N772AS

Part: BATTERY — UNSERVICEABLE (FLASHLIGHT)

FWD CABIN F/A FLASHLIGHT CHARGE INDICATOR INOPERATIVE. R & R SERVICEABLE BATTERY IAW AMM 25-64-06. OPS CHECK GOOD. SECURED WITH SAFETY BREAK AWAY STRAP.

Part: SWITCH — FAILED (COCKPIT)

REPORTED EMERGENCY LIGHTS WILL NOT SHUTOFF WITH SWITCH IN OFF POSITION FROM "ARM" IN FLT DECK. SUSPECT BAD OVERHEAD SWITCH. COULD DUPLICATE. REMOVED AND REPLACED OVERHEAD EMERGENCY LIGHTS SWITCH S7 REF WDM 33 51 11. OPS NORMAL REF MM 33 51 02.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 52,454 hrs · 29,517 cycles

RT OUTBOARD FLAP UPPER AND LOWER SURFACES WERE DELAMINATED. REMOVED AND REPLACED RT AFT FLAP IAW AMM 27 51 39.

Part: SKIN — PUNCTURED (NR 4 SPOILER) · airframe 52,454 hrs · 29,517 cycles

NR 4 SPOILER BLADE SEAL FASTENER PENETRATED THE INSERT AND PUNCTURED THE UPPER SURFACE AND PREVIOUS REPAIR. REMOVED PREVIOUS REPAIR, FABBED FILLED AND DOUBLER AND BONDED REPAIR IAW SRM 51 70 10.

Part: WEDGE — CHAFED (TE FLAP) · airframe 52,454 hrs · 29,517 cycles

RT WING I/B FLAP TRAILING EDGE WEDGE HAS TWO CHAFED AREAS IN PREVIOUS REPAIRS. REMOVED DAMAGED DOUBLERS, PREPPED AREAS, FABRICATED FILLER AND DOUBLER, BONDED REPAIR IAW B737 400 SRM 51 70 10.

Part: SKIN — DELAMINATED (SPOILER) · airframe 52,454 hrs · 29,517 cycles

FOUND DELAMINATION UNDER I/B ARROW ON UPPER SURFACE NR 4 GROUND SPOILER. REMOVED PREVIOUS REPAIR AND DAMAGED AREA FABRICATED FILLER AND DOUBLER AND INSTALLED REPAIR DOUBLERS IAW B737 400 SRM 51 70 10.

Part: INTERCOSTAL — CRACKED (FOREFLAP) · airframe 52,454 hrs · 29,517 cycles

LEFT O/B MID FLAP INTERCOSTAL CRACKED AT I/B FORE FLAP TRACK ROLLER. REMOVED CRACKED INTERCOSTAL, LOCATED DRILLED AND INSTALLED NEW INTERCOSTAL IAW B737 400 SRM 51 40 05.

Part: SKIN — DENTED (TE FLAP) · airframe 52,454 hrs · 29,517 cycles

LEFT INBOARD MID FLAP BULLNOSE DENTED 24 INCHES FROM I/B END. REMOVED DAMAGED SECTION, FABRICATED AND INSTALLED REPAIR DOUBLER IAW B737 400 SRM 57 53 01 FIG 201.

Part: FRAME — DENTED (FUSELAGE) · airframe 52,454 hrs · 29,517 cycles

FRAME DENTED STA 727G BETWEEN 26R 25R. CUT OUT DAMAGED SECTION, FABRICATED AND INSTALLED REPAIR CHANNEL IAW B737 400 SRM 51 70 11 FIG 1.

Part: SKIN — DAMAGED (TE FLAP) · airframe 52,454 hrs · 29,517 cycles

RT OUTBOARD AFT FLAP O/B LOWER END DAMAGED. REMOVED DAMAGED SECTION, FABRICATED AND BONDED FILLER AND DOUBLER IAW B737 400 SRM 51 70 10.

Part: SKIN — DENTED (TE FLAP) · airframe 52,454 hrs · 29,517 cycles

RIGHT I/B AFT FLAP HAS TWO DENTS ON LOWER T/E. REMOVED DAMAGED AREA, FABRICATED AND BONDED REPAIR MATERIAL IAW B737 400 SRM 51 70 10.

Part: DOUBLER — CRACKED (R1 DOOR) · airframe 52,454 hrs · 29,517 cycles

R1 DOOR AFT LOWER CORNER INNER DOUBLER CRACKED. REMOVED DOUBLER, FABRICATED AND INSTALLED NEW DOUBLER IAW B737 400 SRM 51 40 02.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,454 hrs · 29,517 cycles

FUSELAGE SKIN CRACKED AT R1 DOOR LOWER HINGE CUTOUT. REMOVED DAMAGE, FABRICATED DOUBLER FILLER AND TRIPLER. INSTALLED REPAIR PARTS IAW ASA EA 400 53EA 00843.

Part: SKIN — DENTED (FOREFLAP) · airframe 52,454 hrs · 29,517 cycles

LEFT O/B FOREFLAP JUST OUTBOARD OF I/B END HAS 3 DENTS. REPAIRED, BONDED LT O/B FOREFLAP IAW B737 400 SRM 51 70 10.

Part: SKIN — DENTED (FOREFLAP) · airframe 52,454 hrs · 29,517 cycles

LEFT I/B FORE FLAP HAS 2 DENTS AT I/B END LOWER SIDE. PREPPED DAMAGE AREA, FABRICATED REPAIR DOUBLER AND BONDED DOUBLER IAW B737 400 SRM 51 70 10.

Part: DOUBLER — CHAFED (MIDFLAP) · airframe 52,454 hrs · 29,517 cycles

LEFT O/B MID FLAP CHAFED ABOVE I/B AFT FLAP TRACK. REMOVED CHAFED DOUBLER, FABRICATED AND BONDED REPAIR DOUBLER IAW B737 400 SRM 57 53 01.

Part: SLAT — DELAMINATED (RT WING) · airframe 52,454 hrs · 29,517 cycles

RIGHT NR 5 SLAT OUTBOARD T/E DELAMINATED. REMOVED DAMAGED AREA, FABRICATED AND BONDED REPAIR IAW B737 400 SRM 51 70 10.

Part: ACM — LEAKING (RIGHT) · airframe 46,470 hrs · 26,164 cycles

RIGHT PACK TRIP AND CABIN FILLED WITH SMOKE. SMOKE REMOVED FROM CABIN PER AMM 21 00 01. FOUND RT ACM LEAKING BETWEEN TURBINE AND COMPRESSOR SECTIONS. REMOVED AND REPLACED ACM HEPA FILTERS AND COMPLETED CONDITIONAL INSPECTION.

Part: ACM — LEAKING (RIGHT) · airframe 46,442 hrs · 26,146 cycles

RIGHT PACK TRIP AND FILLED CABIN WITH SMOKE. SMOKE REMOVED FROM CABIN PER AMM 21-00-01. FOUND RIGHT ACM LEAKING BETWEEN TURBINE AND COMPRESSOR SECTIONS. REMOVED AND REPLACED ACM O2 FILTER AND COMPLETED CONDITIONAL INSPECTION.

Part: TAB — DAMAGED (RT ELEVATOR) · airframe 45,420 hrs · 25,579 cycles

RIGHT ELEVATOR TAB HAS COMPOSITE LAYERS DAMAGED AT T/E. PREPPED AREA FOR BONDING, FABRICATED AND INSTALLED REPAIR PIECES IAW SRM 51-70-17 AND ASA EA 2730 01107.

Part: SKIN — CHAFED (BS 867-887) · airframe 45,384 hrs · 25,564 cycles

TRIMMED OUT SKIN DAMAGE AND REPAIR FUSELAGE SKIN. REMOVED DAMAGE FABRICATED AND INSTALLED REPAIR DOUBLER ON FUSELAGE SKIN IAW ASA EA 5330 02152.

Part: SKIN — DENTED (NR 5 SPOILER) · airframe 45,384 hrs · 25,564 cycles

5 SPOILER LOWER SKIN DENTED. PREPPED AREA FABRICATED AND INSTALLED REPAIR PIECES IAW SRM 51 70 10.

Part: SKIN — DENTED (TE FLAP) · airframe 45,384 hrs · 25,564 cycles

RT IB TE FLAP LWR SKIN HAS MULTIPLE DENTS. REMOVED DAMAGE FABRICATED AND INSTALLED REPAIR PIECES IAW SRM 51 70 10 REPAIR 2.

Part: SKIN — NICKED (LT TE FLAPS) · airframe 45,384 hrs · 25,564 cycles

LT OB AFT FLAP TE IS NICKED AND SEPARATING JUST OB OF IB TRACK FAIRING. REMOVED DAMAGE FABRICATED AND INSTALLED FILLER AND DOUBLER IAW SRM 51 70 10.

