N776AS

Part: NUT — LOOSE (L1 GUIDE ARM) · airframe 49,943 hrs · 28,189 cycles

L1 DOOR VERY STIFF HARD TO OPEN. PERFORMED VISUAL INSP OF L1 DOOR FOUND GUIDE ARM LOCK NUT LOOSE. TIGHTENED LOCK NUT IAW AMM 52 11 00 705 007 B00. PERFORMED FWD ENTRY DOOR TEST IAW AMM 52 11 00 755 051 B00. OPS CK GOOD. NO FURTHER DEFECTS NOTED AT THIS TIME.

Part: BEAM — CRACKED (BS 601) · airframe 49,893 hrs · 28,151 cycles

BS 601, STUB BEAM INNER HORD LOWER FASTENER HOLE CRACKED REPAIRED IAW EA 5310-02807.

Part: SKIN — CORRODED (WING) · corrosion level 2 · airframe 49,893 hrs · 28,151 cycles

EXFOLIATION CORROSION FOUND ON UPPER WING PLANK AT FS591, RBL67 REPAIRED IAW EA 5710 01153.

Part: SKIN — CORRODED (WING) · corrosion level 2 · airframe 49,893 hrs · 28,151 cycles

EXFOLIATION CORROSION FOUND ON UPPER WING SKIN AT FS 608.5 RBL 62 REPAIRED IAW EA 5710 01153.

Part: SKIN — CORRODED (WING) · corrosion level 2 · airframe 49,893 hrs · 28,151 cycles

EXFOLIATION CORROSION FOUND ON UPPER WING PLANK AT FS 661, RBL 57 REPAIRED IAW EA-5710 01153.

Part: SKIN — CORRODED (WING) · corrosion level 2 · airframe 49,893 hrs · 28,151 cycles

EXFOLIATION CORROSION FOUND ON UPPER WING SKIN AT FS 592 RBL 63 REPAIRED IAW EA 5710 01153.

Part: SKIN — DELAMINATED (ELEVATOR TAB) · airframe 46,003 hrs · 25,984 cycles

LT ELEV TAB UPPER SURFACE T E IS SPLIT 51" FROM I B END. PREPPED THE TAB UPPER SKIN SURFACE FOR BONDING CUT AND APPLIED REPAIR PLIES IAW SRM 51 70 05 PAPR 3.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 46,003 hrs · 25,984 cycles

SHEAR TIE CRACKED. CUT OUT DAMAGED SECTION OF FRAME (SHEAR TIE) FABRICATED AND INSTALLED A REPAIR SHEAR TIE DOUBLER AND RADIUS FILLERS IAW SRM 53 00 07 FIG 201 REPAIR 5.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 46,003 hrs · 25,984 cycles

OUTWARD DING IN FUSELAGE SKIN REMOVED SKIN DAMAGE BY DRILLING A 0.1935" HOLE INSTALLED A BACR15BB6 RIVET IAW ASA EA 5330 02205 REV NEW AND AAR EA 112004 REV IR.

Part: DOUBLER — CHAFED (T/E FLAP) · airframe 46,003 hrs · 25,984 cycles

RT IB FORE FLAP CHAFED ON AN EXITING REPAIR DOUBLER ON THE UPPER SIDE. REMOVED THE EXITING REPAIR DOUBLER AND FILLER FABRICATED AND INSTALLED A REPLACEMENT DOUBLER AND FILLER IAW SRM 51 70 10 PARA 7 8 11 15 18 AND 20.

Part: SKIN — CRACKED (L/E SLAT) · airframe 46,003 hrs · 25,984 cycles

NR 2 SLAT SKIN LWR LIP IS CRACKED AROUND FASTENER HOLES JUST BELOW THE O B AUX TRACK. CUT OUT THE DAMAGED AREA OF SKIN FABRICATED AND INSTALLED A SKIN FILLER AND EXTERNAL SPLICE PLATE IAW SRM 57 40 01 FIG 206 REPAIR 6.

