJACENT TO AFT FLIGHT ATTENDANT SEAT INOPERATIVE. REPLACED BATTERY PACK AT BS 950 PER AMM.

Part: BATTERY — DISCHARGED (BARRIER LIGHT) · airframe 60,542 hrs · 54,036 cycles

AFTER RECON SMOKE BARRIER EMERGENCY LIGHT INOP DURING TEST. REPLACED SMOKE BARRIRER EXIT SIGN EMERGENCY LIGHT BATTERY.

Part: SEAT TRACK — CORRODED (BS 540-616) · airframe 60,349 hrs · 53,855 cycles

FOUND CORROSION ON SEAT TRACK BEAM. REPLACED SEAT TRACK BEAM PER EA 5310 02604.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 60,349 hrs · 53,855 cycles

FOUND STRINGER CRACKED AT GND FASTENER HOLES. REPAIRED PER ERO 5373 AND EA 5310 02599.

Part: FRAME — CORRODED (FUSELAGE) · airframe 60,349 hrs · 53,855 cycles

FOUND FRAME CORRODED. REPAIRED FRAME PER SRM 53 10 4 FIG 6.

Part: STRINGER — CRACKED (BS 332 S8R) · airframe 60,349 hrs · 53,855 cycles

FOUND CRACKED STRINGER. REPLACED STRINGER WITH FABRICATED REPAIR PART PER SRM 51 30 05 AND ASA EA 5310 02583.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 60,349 hrs · 53,855 cycles

FOUND PASSENGER CABIN TIE CLIP CRACKED. REPLACED PER SRM 51 30 02 AND 53 10 01 FIG 1.

Part: FRAME — CORRODED (BS 344) · corrosion level 2 · airframe 60,349 hrs · 53,855 cycles

FOUND FRAME CORRODED UNDER STRINGER LOWER LOBE FUSELAGE. REPAIRED PER SRM 51 40 3 FIG 1.

Part: CLIP — CRACKED (BS 440) · airframe 60,349 hrs · 53,855 cycles

FOUND PASSENGER CABIN INTERIOR TIE CLIP CRACKED. REPLACED TIE CLIP PER 51 30 02 AND 53 10 1 FIG 1.

Part: REPAIR — NONE (FUSELAGE) · airframe 60,349 hrs · 53,855 cycles

TIME LIMITED REPAIR. REPAIRED PER ASA EA 5330 02075.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 60,349 hrs · 53,855 cycles

FOUND PASSENGER CABIN INTERIOR TIE CLIP CRACKED. REPLACED CRACKED TIE CLIP PER SRM 51 30 05 FIG 4 AND 51 30 2 PARA 7D.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,349 hrs · 53,855 cycles

FOUND FLOORBEAM CORRODED. REPAIRED PER SRM 53 10 1 FIG 1 AND 51 30 7 REF NRC 4926376.

Part: SPLICE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,349 hrs · 53,855 cycles

FOUND FRAME SPLICE CORRODED. REPLACED FRAME SPLICE PER SRM 53 10 1 FIG 1.

Part: DOOR FRAME — CRACKED (BS 492) · airframe 60,349 hrs · 53,855 cycles

FOUND MAIN CARGO DOOR CRACKED 6" BELOW HINGE AT FRAME LIGHTING HOLE TO INBD EDGE. REPAIRED PER ERO 5682 AND EA 5310 02608.

Part: FLOORBEAM — CORRODED (BS 520) · corrosion level 2 · airframe 60,349 hrs · 53,855 cycles

FOUND FLOORBEAM IS CORRODED. REPLACED UPPER FLOORBEAM PER EA 5310 02602.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,349 hrs · 53,855 cycles

FOUND FLOORBEAM CORRODED. REPAIRED FLOORBEAM PER SRM 51 30 02 AND ASA EA 5310 02601

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,349 hrs · 53,855 cycles

FOUND MAIN DECK FLOOR ACROSS I BEAM FOUND CORRODED. REPAIRED IAW SRM 53 10 01.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 60,349 hrs · 53,855 cycles

TIE CLIP CRACKED. REPLACED TIE CLIP PER SRM 51 30 02.

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,349 hrs · 53,855 cycles

FOUND FRAME TO SKIN WEB CRACKED REPAIRED PER SRM 53 10 4 FIG 10.

Part: TIE CLIP — CORRODED (FUSELAGE) · airframe 60,349 hrs · 53,855 cycles

FOUND TIE CLIP CORRODED. REPLACED TIE CLIP PER SRM 51 30 02 AND 51 30 05.

Part: REPAIR — NONE (FUSELAGE) · airframe 60,349 hrs · 53,855 cycles

TIME LIMITED SKIN REPAIR. REPAIRED PER ASA EA 5330 02075

Part: STRINGER — CRACKED (FUSELAGE) · airframe 60,349 hrs · 53,855 cycles

FOUND STRINGER CRACKED. REPLACED CRACKED STRINGER IAW SRM 53 10 3 ERO 5735 AND EA5360 01056.

Part: STRINGER — CORRODED (BS 467-1006) · corrosion level 2 · airframe 60,349 hrs · 53,855 cycles

FOUND STRINGER CORRODED. REPAIRED PER SRM 53-10-03.

Part: FRAME — CRACKED (CARGO DOOR) · airframe 60,349 hrs · 53,855 cycles

FOUND MAIN CARGO DOOR INTERIOR FRAME TO SKIN WEB CRACKED. REPAIRED PER SRM 53 10 4 FIG 10.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 60,349 hrs · 53,855 cycles

FOUND TIE CLIP CRACKED. REPLACED TIE CLIP PER SRM 51 30 02 FIG 11.

Part: SUPPORT BRACKET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,349 hrs · 53,855 cycles

FOUND L2 DOOR SILL ANGLE CORRODED. REPLACED SILL CHORD ANGLE SUPPORT BRACKET PER SRM 51 30 2.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 60,349 hrs · 53,855 cycles

FOUND STRINGER CRACKED. REPAIRED CRACKED STRINGER PER SRM 53 10 3 FIG 1.

Part: FRAME — CORRODED (BS 344 S25-26L) · airframe 60,349 hrs · 53,855 cycles

FOUND FRAME CORRODED. REPAIRED FRAME PER SRM 53 10 4 FIG 6.

Part: FLOORBEAM — CORRODED (BS 520) · corrosion level 2 · airframe 60,349 hrs · 53,855 cycles

FOUND FLOORBEAM CORRODED. REPLACED FLOORBEAM PER EA 5310 02602 AND ERO 5606.

Part: FRAME — CORRODED (FUSELAGE) · airframe 60,349 hrs · 53,855 cycles

FOUND MAIN CARGO DOOR FRAME TO SILL WEB IS CORRODED. REPAIRED PER SRM 51 40 3 FIG 1.

Part: FLOORBEAM — CRACKED (FUSELAGE) · corrosion level 2 · airframe 60,349 hrs · 53,855 cycles

FOUND FLOORBEAM CORRODED. REPLACED FLOORBEAM IAW EA 5310 02602 AND ERO 5606.

Part: STRINGER — CORRODED (BS 500B-520) · corrosion level 2 · airframe 60,349 hrs · 53,855 cycles

FOUND STRINGER CORRODED. STRINGER REPAIRED PER EA 5310 02574.

Part: STRINGER CLIP — CRACKED (BS 440) · airframe 60,349 hrs · 53,855 cycles

FOUND TIE CLIP CRACKED. REPLACED PER SRM 51 30 02 ANS 53 10 01 FIG 1.

Part: FRAME — CORRODED (BS 344) · airframe 60,349 hrs · 53,855 cycles

FOUND FRAME CORRODED. REPAIRED FRAME PER SRM 53 10 4 FIG 6.

Part: FRAME — CORRODED (BS 344) · corrosion level 2 · airframe 60,349 hrs · 53,855 cycles

FOUND FRAME CORRODED UNDER STRINGER. REPAIRED PER SRM 51 40 3 FIG 1.

Part: STRINGER CLIP — CRACKED (BS 460) · airframe 60,349 hrs · 53,855 cycles

FOUND TIE CLIP CRACKED. REPLACED PER SRM 51 30 02 FIG 11.

Part: FLOOR SUPPORT — CORRODED (BS 986-1006) · corrosion level 2 · airframe 60,349 hrs · 53,855 cycles

FOUND FLOOR SUPPORT CORRODED. REPLACED PER SRM 53 10 01 FIG 1 AND 51 30 7 REF NRC #4926376.

Part: FRAME — CORRODED (BS 947) · corrosion level 2 · airframe 60,349 hrs · 53,855 cycles

FOUND FRAME SPLICE CORRODED. REPLACED SPLICE PER SRM 53 10 1 FIG 1.

Part: SKIN — DENTED (BS 500) · airframe 60,349 hrs · 53,855 cycles

FOUND FUSELAGE SKIN DENTED. REPAIRED PER SRM 53 30 3 FIG 23.

Part: STRINGER — CRACKED (BS 500-520) · airframe 60,349 hrs · 53,855 cycles

FOUND STRINGER CRACKED AT FASTENER HOLE. REPAIRED STRINGER PER EA 5310 02599 AND ERO 5373.

Part: SKIN — GOUGED (CARGO DOOR) · airframe 60,349 hrs · 53,855 cycles

FOUND MAIN CARGO DOOR SKIN AT NR 6 HINGE ATTACH AREA GOUGED. REPAIRED PER ERO 5327 AND EA 5230 01310.

Part: SKIN — GOUGED (BS 406) · airframe 60,349 hrs · 53,855 cycles

FOUND MAIN CARGO DOOR SKIN AT NR 4 HINGE ATTACH AREA GOUGED. BLENDED OUT GOUGE PER ERO 5327 AND EA 5230 01310.

Part: SKIN — GOUGED (CARGO DOOR) · airframe 60,349 hrs · 53,855 cycles

FOUND MAIN CARGO DOOR SKIN AT NR 5 HINGE GOUGED. BLENDED OUT GOUGE PER ERO 5327 AND EA 5230 01310.

Part: STRINGER — GOUGED (BS 927-947) · airframe 60,349 hrs · 53,855 cycles

FOUND STRINGER GOUGED. REPAIRED IAW SRM 53 10 3 AND EA 5360 01054.

Part: STRINGER — CORRODED (BS 898-907) · airframe 60,349 hrs · 53,855 cycles

FOUND STRINGER CORRODED. REPAIRED STRINGER PER SRM 53 10 3 FIG 1.

Part: STRINGER — GOUGED (BS 927-947) · airframe 60,349 hrs · 53,855 cycles

FOUND STRINGER GOUGED REPAIRED PER SRM 53 10 3 FIG 1.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 60,349 hrs · 53,855 cycles

FOUND FLOORBEAM STIFFENER CRACKED. REPLACED STIFFENER WITH FABRICATED REPAIR PART PER SRM 51 20 01 FIG 7 AND 51 30 02.

Part: ATTACH FITTING — NICKED (STABILIZER) · airframe 60,349 hrs · 53,855 cycles

LT STAB CTR SECTION AFT SPAR UPPER FWD ATTACH LUG FACE NICKED. BLENDED LUG IAW ERO 5334 PARTS 1 16 AND EA 5510 01235.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,349 hrs · 53,855 cycles

FOUND SHEAR TIE CORRODED. REPLACED SHEAR TIE PER SRM 51 10 1 AND 51 70 1.

Part: TIE CLIP — CORRODED (FUSELAGE) · airframe 60,349 hrs · 53,855 cycles

FOUND TIE CLIP CORRODED. REPLACED TIE CLIP IAW SRM 51 30 2 AND 51 30 05.

Part: TIE CLIP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,349 hrs · 53,855 cycles

FOUND TIE CLIP CORRODED. REPLACED TIE CLIP.

Part: FRAME — CORRODED (FUSELAGE) · airframe 60,349 hrs · 53,855 cycles

FOUND FRAME TO SKIN CORRODED. FRAME TO SKIN REPAIRED PER SRM 51 10 4.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 60,349 hrs · 53,855 cycles

FOUND SHEAR TIE CORRODED. REPLACED SHEAR TIE PER SRM 51 10 1 AND 53 10 1.

Part: TIE CLIP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,349 hrs · 53,855 cycles

FOUND TIE CLIP CORRODED. REPLACED TIE CLIP PER SRM 51 30 02.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,349 hrs · 53,855 cycles

FOUND SHEAR TIE CORRODED. REPLACED SHEAR TIE PER SRM 53 10 4 FIG 8.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,349 hrs · 53,855 cycles

FOUND SHEAR TIE CORRODED. FABRICATED AND REPLACED SHEAR TIE PER SRM 51 30 02.

Part: FRAME — CORRODED (FUSELAGE) · airframe 60,349 hrs · 53,855 cycles

FOUND FRAME CORRODED. FRAME WEB REPAIRED PER SRM 53 10 04 FIG 8.

Part: SHEAR TIE — CORRODED (BS 767 S25-26L) · airframe 60,349 hrs · 53,855 cycles

FOUND SHEAR TIE CORRODED. REPAIRED SHEAR TIE IAW SRM 53 10 4 FIG 9A.

Part: SHEAR TIE — CORRODED (BS 986 S18-19L) · airframe 60,349 hrs · 53,855 cycles

FOUND SHEAR TIE CORRODED. REPLACED SHEAR TIE PER SRM 51 20 1 AND 51 30 02.

Part: SPAR — CORRODED (HORIZONTAL STAB) · airframe 60,349 hrs · 53,855 cycles

CARRY OUT CASCADE ERO 5344 RT HORIZ STAB FRONT AND REAR SPAR BUSHING INSPECTION AND REPLACEMENT DUE TO CORROSION, ERO 5334 PARTS 1 TO 16 AS APPLICABLE TO RT HORIZ STAB AND AS EA 5510 01235 CARRIED OUT.

Part: SPAR — CORRODED (HORIZONTAL STAB) · airframe 60,349 hrs · 53,855 cycles

CARRY OUT CASCADE ERO 5344 RT HORIZ STAB FRONT AND REAR SPAR BUSHING INSPECTION AND REPLACEMENT DUE TO CORROSION. ERO 5334 PARTS 1 TO 16 AS APPLICABLE TO RT HORIZ STAB AND AS EA 5510 01235 CARRIED OUT.

Part: FLOORBEAM — CORRODED (BS 986) · corrosion level 2 · airframe 60,349 hrs · 53,855 cycles

FOUND FLOORBEAM CORRODED. REPAIRED CORRODED FLOORBEAM PER EA 5310 02589.

Part: ANGLE — CRACKED (CARGO DOOR LATCH) · airframe 60,349 hrs · 53,855 cycles

FOUND MAIN CARGO DOOR NR 1 LATCH SUPPORTING ANGLE CRACKED. LATCH REPAIRED IAW SRM 53 30 02 AND EA 5230 01269.

Part: SILL — CORRODED (BS 907-1008) · corrosion level 2 · airframe 60,349 hrs · 53,855 cycles

FOUND SILL CORRODED. REPLACED CORRODED SILL PER SRM 53 10 2.

Part: STRINGER — CORRODED (BS 937 S24L) · corrosion level 2 · airframe 60,349 hrs · 53,855 cycles

FOUND STR 24 LT CORRODED. REPAIRED PER SRM 53 10 3 FIG 1 AND EA 5310 02603.

Part: TANK — CRACKED (RT WING FUEL) · airframe 60,349 hrs · 53,855 cycles

FOUND RT WING FUEL TANK CRACKED. REPAIRED IAW SB 737 57 1186 ERO 5287 AND ASA EA 5710 01127.

Part: STRINGER — CRACKED (BS 1064 S17R) · airframe 60,349 hrs · 53,855 cycles

FOUND STR 17R CRACKED AT TIE CLIP RIVET, STR 17R REPAIRED IAW SRM 52 10 3.

Part: FRAME — CRACKED (BS 380 S16R) · airframe 60,349 hrs · 53,855 cycles

FOUND FWD PASSENGER CABIN FRAME CRACKED. REPAIRED CRACKED FRAME PER SRM 53 10 4 FIG 11.

Part: SPAR — CORRODED (HORIZONTAL STAB) · airframe 60,349 hrs · 53,855 cycles

CARRY OUT CASCADE ERO 5344 RT HORIZ STAB FRONT AND REAR SPAR BUSHING INSPECTION AND REPLACEMENT DUE TO CORROSION. ERO 5334 PARTS 1 TO 16 AS APPLICABLE TO RT HORIZ STAB AND AS EA 5510 01235 CARRIED OUT.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 60,349 hrs · 53,855 cycles

FOUND TIE CLIP CRACKED. REPLACED TIE CLIP PER SRM 53 30 02 FIG 11.

Part: SHEAR TIE — CRACKED (BS 400 S13-14R) · airframe 60,349 hrs · 53,855 cycles

FOUND FRAME TO SKIN ATTACH ANGLE CRACKED. REPLACED ANGLE PER SRM 51 40 3 FIG 1.

Part: SHEAR TIE — CORRODED (BS 380 S25-26L) · corrosion level 2 · airframe 60,349 hrs · 53,855 cycles

FOUND SHEAR TIE CORRODED. REPLACED SHEAR TIE PER SRM 51 30 2.

Part: SHEAR TIE — CORRODED (BS 986) · airframe 60,349 hrs · 53,855 cycles

FOUND SHEAR TIE CORRODED. SHEAR TIE ANGLE REPLACED WITH FABRICATED REPAIR PART PER SRM 51 20 1.

Part: SPAR — CORRODED (HORIZONTAL STAB) · airframe 60,349 hrs · 53,855 cycles

CARRY OUT CASCADE ERO 5344 RT HORIZ STAB FRONT AND REAR SPAR BUSHING INSPECTION AND REPLACEMENT DUE TO CORROSION, ERO 5334 PARTS 1 TO 16 AS APPLICABLE TO RT HORIZ STAB AND AS EA 5510 01235 CARRIED OUT.

Part: SHEAR TIE — CRACKED (CARGO DOOR) · airframe 60,349 hrs · 53,855 cycles

FOUND MAIN CARGO DOOR FRAME TO SKIN CRACKED. REPAIRED PER SRM 51 40 30 FIG 1.