Part: SKIN — CHAFED (NR 2 FLAP) · airframe 45,384 hrs · 25,564 cycles

LT OB MID FLAP PREVIOUS REPAIR AT NR 2 FLAP TRACK IS CHAFED. REMOVED DAMAGED DOUBLER. FABRICATED AND INSTALLED REPAIR DOUBLER IAR SRM 51 70 10.

Part: SKIN — CHAFED (NR 3 SLAT) · airframe 45,384 hrs · 25,564 cycles

NR 3 SLAT IS CHAFED AT LOWER AFT AREA NEAR ACTUATOR. REMOVED DAMAGED AREA FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER IAW SRM 51 70 10.

Part: SKIN — DAMAGED (FORE FLAP) · airframe 45,384 hrs · 25,564 cycles

LT IB FORE FLAP HAS NUMEROUS DINGS BELOW CENTERLINE TRACK. PREPPED AREA FABRICATED AND INSTALLED REPAIR PIECES IAW SRM 51 70 10 REPAIR 2.

Part: WEDGE — CHAFED (RT TE FLAP) · airframe 45,384 hrs · 25,564 cycles

RIGHT I/B MID FLAP T/E WEDGE IS CHAFED. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR FILLERS AND DOUBLERS IAW SRM 51-70-10.

Part: SKIN — DENTED (FORE FLAP) · airframe 45,384 hrs · 25,564 cycles

RT IB FORE FLAP LWR SKIN DENTED. REMOVED DAMAGED AREAS FABRICATED AND INSTALLED REPAIR PIECES IAW SRM 51 70 10.

Part: SKIN — DENTED (NR 5 SPOILER) · airframe 45,384 hrs · 25,564 cycles

NR 5 SPOILER UPPER SKIN HAS CLUSTERS OF DENTS. PREPPED AREA FABRICATED AND INSTALLED REPAIR PIECES IAW SRM 51 70 10.

Part: SKIN — CHAFED (NR 3 SLAT) · airframe 45,384 hrs · 25,564 cycles

NR 3 SLAT CHAFED AT OB END LWR SURFACE. REMOVED DAMAGE FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER IAW SRM 51 70 10.

Part: SKIN — GROUND DAMAGE (BS 315) · airframe 43,500 hrs · 24,529 cycles

FOUND L1 UPPER FWD HINGE CUTOUT HAS TORN SKIN FROM JETWAY DAMAGE. INSTALLED REPAIR DOUBLER PER SRM 52 00 01 REPAIR 2.

Part: SHAFT — DAMAGED (R1 DOOR HANDLE)

SEA - R-1 DOOR HANDLE WILL NOT STAY IS STOWED POSTION. DOOR HANDLE SHAFT AND SLEEVE ASSY WAS REPLACED AND DOOR RIGGED PER AMM. (M)

Part: COMPRESSOR — CONTAMINATED (ENGINE)

OKC - FOUND TAKEOFF ROLL POWER SET, COCKPIT FILLED WITH SMOKE. TAKEOFF ABORTED LESS THAN 45 KTS. REMOVED SMOKE FUMES FROM CABIN PER B737-400 AMM 21-00-01 AND AMM SUPPLEMENT 72-00-00. PARTIAL WORK ACCOMPLISHED ON MIG-2C 057320. ENGINE COMPRESSOR WASH PERFORMED DURING OVERNIGHT MAINTENANCE. A SLIGHT RESIDUAL DETERGENT ODOR MAY BE EVIDENT DURING THE FIRST TAKEOFF OF THE DAY, BUT IS NOT HARMFUL AND WILL CLEAR FRO THE CABIN QUICKLY. (M)

Part: STRUCTURE — BENT (TE FLAP)

OKC - FOUND RIGHT INBOARD AFT FLAP OUTBOARD EDGE BENT, LOWER SIDE. REMOVED DAMAGE, FABRICATED AND INSTALLED FILLER AND DOUBLER IAW 737-400 SRM 51-70-10. (M)

Part: SKIN — DENTED (FS 986-1016)

OKC - FOUND FUSELAGE SKIN DENTED AT BS 1000 .5 INCH BELOW STRINGER 14R. REMOVED DAMAGED SECTION OF STRAP, FABRICATED AND INSTALLED LAP REPAIR IAW 737-400 SRM 53-00-01 FIGURE 201 AND ASA EA 5330-01999. (M)

Part: SKIN — PUNCTURED (TE FLAP)

OKC - FOUND LEFT OUTBOARD AFT FLAP PUNCTURED. REMOVED DAMAGE, FABRICATED AND INSTALLED FILLER AND DOUBLER IAW 737-400 SRM 51-70-10. (M)

Part: FLOOR SUPPORT — CORRODED (FS 270)

OKC - FOUND FLOOR SUPPORT IN FLIGHT DECK ENTRY WAY IS CORRODED AT STATION 270. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR PIECES IAW ASA EA 5310-02501. (M)

Part: FLOORBEAM — CORRODED (FS 986.5)

OKC - FOUND FLOORBEAM STATION 986.5 CORRODED ON UPPER CHORD. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR PIECES IAW ASA EA 5310-02498. (M)

Part: SKIN — DENTED (FS 986-1016)

OKC - FOUND FUSELAGE SKIN DENTED AT BS 1006.5 BETWEEN STRINGER 13-14 RT. REMOVED SKIN, REPLACED WITH NEW SKIN IAW ASA EA 5330-01999 AND 737-400 SRM 51-40-2. (M)

Part: FLOORBEAM — PUNCTURED (FS 947)

OKC - FOUND FLOORBEAM BS 947 CORRODED AROUND FASTENER HOLES AT LBL 45, RBL 45. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR PIECES IAW ASA EO 5310-02500. (M)

Part: SKIN — PUNCTURED (TE FLAP)

OKC - FOUND RIGHT OUTBOARD AFT FLAP HAS PUNCTURE APPROX 44 INCH FROM INBOARD END. REMOVED DAMAGE, FABRICATED AND INSTALLED FILLER AND DOUBLER IAW 737-400 SRM 51-70-10. (M)

Part: SKIN — BENT (TE FLAP)

OKC - FOUND LEFT OUTBOARD FORE FLAP DENTED, LOWER T/E 21 INCHES FROM INBOARD END. REMOVED DAMAGE, FABRICATED AND INSTALLED FILLER AND DOUBLER IAW 737-400 SRM 51-70-10. (M)

Part: SKIN — BENT (TE FLAP)

OKC - FOUND RIGHT INBOARD AFT FLAP T/E BENT. REMOVED DAMAGE, FABRICATED AND INSTALLED FILLER AND DOUBLER IAW 737-400 SRM 51-90-10. (M)

Part: STRAP — GOUGED (FS 1152)

OKC - FOUND FUSELAGE SKIN STRAP AT BS 1150 STRINGER 20R GOUGED. REMOVED DAMAGED SECTION OF STRAP, FABRICATED AND INSTALLED REPAIR STRAP AND FILLER IAW ASA EA 5310-02499. (M)

Part: SPLICE — CORRODED (FS 344)

OKC - FOUND BS 344 UPPER CHORD SPLICE REPAIR CORRODED. REMOVED CORRODED CHORD REPAIR, FABRICATED AND INSTALLED REPAIR PIECES IAW ASA EA 5310-02494. (M)

Part: STIFFENER — CORRODED (FS 1127)

OKC - FOUND VERTICAL STIFFENER EXFOLIATED RIGHT SIDE OF TORQUE BOX AT BS 1127. REMOVED STIFFENER, FABRICATED AND INSTALLED REPLACEMENT STIFFENER IAW 737-400 SRM 51-40-5 AND 51-40-3. (M)

Part: FLOORBEAM — CORRODED (FS 328)

OKC - FOUND FLOORBEAM UPPER CAP CORRODED AT BS 328. REMOVED CHORD, UPPER, FABRICATED AND INSTALLED CHORD AND REPAIR PIECES IAW ASA EA 5310-02489. (M)

Part: FLOORBEAM — DAMAGED (FS 312)

OKC - FOUND BS 312 FLOORBEAM UPPER CHORD DAMAGED. REMOVED DAMAGE, FABRICATED AND INSTALLED UPPER CHORD REPAIR PIECES IAW B737-400 SRM 53-10-51 FIG 201. (M)

Part: SKIN — DENTED (TE FLAP)

OKC - FOUND RIGHT INBOARD FORE FLAP DENTED ON LOWER SURFACE 42 INCHES INBOARD END AND PERCENT FROM L/E. REMOVED DAMAGE, FABRICATED FILLER AND DOUBLER, THE INSTALLED REPAIR FILLER AND DOUBLER IAW 737-400 SRM 51-70-10. (M)

Part: SKIN — GOUGED (TE FLAP)

OKC - FOUND RIGHT INBOARD AFT FLAP T/E DAMAGED THREE PLACES. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR SIN AND DOUBLER IAW 737-400 SRM 51-70-10. (M)

Part: SKIN — DENTED (TE FLAP)