Part: SKIN — DENTED (T/E FLAP) · airframe 46,003 hrs · 25,984 cycles

LT IB FOR FLAP DENTED OUT OF LIMITS NEAR CENTER TRACK. REMOVED THE DAMAGED AREA OF LOWER SKIN FABRICATED AND INSTALLED A SKIN FILLER AND REPAIR DOUBLER IAW SRM 51 70 10 PARA 8 11 15 18 AND 20.

Part: SKIN — CHAFED (T\E FLAP) · airframe 46,003 hrs · 25,984 cycles

THE RT OB MID FLAP IS CHAFED ON AN EXITING LE DOUBLER AT THE IB END. REMOVED THE EXITING REPAIR DOUBLER FABRICATED AND INSTALLED A REPAIR DOUBLER IAW SRM 57 53 01 FIG 201 REPAIR 8.

Part: SKIN — PUNCTURED (T/E FLAP) · airframe 46,003 hrs · 25,984 cycles

THE IB FORE FLAP IS PUNCTURED NEAR THE CENTER TRACK. REMOVED THE DAMAGED AREA OF LWR SKIN FABRICATED AND INSTALLED A SKIN FILLER AND A REPAIR DOUBLER IAW SRM 51 70 10 PARA 8 11 15 18 AND 20.

Part: SKIN — DENTED (BS 332 S23-24R) · airframe 42,307 hrs · 23,927 cycles

SKIN DENTED. FABRICATED AND INSTALLED REPAIR PARTS PER EA 5330 02061 AND ER 06 1486.

Part: DOOR FRAME — CRACKED (BS 303) · airframe 42,307 hrs · 23,927 cycles

L1 DOOR FRAME CRACKED AT LOWER STOP FITTING FWD SIDE. REPAIRED PER EA 5310 02594.

Part: SKIN — DENTED (BS 360-380) · airframe 42,307 hrs · 23,927 cycles

FUSELAGE SKIN DENT. REPAIRED PER EA 5330 02064 AND EO 06 1319.

Part: SKIN — CHAFED (BS 863-907) · airframe 42,307 hrs · 23,927 cycles

CHAFE MARKS ON SKIN. INSTALLED REPAIR PER ASA EA 5360 01055.

Part: FLOORBEAM — CORRODED (BS 344) · corrosion level 2 · airframe 42,307 hrs · 23,927 cycles

FLOORBEAM CORRODED. REMOVED CORRODED AREA AND INSTALLED REPAIR PER EA 5310 02591.

Part: FLOORBEAM — CORRODED (BS 986) · corrosion level 2 · airframe 42,307 hrs · 23,927 cycles

FOUND CORROSION ON FLOORBEAM. REPAIRED PER GOODRICH ER 06 1383 AND ASA EA 5310 02585.

Part: FLOORBEAM — CORRODED (BS 360) · corrosion level 2 · airframe 42,307 hrs · 23,927 cycles

FOUND TOP FLANGE OF FLOORBEAM CORRODED. REPAIRED PER SRM 51 70 11.

Part: FRAME — CRACKED (BS 907) · airframe 42,307 hrs · 23,927 cycles

FOUND BSTA 907 STR 8L FRAME CRACKED. REPAIRED PER SRM 53 00 07.

Part: FLOORBEAM — CORRODED (BS 360) · airframe 42,307 hrs · 23,927 cycles

FOUND TOP FLANGE OF FLOORBEAM AT BSTA 360 RBL 12 TO 25 WL 208 CORRODED. REPAIRED FLOORBEAM PER SRM 51 70 11.

Part: WEB — CRACKED (BS 986) · airframe 42,307 hrs · 23,927 cycles

FOUND FLOOR WEB IS CRACKED. REMOVED AND REPLACED WEB.

Part: SILL — CORRODED (BS 947-992) · airframe 42,307 hrs · 23,927 cycles

AFT SERVICE DOOR CREASE BEAM MOPSILL CORRODED. REMOVED AND REPLACED AFT SVC DOOR MOPSILL PER SRM 51 40 02.

Part: CREASE BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,307 hrs · 23,927 cycles

FOUND CREASE BEAM CORRODED. REPLACED CREASE BEAM PER SRM 51 40 02.

