N77780

Part: LIGHT — INOPERATIVE (L1 DOOR)

BOS - MAIN ENTRY EMERGENCY EXIT LIGHT WILL NOT TEST. REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSY. OPS CHECK GOOD ON GROUND. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: ACTUATOR — INOPERATIVE (NR 5 LE FLAP)

FLT 3736 - BNA-FWA - NR 5 LEADING EDGE FLAP DID NOT FULLY EXTEND ON FLAP EXTENSION. HOWEVER, AT SLOW SPEED, FLAP FULLY EXTENDED. AIRCRAFT MADE AN UNEVENTFUL LANDING AT FWA. REMOVED AND REPLACED NR 5 KRUEGER FLAP ACTUATOR IAW 272 MM 27-81-22. OPS CHECK GOOD ON GROUND AND NO LEAKS NOTED. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: ACTUATOR — INOPERATIVE (NR 5 LE FLAP)

BNA/FWA - FLT 3735 - DURING LANDING, THE NR 5 LE KRUGER FLAP DID NOT FULLY EXTEND ON FLAP EXTENSION. THE CREW DECLARED AN EMERGENCY. AIRCRAFT LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED THE NR 5 LE KRUGER FLAP ACTUATOR. OPS CHECK PERFORMED, AIRCRAFT RETURNED TO SERVICE. (X)

Part: BATTERY — INOPERATIVE (CABIN)

DFW MAINTENANCE FOUND MAIN ENTRY EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REINSTALLED SERVICEABLE BATTERIES. OPS CHECK GOOD ON GROUND. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: LIGHT — INOPERATIVE (COCKPIT)

DFW MAINTENANCE FOUND COCKPIT EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REINSTALLED SERVICEABLE EMERGENCY LIGHT ASSEMBLY. OPS CHECK GOOD ON GROUND. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: BATTERY — DISCHARGED (COCKPIT)

CLT - EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REINSTALLED SERVICEABLE BATTERY FOR L-1 AND COCKPIT EMERGENCY LIGHT UNITS. OPS CHECK GOOD ON GROUND. RECYCLED BATTERY CHARGER SYSTEM. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: WIRE — CHAFED (PROX SWITCH)

FLT 1759 - MEM-FWA - RIGHT MAIN GEAR, RED UNSAFE LIGHT AND GREEN LIGHT ILLUMINATED DURING FLIGHT. AIRCRAFT LANDED IN FWA WITH NO FURTHER DIFFICULTIES. FOUND INSULATION CHAFED ON UPLOCK PROXIMITY SWITCH FOR RIGHT MAIN LANDING GEAR. REPAIRED WIRE AND SECURED WIRES. TESTED AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: CONNECTOR — DIRTY (WING LEADING EDG)

MEM/IAH - FLT 1760 - AFTER FLAP RETRACTION, NR 4 LEADING EDGE DEVICE DID NOT INDICATE RETRACTED. PERFORMED ABNORMAL PROCEDURE WITH THE SAME RESULTS. THE CREW RETURNED TO MEM AND LANDED WITHOUT ANY FURTHER DIFFICULTIES. CLEANED CONNECTOR AT SWITCH AND OPERATIONALLY CHECKED NORMAL. THE AIRCRAFT WAS RETURNED TO SERVICE. (X)

Part: INDICATOR — MALFUNCTIONED (MLG)

FLT 2030 - MHR-PDX - AFTER TAKEOFF, RIGHT MAIN GEAR FAILED TO INDICATE UP AND LOCKED. AFTER THREE MINUTES, WITH GEAR UP, LIGHTS EXTINGUISHED. PERFORMED FLY-BY BY TOWER, AND GEAR WAS VISUALLY CHECK UP. OPERATIONALLY CHECKED NORMAL DURING GEAR EXTENSION FOR APPROACH AND LANDING TO PDX. THE AIRCRAFT LANDED SAFELY WITHOUT ANY FURTHER PROBLEMS. VISUALLY INSPECTED LEFT AND RIGHT GEAR SAFETY SWITCHES AND FOUND SECURE AND TIGHT. ALL INDICATIONS NORMAL ON GROUND AND NO DEFECTS WERE NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: CONNECTOR — DIRTY (CONTROL BOX)

FLT 2507 - PDX - RIGHT GEAR LIGHT ON DURING TAKEOFF ROLL. CLEANED CANNON PLUG. FUNCTIONAL TEST GOOD. LIGHT STAYED GREEN AIRCRAFT RETURNED TO SERVICE. (M)

Part: SEAT TRACK — MISMANUFACTURED (BS 680)

FOUND DURING 'ZERO B TRANSITION' CHECK AT AVBORNE HEAVY MAINTENANCE FACILITY, PRIOR TO THIS AIRCRAFT BEING ON THE KGA CERTIFICATE, SEAT TRACK AT RBL 45.5, BS 680 TO BS 720A HAS WRONG SPLICE FOR 9G BULKHEAD. REMOVED AND REPLACED SEAT TRACK AT RBL 45.5 FROM STATION 560 TO 720A, IAW AEISTC SA 1797SO AND SA1798SO. (M)