Part: SPAR — CORRODED (HORIZONTAL STAB) · airframe 60,349 hrs · 53,855 cycles

CARRY OUT CASCADE ERO 5344 RT HORIZ STAB FRONT AND REAR SPAR BUSHING INSPECTION AND REPLACEMENT DUE TO CORROSION. ERO 5334 PARTS 1 TO 16 AS APPLICABLE TO RT HORIZ STAB AND AS EA 5510 01235 CARRIED OUT.

Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 60,349 hrs · 53,855 cycles

CARRY OUT CASCADE ERO 5344 RT HORIZ STAB FRONT AND REAR SPAR BUSHING INSPECTION AND REPLACEMENT DUE TO CORROSION. ERO 5334 PARTS 1 TO PART 16 AS APPLICABLE TO RT HORIZ STAB AND AS EA 5510 01235.

Part: FLOORBEAM — MAINT ERROR (FUSELAGE) · airframe 60,349 hrs · 53,855 cycles

FOUND FLOORBEAM HAS DOUBLE DRILLED HOLES. REPAIRED FLOORBEAM WITH FABRICATED REPAIR PART.

Part: STRINGER CLIP — CORRODED (BS 947 S20L) · corrosion level 2 · airframe 60,349 hrs · 53,855 cycles

FOUND TIE CLIP CORRODED. REPLACED TIE CLIP IAW SRM 51 30 02 AND 51 30 05.

Part: FRAME — CORRODED (BS 488 S27-28R) · airframe 60,349 hrs · 53,855 cycles

FOUND FRAME CORRODED. REPAIRED CORRODED FRAME SECTION PER SRM 53 10 4.

Part: STRINGER CLIP — CRACKED (BS 440 S1R) · airframe 60,349 hrs · 53,855 cycles

FOUND TIE CLIP CRACKED. REPLACED TIE CLIP PER SRM 51 30 02 AND 53 10 01 FIG 1.

Part: SPAR — CORRODED (HORIZONTAL STAB) · airframe 60,349 hrs · 53,855 cycles

CARRY OUT CASCADE ERO 5344 RT HORIZ STAB FRONT AND REAR SPAR BUSHING INSPECTION AND REPLACEMENT DUE TO CORROSION. ERO 5334 PARTS 1 TO 16 AS APPLICABLE TO RT HORIZ STAB AND AS EA 5510 01235 CARRIED OUT.

Part: STRINGER CLIP — CRACKED (BS 947 S26R) · airframe 60,349 hrs · 53,855 cycles

FOUND TIE CLIP CRACKED. REPLACED CRACKED TIE CLIP PER SRM 51 30 5.

Part: SKIN — CRACKED (RT WING) · airframe 60,349 hrs · 53,855 cycles

FOUND RT WING LE SKIN CRACKED AT NUMBER 4 SLAT ACTUATOR CUTOUT. REPAIRED PER SRM 57 30 4 FIG 5.

Part: SHEAR TIE — CRACKED (BS 420 S10-11L) · airframe 60,349 hrs · 53,855 cycles

FOUND MAIN CARGO DOOR INTERIOR FRAME TO SKIN WEB CRACKED. REPAIRED PER SRM 51 40 3 FIG 1.

Part: SKIN — CRACKED (RT WING) · airframe 60,349 hrs · 53,855 cycles

RT WING LE SKIN CRACKED AT NR 5 SLAT CENTER STOP. REPAIRED PER SRM 57 30 4 FIG 5.

Part: SHEAR TIE — GOUGED (BS 927 S24-25R) · airframe 60,349 hrs · 53,855 cycles

FOUND SHEAR TIE GOUGED. REPLACED SHEAR TIE IAW SRM 53 10 2.

Part: STRINGER CLIP — CORRODED (BS 540) · corrosion level 2 · airframe 60,349 hrs · 53,855 cycles

FOUND TIE CLIP CORRODED. INSTALLED FABRICATED REPAIR PART PER SRM 51 30 2 PG 8 PARAGRAPH 8.

Part: STRINGER — CORRODED (BS 467-1006) · corrosion level 2 · airframe 60,349 hrs · 53,855 cycles

STRINGER 18L CORRODED. REPAIRED PER SRM 53-10-03.

Part: SHEAR TIE — DAMAGED (BS 727A) · airframe 60,349 hrs · 53,855 cycles

SHEAR TIE HAS LOW EDGE MARGIN AT FASTENER HOLES. REPAIRED FRAME IAW EA 5330 020595.

Part: FLOORBEAM — CORRODED (BS 767) · corrosion level 2 · airframe 60,349 hrs · 53,855 cycles

FLOORBEAM CORRODED. REPAIRED FLOORBEAM PER SRM 51-30-12 AND EA 5310 02601.

Part: SILL — CORRODED (BS 827-1016) · corrosion level 2 · airframe 60,349 hrs · 53,855 cycles

FOUND L2 DOOR SILL ANGLE CORRODED. REPLACED SILL CHORD IAW SRM 53 30 2.

Part: STRINGER — CORRODED (BS 540) · airframe 60,349 hrs · 53,855 cycles

FOUND STRINGER CORRODED. REPAIRED STRINGER IAW SRM 53 10 3 FIG 1.

Part: STRINGER — GOUGED (BS 907-927) · airframe 60,349 hrs · 53,855 cycles

FOUND STRINGER GOUGED. REPAIRED GOUGED STRINGER PER EA 5310 02605 AND ERO 5549.

Part: FLOORBEAM — CORRODED (BS 947) · airframe 60,349 hrs · 53,855 cycles

FOUND FLOORBEAM CAP CORRODED. REPAIRED AFT CABIN FLOOR BEAM CAP IAW EA 5310 02232.

Part: FITTING — CORRODED (BS 540) · corrosion level 2 · airframe 60,349 hrs · 53,855 cycles

FOUND STRINGER END FITTING CORRODED. REPLACED END FITTING PER SRM 51 20 1.

Part: SEAT TRACK — CORRODED (BS 540-616) · airframe 60,349 hrs · 53,855 cycles

FOUND CORROSION ON SEAT TRACK BEAM. REPLACED SEAT TRACK BEAM PER EA 5310 02604 AND ERO 5698.

Part: FLOORBEAM — CORRODED (BS 520) · corrosion level 2 · airframe 60,349 hrs · 53,855 cycles

FOUND FLOORBEAM CORRODED. REPAIRED FLOORBEAM IAW EA 5310 02602 AND ERO 5606.

Part: STRINGER — CRACKED (BS 947 S18L) · airframe 60,349 hrs · 53,855 cycles

FOUND STRINGER CRACKED. REPLACED STRINGER PER SRM 51 30 02 AND ERO 5735 AND EA 5360 01056.

Part: STRINGER — CRACKED (BS 500B-520) · airframe 60,349 hrs · 53,855 cycles

STRINGER CRACKED AT FASTENER HOLE. REPAIRED STRINGER IAW ERO 5373 AND EA 5310 02599.

Part: FLOOR SUPPORT — CORRODED (BS 520-540) · airframe 60,349 hrs · 53,855 cycles

FOUND FLOOR SUPPORT CORRODED. REPAIRED FLOOR SUPPORT IAW SRM 51 30 5 51 30 2 AND AMM 20 50 11.

Part: FLOORBEAM — CORRODED (BS 947) · airframe 60,349 hrs · 53,855 cycles

FLOORBEAM CAP CORRODED. REPAIRED FLOORBEAM CAP PER EA 5310 032374.

Part: FRAME — CORRODED (BS 344 S25-26R) · airframe 60,349 hrs · 53,855 cycles

FRAME CORRODED. REPAIRED FRAME PER SRM 53-10-4 FIG 6.

Part: STRINGER — CORRODED (BS 520) · corrosion level 2 · airframe 60,349 hrs · 53,855 cycles

FOUND STRINGER CORRODED. REPAIRED STRINGER PER SRM 53 10 3 AND EA 5310 02582.

Part: FRAME — CORRODED (BS 947 S20-22R) · airframe 60,349 hrs · 53,855 cycles

AFT CARGO PIT FRAME SPLICE CORRODED. REPLACED FRAME SPLICE PER SRM 53-10-1 FIG 1.

Part: STRINGER — CRACKED (BS 332 S8R) · airframe 60,349 hrs · 53,855 cycles

FOUND STRINGER 8R CRACKED. FABRICATED AND REPLACED CRACKED STRINGER PER SRM 51 30 05 AND EA 5310 02583.

Part: STRINGER CLIP — CRACKED (BS 947 S18R) · airframe 60,349 hrs · 53,855 cycles

TIE CLIP CRACKED. REPLACED TIE CLIP AND STRINGER 18R PER SRM 51-30-02.

Part: WEB — CRACKED (BS 924 S11-12L) · airframe 60,349 hrs · 53,855 cycles

FOUND WEB CRACKED BETWEEN STR 11C AND 12C AT FRAME ATTACH POINT REPAIRED WEB PER SRM 51 20 1 FIG 3 AND 51 30 2 FIG 3 AND 11.

Part: STRINGER — CORRODED (BS 500B-520) · corrosion level 2 · airframe 60,349 hrs · 53,855 cycles

STRINGER CORRODED. REPAIRED STRINGER PER EA 5310 02574.

Part: SKIN — DENTED (BS 500) · airframe 60,349 hrs · 53,855 cycles

FOUND FUSELAGE SKIN DENTED. REPAIRED DENTED SKIN IAW SRM 53 30 3 FIG 23.

Part: STRINGER — CORRODED (BS 350-366) · corrosion level 2 · airframe 60,349 hrs · 53,855 cycles

FOUND STRINGER CORRODED. STRINGER SPLICE REPAIRED IAW SRM 53 10 1 AND EA 5310 02588.

Part: STRINGER CLIP — GOUGED (BS 927 S24R) · airframe 60,349 hrs · 53,855 cycles

AFT CARGO PIT TIE CLIP GOUGED. REPLACED PER SRM 51-30-2 AND 51-30-05.

Part: REVEAL — CRACKED (R2 DOOR) · airframe 42,307 hrs · 23,927 cycles

LWR FWD CORNER R2 DOOR REVEAL FASTENER HOLES CRACKED. REPLACED PER SRM 51-30-2 FIG 3.

Part: SHEAR TIE — MISDRILLED (BS 980) · airframe 42,307 hrs · 23,927 cycles

TIE CLIP HAS DOUBLE DRILLED HOLES. REPLACED TIE CLIP WITH FABRICATED REPAIR PARTS IAW SRM 51-10-1.

Part: STRINGER — CRACKED (BS 535 S15R) · airframe 60,349 hrs · 53,855 cycles

STRINGER CRACKED. REPAIRED PER SRM 53-10-3 FIG 1.

Part: STRINGER — GOUGED (BS 900-912) · airframe 60,349 hrs · 53,855 cycles

AFT CARGO PIT STRINGER GOUGED. REPAIRED PER SRM 51-20-1 FIG 3, 7, 8, 9 AND 51-30-2.

Part: FLOORBEAM — CORRODED (BS 727B) · corrosion level 2 · airframe 60,349 hrs · 53,855 cycles

AFT CARGO PIT FLOORBEAM UPPER CHORD CORRODED. REPAIRED PER WORKCARD 4930579 ERO 5404 AND EA 5330 02503.

Part: STRINGER CLIP — CORRODED (BS 927) · corrosion level 2 · airframe 42,307 hrs · 23,927 cycles

CORRODED TIE CLIP. REPLACED TIE CLIP PER SRM 51-30-2.

Part: STOP FITTING — CRACKED (R2 DOOR) · airframe 42,307 hrs · 23,927 cycles

R2 DOOR FITTING LOWER STOP FASTENER HOLES CRACKED. REPLACED FITTING PER SRM 51-30-2 FIG 11 & 13.

Part: SHEAR TIE — CORRODED (BS 727A) · airframe 60,349 hrs · 53,855 cycles

SHEAR TIE CORRODED. REPLACED WITH FABRICATED REPAIR PARTS PER SRM 53-10-4 AND 51-40-04.

Part: SKIN — DENTED (VERTICAL STAB) · airframe 60,349 hrs · 53,855 cycles

DENT IN THE VERTICAL STAB RIGHT SIDE 12 INCHES AFT OF UPPER DORSAL FIN. REPAIRED PER ASA EA 5530 01139 AND CASCADE AREOSPACE ERO 5492.

Part: FLOORBEAM — CORRODED (BS 520) · airframe 60,349 hrs · 53,855 cycles

FLOORBEAM CORRODED. REPAIRED PER SRM 51-30-2.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 60,349 hrs · 53,855 cycles

LEFT HORZ STAB AFT STUB RIB ATTACH ANGLE DAMAGED CRACKED. REPLACED ATTACH ANGLE LEFT HORZ STAB INBOARD END AFT STAB RIB. ATTACH ANGLE REPLACED IAW SRM 51-30-2.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,349 hrs · 53,855 cycles

CABIN FLOORBEAM CORRODED AT LOWER FLANGE. REPLACED WITH FABRICATED PARTS PER SRM 51-10-1 AND 51-30-02.

Part: FLOORBEAM — CORRODED (BS 986) · airframe 60,349 hrs · 53,855 cycles

FLOORBEAM DOUBLER WEB CORRODED. REPLACED WITH FABRICATED REPAIR PART PER SRM 51-30-02 AND 51-30-5 FIG 3.

Part: SHEAR TIE — CORRODED (BS 986) · corrosion level 2 · airframe 60,349 hrs · 53,855 cycles

SHEAR TIE CORRODED. REPLACED WITH FABRICATED REPAIR PART PER SRM 51-30-02.

Part: ATTACH ANGLE — CORRODED (RUDDER) · airframe 60,349 hrs · 53,855 cycles

VERT STAB LEFT T/E AT RUDDER STA 174 PANEL ATTACH ANGLE HAS CORROSION. REPLACED PER SRM 55-30-1.

Part: SPLICE — CORRODED (BS 420 S26R) · corrosion level 2 · airframe 60,349 hrs · 53,855 cycles

FWD CARGO PIT STR 26R, STRINGER TERMINAL SPLICE CORRODED. REPLACED PER SRM 51-30-5 FIG 3 AND 53-10-01 FIG 1.

Part: FLOORBEAM — CORRODED (BS 560) · airframe 60,349 hrs · 53,855 cycles

CABIN FLOOR SUPPORT BEAM CORRODED AT LWR FLANGE. REPLACED PER SRM 51-10-1 AND 51-30-2.

Part: FLOORBEAM — CORRODED (BS 807) · corrosion level 2 · airframe 60,349 hrs · 53,855 cycles

CORROSION ON FWD FLANGE OF FLOORBEAM. FLOORBEAM FWD WEB AND FLANGE REPAIRED PER EA 5310 02578.

Part: FRAME — CORRODED (BS 520) · airframe 60,349 hrs · 53,855 cycles

CORRODED FRAME TO SKIN ATTACH ANGLE. REPAIRED FRAME PER SRM 53-10-4.

Part: STRAP — CORRODED (BS 794 FRAME) · corrosion level 2 · airframe 42,307 hrs · 23,927 cycles

CORROSION ON FRAME REINFORCEMENT STRAP. REMOVED AND REPLACED PER SRM 51-20-05.

Part: STRINGER CLIP — CORRODED (BS 540) · corrosion level 2 · airframe 60,349 hrs · 53,855 cycles

TIE CLIP CORRODED. INSTALLED FABRICATED REPAIR PART PART SRM 51-30-02.

Part: FRAME — CORRODED (BS 344) · airframe 60,349 hrs · 53,855 cycles

FRAME CORRODED ON FRAME UNDER STRINGER LOWER LOBE FUSELAGE. FRAME UNDER STRINGER REPAIRED.

Part: FLOOR SKIN — CORRODED (BS 260) · airframe 60,349 hrs · 53,855 cycles

FLOOR DECK CORRODED. REPLACED FLOOR SKIN PER SRM 51-20-1, 51-30-2 FIG 3 AND 11.

Part: FLOORBEAM — CRACKED (BS 328) · airframe 60,349 hrs · 53,855 cycles

FOUND FLOORBEAM AT BS 328 RBL 18 WEB CRACKED. REPAIRED FLOORBEAM WEB IAW SRM 51 40 02 FIG 1.

Part: BULKHEAD — CORRODED (BS 367) · airframe 60,349 hrs · 53,855 cycles

NWW COMPARTMENT AFT PRESSURE BULKHEAD LT ACCESS HOLE AT BSTA 267 LWR CORNER BEAM HAS CORROSION. REPLACED PWR SRM 51 30 02.

Part: ATTACH BRACKET — CRACKED (NLG WW) · airframe 60,349 hrs · 53,855 cycles

FOUND CRACKED NLG FWD SUPPORT FITTING TO WHEEL PRESSURE DECK ATTACH BRACKET. REPLACED ATTACH BRACKET PER SRM 51-20-1 AND 51-30-2.

Part: SKIN — GOUGED (FUSELAGE) · airframe 60,349 hrs · 53,855 cycles

FOUND SKIN GOUGED, REPAIRED PER SRM AND EA 5330 02051.

Part: SKIN — CHAFED (LT WING) · airframe 60,349 hrs · 53,855 cycles

FOUND LT WING UPPER SKIN CHAFED. REPAIRED PER ERO 5279 AND EA 5720 01297.

Part: SKIN — CHAFED (WS 76) · airframe 60,349 hrs · 53,855 cycles

FOUND LT WING UPPER SKIN AT WBL 76.75 FM AFT EDGE OF SKIN FWD FOR 9.5" SKIN CHAFED. REPAIRED PER ERO 5279 AND EA 5720 01297.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 60,349 hrs · 53,855 cycles

MAIN CARGO DOOR INTERIOR FRAME TO SKIN WEB CRACKED. REPAIRED PER SRM 53 10 1 FIG 10.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 60,349 hrs · 53,855 cycles

STR 26L AT BSTA 460 TO 480 CORRODED. REPAIRED PER SRM 53 10 3 FIG 1.

Part: RIVET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,349 hrs · 53,855 cycles

CORROSION ON RIVETS. REPAIRED PER SRM 53 10 3 FIG 1.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,349 hrs · 53,855 cycles

FUSELAGE SKIN CRACKED AT BSTA 533 535 ABOVE STR 15R. SKIN CRACK REPAIRED PER EA 5330 02037.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 60,349 hrs · 53,855 cycles

MAIN CARGO DOOR FRAME TO SKIN WEB CRACKED. REPAIRED PER SRM 53 10 4 FIG 10.