Part: FRAME — CHAFED (FUSELAGE) · airframe 42,307 hrs · 23,927 cycles

FOUND FRAME FLANGE CHAFED. REPAIRED PER SRM 51 70 11.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,307 hrs · 23,927 cycles

CORROSION ON THRESHOLD Z ANGLE. REMOVED AND REPLACED PER SRM 51 40 02.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,307 hrs · 23,927 cycles

CRACKED FRAME AT BIN RAIL ATTACHMENT. REPAIRED PER SRM 53 00 07

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 42,307 hrs · 23,927 cycles

CRACKED STRINGER CLIP. REMOVED AND REPLACED PER SRM 51 40 02.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,307 hrs · 23,927 cycles

CORRODED SHEAR TIE. REPAIRED PER SRM 53 00 07.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,307 hrs · 23,927 cycles

CORRODED SHEAR TIE. REPAIRED PER SRM 53 00 07.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,307 hrs · 23,927 cycles

CORRODED SHEAR TIE. REPAIRED PER SRM 53 00 07.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,307 hrs · 23,927 cycles

CORRODED SHEAR TIE. REPAIRED PER SRM 53 00 07.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,307 hrs · 23,927 cycles

CORROSION ON SHEAR TIE. REMOVED AND REPAIRED PER SRM 53 00 07.

Part: CREASE BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,307 hrs · 23,927 cycles

CORROSION AT RT SIDE CREASE BEAM. REMOVED AND REPLACED OUT OF LIMITS CORRODED CREASE BEAM PER SRM 57 48 02.

Part: STRINGER CLIP — CHAFED (FUSELAGE) · airframe 42,307 hrs · 23,927 cycles

STRINGER CLIP CHAFED. REMOVED AND REPLACED STRINGER CLIP PER SRM 51 40 02.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,307 hrs · 23,927 cycles

CORRODED FLOOR BEAM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,307 hrs · 23,927 cycles

FLOOR BEAM FASTENER HOLES HAVE CORROSION.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 42,307 hrs · 23,927 cycles

STRINGER CLIP CRACKED. REMOVED AND REPLACED STRINGER CLIP PER SRM 51 40 02.

Part: SKIN — DENTED (LTWING TE FLAP)

DENT FOUND AT LT WING IB T/E FORE FLAP. REPAIRED LT WING IB T/E FORE FLAP IAW SRM. (K)

Part: SKIN — GOUGED (LT WING)

LT WING UPPER SKIN GOUGED AT WING STA 223 BETWEEN STA 12 AND 13. BLENDED AREA, TREATED AND PRIMED IAW EA. (K)

Part: SKIN — CHAFED (NR 4 SLAT)

NR 4 SLAT IB T/E CHAFED. REMOVED DAMAGE, FABRICATED FILLER SKIN AND DOUBLER AND INSTALLED REPAIR IAW SRM. (K)

Part: SKIN — DELAMINATED (NR 2 SLAT)

NR 2 SLAT HAS DELAMINATED AT IB TRAILING EDGE. REPAIRED DAMAGED AREA OF NR 2 SLAT IAW SRM. (K)

Part: SKIN — DELAMINATED (FORE FLAP)

LT WING OB FORE FLAP DELAMINATED AT IB END. REMOVED DAMAGED AREA OF LT OB FORE FLAP IAW SRM. (K)

Part: SKIN — DELAMINATED (RT WING TE FLAP)

RT WING OB AFT FLAP DELAMINATED AT IB TRAILING EDGE. REMOVED DAMAGED MATERIAL, INSTALLED CORE, SKIN, AND DOUBLER IAW SRM. (K)

Part: SHEAR TIE — CRACKED (FUSLEAGE)

SHEAR TIE CRACKED AND CORRODED AT STR 28L B-STA 500G. FABRICATED SHEAR TIE, REMOVED AND REPLACED SHEAR TIE IAW SRM AND MFG DWG. (K)

Part: SHEAR TIE — CRACKED (FUSLAGE)

SHEAR TIE CRACKED AND CORRODED AT STR 28L B-STA 500G. FABRICATED SHEAR TIE, REMOVED AND REPLACED SHEAR TIE IAW SRM AND MFG DWG. (K)

Part: SKIN — CORRODED (NR 5 SLAT)

