N747AS

Part: HINGE — LOOSE (L1 DOOR) · airframe 56,859 hrs · 48,970 cycles

L1 DOOR DOES NOT CLOSE NORMALLY. FOUND L1 DOOR TOP HINGE PLATE LOOSE. TIGHTENED BOLTS LUBED DOOR CHECKS OKAY.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHT) · airframe 56,666 hrs · 48,776 cycles

OUTSIDE EMERGENCY EXIT LIGHT INOP (LEFT OVERWING). REPLACED LT OVERWING BATTERY PACK PER AMM.

Part: GLOWSTRIP — DETACHED (AFT PAX CABIN) · airframe 56,659 hrs · 48,768 cycles

DURING DEPLANING EMERGENCY PHOTOLUMINSCENT LIGHT STRIP IN AFT CABIN DETACHED FROM FLOOR. REPLACED SECTION OF PHOTOLUMINSCENT LIGHT STRIP IN FIXED PORTION OF AFT CABIN.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,244 hrs · 48,352 cycles

THREE INCH CRACK IN FUSELAGE SKIN JUST BELOW NUMBER 2 WINDOW ON RIGHT SIDE OF AIRCRAFT. REPAIRED PER SRM 53-30-3 REPAIR COMPLETED WITH DOUBLER AND TRIPLER FABRICATED AND INSTALLED.

Part: SEAL — WORN (AFT CARGO DOOR) · airframe 55,393 hrs · 47,572 cycles

AT FL 240, LOST CABIN ALT CONTROL. RT PACK WAS ON MEL. FOUND AFT CARGO DOOR SEAL BLOWN OUT. CLEARED RT PACK MEL. REPLACED AFT CARGO DOOR SEAL PRESS CHK GOOD. FWD OUTFLOW VLV INOP OPEN REPLACED FWD OUTFLOW VLV.

Part: SKIN — CRACKED (FS 749-752)

YXX - BS 749 TO 752 AT STRINGER 19 ON RIGHT SIDE, CRACK IN FUSSELAGE SKIN. REPAIRED PER ASA T/C 18150000. (M)

Part: SKIN — DENTED (FORE FLAP)

OKC - C-CHECK DENT WITH CREASE, CENTER OF LEFT INBOARD FORE FLAP, UPPER SURFACE. FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 51-40-20. (M)

Part: SKIN — CHAFED (TE FLAP) · airframe 52,097 hrs · 44,561 cycles

OKC - FOUND LEFT WING TRAILING EDGE OUTBOARD MID FLAP HAS TWO CHAFED AREAS IN SKIN, LOWER SURFACE, AREA AT SECOND TRACK FAIRING. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR FILLERS AND DOUBLERS IAW AS EA AND AAR EA. (M)

Part: SKIN — DENTED (MID FLAP) · airframe 52,098 hrs · 44,561 cycles

OKC - DURING C-CHECK, LEFT OUTBOARD MID FLAP UPPER SURFACE HAS A DENT INBOARD OF NR 1 FLAP SPINDLE. FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 51-40-20. (M)

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 52,097 hrs · 44,561 cycles

OKC - FOUND INTERCOSTAL CORRODED. REMOVED DAMAGED INTERCOSTAL, FABRICATED AND INSTALLED REPLACEMENT INTERCOSTAL IAW SRM. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

LONGITUDINAL BEAM TRACK HAS CORROSION IN THE INBOARD FLANGE BOTTOM SIDE AROUND SCREW HOLES. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR FILLERS, STRAPS, AND TRIPPER STRAP IAW AS EA AND AAR EA. (M)

Part: FITTING — CHAFED (FUSELAGE) · airframe 52,097 hrs · 44,561 cycles

AFT CARGO COMPARTMENT MOST LOWER FORWARD DOOR STOP FITTING CHAFED/WORN. REMOVED DAMAGED FITTINGS, ORDERED AND INSTALLED NEW FITTINGS IAW EA. (M)

Part: DOOR FRAME — CRACKED (CARGO DOOR)

OKC - AFT CARGO DOOR FRAME CRACKED AT FORWARD LOWER CORNER. REMOVED DAMAGED FORWARD LOWER DOOR FRAME CORNER, ORDERED AND INSTALLED A NEW FRAME CORNER IAW SRM. (M)

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 52,097 hrs · 44,561 cycles

OKC - INTERCOSTAL CRACKED. REMOVED DAMAGED INTERCOSTAL, FABRICATED AND INSTALLED REPLACEMENT INTERCOSTAL IAW SRM. (M)

Part: FRAME — CORRODED (FUSELAGE) · airframe 52,097 hrs · 44,561 cycles

OKC - FRAME STATION 767 CORRODED BETWEEN STRINGER 26L AND 26R. REMOVED DAMAGE, FABRICATED AND INSTALLED A REPAIR SHEAR TIE, DOUBLERS, RADIUS FILLERS AND SHIMS, IAW SRM. (M)

Part: JACKSCREW — CHAFED (RT WING TE FLAP) · airframe 52,097 hrs · 44,561 cycles

OKC - FOUND RIGHT WING OUTBOARD MID FLAP BEHIND OUTBOARD JACKSCREW IS CHAFED. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLERS AND FILLED BLENDED AREA IAW AS AND AAR EA. (M)

Part: BEAM — CORRODED (FUSELAGE) · airframe 52,097 hrs · 44,561 cycles

OKC - LONGITUDINAL BEAM BETWEEN STATION 540-727B BL 0, HAS CORROSION. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR STRAP AND FILLERS BLENDED AREA IAW AS AND AAR EA. (M)

Part: STRINGER — CORRODED (FUSELAGE) · airframe 52,097 hrs · 44,561 cycles

OKC - AFT CARGO PIT BILGE AREA AT STRINGER 27R HAS BLOWN OUT CORROSION BETWEEN STATION 947 AND 967. REMOVED DAMAGED SECTION, FABRICATED AND INSTALLED REPAIR SECTION AND SPLICED IAW SRM. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 52,097 hrs · 44,561 cycles

OKC - FLOORBEAM STATION 500A RBL 24 TO 63 IC CORRODED. REMOVED EXISTING REPAIR STRAPS, REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR STRAPS IAW AS AND AAR EA. (M)

Part: STRINGER — CORRODED (FUSELAGE)

OKC - FOUND CORROSION UNDER AND AROUND NUTPLATES, STRINGER 27L INSIDE STRINGER CHANNEL STATION 500. REMOVED DAMAGED SECTION, FABRICATED AND INSTALLED REPLACEMENT SECTION, REPAIR ANGLE AND INSTALLED A REPLACEMENT STRINGER CLIP IAW DRAWING 69-35352. (M)

Part: SHEAR TIE — GOUGED (FUSELAGE) · airframe 52,097 hrs · 44,561 cycles

OKC - SHEAR TIE AT STATION 727B AND STRINGER 18 GOUGED IN RADIUS. REMOVED DAMAGED SHEAR TIE, FABRICATED AND INSTALLED REPLACEMENT IAW SRM. (M)

Part: SKIN — LIGHTNING STRIKE (FUSELAGE)

OKC - FOUND STATION 188 STRINGER 17L HAS LIGHTING STRIKE DAMAGE THAT IS OUT OF LIMITS IAW SRM. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR FILLERS, DOUBLERS AND TRIPLER IAW SRM. (M)