Part: FRAME — DENTED (FUSELAGE) · airframe 60,349 hrs · 53,855 cycles

FRAME AT BSTA 500B BETWEEN STR 20R TO 21R DENTED. FRAME REPAIRED BY MADE REPAIR PART PER SRM 51 40 03.

Part: ATTACH ANGLE — CORRODED (FUSELAGE) · airframe 60,349 hrs · 53,855 cycles

FRAME TO SKIN ATTACH ANGLE CORRODED. REPAIRED BY MADE UP REPAIR PART PER SRM 53 10 1.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 60,349 hrs · 53,855 cycles

STRINGER CORRODED. REPAIRED PER ASA EA 5330 02046.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 60,349 hrs · 53,855 cycles

MAIN CARGO DOOR FRAME TO SKIN WEB AT BSTA 400 BETWEEN STR 11L AND STR 13 L CRACKED 13 PLACES. REPAIRED PER SRM 53 10 4 FIG 10.

Part: ATTACH ANGLE — CORRODED (FUSELAGE) · airframe 60,349 hrs · 53,855 cycles

FRAME TO SKIN ATTACH ANGLE CORRODED. REPAIRED ATTACH ANGLE PER SRM 53 10 1 FIG 1.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,350 hrs · 53,855 cycles

FUSELAGE SKIN CRACKED AT BS 533-535 ABOVE STRINGER 15R. REPAIRED PER EA5330 02037.

Part: FRAME — DENTED (FUSELAGE) · airframe 60,350 hrs · 53,855 cycles

FRAME DENTED. FABBED REPAIR PART PER SRM 51-40-03.

Part: ATTACH ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,350 hrs · 53,855 cycles

FRAME TO SKIN ATTACH ANGLE CORRODED. REPAIRED ATTACH ANGLE PER SRM 53-10-1 FIG 1.

Part: ATTACH ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,350 hrs · 53,855 cycles

FRAME TO SKIN ATTACH ANGLE CORRODED. FABBED REPAIR PART PER SRM 52-10-1.

Part: FRAME — CRACKED (BS 294) · airframe 60,349 hrs · 53,855 cycles

FRAME ATTACH AT BS 294.5 STR 12C CRACKED WEB. WEB AT BS 294.5 STR 12L FABRICATED IAW SRM 57 20 1 FIG 3 7 8 9.

Part: STRINGER CLIP — CRACKED (BS 400)

YXX - FOUND TIE CLIP AT BS 400, STRINGER 3 RT IS CRACKED. REMOVED AND REPLACED TIE CLIP PER B737-200 SRM 53-10-05 FIG 3. (M)

Part: STRINGER CLIP — CORRODED (FS 907 S24L)

YXX - FOUND STRINGER 24L AT BS 907 CORRODED TIE CLIP. REMOVED AND REPLACED TIE CLIP PER B737-200 SRM 51-30-02 FIG 8. (M)

Part: STRINGER CLIP — CRACKED (BS 402 S1R)

YXX - FOUND PASSENGER CABIN INTERIOR, AT BS 420, STRINGER 1 RIGHT, TIE CLIP CRACKED. REPAIRED WITH FABRICATED REPAIR PART FROM CASCADE, P/N 0000A51503-9, AND B737-200 SRM 51-30-02. (M)

Part: WEDGE — DENTED (NR 6 SLAT)

YXX - FOUND RIGHT NR 6 SLAT T/E WEDGE UPPER SURFACE HAS A DENT AT SLAT STATION 359.03 AND 1.5 INCHES FROM T/E. PERMANENT REPAIR COMPLETED IAW B737-200 SRM 51-40-20 REPAIR 11 FIG 20. (M)

Part: KEELBEAM — CORRODED (FUSELAGE)

YXX - FOUND CORROSION ON RIGHT KEEL BEAM AT BS 636. RIGHT KEEL BEAM REPLACED IAW B737-200 SRM. (M)

Part: WEB — DENTED (LT WING)

DENT ON WEB ON LT WING RSS 497 APPROX 10 INCHES AFT OF REAR SPAR. REPAIRED IAW SRM. (K)

Part: KEELBEAM — DAMAGED (FUSELAGE)

YXX - FOUND BS 535 BETWEEN LEFT AND RIGHT KEEL BEAMS SUPPORT ANGLES HAS LOW EDGE MARGIN AT FASTENER HOLE. REMOVED AND REPLACED ANGLE IAW B737-200 SRM. (M)

Part: SKIN — CORRODED (FUSELAGE)

YXX - FOUND FUSELAGE SKIN BULGING AT BS 535 STRINGER 28 LEFT KEEL BEAM. REMOVED AND REPLACED KEEL BEAM AND REPAIRED SKIN IAW B737-200 SRM. (M)

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2

OB SIDE OF STR 26L AT B-STA 986 CORRODED. REMOVED AND REPLACED STRINGER 26L IAW SRM. (K)

Part: STIFFENER — CORRODED (FUSELAGE)

CORROSION FOUND ON VERTICAL STIFFENER LOCATED AT BS 328, RBL 14, WL 150, IN E AND E BAY. REMOVED AND REPLACED VERTICAL STIFFENER IAW SRM. (K)

Part: SPLICE — CORRODED (FUSELAGE)

CORROSION ON STRINGER 26L END SPLICE AT BS 540. REMOVED AND REPLACED END SPLICE IAW SRM. (K)

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2

FUSELAGE SKIN BULGING AT BS 535, STR 28 LT KEELBEAM. KEELBEAM REPLACED AND SKIN REPAIRED. (K)

Part: RIB — WORN (LT WING)

YXX - FOUND LEFT WING RIB BETWEEN AILERON AND FORE FLAP T/E ANGLE SUPPORT CHANNEL HAS WEAR DAMAGE. REMOVED AND REPLACED SUPPORT ANGLE IAW B737-200 SRM. (M)

Part: SKIN — CHAFED (FUSLEAGE)

YXX - FUSELAGE SKIN LEFT BS 262 3.5 INCHES ABOVE NLG DOOR CUTOUT CHAFED. SKIN CHAFED REPAIRED IAW B737-200 SRM. (M)

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2

AFT CARGO PIT B-STA 807 IB OF STRINGER 27L FRAME TO SKIN SHEAR TIE AFT FACE CORROSION FOUND AS MARKED. REMOVED AND REPLACED SHEAR TIE IAW SRM. (K)

Part: SKIN — DELAMINATED (NR 6 SLAT)

YXX - FOUND RIGHT NR 6 SLAT FS 540, UPPER EDGE HAS DAMAGE. PERMANENT REPAIR COMPLETED IAW B737-200 SRM 51-40-20 REPAIR 14 FIG 23. (M)

Part: STRINGER CLIP — CORRODED (FUSELAGE)

YXX - FOUND AFT CARGO PIT TIE CLIP HAS CORROSION AT BS 747 AND STRINGER 26R. REMOVED AND REPLACED TIE CLIP AT AFT CARGO BS 747 AND 26R IAW B737-200 SRM. (M)

Part: SPLICE — CORRODED (FUSELAGE) · corrosion level 2

FRAME SPLICE AT BSTA 847, STRINGER 27R FOUND CORRODED. FRAME SPLICE AT BSTA 847, STRINGER 27R REPLACED WITH MADE REPAIR PART IAW SRM. (K)

Part: ANGLE — DAMAGED (FUSELAGE)

YXX - FOUND U-CHANNEL AT AFT CARGO PIT DOOR SILL HAS ELONGATED HOLES FROM PREVIOUS REPAIR. REMOVED AND REPLACED U-CHANNEL IAW B737-200 SRM. (M)

Part: STRINGER CLIP — CORRODED (FUSELAGE) · corrosion level 2

AFT CRGO B-STA 747, STR 22L TIE CLIP CORRODED. REMOVED AND REPLACED TIE CLIP IAW SRM. (K)

Part: WEDGE — DENTED (NR 6 SLAT)

YXX - FOUND RIGHT NR 6 SLAT T/E WEDGE UPPER SURFACE HAS A DENT AT SLAT STATION 346.53 AND 4.5 INCH FROM T/E. PERMANENT REPAIR COMPLETED IAW B737-200 SRM 51-40-20 REPAIR 7 FIG 16. (M)

Part: DOOR FRAME — CRACKED (FUSELAGE)

DOOR FRAME ON FUSELAGE IS CRACKED (AFT END FWD FRAME. REPLACED IAW SRM. (K)

Part: STRINGER — CRACKED (FUSELAGE)

YXX - FOUND CRACKED STRINGER AT BS 836 STRINGER 26R. REMOVED AND REPLACED STRINGER 26R IAW B737-200 SRM. (M)

Part: KEELBEAM — CORRODED (FUSELAGE)

YXX - FOUND CORROSION ON RIGHT KEEL BEAM AT BS 636. LEFT KEEL BEAM REPLACED IAW B737-200 SRM. (M)

Part: BRACKET — CORRODED (FUSELAGE) · corrosion level 2

A BRACKET AT B-STA 847, STRINGER 18R FOUND CORROED. BRACKET REPLACED WITH THE REPAIR PART AT BSTA 847 STRINGER 18R IAW SRM. (K)

Part: STRINGER CLIP — CRACKED (FUSELAGE)

YXX - FOUND AFT CARGO TIE CLIP CRACKED AT BS 787 STRINGER 24R. REMOVED AND REPLACED TIE CLIP IAW B737-200 SRM. (M)

Part: STRINGER CLIP — CORRODED (FUSELAGE) · corrosion level 2

AFT CARGO B-STA 747, STR 21L TIE CLIP CORRODED. REMOVED AND REPLACED TIE CLIP IAW SRM. (K)

Part: SKIN — CORRODED (FUSELAGE)

FUSELAGE SKIN BULGE AT B-STRA 535, STR 28, LT. REPAIRED IAW SRM. (K)

Part: FLOORBEAM — CORRODED (FUSELAGE)

YXX - AFT CARGO PIT FLOOR SUPPORT BEAM TIE DOWN AREA AND ANCHOR NUT HOLES HAVE CORROSION AT BS 787 RBL 14. FLOORBEAM SECTION REPLACED IAW B737-200 SRM. (M)

Part: STRINGER — CORRODED (FUSELAGE)

STRINGER CORRODED AT BS 967-986. REMOVED AND REPLACED STRINGER IAW SRM. (K)

Part: SHEAR TIE — CRACKED (FUSELAGE)

YXX- SHEAR TIE CRACKED AT BS 787 STRINGER 26R AT HOLE. REPLACED SHEAR TIE IAW B737-200 SRM. (M)

Part: SKIN — CHAFED (FORE FLAP)

YXX - FOUND RIGHT INBOARD FORE FLAP CHAFE DAMAGE ON OUTBOARD TOP SURFACE AT WBL 181. RIGHT OUTBOARD FORE FLAP OUTBOARD TOP SURFACE AT WBL 181 CHAFED LOCATION REPAIRED IAW B737-200 SRM 51-40-20 REPAIR 4 FIG 13 WBL 181. (M)

Part: FLOOR SUPPORT — DAMAGED (FUSELAGE)

YXX - FOUND FLOOR SUPPORT FORMER AT BS 793 RBL 21 ELONGATED HOLES. REMOVED AND REPLACED FORMER IAW B737-200SRM. (M)

Part: SKIN — DELAMINATED (NR 3 SLAT)

YXX - NR 3 SLAT DELAMINATED AT OUTBOARD END LOWER SURFACE SLAT STATION 124.27. PERMANENT REPAIR COMPLETED. (M)

Part: FRAME — SCRATCHED (FUSELAGE)

AFT CARGO PIT BS 787, RBL 8 HAS SCRATCHED FRAME. FOUND BEYOND LIMITS AND REPAIRED IAW SRM. (K)

Part: KEELBEAM — CRACKED (FUSELAGE)

YXX - BS 727 LEFT KEEL BEAM FOUND CRACKED. REMOVED AND REPLACED KEEL BEAM IAW B737-200 SRM. (M)

Part: STRINGER — CRACKED (FUSELAGE)

CRACKED STRINGER AT B-STA 789, STRINGER 26R. REMOVED AND REPLACED STRINGER IAW SRM. (K)

Part: SKIN — DAMAGED (TE FLAP)

YXX - IMPACT DAMAGE ON OUTBOARD T/E O RIGHT INBOARD MID FLAP. RIGHT INBOARD MID FLAP IMPACT DAMAGE LOCATION REPAIRED IAW B737-200 SRM 51-40-20 REPAIR NR 2. (M)

Part: RAMP — DAMAGED (TE FLAP)

YXX - LEFT WING OUTBOARD FORE FLAP OUTBOARD RAMP DAMAGED. LEFT WING OUTBOARD FORE FLAP OUTBOARD RAMP REPLACED WITH NEW PART PER IAW B737-200 SRM. (M)

Part: STRINGER CLIP — CORRODED (FUSELAGE)

YXX - TIE CLIP A BS 847 STRINGER 27R FOUND CORRODED. TIE CLIP REPLACED WITH FABRIATED REPAIR PART AT BS 847 STRINGER 27R IAW B737-200 SRM 51-30-02 FIG 11. (M)

Part: ATTACH ANGLE — CRACKED (FUSELAGE)

YXX - FOUND INTERCOSTAL ATTACH ANGLE AT BS 791 CRACKED BETWEEN STRINGER 25-26 RT. ATTACH ANGLE REPLACED FROM BS 767-867. (M)

Part: SHEAR TIE — CORRODED (FUSELAGE)

YXX - AFT CARGO PIT SHEAR TIE HAS CORROSION OUTBOARD OF RIGHT KEELBEAM, STRINGER 27R BS 767. REMOVED AND REPLACED SHEAR TIE IAW B737-200 SRM. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

CORROSION ON FLOORBEAM AT B-STA 727B, RBL 10-21. CORROSION REPAIRED IAW SRM. (K)

Part: FLOOR SUPPORT — DAMAGED (FUSELAGE)

YXX - FOUND FLOOR SUPPORT FORMER AT BS 790 RBL 21 ELONGATED HOLES. REMOVED AND REPLACED FORMER IAW B737-200 SRM. (M)

Part: SKIN — DAMAGED (FLAP)

YXX - FOUND IMPACT DAMAGE ON OUTBOARD T/E OF RIGHT INBOARD MID FLAP. RIGHT INBOARD MID FLAP IMPACT DAMAGE LOCATION REPAIRED IAW B737-200 SRM. (M)

Part: KEELBEAM — CORRODED (FUSELAGE)

KEELBEAM, BS 647-663 LT LWR CHORD CORROSION FOUND UPPER AND LOWER FACE. LT KEELBEAM REPLACED IAW SRM. (K)

Part: KEELBEAM — CRACKED (FUSELAGE)

YXX - BS 727 RT KEELBEAM FOUND CRACKED. REMOVED AND REPLACED KEEL BEAM IAW B737-200 SRM. (M)

Part: FLOOR SUPPORT — DAMAGED (FUSELAGE)

YXX - FOUND FLOOR SUPPORT FORMER AT BS 810 810 RBL 21 ELONGATED HOLES. REMOVED AND REPLACED FORMER IAW B737-200 SRM. (M)

Part: SKIN — CHAFED (FORE FLAP)

YXX - FOUND RIGHT INBOARD FORE FLAP CHAFED ON INBOARD TOP SURFACE AT WBL 83. RIGHT INBOARD FORE FLAP INBOARD TOP SURFACE CHAFED LOCATION REPAIRED IAW B737-200 SRM 51-40-20 REPAIR 7 FIG 16 WBL 83. (M)

Part: FLOOR SUPPORT — DAMAGED (FUSELAGE)

YXX - FOUND FLOOR SUPPORT FORMER AT BS 813 RBL 21 ELONGATED HOLES. REMOVED AND REPLACED FORMER IAW B737-200 SRM. (M)

Part: SKIN — MISMANUFACTURED (FUSELAGE)

SKIN PANEL BETWEEN KEELBEAMS BSTA 727 TO S-STA 663 HAS LOW EDGE MARGIN AT FASTENER HOLES. REMOVED AND REPLACED PANEL IAW SRM. (K)

Part: STRINGER — CRACKED (FUSELAGE)

YXX- CRACKED FRAME AT BS 805 OUTBOARD STRINGER 26R. REPAIRED IAW B737-200SRM. (M)

Part: SKIN — DELAMINATED (NR 6 SLAT)

YXX - FOUND RIGHT NR 6 SLAT FOUND WITH DELAMINATION ON UPPER SURFACE MID-SPAN AT SLAT STATION 327, 359.03, 346.53 AND FS 540. PERMANENTLY REPAIRED IAW B737-200 SRM. (M)

Part: SKIN — DENTED (FLAP)

YXX - FOUND RIGHT INBOARD FLORE FLAP DENTED AND DELAMINATED AT OLD REPAIR AT BL 118. RIGHT INBOARD FORE FLAP AT WBL 118 DENTED AND DELAMINATED LOCATIONS REPAIRED IAW 737-200SRM. (M)

Part: SKIN — DAMAGED (TE FLAP)

YXX - IMPACT DAMAGE ON OUTBOARD TRAILING EDGE OF RIGHT INBOARD MID FLAP. RIGHT INBOARD MID FLAP IMPACT DAMAGE LOCATION REPAIRED IAW B737-200 SRM 51-40-20 REPAIR 1. (M)

Part: FLOOR SUPPORT — DAMAGED (FUSELAGE)

YXX - FOUND FLOOR SUPPORT FORMER AT BS 801 RBL 21 ELONGATED HOLES. REMOVED AND REPLACED FORMER IAW B737-200SRM. (M)

Part: STRINGER CLIP — CORRODED (FUSELAGE)

YXX - AFT CARGO PIT BS 827 STRINGER 26L TIE CLIP HAS CORROSION. REMOVED AND REPLACED TIE CLIP IAW B737-200 SRM. (M)

Part: ATTACH ANGLE — CORRODED (FUSELAGE)

YXX - AFT CARGO PIT BS 727 BUTT AND STRINGER 26L ATTACHED ANGLE HAS CORROSION. REPAIRED BY REMOVAL AND REPLACEMENT WITH FABRICATED REPAIR PART IAW B737-200 SRM. (M)