NR 5 SLAT IB TRAILING EDGE CHAFED. REMOVED DAMAGE, BONDED FILLER SKIN AND DOUBLER IAW SRM. (K)

Part: SHEAR WEB — CORRODED (SEAT ROW 8)

LT SHEAR WEB IS CORRODED AT SEAT ROW 8. REMOVED DAMAGED AREA AND INSTALLED REPAIR DOUBLER AND FILLER IAW SRM. (K)

Part: SHEAR TIE — CORRODED

SHEAR TIE BETWEEN STR 26L AND 25R, B-STA 947 HAS SURFACE CORROSION. REMOVED FABRICATED AND INSTALLED SHEAR TIE AND CLIP IAW SRM . (K)

Part: SKIN — DENTED (FUSELAGE)

DENT AT FUSELAGE STATION 1019, 1 INCH ABOVE STR 13L. REPAIRED FUSELAGE SKIN IAW SRM. (K)

Part: SUPPORT — CORRODED (CNTR WING BOX)

GYR - FOUND LEFT AC BAY HEAT EXCHANGER DUCT MOUNTING FLANGE CORRODED AT APPROX BS 580 LBL 36. REPAIRED LEFT CENTER WING SUPPORT WEB AT STATION 587 PER EA NR 5710-01104. (M)

Part: SKIN — CRACKED (FUSELAGE)

DURING C-CHECK, FOUND GOUGE ON FUSELAGE SKIN. REPAIRED IAW EA. (M)

Part: DOUBLER — CRACKED (FUSELAGE)

DURING C-CHECK, FOUND EXTERNAL POWER RECEPTACLE INTERNAL DOUBLER CRACKED ON LOWER EDGE. REPAIRED IAW SRM. (M)

Part: ANTENNA — CORRODED (FUSELAGE)

DURING C-CHECK, FOUND CORROSION ON ANTENNA STRUCTURE AFT CARGO BAY AT BS 727D. REPAIRED IAW SRM. (M)

Part: SKIN — DENTED (FUSELAGE)

DURING C-CHECK, FOUND SKIN DENTED RIGHT SIDE FORWARD OF FORWARD PIT DOOR. REPAIRED IAW SRM. (M)

Part: STANCHION — CRACKED (FUSELAGE)

DURING C-CHECK, FOUND E-1 RACK LEFT FORWARD STANCHION CRACKED. REPAIRED IAW SRM. (M)

Part: STANCHION — CRACKED (WX RADAR RACK)

DURING C-CHECK, FOUND CRACK IN WEATHER RADAR SHELF. REPAIRED IAW SRM. (M)

Part: SHEAR TIE — CORRODED (FUSELAGE)

DURING C-CHECK, FOUND SHEAR TIE CORRODED. REPAIRED IAW SRM. (M)

Part: THRESHOLD — CRACKED (FUSELAGE)

DURING C-CHECK, FOUND AFT CARGO BAY UPPER THRESHOLD PLATE IS CRACKED. REPAIRED IAW SRM. (M)

Part: SUPPORT — CORRODED (FUSELAGE)

DURING C-CHECK, FOUND CORROSION ON FLOOR TO BULKHEAD SUPPORT. REPAIRED IAW SRM. (M)

Part: DOOR — CHAFED (FUSELAGE)

DURING C-CHECK, FOUND AFT GALLEY SERVICE DOOR UPPER AFT INNER CORNER CHAFED. REPAIRED IAW SRM. (M)

Part: INTERCOSTAL — CORRODED (FUSELAGE)

DURING C-CHECK, FOUND INTERCOSTAL CORRODED AT BS 867. REPAIRED IAW SRM. (M)

Part: SHEAR TIE — CORRODED (FUSELAGE)

DURING C-CHECK, FOUND SHEAR TIE CORRODED AT BS 727D. REPAIRED IAW SRM. (M)

Part: FRAME — CORRODED (FUSELAGE)

DURING C-CHECK, FOUND FORWARD CARGO BAY FRAME CORRODED AT BS 500. REPAIRED IAW SRM. (M)

Part: FRAME — CORRODED (FUSELAGE)

DURING C-CHECK, FOUND CORROSION ON FRAME AT BS 727 BETWEEN BL 26 AND 27 RT. REPAIRED IAW SRM. (M)