Part: STRINGER — CORRODED (BS 1148)

FOUND DURING 'ZERO B, TRANSITION' CHECK AT AVBORNE HEAVY MAINTENANCE FACILITY (MIAMI) PRIOR TO THIS AIRCRAFT BEING ON THE KHA CERTIFICATE. CORROSION AT STRINGER 7R UPPER FLANGE, JUST FORWARD OF BS 1148. REMOVED CORRODED AREA AT STRINGER 7R UPPER FLANGE FORWARD OF BS 1148. CUT OUT DAMAGED AREAS AND REPAIRED AREA AND STRINGER UPPER FLANGE FORWARD OF BS 1148. CUT OUT DAMAGED AREAS AND REPAIRED AREA AND STRINGER UPPER FLANGE PER SRM 53-10-3 FIG 1. (M)

Part: FRAME — CORRODED (BS 303)

FOUND DURING 'ZERO B TRANSITION' CHECK AT AVBORNE HEAVY MAINTENANCE FACILITY, PRIOR TO THIS AIRCRAFT BEING ON THE KHA CERTIFICATE. NOSE SECTION INTERNAL CIRCUMFERENTIAL FRAME HAS CORROSION ON LEFT SIDE OF DOG HOUSE BELOW HORIZONTAL WALKWAY BEAM BS 303 AND STRINGER 26L AND LOWER END. CUT OUT DAMAGED AREA ON FRAME IAW 53-10-4. INSTALLED REPAIR AT CIRCUMFERENTIAL FRAME AT BODY STATION 303 STRINGER 26L IAW B727 SRM 53-10-4. (M)

Part: SEAT TRACK — MISMANUFACTURED (BS 1050)

FOUND DURING 'ZERO B, TRANSITION' CHECK AT AVBORNE HEAVY MAINTENANCE FACILITY, PRIOR TO THIS AIRCRAFT BEING ON THE KHA CERTIFICATE. SEAT TRACK AT LBL 24.75 TOO SHORT AT SPLICES FOR CARGO MOD BODY STATION 1050 TO 1070. REMOVED AND REPLACED SEAT TRACK AT LBL 24.75 FROM BS 1050 TO BS 1070, PER B727 SRM 51-30-2. (M)

Part: VENT LINES — CHAFED (FUEL SYSTEM)

FOUND DURING 'ZERO B, TRANSITION' CHECK AT AVBORNE HEAVY MAINTENANCE FACILITY, PRIOR TO THIS AIRCRAFT BEING ON THE KHA CERTIFICATE. FUEL VENT TUBING WAS FOUND TO BE CHAFING AT THE FOLLOWING WING STATIONS, LWS 656.5, LWS 546.5, LWS 519.0, RWS 601.5 AND RWS 546.5. REPAIRED ALL ABOVE NOTED FUEL VENT LINES IAW AVITAS ENGINEERING REPAIR ORDER. WORK ORDER NR 99AVHM.063RO-1. (M)

Part: FLOORBEAM — CORRODED (BS 380)

FOUND DURING ZERO B, TRANSITION CHECK AT AVBORNE HEAVY MAINTENANCE FACILITY, PRIOR TO THIS AIRCRAFT BEING ON THE KHA CERTIFICATE, CABIN FORWARD GALLEY FLOORBEAM AT BODY STATION 380, RBL 14 TO RBL 64 IS CORRODED. REMOVED CORROSION AT FLOORBEAM. CUTOUT AND REMOVED DAMAGED AREAS AT BS 380 FROM RBL 14 TO RBL 58 PER SRM 53-10-8. FABRICATED REPAIR PARTS AND INSTALLED IAW 53-10-8 FIG 3. (M)

Part: SEAT TRACK — MISMANUFACTURED (BS 1090)

FOUND DURING 'ZERO B TRANSITION' CHECK AT AVBORNE HEAVY MAINTENANCE FACILITY, PRIOR TO THIS AIRCRAFT BEING ON THE KHA CERTIFICATE, SEAT TRACK AT RBL 24.75 TOO SHORT FOR CARGO MOD BODY STATION 1090 TO 1110. REMOVED AND REPLACED SEAT TRACK AT RBL 24.75 FROM BS 970 TO BS 1136 PER B727 SRM 53-10-5. (M)

Part: SEAT TRACK — MISMANUFACTURED (BS 1110)

FOUND DURING ZERO B TRANSITION CHECK AT AVBORNE HEAVY MAINTENANCE FACILITY, PRIOR TO THIS AIRCRAFT BEING ON THE KHA CERTIFICATE, SEAT TRACK AT LBL 45.5 TOO SHORT FOR CARGO MOD BODY STATION 1110 TO 1130. REMOVED AND REPLACED SEAT TRACK AT LBL 45.5 FROM BS 1030 TO BS 1136, PER B727 SRM 53-10-5, FIG 7. (M)

Part: FLOORBEAM — CORRODED (BS 400)