Part: KEELBEAM — CORRODED (FUSELAGE)

KEELBEAM B-STA 707-747 LT LOWER CHORD CORRODED. REMOVED AND REPLACED KEELBEAM IAW SRM. (K)

Part: SHEAR TIE — CORRODED (FUSLEAGE)

YXX - AFT CARGO PIT BS 727A RBL 10 FRAME TO SHEAR TIE CORRODED. REPLACED SHEAR TIE. (M)

Part: SHEAR TIE — CORRODED (FUSELAGE)

YXX - FOUND AFT CARGO PIT SHEAR TIE HAS CORROSION OUTBOARD OF RIGHT KEEL BEAM, STRINGER 27R AND BS 747. REPLACED SHEAR TIE. (M)

Part: FLOORBEAM — CHAFED (FUSELAGE)

YXX - FOUND AFT CARGO PIT FLOORBEAM HAS CORROSION ON ANCHOR NUT HOLE AFT OF BS 727B AND LBL 3. REPLACED SUPPORT BEAM. (M)

Part: KEELBEAM — CORRODED (FUSELAGE) · corrosion level 2

CORROSION ON RT KEELBEAM AT B-STA 618. REPLACED KEELBEAM. (K)

Part: ATTACH ANGLE — CORRODED (FUSELAGE)

YXX - FOUND AFT CARGO PIT BS 727B INBOARD OF RIGHT KEEL BEAM STRINGER 27R, FRAME ATTACHED ANGLE TO FLOOR SUPPORT BEAM HAS CORROSION. ATTACH ANGLE REPLACED. (M)

Part: STIFFENER — CORRODED (FUSELAGE)

YXX - FOUND CORROSION ON VERTICAL STIFFENER AT BS 328, RBL 14, WL 150. REPLACED VERTICAL STIFFENER. (M)

Part: SKIN — CHAFED (FORE FLAP)

YXX - FOUND RIGHT INBOARD FORE FLAP CHAFED DAMAGED ON OUTBOARD TOP SURFACE AT WBL 83. RIGHT INBOARD FORE FLAP, OUTBOARD TOP SURFACE AT WBL 83 CHAFED LOCATIONS REPAIRED IAW B737-200 SRM CHAPTER 51-40-20 REPAIR 7 FIGURE 16. (M)

Part: SKIN — DENTED (FORE FLAP)

YXX - RIGHT INBOARD FORE FLAP DENTED AND DELAMINATED AT OLD REPAIR AT WBL 118. RIGHT INBOARD FORE FLAP AT WBL 118 DENTED AND DELAMINATED LOCATIONS REPAIRED IAW B737-200 SRM CHAPTER 51-40-20 REPAIR 7 FIGURE 16. (M)

Part: SKIN — CHAFED (FORE FLAP)

YXX - FOUND RIGHT INBOARD FORE FLAP CHAFED DAMAGED ON OUTBOARD TOP SURFACE AT WBL 181. RIGHT INBOARD FORE FLAP, OUTBOARD TOP SURFACE AT WBL 181 CHAFED LOCATION REPAIRED IAW B737-200 SRM CHAPTER 51-40-20 REPAIR 4 FIGURE 13. (M)

Part: BRACKET — CORRODED (FUSELAGE)

AFT CARGO PIT B-STA 727B FRAME TO KEELBEAM (STA 27R) ATTACH ANGLE HAS CORROSION. REPLACED ATTACH ANGLE. (K)

Part: ATTACH ANGLE — CORRODED (FUSLEAGE)

AFT CARGO PIT B-STA 727B FRAME TO KEELBEAM (STA 27L) ATTACH ANGLE HAS CORROSION. REPLACED ATTACH ANGLE. (K)

Part: STRINGER CLIP — CORRODED (AFT CARGO)

AFT CARGO B-STA 907, STR 20L, TIE CLIP CORRODED. TIE CLIP REPLACED. (K)

Part: KEELBEAM — CRACKED (FUSELAGE)

B-STA 727 BETWEEN LT AND RT KEELBEAM SUPPORT ANGLE FOUND CRACKED. SUPPORT ANGLE REPLACED. (K)

Part: SKIN — CORRODED (FUSELAGE)

B-STA 597 TO B-STA 618 BETWEEN LT AND RT KEELBEAMS PANEL CORRODED. REPLACED KEELBEAM PANEL. (K)

Part: KEELBEAM — CORRODED (FUSELAGE)

KEELBEAM CORRODED AT B-STA 535, STR 28 RT. REPLACED KEELBEAM . (K)

Part: SUPPORT BRACKET — CRACKED (FUSELAGE)

BS 670 AT LT KEELBEAM SUPPORT BRACKET CRACKED. REPLACED SUPPORT BRACKET. (K)

Part: SUPPORT ANGLE — CORRODED (FUSELAGE)

SUPPORT ANGLE CORRODED AT B-STA 520 RT KEELBEAM. REPLACED SUPPORT ANGLE. (K)

Part: SUPPORT ANGLE — CORRODED (FUSLEAGE)

CORROSION FOUND ON SUPPORT ANGLE AT BAST 622 BETWEEN LT AND RT KEELBEAMS. REPLACED SHEAR TIE. (K)

Part: STRINGER — CRACKED (FUSELAGE)

STRINGER CRACKED AT B-STA 868, STR 25R. REPAIRED IAW SRM WITH MADE REPAIR PARTS. (K)

Part: KEELBEAM — DAMAGED (FUSELAGE)

KEELBEAM WEB B-STA 702 LT ONE HOLE BELOW MINIMUM EDGE MARGIN. REPLACED STRUCTURE, LOW EDGE MARGIN AREA CUTOUT AND REPAIR ANGLE INSTALLED. (K)

Part: KEELBEAM — CORRODED (FUSELAGE)

KEELBEAM CORRODED B-STA 516 TO 535 STR 28L. REPAIRED WITH MADE REPAIR PART. (K)

Part: SHEAR TIE — CORRODED (FUSELAGE)

AFT CARGO PIT AND AFT SHEAR TIE HAS CORROSION AT B-STA 727A BETWEEN STR 27L AND 26L. SHEAR TIE REPLACED. (K)

Part: SUPPORT ANGLE — CORRODED (BSTA630)

SUPPORT ANGLE CORRODED AT BSTA 630 BETWEEN LT AND RT KEELBEAMS. REPLACED SUPPORT ANGLE. (K)

Part: KEELBEAM — CORRODED (FUSELAGE)

KEELBEAM AT B-STA 648-662 RT LOWER SECTION CORROSION FOUND AT UPPER GATE. REPLACED KEELBEAM. (K)

Part: STIFFENER — CORRODED (FUSELAGE)

CORROSION FOUND ON VERTICAL STIFFENER. VERTICAL STIFFENER REPLACED. (K)

Part: STRUCTURE — CORRODED (AFT CARGO AREA)

AFT CARGO AREA B-STA 940 TO 947, STA 22L CORRODED. CORRODED STR 22L AT B-STA 947 REPLACED WITH FABRICATED REPAIR PART. (K)

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2

AFT CARGO FLOOR SUPPORT BEAM ANCHOR NUTS HOLES HAS CORROSION AFT OF B-STA 767, RBL 3. AFT CARGO PIT FLOOR SUPPORT BEAM AFT OF B-STA 767, RBL 3 REPAIRED WITH FABRICATED REPAIR PARTS. (K)

Part: SPLICE — CORRODED (FUSLEAGE)

AFT CARGO PIT BS 907 BUTT SPLICE HAS CORROSION AT STR 27R. REMOVED AND REPLACED STRINGER SPLICE. (K)

Part: SHEAR TIE — CORRODED (FUSELAGE)

SKIN TO FRAME ATTACHMENT AT B-STA 572 BETWEEN LT AND RT BEAM DAMAGED. REMOVED AND REPLACED SKIN TO FRAME ATTACHMENT. (K)

Part: SHEAR TIE — CORRODED (FUSELAGE)

SKIN TO FRAME ATTACHMENT AT B-STA 614 BETWEEN LT AND RT BEAM DAMAGED. REMOVED AND REPLACED SKIN TO FRAME ATTACHMENT. (K)

Part: STRINGER CLIP — CORRODED (FUSELAGE)

UXX - AFT CARGO BS 907 CORRODED TIE CLIP AT STRINGER 21L. REMOVED AND REPLACED TIE CLIP. (M)

Part: STRINGER CLIP — CORRODED (FUSELAGE)

AFT CARGO B-STA 907 CORRODED TIE CLIP AT STR 21L. REMOVED AND REPLACED TIE CLIP. (K)

Part: STRINGER CLIP — CORRODED (FUSELAGE)

YXX - AFT CARGO BS 767 STRINGER 23L TIE CLIP CORRODED. REMOVED AND REPLACED TIE CLIP AT BS 767. (M)

Part: SHEAR TIE — CORRODED (FUSELAGE)

YXX - AFT CARGO BS 727A STRINGER 19L TO STRINGER 20L SHEAR TIE CORRODED. REPLACED CORRODED SHEAR TIE. (M)

Part: FAILSAFE — CORRODED (FUSELAGE)

YXX - FRAME FAILSAFE CORRODED AT BS 986 STRINGER 21L. REPAIRED IAW B737-200 SRM 51-40-3 FIG 1. (M)

Part: BEARING — MISSING (AIRSTAIRS)

SEA - FUND HANDRAIL FITTING CORRODED, BEARING MISSING, AND RETAINER - 176 CORRODED. LOOSE BEARING/ CASTING JAMS DOOR WHEN OPENING. PIVOT POINT WAS REPAIRED WITH BUSHING IAW EA. (K)

Part: PRESSURE BLKHD — CRACKED (FUSLAGE)

PAE - LFEC OF AFT PRESSURE BULKHEAD FOUND CRACK INDICATION AT STR 7 LT OB RIVET. REPAIRED AFT PRESSURE BULKHEAD IAW SRM.

Part: RECEIVER — INOPERATIVE (EMERGENCY LIGHT)

FOUND EMERGENCY FLOOR TRACK LIGHTS AT ROW 14 INOPERATIVE. REPLACED LIGHT RECEIVER, OPS CHECK GOOD. (M)

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT)

FOUND AFTER RECON, FLOOR EMERGENCY LIGHTS ON SEAT PALLET 8-5 WILL NOT SHUT OFF. REPLACED SEAT PALLET BATTERY PACK, OPS OK. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

PAE - FOUND CORROSION ON LOWR CHORD FLOORBEAM. REMOVED CORROSION, FABRICATED REPAIR PARTS AND INSTALLED IAW EA5310-02377. (M)

Part: FITTING — DAMAGED (CARGO DOOR)

PAE - FOUND MAIN CARGO DOOR NR 2 FORWARD LATCH FITTING HAS ELONGATED HOLES. REMOVED AND REPLACED FITTING. (M)

Part: FRAME — CORRODED (FUSELAGE)

PAE - FOUND CORROSION AFT PIT BAY FRAME. ACCOMPLISHED REPAIR OF THE AFT CARGO DOOR CUTOUT FORWARD FRAME. (M)

Part: FITTING — DAMAGED (CARGO DOOR)

PAE - FOUND MAIN CARGO DOOR NR 1 AFT LATCH FITTING HAS FASTENER HOLES ARE ELONGATED. REMOVED AND REPAIRED ON MIG 5 4841772 AND GOODRICH ER 04-2573. (M)

Part: ANGLE — CRACKED (CARGO DOOR)

PAE - FOUND MAIN CARGO DOOR LATCH FITTING ANGLE CRACKED. REPAIRED MAIN CARGO DOOR LOEWR BEAM AND LATCH FITTING. (M)

Part: SKIN — CRACKED (FUSELAGE)

PAE - FOUND FUSELAGE SKIN CRACKED. REPAIRED PER EA 5330-01787. (M)

Part: FITTING — DAMAGED (CARGO DOOR)

PAE - FOUND MAIN CARGO DOOR NR 2 AFT LATCH FITTING HAS ELONGATED HOLES. REMOVED AND REPLACED FITTING. (M)

Part: FRAME — DAMAGED (FUSELAGE)

PAE - FOUND MAIN CARGO DOOR LOWER AFT STUB FRAME HAS ELONGATED HOLES. REMOVED, FABRICATED AND INSTALLED STUB FRAME IAW 51-20-01. (M)

Part: STIFFENER — GOUGED (CARGO DOOR)

FOUND MAIN CARGO DOOR STIFFENER COMMON TO TORQUE TUBE MOUNT IS GOUGED. REMOVED, FABRICATED AND INSTALLED STIFFENER IAW 51-30-2. (M)

Part: FRAME — GOUGED (FUSELAGE)

PAE - FOUND MAIN CARGO DOOR STUB FRAME IS GOUGED. REMOVED, FABRICATED AND INSTALLED STUB FRAME IAW 51-30-2. (M)

Part: FITTING — DAMAGED (CARGO DOOR)

PAE - FOUND MAIN CARGO DOOR FORWARD LATCH FITTING HAS ELONGATED HOLES. REMOVED AND REPAIRED IAW GOODRICH EO 04-2573. (M)

Part: FRAME — DAMAGED (FUSELAGE)

PAE - MAIN CARGO DOOR LOWER AFT STUB FRAME HAS ELONGATED HOLES. REMOVED, FABRICATED AND INSTALLED STUB FRAME IAW 51-20-01. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

PAE - FOUND CORROSION ON LOWER CHORD FLOORBEAM. REMOVED CORROSION. FABRICATED REPAIR PARTS AND INSTALLED. (M)

Part: BEAR STRAP — CRACKED (FUSELAGE)

FOUND FUSELAGE SKIN CRACKED AT MAIN CARGO DOOR CUTOUT UPPER FORWARD CORNER. REMOVED DAMAGE/CRACKED AREA, FABRICATED REPAIR PARTS AND INSTALLED. (M)

Part: FLOORBEAM — CORRODED (FUSLEAGE)

PAE - FOUND CORROSION ON FLOORBEAM UPPER CHORD. REMOVED CORROSION, FABRICATED REPAIR PARTS AND INSTALLED. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

PAE - FOUND CORROSION ON FLOORBEAM LOWER SURFACE. REMOVED CORROSION, FABRICATED REPAIR PARTS AND INSTALLED. (M)

Part: BEAM — CORRODED (FUSELAGE)

PAE - FOUND CORROSION ON LONGITUDINAL BEAM. REMOVED CORROSION AND REPAIRED LONGITUDINAL BEAM. (M)

Part: SHEAR TIE — CORRODED (FUSELAGE)

PAE - FOUND CORROSION ON SHEAR TIE. REMOVED CORROSION AND REPAIRED WEB. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

PAE - FOUND CORROSION ON FLOORBEAM. REMOVED DAMAGE FABRICATED REPAIR PARTS AND INSTALLED. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

PAE - FOUND CORROSION ON FLOORBEAM. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR. (M)

Part: FRAME — CRACKED (FUSELAGE)

FOUND CRACKED FRAME. REPLACED FRAME. (M)

Part: SHEAR TIE — DAMAGED (FUSELAGE)

FOUND DAMAGED FASTENER HOLES ON SHEAR TIE. REPAIRED SHEAR TIE. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

PAE - FOUND CORROSION ON FLOORBEAM. REPAIRED FLOORBEAM. (M)

Part: FAILSAFE — CORRODED (FUSELAGE)

PAE - FOUND CORROSION ON BS 787 FRAME FAIL/SAFE CHORD RBL 20 WL 155. REPAIRED FAIL/SAFE CHORD. (M)

Part: FAILSAFE — CORRODED (FUSELAGE)

PAE - FOUND CORROSION ON BS 794 FRAME FAIL/SAFE CHORD RBL 8-20 WL 155. INSTALLED NEW FAIL/SAFE CHORD. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

PAE - FOUND CORROSION ON UNDERSIDE OF UPPER CHORD AFT SIDE OF FLOORBEAM. REMOVED DAMAGE AND REPAIRED PER SRM. (M)

Part: BEAM — CORRODED (FUSELAGE)

PAE - FOUND CORROSION ON LONGITUDINAL BEAM OUT OF LIMITS. REPLACED WITH NEW LONGITUDINAL BEAM. (M)

Part: BULKHEAD — CHAFED (FUSELAGE)

PAE - FOUND BULKHEAD WEB CHAFED. REPAIRED NOSE WHEEL WELL AFT BULKHEAD PER SRM 51-40-2 FIG 1. (M)

Part: BEAM — CORRODED (FUSELAGE)

PAE - FOUND CORROSION ON LONGITUDINAL BEAM OUT OF LIMITS. REPLACED WITH NEW LONGITUDINAL BEAM. (M)

Part: FLOORBEAM — GOUGED (FUSELAGE)

PAE - DURING C-CHECK, FOUND UPPER CHORD DAMAGE ON FLOORBEAM WEB. REMOVED DAMAGE AND INSTALLED RPR PARTS IAW SRM 51-40-2. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

DURING C-CHECK, FOUND AFT CARGO BAY MAIN FLOORBEAM IS CORRODED. INSTALLED PERMANENT REPAIR IAW SRM 51-30-2. (M)

Part: BULKHEAD — CHAFED (NLG WW)

DURING C-CHECK, FOUND NOSE WHEEL WELL AFT BULKHEAD IS CHAFED. REPAIRED NOSE WHEEL WELL AFT BULKHEAD IAW SRM 51-40-2. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

PAE - DURING C-CHECK, FOUND CORROSION ON FLOORBEAM. REPAIRED FLOOR BEAM IAW SRM 53-10-1. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

PAE - FOUND CORROSION AFT CARGO BAY MAIN CABIN FLOORBEAM REPAIR STRAP LOWER FLANGE. REMOVED CORRODED REPAIR STRAP ON FLOORBAM LOWER FLANGE, FABRICATED REPAIR STRAP AND INSTALLED. (M)

Part: BATTERY — DISCHARGED (CABIN)

ANC - DURING MAINTENANCE CHECK, FOUND PALLET 9-5 EMERGENCY FLOOR LIGHTS INOPERATIVE. REPLACED BATTERY, OPS CHECKED GOOD. (M)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