Part: FRAME — CORRODED (FUSELAGE) · airframe 52,097 hrs · 44,561 cycles

OKC - FOUND CORROSION STATION 500 UNDER NUTPLATE AT STRINGER 27R INSIDE LONGERON CHANNEL. REMOVED DAMAGED SECTION, FABRICATED AND INSTALLED A REPLACEMENT SECTION, ANGLE, AND CHANNEL IAW SRM. (M)

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 52,097 hrs · 44,561 cycles

OKC - FOUND AFT PIT, LEFT HAND SIDE STATION 927 AND 947 AT 24L STRINGER CLIPS ARE CORRODED. REMOVED DAMAGED STRINGER CLIPS, FABRICATED AND INSTALLED REPLACEMENT STRINGER CLIPS IAW DRAWING 69-35364 AND SRM. (M)

Part: SKIN — CORRODED (FUSELAGE) · airframe 52,097 hrs · 44,561 cycles

OKC - FUSELAGE EXTERIOR LOWER SKIN CORRODED FROM STATION 927 TO 947 BETWEEN 26L AND 27L. REMOVED DAMAGE, AND EXISTING DOUBLER, FABRICATED AND INSTALLED REPAIR FILLERS AND DOUBLERS IAW AS AND AAR EA. (M)

Part: STRINGER — CRACKED (FUSELAGE) · airframe 52,097 hrs · 44,561 cycles

OKC - FOUND AFT PIT LEFT SIDE AT LBL 24 FROM BS 907-947 STRINGER IS CORRODED AND CRACKED. REMOVED DAMAGED SECTION OF STRINGER, FABRICATED AND INSTALLED REPLACEMENT SECTION IAW SRM. (M)

Part: BEAM — CORRODED (FUSELAGE) · airframe 52,097 hrs · 44,561 cycles

OKC - LONGITUDINAL BEAM HAS CORROSION. REMOVED DAMAGE, COMPLIED WITH HFEC INSPECTION AND NO DEFECTS NOTED. FLAP PEENED AFFECTED AREA. FABRICATED AND INSTALLED REPAIR FILLERS, STRAPS, AND WASHERS IAW EA. (M)

Part: SKIN — LIGHTNING STRIKE (FUSELAGE) · airframe 52,097 hrs · 44,561 cycles

OKC - FOUND LIGHTNING STRIKES OUT OF LIMITS. REMOVED DAMAGE, COMPLIED WITH HFEC INSPECTION, NO DEFECTS NOTED. FABRICATED AND INSTALLED REPAIR FILLERS, DOUBLER, AND PLATES IAW EA. (M)

Part: FRAME — CORRODED (FUSELAGE) · airframe 52,097 hrs · 44,561 cycles

OKC - FOUND FRAME CORRODED BETWEEN 26 AND 20L AROUND NUMEROUS NUTPLATES. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 52,097 hrs · 44,561 cycles

OKC - FLOORBEAM HAS CORROSION ON TOP. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR T-CHORD, ANGLES, STRAPS AND FILLERS IAW EA. (M)

Part: STRINGER — CORRODED (FUSELAGE) · airframe 52,097 hrs · 44,561 cycles

OKC - FOUND AFT PIT STATION STRINGER RT IS CORRODED. REMOVED DAMAGED SECTION FABRICATED AND INSTALLED REPLACEMENT SECTION IAW SRM. (M)

Part: SKIN — LIGHTNING STRIKE (FUSELAGE) · airframe 52,097 hrs · 44,561 cycles

OKC - LIGHTNING STRIKES OUT OF LIMITS PER SRM. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR FILLER, DOUBLER AND TRIPLER PER SRM. (M)

Part: ANGLE — CORRODED (FUSELAGE) · airframe 52,097 hrs · 44,561 cycles

OKC - FOUND ZEE ANGLE CORRODED UNDER R1 DOOR THRESHOLD. REMOVED DAMAGED ANGLE, FABRICATED AND INSTALLED REPLACEMENT ANGLE IAW SRM. (M)

Part: FRAME — CORRODED (FUSELAGE) · airframe 52,097 hrs · 44,561 cycles

OKC - FOUND FRAME CORRODED ALL AROUND NUTPLATES IN INTERIOR CAVITY. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR ANGLE PER SRM. (M)

Part: SHEAR TIE — GOUGED (FUSELAGE) · airframe 52,097 hrs · 44,561 cycles

OKC - FOUND FRAME GOUGED ON UPPER FLANGE AFT RADIUS BETWEEN STRINGERS. REMOVED DAMAGED SHEAR-TIE, FABRICATED AND INSTALLED REPAIR FILLERS AND ANGLES PER SRM. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 52,097 hrs · 44,561 cycles

OKC - FLOORBEAM HAS CORROSION. REMOVED DAMAGE, REMOVED PRE-EXISTING REPAIRS, FLAT PEENED, TREATED, PRIMED, TOPCOATED, AND REINSTALLED PRE-EXISTING REPAIRS IAW EA. (M)

Part: SKIN — CHAFED (TE FLAP) · airframe 52,097 hrs · 44,561 cycles

OKC - FOUND LEFT WING T/E OUTBOARD MID FLAP HAS TWO CHAFING AREAS IN SKIN, LOWR SURFACE, AREA AT SECOND TRACK FAIRING. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR FILLERS AND DOUBLERS IAW EA. (M)

Part: STRINGER — CORRODED (FUSELAGE) · airframe 52,097 hrs · 44,561 cycles

OKC - AFT PIT BILGE AREA HAS CORROSION IN STRINGER, AND EXTERIOR SIDES AT FRAME. REMOVED DAMAGED SECTION, FABRICATED AND INSTALLED REPLACEMENT SECTION OF STRINGER IAW SRM. (M)

Part: SHEAR TIE — GOUGED (FUSELAGE) · airframe 53,097 hrs · 44,561 cycles

OKC - SHEAR TIE GOUGED IN RADIUS. REMOVED DAMAGED SHEAR TIE, FABRICATED REPLACEMENT SHEAR TIE PER SRM. (M)

Part: DOOR — DENTED (E/E BAY) · airframe 52,097 hrs · 44,561 cycles

OKC - FOUND E/E DOOR DENTED TWO PLACES ALONG OUTER EDGE. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR FILLERS AND DOUBLER IAW SRM. (M)

Part: FRAME — GOUGED (FUSELAGE) · airframe 52,097 hrs · 44,561 cycles

OKC - FOUND FRAME GOUGED ON UPPER FLANGE AFT RADIUS BETWEEN STRINGERS. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR FILLERS AND ANGLES IAW SRM. (M)

Part: SKIN — CHAFED (TE FLAPS) · airframe 52,097 hrs · 44,561 cycles

OKC - FOUND RIGHT OUTBOARD MID FLAP CHAFED AT INBOARD LEADING EDGE. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR FILLER AND DOULER IAW SRM. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 52,097 hrs · 44,561 cycles

OKC - FOUND FLOORBEAM HAS CORROSION AT TOP FLANGE. REMOVED DAMAGED REPAIR, FABRICATED AND INSTALLED REPLACEMENT FLOORBEAM T-CAP IAW EA. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 52,097 hrs · 44,561 cycles

OKC - FOUND FLOORBEAM HAS CORROSION AT TOP FLANGE. REMOVED DAMAGED REPAIR, FABRICATED AND INSTALLED REPAIR TEE CHORD, TRIPLER ANGLE, SPLICE ANGLE, REPAIR STRAP, TRIPLER STRAP, AND FILLER IAW EA. (M)

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,097 hrs · 44,561 cycles

FOUND R1 DOOR CUTOUT FUSELAGE SKIN CRACKED TWO PLACES LOWER AFT CORNER. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR FILLERS, DOUBLER, AND TRIPLER IAW SRM. (M)

Part: SKIN — LIGHTNING STRIKE (FUSELAGE) · airframe 52,097 hrs · 44,561 cycles

OKC - LIGHTNING STRIKE DAMAGE OUT OF LIMITS ON SKIN IAW SRM. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR FILLER, DOUBLER AND TRIPLER IAW SRM.