Part: WEB — CORRODED (FUSELAGE)

DURING C-CHECK, FOUND AFT CARGO DOR WAY THRESHOLD WEB IS CORRODED AT CORNER NUT PLATES. REPAIRED IAW SRM. (M)

Part: CHANNEL — CORRODED (FUSELAGE)

DURING C-CHECK, FOUND SIDE WALL FLOOR CHANNEL CORRODED. REPAIRED IAW SRM. (M)

Part: STRAP — CORRODED (FUSELAGE)

DURING C-CHECK, FOUND AFT CARGO DOOR WAY STRAP CORRODED. REPAIRED IAW SRM. (M)

Part: SHEAR TIE — CORRODED (FUSELAGE)

DURING C-CHECK, FOUND CORROSION ON FRAME SHEAR TIE. REPAIRED IAW SRM. (M)

Part: SUPPORT — DENTED (FUSELAGE)

DURING C-CHECK, FOUND AFT CARGO SIDE WALL SUPPORT IS DENTED. REPAIRED IAW SRM. (M)

Part: SUPPORT — CORRODED (FUSELAGE)

PAE - DURING C-CHECK, FOUND FORWARD CARGO BAY LEFT FLOOR TO SIDEWALL SUPPORT HAS CORROSION AT NUT PLATES. REPAIRED IAW SRM. (M)

Part: CHANNEL — CRACKED (FUSELAGE)

PAE - DURING C-CHECK, FOUND WX RADAR SHELF CHANNEL CRACKED. REPAIRED IAW SRM. (M)

Part: SUPPORT — CORRODED (FUSELAGE)

PAE - DURING C-CHECK, FOUND CORROSION ON SIDE WALL SUPPORT. REPAIRED IAW SRM. (M)

Part: SUPPORT ANGLE — CORRODED (FUSELAGE)

PAE - DURING C-CHECK, FOUND FORWARD CARGO BAY FLOOR TO AFT BULKHEAD SUPPORT ANGLE HAS CORROSION AT NUT PLATES. REPAIRED IAW SRM. (M)

Part: WIRE — DISCONNECTED (CABIN)

FAI - DURING LINE CHECK, FOUND FLOOR TRACK EMERGENCY LIGHTS INOPERATIVE AT ROW 25, 26 AND AFT LAVATORY AREA. RECONNECTED FLOOR TRACK WIRING, OPERATIONAL CHECKED GOOD. (M)

Part: LIGHT — INOPERATIVE (CABIN)

ANC - DURING LINE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTING INOPERATIVE AT ROW 13 TO 16. REPLACED EMERGENCY FLOOR TRACK LIGHTING. OPERATIONS CHECK GOOD. (M)

Part: CONNECTOR — DISCONNECTED (CABIN)

SEA - DURING LINE CHECK, FOUND EMERGENCY TRACK LIGHTING INOPERATIVE AT ROW 15/16 ABC. RECONNECTED EMERGENCY TRACK LIGHT WIRES. OPS CHECK NORMAL. (M)

Part: LIGHT — DISCONNECTED (CABIN)

PDX - DURING LINE CHECK, FOUND EMERGENCY TRACK LIGHT INOPERATIVE AT ROWS 13-15. RECONNECTED EMERGENCY FLOOR LIGHTS AT ROWS 13-15. OPERATIONAL CHECKS NORMAL. (M)

Part: FRAME — CRACKED (FUSELAGE)

PAE - DURING SI CHECK, FOUND CRACK AT BS 178 LEFT AND RIGHT SIDE AT WL 205. REMOVED AND REPLACED BS 178 LEFT AND RIGHT SIDE CHORD PER EA 5310-01890. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

PAE - DURING SI CHECK, FOUND CORROSION ON FLOORBEAM AT BS 986.6 RBL 44 TO LBL 31, WL 208 AROUND FASTENER HOLES. REPAIRED FLOORBEAM IAW EA 5310-01891. (M)

Part: SKIN — DENTED (FUSELAGE)

PAE - DURING SCHEDULED C-CHECK, THE FUSELAGE SKIN AT BS 495 WAS FOUND TO BE DENTED ABOVE AND BELOW STRINGER 26R SKIN LAP. REPAIRED PER EA 5330-01445. (M)