ANC - DURING INSPECTION, FOUND TRACK LIGHTING INOPERATIVE AT ROW 17. REPLACED BATTERY ON SEAT PALLET 8-13. OPS CHECK GOOD. (M)

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT)

ANC - DURING SCHEDULED INSPECTION, FOUND EMERGENCY EXIT IDENTIFIER AT THE SMOKE BARRIER INOPERATIVE. REPLACED REMOTE ASSEMBLY BATTERY, THEN EXIT IDENTIFIER TESTED NORMAL. (M)

Part: SKIN — CORRODED (FUSELAGE)

OKC - DURING C-CHECK, FOUND THE ANTENNA PANEL AT FUSELAGE STATION 585, BUTTOCK LINE 0 CORRODED. REPAIRED SKIN PER EA. (M)

Part: SKIN — CRACKED (THRUST REVERSER)

OKC - DURING C-CHECK, FOUND NR 1 ENGINE THRUST REVERSER LOWER BUCKET SKIN AT THRUST REVERSER STATION 200.70 CRACKED. REMOVED DAMAGE AND REPAIRED PER SRM. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

OKC - DURING C-CHECK, FOUND FLOORBEAM AT FUSELAGE STATION 543-602, BUTTOCK LINE 0 CORRODED. REMOVED CORROSION AND REPAIRED PER EA. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

OKC - DURING C-CHECK, FOUND FLOOR SUPPORT AT FUSELAGE STATION 827, STRINGER 26R-27R CORRODED. CUT OUT DAMAGE AND REPAIRED PER SRM. (M)

Part: SKIN — WORN (LT WING)

OKC - DURING C-CHECK, FOUND LEFT WING LEADING EDGE AT WING STATION 360 WORN. REMOVED DAMAGE AND REPAIRED PER SRM. (M)

Part: SKIN — CORRODED (LE FLAP)

DURING C-CHECK, FOUND LEFT WING FORE FLAP LEADING EDGE SKIN AT WING STATION 417 CORRODED. REMOVED CORROSION AND REPAIRED PER SRM. (M)

Part: ANGLE — CORRODED (FUSELAGE)

DURING C-CHECK, FOUND ANGLE AT FUSELAGE STATION 348-360, STRINGER 27R CORRODED. REPLACED ANGLE PER EA. (M)

Part: SKIN — DAMAGED (LT WING TE FLAP)

DURING C-CHECK, FOUND LEFT WING AFT FLAP SKIN AT WING STATION 417 CREASED. REMOVED DAMAGE AND REPAIRED PER SRM. (M)

Part: SPOILER — DELAMINATED (WING)

OKC - DURING C-CHECK, FOUND THE NR 8 SPOILER AT WING STATION 395.47 - 447.47 DELAMINATED. CUT OUT DAMAGED AREA AND REPAIRED PER EA. (M)

Part: STRUCTURE — DENTED (NR 1 PYLON)

OKC - DURING C-CHECK, FOUND NR 1 ENGINE PYLON AT WING STATION 191 DENTED. REMOVED DAMAGED AREA AND REPAIRED PER EA. (M)

Part: FRAME — CORRODED (FUSELAGE)

DURING C-CHECK, FOUND THE FRAME AT FUSELAGE STATION 420, LEFT BUTTOCK LINE 20, RIGHT BUTTOCK LINE 31 CORRODED. REPAIRED FRAME PER EA. (M)

Part: STRINGER — CORRODED (FUSELAGE)

OKC - DURING C-CHECK, FOUND STRINGER 28R AT FUSELAGE STATION 500B CORRODED. CUT OUT DAMAGE AND REPAIRED PER SRM. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

OKC - DURING C-CHECK, FOUND FLOORBEAM AT FUSELAGE STATION 480, RIGHT BUTTOCK LINE 24.75, RIGHT BUTTOCK LINE 45.5 CORRODED. REMOVED DAMAGE AND REPAIRED PER EA. (M)

Part: SKIN — WORN (TE FLAP)

DURING C-CHECK, FOUND RIGHT WING FORE FLAP SKIN AT WING STATION 417 WORN. REMOVED DAMAGE AND REPAIRED PER SRM. (M)

Part: SKIN — CHAFED (TE FLAP)

DURING C-CHECK, FOUND LEFT WING MID FLAP SKIN AT WING STATION 204.4 CHAFED. REMOVED DAMAGE AND REPAIRED PER SRM. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

OKC - DURING C-CHECK, FOUND FLOORBEAM AT FUSELAGE STATION 590, LEFT BUTTOCK LINE 24.5 CORRODED. REMOVED CORROSION AND REPAIRED PER EA. (M)

Part: SKIN — DENTED (TE FLAP)

DURING C-CHECK, FOUND RIGHT WING FORE FLAP SKIN AT WING STATION 395.47 DENTED. REMOVED DAMAGE AND REPAIRED PER SRM. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

DURING C-CHECK, FOUND THE FLOORBEAM AT FUSELAGE STATION 967, LEFT BUTTOCK LINE 40 CORRODED. REPAIRED FLOORBEAM PER EA. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

DURING C-CHECK, FOUND FLOORBEAM AT FUSELAGE STATION 540-706, RIGHT BUTTOCK LINE 24.5 CORRODED. REMOVED DAMAGE AND REPAIRED PER EA. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

DURING C-CHECK, FOUND THE FLOORBEAM AT FUSELAGE STATION 947, LEFT BUTTOCK LINE 26, LEFT BUTTOCK LINE 30 CORRODED. REPAIRED FLOORBEAM PER EA. (M)

Part: INTERCOSTAL — CORRODED (FUSELAGE)

OKC - DURING C-CHECK, FOUND INTERCOSTAL AT BODY STATION 947-967, LEFT BUTTOCK LINE 45, LEFT BUTTOCK LINE 55 CORRODED. REPLACED INTERCOSTAL PER SRM. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

OKC - DURING C-CHECK, FOUND FLOOR SUPPORT AT BS 859, STRINGER 3L CORRODED. REPLACED SUPPORT ANGLES PER SRM. (M)

Part: SUPPORT ANGLE — CHAFED (NR 1 ENGINE)

DURING C-CHECK, FOUND NR 1 ENGINE TAILPIPE FAIRING AT THRUST REVERSER STATION 98.60 CHAFED. REPLACED ANGLE PER SRM. (M)

Part: SKIN PANEL — CORRODED (FUSELAGE)

OKC - DURING C-CHECK, FOUND SKIN PANEL AT BS 360-366, STRINGER 27R CORRODED. CUT OUT DAMAGED SKIN AND REPAIRED PER SRM. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

OKC - DURING C-CHECK, FOUND FLOOR SUPPORT AT BS 859, RIGHT BUTTOCK LINE 8 CORRODED. CUT OUT DAMAGE AND REPAIRED FLOOR SUPPORT PER SRM. (M)

Part: LONGERON — DAMAGED (FUSELAGE)

OKC - DURING C-CHECK, FOUND NR 2 ENGINE FAIRING LONGERON AT NACELLE STATION 99.25 HAS A HOLE. REPLACED LONGERON PER SRM. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

OKC - DURING C-CHECK, FOUND FLOOR SUPPORT AT BS 859, LEFT BUTTOCK LINE 8 CORRODED. REPLACED FLOOR SUPPORTS PER SRM. (M)

Part: SEAT TRACK — BROKEN (FUSELAGE)

DURING C-CHECK, FOUND SEAT TRACK AT BS 400-480, BUTTOCK LINE 0 HAS A BROKEN LUG. REPLACED SEAT TRACK PER SRM. (M)

Part: ANGLE — CORRODED (FUSELAGE)

DURING C-CHECK, FOUND ANGLES AT BODY STATION 947, STRINGER 45L CORRODED. REPLACED TWO ANGLES PER SRM. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

OKC - DURING C-CHECK, FOUND FLOOR SUPPORT AT BS 879, RIGHT BUTTOCK LINE 8 CORRODED. CUTOUT DAMAGE AND REPAIRED FLOOR SUPPORT PER SRM. (M)

Part: STRAP — CORRODED (FUSELAGE)

OKC - DURING C-CHECK, FOUND STRAP AT BODY STATION 440, STRINGER 24R-26R CORRODED. REPLACED STRAP PER SRM. (M)

Part: SKIN — DENTED (FUSELAGE)

DURING C-CHECK, FOUND SKIN PANEL AT BS 925, STRINGER 24R DENTED. REMOVED DAMAGED AREA AND REPAIRED PER SRM. (M)

Part: FLOOR SUPPORT — CORRODED (FS)

DURING C-CHECK, FOUND FLOOR SUPPORT AT BS 663.73, LEFT BUTTOCK OINE 24.5 CORRODED. REMOVED DAMAGED FLOOR SUPPORT AND REPAIRED PER SRM. (M)

Part: SHEAR TIE — CORRODED (FUSELAGE)

OKC - DURING C-CHECK, FOUND WEB SHEAR TIE AT BS 277, STRINGER 27L CORRODED. REPLACED SHEAR TIE AND REPAIRED PER SRM. (M)

Part: SKIN — DENTED (FUSELAGE)

OKC - DURING C-CHECK, FOUND SKIN PANEL AT BS 901, STRINGER 23R DENTED. REMOVED DAMAGED AREA AND REPAIRED PER SRM. (M)

Part: WEB — CHAFED (FUSELAGE)

DURING C-CHECK, FOUND E/E DOOR RISER PANEL WEB AT BS 323.7-351.2, STRINGER 27R CHAFED. REPLACED WEB PER SRM. (M)

Part: SKIN — DENTED (FUSELAGE)

DURING C-CHECK, FOUND SKIN PANEL AT BS 273, STRINGER 24R DENTED. CUT OUT DAMAGED AREA AND REPAIRED PER SRM. (M)

Part: DOUBLER — CORRODED (FUSELAGE)

OKC- DURING C-CHECK, FOUND DOUBLER AT BODY STATION 947, LEFT BUTTOCK LINE 45.5 CORRODED. REMOVED CORROSION AND REPLACED DOUBLER PER SRM. (M)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

ANC - DURING PREFLIGHT INSPECTION, FOUND EMERGENCY TRACK LIGHTS INOPERATIVE ON PALLET NR 2. REMOVED AND REPLACED BATTERY PACK, THEN LIGHT OPERATED NORMALLY. (M)

Part: LIGHT — INOPERATIVE (ROW 17)

ANC - FOUND EMERGENCY EXIT LIGHTS AT ROW 17 INOPERATIVE. REPAIRED BROKEN WIRE AT ROW 17, THEN LIGHT TESTED NORMAL. (M)

Part: GUIDE ARM — LACK OF LUBE (L1 DOOR)

ANC - FLIGHT CREW REPORTED L1 DOOR DIFFICULT TO CLOSE. APPLIED HEAT AND LUBED UPPER GUIDE ARM, THEN OPS CHECKED GOOD. (M)

Part: BATTERY — INOPERATIVE (CABIN)

ANC - DURING INSPECTION, FOUND EMERGENCY EXIT IDENTIFIER AT THE SMOKE BARRIER INOPERATIVE. REMOVED AND REPLACED REMOTE ASSEMBLY RECEIVER AND BATTERY, THE EXIT IDENTIFIER TESTED NORMAL. (M)

Part: ACTUATOR — FAULTY (RT MLG)

ANC - ON APROACH INTO ANC, RIGHT MLG DID NOT EXTEND ON FIRST TRY. RT MLG EXTENDED ON SECOND ATTEMPT. REMOVED AND REPLACED RIGHT MLG LIB/ROB LOCK ACTUATOR, THEN GEAR CYCLED SEVERAL TIME WITH NO PROBLEMS. (M)

Part: BATTERY — DISCHARGED (CABIN)

SEA - DURING INSPECTION, FOUND EMERGENCY FLOOR TRACK LIGHTING INOPERATIVE ON ROWS 1-20. REMOVED AND REPLACED REMOTE ASSEMBLY RECEIVER AND BATTERIES AT ROWS 2 AND 3, THEN LIGHTS TESTED NORMAL. (M)

Part: DOOR — OUT OF ADJUST (L1)

ANC - FLIGHT CREW REPORTED L1 DOOR HAD TO OPERATE INTO CLOSED POSITION. ADJUSTED L1 DOOR PER MANUFACTURERS MM, THEN OPS CHECKED GOOD. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE CHECK, FOUND EMERGENCY LIGHT PACK INOPERATIVE AT ROW 8. REMOVED AND REPLACED THE BATTERY PACK. THE EMERGENCY LIGHT PACK THEN OPERATED NORMALLY. (M)

Part: SIGN — INOPERATIVE (CABIN)

ANC - EMERGENCY EXIT IDENTIFIER OVER R2 DOOR INOPERATIVE. REMOVED AND REINSTALLED EMERGENCY LIGHT ASSEMBLY OVER R2 DOOR, THEN OPS CHECKED GOOD. (M)

Part: GUIDE — OUT OF ADJUST (L1 DOOR)

ANC - L1 DOOR DIFFICULT TO CLOSE. ADJUSTED UPPER GUIDE ARM AND LUBED HINGES, THEN OPS CHECKED GOOD. (M)

Part: GUIDE — OUT OF ADJUST (L1 DOOR)

ANC - FLIGHT CREW REPORTED L1 DOOR HARD TO OPERATE INTO CLOSED POSITION. ADJUSTED, CLEANED AND LUBED UPPER GUIDE ARM, THEN OPS CHECKED GOOD. (M)

Part: BATTERY — DISCHARGED (CABIN)

ANC - DURING MAINTENANCE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTING AT ROWS 14 AND 15 INOPERATIVE. REMOVED AND REPLACED REMOTE ASSEMBLY BATTERY, THEN FLOOR TRACK LIGHTS OPERATED NORMAL. (M)

Part: SKIN PANEL — CORRODED (CARGO DOOR)

PAE - DURING SCHEDULED C-CHECK, FOUND SKIN PANEL ON CARGO DOOR AT BS 446, RBL 65 CORRODED. REPAIRED PER SRM. (M)

Part: KEELBEAM — CORRODED (FUSELAGE)

PAE - DURING SCHEDULED C-CHECK, FOUND KEEL BEAM AT BS 675-727, RBL 5 CORRODED. REPAIRED PER EA. (M)

Part: FRAME — CORRODED (FUSELAGE)

PAE - DURING SCHEDULED C-CHECK, FOUND FRAME AT BS 787, LBL 24, LBL 34 CORRODED. REPAIRED PER SRM. (M)

Part: FRAME — DENTED (FUSELAGE)

PAE - DURING SCHEDULED C-CHECK, FOUND FRAME AT BS 827, LBL 27 DENTED. REPAIRED PER SRM. (M)

Part: SHEAR TIE — CORRODED (FUSELAGE)

PAE- DURING SCHEDULED C-CHECK FOUND SHEAR TIE AT BODY STATION 727A, STRINGER 21L-22L CORRODED. REPAIRED PER SRM.

Part: BEAM — CRACKED (FUSELAGE)

PAE- DURING SCHEDULED C-CHECK FOUND LOWER GATE BEAM AT BODY STATION 312-344, WATERLINE 210, CRACKED. REPAIRED PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE)

PAE - DURING SCHEDULED C-CHECK, FOUND SHEAR TIE AT BODY STATION 847, RBL 10 CORRODED. REPAIRED PER SRM. (M)

Part: FRAME — CORRODED (FUSELAGE)

PAE - DURING SCHEDULED C-CHECK, FOUND FRAME AT BS 887, STRINGER 19L-22L CORRODED. REPAIRED PER SRM. (M)

Part: SHEAR TIE — CORRODED (FUSELAGE)

PAE - DURING SCHEDULED C-CHECK, FOUND SHEAR TIE AT BS 727A, STRINGER 24L-25L CORRODED. REPAIRED PER SRM. (M)

Part: SHEAR TIE — CORRODED (FUSELAGE)

PAE - DURING SCHEDULED C-CHECK, FOUND SHEAR TIE AT BS 807, STRINGER 26R-27R CORRODED. REPAIRED PER SRM. (M)

Part: STRINGER CLIP — CRACKED (FUSELAGE)

SEA - DURING SCHEDULED C-CHECK, FOUND STRINGER CLIP AT BS 747, STRINGER 22R CRACKED. REPAIRED PER SRM. (M)

Part: STRINGER CLIP — CORRODED (FUSELAGE)

SEA - DURING SCHEDULED C-CHECK, FOUND STRINGER CLIP AT BS 792, STRINGER 19L CORRODED. REPAIRED PER SRM. (M)

Part: STRINGER CLIP — CORRODED (FUSELAGE)

SEA - DURING SCHEDULED C-CHECK, FOUND STRINGER CLIP AT BS 747, STRINGER 26L CORRODED. REPAIRED PER SRM. (M)

Part: STRINGER CLIP — CORRODED (FUSELAGE)

SEA - DURING SCHEDULED C-CHECK, FOUND STRINGER CLIP AT BS 847, STRINGER 26L CORRODED. REPAIRED PER SRM. (M)

Part: CABLE — OUT OF ADJUST (ESCAPE SLIDE)

ANC - DURING MAINTENANCE CHECK, FOUND GIRT BAR DIFFICULT TO ARM AND DISARM. ADJUSTED CABLE AND LATCH ASSEMBLY THEN GIRT BAR ARMED NORMALLY. (M)

Part: ROD END — OUT OF ADJ (L1 DOOR)

ANC - L1 DOOR DIFFICULT TO CLOSE FROM THE INSIDE. ADJUSTED UPPER ROD END ASSEMBLY THEN OPS CHECKED GOOD. (M)

Part: LIGHT — INOPERATIVE (R2 DOOR)

ANC - DURING MAINTENANCE CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED EXIT LIGHT ASSEMBLY THEN LIGHT OPERATED NORMALLY. (M)

Part: BATTERY PACK — INOPERATIVE (CABIN)

SEA - DURING MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS AT SEAT PALLETS 7-4, 9-2, 7-5, 6-2 AND 5-6 WOULD NOT TEST. REMOVED AND REPLACED BATTERY PACKS THEN LIGHTS OPERATED NORMALLY. (M)

Part: BATTERY — DISCHARGED (MID CABIN)