Part: SKIN — DEBONDED (LT MLG DOOR) · airframe 52,097 hrs · 44,561 cycles

OKC - LT MAIN LANDING GEAR, UPPER STRUT DOOR FWD AND AFT HINGE AREA DISBONDING. REMOVED DAMAGE, COMPLIED WITH COMPOSITE REPAIR IAW EA.

Part: FRAME — BENT (FUSELAGE) · airframe 52,097 hrs · 44,561 cycles

OKC - FRAME BENT AND DEFORMED AT LOWER FLANGE. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR ANGLE AND REPLACEMENT STRINGER CLIP IAW SRM.

Part: STRINGER — CORRODED (E/E BAY) · airframe 52,097 hrs · 44,561 cycles

OKC - E AND E BAY STRINGER EXFOLIATED. REMOVED DAMAGE, ORDERED AND INSTALLED NEW STRINGER IAW SRM.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 52,097 hrs · 44,561 cycles

OKC - AFT CARGO BAY U CHANNEL IN HAT STRINGER IS CRACKED. REMOVED DAMAGED U CHANNEL, FABRICATED AND INSTALLED REPLACEMENT U CHANNEL IAW SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 52,097 hrs · 44,561 cycles

OKC - LONGITUDINAL BEAM HAS CORROSION. REMOVED DAMAGE, COMPLIED WITH HFEC, NO DEFECTS NOTED FLAP PEENED, TREATED, PRIMED, AND TOP-COATED IAW EA.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 52,097 hrs · 44,561 cycles

OKC - LONGITUDINAL FLOOR SUPPORT HAS CORROSION. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR BEAM IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 52,097 hrs · 44,561 cycles

OKC- FLOORBEAM HAS CORROSION ON FORWARD FLANGE. REMOVED DAMAGE, FLAP PEENED, FABRICATED AND INSTALLED REPAIR STRAP SECTION IAW EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 52,097 hrs · 44,561 cycles

OKC - FLOORBEAM CORRODED. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR CHORD SECTION AND REPAIR ANGLES IAW SRM.

Part: SKIN — CHAFED (FORE FLAP) · airframe 52,097 hrs · 44,561 cycles

OKC - LT WING T/E FORE FLAP HAS CHAFING AREA IN OB EDGE. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM.

Part: SKIN — CHAFED (FORE FLAP) · airframe 52,097 hrs · 44,561 cycles

OKC- RT WING IB FORE FLAP UPPER SURFACE HAS 6 AREAS THAT ARE CHAFED TO BARE METAL. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 52,097 hrs · 44,561 cycles

OKC - STA 328 FLOORBEAM CORRODED AT RBL 11. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR FILLER AND ANGLES IAW SRM.

Part: STRUCTURE — CRACKED (AFT CARGO DOOR) · airframe 52,097 hrs · 44,561 cycles

OKC- AFT CARGO DOOR, CENTER SECTION, INTERNAL LIGHTING HOLE HAS .5 INCH CRACK. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 52,097 hrs · 45,561 cycles

OKC - AFT CARGO PIT BILGE AREA CORROSION IN STRINGER FLANGE. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR STRINGER SECTION IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 52,097 hrs · 44,561 cycles

OKC- FLOORBEAM HAS CORROSION ON UPPER AND LOWER SURFACES OF TOP FLANGE. REMOVED DAMAGE, FABRICATED, AND INSTALLED REPAIR FILLER SHIM, AND REPAIR ANGLES IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 52,097 hrs · 44,561 cycles

OKC - FLOORBEAM CORRODED. REMOVED DAMAGE, FABRICATED, AND INSTALLED REPAIR FILLER SECTION, SUPPORT ANGLES, AND REPAIR STRAPS IAW SRM.

Part: SKIN — LIGHTNING STRIKE (FUSELAGE) · airframe 52,097 hrs · 44,561 cycles

OKC- EXTERIOR SKIN BLEND-OUT FOR LIGHTNING STRIKE IS OUT OF LIMITS. REMOVED DAMAGE, FABRICATED, AND INSTALLED REPAIR FILLERS, DOUBLER, AND TRIPLER IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 52,097 hrs · 44,561 cycles

OKC - RT SIDE STA 948 FORWARD FLOORBOARD STRIP ANGLE RBL 44 FASTENER HOLES AND LOWER SIDE FLOORBEAM HAS CORROSION. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR STRAP, FILLER AND WASHERS IAW EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 52,097 hrs · 44,561 cycles

OKC - CORROSION ON FLOORBEAM TOP FLANGE. REMOVED CORROSION, OUT OF LIMITS IAW SRM. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PARTS IAW SRM.

Part: SKIN — DENTED (AFT CARGO DOOR) · airframe 52,097 hrs · 44,561 cycles

OKC - AFT CARGO PIT DOOR EDGE DENTED A=1.0, Y=0.120, A/Y=8.3. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER IAW SRM.

Part: LENS — MISSING (EMERGENCY LIGHT)

ANC - FOUND ROW 18 EMERGENCY FLOOR TRACK LIGHT MISSING LAMP IN GALLEY AREA. REPLACED MISSING CLEAR LENS COVER. (M)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

ANC- DURING INSPECTION, FOUND THE EMERGENCY FLOOR TRACK LIGHTS ON SEAT PALLET 8-6 INOPERATIVE. REPLACED BATTERY PACK, THEN LIGHTS TESTED NORMAL. (M)

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT)

ANC - DURING INSPECTION, FOUND THE EXIT IDENTIFIER IN THE MID CABIN INOPERATIVE. REPLACED BATTERY AND REPAIRED WIRE, THEN LIGHTS TESTED NORMAL. (M)

Part: BATTERY — NOT SEATED (CABIN)

ANC - DURING INSPECTION, FOUND THE OVERHEAD EMERGENCY EXIT IDENTIFIER IN THE MID CABIN INOPERATIVE. RESEATED THE BATTERY, THEN EXIT IDENTIFIER OPERATED NORMAL. (M)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

ANC - DURING INSPECTION, FOUND TRACK LIGHTING INOPERATIVE AT PALLET 9-10. REPLACED BATTERY ON SEAT PALLET 9-10. OPS CHECK GOOD. (M)

Part: WIRE — DAMAGED (EMERGENCY LIGHT)

ANC - DURING INSPECTION FOUND EMERGENCY EXIT LIGHTING CONTROL CIRCUIT BREAKER WILL NOT TEST. REPAIRED WIRING. OPS CHECK GOOD. (M)

Part: CIRCUIT BREAKER — INOPERATIVE (EMERGENCY LIGHT)

DURING INSPECTION FOUND, THE EMERGENCY FLOOR PATH LIGHTING ON WITH SWITCH IN ARMED OR OFF POSITION. RESET THE EMERGENCY FLOORPATH LIGHTING CIRCUIT BREAKER THEN LIGHT TESTED NORMAL. (M)

Part: CIRCUIT BREAKER — INOPERATIVE (EMERGENCY LIGHTS)