OKC - FOUND RIGHT OUTBOARD FLAP DISBONDING AT INBOARD TRAILING EDGE. REMOVED DAMAGE, FABRICATED FILLER AND DOUBLER, THEN INSTALLED REPAIR FILLER AND DOUBLER IAW 737-400 SRM 51-70-10. (M)

Part: STRINGER — CORRODED (FUSELAGE)

OKC - FOUND STRINGER "T" CHORD RT SIDE OF APU CUTOUT TORQUE BOX IS EXFOLIATED. REMOVED "T" CHORD, FABRICATED AND INSTALLED REPLACEMENT "T" CHORD IAW 737-400 SRM 51-40-60 AND 51-40-02. (M)

Part: REPAIR — DEBONDED (TE FLAP)

OKC - FOUND RIGHT INBOARD FORE FLAP PREVIOUS REPAIR IS DISBONDING. REMOVED DAMAGE, FABRICATED FILLER AND DOUBLER, THEN INSTALLED REPAIR PIECES IAW 737-400 SRM 51-70-10. (M)

Part: SKIN — DENTED (FS 385)

OKC - FOUND DENT ON PREVIOUS REPAIR DOUBLER ON FUSELAGE SKIN STATION 385 ABOVE STRINGER 16 LEFT. REMOVED PREVIOUS REPAIR, FABRICATED REPAIR DOUBLER AND TRIPLER, INSTALLED REPAIR PIECES IAW B737-400 SRM 53-00-01 FIG 201. (M)

Part: STRAP — CRACKED (FS 312-328)

OKC - FOUND FLOORBEAM STABILIZER STRAP AT BS 312, RBL 46 IS CRACKED. FABRICATED STRAP AND REPAIR SPLICE, INSTALLED REPAIR PIECE IAW 737-400 SRM 53-10-51 FIG 201. (M)

Part: SKIN — DENTED (TE FLAP)

OKC - FOUND RIGHT INBOARD AFT FLAP IS DENTED 36 INCHES FROM INBOARD END. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR SKIN AND DOUBLER IAW 737-400 SRM 51-70-10. (M)

Part: SUPPORT — CORRODED (FS 344-360)

OKC - FOUND INTERCOSTAL AT BS 344-360 RBL 50 IS GOUGED AND CORRODED. REMOVED CORRODED T-EXTRUSION, FABRICATED AND INSTALLED REPLACEMENT "T" IAW ASA EA 5310-02490.

Part: DOOR — CORRODED (FS 927-1006)

OKC - FOUND CORROSION AROUND FASTENER HOLES ON INNER CHORD AT BS 927-1006, INBOARD OF R-2 DOOR. REMOVED CORRODED CHORD, REPLACED WIT NEW CHORD IAW 737-400 SRM 51-40-02. (M)

Part: FLOOR SUPPORT — CORRODED (BS 267-350)

OKC - FOUND FLOOR SUPPORT ANGLE CHORD IS CORRODED AT BS 267-350 LBL 54. REMOVED CORRODED CHORD, REPLACED CHORD IAW 737-400 SRM 51-40-02.

Part: DOOR FRAME — CORRODED (BS 259-360)

OKC - FOUND INNER CHORD AT BS 259-360 AT RBL 55 IS CORRODED AT R-1 DOOR AREA. REMOVED CORRODED CHORD, REPLACED WITH NEW CHORD IAW 737-400 SRM 51-40-02. (M)

Part: FITTING — CORRODED (TE FLAP)

OKC - FOUND RIGHT INBOARD MID FLAP OUTBOARD TORQUE TUBE FITTING CORRODED. REMOVED AND REPLACED TORQUE TUBE FITTING IAW 737-400 SRM 51-40-02. (M)

Part: TAB — GOUGED (RT ELEVATOR)

OKC - FOUND RIGHT ELEVATOR DAMAGED AT T/E, OUTBOARD OF TRIM TAB. PREPPED DAMAGED AREA, BONDED REPAIR IAW 737-400 SRM 51-70-04 REPAIR 11. (M)

Part: FLOOR SUPPORT — CORRODED (FS 942-969)

OKC - FOUND INNER CHORD ON FLOOR SUPPORT AT BS 942-989 IS CORRODED. REMOVED CORRODED CHORD, REPLACED WITH NEW CHORD IAW 737-400 SRM 51-40-02. (M)

Part: CREASE BEAM — DAMAGED (FS 360-385)

OKC - FOUND STRINGER 17 CREASE BEAM HAS SHORT EDGE DISTANCE FROM PREVIOUS REPAIR. REMOVED DAMAGED SECTION OF CREASE BEAM AND INSTALLED NEW SECTION OF CREASE BEAM IAW B737-400 SRM 53-00-01 FIG 201 AND SRM 51-40-02. (M)

Part: FLANGE — DELAMINATED (WS 613)

OKC - FOUND LEFT AILERON L/E FLANGE DELAMINATED AT WS 613. PREPPED DAMAGED AREA, ACCOMPLISHED HOT BOND REPAIR AT WS 613 IAW B737-400 SRM 51-70-05. (M)

Part: FLANGE — DELAMINATED (WS 607)

OKC - FOUND LEFT AILERON L/E FLANGE DELAMINATED AT WS 607. PREPPED DAMAGED AREA, ACCOMPLISHED HOT BOND REPAIR AT WS 607 IAW B737-400 SRM 51-70-05. (M)

Part: TEAR STRAP — DAMAGED (FS 375)

OKC - FOUND TEAR STRAP DAMAGED BEHIND SKIN REPAIR AT BS 375, STRINGER 16 LEFT. FABRICATED AND INSTALLED DOUBLER FOR TEAR STRAP IAW B737-400 SRM 53-00-01 FIG 201. (M)

Part: SKIN — DELAMINATED (LT AILERON)

OKC - FOUND LEFT AILERON NOSE SKIN DAMAGED AT WS 574. PREPPED DAMAGED AREA, ACCOMPLISHED HOT BOND REPAIR IAW B737-400 SRM 51-70-05. (M)

Part: SKIN — GOUGED (AILERON)

OKC - FOUND LEFT AILERON OUTBOARD ATTACH AREA IS GOUGED. PREPPED GOUGED AREA, ACCOMPLISHED HOT BOND REPAIR IAW B737-400 SRM 51-70-05. (M)

Part: TAB — PUNCTURED (RT ELEVATOR)

OKC - FOUND RIGHT ELEVATOR TAB IS PUNCTURED. PREPPED DAMAED AREA, APPLIED HOT BOND REPAIR IAW 737-400 SRM 51-70-04 REPAIR 1. (M)

Part: SHEAR TIE — CORRODED (FS 807)

OKC - FOUND BS 807 SHEAR TIE CORRODED BETWEEN STRINGER 26-27 LEFT. REMOVED DAMAGED SECTION OF SHEAR TIE, FABRICATED SHEAR TIE AND REPAIR PARTS AND INSTALLED PARTS IAW B737-400 SRM 53-00-07 FIG 101 AND 53-00-07 FIG 201. (M)

Part: FLOORBEAM — CORRODED (FS 312)

OKC - FOUND FLOORBEAM AT BS 312 UPPER CHORD IS CORRODED. REMOVED CORRODED SECTION OF UPPER CHORD, FABRICATED AND INSTALLED REPAIR CHORD AND REPAIR PARTS IAW B737-400 SRM 53-10-51 FIGURE 201. (M)

Part: SHEAR TIE — CORRODED (FS 847)

OKC - FOUND BS 847 SHEAR TIE BETWEEN STRINGERS 26 LEFT AND 27 LEFT CORRODED. REMOVED DAMAGED SECTION OF SHEAR TIE, FABRICATED AND INSTALLED REPAIR PIECES IAW B737-400 SRM 53-00-07. (M)

Part: FLOORBEAM — CORRODED (FS 360)

OKC - FOUND CORROSION ON FLOORBEAM AT BS 360. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR PARTS IAW B737-400 SRM 53-00-51 FIG 201. (M)

Part: FLOORBEAM — CORRODED (BS 294.5)

OKC - FOUND HAT CHANNEL ON FLOORBEAM AT BS 294.5 IS CORRODED. REMOVED CHANNEL, FABRICATED AND INSTALLED REPLACEMENT CHANNEL IAW B737-200 SRM 51-40-02 AND AMM 51-21-21. (M)

Part: SHEAR TIE — CORRODED (FS 827)

OKC - FOUND BS 827 SHEAR TIE BETWEEN 26 LEFT AND 27 LEFT CORRODED OUT OF LIMITS ON ATTACH FLANGE. CORRODED SHEAR TIE REMOVED AND REPLACEMENT SHEAR TIE SPLICED INTO FRAME. (M)

Part: FLOORBEAM — CORRODED (FS 294.5)