FOUND DURING ZERO B, TRANSITION CHECK AT AVBORNE HEAVY MAINTENANCE FACILITY, PRIOR TO THIS AIRCRAFT BEING ON THE KHA CERTIFICATE, CABIN FLOORBEAM AT BODY STATION 400, RBL 12 CORRODED. REMOVED CORROSION AT FLOORBEAM. CUTOUT AND REMOVED DAMAGED AREAS PER SRM 53-10-8 PAGE 18. FABRICATED REPAIR PARTS AND INSTALLED IAW 53-10-8. (M)

Part: BULKHEAD — CRACKED (BS 1183)

FOUND DURING 'ZERO B TRANSITION' CHECK AT AVBORNE HEAVY MAINTENANCE FACILITY, PRIOR TO THIS AIRCRAFT BEING ON THE KHA CERTIFICATE. TAIL SKID CAVITY BULKHEAD WEB AT STATION 1183 HAS CRACK ON LEFT SIDE 5 INCHES BELOW FLOOR. REMOVED EXISTING REPAIR AND INSPECTED IAW B727 NDT MANUAL PART 6 51-00-00 FIG 4. ROUTED OUT CRACK IAW B727 S/B 53-175. ACCOMPLISHED REPAIR IAW B727 S/B 53-175. (M)

Part: BEAR STRAP — CRACKED (FUSELAGE)

FOUND DURING 'ZERO B TRANSITION' CHECK AT AVBORNE HEAVY MAINTENANCE FACILITY, PRIOR TO THIS AIRCRAFT BEING ON THE KHA CERTIFICATE. FORWARD GALLEY DOOR CUTOUT AT LOWER AFT CORNER BEAR STRAP HAS CRACK. STOP DRILLED CRACK AT GALLEY DOOR CUTOUT BEAR STRAP IAW B727 SRM 51-10-1. PERFORMED HFEC TO VERIFY NO ADDITIONAL CRACKS. INSTALLED REPAIR IAW BOEING SB 727-53-188 REV 2. (M)

Part: SEAT TRACK — MISMANUFACTURED (BS 970)

FOUND DURING ZERO B TRANSITION CHECK AT AVBORNE HEAVY MAINTENANCE FACILITY, PRIOR TO THIS AIRCRAFT BEING ON THE KHA CERTIFICATE, SEAT TRACK AT RBL 45.5 IS TOO SHORT FOR CARGO MOD AT SPLICE, BODY STATION 1090 TO 1110. REMOVED AND REPLACED SEAT TRACK AT RBL 45.5 FROM STATION 970 TO 1136 IAW B727 SRM 53-10-5. (M)

Part: FLOORBEAM — CRACKED (BS 1183)

FOUND DURING 'ZERO B, TRANSITION' CHECK AT AVBORNE HEABY MAINTENANCE FACILITY, PRIOR TO THIS AIRCRAFT BEING ON THE KHA CERTIFICATE, BS 1183 BULKHEAD LEFT VERTICAL BEAM HAS CRACK AT LOWER END, LBL 8. PERFORMED NDT INSPECTION TO DETERMINE END OF CRACK, PER B727 NDT PART 6 OF 51-00-00. CUTOUT DAMAGED AREA PER B727 S/B 53-0175. ACCOMPLISHED VERTICAL BEAM REPAIR IAW B727, S/B 53-175. (M)

Part: ANGLE — CRACKED (BS 850)

FOUND DURING 'ZERO B, TRANSITION' CHECK AT AVBORNE HEAVY MAINTENANCE FACILITY, PRIOR TO THIS AIRCRAFT BEING ON THE KHA CERTIFICATE. MAIN CABIN STRINGER 17L BODY STATION 850, ANGLE IS CRACKED, INBOARD SIDE OF FRAME. ACCOMPLISHED REPAIR ON MAIN CABIN STRINGER 17L STATION 850, ANGLE IS CRACKED, INBOARD SIDE OF FRAME, IAW AVITAS ENGINEERING REPAIR ORDER 99AVHM 067. RO-1 REV 1, DATED 10/5/99. (M)

Part: LIGHT — INOPERATIVE (PASSENGER DOOR)

INSPECTION FOUND AFT ENTRY OVERHEAD EMERGENCY EXIT LIGHT INOPERATIVE. THE LIGHT ASSEMBLY WAS REMOVED AND REPLACED AND OPERATION CHECKED GOOD IAW MM 33-50-00.

Part: PANEL — BENT (NR 8 SPOILER)

INSPECTION FOUND RT WING NR 8 SPOILER OUTBOARD AREA BENT UP. THE SPOILER PANEL WAS REMOVED AND REPLACED IAW MM 27-62-1.

Part: SKIN — DENTED (NR 9 SPOILER)

INSPECTION FOUND RT WING NR 9 SPOILER DENTED ON LOWER END. THE NR 9 SPOILER WAS REMOVED AND REPLACED IAW MM 27-62-1.