ANC- DURING INSPECTION, FOUND THE EMERGENCY FLOOR PATH LIGHTING ON WITH SWITCH IN 'ARMED' OR 'OFF' POSITION. RESET THE EMERGENCY FLOOR PATH LIGHTING CIRCUIT BREAKER THEN LIGHTS TESTED NORMAL. (M)

Part: CIRCUIT BREAKER — INOPERATIVE (BREAKER PANEL)

DURING INSPECTION, FOUND THE EMERGENCY FLOORPATH LIGHTING ON WITH SWITCH IN 'ARMED' OR 'OFF' POSITION.RESET THE EMERGENCY FLOORPATH LIGHTING CIRCUIT BREAKER THEN LIGHTS TESTED NORMAL. (M)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

DURING INSPECTION, FOUND THE EMERGENCY FLOORPATH LIGHING ON WITH SWITCH IN 'ARMED' OR 'OFF' POSITION. RESET BATTERY PACKS ON PALLETS 5-12, 6-11, 9-11, 9-5, 7-6, AND 10-11 THEN LIGHTS TESTED NORMAL. (M)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

SEA - DURING INSPECTION, FOUND THE EMERGENCY FLOOR PATH LIGHTING ON WITH SWITCH IN 'ARMED' OR 'OFF' POSITION. RESET BATTERY PACKS ON PALLETS 5-12, 6-11, 9-11, 9-5, 7-6, AND 10-11 THEN LIGHTS TESTED NORMAL. (M)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

DURING INSPECTION FOUND THE EMERGENCY FLOORPATH LIGHTING ON WITH SWITCH IN 'ARMED' OR 'OFF' POSITION. RESET BATTERY PACKS ON PALLETS 5-12, 6-11, 9-11, 9-5, 7-6, AND 10-11 THEN LIGHTS TESTED NORMAL. (M)

Part: BATTERY — DISCHARGED (EMERGENCY LIGHT)

SEA - DURING INSPECTION, FOUND MID CABIN OVERHEAD EXIT SIGN INOPERATIVE AND FLOOR TRACK LIGHTING ON WITH SWITCH IN 'ARMED' OR 'OFF' POSITION. REPLACED MID CABIN OVERHEAD SIGN BATTERY PACK AND TRACK LIGHTING CONTROL MODULE (P/N 873203041) THEN LIGHTS TESTED NORMAL. (M)

Part: LIGHT — INOPERATIVE (CABIN)

SEA - DURING INSPECTION FOUND MID CABIN OVERHEAD EXIT SIGN INOPERATIVE AND FLOOR TRACK LIGHTING ON WITH SWITCH IN 'ARMED' OR 'OFF' POSITION. REPLACED MID CABIN OVERHEAD SIGN BATTERY P/N 86210144 PACK AND TRACK LIGHTING CONTROL MODULE P/N 873203041 THEN LIGHTS TESTED NORMAL. (M)

Part: BATTERY — DISCHARGED (SMOKE BARRIER)

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

Part: TRANSMITTER — INOPERATIVE (EMERGENCY LIGHT)

SEA - DURING RECON INSPECTION, FOUND EMERGENCY FLOOR TRACK LIGHTS AT ROWS 8-10 AND 14-16 INOPERATIVE. REPLACED BATTERY PACK (P/N 8821004) AT ROW 14 AND TRANSMITTER (P/N 883200312) AT ROW 11, THEN LIGHTS TESTED NORMAL. (M)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

SEA - DURING RECON INSPECTION, FOUND BATTERY PACKS AT SEAT PALLETS 5-12 AND 8-9 INOPERATIVE. REPLACED BATTERY PACKS, THEN LIGHTS TESTED NORMAL. (M)

Part: CONTROL MODULE — INOPERATIVE (MID CABIN)

FOUND EMERGENCY TRACK LIGHTING ILLUMINATED ON DESCENT AND THEN EXTINGUISHED PRIOR TO LANDING. REMOVED AND REPLACED CENTER CONTROL MODULE, THEN LIGHTS TESTED NORMAL. (M)

Part: MODULE — FAULTY (CABIN)

ANC - DURING TAXI, EMERGENCY FLOOR TRACK LIGHTING FLICKERED ON AND OFF AFTER LANDING. REMOVED AND REPLACED AFT CONTROL MODULE, THEN LIGHTS OPERATED NORMAL. (M)

Part: BATTERY — DISCHARGED (CABIN)

ANC - DURING DESCENT INTO ANC, EMERGENCY FLOOR TRACK LIGHTING ILLUMINATED ON PALLETS 9-3 AND 7-12. REMOVED AND REPLACED REMOTE ASSEMBLY BATTERIES AT PALLETS 9-3 AND 7-12, THEN LIGHTS OPERATED NORMAL. (M)

Part: SHEAR TIE — CORRODED (FUSELAGE)

PAE - DURING SCHEDULED C-CHECK, FOUND SHEAR TIE AT BS 727A, STRINGER 27R CORRODED. REMOVED CORRODED, FABRICATED AND INSTALLED REPAIR PER SRM. (M)

Part: KEELBEAM — DAMAGED (FUSELAGE)

PAE - DURING SCHEDULED C-CHECK, REQUIRED KEEL BEAM ACCESS, CUT OUT OF SKIN PANEL AT BS 727-727 PLUS 16, LEFT BUTTOCK LINE 7. (M)

Part: DOOR FRAME — CRACKED (CARGO DOOR)

PAE - DURING SCHEDULED C-CHECK, FOUND AFT CARGO DOOR FRAME AT BS 787, RIGHT BUTTOCK LINE 40 CRACKED. REPAIRED CRACK PER EA. (M)

Part: KEELBEAM — CRACKED (FUSELAGE)

PAE - DURING SCHEDULED C-CHECK, FOUND KEEL BEAM FLANGE AT BS 727-735, LBL 7 CRACKED. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR PER SRM. (M)

Part: FRAME — CORRODED (FUSELAGE)

PAE - DURING SCHEDULED C-CHECK, FOUND FRAME AT BS 685, LBL 68 CORRODED. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR PER EA. (M)

Part: FRAME — CORRODED (FUSELAGE)

PAE - DURING SCHEDULED C-CHECK, FOUND FRAME AT BS 685, RBL 68 CORRODED. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR PER EA. (M)

Part: KEELBEAM — CHAFED (FUSELAGE)

PAE - DURING SCHEDULED C-CHECK, FOUND KEEL BEAM AT BS 720-727, LBL 7 CHAFED. REMOVED AND REPLACED KEEL BEAM PER EA. (M)

Part: FRAME — DENTED (FUSELAGE)

PAE - DURING SCHEDULED C-CHECK, FOUND FRAME INNER CHORD AT BS 808, STRINGER 25L DENTED. REMOVED AND REPLACED FRAME PER SRM. (M)

Part: TEE FITTING — CORRODED (CARGO DOOR)

PAE - DURING SCHEDULED C-CHECK, FOUND AFT CARGO DOOR NR 5 T-ANGLE AT BS 808, RBL 65 CRACKED 1 INCH. FABRICATED REPAIR ANGLE PER EA. (M)

Part: ANGLE — CRACKED (FUSELAGE)

DURING SCHEDULED C CHECK, FOUND SPLICE ANGLE AT BODY STATION 540, STR 22L-23L CRACKED. REMOVED AND REPLACED SPLICE ANGLE IAW SRM.