OKC - FOUND UPPER CHORD OF FLOORBEAM AT BS 294.5 IS CORRODED. REMOVED CORRODED SECTION OF CHORD. FABRICATED REPLACEMENT CHORD AND INSTALLED IAW B737-200 SRM 53-10-51 FIG 201. (M)

Part: FLOOR PANEL — DAMAGED (FS 983)

OKC - FOUND FLOOR WEB AT RBL 45 BS 983 HAS ELONGATED HOLES. REMOVED DAMAGED PART, FABRCIATED AND INSTALLED REPAIR PIECES IAW 737-400 SRM 51-30-01 AND 51-40-2. (M)

Part: ANGLE — CRACKED (BS 289)

OKC - FOUND ANGLE CRACKED AT BS 289 STRINGER 10 RIGHT. REMOVED CRACKED ANGLE, REPLACED WITH NEW PART IAW 737-400 SRM 51-40-2. (M)

Part: WEDGE — GOUGED (TE FLAP)

OKC - FOUND RIGHT INBOARD FLAP TRAILING EDGE WEDGE GOUGED IN TWO PLACES. REPLACED RIGHT INBOARD FLAP TRAILING EDGE IAW B737-400 SRM 51-40-5, AND 08. (M)

Part: SHEAR WEB — CORRODED (FS 989-992)

OKC - FOUND SHEAR WEB CORRODED AT BS 989 LBL 35. REMOVED SHEAR WEB, FABRICATED AND INSTALLED REPLACEMENT PARTS IAW B737-400 SRM 53-60-1 AND 51-40-05. (M)

Part: ANGLE — CRACKED (FS 289)

OKC - FOUND ANGLE CRACKED AT BS 289 STRINGER 12 RT. REMOVED CRACKED ANGLE, REPLACED WITH NEW PART IAW B737-400 SRM 51-40-2. (M)

Part: RIB — CRACKED (HORIZONTAL STAB)

OKC - FOUND LEFT HORIZONTAL L/E HAS CRACKED RIB AT BS 244.72. REMOVED AND REPLACED RIB ON L/E AT BS 244.72 IAW B737-400 SRM 51-40-02. (M)

Part: SKIN — GOUGED (RT AILERON)

OKC - FOUND RIGHT AILERON GOUGED AT CUTOUT FOR INBOARD MOUNT. PREPPED DAMAGED AREA, APPLIED LAY-UP REPAIR IAW B737-400 SRM 51-70-03 REPAIR 10. (M)

Part: ANGLE — CRACKED (FS 289)

OKC - FOUND ANGLE CRACKED AT BS 289, STRINGER 11R. REMOVED AND REPLACED CRACKED ANGLE WITH NEW PART IAW B737-400 SRM 51-40-2. (M)

Part: SHEAR TIE — DAMAGED (BS 986)

OKC - SHEAR TIE AT BS 986, RBL 49 HAS ELONGATED FASTENER HOLES. REMOVED DAMAGED SHEAR TIE, FABRICATED AND INSTALLED REPLACEMENT SHEAR TIE IAW B737-400 SRM 51-30-1, AND 51-30-3.

Part: PLATE — CRACKED (FS 601)

OKC - FOUND SPLICE PLATE RIGHT SIDE CRACKED AT BS 601, STRINGER 15 RT. REMOVED CRACKED SPLICE PLATE, FABRICATED AND INSTALLED REPLACEMENT SPLICE PLATED IAW B737-400 SRM 51-30-1 AND 2. (M)

Part: STRINGER CLIP — CORRODED (FS 807)

OKC - FOUND STRINGER TIE CLIP BS 807 STRINGER RT IS CORRODED. REMOVED CLIP, FABRICATED AND INSTALLED NEW CLIP IAW B737-400 SRM 51-30-1, AND 51-40-2. (M)

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

PAE - FWD CARGO BAY AREAS OF CORROSION ON FLOOR TO SIDEWALL SUPPORT BS 500F TO 500G, LBL 23, WL 156. (K)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2

PAE - CORROSION AFT CARGO BAY CORROSION AT FLOOR SUPPORT. REPAIRED IAW SRM, FABRICATED AND INSTALLED SPLICE. (K)

Part: SUPPORT — CORRODED (FUSELAGE)

PAE - FWD CARGO BAY AREAS OF CORROSION ON FLOOR TO SIDEWALL SUPPORT, BS 757 TO 897, LBL23, WL 156. REMOVED AND REPLACED FLOOR TO SIDEWALL STRAP. (K)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2

PAE - AFT CARGO BAY AREAS OF CORROSION ON FLOOR SUPPORT JOGGLE FOR NR 3 FLOOR PANEL SUPPORT. REPAIRED IAW SRM. (K)

Part: SUPPORT — CORRODED (FUSELAGE)

PAE - FWD CARGO BAY AREAS OF CORROSION ON FLOOR TO SIDEWALL SUPPORT BS 390 TO 452, LBL 23, WL 156. REMOVED AND REPLACED FLOOR TO SIDEWALL STRAP. (K)

Part: SILL — GOUGED (FUSELAGE)

PAE - AFT CARGO DOOR CUTOUT CENTER SILL PLATE GOUGED. REPLACED GOUGED SILL PLATE WITH NEW IAW SRM. (K)

Part: SHEAR TIE — CORRODED (FUSELAGE)

PAE - CORRODED SHEAR TIE AT BS 747, LBL 12.5 TO RBL 24. WI 148. REPAIRED SHEAR TIE BS 747, LBL8-13. (K)

Part: SHEAR TIE — CORRODED (FUSELAGE)

PAE - CORROSION AFT CARGO BAY CORROSION SHEAR TIE AT BS 727G, LBL 17.20 TO RBL 13.8, WL 148. REPAIRED SHEAR TIE IAW SRM AND DWG. (K)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

PAE - CORROSION ON FLOOR SUPPORT. REMOVED AND REPLACED. (K)

Part: SHEAR TIE — CORRODED (FUSELAGE)

PAE - CORROSION ON SHEAR TIE. REMOVED AND REPLACED SHEAR TIE. (K)

Part: SHEAR WEB — DAMAGED (FUSELAGE)

PAE - DAMAGED SHEAR WEB BS 460-480, LBL 36, WL 152. REPLACED SHEAR WEB IAW SRM AND DWG. (K)

Part: SHEAR TIE — CORRODED (FUSELAGE)

PAE - CORROSION ON SHEAR TIE AT BS 747, RBL 6 TO LBL 6. REPAIRED SHEAR TIE (FRAME) AT BS 747, RBL 6, LBL6. (K)

Part: PRESSURE PANEL — CHAFED (FUSELAGE)

PAE - LT MAIN WHEEL WELL CUTOUT VERTICAL WEB CHAFED AT LBL 45. REPAIRED LT MAIN WHEEL WELL CUTOUT VERTICAL WEB AT BS 700 WL, 140 LBL 45. (K)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

PAE - CORROSION ON NR 1 FLOOR SUPPORT STRAP AT BS 727D + 5 INCHES. REMOVED AND REPLACED NR 1 FLOOR SUPPORT STRAP. (K)

Part: SUPPORT ANGLE — CORRODED (FUSELAGE)

PAE - CORROSION ON BULKHEAD SUPPORT ANGLE. REMOVED AND REPLACED. (K)

Part: ANGLE — CORRODED (FUSELAGE)

PAE - CORROSION ON FAIL SAFE ANGLE. CUT OUT DAMAGE, INSTALLED REPAIR. (K)

Part: STRINGER CLIP — CRACKED (FUSELAGE)

PAE - CRACKED STRINGER CLIP. REPLACED AFTER REMOVAL OF DAMAGED (CRACKED) STRINGER CLIP. (K)

Part: COVER — CORRODED (COCKPIT) · corrosion level 2

PAE - FLIGHT DECK MANUAL GEAR EXTENSION COVER CORROSION ON LOWER SURFACE. REMOVED, FABRICATED, AND INSTALLED NEW COVER. (K)

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · corrosion level 2

PAE - AFT CARGO BAY CORROSION ON (Z) SUPPORT ANGLE, AFT SIDE OF 948 BULKHEAD. REMOVED, FABRICATED AND INSTALLED THE (Z) ANGLE AFTER CORROSION BLENDED OUT OF LIMITS. (K)

Part: SKIN — CRACKED (L/E SLAT)

PAE - L/W NR 1 SLAT LOWER L/E SKIN CRACKED. ACCESSED AREA, FABRICATED REPAIR, INSTALLED REPAIR PARTS, CLOSED AREA. (K)

Part: SHEAR TIE — CORRODED (FUSELAGE)

PAE - CORROSION ON SHEAR TIE AT STA 747 RBL 8 TO RBL 13. REMOVED CORRODED SHEAR TIE, FABRICATED SHEAR TIE REPAIR ANGLE AND CLIPS AND INSTALLED. (K)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