Part: SKIN — CRACKED (NR 13 SPOILER)

INSPECTION FOUND A .1875 INCH CRACK AT RT WING UPPER TRAILING EDGE AT CUTOUT FOR NR 13 SPOILER SECOND FROM O/B HINGE CUTOUT. THE CRACK WAS STOP DRILLED. A REPAIR WAS INSTALLED AND EDGES WERE SEALED IAW SRM 51-10-1 AND 51-10-3, PAGE 4.

Part: SKIN — CRACKED (LT ELEVATOR)

INSPECTION FOUND A 1 INCH CRACK IN LEFT ELEVATOR LOWER SKIN JUST I/B AND AFT OF PANEL NR 9311. THE CRACK WAS STOP DRILLED IAW SRM 55-20-3. A DOUBLER WAS INSTALLED IAW SRM 55-20-3, 51-10-2, AND 51-30. A CALCULATED BALANCE WAS PERFORMED IAW SRM 51-80-7 AND WAS WITHIN LIMITS.

Part: INTERCOSTAL — CORRODED (BS 1128-1148)

INSPECTION FOUND LOWER FLANGE OF INTERCOSTAL CORRODED IN AFT CARGO AREA AT STA 1128-1148 OUTBOARD OF STRINGER 28R. THE INTERCOSTAL WAS REMOVED AND A NEW INTERCOSTAL WAS INSTALLED IAW SRM 51-30-2 AND 51-10-2.

Part: STIFFENER — CORRODED (WS 249)

INSPECTION FOUND STIFFENER CORRODED AT RT WING FRONT SPAR FS 249. THE CORRODED SECTION OF STIFFENER WAS REMOVED AND A NEW SECTION WAS INSTALLED IAW SRM 51-30-02, PAGE 4.

Part: WIRE — BROKEN (R2 DOOR)

INSPECTION FOUND EXIT IDENTIFIER LIGHT AT R-2 DOOR INOPERATIVE. MAINTENANCE FOUND EXIT LIGHT WIRE BROKEN. THE WIRE WAS REPAIRED IAW MM 33-51-00, PAGE 903 AND OPERATION WAS RESTORED.

Part: BRACKET — CRACKED (NR 6 LE FLAP ACT)

INSPECTION FOUND A 1 INCH CRACK IN INBOARD SUPPORT BRACKET AT TOP AND BOTTOM OF NR 6 LEADING EDGE FLAP ACTUATOR. THE BRACKET WAS REMOVED AND A NEW BRACKET WAS INSTALLED IAW SRM 51-30-2.

Part: SKIN — CRACKED (NR 7 LE SLAT)

INSPECTION FOUND TWO .5 INCH CRACKS COMING FROM SCREW HOLE TO RIVETS AT RT WING NR 7 SLAT UPPER TRAILING EDGE WHERE O/B HOOK MOUNTS. REMOVED FASTENERS IAW SRM 51-30-2. A REPAIR DOUBLER WAS INSTALLED IAW SRM 57-20-3.

Part: HOUSING — CORRODED (HORIZ STAB)

INSPECTION FOUND HORIZONTAL STABILER LEFT AND RIGHT HINGE BUSHING HOUSINGS CORRODED. THE BUSHINGS AND BEARINGS WERE REMOVED AND REPLACED IAW ECRA 555C028 AND ECRA 5550-01033.

Part: BOLTS — CORRODED (VERT STAB)

INSPECTION FOUND VERTICAL STABILIZER TENSION TIE BOLTS (8) PITTED AND CORRODED. THE TENSION TIE BOLTS WERE REMOVED AND REPLACED IAW MM 55-30-51, PAGE 406-408.

Part: BOLT — CORRODED (HORIZ STAB)

INSPECTION FOUND BOTH HORIZONTAL STABILIZER HINGE PIN BOLTS CORRODED. BOTH HINGE PINS WERE REPLACED IAW MM 55-00.

Part: WIRE — LOOSE (LAVATORY)

INSPECTION FOUND EXIT IDENTIFIER LIGHT AT LEFT AFT LAV WALL INOPERATIVE. MAINTENANCE FOUND A LOOSE GROUND WIRE. THE WIRE WAS SECURED IAW MM 33-51-00, PAGE 903 AND OPERATION WAS RESTORED.

Part: COWL — CRACKED (NR 3 ENGINE)

INSPECTION FOUND A 2 INCH CRACK IN NR 3 ENGINE NOSE COWL ACOUSTIC LINING WITH LINING ERODED IN SEVERAL AREAS. THE NR 3 ENGINE NOSE COWL WAS REMOVED AND REPLACED IAW MM 54-00.

Part: STRINGER — CORRODED (BS 1164)

INSPECTION FOUND STRINGER 28R CORRODED AT BS 1164. THE CORRODED SECTION OF STRINGER WAS REMOVED AND A NEW SECTION OF STRINGER WAS INSTALLED IAW SRM 51-30-2 AND 51-10-2.