SEA - DURING MAINTENANCE CHECK, FOUND EMERGENCY EXIT IDENTIFIER ON THE SMOKE BARRIER INOPERATIVE. REMOVED AND REPLACED REMOTE ASSEMBLY BATTERY THEN EXIT IDENTIFIER OPERATED NORMALLY. (M)

Part: BATTERY — DISCHARGED (MID CABIN)

SEA - DURING MAINTENANCE CHECK, FUOND EMERGENCY EXIT LIGHT AT SEAT PALLETS 6-7, 7-5 AND 9-3 INOPERATIVE. REMOVED AND REPLACED REMOTE ASSEMBLY BATTERIES THEN LIGHTS OPERATED NORMAL. (M)

Part: DOOR — STIFF (R2 DOOR)

ANC - DURING MAINTENANCE CHECK, FOUND R2 DOOR DIFFICULT TO OPEN OR CLOSE. LUBED R2 DOOR AND DOOR OPENED NORMALLY. (M)

Part: DOOR — LACK OF LUBE (L1)

ANC - DURING MAINTENANCE CHECK, FOUND L1 DOOR DIFFICULT TO OPEN. CLEANED AND LUBED L1 DOOR AND DOOR OPENED NORMALLY. (M)

Part: HINGE — LACK OF LUBE (L1 DOOR)

SEA - DURING MAINTENANCE CHECK, FOUND L1 DOOR HARD TO CLOSE. LUBED HINGES, DOOR OPERATED NORMALLY. (M)

Part: RECEIVER — INOPERATIVE (MID CABIN)

SEA - DURING MAINTENANCE CHECK, FOUND EXIT LIGHTS AT ROWS 2, 3, 12, 14 AND 18 INOPERATIVE. REMOVED AND REPLACED REMOTE ASSEMBLY BATTERY ON ROWS 2, 3, 12, 14, AND 18, AND REMOTE ASSEMBLY RECEIVER ON ROWS 2 AND 3 THEN LIGHTS OPERATED NORMALLY. REF ASAA0110099. (M)

Part: BATTERY — DISCHARGED (MID CABIN)

SEA - DURING MAINTENANCE CHECK, FOUND EXIT LIGHTS AT ROWS 2, 3, 12, 14 AND 18 INOPERATIVE. REMOVED AND REPLACED REMOTE ASSEMBLY BATTERY ON ROWS 2, 3, 12, 14, AND 18, AND REMOTE ASSEMBLY RECEIVER ON ROWS 2 AND 3 THEN LIGHTS OPERATED NORMALLY. (M)

Part: FRAME — CRACKED (FUSELAGE)

PHX - DURING SCHEDULED D-CHECK, FOUND CHORD AT BS 1138-1156, WATERLINE 260 CRACKED. REPAIRED PER SRM. (M)

Part: SEAT TRACK — CORRODED (CABIN)

PHX - DURING SCHEDULED D-CHECK, FOUND SEAT TRACK AT BS 727-727B, LEFT BUTTOCK LINE 40 CORRODED. REPAIRED PER EA. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

PHX - DURING SCHEDULED D-CHECK, FOUND FLOORBEAM AT BODY STATION 460, LEFT BUTTOCK LINE 10-53 CORRODED. REPAIRED PER EA. (M)

Part: SEAT TRACK — CORRODED (CABIN)

PHX - DURING SCHEDULED D-CHECK, FOUND SEAT TRACK AT BODY STATION 807-887, LEFT BUTTOCK LINE 45.5 CORRODED. REPAIRED PER SRM. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

PHX - DURING SCHEDULED D-CHECK, FOUND FLOORBEAM AT BS 947, RIGHT BUTTOCK LINE 36, LEFT BUTTOCK LINE 47 CORRODED. REPAIRED PER EA. (M)

Part: INTERCOSTAL — CORRODED (FUSELAGE)

PHX - DURING SCHEDULED D-CHECK, FOUND INTERCOSTAL AT BS 269, LEFT BUTTOCK LINE 10 TO RIGHT BUTTOCK LINE 10 CORRODED. REPAIRED PER SRM. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

PHX - DURING SCHEDULED D-CHECK, FOUND FLOORBEAM AT BODY STATION 500B, LEFT BUTTOCK LINE 0-45.5 CORRODED. REPAIRED PER EA. (M)

Part: SPLICE — CORRODED (FUSELAGE)

PHX - DURING SCHEDULED D-CHECK, FOUND FRAME SPLICE AT BS 947, STRINGER 25R CORRODED. REPAIRED PER SRM. (M)

Part: SKIN — CRACKED (AILERON)

PHX - DURING SCHEDULED D-CHECK, FOUND LEADING EDGE OF LEFT AILERON CRACKED. REPAIRED PER EA. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

PHX - DURING SCHEDULED D-CHECK, FOUND FLOORBEAM AT BODY STATION 480, LEFT BUTTOCK LINE 42.5-46 CORRODED. REPAIRED PER EA. (M)

Part: SHEAR TIE — CORRODED (FUSELAGE)

PHX - DURING SCHEDULED D-CHECK, FOUND SHEAR TIE AT BS 907, STRINGER 27L-27R CORRODED. REPAIRED PER SRM. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

PHX - DURING SCHEDULED D-CHECK, FOUND FLOORBEAM AT BS 420, LEFT BUTTOCK LINE 0-46 CORRODED. REPAIRED PER EA. (M)

Part: SEAT TRACK — CORRODED (CABIN)

PHX - DURING SCHEDULED D-CHECK, FOUND SEAT TRACK AT BODY STATION 880-947, LEFT BUTTOCK LINE 24.75 CORRODED. REPAIRED PER SRM. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

PHX - DURING SCHEDULED D-CHECK, FOUND FLOORBEAM AT BODY STATION 260, LEFT BUTTOCK LINE 12, RIGHT BUTTOCK LINE 14 CORRODED. REPAIRED PER EA. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

PHX - DURING SCHEDULED D-CHECK, FOUND FLOOR SUPPORT ANGLE AT BS 269, LEFT BUTTOCK LINE 12 TO RIGHT BUTTOCK LINE 12 CORRODED. REPAIRED PER SRM. (M)

Part: DOOR FRAME — CORRODED (FUSELAGE)

PHX - DURING SCHEDULED D-CHECK, FOUND DOOR FRAME ANGLE AT BODY STATION 947-990, LEFT BUTTOCK LINE 51 CORRODED. REPAIRED PER SRM. (M)

Part: SKIN — CRACKED (FUSELAGE)

PHX - DURING SCHEDULED D-CHECK, FOUND SKIN PANEL AT BS 967, STRINGER 18R CRACKED. REPAIRED PER EA. (M)

Part: ANGLE — CRACKED (FUSELAGE)

PHX - DURING SCHEDULED D-CHECK, FOUND CHORD ANGLE AT BS 1088-1156, ABOVE RIGHT HORIZONTAL STABILIZER AFT UPPER ATTACHMENT POINT CRACKED. REMOVED AND REPLACED CORD ANGLE PER SRM. (M)

Part: BRACKET — CORRODED (FUSELAGE)

PHX - DURING SCHEDULED D-CHECK, FOUND WEB BRACKET AT BODY STATION 1121-1138, WATERLINE 260 CORRODED. REPAIRED PER SRM (M)

Part: DOOR FRAME — CORRODED (FUSELAGE)

PHX - DURING SCHEDULED D-CHECK, FOUND DOOR FRAME AT BODY STATION 790, STRINGER 20R-26R CORRODED. REPAIRED PER SRM. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

PHX - DURING SCHEDULED D-CHECK, FOUND FLOORBEAM AT BODY STATION 540-727B, LEFT BUTTOCK LINE 45.5 CORRODED. REPAIRED PER EA. (M)

Part: SKIN — DAMAGED (FUSELAGE)

PHX - DURING SCHEDULED D-CHECK, FOUND PLUGGED HOLE ON SKIN PANEL AT BODY STATION 767, STRINGER 4L. REPAIRED PER PER. (M)

Part: FRAME — CORRODED (FUSELAGE)

PHX - DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 987, STRINGER 24L-24R CORRODED. REPAIRED PER SRM. (M)

Part: INTERCOSTAL — CORRODED (FUSELAGE)

PHX - DURING SCHEDULED D-CHECK, FOUND INTERCOSTAL AT BS 967-986, LEFT BUTTOCK LINE 39 CORRODED. REPAIRED PER SRM. (M)

Part: ANGLE — CORRODED (FUSELAGE)

PHX - DURING SCHEDULED D-CHECK, FOUND ANGLE ON INTERCOSTAL AT BS 967-986, LEFT BUTTOCK LINE 39 CORRODED. REPAIRED PER SRM. (M)

Part: BEAM — BROKEN (FUSELAGE)

PHX - DURING SCHEDULED D-CHECK, FOUND CARGO BEAM AT BS 491-520, STRINGER 27R BROKEN OUT. REPAIRED PER SRM. (M)

Part: BEAM — CORRODED (FUSELAGE)

PHX - DURING SCHEDULED D-CHECK, FOUND BEAM AT BS 727, LEFT BUTTOCK LINE 26 CORRODED. REPAIRED PER SRM. (M)

Part: INTERCOSTAL — CORRODED (FUSELAGE)

PHX - DURING SCHEDULED D-CHECK, FOUND INTERCOSTAL AT BS 791, STRINGER 25L CORRODED. REPAIRED PER SRM. (M)

Part: CLIP — CORRODED (FUSELAGE)

PHX - DURING SCHEDULED D-CHECK, FOUND SHEAR CLIP AT BS 807, STRINGER 7R CORRODED. REPAIRED PER SRM. (M)

Part: ANGLE — CRACKED (FUSELAGE)

PHX - DURING SCHEDULED D-CHECK, FOUND L-ANGLE BRACKET AT BS 178, STRINGER 25L CRACKED. REPAIRED PER SRM. (M)

Part: BULKHEAD — CORRODED (FUSELAGE)

PHX - DURING SCHEDULED D-CHECK, FOUND AFT PRESSURE BULKHEAD AT BS 1016-1030, STRINGER 27L-27R CORRODED. REPAIRED PER EA. (M)

Part: SPLICE — CORRODED (FUSELAGE)

PHX - DURING SCHEDULED D-CHECK, FOUND STRINGER SPLICE AT BS 907, STRINGER 20L CORRODED. REPAIRED PER SRM. (M)

Part: FITTING — CORRODED (FUSELAGE)

PHX - DURING SCHEDULED D-CHECK, FOUND TIE DOWN AT BS 915-947, STRINGER 27L CORRODED. REPAIRED PER SRM. (M)

Part: ANGLE — CORRODED (FUSELAGE)

PHX - DURING SCHEDULED D-CHECK, FOUND ANGLE AT BS 986, LEFT BUTTOCK LINE 39 CORRODED. REPAIRED PER SRM. (M)

Part: DOUBLER — CORRODED (FUSELAGE)

PHX - DURING SCHEDULED D-CHECK, FOUND DOUBLER ON INTERCOSTAL AT BS 980-986, STRINGER 46L CORRODED. REPAIRED PER SRM. (M)

Part: ATTACH FITTING — CORRODED (FUSELAGE)

PHX - DURING SCHEDULED D-CHECK, FOUND ATTACH FITTING AT BS 727, STRINGER 27L CORRODED. REPAIRED PER SRM. (M)

Part: SEAT TRACK — CORRODED (CABIN)

PHX - DURING SCHEDULED D-CHECK, FOUND SEAT TRACK AT BS 887-907, BUTTOCK LINE 0 CORRODED. REPAIRED PER SRM. (M)

Part: SKIN — DENTED (FUSELAGE)

PHX - DURING SCHEDULED D-CHECK, FOUND SKIN PANEL AT BS 197-203, STRINGER 26R-27R DENTED. REPAIRED PER SRM. (M)

Part: STRINGER — DAMAGED (FUSELAGE)

PHX - DURING SCHEDULED D-CHECK, FOUND A STRINGER AT BS 937-977, STRINGER 27L. REPAIRED PER SRM. (M)

Part: FRAME — CRACKED (FUSELAGE)

PHX - DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 480, STRINGER 21L-22L CRACKED. REPAIRED PER SRM. (M)

Part: SEAT TRACK — CORRODED (CABIN)

PHX - DURING SCHEDULED D-CHECK, FOUND SEAT TRACK AT BS 540-649, RIGHT BUTTOCK LINE 45.5 CORRODED. REPAIRED PER SRM. (M)

Part: INTERCOSTAL — CRACKED (FUSELAGE)

PHX - DURING SCHEDULED D-CHECK, FOUND INTERCOSTAL STRAP AT BS 312-352, RIGHT BUTTOCK LINE 24 CRACKED. REPAIRED PER SRM. (M)

Part: SKIN — DENTED (FUSELAGE)

PHX - DURING SCHEDULED D-CHECK, FOUND SKIN PANEL AT BS 867, STRINGER 21R DENTED BEYOND SRM LIMITS. REPAIRED PER SRM. (M)

Part: SHEAR TIE — CORRODED (FUSELAGE)

PHX - DURING SCHEDULED D-CHECK, FOUND CENTER SHEAR TIE AT BS 927, STRINGER 27L-27R CORRODED. REPAIRED PER SRM. (M)

Part: STRINGER — CORRODED (FUSELAGE)

PHX - DURING SCHEDULED D-CHECK, FOUND STRINGER AT BS 727-739, STRINGER 25L CORRODED. REPAIRED PER SRM. (M)

Part: FRAME — CORRODED (FUSELAGE)

PHX - DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 787, STRINGER 17L-22L CORRODED. REPAIRED PER SRM. (M)

Part: SKIN — DENTED (FUSELAGE)

PHX - DURING SCHEDULED D-CHECK, FOUND SKIN PANEL AT BS 836, STRINGER 20L DENTED BEYOND SRM LIMITS. REPAIRED PER SRM. (M)

Part: WEB — CRACKED (FUSELAGE)

PHX - DURING SCHEDULED D-CHECK, FOUND WEB AT BS 967-976, LEFT BUTTOCK LINES 39-46 CRACKED. REPAIRED PER SRM. (M)

Part: FRAME — CORRODED (FUSELAGE)

DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 219, STRINGER 15R-16R CORRODED. REPAIRED PER SRM. (M)

Part: WEB — CORRODED (FUSELAGE)

PHX - DURING SCHEDULED D-CHECK, FOUND CUSP WEB AT BS 947-986, STRINGER 17L CORRODED. REPAIRED PER SRM. (M)

Part: SKIN — DENTED (FUSELAGE)

PHX - DURING SCHEDULED D-CHECK, FOUND SKIN PANEL AT BS 912, STRINGER 21R DENTED BEYOND SRM LIMITS. REPAIRED PER SRM. (M)

Part: INTERCOSTAL — CRACKED (FUSELAGE)

PHX - DURING SCHEDULED D-CHECK, FOUND INTERCOSTAL AT BS 967-986, LEFT BUTTOCK LINE 46 CRACKED. REPAIRED PER SRM. (M)

Part: FRAME — CORRODED (FUSELAGE)

PHX - DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 947, STRINGER 24L-26L CORRODED. REPAIRED PER SRM. (M)

Part: BULKHEAD — CRACKED (FUSELAGE)

DURING SCHEDULED D-CHECK, FOUND BULKHEAD WEB AT BS 178, LEFT BUTTOCK LINE 6-18 CRACKED. REPAIRED PER SRM. (M)

Part: BULKHEAD — CRACKED (FUSELAGE)

PHX - DURING SCHEDULED D-CHECK, FOUND WEB AT STATION 178, RIGHT BUTTOCK LINE 11 CRACKED. REPAIRED PER SRM. (M)

Part: DOUBLER — CRACKED (FUSELAGE)

PHX - DURING SCHEDULED D-CHECK, FOUND BEAR STRAP AT STATION 967, STRINGER 24L-26L CRACKED. REPAIRED PER EA 5310-01899. (M)

Part: ANGLE — CORRODED (FUSELAGE)

PHX - DURING SCHEDULED D-CHECK, FOUND LOWER ANGLE ATTACHED TO INTERCOSTAL AT BS 967-986, LBL 46, CORRODED. REPAIRED PER SRM. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

PHX - DURING SCHEDULED D-CHECK, FOUND FLOORBEAM ANGLE AT BS 986, LBL 39, CORRODED. REPAIRED PER SRM. (M)

Part: PLATE — DAMAGED (FUSELAGE)

PHX - DURING SCHEDULED D-CHECK, SPLICE PLATE AT BS 727, STRINGER 4L CUT APPROXIMATELY TWO INCHES. REPAIRED PER EA 5330-01502. (M)

Part: SHEAR TIE — CORRODED (FUSELAGE)

PHX - DURING SCHEDULED D-CHECK, FOUND SHEAR TIE AT BS 967, STRINGER 24L-26L, CORRODED. REPAIRED PER SRM. (M)

Part: CHANNEL — CORRODED (FUSELAGE)

PHX - DURING SCHEDULED D-CHECK, FOUND CHANNEL AT BS 790-847, STRINGER 25R, CORRODED. REPAIRED PER SRM. (M)

Part: ANGLE — CORRODED (FUSELAGE)

PHX - DURING SCHEDULED D-CHECK, FOUND ANGLE AT BS 887, STRINGER 22L-24, CORRODED. REPAIRED PER SRM. (M)

Part: TIE CLIP — CORRODED (FUSELAGE)

PHX - DURING SCHEDULED D-CHECK, FOUND TIE CLIP AT BS 867, STRINGER 20L CORRODED. REPAIRED PER SRM. (M)

Part: FLOOR SUPPORT — DAMAGED (FUSELAGE)

PHX - DURING SCHEDULED D-CHECK, FLOOR SUPPORT HAS DOUBLER DRILLED HOLES AT BS 1006-1016, LBL 18. REPAIRED PER SRM. (M)

Part: SKIN — CHAFED (HORIZ STAB)

PHX - DURING SCHEDULED D-CHECK, FOUND RIGHT HORIZONTAL STABILIZER CHAFED ON TRAILING EDGE OF STATION 121.5. REPAIRED PER SRM. (M)

Part: SKIN — DAMAGED (FUSELAGE)

PHX - DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DING OUT OF LIMITS AT BS 954, STRINGER 20R-21R. REMOVED DAMAGED SECTION OF SKIN AND REPAIRED PER SRM. (M)

Part: WEB — CORRODED (FUSELAGE)