PAE - AFT CARGO BAY, CORROSION ON NR 2 FLOOR SUPPORT STRAP AT BS 727F+7 INCHES, LBL 23 TO RBL23, WL 156. REPLACED NR 2 FLOOR SUPPORT STRAP AT BSTA 727F + 7 INCHES, LBL 23 TO RBL 23, WL 156 IN AFT CARGO BAY. (K)

Part: SHEAR WEB — DAMAGED (FUSELAGE)

PAE - FWD CARGO BAY SHEAR WEB DAMAGED AT BS 400-420, LBL 23, WL 156. REPLACED SHEAR WEB IAW SRM AND DWG. (K)

Part: SHEAR TIE — CORRODED (FUSELAGE)

PAE - AFT CARGO BAY CORROSION ON SHEAR TIE (FRAME) STA 787. REPAIRED IAW SRM, SHEAR TIE AT B-STA 787, LBL 12.5, RBL 13.8, WI 146. (K)

Part: PANEL — DAMAGED (NR 4 SPOILER)

PAE - NR 4 SPOILER PANEL LOWER SURFACE HAS GRAVEL DAMAGE. CUT OUT SKIN AND CORE FOR 3 EACH AREAS THAT WERE OUT OF ALLOWABLE LIMITS AND REPAIRED USING HOT BOND IAW SRM. (K)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

PAE - AFT CARGO BAY CORROSION ON NR 3 FLOOR SUPPORT STRAP. REPLACED STRAP. (K)

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

PAE - AFT CARGO BAY CORROSION ON SHEAR TIE. REPAIRED SHEAR TIE. (K)

Part: STRAP — CORRODED (FUSELAGE) · airframe 39,770 hrs · 22,543 cycles

PAE - AFT CARGO BAY CORROSION ON FLOOR STRAP. REPLACED FLOOR STRAP. (K)

Part: SHEAR TIE — CORRODED (FUSELAGE)

PAE - AFT CARGO BAY CORROSION ON SHEAR TIE. REPLACED DAMAGED SECTION OF SHEAR TIE B-STA 867, LBL 5 TO RBL 5, WL 154, IAW SRM. (K)

Part: SHEAR TIE — CORRODED (FUSELAGE)

PAE - FWD CARGO BAY CORROSION ON SHEAR TIE AT BSTA 500F, RBL 10, WL 148. REPAIRED SHEAR TIE AT B-STA 500F, RBL 10, WI 148 IAW SRM. (K)

Part: STRAP — CORRODED (FUSELAGE)

PAE - CORROSION ON FLOOR STRAP. REPLACED STRAP. (K)

Part: SHEAR TIE — CORRODED (FUSELAGE)

PAE - AFT CARGO BAY CORROSION ON SHEAR TIE (FRAME). REPAIRED SHEAR TIE IAW SRM. (K)

Part: SHEAR TIE — CORRODED (FUSELAGE)

PAE - AFT CARGO BAY CORROSION ON SHEAR TIE (FRAME). REPAIRED SHEAR TIE. (K)

Part: SHEAR WEB — DAMAGED (FUSELAGE)

PAE - DAMAGED SHEAR WEB. REMOVED AND REPLACED. (K)

Part: SHEAR WEB — DAMAGED (FUSELAGE)

PAE - DAMAGED SHEAR WEB. REMOVED AND REPLACED. (K)

Part: SHEAR WEB — DAMAGED (FUSELAGE)

PAE - DAMAGED FLOOR SHEAR WEB AT 500D-500E, LBL 36, WL 152. REMOVED AND REPLACED. (K)

Part: SHEAR TIE — CORRODED (FUSELAGE)

PAE - CORROSION ON SHEAR-TIE AT B-STA 440, LBL 3, WL 148. REPAIRED SHEAR TIE IAW SRM. (K)

Part: SHEAR WEB — BENT (FUSELAGE)

PAE - DAMAGED FLOOR SUPPORT SHEAR WEB AT B-STA 500-500A, LBL 36, WL 152. REMOVED AND REPLACED SHEAR WEB AT B-STA 500-500A, LBL36, WL 152. (K)

Part: SHEAR WEB — DAMAGED (FUSELAGE)

PAE - DAMAGED SHEAR WEB. REMOVED AND REPLACED.

Part: SHEAR TIE — CORRODED (FUSELAGE)

PAE - AFT CARGO BAY CORROSION ON SHEAR TIE B-STA 807, LBL5 TO RBL 5, WL 148. REPAIRED IAW SRM. (K)

Part: SHEAR WEB — DAMAGED (FUSELAGE)

PAE - DAMAGED SHEAR WEB. REMOVED AND REPLACED. (K)

Part: SUPPORT — CORRODED (FUSELAGE)

PAE - AFT CARGO BAY CORROSION ON FLOOR-TO-SIDEWALL SUPPORT. REMOVED AND REPLACED. (K)

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

PAE - AFT CARGO BAY CORROSION ON FLOOR -TO-SIDEWALL SUPPORT. REMOVED AND REPLACED. (K)

Part: SHEAR TIE — CORRODED (FUSELAGE)

PAE - CORROSION ON SHEAR TIE B-STA 747, RLB 15 TO RBL 20. REPAIRED SHEAR TIE IAW SRM. (K)

Part: SKIN — GOUGED (LT FORE FLAP)

PAE - LT IB FORE FLAP IS GOUGED 44 INCHES FROM IB END, 8 INCHES FROM T/E ON UPPER SURFACE. CUTOUT UPPER SKIN AND CORE (APPROX 56 SQ INCHES) AND REPAIRED WITH HOT BOND IAW SRM. (K)

Part: DOOR FRAME — GOUGED (AFT GALLEY DOOR)

PAE - AFT GALLEY DOOR FWD SLIDE GOUGED ADJACENT TO UPPER LATCH CRANK. REMOVED AND REPLACED AFT GALLEY DOOR SIDE FRAME. (K)

Part: SHEAR TIE — CORRODED (FUSELAGE)

PAE - CORROSION ON SHEAR TIE B-STA 767, LBL 8.10, WL 146. REMOVED AND REPLACED FRAME SECTION. (K)

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

PAE - CORROSION ON FAIL SAFE CHORD. B-STA 767. REMOVED AND REPLACED IAW SRM. (K)

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

PAE - AFT CARGO BAY CORROSION ON FLOOR TO SIDEWALL SUPPORT. REMOVED CORROSION, FABRICATED REPAIR PARTS AND INSTALLED. (K)

Part: SUPPORT — CORRODED (FUSELAGE)

PAE - FORWARD CARGO BAY, AREAS OF CORROSION ON FLOOR TO SIDEWALL SUPPORT BS 420 TO 440 RBL 23, WL 156. REMOVED AND REPLACED PER 53-30-15, 51-40-02. (M)

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2

PAE - CORROSION ON CARGO TRACK, AFT CARGO BAY, BSTA 947-940, WL 156. REMOVED CARGO TRACK AND INSTALLED NEW CARGO TRACK IAW SRM. (K)

Part: SUPPORT — CORRODED (FUSELAGE)

PAE - FOUND FORWARD CARGO BAY, CORROSION ON FLOOR TO SIDEWALL SUPPORT, BS 500A PLUS 15 INCHES TO 500D PLUS 10 INCHES RBL 23 WL 156. CORROSION OUT OF LIMITS. REMOVED, FABRICATED AND INSTALLED NEW FLOOR TO SIDEWALL SUPPORT BS 500A TO 500G RBL 23 WL 156. (M)

Part: DOOR FRAME — GOUGED (GALLEY DOOR)

PAE - FOUND AFT GALLEY DOOR FORWARD SIDE FRAME GOUGED ADJACENT TO UPPER LATCH CRANK. REMOVED AND REPLACED AFT GALLEY DOOR SIDE FRAME. (M)

Part: WEB — DAMAGED (FUSELAGE)

PAE - FOUND DAMAGED FLOOR SUPPORT SHEAR WEB AT BS 500E-500F RBL 36 WL 152. REMOVED, FABRICATED AND INSTALLED NEW SHEAR WEB. (M)

Part: WEB — DAMAGED (FUSELAGE)

PAE - FOUND DAMAGED FLOOR SUPPORT SHEAR WEB AT BS 500F-500G RBL 36 WL 152. REMOVED, FABRICATED AND INSTALLED NEW SHEAR WEB. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

PAE - FOUND CORROSION AFT CARGO BAY, CORROSION ON FLOOR SUPPORT. REPLACED FLOOR SUPPORT, CUTTING OUT SECTIONS AND SPLICING IN NEW SECTION BS 727E PLUS 10 INCHES TO 727G PLUS 10 INCHES. (M)

Part: FLOOR SUPPORT — DAMAGED (FUSELAGE)

PAE - AFT CARGO BAY FLOOR SUPPORT DAMAGED AT BS 727D PLUS 17. REPAIRED FLOOR SUPPORT PER SRM 53-00-53 FIG 201. (M)

Part: ANGLE — CORRODED (FUSELAGE)