Part: LIGHT — INOPERATIVE (CABIN)

SEA - DURING MAINTENANCE CHECK, THE AFT RED EMERGENCY EXIT FLOOR TRACK LIGHT WAS FOUND TO BE INOPERATIVE. REPLACED THE LAST TWO LIGHT ASSEMBLIES AND THE TRACK COVER AND LIGHTS OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

PDX - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS AT ROWS 3-7 WERE FOUND TO BE INOPERATIVE. RECONNECTED WIRING AND LIGHTS OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (ROW 20)

SEA - PRIOR TO FLIGHT 388, THE EMERGENCY EXIT FLOOR TRACK LIGHTS AT ROWS 20-24 WERE FOUND TO BE INOPERATIVE. RECONNECTED WIRING AND LIGHTS OPERATED NORMALLY. (M)

Part: WIRE — FAILED (CABIN)

SEA - DURING MAINTENANCE CHECK, 2 EACH AFT EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. REPAIRED WIRING AND LIGHTS OPERATED NORMALLY. (X)

Part: LENS — MISSING (L-2 EXIT SIGN)

SEA - FLT 215 - PRIOR TO DEPARTURE, THE PLASTIC 'EXIT SALIDA' LENS WAS FOUND MISSING FROM THE EXIT SIGN ADJACENT TO THE L-2 DOOR. REPLACED 'EXIT' SIGN LENS ASSEMBLY. (M)

Part: GUIDE ARM — OUT OF ADJUST (L-1 DOOR)

PDX - FLT 343 - L-1 DOOR DIFFICULT TO CLOSE. ADJUSTED GUIDE ARM AND DOOR OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

PDX - DURING MAINTENANCE CHECK, THE FORWARD TWO TRACK LIGHTS WERE FOUND INOPERATIVE. RECONNECTED WIRING AND LIGHTS OPERATED NORMALLY. (M)

Part: LIGHT — BROKEN (CABIN)

PDX - DURING MAINTENANCE CHECK, THE FORWARD THREE EMERGENCY TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. REPLACED BROKEN LIGHT ASSEMBLY AND LIGHTS OPERATED NORMALLY. (M)

Part: MECHANISM — LACK OF LUBE (L1 DOOR)

LAX - PRIOR TO FLT 477 - THE L1 DOOR WOULD NOT CLOSE PROPERLY. CLEANED AND LUBRICATED ROLLER GUIDES AND LOCK ROLLERS, DOOR CLOSED AND LOCKED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

PDX - FLT 424 - PRIOR TO FLT, THE EMERGENCY FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE AT ROWS 22-25. RECONNECTED LIGHTS AND LIGHTS OPERATED NORMALLY. (M)

Part: WINDOW MECH — OUT OF ADJUST (LT COCKPIT)

SEA - FLT 299 - CREW REPORTED THAT THE CAPTAINS L-2 SLIDING WINDOW WAS EXTREMELY DIFFICULT TO CLOSE. ADJUSTED CAPTAINS L-2 SLIDING WINDOW AND THE WINDOW OPENED AND CLOSED NORMALLY. (M)

Part: SKIN — GOUGED (RUDDER)

SEA - DURING C-CHECK, THE RUDDER LEFT SIDE FORWARD EDGE SKIN WAS FOUND TO BE GOUGED. REPAIRED PER EA 5540-01016 AND BOEING TELEX ASA-SEA-97-0415RR. (M)

Part: RETAINER — MISDRILLED (BS 200)

SEA - DURING C-CHECK, THE L1 WINDOW POST RETAINER WAS FOUND TO BE MISDRILLED. REPAIRED PER FIELD REWORK RECORD NR 1, DATED 9/30/97. (M)

Part: SPOILER — PUNCTURED (RT WING)

SEA - DURING C-CHECK, A PUNCTURE WAS FOUND ON THE RIGHT INBOARD GROUND SPOILER LOWER SURFACE. REPAIRED PER EA 5770-01002 AND BOEING TELEX ASA-SEA-97-0461RR. (M)

Part: SPAR — GOUGED (WS 196)