Part: WIRE — BROKEN (L2 DOOR)

INSPECTION FOUND THE EXIT IDENTIFIER LIGHT AT L-2 DOOR INOPERATIVE. MAINTENANCE FOUND A BROKEN GROUND WIRE. THE WIRE WAS REPAIRED IAW MM 33-51-00, PAGE 903 AND OPERATION WAS RESTORED.

Part: SKIN — DEBONDED (RT AILERON TAB)

INSPECTION FOUND TWO SMALL DEBONDED AREAS IN RT O/B AILERON TAB TRAILING EDGE. THE RT O/B AILERON TAB WAS REMOVED AND REPLACED IAW MM 27-10-41.

Part: SKIN — CRACKED (RT TE FOREFLAP)

INSPECTION FOUND A 1.25 INCH CRACK IN RT O/B FOREFLAP LEADING EDGE. THE CRACK WAS STOP DRILLED. A DOUBLER WAS INSTALLED IAW SRM 57-50-4 AND 51-30-2, PAGE 7.

Part: SKIN — SEPARATED (LT ELEVATOR TAB)

INSPECTION FOUND LT ELEVATOR CONTROL TAB TRAILING EDGE SKIN SEPARATING IN TWO PLACES. THE ELEVATOR CONTROL TAB WAS REMOVED AND REPLACED IAW 55-20-2.

Part: ANGLE — CRACKED (NR 7 LE SLAT)

INSPECTION FOUND A .125 INCH CRACK IN RT WING NR 7 SLAT LOWER SPANWISE CHORD ANGLE AT CUTOUT FOR I/B TRACK AND A .3125 INCH CRACK AT STOP PAD AREA SIX INCHES INBOARD. THE ANGLE WAS REMOVED. AN ANGLE AND REPAIR SPLICE WERE INSTALLED IAW SRM 51-40-3, 51-10-2, AND 57-30-2.

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION FOUND EMERGENCY PATH LIGHTING IN FORWARD SECTION OF FIRST CLASS CABIN INOPERATIVE. THE BATTERY PACK WAS REMOVED AND REPLACED IAW MM 33-51-00, PAGE 201.

Part: SKIN — TORN (RT TE FOREFLAP)

INSPECTION FOUND RT I/B FOREFLAP INBOARD MOST END UPPER LEADING EDGE SKIN TORN FORWARD OF SPRING DOOR. THE FOREFLAP WAS REMOVED AND REPLACED IAW MM 27-51-3.

Part: SKIN — DISBONDED (LT TE FOREFLAP)

INSPECTION FOUND LT TRAILING EDGE I/B FOREFLAP DISBONDED AT UPPER AND LOWER SURFACE. THE FOREFLAP WAS REMOVED AND REPLACED IAW MM 27-51-4.

Part: WIRE — BROKEN (ROW 23-30)

INSPECTION FOUND EMERGENCY PATH SEAT MOUNTED LIGHTING INOPERATIVE FROM ROW 23 TO 30. REPAIRED WIRING AND OPERATIONAL CHECK WAS GOOD IAW MM 33-50-00, PAGE 201.

Part: SKIN — CRACKED (RT TE MIDFLAP)

INSPECTION FOUND A .3125 INCH CRACK AT RT I/B MIDFLAP LOWER TRAILING EDGE. THE CRACK WAS STOP DRILLED. A DOUBLER WAS INSTALLED IAW SRM 51-40-2 AND 51-30-2.

Part: SKIN — GOUGED (LT HORIZ STAB)

INSPECTION FOUND LT HORIZONTAL STABILIZER I/B LEADING EDGE AREA GOUGED. A DOUBLER AND FILLER WERE INSTALLED IAW SRM 51-10-6 AND 51-30-2, PAGE 4.

Part: WIRE — BROKEN (ROW 11)

INSPECTION FOUND LT EMERGENCY PATH LIGHT ON SEAT AT ROW 11 INOPERATIVE. INSPECTION FOUND PATH LIGHT WIRE BROKEN. THE WIRE WAS REPAIRED AND STOWED. OPERATIONAL CHECKS WERE GOOD IAW MM 33-51-00, PAGE 102.

Part: STRINGER — CRACKED (WS 629)

INSPECTION FOUND A .75 CRACK IN LT WING THIRD FROM REAR SPAR UPPER STRINGER AT WS 629, ACCESS CUTOUT NR 7216. THE STRINGER WAS CUT OUT. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 57-10-4, FIGURE 5, AND ECRA 5710-01859.

Part: ANGLE — CRACKED (LT WING)

INSPECTION FOUND A .75 CRACK IN J ANGLE AT LT WING T/E AREA JUST ABOVE AND INBOARD OF NR 7 SPOILER ACTUATOR. THE TOP PANEL WAS REMOVED. A J ANGLE BRACKET REPAIR WAS INSTALLED AND THE PANEL WAS REINSTALLED. WORK WAS PERFORMED IAW SRM 51-10-2, 51-10-1, 51-30-2, AND ECRA 5750-02828.