PAE - CORROSION OF FLOOR TO SIDEWALL L-ANGLE TIE. REMOVED, FABRICATED AND INSTALLED PART PER SRM 53-60-53, 51-20-01 AND 51-40-02. (M)

Part: SUPPORT — CORRODED (FUSELAGE)

PAE - AFT CARGO BAY CORROSION ON FLOOR TO SIDEWALL SUPPORT. REMOVED AND REPLACED DAMAGED FLOOR TO SIDEWALL SUPPORT PER SRM 51-40-02, AND 53-60-53. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

PAE - AFT CARGO BAY CORROSION ON UPPER SURFACE OF FLOOR SUPPORT AT FLOORBOARD SUPPORT STRAP. REPAIRED PER SRM 53-00-53 AND EA 5320-01378. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

PAE - AFT CARGO BAY CORROSION ON UPPER SURFACE OF FLOOR SUPPORT AT FLOORBOARD SUPPORT STRAP TOGGLE. REPAIRED PER SRM 53-00-53 AND EA 5320-01378. (M)

Part: SUPPORT — CORRODED (FUSELAGE)

PAE - FORWARD CARGO BAY AREAS OF CORROSION ON FLOOR TO SIDEWALL SUPPORT BS 500G LBL 23 WL 156. PART WILL BE REPLACED ON MIG-5 4878962. (M)

Part: DOOR — GOUGED (APU)

PAE - APU DOOR HAS A GOUGE 3 INCHES AFT FROM HATCH. REPAIRED PER SRM 51-70-13. (M)

Part: FLOOR SUPPORT — DAMAGED (FUSELAGE)

PAE - AFT CARGO BAY FLOOR SUPPORT DAMAGED BS 727F PLUS 7 INCHES TO 727G PLUS 13 INCHES RBL 3, WL 156. COMPLETION ON THIS CARD WILL BE ACCOMPLISHED ON CARD NR 4879499. (M)

Part: SUPPORT — CORRODED (FUSELAGE)

PAE - AFT CARGO BAY CORROSION ON FLOOR TO SIDEWALL SUPPORT. AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT BS 727B PLUS 8 INCHES TO 727F PLUS 7 INCHES, RBL 23 WL 156 WILL BE REPLACED ON 4879144. (M)

Part: SUPPORT — CORRODED (FUSELAGE)

PAE - FOUND FORWARD CARGO BAY AREAS OF CORROSION ON FLOOR TO SIDEWALL SUPPORT AT BS 500D PLUS 10 INCHES TO 500G RBL 23 WL 156. FLOOR TO SIDEWALL SUPPORT OUT OF LIMITS THROUGHOUT ENTIRE LENGTH, TO BE REPLACED ON 4878974. (M)

Part: RETAINER — GOUGED (AFT CARGO BAY)

PAE - AFT CARGO BAY FLOOR RETAINER STRIP GOUGED. GOUGED OUT OF LIMITS. FABRICATED NEW AFT CARGO BAY FLOOR RETAINER STRIP IAW BOEING DWG 65-47951, AMM 51-40-02 PAGE 1 STEP 2. (M)

Part: SUPPORT — CRACKED (FUSELAGE)

PAE - FOUND FORWARD CARGO BAY 1 INCH CRACK ON FLOOR TO SIDEWALL SUPPORT BS 500B RBL 23 WL 156. FLOOR-TO-SIDEWALL SUPPORT TO BE REPLACED ON CARD 478974 BECAUSE OF ADDITIONAL OUT OF LIMITS DISCREPANCIES. (M)

Part: RETAINER — DAMAGED (FUSELAGE)

PAE - AFT CARGO BAY TO FLOOR TO SIDEWALL SUPPORT, HAS EXTRA HOLE IN RETAINER STRIP. REMOVED DAMAGED PART, FABRICATED NEW RETAINER STRIP USING 2024-T3 .063 LOT NR 593315. (M)

Part: FLOORBOARD — GOUGED (FUSELAGE)

PAE - AFT CARGO BAY FLOORBOARD NR 4 GOUGED AT RT FORWARD TIE DOWN CUTOUT. REMOVED GOUGED BY .25 INCH BY 1 INCH, FOUND TO BE OUT OF LIMITS IAW SRM 53-60-53 FIG 101 DETAIL V. FABRICATED, ALODINED AND PRIMED ACB NR 4 FLOORBOARD IAW 51-40-2 STEP 8B AND AMM 51-21-21 STEP 3 MADE OUT OF 2024 T3 .071 INCH LOT 586654 IAW SRM 53-60-95 FIG 1, SH 4, DETAIL NR. (M)

Part: SOCKET — DISCONNECTED (EMERGENCY LIGHT)

JNU - FOUND FLOOR TRACK LIGHTS INOPERATIVE AT SECTION FIRST CLASS ROWS 2-6. RECONNECTED LAMP SOCKET AT ROW 2. OPS CHECK NORMAL. (M)

Part: WIRE — DISCONNECTED (EMERGENCY LIGHT)

JNU - FOUND SIX ADJACENT TRACK LIGHTS INOPERATIVE SEAT ROWS 2-6. RECONNECTED LIGHT ASSEMBLY AT ROW 2. (M)

Part: SEAL DEPRESSOR — CRACKED (R1 DOOR)

GYR - DURING C-CHECK, FOUND CRACK IN UPPER SEAL DEPRESSOR OF R1 DOOR. REPAIR IAW SRM. (M)

Part: STRUCTURE — GOUGED (THRUST REVERSER)

GYR - DURING C-CHECK, FOUND NR 2 ENGINE THRUST REVERSER OUTBOARD HALF INNER CHORD GOUGED AT 6 AND 12 O'CLOCK POSITION. REPAIR IAW SRM. (M)

Part: WIRE — LOOSE (EMERGENCY LIGHT)

SEA - DURING SERVICE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHT INOPERATIVE AT ROW 17. REATTACHED WIRE, OPERATIONAL CHECKED GOOD, RELEASED. (M)

Part: DOUBLER — CORRODED (FUSELAGE)

DURING C-CHECK, FOUND CORROSION ON FRAME DOUBLER AT BS 794 RBL 22-28 AND WL 154. REPAIRED IAW SRM. (M)

Part: CHANNEL — DAMAGED (FUSELAGE)

PAE - DURING C-CHECK, FOUND OVERSIZED HOLES ON CHANNEL AT BS 178 RBL 6-18 AND WL 218. REPAIRED IAW SRM. (M)

Part: MOUNT — CRACKED (FUSELAGE)

PAE - DURING C-CHECK, FOUND MOUNT CRACKED AT BS 204, LBL 5 AND WL 175. REPAIRED IAW SRM. (M)

Part: BRACKET — DAMAGED (FUSELAGE)

DURING C-CHECK, FOUND BRACKETS AT BS 178 RIGHT BL 17-23 AND LEFT BL 25 AND WL 25 HAVE OVERSIZED HOLES. REPAIRED IAW SRM. (M)

Part: CLIP — CRACKED (FUSELAGE)

DURING C-CHECK, FOUND FRAME CLIP AT BS 807, RIGHT BL 20 IS CRACKED IN AFT CARGO BAY. REPAIRED IAW SRM. (M)

Part: FRAME — DAMAGED (FUSELAGE)

DURING C-CHECK, FOUND FRAME AT BS 178 RBL 17 AND WL 182-239 HAS OVERSIZED HOLES. REPAIRED IAW SRM. (M)

Part: BRACKET — DAMAGED (FUSELAGE)

DURING C-CHECK, FOUND BRACKET AT BS 178 RBL 25 AND WL 195 HAS OVERSIZED HOLES. REPAIRED IAW SRM. (M)

Part: STIFFENER — DAMAGED (FUSELAGE)

DURING C-CHECK, FOUND HORIZONTAL STIFFENER AT BS 178 LEFT/RIGHT BL 17-28 AND WL 195 HAS OVERSIZED HOLES. REPAIRED IAW SRM. (M)

Part: BULKHEAD — DAMAGED (FUSELAGE)

DURING C-CHECK, FOUND VERTICAL CHORD AT BS 178 BL 17.1 AND WL 182-239 HAS DAMAGED HOLES. REPAIRED IAW SRM. (M)

Part: SUPPORT — CORRODED (FUSELAGE)

PAE - DURING C-CHECK, FOUND CORROSION ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORTS. REPAIRED IAW SRM. (M)

Part: CHANNEL — DAMAGED (FUSELAGE)

DURING C-CHECK, FOUND HORIZONTAL CHANNELS AT BS 178 REQUIRE REPLACEMENT DUE TO OVERSIZED HOLES. REPAIRED IAW SRM. (M)

Part: CARGO TRACK — CORRODED (FUSELAGE)

DURING C-CHECK, FOUND CORROSION ON CARGO FLOOR TRACK IN AFT CARGO BAY FROM BS 787-847 AND RBL 14. REPAIRED IAW SRM. (M)