Part: SKIN — DENTED (SLATS)

DURING SCHEDULED C CHECK, FOUND NR 4 SLAT MAIN TRACK COVER AT SLAT STA 28, SLAT STA 31 DENTED. REPAIRED DENT TO ORIGINAL CONTOUR IAW EA.

Part: FITTING — DAMAGED (INTERCOSTAL)

DURING SCHEDULED C CHECK FOUND INTERCOSTAL CHORD FITTING AT BODY STA 360-385, LEFT BUTTOCK LINE 9. LEFT BUTTOCK LINE 16 WITH AN ELONGATED HOLE. REMOVED AND REPLACED INTERCOSTAL CHORD FITTING IAW SRM.

Part: SKIN — CRACKED (GALLEY DOOR)

DURING SCHEDULED C CHECK, FOUND R1 GALLEY DOOR SKIN CRACKED AT UPPER HINGE CUTOUT. REPAIRED CRACKS TO R1 DOOR IAW EA.

Part: FRAME — CRACKED (FUSELAGE)

DURING SCHEDULED C CHECK, FOUND FRAME AT STA 480, BUTTOCK LINE 0, CRACKED. FABRICATED REPAIR PARTS AND INSTALLED IAW EA.

Part: STRINGER — CORRODED (FUSELAGE)

DURING SCHEDULED -C- CHECK FOUND STRINGER 26 RT AT BODY STATION 360-380 CORRODED. REMOVED, FABRICATED AND INSTALLED REPAIR IAW SRM.

Part: SKIN — WORN (NR 2 SLAT)

DURING SCHEDULED C CHECK, FOUND LEADING EDGE SKIN AT NR 2 SLAT ACTUATOR CUTOUT AT WING STATION 409-447 WORN. REMOVED AND REPLACED SKIN IAW SRM.

Part: SUPPORT FITTING — CORRODED (FUSELAGE)

DURING SCHEDULED C CHECK, FOUND FAIRING SUPPORT ANGLE BODY STATION 676, RIGHT BUTTOCK LINE 17, RIGHT BUTTOCK LINE 44, CORRODED. REMOVED AND REPLACED SUPPORT ANGLE IAW SRM.

Part: SUPPORT — CORRODED (FUSELAGE)

DURING SCHEDULED C CHECK FOUND SIDEWALL SUPPORT PLATE AT BODY STR 787-787+10, STRINGER 26R CORRODED. REMOVED AND REPLACED SIDEWALL SUPPORT PLATE IAW SRM.

Part: ATTACH ANGLE — BROKEN (NACELLE)

DURING SCHEDULED C CHECK FOUND NR 2 ENGINE OUTBOARD FIXED FAIRING ATTACH ANGLE AT NACELLE STATION 139 BROKEN. REMOVED, FABRICATED AND INSTALLED NEW ATTACH ANGLE PER SRM.

Part: RIB — CORRODED (WING)

DURING SCHEDULED C CHECK, FOUND OUTBOARD RIB AT WING STATION 453, CORRODED. REMOVED AND REPLACED OUTBOARD RIB IWA SRM.

Part: RIB — CORRODED (WING)

DURING SCHEDULED C CHECK, FOUND INBOARD RIB AT WING STATION 453, CORRODED. REMOVED AND REPLACED RIB IAW SRM.

Part: BULKHEAD — CRACKED (FUSELAGE)

DURING SCHEDULED C CHECK FOUND AFT PRESSURE BULKHEAD WEB AT BODY STA 1042, RIGHT BUTTOCK LINE 2 CRACKED. REPAIRED AFT PRESSURE BULKHEAD WEB IAW EA.

Part: SKIN — WORN (NR 5 SLAT)

DURING SCHEDULED C CHECK, FOUND LEADING EDGE SKIN AT NR 5 SLAT ACTUATOR AT WING STATION 399-462.5, WORN. REPAIRED SKIN IAW SRM.

Part: BRACKET — CRACKED (RAM AIR PLENUM)

DURING SCHEDULED C CHECK, FOUND RAM AIR PLENUM BRACKET AT BODY STATION 565, RIGHT BUTTOCK LINE 50 CRACKED. REMOVED AND REPLACED BRACKET IWA SRM.

Part: SKIN — GOUGED (FUSELAGE)

DURING SCHEDULED C CHECK, FOUND SKIN PANEL AT BODY STATION 312-328, STRINGER 17L-18L GOUGED. INSTALLED DOUBLER AND TRIPLER IAW EA.

Part: STRUCTURE — DAMAGED (NR 5 SLAT)

DURING SCHEDULED C CHECK, FOUND NR5 SLAT AT WING STATION 227-329 DAMAGED. REMOVED AND REPLACED NR5 SLAT.

Part: SKIN — WORN (NR 3 SLAT)

DURING SCHEDULED C CHECK, FOUND SKIN ON NR3 SLAT ACTUATOR CUTOUT AT WING STATION 272-313 WORN. REPAIRED SLAT SKIN IAW SRM.

Part: LATCH — OUT OF ADJUST (EMER EXIT HATCH)

DURING SCHEDULED C CHECK, FOUND LT OVERWING EMERGENCY EXIT HATCH HARD TO OPEN. ADJUSTED LT OVERWING EXIT DOOR IAW MM, THEN DOOR OPERATED NORMAL.

Part: ANGLE — DAMAGED (FAIRING)

DURING SCHEDULED C CHECK, FOUND FAIRING ANGLES AT BODY STATION 688, RIGHT BUTTOCK LINE 6, RIGHT BUTTOCK LINE 8 DAMAGED. REMOVED AND REPLACED ANGLES IAW SRM.

Part: KEELBEAM — CHAFED (FUSELAGE)

DURING SCHEDULED C CHECK, FOUND KEELBEAM AT BODY STATION 720-727, RIGHT BUTTOCK LINE 7 CHAFFED. REPAIRED KEEL BEAM IAW EA.

Part: KEELBEAM — CRACKED (FUSELAGE)

PAE - DURING SCHEDULED C-CHECK, FOUND KEEL BEAM WEB AT BS 663-727, LBL 5 CRACKED. REMOVED AND REPLACED KEEL BEAM WEB PER SRM. (M)

Part: DOOR FRAME — GOUGED (L1 DOOR)

PAE - DURING SCHEDULED C-CHECK, FOUND L1 DOOR FRAME AT BS 320 LBL 65 GOUGED. REPAIRED DOOR FRAME PER SRM. (M)

Part: STRINGER — CORRODED (FUSELAGE)

PAE - DURING SCHEDULED C-CHECK, FOUND STRINGER 26R AT BODY STATION 337-357 CORRODED. REMOVED CORRODED SECTION, FABRICATED AND REPAIRED STRINGER PER SRM. (M)

Part: STRINGER — DENTED (FUSELAGE)

PAE - DURING SCHEDULED C-CHECK, FOUND STRINGER 20L AT BODY STATION 1040 DENTED. REPAIRED STRINGER PER SRM. (M)

Part: STRINGER — CRACKED (FUSELAGE)

PAE - DURING SCHEDULED C-CHECK, FOUND STRINGER 18L AT BODY STATION 1040 CRACKED. REPAIRED STRINGER PER SRM. (M)

Part: PRESSURE PANEL — CRACKED (FUSELAGE)

PAE - DURING SCHEDULED C-CHECK, FOUND RIGHT MAIN WHEEL WELL WEB AT BODY STATION 706-721, RBL 20, RBL 34 CRACKED. REMOVED AND REPLACED WEB PER SRM. (M)