Part: STRINGER — CRACKED (WS 686.50)

INSPECTION FOUND A .75 CRACK IN AFT TANG AT FORWARD VENT BOX STRINGER WHERE IT MOUNTS TO TOP OF LT WING RIB, WS 686.50, TANK CUTOUT NR 7218. THE FASTENERS WERE REMOVED. CUTOUT ACCESS HOLE TO ACCESS REPAIR IAW EA 5762-01050. REPAIR ANGLE AND SHIMS WERE FABRICATED AND INSTALLED IAW EA 5762-01050 AND SRM 51-10-6.

Part: STRINGER — CRACKED (WS 686.50)

INSPECTION FOUND A .75 CRACK IN AFT TANG AND A .75 CRACK IN FORWARD TANG AT AFT VENT BOX STRINGER WHERE IT MOUNTS TO TOP OF LT WING RIB, WS 686.50, TANK CUTOUT NR 7218. THE FASTENERS WERE REMOVED. CUTOUT ACCESS HOLE TO ACCESS REPAIR IAW EA 5762-01050. REPAIR ANGLES AND SHIMS WERE FABRICATED AND INSTALLED IAW EA 5762-01050, SRM 51-10-6, AND SRM 51-30-2.

Part: SKIN — DENTED (RT TE FOREFLAP)

INSPECTION FOUND RT WING FORWARD FOREFLAP DENTED ON BOTTOM SURFACE ABOVE NR 5 FLAP TRACK. THE FOREFLAP WAS REMOVED, REPAIRED, AND REINSTALLED IAW MM 27-51-00.

Part: RIB — CRACKED (WS 738.50)

INSPECTION FOUND A 2 INCH CRACK IN RIB AT FIRST LOWER STRINGER FROM FRONT SPAR, WS 738.50 AT ACCESS CUTOUT 7701, RT WING. THE RIB WAS REPAIRED IAW SRM 57-10-5, FIGURE 2, 51-30-2 AND 51-10-2.

Part: CONTROL TAB — DISBONDED (RT ELEVATOR)

INSPECTION FOUND RT ELEVATOR CONTROL TAB TRAILING EDGE DISBONDING. THE TAB WAS REMOVED AND A SERVICEABLE TAB WAS INSTALLED IAW SRM 51-40-10.

Part: STRINGER — CRACKED (WS 629)

INSPECTION FOUND A .75 INCH CRACK IN AFT TANG AT AFT VENT BOX STRINGER INSIDE RT WING TANK ACCESS CUTOUT 7616, WS 629. THE AREA WAS REPAIRED IAW EA 5762-01050.

Part: SKIN — CORRODED (BS 680)

INSPECTION FOUND FUSELAGE SKIN CORRODED WITH A BROKEN RIVET AT STA 680, STRINGER 26R. THE CORROSION WAS REMOVED AND THE CORRODED AREA WAS CUT OUT. A DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-30-3, 51-10-2, AND 51-40-5.

Part: ANGLE — CRACKED (BS 1263)

INSPECTION FOUND A 1 INCH CRACK IN UPPER INBOARD AREA OF ANGLE AT RT AFT STAIR TORQUE BOX, STA 1263R. THE CRACKED ANGLE WAS REMOVED IAW SRM 51-30-2. THE WEB WAS REMOVED IAW SRM 51-30-2. A NEW ANGLE WAS INSTALLED IAW SRM 51-10-2 AND 51-30-2. THE WEB WAS INSTALLED IAW SRM 51-30-2.

Part: SKIN — CRACKED (BS 294.5)

INSPECTION FOUND TWO EACH .125 INCH CRACKS IN NLG WHEEL WELL TOP CENTER PANEL AT BL 0, JUST FORWARD OF STA 294.5. THE CRACKS WERE STOP DRILLED, A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-40-2 AND 51-30-2.

Part: FLOORBEAM — CRACKED (BS 940)

INSPECTION FOUND A .5 INCH CRACK OUT OF FORWARD FASTENER HOLE TO EDGE IN FLOORBEAM AT BS 940, LBL 59. A REPAIR WAS PERFORMED IAW JA5310-0185301001 AND REPAIR DOCUMENT M AND E NR 07-5310-1-0143.

Part: RIB — CRACKED (WS 656.5)

INSPECTION FOUND A 1.5 INCH CRACK IN LT WING RIB. THE CRACK WAS LOCATED AT LOWER FLANGE WHERE IT MOUNTS TO SECOND FROM FORWARD END HEAVY STRINGER, WS 656.50, ACCESS CUTOUT 7217. THE RIB WAS REPAIRED IAW SRM 57-10-5, FIGURE 1.

Part: CONTROL TAB — DISBONDED (LT ELEVATOR)

INSPECTION FOUND LT ELEVATOR CONTROL TAB OUTBOARD TRAILING EDGE CORNER SEPARATING. THE ELEVATOR TAB WAS REMOVED AND A SERVICEABLE TAB WAS INSTALLED IAW MM 27-30.