Part: STRAP — CORRODED (FUSELAGE)

DURING C-CHECK, FOUND CORROSION ON STRAP IN AFT CARGO BAY AT BS 771 WL 156 BL 24. REPAIRED IAW SRM. (M)

Part: SUPPORT — CORRODED (FUSELAGE)

PAE - DURING C-CHECK, FOUND SIDEWALL TO BULKHEAD SUPPORT CORRODED AT BS 727 RBL 24 AND WL 156. REPAIRED IAW SRM. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

PAE - DURING C-CHECK, FOUND AFT CARGO BAY FLOOR SUPPORT CORRODED AT BS 727A, RBL 3 AND WL 156. REPAIRED IAW SRM. (M)

Part: SUPPORT ANGLE — CORRODED (FUSELAGE)

PAE - DURING C-CHECK, FOUND CORROSION ON SIDEWALL SUPPORT ANGLE AT STATION 727D AND STRINGER 25R. REPAIRED IAW SRM. (M)

Part: SKIN — LIGHTNING STRIKE (FUSELAGE)

PAE - DURING C-CHECK, FOUND UPPER FUSELAGE EXTERNAL SKIN HAS LIGHTNING STRIKES AT BS 369.5 THROUGH BS 500F PLUS 1.25 AND WL 304 THROUGH WL 147 AND LBL 0.0 THROUGH LBL 26. REPAIRED IAW SRM. (M)

Part: SUPPORT — CORRODED (FUSELAGE)

PAE - DURING C-CHECK, FOUND FLOOR TO SIDEWALL SUPPORTS CORRODED AT BS 727B PLUS 12 THROUGH 947 AND WL 156 TO 160 AND LEFT AND RIGHT BL 24. REPAIRED IAW SRM. (M)

Part: WIRE — DISCONNECTED (CABIN)

LAX - DURING PREFLIGHT CHECK, FOUND EMERGENCY TRACK LIGHTING AT ROW 12 INOPERATIVE. RECONNECTED WIRES. LIGHTS THEN FUNCTIONED PROPERLY. (M)

Part: MECHANISM — OUT OF ADJUST (SERVICE DOOR)

SEA - DURING LINE CHECK, FOUND R-1 DOOR HARD TO OPEN. ADJUSTED R-1 DOOR GUIDE ARM PER MM. OPERATIONAL CHECKED GOOD. (M)

Part: ROLLER — OUT OF POSITION (SLIDING WINDOW)

SFO - DURING LINE CHECK, FOUND FIRST OFFICERS SLIDING WINDOW STUCK IN THE CLOSED POSITION. REMOVED WINDOW AND REINSTALLED LOWER TRACK ROLLER, REINSTALLED WINDOW. OPERATIONS CHECK NORMAL. (M)

Part: FLAP TRACK — CORRODED (T/E FLAP)

SEA - DURING C-CHECK, FOUND RIGHT OUTBOARD FLAP TRACK NR 8 AND NR 7 CORRODED FROM UPPER SURFACE AT REAR SPAR, SHIM NOT SEALED PROPERLY. REMOVED AND REPLACED IAW MM. (M)

Part: FLAP TRACK — CORRODED (T/E FLAP)

SEA - DURING C-CHECK, FOUND LEFT OUTBOARD FLAP TRACK NR 2 CORRODED FROM UPPER SURFACES AT REAR SPAR, SHIM NOT SEALED PROPERLY. REMOVED AND REPLACED IAW MM. (M)

Part: WIRE — DISCONNECTED (CABIN)

SEA - DURING PREFLIGHT CHECK, FOUND EMERGENCY FLOOR TRACK LIGHT INOPERATIVE AT ROW 20. RECONNECTED WIRES AT ROW 20. FLOOR TRACK LIGHTS THEN OPERATED NORMALLY. (M)

Part: LIGHT — BROKEN (CABIN)

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

Part: WIRE — BROKEN (ROW 15 - 17)

SEA - DURING MAINTENANCE CHECK, THE FORWARD ENTRY EMERGENCY EXIT TRACK LIGHTS AND THE EMERGENCY EXIT TRACK LIGHTS AT ROWS 15-17 WERE FOUND TO BE INOPERATAIVE. REPAIRED BROKEN WIRE AT ROW 17 AND RECONNECTED FORWARD LIGHT/WIRING AND LIGHTS OPERATED NORMALLY. (M)

Part: PIN — DISCONNECTED (LIGHT CONNECTOR)

LAX - PRIOR TO FLIGHT 679, THE FORWARD TWO EMERGENCY EXIT LIGHTS WERE FOUND TO BE INOPERATIVE. REATTACHED PINS IN LIGHT SOCKETS AND LIGHTS OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

GEG - PRIOR TO FLT 570, 3 EACH EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. REPAIRED LOOSE WIRING/CONNECTION AND LIGHTS OPERATED NORMALLY. (X)

Part: HARNESS — FAILED (FUSELAGE)

PDX-ATB OF F500 DUE TO MULTIPLE CIRCUIT BREAKERS POPPED. AIRCRAFT RETURNED TO PDX. PDX MAINTENANCE INSPECTED AND FOUND A FAILURE OF THE WIRE BUNDLE INSULATION AT BS 410, WL 203, RBL 58 (BEHIND LINER IN FORWARD CARGO COMPARTMENT AFT OF E/E BULKHEAD AND FORWARD OF THE FORWARD CARGO DOOR). MAINTENANCE REPLACED THE WIRING ON A/C 772. THERE WERE NO SYSTEM PROBLEMS FOUND DURING THE REPAIR OR SUBSEQUENT SYSTEM CHECKS THAT WOULD HAVE CAUSED THE WIRING TO OVERLOAD. EO 2400-01047 WAS ACCOMPLISHED ON THE 737-400 FLEET WITH NO EVIDENT SYSTEM FINDINGS. BASED ON THESE FINDINGS IT WOULD INDICATE THAT THE DISCREPANCY ON A/C 772 WAS AN ISOLATED OCCURANCE OF WIRE CHAFING. (M)

Part: WIRE — DISCONNECTED (ROWS 20 & 23)

PDX - PRIOR TO FLT 602, THE FLOOR TRACK LIGHT COVER WAS FOUND LOOSE AT ROW 20. MAINTENANCE INSPECTED AND FOUND LIGHTS TO BE INOPERATIVE. RECONNECTED WIRING AT ROWS 20 AND 23. LIGHTS OPERATED NORMALLY. (X)

Part: LENS — MISSING (ROWS 21 & 22)

SEA - PRIOR TO FLT 394, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERABLE AND LENSES MISSING AT ROWS 21 AND 22. REPLACED LENSES AT ROWS 21 AND 22. RELAMPED LIGHT AT ROW 22, LIGHT OPERATED NORMALLY. EMERGENCY EXIT FLOOR TRACK LIGHT AT ROW 21 WAS STILL INOPERABLE. RELEASED PER ME 33-33-19C. SUBSEQUENTLY, RECONNECTED WIRING/LIGHT AT ROWS 21 AND LIGHT OPERATED NORMALLY. REF: OPER CONTROL NR ASAA9940156.

Part: WIRE — DISCONNECTED (ROW 21)

SEA - PRIOR TO FLT 394, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERABLE AND LENSES MISSING AT ROWS 21 AND 22. REPLACED LENSES AT ROWS 21 AND 22. RELAMPED LIGHT AT ROW 22, LIGHT OPERATED NORMALLY. EMERGENCY EXIT FLOOR TRACK LIGHT AT ROW 21 WAS STILL INOPERABLE. RELEASED PER ME 33-33-19C. SUBSEQUENTLY, RECONNECTED WIRING/LIGHT AT ROWS 21 AND LIGHT OPERATED NORMALLY. REF: OPER CONTROL NR 99ZZZX4626. (X)

Part: LIGHT — INOPERATIVE (CABIN)

PDX - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE AT ROWS 14-17. REPLACED LIGHT ASSEMBLY AND LIGHTS OPERATED NORMALLY. (X)

Part: WIRE — FAILED (CABIN)

SEA - PRIOR TO FLT 364, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE AT ROWS 20-24. REPAIRED WIRING AND LIGHTS OPERATED NORMALLY. (X)

Part: LIGHT — INOPERATIVE (CABIN)

SEA - DURING MAINTENANCE CHECK, ONE EMERGENCY EXIT FLOOR TRACK LIGHT WAS FOUND INOPERATIVE BETWEEN AFT LAVS. REPLACED LIGHT ASSEMBLY AND LIGHTS OPERATED NORMALLY. (X)

Part: WIRE — DISCONNECTED (CABIN)

PDX - DURING MAINTENANCE CHECK, TWO FORWARD RED EMERGENCY EXIT TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. RECONNECTED LIGHTS/WIRING AND LIGHTS OPERATED NORMALLY. (M)

Part: BATTERY — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE AFT SECTION OF EMERGENCY FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. REPLACED THE RT AFT CHARGER AND BATTERY, LIGHTS OPERATED NORMALLY. REF: OPER CONTROL NR 99ZZZX741. (X)

Part: BATTERY CHARGER — INOPERATIVE (CABIN)

SEA - DURING MAINTENANCE CHECK, THE AFT SECTION OF EMERGENCY FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. REPLACED THE RT AFT CHARGER AND BATTERY, LIGHTS OPERATED NORMALLY. REF: OPER CONTROL NR ASAA9940006.