Part: FITTING — GOUGED (FUSELAGE)

PAE - DURING SCHEDULED C-CHECK, FOUND 9-G FLOOR PAN FITTING AT BS 344-360, RBL 60, RBL 65 GOUGED. REMOVED AND REPLACED FITTING PER SRM. (M)

Part: RIB — GOUGED (NR 2 COWLING)

PAE - DURING SCHEDULED C-CHECK, FOUND NR 2 ENGINE INBOARD COWL RIB UPPER MID SPLICE AT ENGINE STATION 136 GOUGED. REMOVED AND REPLACED INBOARD COWL. (M)

Part: SHEAR TIE — CORRODED (FUSELAGE)

PAE - DURING SCHEDULED C-CHECK, FOUND STUB FRAME SHEAR TIE AT BODY STATION 787, STRINGER 26R CORRODED. FABRICATED, REMOVED AND REPLACED SHEAR TIE PER SRM. (M)

Part: FAILSAFE — CORRODED (FUSELAGE)

PAE - DURING SCHEDULED C-CHECK, FOUND FRAME FAIL/SAFE CHORD AT BS 520, STRINGER 27L CORRODED. REPAIRED FRAME FAIL/SAFE CHORD PER SRM. (M)

Part: SKIN — DENTED (FUSELAGE)

PAE - DURING SCHEDULED C-CHECK, FOUND SKIN PANEL AT BS 1039, STRINGER 10R DENTED. REPAIRED SKIN PANEL PER SRM. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

PAE - DURING SCHEDULED C-CHECK, FOUND LATERAL FLOOR SUPPORT AT BS 967-980, LBL 23, LBL 40 CORRODED. REMOVED AND REPLACED FLOOR SUPPORT PER SRM. (M)

Part: SKIN PANEL — CRACKED (FUSELAGE)

PAE - DURING SCHEDULED C-CHECK, FOUND SKIN PANEL AT BS 950, STRINGER 11R CRACKED. REPAIRED SKIN PANEL PER SRM. (M)

Part: SKIN PANEL — GOUGED (T/E FLAP)

PAE - DURING SCHEDULED C-CHECK, FOUND FORE FLAP LOWER LEADING EDGE SKIN PANEL AT WING STATION 505R GOUGED. BLENDED AND INSTALLED REPAIR PER SRM. (M)

Part: ANGLE — WORN (FUSELAGE)

PAE - DURING SCHEDULED C-CHECK, FOUND RIGHT MAIN LANDING GEAR BAY FAIRING SUPPORT ANGLE AT FUSELAGE BS 727, RBL 9, RBL 17 WITH WORN FASTENER HOLES. REMOVED AND REPLACED ANGLE PER SRM. (M)

Part: FAIRING — CHAFED (RT NACELLE)

PAE - DURING SCHEDULED C-CHECK, FOUND NR 2 ENGINE OUTBOARD FIXED FAIRING AT NACELLE STATION 155, WING STATION 255R CHAFED. REPAIRED FAIRING PER SRM. (M)

Part: SUPPORT — CORRODED (FUSELAGE)

PAE - DURING SCHEDULED C-CHECK, FOUND FLOOR TO SIDEWALL SUPPORT AT FUSELAGE BODY STATION 500-500A, STRINGER 26R CORRODED. REMOVED AND REPLACED FLOOR TO SIDEWALL SUPPORT PER SRM. (M)

Part: DOOR FRAME — GOUGED (FUSELAGE)

PAE - DURING SCHEDULED C-CHECK, FOUND AFT CARGO DOOR CUTOUT FORWARD FRAME STABILIZING WEB AT FUSELAGE BS 787, STRINGER 24R DENTED AND GOUGED. REMOVED AND REPLACED WEB PER SRM. (M)

Part: FITTING — DAMAGED (FUSELAGE)

PAE - DURING SCHEDULED C-CHECK, FOUND INTERCOSTAL CHORD FITTING AT BS 360-385, LBL 9, LBL 16 WITH AN ELONGATED HOLE. REMOVED AND REPLACED INTERCOSTAL CHORD FITTING PER SRM. (M)

Part: SUPPORT — DAMAGED (NR 2 COWLING)

PAE - DURING SCHEDULED C-CHECK, FOUND NR 2 ENGINE INBOARD COWL BLOWOUT DOOR SUPPORT DAMAGED AT ENGINE STATION 230. REMOVED, FABRICATED AND REPLACED ENGINE COWL BLOWOUT DOOR SUPPORT PER SRM. (M)

Part: SUPPORT — CORRODED (FUSELAGE)

PAE - DURING SCHEDULED C-CHECK, FOUND FLOOR TO SIDEWALL SUPPORT AT FUSELAGE BODY STATION 490-520, LEFT BUTTOCK LINE 25 CORRODED. REMOVED AND REPLACED FLOOR TO SIDEWALL SUPPORT PER SRM. (M)

Part: SKIN — CHAFED (T/E FLAP)

PAE - DURING SCHEDULED C-CHECK, FOUND LEADING EDGE OF OUTBOARD FORE FLAP AT LEFT WING STATION 495-499 CHAFED. FABRICATED REPAIRS TO FLAP PER SRM. (M)

Part: SUPPORT — WORN (FUSELAGE)

PAE - DURING SCHEDULED C-CHECK, FOUND TIE DOWN SUPPORT AT FUSELAGE BODY STATION 410-520, RBL 21 WORN. REMOVED AND FABRICATED REPAIRS TO TIE DOWN SUPPORT PER SRM. (M)

Part: SUPPORT — CORRODED (FUSELAGE)

PAE - DURING SCHEDULED C-CHECK, FOUND BULKHEAD SUPPORT AT FUSELAGE BS 520, LBL 24, RBL 30 CORRODED. REMOVED CORROSION AND REPAIRED PER SRM BY FABRICATING AND INSTALLING NEW SUPPORT. (M)

Part: INTERCOSTAL — CRACKED (FUSELAGE)

PAE - DURING SCHEDULED C-CHECK, FOUND INTERCOSTAL AT FUSELAGE BS 500-500A, STRINGER 26R CRACKED. REMOVED DAMAGED INTERCOSTAL AND REPAIRED PER SRM BY FABRICATING AND INSTALLING NEW INTERCOSTAL. (M)

Part: SUPPORT — CORRODED (FUSELAGE)

PAE - DURING SCHEDULED C-CHECK, FOUND FLOOR TO SIDEWALL SUPPORT AT FUSELAGE BODY STATION 500-500A, STRINGER 26R CORRODED. REMOVED AND REPLACED FLOOR TO SIDEWALL SUPPORT PER SRM. (M)

Part: FRAME — CORRODED (FUSELAGE)

PAE - DURING SCHEDULED C-CHECK, FOUND FRAME AT FUSELAGE BS 520, RIGHT BUTTOCK LINE 6, RIGHT BUTTOCK LINE 14 CORRODED. REMOVED CORROSION AND REPAIRED PER SRM BY FABRICATING AND INSTALLING REPAIR PARTS. (M)

Part: KEELBEAM — CORRODED (FUSELAGE)

PAE - DURING SCHEDULED C-CHECK, FOUND KEEL BEAM WEB AT FUSELAGE BS 642, LBL 2 CORRODED. REMOVED CORROSION AND REPAIRED PER SRM BY FABRICATING AND INSTALLING REPAIR PARTS. (M)

Part: SUPPORT ANGLE — CORRODED (FUSELAGE)