Part: CLIP — CORRODED (BS 1183)

INSPECTION FOUND CORROSION ON CLIP RT SIDE UNDER CABIN FLOOR EIGHT INCHES FORWARD OF FS 1183, STRINGER 18R. FASTENERS AND PARTS WERE REMOVED, A DOUBLER ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-40-3.

Part: SKIN — CORRODED (BS 720)

INSPECTION FOUND LEFT CENTER FUSELAGE SKIN CORRODED WITH A BROKEN RIVET AT STA 720A, STRINGER 26L. THE CORRODED AREA WAS CUT OUT AND THE CORROSION WAS CLEANED IAW SRM 51-10-6. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-10-2, 53-30-3, AND 51-30-2.

Part: SKIN — CORRODED (FUSELAGE)

INSPECTION FOUND FUSELAGE SKIN CORRODED AT RT AFT OVERWING EXIT CUTOUT. THE SKIN WAS REPAIRED IAW SRM 53-30-3, FIGURE 16. THE EXIT HATCH WAS TESTED IAW MM 52-21-0.

Part: POWER SUPPLY — INOPERATIVE (CARGO COMPT)

INSPECTION FOUND AFT CARGO DOOR EXTERIOR EMERGENCY LIGHTS INOPERATIVE. THE BATTERY POWER SUPPLY WAS REMOVED AND REPLACED.

Part: FLOOR BEAM — CORRODED (BS 460)

INSPECTION FOUND CORROSION ON FLOOR BEAM AT BS 460, RBL 45. THE CORRODED AREA WAS REMOVED AND A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-10-8. (M)

Part: DOUBLER — CORRODED (BS 714)

INSPECTION FOUND SKIN DOUBLER CORRODED AT STRINGER 14R AND BS 714. THE CORRODED SECTION OF SKIN DOUBLER WAS REMOVED. A FILLER AND DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-30-3. (M)

Part: FRAME — CORRODED (BS 740)

INSPECTION FOUND AIRCRAFT BAY AFT FRAME CORRODED AT PANEL NR 3458R, BS 740. THE CORRODED SECTION OF FRAME WAS REMOVED. AN L-ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-40-3. (M)

Part: FLOOR PANEL — CORRODED (BS 950)

THE RIGHT FLOOR SUPPORT PANEL WAS FOUND CORRODED IN THE AFT CARGO COMPARTMENT AT BS 950-950F. THE FLOOR SUPPORT PANEL WAS REMOVED. A NEW FLOOR SUPPORT PANEL WAS FABRICATED AND INSTALLED IAW SRM 51-40-2, 51-10-6, AND 51-10-2. (M)

Part: INTERCOSTAL — CORRODED (BS 1130-1148)

INSPECTION FOUND CORROSION ON INTERCOSTAL AT BS 1130-1148, LT SIDE. THE INTERCOSTAL WAS REMOVED. A NEW INTERCOSTAL WAS FABRICATED AND INSTALLED IAW SRM 51-40-3. (M)

Part: THRESHOLD — CORRODED (BS 560)

INSPECTION FOUND CORROSION AT FORWARD CARGO DOOR THRESHOLD, STATION 560. THE CORROSION WAS REMOVED. A FILLER AND DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-2. (M)

Part: INTERCOSTAL — CORRODED (BS 680-700)

INSPECTION FOUND THE INTERCOSTAL CORRODED AT BS 680-700 AND STRINGER 27R. THE INTERCOSTAL WAS REMOVED AND THE CORROSION WAS CUT OUT. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-3. (M)

Part: SKIN — CORRODED (BS 294)

INSPECTION FOUND CORROSION ON SKIN AT BS 294, RBL 16, STRINGER 22R. THE SKIN WAS REPAIRED IAW SRM 51-10-6, 51-10-2, AND 51-30-2. (M)

Part: L-ANGLE — CRACKED (BS 804)

INSPECTION FOUND A .75 INCH CRACK IN ATTACH L-ANGLE AT LEFT BS 804 LATERAL FLOOR BEAM WEB TO LBL 46 LONGITUDINAL FLOOR BEAM WEB. THE CRACK WAS LOCATED AT THE LIGHTENING HOLE ON AFT SIDE. THE CRACK ANGLE WAS REMOVED. A NEW L-ANGLE WAS FABRICATED AND INSTALLED IAW SRM 53-10-2. (M)

Part: DOUBLER — CRACKED (BS 826)

INSPECTION FOUND A 1 INCH CRACK IN DOUBLER ON AFT SIDE OF BS 826 LATERAL FLOOR BEAM WEB, LBL 54. THE CRACK WAS STOP DRILLED. A WEB REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-2. (M)

Part: DOUBLER — CRACKED (WS 656.5)

INSPECTION FOUND A 1.5 INCH CRACK IN RIB DOUBLER WS 656.50, NR 3 FUEL TANK. THE CRACK WAS STOP DRILLED. A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 57-10-5. (M)

Part: STRINGER — CORRODED (BS 1030-1166)