Part: WIRE — DISCONNECTED (ROWS 22-25)

PDX - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT TRACK LIGHTS AT ROWS 22-25 WERE FOUND INOPERATIVE. RECONNECTED WIRING/LIGHTS AND LIGHTS OPERATED NORMALLY. (X)

Part: WIRE — DISCONNECTED (ROW 22-25)

PDX - DURING MAINTENANCE CHECK, THE AFT TWO EMERGENCY EXIT FLOOR TRACK LIGHTS AND THE EMERGENCY EXIT FLOOR TRACK LIGHTS AT ROWS 22 THROUGH 25 WERE FOUND TO BE INOPERATIVE. RECONNECTED WIRING AT BOTH LOCATIONS AND LIGHTS OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

SEA - PRIOR TO FLIGHT 412, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE DISCONNECTED AND EXPOSED IN THE MID CABIN AREA. RECONNECTED WIRING TO LIGHT ASSEMBLIES AND REPLACED COVERS, LIGHTS OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

PDX - DURING MAINTENANCE CHECK, THE AFT THREE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. RECONNECTED WIRING/LIGHTS AND LIGHTS OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (ROW 14)

JNU - PRIOR TO FLT 76 - FOUR EACH EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. RECONNECTED WIRING AND LIGHTS OPERATED NORMALLY. (M)

Part: LIGHT — INOPERATIVE (ROW 15-20)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE AT ROWS 15-20. REPAIRED WIRING AND THE LIGHTS OPERATED NORMALLY. (M)

Part: LIGHT — INOPERATIVE (CABIN)

SEA - DURING MAINTENANCE CHECK, THREE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. REPLACED LIGHT ASSEMBLIES AND LIGHTS OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

ANC - FLT 62 - PRIOR TO DEPARTURE, CREW REPORTED THE EMERGENCY EXIT FLOOR TRACK LIGHTING WAS INOPERATIVE AT ROW 21. SECURED WIRE TO LAMP SOCKET AND LIGHTS OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

PDX - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE AT ROWS 22-25. RECONNECTED WIRING AND LIGHTS OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE AT ROW 1 AND AT ROWS 14 THROUGH 18. RECONNECTED WIRING AT ROW 1 AND AT ROW 18, AND LIGHTS OPERATED NORMALLY. (X)

Part: WIRE — DISCONNECTED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE AT ROW 1. REPAIRED WIRING AND LIGHTS OPERATED NORMALLY. (M)

Part: LIGHT — INOPERATIVE (CABIN)

SEA - DURING MAINTENANCE CHECK, THE FORWARD 2 RED EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. REPLACED LIGHT ASSEMBLIES AND LIGHTS OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (AFT CABIN)

SEA - FLT 194 - PRIOR TO FLIGHT, THE CREW REPORTED THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE IN THE AFT CABIN. RECONNECTED WIRING TO STRIP AND LIGHTS OPERATED NORMALLY. (X)

Part: LIGHT — INOPERATIVE (CABIN)

SEA - DURING MAINTENANCE CHECK, THE AFT RED EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. REPLACED FIRST RED EMERGENCY EXIT FLOOR TRACK LIGHT ASSEMBLY AND LIGHTS OPERATED NORMALLY. (M)

Part: WIRE — BROKEN (CABIN)

SEA - FLT 522 - PRIOR TO FLIGHT, THE CREW REPORTED THE EMERGENCY EXIT FLOOR TRACK LIGHTS HAD COME APART AT ROW 21 AND WERE INOPERATIVE. MAINTENANCE REPAIRED AND REPLACED WIRING AND LIGHTS OPERATED NORMALLY. (X)

Part: WIRE — BROKEN (CABIN)

SAN - FLT 555 - PRIOR TO FLIGHT, CREW REPORTED THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE AT ROW 15. MAINTENANCE REPAIRED BROKEN WIRE AND LIGHTS OPERATED NORMALLY. (X)

Part: WIRE — DISCONNECTED (CABIN)

PDX - FLT 453 - PRIOR TO FLIGHT, THE CREW REPORTED THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE INOPERATIVE AT ROWS 18-21. RECONNECTED WIRING AND LIGHTS OPERATED NORMALLY. (X)

Part: WIRE — BROKEN (CABIN)

SJC - FLT 357 - PRIOR TO FLIGHT, THE CREW REPORTED THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE INOPERATIVE AT ROW 21. REPAIRED BROKEN WIRE AND REPLACED TRACK COVERS AND LIGHTS OPERATED NORMALLY. (X)

Part: LIGHT — INOPERATIVE (CABIN)

JNU - FLT 74 - PRIOR TO DEPARTURE, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE AT ROWS 18-21. FOUND TRACK LIGHT ASSEMBLY AND WIRING TORN LOOSE AT SEAT 21C. REPLACED LIGHT ASSEMBLY, REPAIRED WIRING AND LIGHTS OPERATED NORMALLY. (X)

Part: WIRE — DISCONNECTED (CABIN)

OAK - FLT 451 - DURING PREFLIGHT, CREW REPORTED THAT THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE AT ROWS 18-21. RECONNECTED WIRING AND LIGHTS OPERATED NORMALLY. (M)

Part: WIRE — BROKEN (CABIN)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE FROM ROW 26 AFT. REPAIRED BROKEN WIRE AT ROW 26 AND LIGHTS OPERATED NORMALLY. (M)

Part: BEARING — SEIZED (R1 DOOR)

ANC - UPON OPENING, THE R1 DOOR WAS FOUND TO BE JAMMED AND WOULD NOT OPEN FULLY. REPLACED BOTH CAM BEARINGS AND DOOR OPERATED NORMALLY. (M)

Part: LIGHT — INOPERATIVE (CABIN)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTING IN THE AREA OF ROW 20 WERE FOUND TO BE INOPERATIVE AND WIRING EXPOSED. REPLACED TWO LIGHT ASSEMBLIES AND LIGHTS OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE TWO FORWARD MOST EMERGNCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. RECONNECTED WIRING AND LIGHTS OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

SEA - FLT 102 - DURING PRE-FLT, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE AND WIRES EXPOSED AT THE AFT EMERGENCY EXIT DOORS. RECONNECTED AND STOWED WIRING, AND LIGHTS OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE AFT 2 EMERGENCY EXIT LIGHTS WERE FOUND TO BE INOPERATIVE. RECONNECTED WIRES AND LIGHTS OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

SNA - FLT 449 - PRIOR TO DEPARTURE, CREW REPORTED THAT THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE RECONNECTED WIRING AND LIGHTS OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

SEA - FLT 8 - CREW REPORTED AFT SECTION OF EMERGENCY EXIT FLOOR TRACK LIGHTS WAS DAMAGED AND INOPERATIVE. RECONNECTED LOOSE TRACK WIRES AND LIGHTS OPERATED NORMALLY. (X)

Part: WIRE — DISCONNECTED (CABIN)

ANC - DURING MAINTENANCE CHECK, THE AFT FIVE EMERGENCY FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. RECONNECTED AFT FIVE EMERGENCY LIGHTS AND LIGHTS OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

SEA - DURING MAINTENANCE CHECK, SEVERAL EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE FROM ROW 22 TO THE AFT CABIN. RECONNECTED WIRES AT FEED THROUGH FROM BATTERY PACK AND LIGHTS OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE AFT 3 EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. RECONNECTED WIRES/LIGHTS AND THE LIGHTS OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

JNU - DURING MAINTENANCE CHECK, SEVERAL EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE FROM ROW 22 TO THE AFT CABIN. RECONNECTED WIRES AT FOUR SOCKETS FROM ROW 22 TO THE AFT CABIN AND ALL EMERGENCY EXIT FLOOR TRACK LIGHTS OPERATED NORMALLY.

Part: EEL SOCKET — INOPERATIVE (CABIN)

SEA - FORWARD EMERGENCY EXIT PEEPLES LIGHT INOP, ROW 1. MAINTENANCE REPLACED SOCKET. (W)

Part: EEL WIRING — DAMAGED (CABIN)

SEA - DURING CHECK, THREE AFT MOST EMERGENCY LIGHTS INOP. MAINTENANCE REPAIRED WIRING. (W)

Part: EEL WIRING — DISCONNECTED (CABIN)

SEA - DURING MAINTENANCE CHECK THE AFT TWO EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. RECONNECTED WIRING AND LIGHTS OPERATED NORMALLY. (W)