PAE - DURING SCHEDULED C-CHECK, FOUND SUPPORT ANGLE AT FUSELAGE BODY STATION 664-675, RBL 27 CORRODED. REMOVED CORRODED AND REPAIRED PER SRM BY FABRICATING AND INSTALLING REPAIR PARTS. (M)

Part: RIB — DAMAGED (AFT AIRSTAIRS)

PAE - DURING SCHEDULED C-CHECK, FOUND AFT AIRSTAIR RIB AT FUSELAGE BS 947-987 DAMAGED. REMOVED DAMAGED AREA AND REPAIRED PER SRM BY FABRICATING AND INSTALLING REPAIR PARTS. (M)

Part: FRAME — CORRODED (FUSELAGE)

PAE - DURING SCHEDULED C-CHECK, FOUND FRAME AT FUSELAGE BS 400, STRINGER 19R CORRODED. REMOVED CORROSION AND REPAIRED PER SRM BY DRILLING OUT DAMAGE AND INSTALLING RIVET. (M

Part: SKIN — CRACKED (FUSELAGE)

SEA - FUSELAGE SKIN CRACKED AT THE R2 DOOR LOWER FORWARD CORNER. REPAIRED PER EA. (M)

Part: SLAT — DELAMINATED (WING)

ANC - DURING SCHEDULED A-CHECK, FOUND NR 2 LEADING EDGE SLAT DELAMINATING AT WING BODY LINE 329.75. REPAIRED PER EA. (M)

Part: BATTERY — DISCHARGED (CABIN)

ANC - DURING MAINTENANCE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTING AT ROWS 7 AND 8 INOPERATIVE. REMOVED AND REPLACED REMOTE ASSEMBLY BATTERY AT ROWS7 AND 8, THEN LIGHTS OPERATED NORMAL. (M)

Part: LIGHT — INOPERATIVE (CABIN)

ANC - DURING MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS AT SEAT PALLET 7-4 INOPERATIVE. REMOVED AND REPLACED REMOTE ASSEMBLY RECEIVER, THEN LIGHTS TESTED NORMAL. (M)

Part: CONTROL HANDLE — OUT OF ADJUST (AIR STAIR)

ANC - CREW REPORTED AIRSTAIR CONTROL HANDLE DIFFICULT TO OPERATE. ADJUSTED STOP DOOR LATCH FITTING, THEN OPS CHECKED GOOD. (M)

Part: HANDLE — LACK OF LUBE (AIRSTAIRS)

ANC - CREW REPORTED AIRSTAIR CONTROL HANDLE BINDING AND DIFFICULT TO OPERATE. LUBRICATED MECHANISM, THEN OPS CHECKED GOOD. (M)

Part: HANDLE — LACK OF LUBE (L1 DOOR)

ANC - DURING LINE CHECK, FOUND EXTERIOR DOOR HANDLE ON L-1 DOOR STICKS, HARD TO OPEN. CLEANED OFF ICE FROM HANDLE AREA, CLEANED AND LUBED SHAFT, OPERATIONS CHECK NORMAL. (M)

Part: SIGN — INOPERATIVE (CABIN)

ANC - DURING SCHEDULED MAINTENANCE, FOUND RIGHT OVERWING EMERGENCY EXIT SIGN INOPERATIVE. REMOVED AND REPLACED EXIT LIGHT ASSEMBLY, LIGHT TESTED NORMAL. (M)

Part: SIGN — INOPERATIVE (CABIN)

PAE - DURING SCHEDULED MAINTENANCE, FOUND AFT CABIN EMERGENCY EXIT SIGN INOPERATIVE. REMOVED AND REPLACED EXIT LIGHT ASSEMBLY AND BATTERY, LIGHT TESTED NORMAL. (M)

Part: BATTERY — DISCHARGED (CABIN)

PAE - DURING SCHEDULED MAINTENANCE, FOUND AFT CABIN EMERGENCY EXIT SIGN INOPERATIVE. REMOVED AND REPLACED EXIT LIGHT ASSEMBLY AND BATTERY, LIGHT TESTED NORMAL. REF ASAA0110556. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

PHX - DURING SCHEDULED D-CHECK, FOUND SEAT TRACK AT BS 344-520, LBL 62.5 CORRODED. REPAIRED PER SRM. (M)

Part: SKIN — GOUGED (FUSELAGE)

PHX - DURING SCHEDULED D-CHECK, FOUND SKIN PANEL AT BS 967-977, STRINGER 19L-22L GOUGED. REPAIRED PER SRM. (M)

Part: GUSSET — CORRODED (FUSELAGE)

PHX - DURING SCHEDULED D-CHECK, FOUND BULKHEAD GUSSET AT BS 227, LBL 3 CORRODED. REPAIRED PER SRM. (M)

Part: INTERCOSTAL — CORRODED (FUSELAGE)

PHX - DURING SCHEDULED D-CHECK, FOUND INTERCOSTAL AT BS 685, LEFT BUTTOCK LINE 60-66 CORRODED. REPAIRED PER SRM. (M)

Part: TIE CLIP — CRACKED (FUSELAGE)

PHX - DURING SCHEDULED D-CHECK, FOUND FRAME TIE CLIP AT BS 380, LBL 64 CRACKED. REPAIRED PER SRM. (M)

Part: TIE CLIP — CORRODED (FUSELAGE)

PHX - DURING SCHEDULED D-CHECK, FOUND STRINGER TIE AT BS 540, STRINGER 23L-24L CORRODED. REPAIRED PER SRM. (M)

Part: INTERCOSTAL — CORRODED (FUSELAGE)

PHX - DURING SCHEDULED D-CHECK, FOUND INTERCOSTAL AT BS 705, LEFT BUTTOCK LINE 60-66 CORRODED. REPAIRED PER SRM. (M)

Part: ANGLE — CORRODED (FUSELAGE)

PHX - DURING SCHEDULED D-CHECK, FOUND SUPPORT ANGLE AT BS 300-344, LEFT BUTTOCK LINE 38 CORRODED. REPAIRED PER SRM. (M)

Part: INTERCOSTAL — CRACKED (FUSELAGE)

PHX - DURING SCHEDULED D-CHECK, FOUND INTERCOSTAL AT BS 440-460, STRINGER 26L CRACKED. REPAIRED PER SRM. (M)

Part: STRUCTURE — CRACKED (CARGO DOOR)

PHX - DURING SCHEDULED D-CHECK, FOUND MAIN CARGO DOOR AT BS 380-480, STRINGER 16L HAS CRACKED AND BROKEN RIVET HEADS WITH CRACKS EMANATING FROM RIVETS. REPAIRED PER SRM. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

PHX - DURING SCHEDULED D-CHECK, FOUND FLOOR SUPPORT AT BS 887-916, STRINGER 26R-27R CORRODED. REPAIRED PER SRM. (M)

Part: STRAP — CORRODED (FUSELAGE)

PHX - DURING SCHEDULED D-CHECK, FOUND STRAP AT BS 680-690, LEFT BUTTOCK LINE 60-66 CORRODED. REPAIRED PER SRM. (M)

Part: STRAP — CORRODED (FUSELAGE)

PHX - DURING SCHEDULED D-CHECK, FOUND STRAP AT BS 540-727, LEFT BUTTOCK LINE 60 CORRODED. REPAIRED PER SRM. (M)

Part: STRAP — CORRODED (FUSELAGE)