INSPECTION FOUND CORROSION ON FLOOR SUPPORT STRINGER NR 9 AT BS 1030-1166. THE CORRODED SECTIONS WERE REMOVED. L-ANGLES AND FILLERS WERE FABRICATED AND INSTALLED IAW SRM 53-10-2. (M)

Part: FRAME — CORRODED (BS 1130)

CORROSION WAS FOUND AT STATION 1130 FRAME DURING INSPECTION ON RIGHT FUSELAGE WALL. THE CORROSION EXTENDED ABOVE AND BELOW FLOOR LEVEL. THE CORRODED SECTION WAS REMOVED. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-10-6, 51-10-2, AND 53-10-4. (M)

Part: FLOOR BEAM — CRACKED (BS 840)

INSPECTION FOUND A .5 INCH CRACK IN LATERAL FLOOR BEAM WEB AT CABLE PASS THROUGH, BS 840, LBL 54. THE CRACK WAS STOP DRILLED. A WEB REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-2. (M)

Part: STRINGER — CRACKED (WS 656.5)

INSPECTION FOUND A .5 INCH CRACK IN LEFT WING STRINGER FLANGE AT WS 656.5. THE CRACK WAS STOP DRILLED. REPAIR CHANNELS WERE FABRICATED AND INSTALLED IAW SRM 57-10-4, 51-10-2, AND 51-20-4. (M)

Part: STRINGER — CRACKED (WS 629)

INSPECTION FOUND A 2 INCH IN THE STRINGER FLANGE AT LT WS 629. THE CRACK WAS STOP DRILLED. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 57-10-4, 51-10-2, AND 51-20-4. (M)

Part: DOOR FRAME — CRACKED (AFT ENTRY)

INSPECTION FOUND A 6 INCH CRACK IN AFT ENTRY DOOR FRAME ON LEFT SIDE BETWEEN THIRD AND FOURTH DOOR STOP FROM BOTTOM. THE CRACK WAS STOP DRILLED. A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-40-2. (M)

Part: SKIN — CORRODED (BS 430)

INSPECTION FOUND CORROSION ON LOWER FUSELAGE BELLY SKIN AT STATION 430, RBL 15. THE CORRODED SECTION WAS REMOVED. A FILLER AND DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-2 AND 53-30-3. (M)

Part: SKIN — CRACKED (VERTICAL)

INSPECTION FOUND A .75 INCH CRACK IN VERTICAL STABILIZER, 24 INCHES FROM LEADING EDGE. THE CRACK WAS ROUTED OUT. A FILLER AND DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 55-30-6. (M)

Part: FRAME — CORRODED (BS 720)

INSPECTION FOUND FRAMES CORRODED AT NUT PLATES FOR LOWER FUSELAGE PANEL IN AIRCRAFT BAY AT STA 720 C/D, LBL 10 TO RBL 10. THE CORROSION WAS REMOVED. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-2. (M)

Part: KEEL BEAM — CRACKED (BS 740)

INSPECTION FOUND A 1 INCH CRACK IN KEEL BEAM, AT BS 740 AND STRINGER 28R, IN AIRCRAFT BAY. THE CRACK WAS TRIMMED OUT. A FILLER AND DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW ECRA 5310-03180. (M)

Part: SKIN — CORRODED (BS 1342.4)

INSPECTION FOUND THE CENTER ENGINE SUPPORT STRUCTURE SKIN CORRODED AT STATION 1342.4, LEFT SIDE. THE CORRODED SECTION OF SKIN WAS REMOVED. A NEW SECTION OF SKIN AND ANGLES WERE FABRICATED AND INSTALLED IAW SRM 54-30-3 AND ECRA 5330-02330. (M)

Part: EEL WIRING — BROKEN (CABIN)

IAH - FLT NR 0650 - INSPECTION FOUND SEVERAL SECTION OF CABIN EMERGENCY AISLE LIGHTING INOPERATIVE. MAINTENANCE REPAIRED BROKEN AISLE LIGHTING WIRING AND OPERATION OF THE EMERGENCY AISLE LIGHTS WAS RESTORED. (M)

Part: SUPPORT — CORRODED (BS 320)

DEN - INSPECTION FOUND CABIN FLOOR SUPPORT CORRODED AT STA 320, RBBL 12. THE CORRODED SECTION OF FLOOR SUPPORT WAS REMOVED AND A NEW SECTION WAS INSTALLED PER SRM 53-10-8. (X)

Part: SUPPORT — CORRODED (BS 312)

DEN - INSPECTION FOUND CABIN FLOOR SUPPORT CORRODED AT STA 312, RBBL 48.75. THE CORRODED SECTION OF FLOOR SUPPORT WAS REMOVED AND A NEW SECTION WAS INSTALLED PER SRM 53-10-8. (X)

Part: SUPPORT — CORRODED (BS 344)

DEN - INSPECTION FOUND CABIN FLOOR SUPPORT CORRODED AT STA 344, BBL ZERO TO RBBL 48.75. THE CORRODED SECTION OF FLOOR SUPPORT WAS REMOVED AND A NEW SECTION WAS INSTALLED PER SRM 53-10-8. (X)