SEA - DURING C-CHECK, GOUGES WERE FOUND ON THE FORWARD CHORD FLANGE AT RIGHT AND LEFT OUTER WING FRONT SPAR WING STATION 796.846. REPAIRED PER EA 5720-01131 AND BOEING TELEX M-7272-974829. (M)

Part: RETAINER — MISDRILLED (BS 200)

SEA - DURING C-CHECK, THE R1 WINDOW POST RETAINER WAS FOUND TO BE MISDRILLED. REPAIRED PER FIELD REWORK RECORD NR 1, DATED 9/30/97. (M)

Part: SUPPORT — CORRODED (FS807-827)

SEA - DURING C-CHECK, THE FLOOR SUPPORT AT STATION RBL 20 STATION 807 TO 827 WAS FOUND TO BE CORRODED. REPAIRED PER EA 5320-01322. (M)

Part: TAPE REPRODUCER — SMOKING (CABIN)

SNA - FLT 186 - BEFORE DESCENT INTO SNA, THE TAPE REPRODUCER HAD AN ELECTRICAL SMOKE EMANATING FROM IT. THE CREW ISOLATED THE SYSTEM BY PULLING THE APPROPRIATE CIRCUIT BREAKER CAUSING THE SMOKE TO STOP. CONTRACT MX INSPECTED, DEACTIVATED AND DEFERRED THE TAPE REPRODUCER. THE TAPE REPRODUCER WAS SUBSEQUENTLY REMOVED AND REPLACED BY MX AND REMOVED UNIT WAS ROUTED TO SEA AVIONICS SHOP FOR INSPECTION AND REPAIR. THE TAPE REPRODUCER DOOR LOCK SOLENOID AND LATCH WERE REPLACED AND THE TAPE REPRODUCER OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

ANC - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS AT ROWS 22 THROUGH 25 AND ROWS 26 AFT WERE FOUND INOPERATIVE. RECONNECTED LOOSE WIRING AND LIGHTS OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

SEA - FLT 230 - DURING CREW PREFLIGHT, THE CREW REPORTED THAT THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE INOPERATIVE ROWS 20 TO 26. REPAIRED WIRING AND LIGHTS OPERATED NORMALLY. (W)

Part: WIRE — DISCONNECTED (CABIN)

SMF - FLT NR 409 - DURING CREW PRE-FLIGHT THE CREW REPORTED THAT THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE INOPERATIVE ROWS 23-25. RECONNECTED WIRES IN SECTION OF INOPERATIVE TRACK LIGHTS AND LIGHTS OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

ANC - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS FOUND INOPERATIVE FROM ROW 26 AFT. RECONNECTED TRACK WIRING AT ROW 26. LIGHTS OPERATED NORMALLY. (X)

Part: SOCKET — DISCONNECTED (CABIN)

SEA - DURING MAINTENANCE CHECK, FOUND AFT MOST SECTION OF EMERGENCY EXIT FLOOR TRACK LIGHTING INOPERATIVE. RECONNECTED TRACK LIGHT SOCKET; LIGHTS OPERATED NORMALLY. (X

Part: TIRE ASSY — LOST TREAD (NR 1 MLG)

SEA - AIR TURN BACK OF FLIGHT 468 - CREW REPORTED, NR 1 MAIN LANDING GEAR TIRE BLEW TREAD ON TAKEOFF. LANDED WITHOUT INCIDENT. REPLACED NR 1 AND NR 2 MAIN LANDING GEAR TIRE AND WHEEL ASSEMBLIES. REPLACED DAMAGED LEFT INBOARD TRAILING EDGE FLAP. REMOVED LEFT MAIN LANDING GEAR INNER DOOR FOR REPAIRS PER CDL 32-10-4, AND PERFORMED INTERIM REPAIR TO LEFT STRUT PER EA 5720-01085. (M)

Part: WIRE — DISCONNECTED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE AT ROWS 18 AND AFT. RECONNECTED LOOSE TRACK WIRING AT ROW 18 AND LIGHTS OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

JNU - DURING MAINTENANCE CHECK, THE AFT 2 EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. RECONNECTED WIRING AND LIGHTS OPERATED NORMALLY. (M)