PHX - DURING SCHEDULED D-CHECK, FOUND STRAP AT BODY STATION 693-696, LEFT BUTTOCK LINE 60-66 CORRODED. REPAIRED PER SRM. (M)

Part: STRAP — CORRODED (FUSELAGE)

PHX - DURING SCHEDULED D-CHECK, FOUND STRAP AT BODY STATION 696-705, STRINGER 18L CORRODED. REPAIRED PER SRM. (M)

Part: STRAP — CORRODED (FUSELAGE)

PHX - DURING SCHEDULED D-CHECK, FOUND STRAP AT BS 690-693, LEFT BUTTOCK LINE 60-66 CORRODED. REPAIRED PER SRM. (M)

Part: TIE CLIP — CORRODED (FUSELAGE)

PHX - DURING SCHEDULED D-CHECK, FOUND TIE CLIP AT BS 867, STRINGER 27L CORRODED. REPAIRED PER SRM. (M)

Part: ANGLE — CORRODED (FUSELAGE)

PHX - DURING SCHEDULED D-CHECK, FOUND ANGLE AT BS 695, STRINGER 18L CORRODED. REPAIRED PER SRM. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

PHX - DURING SCHEDULED D-CHECK, FOUND FLOOR SUPPORT AT BODY STATION 520-540, LEFT BUTTOCK LINE 25 CORRODED. REPAIRED PER SRM. (M)

Part: SEAT TRACK — WORN (FUSELAGE)

PHX - DURING SCHEDULED D-CHECK, FOUND SEAT TRACK LUGS AT BS 420-480, LEFT BUTTOCK LINE 24.5 WORN. REPAIRED PER SRM. (M)

Part: ATTACH ANGLE — CORRODED (FUSELAGE)

PHX - DURING SCHEDULED D-CHECK, FOUND ATTACH ANGLES AT BODY STATION 695, LEFT BUTTOCK LINE 60 CORRODED. REPAIRED PER BOEING DRAWING. (M)

Part: ATTACH ANGLE — CORRODED (FUSELAGE)

PHX - DURING SCHEDULED D-CHECK, FOUND ATTACH ANGLES AT BS 695, LEFT BUTTOCK LINE 60 CORRODED. REPAIRED PER BOEING DRAWING. (M)

Part: ATTACH ANGLE — CORRODED (FUSELAGE)

PHX - DURING SCHEDULED D-CHECK, FOUND ATTACH ANGLES AT BS 695, LEFT BUTTOCK LINE 60 CORRODED. REPAIRED PER BOEING DRAWING. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

PHX - DURING SCHEDULED D-CHECK, FOUND FLOOR SUPPORT AT BS 520-540, LEFT BUTTOCK LINE 24.7 CORRODED. REPAIRED PER SRM. (M)

Part: ATTACH ANGLE — CORRODED (FUSELAGE)

PHX - DURING SCHEDULED D-CHECK, FOUND ATTACH ANGLES AT BS 695, LEFT BUTTOCK LINE 60 CORRODED. REPAIRED PER BOEING DRAWING. (M)

Part: FRAME — CORRODED (FUSELAGE)

PHX - DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 500A, STRINGER 21R-25R CORRODED. REPAIRED PER SRM. (M)

Part: SKIN PANEL — DENTED (FUSELAGE)

PHX - DURING SCHEDULED D-CHECK, FOUND SKIN PANEL AT BODY STATION 897, STRINGER 18R DENTED. REPAIRED PER SRM. (M)

Part: ATTACH ANGLE — CRACKED (FUSELAGE)

PHX - DURING SCHEDULED D-CHECK, FOUND ATTACH ANGLE BS 380, STRINGER 25L-26L CRACKED. REPAIRED PER SRM. (M)

Part: INTERCOSTAL — CRACKED (FUSELAGE)

PHX - DURING SCHEDULED D-CHECK, FOUND INTERCOSTAL SUPPORT AT BS 400-420, LBL 22 CRACKED. REPAIRED PER BOEING DRAWING. (M)

Part: SUPPORT — CORRODED (FUSELAGE)

PHX - DURING SCHEDULED D-CHECK, FOUND SEAT TRACK SUPPORT BEAM AT BS 520, RBL 46 CORRODED. REPAIRED PER SRM. (M)

Part: SKIN — CORRODED (FUSELAGE)

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

Part: SUPPORT — CORRODED (FUSELAGE)

PHX - DURING SCHEDULED D-CHECK, FOUND SEAT TRACK SUPPORT BEAM AT BS 663-685, LEFT BUTTOCK LINE 64 CORRODED. REPAIRED PER SRM. (M)

Part: SHEAR TIE — CRACKED (FUSELAGE)

PHX - DURING SCHEDULED D-CHECK, FOUND SHEAR TIE AT BS 440, LBL 69 CRACKED. REPAIRED PER SRM. (M)

Part: INTERCOSTAL — CORRODED (FUSELAGE)

PHX - DURING SCHEDULED D-CHECK, FOUND INTERCOSTAL AT BODY STATION 847-867, STRINGER 26R CORRODED. REPAIRED PER SRM. (M)

Part: SHEAR TIE — CRACKED (FUSELAGE)

PHX - DURING SCHEDULED D-CHECK, FOUND SHEAR TIE AT BS 480, LBL 69 CRACKED. REPAIRED PER SRM. (M)

Part: SHEAR TIE — CORRODED (FUSELAGE)

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

Part: ANGLE — DAMAGED (FUSELAGE)

PHX - DURING SCHEDULED D-CHECK, FOUND ANGLE AT BS 440, STRINGER 27R DAMAGED. REPAIRED PER SRM. (M)

Part: ATTACH ANGLE — DAMAGED (FUSELAGE)

PHX - DURING SCHEDULED D-CHECK, FOUND ATTACH ANGLE AT BS 480, RBL 74 HAS ELONGATED HOLES. REPAIRED PER BOEING DRAWING. (M)

Part: INTERCOSTAL — CRACKED (FUSELAGE)

PHX - DURING SCHEDULED D-CHECK, FOUND INTERCOSTAL AT BS 330, STRINGER 26L-27L CRACKED. REPAIRED PER SRM. (M)

Part: INTERCOSTAL — CORRODED (FUSELAGE)

PHX - DURING SCHEDULED D-CHECK, FOUND INTERCOSTAL LINK AT BS 520-540, LBL 45 CORRODED. REPAIRED PER SRM. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

PHX - DURING SCHEDULED D-CHECK, FOUND FLOOR SUPPORT AT BS 520-540, LBL 45 CORRODED. REPAIRED PER SRM. (M)

Part: SKIN PANEL — DAMAGED (FUSELAGE)

PHX - DURING SCHEDULED D-CHECK, FOUND SKIN PANEL REPAIR AT BS 727, STRINGER 23L-24L REQUIRED PERMANENT REPAIR. REPAIRED PER SRM. (M)

Part: FRAME — GOUGED (FUSELAGE)

PHX - DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 348.2, STRINGER 11L-12L GOUGED. REPAIRED PER EA. (M)

Part: INTERCOSTAL — CORRODED (FUSELAGE)

PHX - DURING SCHEDULED D-CHECK, FOUND INTERCOSTAL AT BS 500B-520, STRINGER 25L-26L CORRODED. REPAIRED PER SRM. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

PHX - DURING SCHEDULED D-CHECK, FOUND FLOORBEAM AT BS 500B, RIGHT BUTTOCK LINE 24, LEFT BUTTOCK LINE 44, CORRODED. REPAIRED PER EA. (M)