PHX - DURING SCHEDULED D-CHECK, FOUND WEB CORRODED. REMOVED AND REPLACED WEB PER SRM. (M)

Part: WEB — CRACKED (FUSELAGE)

PHX - DURING SCHEDULED D-CHECK, FOUND FLOOR WEB CRACKED. REMOVED, FABRICATED AND REPLACED FLOOR WEB PER SRM. (M)

Part: STIFFENER — CORRODED (FUSELAGE)

PHX - DURING SCHEDULED D-CHECK, FOUND CORROSION AT NUT CLIP HOLES ON UPPER AND LOWER SIDE OF FLOORBEAM STIFFENER. REMOVED AND REPLACED FLOORBEAM STIFFENER PER SRM. (M)

Part: FRAME — CORRODED (FUSELAGE)

PHX - DURING SCHEDULED D-CHECK, FOUND STUB FRAME CORRODED BEYOND LIMITS. REMOVED, FABRICATED AND REPLACED STUB FRAME PER SRM. (M)

Part: STRINGER — CORRODED (FUSELAGE)

PHX - DURING SCHEDULED D-CHECK, FOUND STRINGER CORRODED BEYOND LIMITS. REMOVED, FABRICATED AND REPLACED STRINGER FRAME PER SRM. (M)

Part: FRAME — CRACKED (FUSELAGE)

PHX - DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 480, STRINGER 21-22R CRACKED. REPAIRED FRAME PER SRM. (M)

Part: SKIN — DENTED (FUSELAGE)

PHX - DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN PANEL AT BS 197 TO 203, STRINGER 26-27R DENTED. REPAIRED PER SRM. (M)

Part: STRAP — CRACKED (FUSELAGE)

PHX - DURING SCHEDULED D-CHECK, FOUND STRAP AT BS 310-352, BUTTOCK LINE 24R CRACKED. INSTALLED NEW STRAP PER SRM. (M)

Part: SKIN — DENTED (FUSELAGE)

PHX - DURING SCHEDULED D-CHECK, MAINTENANCE FOUND DENT IN EXTERIOR SKIN. REPAIRED DENT PER SRM. (M)

Part: BATTERY — DISCHARGED (SMOKE BARRIER)

ANC - PRIOR TO FLT 20, THE EXIT TO REAR EXIT LIGHT ON THE SMOKE BARRIER WAS FLASHING. REPLACED BATTERY AND LIGHT OPERATED NORMALLY. (M)

Part: SIGN — INOPERATIVE (SMOKE BARRIER)

ANC - PRIOR TO FLIGHT 145 - THE SMOKE BARRIER EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. REPLACED THE EXIT IDENTIFIER AND BATTERY, LIGHT OPERATED NORMALLY. REF ASAA0010112. (M)

Part: BATTERY — DISCHARGED (SMOKE BARRIER)

ANC - PRIOR TO FLIGHT 145, THE SMOKE BARRIER EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. REPLACED THE EXIT IDENTIFIER AND BATTERY, LIGHT OPERATED NORMALLY. (M)

Part: RECEIVER — INOPERATIVE (PALLET 9-10)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT LIGHTS ON PALLET 9-10 WERE FOUND TO BE INOPERATIVE. REPLACED RECEIVER AND BATTERY PACK, LIGHTS OPERATED NORMALLY. (M)

Part: BATTERY PACK — DISCHARGED (PALLET 9-10)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT LIGHTS ON PALLET 9-10 WERE FOUND TO BE INOPERATIVE. REPALCED RECEIVER AND BATTERY PACK, LIGHTS OPERATED NORMALLY. REF ASAA0010108. (M)

Part: LOCK — DIRTY (PAX DOOR)

SEA - DURING MAINTENANCE CHECK, THE L1 DOOR GUST LOCK WAS FOUND TO BE DIFFICULT TO DEPRESS. CLEANED AND LUBRICATED GUST LOCK AND THE L1 DOOR GUST LOCK OPERATED NORMALLY. (M)

Part: BATTERY PACK — DISCHARGED (EMERGENCY EXIT)

SEA - DURING MAINTENANCE CHECK, THE LEFT WING EXTERIOR OVERWING EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. REPLACED BATTERY PACK AND LIGHT OPERATED NORMALLY. (M)

Part: BATTERY — DISCHARGED (ROW 4)

ANC - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT TRACK LIGHTS AT ROW 4 WERE FOUND TO BE INOPERATIVE. REPLACED BATTERY AND LIGHTS OPERATED NORMALLY. (M)

Part: LIGHT — INOPERATIVE (CABIN)

ANC - DURING MAINTENANCE CHECK, THE L2 DOOR EVACUATION SLIDE LIGHT WAS FOUND TO BE INOPERATIVE. RELEASED PER MEL 33-14A. SUBSEQUENTLY REPLACED LIGHT ASSEMBLY AND RELAMPED, LIGHT OPERATED NORMALLY. (M)

Part: CHARGER — OVERHEATED (MAIN BATTERY)

PSG - FLT 64 - EXPERIENCED SMOKE IN CABIN JUST PRIOR TO ARRIVAL INTO PSG. INSPECTION AND FOUND BATTERY CHARGER CIRCUIT BREAKER OPEN AND BATTERY VERY HOT. REPLACED BATTERY AND BATTERY CHARGER, BOTH OPERATED NORMALLY. RAN AC PACKS, NO SMOKE OR ODOR NOTED. (M)

Part: BATTERY — OVERHEATED (BATTERY BAY)

PSG - FLT 64 - EXPERIENCED SMOKE IN CABIN JUST PRIOR TO ARRIVAL INTO PSG. INSPECTION AND FOUND BATTERY CHARGER CIRCUIT BREAKER OPEN AND BATTERY VERY HOT. REPLACED BATTERY AND BATTERY CHARGER, BOTH OPERATED NORMALLY. RAN AC PACKS, NO SMOKE OR ODOR NOTED. REF ASAA0010058(M)

Part: BATTERY — DISCHARGED (ROW 18)

ANC - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS AT ROW 18 WOULD NOT SWITCH OFF. REPLACED RECEIVER AND BATTERY, LIGHTS OPERATED NORMALLY. (M)

Part: BATTERY — DISCHARGED (ROW 11)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT TRACK LIGHTS AT ROW 11 WOULD NOT TEST. REPLACED BATTERY AND LIGHTS OPERATED NORMALLY. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

SEA - AFTER RECON AND PRIOR TO FLIGHT 61, THE EMERGENCY EXIT TRACK LIGHTS WOULD NOT TEST PROPERLY. REPLACED BATTERY PACK AT AFT SEAT PALLET AND LIGHT OPERATED NORMALLY. (M)

Part: BATTERY — DISCHARGED (ROW 14)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT TRACK LIGHTS AT ROW 14 WERE FOUND TO BE INOPERATIVE. REPLACED BATTERY AND BATTERY PACK, LIGHTS OPERATED NORMALLY. (M)

Part: BATTERY PACK — DISCHARGED (ROW 14)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT TRACK LIGHTS AT ROW 14 WERE FOUND TO BE INOPERATIVE. REPLACED BATTERY AND BATTERY PACK. LIGHTS OPERATED NORMALLY. REFERENCE ASAA0010023. (M)

Part: BATTERY — DISCHARGED (SMOKE BARRIER)

SEA - DURING MAINTENANCE CHECK, THE FORWARD SMOKE BARRIER EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. REPLACED BATTERY AND LIGHTS OPERATED NORMALLY. (M)

Part: INTERCOSTAL — CORRODED (FUSELAGE)

PHX - DURING SCHEDULED D-CHECK, FOUND INTERCOSTAL AT STATION 927 TO 947.5, STRINGER 21R, CORRODED. REMOVED, FABRICATED AND REPLACED INTERCOSTAL PER SRM. (M)

Part: SPLICE — CORRODED (FUSELAGE)

PHX - DURING SCHEDULED D-CHECK, FOUND CORROSION ON STRINGER SPLICE. REMOVED AND REPLACED SPLICE PER SRM. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

PHX - DURING SCHEDULED D-CHECK, FOUND CORROSION ON CARGO COMPARTMENT FLOOR SUPPORT. REMOVED, FABRICATED AND REPLACED SECTION OF CARGO TRACK PER SRM. (M)

Part: BATTERY — DISCHARGED (CABIN)

ANC - PRIOR TO FLT 23, THE AFT GALLEY EMERGENCY EXIT LIGHT WAS FOUND TO BE FLICKERING. REPLACED THE BATTERY ASSEMBLY AND THE LIGHT OPERATED NORMALLY. (M)

Part: BATTERY — DISCHARGED (CABIN)

SEA - AFTER RECONFIGURATION AND PRIOR TO FLT 65, THE EMERGENCY EXIT LIGHTS AT ROW 12 WERE FOUND INOPERATIVE AND THE MID TRANSMITTER WAS NOT BEING RECEIVED. REPLACED RECEIVER AT ROW 12 AND THE BATTERY FOR THE MID CABIN TRANSMITTER, ALL OPERATED NORMALLY. REF: OPER CNTRL NR ASAA9910263.

Part: RECEIVER — INOPERATIVE (ROW 12)

SEA - AFTER RECONFIGURATION AND PRIOR TO FLT 65, THE EMERGENCY EXIT LIGHTS AT ROW 12 WERE FOUND INOPERATIVE AND THE MID TRANSMITTER WAS NOT BEING RECEIVED. REPLACED RECEIVER AT ROW 12 AND THE BATTERY FOR THE MID CABIN TRANSMITTER, ALL OPERATED NORMALLY. REF: OPER CNTRL NR 2000ZZZX253. (X)

Part: WIRE — DISCONNECTED (CABIN)

ANC - PRIOR TO F55, ONE SECTION OF EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATAIVE. REPAIRED WIRING AND THE LIGHTS OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

ANC - DURING RECON, PRIOR TO F41, AN AFT CABIN EMERGENCY EXIT FLOOR LIGHT WAS FOUND TO BE INOPERATIVE. REPAIRED LIGHT/WIRING AND THE LIGHT OPERATED NORMALLY. (M)

Part: LIGHT — INOPERATIVE (CABIN)

SEA - DURING MAINTENANCE CHECK, THE R1 DOOR OVERHEAD EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. REPLACED LIGHT ASSEMBLY AND THE LIGHT OPERATED NORMALLY. (X)

Part: WIRE — DISCONNECTED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE R1 OVERHEAD EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. RE-CONNECTED R-1 OVERHEAD LIGHT ASSEMBLY AND LIGHT OPERATED NORMALLY. (X)

Part: WIRE — BROKEN (ROW 17)

ANC - PRIOR TO FLIGHT 143, THE EMERGENCY EXIT FLOOR TRACK LIGHTS AT ROW 17 WERE FOUND TO BE INOPERATIVE. REPAIRED BROKEN WIRE AND LIGHTS OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (ROW 12)

ANC - DURING MAINTENANCE CHECK, FOUND 2 EACH EMERGENCY EXIT FLOOR TRACK LIGHTS INOPERATIVE AT ROW 12. REPAIRED WIRING AND LIGHTS OPERATED NORMALLY. (X)

Part: BATTERY PACK — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHT ON THE SMOKE BARRIER WAS FOUND INOPERATIVE. REPLACED BATTERY PACK AND LIGHTS OPERATED NORMALLY. (M)

Part: BATTERY — DISCHARGED (ROW 8)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHT AT ROW 8 WAS FOUND INOPERATIVE. REPLACED RECEIVER AND BATTERY, LIGHTS OPERATED NORMALLY. (M)

Part: RECEIVER — FAILED (ROW 8)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHT AT ROW 8 WAS FOUND INOPERATIVE. REPLACED RECEIVER AND BATTERY, LIGHTS OPERATED NORMALLY. (M)

Part: BATTERY — DISCHARGED (ROW 11)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT PACK AT ROW 11 IS ONLY SHOWING ONE OF THREE TRANSMITTER LED'S FLASHING. REPLACED BATTERY AND OPERATED NORMALLY. (M)

Part: BATTERY — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT SIGN ON REMOVABLE BULKHEAD WOULD NOT TEST PROPERLY. REPLACED BATTERY AND LIGHT OPERATED NORMALLY. (M)

Part: BATTERY — DISCHARGED (ROW 16)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS AT ROW 16 WOULD NOT SHUTOFF. REPLACED BATTERY AND LIGHTS OPERATED NORMALLY. (M)

Part: RETRACT MECH — ICED UP (NLG)

FLT 66 - YAK-JNU - FLIGHT DIVERTED TO SEA DUE TO NOSE LANDING GEAR TRANSIT LIGHT REMAINED ILLUMINATED AFTER DEPARTURE YAK WHEN LANDING GEAR LEVER WAS PLACED IN THE UP POSITION. WHEN GEAR LEVER WAS POSITIONED TO OFF, THE NOSE LANDING GEAR FREE FELL TO AN EXTENDED POSITION. CYCLED GEAR TO THE DOWN POSITION AND THREE GREEN LIGHTS ILLUMINATED. PLACED GEAR HANDLE IN THE UP POSITION AND THE NOSE LANDING GEAR TRANSIT LIGHT REMAINED ILLUMINATED. MADE UNSCHEDULED LANDING IN YVR DUE TO MEDICAL EMERGENCY ONBOARD AND LANDED WITHOUT INCIDENT. ICE WAS NOTED IN NOSE LANDING GEAR AREA. FERRIED AIRCRAFT FROM YVR TO SEA FOR TROUBLESHOOTING. AIRCRAFT LANDED IN SEA WITHOUT INCIDENT. INSPECTED NOSE LANDING GEAR SYSTEM, PERF

Part: BATTERY PACK — DISCHARGED (ROW 2)

ANC - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE AT ROW 2. REPLACED BATTERY PACK AND LIGHTS OPERATED NORMALLY. (M)

Part: BATTERY — DISCHARGED (ROW 12/18)

SEA - PRIOR TO FLIGHT 61, THE NUMEROUS EMERGENCY EXIT TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. REPLACED BATTERY AT ROW 12 AND BATTERY AND RECEIVER AT ROW 18, LIGHTS OPERATED NORMALLY. (M)

Part: BATTERY — DISCHARGED (PALLET 6-8)

ANC - DURING MAINTENANCE CHECK, THE EMERGENCY TRACK LIGHTS AT PALLET 6-8 WERE OPERATING ERRATIC. REPLACED RECEIVER AND BATTERY, LIGHTS OPERATED NORMALLY. (M)

Part: RECEIVER — INOPERATIVE (PALLET 6-8)

ANC - DURING MAINTENANCE CHECK, THE EMERGENCY TRACK LIGHTS AT PALLET 6-8 WERE OPERATING ERRATIC. REPLACED RECEIVER AND BATTERY, LIGHTS OPERATED NORMALLY. (M)

Part: SWITCH — ICED UP (NLG)

ANC - FLT 65 - WHEN SELECTING THE OFF POSITION WITH THE GEAR LEVER, THE NOSE GEAR EXTENDS. WHEN SELECTING THE UP POSITION, THE RED NOSE GEAR LIGHT ILLUMINATES, BUT THE NOSE GEAR AND MAIN GEAR RETRACTED. INSPECTED AND FOUND THE NOSE GEAR AND GRAVEL DEFLECTOR SLED ICED UP. DEICED NOSE GEAR AND SKIN. JACKED AND SWUNG GEAR, OPERATED NORMALLY. (M)

Part: LIGHT — INOPERATIVE (CABIN)

SEA - DURING MAINTENANCE CHECK, THE SMOKE BARRIER LIGHT WAS FOUND TO BE INOPERATIVE. REPLACED LIGHT ASSEMBLY AND LIGHT OPERATED NORMALLY. (M)

Part: BATTERY CHARGER — INOPERATIVE (CABIN)

ANC - PRIOR TO FLIGHT 51, THE LAST THREE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. REPLACED BATTERY CHARGER AND LIGHTS OPERATED NORMALLY. (M)

Part: BATTERY — DISCHARGED (ROW 18)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE AT ROW 18. REPLACED BATTERY AND LIGHTS OPERATED NORMALLY. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

ANC - PRIOR TO FLIGHT 145, THE EMERGENCY EXIT LIGHT ON BULKHEAD WAS FOUND TO NOT BE TESTING PROPERLY. REPLACED BATTERY PACK AND LIGHT OPERATED NORMALLY. (M)

Part: WIRE — BROKEN (ROW 20)

SEA - FLT 42 - PRIOR TO DEPARTURE, THE EMERGENCY EXIT FLOOR TRACK LIGHT AT ROW 20 WAS FOUND INOPERATIVE. RELAMPED AND REPAIRED BROKEN WIRING, LIGHT OPERATED NORMALLY. (M)

Part: LIGHT — MISSING (CABIN)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT LIGHT AT ROW 9 WAS FOUND TO BE MISSING. REPLACED LIGHT ASSEMBLY AND LENS, AND LIGHT OPERATED NORMALLY. (M)

Part: FLOORBEAM — CORRODED (BS 947)

SEA - DURING C-CHECK, FOUND THE FLOORBEAM CORRODED AT STATION 947, LBL 29.5 TO LBL 35.62. REPAIRED PER EA 5310-01590 AND BOEING TELEX ASA-SEA-98-0275RR. (M)

Part: BATTERY — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE SMOKE BARRIER EMERGENCY EXIT LIGHT WOULD NOT TEST. REPLACED BATTERY AND LIGHT OPERATED NORMALLY. (M)

Part: BATTERY — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE FORWARD WINDSCREEN 'EXIT TO REAR' LIGHT WAS FOUND TO BE INOPERATIVE. REPLACED BATTERY AND LIGHT OPERATED NORMALLY. (M)

Part: BATTERY — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE SMOKE BARRIER EMEREGNCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. REPLACED BATTERY AND LIGHT OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

ANC - DURING MAINTENANCE CHECK, ONE EMERGENCY EXIT FLOOR TRACK LIGHT WAS FOUND TO BE INOPERATIVE AT ROW 18. RECONNECTED WIRING AND LIGHTS OPERATED NORMALLY. (M)

Part: BEARING — DRY (SELECTOR VALVE)

ANC - FLT 52 - AFTER TAKEOFF, GEAR HANDLE WOULD NOT MOVE TO OFF OR DOWN POSITION. AIRCRAFT RETURNED TO ANC AND LANDED WITHOUT INCIDENT. INSPECTED AND FOUND GEAR SELECTOR VALVE CONTROL QUADRANT UPPER BEARING DRY, LUBRICATED SAME. INSPECTED CABLE RUN AND PULLEYS FROM GEAR HANDLE TO SELECTOR VALVE, NO DEFECTS NOTED. LUBRICATED PULLEYS. COMPLETED EXTENSION AND RETRACTION TEST AND GEAR OPERATED NORMALLY. (X)

Part: BATTERY PACK — DISCHARGED (CABIN)

ANC - DURING RECON, THE EMERGENCY EXIT FLOOR TRACK LIGHTS AT PALLET NR 4-8 WERE FOUND TO BE INOPERATIVE. REPLACED BATTERY PACK AND LIGHTS OPERATED NORMALLY. (M)

Part: BATTERY PACK — DISCHARGED (PALLET 9-2)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT TRACK LIGHTS WERE FOUND TO BE INOPERATIVE AT PALLET POSITIONS 9-2 AND 10-6. REPLACED BOTH BATTERY PACKS AND THE RECEIVER ON PALLET 9-2 AND LIGHTS OPERATED NORMALLY. (M)

Part: RECEIVER — INOPERATIVE (PALLET 10-6)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT TRACK LIGHTS WERE FOUND TO BE INOPERATIVE AT PALLET POSITIONS 9-2 AND 10-6. REPLACED BOTH BATTERY PACKS AND THE RECEIVER ON PALLET 9-2 AND LIGHTS OPERATED NORMALLY. (M)

Part: BATTERY — DISCHARGED (CABIN)

SEA - PRIOR TO FLIGHT 61, THE SMOKE BARRIER EXIT LIGHT WAS FOUND TO STAY ILLUMINATED. REPLACED BATTERY AND LIGHT OPERATED NORMALLY. (M)

Part: BEARING — BROKEN (AFT AIRSTAIR)

ANC - DURING MAINTENANCE CHECK, FOUND THE AFT AIRSTAIRS WOULD NOT EXTEND IN EMERGENCY. REPLACED BROKEN CAM FOLLOWER BEARING AND EMERGENCY EXTENSION OPERATED NORMALLY. TT: 37,465 HOURS. TC: 33,390. (X)

Part: BATTERY PACK — DISCHARGED (CABIN)

ANC - FLT 148 - DURING FLT, ONE SECTION OF THE EMERGENCY EXIT FLOOR TRACK LIGHTS ILLUMINATED AT ROWS 16 AND 17. REPLACED BATTERY PACK AND THE EMERGENCY EXIT FLOOR TRACK LIGHTS OPERATED NORMALLY. (M)

Part: BATTERY PACKS — DISCHARGED (CABIN)

SEA - FLT 61 - DURING RECON PRIOR TO FLIGHT, THE EMERGENCY EXIT TRACK LIGHTS WERE FOUND TO BE INOPERATIVE AT ROW S1-5 AND 12-13. REPLACED BATTERY PACK AND LIGHTS OPERATED NORMALLY. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

ANC - FLT 57 - PRIOR TO FLIGHT THE EMERGENCY EXIT TRACK LIGHTS ON SEAT PALLET NR 1 WOULD NOT EXTINGUISH. REPLACED BATTERY PACK AND THE LIGHTS OPERATED NORMALLY. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE, THE R2 AND L2 EXTERIOR EMERGENCY EXIT LIGHTS WERE FOUND TO BE INOPERATIVE. REPLACED BATTERY PACK AND LIGHTS OPERATED NORMALLY. (M)

Part: LIGHT — INOPERATIVE (CABIN)

SEA - DURING SCHEDULED MAINTENANCE, THE FORWARD EMERGENCY ESCAPE SLIDE LIGHTS WERE FOUND TO BE INOPERATIVE. REPLACED THE L1 AND R1 EMERGENCY ESCAPE SLIDE LIGHT ASSEMBLIES AND LIGHTS OPERATED NORMALLY. (M)

Part: SOCKET — WET (CABIN)

SEA - DURING MAINTENANCE, THE R2 AND L2 EMERGENCY ESCAPE SLIDE LIGHTS WERE FOUND TO BE INOPERATIVE. REMOVED WATER FROM THE L2 LIGHT SOCKET AND LIGHTS OPERATED NORMALLY. (M)

Part: INFLATION BOTTLE — LOW PRESSURE (L1 SLIDE)

ANC - DURING MAINTENANCE CHECK, THE L1 DOOR EMERGENCY EVACUATION SLIDE INFLATION BOTTLE PRESSURE WAS FOUND LOW. REPLACED THE EMERGENCY EVACUATION SLIDE. (M)

Part: BATTERY — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACKS LIGHTS WERE FOUND TO BE INOPERATIVE AT ROW 18. REPLACED BATTERY AND LIGHTS OPERATED NORMALLY. (M)

Part: FIRE MODULE — INOPERATIVE (WHEEL WELL)

ANC - FLT 55 - UPON DESCENT INTO ANC, THE WHEEL WELL FIRE WARNING LIGHT ILLUMINATED INTERMITTENTLY. FIRE WARNING TEST NORMAL AND AIRCRAFT LANDED WITHOUT INCIDENT. INSPECTED WHEEL WELL WIRING AND DETECTION LOOP, NO FAULTS FOUND. REPLACED WHEEL WELL FIRE DETECTION MODULE AND SYSTEM OPS CHECKS NORMAL. (M)

Part: BATTERY PACK — DISCHARGED (CARGO COMPT)

SEA - DURING MAINTENANCE, THE FWD PALLET EMERGENCY TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. REPLACED BATTERY PACK AND LIGHTS OPERATED NORMALLY. (M)

Part: RECEIVER — INOPERATIVE (CABIN)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHT RECEIVER WAS FOUND TO BE INOPERATIVE AT ROW 16. REPLACED RECEIVER AND BATTERY PACK AND LIGHTS OPERATED NORMALLY. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHT RECEIVER WAS FOUND TO BE INOPERATIVE AT ROW 16. REPLACED RECEIVER AND BATTERY PACK AND LIGHTS OPERATED NORMALLY. REFERENCE ASAA9610113.

Part: BATTERY PACK — DEFECTIVE (CABIN)

SEA - DURING MAINTENANCE CHECK, THE RIGHT EXTERIOR OVERWING AND AFT WING EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. REPLACED BATTERY PACK AND LIGHTS OPERATED NORMALLY. (M)

Part: MODULE — MALFUNCTIONED (NLG)

SEA - FLT 896 - DURING APPROACH CREW REPORTED THAT THE NOSE LANDING GEAR FAILED TO EXTEND ON FIRST ATTEMPT. RECYCLED AND GEAR EXTENDED NORMALLY. LANDED WITHOUT INCIDENT. REPLACED NOSE LANDING GEAR MODULE, PERFORMED GEAR RETRACTION AND GEAR OPERATED NORMALLY. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE AT ROW 18. REPLACED BATTERY PACK AND LIGHTS OPERATED NORMALLY. (M)

Part: SAFETY SENSOR — OUT OF ADJUST (LANDING GEAR)

SEA - ATB OF FLT 9301 - ALL THREE LANDING GEARS FAILED TO RETRACT AFTER TAKEOFF, GEAR HANDLE ONLY WENT TO 'OFF' POSITION. LANDED WITHOUT INCIDENT. ADJUSTED AIR SAFETY SENSOR GAP, COMPLETED GEAR SWING AND GEAR OPERATED NORMALLY. (M)

Part: FRAME — CORRODED (BS 227)

SEA - DURING D-CHECK, CORROSION WAS FOUND ON THE BULKHEAD FRAME LOWER SECTION AT BS 227, BL 0. REPAIRED PER EA 531001421 AND BOEING TELEX ASA-SEA-960136RR. (W)

Part: FLOOR BEAM — CORRODED (BS 787)

SEA - DURING D-CHECK, CORROSION WAS FOUND ON THE FLOOR BEAM LOWER FLANGE, BS 787 AT EACH FASTENER HOLE USED TO SECURE THE CEILING PANELS IN THE AFT CARGO COMPARTMENT. REPAIRED PER EA 531001415 AND BOEING TELEX ASA-SEA 960108RR. (W)

Part: FLOOR BEAM — CORRODED (BS 847)

SEA - DURING D-CHECK, CORROSION WAS FOUND ON THE FLOOR BEAM LOWER FLANGE, BS 847 AT EACH FASTENER HOLE USED TO SECURE THE CEILING PANELS IN THE AFT CARGO COMPARTMENT. REPAIRED PER EA 531001416 AND BOEING TELEX ASA-SEA 960108RR. (W)

Part: FLOOR BEAM — CORRODED (BS 867)

SEA - DURING D-CHECK, CORROSION WAS FOUND ON THE FLOOR BEAM LOWER FLANGE BS 867 AT EACH FASTENER HOLE USED TO SECURE THE CEILING PANELS FOR THE AFT CARGO COMPARTMENT. REPAIRED PER EA 531001414 AND BOEING TELEX ASA-SEA 960108RR. (W)

Part: FLOOR BEAM — CORRODED (BS 500B)

SEA - DURING D-CHECK, CORROSION WAS FOUND ON THE FLOOR BEAM AT BS 500B LBL 8 TO 43 ON THE UPPER SURFACE OF THE LOWER FORWARD FLANGE. CORROSION IS AROUND THE FASTENER HOLES USED TO SECURE THE CEILING PANELS FOR THE LOWER CARGO COMPARTMENT. REPAIRED PER EA 531001401 AND BOEING TELEX ASA-SEA 960076RR. (W)

Part: FLOOR BEAM — CORRODED (BS 967)

SEA - DURING D-CHECK, CORROSION FOUND ON THE UPPER CHORD FLANGE OF THE FLOOR BEAM AT RBL 24.5 AND RBL 45, BS 967. DUE TO PREVIOUS REPAIRS THE FLANGE MUST BE RESTORED TO PROVIDE FUTURE ACCOMPLISHMENT OF SRM REPAIRS. REPAIRED PER EA 5310-01407 AND BOEING TELEX ASA-SEA-96-0086RR.

Part: STRINGER — CRACKED (BS 500B)

SEA - DURING D-CHECK A CRACK WAS FOUND AT THE ENDS OF STRINGER 16R, BS 500B WHICH TERMINATES AT THE OVERWING LIGHT. REPAIRED PER EA 5310-01400 AND BOEING SB 737-53-1145. REFERENCE ASAA9610031.

Part: FLOOR BEAM — CORRODED (BS 578)

SEA - DURING D-CHECK, THE LONGITUDINAL FLOOR BEAM INBOARD FLANGE AT RBL 45.5, BS 578 WAS FOUND CORRODED. REPAIRED PER EA 5310-01403 AND BOEING TELEX ASA-SEA-96-0061RR. (M)

Part: FLOOR BEAM — CORRODED (BS 727B)

SEA - DURING D-CHECK, THE FLOOR BEAM AT BS 727B WAS FOUND TO HAVE CORROSIO ON THE UPPER CHORD FORWARD AND AFT FLANGE BETWEEN RBL 15 TO RBL 55, CONCENTRATED AT A FASTENER HOLE ON THE UPPER SURFACE OF THE FLANGE. REPAIRED PER EA 5310-01406 AND BOEING TELEX ASA-SEA-96-0077RR. (M)

Part: FLOOR BEAM — CORRODED (BS 600-727)

SEA - DURING D-CHECK CORROSION WAS FOUND ON THE LONGITUDINAL FLOOR BEAM INBOARD FLANGE AT BL 0, BS 600, BS 680, BS 687, AND AT RBL 25, BS 727. REPAIRED PER EA 5310-01412 AND BOEING TELEX ASA-SEA-96-0098. (M)

Part: KEEL BEAM — CORRODED (BS 716/720)

SEA - DURING D-CHECK, THE KEEL BEAM AT LBL 6.30 AND RBL 6.30, BL 716 AND 720 WAS FOUND TO BE CORRODED. REPAIRED PER EA 5310-01401 AND BOEING TELEX ASA-SEA-96-0055RR. (M)

Part: FLOOR BEAM — CRACKED (BS 520)

SEA - DURING D-CHECK, A CRACK WAS FOUND IN THE RADIUS OF THE UPPER FLANGE TO WEB OF THE FLOOR BEAM AT BS 520, RBL 24.75. REPAIRED PER EA 5320-01260 AND BOEING SB 737-53-1120. (M)

Part: STRINGER — CRACKED (BS 500B)

SEA - DURING D-CHECK A CRACK WAS FOUND AT THE ENDS OF STRINGER 16R, BS 500B WHICH TERMINATES AT THE OVERWING LIGHT. REPAIRED PER EA 5310-01400 AND BOEING SB 737-53-1145. (M)

Part: SUPPORT FITTING — CRACKED (NR 2 ENGINE)

SEA - DURING D-CHECK, THE NR 2 ENGINE OUTBOARD THRUST LINK AFT SUPPORT FITTING WAS FOUND TO HAVE A GOUGE ON THE LOWER SURFACE. AFTER BLENDING OF THE GOUGED AREA, A CRACK WAS FOUND AT THE BOTTOM OF THE BLEND AREA. REPLACED SUPPORT FITTING. (M)

Part: UPPER BEAM — CRACKED (CARGO DOOR)

SEA - DURING D-CHECK, A 1 INCH CRACK WAS FOUND IN THE MAIN CARGO DOOR UPPER BEAM 1.3 INCHES FORWARD OF THE MAIN CARGO DOOR ACTUATOR ATTACHMENT FITTING, BS 465.5. REPAIRED PER EA 5230-01056 AND BOEING TELEX ASA-SEA-96-0069RR. (M)

Part: BATTERY — DISCHARGED (CABIN)

ANC - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS ON SEVERAL PALLETS WERE FOUND INOPERATIVE. REPLACED BATTERIES AND LIGHTS OPERATED NORMALLY. (M)

Part: MODULE — FAILED (NLG)

ANC - FLT NR 65 - DURING APPROACH CREW REPORTED, THE NOSE LANDING GEAR FAILED TO EXTEND ON FIRST ATTEMPT. RECYCLED AND GEAR EXTENDED NORMALLY. LANDED WITHOUT INCIDENT. REPLACED NOSE LANDING GEAR MODULE, PERFORMED GEAR RETRACTION AND OPERATED NORMALLY. (M)

Part: CYLINDER — FAILED (NLG)

ANC - FLIGHT 44 - DURING APPROACH, THE NOSE LANDING GEAR FAILED TO EXTEND. RECYCLED GEAR AND ALL LANDING GEAR EXTENDED NORMALLY. LANDED WITHOUT INCIDENT. CLEANED AND LUBED NOSE LANDING GEAR ASSEMBLY. REPLACED NOSE LANDING GEAR TRANSFER CYLINDER, PERFORMED GEAR RETRACTION, SERVICED STRUT AND OPERATED NORMALLY. (M)

Part: EEL BATT PACK — DISCHARGED (CABIN)

ANC - DURING MAINTENANCE CHECK, THE INTERIOR OVERWING EMERGENCY EXIT LIGHTS FLASHED ON AND OFF WHEN ACTIVATED. REPLACED BATTERY PACK AND LIGHTS OPERATED NORMALLY. (M)

Part: EEL BATTERY PACK — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE AT ROWS 6 AND 7. REPLACED BATTERY BACK AND LIGHTS OPERATED NORMALLY. (W)

Part: EEL HOUSING RCVR — INOPERATIVE (CABIN)

SEA - DURING MAINTENANCE CHECK, TWO EMERGENCY EXIT FLOOR TRACK LIGHTS AT ROW 16 WERE FOUND INOPERATIVE. REPLACED FLOOR PROXIMITY LIGHT HOUSING RECEIVER ASSEMBLY AND LIGHTS OPERATED NORMALLY. (W)

Part: EEL BATTERY — DISCHARGED (FIRST PALLET)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY TRACK LIGHTS WERE FOUND INOPERATIVE ON THE FIRST PALLET. REPLACED BATTERY AND LIGHTS OPERATED NORMALLY. (W)

Part: EEL ASSY — INOPERATIVE (BULKHEAD)

ANC - DURING MAINTENANCE CHECK, THE BULKHEAD EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. REPLACED LIGHT ASSEMBLY AND OPERATED NORMALLY. (W)

Part: RETRACT MECH — FAILED (NLG)

ANC - FLT 145 - ON ARRIVAL, THE CREW REPORTED THE NLG FAILED TO EXTEND WHEN LANDING GEAR HANDLE WAS PLACED TO DOWN. PERFORMED MANUAL EXTENSION AND LANDED WITHOUT INCIDENT. CLEANED AND INSPECTED NLG, NO DEFECTS NOTED. PERFORMED EXTENSION AND RETRACTION TEST, NO DISCREPANCIES NOTED. (W)

Part: EEL BATTERY — DISCHARGED (CABIN)

SEA - CHECK, SMOKE BARRIER EXIT LIGHTS INOP. MAINTENANCE REPLACED BATTERY. (W)

Part: EEL RECEIVER — INOP (CABIN)

SEA -CHECK, TRACK LIGHTS INOP AT ROW 11. MAINTENANCE REPLACED RECEIVER ASSY AT ROW 11. (W)

Part: EEL BATT PACK — DEFECTIVE (CABIN)

ANC - FLT 51 - PRIOR TO DEPARTURE, CREW REPORTED EMERGENCY EXIT LIGHTS ILLUMINATE WITH THE EMERGENCY LIGHT SWITCH IN 'OFF' ARM, OR 'ON' POSITIONS. REPLACED BATTERY PACK AT ROW 10 AND LIGHTS OPERATED NORMALLY. (W)

Part: EEL TRANSMITTER — WEAK (CABIN)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS AT ROW 16 WOULD NOT ILLUMINATE. REPLACED AFT TRACK LIGHTING TRANSMITTER AND LIGHTS OPERATED NORMALLY. (W)

Part: EEL TRACK — DEFECTIVE (CABIN)

SEA - DURING C-CHECK, THE AFT SECTION OF EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. REPLACED FLOOR TRACKS AND REWIRED TRACK SECTION, LIGHTS OPERATED NORMALLY. (W)